{"meta":{"query_hash":"d02254ce52e2","filters":{"topic":"Aerodynamics and Acoustics in Jet Flows"},"cohort_total":771,"direct_labels_cover":0,"predictions_cover":771,"exported":771,"export_cap":100000,"truncated":false,"label_status":"direct model label, unvalidated","prediction_status":"machine_predicted_unvalidated (Codex and Gemma teacher distillation)","score_status":"score_only:v0-immature-baseline","snapshot":{"source":"OpenAlex, pinned release, all 482 partitions","release":"2026-06-24","frame_built":"2026-07-12"},"permalink":"https://metacan.xera.ac/q/d02254ce52e2","api":"https://metacan.xera.ac/api/v1/cohort?topic=Aerodynamics+and+Acoustics+in+Jet+Flows"},"results":[{"id":"W12433993","doi":"10.1093/nar/gkf626","title":"Virtual methodology for predicting whistling noise over the front grill of a vehicle","year":2014,"lang":"en","type":"article","venue":"Nucleic Acids Research","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Windsor","funders":"National Institute of General Medical Sciences","keywords":"Noise (video); Compressibility; Acoustics; Flow (mathematics); Front (military); Compressible flow; Vortex; Simulation; Incompressible flow; Aerodynamics; Computer science; Mechanics; Geometry; Physics; Mathematics; Computer vision; Meteorology; Image (mathematics)","score_opus":0.05811005866274409,"score_gpt":0.33517015429475605,"score_spread":0.27706009563201195,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W12433993","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.78985435,0.00010663759,0.20610553,0.00009143546,0.0003869693,0.00029627,0.000027299493,0.00007851586,0.003053027],"genre_scores_gemma":[0.9865599,0.00003618552,0.0126545075,0.000025194837,0.00039917693,0.000047961654,0.0000047603735,0.00005743615,0.00021486846],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9984243,0.00021725253,0.0002796626,0.00020446781,0.00038533844,0.0004889929],"domain_scores_gemma":[0.99717045,0.002120096,0.00003263943,0.0004069014,0.00019742035,0.00007246874],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0036920204,0.00011544893,0.00022248946,0.0001034351,0.00021435591,0.00003303335,0.00045250912,0.00013691265,0.00006525688],"category_scores_gemma":[0.0014692632,0.00008920915,0.00008173865,0.00016191848,0.00018934358,0.00005685191,0.00016343001,0.0005070777,0.000015641524],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00027695336,0.00014151991,0.009081544,0.0006795028,0.00035121123,0.0000048298784,0.0066636633,0.31289354,0.46821612,0.04457663,0.0126777375,0.14443675],"study_design_scores_gemma":[0.00037548595,0.00016601733,0.0030935488,0.00003083847,0.0000123070795,0.0000012974356,0.00034269903,0.9859361,0.0013890547,0.0023975524,0.0061548487,0.00010021711],"about_ca_topic_score_codex":0.000039349918,"about_ca_topic_score_gemma":0.000027450395,"teacher_disagreement_score":0.6730426,"about_ca_system_score_codex":0.00008021426,"about_ca_system_score_gemma":0.000024709509,"threshold_uncertainty_score":0.36378434},"labels":[],"label_agreement":null},{"id":"W1485317015","doi":"10.1115/imece2014-39160","title":"Aeroacoustics of a Low-Speed Free Tip Fan With a Complex Clearance Geometry","year":2014,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Fonds de recherche du Québec – Nature et technologies; Compute Canada; Robert Bosch; Université de Sherbrooke","keywords":"Tip clearance; Turbomachinery; Aerodynamics; Aeroacoustics; Acoustics; Lattice Boltzmann methods; Leakage (economics); Mechanical fan; Axial compressor; Computational fluid dynamics; Noise (video); Mechanics; Physics; Engineering; Vortex; Aerospace engineering; Mechanical engineering; Computer science; Sound pressure","score_opus":0.006525140047746267,"score_gpt":0.18365220264155577,"score_spread":0.1771270625938095,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1485317015","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.40440825,0.00001994556,0.5703621,0.000028578761,0.00016593498,0.00009522049,0.00003066156,0.00020061785,0.02468867],"genre_scores_gemma":[0.9695336,0.000017502796,0.029997323,0.00007330886,0.00008380468,0.0000011388884,0.000010036851,0.000047371483,0.000235906],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991888,0.000008221686,0.0002126446,0.00014329834,0.0002043262,0.00024270576],"domain_scores_gemma":[0.99928063,0.00006807278,0.00003565515,0.00047065076,0.00007304923,0.000071967705],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000107394444,0.00015754387,0.00024548513,0.00007164696,0.00003242922,0.000019048599,0.0002869302,0.00009817486,0.000115167],"category_scores_gemma":[0.000046180976,0.0001329163,0.00003796208,0.0002242771,0.00007616406,0.000036545734,0.00005196423,0.00020216979,0.000019565357],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000428207,0.00007822926,0.00048884004,0.00058115064,0.00012286447,0.0000067709093,0.00012258282,0.90166104,0.06944985,0.01166808,0.010378447,0.0053993254],"study_design_scores_gemma":[0.00048334326,0.00006444951,0.0048889783,0.00004510675,0.00001915755,0.0000042566244,0.00003713037,0.9928332,0.00047103528,0.00035321742,0.0005958555,0.00020428452],"about_ca_topic_score_codex":0.000017415217,"about_ca_topic_score_gemma":0.000055459615,"teacher_disagreement_score":0.56512535,"about_ca_system_score_codex":0.000021899068,"about_ca_system_score_gemma":0.000007061109,"threshold_uncertainty_score":0.542017},"labels":[],"label_agreement":null},{"id":"W1490670299","doi":"","title":"An accurate coupled structural-acoustic analytical framework for the prediction of random and flow-induced noise in transport vehicles: Its Uddation","year":2009,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"University of Victoria","funders":"","keywords":"Spectral density; Boundary layer; Acoustics; Noise (video); Turbulence; Noise control; Sound pressure; Mechanics; Physics; Engineering; Computer science; Noise reduction","score_opus":0.01395165108936791,"score_gpt":0.24151412173334064,"score_spread":0.22756247064397273,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1490670299","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.5946078,0.00008602056,0.40420058,0.00006775306,0.00026630855,0.00038831175,0.00033086605,0.000035213256,0.00001716023],"genre_scores_gemma":[0.9960945,0.00016913368,0.0033310677,0.000088573826,0.00016634323,0.000015157403,0.00009852837,0.000031231582,0.0000054398265],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989359,0.000012720526,0.00037570606,0.00019236187,0.0001369076,0.00034642057],"domain_scores_gemma":[0.9991291,0.00023662552,0.000044527413,0.00023819608,0.000110459834,0.00024106455],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00019561671,0.00018678246,0.00025388825,0.00014479776,0.00010888439,0.00003624316,0.00017114951,0.00022195844,0.000014377846],"category_scores_gemma":[0.00015914052,0.00016713391,0.000042798627,0.00023904916,0.0000429545,0.0001164658,0.000002934245,0.00028326968,5.2845655e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000037094596,0.000007930366,0.00021282294,0.00006649529,0.000025037602,0.000007370011,0.00027870326,0.96684587,0.027356055,0.00056176406,0.000035753226,0.0045651095],"study_design_scores_gemma":[0.0006815144,0.000078130695,0.060464893,0.000048859598,0.00013346705,0.0000033175268,0.00013420173,0.93718463,0.000054785036,0.0010581898,0.000007865733,0.00015014055],"about_ca_topic_score_codex":0.00030625175,"about_ca_topic_score_gemma":0.0017463843,"teacher_disagreement_score":0.40148675,"about_ca_system_score_codex":0.0001487472,"about_ca_system_score_gemma":0.0001267476,"threshold_uncertainty_score":0.6815523},"labels":[],"label_agreement":null},{"id":"W1503598358","doi":"10.1061/(asce)hy.1943-7900.0001044","title":"Density Effects on Dilution and Height of Vertical Fountains","year":2015,"lang":"en","type":"article","venue":"Journal of Hydraulic Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Western University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Froude number; Dilution; Buoyancy; Mechanics; Meteorology; Maximum density; Turbulence; Atmospheric sciences; Density of air; Relative density; Environmental science; Hydrology (agriculture); Flow (mathematics); Mathematics; Geology; Chemistry; Geotechnical engineering; Physics; Thermodynamics","score_opus":0.006161661758817992,"score_gpt":0.192433168925874,"score_spread":0.186271507167056,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1503598358","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.92306596,0.00037137637,0.07558053,0.000034100012,0.000629111,0.00003624682,6.415089e-7,0.000025741094,0.0002562785],"genre_scores_gemma":[0.9975747,0.00006369459,0.00210861,0.0000140700795,0.00021540836,5.1364924e-7,3.8588948e-7,0.000019882424,0.0000027742467],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99936384,0.000007855799,0.00024556983,0.000052677904,0.00019547566,0.00013458295],"domain_scores_gemma":[0.9995876,0.00009574415,0.00003087825,0.00008519191,0.00006246955,0.0001381435],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020801945,0.000106783424,0.00021735461,0.00010118662,0.000010961712,0.000010940284,0.000072265524,0.000059744663,9.07425e-7],"category_scores_gemma":[0.00016127682,0.0000948651,0.00004761123,0.00007676459,0.000012661481,0.00008069039,0.000019082636,0.00022873635,0.0000014576793],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000022523218,0.000025798161,0.0004772495,0.0001882804,0.000082532584,0.000077648074,0.00017161781,0.9598121,0.03553969,0.0012608555,0.00029890588,0.0020428097],"study_design_scores_gemma":[0.0006905393,0.00030066824,0.0075963205,0.00023497744,0.00005476846,0.00013984439,0.000018119938,0.9706442,0.019303925,0.00028200157,0.0005700639,0.00016460619],"about_ca_topic_score_codex":0.0000011930717,"about_ca_topic_score_gemma":7.6571234e-7,"teacher_disagreement_score":0.07450868,"about_ca_system_score_codex":0.00008368496,"about_ca_system_score_gemma":0.000012002264,"threshold_uncertainty_score":0.38684866},"labels":[],"label_agreement":null},{"id":"W1507490827","doi":"","title":"Screech suppression of supersonic jet noise","year":2009,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":true,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Supersonic speed; Jet (fluid); Noise (video); Jet noise; Nozzle; Tone (literature); Acoustics; Chevron (anatomy); Aeroacoustics; Physics; Engineering; Aerospace engineering; Geology; Mechanics; Sound pressure; Computer science","score_opus":0.00583224596962921,"score_gpt":0.1914866271959325,"score_spread":0.1856543812263033,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1507490827","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9433733,0.00048307865,0.029774494,0.00017350257,0.0011246433,0.00021042718,0.0004932016,0.00017615035,0.024191204],"genre_scores_gemma":[0.9960909,0.00011990051,0.0033029187,0.00014798625,0.000121219215,0.0000013606198,0.000034639233,0.000029298639,0.00015178886],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991663,0.0000061535043,0.00019348357,0.00012217781,0.00012879036,0.0003830939],"domain_scores_gemma":[0.99926984,0.000026524343,0.000018126824,0.00028993652,0.000062054816,0.00033351628],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0000699643,0.00015105694,0.00017531187,0.00014718382,0.00005613738,0.000019896483,0.00021938475,0.00014075573,0.00011246619],"category_scores_gemma":[0.000052105708,0.00015779391,0.00004871626,0.00017070596,0.000035927776,0.000047231333,0.0000084248195,0.00019596303,0.000020385127],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000064923024,0.000035328638,0.0007753429,0.00014228621,0.000046688412,0.00013720183,0.00030493503,0.44884452,0.45819274,0.0031426412,0.071303,0.017068833],"study_design_scores_gemma":[0.0002916618,0.000074956144,0.017963681,0.00008832443,0.000060369122,0.00001332215,0.00012958712,0.9763437,0.0013382473,0.00085840473,0.0024233547,0.00041439765],"about_ca_topic_score_codex":0.0008940623,"about_ca_topic_score_gemma":0.0016776957,"teacher_disagreement_score":0.52749914,"about_ca_system_score_codex":0.0001682874,"about_ca_system_score_gemma":0.00012426107,"threshold_uncertainty_score":0.6434649},"labels":[],"label_agreement":null},{"id":"W1513573834","doi":"","title":"Effect of next generation computer cooling fan speed on acoustic noise emissions","year":2005,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"University of Windsor","funders":"","keywords":"Mechanical fan; Acoustics; Sound pressure; Sound power; Anechoic chamber; Engineering; Voltage; Noise (video); Electrical engineering; Computer science; Sound (geography); Physics","score_opus":0.012143921998286573,"score_gpt":0.2188681736638827,"score_spread":0.20672425166559613,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1513573834","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8675956,0.00013659766,0.12827486,0.00004753025,0.001803876,0.00026090888,0.00017574803,0.00012411652,0.0015807465],"genre_scores_gemma":[0.9944213,0.00006332924,0.0033335688,0.00018713738,0.0017151508,0.000003715749,0.000078357465,0.000068389905,0.00012906209],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9988882,0.000025753892,0.00029744572,0.00019263552,0.00017312974,0.00042285532],"domain_scores_gemma":[0.9989452,0.00018542235,0.000040606003,0.00031990002,0.00007131798,0.0004375967],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00016909394,0.00024340396,0.00025963178,0.00020451202,0.00012438605,0.000054593642,0.00019547922,0.00017512549,0.00008867795],"category_scores_gemma":[0.00011238905,0.000246157,0.0000682433,0.00017046464,0.000042949534,0.00006489679,0.000017049546,0.000289628,0.0000611763],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000038526923,0.000007101801,0.000019807727,0.00006388301,0.000020111358,0.000014584676,0.00005088629,0.8221259,0.15443817,0.000052338928,0.008938894,0.014264484],"study_design_scores_gemma":[0.00025417248,0.00012034089,0.00022051818,0.00006247858,0.00007511056,0.0000065041836,0.000008253953,0.99593556,0.0023246428,0.0000038715743,0.00074622384,0.0002423075],"about_ca_topic_score_codex":0.00033115264,"about_ca_topic_score_gemma":0.0016155203,"teacher_disagreement_score":0.17380969,"about_ca_system_score_codex":0.0003763939,"about_ca_system_score_gemma":0.00010650984,"threshold_uncertainty_score":0.99999905},"labels":[],"label_agreement":null},{"id":"W1523962742","doi":"","title":"Hybrid methodology for the identification of incoherent noise sources","year":2000,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"Office of Naval Research; National Aeronautics and Space Administration","keywords":"Tikhonov regularization; Microphone; Acoustics; Singular value decomposition; Noise (video); Mathematics; Frequency domain; Mathematical analysis; Singular value; Physics; Algorithm; Computer science; Inverse problem; Eigenvalues and eigenvectors","score_opus":0.020015170535611734,"score_gpt":0.2364913249673525,"score_spread":0.21647615443174079,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1523962742","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.49520814,0.0005147591,0.50130117,0.0001429772,0.0009109329,0.0003700171,0.00061604625,0.000053388438,0.0008825866],"genre_scores_gemma":[0.9946201,0.00019859232,0.0043149316,0.00008023968,0.00015590605,0.000028961591,0.00002726979,0.000030047426,0.0005439464],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99932784,0.000014899529,0.0002655316,0.000097014876,0.00006572005,0.00022902437],"domain_scores_gemma":[0.9992616,0.0002874141,0.00003293661,0.00025336258,0.000060421928,0.0001042555],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00028230617,0.00009415845,0.00012306764,0.00005933766,0.0000943405,0.000021048454,0.00023182,0.000056335968,0.00014997512],"category_scores_gemma":[0.00010990035,0.00008238859,0.00004686564,0.0000679989,0.00006758883,0.000020005718,0.0000054898005,0.00009697859,0.000013535681],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000003166141,0.000004614047,0.000028974595,0.000060110517,0.00004533236,0.0000019979536,0.00013357836,0.9221775,0.02650263,0.00070050784,0.0058905706,0.044450995],"study_design_scores_gemma":[0.00010582607,0.000013225758,0.0018359673,0.0000073359047,0.00008586711,0.0000047926587,0.00007839283,0.9855487,0.0009755704,0.0016151688,0.009605396,0.00012376973],"about_ca_topic_score_codex":0.0013316883,"about_ca_topic_score_gemma":0.0022308154,"teacher_disagreement_score":0.49941194,"about_ca_system_score_codex":0.00008966557,"about_ca_system_score_gemma":0.00006990276,"threshold_uncertainty_score":0.33597094},"labels":[],"label_agreement":null},{"id":"W1538932135","doi":"","title":"Turbulent boundary layer induced noise and vibration of a multi-panel walled acoustic enclosure","year":2010,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"University of Victoria","funders":"","keywords":"Enclosure; Acoustics; Fuselage; Sound pressure; Noise (video); Vibration; Structural acoustics; Soundproofing; Boundary layer; Noise control; Turbulence; Engineering; Structural engineering; Mechanics; Physics; Noise reduction; Computer science; Aerospace engineering; Telecommunications","score_opus":0.014947530283596269,"score_gpt":0.21058397182028932,"score_spread":0.19563644153669305,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1538932135","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9754839,0.00011283101,0.02233088,0.00008207695,0.0010682524,0.00024593447,0.000160919,0.00008399069,0.0004312429],"genre_scores_gemma":[0.99338484,0.000070041766,0.0060310275,0.00013070129,0.00017506887,0.000011460234,0.000038507238,0.00006494754,0.00009343353],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989331,0.00001053117,0.0003010311,0.00020505289,0.00015595804,0.00039437864],"domain_scores_gemma":[0.998995,0.000060185263,0.00004849803,0.00032670915,0.00012802352,0.00044159155],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00013122307,0.00022850098,0.00023783158,0.00014872855,0.00012035763,0.00006591199,0.00018532245,0.00029799427,0.00007233027],"category_scores_gemma":[0.00014602418,0.00024787636,0.00004189555,0.00015222415,0.000092195296,0.000082780876,0.000025614234,0.0005263372,0.0000103512775],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":true,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000033023134,0.000020385784,0.0002756247,0.00014163976,0.000041794978,0.000048546288,0.00035316392,0.062315516,0.93422467,0.00017305935,0.0008129368,0.0015893687],"study_design_scores_gemma":[0.00043286325,0.000033588727,0.017049648,0.000030068059,0.00008523084,0.000031920463,0.000108309054,0.9806055,0.0007643171,0.00014659003,0.00037317097,0.0003388026],"about_ca_topic_score_codex":0.0015060974,"about_ca_topic_score_gemma":0.023166865,"teacher_disagreement_score":0.93346035,"about_ca_system_score_codex":0.00010659739,"about_ca_system_score_gemma":0.00028938917,"threshold_uncertainty_score":0.9999974},"labels":[],"label_agreement":null},{"id":"W1542164111","doi":"","title":"Noise generated by impingement of a planar jet on a flat plate","year":2007,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"","keywords":"Plenum space; Jet (fluid); Acoustics; Nozzle; Piping; Planar; Mechanics; Noise (video); Aeroacoustics; Baffle; Amplitude; Sound pressure; Physics; Optics; Materials science","score_opus":0.006635260451410217,"score_gpt":0.19516288713501984,"score_spread":0.18852762668360962,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1542164111","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.89042383,0.00022801557,0.098666266,0.000047425274,0.0010901152,0.0002227374,0.0011321054,0.00011200666,0.008077481],"genre_scores_gemma":[0.9966815,0.00008600013,0.0024471106,0.0002710646,0.00013182261,0.0000029445075,0.00011693726,0.000057007073,0.00020561229],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9988913,0.000004854433,0.00028462175,0.00015252254,0.00015730596,0.0005093816],"domain_scores_gemma":[0.99919593,0.00004735823,0.000034980872,0.00025168885,0.00005965512,0.00041040752],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016790007,0.00019252069,0.00018636242,0.00018902078,0.00006161977,0.000020343932,0.00017627707,0.00014342257,0.000056260822],"category_scores_gemma":[0.000034460303,0.00020661937,0.00003795949,0.00019144172,0.000036689773,0.000021850954,0.000008451702,0.00020676096,0.000028633587],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000019844796,0.000026284679,0.0003511715,0.00014488588,0.00015797128,0.0002693631,0.00023864068,0.34849262,0.47016278,0.0014116898,0.17330846,0.005416299],"study_design_scores_gemma":[0.0006575597,0.00014565045,0.0028493144,0.000100202604,0.00009512379,0.000010963887,0.00013802072,0.9725201,0.0067704264,0.00022320884,0.015763173,0.00072626537],"about_ca_topic_score_codex":0.0019317104,"about_ca_topic_score_gemma":0.008268973,"teacher_disagreement_score":0.6240275,"about_ca_system_score_codex":0.00037276873,"about_ca_system_score_gemma":0.0000866783,"threshold_uncertainty_score":0.84256935},"labels":[],"label_agreement":null},{"id":"W1560309987","doi":"","title":"The Development of the Acoustic Design of NASA Glenn Research Center's New Reverberant Acoustic Test Facility","year":2013,"lang":"en","type":"book","venue":"NASA STI Repository (National Aeronautics and Space Administration)","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"National Aeronautics and Space Administration","keywords":"Engineering; Test (biology); Sound pressure; Acoustics; Research center; Noise (video); Aeronautics; Computer science; Telecommunications; Physics; Artificial intelligence; Geology","score_opus":0.031640331092814444,"score_gpt":0.26150173467381843,"score_spread":0.229861403581004,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1560309987","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.06909832,0.009998769,0.62329376,0.0029377104,0.0126861865,0.015032119,0.004256328,0.00061213545,0.2620847],"genre_scores_gemma":[0.8537557,0.00027835247,0.0057950607,0.0000122398815,0.0002731909,0.000058198006,0.000119466626,0.000058128528,0.13964967],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9965138,0.00010305765,0.0010537622,0.0003822528,0.0015746402,0.00037250714],"domain_scores_gemma":[0.99603003,0.0018751106,0.00035449833,0.0004996038,0.0010804603,0.00016029713],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00096502545,0.0003917514,0.00039837116,0.00009282663,0.00070520496,0.00014742724,0.0005634373,0.00036672762,0.000020290594],"category_scores_gemma":[0.0005268086,0.00028711822,0.00010805883,0.0001600262,0.00049326714,0.000085965854,0.0001735188,0.00080584816,0.000008270524],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00039781613,0.0014498181,0.0022922799,0.0060280147,0.0026684871,0.000049377708,0.0030647148,0.58435297,0.1113309,0.040427458,0.23678991,0.011148288],"study_design_scores_gemma":[0.0038241788,0.0018313703,0.04989335,0.0041668103,0.0010112046,0.0003550025,0.00076175516,0.7250312,0.012443844,0.033950966,0.1625184,0.0042119245],"about_ca_topic_score_codex":0.000005860017,"about_ca_topic_score_gemma":0.00012428194,"teacher_disagreement_score":0.78465736,"about_ca_system_score_codex":0.00056593213,"about_ca_system_score_gemma":0.0036520464,"threshold_uncertainty_score":0.9999581},"labels":[],"label_agreement":null},{"id":"W1562003470","doi":"","title":"A Nonlinear Geometrical Acoustic Model for Sonic Boom Propagation","year":2010,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Sonic boom; Acoustics; Nonlinear system; Nonlinear acoustics; Boom; Geology; Physics; Mechanics","score_opus":0.009623261633363824,"score_gpt":0.21225943773903963,"score_spread":0.2026361761056758,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1562003470","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.16665472,0.000038337817,0.8297399,0.00007649372,0.0013906118,0.00041827737,0.0006982875,0.00018403813,0.00079930405],"genre_scores_gemma":[0.94476986,0.00002657073,0.0537137,0.00016407765,0.00053800136,0.000053744247,0.00011828208,0.00010219047,0.0005135447],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9986773,0.0000033835906,0.00026681824,0.0002331918,0.00016239364,0.0006568739],"domain_scores_gemma":[0.9988068,0.00009815096,0.000030315932,0.00034195947,0.00017371206,0.0005490702],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0001648912,0.00022354504,0.00019787946,0.000321014,0.0001697656,0.000085640306,0.00027421716,0.0002896129,0.000039676597],"category_scores_gemma":[0.0003993399,0.00024743436,0.000074603326,0.000308256,0.00006049721,0.00007301527,0.000017439957,0.000512017,0.000035373218],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000022384838,0.0000138180485,0.000021314647,0.00008626841,0.000020111498,0.000009124145,0.000047344463,0.93043786,0.05988112,0.0007632326,0.0059437267,0.002773867],"study_design_scores_gemma":[0.00022569954,0.00002394269,0.00013945889,0.000008637623,0.000066851615,0.000009099295,0.000016005379,0.99708384,0.00006190352,0.0008206775,0.0012297004,0.00031418394],"about_ca_topic_score_codex":0.00027569133,"about_ca_topic_score_gemma":0.012702596,"teacher_disagreement_score":0.77811515,"about_ca_system_score_codex":0.0002655965,"about_ca_system_score_gemma":0.00044901296,"threshold_uncertainty_score":0.9999978},"labels":[],"label_agreement":null},{"id":"W1567484162","doi":"10.1115/imece2014-38602","title":"A Comparison of Classic and Snapshot Proper Orthogonal Decomposition on the Three Dimensional Wall Jet Flow Field","year":2014,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of New Brunswick","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Cartesian coordinate system; Proper orthogonal decomposition; Nozzle; Turbulence; Reynolds number; Mechanics; Snapshot (computer storage); Transverse plane; Jet (fluid); Eigenfunction; Physics; Mathematics; Geometry; Computational physics; Computer science; Engineering","score_opus":0.015259449996925703,"score_gpt":0.2491425930087868,"score_spread":0.23388314301186108,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1567484162","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9593384,0.000028114775,0.031119471,0.00052719255,0.0001655563,0.000113674614,0.0000047414946,0.000035782985,0.008667051],"genre_scores_gemma":[0.99661523,0.0000030198653,0.0030180416,0.00025883614,0.00004872036,0.0000067850383,0.000016642654,0.000011512174,0.000021185477],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99948174,0.000013469597,0.00015825013,0.000100406935,0.00013558634,0.00011056397],"domain_scores_gemma":[0.99954873,0.00023236143,0.000019769055,0.00014073173,0.00002644273,0.000031961754],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00011752743,0.0001007945,0.0001347848,0.0000223631,0.00005449356,0.000015994157,0.00007640052,0.00005687022,0.00023582211],"category_scores_gemma":[0.000018857721,0.000060215843,0.00003092652,0.000036333913,0.00002995824,0.000023890218,0.000029327188,0.00015509031,0.0000068445593],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00020568517,0.00030774085,0.028685804,0.00019219225,0.00018546589,0.0000026375126,0.00027363628,0.76722044,0.034028012,0.10795506,0.03802385,0.022919476],"study_design_scores_gemma":[0.000118335665,0.00016757814,0.004531614,0.000028977016,0.000011217628,0.0000012656753,0.0000054923803,0.9921907,0.0013269914,0.001079287,0.00045056676,0.00008792697],"about_ca_topic_score_codex":0.0000056190393,"about_ca_topic_score_gemma":0.00012082053,"teacher_disagreement_score":0.22497031,"about_ca_system_score_codex":0.000009800961,"about_ca_system_score_gemma":0.000004477605,"threshold_uncertainty_score":0.25820866},"labels":[],"label_agreement":null},{"id":"W1579996574","doi":"10.3390/coatings5020186","title":"Effects of Bell Speed and Flow Rate on Evaporation of Water Spray from a Rotary Bell Atomizer","year":2015,"lang":"en","type":"article","venue":"Coatings","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Chrysler (Canada); University of Windsor","funders":"University of Windsor","keywords":"Anemometer; Evaporation; Volumetric flow rate; Mechanics; Materials science; Thermodynamics; Analytical Chemistry (journal); Physics; Chemistry; Chromatography; Turbulence","score_opus":0.006616491805093626,"score_gpt":0.18703129962661347,"score_spread":0.18041480782151983,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1579996574","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9954137,0.00009963288,0.0035018532,0.0000174525,0.00023982348,0.00016695047,0.000018101493,0.00003407845,0.0005084006],"genre_scores_gemma":[0.9974278,0.000013487753,0.002342199,0.000025723048,0.0000683465,0.0000028236068,0.00003865687,0.000023934741,0.00005703246],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99944335,0.000021877155,0.00019973042,0.00011288455,0.0001113877,0.00011077974],"domain_scores_gemma":[0.99960333,0.00011618714,0.00004448759,0.00012385816,0.000060797367,0.000051316165],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018539594,0.0001090024,0.00019781665,0.000035774567,0.000015542479,0.000009100721,0.00006115089,0.000065451626,0.000009738186],"category_scores_gemma":[0.00007163727,0.00008802326,0.00002544389,0.000040209987,0.00002946006,0.00005215365,0.00003694618,0.00008956243,0.0000115524135],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00004854426,0.000027422102,0.00032637847,0.00018839052,0.000029019235,0.0000053634785,0.0015869007,0.054384083,0.94154227,0.0000446824,0.0007405924,0.0010763729],"study_design_scores_gemma":[0.00105554,0.000089074325,0.00057061604,0.00010237581,0.000040758136,3.6982087e-7,0.00003084642,0.47463778,0.52217144,0.0010493895,0.00012407586,0.00012770211],"about_ca_topic_score_codex":0.000044640183,"about_ca_topic_score_gemma":0.000007357804,"teacher_disagreement_score":0.4202537,"about_ca_system_score_codex":0.000019039493,"about_ca_system_score_gemma":0.0000070160936,"threshold_uncertainty_score":0.35894844},"labels":[],"label_agreement":null},{"id":"W1587498870","doi":"10.1115/gt2015-43737","title":"Aeroacoustic Analysis of a Low-Subsonic Axial Fan","year":2015,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":15,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Wake; Acoustics; Noise (video); Rotor (electric); Sound pressure; Aeroacoustics; Physics; Mechanics; Convergence (economics); Computer science","score_opus":0.011835795579195346,"score_gpt":0.21429057520604766,"score_spread":0.20245477962685232,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1587498870","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.71933293,0.000077959245,0.25922093,0.0000071073555,0.00032330997,0.000051813167,0.000022910546,0.00014809934,0.020814952],"genre_scores_gemma":[0.99723095,0.000015360445,0.0023730355,0.00001307433,0.00005052297,0.0000034053176,0.000017968341,0.000018608782,0.00027708616],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993243,0.0000068183544,0.0002115066,0.000107466505,0.00017564149,0.0001742367],"domain_scores_gemma":[0.9995349,0.00003068403,0.000021696325,0.00024300446,0.000068173606,0.00010154703],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012852487,0.00010397522,0.00024190306,0.00017948876,0.000012108529,0.000013192879,0.00014086501,0.00006182449,0.00013325652],"category_scores_gemma":[0.000036972062,0.000095827854,0.00010174797,0.00061837013,0.000026538451,0.000036556667,0.000028474788,0.000084050436,0.00002196176],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000003070396,0.000022274424,0.0006451246,0.000024430781,0.0004716202,0.0000036008473,0.0001243512,0.9933053,0.0026530467,0.0012134836,0.000858559,0.00067512254],"study_design_scores_gemma":[0.00015461819,0.000016996073,0.0012016698,0.000004738526,0.00040174896,5.745869e-7,0.00009750804,0.9975496,0.00020563432,0.00017658927,0.00007033435,0.000120019424],"about_ca_topic_score_codex":0.000024170502,"about_ca_topic_score_gemma":0.00012123208,"teacher_disagreement_score":0.277898,"about_ca_system_score_codex":0.000052567026,"about_ca_system_score_gemma":0.000020303365,"threshold_uncertainty_score":0.39077467},"labels":[],"label_agreement":null},{"id":"W1595860808","doi":"","title":"Jet noise prediction: Past, present and future","year":2007,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":6,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"McGill University; Florida State University","keywords":"Jet noise; Reynolds-averaged Navier–Stokes equations; Takeoff; Anechoic chamber; Jet (fluid); Extrapolation; Noise (video); Turbulence; Acoustics; Mechanics; Aeroacoustics; Reynolds number; Physics; Computer science; Aerospace engineering; Engineering; Mathematics; Mathematical analysis; Sound pressure","score_opus":0.004274137397082604,"score_gpt":0.1813085546624489,"score_spread":0.1770344172653663,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1595860808","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6482257,0.003096061,0.24708687,0.0021664456,0.012647126,0.00079776923,0.0018501654,0.0008613642,0.08326845],"genre_scores_gemma":[0.9903867,0.00027449426,0.0024635606,0.00016805573,0.0063371975,0.0000036869708,0.00003911179,0.00004883712,0.0002783386],"study_design_codex":"not_applicable","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99914926,0.0000034455823,0.00016695351,0.00014146764,0.0001149693,0.00042392247],"domain_scores_gemma":[0.9991396,0.00003138807,0.000013017908,0.0002044491,0.000049805207,0.0005617599],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000121849844,0.00015154568,0.00011119602,0.000118970805,0.000104566825,0.00004369955,0.00010507851,0.00015388787,0.00005734109],"category_scores_gemma":[0.000006257316,0.00016009722,0.000022821256,0.0001317736,0.000045735098,0.00004485073,0.000015454438,0.00022548356,0.000013563717],"study_design_candidate":"not_applicable","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000013241779,0.000035839534,0.011408614,0.00040664227,0.00021035028,0.0008832747,0.0009388346,0.23337962,0.012772046,0.004080188,0.63040125,0.10547009],"study_design_scores_gemma":[0.00028339514,0.000033625412,0.09577886,0.00002116451,0.00006839687,0.00006323907,0.00037437692,0.53603464,0.000029486184,0.00030573522,0.36660513,0.00040195748],"about_ca_topic_score_codex":0.0004862907,"about_ca_topic_score_gemma":0.002608251,"teacher_disagreement_score":0.34216097,"about_ca_system_score_codex":0.00018689445,"about_ca_system_score_gemma":0.000053716536,"threshold_uncertainty_score":0.65285754},"labels":[],"label_agreement":null},{"id":"W1611856165","doi":"","title":"The effect of high frequency vortex generator on the acoustic resonance excitation in shallow rectangular cavities","year":2014,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"Ontario Tech University","funders":"","keywords":"Vortex shedding; Acoustics; Resonance (particle physics); Acoustic resonance; Excitation; Vortex; Enclosure; Mechanics; Materials science; Cylinder; Mach number; Wind tunnel; Large eddy simulation; Optics; Physics; Turbulence; Geometry; Engineering; Atomic physics; Telecommunications","score_opus":0.0032288682240553426,"score_gpt":0.17022170058098457,"score_spread":0.16699283235692922,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1611856165","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9898254,0.0005585694,0.0065230005,0.0001494958,0.0010854532,0.00029112183,0.000113707465,0.000041218485,0.0014119794],"genre_scores_gemma":[0.99898976,0.00015565513,0.00030450648,0.000118549004,0.0002076428,0.000043577023,0.00001361919,0.00005227711,0.00011438514],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99884003,0.00009747021,0.0002816283,0.00016247938,0.00020147988,0.00041689805],"domain_scores_gemma":[0.99834377,0.0009793435,0.00004681858,0.00044810647,0.00005835967,0.00012360256],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005678906,0.0002028226,0.00020600602,0.00010000711,0.00018831414,0.000051474482,0.0003461096,0.0001285083,0.000015149598],"category_scores_gemma":[0.0007710979,0.00013942245,0.00004507677,0.00023787367,0.00012066693,0.000031828822,0.000012130993,0.00032496234,0.000011196609],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":true,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000014647153,0.000007485298,0.0015870178,0.00017885727,0.000048868013,0.00004339817,0.0003401225,0.91328764,0.042967435,0.027453372,0.004183205,0.009887953],"study_design_scores_gemma":[0.00030348887,0.00017333227,0.031266112,0.00013651757,0.00005321608,0.000003364415,0.000108268796,0.9627151,0.00035420776,0.003963325,0.0005972207,0.00032587835],"about_ca_topic_score_codex":0.0036859352,"about_ca_topic_score_gemma":0.047564376,"teacher_disagreement_score":0.049427427,"about_ca_system_score_codex":0.0003285278,"about_ca_system_score_gemma":0.000086030814,"threshold_uncertainty_score":0.9698151},"labels":[],"label_agreement":null},{"id":"W1854011020","doi":"","title":"Uncommon noise signatures in a wind tunnel","year":2001,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Wind tunnel; Noise (video); Acoustics; Stator; Trailing edge; Noise control; Leading edge; Engineering; Structural engineering; Enhanced Data Rates for GSM Evolution; Aeroacoustics; Physics; Aerospace engineering; Sound pressure; Electrical engineering; Computer science; Noise reduction; Telecommunications","score_opus":0.0062149967028106755,"score_gpt":0.1873007513350476,"score_spread":0.18108575463223692,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1854011020","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.96385634,0.0005937787,0.004588252,0.00010630839,0.0011270697,0.00017180193,0.00012609467,0.00013621672,0.02929415],"genre_scores_gemma":[0.9980611,0.00023373833,0.0007261783,0.0002733311,0.00019918666,0.000003894081,0.000019603038,0.00005454618,0.00042838015],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99903065,0.000007760679,0.00018852323,0.00015011377,0.000107833526,0.0005151322],"domain_scores_gemma":[0.99930775,0.000043901935,0.000013137274,0.00024869395,0.00003229463,0.0003541964],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00008153722,0.00017423657,0.00015877585,0.00024641567,0.00005465806,0.00004314142,0.00022052955,0.00018264106,0.00013283196],"category_scores_gemma":[0.000052193118,0.00020059141,0.00003258071,0.00031695075,0.000034291414,0.000049964056,0.000014625194,0.00037831927,0.000039144285],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":true,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000017829716,0.000008039937,0.0017441182,0.000022054324,0.000010147096,0.0004333955,0.0000934524,0.9782405,0.0049835662,0.00028955718,0.012419017,0.0017543751],"study_design_scores_gemma":[0.0002587222,0.000014476161,0.04260007,0.00004165271,0.00001743325,0.000012040843,0.000112435046,0.9467012,0.0000064915866,0.00075476203,0.009109626,0.00037105198],"about_ca_topic_score_codex":0.0050251978,"about_ca_topic_score_gemma":0.09714215,"teacher_disagreement_score":0.09211695,"about_ca_system_score_codex":0.0004210685,"about_ca_system_score_gemma":0.00011925625,"threshold_uncertainty_score":0.9193326},"labels":[],"label_agreement":null},{"id":"W1872464068","doi":"10.2514/1.j051696","title":"Uncertainty Quantification for the Trailing-Edge Noise of a Controlled-Diffusion Airfoil","year":2011,"lang":"en","type":"article","venue":"AIAA Journal","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Airfoil; Reynolds-averaged Navier–Stokes equations; Trailing edge; Computation; Laminar flow; Robustness (evolution); Turbulence; Mechanics; Computational fluid dynamics; Boundary layer; Mathematics; Noise (video); Applied mathematics; Physics; Computer science; Algorithm","score_opus":0.026530279376246357,"score_gpt":0.2302676298957516,"score_spread":0.20373735051950526,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1872464068","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.4209287,0.0007679393,0.57456774,0.00012520944,0.0015137519,0.00035258313,0.0000237667,0.00004285201,0.0016774881],"genre_scores_gemma":[0.9972268,0.00037638747,0.0020557842,0.000020004783,0.00019679994,0.00001576995,0.0000024321666,0.000020018259,0.00008605299],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993151,0.000014888805,0.00033211283,0.00006758993,0.00011499258,0.00015532441],"domain_scores_gemma":[0.9993836,0.0001789091,0.00010434917,0.00015571127,0.00013107106,0.00004635848],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00049178215,0.00009343437,0.00017493386,0.00004349212,0.00013445431,0.000020769361,0.0001994371,0.00005542184,0.00006171248],"category_scores_gemma":[0.000097444674,0.00006026049,0.00014206687,0.000059162165,0.000039675986,0.000046609286,0.000010464349,0.0001864873,0.0000034248073],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0011009092,0.0003559456,0.0006664882,0.00022577778,0.00066553074,0.00001032047,0.0054098293,0.65860283,0.19639826,0.022770634,0.006011676,0.1077818],"study_design_scores_gemma":[0.0016945654,0.00006541413,0.0011225983,0.000033212687,0.00008897888,0.000018758672,0.00022831924,0.9926392,0.0007063553,0.0021005636,0.0012064256,0.00009563755],"about_ca_topic_score_codex":0.000007494085,"about_ca_topic_score_gemma":0.000016470676,"teacher_disagreement_score":0.57629806,"about_ca_system_score_codex":0.000020693118,"about_ca_system_score_gemma":0.000022972294,"threshold_uncertainty_score":0.24573514},"labels":[],"label_agreement":null},{"id":"W1884846484","doi":"","title":"Wind tunnel resonances and Helmholtz resonators","year":2007,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Helmholtz resonator; Wind tunnel; Resonator; Helmholtz free energy; Wind speed; Acoustics; Nozzle; Parametric statistics; Jet (fluid); Coupling (piping); Supersonic wind tunnel; Physics; Sound pressure; Mechanics; Aerospace engineering; Engineering; Meteorology; Optics; Mechanical engineering","score_opus":0.005730119646466995,"score_gpt":0.19066544147168754,"score_spread":0.18493532182522054,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1884846484","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9644815,0.001829533,0.015483547,0.00007464075,0.0012290394,0.00013202315,0.000165045,0.00014903807,0.016455663],"genre_scores_gemma":[0.9947367,0.00028849705,0.00401334,0.00022700206,0.00026792538,0.000001033649,0.000011273907,0.000049531736,0.00040474537],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989771,0.00000411074,0.00018945556,0.00016701968,0.00012399569,0.00053832063],"domain_scores_gemma":[0.9991364,0.00007192388,0.000016262107,0.00019393768,0.0000437681,0.0005377292],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00022655386,0.00016241221,0.00013540243,0.00016777124,0.00012737732,0.000048277314,0.00014174059,0.00014908846,0.000034020177],"category_scores_gemma":[0.000067679626,0.00018170342,0.000022612836,0.00018004814,0.00009585947,0.00005129361,0.000017526632,0.00023826177,0.000018727465],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":true,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000048170215,0.00007362416,0.023587469,0.0010112184,0.000398149,0.0041794353,0.003688899,0.2600629,0.06834611,0.0594469,0.22051866,0.35863847],"study_design_scores_gemma":[0.00079100573,0.00008891755,0.34309348,0.00015767166,0.00011990058,0.00012637544,0.001334061,0.43412033,0.00021528575,0.0057824585,0.21246633,0.0017041749],"about_ca_topic_score_codex":0.0014500596,"about_ca_topic_score_gemma":0.023797212,"teacher_disagreement_score":0.35693428,"about_ca_system_score_codex":0.0002036325,"about_ca_system_score_gemma":0.00008028407,"threshold_uncertainty_score":0.99401593},"labels":[],"label_agreement":null},{"id":"W1892209963","doi":"","title":"Control of Acoustic Resonance in Shallow Rectangular Cavities Using Surface Mounted Blocks","year":2014,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"Ontario Tech University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Attenuation; Resonance (particle physics); Acoustics; Vortex; Mach number; Acoustic resonance; Acoustic attenuation; Enhanced Data Rates for GSM Evolution; Materials science; Square (algebra); Wind tunnel; Upstream (networking); Flow (mathematics); Optics; Physics; Geometry; Mechanics; Engineering; Telecommunications; Mathematics","score_opus":0.006176407502339384,"score_gpt":0.19680196953178933,"score_spread":0.19062556202944994,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1892209963","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8396994,0.00048403488,0.15768607,0.000018854447,0.0005687967,0.00018179977,0.0003054221,0.00006462066,0.00099102],"genre_scores_gemma":[0.994292,0.0000557306,0.005276605,0.00008744552,0.00011263786,0.0000033736176,0.000013068105,0.000074523276,0.00008458357],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99859786,0.000031418444,0.00039317802,0.00020823037,0.00018224634,0.00058704626],"domain_scores_gemma":[0.9990548,0.00015710219,0.00005187647,0.0003571511,0.0001250978,0.00025396305],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00027120684,0.00023752099,0.00037744912,0.00019282698,0.00006440387,0.000030458752,0.00026242997,0.00021178494,0.00003955795],"category_scores_gemma":[0.00025592983,0.00028515226,0.000051118746,0.00030301328,0.00010904893,0.000058380487,0.000015249339,0.00031485094,0.0000043671703],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":true,"about_ca_topic_consensus":true,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000035537762,0.0000062535432,0.0008392679,0.000082590246,0.000015327383,0.000031465763,0.000092999646,0.88492376,0.11329948,0.00021373724,0.00024137751,0.0002501971],"study_design_scores_gemma":[0.00040701593,0.000021101023,0.0023804659,0.00012405853,0.000049367838,0.000008169908,0.00010731332,0.99594223,0.00012284797,0.0002110878,0.0003333795,0.00029297385],"about_ca_topic_score_codex":0.010227338,"about_ca_topic_score_gemma":0.035601925,"teacher_disagreement_score":0.15459265,"about_ca_system_score_codex":0.00052978826,"about_ca_system_score_gemma":0.00019773605,"threshold_uncertainty_score":0.99996006},"labels":[],"label_agreement":null},{"id":"W1915119597","doi":"","title":"Jet noise prediction model for turbofan engines with internal forced mixers","year":2007,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Turbofan; Jet noise; Noise (video); Jet (fluid); Turbulence; Reynolds-averaged Navier–Stokes equations; Jet engine; Computational fluid dynamics; Near and far field; Plume; Acoustics; Mechanics; Environmental science; Meteorology; Physics; Engineering; Aerospace engineering; Computer science; Optics","score_opus":0.006193257397857154,"score_gpt":0.18928019551625475,"score_spread":0.1830869381183976,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1915119597","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.16996017,0.000027130951,0.8265799,0.000022013539,0.0006742192,0.00022589047,0.0005440239,0.00013301763,0.0018336343],"genre_scores_gemma":[0.9752813,0.000022899158,0.023593502,0.00011109387,0.0003525533,0.000016149788,0.00009360374,0.0000844934,0.00044438764],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989574,0.0000017724365,0.00020958428,0.00016720666,0.000119476965,0.0005445438],"domain_scores_gemma":[0.9991833,0.000051087754,0.000024276289,0.00019938759,0.000109402834,0.00043253688],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00014059892,0.00020217316,0.00014859848,0.00018557509,0.000094045026,0.000042230648,0.00016645156,0.00013839954,0.000008742174],"category_scores_gemma":[0.00004315248,0.00019741336,0.000045982688,0.00011543462,0.000040005598,0.00006688845,0.0000080524205,0.00018855755,0.0000034511372],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":true,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000013338947,0.000003846507,0.0002471503,0.00006091163,0.000039491686,0.000016795075,0.0001426465,0.98615634,0.0065908404,0.0003760767,0.0047441525,0.0016084234],"study_design_scores_gemma":[0.00032324984,0.000041250623,0.0009795505,0.000033508553,0.00006196664,0.000011759734,0.000085897416,0.99723166,0.00010322654,0.00017916065,0.00071706483,0.00023167804],"about_ca_topic_score_codex":0.00066698034,"about_ca_topic_score_gemma":0.018205514,"teacher_disagreement_score":0.80532116,"about_ca_system_score_codex":0.00038822193,"about_ca_system_score_gemma":0.00012629804,"threshold_uncertainty_score":0.99970967},"labels":[],"label_agreement":null},{"id":"W1963748350","doi":"10.2514/2.2009","title":"Comment on \"Large-Eddy Simulation of a Turbulent Compressible Round Jet\" vis-a`-vis Lighthill's Theory of Jet Noise","year":2003,"lang":"en","type":"article","venue":"AIAA Journal","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto","funders":"","keywords":"Physics; Jet (fluid); Jet noise; Turbulence; Aeroacoustics; Context (archaeology); Nozzle; Supersonic speed; Mechanics; Rotational symmetry; Sound pressure; Large eddy simulation; Noise (video); Classical mechanics; Acoustics","score_opus":0.01312232747310144,"score_gpt":0.24512562756205455,"score_spread":0.23200330008895312,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1963748350","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.5725526,0.00091242493,0.4197042,0.00028302893,0.0010388591,0.00024040026,0.000051161118,0.000050485858,0.0051668514],"genre_scores_gemma":[0.99737614,0.00020306872,0.0020763583,0.00018341937,0.00009301569,0.000002161937,0.000006027872,0.000035108005,0.000024667757],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99871635,0.00009678552,0.0004989717,0.000108303146,0.00032724466,0.00025232718],"domain_scores_gemma":[0.99909776,0.00025590556,0.00018096119,0.0002407415,0.00012671885,0.00009791877],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006255951,0.00018359727,0.0002918296,0.00012429048,0.00009647201,0.00003397316,0.00017164057,0.000090020374,0.00023732736],"category_scores_gemma":[0.000061066035,0.00015230037,0.00012746661,0.00011569582,0.000032355038,0.00009435746,0.000022618524,0.00036620974,0.000007867405],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00003270696,0.00020146968,0.00038971932,0.000058575886,0.00011179024,0.000011290082,0.0003162882,0.981454,0.0023797825,0.013012946,0.0013587727,0.00067261484],"study_design_scores_gemma":[0.0013695417,0.0002742047,0.00081639923,0.00032499345,0.00009010919,0.000034631652,0.00020839133,0.96770287,0.0053490805,0.009209452,0.014322338,0.00029801583],"about_ca_topic_score_codex":0.0000015803219,"about_ca_topic_score_gemma":0.0000013194503,"teacher_disagreement_score":0.42482358,"about_ca_system_score_codex":0.000092274764,"about_ca_system_score_gemma":0.00002289782,"threshold_uncertainty_score":0.6210629},"labels":[],"label_agreement":null},{"id":"W1964343580","doi":"10.1115/fedsm2006-98561","title":"CFD Simulations of the Aeroacoustic Noise Generated by a Cavity Flow","year":2006,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Ansys (Canada)","funders":"","keywords":"Turbulence; Computational fluid dynamics; Polygon mesh; Reynolds number; Noise (video); Acoustics; Mechanics; Narrowband; Flow (mathematics); Physics; Optics; Geometry; Computer science; Mathematics","score_opus":0.0032958784451124464,"score_gpt":0.17172619800807168,"score_spread":0.16843031956295923,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1964343580","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.78743905,0.00007376869,0.20623314,0.000030308267,0.00032843626,0.000120683006,0.0002133246,0.00012197063,0.0054392884],"genre_scores_gemma":[0.99623585,0.0000040257955,0.002571745,0.000019607294,0.00005791407,0.0000029472442,0.000034896133,0.000020072333,0.0010529604],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99949306,0.000009205204,0.00017192587,0.00008235532,0.00010915063,0.00013430176],"domain_scores_gemma":[0.9996536,0.000039750616,0.000018761397,0.00021997542,0.000046484547,0.000021426004],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000038229406,0.000093279574,0.000094035255,0.000018040437,0.00005903733,0.000013729245,0.000118125696,0.00005609821,0.00009115294],"category_scores_gemma":[0.000014971222,0.00006882507,0.000041391246,0.00017588491,0.00003090566,0.000026617807,0.000023714783,0.00009075923,0.000005149515],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[3.9088042e-7,0.000019171175,0.00021207453,0.000009751203,0.0000072524836,2.2994406e-7,0.0000064692063,0.8888476,0.10275699,0.00020491086,0.0078056026,0.00012959265],"study_design_scores_gemma":[0.00011135013,0.000003008139,0.0009359152,0.000004559984,0.000019685453,5.3437805e-7,0.0000035031514,0.9947822,0.0034596915,0.00024985624,0.00034180083,0.00008787618],"about_ca_topic_score_codex":0.000099478246,"about_ca_topic_score_gemma":0.0002091927,"teacher_disagreement_score":0.20879675,"about_ca_system_score_codex":0.000033046505,"about_ca_system_score_gemma":0.000010100678,"threshold_uncertainty_score":0.2806605},"labels":[],"label_agreement":null},{"id":"W1964390657","doi":"10.1121/1.1931087","title":"Airflow noise in telephone handsets and methods for its reduction","year":2005,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Institute for Microstructural Sciences","funders":"","keywords":"Airflow; Microphone; Acoustics; Mouthpiece; Noise (video); Noise-canceling microphone; Sound pressure; Physics; Microphone array; Computer science","score_opus":0.00886126113350281,"score_gpt":0.275667048914204,"score_spread":0.2668057877807012,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1964390657","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.05889171,0.0012550962,0.93701035,0.002280412,0.0003424511,0.00014906497,0.000007995588,0.000010604735,0.00005233113],"genre_scores_gemma":[0.61455256,0.0015166649,0.3835035,0.00013247943,0.00024292212,0.0000016741875,2.0175732e-7,0.000016208014,0.000033809854],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99923646,0.000053787808,0.0003434431,0.000055165856,0.00013840059,0.00017274196],"domain_scores_gemma":[0.99921626,0.0003847385,0.00013142612,0.00013399261,0.00008502276,0.00004857536],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0007607209,0.000101376696,0.00024074093,0.000017196684,0.00007324702,0.000009692873,0.00023813482,0.00006336285,0.000008675621],"category_scores_gemma":[0.00016358407,0.000059369602,0.00015914961,0.00015770894,0.00017860672,0.00006422131,0.000052606414,0.00033147426,4.384767e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000501171,0.000050311115,0.000007307287,0.000069082875,0.00008766664,1.16330135e-7,0.0007581436,0.62354517,0.23786843,0.00000549679,0.0067978753,0.13076031],"study_design_scores_gemma":[0.00034065347,0.00007028626,0.00022482162,0.0000473638,0.000106651925,0.00003806742,0.00040222652,0.99230695,0.0041490737,0.0005006128,0.0017384847,0.000074795455],"about_ca_topic_score_codex":0.0000025504257,"about_ca_topic_score_gemma":4.1525115e-7,"teacher_disagreement_score":0.55566084,"about_ca_system_score_codex":0.000066725835,"about_ca_system_score_gemma":0.00001993012,"threshold_uncertainty_score":0.2421022},"labels":[],"label_agreement":null},{"id":"W1966116626","doi":"10.1115/pvp2014-28316","title":"Flow Around a Leading-Edge Slat: Part I — Turbulent Flow Statistics","year":2014,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of New Brunswick","funders":"","keywords":"Reynolds number; Particle image velocimetry; Wind tunnel; Turbulence; Takeoff; Airframe; Airfoil; Lift (data mining); Leading edge; Noise (video); Vorticity; Mechanics; Angle of attack; Geology; Geometry; Physics; Aerospace engineering; Aerodynamics; Engineering; Vortex; Mathematics; Computer science","score_opus":0.008625397191925083,"score_gpt":0.20689134770343995,"score_spread":0.19826595051151485,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1966116626","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0106910905,0.00006753896,0.9583418,0.00006120432,0.0014232777,0.00011282644,0.00008068411,0.00040760305,0.02881401],"genre_scores_gemma":[0.8123556,0.00012611265,0.1808113,0.0002623899,0.0009066371,0.000021691956,0.00012456789,0.000113071095,0.005278664],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99892384,0.000014403368,0.0002700132,0.00020987667,0.00019351763,0.00038835005],"domain_scores_gemma":[0.9993386,0.000111100955,0.000021829634,0.00034503714,0.000049406106,0.00013402136],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017961276,0.00022076549,0.00022713639,0.000048647224,0.000077702294,0.00008744257,0.0001826689,0.0001010783,0.0003404444],"category_scores_gemma":[0.000056156787,0.0002096999,0.000050382096,0.00009044031,0.00003814519,0.00006329322,0.000037207486,0.00022152005,0.00052619114],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000022414433,0.000022572898,0.000058509304,0.000073595664,0.000040211748,0.000010643085,0.00008449226,0.89231753,0.0002783348,0.010970588,0.07699403,0.019147256],"study_design_scores_gemma":[0.00018776859,0.000031238887,0.0000475968,0.000019361205,0.000022442104,0.0000071818995,0.000014306249,0.93001723,0.000069528265,0.0027822908,0.06652764,0.00027338808],"about_ca_topic_score_codex":0.0000041714425,"about_ca_topic_score_gemma":0.0000464956,"teacher_disagreement_score":0.8016645,"about_ca_system_score_codex":0.00006934536,"about_ca_system_score_gemma":0.0000110703495,"threshold_uncertainty_score":0.8551314},"labels":[],"label_agreement":null},{"id":"W1967371752","doi":"10.1260/1475-472x.10.2-3.201","title":"Aeroacoustics of Pipe Systems with Closed Branches","year":2011,"lang":"en","type":"article","venue":"International Journal of Aeroacoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":102,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"","keywords":"Aeroacoustics; Acoustics; Flow (mathematics); Mode (computer interface); Power (physics); Sound power; Computer science; Physics; Mechanics; Sound (geography); Sound pressure","score_opus":0.013423053502439218,"score_gpt":0.18866285994513748,"score_spread":0.17523980644269826,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1967371752","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.20419507,0.00049662904,0.7855314,0.000018004119,0.004093462,0.000104173625,0.000108145316,0.000051574898,0.0054015378],"genre_scores_gemma":[0.97674996,0.00041589918,0.022163225,0.000018791961,0.000520704,0.0000017155116,0.0000056450826,0.00005506168,0.000068985246],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9981157,0.000019226914,0.0007936517,0.000108622655,0.0007503296,0.0002124489],"domain_scores_gemma":[0.99790776,0.00011131654,0.00040656363,0.00019746597,0.001278853,0.0000980504],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00027992172,0.0002140109,0.0003626299,0.00023571345,0.000024660796,0.00004201337,0.0006463496,0.000116653726,0.000042489566],"category_scores_gemma":[0.00009478607,0.00017825651,0.00013398117,0.0001345221,0.00011545012,0.0001546368,0.00004233971,0.00034344493,0.0000045466854],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00036988882,0.00043033285,0.0018863499,0.00028181644,0.0022208786,0.000607839,0.0014000594,0.92703044,0.05574276,0.002549516,0.0028851747,0.0045949593],"study_design_scores_gemma":[0.0042443327,0.0012940796,0.00740504,0.0013465072,0.0011697724,0.0021558662,0.0023651759,0.95877606,0.015561611,0.0018203782,0.0026188542,0.0012423025],"about_ca_topic_score_codex":0.000008549175,"about_ca_topic_score_gemma":0.000004596218,"teacher_disagreement_score":0.77255493,"about_ca_system_score_codex":0.000108860986,"about_ca_system_score_gemma":0.00008243241,"threshold_uncertainty_score":0.7269089},"labels":[],"label_agreement":null},{"id":"W1968180242","doi":"10.1016/j.expthermflusci.2014.10.025","title":"Reynolds number effects in the near-field of a turbulent square jet","year":2014,"lang":"en","type":"article","venue":"Experimental Thermal and Fluid Science","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":43,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Windsor","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Reynolds number; Turbulence; Physics; Mechanics; Jet (fluid); Particle image velocimetry; Vorticity; Strouhal number; Classical mechanics; Vortex","score_opus":0.004822710617345046,"score_gpt":0.2366790952383521,"score_spread":0.23185638462100705,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1968180242","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9910654,0.00024017846,0.00045416746,0.000040635532,0.00015681882,0.00009168658,6.599701e-7,0.000017239408,0.007933204],"genre_scores_gemma":[0.9993099,0.000008378273,0.00049261894,0.00013109721,0.000031032698,0.0000112845755,3.2479585e-7,0.0000060382654,0.000009315542],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99942064,0.000016582018,0.000091790476,0.00011961312,0.00018232114,0.00016903889],"domain_scores_gemma":[0.9997346,0.00006405167,0.0000111057725,0.00014753299,0.000008645617,0.000034065968],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00026606614,0.00008358064,0.00008696545,0.000017902055,0.000082189385,0.000042688374,0.00023060154,0.000026984379,0.000023227716],"category_scores_gemma":[0.000016920463,0.00005516833,0.000019717148,0.0001537503,0.00019477628,0.000083852196,0.000050425155,0.000077127894,0.000005829588],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000008980459,0.000056323086,0.0018764242,0.000032987686,0.0000028278944,0.000005317765,0.0033556586,0.003096652,0.9809934,0.008082203,0.00012594208,0.0023632697],"study_design_scores_gemma":[0.000427719,0.00023384126,0.013940533,0.00007321983,0.0000036881695,0.000020307732,0.00059659174,0.65552074,0.32828403,0.00024878883,0.0004198874,0.00023068982],"about_ca_topic_score_codex":0.000015998226,"about_ca_topic_score_gemma":0.0000013429377,"teacher_disagreement_score":0.65270936,"about_ca_system_score_codex":0.000015451973,"about_ca_system_score_gemma":0.0000061964333,"threshold_uncertainty_score":0.22496991},"labels":[],"label_agreement":null},{"id":"W1968408075","doi":"10.1007/s10494-008-9176-9","title":"Effect of Sudden Expansion on Entrainment and Spreading Rates of a Jet Issuing from Asymmetric Nozzles","year":2008,"lang":"en","type":"article","venue":"Flow Turbulence and Combustion","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":32,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Manitoba","funders":"Manitoba Hydro","keywords":"Nozzle; Entrainment (biomusicology); Mechanics; Jet (fluid); Turbulence; Reynolds number; Body orifice; Physics; Materials science; Acoustics; Engineering; Thermodynamics; Mechanical engineering","score_opus":0.006975420692268264,"score_gpt":0.2144376976080817,"score_spread":0.20746227691581345,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1968408075","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9935057,0.00107012,0.004987574,0.0000054831453,0.00016075135,0.000112581416,0.000022562164,0.000027112967,0.00010810566],"genre_scores_gemma":[0.997426,0.0017358462,0.00075434987,0.0000060697384,0.000039330418,0.0000047000435,0.000017665061,0.000011624504,0.0000044695726],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994185,0.000022519103,0.00017194283,0.00013575361,0.00013888365,0.00011239191],"domain_scores_gemma":[0.99956214,0.00023425014,0.0000414983,0.000104965286,0.000019125071,0.000038008915],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00013709944,0.00012512517,0.00021052427,0.0000939275,0.000049059618,0.000007959735,0.00005078889,0.00006379977,0.000008603534],"category_scores_gemma":[0.00004595257,0.00010673334,0.000026655605,0.00011573234,0.00004741345,0.00006227055,0.000023392564,0.00009122295,0.0000011476678],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00038678735,0.00019435537,0.068879426,0.0017453693,0.00022728331,0.00005369514,0.0036780268,0.358173,0.22122435,0.0004615863,0.0007974822,0.34417862],"study_design_scores_gemma":[0.00055463373,0.00041665215,0.013637851,0.00048502334,0.000052717285,0.0000063703583,0.0000616536,0.84728825,0.13717754,0.00013644173,0.0000113975275,0.0001714644],"about_ca_topic_score_codex":0.00003212718,"about_ca_topic_score_gemma":0.0000018669704,"teacher_disagreement_score":0.48911524,"about_ca_system_score_codex":0.000015930487,"about_ca_system_score_gemma":0.0000033871547,"threshold_uncertainty_score":0.43524593},"labels":[],"label_agreement":null},{"id":"W1969652010","doi":"10.1063/1.3562841","title":"Experimental investigation of the flow in the near-field of a cross-shaped orifice jet","year":2011,"lang":"en","type":"article","venue":"Physics of Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":41,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Polytechnique Montréal","funders":"","keywords":"Physics; Mechanics; Turbulence; Particle image velocimetry; Vortex; Vorticity; Jet (fluid); Body orifice; Entrainment (biomusicology); Momentum (technical analysis); Classical mechanics","score_opus":0.02317948319070674,"score_gpt":0.25291798969137524,"score_spread":0.22973850650066852,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1969652010","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99431103,0.000066155124,0.003542451,0.000008627071,0.00016730864,0.000101187245,0.00001538198,0.000008725283,0.0017791403],"genre_scores_gemma":[0.99808097,0.0000051809484,0.0018339555,0.000020617847,0.000034155084,0.0000073320584,0.0000025414906,0.000011379364,0.000003896219],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99949205,0.000017419423,0.0001938538,0.0000642785,0.0001473582,0.00008503137],"domain_scores_gemma":[0.99957836,0.000059262933,0.000043749085,0.00026393126,0.00004331872,0.000011399935],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012054224,0.000077671364,0.00011943327,0.000010658792,0.000021404472,0.00000682543,0.00027634657,0.000039742146,0.000013522028],"category_scores_gemma":[0.000022240109,0.00005315784,0.000058722384,0.0001609406,0.00012612095,0.00006872143,0.000037027265,0.00010434926,8.7334485e-7],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000016332579,0.000100983765,0.012902691,0.00011718551,0.000029452753,4.152979e-7,0.011367674,0.012893041,0.95214415,0.009847978,0.00013351867,0.00044659572],"study_design_scores_gemma":[0.0002162859,0.000055601304,0.012301127,0.000043516597,0.000011875488,3.236372e-7,0.00023270851,0.4227787,0.56041956,0.0038526221,0.000008182406,0.000079489895],"about_ca_topic_score_codex":0.000060323775,"about_ca_topic_score_gemma":0.000004839755,"teacher_disagreement_score":0.40988564,"about_ca_system_score_codex":0.000009973871,"about_ca_system_score_gemma":0.00001590257,"threshold_uncertainty_score":0.2167714},"labels":[],"label_agreement":null},{"id":"W1970486514","doi":"10.1115/1.2907413","title":"Acoustic Power Calculation in Deep Cavity Flows: A Semiempirical Approach","year":2008,"lang":"en","type":"article","venue":"Journal of Fluids Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":22,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Victoria","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Sound power; Acoustics; Physics; Acoustic wave equation; Acoustic source localization; Acoustic radiation; Vorticity; Particle image velocimetry; Duct (anatomy); Particle velocity; Turbulence; Mechanics; Acoustic wave; Optics; Vortex; Radiation","score_opus":0.008590872950434572,"score_gpt":0.20356394097412397,"score_spread":0.1949730680236894,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1970486514","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.53644514,0.00040904048,0.4624117,0.000006511746,0.00038666994,0.000042332336,0.0000014447788,0.00004225398,0.00025491382],"genre_scores_gemma":[0.9752345,0.00012910295,0.024350371,0.000009079867,0.00021284808,0.0000026450714,0.0000018865734,0.000045576824,0.000014003528],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9987996,0.000011030361,0.00052104914,0.000101548,0.00028404928,0.000282678],"domain_scores_gemma":[0.9995605,0.000064393695,0.000042244454,0.00013869505,0.000072465475,0.000121705496],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025553184,0.00018508088,0.00030911702,0.00026642496,0.000029198342,0.000016535574,0.00016580865,0.00013364437,0.000009829983],"category_scores_gemma":[0.000115847535,0.00018132494,0.000111011796,0.00029778853,0.000014422205,0.00018100505,0.000023183793,0.00054569176,0.0000031632746],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000050555623,0.000033059914,0.00069448946,0.00005790281,0.000022136917,0.00012763376,0.00028976979,0.960502,0.03792072,0.000025894617,0.00017640543,0.00014492506],"study_design_scores_gemma":[0.00034474014,0.000032747444,0.009064114,0.00004970321,0.000015002457,0.000447976,0.000021836131,0.9895705,0.00015656627,0.000011934274,0.00009581491,0.00018904834],"about_ca_topic_score_codex":0.0000019974063,"about_ca_topic_score_gemma":0.0000022377933,"teacher_disagreement_score":0.43878934,"about_ca_system_score_codex":0.0002532285,"about_ca_system_score_gemma":0.000025746718,"threshold_uncertainty_score":0.73942167},"labels":[],"label_agreement":null},{"id":"W1972508225","doi":"10.1115/ht-fed2004-56908","title":"Aeroacoustic Study of Tonal Noise Generated by Axial Flow Fans","year":2004,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Ansys (Canada)","funders":"","keywords":"Anechoic chamber; Acoustics; Noise (video); Thrust; Computational fluid dynamics; Aeroacoustics; Flow (mathematics); Computer science; Engineering; Sound pressure; Physics; Aerospace engineering; Mechanics; Artificial intelligence","score_opus":0.0057947560026714185,"score_gpt":0.1967227431948992,"score_spread":0.19092798719222778,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1972508225","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.83059055,0.000036948022,0.16659528,0.00000842234,0.00038588795,0.00016176375,0.00004926744,0.00014865577,0.002023216],"genre_scores_gemma":[0.9954967,0.000013926416,0.004107323,0.000018652328,0.000089655565,0.000010864817,0.000027980634,0.000035224894,0.00019969179],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99918485,0.000007170096,0.0002524447,0.00015200525,0.00019644761,0.00020709695],"domain_scores_gemma":[0.9996497,0.000016392349,0.00001837612,0.00019691071,0.000050961466,0.00006764305],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000062644314,0.00015326843,0.00018087495,0.000043868353,0.000040286595,0.000018041268,0.00014700239,0.00006688197,0.00013004596],"category_scores_gemma":[0.000011306645,0.00014335173,0.000035028686,0.00015513576,0.000021659527,0.00004166166,0.000029087858,0.00013200368,0.000017591701],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000042531524,0.00023406808,0.000076429635,0.0000144462965,0.00004849722,0.000006971071,0.00019249892,0.93922037,0.058545463,0.000101176585,0.0011285502,0.00042726772],"study_design_scores_gemma":[0.0013264373,0.00018835107,0.0003890447,0.0000088605975,0.000047929825,0.000003056832,0.00029350503,0.99472374,0.0025746685,0.00012348135,0.00007103674,0.0002498669],"about_ca_topic_score_codex":0.00007041609,"about_ca_topic_score_gemma":0.00014107503,"teacher_disagreement_score":0.16490613,"about_ca_system_score_codex":0.000061481005,"about_ca_system_score_gemma":0.000018579818,"threshold_uncertainty_score":0.5845714},"labels":[],"label_agreement":null},{"id":"W1973048400","doi":"10.1115/pvp2006-icpvt-11-93133","title":"Flow Excitation of Diametral Acoustic Modes of Axisymmetric Cavities","year":2006,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"","keywords":"Excited state; Rotational symmetry; Resonance (particle physics); Mach number; Excitation; Mechanics; Physics; Flow (mathematics); Materials science; Acoustics; Optics; Atomic physics","score_opus":0.0038135063971453257,"score_gpt":0.17169156052961346,"score_spread":0.16787805413246812,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1973048400","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.62897825,0.00017307446,0.3583865,0.0000015490216,0.00012490277,0.00004598435,0.000031738105,0.000053818378,0.012204193],"genre_scores_gemma":[0.97875786,0.000032153042,0.020895418,0.0000020343507,0.000044802557,0.0000031238828,0.000014341722,0.000017628208,0.00023262415],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994437,0.0000047866315,0.00023709616,0.00006448521,0.00013071144,0.000119213604],"domain_scores_gemma":[0.99971145,0.00007565014,0.000029978677,0.000109982866,0.000056901954,0.000016042313],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00006363695,0.00008300357,0.00014902612,0.0001777653,0.000011726962,0.000006084685,0.00007199032,0.00004954066,0.000031717133],"category_scores_gemma":[0.000027588336,0.00007947429,0.00004663856,0.00027914692,0.000037266556,0.000053769796,0.000010174068,0.000050831444,0.0000019028481],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000001336096,0.000019764033,0.00030331418,0.0001251173,0.000008801963,4.878477e-7,0.000027480248,0.9441294,0.049225558,0.0043613394,0.00030449836,0.0014929016],"study_design_scores_gemma":[0.00010797403,0.00002085084,0.004291409,0.000012452283,0.000017848872,5.2317665e-7,0.00009088715,0.9867251,0.0055260104,0.0031127352,0.0000083213745,0.0000858809],"about_ca_topic_score_codex":0.00010640348,"about_ca_topic_score_gemma":0.00007065518,"teacher_disagreement_score":0.34977964,"about_ca_system_score_codex":0.000023746765,"about_ca_system_score_gemma":0.0000068288605,"threshold_uncertainty_score":0.32408676},"labels":[],"label_agreement":null},{"id":"W1974489364","doi":"10.2514/6.2011-2785","title":"Airfoil Trailing Edge Noise Source Location for Low to Moderate Reynolds Number","year":2011,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":18,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Independent Electricity System Operator; University of Adelaide","keywords":"Airfoil; Trailing edge; Reynolds number; Noise (video); Computer science; Acoustics; Physics; Turbulence; Mechanics; Artificial intelligence","score_opus":0.016047186824012002,"score_gpt":0.21467827608245602,"score_spread":0.19863108925844403,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1974489364","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.19228753,0.000008236698,0.78403413,0.000017750946,0.00033899985,0.00017382785,0.0000061065066,0.00023440977,0.022899013],"genre_scores_gemma":[0.9533269,0.00000567292,0.043708477,0.000112996815,0.00013576601,0.00005274438,0.000008576477,0.000054452932,0.0025944244],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993551,0.000003512884,0.00017632858,0.00016011395,0.000068733825,0.00023623832],"domain_scores_gemma":[0.9995972,0.00002282261,0.000012752001,0.0001975853,0.00008357532,0.00008609158],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00010480892,0.00012813328,0.00011657186,0.000031697873,0.00005722658,0.000025950223,0.00011686507,0.00007856547,0.00010377106],"category_scores_gemma":[0.00002295489,0.00012885657,0.000040720755,0.000075644006,0.000009590842,0.00007134406,0.00001930536,0.000075027834,0.00013037604],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000025842111,0.000040849092,0.00007709218,0.00015123849,0.000029796338,0.0000010697808,0.0011088902,0.9693353,0.0053764717,0.0072159213,0.0028551295,0.013782401],"study_design_scores_gemma":[0.00017062013,0.000015498686,0.00012718354,0.000023761648,0.000012138504,0.0000015138398,0.00006580118,0.9924941,0.0048908964,0.0005878903,0.0014074459,0.0002031254],"about_ca_topic_score_codex":0.000017985238,"about_ca_topic_score_gemma":0.00004885776,"teacher_disagreement_score":0.7610394,"about_ca_system_score_codex":0.000032643133,"about_ca_system_score_gemma":0.000010748562,"threshold_uncertainty_score":0.52546185},"labels":[],"label_agreement":null},{"id":"W1974761506","doi":"10.1299/jfst.6.437","title":"Flow Structure of a Coaxial Circular Jet with Axisymmetric and Helical Instability Modes","year":2011,"lang":"en","type":"article","venue":"Journal of Fluid Science and Technology","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Victoria","funders":"","keywords":"Instability; Coaxial; Mechanics; Jet (fluid); Vortex; Physics; Rotational symmetry; Reynolds number; Flow visualization; Vortex ring; Convection; Classical mechanics; Flow (mathematics); Turbulence","score_opus":0.007520567290040188,"score_gpt":0.18905178443260717,"score_spread":0.18153121714256698,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1974761506","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9905091,0.00044457824,0.008756365,0.000038154903,0.000068461995,0.00003914351,0.0000054282004,0.00001605923,0.00012273835],"genre_scores_gemma":[0.9881186,0.00014570507,0.011710119,0.000006018875,0.000013958418,2.739014e-7,6.616203e-8,0.000004928229,3.281108e-7],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99932855,0.0000043406517,0.0002020347,0.00010410702,0.00021153763,0.00014941886],"domain_scores_gemma":[0.99947906,0.000015545951,0.00005690031,0.00012632347,0.00026178244,0.00006039287],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025908698,0.000079657126,0.00019753509,0.0004499672,0.0000531061,0.000011854303,0.00021197945,0.00009372718,0.0000044855933],"category_scores_gemma":[0.00015295953,0.00005458549,0.000013315567,0.0008291686,0.0008530431,0.000137807,0.000054049535,0.00021880808,7.0991476e-8],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000037690446,0.00005864768,0.02598563,0.00010167844,0.00004683105,0.000044948258,0.0003202119,0.0017840242,0.9272793,0.00837033,0.000016895423,0.03595384],"study_design_scores_gemma":[0.0014706792,0.0018855021,0.034499638,0.00011588981,0.00010644913,0.0020757406,0.00091739924,0.74431384,0.18382762,0.030186135,0.00015083242,0.00045027983],"about_ca_topic_score_codex":0.0000028556544,"about_ca_topic_score_gemma":0.0000060642224,"teacher_disagreement_score":0.74345165,"about_ca_system_score_codex":0.000026068543,"about_ca_system_score_gemma":0.00006669797,"threshold_uncertainty_score":0.31430727},"labels":[],"label_agreement":null},{"id":"W1974932465","doi":"10.1016/j.jfluidstructs.2010.10.002","title":"The planar jet-plate oscillator","year":2010,"lang":"en","type":"article","venue":"Journal of Fluids and Structures","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":13,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"","keywords":"Jet (fluid); Transverse plane; Oscillation (cell signaling); Physics; Mechanics; Amplitude; Planar; Optics; Instability; Acoustics; Materials science; Structural engineering","score_opus":0.003600470834387882,"score_gpt":0.19965481533127824,"score_spread":0.19605434449689035,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1974932465","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9951738,0.0009444309,0.0010158754,0.000104718034,0.0020149383,0.000021650538,0.000007422118,0.000010957089,0.000706181],"genre_scores_gemma":[0.9963528,0.00059479725,0.0025072913,0.000023481349,0.00047962778,1.6440752e-7,2.470762e-7,0.000010778769,0.000030840674],"study_design_codex":"bench_or_experimental","study_design_gemma":"not_applicable","domain_scores_codex":[0.9995348,0.0000046013565,0.00018914249,0.000037751535,0.000119457225,0.00011428328],"domain_scores_gemma":[0.9997042,0.00006034386,0.000037477956,0.00008701822,0.000043166376,0.00006778466],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00013935576,0.00008114238,0.00010968007,0.000027647166,0.000117477684,0.00007817793,0.00012880743,0.00005901062,0.000015407606],"category_scores_gemma":[0.000032493183,0.00004371285,0.000041048286,0.000028993918,0.000051695042,0.00004316173,0.000009511286,0.00035700464,5.0208473e-7],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00008151874,0.000010521434,0.0054626507,0.00008234647,0.00039677153,0.00012629892,0.00062914507,0.009785795,0.7691995,0.09204145,0.048667673,0.07351637],"study_design_scores_gemma":[0.0021230772,0.00043345647,0.17742234,0.0000756862,0.00021304832,0.002692361,0.00046408662,0.21784334,0.009213606,0.18224373,0.4062331,0.0010421741],"about_ca_topic_score_codex":0.0000011746895,"about_ca_topic_score_gemma":0.000016799706,"teacher_disagreement_score":0.75998586,"about_ca_system_score_codex":0.0000055822984,"about_ca_system_score_gemma":0.000010288849,"threshold_uncertainty_score":0.17825583},"labels":[],"label_agreement":null},{"id":"W1975849928","doi":"10.1007/s00348-011-1177-0","title":"The effect of chamber length and Reynolds number on jet precession","year":2011,"lang":"en","type":"article","venue":"Experiments in Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":14,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Alberta","funders":"","keywords":"Physics; Jet (fluid); Precession; Reynolds number; Mechanics; Entrainment (biomusicology); Nozzle; Range (aeronautics); Materials science; Turbulence; Thermodynamics; Condensed matter physics","score_opus":0.010296963984174193,"score_gpt":0.2611511246558185,"score_spread":0.25085416067164434,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1975849928","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9583116,0.0003661582,0.00011253646,0.0000025205993,0.00052312855,0.0001323659,0.00000252874,0.000035164157,0.040514007],"genre_scores_gemma":[0.99919784,0.00018230476,0.00031080033,0.0000056677222,0.000031739342,0.00003231648,0.0000014096979,0.00002467137,0.00021326091],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9994112,0.000032525226,0.00016633642,0.00011588064,0.00011403826,0.00015997473],"domain_scores_gemma":[0.9996502,0.00007993754,0.00001559162,0.00021713886,0.0000069200114,0.000030246816],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000191424,0.00012717399,0.00013188977,0.000023157098,0.000042643795,0.000009280722,0.00009164078,0.00007030913,0.00006586238],"category_scores_gemma":[0.0000202252,0.000082435916,0.000022196107,0.000059272632,0.000049904796,0.00003965403,0.000049941915,0.0001164686,0.000013171798],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0015269531,0.0007364959,0.2923322,0.0007564989,0.00064080214,0.00011909407,0.043549992,0.005231699,0.4869715,0.021524733,0.016430326,0.13017973],"study_design_scores_gemma":[0.0025480646,0.0008877188,0.030718712,0.00040920303,0.000025440355,0.0000098326755,0.0002833617,0.11172031,0.8479944,0.00055537384,0.004195156,0.0006524379],"about_ca_topic_score_codex":0.000014540847,"about_ca_topic_score_gemma":0.0000031225902,"teacher_disagreement_score":0.36102292,"about_ca_system_score_codex":0.00003632007,"about_ca_system_score_gemma":0.000002984985,"threshold_uncertainty_score":0.3361639},"labels":[],"label_agreement":null},{"id":"W1976360739","doi":"10.1121/1.3097765","title":"Forward projection of transient sound pressure fields radiated by impacted plates using numerical Laplace transform","year":2009,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":29,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Polytechnique Montréal","funders":"Natural Sciences and Engineering Research Council of Canada; Fonds Québécois de la Recherche sur la Nature et les Technologies","keywords":"Aliasing; Inverse Laplace transform; Transient (computer programming); Laplace transform; Fourier transform; Acoustics; Discrete Fourier transform (general); Short-time Fourier transform; Acoustic holography; Projection plane; Mathematics; Projection (relational algebra); Algorithm; Computer science; Mathematical analysis; Physics; Optics; Near and far field; Fourier analysis; Telecommunications; Computer vision","score_opus":0.006662964964210063,"score_gpt":0.227899192371893,"score_spread":0.22123622740768292,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1976360739","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.17337112,0.0005318485,0.82470953,0.0008395084,0.00019665867,0.00017753335,0.000045284596,0.000020770733,0.00010776013],"genre_scores_gemma":[0.99076146,0.0004582772,0.008523555,0.0001466258,0.0000762448,3.5308943e-7,0.000001177635,0.000017876226,0.000014415563],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99875534,0.000049874023,0.0005107521,0.00006689965,0.00037233852,0.00024481193],"domain_scores_gemma":[0.99919623,0.00021330184,0.00023040635,0.00017262726,0.000114188835,0.00007324439],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002856533,0.00016252008,0.0003783586,0.000017996115,0.00009731793,0.000012049685,0.0003519941,0.00011621444,0.000020879332],"category_scores_gemma":[0.00004371736,0.00009462648,0.000371606,0.00029566564,0.00018836129,0.00008109841,0.000014442403,0.0005574275,1.7843583e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00013082127,0.00011468377,0.00001171597,0.000073768686,0.00032360604,4.5570147e-7,0.0011404039,0.90218115,0.084196426,0.0000016342889,0.0069242474,0.00490108],"study_design_scores_gemma":[0.0003817209,0.00034126118,0.00015783729,0.000060602593,0.0004968604,0.000046038094,0.00048351384,0.9945446,0.0025802348,0.00040869677,0.0003878783,0.00011073127],"about_ca_topic_score_codex":0.00002734748,"about_ca_topic_score_gemma":3.0936897e-7,"teacher_disagreement_score":0.8173904,"about_ca_system_score_codex":0.00006234429,"about_ca_system_score_gemma":0.000042336105,"threshold_uncertainty_score":0.38587555},"labels":[],"label_agreement":null},{"id":"W1976633931","doi":"10.1088/1748-3182/7/3/036010","title":"Effect of vehicle configuration on the performance of a submersible pulsed-jet vehicle at intermediate Reynolds number","year":2012,"lang":"en","type":"article","venue":"Bioinspiration & Biomimetics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":11,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lockheed Martin (Canada)","funders":"National Science Foundation","keywords":"Propulsive efficiency; Mechanics; Reynolds number; Nozzle; Body orifice; Propulsion; Jet (fluid); Drag; Thrust; Vortex; Physics; Materials science; Aerospace engineering; Engineering; Turbulence; Mechanical engineering","score_opus":0.009078292568860063,"score_gpt":0.22251081585940782,"score_spread":0.21343252329054777,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1976633931","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9968884,0.000068102025,0.00045196252,0.000032582146,0.00050078076,0.00025603344,0.000032245174,0.00004744707,0.0017224583],"genre_scores_gemma":[0.9995583,0.00007294227,0.00009799092,0.000030710064,0.00010053205,0.00001608721,0.000032930497,0.000026856731,0.00006364686],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99906653,0.00005761602,0.00034452503,0.00009991727,0.00021185492,0.00021952554],"domain_scores_gemma":[0.9993169,0.00016032276,0.00012242098,0.00028242756,0.00006642982,0.00005155107],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00049886946,0.00015900773,0.00018920808,0.00005845658,0.000069740774,0.000013114277,0.00013767176,0.00011212517,0.00011410436],"category_scores_gemma":[0.000054739477,0.00011536735,0.0000695552,0.00021794709,0.00010009356,0.0001134432,0.000034098626,0.00010441618,0.00009412762],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0001434304,0.00010511938,0.058676925,0.000391315,0.000076376076,4.0545052e-7,0.00042657607,0.006330016,0.9218798,0.0014558531,0.00093748624,0.009576684],"study_design_scores_gemma":[0.00033498887,0.000333083,0.008433471,0.00003980441,0.000038669186,7.300214e-7,0.000011223514,0.30015036,0.69008106,0.0000046360124,0.000456617,0.00011535694],"about_ca_topic_score_codex":0.000004796945,"about_ca_topic_score_gemma":0.0000035623318,"teacher_disagreement_score":0.29382035,"about_ca_system_score_codex":0.00007654249,"about_ca_system_score_gemma":0.000009558729,"threshold_uncertainty_score":0.4704544},"labels":[],"label_agreement":null},{"id":"W1976736280","doi":"10.5539/mas.v3n6p119","title":"Research for Characteristics of Rotating Dipole Acoustic Source in Spatial Acoustic Field","year":2009,"lang":"en","type":"article","venue":"Modern Applied Science","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Acoustics; Dipole; Physics; Acoustic source localization; Acoustic space; Directivity; Point source; Sound pressure; Acoustic wave equation; Field (mathematics); Acoustic wave; Harmonic; Optics; Computer science; Mathematics; Telecommunications","score_opus":0.019529190153368386,"score_gpt":0.2871969883997278,"score_spread":0.2676677982463594,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1976736280","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.31249937,0.000011565579,0.6856496,0.000019834828,0.00010183678,0.0002453843,0.0000089985415,0.000041162126,0.00142223],"genre_scores_gemma":[0.994459,0.0000073728966,0.0053075114,0.00003826138,0.00009029329,0.000032774373,0.0000029832174,0.000018481633,0.00004336181],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9983755,0.0000074873374,0.00031251975,0.00028781523,0.00045596674,0.0005607363],"domain_scores_gemma":[0.9991822,0.00030772548,0.000042317464,0.00027892095,0.00010856464,0.00008027473],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0010080661,0.00012550906,0.00020224454,0.00022498662,0.00016561206,0.00006083842,0.00047237167,0.00007577696,0.0000068437917],"category_scores_gemma":[0.0002553699,0.00013187082,0.000025508005,0.00047818123,0.00017026265,0.00006350781,0.00006698617,0.0002976837,0.0000045775205],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000012865881,0.000026669755,0.00006368341,0.000057880632,0.0000010917379,0.0000010318075,0.0003456807,0.3563753,0.58257455,0.00027584797,0.000023029286,0.06024239],"study_design_scores_gemma":[0.00018956178,0.00006672261,0.002170792,0.00003617259,0.000004879058,7.1505536e-7,0.000078685014,0.98905414,0.0048202,0.003429479,0.000009134537,0.00013952328],"about_ca_topic_score_codex":0.000013421798,"about_ca_topic_score_gemma":0.000029745586,"teacher_disagreement_score":0.68195957,"about_ca_system_score_codex":0.000085056476,"about_ca_system_score_gemma":0.000073303265,"threshold_uncertainty_score":0.53775364},"labels":[],"label_agreement":null},{"id":"W1977269363","doi":"10.1260/095745606777071036","title":"Active Local Control of Propeller-Aircraft Run-Up Noise","year":2006,"lang":"en","type":"article","venue":"Noise & Vibration Worldwide","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of British Columbia","funders":"","keywords":"Noise (video); Active noise control; Noise control; Propeller; Noise pollution; Engineering; Acoustics; Channel (broadcasting); Control theory (sociology); Computer science; Noise reduction; Marine engineering; Control (management); Telecommunications; Physics","score_opus":0.004170790672761936,"score_gpt":0.19136622593491537,"score_spread":0.18719543526215343,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1977269363","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.12511978,0.00016276342,0.85629195,0.00019369512,0.00075421866,0.00046610722,0.00009060202,0.0002788651,0.016642012],"genre_scores_gemma":[0.99674606,0.000016908643,0.0019016062,0.00008036203,0.00024704338,0.00003543414,0.00006020264,0.00005535831,0.0008570431],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9988065,0.00002751872,0.00043082243,0.00021119263,0.00025433878,0.00026963506],"domain_scores_gemma":[0.999366,0.00008428792,0.0000875771,0.00027762612,0.0001163889,0.0000681156],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00010551678,0.00021782357,0.00027262777,0.000118350436,0.00006843179,0.000035185298,0.0001602761,0.000103820596,0.00017747449],"category_scores_gemma":[0.000024647936,0.00021593696,0.00009526172,0.00024508155,0.00008418,0.000208536,0.000023261468,0.00020465463,0.00007025556],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00006578837,0.000079510755,0.0003735246,0.00007654355,0.000048532736,0.0000075982252,0.00010221543,0.8610008,0.12287035,0.002946714,0.0041029775,0.008325483],"study_design_scores_gemma":[0.0010472507,0.000038906037,0.004597967,0.000050521274,0.000052478637,0.0000024551316,0.000049622988,0.9590486,0.030829381,0.000988536,0.0029912018,0.0003030508],"about_ca_topic_score_codex":0.000054945467,"about_ca_topic_score_gemma":0.00020154353,"teacher_disagreement_score":0.87162626,"about_ca_system_score_codex":0.00009705092,"about_ca_system_score_gemma":0.000042566913,"threshold_uncertainty_score":0.88056535},"labels":[],"label_agreement":null},{"id":"W1977396033","doi":"10.1016/j.microrel.2005.05.013","title":"Investigation of increased performance of close series stacked tube axial fans due to inclusion of diffuser element","year":2005,"lang":"en","type":"article","venue":"Microelectronics Reliability","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Waterloo","funders":"","keywords":"Diffuser (optics); Tube (container); Series (stratigraphy); Inclusion (mineral); Materials science; Element (criminal law); Structural engineering; Engineering; Optics; Composite material; Physics; Geology; Thermodynamics; Political science","score_opus":0.0038812529026614594,"score_gpt":0.19398663876180663,"score_spread":0.1901053858591452,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1977396033","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99680823,0.00012992257,0.0023221595,0.00009042576,0.00007277901,0.00035633866,0.000095183954,0.000042041316,0.00008288859],"genre_scores_gemma":[0.99305725,0.00016196295,0.006626245,0.000019550052,0.000036154957,0.0000134099755,0.000045185796,0.00002724689,0.000012990411],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99849415,0.000042502186,0.00068790413,0.0002094175,0.00026671487,0.00029933345],"domain_scores_gemma":[0.99907607,0.000052845466,0.00012086965,0.00045270866,0.0002235298,0.00007399765],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005589543,0.00018261705,0.00036643422,0.00008726779,0.000062761384,0.000004705504,0.0002475301,0.000107124404,0.000026944645],"category_scores_gemma":[0.00007629929,0.0001854933,0.000075865646,0.00026788117,0.000108128195,0.00011454962,0.00023771079,0.00020411692,0.0000017110195],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00012595931,0.00008347529,0.0044022813,0.0004902684,0.000026973616,1.7505023e-7,0.0009208795,0.07579176,0.9159623,0.0003759694,0.00008335431,0.0017366385],"study_design_scores_gemma":[0.00045497602,0.00042439712,0.0065797428,0.00006272371,0.000032311356,0.0000014735149,0.000024846597,0.16652603,0.82441646,0.00068236503,0.00060351874,0.00019116857],"about_ca_topic_score_codex":0.00007125854,"about_ca_topic_score_gemma":0.00020073335,"teacher_disagreement_score":0.09154583,"about_ca_system_score_codex":0.0003306642,"about_ca_system_score_gemma":0.000114484865,"threshold_uncertainty_score":0.7564198},"labels":[],"label_agreement":null},{"id":"W1977553111","doi":"10.1002/cnm.1267","title":"Free jet issuing from a pipe with a triangular collar: A numerical simulation","year":2009,"lang":"en","type":"article","venue":"International Journal for Numerical Methods in Biomedical Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Manitoba","funders":"","keywords":"Collar; Reynolds-averaged Navier–Stokes equations; Closure (psychology); Turbulence; Jet (fluid); Mechanics; Reynolds stress; Reynolds number; Mathematics; Engineering; Structural engineering; Physics; Law","score_opus":0.01361604892672882,"score_gpt":0.3386079882675173,"score_spread":0.3249919393407885,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1977553111","genre_codex":"methods","genre_gemma":"methods","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.006930997,0.00026228218,0.98906964,0.0006805986,0.0025543289,0.00018485005,0.00007632038,0.00017084682,0.00007013306],"genre_scores_gemma":[0.39128712,0.000036027574,0.60752213,0.00013510494,0.0009199367,0.000016243055,0.000027631426,0.00004741364,0.0000083957775],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99790424,0.00005347622,0.00069675286,0.00026976512,0.00063453504,0.00044123823],"domain_scores_gemma":[0.99821305,0.0010544137,0.000093361436,0.00019819355,0.00014414375,0.0002968288],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00065289787,0.0002977371,0.00044735076,0.0003572614,0.000053792108,0.00014061717,0.00065364555,0.00019897729,0.000066291715],"category_scores_gemma":[0.00157275,0.00025444932,0.000161427,0.00044890217,0.000031591204,0.00018135433,0.00005048215,0.0006790155,0.0000021089575],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00013977605,0.000102944054,0.00005253039,0.000011361661,0.00016904467,0.00014587722,0.00012242277,0.89590657,0.008058978,0.0003912691,0.00018657403,0.09471265],"study_design_scores_gemma":[0.0016911787,0.00018500176,0.00052635703,0.00015493073,0.000031198146,0.0000688825,0.000022447522,0.9760759,0.00027606124,0.004254021,0.01639742,0.00031663844],"about_ca_topic_score_codex":0.000009629423,"about_ca_topic_score_gemma":6.5398063e-7,"teacher_disagreement_score":0.3843561,"about_ca_system_score_codex":0.000367525,"about_ca_system_score_gemma":0.000037660186,"threshold_uncertainty_score":0.99999076},"labels":[],"label_agreement":null},{"id":"W1977766956","doi":"10.1115/1.4005739","title":"Characteristics of a Jet in the Vicinity of a Free Surface","year":2012,"lang":"en","type":"article","venue":"Journal of Fluids Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":21,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Windsor","funders":"","keywords":"Free surface; Jet (fluid); Turbulence; Nozzle; Plane (geometry); Reynolds number; Surface (topology); Mechanics; Physics; Materials science; Geometry; Thermodynamics; Mathematics","score_opus":0.00808431196818239,"score_gpt":0.20362977503958404,"score_spread":0.19554546307140167,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1977766956","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.96932983,0.0006819197,0.029194294,0.000016113801,0.0005488067,0.00004211814,0.000016871732,0.000008653075,0.00016139209],"genre_scores_gemma":[0.99397194,0.00025890997,0.00556492,0.000004802682,0.00017695878,4.2348978e-7,6.3090505e-7,0.000019908062,0.0000014975327],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9990104,0.000013333422,0.0005468046,0.000029821182,0.00021491676,0.00018476283],"domain_scores_gemma":[0.999438,0.00015591286,0.00009990145,0.00019037051,0.000069499045,0.00004631513],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00071243476,0.00010956008,0.00029417104,0.000094630755,0.000007355366,0.0000062520835,0.00030493105,0.000057813548,0.000008005772],"category_scores_gemma":[0.0001863841,0.000082530976,0.00008178451,0.00018071891,0.00001479928,0.00011126037,0.000027490963,0.00030600323,4.4491662e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00002119777,0.00016892343,0.03145373,0.00078800943,0.00011332396,0.000022195338,0.0026745836,0.4686462,0.49306557,0.0016288592,0.0005480811,0.0008693393],"study_design_scores_gemma":[0.0012126657,0.0002316112,0.29271317,0.00070370716,0.00016129046,0.000193493,0.0003762025,0.67920804,0.023475967,0.00013134732,0.0011348602,0.00045764545],"about_ca_topic_score_codex":0.0000032294672,"about_ca_topic_score_gemma":8.938099e-7,"teacher_disagreement_score":0.4695896,"about_ca_system_score_codex":0.000036807287,"about_ca_system_score_gemma":0.000011563756,"threshold_uncertainty_score":0.33655155},"labels":[],"label_agreement":null},{"id":"W1979312904","doi":"10.1121/1.4779957","title":"Active control of automotive fan noise","year":2002,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Directivity; Acoustics; Mechanical fan; Active noise control; Noise (video); Feed forward; Aeroacoustics; Computer science; Physics; Control theory (sociology); Engineering; Noise reduction; Sound pressure; Electrical engineering; Control (management)","score_opus":0.006541952085932869,"score_gpt":0.2020862037272595,"score_spread":0.19554425164132663,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1979312904","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0508266,0.0005222166,0.94498694,0.0017678044,0.00047191887,0.00016654268,0.00007255521,0.00002281112,0.0011626345],"genre_scores_gemma":[0.99048656,0.00066861464,0.008322759,0.00031675864,0.00013559386,5.92971e-7,1.2955262e-7,0.000020971454,0.0000480255],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99886525,0.00006546986,0.00043103416,0.00005311157,0.00038063267,0.00020452953],"domain_scores_gemma":[0.99852824,0.000584868,0.0003327793,0.00024677368,0.00024133812,0.00006601074],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00026306557,0.0001360322,0.00037495513,0.000014259023,0.00007598305,0.000005919751,0.0005565813,0.00006977697,0.00010255075],"category_scores_gemma":[0.00019509613,0.00007490375,0.0004133466,0.00019901851,0.0005402829,0.000053562904,0.00006559246,0.0005210536,0.0000030476835],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00006151671,0.0001761248,0.000045004494,0.000073617906,0.0007553216,0.0000013301722,0.0023064911,0.89808005,0.061372157,0.000015516982,0.020871613,0.016241241],"study_design_scores_gemma":[0.000436017,0.00014835945,0.0006532571,0.000057448746,0.00032508356,0.000017435286,0.0010675404,0.99482024,0.0016932187,0.0003973484,0.00029515082,0.0000889286],"about_ca_topic_score_codex":0.0000073044534,"about_ca_topic_score_gemma":1.6302414e-7,"teacher_disagreement_score":0.93965995,"about_ca_system_score_codex":0.00006946489,"about_ca_system_score_gemma":0.000016853071,"threshold_uncertainty_score":0.30544862},"labels":[],"label_agreement":null},{"id":"W1982381715","doi":"10.1016/j.icheatmasstransfer.2006.02.007","title":"Prediction of the flow structure in a turbulent rectangular free jet","year":2006,"lang":"en","type":"article","venue":"International Communications in Heat and Mass Transfer","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":43,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Manitoba","funders":"Natural Sciences and Engineering Research Council of Canada; Manitoba Hydro","keywords":"Turbulence; Mechanics; Jet (fluid); Vena contracta; Inlet; Flow (mathematics); Physics; Saddle; Inflow; Vector field; Geology; Mathematics; Regurgitation (circulation)","score_opus":0.010696497118006824,"score_gpt":0.21109834103612302,"score_spread":0.2004018439181162,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1982381715","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98345304,0.0010289312,0.009213166,0.0014432732,0.00035917503,0.0002138671,0.0003823621,0.000032041884,0.003874153],"genre_scores_gemma":[0.9969102,0.00052032724,0.0024292686,0.000015053743,0.00002516461,0.000017450939,0.00005723015,0.00000910262,0.000016194956],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999521,0.000023026987,0.00022024529,0.000065681226,0.00010334756,0.000066681896],"domain_scores_gemma":[0.99950576,0.00004681248,0.000004702693,0.00040356079,0.000030857533,0.000008327232],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00007333762,0.00006715331,0.000074535914,0.00007785912,0.0000258808,0.00001111673,0.000441939,0.000057088968,0.000013652253],"category_scores_gemma":[0.0000102028325,0.00005607141,0.000026562933,0.00011101511,0.000054854572,0.00005053803,0.000037481645,0.00020139324,1.3691681e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000027531689,0.00018314696,0.0863487,0.000087844935,0.00007280051,0.0000030330195,0.000998711,0.7645924,0.09056967,0.054121792,0.00057022425,0.0024241377],"study_design_scores_gemma":[0.0004707768,0.000006769087,0.05628786,0.000083210514,0.000008469471,0.000004617148,0.000032906322,0.9234522,0.0010791712,0.01599927,0.0025014055,0.0000733658],"about_ca_topic_score_codex":0.00012679024,"about_ca_topic_score_gemma":0.0018519697,"teacher_disagreement_score":0.15885976,"about_ca_system_score_codex":0.00006319818,"about_ca_system_score_gemma":0.0000069839184,"threshold_uncertainty_score":0.22865257},"labels":[],"label_agreement":null},{"id":"W1985216944","doi":"10.1115/1.2742721","title":"The Asymmetry of the Large-Scale Structures in Turbulent Three-Dimensional Wall Jets Exiting Long Rectangular Channels","year":2007,"lang":"en","type":"article","venue":"Journal of Fluids Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":25,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Jet (fluid); Turbulence; Physics; Asymmetry; Mechanics","score_opus":0.0048039418873541745,"score_gpt":0.20296641496070567,"score_spread":0.1981624730733515,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1985216944","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9226255,0.0028008497,0.072719835,0.00006605312,0.0016036277,0.00008897709,0.0000027700557,0.000022616905,0.0000698042],"genre_scores_gemma":[0.99539065,0.00006185306,0.004123092,0.000015977877,0.00035451265,8.7624414e-7,5.537102e-7,0.000042178002,0.0000102964705],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99838966,0.000012868151,0.0006908592,0.000088788154,0.0004215002,0.0003963298],"domain_scores_gemma":[0.9992674,0.00022955475,0.000120654935,0.00020799352,0.00010101212,0.000073369556],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0012275183,0.00018119901,0.00024994055,0.00014801513,0.000074847805,0.000029877117,0.00037401274,0.00010576303,0.0000062615895],"category_scores_gemma":[0.00014104265,0.00011798377,0.00016384835,0.00028878578,0.000025150557,0.00008214916,0.00006596401,0.00063086266,3.9084762e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000017907529,0.000013468273,0.0010633987,0.000062233295,0.000050199098,0.00004777106,0.00017163939,0.9659035,0.031259112,0.0003866255,0.00007005662,0.0009540718],"study_design_scores_gemma":[0.0004510284,0.00005171113,0.025965145,0.00035764126,0.00002929802,0.00015482167,0.00008170896,0.9578,0.014137956,0.00041769148,0.0003475957,0.00020540832],"about_ca_topic_score_codex":0.0000038990097,"about_ca_topic_score_gemma":0.00003645846,"teacher_disagreement_score":0.072765194,"about_ca_system_score_codex":0.00014125888,"about_ca_system_score_gemma":0.00002086128,"threshold_uncertainty_score":0.48112386},"labels":[],"label_agreement":null},{"id":"W1986663752","doi":"10.1063/1.1430734","title":"Large eddy simulation of the effects of mild swirl on the near field of a round free jet","year":2002,"lang":"en","type":"article","venue":"Physics of Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":56,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Queen's University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Physics; Braid; Turbulence; Jet (fluid); Mechanics; Vorticity; Large eddy simulation; Entrainment (biomusicology); Classical mechanics; Flow (mathematics); Plane (geometry); Field (mathematics); Vortex; Geometry","score_opus":0.009437332260128538,"score_gpt":0.21832227688540878,"score_spread":0.20888494462528023,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1986663752","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9771496,0.000151848,0.020818196,0.000040681374,0.00023776914,0.0001701013,0.000043789914,0.000011337189,0.0013766894],"genre_scores_gemma":[0.99966097,0.000030539377,0.00018945776,0.00002182027,0.000057088626,0.0000027630615,0.0000013020997,0.00001538143,0.000020693238],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994493,0.000017394335,0.00017989887,0.000063053536,0.00019208223,0.00009823842],"domain_scores_gemma":[0.99881244,0.0005821062,0.000063844294,0.00047175188,0.000058679118,0.000011153262],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00007744166,0.00009005686,0.00017385045,0.000012414313,0.000027420749,0.000003795403,0.00026453283,0.000046934747,0.000014994816],"category_scores_gemma":[0.00013842425,0.000060085975,0.000105277824,0.00013858409,0.00004836311,0.000032403757,0.00005708822,0.0001117513,0.0000010978179],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000091253705,0.00022282981,0.00045460896,0.0005943296,0.000104971565,2.1587448e-7,0.0010394212,0.8930699,0.0863861,0.015421795,0.0015449462,0.0011517183],"study_design_scores_gemma":[0.00025048034,0.00009588425,0.00040966083,0.000120985394,0.00003385741,3.109159e-8,0.000014256822,0.9262169,0.06950838,0.0032392906,0.00005299305,0.000057262765],"about_ca_topic_score_codex":0.000009945781,"about_ca_topic_score_gemma":0.0000032886887,"teacher_disagreement_score":0.03314697,"about_ca_system_score_codex":0.000009215003,"about_ca_system_score_gemma":0.0000042046563,"threshold_uncertainty_score":0.24502349},"labels":[],"label_agreement":null},{"id":"W1986838879","doi":"10.1121/1.3458846","title":"Noise prediction of a subsonic turbulent round jet using the lattice-Boltzmann method","year":2010,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":33,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"National Institute on Deafness and Other Communication Disorders; Université de Sherbrooke; Purdue Research Foundation","keywords":"Lattice Boltzmann methods; Turbulence; Physics; Nozzle; Mach number; Jet (fluid); Acoustics; Computational physics; Jet noise; Large eddy simulation; Mechanics; Noise (video); Rotational symmetry; Aeroacoustics; Sound pressure; Computer science","score_opus":0.013301185053869036,"score_gpt":0.2562506840918576,"score_spread":0.24294949903798854,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1986838879","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.2868231,0.00025323153,0.7109339,0.0010189792,0.00072851835,0.00012988404,0.000024819303,0.0000145887525,0.00007297265],"genre_scores_gemma":[0.8857018,0.00042015247,0.11328086,0.00018355313,0.00036347043,8.040747e-7,3.9558583e-7,0.000029628001,0.00001937767],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99850404,0.000109313965,0.00056262116,0.00007414666,0.0005070677,0.00024283731],"domain_scores_gemma":[0.9981278,0.0007428408,0.000405148,0.0004424962,0.00021532273,0.00006635737],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0012202557,0.00016512432,0.0003358011,0.000016820684,0.00017525729,0.00001971297,0.0007543587,0.00010829573,0.000035312],"category_scores_gemma":[0.00018056385,0.00007859134,0.00043132875,0.00026025812,0.0005040945,0.00007441775,0.00012575432,0.0010852171,7.8772536e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000032839816,0.0000781548,0.00009128037,0.0000736852,0.0003482738,6.1612e-7,0.0009171014,0.69730324,0.29572016,0.000035670313,0.0029373881,0.002461557],"study_design_scores_gemma":[0.00020989928,0.00007613469,0.00083873764,0.000056366785,0.0006002657,0.00009886614,0.000756225,0.99406314,0.0017348226,0.00093620823,0.000551304,0.00007801488],"about_ca_topic_score_codex":0.00003671642,"about_ca_topic_score_gemma":0.0000015160624,"teacher_disagreement_score":0.5988787,"about_ca_system_score_codex":0.00006771208,"about_ca_system_score_gemma":0.00006372598,"threshold_uncertainty_score":0.47147888},"labels":[],"label_agreement":null},{"id":"W1987153231","doi":"10.1016/j.compfluid.2010.05.006","title":"A hybrid algorithm for far-field noise minimization","year":2010,"lang":"en","type":"article","venue":"Computers & Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":31,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto","funders":"","keywords":"Solver; Discretization; Airfoil; Noise (video); Algorithm; Computation; Computer science; Field (mathematics); Computational fluid dynamics; Mathematics; Applied mathematics; Mathematical optimization; Mathematical analysis; Physics; Mechanics","score_opus":0.004710819581091345,"score_gpt":0.20383573750728282,"score_spread":0.19912491792619147,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1987153231","genre_codex":"methods","genre_gemma":"methods","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.029001515,0.00004421929,0.96598244,0.000055805536,0.003961983,0.00016549253,0.000028412389,0.00024226298,0.00051787135],"genre_scores_gemma":[0.42399582,0.00004320283,0.5743081,0.00037964314,0.0009494517,0.000037360354,0.000085047,0.000067652596,0.00013371004],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993978,0.000003322248,0.00015763553,0.0001545626,0.000078780955,0.00020787703],"domain_scores_gemma":[0.9995512,0.00009555785,0.000012891629,0.00021849797,0.000051897638,0.00006997344],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00006102745,0.00013076449,0.00012535864,0.00005235082,0.00006131165,0.00005316528,0.00019030321,0.00007104139,0.000021164644],"category_scores_gemma":[0.00001968852,0.00014156924,0.00006467186,0.000055429682,0.000017439703,0.000059074027,0.000037330767,0.00015541962,0.000012855638],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000004861852,0.000042473614,0.00003786975,0.000064870575,0.000056982095,0.000010777856,0.000119134325,0.045833465,0.028600385,0.0017780368,0.07409285,0.8493583],"study_design_scores_gemma":[0.0002501035,0.00003962901,0.000049245933,0.00000879731,0.0000129283435,0.0000073861474,0.0000029114008,0.97735137,0.0019976976,0.0004306186,0.019678798,0.00017049714],"about_ca_topic_score_codex":0.0000019851245,"about_ca_topic_score_gemma":0.000002163705,"teacher_disagreement_score":0.9315179,"about_ca_system_score_codex":0.000016270427,"about_ca_system_score_gemma":0.000010376874,"threshold_uncertainty_score":0.5773026},"labels":[],"label_agreement":null},{"id":"W1987721383","doi":"10.2514/6.2009-6954","title":"Integration and Application of a Tool Chain for Environmental Analysis of Aircraft Flight Trajectories","year":2009,"lang":"en","type":"article","venue":"9th AIAA Aviation Technology, Integration, and Operations Conference (ATIO)","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":10,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Partenariat Canadien Contre Le Cancer; Deutsches Zentrum für Luft- und Raumfahrt","keywords":"Aerospace engineering; Chain (unit); Computer science; Aeronautics; Systems engineering; Environmental science; Engineering; Physics","score_opus":0.0046453699678263806,"score_gpt":0.21493469949820598,"score_spread":0.2102893295303796,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1987721383","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.2852155,0.00011893507,0.71358234,0.00028127278,0.000052983254,0.00042883708,0.00017555975,0.0000794848,0.00006508586],"genre_scores_gemma":[0.97771966,0.00034248142,0.020888308,0.000019765906,0.000021644699,0.00015017139,0.0007544974,0.000010538593,0.00009290681],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989398,0.000019902387,0.0005545205,0.00024275783,0.00012099465,0.00012202829],"domain_scores_gemma":[0.9993338,0.000052975192,0.00011619327,0.00023114677,0.00023741918,0.000028494916],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00019682443,0.00018177135,0.00031388074,0.0005974002,0.00015863754,0.000047775844,0.00011033953,0.00021647068,0.000017680582],"category_scores_gemma":[0.00010980764,0.0001753002,0.00005420191,0.0005956459,0.00016144764,0.00028130584,0.000010777717,0.0001224635,5.8630286e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00001599632,0.00011296743,0.0038598084,0.000041541516,0.00023456197,9.472427e-8,0.0022644624,0.024719357,0.34970585,0.4324182,0.00005711887,0.18657003],"study_design_scores_gemma":[0.00028722276,0.00015139605,0.017979592,0.000021722835,0.00025854606,0.0000010639733,0.0011476263,0.9481815,0.026682924,0.0050056996,0.000093721144,0.00018894915],"about_ca_topic_score_codex":0.000018623246,"about_ca_topic_score_gemma":0.0005838976,"teacher_disagreement_score":0.92346215,"about_ca_system_score_codex":0.000054257493,"about_ca_system_score_gemma":0.00003132019,"threshold_uncertainty_score":0.71485347},"labels":[],"label_agreement":null},{"id":"W1989595839","doi":"10.3397/1.2919547","title":"Realism assessment of sonic boom simulators","year":2008,"lang":"en","type":"article","venue":"Noise Control Engineering Journal","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":9,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Transport Canada; Purdue University; National Aeronautics and Space Administration","keywords":"Sonic boom; Realism; Boom; Computer science; Aerospace engineering; Aeronautics; Engineering; Philosophy; Epistemology; Supersonic speed","score_opus":0.0048319760589861736,"score_gpt":0.20016543506170775,"score_spread":0.1953334590027216,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1989595839","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.3599534,0.00057385437,0.63710827,0.000025915437,0.0012209074,0.00009609707,0.000020396357,0.00016671464,0.0008344596],"genre_scores_gemma":[0.9924521,0.0003680754,0.006683099,0.000016611379,0.00037994512,0.0000044151175,0.0000021147746,0.000062232466,0.000031438845],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99879575,0.000011383316,0.0004490393,0.000104105595,0.0002962216,0.00034351653],"domain_scores_gemma":[0.99936336,0.000093932846,0.00007204932,0.0002062641,0.000093205155,0.00017121506],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023714318,0.00020580365,0.00034558563,0.00015689453,0.00008010941,0.000023406074,0.00021005058,0.00009946742,0.000045565004],"category_scores_gemma":[0.00005189653,0.0002029931,0.00015372636,0.00012096836,0.000025018924,0.00010670027,0.000016029733,0.0005411103,0.0000030165816],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000029536543,0.000015555997,0.00061767676,0.000031131516,0.00010366086,0.00006481371,0.000044653083,0.98753685,0.010485511,0.0004568222,0.00028252442,0.00035785136],"study_design_scores_gemma":[0.0010040511,0.000036698893,0.009481937,0.00005064649,0.000037064892,0.00019454927,0.0000055830715,0.9878985,0.000079501784,0.000038324717,0.000974113,0.00019901413],"about_ca_topic_score_codex":0.0000020434043,"about_ca_topic_score_gemma":4.885728e-7,"teacher_disagreement_score":0.6324987,"about_ca_system_score_codex":0.0001443218,"about_ca_system_score_gemma":0.00005676539,"threshold_uncertainty_score":0.82778186},"labels":[],"label_agreement":null},{"id":"W1991145390","doi":"10.1016/j.jfluidstructs.2012.12.008","title":"Flow-acoustic coupling in coaxial side branch resonators with rectangular splitter plates","year":2013,"lang":"en","type":"article","venue":"Journal of Fluids and Structures","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":12,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Victoria","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Acoustics; Duct (anatomy); Sound pressure; Particle image velocimetry; Aeroacoustics; Sound power; Physics; Vortex; Amplitude; Splitter plate; Vortex shedding; Acoustic wave; Mechanics; Optics; Turbulence; Reynolds number","score_opus":0.0037392401346032097,"score_gpt":0.18828588339127467,"score_spread":0.18454664325667144,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1991145390","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9899584,0.0013512613,0.008116037,0.00003858942,0.00032732167,0.00007229049,0.000005238637,0.000014821455,0.000116032104],"genre_scores_gemma":[0.99386585,0.00022502443,0.0055853487,0.000034975783,0.00024777077,0.0000020816938,0.0000011249384,0.000026962256,0.000010837321],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991811,0.0000071002205,0.0003325607,0.00009165962,0.00018519384,0.00020238913],"domain_scores_gemma":[0.9996409,0.000063210486,0.000051094914,0.00008613912,0.00007257651,0.00008606883],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000114588605,0.00015547064,0.0002622803,0.00011742409,0.000043303786,0.00007459852,0.000101129335,0.000090316615,0.00006436465],"category_scores_gemma":[0.000028706909,0.00010996008,0.000037228358,0.00008966121,0.000057264395,0.0001331126,0.000015454923,0.00034030242,7.1577387e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000047727506,0.0000081998005,0.004357083,0.00009474953,0.0000775076,0.00010097256,0.00037975033,0.94488984,0.04542521,0.00020849786,0.00090339425,0.0035070418],"study_design_scores_gemma":[0.0008258803,0.00015145435,0.039294586,0.0001510259,0.0000398185,0.00022607118,0.00022633604,0.95026386,0.0009061714,0.0074552973,0.00019414832,0.00026532813],"about_ca_topic_score_codex":0.00001535406,"about_ca_topic_score_gemma":0.000024038769,"teacher_disagreement_score":0.04451904,"about_ca_system_score_codex":0.000037443795,"about_ca_system_score_gemma":0.000017502573,"threshold_uncertainty_score":0.44840416},"labels":[],"label_agreement":null},{"id":"W1991381343","doi":"10.1115/fedsm2014-21282","title":"Experimental Study of Reynolds Number Effects on Three-Dimensional Offset Jets","year":2014,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Manitoba Hydro; University of Manitoba","funders":"","keywords":"Reynolds number; Turbulence; Turbulence kinetic energy; Reynolds stress; Mechanics; Physics; Magnetic Reynolds number; Reynolds stress equation model; Reynolds decomposition; Reynolds-averaged Navier–Stokes equations; Reynolds equation; K-omega turbulence model","score_opus":0.006529122290683821,"score_gpt":0.22816855595483976,"score_spread":0.22163943366415595,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1991381343","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9856552,0.000010349457,0.0015279499,0.0000051516877,0.0005206427,0.0001800187,0.0000024317605,0.000109523746,0.011988744],"genre_scores_gemma":[0.9989343,3.330699e-7,0.0007926991,0.000036838133,0.00008522812,0.000014462706,0.0000046100427,0.000028385079,0.000103114595],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993319,0.000015890148,0.000160968,0.00013936115,0.00021030339,0.00014155792],"domain_scores_gemma":[0.9995723,0.00010680228,0.000018159917,0.00023859907,0.000018567138,0.000045599147],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00009100827,0.00013137687,0.00016620672,0.000028401644,0.00003174114,0.0000079718575,0.000098254524,0.000052480893,0.00013912938],"category_scores_gemma":[0.000012589745,0.00011247685,0.000034114615,0.000056658722,0.000012962063,0.000026519248,0.000042408235,0.00009796265,0.00008286295],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00015466494,0.006248792,0.023284525,0.00033210678,0.00055483973,0.000057466066,0.0012984844,0.66185117,0.2331847,0.021971934,0.034152422,0.016908871],"study_design_scores_gemma":[0.0015139726,0.0009517921,0.008921955,0.000048143047,0.000021941078,0.0000037892262,0.00008519808,0.9455796,0.04201229,0.0003255125,0.0002168926,0.00031894425],"about_ca_topic_score_codex":0.000019678764,"about_ca_topic_score_gemma":0.000030862557,"teacher_disagreement_score":0.2837284,"about_ca_system_score_codex":0.000026344798,"about_ca_system_score_gemma":0.000002596922,"threshold_uncertainty_score":0.4586673},"labels":[],"label_agreement":null},{"id":"W1992662033","doi":"10.2514/2.2840","title":"Numerical Simulation of Aircraft Trailing Vortices Interacting with Ambient Shear or Ground","year":2001,"lang":"en","type":"article","venue":"Journal of Aircraft","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":17,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"National Research Council Canada","funders":"","keywords":"Vortex; Aerospace engineering; Mechanics; Vortex sheet; Shear (geology); Computer simulation; Trailing edge; Ground effect (cars); Physics; Geology; Vorticity; Engineering","score_opus":0.01515553836771648,"score_gpt":0.2609324749053772,"score_spread":0.2457769365376607,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1992662033","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7462795,0.000089775465,0.252712,0.00005989588,0.00047249976,0.00005325166,0.0000013914292,0.000026443926,0.0003052831],"genre_scores_gemma":[0.98735785,0.000073194606,0.012166451,0.00002148488,0.0002911851,7.164535e-7,9.2007053e-7,0.00003639732,0.00005180475],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.998673,0.000021721227,0.0006520035,0.00009641266,0.00034404415,0.00021280402],"domain_scores_gemma":[0.99900824,0.00031561588,0.0002677727,0.00012269738,0.00018793289,0.000097720855],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002698278,0.00015079913,0.00031946096,0.00012874526,0.000047400485,0.000042016258,0.00015543864,0.000063498366,0.000087618086],"category_scores_gemma":[0.00014286066,0.00011100911,0.00009787463,0.0002244285,0.000030479236,0.0003461342,0.000015213378,0.0003613332,0.0000029369437],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00015399861,0.00006673292,0.0015081008,0.00006318653,0.00009262967,0.00010594512,0.00042801228,0.99025816,0.003170329,0.000008751865,0.000039063874,0.004105114],"study_design_scores_gemma":[0.0005254146,0.00038344326,0.0029974072,0.0003221945,0.00007760088,0.00022161935,0.00040888015,0.9932958,0.00036786162,0.000038513877,0.0012037535,0.00015751399],"about_ca_topic_score_codex":0.000009476067,"about_ca_topic_score_gemma":0.000013145057,"teacher_disagreement_score":0.24107839,"about_ca_system_score_codex":0.00007100806,"about_ca_system_score_gemma":0.000037326477,"threshold_uncertainty_score":0.45268202},"labels":[],"label_agreement":null},{"id":"W1995486294","doi":"10.1260/1475-472x.9.3.273","title":"Extensions and limitations of analytical airfoil broadband noise models","year":2010,"lang":"en","type":"article","venue":"International Journal of Aeroacoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":154,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Airfoil; Trailing edge; Noise (video); Vortex shedding; Computer science; Wake; Aeroacoustics; Turbulence; Boundary layer; Acoustics; Physics; Aerospace engineering; Mechanics; Engineering; Reynolds number","score_opus":0.023996430981278398,"score_gpt":0.2447403246448237,"score_spread":0.2207438936635453,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1995486294","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.73591167,0.00011288611,0.25743085,0.00022819066,0.0022961402,0.00003733831,0.00005750773,0.000018403676,0.00390701],"genre_scores_gemma":[0.97494656,0.00079046853,0.023825841,0.0000334447,0.00031059203,5.4173563e-7,0.000003971452,0.000019902782,0.00006868902],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989713,0.0000070222577,0.00046346785,0.0000712536,0.00037542664,0.00011154292],"domain_scores_gemma":[0.9984691,0.00032612894,0.00012676536,0.00010855911,0.00085716,0.00011230136],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017661315,0.00010608256,0.00018258467,0.00017680108,0.000026559706,0.0000374129,0.00024534925,0.00008635909,0.000015471269],"category_scores_gemma":[0.0004421147,0.00009789831,0.00007798651,0.00007200928,0.00010764593,0.00014844025,0.00004378134,0.00040323945,0.0000013181459],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000025107043,0.000109373206,0.0002297936,0.000017484856,0.00025741087,0.000057850968,0.00022536927,0.9206042,0.05194126,0.015131999,0.0020644802,0.009335653],"study_design_scores_gemma":[0.00036097263,0.0000392669,0.0014471562,0.000036301906,0.00009269131,0.00019144322,0.000083498795,0.99141055,0.00022768525,0.005405451,0.000602475,0.00010249431],"about_ca_topic_score_codex":0.0000019095282,"about_ca_topic_score_gemma":0.000014881118,"teacher_disagreement_score":0.23903488,"about_ca_system_score_codex":0.000023522438,"about_ca_system_score_gemma":0.000045659523,"threshold_uncertainty_score":0.3992177},"labels":[],"label_agreement":null},{"id":"W1997128974","doi":"10.2514/1.j052380","title":"Subsonic Jet Noise Simulations Using Both Structured and Unstructured Grids","year":2014,"lang":"en","type":"article","venue":"AIAA Journal","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":62,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Compute Canada","keywords":"Jet noise; Large eddy simulation; Jet (fluid); Computational aeroacoustics; Nozzle; Mach number; Discontinuous Galerkin method; Turbulence; Unstructured grid; Noise (video); Grid; Discretization; Context (archaeology); Dissipative system; Reynolds number; Physics; Total variation diminishing; Mechanics; Computer science; Aeroacoustics; Computational fluid dynamics; Finite element method; Geometry; Acoustics; Mathematics; Mathematical analysis; Geology","score_opus":0.0066094691852885004,"score_gpt":0.2127987667998722,"score_spread":0.20618929761458368,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1997128974","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.89659,0.0001810062,0.102005705,0.000027123016,0.0008865789,0.0000419326,0.000016362388,0.00004844829,0.00020283299],"genre_scores_gemma":[0.98796433,0.000055828637,0.011339995,0.000038597074,0.0005493704,2.4238182e-7,0.0000045601814,0.0000357552,0.00001130963],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992787,0.000022039692,0.00021879899,0.00010200664,0.0001404289,0.00023800433],"domain_scores_gemma":[0.99959207,0.000048650963,0.000049305047,0.00013800224,0.000041720294,0.00013026767],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000113331604,0.00014969276,0.0001592802,0.00008134627,0.0002068944,0.00012628852,0.00011095329,0.000086457236,0.00008197579],"category_scores_gemma":[0.000040514136,0.00013175393,0.000043359123,0.00009368413,0.000037937945,0.00012060917,0.000024130566,0.00035753465,0.0000013950375],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000031952698,0.0000031806367,0.0032709225,0.000016414499,0.00004315869,0.0000056299364,0.00011044006,0.964145,0.027265975,0.0008440642,0.00015263249,0.004139383],"study_design_scores_gemma":[0.00036909457,0.00001610797,0.010066957,0.000021175903,0.000041096955,0.00020771736,0.000015743035,0.98015654,0.00016368667,0.008122377,0.000647778,0.00017174859],"about_ca_topic_score_codex":0.0000031730024,"about_ca_topic_score_gemma":0.000021788266,"teacher_disagreement_score":0.09137433,"about_ca_system_score_codex":0.000057421967,"about_ca_system_score_gemma":0.000018836943,"threshold_uncertainty_score":0.5372769},"labels":[],"label_agreement":null},{"id":"W1997558015","doi":"10.1121/1.4904489","title":"Subharmonic tonal noise from backflow vortices radiated by a low-speed ring fan in uniform inlet flow","year":2015,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":62,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Natural Sciences and Engineering Research Council of Canada; Compute Canada","keywords":"Acoustics; Aeroacoustics; Noise (video); Physics; Rotor (electric); Inlet; Reynolds-averaged Navier–Stokes equations; Vortex; Backflow; Turbofan; Frequency domain; Mechanics; Flow (mathematics); Turbulence; Computer science; Engineering; Mathematics; Aerospace engineering; Sound pressure; Mathematical analysis; Mechanical engineering","score_opus":0.009447435505125674,"score_gpt":0.21548053878298076,"score_spread":0.2060331032778551,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1997558015","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.85858583,0.0011523307,0.1381509,0.0010452614,0.0006099881,0.00014819593,0.00009898939,0.000031374588,0.0001771384],"genre_scores_gemma":[0.9824674,0.0007697684,0.016173944,0.0003283332,0.00019481267,7.7986846e-7,0.000004516694,0.000038136874,0.000022315584],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9982325,0.0000868249,0.00065225264,0.00010237049,0.00056223676,0.0003638058],"domain_scores_gemma":[0.99865437,0.00044732355,0.00027069956,0.00030538102,0.00014076427,0.00018144891],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00066643505,0.00021551125,0.00043556912,0.000024982974,0.000072000796,0.000030787356,0.00082826486,0.00010130619,0.000044284934],"category_scores_gemma":[0.00020448721,0.00013276028,0.0002640904,0.0003682768,0.0003227404,0.00012644612,0.00015570677,0.0008411379,0.0000065175827],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00008881466,0.00009146741,0.00029911345,0.000032677784,0.00021715302,0.0000039209003,0.0013006622,0.9378358,0.040158663,0.0000014159615,0.016297475,0.0036728526],"study_design_scores_gemma":[0.00076900236,0.00007867068,0.00090409577,0.000106784726,0.00015367348,0.000009840743,0.0010728048,0.99518627,0.0006603292,0.00051041367,0.00038454653,0.00016355926],"about_ca_topic_score_codex":0.00011230329,"about_ca_topic_score_gemma":0.000006931021,"teacher_disagreement_score":0.12388158,"about_ca_system_score_codex":0.00024204362,"about_ca_system_score_gemma":0.00009627028,"threshold_uncertainty_score":0.5413807},"labels":[],"label_agreement":null},{"id":"W1997874830","doi":"10.1016/j.expthermflusci.2012.01.028","title":"Mixing in turbulent free jets issuing from isosceles triangular orifices with different apex angles","year":2012,"lang":"en","type":"article","venue":"Experimental Thermal and Fluid Science","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":41,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"St. Francis Xavier University; Dalhousie University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Nozzle; Jet (fluid); Body orifice; Mechanics; Reynolds number; Turbulence; Physics; Turbulence kinetic energy; Mixing (physics); Pitot tube; Isosceles triangle; Materials science; Optics; Flow (mathematics); Thermodynamics; Geometry; Mechanical engineering","score_opus":0.009434102359100341,"score_gpt":0.21515599576301975,"score_spread":0.20572189340391941,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1997874830","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9913927,0.0068096146,0.00040003867,0.000015055028,0.0002957983,0.00010706881,0.00000812119,0.000057506717,0.0009141395],"genre_scores_gemma":[0.9983733,0.00004781579,0.0013539087,0.000024689223,0.00014836015,0.000014621105,0.0000029325988,0.000017438955,0.000016904705],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.998998,0.000012236761,0.00014550211,0.00021068618,0.00024584323,0.00038774125],"domain_scores_gemma":[0.99962574,0.00002765727,0.00001940328,0.0001866562,0.000008616838,0.00013194213],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00014549293,0.00017097089,0.00015094089,0.000064352185,0.00013494374,0.00008934038,0.00027028262,0.000036515798,0.000053194144],"category_scores_gemma":[0.000006512407,0.00012539123,0.000019198445,0.0001371772,0.000201142,0.00033954313,0.00010412888,0.00010131365,0.0000032298497],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000136165545,0.000070567956,0.0037537115,0.000006303679,0.000006705999,0.00000656047,0.0029022088,0.0011227458,0.99083865,0.0003802026,0.000009948687,0.00088876096],"study_design_scores_gemma":[0.0010055457,0.0001161484,0.048964784,0.00013334672,0.00001091478,0.000011625543,0.003928942,0.18084416,0.7641342,0.0000874049,0.00017965848,0.0005832245],"about_ca_topic_score_codex":0.000052661282,"about_ca_topic_score_gemma":0.000008479752,"teacher_disagreement_score":0.22670442,"about_ca_system_score_codex":0.000070087895,"about_ca_system_score_gemma":0.0000063773355,"threshold_uncertainty_score":0.5113306},"labels":[],"label_agreement":null},{"id":"W1998416182","doi":"10.1115/1.3089532","title":"Choking Phenomena in a Vortex Flow Passing a Laval Tube: An Analytical Treatment","year":2009,"lang":"en","type":"article","venue":"Journal of Fluids Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Nozzle; Mechanics; Vortex; Discharge coefficient; Flow (mathematics); Physics; Classical mechanics; Thermodynamics","score_opus":0.009171888807333502,"score_gpt":0.22820724442305523,"score_spread":0.21903535561572174,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1998416182","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8398581,0.00072775764,0.15776789,0.00006198174,0.00066373724,0.00008213451,0.0000040778546,0.000104384984,0.0007299231],"genre_scores_gemma":[0.98159057,0.00021213759,0.017281972,0.000015273577,0.0008440303,0.0000013002738,0.0000018937104,0.00003993285,0.0000128902175],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99867666,0.000011537555,0.00057195587,0.00012453175,0.00024097746,0.00037432296],"domain_scores_gemma":[0.99951184,0.00004046274,0.000041201598,0.0001742975,0.000044953158,0.00018727445],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00027563487,0.00023917404,0.00039373833,0.00034567434,0.00002782907,0.00008001045,0.0001704902,0.00009076229,0.000012705196],"category_scores_gemma":[0.000040205585,0.00022037384,0.00012493193,0.000270381,0.000009365384,0.00027558225,0.0000098002965,0.00035001631,0.0000013093285],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000008882761,0.00007069447,0.00021573069,0.000017214234,0.00003227553,0.00018402108,0.0002717558,0.9464408,0.018662017,0.00014575025,0.000016835784,0.033934],"study_design_scores_gemma":[0.0006147054,0.00028117953,0.0047660307,0.00012125903,0.000041530424,0.00010291111,0.00003604563,0.9931922,0.00021128332,0.00006402265,0.0003486529,0.00022021285],"about_ca_topic_score_codex":0.0000026660543,"about_ca_topic_score_gemma":0.0000037439413,"teacher_disagreement_score":0.14173247,"about_ca_system_score_codex":0.00046630576,"about_ca_system_score_gemma":0.00003392291,"threshold_uncertainty_score":0.89865845},"labels":[],"label_agreement":null},{"id":"W1998815871","doi":"10.1121/1.4806429","title":"Effects of a boundary layer trip in the prediction of noise from flow past tandem cylinders","year":2013,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"","keywords":"Boundary layer; Turbulence; Mechanics; Wind tunnel; Wake; Acoustics; Aeroacoustics; Vortex shedding; Computational fluid dynamics; Flow (mathematics); Noise (video); Geology; Physics; Reynolds number; Computer science; Sound pressure","score_opus":0.005851099353292719,"score_gpt":0.19694823959908012,"score_spread":0.1910971402457874,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1998815871","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6457242,0.0005785056,0.35178933,0.0009328101,0.0004714099,0.00031801048,0.000039218325,0.000010533489,0.00013604175],"genre_scores_gemma":[0.9896377,0.0006339076,0.009296604,0.00021607905,0.0001879443,0.000002811518,8.298553e-7,0.000018035606,0.0000061358437],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99858975,0.0001267496,0.000559985,0.000061063896,0.0004780438,0.00018441341],"domain_scores_gemma":[0.9980871,0.0011770653,0.0003128856,0.00025864737,0.00012231844,0.000041986583],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004545286,0.00013525295,0.00036275908,0.000019212437,0.00006372526,0.000012317847,0.00059455965,0.00009466637,0.000026868462],"category_scores_gemma":[0.00015719786,0.00006732592,0.00032142212,0.0002476882,0.00044894541,0.0000710677,0.000070601505,0.00057771447,0.0000011484901],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000779632,0.0003162859,0.0009019481,0.0002626143,0.00056106347,0.0000015505201,0.0048558833,0.7322315,0.22405213,0.0000045300403,0.02505995,0.011674581],"study_design_scores_gemma":[0.0006060202,0.00016331472,0.020771228,0.00017230319,0.0003015967,0.000006670462,0.0017800578,0.9734563,0.0012185953,0.0013513529,0.00010066953,0.000071862334],"about_ca_topic_score_codex":0.000079724196,"about_ca_topic_score_gemma":0.0000010002872,"teacher_disagreement_score":0.3439135,"about_ca_system_score_codex":0.000057353176,"about_ca_system_score_gemma":0.000039639857,"threshold_uncertainty_score":0.27454713},"labels":[],"label_agreement":null},{"id":"W1999960330","doi":"10.2514/6.2012-2060","title":"On the generation of airfoil tonal noise at zero angle of attack and low to moderate Reynolds number","year":2012,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":11,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Independent Electricity System Operator","keywords":"Airfoil; Reynolds number; Angle of attack; Zero (linguistics); Noise (video); Acoustics; Physics; Computer science; Mechanics; Aerodynamics; Turbulence; Artificial intelligence","score_opus":0.020893918770218414,"score_gpt":0.23346954415197962,"score_spread":0.21257562538176122,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1999960330","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97090495,0.00002577252,0.020907223,0.000054578282,0.00015820579,0.00007376382,0.000017757582,0.000016921618,0.007840855],"genre_scores_gemma":[0.997463,0.000017558077,0.001570247,0.00008429747,0.000066290544,0.0000050961885,0.000005521727,0.000014859734,0.0007731254],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995804,0.0000077905715,0.00013054792,0.00006326346,0.00009974288,0.00011824976],"domain_scores_gemma":[0.99972135,0.00004132762,0.00001708137,0.00014461578,0.000032416556,0.00004320982],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00010594808,0.00007543423,0.00009255332,0.00001456826,0.000029202605,0.0000066797516,0.000047791626,0.000042055704,0.00015938711],"category_scores_gemma":[0.000014069711,0.000053674674,0.000020864829,0.000047806865,0.000017224924,0.000041695213,0.000035380664,0.000044653218,0.000019159841],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000018647746,0.000056009772,0.0013128695,0.00005818127,0.000033756645,3.2602702e-7,0.00039909958,0.78226763,0.17361996,0.01887833,0.022598587,0.00075658323],"study_design_scores_gemma":[0.00010783754,0.000021254249,0.0012385759,0.000015079518,0.0000087411445,0.0000014865167,0.00000991532,0.9556092,0.0425529,0.00015908266,0.00018115235,0.00009476174],"about_ca_topic_score_codex":0.0000064920914,"about_ca_topic_score_gemma":0.000022593977,"teacher_disagreement_score":0.17334156,"about_ca_system_score_codex":0.000023766279,"about_ca_system_score_gemma":0.000003155276,"threshold_uncertainty_score":0.21887897},"labels":[],"label_agreement":null},{"id":"W2003220845","doi":"10.1016/j.jsv.2008.09.019","title":"Experimental validation of tonal noise control from subsonic axial fans using flow control obstructions","year":2008,"lang":"en","type":"article","venue":"Journal of Sound and Vibration","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":21,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Acoustics; Sound power; Noise (video); Noise control; Lift (data mining); Directivity; Harmonics; Aeroacoustics; Rotor (electric); Axial compressor; Acoustic radiation; Flow (mathematics); Physics; Attenuation; Sound pressure; Engineering; Noise reduction; Computer science; Mechanics; Electrical engineering; Sound (geography); Aerospace engineering; Optics; Radiation; Gas compressor","score_opus":0.012943511512770327,"score_gpt":0.22207544005581595,"score_spread":0.20913192854304563,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2003220845","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6459786,0.00019648645,0.3533398,0.000008499697,0.00037825305,0.000037514943,0.000035942172,0.0000060058333,0.000018902905],"genre_scores_gemma":[0.99486214,0.0000316905,0.004610123,0.000010869146,0.00046259558,5.8350275e-7,0.000009362777,0.000011029876,0.0000016169652],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99935925,0.00001740743,0.0003369025,0.000054527423,0.00015355129,0.00007834955],"domain_scores_gemma":[0.9996426,0.00004974022,0.00013697802,0.000047514615,0.00007803563,0.00004514605],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00006917699,0.00008211595,0.00017246456,0.00005923247,0.00009390557,0.000026106649,0.00004022427,0.00005791752,0.000032475527],"category_scores_gemma":[0.000014504217,0.00007779765,0.00006189471,0.000044595832,0.000040210973,0.00028993946,0.0000037958632,0.000107935324,4.2389937e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000044763645,0.00003059629,0.0022003711,0.0000062803997,0.00006918419,0.0000037451016,0.0003606387,0.5671625,0.42987952,0.000091272195,0.0000141684695,0.00013694736],"study_design_scores_gemma":[0.0017382422,0.00008449555,0.0057724514,0.000021933845,0.00006931737,0.000080623,0.00017487378,0.9739717,0.01735695,0.00062156667,0.000010189364,0.00009762604],"about_ca_topic_score_codex":0.000007334236,"about_ca_topic_score_gemma":0.0000018439351,"teacher_disagreement_score":0.41252255,"about_ca_system_score_codex":0.000051272895,"about_ca_system_score_gemma":0.000024141986,"threshold_uncertainty_score":0.31724963},"labels":[],"label_agreement":null},{"id":"W2003552601","doi":"10.1016/s1352-2310(02)00464-8","title":"Water flume study of the enhancement of buoyant rise in pairs of merging plumes","year":2002,"lang":"en","type":"article","venue":"Atmospheric Environment","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":35,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Waterloo","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Plume; Perpendicular; Stack (abstract data type); Mechanics; Flume; Panache; Vortex; Geology; Meteorology; Flow (mathematics); Environmental science; Atmospheric sciences; Physics; Geometry","score_opus":0.004981904693543701,"score_gpt":0.16114249541334214,"score_spread":0.15616059071979843,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2003552601","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99712807,0.0003697232,0.0017190845,0.000013725394,0.00011739656,0.00026779945,0.0000022015545,0.000007361043,0.00037461676],"genre_scores_gemma":[0.9978089,0.00038983935,0.0015783713,0.000003139066,0.000008095841,0.00002221731,4.6503405e-7,0.000020042162,0.00016893038],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99901617,0.000025847474,0.00041838305,0.00012346641,0.00024527492,0.00017084055],"domain_scores_gemma":[0.9995396,0.000018460163,0.000064245,0.0003533668,0.000004303509,0.000019984314],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012057801,0.00012334579,0.000238031,0.000003280821,0.000016568049,0.0000017157878,0.0001825009,0.00003277038,0.000468712],"category_scores_gemma":[0.0000034442178,0.00008407263,0.000050264214,0.00006667716,0.000047604182,0.000022464996,0.00010344905,0.00008598877,0.000005388059],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000004000951,0.0006066977,0.015575004,0.00006759421,0.000070944065,0.0000022332838,0.003904678,0.94107705,0.03668897,0.000008405976,0.000036300273,0.0019580924],"study_design_scores_gemma":[0.0009699914,0.00033870392,0.021566514,0.000078398254,0.00007694732,5.3257344e-7,0.0019808034,0.9425108,0.031598765,0.00004430894,0.0005871392,0.00024708806],"about_ca_topic_score_codex":0.000052338728,"about_ca_topic_score_gemma":0.000014224987,"teacher_disagreement_score":0.0059915096,"about_ca_system_score_codex":0.00007058678,"about_ca_system_score_gemma":0.0000012029433,"threshold_uncertainty_score":0.5132068},"labels":[],"label_agreement":null},{"id":"W2003839931","doi":"10.2514/6.2011-2918","title":"DNS of fully turbulent jet flows in flight conditions including a canonical nozzle","year":2011,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":16,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"General Fusion (Canada)","funders":"Engineering and Physical Sciences Research Council; Royal Academy of Engineering","keywords":"Nozzle; Turbulence; Jet (fluid); Mechanics; Physics; Aerospace engineering; Statistical physics; Computer science; Thermodynamics; Engineering","score_opus":0.025899926272061297,"score_gpt":0.23632031987312993,"score_spread":0.21042039360106862,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2003839931","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.92757875,0.000054000488,0.010978045,0.000038256192,0.00028359843,0.0001277669,0.00003477073,0.000112538364,0.060792267],"genre_scores_gemma":[0.9934822,0.000033961653,0.006228914,0.00002809412,0.000034915334,0.000016029342,0.0000123363425,0.000022269996,0.00014130704],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99925935,0.00000897793,0.00029242912,0.00011998966,0.000102355014,0.00021688607],"domain_scores_gemma":[0.9996579,0.00003771979,0.00002037429,0.00019170062,0.000030307738,0.00006199522],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00010162694,0.000117107615,0.00018158501,0.0000956926,0.000026927499,0.0000063614207,0.0001483309,0.00008160996,0.0006539791],"category_scores_gemma":[0.000019725527,0.000107653424,0.00005115238,0.00014438173,0.000029026167,0.00005554262,0.000053326665,0.00016014396,0.000026157672],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00006585466,0.0013079863,0.02050584,0.0007062068,0.00045718558,0.00047002686,0.00788219,0.47906324,0.206488,0.2626246,0.018174205,0.0022546654],"study_design_scores_gemma":[0.0005640097,0.00005935506,0.00883701,0.000085091524,0.000029186522,0.000016731972,0.00017871086,0.9794138,0.0062621036,0.0026971053,0.0014799616,0.00037694644],"about_ca_topic_score_codex":0.00014235603,"about_ca_topic_score_gemma":0.0013117085,"teacher_disagreement_score":0.50035053,"about_ca_system_score_codex":0.000068687434,"about_ca_system_score_gemma":0.000025851008,"threshold_uncertainty_score":0.71606123},"labels":[],"label_agreement":null},{"id":"W2003954837","doi":"10.1115/pvp2013-97141","title":"The Effect of Fluid-Resonant Coupling in High-Speed Impinging Planar Jet Flows","year":2013,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"","keywords":"Nozzle; Mach number; Jet (fluid); Mechanics; Oscillation (cell signaling); Planar; Coupling (piping); Physics; Excited state; Flow visualization; Materials science; Flow (mathematics); Atomic physics; Chemistry; Thermodynamics","score_opus":0.003414324529992298,"score_gpt":0.19113077011909538,"score_spread":0.18771644558910308,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2003954837","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99163043,0.0003094888,0.0063979174,0.00004690784,0.00043330638,0.00027040724,0.0000046523,0.00010401679,0.00080289395],"genre_scores_gemma":[0.9990079,0.000111465015,0.00069978164,0.0000074707655,0.00006255808,0.000017044169,0.0000050496064,0.000032799577,0.0000559507],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991156,0.000011345942,0.00029251797,0.00012010713,0.0001403311,0.00032010078],"domain_scores_gemma":[0.99924755,0.00042469872,0.000023905493,0.00023848352,0.000021185871,0.00004417843],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000354676,0.00015858417,0.00022084666,0.00006119179,0.00006257875,0.00004252862,0.00021205391,0.00006860558,0.000044080985],"category_scores_gemma":[0.000055127603,0.000098471515,0.00004889255,0.00013849202,0.00002439532,0.00006131303,0.00003502617,0.00017368517,0.00003533443],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000082528495,0.000006007391,0.004788901,0.00009855603,0.0000383831,0.0000055977225,0.000055900702,0.9016263,0.08735348,0.0012293875,0.00082085805,0.0039683636],"study_design_scores_gemma":[0.00030004294,0.00003841335,0.0025872947,0.000048783084,0.000007504487,0.000001104721,0.000030906926,0.99260515,0.0039888653,0.00013600866,0.0001303652,0.0001255633],"about_ca_topic_score_codex":0.00025860732,"about_ca_topic_score_gemma":0.00014863735,"teacher_disagreement_score":0.09097884,"about_ca_system_score_codex":0.000053274976,"about_ca_system_score_gemma":0.000005594019,"threshold_uncertainty_score":0.40155518},"labels":[],"label_agreement":null},{"id":"W2004306531","doi":"10.1115/1.2388995","title":"Acoustic Excitation by Flow in T-Junctions","year":2006,"lang":"en","type":"article","venue":"Journal of Pressure Vessel Technology","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":13,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"","keywords":"Strouhal number; Piping; Amplitude; Pipe flow; Flow (mathematics); Physics; Mechanics; Dimensionless quantity; Acoustic resonance; Open-channel flow; Turbulence; Resonance (particle physics); Acoustics; Optics; Atomic physics; Thermodynamics; Reynolds number","score_opus":0.0024690920330710984,"score_gpt":0.18706301973802428,"score_spread":0.18459392770495317,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2004306531","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.41238397,0.0063541643,0.57613623,0.0007845587,0.0020754603,0.00014826217,0.000036184014,0.0002657004,0.0018154889],"genre_scores_gemma":[0.99385065,0.00017433683,0.0056453953,0.000008152307,0.000118701486,0.000004304497,0.000003671485,0.000022279206,0.00017250133],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99924004,0.000010172629,0.00037810975,0.00007585612,0.00011983785,0.00017595357],"domain_scores_gemma":[0.9996288,0.000036801906,0.00009601959,0.0001241338,0.000092538605,0.000021698765],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00013527738,0.00010387331,0.00019468217,0.0004205101,0.000027625914,0.000015789157,0.00019202093,0.00021705362,0.000021892247],"category_scores_gemma":[0.000059573274,0.00010118385,0.000037745936,0.00037627737,0.00004598531,0.00010766185,0.000017479548,0.00045020413,0.000004068938],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000005444582,0.00007325738,0.0008676889,0.000046922734,0.000043674103,0.00003388166,0.000020085705,0.850756,0.10629998,0.0011700956,0.038581204,0.0021017848],"study_design_scores_gemma":[0.0010881778,0.00014157878,0.0036913122,0.00011179352,0.00015150961,0.00019401284,0.00016582293,0.90086615,0.002126718,0.034668315,0.05645805,0.0003365484],"about_ca_topic_score_codex":0.0000039653464,"about_ca_topic_score_gemma":0.000024193458,"teacher_disagreement_score":0.5814667,"about_ca_system_score_codex":0.000041330302,"about_ca_system_score_gemma":0.000015518066,"threshold_uncertainty_score":0.41261575},"labels":[],"label_agreement":null},{"id":"W2004998459","doi":"10.1115/fedsm-icnmm2010-30043","title":"Non-Stationary Signal Analysis of the von Ka´rma´n Vortex Shedding in the Wake of a Fluttering Airfoil","year":2010,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université Laval; Royal Military College of Canada; Carleton University","funders":"Natural Sciences and Engineering Research Council of Canada; Canada Research Chairs; U.S. Department of Defense","keywords":"Hilbert–Huang transform; Vortex shedding; Airfoil; Strouhal number; Wake; Instantaneous phase; Angle of attack; Hilbert spectral analysis; Reynolds number; Mathematics; Mathematical analysis; Hilbert transform; Harmonic; Acoustics; Kármán vortex street; Fourier transform; Physics; Aerodynamics; Computer science; Mechanics; Spectral density; Energy (signal processing); Filter (signal processing); Turbulence; Statistics","score_opus":0.003847182294078265,"score_gpt":0.2026499710109816,"score_spread":0.19880278871690332,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2004998459","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.970022,0.000008804418,0.02462071,0.000045377437,0.00016519151,0.0000744043,0.000014370027,0.000014764452,0.0050343354],"genre_scores_gemma":[0.9981555,0.0000064979545,0.001697689,0.000030650255,0.000029889005,0.000006178887,0.0000062308613,0.000011805052,0.000055557633],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993005,0.000011631324,0.00028131707,0.000089603775,0.00018936871,0.00012759872],"domain_scores_gemma":[0.99951994,0.00011441503,0.00004638595,0.0002699689,0.000034688575,0.000014618321],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002871217,0.000090222136,0.00016629549,0.00012846963,0.000032282347,0.000011046636,0.0002980683,0.000051686548,0.00017623644],"category_scores_gemma":[0.000015657855,0.000056002893,0.00011204872,0.0006006971,0.000040998544,0.000044370096,0.000043864336,0.000198597,0.0000016325145],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000022285171,0.000027306514,0.01986975,0.000043968277,0.00017761865,0.0000017146451,0.00079403346,0.7056311,0.27092853,0.001252803,0.000067032764,0.0012038997],"study_design_scores_gemma":[0.000067780675,0.000004920241,0.10379173,0.0000113245505,0.00009930552,8.8231764e-7,0.0002068262,0.8945518,0.0010397043,0.00013202189,0.0000303886,0.00006332393],"about_ca_topic_score_codex":0.00006208944,"about_ca_topic_score_gemma":0.0005678615,"teacher_disagreement_score":0.26988885,"about_ca_system_score_codex":0.000012368433,"about_ca_system_score_gemma":0.000010378118,"threshold_uncertainty_score":0.22837317},"labels":[],"label_agreement":null},{"id":"W2006737535","doi":"10.1115/pvp2013-97149","title":"Effect of Upstream Edge Geometry on the Trapped Mode Resonance of Ducted Cavities","year":2013,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":11,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"","keywords":"Resonance (particle physics); Upstream (networking); Acoustic resonance; Excitation; Enhanced Data Rates for GSM Evolution; Rotational symmetry; Physics; Vortex; Wavelength; Optics; Amplitude; Materials science; Geometry; Atomic physics; Mechanics; Engineering; Telecommunications","score_opus":0.003945775631665407,"score_gpt":0.19891714268342778,"score_spread":0.19497136705176238,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2006737535","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98649997,0.00011571226,0.001272974,0.000021706208,0.00013238098,0.00018281551,0.000023836239,0.000054424854,0.011696213],"genre_scores_gemma":[0.9990935,0.000052280993,0.00022453406,0.000010239987,0.000027511554,0.000013582204,0.000002990261,0.000018706023,0.0005566527],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995037,0.000020746405,0.00016179825,0.00007315699,0.00011169705,0.0001289074],"domain_scores_gemma":[0.9993424,0.0003285029,0.000024921803,0.0002539011,0.000030876512,0.000019443718],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000109743996,0.000105223626,0.00016990255,0.000043599786,0.000018786486,0.0000066615953,0.00014983262,0.000050347022,0.00015230954],"category_scores_gemma":[0.000047099697,0.00006340352,0.000051533854,0.00012578936,0.000055925153,0.000028709113,0.000016698752,0.00010406561,0.000012230775],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00010254212,0.00021736656,0.003240322,0.001616841,0.0003468028,0.00000409482,0.0009534969,0.45977142,0.36055788,0.05136966,0.028193016,0.09362654],"study_design_scores_gemma":[0.00031327244,0.000264092,0.0028279305,0.000092437236,0.000023726938,9.841906e-7,0.000085267144,0.79071283,0.20460342,0.00072802376,0.00017067372,0.00017733159],"about_ca_topic_score_codex":0.00009339706,"about_ca_topic_score_gemma":0.000007738046,"teacher_disagreement_score":0.3309414,"about_ca_system_score_codex":0.000013095461,"about_ca_system_score_gemma":0.00000398771,"threshold_uncertainty_score":0.25855204},"labels":[],"label_agreement":null},{"id":"W2006993279","doi":"10.1121/1.4805286","title":"Industrial fan noise control using flow obstructions","year":2013,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"Institut de recherche Robert-Sauvé en santé et en sécurité du travail; Soft dB (Canada); Université de Sherbrooke","funders":"","keywords":"Duct (anatomy); Acoustics; Noise (video); Noise control; Airflow; Environmental science; Computer science; Noise reduction; Physics; Engineering; Mechanical engineering","score_opus":0.012573815690862834,"score_gpt":0.21305007012527172,"score_spread":0.2004762544344089,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2006993279","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.14706346,0.00012842943,0.85023594,0.0010236152,0.001204308,0.00017610413,0.000024730132,0.000020995974,0.00012244497],"genre_scores_gemma":[0.95310587,0.00012652,0.045863517,0.00025547875,0.0006018902,0.0000010456428,2.37031e-7,0.000024674524,0.00002075234],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99885947,0.00006096649,0.0004516898,0.00005325603,0.00033558684,0.00023903835],"domain_scores_gemma":[0.9989075,0.00035249718,0.00022426946,0.00025237259,0.0001731142,0.00009023588],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002535995,0.00013834541,0.00029326993,0.000014730208,0.00017178606,0.000026208263,0.0005002836,0.00010230315,0.00011057256],"category_scores_gemma":[0.0001547908,0.000076990356,0.00034881604,0.00021233785,0.00039912382,0.00009199229,0.00006935234,0.00070370035,0.0000046114706],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000101496025,0.000025259409,0.00006610116,0.000011809469,0.00020047909,2.4233793e-7,0.00015741136,0.9298637,0.04750634,0.0000029094504,0.013287086,0.00886851],"study_design_scores_gemma":[0.00041357504,0.00004539706,0.0003481469,0.000036879377,0.00027900754,0.00003831387,0.00060186716,0.99710023,0.00016767265,0.0005810256,0.00029636486,0.0000915347],"about_ca_topic_score_codex":0.000038471233,"about_ca_topic_score_gemma":2.1647794e-7,"teacher_disagreement_score":0.80604243,"about_ca_system_score_codex":0.00009447109,"about_ca_system_score_gemma":0.000049166134,"threshold_uncertainty_score":0.31395757},"labels":[],"label_agreement":null},{"id":"W2007314459","doi":"10.1063/1.3103948","title":"A strategy to eliminate all nonlinear effects in constant-voltage hot-wire anemometry","year":2009,"lang":"en","type":"article","venue":"Review of Scientific Instruments","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":12,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Queen's University","funders":"Agence Nationale de la Recherche","keywords":"Anemometer; Mechanics; Constant (computer programming); Physics; Harmonics; Voltage; Differential equation; Nonlinear system; Control theory (sociology); Turbulence; Mathematical analysis; Mathematics; Computer science","score_opus":0.010310755662605675,"score_gpt":0.2567887275696573,"score_spread":0.24647797190705165,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2007314459","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9894486,0.004203202,0.00034764485,0.00004515308,0.0010087134,0.0007710418,0.00007336771,0.00006137961,0.0040409076],"genre_scores_gemma":[0.9921819,0.0045796228,0.0027678106,0.00025090948,0.000023121991,0.000009885742,0.000045218643,0.000018070756,0.00012348116],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99837923,0.000023454422,0.0005217337,0.00031080798,0.00037245828,0.00039228657],"domain_scores_gemma":[0.99929786,0.000025262716,0.00007197626,0.00040554747,0.00006735811,0.00013202422],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000631119,0.00020559218,0.00042106665,0.00025956065,0.00004565495,0.000059744598,0.00034326862,0.00006526914,0.000039062677],"category_scores_gemma":[0.00008621026,0.00019618451,0.00008026654,0.0009415991,0.00006543618,0.00011968644,0.00004588299,0.00018110851,0.000063578904],"study_design_candidate":"design_other","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000009197967,0.00020636318,0.00023593,0.010975787,0.00003201924,0.00007614302,0.00010359971,0.0013619825,0.053309433,0.0011807274,0.001813269,0.93069553],"study_design_scores_gemma":[0.004870207,0.0019846305,0.016503152,0.12357395,0.00046174953,0.00012606586,0.00023536486,0.7553669,0.03619411,0.003543843,0.053039294,0.004100726],"about_ca_topic_score_codex":0.000002556358,"about_ca_topic_score_gemma":0.0000046675596,"teacher_disagreement_score":0.9265948,"about_ca_system_score_codex":0.00009671753,"about_ca_system_score_gemma":0.000034913384,"threshold_uncertainty_score":0.80001724},"labels":[],"label_agreement":null},{"id":"W2007765076","doi":"10.1002/cjce.22065","title":"An experimental study of dynamic jet behaviour in a scaled cold flow spray dryer model using PIV","year":2014,"lang":"en","type":"article","venue":"The Canadian Journal of Chemical Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":11,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Turbulence; Mechanics; Jet (fluid); Particle image velocimetry; Reynolds number; Flow (mathematics); Materials science; Physics","score_opus":0.0076936657480633375,"score_gpt":0.21694454616115982,"score_spread":0.20925088041309647,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2007765076","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9916191,0.00009246041,0.007927311,0.0000075641087,0.0002060067,0.00010645551,0.000008220415,0.00001405793,0.000018816243],"genre_scores_gemma":[0.99610555,5.646714e-7,0.0037570766,0.0000075604225,0.00007162846,0.0000027750268,0.000001167084,0.00005211142,0.0000015918152],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989561,0.00001558839,0.00043606394,0.00009628803,0.00018789069,0.00030806346],"domain_scores_gemma":[0.9993411,0.00003521014,0.00006116847,0.00021742334,0.00005190342,0.0002932253],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003204439,0.00017752852,0.00030422275,0.00018303368,0.00003193303,0.00003428947,0.0003628959,0.00008814978,0.000007898816],"category_scores_gemma":[0.00003720622,0.00015658767,0.00006335936,0.00015569324,0.00003247592,0.00010354096,0.0000146019265,0.00044552432,3.0709543e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00000280829,0.00003511008,0.00018642275,0.000008840415,0.000013481176,0.000010699716,0.00046376913,0.67676365,0.32246122,0.000023212384,0.0000029868343,0.000027800825],"study_design_scores_gemma":[0.0005135111,0.00006956812,0.00010458715,0.00006516572,0.00003092242,0.000023597102,0.0001053891,0.9774162,0.021488303,0.000020710953,0.0000014563016,0.00016057203],"about_ca_topic_score_codex":0.00033512275,"about_ca_topic_score_gemma":0.0010333366,"teacher_disagreement_score":0.3009729,"about_ca_system_score_codex":0.00038103564,"about_ca_system_score_gemma":0.000086229295,"threshold_uncertainty_score":0.638546},"labels":[],"label_agreement":null},{"id":"W2012078839","doi":"10.1061/(asce)hy.1943-7900.0000232","title":"Reynolds Number Effects on the Near-Exit Region of Turbulent Jets","year":2010,"lang":"en","type":"article","venue":"Journal of Hydraulic Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":20,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Windsor","funders":"","keywords":"Reynolds number; Vortex; Turbulence; Circulation (fluid dynamics); Physics; Jet (fluid); Mechanics; Vortex ring; Geometry; Classical mechanics; Mathematics","score_opus":0.004680115062672693,"score_gpt":0.19236062695255934,"score_spread":0.18768051188988666,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2012078839","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98499846,0.000103865954,0.010996426,0.0003780005,0.0017370402,0.00008902191,7.666701e-7,0.000049030576,0.001647379],"genre_scores_gemma":[0.99700665,0.00012568317,0.0022647837,0.000048965638,0.00047025408,0.0000026654027,3.976888e-7,0.000049649625,0.00003096468],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9990757,0.000010195481,0.000348105,0.0000759186,0.00027586447,0.00021420975],"domain_scores_gemma":[0.99914724,0.00030940628,0.00011461117,0.00027110561,0.00007117406,0.000086463784],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002894837,0.00017482007,0.00025498346,0.0001018751,0.000036069378,0.00003300158,0.00028851515,0.00010922995,0.000024906358],"category_scores_gemma":[0.00021941909,0.00012539151,0.00014687283,0.00020874514,0.000024426376,0.00007886175,0.000023397042,0.0008333829,0.000012282393],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000010765164,0.000030527914,0.00014476052,0.00018566055,0.00012079362,0.00014559529,0.00021535001,0.92955375,0.05955815,0.001602949,0.006251101,0.0021806222],"study_design_scores_gemma":[0.00055499893,0.00015780653,0.0025231703,0.00052292994,0.00007630455,0.0008949562,0.000023125793,0.9475964,0.02886165,0.00035010415,0.018088209,0.00035036952],"about_ca_topic_score_codex":0.0000014366805,"about_ca_topic_score_gemma":9.3803123e-7,"teacher_disagreement_score":0.0306965,"about_ca_system_score_codex":0.000030591284,"about_ca_system_score_gemma":0.000012760014,"threshold_uncertainty_score":0.51133174},"labels":[],"label_agreement":null},{"id":"W2012712473","doi":"10.2514/6.2005-212","title":"PIV Measurements on a Blowing Flap","year":2005,"lang":"en","type":"article","venue":"43rd AIAA Aerospace Sciences Meeting and Exhibit","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":9,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lockheed Martin (Canada)","funders":"","keywords":"Blowing up; Computer science; Mathematics; Geometry","score_opus":0.02268664566737334,"score_gpt":0.23446412103569123,"score_spread":0.2117774753683179,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2012712473","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.94065344,0.00050289946,0.00070944586,0.00053747185,0.0005443624,0.00010374349,0.0000031019372,0.00027896088,0.056666546],"genre_scores_gemma":[0.991726,0.00010429268,0.0073150704,0.00018216055,0.00028725705,0.0000065333356,0.0000010174367,0.00002422626,0.0003534861],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9984699,0.000020684272,0.00020457293,0.00035452732,0.00046294634,0.00048739588],"domain_scores_gemma":[0.9995569,0.000069779984,0.000037415917,0.00017347603,0.000031892298,0.00013054525],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0008846641,0.00020944394,0.0001811754,0.000083808285,0.00043568204,0.0001916459,0.00022577195,0.00007070079,0.00001915324],"category_scores_gemma":[0.00009611966,0.00018735361,0.000048821355,0.0002714079,0.00014857975,0.00016491883,0.00005789687,0.00019441944,0.000055942295],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000008897638,0.000059485,0.007451064,0.00008176523,0.000039635866,0.000006373477,0.001331698,0.86607754,0.09584104,0.0011362438,0.0041963127,0.023769936],"study_design_scores_gemma":[0.00082296896,0.00023875233,0.0015372825,0.0006734578,0.00004607439,0.00001643735,0.0007792798,0.96304965,0.021239104,0.00031210342,0.010257431,0.0010274606],"about_ca_topic_score_codex":0.000015643696,"about_ca_topic_score_gemma":0.000059410693,"teacher_disagreement_score":0.0969721,"about_ca_system_score_codex":0.00006319671,"about_ca_system_score_gemma":0.000020195712,"threshold_uncertainty_score":0.76400584},"labels":[],"label_agreement":null},{"id":"W2012734995","doi":"10.1115/1.3148188","title":"Flow-Acoustic Coupling in T-Junctions: Effect of T-Junction Geometry","year":2009,"lang":"en","type":"article","venue":"Journal of Pressure Vessel Technology","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":14,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"","keywords":"Acoustic resonance; Resonance (particle physics); Acoustics; Coupling (piping); Flow (mathematics); Oscillation (cell signaling); Bar (unit); Materials science; Mechanics; Physics; Chemistry; Atomic physics; Composite material","score_opus":0.003292655138912083,"score_gpt":0.2132499876618558,"score_spread":0.2099573325229437,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2012734995","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8852191,0.004372056,0.10822585,0.00013599209,0.0015698656,0.00013865257,0.0000045316033,0.00012692799,0.00020700641],"genre_scores_gemma":[0.99717623,0.000498772,0.002153679,0.0000066966777,0.00011982,0.0000025639586,0.0000010273983,0.000020013511,0.00002121191],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989058,0.000013796941,0.0005734716,0.000105828185,0.00018388698,0.00021721347],"domain_scores_gemma":[0.99934065,0.00009721378,0.000195461,0.00020768262,0.00012255882,0.00003645537],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00046535852,0.00016109174,0.00045550303,0.0009969376,0.000028051583,0.000010735967,0.00025320717,0.00032025235,0.000018066597],"category_scores_gemma":[0.00028647232,0.00014278988,0.00008412211,0.000764682,0.00005325017,0.00011936954,0.000021865428,0.0006994562,0.000001988376],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00003688998,0.00004540512,0.0012655106,0.00012674028,0.00007285324,0.000030137619,0.000013564051,0.9215411,0.07066319,0.00016193488,0.00045002316,0.0055926475],"study_design_scores_gemma":[0.0009274668,0.00077442185,0.002327912,0.00023829141,0.00019584667,0.00012946205,0.000048552232,0.98444813,0.007981534,0.0016877882,0.0010697003,0.000170876],"about_ca_topic_score_codex":0.0000011619462,"about_ca_topic_score_gemma":0.000002257762,"teacher_disagreement_score":0.1119571,"about_ca_system_score_codex":0.000051813677,"about_ca_system_score_gemma":0.000019123396,"threshold_uncertainty_score":0.5822803},"labels":[],"label_agreement":null},{"id":"W2013445241","doi":"10.1115/imece2006-15633","title":"CFD Simulation of Flow Tones From Grazing Flow Past a Deep Cavity","year":2006,"lang":"en","type":"article","venue":"Noise Control and Acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lockheed Martin (Canada)","funders":"","keywords":"Mechanics; Compressible flow; Flow (mathematics); Compressibility; Resonator; Acoustics; Large eddy simulation; Physics; Computational fluid dynamics; Geology; Optics; Meteorology; Turbulence","score_opus":0.0036621272559719522,"score_gpt":0.18615496610773535,"score_spread":0.1824928388517634,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2013445241","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.35943782,0.0004913859,0.63909245,0.000011956499,0.0003255593,0.00010696882,0.0002588008,0.00008625975,0.00018882047],"genre_scores_gemma":[0.98945856,0.00005214359,0.009837516,0.00002330486,0.0005059152,0.0000063187163,0.000064200074,0.000034974928,0.000017072725],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99910486,0.000013949682,0.00031555298,0.00017118089,0.00016358911,0.00023086477],"domain_scores_gemma":[0.99935186,0.00024985848,0.00005690004,0.00018101113,0.00009950499,0.000060842318],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00008346526,0.00019483286,0.000298194,0.000050857027,0.0000772171,0.000039735914,0.00008695332,0.00013136261,0.000011778016],"category_scores_gemma":[0.00004351589,0.00019067692,0.00006008,0.00008165824,0.00005074914,0.00007236377,0.00002348229,0.00014882082,0.0000033652848],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00001584158,0.000027445618,0.0018986496,0.00006961898,0.0000311903,0.000006730369,0.00004020576,0.9490219,0.041432086,0.00003472593,0.00006196615,0.0073596635],"study_design_scores_gemma":[0.0008370973,0.000017940038,0.019371122,0.000040808987,0.00013164255,8.313967e-7,0.000019916455,0.9779641,0.00006614327,0.0012854886,0.00006302369,0.00020189818],"about_ca_topic_score_codex":0.000055644585,"about_ca_topic_score_gemma":0.000065586624,"teacher_disagreement_score":0.63002074,"about_ca_system_score_codex":0.000029052819,"about_ca_system_score_gemma":0.000008086705,"threshold_uncertainty_score":0.7775579},"labels":[],"label_agreement":null},{"id":"W2013840503","doi":"10.1121/1.2934517","title":"Optimization problem for the automatic positioning of flow obstructions to control tonal fan noise","year":2008,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Lift (data mining); Microphone; Acoustics; Noise (video); Physics; Rotor (electric); Aeroacoustics; Control theory (sociology); Computer science; Sound pressure; Control (management)","score_opus":0.006319894899276266,"score_gpt":0.20845857554858344,"score_spread":0.20213868064930718,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2013840503","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0111718625,0.00009929129,0.98636943,0.0017470971,0.00024279824,0.00027253228,0.00004309379,0.000014645882,0.00003925514],"genre_scores_gemma":[0.6590144,0.00013582592,0.3404742,0.0002172527,0.00012371471,0.000004794135,6.3101743e-7,0.000015882884,0.0000133374915],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99900997,0.000035293848,0.0004463004,0.000048239737,0.00029572146,0.00016446756],"domain_scores_gemma":[0.9985361,0.0007485092,0.00022972956,0.00019076999,0.00024370698,0.000051192565],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00030168614,0.00010560952,0.00023619048,0.000014624785,0.00029533484,0.000009672449,0.00039708565,0.000045187473,0.000022226532],"category_scores_gemma":[0.00014114006,0.000055261276,0.00029955266,0.00019991763,0.00028359922,0.000049335955,0.00004181392,0.00024094485,4.5104198e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000019601692,0.000026753978,0.000011230368,0.000038089915,0.00018040708,1.0281887e-7,0.00063269335,0.9853672,0.007888807,0.000011029269,0.0035999846,0.0022241087],"study_design_scores_gemma":[0.00029831837,0.00010554401,0.0004028358,0.00006107158,0.00029495207,0.000048542566,0.0004567828,0.9977795,0.00016846006,0.0002702754,0.000049790535,0.00006394553],"about_ca_topic_score_codex":0.0000059820845,"about_ca_topic_score_gemma":2.3724542e-7,"teacher_disagreement_score":0.6478425,"about_ca_system_score_codex":0.00006148662,"about_ca_system_score_gemma":0.00004570224,"threshold_uncertainty_score":0.22715068},"labels":[],"label_agreement":null},{"id":"W2016729367","doi":"10.1007/s10652-014-9372-1","title":"Numerical modeling of $$30^{\\circ }$$ 30 ∘ and $$45{^\\circ }$$ 45 ∘ inclined dense turbulent jets in stationary ambient","year":2014,"lang":"en","type":"article","venue":"Environmental Fluid Mechanics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":74,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Ottawa","funders":"","keywords":"Turbulence; Turbulence modeling; Physics; Reynolds stress; Mechanics; Nonlinear system; Mixing (physics); Reynolds number; Computational fluid dynamics; Large eddy simulation","score_opus":0.006027475950138122,"score_gpt":0.18701975692598252,"score_spread":0.1809922809758444,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2016729367","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7353541,0.00024446333,0.26387623,0.000035549514,0.00017158825,0.00016862957,0.000030810133,0.00004252451,0.000076111086],"genre_scores_gemma":[0.99543154,0.0006331467,0.003641071,0.00007606649,0.00006586689,0.000018175358,0.00005761664,0.000059151334,0.000017339664],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9985858,0.00003844556,0.00045640158,0.0002949015,0.0003196083,0.00030481847],"domain_scores_gemma":[0.9994907,0.00006739617,0.000043078464,0.000263187,0.0000063944985,0.00012926485],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00026693087,0.00023312791,0.00027580818,0.00009883315,0.000052894757,0.000012957373,0.00014363525,0.00013512453,0.00012451438],"category_scores_gemma":[0.000043558088,0.00026194082,0.00005247701,0.00007782473,0.000025515259,0.00007601784,0.00011771408,0.0002394818,0.000029539555],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000010189679,0.000098546974,0.00007804783,0.000041525254,0.000018612043,0.0000081538865,0.00023693751,0.9175804,0.07898027,0.001264214,0.000029174756,0.0016538941],"study_design_scores_gemma":[0.00051802146,0.00008561222,0.00017344886,0.000037070196,0.000017354052,0.000009691316,0.00014098891,0.99402845,0.0020317803,0.002559947,0.0001414778,0.00025618615],"about_ca_topic_score_codex":0.000012535834,"about_ca_topic_score_gemma":0.0000019156923,"teacher_disagreement_score":0.26023516,"about_ca_system_score_codex":0.00025263178,"about_ca_system_score_gemma":0.000011301475,"threshold_uncertainty_score":0.99998325},"labels":[],"label_agreement":null},{"id":"W2017219384","doi":"10.1051/0004-6361:20011417","title":"An analysis of the vertical photospheric velocity field as observed by THEMIS","year":2002,"lang":"en","type":"article","venue":"Astronomy and Astrophysics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":16,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"National Research Council Canada","keywords":"Physics; Astrophysics; Vector field; Convection; Field (mathematics); Proper orthogonal decomposition; Photosphere; Basis (linear algebra); Telescope; Astronomy; Mechanics; Spectral line; Turbulence; Geometry","score_opus":0.006050266713851913,"score_gpt":0.17647907644960298,"score_spread":0.17042880973575106,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2017219384","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8775123,0.000043339656,0.12191367,0.000019437744,0.0000503678,0.00004099225,0.000026124579,0.000022536744,0.00037123438],"genre_scores_gemma":[0.99437994,0.000014754843,0.005499361,0.000024543568,0.000028048054,0.0000038393987,0.000010237307,0.000011028069,0.00002826038],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995004,0.000011310593,0.00013055168,0.00011955896,0.00008598815,0.00015222216],"domain_scores_gemma":[0.99962604,0.000033090928,0.000019330459,0.00024932588,0.000016195474,0.000055987206],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00002143588,0.000109979905,0.00016963453,0.000009572694,0.00005836406,0.000021332575,0.00016290198,0.000041030733,0.0001266539],"category_scores_gemma":[0.0000047086955,0.00008954116,0.00009046681,0.00020933038,0.000045803557,0.000061394654,0.00003155355,0.00013311386,0.0000023537564],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000020553001,0.00043798322,0.019226052,0.000046793717,0.0017639024,0.0000018168292,0.0006218004,0.37840486,0.11080105,0.0016418251,0.0010896141,0.48594376],"study_design_scores_gemma":[0.0001530645,0.00007276356,0.0063037463,0.000006656409,0.00033581522,2.166103e-7,0.00010546863,0.9805543,0.010860113,0.000064553,0.0013977354,0.00014558827],"about_ca_topic_score_codex":0.00002758215,"about_ca_topic_score_gemma":0.0000036375263,"teacher_disagreement_score":0.6021494,"about_ca_system_score_codex":0.000013166613,"about_ca_system_score_gemma":0.0000031594072,"threshold_uncertainty_score":0.36513826},"labels":[],"label_agreement":null},{"id":"W2017716875","doi":"10.1115/1.4023855","title":"Coherent Streamwise Vortex Structures in the Near-Field of the Three-Dimensional Wall Jet","year":2013,"lang":"en","type":"article","venue":"Journal of Fluids Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":18,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of New Brunswick","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Vorticity; Vortex; Physics; Jet (fluid); Turbulence; Particle image velocimetry; Mechanics; Reynolds number; Vortex ring; Vector field; Field (mathematics); Classical mechanics; Geometry; Mathematics","score_opus":0.004915615183658783,"score_gpt":0.19474570145178302,"score_spread":0.18983008626812423,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2017716875","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9932324,0.0005343724,0.0051192585,0.00017197184,0.00070061,0.00012229414,0.000003059965,0.000012544398,0.000103482336],"genre_scores_gemma":[0.99725145,0.000024466704,0.002521573,0.00004566824,0.00012566338,0.0000032625528,4.1355074e-7,0.000022013179,0.000005488672],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9990247,0.000012656079,0.00039520816,0.00005929886,0.00032092675,0.00018721598],"domain_scores_gemma":[0.9994365,0.00016424849,0.00006846614,0.00021149668,0.00007545566,0.00004383243],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020489423,0.00014851765,0.0002068011,0.000060529357,0.000028386468,0.000040276092,0.00040838146,0.000074171054,0.000068592286],"category_scores_gemma":[0.00007909737,0.00008313025,0.00012388112,0.00015250943,0.000019679735,0.00009455604,0.000039027993,0.0004884307,0.0000015648756],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000051984202,0.000016060156,0.0018284966,0.00005072729,0.000041936713,0.000008128918,0.00015726988,0.9698328,0.025261464,0.00043935087,0.0013520243,0.0010065945],"study_design_scores_gemma":[0.00028685248,0.000087012115,0.05305226,0.00013316695,0.000028959987,0.000048357797,0.000039249968,0.9437351,0.0015430648,0.000661458,0.00025167517,0.00013281398],"about_ca_topic_score_codex":0.000029491346,"about_ca_topic_score_gemma":0.000030541305,"teacher_disagreement_score":0.051223766,"about_ca_system_score_codex":0.000043659573,"about_ca_system_score_gemma":0.000023802093,"threshold_uncertainty_score":0.33899534},"labels":[],"label_agreement":null},{"id":"W2018867993","doi":"10.1121/1.2942545","title":"The Rotorcraft Noise Model (RNM)","year":2007,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lockheed Martin (Canada)","funders":"","keywords":"Noise (video); Computer science; Executable; Acoustics; Orientation (vector space); Terrain; Aerospace engineering; Geology; Physics; Engineering; Computer vision","score_opus":0.006926403830274158,"score_gpt":0.22378239463520203,"score_spread":0.21685599080492787,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2018867993","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.021986393,0.0004758374,0.9745802,0.0015028528,0.000514634,0.00012120959,0.000009415103,0.000021540685,0.0007878657],"genre_scores_gemma":[0.96019286,0.0014781998,0.037200987,0.00055537914,0.0003370854,8.392441e-7,1.581367e-7,0.00003445969,0.00020002064],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9985327,0.000034987646,0.00051424076,0.00005654944,0.0005166349,0.00034485327],"domain_scores_gemma":[0.99829924,0.00084083754,0.00022229819,0.0003871983,0.00015740567,0.000092998795],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0012562555,0.00015012806,0.00023284684,0.000009701313,0.00029694356,0.000021643571,0.00097165804,0.00007699475,0.000009269948],"category_scores_gemma":[0.000160418,0.000067414796,0.00040024568,0.00020300857,0.00057265343,0.000046534307,0.00014520598,0.00071814185,0.000003100949],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000035432862,0.000029712362,0.000015675478,0.000019274052,0.0001370233,6.7687023e-7,0.00036732605,0.94216776,0.02252314,0.00003361687,0.026463944,0.00820643],"study_design_scores_gemma":[0.000150162,0.000046640584,0.0001776668,0.000028760094,0.0001387647,0.000021398839,0.0006664217,0.9939763,0.00048730025,0.0018859127,0.0023300122,0.0000906499],"about_ca_topic_score_codex":0.0000062227023,"about_ca_topic_score_gemma":0.000001047933,"teacher_disagreement_score":0.9382065,"about_ca_system_score_codex":0.000094579234,"about_ca_system_score_gemma":0.00004567223,"threshold_uncertainty_score":0.3120009},"labels":[],"label_agreement":null},{"id":"W2019450211","doi":"10.1016/j.jfluidstructs.2003.08.018","title":"Aeroacoustical coupling in a ducted shallow cavity and fluid/structure effects on a steam line","year":2003,"lang":"en","type":"article","venue":"Journal of Fluids and Structures","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":57,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Atomic Energy of Canada Limited","keywords":"Mechanics; Piping; Acoustics; Boundary layer; Duct (anatomy); Aeroacoustics; Physics; Engineering; Sound pressure; Mechanical engineering","score_opus":0.0048373051518645835,"score_gpt":0.21130379430714266,"score_spread":0.20646648915527807,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2019450211","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.993934,0.0027813432,0.0024890208,0.000025050134,0.00057247607,0.00008763053,0.000013121526,0.000015635978,0.000081753664],"genre_scores_gemma":[0.995874,0.0006334687,0.0031954008,0.000047884398,0.0002159077,6.5560016e-7,0.0000013237503,0.000025310916,0.0000060466277],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9990438,0.000025043646,0.00035368672,0.00014089065,0.0002076993,0.00022886854],"domain_scores_gemma":[0.9994867,0.00015471567,0.000049884355,0.00010614156,0.00005898549,0.00014357782],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018638608,0.00021408597,0.00037385552,0.00014611804,0.000058967722,0.000057801266,0.00008174889,0.00016615956,0.00001437087],"category_scores_gemma":[0.0002123668,0.0001643843,0.000045177283,0.000113340364,0.000050998373,0.00006713075,0.000016530214,0.00055798463,1.1331624e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0001802528,0.00005363283,0.007232185,0.00081338396,0.00020945541,0.0005563266,0.0004961275,0.5360462,0.43564138,0.007438685,0.00047534058,0.010857025],"study_design_scores_gemma":[0.0037653334,0.00093702436,0.085530594,0.0004624448,0.00018788398,0.0010405498,0.00020081252,0.8746107,0.010922005,0.021146595,0.00042474928,0.00077127776],"about_ca_topic_score_codex":0.0000025783374,"about_ca_topic_score_gemma":0.000015602514,"teacher_disagreement_score":0.42471936,"about_ca_system_score_codex":0.00004767625,"about_ca_system_score_gemma":0.000023138778,"threshold_uncertainty_score":0.6703397},"labels":[],"label_agreement":null},{"id":"W2019506359","doi":"10.4271/2013-01-0856","title":"Prediction of HVAC System Aero/Acoustic Noise Generation and Propagation using CFD","year":2013,"lang":"en","type":"article","venue":"SAE technical papers on CD-ROM/SAE technical paper series","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":6,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Chrysler (Canada)","funders":"","keywords":"Computational fluid dynamics; HVAC; Acoustics; Noise (video); Computer science; Aeroacoustics; Aerospace engineering; Engineering; Physics; Mechanical engineering; Artificial intelligence; Air conditioning; Sound pressure","score_opus":0.01334405280846897,"score_gpt":0.20647512457191045,"score_spread":0.19313107176344146,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2019506359","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99004525,0.0002663848,0.00031065164,0.00013668576,0.0005081343,0.0012313557,0.00009002581,0.0018473169,0.0055641998],"genre_scores_gemma":[0.99341536,0.00021167344,0.0055859266,0.00006411636,0.00026607222,0.00021605942,0.000067106994,0.00011557046,0.000058113066],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.9973522,0.00006436138,0.0009557551,0.0005884627,0.000550804,0.00048846286],"domain_scores_gemma":[0.9986552,0.00012576231,0.00016653267,0.00067808124,0.00016867217,0.00020576162],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00034531974,0.0004894965,0.00058531517,0.00017192685,0.00023245993,0.00010039152,0.00030768182,0.0005982468,0.000074729534],"category_scores_gemma":[0.00020490888,0.00044614048,0.00014678812,0.00039525767,0.00037086647,0.00049237366,0.0001418327,0.00060445274,0.000021071683],"study_design_candidate":"observational","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000018766466,0.00006710472,0.00009652379,0.00027413166,0.00003187161,0.000004903727,0.00001691432,0.014540598,0.9803678,0.002728958,0.000483875,0.0013685824],"study_design_scores_gemma":[0.00064813497,0.0006652345,0.98718286,0.0005584484,0.00022004193,0.00012191324,0.00015392134,0.008000023,0.0008235681,0.000536815,0.00038741925,0.000701605],"about_ca_topic_score_codex":0.000041947427,"about_ca_topic_score_gemma":0.004224936,"teacher_disagreement_score":0.98708636,"about_ca_system_score_codex":0.00036972793,"about_ca_system_score_gemma":0.00003806438,"threshold_uncertainty_score":0.999799},"labels":[],"label_agreement":null},{"id":"W2019803129","doi":"10.1615/ichmt.2009.turbulheatmasstransf.670","title":"An experimental study of a plane turbulent wall jet using LDA","year":2009,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":6,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Saskatchewan","funders":"","keywords":"Turbulence; Jet (fluid); Mechanics; Scaling; Physics; Reynolds number; Plane (geometry); Power law; Momentum (technical analysis); Classical mechanics; Geometry; Mathematics","score_opus":0.014854069348882054,"score_gpt":0.25986228329737426,"score_spread":0.2450082139484922,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2019803129","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99643254,0.000047998106,0.0021049804,0.0000036623196,0.00009024779,0.0001258562,0.0000022409065,0.00009811094,0.0010943827],"genre_scores_gemma":[0.99707276,0.000002640286,0.0028274327,0.000025235826,0.000038742583,0.0000013044183,0.000004494579,0.000013280623,0.000014138372],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99949086,0.00000670269,0.00015715322,0.00010067324,0.00011595794,0.00012864685],"domain_scores_gemma":[0.9997391,0.000005833117,0.000014063361,0.0001830211,0.000011684464,0.000046275374],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000042770767,0.00010139516,0.00012501294,0.000034964552,0.000022533986,0.000013999656,0.00010418639,0.000031379124,0.000068543915],"category_scores_gemma":[0.0000010564032,0.0000902075,0.000018336836,0.000047954814,0.00000621145,0.000051143696,0.00000861623,0.00006153344,0.0000021333726],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000011906113,0.0014741994,0.0004946857,0.000009542677,0.000032413227,0.000031680254,0.002085724,0.6674001,0.32755935,0.0003041857,0.00015420148,0.000441983],"study_design_scores_gemma":[0.00038553862,0.00062812335,0.00081090204,0.00000697004,0.000011861658,0.000006833436,0.0012596811,0.9878328,0.008855772,0.000034394663,0.000021194193,0.00014594833],"about_ca_topic_score_codex":0.00004675118,"about_ca_topic_score_gemma":0.000018282899,"teacher_disagreement_score":0.32043266,"about_ca_system_score_codex":0.00003747167,"about_ca_system_score_gemma":0.0000033064737,"threshold_uncertainty_score":0.3678555},"labels":[],"label_agreement":null},{"id":"W2019952258","doi":"10.2514/2.1798","title":"Acoustic Noise-Source Identification in Aircraft-Based Atmospheric Temperature Measurements","year":2002,"lang":"en","type":"article","venue":"AIAA Journal","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Calgary","funders":"Air Force Research Laboratory","keywords":"Acoustics; Environmental science; Noise (video); Aircraft noise; Aerospace engineering; Aeroacoustics; Identification (biology); Meteorology; Remote sensing; Atmospheric sciences; Physics; Sound pressure; Computer science; Geology; Noise reduction; Engineering","score_opus":0.013054805439291044,"score_gpt":0.1997052368643204,"score_spread":0.18665043142502935,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2019952258","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.88793546,0.0011758032,0.10795092,0.0002111255,0.0015165106,0.00015256274,0.00000550158,0.00014955745,0.0009025503],"genre_scores_gemma":[0.9969895,0.00013303434,0.0021678982,0.00009757467,0.00023708891,0.000007232898,0.0000038190806,0.000049255148,0.0003146069],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9987994,0.00003243779,0.00037791132,0.00014110382,0.0003444092,0.0003047522],"domain_scores_gemma":[0.9995185,0.000028561624,0.0000637413,0.00019736207,0.00008356,0.000108253334],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002873893,0.00016981209,0.00015555395,0.000041920157,0.00011889521,0.00013824696,0.00022423569,0.00011433786,0.00030413806],"category_scores_gemma":[0.00006574597,0.00016891303,0.00006760392,0.00029689242,0.00002070254,0.0001384015,0.000011458625,0.00056322356,0.00008767275],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000002786338,0.00004845377,0.0020190298,0.000025853937,0.000018952243,0.000022211056,0.00009052956,0.9158608,0.075046904,0.0000025312634,0.0031955945,0.0036664067],"study_design_scores_gemma":[0.0005545944,0.000020943142,0.006818753,0.000081277365,0.00002615684,0.000041947907,0.00004369583,0.99099934,0.00051525375,0.00006420599,0.00061196304,0.00022186014],"about_ca_topic_score_codex":0.0000021989295,"about_ca_topic_score_gemma":0.000016712218,"teacher_disagreement_score":0.10905402,"about_ca_system_score_codex":0.00022719115,"about_ca_system_score_gemma":0.000014169524,"threshold_uncertainty_score":0.68880737},"labels":[],"label_agreement":null},{"id":"W2021184643","doi":"10.2514/1.j051784","title":"Effect of Rotor Shielding on Fan-Outlet Guide Vanes Broadband Noise Prediction","year":2013,"lang":"en","type":"article","venue":"AIAA Journal","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":20,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Sound power; Acoustics; Rotor (electric); Duct (anatomy); Cascade; Stator; Electromagnetic shielding; Noise (video); Scattering; Physics; Spectral density; Sound pressure; Mechanics; Optics; Engineering; Computer science; Telecommunications","score_opus":0.0028798829937086404,"score_gpt":0.2058154760300642,"score_spread":0.20293559303635555,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2021184643","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97782344,0.000112704445,0.015993379,0.000038881404,0.001245854,0.00017519323,0.000010077836,0.000054360036,0.0045460984],"genre_scores_gemma":[0.99857986,0.0001341174,0.0005223507,0.000020162239,0.0005093922,0.000010369527,0.0000025767313,0.000028245631,0.00019293332],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992163,0.00003137648,0.00028627756,0.00008132987,0.00019207505,0.00019261878],"domain_scores_gemma":[0.9995343,0.00013714758,0.00006083375,0.00012953869,0.000050996703,0.00008715014],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00029463923,0.00013032503,0.00017253617,0.00008481554,0.00007353698,0.000058214868,0.00012812133,0.00007876261,0.00022614172],"category_scores_gemma":[0.00008635932,0.000104036415,0.000079074925,0.00006257115,0.000018653991,0.00012961119,0.000015989583,0.0003185568,0.000039671126],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00006469748,0.000062925006,0.01037519,0.00036940875,0.00027047662,0.000040540843,0.0004144835,0.4541085,0.409788,0.00020835653,0.046121113,0.0781763],"study_design_scores_gemma":[0.002215199,0.0018349688,0.021140577,0.0007387316,0.00016631473,0.00026393312,0.000090455665,0.91065985,0.056606654,0.0009275304,0.004779329,0.0005764431],"about_ca_topic_score_codex":0.00000979883,"about_ca_topic_score_gemma":0.0000012047211,"teacher_disagreement_score":0.45655137,"about_ca_system_score_codex":0.000056297133,"about_ca_system_score_gemma":0.000007564252,"threshold_uncertainty_score":0.4242482},"labels":[],"label_agreement":null},{"id":"W2021190193","doi":"10.1121/1.1364489","title":"Spectral broadening of sound scattered by advecting atmospheric turbulence","year":2001,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":24,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Institute for Microstructural Sciences","funders":"Army Research Laboratory; Army Research Office","keywords":"Physics; Homogeneous isotropic turbulence; Turbulence; Computational physics; Scattering; Optics; Isotropy; SIGNAL (programming language); Acoustics; Detector; Large eddy simulation; Eddy; Amplitude; Mechanics; Direct numerical simulation; Computer science","score_opus":0.006364337627750836,"score_gpt":0.21457011831366782,"score_spread":0.20820578068591697,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2021190193","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.43928435,0.00082027016,0.5587609,0.00047285907,0.00031374785,0.00006720938,0.0000075636676,0.000017181814,0.0002559487],"genre_scores_gemma":[0.9545445,0.0010111133,0.044016924,0.0001632512,0.00017847499,3.9308864e-7,2.793878e-7,0.000027733195,0.000057363242],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99861944,0.000050641658,0.000547935,0.000073684314,0.00041710454,0.0002912259],"domain_scores_gemma":[0.9987731,0.00040633182,0.0003793129,0.00026188308,0.00011043738,0.00006895724],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003848605,0.00015865054,0.00034919856,0.0000048386337,0.0001208877,0.000013951053,0.00069033145,0.00006847685,0.00005457801],"category_scores_gemma":[0.00012122036,0.00009622493,0.00034578957,0.0003295009,0.00043502447,0.00007228478,0.000104437066,0.0005861849,0.0000013979313],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000039531224,0.0000677769,0.0005878762,0.00007771228,0.0002657656,0.0000015666229,0.00091565406,0.8774932,0.100834474,0.0000031793636,0.01234873,0.007364521],"study_design_scores_gemma":[0.00023790788,0.000111548274,0.00067413936,0.00011371263,0.0002020044,0.00010657054,0.0013826607,0.99507654,0.0009843652,0.00072016445,0.00025814274,0.00013227448],"about_ca_topic_score_codex":0.000022910259,"about_ca_topic_score_gemma":3.7834212e-7,"teacher_disagreement_score":0.5152601,"about_ca_system_score_codex":0.00008065076,"about_ca_system_score_gemma":0.000026704356,"threshold_uncertainty_score":0.3923939},"labels":[],"label_agreement":null},{"id":"W2023313049","doi":"10.1115/gt2007-28334","title":"Determination of CFD Turbulence Scales for Lobed Mixer Jet Noise Prediction","year":2007,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Concordia University; National Aeronautics and Space Administration","keywords":"Turbulence; Jet noise; Jet (fluid); Nozzle; Noise (video); Aeroacoustics; Turbofan; Acoustics; Jet engine; Mixing (physics); Physics; Mechanics; Flow (mathematics); Engineering; Mechanical engineering; Aerospace engineering; Computer science; Sound pressure","score_opus":0.006648220816770264,"score_gpt":0.2222267724184584,"score_spread":0.21557855160168812,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2023313049","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.29717192,0.000025319354,0.7002638,0.0000050768544,0.00030239834,0.00011078632,0.000027834096,0.00007735938,0.002015509],"genre_scores_gemma":[0.9563354,0.000021829701,0.043372992,0.000007841167,0.00008297137,0.000006818858,0.000016958542,0.000014233364,0.0001409544],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995329,0.0000017873764,0.000180304,0.00007786687,0.000083777966,0.00012338886],"domain_scores_gemma":[0.99972254,0.00006753975,0.000021433741,0.000096877375,0.00006318284,0.000028428869],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001724728,0.00006906696,0.00007728022,0.000049481478,0.000020878651,0.000006615537,0.000061614315,0.000062667204,0.000013314015],"category_scores_gemma":[0.000032526557,0.00006387193,0.000034573237,0.00005975314,0.000018860808,0.000060992934,0.000008779291,0.000040264706,0.0000022913352],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00011118103,0.00023732112,0.009040072,0.0014200497,0.000081167345,0.0000073774563,0.00067242084,0.20856038,0.42866418,0.010065143,0.004938542,0.33620217],"study_design_scores_gemma":[0.00016626467,0.000029777391,0.005151715,0.000019074254,0.000011461738,0.000001322474,0.000027575185,0.97750944,0.01608681,0.0006312552,0.00028993463,0.00007538018],"about_ca_topic_score_codex":0.0000028407653,"about_ca_topic_score_gemma":0.000037803537,"teacher_disagreement_score":0.76894903,"about_ca_system_score_codex":0.000029902238,"about_ca_system_score_gemma":0.0000029430948,"threshold_uncertainty_score":0.26046216},"labels":[],"label_agreement":null},{"id":"W2023958933","doi":"10.1121/1.1528591","title":"Application of an acoustic noise removal method to aircraft-based atmospheric temperature measurements","year":2003,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Calgary","funders":"Air Force Research Laboratory","keywords":"Turbulence; Noise (video); Environmental science; Range (aeronautics); Clear-air turbulence; Atmospheric temperature; Acoustics; Atmospheric wave; Magnitude (astronomy); Standard deviation; Wavenumber; Atmospheric sciences; Meteorology; Physics; Materials science; Optics; Gravity wave; Mathematics; Wave propagation; Computer science","score_opus":0.009037181186672254,"score_gpt":0.24684894386870293,"score_spread":0.23781176268203066,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2023958933","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.04398329,0.00016464168,0.9549829,0.00028261615,0.00023281314,0.00021857618,0.000013395863,0.00002005825,0.00010171948],"genre_scores_gemma":[0.5685912,0.0000291483,0.43092415,0.00034874148,0.00006547443,0.0000021030799,5.147384e-7,0.000027856608,0.000010868249],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.998151,0.00020568765,0.0005877127,0.00011483972,0.0006796635,0.0002610957],"domain_scores_gemma":[0.9983847,0.0003107739,0.00030709396,0.0005008861,0.00035431958,0.00014219967],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0011992701,0.00020311125,0.0004126253,0.000010616875,0.000116314055,0.000012950353,0.0006868195,0.00011435621,0.000020420408],"category_scores_gemma":[0.00025387103,0.00012371915,0.00031664176,0.0005429687,0.00018403595,0.000058434805,0.000045843342,0.00049049646,0.0000017288928],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00002829199,0.00007331657,0.000019645699,0.000050482908,0.00007994352,3.468946e-7,0.00011172704,0.64716285,0.34720936,0.0000031447557,0.0010080966,0.0042528072],"study_design_scores_gemma":[0.00034352453,0.00019648312,0.00031651038,0.00006221184,0.00035551755,0.00003351379,0.0004562929,0.9869513,0.010351405,0.0002562208,0.00052799226,0.00014905981],"about_ca_topic_score_codex":0.000013155001,"about_ca_topic_score_gemma":8.3560866e-7,"teacher_disagreement_score":0.52460784,"about_ca_system_score_codex":0.00012785116,"about_ca_system_score_gemma":0.00009346883,"threshold_uncertainty_score":0.504512},"labels":[],"label_agreement":null},{"id":"W2024264144","doi":"10.1121/1.4803850","title":"Unsteady numerical simulation of a round jet with impinging microjets for noise suppression","year":2013,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":13,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"National Institute on Deafness and Other Communication Disorders; U.S. Public Health Service; National Institutes of Health; Compute Canada; Pratt and Whitney Canada","keywords":"Jet (fluid); Mach number; Turbulence kinetic energy; Large eddy simulation; Sound pressure; Aeroacoustics; Acoustics; Turbulence; Lattice Boltzmann methods; Jet noise; Mechanics; Sound power; Physics; Noise (video); Computational fluid dynamics; Computer simulation; Computational physics; Sound (geography); Computer science","score_opus":0.00806171374090899,"score_gpt":0.23330676018866522,"score_spread":0.22524504644775623,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2024264144","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.14863385,0.000101871796,0.85041517,0.000420113,0.00015738925,0.00021197418,0.000013045069,0.000010982486,0.000035580393],"genre_scores_gemma":[0.94007546,0.00007856055,0.059575982,0.00011213347,0.00011214404,0.0000022756246,8.32787e-7,0.000028263055,0.00001432066],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989031,0.000039742372,0.00045378276,0.00006605463,0.0003138219,0.0002234971],"domain_scores_gemma":[0.99827933,0.0008212595,0.00034001056,0.00022877447,0.00026879273,0.00006183732],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00027366943,0.00014581054,0.00033727233,0.000016992084,0.000101088575,0.000016508318,0.00039075332,0.00006766742,0.000022356875],"category_scores_gemma":[0.000110295194,0.00007285128,0.0002616901,0.0001778975,0.00023908401,0.00010090978,0.000070346105,0.00030522243,8.4743687e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000048150578,0.000045278117,0.00008240243,0.00008913449,0.00012258669,1.11856494e-7,0.00036871107,0.9149205,0.07865534,0.000002166774,0.0026262228,0.003039406],"study_design_scores_gemma":[0.0003634672,0.00018842543,0.0005292286,0.00013844647,0.00020155834,0.000011786386,0.0005908636,0.99594307,0.0014255281,0.00031126346,0.00020157458,0.00009480517],"about_ca_topic_score_codex":0.000018457995,"about_ca_topic_score_gemma":1.5636721e-7,"teacher_disagreement_score":0.7914416,"about_ca_system_score_codex":0.00006143371,"about_ca_system_score_gemma":0.000033623885,"threshold_uncertainty_score":0.2970789},"labels":[],"label_agreement":null},{"id":"W2026024375","doi":"10.5589/q05-007","title":"Investigation of an Asymmetrical Shock-Wave Boundary-Layer Interaction in a Supersonic Planar Nozzle","year":2005,"lang":"en","type":"article","venue":"Canadian aeronautics and space journal","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Supersonic speed; Boundary layer; Turbulence; Nozzle; Mechanics; Transonic; Shock (circulatory); Physics; Reynolds-averaged Navier–Stokes equations; Shock wave; Mach number; Wind tunnel; Aerospace engineering; Aerodynamics; Engineering","score_opus":0.018232937787353014,"score_gpt":0.2165975861771859,"score_spread":0.1983646483898329,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2026024375","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9966479,0.00035957788,0.00087316247,0.0007826323,0.00029955612,0.000056982128,0.000023538785,0.000010488115,0.0009461764],"genre_scores_gemma":[0.9956832,0.00024075851,0.00368769,0.00011651732,0.00019108957,9.731565e-7,0.000010571622,0.000021824942,0.00004735665],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99922305,0.000021624448,0.00024538417,0.000101252095,0.00012948627,0.0002791899],"domain_scores_gemma":[0.9993402,0.000030035293,0.00003915516,0.00009285059,0.000042600484,0.00045519634],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023178234,0.00011745807,0.00015526985,0.0003924152,0.00008767262,0.000092265,0.00007157633,0.00010989475,0.00004273189],"category_scores_gemma":[0.0000343899,0.00012433168,0.000028609582,0.0001901178,0.000049077862,0.00021426224,0.000006290797,0.00046472898,0.0000026110872],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":true,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00016080604,0.00022206845,0.07983374,0.00046273833,0.0005835929,0.001325108,0.021343833,0.5272696,0.056307383,0.029040389,0.024659134,0.25879163],"study_design_scores_gemma":[0.00046324747,0.00010366803,0.020519674,0.000063791435,0.000022158529,0.00027159127,0.00057531794,0.9680639,0.00023263847,0.00071532995,0.008744727,0.00022398883],"about_ca_topic_score_codex":0.0015073357,"about_ca_topic_score_gemma":0.17560896,"teacher_disagreement_score":0.4407943,"about_ca_system_score_codex":0.0005156722,"about_ca_system_score_gemma":0.00018775683,"threshold_uncertainty_score":0.839434},"labels":[],"label_agreement":null},{"id":"W2026592964","doi":"10.1115/1.2842225","title":"Numerical and Experimental Studies of Oscillatory Airflows Induced by Rotation of a Grass-Cutting Blade","year":2008,"lang":"en","type":"article","venue":"Journal of Fluids Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"Ontario Centres of Excellence","keywords":"Blade (archaeology); Acoustics; Finite volume method; Noise (video); Mechanics; Compressibility; Rotation (mathematics); Vibration; Sound pressure; Tetrahedron; Computer simulation; Mathematics; Physics; Structural engineering; Geometry; Computer science; Engineering","score_opus":0.014710537034241073,"score_gpt":0.2421567736535554,"score_spread":0.22744623661931432,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2026592964","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9779919,0.005081652,0.016456658,0.0000060387283,0.0003566709,0.000046350786,0.000003398924,0.000021863958,0.000035494253],"genre_scores_gemma":[0.99300164,0.00041473616,0.006455908,0.0000028882791,0.000091978705,0.0000015656806,5.095745e-7,0.000028608116,0.000002192927],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99899834,0.000008580163,0.00055431144,0.00006938368,0.00022895198,0.00014043598],"domain_scores_gemma":[0.99955577,0.00008504528,0.00011530934,0.00007486245,0.00010377529,0.000065211665],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016202767,0.00014024362,0.00036985584,0.00013291946,0.000027978947,0.0000046777245,0.000085602434,0.000060725542,0.0000021270785],"category_scores_gemma":[0.000100096324,0.00013585156,0.000073403775,0.00012632215,0.000035071404,0.00013302082,0.000023068918,0.00019689799,1.596051e-7],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000056428757,0.000019317527,0.00045785678,0.00011445293,0.00009588908,0.000007882869,0.00070728274,0.23323296,0.7650273,0.000027867227,0.00010574564,0.00019781674],"study_design_scores_gemma":[0.00083681504,0.0003327344,0.002004996,0.0003040797,0.00005145212,0.00017069194,0.00066755293,0.66934854,0.32592478,0.00001540293,0.00006513851,0.00027779775],"about_ca_topic_score_codex":0.0000016544728,"about_ca_topic_score_gemma":7.597627e-8,"teacher_disagreement_score":0.4391025,"about_ca_system_score_codex":0.00007342287,"about_ca_system_score_gemma":0.000014409195,"threshold_uncertainty_score":0.55398655},"labels":[],"label_agreement":null},{"id":"W2027060237","doi":"10.1115/imece2010-39231","title":"Prediction of Turbulent Flow-Induced Noise in Aircraft Cabins","year":2010,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Victoria","funders":"","keywords":"Noise (video); Acoustics; Turbulence; Sound pressure; Flow (mathematics); Enclosure; Aeroacoustics; Noise control; Boundary layer; Position (finance); Structural acoustics; Engineering; Mechanics; Computer science; Aerospace engineering; Physics; Vibration; Noise reduction; Telecommunications","score_opus":0.009148491733949103,"score_gpt":0.19712214479899567,"score_spread":0.18797365306504657,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2027060237","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97936726,0.0000071009076,0.013423845,0.000032347503,0.00068830105,0.000087568915,0.000011608265,0.00011187431,0.0062700906],"genre_scores_gemma":[0.99383307,0.000015141839,0.005938857,0.000009742406,0.000071781746,0.0000069849484,0.000008145489,0.000017213122,0.00009904001],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99950963,0.0000030871925,0.00018383455,0.00008612891,0.000090374546,0.0001269298],"domain_scores_gemma":[0.9997439,0.000015427271,0.00001115112,0.00016815819,0.000023829836,0.000037541955],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000083745705,0.000078414196,0.000097883196,0.00006497809,0.000010427717,0.0000058679366,0.00008154731,0.000091549664,0.00011040681],"category_scores_gemma":[0.000013428371,0.00007493123,0.000027684842,0.00009215686,0.000011134954,0.00004388791,0.000014990251,0.00022940639,0.00001072095],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00000275397,0.000058997633,0.0018500673,0.0000498042,0.000012702672,0.0000058178666,0.00017669491,0.26423368,0.72617835,0.0008335025,0.0006032935,0.005994327],"study_design_scores_gemma":[0.00018878965,0.000015138494,0.011410978,0.000009561377,0.000004565796,0.0000025555391,0.000015067812,0.9809733,0.0067549283,0.0001411953,0.0004134405,0.00007050188],"about_ca_topic_score_codex":0.000038088176,"about_ca_topic_score_gemma":0.00022404229,"teacher_disagreement_score":0.7194234,"about_ca_system_score_codex":0.000022638285,"about_ca_system_score_gemma":0.0000095284895,"threshold_uncertainty_score":0.3055607},"labels":[],"label_agreement":null},{"id":"W2027454211","doi":"10.1115/fedsm2007-37251","title":"PIV Study of Three-Dimensional Wall Jet Over Smooth and Rough Surfaces","year":2007,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Manitoba","funders":"","keywords":"Turbulence; Nozzle; Particle image velocimetry; Jet (fluid); Mechanics; Reynolds number; Transverse plane; Physics; Hydraulic diameter; Reynolds stress; Shear stress; Optics; Materials science; Structural engineering; Thermodynamics; Engineering","score_opus":0.010028037701132432,"score_gpt":0.22371447388358345,"score_spread":0.21368643618245103,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2027454211","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99369323,0.00010789029,0.0028232979,0.000005997784,0.00016473993,0.000113267335,0.000004412095,0.000066192835,0.0030209937],"genre_scores_gemma":[0.99790883,0.000008399816,0.0019117589,0.000017979859,0.00002377945,8.739019e-7,0.0000018905571,0.000017993712,0.00010851177],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993966,0.0000033460267,0.00018105764,0.00011177948,0.00015536536,0.00015184504],"domain_scores_gemma":[0.9997053,0.00007727333,0.000017214572,0.00013250722,0.000025718764,0.00004198514],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018367826,0.000104302824,0.00013584168,0.000033622196,0.000025987167,0.000009912337,0.00006433872,0.000044975808,0.000089118],"category_scores_gemma":[0.000006936951,0.00008534825,0.0000165857,0.00006821308,0.000020848931,0.00004448075,0.000043442753,0.00008561349,0.0000028377083],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00008810552,0.0006485122,0.23734738,0.00011846449,0.0002755699,0.00005426812,0.000899716,0.73943883,0.01177526,0.0032128647,0.0024939456,0.00364709],"study_design_scores_gemma":[0.0005881787,0.0001939115,0.2626185,0.000011094263,0.000023570141,0.000001389299,0.00011286852,0.73537475,0.00016880754,0.0004475104,0.0002701759,0.00018922231],"about_ca_topic_score_codex":0.0001985091,"about_ca_topic_score_gemma":0.0022802672,"teacher_disagreement_score":0.025271118,"about_ca_system_score_codex":0.000013992527,"about_ca_system_score_gemma":0.0000035881935,"threshold_uncertainty_score":0.34804007},"labels":[],"label_agreement":null},{"id":"W2029688928","doi":"10.1615/ichmt.2012.procsevintsympturbheattransfpal.1240","title":"Experimental study of air distribution inside a thermal wall jet produced by a displacement diffuser","year":2012,"lang":"en","type":"article","venue":"Proceeding of THMT-12. Proceedings of the Seventh International Symposium On Turbulence, Heat and Mass Transfer Palermo, Italy, 24-27 September, 2012","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Manitoba","funders":"","keywords":"Diffuser (optics); Jet (fluid); Mechanics; Displacement ventilation; Displacement (psychology); Turbulence; Thermal; Intensity (physics); Materials science; Optics; Physics; Computational fluid dynamics; Meteorology; Light source","score_opus":0.008311453595037682,"score_gpt":0.21566826594337368,"score_spread":0.207356812348336,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2029688928","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9924179,0.00039462696,0.00014471762,0.0002107114,0.0014457077,0.0010938845,0.00021227951,0.00006775977,0.004012462],"genre_scores_gemma":[0.99891376,0.00009264615,0.00007295536,0.000026210739,0.0001996175,0.00012660609,0.00003820902,0.00006899075,0.00046097205],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99724674,0.000013165276,0.0008675416,0.00042509293,0.0009197985,0.0005276687],"domain_scores_gemma":[0.9991786,0.000045951656,0.00016450441,0.00016504609,0.00026633177,0.00017957436],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00042662333,0.0005062239,0.00054354663,0.00012240381,0.00011950751,0.000041857846,0.0005984584,0.00015256551,0.00004611702],"category_scores_gemma":[0.000019390094,0.00039792914,0.00021038686,0.0001820504,0.00015375538,0.0006841035,0.00013262984,0.00034806397,0.0000022244333],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00037769185,0.0030304862,0.07257293,0.0007772154,0.0006099735,3.4423633e-7,0.004135199,0.0012920628,0.9134694,0.0012490819,0.0024127637,0.00007289607],"study_design_scores_gemma":[0.0046902397,0.0014568778,0.015421373,0.0012467152,0.00051329896,0.000018863857,0.0026806048,0.02973826,0.941214,0.00016932396,0.0016347582,0.0012156557],"about_ca_topic_score_codex":0.000020769006,"about_ca_topic_score_gemma":0.0000026139653,"teacher_disagreement_score":0.057151563,"about_ca_system_score_codex":0.0001662929,"about_ca_system_score_gemma":0.000015647945,"threshold_uncertainty_score":0.99984723},"labels":[],"label_agreement":null},{"id":"W2032042733","doi":"10.1115/pvp2014-28859","title":"The Effect of Upstream Edge Geometry on the Acoustic Resonance Excitation in Shallow Rectangular Cavities","year":2014,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Guelph; Ontario Tech University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Resonance (particle physics); Acoustic resonance; Microphone; Amplitude; Sound pressure; Acoustics; Excitation; Mach number; Optics; Vibration; Materials science; Enhanced Data Rates for GSM Evolution; Excited state; Physics; Mechanics; Atomic physics; Telecommunications","score_opus":0.003170720195370418,"score_gpt":0.18760755304820864,"score_spread":0.1844368328528382,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2032042733","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98215836,0.00028279837,0.0068146302,0.000066312154,0.00032609198,0.00017457495,0.0000050217905,0.000054898086,0.010117328],"genre_scores_gemma":[0.99935514,0.00010067133,0.00010591407,0.000021056007,0.000061030856,0.000020225723,0.0000023454834,0.00002128002,0.0003123527],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99935275,0.00006685946,0.00016718818,0.000095160685,0.00014610995,0.00017191519],"domain_scores_gemma":[0.99788487,0.0017793844,0.000024847424,0.00027785622,0.000017111312,0.000015939624],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00065771845,0.00011412055,0.00012697141,0.000045577315,0.00006782027,0.000022681957,0.00019289563,0.000054554446,0.000013021647],"category_scores_gemma":[0.00039353204,0.00006100638,0.000039808594,0.00016989053,0.00005656666,0.000024961775,0.00001942988,0.00016941996,0.000009034737],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00009966144,0.0000390016,0.007107389,0.00036210637,0.00007348778,0.000006208444,0.0007158581,0.82600063,0.0202809,0.04886523,0.004017323,0.09243222],"study_design_scores_gemma":[0.00026144178,0.00021500813,0.011595003,0.0001105666,0.000014977853,0.0000010181961,0.00015394283,0.9815766,0.003002411,0.002118355,0.0007976426,0.00015303888],"about_ca_topic_score_codex":0.00001907081,"about_ca_topic_score_gemma":0.00019041746,"teacher_disagreement_score":0.15557599,"about_ca_system_score_codex":0.000042492138,"about_ca_system_score_gemma":0.00000366509,"threshold_uncertainty_score":0.24877681},"labels":[],"label_agreement":null},{"id":"W2032060153","doi":"10.1007/s00419-010-0494-8","title":"On the effect of inflow conditions in simulation of a turbulent round jet","year":2010,"lang":"en","type":"article","venue":"Archive of Applied Mechanics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":21,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"University of British Columbia; Simon Fraser University","keywords":"Inflow; Turbulence; Turbulence kinetic energy; Mechanics; Jet (fluid); Nozzle; Dissipation; Control volume; Physics; Inlet; Computer simulation; Kinetic energy; Flow (mathematics); Field (mathematics); Classical mechanics; Mathematics; Engineering; Thermodynamics; Mechanical engineering","score_opus":0.0037076324823582573,"score_gpt":0.20800786498897886,"score_spread":0.2043002325066206,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2032060153","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9525208,0.000002548182,0.04498237,0.0000067442033,0.0000975302,0.00029246096,0.000064864194,0.000012967819,0.00201975],"genre_scores_gemma":[0.9989282,0.000006162946,0.0009901286,0.000006663971,0.000012311581,0.000019411138,0.000021014332,0.000015104523,0.0000010020082],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994977,0.00001003706,0.00021159514,0.00007294393,0.00011662638,0.00009108486],"domain_scores_gemma":[0.99893206,0.00075829384,0.00006361884,0.00021394827,0.000014913185,0.000017156955],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018873904,0.00008960848,0.00016814904,0.000070337366,0.000015086728,0.0000023081468,0.000121578814,0.000046954912,0.00001891542],"category_scores_gemma":[0.00004754713,0.0000674042,0.00004235474,0.00008664068,0.00002699895,0.00001144597,0.000024603753,0.00021681772,0.000001755043],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000020997273,0.000013660851,0.000004757298,0.000049850445,0.000013233605,2.1918301e-7,0.0001088143,0.59323496,0.1955456,0.2107441,0.000010030297,0.00025377364],"study_design_scores_gemma":[0.00026646777,0.000095959535,0.00007380759,0.00002953029,0.00001533879,1.7763327e-7,0.000015423142,0.8543405,0.05192078,0.09317317,0.00001536472,0.000053465927],"about_ca_topic_score_codex":0.00000388013,"about_ca_topic_score_gemma":0.00003481046,"teacher_disagreement_score":0.26110554,"about_ca_system_score_codex":0.000008357215,"about_ca_system_score_gemma":0.0000068186405,"threshold_uncertainty_score":0.27486637},"labels":[],"label_agreement":null},{"id":"W2032086515","doi":"10.1115/fedsm-icnmm2010-30881","title":"Experimental Investigation of the Mean Concentration Fields in a Counterflowing Jet","year":2010,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Alberta","funders":"","keywords":"Jet (fluid); Physics; Range (aeronautics); Mechanics; Flow (mathematics); Chemistry; Materials science","score_opus":0.006259282764875554,"score_gpt":0.2043902278877968,"score_spread":0.19813094512292123,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2032086515","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9938469,0.000010311436,0.002073168,0.000029595569,0.0005764005,0.00006540633,0.0000013752045,0.00002171184,0.0033751295],"genre_scores_gemma":[0.9993587,0.0000012567541,0.00054777774,0.000037201447,0.000030160803,0.000003554614,0.0000018227706,0.000005419889,0.000014081959],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997205,0.0000045620227,0.00010842807,0.000042983367,0.00006384797,0.00005964008],"domain_scores_gemma":[0.9998619,0.000014619396,0.000010467858,0.00009170786,0.000009127955,0.000012188767],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000060594044,0.000042665004,0.00004475419,0.000009351582,0.000013456913,0.000008504289,0.00006768979,0.000043671753,0.000039864804],"category_scores_gemma":[0.00000806768,0.00003176731,0.000015647842,0.000050811148,0.000024400966,0.000048440063,0.000011936825,0.000117416435,9.1334886e-7],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[8.157274e-7,0.0000055655,0.010143029,0.000008890967,0.0000031367774,2.4710425e-7,0.0010337804,0.014343614,0.9703609,0.0038776675,0.00011772879,0.00010464762],"study_design_scores_gemma":[0.0001261029,0.0000055687656,0.0056788456,0.000012362625,0.0000016900323,6.369421e-7,0.00014399229,0.66036904,0.33330816,0.00027923027,0.00002354814,0.00005078249],"about_ca_topic_score_codex":0.000026206226,"about_ca_topic_score_gemma":0.00043250152,"teacher_disagreement_score":0.6460255,"about_ca_system_score_codex":0.0000143861835,"about_ca_system_score_gemma":0.000006868186,"threshold_uncertainty_score":0.12954333},"labels":[],"label_agreement":null},{"id":"W2032911019","doi":"10.1115/1.4002653","title":"Experimental and Numerical Study of Laminar Round Jet Flows Along a Wall","year":2010,"lang":"en","type":"article","venue":"Journal of Fluids Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Manitoba","funders":"Natural Sciences and Engineering Research Council of Canada; Manitoba Hydro","keywords":"Laminar flow; Mechanics; Reynolds number; Jet (fluid); Computational fluid dynamics; Particle image velocimetry; Vorticity; Physics; Compressibility; Vortex; Inlet; Classical mechanics; Turbulence; Geology","score_opus":0.005867870212663183,"score_gpt":0.2170477031864442,"score_spread":0.211179832973781,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2032911019","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9672323,0.00041523165,0.031268626,0.000006277634,0.0009015162,0.000081650614,0.0000020468372,0.00003404892,0.000058334812],"genre_scores_gemma":[0.9915929,0.000013418791,0.00810676,0.0000029073005,0.00023173142,0.0000026061682,4.197733e-7,0.00004344588,0.000005830769],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99900734,0.0000070237115,0.0004742282,0.00008971317,0.00023403569,0.00018768001],"domain_scores_gemma":[0.99955845,0.00006197466,0.00005655901,0.00014736198,0.000057788806,0.00011786543],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021928581,0.00017662898,0.00032562143,0.0001405443,0.000025422914,0.000032273183,0.00017039666,0.00007477911,0.00001678302],"category_scores_gemma":[0.000042779753,0.00016152198,0.00006551122,0.00010811224,0.000013432161,0.00015318568,0.000042849955,0.00046751357,7.701015e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000009960407,0.00016147838,0.0015145803,0.000049376096,0.00008656329,0.000070601374,0.00091316114,0.17232148,0.824227,0.000102653765,0.000051427985,0.0004917361],"study_design_scores_gemma":[0.0009143944,0.00051789905,0.006307026,0.000048152608,0.00005468148,0.00024728902,0.0004030185,0.9780397,0.012923958,0.000009026719,0.00029457427,0.0002402696],"about_ca_topic_score_codex":0.000007759146,"about_ca_topic_score_gemma":0.0000025938982,"teacher_disagreement_score":0.811303,"about_ca_system_score_codex":0.000036988273,"about_ca_system_score_gemma":0.000010523982,"threshold_uncertainty_score":0.6586675},"labels":[],"label_agreement":null},{"id":"W2033552873","doi":"10.1115/pvp2009-77071","title":"Azimuthal Behaviour of Self-Excited Diametral Modes of Internal Cavities","year":2009,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"","keywords":"Azimuth; Rotational symmetry; Mechanics; Physics; Spinning; Superposition principle; Amplitude; Oscillation (cell signaling); Excited state; Mach number; Acoustics; Materials science; Optics; Composite material; Chemistry","score_opus":0.005091782439482081,"score_gpt":0.20404378063653553,"score_spread":0.19895199819705345,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2033552873","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.96093047,0.000048630143,0.02849515,0.0000048421725,0.000115464165,0.000040883344,0.00003164559,0.000107482,0.010225446],"genre_scores_gemma":[0.9913795,0.00002014384,0.008383642,0.000010356294,0.000033048596,8.5572213e-7,0.000003446662,0.00001199916,0.00015699767],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994546,0.000004565449,0.00022715445,0.000068117835,0.000114503004,0.00013104541],"domain_scores_gemma":[0.999753,0.000021161468,0.000027807426,0.0001237014,0.000041092975,0.00003324886],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000051571686,0.000093875584,0.00016498605,0.00007730504,0.00000871862,0.00000688071,0.00012583142,0.000054335396,0.000055180484],"category_scores_gemma":[0.0000071506847,0.00008726836,0.000061872845,0.00007845073,0.000024101784,0.00004951642,0.000013758072,0.00009198042,0.0000011407226],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000040995907,0.0006603487,0.049180556,0.00039982208,0.00030588367,0.000031412997,0.0022886267,0.62883747,0.25546253,0.050295617,0.0016197785,0.010876963],"study_design_scores_gemma":[0.0002634016,0.0001235249,0.02514399,0.00003715576,0.000034591078,0.0000051851484,0.00022520366,0.9468468,0.025803437,0.0013263207,0.000012491479,0.00017794009],"about_ca_topic_score_codex":0.000045439047,"about_ca_topic_score_gemma":0.0000137108345,"teacher_disagreement_score":0.3180093,"about_ca_system_score_codex":0.000021316884,"about_ca_system_score_gemma":0.000006187831,"threshold_uncertainty_score":0.35587004},"labels":[],"label_agreement":null},{"id":"W2033981239","doi":"10.2514/6.2013-2058","title":"Measurement of the wavenumber-frequency spectrum of wall pressure fluctuations: spiral-shaped rotative arrays with pinhole-mounted quarter inch microphones","year":2013,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":17,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"Université de Sherbrooke","funders":"Université de Sherbrooke","keywords":"Pinhole (optics); Spiral (railway); Wavenumber; Optics; Acoustics; Frequency spectrum; Physics; Quarter (Canadian coin); Materials science; Engineering","score_opus":0.006088238748477295,"score_gpt":0.19132794579020662,"score_spread":0.18523970704172932,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2033981239","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9302767,0.00031998046,0.062541775,0.00039445405,0.0002814238,0.0010304726,0.000041537074,0.000088432935,0.0050252452],"genre_scores_gemma":[0.995069,0.00001449269,0.004636299,0.000026423166,0.00003163694,0.000049229126,0.000004156288,0.000031364234,0.00013738664],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9988492,0.000029841181,0.0003745427,0.00015864856,0.00037897186,0.00020878714],"domain_scores_gemma":[0.999132,0.000023007307,0.0001141711,0.00039334781,0.00029992382,0.00003754992],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012588364,0.00019219272,0.00023711164,0.000048209775,0.00004720807,0.000018589506,0.00025743345,0.00006576196,0.00029296786],"category_scores_gemma":[0.000026137095,0.00012349308,0.000067379435,0.0002143663,0.00009354394,0.00010019762,0.000029971452,0.00016149307,0.000016856013],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000012200559,0.00012824884,0.0027979277,0.0003602681,0.00043691756,9.664609e-7,0.0016722041,0.06366088,0.92831534,0.0014218033,0.0009577563,0.0002355102],"study_design_scores_gemma":[0.0014397504,0.00028729578,0.07771253,0.0005392105,0.00025732978,0.0000087116005,0.00089906633,0.8388339,0.07266862,0.006518332,0.00016127845,0.00067395315],"about_ca_topic_score_codex":0.00035590387,"about_ca_topic_score_gemma":0.00038305807,"teacher_disagreement_score":0.85564667,"about_ca_system_score_codex":0.000051934294,"about_ca_system_score_gemma":0.000037529808,"threshold_uncertainty_score":0.5035902},"labels":[],"label_agreement":null},{"id":"W2035146531","doi":"10.1016/j.jfluidstructs.2012.06.002","title":"Self-excited oscillations of a high-speed impinging planar jet","year":2012,"lang":"en","type":"article","venue":"Journal of Fluids and Structures","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":33,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"","keywords":"Jet (fluid); Particle image velocimetry; Mechanics; Nozzle; Planar; Dimensionless quantity; Acoustics; Physics; Aeroacoustics; Rotational symmetry; Flow (mathematics); Optics; Materials science; Sound pressure; Turbulence","score_opus":0.006185827991421457,"score_gpt":0.21225398886941507,"score_spread":0.20606816087799362,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2035146531","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98790044,0.0016363433,0.009474926,0.00002619681,0.0005884513,0.000029728453,0.000019568717,0.000018622904,0.00030572677],"genre_scores_gemma":[0.9871366,0.00032417462,0.012160657,0.000011600259,0.00034777928,9.8898404e-8,0.0000016985501,0.000012986731,0.0000044288113],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.99937636,0.000009391112,0.00029153196,0.00003701001,0.00013648388,0.00014923724],"domain_scores_gemma":[0.99965703,0.000045623794,0.00007757811,0.00006987342,0.000063377745,0.00008653972],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012983824,0.00009551826,0.00020451298,0.000118648015,0.000045364446,0.000018982764,0.00007233385,0.00005944435,0.000018389823],"category_scores_gemma":[0.000024661183,0.0000725281,0.00005077185,0.00008385685,0.000020895699,0.00011194255,0.000010988198,0.0001487155,1.8752195e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000111489266,0.00013615366,0.08279267,0.0011386205,0.0019035797,0.000050304196,0.0085651325,0.2316027,0.52899086,0.12074689,0.009022957,0.014938669],"study_design_scores_gemma":[0.0024832976,0.00036665323,0.48951203,0.00024595397,0.0005456573,0.0009075501,0.00076101726,0.46716666,0.007209392,0.021956846,0.0079292115,0.0009157409],"about_ca_topic_score_codex":0.0000038069313,"about_ca_topic_score_gemma":0.0000012755465,"teacher_disagreement_score":0.52178144,"about_ca_system_score_codex":0.00002184578,"about_ca_system_score_gemma":0.000009612236,"threshold_uncertainty_score":0.295761},"labels":[],"label_agreement":null},{"id":"W2035312510","doi":"10.1061/(asce)0733-9429(2009)135:11(989)","title":"Characteristics of a Three-Dimensional Square Jet in the Vicinity of a Free Surface","year":2009,"lang":"en","type":"article","venue":"Journal of Hydraulic Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":9,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Windsor","funders":"","keywords":"Nozzle; Turbulence; Jet (fluid); Mechanics; Free surface; Reynolds stress; Shear stress; Turbulence kinetic energy; Reynolds number; Physics; Materials science; Geology; Thermodynamics","score_opus":0.007358497865081159,"score_gpt":0.20141940422161467,"score_spread":0.1940609063565335,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2035312510","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9850436,0.00041236024,0.013919353,0.00011640981,0.00027110658,0.00006686013,0.000017272823,0.00001352673,0.00013950703],"genre_scores_gemma":[0.9955617,0.00007145005,0.0042209467,0.000024190935,0.00010207991,3.322376e-7,0.0000014819093,0.000016823155,9.781393e-7],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99876875,0.000012458683,0.00066575455,0.000057919005,0.00032148557,0.0001736493],"domain_scores_gemma":[0.99929535,0.00015932033,0.00017431586,0.00023028073,0.000097369215,0.000043366785],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000482619,0.00014692331,0.000380589,0.000119332006,0.000011994156,0.000008974192,0.00036268454,0.00007052783,0.000008285849],"category_scores_gemma":[0.0001505905,0.000111321,0.000113300935,0.00023214867,0.000016277221,0.00008147472,0.000021939128,0.00041547584,4.5681864e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000013276415,0.00006323616,0.0014096765,0.000113844726,0.000033348562,0.000046609144,0.00023834223,0.96760666,0.029453613,0.00020254785,0.00015192632,0.00066691684],"study_design_scores_gemma":[0.00056057004,0.00021461061,0.12883548,0.0004078585,0.00004407558,0.00010195003,0.00003265493,0.86722106,0.0018425662,0.00042548243,0.00014198235,0.00017169579],"about_ca_topic_score_codex":0.0000059457075,"about_ca_topic_score_gemma":0.000008567281,"teacher_disagreement_score":0.1274258,"about_ca_system_score_codex":0.00003868828,"about_ca_system_score_gemma":0.00002149681,"threshold_uncertainty_score":0.4539539},"labels":[],"label_agreement":null},{"id":"W2036960668","doi":"10.1007/s00348-015-1908-8","title":"Passive control of flow-excited acoustic resonance in rectangular cavities using upstream mounted blocks","year":2015,"lang":"en","type":"article","venue":"Experiments in Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":28,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Ontario Tech University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Resonance (particle physics); Acoustic resonance; Excited state; Attenuation; Acoustics; Mach number; Materials science; Sound pressure; Optics; Physics; Mechanics; Atomic physics","score_opus":0.01568869579857133,"score_gpt":0.2628918979534211,"score_spread":0.24720320215484978,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2036960668","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.96855104,0.003169646,0.026341923,0.0000064350106,0.0006833498,0.0002746262,0.0000585763,0.00007436921,0.0008400408],"genre_scores_gemma":[0.99639064,0.00004120887,0.0032988472,0.000021608284,0.000071700546,0.000038982413,0.000011629179,0.000049399798,0.00007598354],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99867755,0.000043471005,0.00046114117,0.00021272447,0.00025679456,0.0003483217],"domain_scores_gemma":[0.9994712,0.00005515501,0.00004066133,0.00028774096,0.00007022271,0.000075040145],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017244855,0.00022333508,0.00036621653,0.00019847079,0.000021069023,0.000016797698,0.00019761042,0.00014500925,0.000025016094],"category_scores_gemma":[0.00010787259,0.00024104858,0.000040771294,0.00031607648,0.00007495728,0.0000934718,0.000044587367,0.00020601331,0.0000022475874],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000058510934,0.000099221616,0.0019806917,0.000026214351,0.00003147489,0.00006660683,0.0029334358,0.8362233,0.1577213,0.00007673585,0.00019293505,0.00058958656],"study_design_scores_gemma":[0.0017371244,0.00004791773,0.00031287505,0.00017672566,0.0000109244875,0.0000038741505,0.00092714146,0.98274165,0.013537315,0.00017628452,0.000091735164,0.00023642207],"about_ca_topic_score_codex":0.00016074003,"about_ca_topic_score_gemma":0.000039828086,"teacher_disagreement_score":0.14651836,"about_ca_system_score_codex":0.000553827,"about_ca_system_score_gemma":0.000065905595,"threshold_uncertainty_score":0.98296756},"labels":[],"label_agreement":null},{"id":"W2037092344","doi":"10.1115/imece2002-33373","title":"Flow Excited Resonance of a Confined Shallow Cavity in Low Mach Number Flow and Its Control","year":2002,"lang":"en","type":"article","venue":"5th International Symposium on Fluid Structure Interaction, Aeroelasticity, and Flow Induced Vibration and Noise","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Atomic Energy (Canada); McMaster University","funders":"","keywords":"Mach number; Duct (anatomy); Acoustics; Mechanics; Flow visualization; Acoustic resonance; Physics; Resonance (particle physics); Amplitude; Oscillation (cell signaling); Optics; Materials science; Flow (mathematics); Resonator; Atomic physics; Chemistry","score_opus":0.009673592330239237,"score_gpt":0.22937294466197244,"score_spread":0.2196993523317332,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2037092344","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9834554,0.0001478648,0.012630186,0.0004543596,0.0015322593,0.00033790013,0.0003687142,0.00007453426,0.0009987693],"genre_scores_gemma":[0.9979172,0.0005446799,0.0008333974,0.00022694303,0.00026342657,0.000022388549,0.00007537092,0.000037013313,0.00007960383],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99837065,0.00005922556,0.00058566,0.00042037628,0.00031994973,0.00024414255],"domain_scores_gemma":[0.9991762,0.00020005056,0.00011475907,0.00014277524,0.00022265855,0.0001435456],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00010699607,0.0003474553,0.00036516567,0.00017492936,0.000112780945,0.00012998021,0.00013850332,0.0002346761,0.00039799197],"category_scores_gemma":[0.00011203637,0.0003428422,0.00005048006,0.00015971925,0.000063884574,0.00039145027,0.000042901436,0.0004269676,0.0000059468734],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00096268824,0.00039485577,0.009155477,0.0004636234,0.00037259885,0.000047445574,0.003024568,0.44225657,0.5194117,0.0037485254,0.00073918706,0.01942276],"study_design_scores_gemma":[0.001715623,0.000100227866,0.014264065,0.00019153173,0.000028942697,0.000055145953,0.000035095298,0.9795616,0.0033373784,0.00014229334,0.00026531884,0.00030277512],"about_ca_topic_score_codex":0.000031347055,"about_ca_topic_score_gemma":0.00017878141,"teacher_disagreement_score":0.53730506,"about_ca_system_score_codex":0.00009410719,"about_ca_system_score_gemma":0.00001105076,"threshold_uncertainty_score":0.99990237},"labels":[],"label_agreement":null},{"id":"W2037292268","doi":"10.1115/fedsm-icnmm2010-30333","title":"Numerical Simulation of Internal Cavities Acoustic Trapped Modes With Mean Flow","year":2010,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"","keywords":"Mach number; Physics; Mechanics; Aerodynamics; Sound pressure; Acoustics; Mean flow; Amplitude; Acoustic streaming; Duct (anatomy); Acoustic wave; Particle velocity; Acoustic resonance; Resonance (particle physics); Optics; Atomic physics","score_opus":0.005713750870134925,"score_gpt":0.20956852307105414,"score_spread":0.20385477220091922,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2037292268","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.44287625,0.000003615631,0.55358773,0.0000027209908,0.00012528007,0.0000356996,0.000005762024,0.00007628792,0.0032866423],"genre_scores_gemma":[0.98555624,0.0000018611548,0.014234528,0.0000092703185,0.0000714226,0.0000028326251,0.0000040595046,0.00002464847,0.00009514982],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99952525,0.0000034468208,0.00014285944,0.00008240119,0.00012242816,0.00012360136],"domain_scores_gemma":[0.99970853,0.000061446466,0.000017665434,0.00012982126,0.00004149309,0.000041030555],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00004379974,0.00009980649,0.00012368089,0.000038740993,0.000019713507,0.000015361507,0.00008908665,0.000053541826,0.00011421148],"category_scores_gemma":[0.00001130995,0.00007832775,0.000027818343,0.000056671666,0.00004036699,0.000060089766,0.000009068742,0.00017680135,0.0000033762456],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000009090814,0.000012517591,0.00016424047,0.000028808163,0.000020317364,0.0000016039971,0.0001307717,0.9699399,0.028009145,0.00029325756,0.00001971091,0.001370634],"study_design_scores_gemma":[0.00015045314,0.0000319717,0.00022406531,0.000012021736,0.000015808291,0.000002946778,0.00006944867,0.99725294,0.0018900004,0.00022672472,0.000016606798,0.00010700758],"about_ca_topic_score_codex":0.000019664043,"about_ca_topic_score_gemma":0.00012230514,"teacher_disagreement_score":0.54267997,"about_ca_system_score_codex":0.000010790527,"about_ca_system_score_gemma":0.000008020539,"threshold_uncertainty_score":0.31941128},"labels":[],"label_agreement":null},{"id":"W2037376203","doi":"10.1007/s00348-005-0011-y","title":"Phase-averaged measurements in an isosceles triangular turbulent free jet","year":2005,"lang":"en","type":"article","venue":"Experiments in Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"St. Francis Xavier University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Turbulence; Reynolds number; Isosceles triangle; Reynolds stress; Jet (fluid); Mechanics; Body orifice; Physics; Shear stress; Anemometer; Classical mechanics; Optics; Mathematics; Geometry; Mechanical engineering","score_opus":0.034597527213436306,"score_gpt":0.2977107948022715,"score_spread":0.2631132675888352,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2037376203","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9929496,0.0014136322,0.0021745919,0.000049137845,0.00049849687,0.00030496434,0.000014062902,0.00014523476,0.002450276],"genre_scores_gemma":[0.9926552,0.00005737887,0.006717324,0.000118766926,0.00018278327,0.00007719299,0.000031150303,0.00006406899,0.0000961337],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9983981,0.000055392993,0.00046368554,0.00029828795,0.0003524137,0.0004320703],"domain_scores_gemma":[0.99929744,0.000015707436,0.00002181531,0.0005389212,0.000022656306,0.00010344047],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00033058412,0.00026769412,0.00027714434,0.00019262425,0.000040639632,0.000049931623,0.0004368537,0.00012890917,0.00024008127],"category_scores_gemma":[0.00003272855,0.00028478977,0.00005038848,0.00018777049,0.000026607298,0.00022322928,0.000059504673,0.00024716492,0.000031917014],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00010387852,0.002647154,0.003241816,0.00003660969,0.00007718681,0.00007418687,0.005216961,0.11250791,0.8570147,0.00031510525,0.0050304434,0.013734034],"study_design_scores_gemma":[0.01564386,0.0003277085,0.0011709232,0.00013588801,0.000014470839,0.000004954202,0.00037640426,0.7971085,0.17597616,0.0003569658,0.007916678,0.0009675261],"about_ca_topic_score_codex":0.000021565013,"about_ca_topic_score_gemma":0.00010607283,"teacher_disagreement_score":0.68460053,"about_ca_system_score_codex":0.000527632,"about_ca_system_score_gemma":0.000022495075,"threshold_uncertainty_score":0.9999604},"labels":[],"label_agreement":null},{"id":"W2038049080","doi":"10.1115/imece2014-37699","title":"Frequency Analysis of a Trailing Vortex Flow Subjected to External Turbulence","year":2014,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Windsor","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Turbulence; Physics; Mechanics; Chord (peer-to-peer); Vortex; Wind tunnel; Wake; Horseshoe vortex; Airfoil; Lift-to-drag ratio; Reynolds number; Wingtip vortices; Drag; K-epsilon turbulence model; Vortex shedding; Angle of attack; Lift (data mining); Wake turbulence; Starting vortex; Aerodynamics; Vortex ring; Computer science","score_opus":0.004261099382290554,"score_gpt":0.19693338329274968,"score_spread":0.19267228391045912,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2038049080","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.5351548,0.00001935988,0.46218005,0.0000041701724,0.000102360485,0.000030863775,0.000009648498,0.00011272718,0.0023859674],"genre_scores_gemma":[0.9266101,0.000010222092,0.073201306,0.00003350646,0.000045279972,0.0000039258875,0.0000047334256,0.000021137395,0.00006979937],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99925214,0.000010036037,0.0002525031,0.0001494471,0.00015015788,0.00018568862],"domain_scores_gemma":[0.9995288,0.000056211557,0.000020545673,0.00025483576,0.00005697069,0.00008258499],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00014329127,0.00011215107,0.00024006996,0.0002036459,0.000020456962,0.00001617257,0.00018298985,0.00005013865,0.00016090347],"category_scores_gemma":[0.000058283582,0.00010530621,0.00010104681,0.0006481157,0.000013623301,0.000037624737,0.000018872099,0.00008835496,0.000013605169],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000012078457,0.000010831157,0.0020621736,0.000020121877,0.00015375954,0.0000014557157,0.00013268321,0.879262,0.10987847,0.0013749122,0.000018747694,0.007083642],"study_design_scores_gemma":[0.00005861164,0.000014878298,0.025233755,0.000015175994,0.00016448498,4.8578636e-7,0.000009233077,0.97247344,0.0015779977,0.00030578728,0.000016310838,0.00012981838],"about_ca_topic_score_codex":0.0000534583,"about_ca_topic_score_gemma":0.00024268765,"teacher_disagreement_score":0.39145523,"about_ca_system_score_codex":0.000017742352,"about_ca_system_score_gemma":0.0000056750764,"threshold_uncertainty_score":0.42942625},"labels":[],"label_agreement":null},{"id":"W2038095757","doi":"10.1007/s00348-014-1873-7","title":"Active and passive flow control on a precessing jet","year":2015,"lang":"en","type":"article","venue":"Experiments in Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Alberta","funders":"","keywords":"Strouhal number; Nozzle; Precession; Mechanics; Physics; Jet (fluid); Reynolds number; Synthetic jet; Flow control (data); Actuator; Turbulence; Thermodynamics; Computer science","score_opus":0.015232484649403506,"score_gpt":0.2582577290712901,"score_spread":0.24302524442188658,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2038095757","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9632362,0.00055366947,0.015172808,0.00004669679,0.0012141039,0.00027817235,0.000032383046,0.00014118037,0.019324757],"genre_scores_gemma":[0.9974085,0.000020021353,0.0022536796,0.000075579905,0.0000980031,0.000045239987,0.00000516002,0.00002898303,0.00006479641],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99933904,0.000019785644,0.00013858272,0.00015988194,0.00014221267,0.00020049825],"domain_scores_gemma":[0.9996986,0.00003891419,0.0000125421075,0.00013729554,0.000020537345,0.0000921471],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000053582808,0.00014660945,0.00015993965,0.000060933453,0.000028410921,0.00003628466,0.00008255585,0.00007245228,0.000016059414],"category_scores_gemma":[0.000039535626,0.00013786576,0.000016485212,0.00006599569,0.000033332777,0.000091983726,0.000027874525,0.00014405254,0.000012832054],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00068235426,0.0007577202,0.006797201,0.000119298726,0.00050124514,0.0002775735,0.040162303,0.54554725,0.23169409,0.004262899,0.015249864,0.15394822],"study_design_scores_gemma":[0.0023512112,0.00012908535,0.00074279576,0.00008377441,0.000008613168,0.0000031119969,0.00072616746,0.9754108,0.018420622,0.0005496993,0.0012674815,0.00030663892],"about_ca_topic_score_codex":0.000005770724,"about_ca_topic_score_gemma":0.0000035117164,"teacher_disagreement_score":0.42986357,"about_ca_system_score_codex":0.00019907688,"about_ca_system_score_gemma":0.000019022202,"threshold_uncertainty_score":0.56220025},"labels":[],"label_agreement":null},{"id":"W2038133661","doi":"10.1007/s00348-009-0731-5","title":"Quantitative imaging of acoustically coupled flows over symmetrically located side branches","year":2009,"lang":"en","type":"article","venue":"Experiments in Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":9,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Victoria","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Turbulence; Particle image velocimetry; Acoustics; Amplitude; Physics; Mechanics; Oscillation (cell signaling); Aeroacoustics; Resonator; Duct (anatomy); Inflow; Mean flow; Optics; Sound pressure","score_opus":0.011436460256738041,"score_gpt":0.27104255048033066,"score_spread":0.2596060902235926,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2038133661","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.80805963,0.0021907198,0.18236296,0.00003225202,0.0005684062,0.0002389458,0.000014741096,0.00018022515,0.00635214],"genre_scores_gemma":[0.9765787,0.00010413388,0.02307087,0.000097255775,0.000047844736,0.000011483318,0.000012846705,0.000039915765,0.000036931568],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99849105,0.000023942477,0.000537665,0.00025566912,0.00030850407,0.0003831668],"domain_scores_gemma":[0.99938214,0.00013468177,0.000037573467,0.00028491765,0.0000740727,0.00008660338],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00018722008,0.00024890585,0.00036104082,0.00024573898,0.00003402534,0.000030252744,0.0002631955,0.00009300884,0.000075149626],"category_scores_gemma":[0.0001637801,0.00025808136,0.00006958538,0.0005386338,0.000062176434,0.00013457982,0.000041146483,0.00021804235,0.000015058158],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000051700223,0.00021342016,0.00053892034,0.000030847714,0.000046449393,0.000039614086,0.0006995512,0.08186655,0.9091383,0.0033637967,0.00032707845,0.0036837251],"study_design_scores_gemma":[0.00075275695,0.00010092637,0.004119448,0.00008838007,0.000012793467,0.0000018716281,0.00014610359,0.97520226,0.018502263,0.0007405054,0.00004927868,0.00028343967],"about_ca_topic_score_codex":0.000019341,"about_ca_topic_score_gemma":0.000003438986,"teacher_disagreement_score":0.8933357,"about_ca_system_score_codex":0.00019599193,"about_ca_system_score_gemma":0.0000371157,"threshold_uncertainty_score":0.9999871},"labels":[],"label_agreement":null},{"id":"W2038462466","doi":"10.2514/1.19457","title":"Optimization of Controlled Jets in Crossflow","year":2006,"lang":"en","type":"article","venue":"AIAA Journal","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":93,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"McGill University","keywords":"Mechanics; Vortex; Transverse plane; Physics; Excitation; Wake; Jet (fluid); Vortex ring; Penetration (warfare); Acoustics; Structural engineering; Mathematics; Engineering","score_opus":0.0026531152326468715,"score_gpt":0.18329490867842818,"score_spread":0.1806417934457813,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2038462466","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.48965213,0.00046784463,0.49980772,0.000080785314,0.00057659205,0.000101544065,0.000005239258,0.000031582997,0.0092765875],"genre_scores_gemma":[0.99152863,0.00011225529,0.008062404,0.0000076437545,0.00019462316,0.0000014988502,0.0000022518577,0.000013221332,0.000077489574],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994442,0.000009778013,0.0002867625,0.000038122602,0.000098755976,0.00012237528],"domain_scores_gemma":[0.9998021,0.000029459135,0.000046907713,0.000054727636,0.000045044264,0.000021720449],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016283836,0.000061281455,0.00015391923,0.000103234044,0.000025055719,0.000027498061,0.00006945314,0.000043259126,0.000052591742],"category_scores_gemma":[0.0000314319,0.000055846103,0.000044939763,0.00010630439,0.000014589894,0.000060653045,0.0000065110007,0.00014467262,0.0000016712585],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000012295428,0.000016149972,0.0007538485,0.0000057436573,0.000007758439,0.000010402278,0.00001485934,0.9962974,0.0017993121,0.00040595717,0.0002422184,0.0004340185],"study_design_scores_gemma":[0.0018388234,0.00001216398,0.0015308055,0.000022693983,0.000005785278,0.000020059202,0.000008035703,0.9948279,0.00012539858,0.0014829868,0.000065524495,0.000059802158],"about_ca_topic_score_codex":0.0000075295006,"about_ca_topic_score_gemma":0.000014953241,"teacher_disagreement_score":0.5018765,"about_ca_system_score_codex":0.00004925785,"about_ca_system_score_gemma":0.000019657124,"threshold_uncertainty_score":0.2277338},"labels":[],"label_agreement":null},{"id":"W2039380683","doi":"10.1080/00221680209499890","title":"A study of a buoyant axisymmetric jet in a small co-flow","year":2002,"lang":"en","type":"article","venue":"Journal of Hydraulic Research","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":18,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"","keywords":"Mechanics; Plume; Entrainment (biomusicology); Turbulence; Jet (fluid); Physics; Flow (mathematics); Rotational symmetry; Sink (geography); Classical mechanics; Meteorology","score_opus":0.10208091992198974,"score_gpt":0.33576419961880255,"score_spread":0.2336832796968128,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2039380683","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9895796,0.00093671534,0.000522239,0.00006854799,0.00015040868,0.00022079448,0.000003388709,0.000009277022,0.008509034],"genre_scores_gemma":[0.9982499,0.00073334057,0.0007529799,0.0000058096134,0.00013050497,0.000005845889,2.9708048e-7,0.000029394278,0.00009192696],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9978434,0.00015652404,0.00070227386,0.00011536714,0.0007763716,0.00040605722],"domain_scores_gemma":[0.99886024,0.00037820413,0.000092915856,0.00025772027,0.00027848568,0.00013242192],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0021484275,0.00012246847,0.00039642936,0.0013803256,0.0000399947,0.00003990724,0.0004796392,0.00007547519,0.00010925876],"category_scores_gemma":[0.00042328096,0.000100648525,0.00008176473,0.0014369048,0.00004877628,0.00008061736,0.00006468906,0.0010672767,0.000022735612],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00026468828,0.0068274806,0.03214349,0.00055475504,0.0006507744,0.0054677175,0.015087737,0.83355856,0.01131463,0.0001949954,0.024149377,0.06978582],"study_design_scores_gemma":[0.0027529472,0.002469068,0.0139464475,0.00016775118,0.00002095913,0.00016535887,0.0021048088,0.9759628,0.00033354296,0.00042687097,0.0014325433,0.00021690976],"about_ca_topic_score_codex":0.000049397953,"about_ca_topic_score_gemma":0.00012956753,"teacher_disagreement_score":0.14240426,"about_ca_system_score_codex":0.00014882254,"about_ca_system_score_gemma":0.000028091321,"threshold_uncertainty_score":0.46368456},"labels":[],"label_agreement":null},{"id":"W2040747143","doi":"10.1063/1.3207837","title":"Natural versus forced convection in laminar starting plumes","year":2009,"lang":"en","type":"article","venue":"Physics of Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":31,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto","funders":"","keywords":"Buoyancy; Plume; Physics; Laminar flow; Mechanics; Reynolds number; Jet (fluid); Momentum (technical analysis); Richardson number; Dimensionless quantity; Natural convection; Convection; Turbulence; Thermodynamics","score_opus":0.00860036731251133,"score_gpt":0.22618934381026484,"score_spread":0.21758897649775352,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2040747143","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9868609,0.0001363742,0.010096439,0.000020939888,0.00056904333,0.00006209057,0.000004094783,0.00007770371,0.0021724545],"genre_scores_gemma":[0.9986217,0.000026661763,0.001177458,0.000010485237,0.00011968739,0.0000017445058,0.000008932645,0.000012122163,0.000021234639],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995136,0.000005003323,0.00015381182,0.00008139161,0.000093902265,0.0001522937],"domain_scores_gemma":[0.9997905,0.000036717447,0.000018231376,0.00010885302,0.000028027674,0.000017702183],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00005549344,0.00008843976,0.00012634583,0.000029294619,0.00001855214,0.000008940677,0.0000754629,0.000033462606,0.0000029097382],"category_scores_gemma":[0.000017662303,0.00009767395,0.00003901427,0.00013185598,0.000015803245,0.00010070281,0.000010129835,0.00013030534,0.0000029264431],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00007740918,0.00006840802,0.00028403374,0.0000917101,0.00004171293,0.000005760389,0.00091368094,0.29759896,0.63304,0.019434744,0.0003216361,0.048121948],"study_design_scores_gemma":[0.0005677065,0.00007590257,0.0012705843,0.00002884095,0.000009170461,1.7140819e-7,0.000067687426,0.9776415,0.01491687,0.005251808,0.000034088032,0.00013567111],"about_ca_topic_score_codex":0.0000070955743,"about_ca_topic_score_gemma":0.000006187654,"teacher_disagreement_score":0.68004256,"about_ca_system_score_codex":0.000049558614,"about_ca_system_score_gemma":0.0000060210464,"threshold_uncertainty_score":0.3983028},"labels":[],"label_agreement":null},{"id":"W2041555985","doi":"10.1115/1.4003935","title":"Flow-Induced Noise and Vibration in Aircraft Cylindrical Cabins: Closed-Form Analytical Model Validation","year":2011,"lang":"en","type":"article","venue":"Journal of vibration and acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":17,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Victoria","funders":"","keywords":"Fuselage; Noise (video); Context (archaeology); Turbulence; Vibration; Acoustics; Boundary layer; Engineering; Aeroacoustics; Flow (mathematics); Range (aeronautics); Jet (fluid); Structural acoustics; Sound pressure; Structural engineering; Mechanics; Aerospace engineering; Physics; Computer science; Geology","score_opus":0.02394716698368661,"score_gpt":0.23533414399020566,"score_spread":0.21138697700651904,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2041555985","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.49673694,0.000030113433,0.50261325,0.000043276166,0.00013174518,0.000054508604,0.0000040679215,0.000014246682,0.00037187868],"genre_scores_gemma":[0.957549,0.00027236663,0.041942872,0.000064974185,0.00012903074,0.0000013536174,0.0000064698434,0.000019984549,0.000013961519],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9990048,0.000017667262,0.0005276238,0.000103169245,0.00019862156,0.00014813436],"domain_scores_gemma":[0.9995399,0.0000424305,0.000105025676,0.000081850834,0.00011258073,0.00011820473],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025704422,0.0001382946,0.00021363795,0.0001510689,0.000049756916,0.00006182136,0.00006632666,0.0001498959,0.000016296579],"category_scores_gemma":[0.00007817848,0.00012696952,0.000036642934,0.00012957265,0.000029369101,0.00041298047,0.000021714137,0.00030397894,0.0000014347623],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00005951763,0.00013115989,0.00072979496,0.00008830907,0.000039316485,0.000030057867,0.0013092738,0.9236023,0.05825695,0.0020501437,0.00018217551,0.013521016],"study_design_scores_gemma":[0.0004989647,0.00010529622,0.0066470383,0.000037152207,0.000055136818,0.00003022213,0.00010856912,0.9895629,0.00073547533,0.0020738333,0.0000056931667,0.00013968929],"about_ca_topic_score_codex":0.0000017140609,"about_ca_topic_score_gemma":0.0000044108288,"teacher_disagreement_score":0.46081206,"about_ca_system_score_codex":0.00005756971,"about_ca_system_score_gemma":0.00004383741,"threshold_uncertainty_score":0.51776665},"labels":[],"label_agreement":null},{"id":"W2042084416","doi":"10.1063/1.2740709","title":"Self-similarity of coflowing jets: The virtual origin","year":2007,"lang":"en","type":"article","venue":"Physics of Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":37,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Queen's University","funders":"","keywords":"Physics; Mechanics; Jet (fluid); Body orifice; Turbulence; RADIUS; Boundary layer; Plane (geometry); Rotational symmetry; Classical mechanics; Geometry","score_opus":0.010545694305144147,"score_gpt":0.23360335211827055,"score_spread":0.2230576578131264,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2042084416","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.75299275,0.00016187316,0.23976576,0.000017023396,0.0005450979,0.000105994906,0.000032932683,0.00010841312,0.0062701628],"genre_scores_gemma":[0.99569917,0.00005931162,0.003973371,0.000017247185,0.00020817581,0.000001476831,0.000005047658,0.000024519184,0.00001168853],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992543,0.000007785132,0.000254709,0.00008723424,0.00020572536,0.00019024473],"domain_scores_gemma":[0.9994363,0.0001494071,0.000030225568,0.00028185992,0.00006903858,0.000033144755],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00032856132,0.00011432262,0.0001779691,0.000021703729,0.00003946392,0.0000072661837,0.00024057137,0.000051776464,0.000006244724],"category_scores_gemma":[0.000014942286,0.00009513516,0.00008497693,0.0001799113,0.000060768776,0.00006598602,0.00004589527,0.00017190386,0.000003587719],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000350731,0.0004349778,0.0038904327,0.0006345894,0.0006099594,0.000011632606,0.0038888666,0.20101246,0.45668954,0.30128822,0.002107696,0.029396556],"study_design_scores_gemma":[0.00049152365,0.000099948964,0.001740065,0.00006750914,0.000115682546,0.0000016919956,0.00026378167,0.90302694,0.0814211,0.009226602,0.0031700404,0.0003751278],"about_ca_topic_score_codex":0.000008023702,"about_ca_topic_score_gemma":0.000003495318,"teacher_disagreement_score":0.70201445,"about_ca_system_score_codex":0.000032398897,"about_ca_system_score_gemma":0.000015554637,"threshold_uncertainty_score":0.3879499},"labels":[],"label_agreement":null},{"id":"W2043989108","doi":"10.2514/1.j053311","title":"Influence of Hot-Wire Probe and Traverse on Low-Reynolds-Number Airfoil Experiments","year":2014,"lang":"en","type":"article","venue":"AIAA Journal","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Waterloo","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Reynolds number; Airfoil; Traverse; Mechatronics; Mechanical engineering; Engineering; Physics; Mechanics; Aerospace engineering; Electrical engineering; Geology; Turbulence; Geodesy","score_opus":0.0044979670766444515,"score_gpt":0.2104757921970076,"score_spread":0.20597782512036314,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2043989108","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99547106,0.00003668437,0.0017730527,0.000026436255,0.00020230202,0.00004418732,0.0000034084064,0.000024416966,0.0024184373],"genre_scores_gemma":[0.9984092,0.00012167865,0.0011837191,0.00007070053,0.0001197758,0.0000021562137,6.7236044e-7,0.000023750672,0.000068311885],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99931747,0.000016062468,0.00021694807,0.00009164686,0.0001753952,0.00018246757],"domain_scores_gemma":[0.9996221,0.00003102198,0.000052787924,0.00015152205,0.000042978198,0.000099593875],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00014715696,0.00012194513,0.00014688478,0.000039570536,0.00006257015,0.000028886208,0.00014470231,0.000064361244,0.0000365929],"category_scores_gemma":[0.000039388648,0.000109312045,0.000037209138,0.000051179046,0.000044229393,0.00009378497,0.000030327776,0.00026008254,0.000019965742],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000074898126,0.00021587055,0.008520534,0.00030672495,0.00021770944,0.00008344728,0.0021992398,0.7657326,0.19453244,0.004074062,0.0046628905,0.019379599],"study_design_scores_gemma":[0.005475336,0.0008223943,0.10143298,0.0017996457,0.00014680576,0.0007269274,0.000629899,0.80783665,0.06431104,0.010239938,0.00485128,0.0017270817],"about_ca_topic_score_codex":0.0000028258066,"about_ca_topic_score_gemma":0.0000011421035,"teacher_disagreement_score":0.13022138,"about_ca_system_score_codex":0.00003222473,"about_ca_system_score_gemma":0.000009799878,"threshold_uncertainty_score":0.4457616},"labels":[],"label_agreement":null},{"id":"W2044227407","doi":"10.2514/6.2008-2977","title":"Configuration Effects on Acoustic Performance of a Duct Liner","year":2008,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":6,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lockheed Martin (Canada)","funders":"Langley Research Center; National Aeronautics and Space Administration","keywords":"Acoustics; Computer science; Duct (anatomy); Physics; Medicine; Anatomy","score_opus":0.006494593268924002,"score_gpt":0.18545271349615872,"score_spread":0.1789581202272347,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2044227407","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.96268773,0.000023296785,0.018979657,0.0000063153434,0.00032793448,0.00007963243,0.0000015665598,0.000095373834,0.017798465],"genre_scores_gemma":[0.9982266,0.00010247539,0.000982534,0.000030995547,0.000119277305,0.000005252161,0.0000046322193,0.000014577478,0.0005136799],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99960786,0.0000037681048,0.000113449874,0.00006349816,0.00010279794,0.0001086106],"domain_scores_gemma":[0.99976486,0.000051957246,0.000013504008,0.000115690986,0.00003099856,0.000022993854],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000039176914,0.00007613048,0.00009713109,0.000026876707,0.00003173363,0.0000026491937,0.000049998456,0.000045390665,0.000040878895],"category_scores_gemma":[0.000018477305,0.00006488373,0.000021595377,0.00006481911,0.000016922468,0.000033609358,0.000005547505,0.00008631469,0.000038922113],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000006441616,0.000011725332,0.00024606238,0.00013579254,0.0000128031825,0.000005116266,0.000041007625,0.92839754,0.067641936,0.00042184375,0.0016140835,0.0014656741],"study_design_scores_gemma":[0.00015682683,0.0001031764,0.0053730723,0.00003187497,0.0000075926173,0.0000059775944,0.0000024644899,0.9620492,0.032036394,0.000018444278,0.000120697936,0.00009431587],"about_ca_topic_score_codex":0.0000014966408,"about_ca_topic_score_gemma":0.000001631834,"teacher_disagreement_score":0.035605546,"about_ca_system_score_codex":0.000015638334,"about_ca_system_score_gemma":0.0000075042226,"threshold_uncertainty_score":0.26458818},"labels":[],"label_agreement":null},{"id":"W2044914967","doi":"10.1016/j.jsv.2013.03.023","title":"Use of a beat effect for the automatic positioning of flow obstructions to control tonal fan noise: Theory and experiments","year":2013,"lang":"en","type":"article","venue":"Journal of Sound and Vibration","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":10,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"AUTO21 Network of Centres of Excellence; Centre Technique des Industries Mécaniques","keywords":"Beat (acoustics); Acoustics; Noise (video); Speech recognition; Computer science; Physics; Artificial intelligence","score_opus":0.007881685634643315,"score_gpt":0.23039207654434699,"score_spread":0.22251039090970368,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2044914967","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.63865304,0.00010442571,0.3609796,0.000024281506,0.00009811293,0.0001253288,0.000008433079,0.0000026546659,0.000004139687],"genre_scores_gemma":[0.992076,0.000012439823,0.007813296,0.000017831255,0.00006195859,0.000007133543,0.0000013225929,0.000006351308,0.000003696854],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996319,0.000018817254,0.00020099618,0.000029999435,0.00006930016,0.000049031307],"domain_scores_gemma":[0.99939555,0.0003950612,0.000075166165,0.000038858867,0.0000673203,0.000028051121],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016042446,0.000051240826,0.00011223588,0.00003954267,0.00006084815,0.000049177987,0.000026734278,0.000024209992,0.000008428292],"category_scores_gemma":[0.00006013012,0.000034492183,0.00003252337,0.00002771513,0.00002294429,0.00019138555,0.0000054663014,0.00004378655,1.0596151e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00009963224,0.00003347655,0.0014852325,0.00023218346,0.00032154878,4.1554128e-7,0.0019159687,0.2857837,0.6849347,0.0036715344,0.0001587469,0.021362841],"study_design_scores_gemma":[0.0005472362,0.00026357884,0.013740937,0.000084871106,0.000090549016,0.000018546007,0.00021058509,0.9773673,0.00442678,0.003188819,0.000005511899,0.000055304576],"about_ca_topic_score_codex":0.0000018140709,"about_ca_topic_score_gemma":7.6206646e-7,"teacher_disagreement_score":0.6915836,"about_ca_system_score_codex":0.000010520653,"about_ca_system_score_gemma":0.0000042575875,"threshold_uncertainty_score":0.14065504},"labels":[],"label_agreement":null},{"id":"W2045558374","doi":"10.3390/coatings3040208","title":"A Study of a Powder Coating Gun near Field: A Case of Staggered Concentric Jet Flow","year":2013,"lang":"en","type":"article","venue":"Coatings","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Queen's University","funders":"Government of Ontario","keywords":"Mechanics; Gambit; Jet (fluid); Reynolds-averaged Navier–Stokes equations; Nozzle; Turbulence; Pitot tube; Coaxial; Fluent; Materials science; Flow (mathematics); Computational fluid dynamics; Mechanical engineering; Physics; Engineering","score_opus":0.009403457990862299,"score_gpt":0.22671497473047944,"score_spread":0.21731151673961713,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2045558374","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99544615,0.00005744068,0.003045468,0.000011339882,0.00015497125,0.0004105453,0.00001608952,0.000065053806,0.0007929462],"genre_scores_gemma":[0.994944,0.0000046376813,0.0049035284,0.000025089788,0.00003182918,0.000026793337,0.0000035168757,0.000028441911,0.00003220591],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99907386,0.000021288173,0.00042019246,0.0001377565,0.00014005268,0.00020682055],"domain_scores_gemma":[0.9992016,0.00022346794,0.000115108116,0.00025321293,0.00015069741,0.000055888137],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012320366,0.00013998388,0.00027735726,0.000039418588,0.000055249842,0.000029155932,0.00013054756,0.000064381966,0.00018616453],"category_scores_gemma":[0.000226112,0.00013404786,0.00004559909,0.00021702674,0.000031907213,0.00006943202,0.00006966865,0.00015701892,0.000007809783],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000059240036,0.0019328395,0.067655645,0.0025861047,0.00071668695,0.0015635684,0.11164773,0.514348,0.20114587,0.00075293443,0.022009179,0.075582206],"study_design_scores_gemma":[0.0010574068,0.0003356493,0.00039508936,0.00008032572,0.000050168856,0.000057671517,0.0065926644,0.9884795,0.0025664032,0.00009750268,0.00005157232,0.00023607089],"about_ca_topic_score_codex":0.0005625355,"about_ca_topic_score_gemma":0.00006744867,"teacher_disagreement_score":0.4741315,"about_ca_system_score_codex":0.000021621669,"about_ca_system_score_gemma":0.000016704733,"threshold_uncertainty_score":0.5466313},"labels":[],"label_agreement":null},{"id":"W2046048581","doi":"10.1121/1.4802898","title":"Reproduction of random pressure fields based on planar nearfield acoustic holography","year":2013,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":22,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Plane (geometry); Planar; Turbulence; Boundary layer; Acoustics; Physics; Supersonic speed; Boundary (topology); Planar array; Acoustic holography; Optics; Holography; Mechanics; Mathematics; Geometry; Computer science; Mathematical analysis","score_opus":0.005592753340007366,"score_gpt":0.2010378281275705,"score_spread":0.19544507478756315,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2046048581","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.043988913,0.00044935016,0.9508453,0.0029783975,0.00084081537,0.00028047257,0.000017999344,0.00002832244,0.0005704052],"genre_scores_gemma":[0.9870369,0.00035611432,0.011907268,0.0004410889,0.00020263299,0.0000020309817,4.0864663e-7,0.000018080998,0.00003550924],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99875176,0.00007701203,0.00044359468,0.00008624552,0.00045752194,0.00018386239],"domain_scores_gemma":[0.9983059,0.0006736196,0.00027928938,0.0004573109,0.0002311922,0.000052656887],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005399914,0.00013712725,0.00033095537,0.000025899591,0.00008194035,0.000010697549,0.00047895507,0.000115288836,0.00009252506],"category_scores_gemma":[0.0003414286,0.00007514065,0.00038565832,0.00023424566,0.00035023846,0.000048351398,0.00003568647,0.0006120823,0.0000017299158],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000073511605,0.000062589774,0.000045209494,0.00008913417,0.00016813035,2.7883902e-7,0.0001572462,0.93199366,0.018284969,0.0000020052862,0.04643691,0.002686351],"study_design_scores_gemma":[0.00046213611,0.00025860217,0.0007664879,0.000083641746,0.00033780764,0.000009491873,0.00032665883,0.9957082,0.000988089,0.00054927316,0.00041935148,0.000090242065],"about_ca_topic_score_codex":0.000027720129,"about_ca_topic_score_gemma":3.0254495e-7,"teacher_disagreement_score":0.94304794,"about_ca_system_score_codex":0.000018065306,"about_ca_system_score_gemma":0.000027918484,"threshold_uncertainty_score":0.3064147},"labels":[],"label_agreement":null},{"id":"W2046673939","doi":"10.1115/pvp2014-28315","title":"Flow Around a Leading Edge Slat: Part II — Cove Flow Dynamics via Snapshot POD","year":2014,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of New Brunswick","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Cove; Vorticity; Reynolds number; Trailing edge; Mechanics; Shear (geology); Leading edge; Turbulence; Geometry; Geology; Materials science; Physics; Vortex; Mathematics; Composite material","score_opus":0.0067353540139797035,"score_gpt":0.19684659928316203,"score_spread":0.19011124526918233,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2046673939","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.06744487,0.00006976849,0.7912071,0.00012430281,0.0030243087,0.0001903221,0.000063305226,0.00048609343,0.13738996],"genre_scores_gemma":[0.972442,0.000041969364,0.024152363,0.0001923963,0.0007188702,0.000013444499,0.0002473235,0.00010478558,0.0020868715],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9984392,0.000019490888,0.00037874747,0.0003356065,0.00023655042,0.00059043564],"domain_scores_gemma":[0.999115,0.00010734889,0.000037610615,0.0005093852,0.00005643091,0.00017422234],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00028082394,0.0003458471,0.00036116707,0.000092468035,0.00020206773,0.00010172985,0.000308999,0.00020780163,0.00060679595],"category_scores_gemma":[0.000054963737,0.00034549733,0.00012558636,0.00019353114,0.00005353291,0.00015728624,0.0001244896,0.00038178597,0.00022322842],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000059630875,0.000048456972,0.000161064,0.00008996875,0.00009140075,0.000008967227,0.0001558403,0.9428636,0.0012898332,0.007854545,0.011546016,0.035884354],"study_design_scores_gemma":[0.00030310106,0.00005797495,0.00005180203,0.00003531724,0.00003664658,0.000014691732,0.00003460223,0.98555887,0.00010830893,0.0019817303,0.011351605,0.00046532677],"about_ca_topic_score_codex":0.00001296504,"about_ca_topic_score_gemma":0.00035709978,"teacher_disagreement_score":0.9049971,"about_ca_system_score_codex":0.00020783974,"about_ca_system_score_gemma":0.000015012225,"threshold_uncertainty_score":0.9998997},"labels":[],"label_agreement":null},{"id":"W2049318166","doi":"10.1115/1.4029695","title":"Investigation of Tabs in Short Annular Diffusers With Swirling Flow","year":2015,"lang":"en","type":"article","venue":"Journal of Engineering for Gas Turbines and Power","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Queen's University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Inlet; Diffuser (optics); Mechanics; Computational fluid dynamics; Stall (fluid mechanics); Reynolds number; Flow separation; Boundary layer; Flow (mathematics); Materials science; Geometry; Optics; Physics; Mathematics; Engineering; Turbulence; Mechanical engineering","score_opus":0.010149940609345962,"score_gpt":0.19227895574865306,"score_spread":0.1821290151393071,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2049318166","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.96009934,0.0006105042,0.038753062,0.000026230262,0.0003951506,0.000064632404,0.000005625804,0.000012985682,0.000032493837],"genre_scores_gemma":[0.98057264,0.000066552406,0.019228904,0.0000057350194,0.00009013201,0.000001839894,0.0000022685458,0.000027238446,0.000004712339],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99941766,0.0000024946896,0.00028248623,0.00005382291,0.00011662066,0.00012693318],"domain_scores_gemma":[0.99965286,0.000035036483,0.000032699747,0.00006422132,0.00012210749,0.00009304802],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00022233154,0.000110316716,0.00021269346,0.00013796095,0.000007638727,0.0000148830995,0.000063777996,0.00005200169,9.1134564e-7],"category_scores_gemma":[0.000048685008,0.00008885259,0.00003595095,0.00010547611,0.000014615104,0.00011890699,0.000008362645,0.00013329265,5.033762e-8],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000024046152,0.000005559535,0.004261108,0.00009347852,0.000033151904,0.000007150953,0.00036329878,0.9860622,0.008772028,0.00009162726,0.00011777832,0.00016857249],"study_design_scores_gemma":[0.0006997825,0.0002477195,0.0038504137,0.00025487557,0.000030809388,0.00005063333,0.000106213476,0.99207276,0.0016477784,0.00014660538,0.0007305924,0.00016184428],"about_ca_topic_score_codex":0.0000016695136,"about_ca_topic_score_gemma":0.000003325637,"teacher_disagreement_score":0.020473301,"about_ca_system_score_codex":0.000030680378,"about_ca_system_score_gemma":0.000016796987,"threshold_uncertainty_score":0.36233035},"labels":[],"label_agreement":null},{"id":"W2049802114","doi":"10.2514/6.2006-313","title":"Investigation of the Large Scale Flow Structures in Dual Planar Attaching Jets","year":2006,"lang":"en","type":"article","venue":"44th AIAA Aerospace Sciences Meeting and Exhibit","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Planar; Dual (grammatical number); Scale (ratio); Flow (mathematics); Computer science; Materials science; Physics; Mechanics; Computer graphics (images); Art","score_opus":0.007276523697330423,"score_gpt":0.20302536672955124,"score_spread":0.19574884303222082,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2049802114","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9961099,0.00031563445,0.0005646405,0.00014980538,0.00032286506,0.00008438335,0.000016134936,0.000046439614,0.0023901649],"genre_scores_gemma":[0.9942396,0.000017062774,0.005572607,0.000029506222,0.000084156025,0.000002289498,0.0000034008258,0.000010651411,0.000040684317],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.998988,0.00003447589,0.00022002815,0.00020201308,0.0002591188,0.00029640086],"domain_scores_gemma":[0.99968857,0.000067642686,0.000062438754,0.00012490824,0.00001799915,0.00003843929],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000651405,0.00012479445,0.00014197452,0.00006204045,0.00025158553,0.00006643691,0.0001347293,0.00006469082,0.0000028315712],"category_scores_gemma":[0.00004767368,0.00009305146,0.000030324989,0.0003473617,0.00021928329,0.0001066641,0.0000516106,0.00017341497,6.805759e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000022591414,0.0000065941726,0.22167471,0.000086215245,0.0000037865252,0.0000021019346,0.0015605604,0.7245802,0.049451835,0.0017996975,0.00058321905,0.00024882262],"study_design_scores_gemma":[0.0003251971,0.000026637346,0.113641486,0.00024246128,0.00001126418,0.000009297359,0.0008558186,0.87123173,0.009298053,0.0040017287,0.00009845167,0.00025784865],"about_ca_topic_score_codex":0.00020627143,"about_ca_topic_score_gemma":0.0015116278,"teacher_disagreement_score":0.14665155,"about_ca_system_score_codex":0.0000243197,"about_ca_system_score_gemma":0.000023547347,"threshold_uncertainty_score":0.37945282},"labels":[],"label_agreement":null},{"id":"W2050116964","doi":"10.1121/1.2934278","title":"Effects of notches on span wise correlation of surface pressure fluctuations downstream of a wall-mounted spoiler","year":2008,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"","keywords":"Lattice Boltzmann methods; Mechanics; Vortex; Materials science; Drag; Flow (mathematics); Turbulence; Span (engineering); Acoustics; Physics; Structural engineering","score_opus":0.005221756785078662,"score_gpt":0.2079170421335586,"score_spread":0.20269528534847994,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2050116964","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8143824,0.0003564846,0.1844004,0.00027190894,0.00021785752,0.00018309265,0.000036265188,0.000010656408,0.00014094339],"genre_scores_gemma":[0.98961,0.00089047727,0.009341147,0.00004325894,0.000046301695,4.784315e-7,0.0000010414246,0.000019894416,0.000047381098],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99866104,0.000070266455,0.0005681876,0.00006100531,0.000489651,0.0001498709],"domain_scores_gemma":[0.99776083,0.0010879309,0.00054810167,0.0002691366,0.00028641528,0.00004759998],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00026752174,0.0001418061,0.00043003392,0.0000213619,0.000065640466,0.0000021863111,0.00037847442,0.00009458844,0.00001918954],"category_scores_gemma":[0.00028235305,0.00008594186,0.0003369905,0.00026373996,0.00056381716,0.000048437374,0.00005598546,0.00038020484,7.252353e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000687611,0.00014772262,0.000146452,0.00021132437,0.0002894089,3.6324275e-7,0.0011044813,0.86165434,0.13375346,0.000009184978,0.002072032,0.00054244953],"study_design_scores_gemma":[0.00039779677,0.00026004273,0.009686099,0.000252809,0.00049650454,0.0000107695105,0.00027789013,0.9719359,0.016372524,0.00016891058,0.000055063647,0.00008568748],"about_ca_topic_score_codex":0.000039183607,"about_ca_topic_score_gemma":4.4369685e-7,"teacher_disagreement_score":0.17522763,"about_ca_system_score_codex":0.000030538904,"about_ca_system_score_gemma":0.00005139648,"threshold_uncertainty_score":0.35046074},"labels":[],"label_agreement":null},{"id":"W2050291671","doi":"10.2514/6.2013-2213","title":"3D Source localization in a closed wind-tunnel using microphone arrays","year":2013,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":12,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Natural Sciences and Engineering Research Council of Canada; Pratt and Whitney Canada","keywords":"Microphone; Acoustics; Wind tunnel; Computer science; Microphone array; Aerospace engineering; Engineering; Physics; Loudspeaker","score_opus":0.007138243323469464,"score_gpt":0.1870380323374765,"score_spread":0.17989978901400705,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2050291671","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.43236133,0.000028063003,0.56600195,0.000009247459,0.00019328606,0.000094818635,9.27006e-7,0.00008903411,0.0012213461],"genre_scores_gemma":[0.9704814,0.0000178277,0.029047837,0.00008751279,0.000072894974,0.0000035882076,0.000007373219,0.000039289294,0.00024230947],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99938536,0.000008091713,0.00019224762,0.00011982423,0.00007949138,0.00021497067],"domain_scores_gemma":[0.9997504,0.000016610362,0.000015713033,0.00014510755,0.000028872439,0.000043346452],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000054018612,0.00011506879,0.000118593656,0.00007736874,0.000032033193,0.000041761978,0.000083177685,0.000082577426,0.00025221467],"category_scores_gemma":[0.000010783012,0.00011494605,0.000022871256,0.00019665998,0.00001777219,0.00008555791,0.000023137032,0.00011226062,0.00009095685],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[5.2544993e-7,0.0000111877025,0.00028565538,0.00001908049,0.0000053722247,0.0000013867057,0.0001486677,0.8488788,0.14919004,0.000025798743,0.00037185897,0.0010616415],"study_design_scores_gemma":[0.00019679406,0.000004502929,0.00031123217,0.000021232527,0.0000043560976,0.0000023075447,0.00011621505,0.99757606,0.0009183747,0.00020303857,0.0004911461,0.0001547418],"about_ca_topic_score_codex":0.00021828139,"about_ca_topic_score_gemma":0.000079521255,"teacher_disagreement_score":0.53812003,"about_ca_system_score_codex":0.000080181315,"about_ca_system_score_gemma":0.000007910083,"threshold_uncertainty_score":0.46873638},"labels":[],"label_agreement":null},{"id":"W2051511517","doi":"10.1115/fedsm2007-37167","title":"Effect of Shear Layer Interaction on Acoustic Response of Coaxial Side Branch Resonators","year":2007,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Victoria","funders":"","keywords":"Acoustics; Resonator; Particle image velocimetry; Shear (geology); Coaxial; Amplitude; Acoustic wave; Oscillation (cell signaling); Physics; Optics; Turbulence; Mechanics; Materials science; Engineering; Telecommunications; Chemistry","score_opus":0.006239420383428834,"score_gpt":0.25717748260732715,"score_spread":0.2509380622238983,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2051511517","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.95284784,0.000016509355,0.040884793,0.000005283271,0.00060677755,0.000115722956,0.000008634149,0.00006965665,0.00544478],"genre_scores_gemma":[0.9994157,0.000007891142,0.0003367901,0.000011093415,0.00006058761,0.0000018440646,0.000002481137,0.000027961647,0.00013567784],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9992262,0.00004723659,0.0002810103,0.000103108214,0.00017833879,0.00016408596],"domain_scores_gemma":[0.99851114,0.0011842633,0.00003892753,0.00018538597,0.000036557783,0.000043717213],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00096313393,0.0001193816,0.00019585813,0.0001370948,0.000016680173,0.00000430839,0.00008252335,0.000092056835,0.000059095404],"category_scores_gemma":[0.0002657161,0.000103450024,0.000065591135,0.00013211374,0.000036636873,0.000037942933,0.000017549395,0.00017084547,0.000013003591],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.003101775,0.000044814813,0.00027084994,0.00024720244,0.000051117127,0.000012627802,0.00016303314,0.40280503,0.58107036,0.00034613564,0.00057311077,0.011313957],"study_design_scores_gemma":[0.0010818982,0.00147471,0.0058648298,0.00019129031,0.00006006581,0.0000074968116,0.00009375663,0.3371188,0.65313965,0.00009641595,0.0005888183,0.0002823003],"about_ca_topic_score_codex":0.000014844273,"about_ca_topic_score_gemma":0.000018048639,"teacher_disagreement_score":0.07206928,"about_ca_system_score_codex":0.000063911946,"about_ca_system_score_gemma":0.000007427723,"threshold_uncertainty_score":0.42185694},"labels":[],"label_agreement":null},{"id":"W2052204224","doi":"10.1016/j.euromechflu.2006.10.005","title":"Experimental study of the near field and transition region of a free jet issuing from a sharp-edged elliptic orifice plate","year":2006,"lang":"en","type":"article","venue":"European Journal of Mechanics - B/Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":81,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"St. Francis Xavier University","funders":"","keywords":"Jet (fluid); Mechanics; Body orifice; Reynolds number; Physics; Nozzle; Vorticity; Vortex; Turbulence; Thermodynamics","score_opus":0.010257124572108759,"score_gpt":0.19566086098172594,"score_spread":0.1854037364096172,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2052204224","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.90487534,0.00081162853,0.09345111,0.00003533253,0.00047400602,0.00011368356,0.000013274618,0.000013778856,0.00021183853],"genre_scores_gemma":[0.9978229,0.000064933076,0.0018740402,0.00001598681,0.00016933792,4.742192e-7,0.0000014509205,0.000040775427,0.000010147717],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9988247,0.000137417,0.0005472079,0.00010794692,0.00026032448,0.00012240674],"domain_scores_gemma":[0.9993709,0.000064902095,0.00018668926,0.0002610047,0.00007455491,0.000041967505],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004408269,0.00014559117,0.00026342523,0.000054392833,0.000064966545,0.0000318741,0.0003193965,0.000035951958,0.000015434465],"category_scores_gemma":[0.00003437051,0.000114865,0.00009544354,0.000105909705,0.000016637772,0.000085903426,0.000059260088,0.0003019295,7.720821e-7],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00019057673,0.0005365891,0.000090985326,0.00007728882,0.00025079778,0.00026193392,0.0072448063,0.06621601,0.9217713,0.00086557184,0.0013995122,0.001094635],"study_design_scores_gemma":[0.0049260054,0.0028000772,0.0008150455,0.0008609879,0.00043073785,0.00017406272,0.0039706402,0.87001896,0.11368644,0.0015855414,0.00026507213,0.00046642844],"about_ca_topic_score_codex":0.000021463653,"about_ca_topic_score_gemma":0.000006065417,"teacher_disagreement_score":0.80808485,"about_ca_system_score_codex":0.000025158488,"about_ca_system_score_gemma":0.000010377814,"threshold_uncertainty_score":0.46840584},"labels":[],"label_agreement":null},{"id":"W2052556749","doi":"10.1115/gt2003-38592","title":"Aerodynamic and Aeroacoustic Performance of a Skewed Rotor","year":2003,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":10,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Royal Military College of Canada","funders":"","keywords":"Aerodynamics; Wake; Stall (fluid mechanics); Mechanical fan; Acoustics; Anechoic chamber; Boundary layer; Mach number; Noise (video); Rotor (electric); Noise reduction; Mechanics; Engineering; Structural engineering; Physics; Mechanical engineering; Computer science","score_opus":0.0030819197443231533,"score_gpt":0.15981319598097976,"score_spread":0.1567312762366566,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2052556749","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9652328,0.00012251147,0.016555993,0.0000023256753,0.00019892918,0.00011047083,0.00000492,0.000089858884,0.017682225],"genre_scores_gemma":[0.993032,0.0001781426,0.006366379,0.000009505366,0.000012445486,0.0000090032445,0.0000016683299,0.000022614355,0.00036826095],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994795,0.0000070124956,0.00016457817,0.00010050906,0.00008460887,0.00016382463],"domain_scores_gemma":[0.99972373,0.00003232241,0.000016383785,0.00015404058,0.000025435123,0.000048087288],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00009994126,0.00010812382,0.00013762458,0.000043955723,0.00002794448,0.000009571746,0.000061769024,0.000051545445,0.000075996766],"category_scores_gemma":[0.000024702334,0.000099849225,0.00002108163,0.00009070864,0.00003951556,0.000047717724,0.000012456573,0.0000871636,0.0000072108155],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000022926617,0.00012655139,0.014107404,0.0015791102,0.00018466124,0.000010857313,0.0003494425,0.70752925,0.22985652,0.034286622,0.0010015819,0.010945074],"study_design_scores_gemma":[0.00022534649,0.00004440578,0.0042598536,0.000021113143,0.000017036971,0.000009954568,0.000031194264,0.993839,0.0010297387,0.00015225365,0.00021007497,0.00015998178],"about_ca_topic_score_codex":0.0000023386133,"about_ca_topic_score_gemma":0.000008452597,"teacher_disagreement_score":0.28630978,"about_ca_system_score_codex":0.00001923767,"about_ca_system_score_gemma":0.00000891448,"threshold_uncertainty_score":0.40717334},"labels":[],"label_agreement":null},{"id":"W2052837339","doi":"10.1260/0309-524x.37.6.637","title":"The Application of a MEMS Microphone Phased Array to Aeroacoustics of Small Wind Turbines","year":2013,"lang":"en","type":"article","venue":"Wind Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Waterloo","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Acoustics; Aeroacoustics; Microphone array; Beamforming; Anechoic chamber; Wind tunnel; Azimuth; Turbine; Microphone; Noise (video); Rotor (electric); Wind power; Acoustic source localization; Marine engineering; Aerospace engineering; Sound pressure; Physics; Engineering; Computer science; Electrical engineering; Optics; Electronic engineering; Sound (geography)","score_opus":0.004726363152313517,"score_gpt":0.17855594627089236,"score_spread":0.17382958311857885,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2052837339","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.50498396,0.00018851856,0.49396917,0.000021163412,0.00030664328,0.00023233448,0.000013551405,0.00006427839,0.00022037642],"genre_scores_gemma":[0.9808199,0.000036764235,0.018894814,0.000005867801,0.0001308064,0.0000200158,0.000005410281,0.00004998475,0.000036444744],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999176,0.000002990308,0.00033252625,0.000121652876,0.00012291587,0.00024386715],"domain_scores_gemma":[0.99936044,0.00009676489,0.000043580003,0.00032955944,0.00009494378,0.00007472232],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000104664,0.0001653071,0.00020256417,0.00007313646,0.000032753378,0.00002161591,0.00024684385,0.000073238,0.000007184335],"category_scores_gemma":[0.000047305643,0.00014090158,0.00005366456,0.00024603502,0.000024949848,0.000034685654,0.000016934971,0.0001313502,0.000013383301],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000011090365,0.000007069757,0.00001593007,0.00006283165,0.00002045128,9.3891245e-8,0.00007229157,0.45949194,0.5390666,0.00003767706,0.000044328186,0.0011796409],"study_design_scores_gemma":[0.000280407,0.00004201536,0.0017304464,0.00007570193,0.000036847097,0.0000033626657,0.000091421396,0.7356638,0.25908074,0.00007927836,0.0026097454,0.00030630128],"about_ca_topic_score_codex":0.000032297663,"about_ca_topic_score_gemma":0.0000058483583,"teacher_disagreement_score":0.47583595,"about_ca_system_score_codex":0.000034662633,"about_ca_system_score_gemma":0.000008439865,"threshold_uncertainty_score":0.57458},"labels":[],"label_agreement":null},{"id":"W2052877582","doi":"10.1007/s00348-008-0606-1","title":"PIV investigation of flowfield behind perforated Gurney-type flaps","year":2008,"lang":"en","type":"article","venue":"Experiments in Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":33,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"","keywords":"Mechanics; Type (biology); Materials science; Computer science; Geology; Physics","score_opus":0.023812872408810134,"score_gpt":0.2365984823462602,"score_spread":0.21278560993745008,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2052877582","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.992505,0.00049908244,0.0009841331,0.000009141942,0.00081950513,0.000109025415,0.0000042031347,0.000074071766,0.0049958117],"genre_scores_gemma":[0.9961621,0.0001348051,0.0032200874,0.000029197927,0.00007516791,0.000010725161,0.00002516258,0.000030371235,0.0003123811],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991774,0.000015503394,0.00030609075,0.00014161867,0.00016974105,0.00018966003],"domain_scores_gemma":[0.99963784,0.000020710391,0.000021452492,0.00021753687,0.000046412984,0.000056045592],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00008813054,0.00013902318,0.0001726648,0.0000961794,0.000043023138,0.000007426026,0.00014912445,0.00011504241,0.00014252699],"category_scores_gemma":[0.0000282079,0.0001494402,0.000027820446,0.00018978836,0.00006749259,0.00009749659,0.000034938883,0.00015978533,0.000021781729],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000019467614,0.000059328817,0.015454038,0.00004592672,0.000042096704,0.000027787464,0.0060741752,0.046740692,0.925998,0.00035187788,0.0048705065,0.0003161159],"study_design_scores_gemma":[0.00077479554,0.00012784053,0.0068431967,0.000079101956,0.000008275052,0.000009490501,0.00021403418,0.52130544,0.4694058,0.00027884697,0.00058302307,0.00037013646],"about_ca_topic_score_codex":0.000019594436,"about_ca_topic_score_gemma":0.0000041240223,"teacher_disagreement_score":0.47456476,"about_ca_system_score_codex":0.0000843724,"about_ca_system_score_gemma":0.0000392291,"threshold_uncertainty_score":0.60939944},"labels":[],"label_agreement":null},{"id":"W2052968987","doi":"10.1121/1.4805994","title":"A robust numerical approach for prediction of turbofan engine noise","year":2013,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"","keywords":"Turbofan; Turbulence; Takeoff; Jet engine; Acoustics; Nozzle; Jet noise; Noise (video); Jet (fluid); Computer science; Intermittency; Computational fluid dynamics; Sound pressure; Computational aeroacoustics; Simulation; Aeroacoustics; Physics; Mechanics; Aerospace engineering; Engineering","score_opus":0.011088499751808183,"score_gpt":0.19478392963629154,"score_spread":0.18369542988448337,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2052968987","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0112480745,0.00017144688,0.9873546,0.00047715424,0.000264255,0.0002485519,0.00005417294,0.00001803393,0.00016373383],"genre_scores_gemma":[0.7602597,0.00024812215,0.23908558,0.00009927587,0.00024173332,0.000005681918,0.000002003746,0.000027226644,0.000030665302],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9988122,0.000035447596,0.00052579056,0.00006764535,0.00033625818,0.00022264561],"domain_scores_gemma":[0.9988099,0.00035353517,0.00026113054,0.00025970614,0.00023883497,0.00007689492],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00035019402,0.00014313804,0.00035303636,0.000016250127,0.000076028984,0.000010385605,0.0005068258,0.00008654385,0.000029371156],"category_scores_gemma":[0.00014437022,0.0000788348,0.00041760347,0.00021211004,0.00028995893,0.000070425966,0.000073585186,0.0003986741,7.9551626e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00002087871,0.00009358369,0.000033602886,0.00012326532,0.00018953792,4.5616392e-8,0.00024619314,0.94955397,0.024372911,0.000005950534,0.020490266,0.004869796],"study_design_scores_gemma":[0.0002890391,0.00015859395,0.00068788254,0.000033313925,0.00023258456,0.000015694284,0.0005092647,0.99697495,0.0004611433,0.00036606693,0.00019827772,0.00007317383],"about_ca_topic_score_codex":0.000012069716,"about_ca_topic_score_gemma":2.637876e-8,"teacher_disagreement_score":0.74901164,"about_ca_system_score_codex":0.0000565715,"about_ca_system_score_gemma":0.000028199956,"threshold_uncertainty_score":0.32147896},"labels":[],"label_agreement":null},{"id":"W2054976678","doi":"10.1088/0957-0233/18/7/003","title":"Simultaneous measurement of acoustic and streaming velocities using synchronized PIV technique","year":2007,"lang":"en","type":"article","venue":"Measurement Science and Technology","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":43,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Concordia University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Particle image velocimetry; Acoustic streaming; Acoustics; Waveform; Particle velocity; Velocimetry; Amplitude; Measure (data warehouse); Phase velocity; Physics; Acoustic wave; Phase (matter); Acoustic Doppler velocimetry; Optics; Mechanics; Laser Doppler velocimetry; Computer science","score_opus":0.015475646108764583,"score_gpt":0.22550581394254768,"score_spread":0.2100301678337831,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2054976678","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6224459,0.0012300736,0.37502846,0.000031508698,0.0001721002,0.00033283472,0.0000029358303,0.00022950888,0.00052667654],"genre_scores_gemma":[0.9907467,0.00009703651,0.009109683,0.0000052596265,0.000015813175,0.000008387711,1.2836195e-7,0.000015529615,0.0000014776269],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9980156,0.00000563422,0.0002892135,0.00025779314,0.0010169968,0.00041475572],"domain_scores_gemma":[0.99875504,0.00003189632,0.000058780817,0.00021582068,0.00087270245,0.00006576156],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0031152288,0.00016460771,0.00021848785,0.00049472204,0.00020103568,0.000026966192,0.00021466614,0.0001249114,0.000002226646],"category_scores_gemma":[0.0007389363,0.00015845429,0.000013021649,0.00069208513,0.0008502286,0.000085336134,0.00010166178,0.00017514025,2.9511676e-7],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000031782874,0.000015852378,0.00027926007,0.00009763249,0.000014708056,0.000010063621,0.000044290005,0.004115469,0.9757569,0.0005154098,0.0000032490655,0.019143978],"study_design_scores_gemma":[0.0005603652,0.00020089292,0.000413973,0.00039166512,0.00008751132,0.00009941967,0.0013243889,0.5549658,0.43919027,0.0020807695,0.00017655878,0.0005084219],"about_ca_topic_score_codex":0.00001386809,"about_ca_topic_score_gemma":0.000080997284,"teacher_disagreement_score":0.55085033,"about_ca_system_score_codex":0.00051265623,"about_ca_system_score_gemma":0.00013374409,"threshold_uncertainty_score":0.64615786},"labels":[],"label_agreement":null},{"id":"W2056659040","doi":"10.2514/6.2008-2830","title":"Time-Domain Simulation of Nonlinear Acoustic Propagation in a Lined Duct","year":2008,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Kootenay Association for Science & Technology","funders":"Langley Research Center; Boeing","keywords":"Acoustics; Nonlinear system; Acoustic wave equation; Attenuation; Physics; Duct (anatomy); Frequency domain; Wave propagation; Nonlinear acoustics; Acoustic wave; Mathematical analysis; Optics; Mathematics","score_opus":0.008642690421978554,"score_gpt":0.21537758079554886,"score_spread":0.20673489037357032,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2056659040","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7830837,0.000013371148,0.21514179,0.000007728606,0.00006752472,0.00012769064,0.0000051377488,0.00007969923,0.0014733787],"genre_scores_gemma":[0.9879643,0.000014201343,0.011705371,0.0000063702396,0.00005951881,0.0000037359946,0.000020565667,0.000019449522,0.00020648955],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99945873,0.000008521092,0.0002322839,0.000083571824,0.00010635882,0.0001105292],"domain_scores_gemma":[0.99974775,0.000053746382,0.000022894412,0.000113346796,0.000040565676,0.000021700931],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00008613192,0.000079894206,0.000120756384,0.00008086519,0.000017863096,0.0000028382856,0.00005432482,0.000057170673,0.000059400736],"category_scores_gemma":[0.000044866854,0.00007734002,0.00002316413,0.00017429153,0.000027866647,0.000056610093,0.000011174035,0.00007938682,0.000024979134],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000044094445,0.000023598377,0.00010230668,0.000027900913,0.000004295867,0.0000049266932,0.0001169045,0.96792203,0.031469077,0.00002045918,0.000032870117,0.00027119092],"study_design_scores_gemma":[0.00023050414,0.000019446466,0.0006898911,0.000014972622,0.0000036290917,0.0000022498798,0.000015533184,0.99812865,0.0006737609,0.00010261532,0.00003216582,0.00008660564],"about_ca_topic_score_codex":0.00000410332,"about_ca_topic_score_gemma":0.000014505353,"teacher_disagreement_score":0.20488063,"about_ca_system_score_codex":0.000040008003,"about_ca_system_score_gemma":0.00001484287,"threshold_uncertainty_score":0.31538343},"labels":[],"label_agreement":null},{"id":"W2056799751","doi":"10.1002/aic.690470605","title":"Three‐dimensional wall jets: Axial flow in a stirred tank","year":2001,"lang":"en","type":"article","venue":"AIChE Journal","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":34,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Alberta","funders":"","keywords":"Dimensionless quantity; Baffle; Mechanics; Jet (fluid); Turbulence; Flow (mathematics); Axial compressor; Impeller; Physics; Materials science; Thermodynamics","score_opus":0.009714602448886778,"score_gpt":0.2122450918362542,"score_spread":0.20253048938736742,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2056799751","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.95114297,0.0006727294,0.04370458,0.0006162077,0.0017088826,0.00009481775,0.000009239745,0.0000981923,0.0019523669],"genre_scores_gemma":[0.98714495,0.00023718333,0.011554717,0.00015616803,0.0006902184,0.0000034542688,0.000006809702,0.000046692287,0.00015982985],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9988833,0.000014060995,0.000343353,0.00011763774,0.0002691468,0.00037247763],"domain_scores_gemma":[0.9995774,0.00005353232,0.00003891783,0.00014259336,0.000052031566,0.00013554715],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00031901302,0.0001629371,0.00018327778,0.00012023422,0.000079408164,0.00006076067,0.00019397087,0.00011259597,0.00037451342],"category_scores_gemma":[0.000048298392,0.00015127765,0.000076540135,0.00018318012,0.000024002897,0.00012833292,0.000035156685,0.00067918265,0.00006523411],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00008783635,0.00008374736,0.0045162165,0.0000136402205,0.000072151095,0.00077777053,0.00014977496,0.9611957,0.004931513,0.00010469538,0.0144726755,0.013594243],"study_design_scores_gemma":[0.0007372,0.000055823657,0.006766869,0.000054315577,0.000014312064,0.00040013235,0.000013701047,0.9827017,0.000020233601,0.0034714758,0.0055528153,0.00021140501],"about_ca_topic_score_codex":0.000015529677,"about_ca_topic_score_gemma":0.00037862637,"teacher_disagreement_score":0.036001947,"about_ca_system_score_codex":0.00015545606,"about_ca_system_score_gemma":0.00003962025,"threshold_uncertainty_score":0.6168924},"labels":[],"label_agreement":null},{"id":"W2057544506","doi":"10.1016/j.ijheatfluidflow.2012.01.006","title":"DNS of compressible pipe flow exiting into a coflow","year":2012,"lang":"en","type":"article","venue":"International Journal of Heat and Fluid Flow","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":53,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"General Fusion (Canada)","funders":"Engineering and Physical Sciences Research Council; Royal Academy of Engineering","keywords":"Mach number; Mechanics; Turbulence; Jet (fluid); Nozzle; Physics; Direct numerical simulation; Reynolds number; Compressible flow; Compressibility; Flow (mathematics); Reynolds stress; Classical mechanics; Thermodynamics","score_opus":0.008411247355091066,"score_gpt":0.23739960097223467,"score_spread":0.2289883536171436,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2057544506","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.83012843,0.005493581,0.15763482,0.00018206415,0.0041187718,0.000058888374,0.000038814826,0.000028410446,0.0023162088],"genre_scores_gemma":[0.97561026,0.00066395453,0.022687975,0.00004305056,0.0009393811,0.0000010438054,0.00000651613,0.000019702755,0.000028148608],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9990011,0.00001359929,0.0004346291,0.00005738523,0.00032406396,0.00016922677],"domain_scores_gemma":[0.9994364,0.00008181513,0.000058204892,0.00007520402,0.00023479479,0.00011360803],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002625615,0.00011733814,0.0002138167,0.00014421367,0.000032077718,0.000030618445,0.00021805523,0.000059738715,0.00007899882],"category_scores_gemma":[0.000045510213,0.000104774736,0.000086653265,0.00005343919,0.000045609202,0.00025923373,0.00005221463,0.00019221954,0.0000037384439],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00020715622,0.00037026475,0.019137844,0.00027559226,0.0010742517,0.000103406186,0.0038625642,0.42026863,0.409498,0.0021323846,0.008355499,0.13471442],"study_design_scores_gemma":[0.0006674842,0.00005523081,0.0027775324,0.00022026434,0.00003662097,0.00019599908,0.00011051893,0.9865961,0.0058538956,0.0005464568,0.0027817977,0.0001580836],"about_ca_topic_score_codex":0.0000068717695,"about_ca_topic_score_gemma":0.0000030912588,"teacher_disagreement_score":0.5663275,"about_ca_system_score_codex":0.00005302907,"about_ca_system_score_gemma":0.000016961114,"threshold_uncertainty_score":0.42725897},"labels":[],"label_agreement":null},{"id":"W2059501520","doi":"10.1016/j.jfluidstructs.2012.05.011","title":"Effect of mean flow on the trapped modes of internal cavities","year":2012,"lang":"en","type":"article","venue":"Journal of Fluids and Structures","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":23,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"","keywords":"Mach number; Mean flow; Mechanics; Physics; Amplitude; Acoustic resonance; Particle velocity; Sound pressure; Acoustics; Resonance (particle physics); Optics; Atomic physics; Turbulence","score_opus":0.0055375294201131416,"score_gpt":0.21785547912345826,"score_spread":0.2123179497033451,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2059501520","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9960571,0.0011373765,0.0019227711,0.000010293877,0.00035279075,0.00003133885,0.000013782069,0.0000032079865,0.00047135173],"genre_scores_gemma":[0.99915326,0.00013053317,0.0004966656,0.000008941621,0.00019436493,2.8017595e-7,2.1774058e-7,0.000009402532,0.000006360279],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9994525,0.000030893316,0.00023960805,0.00002658717,0.00015220798,0.000098248165],"domain_scores_gemma":[0.99962306,0.00016497947,0.00006936299,0.000071306546,0.00003217512,0.000039112332],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00030095075,0.00009139966,0.00021668365,0.00005128288,0.000022376142,0.000009985945,0.00010578513,0.000040151666,0.00002023128],"category_scores_gemma":[0.00003280323,0.00004802917,0.00008217364,0.000027020953,0.000057870147,0.000048744012,0.000011669633,0.00016584808,5.7739097e-8],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00051012286,0.00004301641,0.0067068795,0.0008216103,0.00079623325,0.0000095567175,0.004916367,0.15598011,0.7410959,0.023854116,0.0022494774,0.06301661],"study_design_scores_gemma":[0.0017110732,0.002404503,0.021953158,0.00054364844,0.0003725733,0.00022967254,0.000895006,0.37495324,0.58756566,0.0087126875,0.0002517559,0.0004070368],"about_ca_topic_score_codex":0.000003084933,"about_ca_topic_score_gemma":0.0000010818932,"teacher_disagreement_score":0.21897314,"about_ca_system_score_codex":0.000009289266,"about_ca_system_score_gemma":0.000004153788,"threshold_uncertainty_score":0.19585729},"labels":[],"label_agreement":null},{"id":"W2059506682","doi":"10.1080/14685248.2013.780659","title":"A study in the developing region of square jet","year":2013,"lang":"en","type":"article","venue":"Journal of Turbulence","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":23,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Windsor","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Vortex; Jet (fluid); Turbulence; Particle image velocimetry; Physics; Plane (geometry); Mechanics; Instability; Classical mechanics; Geometry; Mathematics","score_opus":0.018807954705901114,"score_gpt":0.23898697678467168,"score_spread":0.22017902207877058,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2059506682","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9941559,0.00017568347,0.004940071,0.00016533953,0.00020338516,0.00010922173,3.206572e-7,0.000004425047,0.00024566482],"genre_scores_gemma":[0.9981055,0.00010438937,0.0016936804,0.000028492834,0.00005457747,0.000002484868,5.6638232e-8,0.000006484961,0.0000043119517],"study_design_codex":"simulation_or_modeling","study_design_gemma":"observational","domain_scores_codex":[0.9993716,0.000024493673,0.00030483102,0.00003654429,0.00017259024,0.00008995405],"domain_scores_gemma":[0.9996303,0.00006492352,0.00009594956,0.000106568456,0.000086414126,0.000015888172],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00026075722,0.0000618741,0.00012788399,0.00006384524,0.000014689129,0.000018311208,0.00026551198,0.000024232902,0.000005135213],"category_scores_gemma":[0.000056162233,0.000038469992,0.000032570773,0.00013696922,0.00001634676,0.00010622415,0.00001634309,0.00020167258,0.0000020752348],"study_design_candidate":"observational","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000038921044,0.0006828583,0.18258215,0.0006185948,0.00027574628,0.0011542835,0.03257685,0.7321229,0.0036334838,0.0025149353,0.011335873,0.032463405],"study_design_scores_gemma":[0.0012951005,0.00066858256,0.77468395,0.0011907225,0.00006739426,0.0006898228,0.011953068,0.20154916,0.00026635925,0.006716508,0.00045656212,0.0004627707],"about_ca_topic_score_codex":0.000009259376,"about_ca_topic_score_gemma":0.0000109616485,"teacher_disagreement_score":0.5921018,"about_ca_system_score_codex":0.00003315975,"about_ca_system_score_gemma":0.000016071888,"threshold_uncertainty_score":0.15687607},"labels":[],"label_agreement":null},{"id":"W2059984123","doi":"10.1115/1.1286031","title":"The Effect of Seat Geometry on Gate Valve Noise","year":2000,"lang":"en","type":"article","venue":"Journal of Pressure Vessel Technology","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":34,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Atomic Energy (Canada)","funders":"","keywords":"Piping; Valve seat; Noise (video); Gate valve; Globe valve; Acoustics; Vortex shedding; Butterfly valve; Engineering; Structural engineering; Marine engineering; Mechanical engineering; Physics; Computer science; Mechanics; Turbulence","score_opus":0.0020859035008601898,"score_gpt":0.20055846032755015,"score_spread":0.19847255682668996,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2059984123","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99180627,0.0043028058,0.0008720209,0.00027799397,0.0005834127,0.00010711421,0.00001032709,0.00008501033,0.0019550622],"genre_scores_gemma":[0.99800587,0.0013660247,0.0002769712,0.00000774533,0.00010460877,0.000002868627,3.5044042e-7,0.000027013553,0.00020857589],"study_design_codex":"simulation_or_modeling","study_design_gemma":"not_applicable","domain_scores_codex":[0.9991082,0.000030915577,0.000363211,0.00008048956,0.00019830996,0.0002188613],"domain_scores_gemma":[0.99920666,0.0002538823,0.00012768581,0.00030577046,0.0000672271,0.000038773625],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00039631198,0.0001445024,0.0003158132,0.00022333249,0.00006142082,0.000015500025,0.0004950373,0.00021960997,0.000057484907],"category_scores_gemma":[0.00011812254,0.00009153471,0.00014251977,0.000310307,0.00011641433,0.000046444406,0.000028689321,0.0006307934,0.000011381573],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00021911194,0.000066177294,0.0018244475,0.00028564187,0.0011318227,0.00008521116,0.000055713605,0.79931694,0.031981397,0.0017749234,0.00798437,0.15527423],"study_design_scores_gemma":[0.0058209216,0.0076238494,0.0070809866,0.0011191835,0.0019498912,0.0009853145,0.00015022905,0.33083683,0.21223907,0.012941286,0.417979,0.0012734304],"about_ca_topic_score_codex":6.5086687e-7,"about_ca_topic_score_gemma":5.579732e-7,"teacher_disagreement_score":0.46848014,"about_ca_system_score_codex":0.000019385594,"about_ca_system_score_gemma":0.000009591511,"threshold_uncertainty_score":0.3732677},"labels":[],"label_agreement":null},{"id":"W2060124460","doi":"10.1115/pvp2013-97037","title":"Aeroacoustics of Opposing Planar Air Jets","year":2013,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"","keywords":"Mach number; Physics; Jet (fluid); Oscillation (cell signaling); Mechanics; Aeroacoustics; Planar; Flapping; Acoustics; Sound pressure; Thermodynamics; Chemistry","score_opus":0.005409945337935772,"score_gpt":0.17512570334197336,"score_spread":0.1697157580040376,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2060124460","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.58511794,0.00010281947,0.32609552,0.000054341854,0.00062484166,0.00017254734,0.000017386454,0.0003080791,0.08750651],"genre_scores_gemma":[0.97701555,0.000034725377,0.022404509,0.00004321402,0.00005430757,0.0000044659005,0.000005556469,0.000024800223,0.00041287104],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994894,0.0000032228309,0.00017278864,0.00007340748,0.000096695265,0.0001644787],"domain_scores_gemma":[0.99968654,0.00003725931,0.00001597845,0.00016333886,0.00004361055,0.000053254826],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000038195743,0.00009282411,0.00011847292,0.000038709546,0.000021148604,0.000011506669,0.00011079395,0.000058683043,0.00019509833],"category_scores_gemma":[0.000012390624,0.00008499904,0.000029926034,0.00006557804,0.00002391709,0.00005828232,0.00001612338,0.00008643619,0.000069038804],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000015462462,0.0000467856,0.0004710757,0.00023778298,0.000083505,0.0000065823033,0.00017093588,0.73096675,0.2124719,0.008535759,0.037012443,0.009994927],"study_design_scores_gemma":[0.00009946373,0.000015370566,0.0013591958,0.000020433947,0.000012706117,0.0000032205085,0.000079710255,0.99428713,0.0025236313,0.0010613673,0.00039099183,0.000146785],"about_ca_topic_score_codex":0.000024239238,"about_ca_topic_score_gemma":0.000006091238,"teacher_disagreement_score":0.3918976,"about_ca_system_score_codex":0.000019538227,"about_ca_system_score_gemma":0.000005710101,"threshold_uncertainty_score":0.34661603},"labels":[],"label_agreement":null},{"id":"W2061015739","doi":"10.1299/jsmec.46.873","title":"Control of Fluid-Structure-Sound Interaction Mechanisms by Means of Synthetic Jets","year":2003,"lang":"en","type":"article","venue":"JSME International Journal Series C","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"","keywords":"Synthetic jet; Acoustics; Loudspeaker; SIGNAL (programming language); Oscillation (cell signaling); Actuator; Vibration; Flow control (data); Jet (fluid); Control theory (sociology); Physics; Turbulence; Flow (mathematics); Engineering; Mechanics; Computer science; Control (management)","score_opus":0.0038326114722479583,"score_gpt":0.20730998857251742,"score_spread":0.20347737710026947,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2061015739","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.44274312,0.00013181724,0.55079293,0.00012958406,0.0040812157,0.0000760141,0.00020073386,0.000029765797,0.001814812],"genre_scores_gemma":[0.9963968,0.0001017321,0.0032785863,0.000028066197,0.00008570127,0.0000016505842,0.000008929298,0.000023427949,0.00007510694],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99899364,0.00002837824,0.00043051728,0.00008044871,0.00034260924,0.00012443801],"domain_scores_gemma":[0.9993707,0.000062265346,0.00016840787,0.000092702256,0.0002558125,0.00005014494],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00014321861,0.00012353467,0.00018861309,0.00009387287,0.000031606975,0.00004084169,0.00022839944,0.00006602013,0.0004193068],"category_scores_gemma":[0.00012428769,0.000115247116,0.00009171635,0.000050318944,0.000040688108,0.0002025523,0.000013447349,0.00020717022,0.0000024653639],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00011718768,0.00006486338,0.00021970202,0.000038695332,0.0006114188,0.000020218578,0.00024870245,0.18871208,0.76134586,0.046177663,0.00075388903,0.0016897006],"study_design_scores_gemma":[0.003584334,0.00045236555,0.0004051554,0.00038496678,0.00022651095,0.002269596,0.0010595996,0.2329447,0.46685287,0.27105263,0.019910932,0.00085636065],"about_ca_topic_score_codex":0.0000031435861,"about_ca_topic_score_gemma":0.000009003568,"teacher_disagreement_score":0.5536537,"about_ca_system_score_codex":0.00010002609,"about_ca_system_score_gemma":0.000016222219,"threshold_uncertainty_score":0.4699641},"labels":[],"label_agreement":null},{"id":"W2061970459","doi":"10.1002/cjce.5450790113","title":"The jet shape of concentric mixers","year":2001,"lang":"en","type":"article","venue":"The Canadian Journal of Chemical Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Concentric; Mixing (physics); Nozzle; Jet (fluid); Mechanics; Materials science; Optics; Geometry; Physics; Mathematics; Thermodynamics","score_opus":0.005047078023851262,"score_gpt":0.16878849139817662,"score_spread":0.16374141337432535,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2061970459","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9944911,0.002089561,0.0017841805,0.00029373134,0.00071294984,0.00004710212,0.0000061745327,0.0000144878,0.00056073733],"genre_scores_gemma":[0.9994652,0.00007461335,0.00021117924,0.000017862418,0.00019638805,7.2384023e-7,5.1548244e-7,0.00002180509,0.000011711549],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992655,0.0000047195094,0.00028419224,0.000037373182,0.00013438151,0.00027387083],"domain_scores_gemma":[0.9993697,0.00015462897,0.000051057235,0.0001330605,0.00007319444,0.00021839669],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00022264426,0.00010022447,0.00014450378,0.00004202078,0.00005266918,0.00003327494,0.00039203663,0.00005332722,0.00002475095],"category_scores_gemma":[0.00015572757,0.00006341957,0.00008197312,0.00018818583,0.00007215893,0.000036368914,0.0000089897085,0.0003459348,0.0000017561429],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000009107716,0.000004394383,0.00050908653,0.00004591854,0.00018016611,0.00009508864,0.00029929428,0.9165306,0.07061524,0.0028470494,0.0024286704,0.006435394],"study_design_scores_gemma":[0.00026862771,0.00001734497,0.00023162109,0.000088312096,0.00004634846,0.00024008461,0.00003355867,0.97303236,0.010787467,0.00027021297,0.014802724,0.0001813484],"about_ca_topic_score_codex":0.00009294802,"about_ca_topic_score_gemma":0.00010768081,"teacher_disagreement_score":0.059827775,"about_ca_system_score_codex":0.00013807829,"about_ca_system_score_gemma":0.000091752954,"threshold_uncertainty_score":0.2586175},"labels":[],"label_agreement":null},{"id":"W2062161891","doi":"10.1115/1.4004071","title":"Characteristics of Turbulent Three-Dimensional Offset Jets","year":2011,"lang":"en","type":"article","venue":"Journal of Fluids Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":35,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Manitoba; Research Manitoba","funders":"","keywords":"Turbulence; Reynolds number; Offset (computer science); Particle image velocimetry; Physics; Mechanics; Reynolds stress; Turbulence kinetic energy; Mean flow; Geometry; Optics; Mathematics","score_opus":0.011832505833953474,"score_gpt":0.18656631978273594,"score_spread":0.17473381394878246,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2062161891","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9047045,0.0004511796,0.0933028,0.000008705601,0.0012397525,0.000043249423,0.000013920099,0.000041654188,0.00019421555],"genre_scores_gemma":[0.9789378,0.00009592909,0.020680752,0.0000074917066,0.00022622923,8.1880876e-7,0.0000022493782,0.00004009572,0.000008611586],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989003,0.0000040090163,0.0005956766,0.00006352564,0.00024596706,0.00019054758],"domain_scores_gemma":[0.9994593,0.00003761207,0.00010365495,0.0001454834,0.0001511179,0.0001027896],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002115427,0.00015769168,0.00030973463,0.00015796271,0.000014715095,0.000008210027,0.00019593356,0.00008123129,0.00006820692],"category_scores_gemma":[0.00004531876,0.00014627293,0.00012257168,0.00010254752,0.000017574675,0.000101966805,0.000027101418,0.0002851467,0.0000041195212],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00008205239,0.00023632485,0.0032396792,0.00078169495,0.0005400881,0.00047685896,0.00069688464,0.65582395,0.32390055,0.002850734,0.0025774895,0.008793702],"study_design_scores_gemma":[0.00039636125,0.00015442706,0.026563514,0.00027973813,0.00008398686,0.00027378314,0.000007744627,0.9623119,0.008922718,0.00014973806,0.0005712552,0.0002848388],"about_ca_topic_score_codex":0.0000015837248,"about_ca_topic_score_gemma":4.9349865e-7,"teacher_disagreement_score":0.31497785,"about_ca_system_score_codex":0.000051425115,"about_ca_system_score_gemma":0.000020054566,"threshold_uncertainty_score":0.59648365},"labels":[],"label_agreement":null},{"id":"W2063111089","doi":"10.1063/1.2717177","title":"Sound generation by a street of vortices in a nonuniform flow","year":2007,"lang":"en","type":"article","venue":"Physics of Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":9,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Concordia University","funders":"","keywords":"Physics; Vortex; Mach number; Sound pressure; Vorticity; Acoustics; Amplitude; Starting vortex; Acoustic wave; Mechanics; Mean flow; Aeroacoustics; Directivity; Vortex ring; Turbulence; Optics","score_opus":0.010687349210333057,"score_gpt":0.228253458374125,"score_spread":0.21756610916379193,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2063111089","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.77449894,0.000118999866,0.22427315,0.0000021063247,0.00010468854,0.000046812474,0.000034229706,0.000014342585,0.00090670853],"genre_scores_gemma":[0.9939864,0.000040640614,0.005808118,0.0000045585625,0.00010272445,0.0000018677559,0.000033025386,0.000015118448,0.0000075163935],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99942595,0.000002859482,0.00024449246,0.00007040923,0.00012488753,0.00013140096],"domain_scores_gemma":[0.9997469,0.000029331966,0.000028195469,0.00013224389,0.000040546118,0.000022748853],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001363104,0.00007946943,0.00013563897,0.00003183777,0.000009938907,0.000005210172,0.000087558234,0.000040815386,0.000004534436],"category_scores_gemma":[0.000009144362,0.00008518613,0.000032603617,0.00013446683,0.000026383668,0.000083018305,0.000014937894,0.00006872042,0.0000010340913],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000006605692,0.00012253756,0.003788692,0.00014507708,0.000038073198,0.0000015263173,0.0005182673,0.3001383,0.6763532,0.004326699,0.00038309034,0.014177927],"study_design_scores_gemma":[0.00018443847,0.000028274797,0.00056957686,0.000016130543,0.000010411496,1.0361038e-7,0.000042487372,0.95128345,0.045618523,0.002118575,0.000032285403,0.00009573831],"about_ca_topic_score_codex":0.000030365341,"about_ca_topic_score_gemma":0.00017118499,"teacher_disagreement_score":0.65114516,"about_ca_system_score_codex":0.000026606385,"about_ca_system_score_gemma":0.0000070708275,"threshold_uncertainty_score":0.34737897},"labels":[],"label_agreement":null},{"id":"W2063812316","doi":"10.1115/fedsm2002-31410","title":"Application of the POD to the Similarity Region of an Axisymmetric Turbulent Jet","year":2002,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Air Force Office of Scientific Research; University at Buffalo; York University; Chalmers Tekniska Högskola; National Science Foundation","keywords":"Strouhal number; Physics; Jet (fluid); Turbulence; Azimuth; Rotational symmetry; Reynolds number; Point of delivery; Similarity (geometry); Geometry; Fourier transform; Mathematical analysis; Mathematics; Computational physics; Mechanics; Optics; Image (mathematics); Quantum mechanics","score_opus":0.01171097640557225,"score_gpt":0.20037609396868808,"score_spread":0.18866511756311583,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2063812316","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.65306044,0.00016758668,0.3306385,0.0016289788,0.0002550091,0.0005967105,0.000016173164,0.00009283925,0.013543764],"genre_scores_gemma":[0.9986232,0.000032137854,0.0011190125,0.00008558826,0.000036696652,0.000007831924,0.0000013483931,0.000009560468,0.00008462097],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995671,0.000011133878,0.00014275525,0.0000739546,0.00012482099,0.000080270416],"domain_scores_gemma":[0.9994608,0.000029702851,0.000028621476,0.00041963562,0.000038133014,0.000023116672],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000091108464,0.00006049411,0.00007504658,0.00003418804,0.000028843177,0.0000052146947,0.00025338674,0.000037693604,0.0000134945385],"category_scores_gemma":[0.000023719445,0.00003377141,0.00003636707,0.00035624174,0.000016936921,0.000021561871,0.00003253364,0.00007691073,0.0000041575004],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00000499562,0.0002227985,0.0013578999,0.000108358305,0.000046476533,9.184604e-7,0.0006441676,0.8642134,0.0056214468,0.019069795,0.0112177115,0.09749201],"study_design_scores_gemma":[0.00005266364,0.000019751331,0.0061561596,0.0000047664275,0.000010507711,0.0000024609835,0.0000290276,0.9895114,0.0013940454,0.0003234891,0.0024426344,0.000053129475],"about_ca_topic_score_codex":0.000033573022,"about_ca_topic_score_gemma":0.0000441916,"teacher_disagreement_score":0.34556276,"about_ca_system_score_codex":0.00001997009,"about_ca_system_score_gemma":0.0000015060626,"threshold_uncertainty_score":0.1377158},"labels":[],"label_agreement":null},{"id":"W2064488961","doi":"10.1016/j.jfluidstructs.2008.03.007","title":"Flow-excited acoustic resonances of coaxial side-branches in an annular duct","year":2008,"lang":"en","type":"article","venue":"Journal of Fluids and Structures","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":39,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"","keywords":"Duct (anatomy); Coaxial; Acoustics; Acoustic resonance; Wavelength; Resonance (particle physics); Excited state; Materials science; Mechanics; Optics; Physics; Engineering; Electrical engineering; Atomic physics","score_opus":0.010294541967594153,"score_gpt":0.21896008426816616,"score_spread":0.208665542300572,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2064488961","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99192125,0.0034282603,0.0040922803,0.000013433993,0.0003976323,0.000038933453,0.000020458547,0.000010015974,0.00007775669],"genre_scores_gemma":[0.9945844,0.0013206423,0.0037804258,0.0000137715115,0.00027637277,3.7499666e-7,0.0000019597026,0.000016509786,0.0000055396645],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9990859,0.000021957705,0.00044602444,0.00008500549,0.00020546911,0.00015566494],"domain_scores_gemma":[0.99960184,0.000047479436,0.00007868865,0.00010325441,0.000093686394,0.000075074524],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00013262041,0.00013437176,0.00033027455,0.00015010852,0.000046359546,0.00001681504,0.00013834244,0.000091007205,0.0000149218085],"category_scores_gemma":[0.000055378525,0.000107274966,0.000055911885,0.000120516204,0.00010244362,0.00015995505,0.000014895243,0.00024292944,8.7888246e-8],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00015349106,0.000046237692,0.01908703,0.00020134864,0.00008979465,0.0003786249,0.001984959,0.7058486,0.25587562,0.0004171368,0.00080221985,0.01511498],"study_design_scores_gemma":[0.0014057308,0.00046804387,0.37279427,0.00014575735,0.000055712924,0.0005952211,0.0003448913,0.6132213,0.0041096373,0.006076502,0.0004230271,0.00035992535],"about_ca_topic_score_codex":0.0000076250403,"about_ca_topic_score_gemma":0.000029570067,"teacher_disagreement_score":0.35370722,"about_ca_system_score_codex":0.000019355512,"about_ca_system_score_gemma":0.000028586728,"threshold_uncertainty_score":0.4374546},"labels":[],"label_agreement":null},{"id":"W2064903236","doi":"10.1115/imece2006-16353","title":"Effects of Density on Mixing of Low Reynolds Number Vertical Jets","year":2006,"lang":"en","type":"article","venue":"Fluids Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Alberta","funders":"","keywords":"Mechanics; Flow visualization; Optics; Reynolds number; Jet (fluid); Physics; Vortex; Entrainment (biomusicology); Vortex ring; Particle image velocimetry; Instability; Planar laser-induced fluorescence; Laser; Materials science; Flow (mathematics); Acoustics; Turbulence","score_opus":0.0017775535415547206,"score_gpt":0.16729334192820616,"score_spread":0.16551578838665143,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2064903236","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9237098,0.000096244316,0.074366525,0.0000025227787,0.0005112229,0.0000864066,0.000004381095,0.00015592034,0.0010669734],"genre_scores_gemma":[0.99657303,0.00001492056,0.0031905773,0.0000030152412,0.00013237749,0.000005229818,0.000004701453,0.00005170347,0.000024415787],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99914163,0.0000056669955,0.00028280594,0.000130031,0.00018696372,0.00025287643],"domain_scores_gemma":[0.99954265,0.00015762239,0.000012675039,0.00020241809,0.00003726639,0.000047370635],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00007518158,0.00017441274,0.00026222953,0.00006874802,0.000015257838,0.000007215892,0.0001169866,0.00011244831,0.000009854034],"category_scores_gemma":[0.00006549694,0.00018916267,0.00008071627,0.00015114738,0.000020937334,0.000040367126,0.00003155181,0.00016782731,0.000012057389],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000004030301,0.000032972177,0.00036135767,0.0007186386,0.000019517935,0.0000140290795,0.000021139744,0.5165895,0.4787508,0.0031766875,0.00018621121,0.00012510232],"study_design_scores_gemma":[0.00023805824,0.000023738563,0.0069910157,0.0002382065,0.000021729842,0.0000034170796,0.0000013625795,0.60330164,0.38889736,0.0000702987,0.000041757638,0.00017140835],"about_ca_topic_score_codex":0.000010752572,"about_ca_topic_score_gemma":0.0000011990222,"teacher_disagreement_score":0.08985346,"about_ca_system_score_codex":0.00006196344,"about_ca_system_score_gemma":0.0000057733914,"threshold_uncertainty_score":0.77138305},"labels":[],"label_agreement":null},{"id":"W2065586692","doi":"10.4271/2011-01-0933","title":"Control of Airflow Noise From Diesel Engine Turbocharger","year":2011,"lang":"en","type":"article","venue":"SAE technical papers on CD-ROM/SAE technical paper series","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":14,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Kootenay Association for Science & Technology","funders":"","keywords":"Turbocharger; Automotive engineering; Airflow; Diesel engine; Noise (video); Diesel fuel; Environmental science; Computer science; Noise control; Engineering; Noise reduction; Aerospace engineering; Mechanical engineering; Artificial intelligence; Gas compressor","score_opus":0.008612428346479056,"score_gpt":0.19767202842046813,"score_spread":0.1890596000739891,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2065586692","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.92480254,0.0013711648,0.00018555918,0.00059977063,0.0013001485,0.0013518882,0.000941554,0.005010136,0.06443722],"genre_scores_gemma":[0.98954046,0.0005025944,0.008577373,0.0005098529,0.00024152598,0.00019994132,0.000069691196,0.00021975963,0.00013878984],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.9961797,0.000066168235,0.0012275429,0.0008485592,0.0007304614,0.0009475673],"domain_scores_gemma":[0.99727386,0.00046844882,0.00016991135,0.0015612019,0.000137068,0.0003895103],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00040127375,0.0008579065,0.0012205276,0.00019061846,0.00015756147,0.000040311937,0.0011676638,0.0008849941,0.0013148441],"category_scores_gemma":[0.00045814953,0.0007548367,0.00052895397,0.0004967798,0.0007508385,0.00029799883,0.00024904576,0.0013304917,0.00013739192],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0001776314,0.00032772732,0.00021924515,0.00006690404,0.00015151307,0.0000482828,0.00005252964,0.00062743644,0.987274,0.00701293,0.0016094655,0.0024323666],"study_design_scores_gemma":[0.0012752947,0.00068153255,0.98188055,0.00024565548,0.00021659385,0.000019381918,0.00006195516,0.000031411753,0.00089165894,0.004287747,0.009356575,0.001051622],"about_ca_topic_score_codex":0.00008084593,"about_ca_topic_score_gemma":0.013736479,"teacher_disagreement_score":0.9863823,"about_ca_system_score_codex":0.00018813992,"about_ca_system_score_gemma":0.000042988322,"threshold_uncertainty_score":0.9995981},"labels":[],"label_agreement":null},{"id":"W2069361672","doi":"10.3826/jhr.2008.3043","title":"Tailwater effects on the characteristics of a square jet near a free-surface","year":2008,"lang":"en","type":"article","venue":"Journal of Hydraulic Research","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":11,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Windsor","funders":"","keywords":"Tailwater; Jet (fluid); Free surface; Turbulence; Anemometer; Mechanics; Geology; Physics; Geotechnical engineering","score_opus":0.03109686661179764,"score_gpt":0.27637205276868293,"score_spread":0.2452751861568853,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2069361672","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9962782,0.0002168359,0.0005678736,0.0007982775,0.0003059527,0.0001595274,0.000011787123,0.000012390126,0.0016491571],"genre_scores_gemma":[0.9983989,0.00054887723,0.00056927046,0.000042253716,0.0002806492,0.000002576829,0.0000010316227,0.000036297406,0.00012013575],"study_design_codex":"not_applicable","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99803275,0.00015495668,0.00042760803,0.00008929732,0.00094336475,0.0003520432],"domain_scores_gemma":[0.9981611,0.0008540236,0.0000977667,0.0004193965,0.00035651974,0.00011123738],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0013191557,0.00013228558,0.00030327187,0.00010653868,0.00016562684,0.000044403172,0.0006245186,0.000086410204,0.000060815884],"category_scores_gemma":[0.0006090515,0.000080320875,0.00012575225,0.00027731963,0.00017194274,0.00006882009,0.00009693747,0.001056651,0.000037256144],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0010061875,0.0010873488,0.024924196,0.0026306538,0.0017988676,0.0057750233,0.011125012,0.30665556,0.2907598,0.0020820035,0.33085904,0.021296326],"study_design_scores_gemma":[0.0036618754,0.0043392386,0.08843272,0.0019673153,0.00010671637,0.001015002,0.00048605533,0.77785724,0.06678112,0.004536047,0.04986075,0.0009559244],"about_ca_topic_score_codex":0.000009256899,"about_ca_topic_score_gemma":0.0000018872984,"teacher_disagreement_score":0.4712017,"about_ca_system_score_codex":0.0000799598,"about_ca_system_score_gemma":0.00007342283,"threshold_uncertainty_score":0.45906818},"labels":[],"label_agreement":null},{"id":"W2070175336","doi":"10.1016/j.jfluidstructs.2009.07.008","title":"Flow-excited resonance of trapped modes of ducted shallow cavities","year":2009,"lang":"en","type":"article","venue":"Journal of Fluids and Structures","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":43,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"","keywords":"Strouhal number; Excitation; Mach number; Resonance (particle physics); Excited state; Acoustic resonance; Mechanics; Amplitude; Physics; Optics; Materials science; Atomic physics; Reynolds number; Turbulence","score_opus":0.005811835123288562,"score_gpt":0.20514556476730988,"score_spread":0.19933372964402132,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2070175336","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9891694,0.0062304167,0.0040330347,0.000031529602,0.00015478466,0.000032188735,0.0000351161,0.000009479823,0.00030405697],"genre_scores_gemma":[0.9908026,0.0014519377,0.0076001473,0.0000134382635,0.00010311158,1.2899497e-7,0.0000014448117,0.000009666266,0.000017543509],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991971,0.000011145256,0.0004342886,0.000057417772,0.00018439247,0.00011560824],"domain_scores_gemma":[0.9995993,0.00003085929,0.00010023243,0.000093688686,0.00012761907,0.00004829872],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00009108243,0.00011537066,0.00032742252,0.00010663482,0.00002421567,0.000012680773,0.00012138162,0.000075130236,0.000015046075],"category_scores_gemma":[0.00003069803,0.00009031763,0.00007941792,0.000092077076,0.000060490052,0.000075701326,0.00000745102,0.00015955848,2.223429e-8],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00014384669,0.000033091903,0.0007195905,0.00025869944,0.00013485517,0.000028114277,0.0009993928,0.2098903,0.7416939,0.005938995,0.0010617933,0.039097402],"study_design_scores_gemma":[0.0014046493,0.00063497457,0.1366826,0.00030872342,0.00012025858,0.00014561228,0.00040662554,0.7987766,0.028032148,0.032672413,0.00046274927,0.0003526484],"about_ca_topic_score_codex":0.000003236643,"about_ca_topic_score_gemma":0.0000032670152,"teacher_disagreement_score":0.7136618,"about_ca_system_score_codex":0.00001136065,"about_ca_system_score_gemma":0.000016422351,"threshold_uncertainty_score":0.3683046},"labels":[],"label_agreement":null},{"id":"W2070416582","doi":"10.2514/1.29273","title":"Tip Vortex Control via a Tab Deflecting at Higher Harmonic Frequencies","year":2008,"lang":"en","type":"article","venue":"AIAA Journal","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"","keywords":"Vortex; Mechanics; Physics; Trailing edge; RADIUS; Airfoil; Harmonic; Deflection (physics); Optics; Acoustics","score_opus":0.01283790687459466,"score_gpt":0.19733670560300043,"score_spread":0.18449879872840577,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2070416582","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.89933664,0.0022183615,0.090539485,0.0001923493,0.0021821049,0.000081676575,0.00000790984,0.00017479942,0.0052666613],"genre_scores_gemma":[0.9948464,0.000455013,0.0027734963,0.00014672687,0.000906083,0.0000037966668,0.0000014369597,0.000050674378,0.0008163651],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989245,0.000020341757,0.00030865154,0.000114887946,0.00022651198,0.0004051124],"domain_scores_gemma":[0.99950284,0.000071486356,0.000068540605,0.00014417054,0.000070315786,0.00014267399],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017075546,0.00017265264,0.00020317911,0.0000543989,0.00039190246,0.000047084373,0.00018166252,0.00008939863,0.000466068],"category_scores_gemma":[0.000027322913,0.00015892767,0.00011200393,0.000107255626,0.000048808495,0.00012535171,0.000026236063,0.0005208247,0.00014866315],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000073055504,0.00013454721,0.023451414,0.000107284795,0.0010615638,0.0029509037,0.0014573981,0.3675084,0.5420259,0.0011781971,0.045744006,0.014307281],"study_design_scores_gemma":[0.0026793457,0.00019096314,0.032107122,0.000119062985,0.00019584845,0.008892163,0.00007062714,0.9248549,0.0023391522,0.007843085,0.01945441,0.0012533407],"about_ca_topic_score_codex":0.000006751679,"about_ca_topic_score_gemma":0.000010103772,"teacher_disagreement_score":0.55734646,"about_ca_system_score_codex":0.00025448567,"about_ca_system_score_gemma":0.0000298402,"threshold_uncertainty_score":0.6480882},"labels":[],"label_agreement":null},{"id":"W2072026159","doi":"10.1115/fedsm2009-78540","title":"Characteristics of 3D Turbulent Wall Jets and Offset Jets With Small Offset Ratios","year":2009,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Manitoba","funders":"","keywords":"Turbulence; Reynolds number; Particle image velocimetry; Physics; Mechanics; Turbulence kinetic energy; Offset (computer science); Reynolds stress; Proper orthogonal decomposition; Shear (geology); Salient; Optics; Materials science","score_opus":0.008001348963099654,"score_gpt":0.18722546735815782,"score_spread":0.17922411839505817,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2072026159","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9664084,0.00007349796,0.028137011,0.00021351848,0.000101236474,0.00018010661,0.000043086806,0.00012622231,0.0047169356],"genre_scores_gemma":[0.9874196,0.00020158228,0.0117790215,0.00014924863,0.000048585152,0.000003063102,0.000057669007,0.000020465195,0.00032074522],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992969,0.0000068246586,0.0002512198,0.000142311,0.00012120162,0.00018152819],"domain_scores_gemma":[0.99959177,0.00002692748,0.000044391498,0.0002026935,0.000060960825,0.00007327474],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00007443512,0.00016266,0.00021716472,0.000047298698,0.000030246458,0.000026479976,0.00009186578,0.000073298186,0.000041771833],"category_scores_gemma":[0.0000107549195,0.00013193631,0.000020420717,0.000067138535,0.000029137027,0.00004693434,0.000014825587,0.00012308742,0.000005272063],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0005022241,0.0015549327,0.021371352,0.0022359914,0.0009260347,0.00052795594,0.0039314604,0.16534844,0.13493267,0.032470576,0.021177422,0.61502093],"study_design_scores_gemma":[0.00066852174,0.00029931782,0.044787932,0.000096249605,0.000064606946,0.0000426854,0.000027454225,0.94870776,0.0012721247,0.00025672888,0.0033299346,0.00044666708],"about_ca_topic_score_codex":0.0000046810314,"about_ca_topic_score_gemma":0.000026734819,"teacher_disagreement_score":0.78335935,"about_ca_system_score_codex":0.000020929541,"about_ca_system_score_gemma":0.000011277644,"threshold_uncertainty_score":0.5380207},"labels":[],"label_agreement":null},{"id":"W2073361070","doi":"10.1080/10618560802432944","title":"Application of the SAS turbulence model to predict the unsteady flow field behaviour in a forward centrifugal fan","year":2008,"lang":"en","type":"article","venue":"International journal of computational fluid dynamics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":26,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Ansys (Canada)","funders":"","keywords":"Turbulence; Mechanics; K-epsilon turbulence model; Physics; K-omega turbulence model; Flow (mathematics); Turbulence modeling; Computational fluid dynamics; Field (mathematics); Statistical physics; Mathematics","score_opus":0.0054045035135402335,"score_gpt":0.22524670244106643,"score_spread":0.21984219892752618,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2073361070","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.38045076,0.000026394036,0.6179064,0.0008025547,0.0005384059,0.0001061183,0.00007135707,0.000007675661,0.00009033209],"genre_scores_gemma":[0.9861504,0.000036548474,0.01342916,0.00018597509,0.00013292937,0.000005878157,0.000018675242,0.00001547475,0.000024945748],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99846494,0.000021829639,0.0005773475,0.000092233684,0.0007187676,0.00012485932],"domain_scores_gemma":[0.998983,0.00019428914,0.00014945309,0.00012742459,0.0004959189,0.000049869723],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020923422,0.000117234544,0.00014983097,0.00013597366,0.000050955696,0.000020456073,0.0007447263,0.000059714173,0.0000040094124],"category_scores_gemma":[0.00009279555,0.00008545357,0.00011974275,0.00017807794,0.000046968453,0.00010897959,0.00007871228,0.0002884513,0.000001729789],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000030088144,0.000046368485,0.006942918,0.000004805383,0.000041842457,0.000006628804,0.00023249096,0.98748666,0.00016831406,0.0029616272,0.00033565427,0.0017425745],"study_design_scores_gemma":[0.00030705138,0.000029661584,0.0148501955,0.000049041064,0.000012746222,0.00010735797,0.000029398334,0.98015326,0.00006247853,0.004288419,0.000031761756,0.00007863914],"about_ca_topic_score_codex":0.000011462719,"about_ca_topic_score_gemma":0.000053476342,"teacher_disagreement_score":0.60569966,"about_ca_system_score_codex":0.00024164352,"about_ca_system_score_gemma":0.00011504509,"threshold_uncertainty_score":0.34846953},"labels":[],"label_agreement":null},{"id":"W2073940740","doi":"10.1115/gt2014-25935","title":"Acoustic Design and Validation of Radial Inflow Turbine","year":2014,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Inflow; Turbine; Rotor (electric); Factory (object-oriented programming); Marine engineering; Noise (video); Process (computing); Computer science; Engineering; Automotive engineering; Mechanical engineering; Geology","score_opus":0.007205537097050812,"score_gpt":0.19161752414110397,"score_spread":0.18441198704405315,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2073940740","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.26041844,0.000017501545,0.7376432,0.0000065022587,0.00013454192,0.00004959709,0.0000011948549,0.000054042684,0.0016749784],"genre_scores_gemma":[0.9733315,0.000026913927,0.026488895,0.000010438301,0.00006226482,0.0000022103115,0.0000033220936,0.0000123173395,0.00006214924],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99969006,0.00000979247,0.00010699865,0.00005801155,0.000056845824,0.0000782792],"domain_scores_gemma":[0.9997678,0.000087242486,0.000011604715,0.00008557214,0.000018573644,0.00002922823],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00013088237,0.00006058429,0.00008452185,0.00003057287,0.000013814561,0.000010047663,0.000040724688,0.00003913977,0.000031930584],"category_scores_gemma":[0.000043960456,0.000055448276,0.000010927483,0.000042243508,0.000017597456,0.000035815076,0.000010774967,0.0000453376,0.0000039737283],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000020716761,0.0000039605734,0.000064984095,0.000034137443,0.000007989093,1.9524764e-7,0.000029035906,0.9460742,0.048924334,0.0007858451,0.0003071582,0.0037661006],"study_design_scores_gemma":[0.0001491434,0.00002629883,0.00032567838,0.0000067236597,0.000012868154,0.0000012378678,0.000003498921,0.9907473,0.0077162306,0.00083353167,0.00010925929,0.000068265486],"about_ca_topic_score_codex":0.00000233721,"about_ca_topic_score_gemma":0.0000012495761,"teacher_disagreement_score":0.71291304,"about_ca_system_score_codex":0.0000079954425,"about_ca_system_score_gemma":0.0000030506035,"threshold_uncertainty_score":0.2261115},"labels":[],"label_agreement":null},{"id":"W2074321054","doi":"10.1121/1.3675942","title":"A wave field synthesis approach to reproduction of spatially correlated sound fields","year":2012,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":23,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Supersonic speed; Acoustics; Wavelength; Turbulence; Physics; Plane wave; Sound pressure; Planar; Plane (geometry); Sound transmission class; Field (mathematics); Acoustic wave; Optics; Mechanics; Mathematics; Computer science; Geometry","score_opus":0.012591816547464697,"score_gpt":0.21526003581174188,"score_spread":0.2026682192642772,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2074321054","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.086628415,0.00020583722,0.91075027,0.0008294887,0.00064532785,0.000106553634,0.000005503806,0.000012341136,0.00081624236],"genre_scores_gemma":[0.94993323,0.00020531371,0.049302533,0.00020707614,0.00029873577,0.0000012451231,1.9231794e-7,0.00001653669,0.00003515843],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99894845,0.00005439783,0.00042136057,0.00006172962,0.00030838285,0.00020568934],"domain_scores_gemma":[0.9986741,0.00055591174,0.00021973607,0.0003495746,0.00012641086,0.000074292155],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006482067,0.000111682355,0.00028178171,0.000016436854,0.00006751743,0.0000062371164,0.00033401907,0.00009892604,0.000028830185],"category_scores_gemma":[0.0006090738,0.000064815984,0.00025562354,0.00022039932,0.00014162366,0.000053514654,0.00009348952,0.0004384259,0.0000013719424],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000739321,0.00017873995,0.00011546612,0.000115773306,0.0003395856,1.6690348e-7,0.0022145393,0.94764787,0.015866205,0.000018773168,0.019321017,0.014107948],"study_design_scores_gemma":[0.00012851057,0.00015914104,0.0006316991,0.000084762876,0.00047832206,0.0000585075,0.0011069475,0.9907891,0.00561501,0.0005191494,0.0002832286,0.00014561605],"about_ca_topic_score_codex":0.000021896576,"about_ca_topic_score_gemma":2.2295688e-7,"teacher_disagreement_score":0.8633048,"about_ca_system_score_codex":0.000042945725,"about_ca_system_score_gemma":0.000018962792,"threshold_uncertainty_score":0.26431194},"labels":[],"label_agreement":null},{"id":"W2074454379","doi":"10.1007/s00348-013-1531-5","title":"Aeroacoustic source analysis using time-resolved PIV in a free jet","year":2013,"lang":"en","type":"article","venue":"Experiments in Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":24,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Natural Sciences and Engineering Research Council of Canada; Science Foundation Ireland","keywords":"Particle image velocimetry; Acoustics; Jet (fluid); Coherence (philosophical gambling strategy); Jet noise; Noise (video); Time domain; Physics; Frequency domain; Wavelet; Anemometer; Sound pressure; Cross-correlation; Optics; Computer science; Turbulence; Mechanics; Mathematics; Image (mathematics)","score_opus":0.010263563147626071,"score_gpt":0.23461148613034424,"score_spread":0.22434792298271816,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2074454379","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9129131,0.0010551971,0.08282156,0.000013469384,0.00034596343,0.00024326096,0.00001031944,0.00012740532,0.0024697431],"genre_scores_gemma":[0.9856867,0.000023424558,0.013374936,0.00004373876,0.00008027233,0.00006361329,0.000015681475,0.000060142273,0.00065148954],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9985699,0.000034815417,0.0004162998,0.0002798831,0.00022550525,0.00047361644],"domain_scores_gemma":[0.9992808,0.000048803966,0.00002347549,0.000532689,0.000025375617,0.00008887363],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0001614942,0.0002463038,0.00036187127,0.0004408671,0.000036844733,0.00006945951,0.0003558664,0.00014432997,0.00082807895],"category_scores_gemma":[0.000044905664,0.0002656306,0.00009109157,0.0008479005,0.000045644883,0.00016346795,0.00013430936,0.0002307168,0.00010288675],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000036922693,0.00010289407,0.0031721103,0.000017792505,0.0001632917,0.00001692873,0.0010629481,0.8023616,0.19096403,0.0000307238,0.0014015532,0.0007024461],"study_design_scores_gemma":[0.0004892033,0.000012548355,0.0011675198,0.000033315704,0.000046394114,0.0000011848321,0.00018652309,0.9959331,0.0015592327,0.00015678396,0.00012767571,0.00028647706],"about_ca_topic_score_codex":0.0004139046,"about_ca_topic_score_gemma":0.000045346136,"teacher_disagreement_score":0.19357155,"about_ca_system_score_codex":0.00036618536,"about_ca_system_score_gemma":0.000018880512,"threshold_uncertainty_score":0.9999796},"labels":[],"label_agreement":null},{"id":"W2075401311","doi":"10.2514/1.9751","title":"Influence of Jet Inlet Conditions on Time-Average Behavior of Transverse Jets","year":2005,"lang":"en","type":"article","venue":"AIAA Journal","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"","keywords":"Nozzle; Mechanics; Jet (fluid); Transverse plane; Plenum space; Penetration (warfare); Physics; Aerodynamics; Computational fluid dynamics; Engineering; Thermodynamics; Structural engineering","score_opus":0.0053245040257134816,"score_gpt":0.22108384140706966,"score_spread":0.21575933738135616,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2075401311","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99735254,0.00003245966,0.0012893114,0.000037905054,0.000068401816,0.000053089123,0.00010255472,0.000019147323,0.0010446106],"genre_scores_gemma":[0.99880975,0.00009422974,0.0009013696,0.000029119421,0.00007747744,0.0000021346546,0.0000051288353,0.000017119191,0.00006366479],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99933606,0.000011246977,0.00029259024,0.00005480157,0.00016871473,0.00013656942],"domain_scores_gemma":[0.99964267,0.000040422805,0.00006461412,0.00011928283,0.0000660638,0.00006697178],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00010108513,0.00009402244,0.00015060006,0.00008735542,0.000041773023,0.000008681079,0.00013459905,0.000056943656,0.0003398907],"category_scores_gemma":[0.000015484873,0.00008962768,0.00007259491,0.00007489448,0.000044857825,0.00010555915,0.0000073941264,0.0002653995,0.000033718028],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000046562036,0.000055148284,0.00042426342,0.000012376768,0.000025194111,0.000014621177,0.0001671682,0.9058866,0.09152866,0.00023536445,0.00082440703,0.00082155917],"study_design_scores_gemma":[0.005792052,0.0012257602,0.17518695,0.0011721428,0.00068060507,0.00092005474,0.0002117391,0.65323585,0.14630874,0.002240145,0.011394741,0.001631191],"about_ca_topic_score_codex":0.0000013534163,"about_ca_topic_score_gemma":0.0000044442227,"teacher_disagreement_score":0.2526507,"about_ca_system_score_codex":0.00003764027,"about_ca_system_score_gemma":0.000017804985,"threshold_uncertainty_score":0.3721565},"labels":[],"label_agreement":null},{"id":"W2075756871","doi":"10.1063/1.2946443","title":"Linear stability of a compressible coaxial jet with continuous velocity and temperature profiles","year":2008,"lang":"en","type":"article","venue":"Physics of Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":18,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"","keywords":"Physics; Mechanics; Wavenumber; Compressibility; Instability; Jet (fluid); Coaxial; Turbofan; Rotational symmetry; Classical mechanics; Optics; Aerospace engineering","score_opus":0.011232145041972827,"score_gpt":0.20446387744874214,"score_spread":0.19323173240676933,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2075756871","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9935745,0.00017995748,0.005361934,0.0000053495564,0.000055177294,0.00013558567,0.00015085124,0.000037361402,0.00049925764],"genre_scores_gemma":[0.9887076,0.000072339426,0.011090161,0.0000033670306,0.00007714782,0.0000054675784,0.000017146042,0.00001975446,0.0000069900666],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994318,0.000010354701,0.00017261515,0.000118868746,0.00014264853,0.0001237216],"domain_scores_gemma":[0.9995624,0.00004251197,0.000033395492,0.00019628143,0.00012740641,0.000038012604],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000051777468,0.0001274611,0.00028988172,0.000013350176,0.000037496255,0.00000397662,0.00008956559,0.000055097968,0.0000064244364],"category_scores_gemma":[0.0000091409065,0.00010543413,0.000032489228,0.00009724215,0.00021409808,0.00006313152,0.000033273576,0.00014211233,4.506666e-7],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00012830777,0.00034655185,0.04505929,0.001125393,0.00021469248,0.000008644377,0.0018683282,0.021619046,0.9242683,0.0036077732,0.00058706454,0.0011665812],"study_design_scores_gemma":[0.0017243039,0.00042952862,0.033744954,0.00019806971,0.00008716788,0.000013748493,0.00019267829,0.51922184,0.44239673,0.0013241139,0.000086978216,0.0005798976],"about_ca_topic_score_codex":0.000017874305,"about_ca_topic_score_gemma":0.0000035369076,"teacher_disagreement_score":0.49760276,"about_ca_system_score_codex":0.000010082797,"about_ca_system_score_gemma":0.000025879119,"threshold_uncertainty_score":0.4299479},"labels":[],"label_agreement":null},{"id":"W2076124333","doi":"10.1080/14685240802301965","title":"On the phase velocities of the motions in an offset attaching planar jet","year":2008,"lang":"en","type":"article","venue":"Journal of Turbulence","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":16,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Turbulence; Spectral line; Mechanics; Physics; Reynolds number; Jet (fluid); Phase velocity; Optics","score_opus":0.021468435737413288,"score_gpt":0.2479809653227403,"score_spread":0.22651252958532703,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2076124333","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99697036,0.00009189761,0.0020479688,0.0002476852,0.0003273503,0.000036146426,0.000021271664,0.000005295071,0.0002520558],"genre_scores_gemma":[0.99930316,0.00012952805,0.00041433307,0.00006139097,0.000068409114,6.2553596e-7,4.774987e-7,0.000007867078,0.000014177122],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99940634,0.000031949985,0.00025032257,0.000037427966,0.00018296715,0.00009101561],"domain_scores_gemma":[0.9995958,0.000096921845,0.00009564271,0.0001479916,0.000038915845,0.000024677698],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00022353548,0.00006730081,0.00010912213,0.000048738388,0.00007858378,0.000009053335,0.00029683075,0.000028963315,0.0000079289675],"category_scores_gemma":[0.000086879074,0.000036939306,0.000054962413,0.00009483949,0.00007110477,0.00008685132,0.000011876526,0.00035665568,6.296292e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000015962649,0.00013892035,0.0017793452,0.000025601861,0.000024628898,0.00004298989,0.0021738964,0.9845432,0.004686495,0.0033337723,0.0024333254,0.0008018769],"study_design_scores_gemma":[0.00070034625,0.0002507604,0.033956993,0.00044209618,0.000024315554,0.00020904448,0.00050888816,0.9576604,0.0012195637,0.0046334234,0.00021964728,0.00017454091],"about_ca_topic_score_codex":0.000004257812,"about_ca_topic_score_gemma":0.000013950781,"teacher_disagreement_score":0.03217765,"about_ca_system_score_codex":0.00003660235,"about_ca_system_score_gemma":0.000021645797,"threshold_uncertainty_score":0.15495113},"labels":[],"label_agreement":null},{"id":"W2077153344","doi":"10.1121/1.4806342","title":"Fly-over aircraft noise measurement campaign at Montreal-Trudeau airport using a microphone array","year":2013,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"Université de Sherbrooke; Bombardier (Canada)","funders":"","keywords":"Beamforming; Microphone array; Airframe; Microphone; Acoustics; Noise (video); Computer science; Instrumentation (computer programming); Aircraft noise; Aerospace engineering; Range (aeronautics); Landing gear; Aeronautics; Engineering; Telecommunications; Sound pressure; Physics; Noise reduction","score_opus":0.009963424324457437,"score_gpt":0.20373998764128695,"score_spread":0.19377656331682952,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2077153344","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.26068717,0.00075607264,0.7365657,0.00076545216,0.0006920103,0.0002592748,0.00001632445,0.000029199975,0.00022878108],"genre_scores_gemma":[0.9305529,0.00054580247,0.06789834,0.0005716305,0.00030192378,0.0000022155057,4.0568594e-7,0.000053795375,0.00007298288],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9980257,0.00007304494,0.0006384248,0.0001077355,0.0007595497,0.00039554082],"domain_scores_gemma":[0.99850583,0.00017929761,0.0003645465,0.00044969496,0.00034784258,0.00015280876],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006153695,0.00024906878,0.0004476588,0.000020145762,0.00021620696,0.000025850648,0.00065844395,0.00010266765,0.00017568345],"category_scores_gemma":[0.00010054711,0.00014192944,0.00049740454,0.00023321927,0.0004114764,0.0000889002,0.00015657271,0.0005474935,0.000013861062],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000019464958,0.000057292073,0.00010849917,0.000046146204,0.0002536249,0.0000010338899,0.00042791737,0.34791827,0.61873424,2.8055072e-7,0.031340703,0.0010925262],"study_design_scores_gemma":[0.00052540906,0.000107799926,0.0035907787,0.00015702762,0.0005578973,0.00009821192,0.00085902534,0.98511684,0.0074303807,0.0005651982,0.0007024244,0.0002889995],"about_ca_topic_score_codex":0.00030007743,"about_ca_topic_score_gemma":0.000005620923,"teacher_disagreement_score":0.6698657,"about_ca_system_score_codex":0.00046287375,"about_ca_system_score_gemma":0.000074019845,"threshold_uncertainty_score":0.5787715},"labels":[],"label_agreement":null},{"id":"W2077736329","doi":"10.1063/1.4906235","title":"Self-excited oscillations of two opposing planar air jets","year":2015,"lang":"en","type":"article","venue":"Physics of Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Physics; Planar; Jet (fluid); Mechanics; Mach number; Flapping; Entrainment (biomusicology); Oscillation (cell signaling); Particle image velocimetry; Phase (matter); Optics; Acoustics","score_opus":0.020465057514067127,"score_gpt":0.24598534879990575,"score_spread":0.22552029128583861,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2077736329","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.71091664,0.00025692495,0.26948044,0.00003523465,0.000582849,0.00015306525,0.00011793394,0.0002522291,0.018204713],"genre_scores_gemma":[0.98219013,0.000022395749,0.017576484,0.000008341861,0.00013566803,0.0000020593236,0.000023841896,0.000026708505,0.000014387874],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993859,0.000008429599,0.00020967588,0.00008516294,0.00017694528,0.0001338982],"domain_scores_gemma":[0.9995145,0.00004041179,0.000034737834,0.00021630948,0.00012944086,0.00006457519],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00008406773,0.00010330091,0.00017863367,0.00003942238,0.000021159129,0.0000056431595,0.00012851741,0.000035507983,0.0000021087408],"category_scores_gemma":[0.000014687262,0.00011160184,0.00005042466,0.00018529755,0.000032462554,0.00008569396,0.000023981926,0.00008044196,0.000005645512],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000005410133,0.00011203215,0.0010513465,0.00020071714,0.00013890049,0.0000020827792,0.0012522319,0.8707444,0.08955383,0.033879206,0.0015457032,0.0015141171],"study_design_scores_gemma":[0.00035723508,0.000031496973,0.00021787029,0.00003426972,0.00003902466,9.202053e-7,0.000038683203,0.98240066,0.005658605,0.010653046,0.00042522998,0.00014295553],"about_ca_topic_score_codex":0.000013556639,"about_ca_topic_score_gemma":0.000002415043,"teacher_disagreement_score":0.2712735,"about_ca_system_score_codex":0.00003870153,"about_ca_system_score_gemma":0.000028580827,"threshold_uncertainty_score":0.4550991},"labels":[],"label_agreement":null},{"id":"W2078400803","doi":"10.1115/1.4027228","title":"Investigation of Diametral Acoustic Modes in a Model of a Steam Control Gate Valve","year":2014,"lang":"en","type":"article","venue":"Journal of Pressure Vessel Technology","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":9,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Victoria","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Mechanics; Acoustics; Turbulence; Materials science; Acoustic impedance; Coupling (piping); Internal pressure; Amplitude; Helmholtz resonator; Inflow; Physics; Optics; Resonator; Ultrasonic sensor; Composite material","score_opus":0.007454819706976259,"score_gpt":0.19911005851416547,"score_spread":0.1916552388071892,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2078400803","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6740036,0.00058751873,0.32507616,0.000049602088,0.00009271168,0.00007227993,0.000014565238,0.0000267231,0.000076820375],"genre_scores_gemma":[0.9915622,0.00013226438,0.008231329,0.000008713563,0.00003238017,0.0000036429037,5.036736e-7,0.00002295766,0.000006043501],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.998888,0.000029151786,0.00064793613,0.000085610875,0.0001727121,0.00017655782],"domain_scores_gemma":[0.99914414,0.00009177024,0.00033903794,0.00019574749,0.00018931774,0.000039992417],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00042671832,0.00012625374,0.0004876474,0.0005737941,0.000010552106,0.000004546723,0.00030412563,0.00025320012,0.0000024689177],"category_scores_gemma":[0.000260852,0.00011649818,0.00009196054,0.0002769541,0.0001403382,0.00009817798,0.000028410024,0.00042700177,2.4541941e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000126341365,0.00001793982,0.0011506049,0.00015691947,0.00007153779,0.0000012342056,0.00007286522,0.720289,0.2760354,0.0015731377,0.000037130816,0.0005815917],"study_design_scores_gemma":[0.000772022,0.00013327098,0.00047374642,0.00014635826,0.00014170105,0.000010477791,0.00006482257,0.96565175,0.010734388,0.021766674,0.000013342544,0.00009141774],"about_ca_topic_score_codex":0.0000032739752,"about_ca_topic_score_gemma":0.000007886507,"teacher_disagreement_score":0.31755853,"about_ca_system_score_codex":0.000022897826,"about_ca_system_score_gemma":0.000038113332,"threshold_uncertainty_score":0.4750658},"labels":[],"label_agreement":null},{"id":"W2078919111","doi":"10.1121/1.3081496","title":"Characteristics of air puffs produced in English “pa”: Experiments and simulations","year":2009,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":17,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of British Columbia","funders":"National Institute on Deafness and Other Communication Disorders; Natural Sciences and Engineering Research Council of Canada; National Institutes of Health","keywords":"Environmental science; Acoustics; Materials science; Statistical physics; Computer science; Physics","score_opus":0.0075961309383621506,"score_gpt":0.23440950940179517,"score_spread":0.22681337846343302,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2078919111","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.96483845,0.00020469293,0.033948343,0.00050246157,0.00026406717,0.00011967596,0.000020201329,0.000011701426,0.00009043192],"genre_scores_gemma":[0.9911358,0.0004138148,0.008144981,0.00015750618,0.00012778514,2.836827e-7,5.140922e-7,0.000010852193,0.000008492182],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99907935,0.00003488042,0.00045397,0.000053605057,0.00023187429,0.00014634273],"domain_scores_gemma":[0.99919283,0.000218037,0.00020965285,0.0001989618,0.00013793733,0.000042585772],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002470772,0.00010363284,0.0002799774,0.000017798413,0.00004762283,0.0000060610014,0.00027537404,0.000051755553,0.0000073338306],"category_scores_gemma":[0.00023590581,0.00006383419,0.00011159504,0.0001770552,0.0001981009,0.000052424937,0.000051175815,0.00032256893,1.4182216e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00007771333,0.00033706374,0.0017240298,0.00011615557,0.00017749661,0.0000012961899,0.0069701113,0.7496541,0.22292134,0.000032344415,0.0024942,0.01549415],"study_design_scores_gemma":[0.00033616362,0.00014991903,0.017445477,0.00010056826,0.000107812404,0.0000056443887,0.00079370255,0.9774117,0.0028841998,0.000512734,0.00014677101,0.00010532017],"about_ca_topic_score_codex":0.0000027811277,"about_ca_topic_score_gemma":1.2869626e-7,"teacher_disagreement_score":0.2277576,"about_ca_system_score_codex":0.00004094154,"about_ca_system_score_gemma":0.000022085444,"threshold_uncertainty_score":0.26030827},"labels":[],"label_agreement":null},{"id":"W2079890262","doi":"10.2514/1.j053008","title":"Evaluation of a Cascade-Based Acoustic Model for Fan Tonal Noise Prediction","year":2014,"lang":"en","type":"article","venue":"AIAA Journal","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":16,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Natural Sciences and Engineering Research Council of Canada; Compute Canada","keywords":"Cascade; Turbomachinery; Inviscid flow; Aerodynamics; Acoustics; Stator; Duct (anatomy); Turbofan; Aeroelasticity; Aeroacoustics; Axial compressor; Airfoil; Noise (video); Gas compressor; Solver; Physics; Mechanics; Sound pressure; Computer science; Engineering; Aerospace engineering","score_opus":0.022168129933886026,"score_gpt":0.25370028718942716,"score_spread":0.23153215725554113,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2079890262","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.2818415,0.000046792207,0.7172973,0.000023683371,0.0003832973,0.000102821716,0.00003573996,0.000023000568,0.0002458708],"genre_scores_gemma":[0.9918598,0.000013865633,0.0077183885,0.000022299551,0.00031507702,0.000015852143,0.0000119796305,0.00002493624,0.000017797216],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99902993,0.000027779877,0.00026298923,0.000075771015,0.00044822696,0.00015531588],"domain_scores_gemma":[0.9993171,0.0000650625,0.00006825767,0.000102014536,0.00038138515,0.00006619635],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0013210331,0.00009141167,0.00011666782,0.00006231151,0.00007295579,0.000022545686,0.00009139226,0.0000720238,0.000024597424],"category_scores_gemma":[0.00018271328,0.000087488865,0.00007698404,0.000049931397,0.000016760376,0.000072548864,0.000006049859,0.00016531709,0.0000013987886],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000008359378,0.000017216336,0.00004506182,0.000028676062,0.000026448288,1.4898377e-7,0.00004978906,0.97132087,0.01684658,0.00008141408,0.0005122782,0.011063145],"study_design_scores_gemma":[0.00083333324,0.000063917054,0.000424086,0.000040394727,0.00021244136,0.000011167727,0.0000094512625,0.99355257,0.00040612984,0.004337574,0.000027217171,0.00008170445],"about_ca_topic_score_codex":7.8369527e-7,"about_ca_topic_score_gemma":0.0000072880475,"teacher_disagreement_score":0.71001834,"about_ca_system_score_codex":0.00012428893,"about_ca_system_score_gemma":0.00008935152,"threshold_uncertainty_score":0.35676923},"labels":[],"label_agreement":null},{"id":"W2080506485","doi":"10.2514/6.2001-986","title":"Computation of an underexpanded 3-D rectangular jet by the CE/SE method","year":2001,"lang":"en","type":"article","venue":"39th Aerospace Sciences Meeting and Exhibit","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Computation; Jet (fluid); Computer science; Computer graphics (images); Physics; Mechanics; Algorithm","score_opus":0.016154487881458065,"score_gpt":0.27911996322636734,"score_spread":0.26296547534490927,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2080506485","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9299715,0.0007642584,0.062453818,0.00017832614,0.00019928101,0.000097635755,0.000006192261,0.00009823691,0.006230734],"genre_scores_gemma":[0.9777141,0.00015162972,0.021928674,0.00003954529,0.000048035887,0.0000031808854,0.0000042273227,0.000013345359,0.000097217206],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9990369,0.000063621286,0.00018067933,0.00022118901,0.00024562082,0.00025196635],"domain_scores_gemma":[0.9995496,0.00014733728,0.00006246044,0.0001325001,0.000037626625,0.00007045954],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0011234881,0.0001291322,0.000155268,0.000038575738,0.0002906824,0.00009442405,0.00018684662,0.00005521893,0.000007325565],"category_scores_gemma":[0.00006417187,0.00009198502,0.000029450906,0.00035138364,0.00019685153,0.00012074995,0.00003627066,0.000119180266,0.000001491106],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00001599591,0.00005807316,0.0040378496,0.00009710153,0.000036881473,0.0000055995374,0.0037268486,0.81349343,0.14018287,0.0012012648,0.0020546198,0.03508945],"study_design_scores_gemma":[0.00019255077,0.000095519405,0.00035575565,0.00006179314,0.000017409755,0.000018917925,0.0018494212,0.99116486,0.004378334,0.0013110022,0.0003754385,0.0001789978],"about_ca_topic_score_codex":0.00017900215,"about_ca_topic_score_gemma":0.00011993276,"teacher_disagreement_score":0.17767142,"about_ca_system_score_codex":0.000019780007,"about_ca_system_score_gemma":0.000019160003,"threshold_uncertainty_score":0.375104},"labels":[],"label_agreement":null},{"id":"W2081011533","doi":"10.1007/s00348-002-0567-8","title":"Uncertainty analysis of four-sensor hot-wires and their data-reduction schemes used in the near field of a turbulent jet","year":2003,"lang":"en","type":"article","venue":"Experiments in Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":10,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Queen's University","funders":"","keywords":"Jet (fluid); Turbulence; Data reduction; Reduction (mathematics); Turbulence kinetic energy; Computation; Mechanics; Field (mathematics); Flow (mathematics); Physics; Computer science; Algorithm; Mathematics; Data mining; Geometry","score_opus":0.02998414382409949,"score_gpt":0.28453459977857937,"score_spread":0.2545504559544799,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2081011533","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9972748,0.0007555054,0.001464074,0.000023370978,0.000103685525,0.000114318034,0.000026468093,0.0000097481325,0.00022800577],"genre_scores_gemma":[0.9980733,0.00012308157,0.001725416,0.000015040973,0.0000117857335,0.000010690019,0.000023520519,0.000009540598,0.000007644489],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992861,0.000051323423,0.00025337635,0.00015624966,0.00012318134,0.00012973718],"domain_scores_gemma":[0.9994032,0.000097315555,0.00003036941,0.0004359136,0.000016206594,0.000016991067],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002787704,0.00011617172,0.00024554532,0.00012524921,0.000020571795,0.000015424443,0.00020247164,0.000059795108,0.000033322704],"category_scores_gemma":[0.000060972623,0.00008358825,0.000038957936,0.00038955203,0.00005319038,0.000056463974,0.000035907004,0.000104461964,2.2213193e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00007982395,0.00047950103,0.02356691,0.00014118516,0.0013088639,0.000014685455,0.025400206,0.49873024,0.44394392,0.0025830388,0.0010378921,0.002713744],"study_design_scores_gemma":[0.0005029734,0.000057470723,0.0021795828,0.000042212723,0.00007615911,0.0000026333237,0.003740863,0.93129337,0.061141837,0.00010005888,0.00068589573,0.00017692891],"about_ca_topic_score_codex":0.0001052123,"about_ca_topic_score_gemma":0.000037450467,"teacher_disagreement_score":0.43256316,"about_ca_system_score_codex":0.000032484066,"about_ca_system_score_gemma":0.000014210877,"threshold_uncertainty_score":0.34086302},"labels":[],"label_agreement":null},{"id":"W2083263473","doi":"10.1615/atomizspr.v16.i8.70","title":"TRAJECTORY OF WATER JET EXPOSED TO LOW SUBSONIC CROSS-FLOW","year":2006,"lang":"en","type":"article","venue":"Atomization and Sprays","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":37,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Manitoba","funders":"","keywords":"Jet (fluid); Nozzle; Mechanics; Supersonic speed; Physics; Range (aeronautics); Momentum (technical analysis); Trajectory; Flow (mathematics); Flux (metallurgy); Classical mechanics; Materials science; Aerospace engineering; Thermodynamics; Engineering","score_opus":0.004046778818415188,"score_gpt":0.19169710244146537,"score_spread":0.18765032362305017,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2083263473","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.91577744,0.000055312117,0.08228386,0.000017396547,0.00018655998,0.00008807532,0.000014710107,0.00007512093,0.0015015122],"genre_scores_gemma":[0.99755055,0.000027529997,0.0020444721,0.00003434593,0.000063517844,0.0000049530163,0.000041371688,0.00002288224,0.00021035335],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994851,0.0000069835273,0.00018497212,0.00010142715,0.00007966347,0.00014186827],"domain_scores_gemma":[0.9997853,0.00001534503,0.000012804289,0.00010886796,0.00003838051,0.000039271523],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00007887041,0.00009119837,0.00011773669,0.00005219337,0.000036627895,0.000029607874,0.00005317233,0.000058334568,0.000083601466],"category_scores_gemma":[0.0000073977717,0.00007603571,0.00002549082,0.000072732306,0.000021993405,0.000054123695,0.000014093068,0.000047382364,0.000015452457],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000010183436,0.00002333062,0.0045216233,0.00006941719,0.0000115570865,0.0000024190017,0.0002097209,0.9266174,0.0657449,0.0012076226,0.00064481294,0.0009370128],"study_design_scores_gemma":[0.0005748613,0.000019416078,0.009013729,0.000017758613,0.000010163677,0.0000017559529,0.000012717185,0.9461995,0.042245734,0.00029389522,0.0014199446,0.00019055278],"about_ca_topic_score_codex":0.0000068631207,"about_ca_topic_score_gemma":0.000029844527,"teacher_disagreement_score":0.081773125,"about_ca_system_score_codex":0.000018872333,"about_ca_system_score_gemma":0.0000053227873,"threshold_uncertainty_score":0.3100646},"labels":[],"label_agreement":null},{"id":"W2084206767","doi":"10.1007/s00348-007-0305-3","title":"Experimental investigation of planar offset attaching jets with small offset distances","year":2007,"lang":"en","type":"article","venue":"Experiments in Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":47,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Offset (computer science); Planar; Reynolds number; Mechanics; Jet (fluid); Materials science; Convection; Optics; Physics; Turbulence","score_opus":0.01783614669575413,"score_gpt":0.25109425668872865,"score_spread":0.23325810999297453,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2084206767","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9682869,0.00093082315,0.026924584,0.000006073924,0.00037018102,0.00016407124,0.000020317879,0.00007959043,0.003217475],"genre_scores_gemma":[0.9828345,0.000012708368,0.016903788,0.000028154156,0.000066183056,0.00001739295,0.000059378697,0.000038930557,0.000038947634],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9988672,0.000017029473,0.0003940074,0.00020167914,0.0002356513,0.00028439402],"domain_scores_gemma":[0.99959165,0.00004330383,0.000046838628,0.00021830127,0.000019924792,0.00007996735],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024464665,0.00019733419,0.00021029876,0.00012550183,0.000047566726,0.000019126239,0.00017890373,0.00008292435,0.000023968567],"category_scores_gemma":[0.000007818307,0.00018721628,0.000029923336,0.00017987542,0.00009293996,0.000118817625,0.000027118323,0.00015342717,0.000003907662],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00009744225,0.00012812996,0.019050976,0.000072250106,0.000061771956,0.000043049276,0.0071896785,0.007972457,0.9608993,0.0030145512,0.00040501988,0.0010653742],"study_design_scores_gemma":[0.0014558876,0.000239217,0.0097501,0.00027957515,0.000011980764,0.000009767167,0.0030054208,0.054074313,0.9296557,0.00025361357,0.0006701637,0.0005942902],"about_ca_topic_score_codex":0.000033526627,"about_ca_topic_score_gemma":0.000051199706,"teacher_disagreement_score":0.046101857,"about_ca_system_score_codex":0.00019203324,"about_ca_system_score_gemma":0.000019844249,"threshold_uncertainty_score":0.76344585},"labels":[],"label_agreement":null},{"id":"W2084503368","doi":"10.1063/1.4767535","title":"Effects of passive control rings positioned in the shear layer and potential core of a turbulent round jet","year":2012,"lang":"en","type":"article","venue":"Physics of Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":45,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Queen's University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Physics; Turbulence; Mechanics; Instability; Jet (fluid); Reynolds number; Vortex ring; Nozzle; Vortex; Shear (geology); Shear flow; Turbulence kinetic energy; Classical mechanics; Materials science; Thermodynamics; Composite material","score_opus":0.005886807679387395,"score_gpt":0.20849750158950014,"score_spread":0.20261069391011274,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2084503368","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9778237,0.00032694015,0.02142801,0.00002006826,0.00009194194,0.00016866463,0.000022298405,0.0000071428035,0.00011124829],"genre_scores_gemma":[0.99948364,0.000042684842,0.00034350433,0.000016664177,0.00008650813,0.000009179827,0.000004262141,0.000012380269,0.0000011906693],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995031,0.000015321139,0.00016253135,0.000054426397,0.00013612187,0.00012853355],"domain_scores_gemma":[0.99967235,0.00011239693,0.00003878915,0.000112301015,0.000041768766,0.000022379187],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00008855881,0.00008811245,0.00019415891,0.000021594675,0.0000135617975,0.0000044702256,0.00008346739,0.000037240592,0.0000014575755],"category_scores_gemma":[0.000011066009,0.000069208094,0.000047253267,0.0000678721,0.000052664673,0.000067708716,0.000017414064,0.00008609271,4.2913655e-7],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00004122891,0.0003098958,0.001879763,0.0007089584,0.00014278005,0.0000037860996,0.0021744906,0.026124256,0.95015186,0.01731272,0.000093965806,0.0010562892],"study_design_scores_gemma":[0.0045396616,0.00039378705,0.0933318,0.00041030764,0.00046886463,0.000009916578,0.00028408997,0.7446371,0.14090471,0.014511156,0.000027818176,0.00048080375],"about_ca_topic_score_codex":0.000018588204,"about_ca_topic_score_gemma":4.9905447e-7,"teacher_disagreement_score":0.80924714,"about_ca_system_score_codex":0.000012182092,"about_ca_system_score_gemma":0.0000044487965,"threshold_uncertainty_score":0.2822224},"labels":[],"label_agreement":null},{"id":"W2084573563","doi":"10.1115/fedsm2006-98269","title":"Quantitative Investigation of Coherent Structures in a Free Jet Using PIV and POD","year":2006,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Windsor; University of Saskatchewan","funders":"","keywords":"Vortex; Jet (fluid); Particle image velocimetry; Mechanics; Reynolds number; Eddy; Physics; Vortex ring; Circulation (fluid dynamics); Turbulence; Nozzle; Turbulence kinetic energy; Rotation (mathematics); Kinetic energy; Classical mechanics; Geometry; Mathematics; Thermodynamics","score_opus":0.01351987160977996,"score_gpt":0.2226137252521117,"score_spread":0.20909385364233174,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2084573563","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9801721,0.00026004776,0.018178817,0.00001464228,0.00007935153,0.000056613113,0.000014101623,0.000021062056,0.0012032437],"genre_scores_gemma":[0.9629498,0.000009640713,0.0369977,0.0000053192075,0.000014417903,9.0449873e-7,0.000004728305,0.00000824014,0.0000092234795],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99969476,0.000006509723,0.00012625023,0.00005722002,0.000045194065,0.00007004011],"domain_scores_gemma":[0.9998619,0.00002700363,0.000016634536,0.0000660719,0.000015492407,0.000012929276],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00004207617,0.000058002173,0.00008140576,0.00004897993,0.000008867712,0.000008306515,0.00003539209,0.00003437132,0.000010016695],"category_scores_gemma":[0.000012041344,0.000053450738,0.00000830364,0.00007228859,0.00003571135,0.00004291254,0.000016044794,0.000051124967,1.4120123e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000048599422,0.000009633744,0.018588286,0.00014292535,0.000016353359,0.00000334287,0.00028946862,0.64382285,0.13996123,0.1962238,0.00048285478,0.00045443594],"study_design_scores_gemma":[0.00018413141,0.000013498622,0.029852873,0.000025253095,0.000005461573,0.0000012792154,0.00008030945,0.8757557,0.0023275455,0.091673315,0.0000057320467,0.00007489347],"about_ca_topic_score_codex":0.00050434144,"about_ca_topic_score_gemma":0.0010529005,"teacher_disagreement_score":0.2319329,"about_ca_system_score_codex":0.00002010994,"about_ca_system_score_gemma":0.000005354748,"threshold_uncertainty_score":0.21796578},"labels":[],"label_agreement":null},{"id":"W2086797461","doi":"10.1115/fedsm2005-77424","title":"Comparative Study of the Aeroacoustic Behavior of Two Axial Flow Fans With Different Sweep Angles","year":2005,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Ansys (Canada)","funders":"","keywords":"Aerodynamics; Acoustics; Computational fluid dynamics; Turbulence; Mechanics; Flow (mathematics); Physics","score_opus":0.013601028897424419,"score_gpt":0.2422160810475076,"score_spread":0.22861505215008318,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2086797461","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9795362,0.000018343986,0.018679673,0.0000051156776,0.00013820361,0.00040225498,0.000029852852,0.00004363522,0.0011467395],"genre_scores_gemma":[0.99796325,0.0000025578588,0.0018383196,0.0000035594933,0.00005417073,0.000026792763,0.0000025812076,0.00001884129,0.0000898997],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992551,0.000018745319,0.00024369839,0.00011323248,0.00022658546,0.00014262117],"domain_scores_gemma":[0.9995443,0.00004389639,0.00004613471,0.00027646468,0.000056877525,0.000032297925],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000037739286,0.0001545033,0.00027837232,0.000032554868,0.000038653878,0.0000085301535,0.0002004134,0.00002799451,0.000058608846],"category_scores_gemma":[0.000002743014,0.000089204565,0.000043856424,0.00010632134,0.000063838466,0.000031326417,0.000047171914,0.00012910558,0.0000012476527],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000011516132,0.0007050177,0.0074890223,0.000021324686,0.000090287176,0.000001216562,0.0019884421,0.9794001,0.008832495,0.00016396171,0.000064329324,0.0012322777],"study_design_scores_gemma":[0.001155015,0.0002914539,0.06294492,0.000027897268,0.00023647629,0.0000023179675,0.0017847406,0.9289185,0.004427687,0.00001961227,0.000005662786,0.0001857253],"about_ca_topic_score_codex":0.000039579252,"about_ca_topic_score_gemma":0.0025552725,"teacher_disagreement_score":0.055455897,"about_ca_system_score_codex":0.000033804266,"about_ca_system_score_gemma":0.0000079660185,"threshold_uncertainty_score":0.36376566},"labels":[],"label_agreement":null},{"id":"W2087343756","doi":"10.1016/j.ijheatmasstransfer.2009.03.029","title":"Reynolds number effects within the development region of a turbulent round free jet","year":2009,"lang":"en","type":"article","venue":"International Journal of Heat and Mass Transfer","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":161,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Queen's University","funders":"Syracuse University","keywords":"Reynolds number; Turbulence; Mechanics; Physics; Jet (fluid); Nozzle; Turbulence kinetic energy; Reynolds stress; Thermodynamics","score_opus":0.00666047277659002,"score_gpt":0.21770472719500183,"score_spread":0.21104425441841182,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2087343756","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8820072,0.00029616864,0.115020186,0.0010762439,0.00072389515,0.00006123976,0.0000021721241,0.000009529281,0.0008033836],"genre_scores_gemma":[0.9975692,0.000210646,0.0019296843,0.000111700814,0.00013656648,0.000001004447,0.0000012210359,0.000008404133,0.00003157256],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99925584,0.00001201249,0.0003229559,0.0000512667,0.0002795745,0.00007838305],"domain_scores_gemma":[0.9997007,0.000051683408,0.000019719693,0.000068976566,0.00012137994,0.000037526734],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001608206,0.00009223555,0.00013074887,0.000046282777,0.00002315809,0.000028503366,0.00022146176,0.000044573946,0.000007119124],"category_scores_gemma":[0.000011903617,0.000060386752,0.000057335576,0.00003158129,0.000022793743,0.00008146651,0.0000061894416,0.00016442161,6.3688435e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0020640853,0.0012520615,0.017215032,0.0008679029,0.0058172857,0.0028205945,0.024949927,0.4066865,0.30730936,0.108421646,0.019436117,0.10315949],"study_design_scores_gemma":[0.025075367,0.0023607716,0.1409307,0.006154824,0.00106861,0.0095458785,0.0012295082,0.34560168,0.2652264,0.15105,0.0486994,0.0030568899],"about_ca_topic_score_codex":0.0000018476599,"about_ca_topic_score_gemma":0.0000080410355,"teacher_disagreement_score":0.12371566,"about_ca_system_score_codex":0.000047097208,"about_ca_system_score_gemma":0.000021867656,"threshold_uncertainty_score":0.24625003},"labels":[],"label_agreement":null},{"id":"W2087832967","doi":"10.1080/00221686.2004.9641222","title":"The effect of background turbulence on jet entrainment: an experimental study of a plane jet in a shallow coflow","year":2004,"lang":"en","type":"article","venue":"Journal of Hydraulic Research","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":35,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"","keywords":"Dilution; Turbulence; Entrainment (biomusicology); Effluent; Jet (fluid); Plume; Mechanics; Buoyancy; Environmental science; Turbulent diffusion; Diffusion; Chemistry; Physics; Meteorology; Thermodynamics; Environmental engineering","score_opus":0.030230469120529346,"score_gpt":0.33770392077273803,"score_spread":0.3074734516522087,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2087832967","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9982987,0.00047893907,0.000048330014,0.000040591043,0.00016864874,0.00036056162,0.0000053225413,0.000005053672,0.00059387827],"genre_scores_gemma":[0.99961764,0.00017353761,0.000078822966,0.000003671998,0.00008622524,0.000010986332,0.0000010575931,0.000022951159,0.0000050984418],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99755764,0.0002580657,0.000569535,0.00012673189,0.0011338438,0.00035419993],"domain_scores_gemma":[0.9988329,0.000574262,0.00010731055,0.00029512364,0.0000800329,0.00011041408],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0026874123,0.00014871875,0.0003519998,0.0002370241,0.00007269953,0.000043950946,0.0005665244,0.000060677692,0.00001879528],"category_scores_gemma":[0.00010937102,0.00009400714,0.00007150932,0.00028603815,0.000117040654,0.000110349065,0.000064604785,0.0007413528,0.000002776043],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0021066812,0.0039194115,0.009948078,0.00028378644,0.00037306646,0.00093490153,0.010196599,0.77796656,0.19018158,0.00037304932,0.00024986258,0.0034664117],"study_design_scores_gemma":[0.04147821,0.16490464,0.051897015,0.0031007924,0.00014249675,0.0005243938,0.03824209,0.3336053,0.36192426,0.0021461833,0.00066759967,0.0013670068],"about_ca_topic_score_codex":0.00006673058,"about_ca_topic_score_gemma":0.00013319986,"teacher_disagreement_score":0.44436127,"about_ca_system_score_codex":0.00025252308,"about_ca_system_score_gemma":0.000045241377,"threshold_uncertainty_score":0.38335},"labels":[],"label_agreement":null},{"id":"W2088451011","doi":"10.1121/1.4806621","title":"Effects of scalloping depth on the sound generated by turbofan engine lobed mixers","year":2013,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"","keywords":"Turbofan; Acoustics; Mach number; Nozzle; Noise (video); Aeroacoustics; Jet engine; Shroud; Computer science; Solver; Flow (mathematics); Physics; Aerospace engineering; Mechanics; Sound pressure; Engineering; Structural engineering","score_opus":0.004717115415308274,"score_gpt":0.1942445559914575,"score_spread":0.18952744057614923,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2088451011","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.5872851,0.00068190583,0.40879175,0.0022190977,0.0004978066,0.00031138508,0.000010036542,0.000024311355,0.00017862159],"genre_scores_gemma":[0.99089086,0.0006912067,0.0075292317,0.0006670927,0.00014842731,0.0000026789742,5.974799e-7,0.00003352284,0.00003635179],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9986689,0.00010335697,0.00044544417,0.00007206934,0.0004363209,0.00027392627],"domain_scores_gemma":[0.99796534,0.0012436314,0.00026740588,0.0002916585,0.00015587175,0.000076096745],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00037335372,0.00018865419,0.00034625368,0.000013893019,0.00012916252,0.000022537559,0.00071936694,0.0000842719,0.000035982644],"category_scores_gemma":[0.00023388883,0.000088015804,0.00032354976,0.00025630512,0.00043580108,0.000047208217,0.000092160575,0.00061983184,0.000004432359],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00002313439,0.00009507199,0.000025160602,0.00014423892,0.00048127986,5.4322135e-7,0.00044845467,0.52695537,0.39963198,0.000016649446,0.06661265,0.005565466],"study_design_scores_gemma":[0.0003172108,0.00016068139,0.00054541975,0.00014164539,0.000246035,0.000009203499,0.00041474463,0.98182786,0.015136787,0.0008729623,0.0001892759,0.00013820577],"about_ca_topic_score_codex":0.000025388656,"about_ca_topic_score_gemma":2.9673157e-7,"teacher_disagreement_score":0.45487246,"about_ca_system_score_codex":0.0000727863,"about_ca_system_score_gemma":0.000024455021,"threshold_uncertainty_score":0.35891804},"labels":[],"label_agreement":null},{"id":"W2088828026","doi":"10.1063/1.2182006","title":"Formation of vortex dipoles","year":2006,"lang":"en","type":"article","venue":"Physics of Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":59,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Memorial University of Newfoundland","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Physics; Vorticity; Vortex; Dipole; Vortex ring; Mechanics; Jet (fluid); Classical mechanics; Quantum mechanics","score_opus":0.005479513845150453,"score_gpt":0.1918385043971831,"score_spread":0.18635899055203267,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2088828026","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.64120877,0.00014760299,0.34999692,0.0000047596877,0.000117106174,0.000040430074,0.000030592353,0.000041817555,0.008411987],"genre_scores_gemma":[0.9977437,0.000024148178,0.0020888506,0.000001552402,0.000092939335,0.0000015713376,0.000018435123,0.000011301802,0.000017477927],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996433,0.0000021359865,0.00015999534,0.000034938672,0.000087771936,0.00007184471],"domain_scores_gemma":[0.999805,0.000014089546,0.000023550045,0.00011000426,0.000038553735,0.000008847297],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000029367664,0.00005522239,0.0000976161,0.000015935759,0.000009415514,0.000003128797,0.000066409426,0.000022034015,0.000003286748],"category_scores_gemma":[0.0000023460234,0.000056972942,0.000039206796,0.000067334426,0.000022756994,0.00007766692,0.000011576093,0.000034202283,0.0000028520299],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000018122274,0.000051743093,0.00027133196,0.0002466233,0.000015332802,2.7902846e-7,0.000100647885,0.2945962,0.62234694,0.074828476,0.0008154707,0.0067251446],"study_design_scores_gemma":[0.00010906093,0.000013570479,0.0010819859,0.00002396554,0.00001565308,2.4204368e-7,0.000011384517,0.84631747,0.11920366,0.032986525,0.00015096097,0.00008550811],"about_ca_topic_score_codex":0.000013536972,"about_ca_topic_score_gemma":0.0000027192764,"teacher_disagreement_score":0.5517213,"about_ca_system_score_codex":0.000010342404,"about_ca_system_score_gemma":0.0000030976541,"threshold_uncertainty_score":0.2323289},"labels":[],"label_agreement":null},{"id":"W2090246056","doi":"10.1016/j.jfluidstructs.2013.09.021","title":"Effect of nozzle thickness on the self-excited impinging planar jet","year":2013,"lang":"en","type":"article","venue":"Journal of Fluids and Structures","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":15,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"","keywords":"Oscillation (cell signaling); Jet (fluid); Nozzle; Mechanics; Physics; Transonic; Acoustics; Instability; Flow visualization; Materials science; Flow (mathematics); Aerodynamics; Chemistry","score_opus":0.0033479059035301873,"score_gpt":0.2022519373532739,"score_spread":0.19890403144974372,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2090246056","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9975648,0.00039051982,0.0010978476,0.00009793931,0.0003603825,0.00007575077,0.000005193939,0.000014857423,0.00039270025],"genre_scores_gemma":[0.99910337,0.0001614315,0.00051257457,0.000040068546,0.0001619853,9.749912e-7,5.0482583e-7,0.000013961034,0.0000051042275],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99939424,0.000034150708,0.00023836929,0.000050146646,0.0001614158,0.000121692596],"domain_scores_gemma":[0.99945664,0.00027060666,0.000069413516,0.000100755286,0.00005603788,0.000046535046],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00026083205,0.00012060008,0.00021909198,0.00006800606,0.00005911564,0.00004444616,0.00013981262,0.000062219384,0.000036224064],"category_scores_gemma":[0.00004763179,0.000062124054,0.00006534612,0.00006165828,0.000029178142,0.00005703272,0.000012312448,0.00026507233,6.8280764e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0002299356,0.000058258134,0.010545599,0.0016192648,0.0015639544,0.00009097241,0.0030580978,0.12730359,0.7374742,0.032766093,0.026545351,0.058744684],"study_design_scores_gemma":[0.0024546366,0.0024896264,0.08804837,0.00063299807,0.00039123656,0.0006266987,0.00044265398,0.83858407,0.045828708,0.017955983,0.0017430465,0.000801954],"about_ca_topic_score_codex":0.0000053049916,"about_ca_topic_score_gemma":7.557458e-7,"teacher_disagreement_score":0.7112805,"about_ca_system_score_codex":0.000014918488,"about_ca_system_score_gemma":0.0000071362792,"threshold_uncertainty_score":0.25333455},"labels":[],"label_agreement":null},{"id":"W2090776283","doi":"10.1115/fedsm2006-98458","title":"Two-Point Correlations of the Near and Far-Field Pressure in a Transonic Jet","year":2006,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":40,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Air Force Office of Scientific Research; Natural Sciences and Engineering Research Council of Canada; National Science Foundation","keywords":"Jet (fluid); Azimuth; Near and far field; Transonic; Field (mathematics); Point source; Rotational symmetry; Mach number; Physics; Sound pressure; Mechanics; Acoustics; Optics; Aerodynamics; Mathematics","score_opus":0.002948977345196101,"score_gpt":0.18178685570442515,"score_spread":0.17883787835922904,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2090776283","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.91069746,0.00063068816,0.051825326,0.00027040023,0.00021512092,0.00018222071,0.000017392025,0.000055054796,0.036106337],"genre_scores_gemma":[0.9985036,0.000022924689,0.0011562482,0.000018188006,0.0000135837845,0.0000030704628,9.0889864e-7,0.000007456798,0.00027400136],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997237,0.0000052832756,0.000099275334,0.00005069772,0.000045669818,0.00007538343],"domain_scores_gemma":[0.999827,0.00004702774,0.000008483325,0.000100791905,0.0000076033625,0.000009057499],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00004249096,0.00005015555,0.00006516559,0.00001326137,0.000021343887,0.000009437541,0.000054591088,0.00003657966,0.00004204832],"category_scores_gemma":[0.0000074258746,0.000036000678,0.000020932112,0.00007239006,0.000019092184,0.000023394616,0.000010968709,0.00010568308,7.8306476e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000015204793,0.000014982387,0.010370174,0.000031465137,0.000009332955,5.839742e-7,0.0001088506,0.966147,0.0017514011,0.020224137,0.0007823868,0.000558138],"study_design_scores_gemma":[0.00017703236,0.0000065164213,0.016840056,0.000013639283,0.000012789438,0.0000012762999,0.000022530085,0.98074204,0.00023348558,0.0010332688,0.0008651768,0.000052162635],"about_ca_topic_score_codex":0.00018362574,"about_ca_topic_score_gemma":0.0013629362,"teacher_disagreement_score":0.08780616,"about_ca_system_score_codex":0.000004868687,"about_ca_system_score_gemma":0.0000055555956,"threshold_uncertainty_score":0.1468065},"labels":[],"label_agreement":null},{"id":"W2091209377","doi":"10.1016/j.jsv.2005.01.023","title":"Control of tonal noise from subsonic axial fan. Part 1: reconstruction of aeroacoustic sources from far-field sound pressure","year":2005,"lang":"en","type":"article","venue":"Journal of Sound and Vibration","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":46,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"AUTO21 Network of Centres of Excellence","keywords":"Acoustics; Sound pressure; Aeroacoustics; Harmonics; Noise (video); Near and far field; Inverse problem; Acoustic source localization; Physics; Acoustic wave; Computer science; Mathematics; Mathematical analysis; Optics","score_opus":0.006513864727711817,"score_gpt":0.19787519002784343,"score_spread":0.1913613253001316,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2091209377","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.74076277,0.00096982677,0.25758457,0.000037666756,0.00044414663,0.000045856454,0.000089632355,0.00000773984,0.000057795165],"genre_scores_gemma":[0.99628675,0.00020411378,0.0024506785,0.000022851958,0.0010046554,6.894698e-7,0.000010234009,0.000012725854,0.0000072887337],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9990508,0.000023314904,0.00054228446,0.000085447755,0.0001975951,0.00010054892],"domain_scores_gemma":[0.9992556,0.00019554827,0.0003129331,0.00008369727,0.000098794066,0.000053432595],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00013950841,0.00011315483,0.0002799444,0.00006332398,0.000044869736,0.000041556254,0.00007898516,0.00012401593,0.00011430628],"category_scores_gemma":[0.000051179395,0.00010242556,0.00008061228,0.00003957546,0.000045383422,0.00028196597,0.0000091215115,0.00019914309,6.648534e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00037453356,0.00011784149,0.022658462,0.00012346376,0.0007105268,0.0000033453427,0.0011814651,0.7144737,0.23443237,0.00051032094,0.0002732741,0.02514068],"study_design_scores_gemma":[0.0022868156,0.00036445181,0.014470731,0.0002039831,0.00060373696,0.00003309694,0.000472469,0.9608622,0.009203914,0.010826019,0.0003950519,0.0002775204],"about_ca_topic_score_codex":0.000025057068,"about_ca_topic_score_gemma":0.000079692574,"teacher_disagreement_score":0.25552398,"about_ca_system_score_codex":0.000018193721,"about_ca_system_score_gemma":0.000022344171,"threshold_uncertainty_score":0.4176793},"labels":[],"label_agreement":null},{"id":"W2091409042","doi":"10.1017/s0022112006004538","title":"Two-point similarity in the round jet","year":2007,"lang":"en","type":"article","venue":"Journal of Fluid Mechanics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":53,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"","keywords":"Reynolds number; Physics; Turbulence; Jet (fluid); Similarity (geometry); Mechanics; Dynamic similarity; Classical mechanics; Statistical physics; Mathematical analysis; Mathematics","score_opus":0.010589620278532946,"score_gpt":0.23971200781767227,"score_spread":0.22912238753913933,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2091409042","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.4767594,0.0005747867,0.5189432,0.00017796438,0.0015435393,0.000083297586,0.0000044615317,0.000019392475,0.0018939506],"genre_scores_gemma":[0.994251,0.00030533547,0.0048764236,0.00020306998,0.00033841174,4.018236e-7,6.396033e-7,0.00001839938,0.000006288398],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989711,0.000020909338,0.0004429472,0.000055020464,0.00028453858,0.0002254714],"domain_scores_gemma":[0.9994947,0.00013410939,0.00007190207,0.00016539417,0.00007682892,0.000057078534],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0022781836,0.00010934277,0.00017284557,0.00009878689,0.00003430923,0.00003698648,0.00030678496,0.000070863156,0.000016839635],"category_scores_gemma":[0.0000935024,0.000076565615,0.000089431094,0.00017366231,0.000006809392,0.00010317715,0.000022691867,0.0005229288,0.0000036402746],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00012256578,0.00039897245,0.00030214546,0.00014671496,0.00020006736,0.0017197514,0.002288752,0.59961504,0.21068415,0.15838239,0.01126211,0.014877324],"study_design_scores_gemma":[0.0008582181,0.00016146249,0.0003086171,0.000071343,0.000051360148,0.0004052376,0.0009163307,0.9655468,0.003469124,0.024332771,0.0036446147,0.00023414295],"about_ca_topic_score_codex":0.0000031804116,"about_ca_topic_score_gemma":0.00008551776,"teacher_disagreement_score":0.51749164,"about_ca_system_score_codex":0.00011614737,"about_ca_system_score_gemma":0.000021398286,"threshold_uncertainty_score":0.31222552},"labels":[],"label_agreement":null},{"id":"W2092693031","doi":"10.1115/pvp2011-57437","title":"Aeroacoustic Source of a Shallow Cavity in a Pipeline","year":2011,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":9,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"","keywords":"Strouhal number; Acoustics; Dimensionless quantity; Oscillation (cell signaling); Physics; Acoustic source localization; Acoustic resonance; Turbulence; Mechanics; Acoustic wave; Resonator; Optics; Reynolds number","score_opus":0.014713824638566238,"score_gpt":0.1861409317478919,"score_spread":0.17142710710932565,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2092693031","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6596091,0.000047199,0.30061194,0.0000028985885,0.00013076197,0.00007039895,0.000004382663,0.00010212251,0.039421216],"genre_scores_gemma":[0.99168706,0.000020447424,0.0077591157,0.000013422499,0.000020337538,0.000004458693,0.0000018277991,0.000020220074,0.0004731158],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99947375,0.000005488998,0.00019938267,0.00008889554,0.00007449063,0.00015800846],"domain_scores_gemma":[0.9997407,0.00002191815,0.000014727423,0.00016486025,0.000020813424,0.00003695489],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00010640184,0.0000884811,0.00014044128,0.00006259967,0.000007429158,0.000002820835,0.000115687,0.000057128793,0.00020874609],"category_scores_gemma":[0.000023499177,0.00008383034,0.000030870196,0.00012180054,0.000023499244,0.000028973882,0.000028136785,0.00011289306,0.000013350176],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000418224,0.00050629204,0.02734721,0.0005507895,0.00006767581,0.00006888167,0.0037035279,0.8996302,0.036499426,0.004840026,0.0017552841,0.024988865],"study_design_scores_gemma":[0.00018625728,0.000014771617,0.0052625653,0.000019530838,0.000008978794,0.0000023524474,0.000089930334,0.99318177,0.00058234826,0.00046681243,0.000066357796,0.00011834187],"about_ca_topic_score_codex":0.00019030522,"about_ca_topic_score_gemma":0.00053161243,"teacher_disagreement_score":0.33207798,"about_ca_system_score_codex":0.000022826598,"about_ca_system_score_gemma":0.000006868115,"threshold_uncertainty_score":0.34185022},"labels":[],"label_agreement":null},{"id":"W2093137888","doi":"10.1121/1.3384291","title":"Toward the prediction of fan noise: From low-speed to high-speed turbomachineries.","year":2010,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Turbofan; Noise (video); Train; Computer science; Jet engine; Duct (anatomy); Turbomachinery; Aeroacoustics; Airplane; Aircraft noise; Fan-in; Automotive engineering; Acoustics; Aerospace engineering; Noise reduction; Sound pressure; Engineering; Physics; Telecommunications","score_opus":0.006814717430456025,"score_gpt":0.20703236366695008,"score_spread":0.20021764623649405,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2093137888","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.76596683,0.00010346924,0.2266992,0.0047177216,0.0018781713,0.00020608361,0.0002216919,0.00003309556,0.00017370968],"genre_scores_gemma":[0.98517466,0.00021640278,0.013501444,0.0004423867,0.00059964857,6.3446765e-7,0.0000021590001,0.00003395075,0.000028694334],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99844444,0.000058421185,0.0005920148,0.00009067077,0.00057230657,0.00024213304],"domain_scores_gemma":[0.99831814,0.0005521566,0.00030377376,0.0005128732,0.000204829,0.00010821723],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00045541974,0.0001894686,0.00038551848,0.000017269705,0.00012499679,0.000021201213,0.0010598383,0.000114582486,0.000088579574],"category_scores_gemma":[0.0002787198,0.00009223737,0.00036161172,0.00028157115,0.0005441212,0.000062007515,0.00019967984,0.0010349653,0.0000034758464],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00006572818,0.00006374038,0.000084313346,0.00003430132,0.00027202704,5.359271e-7,0.0018958991,0.33189517,0.6475556,0.000016256025,0.014818775,0.0032976791],"study_design_scores_gemma":[0.00040468844,0.00016001187,0.007445314,0.0000751647,0.00039446776,0.000017486014,0.0012735522,0.98072296,0.007325568,0.0012858985,0.0007514277,0.00014342851],"about_ca_topic_score_codex":0.00013554629,"about_ca_topic_score_gemma":0.0000026295606,"teacher_disagreement_score":0.64882785,"about_ca_system_score_codex":0.000048968952,"about_ca_system_score_gemma":0.000044739143,"threshold_uncertainty_score":0.44964668},"labels":[],"label_agreement":null},{"id":"W2094543791","doi":"10.1121/1.2934516","title":"Trailing edge noise computation of a fan blade profile","year":2008,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":6,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Trailing edge; Airfoil; Acoustics; Noise (video); Chord (peer-to-peer); Computation; Microphone; Sound pressure; Leading edge; Reynolds number; Aeroacoustics; Physics; Computer science; Aerospace engineering; Engineering; Mechanics; Turbulence; Algorithm","score_opus":0.010891407886620977,"score_gpt":0.2229548371558061,"score_spread":0.21206342926918514,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2094543791","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.26903683,0.00026127242,0.7298477,0.00026118237,0.00023662054,0.000089046946,0.000013529597,0.000014008948,0.00023978116],"genre_scores_gemma":[0.95720667,0.00049267354,0.042033315,0.00009472287,0.00012783619,4.91288e-7,3.8778697e-7,0.0000190915,0.000024813344],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99893516,0.00004224959,0.00046352838,0.000048533027,0.00034529532,0.00016525727],"domain_scores_gemma":[0.9991075,0.00026337683,0.00027298415,0.00015656448,0.00014778884,0.00005182813],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00026339586,0.000110601606,0.00028635567,0.000014481385,0.00010643079,0.0000040810096,0.00037819307,0.000057394995,0.000013603743],"category_scores_gemma":[0.000056055513,0.00006473147,0.0003008015,0.00020945707,0.00046599875,0.000045242712,0.00005975384,0.00039576617,0.000001376629],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00002314518,0.000067031346,0.00006480946,0.00008869296,0.00014108626,9.1886585e-7,0.0015309894,0.90009564,0.08623763,0.000004513061,0.0052904873,0.006455039],"study_design_scores_gemma":[0.00021681593,0.00009345001,0.0010937797,0.00007121942,0.00013160752,0.00005166366,0.0007437011,0.99481815,0.0024236906,0.00018427962,0.0000951524,0.00007647685],"about_ca_topic_score_codex":0.0000060425323,"about_ca_topic_score_gemma":1.14840894e-7,"teacher_disagreement_score":0.68816984,"about_ca_system_score_codex":0.00003528202,"about_ca_system_score_gemma":0.000047797497,"threshold_uncertainty_score":0.26396725},"labels":[],"label_agreement":null},{"id":"W2095269742","doi":"10.1007/s00348-001-0391-6","title":"Rayleigh scattering in supersonic high-temperature exhaust plumes","year":2002,"lang":"en","type":"article","venue":"Experiments in Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto","funders":"","keywords":"Plume; Supersonic speed; Rayleigh scattering; Mechanics; Nozzle; Jet (fluid); Turbulence; Choked flow; Materials science; Flow (mathematics); Scattering; Physics; Meteorology; Optics; Thermodynamics","score_opus":0.010676051091661472,"score_gpt":0.21117947409456225,"score_spread":0.20050342300290078,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2095269742","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99233234,0.0021120603,0.00005928066,0.00003925299,0.0010068102,0.00015255364,0.000008402435,0.00013590892,0.004153398],"genre_scores_gemma":[0.9973501,0.0003304879,0.0013103338,0.00006674392,0.00014798593,0.00006020049,0.0000102845925,0.000063805615,0.00066004304],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99878407,0.000017982016,0.0003083641,0.0002714381,0.00017792558,0.00044023397],"domain_scores_gemma":[0.99959177,0.000020743712,0.000010517454,0.00030244674,0.000010103953,0.000064415544],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.000088745735,0.00024297147,0.00024666518,0.00018336409,0.00004131989,0.000066003195,0.00025113154,0.00015929774,0.00079886545],"category_scores_gemma":[0.000010732341,0.00026417154,0.00004059051,0.00027487907,0.000039618142,0.00017660898,0.0000658017,0.00034016167,0.000088408306],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000009077198,0.00022612835,0.0061796317,0.000084853855,0.00004349743,0.00019688292,0.004893154,0.05173117,0.9296111,0.0008009032,0.0050647473,0.0011588638],"study_design_scores_gemma":[0.00581045,0.0001741629,0.017174747,0.0007375705,0.000020474625,0.000035133387,0.0022566896,0.7888819,0.17720012,0.00041176757,0.0046706083,0.0026263779],"about_ca_topic_score_codex":0.00003253117,"about_ca_topic_score_gemma":0.00002221634,"teacher_disagreement_score":0.75241095,"about_ca_system_score_codex":0.0003434474,"about_ca_system_score_gemma":0.0000064702162,"threshold_uncertainty_score":0.99998105},"labels":[],"label_agreement":null},{"id":"W2096073130","doi":"10.5539/mas.v5n5p64","title":"Analytical and Numerical Investigation of Transient Gas Blow down","year":2011,"lang":"en","type":"article","venue":"Modern Applied Science","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Isentropic process; Mechanics; Transient (computer programming); Stack (abstract data type); Isothermal process; Flow (mathematics); Conservation of mass; Transient flow; Volume (thermodynamics); Atmosphere (unit); Compressibility; Thermodynamics; Materials science; Physics; Meteorology; Computer science","score_opus":0.016400139236994224,"score_gpt":0.19753692278319143,"score_spread":0.18113678354619722,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2096073130","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.62957746,0.0000118046755,0.36356005,0.000007609307,0.00004039494,0.00005168437,0.0000020482355,0.00003477409,0.0067141913],"genre_scores_gemma":[0.99048394,0.000006604925,0.009465186,0.000018026318,0.000009697396,0.000004429369,6.1123905e-7,0.0000074153277,0.000004064793],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99931496,0.00000221449,0.00013413705,0.00017027259,0.00020668568,0.00017171803],"domain_scores_gemma":[0.9997053,0.000011830554,0.000014936962,0.00013989511,0.000022967932,0.00010505394],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018515406,0.00007443085,0.00009956787,0.00005873308,0.00004916893,0.000014158211,0.00015139954,0.00003105047,0.000019028857],"category_scores_gemma":[0.00000690099,0.000068414636,0.000013079843,0.00023099539,0.00041451078,0.000053501786,0.000027476939,0.00008115122,0.000002973714],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000010702201,0.000032722666,0.0010529751,0.000058133515,0.000011210286,0.0000026826103,0.004520852,0.02400188,0.91811484,0.031062253,0.00004084942,0.021090869],"study_design_scores_gemma":[0.000070798815,0.000011530041,0.0046111336,0.0000043047294,0.000007882866,0.0000015717535,0.000021328535,0.97886264,0.009361073,0.0069612237,0.0000059336057,0.00008058819],"about_ca_topic_score_codex":0.0000042247916,"about_ca_topic_score_gemma":0.0000011442754,"teacher_disagreement_score":0.95486075,"about_ca_system_score_codex":0.000019845902,"about_ca_system_score_gemma":0.00002028722,"threshold_uncertainty_score":0.27898678},"labels":[],"label_agreement":null},{"id":"W2097081826","doi":"10.1260/147547204323022248","title":"Airframe Noise Study of a Bombardier CRJ-700 Aircraft Model in the NASA Ames 7-by 10-Foot Wind Tunnel","year":2004,"lang":"en","type":"article","venue":"International Journal of Aeroacoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":24,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Bombardier (Canada)","funders":"","keywords":"Wind tunnel; Airframe; Landing gear; Takeoff; Aerodynamics; Scale model; Acoustics; Noise (video); Aircraft noise; Aeroacoustics; Aerospace engineering; Fuselage; Mach number; Airplane; Marine engineering; Full scale; Ceiling (cloud); Computer science; Structural engineering; Engineering; Physics; Sound pressure; Noise reduction","score_opus":0.00933754788906673,"score_gpt":0.24008540946208876,"score_spread":0.23074786157302202,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2097081826","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9105922,0.00013804711,0.08718723,0.00021139893,0.0008479795,0.00014656146,0.00008119591,0.000016362765,0.00077904516],"genre_scores_gemma":[0.99627984,0.00013285043,0.003089926,0.00010084004,0.00027558996,0.0000031773845,0.0000058728165,0.00003887396,0.00007302841],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99784684,0.000029828887,0.000809612,0.00013160473,0.00095961324,0.00022248861],"domain_scores_gemma":[0.9988455,0.000118209544,0.00023402997,0.00021353495,0.00051835977,0.00007036479],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00045147643,0.0002145499,0.00031572752,0.00021530244,0.00003489058,0.000070142756,0.0009163237,0.00010181312,0.000017187936],"category_scores_gemma":[0.00015795682,0.00017080597,0.00012844778,0.00016009425,0.00006794401,0.00016430287,0.000069589936,0.00055090064,0.0000045058896],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00004649129,0.000752259,0.00032186613,0.000013769695,0.00021887964,0.000091039,0.0019993456,0.9887024,0.0052163927,0.00021344937,0.0020896117,0.00033450645],"study_design_scores_gemma":[0.0042710453,0.0004509419,0.005404354,0.00022309228,0.00020686607,0.00018600488,0.0035646202,0.9787285,0.00027982122,0.0059925485,0.00025934685,0.0004328735],"about_ca_topic_score_codex":0.000023379349,"about_ca_topic_score_gemma":0.000034182136,"teacher_disagreement_score":0.08568766,"about_ca_system_score_codex":0.00022979871,"about_ca_system_score_gemma":0.000088908404,"threshold_uncertainty_score":0.6965265},"labels":[],"label_agreement":null},{"id":"W2097451411","doi":"10.1260/095745607780886433","title":"A Compact Active Control System for Tonal Noise Reduction in Axial Fans","year":2007,"lang":"en","type":"article","venue":"Noise & Vibration Worldwide","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Acoustics; Loudspeaker; Directivity; Microphone; Active noise control; Noise (video); Noise reduction; Sound pressure; Engineering; Noise control; Physics; Electrical engineering; Computer science","score_opus":0.007083966523861558,"score_gpt":0.22952499644842828,"score_spread":0.2224410299245667,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2097451411","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.37074068,0.000036126115,0.6218236,0.00014307065,0.0014849679,0.00075182744,0.000109509216,0.0002655397,0.0046446533],"genre_scores_gemma":[0.9971617,0.0000037185116,0.0019598845,0.0000363324,0.0005811879,0.00004135987,0.00008087441,0.000043348107,0.00009163083],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9988587,0.00002039545,0.0004087627,0.00020771162,0.00017775739,0.000326658],"domain_scores_gemma":[0.9994598,0.00014254551,0.0000698144,0.00016189436,0.00007727452,0.00008865816],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00033689578,0.00018423164,0.00023359754,0.00020292276,0.000086789965,0.00005068744,0.00010093829,0.000105811494,0.000020915435],"category_scores_gemma":[0.000038514554,0.00019926425,0.000084449144,0.00023797492,0.000025188498,0.0002318359,0.0000066762764,0.00019388732,0.000014201304],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00043264686,0.00006851678,0.00037186302,0.00014409058,0.000059624068,0.000010251378,0.00049094,0.76512444,0.22260392,0.0041788113,0.000993245,0.005521654],"study_design_scores_gemma":[0.0019514556,0.0000517604,0.012014422,0.0001025396,0.000040210805,0.000011483142,0.00041670055,0.9694802,0.014556248,0.00023645243,0.0008145917,0.000323894],"about_ca_topic_score_codex":0.000025159257,"about_ca_topic_score_gemma":0.00027387688,"teacher_disagreement_score":0.626421,"about_ca_system_score_codex":0.00042142984,"about_ca_system_score_gemma":0.000033368015,"threshold_uncertainty_score":0.81257606},"labels":[],"label_agreement":null},{"id":"W2097769797","doi":"10.1006/jfls.2000.0293","title":"FLOW PAST A 2-D BACKWARD-FACING STEP WITH AN OSCILLATING WALL","year":2000,"lang":"en","type":"article","venue":"Journal of Fluids and Structures","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":11,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Mechanics; Flow visualization; Oscillation (cell signaling); Amplitude; Flow (mathematics); Computational fluid dynamics; Flow separation; Visualization; Function (biology); Motion (physics); Geometry; Physics; Geology; Acoustics; Mathematics; Optics; Classical mechanics; Engineering; Mechanical engineering; Turbulence","score_opus":0.0047449016578434925,"score_gpt":0.1962825126525101,"score_spread":0.1915376109946666,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2097769797","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9916893,0.00041208955,0.0065482957,0.000028492675,0.00014598608,0.00003316882,0.00000715504,0.000023104469,0.0011123879],"genre_scores_gemma":[0.95739204,0.00021020247,0.041923843,0.000037468166,0.00036760178,2.4386947e-7,0.0000012452796,0.000023919769,0.000043413063],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99928564,0.000012745661,0.00025954522,0.00008468341,0.00018501813,0.00017236221],"domain_scores_gemma":[0.9996684,0.000021517526,0.0000398409,0.000098250704,0.000054194286,0.00011780524],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00011027593,0.00014065547,0.0002122891,0.00005447529,0.0000849964,0.00009206126,0.000097430784,0.00005881697,0.00014210472],"category_scores_gemma":[0.000005432066,0.00009692486,0.000038521324,0.00006189835,0.000032047403,0.00015349388,0.0000072759926,0.00023859025,5.4333645e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00008497803,0.00001016477,0.0021915252,0.00007583793,0.00013016562,0.0000950932,0.0008166415,0.7539361,0.00913504,0.00026670317,0.000689648,0.2325681],"study_design_scores_gemma":[0.0006885657,0.00040274643,0.011599762,0.00009635819,0.000054945394,0.0005549519,0.00019007399,0.98180395,0.00013843403,0.0010848072,0.0031159904,0.00026943412],"about_ca_topic_score_codex":0.0000040648624,"about_ca_topic_score_gemma":0.000011731103,"teacher_disagreement_score":0.23229867,"about_ca_system_score_codex":0.000021809772,"about_ca_system_score_gemma":0.000012387708,"threshold_uncertainty_score":0.3952481},"labels":[],"label_agreement":null},{"id":"W2098706074","doi":"10.2514/6.2009-496","title":"Radiation and Absorbing Boundary Conditions for the Lattice Boltzmann Method","year":2009,"lang":"en","type":"article","venue":"47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"","keywords":"Lattice Boltzmann methods; HPP model; Boundary value problem; Physics; Statistical physics; Computer science; Computational physics; Mechanics; Quantum mechanics","score_opus":0.014940272633266655,"score_gpt":0.2853416700855851,"score_spread":0.27040139745231845,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2098706074","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.42935804,0.007817562,0.5125622,0.04283241,0.002227699,0.001694503,0.00008398113,0.0006631183,0.0027604792],"genre_scores_gemma":[0.96821916,0.0008745438,0.029735666,0.0004682626,0.00043628667,0.00004403123,0.000015898162,0.00003288709,0.00017324246],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99826586,0.000062502426,0.00029698506,0.00042359845,0.0003296281,0.00062143145],"domain_scores_gemma":[0.99836415,0.0010178736,0.00014969216,0.00026146276,0.000060537834,0.00014630302],"candidate_categories":["sts"],"consensus_categories":[],"category_scores_codex":[0.0014205711,0.00030214892,0.00024230889,0.000091489026,0.0038712204,0.0006836925,0.00034235386,0.000121045276,0.0000032553608],"category_scores_gemma":[0.0002177889,0.00021468122,0.00008508482,0.00046340376,0.00034154093,0.0004780245,0.0000871755,0.00030606677,0.000002351975],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00013477806,0.00010845914,0.0026510179,0.00019191853,0.00027508466,0.000005462946,0.007933203,0.38081172,0.27811664,0.17741914,0.057563093,0.094789475],"study_design_scores_gemma":[0.0009795235,0.0007703186,0.0026192549,0.00031176442,0.00026132024,0.00006562623,0.006084107,0.95368946,0.0053412844,0.022456886,0.0066855988,0.0007348598],"about_ca_topic_score_codex":0.00007252675,"about_ca_topic_score_gemma":0.00009728364,"teacher_disagreement_score":0.5728777,"about_ca_system_score_codex":0.00008830121,"about_ca_system_score_gemma":0.00006241278,"threshold_uncertainty_score":0.9974256},"labels":[],"label_agreement":null},{"id":"W2099077653","doi":"10.2514/6.2011-2720","title":"A Modification to Logarithmic Spiral Beamforming Arrays for Aeroacoustic Applications","year":2011,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":14,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Independent Electricity System Operator; University of Adelaide","keywords":"Beamforming; Acoustics; Logarithmic spiral; Anechoic chamber; Logarithm; Noise (video); Spiral (railway); Range (aeronautics); Physics; Computer science; Engineering; Telecommunications; Mathematics; Geometry","score_opus":0.033859839023329556,"score_gpt":0.23919964092523613,"score_spread":0.20533980190190657,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2099077653","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.009631054,0.000011155361,0.9721331,0.000012294343,0.00015921974,0.00070641155,0.000027832633,0.00029810547,0.01702084],"genre_scores_gemma":[0.72054523,0.0000052667124,0.27817872,0.000055062148,0.000109178516,0.0006674804,0.000020648642,0.000031951204,0.0003864348],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993893,0.0000016284682,0.00017368911,0.00015443191,0.0000639484,0.00021703435],"domain_scores_gemma":[0.9995925,0.000022193663,0.000015419095,0.00023592751,0.000051638755,0.00008236509],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00007786434,0.000109314715,0.00009508322,0.00007198209,0.00007584061,0.000017023665,0.00016008795,0.000057152447,0.000030863324],"category_scores_gemma":[0.000011948691,0.00011133321,0.000040518666,0.00011778937,0.00001292734,0.00005675989,0.000017629247,0.00006366795,0.00006455727],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000018113848,0.00014228419,0.00007155776,0.00025937377,0.00007894794,9.335134e-7,0.0011389244,0.76069057,0.05334338,0.10633225,0.0032070568,0.074716605],"study_design_scores_gemma":[0.00013047771,0.000033476295,0.00012703947,0.0000069319035,0.000026175567,0.000001942768,0.00010721062,0.98886335,0.001179367,0.0039150016,0.005398662,0.00021034206],"about_ca_topic_score_codex":0.0000081976195,"about_ca_topic_score_gemma":0.000014161691,"teacher_disagreement_score":0.7109142,"about_ca_system_score_codex":0.000053641746,"about_ca_system_score_gemma":0.0000084670755,"threshold_uncertainty_score":0.45400366},"labels":[],"label_agreement":null},{"id":"W2099145561","doi":"10.1061/(asce)0733-9429(2007)133:2(234)","title":"Mean Flow Field of a Nonbuoyant Rectangular Surface Jet","year":2007,"lang":"en","type":"article","venue":"Journal of Hydraulic Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":16,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Calgary; Western University","funders":"","keywords":"Froude number; Jet (fluid); Laminar flow; Turbulence; Mechanics; Velocimetry; Free surface; Plane (geometry); Optics; Current (fluid); Laser Doppler velocimetry; Particle image velocimetry; Flow (mathematics); Physics; Geometry; Thermodynamics; Mathematics","score_opus":0.004085990414011245,"score_gpt":0.2071288620175218,"score_spread":0.20304287160351053,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2099145561","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.58934176,0.00096452463,0.40764537,0.000027703856,0.0009680097,0.00004150946,0.0000029456298,0.000045223962,0.0009629501],"genre_scores_gemma":[0.9570439,0.00017552024,0.042417884,0.000018826599,0.00028273702,2.0901545e-7,7.2812185e-7,0.00004382753,0.000016367489],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9987361,0.0000053158665,0.000621685,0.000075069285,0.00027975172,0.00028207025],"domain_scores_gemma":[0.9992961,0.0001909929,0.000113826914,0.00017772222,0.0000981821,0.00012316558],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006666972,0.00017214526,0.00034284827,0.00015588193,0.00001676975,0.000013548009,0.0002271639,0.00010358288,0.000027911092],"category_scores_gemma":[0.00012143508,0.00015943029,0.00015216367,0.00022135487,0.000010180093,0.00010206782,0.000025193138,0.00040835477,0.0000022767365],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000009997653,0.000015299778,0.00012709197,0.000093460025,0.00008628473,0.00010371039,0.00022854694,0.90782446,0.08922102,0.00009716421,0.00033541603,0.0018575664],"study_design_scores_gemma":[0.00035550096,0.00013597596,0.0004887442,0.00022779354,0.0000488853,0.00016675927,0.00006539241,0.93985206,0.05551143,0.000053393585,0.0028604043,0.00023368832],"about_ca_topic_score_codex":0.000004585907,"about_ca_topic_score_gemma":0.000008352551,"teacher_disagreement_score":0.36770216,"about_ca_system_score_codex":0.0000716298,"about_ca_system_score_gemma":0.000015233587,"threshold_uncertainty_score":0.65013784},"labels":[],"label_agreement":null},{"id":"W2099949641","doi":"10.1061/(asce)hy.1943-7900.0000588","title":"Dilution and Penetration of Vertical Negatively Buoyant Thermal Jets","year":2012,"lang":"en","type":"article","venue":"Journal of Hydraulic Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":13,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Western University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Froude number; Penetration (warfare); Dilution; Mechanics; Turbulence; Penetration depth; Nozzle; Thermocouple; Thermal; Jet (fluid); Plume; Thermodynamics; Meteorology; Materials science; Physics; Flow (mathematics); Optics","score_opus":0.005759237750829981,"score_gpt":0.19034182448602438,"score_spread":0.1845825867351944,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2099949641","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9091382,0.00091675203,0.089181274,0.00001930248,0.00042643255,0.000030033687,0.0000011943414,0.000017723938,0.0002690555],"genre_scores_gemma":[0.99602395,0.000113489965,0.0035694633,0.0000051828583,0.00026586594,6.5381283e-7,5.5212223e-7,0.000018608196,0.0000022494864],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99934965,0.0000069755915,0.0002975635,0.00003526225,0.000146852,0.00016367716],"domain_scores_gemma":[0.99971324,0.000054440497,0.00004243043,0.000055543227,0.000042405438,0.00009191254],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021229581,0.00009426695,0.00016177984,0.00008152839,0.0000145007925,0.000010315346,0.000059593327,0.000052775285,0.000007855789],"category_scores_gemma":[0.000060770108,0.00008395316,0.000043131175,0.00007085519,0.000015376534,0.00023665364,0.000013943289,0.0001844527,8.954017e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000066065177,0.00002349792,0.0009055372,0.00007875476,0.000055517874,0.0000037147192,0.00035575358,0.6360776,0.35983345,0.00076436077,0.000032984557,0.0018622347],"study_design_scores_gemma":[0.0003158486,0.000074556425,0.08073544,0.000097920696,0.00005138258,0.00008658097,0.000036160985,0.89555746,0.022574415,0.000034328903,0.00028645372,0.00014946061],"about_ca_topic_score_codex":0.0000010545494,"about_ca_topic_score_gemma":3.123181e-7,"teacher_disagreement_score":0.33725902,"about_ca_system_score_codex":0.00004133965,"about_ca_system_score_gemma":0.0000070175006,"threshold_uncertainty_score":0.34235105},"labels":[],"label_agreement":null},{"id":"W2102708499","doi":"10.1016/j.crme.2009.05.002","title":"A mean flow field solution to a moderately under/over-expanded turbulent supersonic jet","year":2009,"lang":"en","type":"article","venue":"Comptes Rendus Mécanique","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto","funders":"","keywords":"Inviscid flow; Jet (fluid); Turbulence; Supersonic speed; Physics; Reynolds number; Mechanics; Mathematics","score_opus":0.014225738894518994,"score_gpt":0.23507652752062683,"score_spread":0.22085078862610782,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2102708499","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.51034385,0.0006624554,0.48132133,0.0013096452,0.0005551196,0.0003866901,0.000028662815,0.00067219354,0.004720057],"genre_scores_gemma":[0.9899628,0.00017149778,0.008358534,0.0010965301,0.00018505444,0.00002135753,0.00003034773,0.00003839454,0.00013547839],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99878114,0.000025664915,0.00026174262,0.00028949344,0.00019256769,0.00044941602],"domain_scores_gemma":[0.99932164,0.00006022249,0.000022393517,0.0003570863,0.000050463634,0.00018821118],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.000110311375,0.00027624558,0.00027094656,0.00010125067,0.000111388836,0.00008891174,0.00025117668,0.00017417589,0.0002197628],"category_scores_gemma":[0.000021139578,0.00028073398,0.00009554994,0.00017871162,0.000013252008,0.000082062834,0.000038332157,0.00034912943,0.0000638283],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000061458784,0.000133677,0.000058267236,0.000051920233,0.00009416411,0.00005404128,0.00091179943,0.83427584,0.057393312,0.004813356,0.08158554,0.020566627],"study_design_scores_gemma":[0.00030841946,0.000238989,0.0005336945,0.000076043776,0.000019839043,0.000020441445,0.000041491185,0.98902166,0.005414011,0.00261563,0.0013025574,0.0004071974],"about_ca_topic_score_codex":0.000051641848,"about_ca_topic_score_gemma":0.00020613863,"teacher_disagreement_score":0.47961897,"about_ca_system_score_codex":0.0002360806,"about_ca_system_score_gemma":0.000033384855,"threshold_uncertainty_score":0.9999645},"labels":[],"label_agreement":null},{"id":"W2103678691","doi":"","title":"Prediction of Flow-Induced Noise in Aircraft Cylindrical Cabins","year":2010,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"University of Victoria","funders":"","keywords":"Takeoff; Noise (video); Aircraft noise; Noise control; Boundary layer; Turbulence; Acoustics; Jet engine; Aerospace engineering; Aeroacoustics; Takeoff and landing; Cruise; Flow (mathematics); Engineering; Computer science; Meteorology; Physics; Noise reduction; Mechanics","score_opus":0.009675243728834599,"score_gpt":0.19191336082935817,"score_spread":0.18223811710052357,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2103678691","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.973938,0.000017113603,0.018439332,0.000042748954,0.001966419,0.00014245172,0.0003569973,0.00007393853,0.005023027],"genre_scores_gemma":[0.9940103,0.000021594546,0.0055812993,0.000038406695,0.00021240373,0.0000072646667,0.000036876012,0.000043154872,0.000048646976],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9990883,0.0000063120096,0.0002777862,0.00014229896,0.00012532635,0.00035996299],"domain_scores_gemma":[0.999279,0.000039457525,0.000020418569,0.0002729165,0.000064378015,0.00032378908],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00011043632,0.00013969638,0.0001720679,0.00023751466,0.00003610382,0.000014986967,0.0001784881,0.0002535372,0.0000728483],"category_scores_gemma":[0.00010535493,0.00016361277,0.00003758537,0.00024081701,0.000041452786,0.000045197346,0.000013668139,0.00056244794,0.000016326927],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":true,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000022691336,0.000028936629,0.0025729623,0.00007740022,0.00001939754,0.000073690266,0.00022556874,0.49244124,0.49403837,0.0006263471,0.0017513502,0.008142467],"study_design_scores_gemma":[0.00019105192,0.000017720797,0.04192255,0.00001586304,0.00001729941,0.0000070518763,0.000030089306,0.95667225,0.00022076744,0.00014090497,0.0006255332,0.00013894128],"about_ca_topic_score_codex":0.00339666,"about_ca_topic_score_gemma":0.04032909,"teacher_disagreement_score":0.4938176,"about_ca_system_score_codex":0.0001881805,"about_ca_system_score_gemma":0.00021769111,"threshold_uncertainty_score":0.9771824},"labels":[],"label_agreement":null},{"id":"W2103704648","doi":"10.1016/j.apacoust.2005.12.007","title":"Experimental study of the noise emission of personal computer cooling fans","year":2006,"lang":"en","type":"article","venue":"Applied Acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":25,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of British Columbia","funders":"","keywords":"Noise (video); Acoustics; Acoustic emission; Engineering; Environmental science; Computer science; Physics; Artificial intelligence","score_opus":0.005796501487251559,"score_gpt":0.2013998673585112,"score_spread":0.19560336587125965,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2103704648","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9476789,0.00003737851,0.050263025,0.0000013440591,0.00032263072,0.00022280133,0.000021838881,0.000042606756,0.001409456],"genre_scores_gemma":[0.9974745,0.0000020631978,0.0022774027,0.000007393439,0.00017414936,0.000007548233,0.0000052547066,0.000029871813,0.000021844537],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992072,0.000006167384,0.00028158026,0.00011616868,0.00023917039,0.00014970408],"domain_scores_gemma":[0.99964,0.000043207132,0.00006309002,0.00019520501,0.00003382331,0.000024676057],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00005902513,0.0001350925,0.0001817285,0.000028297114,0.000059420374,0.000008688069,0.000184827,0.0000612425,0.000011361184],"category_scores_gemma":[0.0000023477298,0.000107241125,0.00004465145,0.00011051203,0.000051269417,0.000012640316,0.00008589473,0.00014000238,0.0000010951162],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000073324427,0.0003210771,0.0004500938,0.000038776998,0.00001864726,0.0000010309426,0.00069572247,0.54457295,0.4531671,0.00025173504,0.00031557298,0.00015995075],"study_design_scores_gemma":[0.0005792034,0.000066518085,0.0046052006,0.000024596056,0.000053145053,0.000001577633,0.001137651,0.9666202,0.026660936,0.000063521366,0.00003051902,0.00015689629],"about_ca_topic_score_codex":0.000013881084,"about_ca_topic_score_gemma":0.0000018633157,"teacher_disagreement_score":0.42650616,"about_ca_system_score_codex":0.000034301942,"about_ca_system_score_gemma":0.000010212761,"threshold_uncertainty_score":0.43731663},"labels":[],"label_agreement":null},{"id":"W2106354722","doi":"10.1115/pvp2014-28023","title":"Identification of Aeroacoustic Sources in a T-Junction","year":2014,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"","keywords":"Streamlines, streaklines, and pathlines; Acoustics; Sound power; Acoustic resonance; Physics; Acoustic source localization; Acoustic wave; Mechanics; Resonance (particle physics); Sound (geography)","score_opus":0.0032134278175409547,"score_gpt":0.1783042891367391,"score_spread":0.17509086131919815,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2106354722","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.62732685,0.000009523282,0.36933863,0.000005544389,0.00014925067,0.000028686696,5.6293567e-7,0.00004644832,0.003094504],"genre_scores_gemma":[0.9992834,0.000009086154,0.00044398682,0.00000449941,0.00002949582,0.000004023059,0.0000022456047,0.000008810698,0.00021447365],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99963856,0.0000059437402,0.00017187257,0.000056892895,0.000059666854,0.00006707591],"domain_scores_gemma":[0.99982977,0.000025902707,0.00001759149,0.000099356395,0.000015434738,0.000011972852],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00014683786,0.000043091306,0.00006436005,0.000060684717,0.000008205755,0.000007318922,0.000049371858,0.00003200462,0.000019473271],"category_scores_gemma":[0.00003072116,0.00004210582,0.000014073644,0.000070573355,0.000011537285,0.000031576088,0.0000064515752,0.00004477737,0.000011907592],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000012063995,0.000014129888,0.0012241078,0.000060557348,0.0000042825004,1.179328e-7,0.000092879,0.8727583,0.117956065,0.0033359153,0.00016573195,0.0043866592],"study_design_scores_gemma":[0.00007255891,0.000006536112,0.0055062813,0.000007386757,0.0000041710837,3.459469e-7,0.000038272978,0.9911127,0.0022368573,0.000884613,0.00008221806,0.00004806766],"about_ca_topic_score_codex":0.000011978056,"about_ca_topic_score_gemma":0.00006457121,"teacher_disagreement_score":0.37195653,"about_ca_system_score_codex":0.000015418806,"about_ca_system_score_gemma":0.0000016408021,"threshold_uncertainty_score":0.17170256},"labels":[],"label_agreement":null},{"id":"W2112365489","doi":"10.2514/6.2004-4080","title":"Shifted Cross-Wire for Supersonic Jet Control","year":2004,"lang":"en","type":"article","venue":"40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":17,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Nozzle; Jet (fluid); Mechanics; Thrust; Mach number; Core (optical fiber); Supersonic speed; Pitot tube; Mixing (physics); Physics; Materials science; Structural engineering; Optics; Engineering; Flow (mathematics); Thermodynamics","score_opus":0.01790839485082572,"score_gpt":0.23786335108552195,"score_spread":0.21995495623469624,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2112365489","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9539365,0.0006005009,0.0391749,0.00093121786,0.001026359,0.001394787,0.00047456616,0.00051980495,0.001941332],"genre_scores_gemma":[0.99474156,0.0003314333,0.003264228,0.00030303604,0.00035310892,0.0002144647,0.00016492303,0.00011038316,0.0005168928],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.997233,0.000030625768,0.0007303885,0.0007096482,0.00037570813,0.000920655],"domain_scores_gemma":[0.9985747,0.00009279503,0.000117179945,0.00054280786,0.00029701198,0.0003755607],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.000397266,0.0006012598,0.00071238115,0.00017233597,0.00041505357,0.0003806665,0.00031262203,0.00038190547,0.00022375396],"category_scores_gemma":[0.00017433078,0.00052912795,0.000229497,0.00020608267,0.00021100049,0.0003990081,0.000099827645,0.0005337508,0.000082326485],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0015426587,0.0016813104,0.018917898,0.007342782,0.0014208867,0.00052469014,0.0061036735,0.14382392,0.5466168,0.13179885,0.014079432,0.1261471],"study_design_scores_gemma":[0.036388215,0.0032678302,0.06628794,0.003119598,0.0008435885,0.00030774358,0.0019005398,0.73874485,0.023961708,0.09374651,0.024993673,0.0064378115],"about_ca_topic_score_codex":0.00007422161,"about_ca_topic_score_gemma":0.00031537388,"teacher_disagreement_score":0.59492093,"about_ca_system_score_codex":0.00016916764,"about_ca_system_score_gemma":0.00015774909,"threshold_uncertainty_score":0.99971604},"labels":[],"label_agreement":null},{"id":"W2112660203","doi":"10.1007/s10494-008-9133-7","title":"Mixing Measurements in a Supersonic Expansion-Ramp Combustor","year":2008,"lang":"en","type":"article","venue":"Flow Turbulence and Combustion","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":12,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"","keywords":"Freestream; Supersonic speed; Mechanics; Combustor; Mixing (physics); Nozzle; Materials science; Turbulence; Choked flow; Chemistry; Mach number; Thermodynamics; Combustion; Reynolds number; Physics","score_opus":0.023091509510584744,"score_gpt":0.20365790671934833,"score_spread":0.18056639720876358,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2112660203","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9910228,0.00090837374,0.0068938,0.00002442991,0.00048217498,0.0001262574,0.000004579035,0.00011874222,0.00041884108],"genre_scores_gemma":[0.99707675,0.000819961,0.00187754,0.000047367415,0.00006144089,0.00001628799,0.00001393354,0.000020989539,0.000065727356],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991792,0.000014797076,0.00018586607,0.00018254806,0.00019333097,0.00024424662],"domain_scores_gemma":[0.99971545,0.000022356478,0.000015823467,0.00014893671,0.000033330725,0.00006410185],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00013487099,0.00014837137,0.00015480588,0.00009156783,0.00011258955,0.000018581544,0.000095336836,0.000090712594,0.000029288198],"category_scores_gemma":[0.000021804202,0.00015411747,0.000028495158,0.00016440274,0.000044927005,0.00015072172,0.000024215124,0.00020745289,0.000017553833],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00003629058,0.00014866663,0.036336467,0.00024090832,0.0000407256,0.0000789233,0.002494824,0.92141557,0.0147293685,0.00012789306,0.0029942528,0.021356137],"study_design_scores_gemma":[0.0005336465,0.00003504899,0.013013139,0.00015755875,0.000010540462,0.000032706554,0.00011764553,0.985095,0.0004636725,0.00015215618,0.00012655628,0.00026230104],"about_ca_topic_score_codex":0.000018451392,"about_ca_topic_score_gemma":0.000025322686,"teacher_disagreement_score":0.06367949,"about_ca_system_score_codex":0.00007846519,"about_ca_system_score_gemma":0.000016147935,"threshold_uncertainty_score":0.6284728},"labels":[],"label_agreement":null},{"id":"W2117137668","doi":"10.1017/jfm.2013.465","title":"Effect of background turbulence on an axisymmetric turbulent jet","year":2013,"lang":"en","type":"article","venue":"Journal of Fluid Mechanics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":44,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"","keywords":"Turbulence; Physics; Entrainment (biomusicology); Jet (fluid); Reynolds number; Mechanics; Turbulence kinetic energy; Rotational symmetry; K-epsilon turbulence model; Mean flow; Classical mechanics","score_opus":0.007324700277064085,"score_gpt":0.22791674348804758,"score_spread":0.2205920432109835,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2117137668","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9671269,0.00048489464,0.0307322,0.00002825812,0.0011827064,0.00015034409,0.0000052770465,0.000027023849,0.00026236867],"genre_scores_gemma":[0.99696803,0.000519436,0.0021912328,0.000037987043,0.0002207245,0.0000029267032,0.000001603155,0.000039744664,0.000018339751],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9986796,0.000058024518,0.00051200046,0.0001037024,0.00041493337,0.00023176137],"domain_scores_gemma":[0.9990167,0.00019660857,0.00016713871,0.0002667425,0.00019260426,0.00016019477],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00069868634,0.00020101246,0.0003830993,0.00025308863,0.000029342087,0.000039750958,0.00034871828,0.000117175616,0.00009098769],"category_scores_gemma":[0.000098647826,0.0001513095,0.00014849492,0.00026994722,0.000010366937,0.00021375157,0.000025259236,0.00036289607,0.000029971588],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00016665891,0.0003574228,0.00004292858,0.00072899414,0.00036196708,0.00012665118,0.00022048534,0.54518795,0.3679139,0.009089869,0.0078331195,0.067970075],"study_design_scores_gemma":[0.0005774172,0.002854152,0.00006353041,0.00014416226,0.00007120255,0.000097790566,0.000032438526,0.9582707,0.036298342,0.001129566,0.00026563197,0.00019502683],"about_ca_topic_score_codex":0.0000040405257,"about_ca_topic_score_gemma":6.283487e-7,"teacher_disagreement_score":0.4130828,"about_ca_system_score_codex":0.0001087445,"about_ca_system_score_gemma":0.000019128272,"threshold_uncertainty_score":0.6170222},"labels":[],"label_agreement":null},{"id":"W2117539176","doi":"10.2514/1.20386","title":"Three-Dimensional Turbulent Wall Jets Issuing from Moderate-Aspect-Ratio Rectangular Channels","year":2007,"lang":"en","type":"article","venue":"AIAA Journal","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":39,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Turbulence; Aspect ratio (aeronautics); Mechanics; Jet (fluid); Physics; Geometry; Materials science; Mathematics; Composite material","score_opus":0.01054149680377753,"score_gpt":0.21728211528285596,"score_spread":0.20674061847907843,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2117539176","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6740492,0.0015899066,0.32129824,0.00032752255,0.0018947803,0.00008251032,0.000007891214,0.00011767649,0.0006322977],"genre_scores_gemma":[0.9868507,0.00009111352,0.01143977,0.00022258682,0.0012464072,0.000001743257,0.000013861497,0.00006534416,0.00006850086],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9984534,0.00001255631,0.00045043704,0.00019406596,0.0004017174,0.0004878544],"domain_scores_gemma":[0.999302,0.00008962823,0.000075700926,0.00020027091,0.00010942542,0.00022297337],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00042422267,0.0002367152,0.00023409321,0.00010863443,0.00023130252,0.0001587711,0.00021538683,0.000142606,0.00036876198],"category_scores_gemma":[0.000028579607,0.00022256175,0.00011317913,0.00011345924,0.00002449837,0.00016993059,0.00003689805,0.00067115907,0.0000716001],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000042520136,0.00004850067,0.00012793085,0.000009024051,0.00018832553,0.0007438325,0.0004570003,0.953447,0.03137468,0.0005186003,0.007026107,0.006016494],"study_design_scores_gemma":[0.0004209277,0.000040623458,0.0006849239,0.00008398349,0.000031407853,0.0002491077,0.00003375995,0.9791941,0.0038186926,0.013738851,0.0013766414,0.00032697144],"about_ca_topic_score_codex":0.00004027934,"about_ca_topic_score_gemma":0.000107296444,"teacher_disagreement_score":0.31280148,"about_ca_system_score_codex":0.00018487447,"about_ca_system_score_gemma":0.000029918596,"threshold_uncertainty_score":0.9075805},"labels":[],"label_agreement":null},{"id":"W2117768297","doi":"10.2514/6.2008-3072","title":"Aeroacoustic investigations of Blade-Vortex Interaction using Large Eddy Simulation","year":2008,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Carleton University","funders":"","keywords":"Blade (archaeology); Vortex; Large eddy simulation; Acoustics; Aerospace engineering; Mechanics; Eddy current; Physics; Marine engineering; Engineering; Mechanical engineering; Turbulence","score_opus":0.03474358290850666,"score_gpt":0.2635350525785556,"score_spread":0.22879146967004893,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2117768297","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.5143437,0.000015312778,0.4840503,0.0000024187382,0.00022432956,0.00005228053,0.000009842413,0.00008448653,0.0012173372],"genre_scores_gemma":[0.9861488,0.000023101438,0.013594826,0.000017538827,0.00007790943,0.0000020061245,0.000020241752,0.00002364184,0.00009196765],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994005,0.000008303439,0.0002443199,0.000092233895,0.0001165266,0.00013810601],"domain_scores_gemma":[0.9996077,0.000084640444,0.00003948801,0.00013908723,0.00008413433,0.00004499227],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000054280994,0.00009506835,0.00011246013,0.00008751578,0.0000803047,0.0000075109183,0.000056951445,0.000062299514,0.000095198404],"category_scores_gemma":[0.000074327894,0.00010004595,0.000032830038,0.00020504567,0.000032470263,0.00014640842,0.00001758937,0.000109601686,0.000010926418],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[9.239753e-7,0.000019153127,0.0005197725,0.00003645467,0.000015710679,0.0000015220038,0.0001588363,0.9879913,0.010832023,0.00030048555,0.00007009965,0.00005372003],"study_design_scores_gemma":[0.00012128533,0.000008797914,0.00066558574,0.00002185868,0.000021716018,0.000006671292,0.000072657356,0.99807835,0.00059687474,0.00019594336,0.00010593336,0.000104328945],"about_ca_topic_score_codex":0.000013154889,"about_ca_topic_score_gemma":0.0000216369,"teacher_disagreement_score":0.47180507,"about_ca_system_score_codex":0.00005802337,"about_ca_system_score_gemma":0.000024175039,"threshold_uncertainty_score":0.40797555},"labels":[],"label_agreement":null},{"id":"W2122755935","doi":"","title":"Prediction and Measurement of Turbulent Boundary Layer Wall-Pressure Fluctuations on the Surface of a Single Panel at Low Mach Numbers","year":2014,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"Carleton University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Mach number; Boundary layer; Wind tunnel; Turbulence; Mechanics; Boundary layer thickness; Physics; Acoustics","score_opus":0.021397386919177933,"score_gpt":0.18546540968325217,"score_spread":0.16406802276407423,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2122755935","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9874521,0.00022209858,0.0094336085,0.00023417486,0.0003829294,0.00022283944,0.0003420139,0.00003283153,0.0016774009],"genre_scores_gemma":[0.99924934,0.000049828537,0.00039577615,0.00008614691,0.000047457936,0.0000037568159,0.00001898228,0.00002943905,0.000119301934],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99915975,0.000022860037,0.00021465619,0.00012083007,0.0002716677,0.0002102579],"domain_scores_gemma":[0.99930245,0.000080081954,0.00004702061,0.00027586674,0.00014761204,0.00014699086],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024775107,0.00012817244,0.00014435097,0.00004918281,0.00011096276,0.000019437992,0.00012309918,0.000092242255,0.00004591224],"category_scores_gemma":[0.0001164507,0.00011351732,0.00003192217,0.000086916254,0.00009232959,0.000021688444,0.00001675031,0.00013248876,0.00000322901],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000037821715,0.000017616823,0.000272844,0.00015117334,0.00007940932,0.0000013734857,0.00032984308,0.8259167,0.1653803,0.0004200224,0.007153392,0.00027354306],"study_design_scores_gemma":[0.00016856262,0.000054613236,0.007040324,0.00009532768,0.000123009,0.000004172105,0.00008990815,0.98827595,0.0011397883,0.0001802622,0.002689454,0.00013865127],"about_ca_topic_score_codex":0.0011861295,"about_ca_topic_score_gemma":0.004245203,"teacher_disagreement_score":0.16424051,"about_ca_system_score_codex":0.00026147798,"about_ca_system_score_gemma":0.000079032296,"threshold_uncertainty_score":0.4629102},"labels":[],"label_agreement":null},{"id":"W2126923927","doi":"10.1243/09544100jaero117","title":"An experimental investigation of turbulent boundary layer flow over surface-mounted circular cavities","year":2008,"lang":"en","type":"article","venue":"Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":28,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Western University","funders":"","keywords":"Strouhal number; Boundary layer; Turbulence; Wake; Mechanics; Physics; Optics; Drag; Vortex; Vortex shedding; Mach number; Reynolds number","score_opus":0.011295633897379895,"score_gpt":0.21382155444477963,"score_spread":0.20252592054739973,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2126923927","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97913384,0.0006259019,0.018943727,0.000034910317,0.0010224516,0.00014597553,0.000014929872,0.00005309896,0.000025139167],"genre_scores_gemma":[0.9880362,0.00018029017,0.011586177,0.000007010519,0.00013754232,0.0000026699868,0.0000023034518,0.000041776104,0.000005994014],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99815315,0.000006429141,0.0008307612,0.00013340829,0.00063560525,0.0002406169],"domain_scores_gemma":[0.9989431,0.00003526077,0.00035161313,0.00014876893,0.00037549788,0.00014574498],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00042096368,0.0002625386,0.00050198456,0.00014363254,0.00006501635,0.00001658425,0.00040851027,0.0001670391,0.000009821897],"category_scores_gemma":[0.00012630524,0.00023045336,0.00023310236,0.00033105793,0.00015371354,0.00049919926,0.000047728896,0.0004284558,2.887513e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000013761961,0.000028552668,0.00008339265,0.00015655496,0.00006063069,0.0000017225444,0.00032224727,0.53625065,0.46181795,0.0011588043,0.00010161735,0.0000040775562],"study_design_scores_gemma":[0.00040997542,0.00012581429,0.00019716617,0.0003445368,0.00004334526,0.00007664991,0.00015971492,0.5275601,0.47080922,0.000032417585,0.000089315974,0.0001517477],"about_ca_topic_score_codex":0.000004685596,"about_ca_topic_score_gemma":2.6910274e-7,"teacher_disagreement_score":0.008991251,"about_ca_system_score_codex":0.0001890771,"about_ca_system_score_gemma":0.00007509381,"threshold_uncertainty_score":0.9397615},"labels":[],"label_agreement":null},{"id":"W2127647218","doi":"10.1017/s0022112010003368","title":"On a uniformly valid analytical rectilinear cascade response function","year":2010,"lang":"en","type":"article","venue":"Journal of Fluid Mechanics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":87,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Cascade; Turbofan; Airfoil; Jump; Computer science; Physics; Mechanics; Aerospace engineering","score_opus":0.008531078941486567,"score_gpt":0.2331999549567723,"score_spread":0.22466887601528573,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2127647218","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8751448,0.0000338746,0.12025051,0.00013084203,0.003847629,0.000052711526,0.000007814752,0.000049041704,0.00048277926],"genre_scores_gemma":[0.99638593,0.00007192435,0.0028225514,0.000094065676,0.00045032686,7.353806e-7,0.0000010169709,0.000039054878,0.0001344061],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99894714,0.000032387554,0.0004053124,0.0000886569,0.00032377284,0.00020273919],"domain_scores_gemma":[0.9991811,0.000200982,0.00008318481,0.00021570563,0.00016595675,0.0001530794],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0011175226,0.00014206726,0.00021252973,0.0001894794,0.00005219983,0.000036562982,0.00017267189,0.0001814217,0.00008761294],"category_scores_gemma":[0.00055022683,0.00012188005,0.00014027684,0.00018116191,0.000010269603,0.000094613875,0.000018503437,0.00092733145,0.0000254795],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0015847337,0.0001208236,0.000005497567,0.0000347796,0.00017833116,0.00017797895,0.00009825081,0.16758354,0.76702553,0.049386866,0.008468178,0.0053354804],"study_design_scores_gemma":[0.00042870204,0.0005623434,0.000053133106,0.00003139232,0.00008078978,0.00023432846,0.000035499255,0.9789968,0.0066168928,0.0044817966,0.008328017,0.00015030033],"about_ca_topic_score_codex":6.1260533e-7,"about_ca_topic_score_gemma":0.0000046189684,"teacher_disagreement_score":0.8114133,"about_ca_system_score_codex":0.00008514098,"about_ca_system_score_gemma":0.0000603348,"threshold_uncertainty_score":0.49701244},"labels":[],"label_agreement":null},{"id":"W2129129282","doi":"10.2514/6.2010-3706","title":"An Acoustic Analogy Formulation for Uniformly Moving Media: Formulation 1C","year":2010,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"","keywords":"Analogy; Computer science; Acoustics; Physics; Philosophy","score_opus":0.0074981096130361845,"score_gpt":0.23363940911013859,"score_spread":0.2261412994971024,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2129129282","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.4185337,0.0000034482393,0.5789445,0.000010663122,0.0006954758,0.0001634889,0.000018762868,0.00021659279,0.0014133353],"genre_scores_gemma":[0.9648401,0.000005503814,0.034423772,0.000030064746,0.00037946002,0.000023200697,0.00021205792,0.00004515075,0.000040657225],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999227,0.0000032892071,0.0002397297,0.00014722867,0.000111412,0.00027136586],"domain_scores_gemma":[0.99941707,0.00013310458,0.000031557876,0.00023715029,0.00009193436,0.00008917051],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018199977,0.00014036238,0.00013124644,0.000104930885,0.00010489238,0.000047523612,0.00013119046,0.00017244321,0.00007259586],"category_scores_gemma":[0.00006048549,0.00013457122,0.000046707006,0.00010187969,0.000008428733,0.00035522337,0.000013146477,0.00017831381,0.000007777707],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000008827471,0.000023912608,0.00045616447,0.00006639642,0.000020024698,9.454023e-7,0.00022227244,0.6934884,0.21677247,0.07478226,0.00017370554,0.013984582],"study_design_scores_gemma":[0.00026766953,0.000034025303,0.003070751,0.0000036880656,0.000023827826,0.00000298517,0.00004944274,0.9861152,0.0007464893,0.009239599,0.00026454966,0.00018177462],"about_ca_topic_score_codex":0.0000117198015,"about_ca_topic_score_gemma":0.0014154384,"teacher_disagreement_score":0.54630643,"about_ca_system_score_codex":0.00003851416,"about_ca_system_score_gemma":0.00001432597,"threshold_uncertainty_score":0.54876554},"labels":[],"label_agreement":null},{"id":"W2132734693","doi":"10.2514/6.2007-7789","title":"Investigations on Variable Fan Nozzle Area to Reduce the Aircraft Jet Noise","year":2007,"lang":"en","type":"article","venue":"7th AIAA ATIO Conf, 2nd CEIAT Int'l Conf on Innov and Integr in Aero Sciences,17th LTA Systems Tech Conf; followed by 2nd TEOS Forum","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Bombardier (Canada)","funders":"","keywords":"Nozzle; Jet noise; Jet (fluid); Variable (mathematics); Noise (video); Aerospace engineering; Environmental science; Aircraft noise; Acoustics; Automotive engineering; Engineering; Computer science; Physics; Noise reduction; Mathematics; Artificial intelligence","score_opus":0.013188303189658544,"score_gpt":0.24205193796260271,"score_spread":0.22886363477294416,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2132734693","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7784547,0.00083424756,0.07205179,0.004735636,0.0082691265,0.0046490044,0.00077566924,0.0009107908,0.129319],"genre_scores_gemma":[0.9936391,0.00008435979,0.0011626084,0.0020886906,0.00019323899,0.00032386338,0.0000829374,0.000096576616,0.0023286396],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"not_applicable","domain_scores_codex":[0.99437016,0.00012769317,0.0016013585,0.0011683827,0.0011722355,0.0015601816],"domain_scores_gemma":[0.9969001,0.00077454303,0.00033466457,0.0010420883,0.00044329677,0.0005053254],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0032327026,0.0008682679,0.00087328855,0.0008514663,0.0009203003,0.00075727433,0.0014393616,0.0005177916,0.000113137605],"category_scores_gemma":[0.0008636394,0.00067550084,0.0001341437,0.0026115447,0.00076351385,0.0004089446,0.00022056128,0.0013111355,0.000065823886],"study_design_candidate":"not_applicable","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00026738725,0.00061323075,0.01652053,0.00051283557,0.0004134393,0.000085554246,0.0030378192,0.037627436,0.18899234,0.5133285,0.22604614,0.012554782],"study_design_scores_gemma":[0.004299627,0.0030433056,0.0018273043,0.0033666866,0.00016501169,0.00014912874,0.013191587,0.31721964,0.026049346,0.00403357,0.62243843,0.004216342],"about_ca_topic_score_codex":0.0012327926,"about_ca_topic_score_gemma":0.00093257247,"teacher_disagreement_score":0.5092949,"about_ca_system_score_codex":0.00044368504,"about_ca_system_score_gemma":0.00036655023,"threshold_uncertainty_score":0.9995696},"labels":[],"label_agreement":null},{"id":"W2133901499","doi":"10.2514/6.2010-3967","title":"Simulation of a Low-Mach, High Reynolds Number Jet: First Step Towards the Simulation of Jet Noise Control by Micro-jets","year":2010,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Mach number; Reynolds number; Jet (fluid); Jet noise; Large eddy simulation; Turbulence; Nozzle; Physics; Mechanics; Transonic; Computation; Computer science; Aerospace engineering; Aerodynamics; Engineering; Algorithm","score_opus":0.005348516833145121,"score_gpt":0.21998941468402447,"score_spread":0.21464089785087934,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2133901499","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7706188,0.000026079282,0.22679096,0.00007654713,0.00046232017,0.0003042647,0.00017334786,0.00008016219,0.0014675449],"genre_scores_gemma":[0.9981418,0.0000119629185,0.0014819135,0.000040725892,0.000105273306,0.000008966922,0.000041776246,0.000045553268,0.00012200149],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.998906,0.00001807239,0.00045691413,0.00016444571,0.00024639585,0.0002081738],"domain_scores_gemma":[0.99884623,0.0003839442,0.00011708601,0.00041212724,0.00018982847,0.000050760627],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021537406,0.0002016093,0.00028112458,0.000038913164,0.000058240315,0.000022898379,0.0002168976,0.00019208001,0.0003343009],"category_scores_gemma":[0.00013177206,0.00014869691,0.000097570366,0.00013966011,0.000071742834,0.00009717718,0.00003396156,0.00023586444,0.000015461581],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000020740634,0.00004686004,0.0017524163,0.000084163075,0.00003980611,4.5837928e-7,0.000096986194,0.95417535,0.042178184,0.0002753594,0.0003642518,0.00096540374],"study_design_scores_gemma":[0.00077186874,0.000020732627,0.002559804,0.000023239398,0.000047312824,4.09408e-7,0.000016099295,0.99189055,0.003326896,0.00015053051,0.0010269537,0.00016557425],"about_ca_topic_score_codex":0.00013009162,"about_ca_topic_score_gemma":0.00019756478,"teacher_disagreement_score":0.22752304,"about_ca_system_score_codex":0.00003051843,"about_ca_system_score_gemma":0.000015092554,"threshold_uncertainty_score":0.6063684},"labels":[],"label_agreement":null},{"id":"W2134696443","doi":"10.5589/q09-002","title":"Improved transonic flutter analysis in the frequency domain using computational fluid dynamics","year":2008,"lang":"en","type":"article","venue":"Canadian aeronautics and space journal","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Flutter; Aeroelasticity; Transonic; Aerodynamics; Frequency domain; Nonlinear system; Time domain; Computational fluid dynamics; Aerodynamic force; Boundary (topology); Domain (mathematical analysis); Mechanics; Control theory (sociology); Physics; Mathematics; Computer science; Mathematical analysis","score_opus":0.008551901309661306,"score_gpt":0.19667702790470237,"score_spread":0.18812512659504108,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2134696443","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9041321,0.00042819462,0.09387173,0.0008041255,0.00017776174,0.00007643607,0.00006467745,0.000009437648,0.00043548946],"genre_scores_gemma":[0.98490083,0.0002352784,0.014492448,0.00022452952,0.000089766014,0.0000012463477,0.00001935825,0.00002160414,0.0000149272755],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9990186,0.000035937584,0.00026375122,0.00011980295,0.000164238,0.00039768324],"domain_scores_gemma":[0.9994904,0.000044457716,0.00003443933,0.00012689827,0.00004582013,0.00025803188],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00029154366,0.00015975795,0.00020290313,0.00033432496,0.0003293589,0.000098809076,0.00017852888,0.00009701993,0.000037518224],"category_scores_gemma":[0.000008936763,0.0001375916,0.00009205768,0.00044271944,0.00008603571,0.000077404875,0.0000061914766,0.0004731712,9.924961e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":true,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000030461022,0.000017855922,0.015135443,0.000017515637,0.0003351703,0.00047819296,0.0021993096,0.9734479,0.00055462646,0.006996671,0.00027175478,0.0005424931],"study_design_scores_gemma":[0.00024529823,0.00001603492,0.023306306,0.000008695058,0.00009352991,0.00039726865,0.0003054621,0.972809,4.4799535e-7,0.002520152,0.00012705846,0.0001707142],"about_ca_topic_score_codex":0.0024756119,"about_ca_topic_score_gemma":0.1822875,"teacher_disagreement_score":0.17981188,"about_ca_system_score_codex":0.00048776274,"about_ca_system_score_gemma":0.00021898377,"threshold_uncertainty_score":0.8326336},"labels":[],"label_agreement":null},{"id":"W2137468116","doi":"10.1098/rspa.2010.0172","title":"An acoustic analogy formulation for moving sources in uniformly moving media","year":2010,"lang":"en","type":"article","venue":"Proceedings of the Royal Society A Mathematical Physical and Engineering Sciences","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":216,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"","keywords":"Computation; Analogy; Robustness (evolution); Fluid dynamics; Acoustic wave equation; Computer science; Wave equation; Rest (music); Flow (mathematics); Acoustic wave; Mathematics; Acoustics; Mathematical analysis; Mechanics; Physics; Algorithm","score_opus":0.005937537063296527,"score_gpt":0.21059610562373393,"score_spread":0.2046585685604374,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2137468116","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98413724,0.000010653891,0.0153545635,0.00003086575,0.00009567214,0.00013046278,0.0000042569886,0.00006552435,0.00017074984],"genre_scores_gemma":[0.98503363,0.000002144662,0.014797608,0.0000063462876,0.00012472252,0.00001657557,4.2422678e-7,0.000014507786,0.000004020105],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992215,8.085767e-7,0.00018624398,0.00015228541,0.00018140055,0.00025773415],"domain_scores_gemma":[0.99960077,0.0002113221,0.000036958376,0.000051394683,0.000037321566,0.00006220793],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00032980906,0.00013054744,0.0001957391,0.000027508926,0.00010873274,0.00006142225,0.00027344277,0.00007050847,0.0000016366009],"category_scores_gemma":[0.00018057245,0.00009111805,0.00008724777,0.00020917608,0.00012186162,0.00018513761,0.000054055483,0.00022121725,2.1142043e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00000255305,0.00008203796,0.00080154935,0.00096467405,0.000018871096,5.237523e-8,0.0034793003,0.63043356,0.23437992,0.12913871,0.000016939988,0.0006818553],"study_design_scores_gemma":[0.0000872893,0.000026114421,0.0022529636,0.000058513313,0.000015503885,7.125729e-7,0.00028487638,0.9653762,0.0013220056,0.03045521,0.0000028989102,0.00011771683],"about_ca_topic_score_codex":0.0000029554853,"about_ca_topic_score_gemma":0.0000023127557,"teacher_disagreement_score":0.33494264,"about_ca_system_score_codex":0.000014512335,"about_ca_system_score_gemma":0.0000078122275,"threshold_uncertainty_score":0.37156862},"labels":[],"label_agreement":null},{"id":"W2137511765","doi":"","title":"Review of computational aeroacoustics for application in electronics cooler noise","year":2006,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"University of Windsor","funders":"","keywords":"Computational aeroacoustics; Aeroacoustics; Computational fluid dynamics; Noise (video); Muffler; Airflow; Acoustics; Boundary element method; Heat transfer; Heat sink; Finite element method; Computer science; Engineering; Aerospace engineering; Mechanical engineering; Mechanics; Physics; Structural engineering; Sound pressure","score_opus":0.004173444021898006,"score_gpt":0.20166622442798687,"score_spread":0.19749278040608886,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2137511765","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.01264725,0.01052459,0.9733099,0.00008637015,0.00026107277,0.00071808265,0.00073616445,0.000057535028,0.0016590863],"genre_scores_gemma":[0.9796094,0.002143282,0.017019376,0.00037990985,0.00013369533,0.000063224004,0.0005495389,0.000053481446,0.000048132017],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99903834,0.000005931819,0.00038104103,0.00013431767,0.000104389546,0.00033598984],"domain_scores_gemma":[0.9994068,0.000087350134,0.000050789993,0.00017501663,0.0001793692,0.000100644094],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015282292,0.00013678936,0.0002124408,0.0001339474,0.00003496086,0.000009924119,0.00014840013,0.00010057728,0.000009615119],"category_scores_gemma":[0.000055030745,0.00016708089,0.000045177178,0.0002501078,0.000035275287,0.000026467205,0.0000066783514,0.0001389627,0.0000046652904],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000011429895,0.000013247718,0.00008878575,0.0019159752,0.000007758319,0.0000014538663,0.0000048380657,0.9730333,0.0018568933,0.0038795406,0.017263053,0.0019339751],"study_design_scores_gemma":[0.00018921404,0.000016369164,0.0015735605,0.0003736988,0.000042993914,0.000002612521,0.000005502988,0.9880683,0.000013308751,0.0037734786,0.005757972,0.00018301242],"about_ca_topic_score_codex":0.0009852094,"about_ca_topic_score_gemma":0.0073018773,"teacher_disagreement_score":0.9669621,"about_ca_system_score_codex":0.0003956803,"about_ca_system_score_gemma":0.0002629765,"threshold_uncertainty_score":0.6813361},"labels":[],"label_agreement":null},{"id":"W2138712021","doi":"10.2514/6.2010-3879","title":"Numerical Simulation of Sound from Flow over an Airfoil with a Blunt Trailing Edge","year":2010,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":6,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"","keywords":"Trailing edge; Freestream; Airfoil; Computational fluid dynamics; Mach number; Acoustics; Large eddy simulation; Lattice Boltzmann methods; Physics; Mechanics; Vortex shedding; Turbulence; Reynolds number","score_opus":0.006758641178875545,"score_gpt":0.22220188639692987,"score_spread":0.21544324521805433,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2138712021","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.62273633,0.0000042909687,0.37554663,0.000002232212,0.00016955163,0.00003506052,0.000012329849,0.00007370378,0.0014198632],"genre_scores_gemma":[0.96915066,0.0000010871942,0.030593479,0.000012929894,0.00016508522,0.0000020254631,0.000022536806,0.000028860646,0.00002333732],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99948704,0.000004253517,0.0001437164,0.000121407764,0.00012064872,0.00012293886],"domain_scores_gemma":[0.99962145,0.00006981776,0.000018326014,0.00019981584,0.000031937012,0.000058639544],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000048653063,0.0001018188,0.00012510322,0.000025539182,0.00002469181,0.000020037287,0.00008157016,0.00007745588,0.0003079702],"category_scores_gemma":[0.000012732566,0.000083716885,0.000026037407,0.00006579288,0.000024003342,0.00009247811,0.000008431399,0.00018548241,0.0000056585295],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000007629455,0.000024370718,0.00080494833,0.000009145401,0.000017589988,0.0000013082871,0.00015273511,0.9833512,0.012894517,0.00025045362,0.000008522124,0.0024776363],"study_design_scores_gemma":[0.00022119471,0.000029660547,0.003225611,0.0000061258074,0.000015187866,5.255816e-7,0.000023005887,0.9952714,0.00045263735,0.00051763793,0.00011119475,0.00012581487],"about_ca_topic_score_codex":0.000053131578,"about_ca_topic_score_gemma":0.0002929173,"teacher_disagreement_score":0.34641433,"about_ca_system_score_codex":0.000008966806,"about_ca_system_score_gemma":0.00000899421,"threshold_uncertainty_score":0.34138757},"labels":[],"label_agreement":null},{"id":"W2142206837","doi":"10.3390/su4061104","title":"Noise Pollution Prevention in Wind Turbines: Status and Recent Advances","year":2012,"lang":"en","type":"article","venue":"Sustainability","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":60,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Ontario Tech University","funders":"","keywords":"Wind power; Noise pollution; Noise (video); Noise control; Turbine; Environmental science; Aerodynamics; Marine engineering; Trailing edge; Engineering; Noise reduction; Computer science; Aerospace engineering; Electrical engineering; Structural engineering","score_opus":0.0053572710573435225,"score_gpt":0.24726379597306508,"score_spread":0.24190652491572157,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2142206837","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99224484,0.0042666085,0.002312775,0.00008665966,0.0002996104,0.0002791171,0.0000061335986,0.00006597505,0.00043829743],"genre_scores_gemma":[0.99776906,0.0017841799,0.0003074071,0.000006918415,0.000064994114,0.000011673835,0.0000071850527,0.000011502241,0.000037092374],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.9992415,0.000030825504,0.00016923786,0.00011851216,0.00007988835,0.00036003796],"domain_scores_gemma":[0.99965155,0.000021903166,0.000018473787,0.0001456411,0.00008177329,0.00008067528],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00030721052,0.000098918055,0.00010519094,0.00005033145,0.000033680783,0.000012991089,0.000036641963,0.000059030328,0.000018113471],"category_scores_gemma":[0.00023875223,0.000098571654,0.000017948463,0.00015470953,0.000044238925,0.0002932947,0.000030241063,0.00012255023,0.000001109642],"study_design_candidate":"observational","study_design_consensus":"observational","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000057522182,0.00032972536,0.6171812,0.0013132611,0.00001836686,0.0000033467572,0.0020611447,0.118591726,0.0003529736,0.0067000724,0.00008336042,0.2533073],"study_design_scores_gemma":[0.0004833324,0.000045025627,0.912912,0.000023055303,0.000014682943,0.0000016821627,0.001485687,0.027974432,0.00005413927,0.040937338,0.015784424,0.00028420467],"about_ca_topic_score_codex":0.00001561474,"about_ca_topic_score_gemma":0.00004785761,"teacher_disagreement_score":0.29573083,"about_ca_system_score_codex":0.0006634942,"about_ca_system_score_gemma":0.000037189908,"threshold_uncertainty_score":0.40196353},"labels":[],"label_agreement":null},{"id":"W2142528210","doi":"10.2514/6.2008-2936","title":"Linear Stability of a Compressible Coaxial Jet with Continuous Mean Flow Profiles","year":2008,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"","keywords":"Coaxial; Jet (fluid); Compressibility; Mechanics; Stability (learning theory); Mean flow; Compressible flow; Flow (mathematics); Physics; Materials science; Computer science; Turbulence; Telecommunications","score_opus":0.01361972753700784,"score_gpt":0.19942297136996395,"score_spread":0.1858032438329561,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2142528210","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9235757,0.000051183844,0.06409875,0.000007704589,0.00012225939,0.00019217268,0.00006736098,0.00020564307,0.011679238],"genre_scores_gemma":[0.96192735,0.0000291832,0.037831713,0.000007127758,0.00006205557,0.000008972692,0.000016733948,0.000026327329,0.000090515736],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992861,0.000011096885,0.00021323464,0.00013514682,0.00016950538,0.00018488754],"domain_scores_gemma":[0.9995228,0.000045767752,0.000027154392,0.00025529103,0.00009233472,0.00005665774],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00007640788,0.00013645123,0.0002510557,0.00002724073,0.000041407144,0.0000049834757,0.00012297553,0.00005663189,0.00016700523],"category_scores_gemma":[0.000011933547,0.000101753576,0.000038405615,0.00009338586,0.00012001616,0.000049009483,0.00002923416,0.00012753016,0.0000068963495],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00028975686,0.00073089433,0.09595444,0.0010704102,0.00044797867,0.00013139789,0.0031932832,0.79651594,0.0872437,0.002748518,0.007512135,0.004161568],"study_design_scores_gemma":[0.0005170202,0.00010718312,0.0025113246,0.000026421387,0.000016017431,0.000014151278,0.00011914173,0.9738817,0.022343567,0.000046212335,0.00021625753,0.00020097184],"about_ca_topic_score_codex":0.00003888259,"about_ca_topic_score_gemma":0.000104404484,"teacher_disagreement_score":0.17736581,"about_ca_system_score_codex":0.000018917945,"about_ca_system_score_gemma":0.000024215873,"threshold_uncertainty_score":0.41493902},"labels":[],"label_agreement":null},{"id":"W2143113720","doi":"10.1017/jfm.2013.118","title":"Solution of the quasi-one-dimensional linearized Euler equations using flow invariants and the Magnus expansion","year":2013,"lang":"en","type":"article","venue":"Journal of Fluid Mechanics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":158,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Physics; Nozzle; Euler equations; Mach number; Mathematical analysis; Dimensionless quantity; Asymptotic expansion; Euler's formula; Mechanics; Mathematics; Thermodynamics","score_opus":0.01568403420143865,"score_gpt":0.20639766119792427,"score_spread":0.1907136269964856,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2143113720","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.34712,0.00040222582,0.65074253,0.00030693662,0.0012225596,0.00017029126,0.0000075184034,0.000008579169,0.00001939713],"genre_scores_gemma":[0.977775,0.00015668405,0.021831032,0.000054898697,0.00014825504,0.0000018348519,9.474932e-7,0.000018738121,0.000012614449],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989876,0.000063469546,0.00044608986,0.00006015606,0.0003113067,0.00013133998],"domain_scores_gemma":[0.999143,0.00020377993,0.00017192251,0.0001690425,0.0002650969,0.00004712474],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005994581,0.00010057665,0.00020786001,0.000053195705,0.00012118379,0.0000328227,0.00016168895,0.00008178976,0.000039794057],"category_scores_gemma":[0.00029554046,0.00005967571,0.00009665875,0.00012272537,0.00003454591,0.00014592122,0.00007429171,0.00026534195,0.0000022803495],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00003204061,0.00004940618,0.0000027208694,0.000029656352,0.00008065757,0.0000012438538,0.00022222936,0.40251088,0.58991295,0.0046912287,0.00032989454,0.002137107],"study_design_scores_gemma":[0.0008660142,0.000032154283,0.000035714285,0.00009506043,0.00008699889,0.000034489927,0.000045210996,0.9906423,0.002018891,0.006059587,0.000016724167,0.00006686795],"about_ca_topic_score_codex":0.000015291034,"about_ca_topic_score_gemma":0.0000052335763,"teacher_disagreement_score":0.63065505,"about_ca_system_score_codex":0.00004778477,"about_ca_system_score_gemma":0.000055618344,"threshold_uncertainty_score":0.24335048},"labels":[],"label_agreement":null},{"id":"W2144271433","doi":"10.2514/1.b35000","title":"Prediction of Noise Sources in Axial Compressor from URANS Simulation","year":2014,"lang":"en","type":"article","venue":"Journal of Propulsion and Power","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":17,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Natural Sciences and Engineering Research Council of Canada; Compute Canada","keywords":"Stator; Rotor (electric); Axial compressor; Wake; Gas compressor; Noise (video); Turbulence; Mechanics; Acoustics; Computational fluid dynamics; Physics; Flow (mathematics); Aerospace engineering; Engineering; Mechanical engineering; Computer science","score_opus":0.008963146967472463,"score_gpt":0.20939431757272056,"score_spread":0.2004311706052481,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2144271433","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9691427,0.00019965055,0.029758804,0.000028808734,0.00056880224,0.00003704664,0.000013222728,0.000006741425,0.00024425544],"genre_scores_gemma":[0.99892575,0.00006457029,0.00085961015,0.000008300814,0.00011980108,2.1443715e-7,0.000002298806,0.0000076016913,0.000011859594],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99948937,0.000019065921,0.00027888655,0.000039540777,0.00011802349,0.00005508965],"domain_scores_gemma":[0.999742,0.00004794764,0.00008231015,0.000047250713,0.000047398382,0.000033101347],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00014422188,0.000054281874,0.00013041205,0.00006867715,0.0000141598,0.000010057951,0.000043338547,0.00005357176,0.00003365354],"category_scores_gemma":[0.000034286462,0.000042681157,0.000028796416,0.00003699799,0.000014514513,0.00007258886,0.000008353973,0.00012767222,5.891343e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000105154686,0.00007002014,0.018180469,0.0000598778,0.000026502425,0.0000032760915,0.001112154,0.9133816,0.0541598,0.000078461286,0.00025515072,0.012567557],"study_design_scores_gemma":[0.0006348459,0.00010578167,0.057629697,0.00011614135,0.0000140031325,0.0000021757987,0.00004810734,0.93835247,0.0005293127,0.0006385273,0.0018775121,0.000051457446],"about_ca_topic_score_codex":0.0000058739474,"about_ca_topic_score_gemma":0.000004368714,"teacher_disagreement_score":0.05363049,"about_ca_system_score_codex":0.000010725367,"about_ca_system_score_gemma":0.000003078454,"threshold_uncertainty_score":0.1740487},"labels":[],"label_agreement":null},{"id":"W2147239442","doi":"10.2514/6.2011-2848","title":"Statistical Properties of Pressure Loadings and Vibroacoustic Response of a Simplified Side Glass Induced by the Flow over Generic Flow-deflector and Side-mirror","year":2011,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Purdue University","keywords":"Flow (mathematics); Materials science; Acoustics; Mechanics; Computer science; Physics","score_opus":0.02330603744793034,"score_gpt":0.21641232293053844,"score_spread":0.1931062854826081,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2147239442","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9769259,0.0006297961,0.021459995,0.000013720277,0.000099246405,0.0002645114,0.00016855901,0.000059458125,0.00037882288],"genre_scores_gemma":[0.99006385,0.00005546185,0.009639339,0.000030589184,0.000013469826,0.00001753741,0.0000034043728,0.00004383893,0.00013252105],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.998945,0.000060041173,0.00034773958,0.00021260738,0.00018745822,0.00024716134],"domain_scores_gemma":[0.99929166,0.00024138941,0.000055677603,0.00025290408,0.00006865514,0.00008968994],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002514644,0.0002129618,0.00031045775,0.000053145362,0.00005326036,0.000024245346,0.00014093026,0.000120348246,0.000044056185],"category_scores_gemma":[0.00023148331,0.00014465311,0.000029184177,0.00010751874,0.00018538379,0.00007223589,0.00009250153,0.00017265778,0.0000010390166],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00038157275,0.00003782057,0.00013216412,0.0003970966,0.00012867936,0.000002996869,0.001074086,0.0018645917,0.9943753,0.00023807852,0.00037356,0.0009940842],"study_design_scores_gemma":[0.00050305075,0.00018364859,0.013871693,0.000057418638,0.00016206768,0.000010159079,0.00018964475,0.9381819,0.046279386,0.00023421217,0.00006532413,0.00026150252],"about_ca_topic_score_codex":0.00019439629,"about_ca_topic_score_gemma":0.00005178981,"teacher_disagreement_score":0.94809586,"about_ca_system_score_codex":0.000015299234,"about_ca_system_score_gemma":0.00002822111,"threshold_uncertainty_score":0.58987826},"labels":[],"label_agreement":null},{"id":"W2148208371","doi":"10.2514/6.2011-2885","title":"Simulation of Sound Radiated from Turbulent Heated Jets Using the Lattice-Boltzmann Method","year":2011,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"","keywords":"Lattice Boltzmann methods; Turbulence; Sound (geography); Acoustics; Physics; Sound propagation; Mechanics; Statistical physics; HPP model; Computational physics; Computer science; Reynolds number","score_opus":0.048323592137634895,"score_gpt":0.2800868406673684,"score_spread":0.23176324852973348,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2148208371","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.46088007,0.000077078425,0.5376508,0.000004696626,0.00015879936,0.000084443695,0.000010177264,0.00007939156,0.0010545336],"genre_scores_gemma":[0.9415792,0.000008321287,0.0582688,0.000025881767,0.000048610254,0.0000015039892,0.000013969262,0.000027371892,0.000026301845],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99935603,0.000033069213,0.00023894866,0.00011213539,0.00011144469,0.00014838019],"domain_scores_gemma":[0.9994106,0.00021461233,0.000039557202,0.00024262228,0.0000576784,0.000034887515],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015754432,0.00011794909,0.00014623269,0.000037249305,0.00004681425,0.0000140906195,0.00012952367,0.00007839683,0.00025368133],"category_scores_gemma":[0.00002818042,0.000086330816,0.00004721318,0.00012411013,0.000023412593,0.000059039157,0.000024460374,0.000112883085,0.0000073426027],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000005321551,0.000014277309,0.00013881002,0.000008257661,0.0000663404,0.000001603993,0.0005198344,0.9926901,0.005811765,0.00031636478,0.000016762973,0.00041055353],"study_design_scores_gemma":[0.0001579479,0.0000091083575,0.0010642259,0.000011110773,0.00006121905,6.595459e-7,0.000074085234,0.9930047,0.0024154026,0.00305182,0.000039775452,0.00010995418],"about_ca_topic_score_codex":0.00030512892,"about_ca_topic_score_gemma":0.00002837682,"teacher_disagreement_score":0.48069918,"about_ca_system_score_codex":0.0000354245,"about_ca_system_score_gemma":0.0000069754756,"threshold_uncertainty_score":0.35204685},"labels":[],"label_agreement":null},{"id":"W2156945944","doi":"10.1115/1.2427084","title":"Small Scale Modeling of Vertical Surface Jets in Cross-Flow: Reynolds Number and Downwash Effects","year":2006,"lang":"en","type":"article","venue":"Journal of Fluids Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Alberta","funders":"","keywords":"Reynolds number; Turbulence; Mechanics; Entrainment (biomusicology); Plume; Jet (fluid); Physics; Meteorology","score_opus":0.005048854813143305,"score_gpt":0.20052843772810847,"score_spread":0.19547958291496517,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2156945944","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.82878983,0.0006841611,0.1698669,0.000008834731,0.00034050344,0.000047445497,0.0000026092732,0.000028866372,0.00023085557],"genre_scores_gemma":[0.9732438,0.00014662035,0.026362002,0.0000029256378,0.00018794124,7.9481623e-7,8.990986e-7,0.00004380394,0.000011215921],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99881876,0.00000952446,0.0005969832,0.00010100827,0.00019582643,0.00027793],"domain_scores_gemma":[0.9995732,0.00011064737,0.00002891209,0.00012068917,0.00008237002,0.000084239764],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00032511636,0.00017726075,0.00035521667,0.00012825092,0.000017147318,0.000038047983,0.0001334748,0.00013140288,0.0000036314063],"category_scores_gemma":[0.000077127355,0.00017793018,0.00008043152,0.00019282811,0.000022544642,0.00013499941,0.0000385122,0.00036106963,0.000001103697],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000008607345,0.000021360935,0.0047079935,0.00025880962,0.000015658417,0.00003616809,0.000045578094,0.89953244,0.09499622,0.00015409818,0.000015899024,0.0002071442],"study_design_scores_gemma":[0.0006053942,0.00002899049,0.0054953815,0.00027854025,0.000019208075,0.000065401015,0.000004535912,0.987727,0.0054496746,0.00014258934,0.000016351858,0.00016695898],"about_ca_topic_score_codex":0.000016287346,"about_ca_topic_score_gemma":0.0000067546544,"teacher_disagreement_score":0.14445399,"about_ca_system_score_codex":0.00010621058,"about_ca_system_score_gemma":0.000020483043,"threshold_uncertainty_score":0.72557825},"labels":[],"label_agreement":null},{"id":"W2157713684","doi":"10.1139/p08-086","title":"Control of cavity tones using a spanwise cylinder","year":2008,"lang":"en","type":"article","venue":"Canadian Journal of Physics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":13,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Physics; Cylinder; Attenuation; Acoustics; Optics; Mechanics; Position (finance); Parametric statistics; Geometry","score_opus":0.01729437188585989,"score_gpt":0.19821890160821237,"score_spread":0.18092452972235248,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2157713684","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.866173,0.0002485768,0.13270685,0.000013263515,0.0004892339,0.00003203773,0.00004435942,0.0000041553644,0.0002884831],"genre_scores_gemma":[0.99837744,0.000016158197,0.0012265063,0.000024274084,0.0003261547,1.535298e-7,6.542941e-7,0.000019599045,0.000009063601],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994553,0.000008716956,0.00022306126,0.00003933797,0.00009799359,0.0001756278],"domain_scores_gemma":[0.99941456,0.00002322756,0.000083360464,0.00009649306,0.00015209505,0.00023025807],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00006778817,0.00008462648,0.00020684417,0.00005792426,0.00005545747,0.000007464066,0.00011660637,0.000043444434,0.00001512531],"category_scores_gemma":[0.000019811649,0.00008601538,0.00008610389,0.00009667271,0.00007062121,0.000079509075,0.0000026946036,0.00017758712,0.0000012006387],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000004802416,0.000013949407,0.005177122,0.000042934105,0.00011970991,0.00023857356,0.00049595255,0.97953475,0.010423745,0.0012948347,0.0004867986,0.002166856],"study_design_scores_gemma":[0.0012946045,0.00008656745,0.006315805,0.00015402716,0.00016018064,0.0003979811,0.000116149145,0.98317295,0.0032442303,0.0030579607,0.0015802723,0.0004192465],"about_ca_topic_score_codex":0.000756672,"about_ca_topic_score_gemma":0.0011230056,"teacher_disagreement_score":0.1322044,"about_ca_system_score_codex":0.00010369164,"about_ca_system_score_gemma":0.00036888212,"threshold_uncertainty_score":0.35076055},"labels":[],"label_agreement":null},{"id":"W2158934352","doi":"","title":"3D parallel spectral computations of fan noise","year":2006,"lang":"en","type":"article","venue":"Research Repository (Delft University of Technology)","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"","keywords":"Discretization; Euler equations; Preconditioner; Domain decomposition methods; Computer science; Computational aeroacoustics; Finite element method; Acoustic wave equation; Noise (video); Applied mathematics; Computation; Iterative method; Algorithm; Computational science; Acoustics; Mathematics; Aeroacoustics; Mathematical analysis; Acoustic wave; Physics; Sound pressure","score_opus":0.009822918424761969,"score_gpt":0.22409785749327263,"score_spread":0.21427493906851067,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2158934352","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.940167,0.00019467945,0.03808996,0.000088006906,0.0000751948,0.00014313684,0.000017539309,0.00023377896,0.020990677],"genre_scores_gemma":[0.97768277,0.000059778667,0.021442095,2.9260542e-7,0.000024922028,3.2242679e-7,0.0000065760973,0.000011944204,0.0007713042],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991339,0.000023449746,0.00016037076,0.00015444358,0.00025994264,0.00026793467],"domain_scores_gemma":[0.9993319,0.00005029346,0.00004260687,0.00031173025,0.00022461826,0.00003885486],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00014668866,0.00008517618,0.0001767768,0.0005097659,0.00017128953,0.000006806448,0.00041635087,0.0001757321,0.000008019668],"category_scores_gemma":[0.000016334066,0.000105883315,0.00006165715,0.00053514575,0.0005369092,0.000058864935,0.00012027026,0.00038363828,0.000006215352],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000036920417,0.00027746413,0.0059206276,0.00027026227,0.0001440988,0.00029200647,0.00011320831,0.49312168,0.4445738,0.04993749,0.0035049424,0.0018074936],"study_design_scores_gemma":[0.0013964224,0.0003694071,0.02423082,0.00017801857,0.00007473612,0.00006056809,0.001836352,0.90581346,0.050136954,0.010235676,0.0051396433,0.0005279611],"about_ca_topic_score_codex":0.0002336085,"about_ca_topic_score_gemma":0.000029301606,"teacher_disagreement_score":0.41269177,"about_ca_system_score_codex":0.000114589995,"about_ca_system_score_gemma":0.000046563015,"threshold_uncertainty_score":0.43177962},"labels":[],"label_agreement":null},{"id":"W2159814961","doi":"10.1017/s002211201000145x","title":"The rise and fall of turbulent fountains: a new model for improved quantitative predictions","year":2010,"lang":"en","type":"article","venue":"Journal of Fluid Mechanics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":47,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of British Columbia","funders":"","keywords":"Turbulence; Froude number; Mechanics; Scaling; Physics; Reynolds number; Dimensionless quantity; Statistical physics; Flow (mathematics); Entrainment (biomusicology); Meteorology; Classical mechanics; Mathematics; Geometry","score_opus":0.011668778318692199,"score_gpt":0.23913262850217631,"score_spread":0.2274638501834841,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2159814961","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.08724647,0.00072917773,0.91087705,0.00020867659,0.00074052974,0.00013971118,0.000029968569,0.000011124535,0.000017290522],"genre_scores_gemma":[0.8930367,0.002090496,0.104509085,0.000018774394,0.00020410825,0.0000055878054,8.3731004e-7,0.00003506813,0.00009933723],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99937695,0.000005078321,0.0003406185,0.000052663938,0.00009970878,0.00012496398],"domain_scores_gemma":[0.9993452,0.00012406147,0.000118892065,0.00011627326,0.00021360567,0.00008197824],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00035555163,0.00008746478,0.00015020336,0.00004384459,0.00007281758,0.00002522706,0.00014165624,0.00006911702,9.613015e-7],"category_scores_gemma":[0.0001618581,0.000062366445,0.00008331964,0.000044794484,0.000015904354,0.000077479424,0.000018884628,0.00025929025,1.3259917e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00010092033,0.00004412686,0.0000017416905,0.00006102463,0.0002148316,0.0000014882337,0.00076110265,0.4608511,0.4236512,0.10657431,0.003440138,0.0042980276],"study_design_scores_gemma":[0.0004099607,0.00017140972,0.0000028057918,0.00001986158,0.000068661975,0.000020648207,0.00011873816,0.97170293,0.00055845553,0.025677303,0.0011894972,0.00005972471],"about_ca_topic_score_codex":0.0000028063612,"about_ca_topic_score_gemma":0.00006760122,"teacher_disagreement_score":0.806368,"about_ca_system_score_codex":0.000023363024,"about_ca_system_score_gemma":0.00007497809,"threshold_uncertainty_score":0.25432298},"labels":[],"label_agreement":null},{"id":"W2161817585","doi":"","title":"Effect of mean flow on the acoustic trapped modes of a cavity-duct system","year":2007,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"","keywords":"Mean flow; Duct (anatomy); Acoustics; Mach number; Acoustic resonance; Mechanics; Dissipation; Physics; Optics; Resonator; Turbulence","score_opus":0.0054788433170707565,"score_gpt":0.19604704794310043,"score_spread":0.19056820462602966,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2161817585","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9129824,0.000112321984,0.079422586,0.000014539683,0.0007303765,0.00040013468,0.0003976022,0.00008612696,0.0058539165],"genre_scores_gemma":[0.99915445,0.000016538957,0.00053271523,0.000026858794,0.00014139709,0.0000066962875,0.00001267014,0.00006557837,0.000043080367],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9986326,0.000043162025,0.0003981697,0.000163354,0.0002613342,0.0005013915],"domain_scores_gemma":[0.99838185,0.0006838696,0.000069591355,0.0004924396,0.00009537783,0.00027686066],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00089528685,0.0002512872,0.0003719671,0.00021756957,0.000091964524,0.000015678937,0.00034581873,0.00016949423,0.000017133567],"category_scores_gemma":[0.00017925104,0.00019742564,0.00010566663,0.0002943429,0.000119377815,0.000023390103,0.000014904373,0.00030888658,0.000008606152],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000019264578,0.000009053341,0.000045430246,0.00081419706,0.00008092145,0.000050045015,0.00020727747,0.8971477,0.09621391,0.0015886327,0.0008638464,0.002959692],"study_design_scores_gemma":[0.00022585233,0.00017160713,0.00035862267,0.00019699398,0.00015875627,0.000010659239,0.00033615594,0.9917802,0.006489652,0.000029880879,0.000032078373,0.00020949867],"about_ca_topic_score_codex":0.0016140176,"about_ca_topic_score_gemma":0.0065686996,"teacher_disagreement_score":0.09463251,"about_ca_system_score_codex":0.00037324525,"about_ca_system_score_gemma":0.00011422329,"threshold_uncertainty_score":0.8050784},"labels":[],"label_agreement":null},{"id":"W2164763912","doi":"10.2514/6.2012-2188","title":"CFD investigation of noise around a landing gear","year":2012,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"National Research Council Canada","funders":"","keywords":"Landing gear; Computational fluid dynamics; Noise (video); Wind tunnel; Wake; Aerospace engineering; Marine engineering; Acoustics; Solver; Engineering; Computer science; Physics","score_opus":0.01287105123051078,"score_gpt":0.20639945711432842,"score_spread":0.19352840588381764,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2164763912","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.95000476,0.000072637464,0.036471255,0.000008623695,0.00027882482,0.0000341795,0.0000027527296,0.00007550059,0.013051478],"genre_scores_gemma":[0.9946123,0.000015359741,0.005090268,0.000014008851,0.00012109871,0.0000018853674,0.0000047346152,0.000011734579,0.00012866301],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99969643,0.000003262043,0.00009340261,0.00003224125,0.000059587786,0.0001150963],"domain_scores_gemma":[0.99983233,0.00002088394,0.000011565217,0.00007856611,0.00001093727,0.000045734414],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000089551155,0.000048288548,0.00006061305,0.000028803503,0.000013683029,0.000006327306,0.00003910153,0.000032399534,0.00003905207],"category_scores_gemma":[0.000010386596,0.000044264205,0.000016214748,0.000059585112,0.000013767344,0.00008447488,0.000011500732,0.000048327576,0.000020853735],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000004544034,0.000038120434,0.23460689,0.00032087238,0.00009748486,0.0000015368452,0.0019742406,0.11537971,0.5875736,0.053162083,0.0041580154,0.0026829147],"study_design_scores_gemma":[0.00016602923,0.000011248231,0.026735708,0.000028861537,0.000020505315,0.000003030236,0.0001359625,0.9595417,0.011186839,0.0013586305,0.0006270668,0.00018444161],"about_ca_topic_score_codex":0.000007076372,"about_ca_topic_score_gemma":0.0000028529055,"teacher_disagreement_score":0.844162,"about_ca_system_score_codex":0.000019108955,"about_ca_system_score_gemma":0.000002630975,"threshold_uncertainty_score":0.18050419},"labels":[],"label_agreement":null},{"id":"W2166533727","doi":"10.5139/jksas.2008.36.8.774","title":"Experimental Study on Characteristics of Micro-Supersonic Jet Flows","year":2008,"lang":"en","type":"article","venue":"Journal of the Korean Society for Aeronautical & Space Sciences","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Pitot tube; Jet (fluid); Schlieren; Supersonic speed; Nozzle; Reynolds number; Mechanics; Mach number; Flow visualization; Physics; Choked flow; Materials science; Flow (mathematics); Turbulence; Thermodynamics","score_opus":0.023182236392250578,"score_gpt":0.2642137408572529,"score_spread":0.24103150446500232,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2166533727","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9969707,0.0001667892,0.0011818421,0.00034311673,0.0009039673,0.00021818583,0.000027959284,0.0000139996755,0.00017344888],"genre_scores_gemma":[0.99268925,0.000047239697,0.006929662,0.000058370544,0.00020414032,0.0000028349323,4.3236e-7,0.000017591881,0.000050490053],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99859834,0.000022207885,0.00041004093,0.0001338262,0.0005518792,0.00028370373],"domain_scores_gemma":[0.99932057,0.00017862057,0.00015165434,0.00017366801,0.00008526021,0.000090230926],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00062224927,0.00016875322,0.0003275407,0.000027607788,0.00030542613,0.000028545333,0.00059369375,0.000063482534,0.000013215665],"category_scores_gemma":[0.00008047355,0.00010332085,0.0005485156,0.00021133434,0.0005175806,0.00009828744,0.00007037451,0.00028204048,0.0000015137643],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00033955436,0.0073872707,0.048374858,0.0003006752,0.0016829425,0.000046282577,0.046791386,0.047655754,0.80303204,0.007830998,0.034951806,0.001606416],"study_design_scores_gemma":[0.008103134,0.01838377,0.1239565,0.00074937806,0.000943142,0.00059947895,0.06434508,0.6284609,0.14717531,0.0018247197,0.0033194392,0.00213914],"about_ca_topic_score_codex":0.0000017601764,"about_ca_topic_score_gemma":0.0000012021568,"teacher_disagreement_score":0.6558567,"about_ca_system_score_codex":0.000113614944,"about_ca_system_score_gemma":0.00007622489,"threshold_uncertainty_score":0.42133018},"labels":[],"label_agreement":null},{"id":"W2166556425","doi":"10.1115/fedsm2014-21276","title":"Flow Characteristics and Structure of 3D Turbulent Offset Jets","year":2014,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Manitoba Hydro; University of Manitoba","funders":"","keywords":"Turbulence; Offset (computer science); Turbulence kinetic energy; Reynolds stress; Particle image velocimetry; Reynolds number; Mechanics; Physics; Optics","score_opus":0.003401940066880259,"score_gpt":0.17724528402557285,"score_spread":0.17384334395869258,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2166556425","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9489733,0.000030188081,0.049027756,0.000024613964,0.00029526133,0.000048470036,0.000064508655,0.00006657225,0.0014693205],"genre_scores_gemma":[0.98739785,0.00004531933,0.012341389,0.000034903624,0.000083432395,4.4922925e-7,0.000024975452,0.000015365345,0.000056304998],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99961764,0.0000045076827,0.00013248746,0.000075227195,0.000070497124,0.0000996625],"domain_scores_gemma":[0.9997634,0.000023722825,0.000017118893,0.00013270444,0.000024288924,0.000038708786],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00003356471,0.0000858437,0.00012837286,0.00002287589,0.00001577206,0.000011328957,0.000057223166,0.00005785714,0.000088325214],"category_scores_gemma":[0.000016806114,0.00007338399,0.000012737815,0.000028697594,0.000020888037,0.00002074099,0.000020646718,0.00007983325,0.0000024593808],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000025975176,0.0000864621,0.005561475,0.0016596564,0.00026207283,0.0000147548935,0.0009648429,0.3421719,0.29065767,0.02582206,0.011578335,0.32119477],"study_design_scores_gemma":[0.000094847266,0.00001464951,0.0046987953,0.000011603616,0.000010117052,0.0000047203785,0.000004356071,0.99235696,0.00067532057,0.00042538115,0.0016093088,0.00009392903],"about_ca_topic_score_codex":0.0000016511417,"about_ca_topic_score_gemma":0.0000053886497,"teacher_disagreement_score":0.65018505,"about_ca_system_score_codex":0.000007610923,"about_ca_system_score_gemma":0.0000022995484,"threshold_uncertainty_score":0.29925123},"labels":[],"label_agreement":null},{"id":"W2168685095","doi":"10.1061/(asce)0733-9399(2008)134:3(224)","title":"Comparison of Far-Field Turbulent Structure of a Rectangular Surface Jet to Three-Dimensional Free and Wall Jets","year":2008,"lang":"en","type":"article","venue":"Journal of Engineering Mechanics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Calgary; Western University","funders":"","keywords":"Jet (fluid); Mechanics; Turbulence; Free surface; Physics; Prandtl number; Boundary layer; Classical mechanics; Optics; Convection","score_opus":0.010264077261706816,"score_gpt":0.21874762005700693,"score_spread":0.20848354279530013,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2168685095","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8449442,0.0011145758,0.15333591,0.000043880493,0.0004552155,0.00006571253,0.000017308075,0.000018535773,0.000004665674],"genre_scores_gemma":[0.9471582,0.00009460324,0.05264119,0.000013710387,0.00005548977,2.0792419e-7,0.0000010857833,0.000033232198,0.000002269945],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99883986,0.0000064778587,0.00055849145,0.00008883509,0.00033155427,0.00017476828],"domain_scores_gemma":[0.9992636,0.00010443518,0.00014528919,0.00020536974,0.00016387622,0.00011744796],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00014045884,0.00017530199,0.00046777623,0.0001181133,0.00002077681,0.00000559546,0.00022757589,0.00012649702,0.000013637294],"category_scores_gemma":[0.0001460164,0.00016139867,0.00008750429,0.00014733755,0.00000658984,0.000052669177,0.00006054075,0.00035156382,2.1520479e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000014818749,0.00001651603,0.00013694276,0.00008308258,0.00006770246,0.00001664363,0.0001405572,0.72791684,0.27086535,0.00030362175,0.00034371208,0.00009421361],"study_design_scores_gemma":[0.00031884632,0.00028032274,0.00029574268,0.00017283572,0.00004268927,0.0001541305,0.000014043467,0.92726964,0.070738986,0.00036674275,0.0001820245,0.00016396737],"about_ca_topic_score_codex":0.000006222409,"about_ca_topic_score_gemma":0.0000130545895,"teacher_disagreement_score":0.20012636,"about_ca_system_score_codex":0.000043666172,"about_ca_system_score_gemma":0.000022682767,"threshold_uncertainty_score":0.6581646},"labels":[],"label_agreement":null},{"id":"W2170923009","doi":"10.1007/s10494-013-9476-6","title":"Mean Flow and Turbulence Measurements in a Turbulent Free Cruciform Jet","year":2013,"lang":"en","type":"article","venue":"Flow Turbulence and Combustion","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":16,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"St. Francis Xavier University","funders":"","keywords":"Body orifice; Turbulence; Mechanics; Physics; Jet (fluid); Reynolds number; Turbulence kinetic energy; Vorticity; Strouhal number; Vortex; Engineering","score_opus":0.011492270923746379,"score_gpt":0.19541065379476663,"score_spread":0.18391838287102025,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2170923009","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9894256,0.002025251,0.0065119206,0.00022968788,0.00046554708,0.00046568929,0.000018218157,0.0001789031,0.00067915843],"genre_scores_gemma":[0.99177,0.0013422961,0.006473945,0.00012793447,0.00009158134,0.000076958335,0.000020391855,0.0000338482,0.00006301829],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9985817,0.000020852063,0.00033566513,0.00034957522,0.00030559243,0.00040663357],"domain_scores_gemma":[0.9993409,0.000034755736,0.000040053706,0.00035389085,0.00008082856,0.00014957585],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00024336422,0.00029348035,0.00026069928,0.00013105021,0.000102788086,0.0001300913,0.00022783095,0.00015489294,0.000088011715],"category_scores_gemma":[0.000043269458,0.0002732167,0.000035506928,0.00018601769,0.000076327,0.00039714543,0.00009844314,0.00031408304,0.000033332035],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00006480155,0.00028479597,0.023214364,0.0010836159,0.00014604138,0.000050375682,0.0036742853,0.72543234,0.0070182513,0.0007804828,0.014366348,0.22388433],"study_design_scores_gemma":[0.00063071627,0.000057491157,0.01277191,0.0002474409,0.000021024918,0.00002256476,0.00010798299,0.9818334,0.00026790905,0.003534112,0.00014506835,0.0003603872],"about_ca_topic_score_codex":0.00009007342,"about_ca_topic_score_gemma":0.00011660404,"teacher_disagreement_score":0.2564011,"about_ca_system_score_codex":0.00008636182,"about_ca_system_score_gemma":0.000012794726,"threshold_uncertainty_score":0.999972},"labels":[],"label_agreement":null},{"id":"W2172304755","doi":"10.1299/jsmeintmovic.6.1.537","title":"CONTROL OF FLUID-STRUCTURE-SOUND INTERACTION MECHANISMS BY MEANS OF SYNTHETIC JETS","year":2002,"lang":"en","type":"article","venue":"The Proceedings of the International Conference on Motion and Vibration Control","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"","keywords":"Synthetic jet; Acoustics; Turbulence; Aeroelasticity; Flow (mathematics); Mechanics; Vibration; Excited state; Jet (fluid); Vortex; Physics; Flow control (data); Sound (geography); Aerodynamics; Computer science; Atomic physics; Telecommunications","score_opus":0.012847846553644973,"score_gpt":0.2086104545666517,"score_spread":0.1957626080130067,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2172304755","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6223215,0.000053165903,0.3659922,0.0040406478,0.0010362739,0.00058676506,0.00032306532,0.00005333358,0.005593088],"genre_scores_gemma":[0.99964035,0.000040771236,0.00010816241,0.000097540586,0.000034681063,0.000008678418,0.0000033125802,0.000010869843,0.00005566338],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991888,0.000010428046,0.0003280562,0.00010839358,0.0002862703,0.000078095625],"domain_scores_gemma":[0.9992759,0.000072951625,0.00023464975,0.00007831903,0.00031626603,0.000021898291],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015435547,0.00011491217,0.00016527467,0.000060390325,0.00004916834,0.00003987078,0.0002744523,0.00005815387,0.00018860876],"category_scores_gemma":[0.000103250546,0.00007760525,0.000058632395,0.000059479124,0.000078528195,0.00014424583,0.000018856415,0.00013129035,0.0000010572013],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000047932717,0.000035975594,0.00007905168,0.000034018023,0.00008924173,2.0522222e-8,0.0001863,0.008353696,0.8037351,0.18601874,0.00018883048,0.0012311541],"study_design_scores_gemma":[0.00061033043,0.000059339876,0.00017220879,0.000063479965,0.000041495863,0.0000031465634,0.00013781212,0.9241163,0.058725853,0.015978133,0.00002386207,0.00006803938],"about_ca_topic_score_codex":0.00000489347,"about_ca_topic_score_gemma":0.0000034580962,"teacher_disagreement_score":0.9157626,"about_ca_system_score_codex":0.000027932481,"about_ca_system_score_gemma":0.0000035486196,"threshold_uncertainty_score":0.31646502},"labels":[],"label_agreement":null},{"id":"W2176236458","doi":"10.1115/ajkfluids2015-8224","title":"Characterization of Turbulent Flow and Pressure Fluctuations Over a Hydrophone by LES","year":2015,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Dalhousie University","funders":"","keywords":"Turbulence; Hydrophone; Acoustics; Noise (video); Flow (mathematics); Fluent; Computational fluid dynamics; Turbulence modeling; Vorticity; Flow measurement; Sound pressure; Detached eddy simulation; Geology; Mechanics; Physics; Marine engineering; Engineering; Vortex; Computer science; Reynolds-averaged Navier–Stokes equations","score_opus":0.006721441364439148,"score_gpt":0.19076272462967908,"score_spread":0.18404128326523994,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2176236458","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.86295986,0.00018424186,0.13559192,0.000037828086,0.000112558504,0.000074002106,0.00006268205,0.00006059175,0.000916323],"genre_scores_gemma":[0.99766856,0.000092129565,0.0015303281,0.000011138984,0.000030697367,0.0000041632206,0.00007191139,0.00001252971,0.00057853747],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996975,0.0000039496354,0.00009794757,0.00006021666,0.00007882577,0.00006153017],"domain_scores_gemma":[0.9998277,0.0000073869687,0.000013787283,0.000079328165,0.000031565476,0.00004027422],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000037567777,0.00006078619,0.0000743256,0.000019742825,0.000013823808,0.0000110169,0.00003323202,0.00004107279,0.000055466076],"category_scores_gemma":[0.000009406795,0.00005375552,0.000009710535,0.000044224216,0.000015143634,0.000051530442,0.00001354197,0.000039681043,0.0000020361651],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000003616761,0.000029594192,0.00019080298,0.00006750598,0.000049931292,6.327574e-7,0.00043383223,0.11966942,0.87174773,0.0003119517,0.0045171943,0.0029777775],"study_design_scores_gemma":[0.00014208474,0.000010835666,0.000913884,0.000006750637,0.000015324407,0.0000010414802,0.000012435041,0.99131316,0.0037095756,0.000092120536,0.0037152749,0.00006750581],"about_ca_topic_score_codex":0.0000103013,"about_ca_topic_score_gemma":0.0000037850057,"teacher_disagreement_score":0.8716437,"about_ca_system_score_codex":0.000007651931,"about_ca_system_score_gemma":0.0000044489934,"threshold_uncertainty_score":0.21920864},"labels":[],"label_agreement":null},{"id":"W2180276312","doi":"10.1115/fedsm2007-37372","title":"Spectral Linear Stochastic Estimation of the Turbulent Velocity in a Square Three-Dimensional Wall Jet","year":2007,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Queen's University; University of New Brunswick","funders":"","keywords":"Turbulence; Jet (fluid); Reynolds number; Mechanics; Physics; Offset (computer science); Vortex; Computer science","score_opus":0.008415568914367068,"score_gpt":0.2210822644306355,"score_spread":0.21266669551626843,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2180276312","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7386356,0.000021123851,0.26069713,0.000054380354,0.00015248846,0.00011605706,0.0000038122473,0.000038593484,0.0002807928],"genre_scores_gemma":[0.9887847,6.6079184e-7,0.01111195,0.000026411517,0.000034499837,0.0000019718377,0.000005243941,0.000013700669,0.000020883346],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993297,0.0000044334474,0.00022511257,0.00008871459,0.00017706466,0.00017496069],"domain_scores_gemma":[0.9997066,0.00006517813,0.000023703573,0.0001490042,0.000026210839,0.000029247703],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020163544,0.000096929434,0.000106475934,0.000044203047,0.000023671088,0.000004577737,0.000107348926,0.0000595326,0.000047137673],"category_scores_gemma":[0.000032531836,0.00006943613,0.00004412279,0.00014371441,0.000027894861,0.00002924472,0.000027530228,0.00017019353,0.0000068087306],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00000927131,0.00002284307,0.0002772107,0.000020083171,0.0000060963444,0.0000023114708,0.00005023095,0.99761575,0.00034277345,0.001107182,0.000048835,0.00049738283],"study_design_scores_gemma":[0.00016252053,0.000019873747,0.02657896,0.000037142872,0.000005876486,0.0000030588603,0.000007670018,0.97147983,0.00036279223,0.0012572884,0.0000041736635,0.0000808384],"about_ca_topic_score_codex":0.00006279846,"about_ca_topic_score_gemma":0.0009353835,"teacher_disagreement_score":0.25014907,"about_ca_system_score_codex":0.00008354965,"about_ca_system_score_gemma":0.000014578575,"threshold_uncertainty_score":0.2831523},"labels":[],"label_agreement":null},{"id":"W2181089099","doi":"10.1115/pvp2015-45634","title":"Suppression of Acoustic Resonance in Rectangular Cavities Using Spanwise Control Cylinder","year":2015,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Ontario Tech University","funders":"","keywords":"Vortex shedding; Acoustic resonance; Cylinder; Resonance (particle physics); Acoustics; Materials science; Vortex; Excitation; Mach number; Noise control; Optics; Flow control (data); Mechanics; Physics; Turbulence; Geometry; Atomic physics; Telecommunications; Reynolds number; Engineering","score_opus":0.019123965663812324,"score_gpt":0.23366523278026763,"score_spread":0.2145412671164553,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2181089099","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8662869,0.0010581429,0.12861924,0.000010811894,0.0005079493,0.00014175825,0.000023942399,0.0000795821,0.0032716743],"genre_scores_gemma":[0.99536747,0.000029390154,0.0043896968,0.000016266622,0.000053421252,0.0000037200548,0.0000025280087,0.000026146829,0.00011139207],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992945,0.000017663793,0.00023195964,0.00010545346,0.0001564726,0.00019391085],"domain_scores_gemma":[0.9996358,0.000052160314,0.000024276553,0.00017711987,0.000054002845,0.00005663009],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017972989,0.00010953921,0.00019865077,0.00007096018,0.000012747491,0.000009413534,0.0000980958,0.00008553263,0.000020857027],"category_scores_gemma":[0.00007295554,0.00010089404,0.00002674112,0.00011143521,0.000033897337,0.0000698703,0.00002275805,0.00012541634,0.000002257185],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000019030776,0.000017712626,0.0012599133,0.00004518312,0.000007246317,0.000016403534,0.00022353035,0.9578279,0.039440155,0.0002005644,0.00034318015,0.00059914956],"study_design_scores_gemma":[0.00065209187,0.000015462823,0.0005551194,0.00008084648,0.00001218577,0.0000036546007,0.0002378295,0.99621534,0.0014475028,0.000491905,0.0001605958,0.00012745975],"about_ca_topic_score_codex":0.00008503141,"about_ca_topic_score_gemma":0.000097493095,"teacher_disagreement_score":0.12908053,"about_ca_system_score_codex":0.00008661222,"about_ca_system_score_gemma":0.000028565633,"threshold_uncertainty_score":0.41143394},"labels":[],"label_agreement":null},{"id":"W2188157880","doi":"","title":"SOURCE IDENTIFICATION OF A GAS TURBINE ENGINE USING AN INVERSE METHOD WITH BEAMFORMING","year":2012,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Tikhonov regularization; Beamforming; Inverse problem; Computer science; Regularization (linguistics); Robustness (evolution); Jet engine; Anechoic chamber; Microphone array; Microphone; Mathematical optimization; Acoustics; Algorithm; Mathematics; Engineering; Aerospace engineering; Artificial intelligence; Physics; Telecommunications","score_opus":0.015029314940275349,"score_gpt":0.2482272282506403,"score_spread":0.23319791331036496,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2188157880","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.45775965,0.000017253175,0.54181325,0.0000017793753,0.00007370867,0.000041487256,0.000002049355,0.00006071124,0.00023009634],"genre_scores_gemma":[0.7431918,0.0000045685147,0.25660694,0.000006441421,0.000076037664,0.0000019378233,0.000008362788,0.000025999263,0.000077924204],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994185,0.000010114029,0.00019549268,0.00007852655,0.000108940825,0.00018844202],"domain_scores_gemma":[0.9996258,0.000023063323,0.000041723022,0.00019786814,0.000039028408,0.00007250125],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000304107,0.000099543,0.00011864792,0.00007103786,0.000030232706,0.000012176987,0.00007701905,0.00004391386,0.000029151583],"category_scores_gemma":[0.000013228932,0.00008537379,0.000021001575,0.0001427077,0.000015964779,0.0002613292,0.000016698752,0.0000821656,0.0000027076112],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000025055194,0.000027856306,0.00037357077,0.000048065365,0.00002216685,1.8365274e-7,0.00041355434,0.80478376,0.19014369,0.00032286023,0.000010696156,0.003851098],"study_design_scores_gemma":[0.00010975656,0.000013592477,0.00013736964,0.000013139944,0.000037819154,0.0000112398175,0.00023739102,0.97269773,0.026446948,0.00003434992,0.0001438851,0.000116796764],"about_ca_topic_score_codex":0.0000320641,"about_ca_topic_score_gemma":0.00001455554,"teacher_disagreement_score":0.28543213,"about_ca_system_score_codex":0.00003766609,"about_ca_system_score_gemma":0.00000596983,"threshold_uncertainty_score":0.3481442},"labels":[],"label_agreement":null},{"id":"W2188517371","doi":"10.1139/tcsme-2011-0003","title":"SIMULATION OF VORTEX SOUND USING THE VISCOUS/ACOUSTIC SPLITTING APPROACH","year":2011,"lang":"en","type":"article","venue":"Transactions of the Canadian Society for Mechanical Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Vortex; Acoustics; Sound (geography); Physics; Mechanics; Computer science","score_opus":0.02597225583252901,"score_gpt":0.216442928776695,"score_spread":0.19047067294416598,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2188517371","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.03739148,0.000050274848,0.9616741,0.000007143911,0.00039004468,0.0002965407,0.00007888425,0.000043413052,0.00006814287],"genre_scores_gemma":[0.955856,0.0000040826003,0.044014886,0.0000110204355,0.000041060623,0.0000141660375,0.000002064306,0.000045611345,0.000011103402],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991959,0.0000055446053,0.0002895473,0.00011104971,0.00012913995,0.0002688522],"domain_scores_gemma":[0.99938804,0.00013104893,0.000047216337,0.00028277215,0.00006540087,0.00008549991],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002450723,0.00013680954,0.00017119775,0.000033779295,0.00019722102,0.000011001233,0.0002783251,0.00013303991,0.000012078525],"category_scores_gemma":[0.000034720586,0.00010978264,0.00039555746,0.00023083428,0.00004771377,0.000057257705,0.0000063354923,0.00024379084,1.290828e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000011684034,0.000007984065,0.0000012591811,0.00014872527,0.00011002733,4.5528278e-8,0.00040689588,0.9919751,0.0059793503,0.0012272776,0.0000023296286,0.00013979568],"study_design_scores_gemma":[0.00010936035,0.000010691032,0.000012222522,0.000030373609,0.00016716852,0.0000017656589,0.00023671589,0.9976064,0.0011955667,0.0004940427,0.00002046875,0.000115256626],"about_ca_topic_score_codex":0.0014590581,"about_ca_topic_score_gemma":0.0018317521,"teacher_disagreement_score":0.91846454,"about_ca_system_score_codex":0.00019511771,"about_ca_system_score_gemma":0.00006333783,"threshold_uncertainty_score":0.4476806},"labels":[],"label_agreement":null},{"id":"W2192223059","doi":"10.1007/978-3-642-01273-0_6","title":"Far-Field Noise Minimization Using an Adjoint Approach","year":2009,"lang":"en","type":"book-chapter","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto","funders":"","keywords":"Airframe; Airfoil; Noise (video); Trailing edge; Aerospace engineering; Aircraft noise; Engineering; Lift (data mining); Civil aviation; Turbulence; Thrust; Acoustics; Marine engineering; Aeronautics; Computer science; Aviation; Meteorology; Physics; Noise reduction; Structural engineering","score_opus":0.0206994669783309,"score_gpt":0.21350236021112118,"score_spread":0.1928028932327903,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2192223059","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0000740648,0.00011818331,0.34642628,0.0000045440556,0.00025949412,0.00013211076,0.000012777474,0.00023840634,0.65273416],"genre_scores_gemma":[0.051848724,0.0014450211,0.31318942,0.0008654028,0.0023233031,0.000006885029,0.0009840175,0.00073898595,0.6285982],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99904317,0.000003261512,0.00029742793,0.00027549276,0.00017778084,0.00020286786],"domain_scores_gemma":[0.99940646,0.000015231587,0.00004930132,0.0003841804,0.000051715,0.0000931431],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.000056809717,0.0003333252,0.00028888992,0.00011731607,0.000049126415,0.0000561385,0.00016733844,0.00045988595,0.00030319035],"category_scores_gemma":[0.0000068489,0.00034305538,0.000091024085,0.000022194261,0.000014983113,0.00007955299,0.000029909264,0.00034254248,0.00001932525],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000034003776,0.000023154673,7.1129375e-7,0.00008687574,0.000048072332,0.000009933965,0.000045603978,0.9022661,0.00033664991,0.06939777,0.00106063,0.02672113],"study_design_scores_gemma":[0.00008163889,0.000035183904,0.0000019163456,0.000044286277,0.00006136786,0.000009424012,0.000008066559,0.9844418,0.000028195787,0.003051948,0.011794359,0.00044179938],"about_ca_topic_score_codex":0.000006877178,"about_ca_topic_score_gemma":0.0000114756385,"teacher_disagreement_score":0.08217575,"about_ca_system_score_codex":0.000089252375,"about_ca_system_score_gemma":0.000019111323,"threshold_uncertainty_score":0.9999021},"labels":[],"label_agreement":null},{"id":"W2197067750","doi":"10.4271/2008-01-0406","title":"Aeroacoustic Characteristics of Automotive HVAC Systems","year":2008,"lang":"en","type":"article","venue":"SAE technical papers on CD-ROM/SAE technical paper series","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":6,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"Networks of Centres of Excellence of Canada; Ford Motor Company","keywords":"HVAC; Automotive industry; Automotive engineering; Computer science; Engineering; Systems engineering; Aerospace engineering; Mechanical engineering; Air conditioning","score_opus":0.0097473732801087,"score_gpt":0.2108703521647592,"score_spread":0.2011229788846505,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2197067750","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9357224,0.00067354954,0.000054077216,0.0002816948,0.0015168225,0.0011919532,0.00049795146,0.0044687814,0.055592746],"genre_scores_gemma":[0.9951955,0.0012813153,0.001992143,0.00020707585,0.00028397402,0.00018489422,0.00008422921,0.00022707829,0.0005437969],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.99565387,0.00008639532,0.001493264,0.0008286832,0.0009480588,0.0009897193],"domain_scores_gemma":[0.99719733,0.0004972907,0.00025510963,0.0014118102,0.0002522156,0.00038622238],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00042864814,0.0008635358,0.0013660159,0.00023607204,0.00030878233,0.000057685436,0.001056255,0.00091636664,0.00019191255],"category_scores_gemma":[0.0007186329,0.0007999384,0.00042108583,0.0006998486,0.0011252237,0.00026658928,0.0003025262,0.001421951,0.000105710824],"study_design_candidate":"observational","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000832261,0.00028597546,0.00018980826,0.00025962782,0.000105555824,0.00016457259,0.000046456742,0.0038235402,0.9844932,0.0062461053,0.0035675985,0.00073435967],"study_design_scores_gemma":[0.0005314819,0.00073642196,0.9893497,0.0003774077,0.00013885318,0.00026931375,0.00008418725,0.00004247539,0.00007942838,0.0004364862,0.007016887,0.00093735574],"about_ca_topic_score_codex":0.000021594962,"about_ca_topic_score_gemma":0.002481482,"teacher_disagreement_score":0.9891599,"about_ca_system_score_codex":0.0003727441,"about_ca_system_score_gemma":0.00009197475,"threshold_uncertainty_score":0.99944514},"labels":[],"label_agreement":null},{"id":"W2199922896","doi":"10.1115/pvp2015-45259","title":"Resonance of Trapped Acoustic Modes of a Ducted Rectangular Cavity","year":2015,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"","keywords":"Excited state; Rotational symmetry; Physics; Excitation; Acoustic resonance; Particle velocity; Oscillation (cell signaling); Acoustics; Resonance (particle physics); Sound pressure; Mechanics; Optics; Atomic physics; Chemistry","score_opus":0.015987367554910686,"score_gpt":0.21460422549295996,"score_spread":0.19861685793804928,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2199922896","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.91109544,0.0005167438,0.08036802,0.0000075223606,0.00014424848,0.00008448659,0.000032981872,0.00009754037,0.007653037],"genre_scores_gemma":[0.9906224,0.000048587848,0.009101384,0.0000037980678,0.000024364104,0.0000030211102,0.0000038094124,0.000018857067,0.00017379216],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994124,0.000010016054,0.00021445709,0.00008745495,0.00014773814,0.00012794422],"domain_scores_gemma":[0.9995647,0.000031421765,0.000029499695,0.00021440246,0.00010602117,0.00005397456],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00013572091,0.00008854314,0.00019334532,0.000040485786,0.000007906747,0.000002934892,0.00011649576,0.00006216452,0.0000163108],"category_scores_gemma":[0.00008271018,0.00008250192,0.00003613236,0.00016156406,0.000044350032,0.00003610743,0.000019270172,0.000076922945,0.000001859988],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000022387283,0.000051131003,0.00024620915,0.00014997106,0.000032885506,0.000005106318,0.0002819805,0.59311277,0.40029788,0.0019144814,0.0014556121,0.0024296031],"study_design_scores_gemma":[0.00026142478,0.00003642176,0.00050506165,0.000030097044,0.000019485067,0.0000020279122,0.0001223101,0.979287,0.018466325,0.0010439095,0.000116240095,0.000109645014],"about_ca_topic_score_codex":0.00004378649,"about_ca_topic_score_gemma":0.000048341615,"teacher_disagreement_score":0.3861743,"about_ca_system_score_codex":0.00002778148,"about_ca_system_score_gemma":0.000023952287,"threshold_uncertainty_score":0.33643308},"labels":[],"label_agreement":null},{"id":"W2200822496","doi":"10.1115/1.4032281","title":"Flow-Excited Acoustic Resonance of Trapped Modes of a Ducted Rectangular Cavity","year":2015,"lang":"en","type":"article","venue":"Journal of Pressure Vessel Technology","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":6,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"","keywords":"Excited state; Acoustic resonance; Resonance (particle physics); Physics; Mechanics; Rotational symmetry; Oscillation (cell signaling); Excitation; Acoustics; Atomic physics; Chemistry","score_opus":0.010236874131562206,"score_gpt":0.22024946117421318,"score_spread":0.21001258704265097,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2200822496","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8987571,0.010180211,0.0898452,0.00013682093,0.00050065346,0.00013557707,0.00006373792,0.00012115463,0.0002595689],"genre_scores_gemma":[0.98510677,0.00038426972,0.014364922,0.0000037577327,0.00006950026,0.0000025348636,0.0000015796701,0.000033503355,0.000033184464],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9986349,0.000033669356,0.0006949599,0.00011876807,0.00029193083,0.0002258028],"domain_scores_gemma":[0.99855053,0.00006346736,0.00036233247,0.00034505097,0.0006035716,0.000075033415],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00039498293,0.00016992219,0.0005928441,0.00044877085,0.000018197168,0.0000057930365,0.00048318636,0.0003540769,0.000008586682],"category_scores_gemma":[0.0004912204,0.00015578548,0.00009208111,0.00061987864,0.00017835147,0.00010032088,0.000057939324,0.0005238543,5.624394e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000089711895,0.00011376034,0.00041152776,0.00024918874,0.00024319453,0.00005268554,0.00019723005,0.5575009,0.4354287,0.000629727,0.0018135166,0.0032698705],"study_design_scores_gemma":[0.0012397475,0.0003569905,0.0005491007,0.00028542924,0.00030464068,0.00016911366,0.0003045739,0.9407027,0.04646344,0.006395717,0.0029901483,0.00023843667],"about_ca_topic_score_codex":0.0000051465768,"about_ca_topic_score_gemma":0.000006457894,"teacher_disagreement_score":0.38896528,"about_ca_system_score_codex":0.000035036494,"about_ca_system_score_gemma":0.00008082858,"threshold_uncertainty_score":0.63527477},"labels":[],"label_agreement":null},{"id":"W2212972698","doi":"10.1115/pvp2015-45205","title":"Effect of Cavity Volume on the Flow-Excited Acoustic Resonance of a Shallow Cavity in a Pipe-Line","year":2015,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"","keywords":"Strouhal number; Acoustics; Volume (thermodynamics); Physics; Mechanics; Materials science; Turbulence; Thermodynamics","score_opus":0.010969893445530227,"score_gpt":0.2260343406841455,"score_spread":0.21506444723861526,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2212972698","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98131555,0.00013228285,0.015467125,0.000047694164,0.0002271379,0.0002899755,0.000056451252,0.000063564265,0.0024001868],"genre_scores_gemma":[0.9991636,0.00002150148,0.00045423218,0.000021614562,0.000039827097,0.000018632103,0.0000067943374,0.000026723936,0.0002470492],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989604,0.00008069819,0.0003140987,0.00015770641,0.000260656,0.00022648646],"domain_scores_gemma":[0.99905187,0.00035909098,0.000046794867,0.00040439644,0.00007519879,0.000062676176],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0009290713,0.00017673148,0.00034096348,0.00007051125,0.00001646701,0.000007399236,0.00024600144,0.00010279431,0.00003173792],"category_scores_gemma":[0.00049845036,0.00012107924,0.00006544292,0.00031620957,0.00006885016,0.00003706029,0.000056065786,0.00027176493,0.000010061383],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00013037615,0.00009304312,0.004248385,0.00024353988,0.000023799897,0.000014936876,0.00023545901,0.9767265,0.012290458,0.00024924515,0.000998444,0.0047458257],"study_design_scores_gemma":[0.0005434557,0.0002826778,0.004190248,0.00009462012,0.000018786719,0.000001382308,0.000020277937,0.9925776,0.0019418421,0.0001248436,0.00008158552,0.00012266872],"about_ca_topic_score_codex":0.00022632995,"about_ca_topic_score_gemma":0.0007124958,"teacher_disagreement_score":0.017848043,"about_ca_system_score_codex":0.00009350493,"about_ca_system_score_gemma":0.000024800067,"threshold_uncertainty_score":0.49374682},"labels":[],"label_agreement":null},{"id":"W2222002927","doi":"10.4271/2001-01-1430","title":"Flow-Acoustic Coupling in Quarter-Wave Resonators Using Computational Fluid Dynamics","year":2001,"lang":"en","type":"article","venue":"SAE technical papers on CD-ROM/SAE technical paper series","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Resonator; Coupling (piping); Acoustics; Flow (mathematics); Fluid dynamics; Quarter (Canadian coin); Mechanics; Computational fluid dynamics; Dynamics (music); Computer science; Materials science; Physics; Mechanical engineering; Engineering; Optoelectronics","score_opus":0.01215980405145344,"score_gpt":0.2325840479844579,"score_spread":0.22042424393300444,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2222002927","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98371005,0.00035450648,0.0009342688,0.0005171325,0.000736426,0.00078841246,0.00015081378,0.0026140644,0.010194317],"genre_scores_gemma":[0.9803728,0.00032639905,0.01823961,0.00034522096,0.00019482579,0.0000924621,0.00014789822,0.00022476893,0.00005603721],"study_design_codex":"simulation_or_modeling","study_design_gemma":"observational","domain_scores_codex":[0.99556905,0.00005411179,0.0013344585,0.00097099494,0.00090341526,0.0011679479],"domain_scores_gemma":[0.9979643,0.00053095847,0.0001307837,0.00090380514,0.0001192445,0.00035090666],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00058450067,0.000862314,0.00093676115,0.0003816718,0.0003204737,0.00014038604,0.000685047,0.0008799291,0.00022910087],"category_scores_gemma":[0.00032496362,0.00089036656,0.00032585324,0.00110408,0.0005567697,0.00036723525,0.00025445476,0.0016185837,0.00004545691],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":true,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000086266526,0.00016633216,0.00022432859,0.000062470004,0.000034272805,0.00022850373,0.00002068969,0.61945933,0.3742782,0.004253883,0.00032247932,0.00086329394],"study_design_scores_gemma":[0.0013318097,0.0005557276,0.8012295,0.00058932404,0.00012327352,0.00038211994,0.00029787642,0.18383104,0.000008761836,0.007940139,0.0019380145,0.0017724391],"about_ca_topic_score_codex":0.000030366238,"about_ca_topic_score_gemma":0.054854684,"teacher_disagreement_score":0.8010051,"about_ca_system_score_codex":0.0012386414,"about_ca_system_score_gemma":0.000095932206,"threshold_uncertainty_score":0.9993547},"labels":[],"label_agreement":null},{"id":"W2229036225","doi":"10.1121/1.4939493","title":"Sub-harmonic broadband humps and tip noise in low-speed ring fans","year":2016,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":86,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Acoustics; Harmonics; Physics; Wake; Noise (video); Tip clearance; Narrowband; Mechanical fan; Vortex; Cylinder; Mechanics; Optics; Computer science; Geometry; Mathematics","score_opus":0.006884639924589113,"score_gpt":0.21111579482362536,"score_spread":0.20423115489903623,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2229036225","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8420518,0.0005430802,0.1556271,0.001308774,0.00021938633,0.000091691865,0.000012398006,0.000015195523,0.00013057292],"genre_scores_gemma":[0.99408996,0.003030772,0.0025387234,0.00015644082,0.00012451046,4.0678347e-7,8.380151e-8,0.000023751945,0.000035364475],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989684,0.000044828015,0.0003936564,0.00007196085,0.00026532487,0.00025579674],"domain_scores_gemma":[0.99902266,0.0004777184,0.00014900458,0.00021377378,0.00006159323,0.00007523347],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00042725864,0.00013773498,0.00027806294,0.000019714986,0.000072489,0.000013152599,0.00039391982,0.00006778739,0.000018652496],"category_scores_gemma":[0.000114604336,0.000066580775,0.00017410361,0.0001626089,0.00040176854,0.00006940952,0.00012061441,0.000388111,0.0000022379982],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00006205709,0.000081857084,0.00083032984,0.00013117064,0.00020054415,0.0000038969465,0.000881015,0.15481985,0.8145034,0.000013463588,0.0041796663,0.024292761],"study_design_scores_gemma":[0.0009641241,0.00009302219,0.009759766,0.0005053166,0.00015746537,0.000056014767,0.0005112104,0.981274,0.005140843,0.001084293,0.00024041852,0.00021351024],"about_ca_topic_score_codex":0.000011861744,"about_ca_topic_score_gemma":0.0000015860925,"teacher_disagreement_score":0.82645416,"about_ca_system_score_codex":0.0000886177,"about_ca_system_score_gemma":0.00002609004,"threshold_uncertainty_score":0.2715085},"labels":[],"label_agreement":null},{"id":"W2233604321","doi":"10.3970/fdmp.2010.006.203","title":"Effects of Flow Pulsing on Passive Scalar Mixing in a Turbulent Round Jet","year":2010,"lang":"en","type":"article","venue":"FDMP: Fluid Dynamics & Materials Processing","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Royal Military College of Canada","funders":"","keywords":"Strouhal number; Mechanics; Turbulence; Jet (fluid); Physics; Scalar (mathematics); Mixing (physics); Inlet; Optics; Reynolds number; Mathematics; Geology","score_opus":0.0026094247407953517,"score_gpt":0.19796359146200265,"score_spread":0.1953541667212073,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2233604321","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9802596,0.00014651542,0.016755488,0.00004533902,0.0019122605,0.00037876455,0.000050608618,0.00019274223,0.00025867746],"genre_scores_gemma":[0.98924637,0.00005289886,0.010097999,0.00004060503,0.0002784374,0.000048638914,0.00007321697,0.00014029321,0.000021550222],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9978721,0.000046474062,0.0007259129,0.00041416296,0.00033647785,0.00060486456],"domain_scores_gemma":[0.9991473,0.00014311649,0.00016105836,0.00033540287,0.00010830288,0.00010481883],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0003853597,0.0004460435,0.00061660784,0.00026805865,0.00012682774,0.00025761678,0.00034519765,0.0003146516,0.00002492238],"category_scores_gemma":[0.00017107656,0.0004416411,0.000073811636,0.00029674868,0.00008929287,0.00026643556,0.00008997062,0.00044865822,0.0000112980115],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00003339043,0.00009748624,0.00007304156,0.0015478261,0.000024511008,0.00006898424,0.00031159152,0.04149357,0.94336206,0.0006554845,0.000017126153,0.012314911],"study_design_scores_gemma":[0.00055258936,0.000046057812,0.0009474707,0.0008847871,0.000040606996,0.000020072655,0.000034906378,0.82215786,0.17374967,0.0010989963,0.000024451208,0.00044253728],"about_ca_topic_score_codex":0.000029517816,"about_ca_topic_score_gemma":0.00009950884,"teacher_disagreement_score":0.78066427,"about_ca_system_score_codex":0.00023198852,"about_ca_system_score_gemma":0.000058575883,"threshold_uncertainty_score":0.99980354},"labels":[],"label_agreement":null},{"id":"W2254629731","doi":"10.4271/2004-01-0855","title":"Detection of Obstructions in Automotive Manifolds by Aeroacoustic Means&lt;xref ref-type=\"fn\" rid=\"FN1\"&gt;*&lt;/xref&gt;","year":2004,"lang":"en","type":"article","venue":"SAE technical papers on CD-ROM/SAE technical paper series","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"","keywords":"Automotive industry; Acoustics; Computer science; Automotive engineering; Aeronautics; Engineering; Aerospace engineering; Physics","score_opus":0.006225894023918695,"score_gpt":0.21009441402384998,"score_spread":0.2038685199999313,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2254629731","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9630549,0.0010387158,0.0003541329,0.00059118646,0.0015491773,0.0015247851,0.00034499555,0.004342418,0.02719972],"genre_scores_gemma":[0.9925052,0.0009458044,0.0053970995,0.00018917322,0.00017061233,0.00021803466,0.000089385874,0.00026106337,0.00022365237],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.9948786,0.00010054233,0.001624271,0.001187062,0.0010117824,0.0011977596],"domain_scores_gemma":[0.9973762,0.0003261232,0.00025560768,0.0014205439,0.00024110408,0.00038040034],"candidate_categories":["metaepi_narrow","research_integrity"],"consensus_categories":[],"category_scores_codex":[0.0005592785,0.0010180133,0.0012250225,0.00043768942,0.00032148746,0.00008618973,0.0010269833,0.0013426761,0.00017881523],"category_scores_gemma":[0.0006880183,0.0010118625,0.00044663015,0.0016076152,0.0008482907,0.00046016005,0.0003103237,0.0018526723,0.000076574295],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":true,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00013035319,0.00040875067,0.000022788288,0.00013345129,0.000088826935,0.00004279153,0.000054734082,0.023152672,0.9679093,0.0054494278,0.0006624794,0.0019444542],"study_design_scores_gemma":[0.003573463,0.0034177788,0.9477102,0.0010933887,0.0005153294,0.00034727497,0.00036538256,0.00011819156,0.0056608682,0.015871353,0.0182117,0.0031150375],"about_ca_topic_score_codex":0.00007069433,"about_ca_topic_score_gemma":0.068412885,"teacher_disagreement_score":0.9622484,"about_ca_system_score_codex":0.001259519,"about_ca_system_score_gemma":0.000108532644,"threshold_uncertainty_score":0.9999538},"labels":[],"label_agreement":null},{"id":"W2275068402","doi":"","title":"Study on Supersonic Moist Air Flows over a Rectangular Cavity","year":2009,"lang":"ko","type":"article","venue":"대한기계학회 춘추학술대회","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Mach number; Supersonic speed; Mechanics; Condensation; Amplitude; Oscillation (cell signaling); Choked flow; Airflow; Compressible flow; Physics; Materials science; Meteorology; Thermodynamics; Optics; Chemistry; Compressibility","score_opus":0.009808997485443434,"score_gpt":0.24167628579924452,"score_spread":0.2318672883138011,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2275068402","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98477226,0.0006573553,0.00068227865,0.00022749616,0.0021826916,0.0009546748,0.0001432567,0.0003995107,0.009980486],"genre_scores_gemma":[0.99654734,0.00012013591,0.00057744386,0.0004019868,0.000873691,0.000022471677,0.000029405874,0.0001392122,0.0012883064],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9966493,0.00012054454,0.0006457186,0.00086264807,0.0007208972,0.00100086],"domain_scores_gemma":[0.9980873,0.00013125442,0.000092434784,0.001294273,0.00008468572,0.00031005585],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00051878067,0.0007629747,0.0007584513,0.00020702336,0.00030166202,0.00014388893,0.0005507804,0.00038199563,0.00026954344],"category_scores_gemma":[0.00013431007,0.00080318213,0.00032282784,0.0005183424,0.000051319792,0.00015522356,0.00010098564,0.0011263046,0.0004700502],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00077530084,0.014735171,0.026634183,0.0007046019,0.0022672846,0.010646875,0.028009659,0.7441301,0.04829083,0.011996035,0.027968287,0.083841704],"study_design_scores_gemma":[0.006150709,0.0068870746,0.29735783,0.00069435243,0.0009536612,0.00009428562,0.0035570608,0.67100555,0.0006847728,0.0018370921,0.006715958,0.0040616933],"about_ca_topic_score_codex":0.00016986129,"about_ca_topic_score_gemma":0.00024218633,"teacher_disagreement_score":0.27072364,"about_ca_system_score_codex":0.0005881643,"about_ca_system_score_gemma":0.00007562763,"threshold_uncertainty_score":0.9994419},"labels":[],"label_agreement":null},{"id":"W2295208928","doi":"10.1016/j.jsv.2016.02.032","title":"Prediction of tonal ducted fan noise","year":2016,"lang":"en","type":"article","venue":"Journal of Sound and Vibration","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":47,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Glenn Research Center","keywords":"Stator; Rotor (electric); Cascade; Noise (video); Acoustics; Parametric statistics; Sound power; Context (archaeology); Engineering; Mechanical fan; Parametric model; Gas compressor; Turbine; Aeroacoustics; Sound pressure; Computer science; Physics; Mechanical engineering; Mathematics","score_opus":0.01056435710259531,"score_gpt":0.1980171869424885,"score_spread":0.18745282983989317,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2295208928","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.76210874,0.00006558587,0.237298,0.00004735802,0.0002774141,0.000015089821,0.000012089342,0.0000067573733,0.0001689919],"genre_scores_gemma":[0.99857956,0.00014632923,0.0010121998,0.000004842516,0.00023308341,1.4898295e-7,0.0000012875818,0.000005209123,0.000017339797],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99964654,0.0000049905198,0.00019429995,0.000026118007,0.000086024935,0.000042041756],"domain_scores_gemma":[0.99978745,0.00002318456,0.000068456895,0.000030369923,0.00006409579,0.000026436173],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00008492494,0.000038152117,0.000070047994,0.0000432793,0.000017263656,0.00001071631,0.000024777877,0.00003215638,0.000016312379],"category_scores_gemma":[0.000019506157,0.000025152312,0.000022037839,0.000031581163,0.0000167594,0.00018088886,0.000004038813,0.00004218244,4.7340038e-7],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000022613021,0.000021359174,0.0037633304,0.000040316056,0.000042475618,0.0000017936901,0.00014946317,0.0053709294,0.9787925,0.001698659,0.00038238216,0.009714199],"study_design_scores_gemma":[0.0046459306,0.0012561955,0.3159635,0.0007372715,0.0002443701,0.00033341334,0.00039098135,0.5483305,0.067551516,0.05757109,0.0024520284,0.00052319665],"about_ca_topic_score_codex":2.5355124e-7,"about_ca_topic_score_gemma":6.907114e-7,"teacher_disagreement_score":0.91124094,"about_ca_system_score_codex":0.000015152372,"about_ca_system_score_gemma":0.0000069944967,"threshold_uncertainty_score":0.10256815},"labels":[],"label_agreement":null},{"id":"W2312692450","doi":"10.2514/6.2004-2621","title":"Air Ejector Pumping Enhancement Through Pulsing Primary Flow","year":2004,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":9,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Calgary","funders":"","keywords":"Injector; Materials science; Flow (mathematics); Primary (astronomy); Automotive engineering; Mechanics; Mechanical engineering; Engineering; Physics","score_opus":0.007012941225493776,"score_gpt":0.20012395165326613,"score_spread":0.19311101042777234,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2312692450","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.1753582,0.00015039605,0.7544534,0.00010356588,0.0008946353,0.00012531385,0.0000048566544,0.0003775407,0.06853204],"genre_scores_gemma":[0.89628243,0.0001290445,0.10265728,0.00034565578,0.00020559183,0.000011631238,0.000018087969,0.000041871026,0.00030839248],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991709,0.000003490725,0.0001988299,0.00016726812,0.00015668345,0.0003028293],"domain_scores_gemma":[0.99969184,0.000015651098,0.00001527499,0.00021069583,0.000022039645,0.000044470296],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00006620036,0.00015678047,0.0001438193,0.000027746772,0.00007654265,0.000029447378,0.00012443941,0.00006203531,0.00014869058],"category_scores_gemma":[0.000007449764,0.00015220692,0.00005156454,0.00010836125,0.000020020889,0.00014987965,0.000044456905,0.00014713708,0.00009235494],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000019727183,0.000034789704,0.000012851679,0.00011104941,0.000040620467,0.000010648619,0.00025002414,0.8954246,0.09681836,0.0026421417,0.00036200875,0.004290922],"study_design_scores_gemma":[0.0015816453,0.000103995306,0.0008424757,0.00033623117,0.000063347936,0.000029721574,0.00019494526,0.81372005,0.15704484,0.012964351,0.011715049,0.001403337],"about_ca_topic_score_codex":0.000016159009,"about_ca_topic_score_gemma":0.000016107346,"teacher_disagreement_score":0.72092426,"about_ca_system_score_codex":0.00027864613,"about_ca_system_score_gemma":0.000021961108,"threshold_uncertainty_score":0.6206818},"labels":[],"label_agreement":null},{"id":"W2313208646","doi":"10.2514/6.2011-2748","title":"Large Eddy Simulation of Jet Noise Suppression by Impinging Microjets","year":2011,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"","keywords":"Jet noise; Jet (fluid); Large eddy simulation; Noise (video); Acoustics; Physics; Aerospace engineering; Mechanics; Computer science; Turbulence; Engineering","score_opus":0.010434888363750864,"score_gpt":0.2217431928342095,"score_spread":0.21130830447045865,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2313208646","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.57181567,0.00007890011,0.4201427,0.0000020750324,0.0002672968,0.00007020622,0.000039002498,0.00012300354,0.007461132],"genre_scores_gemma":[0.995699,0.000021777016,0.0040726373,0.000012753583,0.000025513718,0.0000018116051,0.000023920386,0.000025007857,0.00011758881],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99947566,0.0000057374627,0.0001764426,0.0000925492,0.00007684183,0.00017278205],"domain_scores_gemma":[0.9997272,0.000028036085,0.000025195588,0.00015364267,0.000029630251,0.00003633554],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00008321509,0.000096229385,0.0001078242,0.00004181528,0.000028144295,0.00000635683,0.000090365844,0.00006600242,0.00026785137],"category_scores_gemma":[0.000013207416,0.00008634449,0.000034903722,0.000061888575,0.000009322188,0.000075581265,0.000035141988,0.00007526709,0.000012259824],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000011513237,0.00010434176,0.0025716869,0.00014033855,0.000039103685,0.0000030056158,0.0012310242,0.47481343,0.51384866,0.00070062676,0.005038697,0.0014975565],"study_design_scores_gemma":[0.00016971787,0.0000106940315,0.00040876077,0.000023496897,0.000009060787,3.7825671e-7,0.000055858487,0.9650536,0.033321775,0.00013257544,0.0007019859,0.00011210661],"about_ca_topic_score_codex":0.00000879232,"about_ca_topic_score_gemma":0.000004272444,"teacher_disagreement_score":0.49024016,"about_ca_system_score_codex":0.000016190852,"about_ca_system_score_gemma":0.0000031106056,"threshold_uncertainty_score":0.3521026},"labels":[],"label_agreement":null},{"id":"W2313351278","doi":"10.2514/6.2014-0896","title":"Velocity Field Estimation Using Unsteady Wall Pressure Measurements in a Leading Edge Slat Flow","year":2014,"lang":"en","type":"article","venue":"52nd Aerospace Sciences Meeting","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of New Brunswick","funders":"","keywords":"Enhanced Data Rates for GSM Evolution; Flow (mathematics); Mechanics; Field (mathematics); Leading edge; Geology; Materials science; Computer science; Physics; Telecommunications; Mathematics","score_opus":0.02896421359541092,"score_gpt":0.26350400290473885,"score_spread":0.23453978930932792,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2313351278","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8758396,0.00022032614,0.11262129,0.00012422225,0.00091588456,0.00019259007,0.0000020024977,0.00017026192,0.009913844],"genre_scores_gemma":[0.93762904,0.000008065613,0.06213267,0.000053455606,0.00009251317,0.0000049779674,0.0000015002462,0.000020361662,0.000057432015],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9984027,0.000054680775,0.00028387413,0.00032936555,0.00044257758,0.00048677457],"domain_scores_gemma":[0.99946976,0.00015439237,0.00007610887,0.000179262,0.00004714804,0.0000733425],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0016541563,0.00019590667,0.00022170806,0.00011298133,0.00030292996,0.00017355135,0.00031478627,0.000106947424,0.000011894611],"category_scores_gemma":[0.00047201526,0.00019546802,0.000041587795,0.00045980743,0.0000759997,0.0003201742,0.00006873445,0.00024353589,0.000010166588],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000001279129,0.000007973821,0.0068504303,0.00006654345,0.000006102412,4.879327e-7,0.00039451392,0.97088754,0.01716927,0.00007437222,0.0000770191,0.0044644736],"study_design_scores_gemma":[0.000165272,0.000025398429,0.00047144404,0.00029725817,0.00001475585,0.0000018139733,0.000079812606,0.9955796,0.0027963526,0.00021759237,0.000114617775,0.00023605661],"about_ca_topic_score_codex":0.00009876837,"about_ca_topic_score_gemma":0.0002531907,"teacher_disagreement_score":0.061789446,"about_ca_system_score_codex":0.00009664664,"about_ca_system_score_gemma":0.000027589196,"threshold_uncertainty_score":0.7970955},"labels":[],"label_agreement":null},{"id":"W2313584385","doi":"10.1016/j.jsv.2016.03.026","title":"Impact of the chosen turbulent flow empirical model on the prediction of sound radiation and vibration by aircraft panels","year":2016,"lang":"en","type":"article","venue":"Journal of Sound and Vibration","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Carleton University","funders":"","keywords":"Turbulence; Sound (geography); Acoustics; Vibration; Acoustic radiation; Flow (mathematics); Radiation; Empirical modelling; Engineering; Mechanics; Physics; Simulation; Optics","score_opus":0.016375212517386717,"score_gpt":0.24367544956458037,"score_spread":0.22730023704719365,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2313584385","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.77316165,0.00007593295,0.22612214,0.00038773616,0.00010210782,0.00008021719,0.00004213331,0.000004926547,0.000023153429],"genre_scores_gemma":[0.9992808,0.00030336878,0.00023628604,0.000026145715,0.00012875423,0.000001050653,0.0000036893189,0.000010109774,0.000009771131],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993015,0.000032656953,0.0003288869,0.00006185966,0.00020117387,0.00007393997],"domain_scores_gemma":[0.9994928,0.00011058064,0.00019797492,0.000090687194,0.00007359243,0.000034337085],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002151121,0.000089773326,0.00012524553,0.0000428874,0.000067614455,0.000033060904,0.000058664245,0.000072848066,0.0000061810497],"category_scores_gemma":[0.000053359086,0.000042806547,0.0000665872,0.000060455655,0.000047534835,0.00025763657,0.0000099224535,0.00010730553,1.7884156e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00009275331,0.00008796175,0.010346745,0.00004949706,0.00015337177,3.2527498e-7,0.0012795777,0.7422985,0.23641294,0.00047632735,0.0023047128,0.0064972895],"study_design_scores_gemma":[0.00039188427,0.00020992882,0.03541517,0.000058985494,0.000038212078,0.000012515059,0.00003265424,0.95537585,0.0021083981,0.00629263,0.0000108574495,0.000052942763],"about_ca_topic_score_codex":0.0000014329707,"about_ca_topic_score_gemma":0.0000010745257,"teacher_disagreement_score":0.23430455,"about_ca_system_score_codex":0.00005914316,"about_ca_system_score_gemma":0.000023164273,"threshold_uncertainty_score":0.17456003},"labels":[],"label_agreement":null},{"id":"W2314145075","doi":"10.2514/6.2010-3720","title":"Fan Trailing-Edge Noise Prediction Using RANS Simulations","year":2010,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":14,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Reynolds-averaged Navier–Stokes equations; Trailing edge; Noise (video); Computer science; Acoustics; Computational fluid dynamics; Aerospace engineering; Physics; Engineering; Artificial intelligence; Mechanics","score_opus":0.009794495154502467,"score_gpt":0.2225989884850488,"score_spread":0.21280449333054635,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2314145075","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6634686,0.0000052657942,0.33114126,0.000006505137,0.000907826,0.00006168894,0.000039613642,0.0002474751,0.0041217767],"genre_scores_gemma":[0.988088,0.000004344348,0.011455442,0.000011674564,0.00025230163,0.0000015364652,0.000019595564,0.000027006725,0.00014007968],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99955255,0.0000027373826,0.00013891303,0.000092745504,0.000074101554,0.00013893389],"domain_scores_gemma":[0.9997268,0.000029117495,0.000009072795,0.00015516486,0.00002692229,0.00005292398],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000050871513,0.00008612605,0.000070594215,0.000047474707,0.00007961378,0.000027880378,0.00006585196,0.00008600903,0.00025356375],"category_scores_gemma":[0.000012918991,0.00008657779,0.000033881883,0.000073799594,0.000019400912,0.00008293047,0.000009154137,0.00020981317,0.000014707634],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[5.1583373e-7,0.00000801906,0.00084138766,0.000009511308,0.000007716229,5.174865e-7,0.00006599494,0.72987795,0.26785904,0.000784369,0.00005124668,0.0004937268],"study_design_scores_gemma":[0.0001334397,0.000004036769,0.0013520764,0.000004092816,0.000016621945,0.0000024807632,0.000011117095,0.9964005,0.0011811157,0.0001637698,0.0006368586,0.00009391823],"about_ca_topic_score_codex":0.000006905295,"about_ca_topic_score_gemma":0.00012020388,"teacher_disagreement_score":0.32461944,"about_ca_system_score_codex":0.000013156686,"about_ca_system_score_gemma":0.000007631728,"threshold_uncertainty_score":0.353054},"labels":[],"label_agreement":null},{"id":"W2315119774","doi":"10.2514/6.2014-3292","title":"Experimental and numerical investigation on noise induced by a butterfly valve","year":2014,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Natural Sciences and Engineering Research Council of Canada; Consortium de Recherche et d’innovation en Aérospatiale au Québec; Compute Canada; Université de Sherbrooke","keywords":"Butterfly valve; Butterfly; Noise (video); Computer science; Acoustics; Physics; Engineering; Mechanical engineering; Artificial intelligence; Ecology; Biology","score_opus":0.010040558987526049,"score_gpt":0.20998704321564643,"score_spread":0.1999464842281204,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2315119774","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9477149,0.000021203625,0.04679133,0.00005504167,0.00015084841,0.00005324687,0.000002544036,0.00012180432,0.005089057],"genre_scores_gemma":[0.9983439,0.000001391672,0.001210955,0.00029814095,0.000057583453,0.00000840295,0.000008694569,0.0000189696,0.000051971474],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99961126,0.0000086786895,0.000086789965,0.000109021195,0.0000777755,0.00010650227],"domain_scores_gemma":[0.9997938,0.0000277552,0.000008798757,0.00009019737,0.000006080579,0.00007332568],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00004335352,0.000091259564,0.000076215074,0.00002005465,0.000029548253,0.00002645186,0.000043150532,0.000049032446,0.000024610525],"category_scores_gemma":[0.000011502938,0.00008425291,0.000018000135,0.00003576905,0.000015435153,0.00003885233,0.000016289758,0.000087791595,0.000023031176],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000025422546,0.000021842792,0.00022605524,0.0000096785025,0.000014071514,3.25389e-7,0.00018224481,0.0025416308,0.9880497,0.0030199285,0.0035341587,0.0023978068],"study_design_scores_gemma":[0.00025668493,0.00011359275,0.00093321357,0.000010114709,0.0000056137433,0.0000014172147,0.00003951355,0.89537656,0.10218009,0.0003807588,0.0005130285,0.00018938321],"about_ca_topic_score_codex":0.000009582546,"about_ca_topic_score_gemma":3.0914129e-7,"teacher_disagreement_score":0.89283496,"about_ca_system_score_codex":0.000025032128,"about_ca_system_score_gemma":0.0000018483772,"threshold_uncertainty_score":0.34357342},"labels":[],"label_agreement":null},{"id":"W2317473266","doi":"10.2514/6.2014-2324","title":"Direct numerical simulation of acoustic reduction using serrated trailing-edge on an isolated airfoil","year":2014,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":50,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Trailing edge; Airfoil; Reduction (mathematics); Acoustics; Computer science; Materials science; Mechanics; Physics; Mathematics; Geometry","score_opus":0.014642713527257661,"score_gpt":0.25074076832123926,"score_spread":0.2360980547939816,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2317473266","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.5177326,0.0000040861005,0.47935885,0.0000020090015,0.00035522218,0.00005743396,0.0000031286434,0.00020907496,0.0022775864],"genre_scores_gemma":[0.9975622,0.0000032348107,0.002160384,0.00000848192,0.00013982906,0.0000013411186,0.000022335935,0.000043785847,0.000058347836],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99923587,0.000035035744,0.00026066235,0.00017116219,0.00012601109,0.00017124906],"domain_scores_gemma":[0.99956053,0.00005837528,0.00004202382,0.00020129644,0.00007535333,0.0000624398],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00014548813,0.00014383314,0.00018877536,0.00008297737,0.000052943233,0.000017042783,0.00007371191,0.00011635485,0.000048715658],"category_scores_gemma":[0.000050317965,0.0001399432,0.000039287366,0.00022675104,0.000020783986,0.00009864045,0.000008183744,0.00013392727,0.0000064844635],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000014726571,0.000033955115,0.0000086287855,0.000027250373,0.000013828389,3.1067822e-7,0.00006358267,0.84542567,0.15224998,0.000055193046,0.000008892683,0.0020979873],"study_design_scores_gemma":[0.00017323761,0.00012754193,0.0001249428,0.000031865908,0.000031153482,0.0000020190455,0.000027518576,0.9961606,0.0030796381,0.000051051462,0.00002815433,0.00016222344],"about_ca_topic_score_codex":0.000016069313,"about_ca_topic_score_gemma":0.0000046892856,"teacher_disagreement_score":0.47982967,"about_ca_system_score_codex":0.0000465807,"about_ca_system_score_gemma":0.000009304721,"threshold_uncertainty_score":0.5706718},"labels":[],"label_agreement":null},{"id":"W2317722467","doi":"10.2514/6.2014-3187","title":"Active noise control simulation of tonal turbofan noise in aero engines","year":2014,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Deutsches Zentrum für Luft- und Raumfahrt; Compute Canada; National Aeronautics and Space Administration","keywords":"Turbofan; Noise (video); Active noise control; Computer science; Noise measurement; Noise control; Acoustics; Engineering; Automotive engineering; Noise reduction; Artificial intelligence; Physics","score_opus":0.004255897954336095,"score_gpt":0.20530053604248455,"score_spread":0.20104463808814846,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2317722467","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.69108295,0.000013572206,0.30166242,0.000019756655,0.0002042206,0.000114028204,0.000014625339,0.00007161278,0.006816831],"genre_scores_gemma":[0.9988005,0.00000456066,0.0009945441,0.00002499017,0.000083085426,0.000005887612,0.000007415729,0.000018549514,0.00006042407],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994641,0.000011152767,0.00019285621,0.00009424608,0.000099310666,0.00013832941],"domain_scores_gemma":[0.99958843,0.00018715774,0.000022664117,0.00012469613,0.000042656426,0.000034390323],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00009407738,0.00010270857,0.000165881,0.00007012192,0.000010897653,0.0000072305406,0.00007606965,0.00006543128,0.00005954135],"category_scores_gemma":[0.00006598894,0.00009642309,0.00003600451,0.00008709319,0.000016022086,0.00006627362,0.000010825036,0.00009850686,0.000007460416],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000011566042,0.000016334723,0.00059347047,0.00002138018,0.000010939425,4.6786118e-7,0.000060581686,0.9833609,0.011681931,0.0010065192,0.000018925832,0.0032170017],"study_design_scores_gemma":[0.0005243465,0.000017588349,0.013378607,0.000013632909,0.000008045816,2.0680002e-7,0.000013152864,0.9845694,0.0008653851,0.00036142705,0.00014081894,0.000107430824],"about_ca_topic_score_codex":0.000017266413,"about_ca_topic_score_gemma":0.000058847418,"teacher_disagreement_score":0.3077176,"about_ca_system_score_codex":0.000032386233,"about_ca_system_score_gemma":0.000004509398,"threshold_uncertainty_score":0.39320198},"labels":[],"label_agreement":null},{"id":"W2317853655","doi":"10.2514/6.2013-2065","title":"Parameterization and optimization of broadband noise for high-lift devices","year":2013,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":10,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Compute Canada","keywords":"Broadband; Computer science; Lift (data mining); Noise (video); Acoustics; Electronic engineering; Telecommunications; Engineering; Physics; Artificial intelligence","score_opus":0.005549817710578344,"score_gpt":0.19148156717633044,"score_spread":0.1859317494657521,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2317853655","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.33751202,0.000031321553,0.66190416,0.000014151338,0.000071659444,0.00014098904,0.000006765859,0.000035688405,0.00028325355],"genre_scores_gemma":[0.86630195,0.000062339655,0.13349271,0.00001487177,0.000018216251,0.00001956017,0.000025315781,0.000011880226,0.000053183434],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99972737,0.000002141879,0.000112036745,0.00005936361,0.000033877845,0.00006520588],"domain_scores_gemma":[0.9998203,0.000035530342,0.000018150995,0.000059167003,0.000046538138,0.000020327425],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00002558894,0.000053524385,0.000073529314,0.000025209558,0.000016615179,0.000023437395,0.000030166646,0.00003648429,0.000051968378],"category_scores_gemma":[0.000012924034,0.000048147933,0.000009271842,0.000037758964,0.0000119189735,0.00009472718,0.000007868838,0.000016046162,0.0000011516585],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[9.63658e-7,0.000004820103,0.00026341132,0.000093041264,0.00000933898,1.9311885e-8,0.00002122466,0.99037224,0.0055376394,0.001220052,0.00014677361,0.002330452],"study_design_scores_gemma":[0.0001389721,0.000018149165,0.00092578976,0.000009073834,0.0000095621635,3.0557246e-7,0.000013007708,0.9974354,0.0009151123,0.0004390702,0.000033793276,0.00006174695],"about_ca_topic_score_codex":0.000016717675,"about_ca_topic_score_gemma":0.000005450823,"teacher_disagreement_score":0.52878994,"about_ca_system_score_codex":0.0000047623066,"about_ca_system_score_gemma":0.0000018809537,"threshold_uncertainty_score":0.19634157},"labels":[],"label_agreement":null},{"id":"W2318077879","doi":"10.2514/6.2007-16","title":"Investigation of Noise Sources in Turbulent Hot Jets Using Large Eddy Simulation Data","year":2007,"lang":"en","type":"article","venue":"45th AIAA Aerospace Sciences Meeting and Exhibit","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":32,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"McGill University; Purdue Research Foundation; Florida State University; Purdue University","keywords":"Jet noise; Mach number; Physics; Mechanics; Noise (video); Jet (fluid); Large eddy simulation; Acoustics; Turbulence; Ambient noise level; Computational physics; Computer science","score_opus":0.04508071379175165,"score_gpt":0.2874911101347581,"score_spread":0.24241039634300643,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2318077879","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9805634,0.00048606965,0.018259618,0.000030548912,0.00018662756,0.00010480493,0.000011411062,0.000053463315,0.00030402397],"genre_scores_gemma":[0.98813146,0.000048514492,0.011681063,0.000024913626,0.00007784743,5.824445e-7,0.000012517243,0.000013388081,0.000009737495],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9987004,0.000022227747,0.00031429742,0.00030364285,0.00029803222,0.00036142103],"domain_scores_gemma":[0.99939346,0.00015835425,0.000098248885,0.00022849224,0.000039057915,0.000082408165],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0022137684,0.00013585258,0.00017427522,0.00014380777,0.00016781039,0.000065390865,0.00024500175,0.000075706455,0.0000032437017],"category_scores_gemma":[0.00015492062,0.00013059944,0.000017047447,0.0004712371,0.00016912892,0.00028069512,0.000121554454,0.00013299283,9.843151e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000040312807,0.000007044873,0.034912165,0.000058420545,0.0000031433974,0.0000020610305,0.0010547033,0.93692154,0.026637238,0.00007509135,0.000016974676,0.0003075977],"study_design_scores_gemma":[0.00018529767,0.000021412363,0.0060914694,0.00018960224,0.000009836799,0.0000020459183,0.0008112832,0.98951477,0.0028773504,0.00009898012,0.00004307534,0.00015487053],"about_ca_topic_score_codex":0.000097252654,"about_ca_topic_score_gemma":0.00024258069,"teacher_disagreement_score":0.05259325,"about_ca_system_score_codex":0.000035587454,"about_ca_system_score_gemma":0.000028992568,"threshold_uncertainty_score":0.53256905},"labels":[],"label_agreement":null},{"id":"W2318241481","doi":"10.2514/1.j055104","title":"Aeroacoustic Simulations of a Simplified High-Lift Device Accounting for Some Installation Effects","year":2016,"lang":"en","type":"article","venue":"AIAA Journal","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":27,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Mitacs; Compute Canada","keywords":"Anechoic chamber; Aeroacoustics; Acoustics; Directivity; Sound power; Wind tunnel; Mach number; Jet (fluid); Mechanics; Lift (data mining); Large eddy simulation; Detached eddy simulation; Sound pressure; Computational fluid dynamics; Physics; Engineering; Turbulence; Reynolds-averaged Navier–Stokes equations; Computer science","score_opus":0.00853358669935602,"score_gpt":0.22917031011286082,"score_spread":0.2206367234135048,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2318241481","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.59829205,0.000056074674,0.40081438,0.00005098983,0.000541537,0.00011528111,0.000030306835,0.000037254325,0.00006214868],"genre_scores_gemma":[0.99457496,0.000039235776,0.0048102816,0.000033357806,0.0004579751,0.0000049322284,0.0000047702883,0.000038260925,0.000036236346],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99918973,0.00001253502,0.00032775445,0.00009019519,0.00015239086,0.00022738692],"domain_scores_gemma":[0.99896014,0.000614954,0.00011342271,0.00011964457,0.00012986906,0.000061951796],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001859524,0.00011994306,0.00017120155,0.000104709616,0.00011753538,0.000037788413,0.00011891599,0.000066082364,0.000023640803],"category_scores_gemma":[0.00025469167,0.00009222408,0.000068277994,0.00008966845,0.000020197022,0.00026654784,0.000019600064,0.00011587343,0.0000048332386],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000014077769,0.000023885555,0.00045918088,0.00019933234,0.000095935546,0.0000036189913,0.00006555055,0.7473609,0.23007108,0.0032696363,0.00028678944,0.01815001],"study_design_scores_gemma":[0.0018185202,0.000095166775,0.0046910853,0.0003348855,0.00012371721,0.000025251466,0.00002197753,0.9659369,0.0041371603,0.021814387,0.00068866817,0.0003122911],"about_ca_topic_score_codex":0.0000015305137,"about_ca_topic_score_gemma":0.000006615567,"teacher_disagreement_score":0.3962829,"about_ca_system_score_codex":0.00007849726,"about_ca_system_score_gemma":0.000028004046,"threshold_uncertainty_score":0.37607887},"labels":[],"label_agreement":null},{"id":"W2318517974","doi":"10.2514/6.2004-520","title":"3D Computation of Noise Propagation from Ducted Fans Using a Spectral Element Method","year":2004,"lang":"en","type":"article","venue":"42nd AIAA Aerospace Sciences Meeting and Exhibit","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Computation; Noise (video); Acoustics; Computer science; Element (criminal law); Physics; Algorithm; Computer vision","score_opus":0.013898756462983648,"score_gpt":0.25955543102040163,"score_spread":0.245656674557418,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2318517974","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7005823,0.00014515838,0.2983539,0.00006270877,0.00019744298,0.000103305414,0.00000980117,0.00006403999,0.00048127727],"genre_scores_gemma":[0.7557177,0.000027550448,0.24415076,0.000009666753,0.000071488364,0.0000018322313,0.0000055270966,0.00001080677,0.000004684753],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989167,0.000026950202,0.0002581841,0.00026649318,0.0002766252,0.00025504036],"domain_scores_gemma":[0.99965656,0.00004735751,0.00009545948,0.00008701988,0.00005277595,0.000060833],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004946713,0.00014449864,0.00018493197,0.00007222699,0.00020303331,0.00008120129,0.000100738755,0.000052035477,0.0000044082494],"category_scores_gemma":[0.000044114637,0.00013428059,0.000032980064,0.00033302497,0.00012954649,0.00014280439,0.000036498466,0.00010720387,0.0000013414117],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000020554028,0.0000117787295,0.0005589549,0.000027724209,0.000008167068,9.776415e-7,0.00069585966,0.766895,0.23053609,0.00024427145,0.000004135085,0.0010150177],"study_design_scores_gemma":[0.0003208147,0.000059928192,0.0012008344,0.00021650826,0.00003001481,0.0000037068482,0.00063838466,0.96340775,0.032649618,0.0012783856,0.0000071359614,0.00018692929],"about_ca_topic_score_codex":0.00044015513,"about_ca_topic_score_gemma":0.00010106212,"teacher_disagreement_score":0.19788647,"about_ca_system_score_codex":0.00007055861,"about_ca_system_score_gemma":0.000044955214,"threshold_uncertainty_score":0.54758036},"labels":[],"label_agreement":null},{"id":"W2318579152","doi":"10.2514/6.2005-115","title":"The Rectangular Wall Jet - Part 1: The Effect of Varying Aspect Ratio","year":2005,"lang":"en","type":"article","venue":"43rd AIAA Aerospace Sciences Meeting and Exhibit","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Turbulence; Jet (fluid); Scaling; Vorticity; Aspect ratio (aeronautics); Reynolds number; Physics; Mechanics; Flow (mathematics); Reynolds stress; Geometry; Vortex; Root mean square; Mathematics","score_opus":0.006000082178650238,"score_gpt":0.213212610475161,"score_spread":0.20721252829651074,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2318579152","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9779267,0.0028287664,0.0005827635,0.0014167532,0.00056726247,0.00022395165,0.0000037185862,0.00012902023,0.016321111],"genre_scores_gemma":[0.9981508,0.0005298311,0.0007690548,0.000040530485,0.00024590865,0.000012468646,7.7181727e-7,0.000017178249,0.00023341879],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9987214,0.000085564534,0.00024148363,0.00023323273,0.00032845917,0.00038983702],"domain_scores_gemma":[0.99884105,0.0007414766,0.000076912256,0.00025591132,0.000027080721,0.00005759848],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0022737891,0.0001835209,0.00019351103,0.000028467784,0.0008648127,0.00019765762,0.00036057562,0.00005471451,0.000008150482],"category_scores_gemma":[0.00025063657,0.00009703841,0.000066690714,0.00029813653,0.00041448104,0.00011312429,0.00007695697,0.00021067103,0.00000776956],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000034414563,0.000019582134,0.0118170725,0.00017794773,0.000108662454,0.0000056208455,0.002770655,0.863468,0.07578784,0.004165954,0.008874279,0.032769985],"study_design_scores_gemma":[0.00037285077,0.0002778284,0.00042551494,0.00023123236,0.000060416365,0.00001595499,0.0003630102,0.9516039,0.031481437,0.00023491425,0.014568972,0.00036398967],"about_ca_topic_score_codex":0.00003660529,"about_ca_topic_score_gemma":0.00009991534,"teacher_disagreement_score":0.08813589,"about_ca_system_score_codex":0.000030032053,"about_ca_system_score_gemma":0.000017642913,"threshold_uncertainty_score":0.6651528},"labels":[],"label_agreement":null},{"id":"W2318972703","doi":"10.2514/6.2011-2783","title":"Effect of Trailing Edge Blowing Geometry on Broadband Noise Sources","year":2011,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Trailing edge; Broadband; Noise (video); Acoustics; Physics; Geometry; Materials science; Computer science; Optics; Mechanics; Mathematics","score_opus":0.008112717494730054,"score_gpt":0.20193489096914188,"score_spread":0.19382217347441183,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2318972703","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.94272983,0.0001050652,0.008103916,8.9747294e-7,0.0003354668,0.00007738256,0.000004124613,0.00013780456,0.048505522],"genre_scores_gemma":[0.99861276,0.000018568544,0.001105596,0.000008855441,0.00006742941,0.000003453267,0.0000017663705,0.000030211626,0.00015133801],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994288,0.000011886306,0.00016463464,0.00011237798,0.00010320875,0.00017909378],"domain_scores_gemma":[0.9996231,0.0001309879,0.000016853925,0.0001694906,0.000011733273,0.00004783306],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021726049,0.00013249637,0.00018408282,0.000094437746,0.000029363502,0.000008895176,0.00012301066,0.00006868343,0.00015855311],"category_scores_gemma":[0.000034371336,0.00010801752,0.00007451712,0.0001118503,0.00002345133,0.00003824932,0.00001908177,0.00013059002,0.00002127503],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00025038258,0.0003014007,0.021262787,0.0026450248,0.0006674004,0.000076819466,0.004120308,0.43462297,0.31250077,0.0063758297,0.001156145,0.21602014],"study_design_scores_gemma":[0.0010173924,0.0007065712,0.0034626275,0.00019896407,0.00011497751,0.0000054883676,0.0001033265,0.57501054,0.4183152,0.0001363439,0.000378012,0.0005505576],"about_ca_topic_score_codex":0.000012051996,"about_ca_topic_score_gemma":0.000003048888,"teacher_disagreement_score":0.21546958,"about_ca_system_score_codex":0.000010529909,"about_ca_system_score_gemma":0.0000026698087,"threshold_uncertainty_score":0.44048265},"labels":[],"label_agreement":null},{"id":"W2318973162","doi":"10.2514/6.2014-3232","title":"Generation and transmission of spiral acoustic waves in multi-stage subsonic radial compressors","year":2014,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":12,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Acoustics; Spiral (railway); Gas compressor; Acoustic wave; Physics; Aerospace engineering; Engineering; Mechanical engineering","score_opus":0.03025577411288738,"score_gpt":0.25100107025527923,"score_spread":0.22074529614239186,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2318973162","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6339086,0.00007749636,0.3655225,0.0000040412015,0.00008561582,0.00005466647,0.0000033908489,0.000027457982,0.00031617653],"genre_scores_gemma":[0.9899114,0.00010332107,0.009801683,0.000008290164,0.000039542352,0.0000022834702,0.000008167107,0.000015403082,0.00010996067],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995327,0.000013962051,0.0001731431,0.000096146236,0.00006533029,0.00011873733],"domain_scores_gemma":[0.9998256,0.000029733319,0.000013742535,0.0000828435,0.000010177279,0.000037899183],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000101179685,0.00008635878,0.00012818917,0.000053655654,0.000018105711,0.000010012899,0.00004962288,0.000062018225,0.000026081461],"category_scores_gemma":[0.000010578148,0.000078838995,0.000018424953,0.000047332782,0.000024708244,0.000046439014,0.000008864403,0.000083510175,7.738097e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000026029709,0.000016932421,0.0004943419,0.00007089119,0.000004121398,7.976399e-7,0.00014549276,0.7401758,0.25254995,0.00037144645,0.0000192581,0.0061484086],"study_design_scores_gemma":[0.0004726674,0.000022064027,0.0044595,0.0000152757,0.0000061745513,5.1863776e-7,0.00001590353,0.99082386,0.0039524315,0.000022899207,0.00011465607,0.00009403766],"about_ca_topic_score_codex":0.000032020525,"about_ca_topic_score_gemma":0.00020425115,"teacher_disagreement_score":0.3560027,"about_ca_system_score_codex":0.000014079291,"about_ca_system_score_gemma":0.000003714064,"threshold_uncertainty_score":0.32149607},"labels":[],"label_agreement":null},{"id":"W2320364923","doi":"10.2514/6.2014-3037","title":"Unstructured LES of the baseline EXEJET dual-stream jet","year":2014,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":20,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Office National d'études et de Recherches Aérospatiales","keywords":"Baseline (sea); Dual (grammatical number); Computer science; Geology; Art","score_opus":0.004123496684906399,"score_gpt":0.17774354344452206,"score_spread":0.17362004675961568,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2320364923","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.791816,0.00007507078,0.15200213,0.0001494798,0.0011557892,0.00013698431,0.000088318964,0.00023671084,0.054339524],"genre_scores_gemma":[0.99533355,0.000015866728,0.0041223876,0.000034617882,0.00010742306,0.0000014831585,0.0000063017555,0.000018179066,0.00036019195],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995487,0.000015264084,0.00014880045,0.00007468369,0.00009989828,0.00011265067],"domain_scores_gemma":[0.9995918,0.0000604384,0.00001994572,0.00027475355,0.000027237576,0.000025786889],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001174581,0.00009403703,0.0001091814,0.000017597942,0.000031423264,0.000008082606,0.00013096213,0.000055496857,0.00017639075],"category_scores_gemma":[0.000046841877,0.00005749768,0.00004906746,0.00007649974,0.000038029382,0.000016394784,0.000036438345,0.00009753543,0.0000045609736],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00000713406,0.00004599887,0.006315998,0.00028563628,0.000108746186,0.0000018334576,0.00019956724,0.71980804,0.091704234,0.05998827,0.01764837,0.103886195],"study_design_scores_gemma":[0.00017334908,0.000010404994,0.0033827915,0.00002075674,0.000017637592,0.0000031998745,0.000028810346,0.9790995,0.008917193,0.0018230474,0.0063992455,0.00012407837],"about_ca_topic_score_codex":0.000016430162,"about_ca_topic_score_gemma":0.00008703932,"teacher_disagreement_score":0.25929147,"about_ca_system_score_codex":0.00000964547,"about_ca_system_score_gemma":0.0000043316018,"threshold_uncertainty_score":0.23446874},"labels":[],"label_agreement":null},{"id":"W2320657140","doi":"10.2514/6.2012-2190","title":"Jet noise simulation with realistic nozzle geometries using fully unstructured LES solver","year":2012,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":24,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Natural Sciences and Engineering Research Council of Canada; Compute Canada","keywords":"Jet noise; Nozzle; Solver; Noise (video); Computer science; Jet (fluid); Acoustics; Aerospace engineering; Computational science; Physics; Mechanics; Engineering","score_opus":0.017570429628903154,"score_gpt":0.23466758794615813,"score_spread":0.21709715831725498,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2320657140","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.55061394,0.000058741505,0.44658324,0.0000040297614,0.00023694422,0.00006467134,0.000017001987,0.00012119296,0.0023002622],"genre_scores_gemma":[0.9792536,0.000006096771,0.020328548,0.000016207401,0.00021601625,0.0000016088864,0.000026269203,0.000041111118,0.00011052757],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99926114,0.000006843467,0.00017716407,0.00010291817,0.00017254059,0.00027938935],"domain_scores_gemma":[0.9995508,0.0000807692,0.00003152166,0.00019933496,0.00005972292,0.00007783361],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000108031614,0.00015908181,0.0001528129,0.00009120078,0.00008804036,0.00004589756,0.00007667655,0.000081071485,0.00019569113],"category_scores_gemma":[0.00004462169,0.00012032541,0.000029394854,0.00021015127,0.000038384947,0.00017258449,0.000021799971,0.0001100454,0.000009063758],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000060573398,0.000007031444,0.005493689,0.000029162888,0.000023608995,0.0000011259887,0.00007332265,0.98993444,0.0025065423,0.0009947192,0.00009399704,0.00083632383],"study_design_scores_gemma":[0.00016126354,0.0000113343785,0.005886261,0.0000121336925,0.000039509916,0.000005233799,0.000057095804,0.9925737,0.00031417713,0.00014523996,0.0005892564,0.00020482067],"about_ca_topic_score_codex":0.000048822974,"about_ca_topic_score_gemma":0.000050944655,"teacher_disagreement_score":0.4286397,"about_ca_system_score_codex":0.0000663078,"about_ca_system_score_gemma":0.000008613478,"threshold_uncertainty_score":0.49067277},"labels":[],"label_agreement":null},{"id":"W2321122223","doi":"10.2514/6.2013-2042","title":"Compressor Stage Broadband Noise Prediction using a Large-Eddy Simulation and Comparisons with a Cascade Response Model","year":2013,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":20,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Cascade; Broadband; Stage (stratigraphy); Noise (video); Gas compressor; Computer science; Large eddy simulation; Electronic engineering; Physics; Engineering; Aerospace engineering; Mechanics; Telecommunications; Turbulence; Geology; Artificial intelligence","score_opus":0.019159034457097494,"score_gpt":0.2484153453138243,"score_spread":0.22925631085672682,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2321122223","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.51759326,0.000028667795,0.48188004,0.0000071383733,0.000026157915,0.00016530252,0.00004716026,0.000112616726,0.0001396526],"genre_scores_gemma":[0.97195756,0.000008556753,0.027601058,0.000021891747,0.000024297948,0.000012923702,0.000011900025,0.000034618843,0.00032718797],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99930435,0.000020792626,0.00017083464,0.00015682551,0.00013183361,0.00021536135],"domain_scores_gemma":[0.9995812,0.00008419159,0.000026905687,0.00016527264,0.000055818982,0.00008658457],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00011023813,0.00014426962,0.00014656638,0.00006731203,0.000120571895,0.00008085201,0.000050097955,0.00007673725,0.000036513866],"category_scores_gemma":[0.0000126175455,0.00012431554,0.000016494945,0.00007963822,0.000029031224,0.00022037793,0.000030019168,0.000143324,0.0000038709186],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000059763155,0.000021427888,0.0009584304,0.00003445653,0.000021637525,0.0000013654758,0.00025076294,0.98758936,0.010788498,0.000044872377,0.00018451549,0.00004488796],"study_design_scores_gemma":[0.0005883703,0.00003085774,0.0030196167,0.000025120084,0.000025766734,0.0000044434514,0.00014496596,0.9957641,0.00008218991,0.000027016606,0.00013290696,0.00015467661],"about_ca_topic_score_codex":0.000051045292,"about_ca_topic_score_gemma":0.00003924013,"teacher_disagreement_score":0.4543643,"about_ca_system_score_codex":0.000050436527,"about_ca_system_score_gemma":0.000012894939,"threshold_uncertainty_score":0.5069441},"labels":[],"label_agreement":null},{"id":"W2321297293","doi":"10.2514/6.2005-2926","title":"Spectral-Element/Kirchhoff Method for Fan-Tone Directivity Calculations","year":2005,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Pratt and Whitney Canada","keywords":"Directivity; Acoustics; Tone (literature); Physics; Computer science; Telecommunications","score_opus":0.011545437860631823,"score_gpt":0.2972435934357986,"score_spread":0.28569815557516676,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2321297293","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.017956367,0.000040825842,0.9520538,0.000240052,0.00023963224,0.00023967585,0.000049237304,0.00033451593,0.028845923],"genre_scores_gemma":[0.5860722,0.00001448465,0.41190138,0.000046998248,0.00026396487,0.000036790836,0.00001723534,0.000028540895,0.0016183784],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99931556,0.0000096564645,0.0001716499,0.00015328768,0.00009167887,0.00025817184],"domain_scores_gemma":[0.9995832,0.00012487528,0.000014388869,0.00018355662,0.000032026874,0.000061988285],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020135846,0.00012428802,0.00013913523,0.00004783617,0.00008114156,0.00002661139,0.00008944668,0.00005575684,0.00022745415],"category_scores_gemma":[0.000028103714,0.00012212619,0.00007990026,0.000098508855,0.000010913332,0.00008211443,0.000018473916,0.0000971513,0.000025040563],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000035432302,0.00006514822,0.00013914786,0.00003778989,0.000089027744,8.091164e-7,0.0000928073,0.84917897,0.027265713,0.034407433,0.008226179,0.080493465],"study_design_scores_gemma":[0.0002032233,0.000014929643,0.00079841446,0.000003396544,0.00002347196,0.0000015891285,0.000012318733,0.97066355,0.0050873887,0.0012153015,0.021806357,0.00017003443],"about_ca_topic_score_codex":0.000021889826,"about_ca_topic_score_gemma":0.00038568603,"teacher_disagreement_score":0.56811583,"about_ca_system_score_codex":0.00009956352,"about_ca_system_score_gemma":0.000008122723,"threshold_uncertainty_score":0.49801615},"labels":[],"label_agreement":null},{"id":"W2322297067","doi":"10.2514/6.2012-1624","title":"Initial Assessment of a CFD Application for Predicting Jet Fighter Aircraft Cavity Bay Acoustics for Subsonic and Supersonic Aircraft States","year":2012,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lockheed Martin (Canada)","funders":"Chinese Academy of Agricultural Sciences","keywords":"Supersonic speed; Jet (fluid); Computational fluid dynamics; Jet engine; Aerospace engineering; Aeronautics; Acoustics; Sonic boom; Marine engineering; Engineering; Physics","score_opus":0.011156498928723948,"score_gpt":0.2741991444718823,"score_spread":0.26304264554315837,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2322297067","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.41774783,0.000078011064,0.58086485,0.00002318203,0.00020455959,0.0005535429,0.00028704034,0.00008140933,0.00015958337],"genre_scores_gemma":[0.94223285,0.000065452674,0.056875218,0.000026864116,0.0002644712,0.00028485616,0.0001615151,0.00005020148,0.000038601513],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989748,0.000009520656,0.00031298096,0.00017374831,0.00012772433,0.00040123027],"domain_scores_gemma":[0.9991992,0.0003581013,0.000051619954,0.0001860254,0.00010562091,0.00009942584],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00036411846,0.00018536144,0.00024212373,0.000053554955,0.000089885965,0.000023335218,0.000100126,0.00012055017,0.00001678865],"category_scores_gemma":[0.000041023734,0.00017177366,0.000069258196,0.0000638094,0.000040056653,0.00015702854,0.000038054473,0.00012070661,7.2031594e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0001686078,0.0011074491,0.2964149,0.00964956,0.0012228511,0.0000019291092,0.0043709315,0.41113472,0.20889817,0.02538244,0.0063905115,0.035257906],"study_design_scores_gemma":[0.00056632597,0.0000893989,0.008185949,0.000022618073,0.000109431356,0.0000020747282,0.00020148026,0.9885544,0.001103204,0.00042083595,0.00053957145,0.00020470885],"about_ca_topic_score_codex":0.000013574208,"about_ca_topic_score_gemma":0.00004444483,"teacher_disagreement_score":0.5774197,"about_ca_system_score_codex":0.000089854315,"about_ca_system_score_gemma":0.00003179165,"threshold_uncertainty_score":0.70047265},"labels":[],"label_agreement":null},{"id":"W2322925327","doi":"10.2514/6.2010-3778","title":"Experimental Methodology for Aeroacoustic Source Localisation in Ducted Flows with Complex Geometry","year":2010,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Victoria","funders":"Irish Research Council","keywords":"Geometry; Acoustics; Complex geometry; Computer science; Physics; Mathematics","score_opus":0.03224651436255272,"score_gpt":0.2688778560683168,"score_spread":0.2366313417057641,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2322925327","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.503356,0.000009730343,0.49570417,0.000012005938,0.00024682595,0.00015667044,0.0000061852925,0.00010497934,0.00040347228],"genre_scores_gemma":[0.7739581,0.0000011330824,0.2256942,0.000042025174,0.00009646608,0.000046732188,0.000042277716,0.000037298996,0.00008175923],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99925745,0.000017558685,0.00019639613,0.00018170972,0.000088836176,0.00025804932],"domain_scores_gemma":[0.9994808,0.00022535303,0.000020444586,0.00018377468,0.00003483733,0.00005479023],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00022201263,0.00014909211,0.00019327816,0.00012520875,0.000041787807,0.00002209398,0.000120555225,0.00011639438,0.00021128479],"category_scores_gemma":[0.00006290984,0.00013185121,0.000028442617,0.000172994,0.000047526228,0.000054295455,0.000021436383,0.00021594382,0.0000060968755],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000022513615,0.0000391141,0.00019995357,0.00003077057,0.000018633968,0.0000019711053,0.00014350771,0.3655378,0.63048685,0.0013490889,0.00021204245,0.0019577972],"study_design_scores_gemma":[0.0006270162,0.000059214333,0.0008383698,0.00000453527,0.000011372626,0.000012997805,0.0003286814,0.9874192,0.00974961,0.0001916223,0.00055668777,0.00020070659],"about_ca_topic_score_codex":0.000036686215,"about_ca_topic_score_gemma":0.00042142178,"teacher_disagreement_score":0.6218814,"about_ca_system_score_codex":0.000043623844,"about_ca_system_score_gemma":0.000010999226,"threshold_uncertainty_score":0.53767365},"labels":[],"label_agreement":null},{"id":"W2323182861","doi":"10.2514/6.2013-2262","title":"Phased Microphone Array Measurements of a Bombardier Aircraft Scaled Model","year":2013,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"National Research Council Canada","funders":"","keywords":"Phased array; Microphone array; Phased-array optics; Computer science; Acoustics; Microphone; Aerospace engineering; Engineering; Electrical engineering; Physics; Loudspeaker","score_opus":0.014473859830339587,"score_gpt":0.20543383044300798,"score_spread":0.1909599706126684,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2323182861","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.3100305,0.0000776489,0.66121954,0.00002375771,0.0001991873,0.00018434707,0.000009404551,0.000120474535,0.028135115],"genre_scores_gemma":[0.90755266,0.000011382492,0.091564186,0.000036200894,0.000029123146,0.000020001104,0.000003849131,0.000032400727,0.00075019797],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99924517,0.0000056520093,0.00023467289,0.000120430144,0.00017969709,0.00021437189],"domain_scores_gemma":[0.9995581,0.000010364073,0.000020759433,0.00023852706,0.0001005075,0.000071751434],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000080602724,0.00013513962,0.00018648517,0.000046703295,0.000022913126,0.000015763377,0.00013925275,0.000064341984,0.00031547144],"category_scores_gemma":[0.000010569076,0.00012170925,0.00006677246,0.00008440969,0.000028053486,0.00006930795,0.000011855868,0.00008883317,0.00010183407],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000001359194,0.000028695256,0.000104314226,0.000028241655,0.00003861004,1.6476218e-7,0.000032231645,0.16609587,0.8307779,0.000009191274,0.0024272655,0.00045618095],"study_design_scores_gemma":[0.0005104101,0.000012645479,0.00010482706,0.000018541934,0.000019273823,9.615031e-7,0.000014241932,0.74245673,0.25606447,0.0005433445,0.000068698006,0.00018582669],"about_ca_topic_score_codex":0.000024394278,"about_ca_topic_score_gemma":0.0000073204374,"teacher_disagreement_score":0.59752214,"about_ca_system_score_codex":0.000036782476,"about_ca_system_score_gemma":0.0000116604115,"threshold_uncertainty_score":0.49631593},"labels":[],"label_agreement":null},{"id":"W2323294298","doi":"10.2514/6.2007-442","title":"A Spatio-Temporal Decomposition of the Acoustic Source in a Mach 0.85 Jet","year":2007,"lang":"en","type":"article","venue":"45th AIAA Aerospace Sciences Meeting and Exhibit","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Air Force Office of Scientific Research; Natural Sciences and Engineering Research Council of Canada; National Science Foundation","keywords":"Jet (fluid); Mach number; Decomposition; Computer science; Acoustics; Physics; Mechanics","score_opus":0.007157297484147157,"score_gpt":0.2368322468009299,"score_spread":0.22967494931678276,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2323294298","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98150826,0.00021937063,0.014823622,0.00013354218,0.00030697446,0.00012426508,0.000004337254,0.00005662988,0.0028230164],"genre_scores_gemma":[0.9964659,0.00002607219,0.0033301513,0.000040847703,0.000052309617,0.0000027153512,0.0000022865088,0.00001358108,0.00006611157],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9988588,0.00002430065,0.00026850984,0.00021260505,0.00027869342,0.00035708552],"domain_scores_gemma":[0.99957335,0.00011834355,0.00007794829,0.00014621415,0.000029911616,0.00005423295],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0012126984,0.0001395054,0.00017150107,0.00009072508,0.00019156607,0.000054236007,0.00021426541,0.00007029015,0.000005227529],"category_scores_gemma":[0.00006593608,0.00010562801,0.00004155951,0.0004650232,0.00030006224,0.000083250634,0.0000768065,0.00018164376,0.0000018132803],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00001308337,0.000033100434,0.1961673,0.00014447675,0.000007646461,0.0000040755026,0.0016696554,0.76312417,0.03657532,0.0003025067,0.00018122623,0.0017774438],"study_design_scores_gemma":[0.0003487582,0.00007030795,0.021936333,0.00033525162,0.000018224247,0.000015095984,0.0013547809,0.9695325,0.0055742366,0.00029983447,0.00023722868,0.00027745345],"about_ca_topic_score_codex":0.00020344419,"about_ca_topic_score_gemma":0.001990719,"teacher_disagreement_score":0.20640834,"about_ca_system_score_codex":0.00004385819,"about_ca_system_score_gemma":0.000025578423,"threshold_uncertainty_score":0.43073854},"labels":[],"label_agreement":null},{"id":"W2324273917","doi":"10.2514/6.2011-2878","title":"Rotor-shielding effect on fan-OGV broadband noise prediction","year":2011,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Electromagnetic shielding; Broadband; Rotor (electric); Acoustics; Noise (video); Computer science; Electrical engineering; Physics; Engineering; Telecommunications; Artificial intelligence","score_opus":0.010018399085027534,"score_gpt":0.1896177522508378,"score_spread":0.17959935316581027,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2324273917","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.75233144,0.000028267339,0.053725563,0.0000033406748,0.0011125404,0.00023023706,0.00001042588,0.0005436049,0.19201459],"genre_scores_gemma":[0.9983011,0.000021700322,0.00097057933,0.000024449202,0.00016579953,0.00002594548,0.0000058705446,0.000033566834,0.00045098024],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994178,0.000010088352,0.00013210664,0.0001399001,0.00010881201,0.00019132753],"domain_scores_gemma":[0.9996716,0.00004447824,0.000012147973,0.0001965277,0.000012469692,0.00006278665],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000118029675,0.00013792659,0.00011375733,0.00005582913,0.000050645165,0.000020295063,0.000097320364,0.000092628885,0.00026369563],"category_scores_gemma":[0.000020860714,0.00011815268,0.000047368594,0.00007089194,0.00001337759,0.000067940586,0.000017822096,0.0001680821,0.00009700192],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00038244022,0.00047871252,0.050944738,0.0011597153,0.000747833,0.0001703031,0.003265449,0.28116634,0.4076769,0.029802341,0.030811384,0.19339383],"study_design_scores_gemma":[0.00093779713,0.0007873558,0.024388362,0.00012912769,0.00006878986,0.0000102402555,0.000044663648,0.91507524,0.055388696,0.0007009574,0.0018894667,0.0005793084],"about_ca_topic_score_codex":0.000015358253,"about_ca_topic_score_gemma":0.0000068821428,"teacher_disagreement_score":0.63390887,"about_ca_system_score_codex":0.000043246186,"about_ca_system_score_gemma":0.0000027774379,"threshold_uncertainty_score":0.48181266},"labels":[],"label_agreement":null},{"id":"W2324398977","doi":"10.2514/6.2007-1282","title":"Throttling a Laval Nozzle by a Vortex: An Analytical Theory","year":2007,"lang":"en","type":"article","venue":"45th AIAA Aerospace Sciences Meeting and Exhibit","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Bandwidth throttling; Nozzle; Vortex; Aerospace engineering; Physics; Mechanics; Computer science; Engineering","score_opus":0.010128225660567144,"score_gpt":0.25412338106343013,"score_spread":0.24399515540286298,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2324398977","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9537925,0.00069624267,0.02711878,0.00013076876,0.00040979384,0.00010389283,0.000009970441,0.00029862433,0.017439386],"genre_scores_gemma":[0.9931743,0.00010741366,0.0060262484,0.00009989805,0.0001869577,0.000002653189,0.000004009315,0.000029416426,0.00036906757],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9982154,0.000033130604,0.00027036664,0.00042469896,0.00036940427,0.00068702374],"domain_scores_gemma":[0.99926496,0.00017891946,0.000046829035,0.00020380707,0.000039375995,0.0002661245],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0028820413,0.00022327216,0.00023407211,0.00008329877,0.0004483441,0.00021527498,0.0002664412,0.00011363941,0.000019039411],"category_scores_gemma":[0.00014687693,0.00017712869,0.00004997694,0.0003923789,0.00043255946,0.00021680303,0.000071538976,0.00026666455,0.000010340806],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00016704868,0.000535223,0.08235157,0.0005499134,0.00025232477,0.00018111835,0.014049564,0.34171265,0.36471614,0.1040563,0.012507984,0.078920156],"study_design_scores_gemma":[0.0003994374,0.00022184342,0.0012562823,0.00013970546,0.00004947257,0.000029960966,0.0035562157,0.98561996,0.0035073913,0.0026285334,0.0018753355,0.000715869],"about_ca_topic_score_codex":0.0000498308,"about_ca_topic_score_gemma":0.00012721469,"teacher_disagreement_score":0.6439073,"about_ca_system_score_codex":0.000036703997,"about_ca_system_score_gemma":0.000029232222,"threshold_uncertainty_score":0.7223098},"labels":[],"label_agreement":null},{"id":"W2325562064","doi":"10.2514/6.2007-3568","title":"CFD Simulation of the Aeroacoustic Noise Generated by A Generic Side View Car Mirror","year":2007,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":13,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Ansys (Canada)","funders":"","keywords":"Computational fluid dynamics; Noise (video); Acoustics; Computer science; Aeroacoustics; Aerospace engineering; Engineering; Physics; Artificial intelligence; Sound pressure","score_opus":0.0106978842357731,"score_gpt":0.2236727970538821,"score_spread":0.21297491281810899,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2325562064","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6798472,0.0003752144,0.31666857,0.00001252388,0.00039949603,0.00016055471,0.00002119978,0.0001017307,0.002413548],"genre_scores_gemma":[0.99634063,0.000048058802,0.002980968,0.00008405573,0.00004230181,0.0000034339005,0.000013851419,0.000036116602,0.00045060934],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99917907,0.00001201184,0.00029693855,0.00012255833,0.00016723266,0.00022219983],"domain_scores_gemma":[0.99949455,0.00007541921,0.000040777028,0.00026623753,0.000070202615,0.000052818552],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016631662,0.00013963884,0.00014940379,0.000033652464,0.000050445808,0.0000123520595,0.00015864542,0.00008534629,0.000054253167],"category_scores_gemma":[0.000033181248,0.00010325204,0.000060730254,0.00028660745,0.00003077815,0.000034368113,0.000030704003,0.000111741814,0.000010152048],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000015742241,0.000011467273,0.0000615094,0.000033080112,0.000015561523,9.847317e-7,0.000027055252,0.730329,0.26778907,0.000041171163,0.0004058918,0.0012836664],"study_design_scores_gemma":[0.00013432797,0.000008809827,0.00085861917,0.000013738689,0.000034333618,0.0000012370914,0.000020184383,0.9882706,0.009526135,0.00003458699,0.0009626359,0.00013482267],"about_ca_topic_score_codex":0.00003730411,"about_ca_topic_score_gemma":0.000089616115,"teacher_disagreement_score":0.31649342,"about_ca_system_score_codex":0.000060951916,"about_ca_system_score_gemma":0.000012311759,"threshold_uncertainty_score":0.4210496},"labels":[],"label_agreement":null},{"id":"W2326305194","doi":"10.2514/6.2000-2351","title":"The linearity of fluctuating velocity measurements in linearized stability experiments","year":2000,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Calgary","funders":"","keywords":"Linearity; Stability (learning theory); Physics; Control theory (sociology); Computer science; Artificial intelligence; Quantum mechanics","score_opus":0.03383521032209546,"score_gpt":0.24991647893651325,"score_spread":0.2160812686144178,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2326305194","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98489654,0.000091451526,0.0026749861,0.000011474846,0.00016355052,0.0001540844,0.000004615157,0.000061800936,0.011941505],"genre_scores_gemma":[0.9946104,0.000045355686,0.005196255,0.000008856684,0.00002520399,0.000010478772,0.0000025826985,0.000012842518,0.00008800476],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99909973,0.00003108668,0.000343287,0.0001131954,0.00021390947,0.00019876135],"domain_scores_gemma":[0.999578,0.00007967112,0.000019319094,0.00024678843,0.000043601878,0.0000326433],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000563092,0.000100285346,0.00014112938,0.000015026133,0.00006395509,0.000019715599,0.00016604002,0.000052888132,0.00033271097],"category_scores_gemma":[0.00008602832,0.00007612599,0.000037013226,0.00012622811,0.00004668752,0.00004457239,0.000024376424,0.0001556611,0.0000086458795],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0001953262,0.00063008146,0.04086394,0.0002595185,0.0002279109,0.0000034824113,0.0033388608,0.43652356,0.25664106,0.00043163617,0.0003808695,0.26050377],"study_design_scores_gemma":[0.00042077797,0.000012368422,0.0057828827,0.000013503539,0.000003875995,1.9000461e-7,0.00008096506,0.97207355,0.02108476,0.00023501473,0.00018075504,0.00011133293],"about_ca_topic_score_codex":0.000091731636,"about_ca_topic_score_gemma":0.00015656369,"teacher_disagreement_score":0.53555,"about_ca_system_score_codex":0.00007264759,"about_ca_system_score_gemma":0.000015165277,"threshold_uncertainty_score":0.36429518},"labels":[],"label_agreement":null},{"id":"W2326340338","doi":"10.3154/jvs.27.supplement2_67","title":"Acoustic Characteristics of Supersonic Jet from Laval Nozzle with Duct","year":2007,"lang":"en","type":"article","venue":"Journal of the Visualization Society of Japan","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Nozzle; Duct (anatomy); Acoustics; Schlieren; Supersonic speed; Jet noise; Sound pressure; Jet (fluid); Shock wave; Schlieren imaging; Materials science; Physics; Optics; Mechanics","score_opus":0.007533884763061709,"score_gpt":0.23146321051389346,"score_spread":0.22392932575083174,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2326340338","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.84600586,0.00008721379,0.15333496,0.000031519387,0.00039285983,0.000049176117,0.000033964785,0.00001054076,0.00005390558],"genre_scores_gemma":[0.99601614,0.0002491479,0.0033993302,0.00003767947,0.00022126074,1.8453427e-7,0.0000061720775,0.000028731489,0.000041364026],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989328,0.00001599318,0.00051533,0.000058592173,0.00034534538,0.00013194224],"domain_scores_gemma":[0.9990555,0.00009794769,0.00039025725,0.00014941156,0.00026016554,0.000046728273],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00039752896,0.000112518115,0.00027363235,0.000032989392,0.000045097695,0.0000125985935,0.00022250306,0.00008242209,0.000029030747],"category_scores_gemma":[0.000043959524,0.000077583645,0.00018474973,0.0002106753,0.00008959227,0.00008047185,0.000025959163,0.00017359988,4.6567044e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000110042834,0.00024857302,0.10159184,0.0005541657,0.0010940959,0.0000025351844,0.011012061,0.108079955,0.76864123,0.00068408414,0.006574367,0.0014070502],"study_design_scores_gemma":[0.002597836,0.00053488574,0.17760457,0.0010598791,0.0008763765,0.000062452025,0.0064130663,0.7369849,0.07159772,0.0005416256,0.0010943407,0.0006323673],"about_ca_topic_score_codex":0.0000094366005,"about_ca_topic_score_gemma":0.000011101062,"teacher_disagreement_score":0.69704354,"about_ca_system_score_codex":0.00006151679,"about_ca_system_score_gemma":0.000047854457,"threshold_uncertainty_score":0.31637692},"labels":[],"label_agreement":null},{"id":"W2327208743","doi":"10.2514/6.2013-2143","title":"Prediction of the Sound radiated from Low-Mach Internal Mixing Nozzles with Forced Mixers using the Lattice Boltzmann Method","year":2013,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":11,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"Compute Canada; Pratt and Whitney Canada","keywords":"Mach number; Nozzle; Lattice Boltzmann methods; Mixing (physics); Acoustics; Physics; Sound (geography); Mechanics; Computer science; Thermodynamics","score_opus":0.012881125814266873,"score_gpt":0.21865618383403726,"score_spread":0.2057750580197704,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2327208743","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.5459207,0.000030840172,0.45258904,0.000022418639,0.0002658421,0.00014249323,0.00001942457,0.000051114905,0.0009580828],"genre_scores_gemma":[0.968532,0.000009240302,0.031168628,0.00004116878,0.00010199896,0.000008220338,0.0000068449576,0.000034406105,0.00009746062],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992459,0.000042000025,0.00022283763,0.00013060414,0.00017660603,0.0001820565],"domain_scores_gemma":[0.99936306,0.00019215205,0.00006260944,0.00028134565,0.00006559828,0.000035222918],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001494702,0.00014096308,0.00013928382,0.000028973855,0.00010382205,0.0000643577,0.00025857473,0.0000645138,0.000086066786],"category_scores_gemma":[0.000026451484,0.00007560422,0.00005827925,0.00013245063,0.000059312337,0.0001220428,0.00005607309,0.00021492832,0.0000034908203],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000009639866,0.000013189124,0.0028274127,0.000036702386,0.00024116198,7.147646e-7,0.000656313,0.92003924,0.07454205,0.0003091553,0.00024301217,0.0010813958],"study_design_scores_gemma":[0.00023121243,0.000010683189,0.004909502,0.00006917318,0.00008317528,0.000004092363,0.00048106103,0.9899479,0.0034872743,0.0006552748,0.000028222184,0.000092406925],"about_ca_topic_score_codex":0.0009818015,"about_ca_topic_score_gemma":0.000117254975,"teacher_disagreement_score":0.4226113,"about_ca_system_score_codex":0.000055459106,"about_ca_system_score_gemma":0.000011880069,"threshold_uncertainty_score":0.30830505},"labels":[],"label_agreement":null},{"id":"W2328550806","doi":"10.2514/6.2013-2233","title":"On the sources of jet noise: a numerical study using band-pass Filtering","year":2013,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"Compute Canada; Pratt and Whitney Canada","keywords":"Jet noise; Noise (video); Acoustics; Jet (fluid); Computer science; Band-pass filter; Physics; Electronic engineering; Engineering; Mechanics; Optics; Artificial intelligence","score_opus":0.013751188607409648,"score_gpt":0.2212160989173894,"score_spread":0.20746491030997974,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2328550806","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9601946,0.000010715134,0.03581439,0.000026525211,0.00014484671,0.0002080488,0.0000025737143,0.00006901926,0.003529312],"genre_scores_gemma":[0.9987556,0.0000017166092,0.0010683159,0.00002699046,0.000045761026,0.000013870378,3.8829944e-7,0.000023212222,0.00006415146],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994308,0.000014733578,0.00016605487,0.000094679475,0.00013792129,0.00015580995],"domain_scores_gemma":[0.999581,0.00012702565,0.000020784464,0.00021570687,0.000023756205,0.00003174963],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000085140564,0.000110982415,0.00013523138,0.000028576613,0.000051114934,0.000038206104,0.00016112358,0.000028680766,0.00048405782],"category_scores_gemma":[0.000023520943,0.0000685749,0.00003731323,0.00009158918,0.000019223511,0.000040027888,0.000040129147,0.00011782257,0.000027264225],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000004000411,0.00015658994,0.004252991,0.000037431033,0.000114414164,0.0000049278556,0.0008596462,0.9342529,0.057077512,0.0013388346,0.0010234928,0.0008772629],"study_design_scores_gemma":[0.00010914824,0.00005312282,0.003787925,0.000015352132,0.000012885385,0.0000016123781,0.0005052049,0.99372214,0.0013970361,0.000259048,0.000026008212,0.00011053063],"about_ca_topic_score_codex":0.00010132828,"about_ca_topic_score_gemma":0.000003560573,"teacher_disagreement_score":0.05946923,"about_ca_system_score_codex":0.000020646146,"about_ca_system_score_gemma":0.000003556046,"threshold_uncertainty_score":0.5300094},"labels":[],"label_agreement":null},{"id":"W2328655276","doi":"10.2514/6.2014-2756","title":"Dual-stream jet noise simulations with realistic nozzle geometries using a fully unstructured LES solver","year":2014,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":10,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Mach number; Aerodynamics; Jet (fluid); Nozzle; Physics; Mechanics; Coaxial; Transonic; Jet noise; Solver; Wind tunnel; Acoustics; Computer science; Mechanical engineering; Engineering","score_opus":0.009699734768049062,"score_gpt":0.21163541550071563,"score_spread":0.20193568073266657,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2328655276","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.57324016,0.000015715303,0.4221462,0.000016788847,0.00015690461,0.00008576074,0.00007525656,0.00019172169,0.004071464],"genre_scores_gemma":[0.9724939,0.0000048758525,0.026993196,0.00002514809,0.00015422428,0.0000022594782,0.00006056995,0.000051553925,0.00021425779],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991038,0.000011440856,0.00023771253,0.00018893529,0.00019607725,0.00026207697],"domain_scores_gemma":[0.9993018,0.00015269172,0.000039989438,0.00032912925,0.00009515462,0.000081229686],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000087446155,0.00021036982,0.00022039458,0.00013410159,0.00014928907,0.00008911429,0.00010026909,0.00009316278,0.00021443343],"category_scores_gemma":[0.000100118734,0.00016270808,0.00004149153,0.00029978188,0.00007063364,0.00008898858,0.00003161874,0.00014409509,0.000007605425],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000004869369,0.000008809557,0.0015181177,0.000031145028,0.000035466743,0.0000032020905,0.000046603935,0.99053276,0.0038464712,0.002846058,0.00024868644,0.000877809],"study_design_scores_gemma":[0.00027788864,0.00002869309,0.0018274084,0.000020901825,0.00005523154,0.0000108514505,0.000039449278,0.9954164,0.00029061126,0.00087331823,0.00090492476,0.00025433974],"about_ca_topic_score_codex":0.00012038444,"about_ca_topic_score_gemma":0.000540562,"teacher_disagreement_score":0.39925373,"about_ca_system_score_codex":0.000054077344,"about_ca_system_score_gemma":0.000017228205,"threshold_uncertainty_score":0.66350424},"labels":[],"label_agreement":null},{"id":"W2329260350","doi":"10.2514/6.2008-18","title":"Unsteady Optimization Using a Discrete Adjoint Approach Applied to Aeroacoustic Shape Design","year":2008,"lang":"en","type":"article","venue":"46th AIAA Aerospace Sciences Meeting and Exhibit","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":19,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto","funders":"","keywords":"Computer science; Multidisciplinary design optimization; Adjoint equation; Shape optimization; Acoustics; Mathematical optimization; Engineering; Mathematics; Physics; Structural engineering; Finite element method; Mathematical analysis","score_opus":0.03475245695438595,"score_gpt":0.22828653148899775,"score_spread":0.1935340745346118,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2329260350","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.26606116,0.0001704903,0.72717035,0.00003426412,0.00022189069,0.0003339386,0.0000054883276,0.00024081027,0.005761602],"genre_scores_gemma":[0.68473583,0.00007590762,0.3149357,0.000053883654,0.000093008086,0.000017304714,0.000003706297,0.0000335016,0.000051150604],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9980512,0.000037695107,0.00030581455,0.00055942003,0.00042176037,0.00062406174],"domain_scores_gemma":[0.9993148,0.0000949363,0.00006967657,0.00022327878,0.00005125881,0.00024607155],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.000785165,0.00030478553,0.00030977858,0.00015146265,0.00082238467,0.00016098318,0.0002668844,0.00010679676,0.000010799492],"category_scores_gemma":[0.00009433215,0.00028120057,0.00004394692,0.0007211948,0.0002847356,0.00015861305,0.00011723993,0.00020495278,0.000007958017],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000006434212,0.000012026676,0.00019665598,0.000039427796,0.000008289436,0.000003126936,0.0007671356,0.9892212,0.009222769,0.00010784381,0.00015570749,0.0002593695],"study_design_scores_gemma":[0.0001948146,0.000060631235,0.00008796904,0.00007602121,0.000025320644,0.000036369198,0.0006696665,0.9979837,0.00043367015,0.000027205908,0.000016646869,0.00038799504],"about_ca_topic_score_codex":0.000030388657,"about_ca_topic_score_gemma":0.000003498444,"teacher_disagreement_score":0.41867468,"about_ca_system_score_codex":0.00008189915,"about_ca_system_score_gemma":0.00006352586,"threshold_uncertainty_score":0.999964},"labels":[],"label_agreement":null},{"id":"W2329441757","doi":"10.2514/6.2015-2984","title":"A 3D analytical approach for Open rotor Blade Vortex Interaction(BVI) tonal noise","year":2015,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":6,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Safran Electronics (Canada); Université de Sherbrooke","funders":"Fonds de recherche du Québec – Nature et technologies; Compute Canada; Université de Sherbrooke","keywords":"Blade (archaeology); Rotor (electric); Noise (video); Vortex; Acoustics; Physics; Aerospace engineering; Computer science; Engineering; Mechanical engineering; Mechanics; Artificial intelligence","score_opus":0.045089041209585935,"score_gpt":0.29525685378951716,"score_spread":0.2501678125799312,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2329441757","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.011098128,0.000018790384,0.8613114,0.000062412524,0.0005145743,0.00060239265,0.00003482847,0.00014742487,0.12621006],"genre_scores_gemma":[0.8501606,0.000003316907,0.14494328,0.00011070597,0.00034753085,0.00017936996,0.000068174435,0.00004738869,0.00413965],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992208,0.000007207566,0.00021307905,0.00019344973,0.0001346327,0.0002308173],"domain_scores_gemma":[0.99946815,0.00004660314,0.000017765491,0.00021372703,0.0000786963,0.00017506532],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020715373,0.0001392254,0.00018474425,0.000045763707,0.000035986206,0.00013664436,0.00033402414,0.00008172911,0.000128684],"category_scores_gemma":[0.0000645115,0.00012305738,0.000058579113,0.0000920077,0.00002046302,0.00017193789,0.00012400871,0.00014910565,0.00003226938],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000952837,0.00022486804,0.00034509183,0.00009006662,0.00021364033,0.000005817405,0.00021477025,0.9064948,0.00044838802,0.020567825,0.06631663,0.0049828463],"study_design_scores_gemma":[0.0004724823,0.000042652664,0.00008747946,0.000005099598,0.000028289844,0.000007098296,0.00014888245,0.98685575,0.000034594,0.00044129085,0.011696134,0.00018022914],"about_ca_topic_score_codex":0.00001841205,"about_ca_topic_score_gemma":0.000016323083,"teacher_disagreement_score":0.83906245,"about_ca_system_score_codex":0.00011147208,"about_ca_system_score_gemma":0.000035251553,"threshold_uncertainty_score":0.5018134},"labels":[],"label_agreement":null},{"id":"W2329534151","doi":"10.2514/6.2012-2122","title":"Aeroacoustic Prediction of the Tonal Noise Radiated by a Ring Fan in Uniform Inlet Flow","year":2012,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":15,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Inlet; Acoustics; Noise (video); Flow (mathematics); Ring (chemistry); Engineering; Marine engineering; Physics; Computer science; Mechanics; Mechanical engineering","score_opus":0.005606332186435455,"score_gpt":0.1776958510334346,"score_spread":0.17208951884699916,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2329534151","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.92953956,0.00013435302,0.0628184,0.00001574363,0.0007121694,0.00014843291,0.000104448634,0.00009539624,0.0064314944],"genre_scores_gemma":[0.9987545,0.000029675535,0.00095369003,0.000016735352,0.00006611405,0.000008125608,0.00001884818,0.000020291925,0.00013199431],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99935263,0.000009628542,0.00020726609,0.00006699939,0.00012964498,0.00023385107],"domain_scores_gemma":[0.999724,0.000031001917,0.000021056663,0.00015907454,0.000015249087,0.00004966896],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001524536,0.00009998054,0.000104390114,0.000044603028,0.000027378637,0.000007842057,0.00012047788,0.00006210564,0.00005744368],"category_scores_gemma":[0.000023801153,0.00007641667,0.000032938755,0.00019107197,0.000024261164,0.00009784932,0.000036120782,0.00017157277,0.0000047782687],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000051116554,0.000064016946,0.022503296,0.00007874708,0.000031410316,5.650185e-7,0.00040706972,0.93333924,0.038345624,0.00049927755,0.0023841928,0.00234146],"study_design_scores_gemma":[0.00022723875,0.00000734021,0.019176885,0.000026073596,0.000012824449,0.0000025653349,0.000058686106,0.9786459,0.0014767834,0.00003851327,0.00024715532,0.00008004205],"about_ca_topic_score_codex":0.000022598759,"about_ca_topic_score_gemma":0.00004238754,"teacher_disagreement_score":0.06921496,"about_ca_system_score_codex":0.0000896043,"about_ca_system_score_gemma":0.000008689329,"threshold_uncertainty_score":0.31161812},"labels":[],"label_agreement":null},{"id":"W2329799107","doi":"10.2514/6.2015-2531","title":"Experimental Validation of a Semi-Analytical Trailing-Edge Noise Model Including Broadband Scattering","year":2015,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"European Commission","keywords":"Broadband; Trailing edge; Noise (video); Scattering; Computer science; Acoustics; Model validation; Enhanced Data Rates for GSM Evolution; Electronic engineering; Physics; Optics; Telecommunications; Engineering; Artificial intelligence; Data science; Mechanics","score_opus":0.051971584539601295,"score_gpt":0.286052600317378,"score_spread":0.2340810157777767,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2329799107","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7676204,0.00005583211,0.22142294,0.00001086495,0.00013145973,0.00006035989,0.0000062526237,0.000095961565,0.010595942],"genre_scores_gemma":[0.9938066,0.0000033674744,0.0059171626,0.000013877611,0.00006022941,0.0000056819954,0.000009900295,0.000029666135,0.00015352463],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99924767,0.0000061521487,0.0002595846,0.00013254095,0.00018129547,0.0001727475],"domain_scores_gemma":[0.9996557,0.00001894248,0.00002295813,0.00015634141,0.000038634218,0.00010737708],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001579463,0.00012480599,0.00017378246,0.00006581095,0.000025672509,0.000024273504,0.00010241871,0.000064337706,0.000027972028],"category_scores_gemma":[0.000020036947,0.00012443113,0.000051549665,0.00008797896,0.00003247074,0.000114982446,0.000063111656,0.00009354439,0.000007673178],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000033421081,0.0000249741,0.000112136004,0.000021303233,0.000018723194,0.000001100456,0.00042310296,0.85209024,0.14631264,0.0006124028,0.00027409257,0.00010591899],"study_design_scores_gemma":[0.0002538406,0.00001564531,0.000008079328,0.000015962009,0.00001678852,0.000002841447,0.0002376779,0.89527345,0.10387826,0.00014867177,0.000019321806,0.00012946717],"about_ca_topic_score_codex":0.000008335797,"about_ca_topic_score_gemma":0.0000015459411,"teacher_disagreement_score":0.2261862,"about_ca_system_score_codex":0.00007591419,"about_ca_system_score_gemma":0.000018899762,"threshold_uncertainty_score":0.5074154},"labels":[],"label_agreement":null},{"id":"W2330917888","doi":"10.2514/6.2000-2353","title":"Optical transmission through a geometrically-derived free shear layer","year":2000,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Calgary","funders":"","keywords":"Materials science; Shear (geology); Layer (electronics); Transmission (telecommunications); Optics; Computer science; Composite material; Physics; Telecommunications","score_opus":0.010644412048570362,"score_gpt":0.2150949650958372,"score_spread":0.20445055304726684,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2330917888","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.12870137,0.00022533875,0.6238016,0.0002394813,0.00013476402,0.0001087968,0.000007994501,0.00048786617,0.24629278],"genre_scores_gemma":[0.86193675,0.0010199613,0.13447002,0.0001948423,0.00013145304,0.000008697359,0.000007898007,0.000055771005,0.0021745996],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991445,0.000006118766,0.0001953927,0.00016796034,0.0001916488,0.00029438947],"domain_scores_gemma":[0.9995233,0.000056481935,0.0000045518427,0.00029234966,0.000017663264,0.00010565372],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.000057494337,0.00014748503,0.00015903142,0.00004159403,0.000050409875,0.000034520282,0.00022496287,0.00012475897,0.006281257],"category_scores_gemma":[0.000012604922,0.00012439513,0.000071875016,0.00026905627,0.000029930075,0.00008870267,0.000013318804,0.000204924,0.00026162283],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000033887685,0.00017949971,0.000024919309,0.000093158305,0.000097911776,0.00007065528,0.00036464,0.4448697,0.037396196,0.008521065,0.020774374,0.48757398],"study_design_scores_gemma":[0.0006823273,0.000065761276,0.00044792326,0.000023292458,0.000027439242,0.000010241251,0.00001748311,0.8878631,0.002752664,0.0049154437,0.10278292,0.00041139786],"about_ca_topic_score_codex":0.000008355338,"about_ca_topic_score_gemma":0.0000017888378,"teacher_disagreement_score":0.73323536,"about_ca_system_score_codex":0.000028936453,"about_ca_system_score_gemma":0.000006315958,"threshold_uncertainty_score":0.9946271},"labels":[],"label_agreement":null},{"id":"W2331235100","doi":"10.2514/6.2014-3313","title":"Aeroacoustic study of Internal Mixing Nozzles with Forced Lobed Mixers using a High-Mach Subsonic Lattice Boltzmann Scheme","year":2014,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"","keywords":"Mach number; Lattice Boltzmann methods; Nozzle; Mixing (physics); Mechanics; Physics; Acoustics; Aerospace engineering; Engineering","score_opus":0.008712956966648337,"score_gpt":0.21522585955107332,"score_spread":0.20651290258442498,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2331235100","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.68356764,0.000019665165,0.3150596,0.0000030182457,0.00021090815,0.00018808222,0.0000033154536,0.00013141766,0.0008163671],"genre_scores_gemma":[0.9655421,0.0000041778762,0.034161422,0.000021072377,0.00009348144,0.000008649961,0.0000037966015,0.00007967895,0.00008565679],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9985992,0.000031753676,0.00039184798,0.00027798789,0.00031599312,0.00038322253],"domain_scores_gemma":[0.99919957,0.00013302539,0.00008640669,0.00037947745,0.00010636483,0.00009517424],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002597832,0.0002766795,0.00037757395,0.00013029178,0.00007986486,0.000053184653,0.0002923164,0.00008402759,0.000042321157],"category_scores_gemma":[0.000046029225,0.00023782131,0.00005097385,0.00022121293,0.000053916163,0.000116723335,0.00008136913,0.00027127512,0.000005970169],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00004591741,0.00019099492,0.0059413686,0.00024143366,0.00033036247,0.000012250953,0.0006392635,0.9426204,0.048232462,0.0012829916,0.000039253307,0.0004233332],"study_design_scores_gemma":[0.0012416918,0.00025543798,0.0016450823,0.0001179458,0.00015220785,0.000008794505,0.0010156465,0.99439174,0.0007723752,0.000069348396,0.000011527886,0.00031821174],"about_ca_topic_score_codex":0.00033593638,"about_ca_topic_score_gemma":0.00043627454,"teacher_disagreement_score":0.28197443,"about_ca_system_score_codex":0.00009226294,"about_ca_system_score_gemma":0.000017995464,"threshold_uncertainty_score":0.96980715},"labels":[],"label_agreement":null},{"id":"W2331977246","doi":"10.1115/fedsm-icnmm2010-30221","title":"Acoustically-Coupled Flows in Coaxial Side Branch Resonators With Bluff Rectangular Splitter Plates","year":2010,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Victoria","funders":"","keywords":"Acoustics; Particle image velocimetry; Duct (anatomy); Sound pressure; Amplitude; Physics; Vortex; Aeroacoustics; Splitter plate; Sound power; Acoustic wave; Splitter; Turbulence; Mechanics; Optics","score_opus":0.0028931972748953852,"score_gpt":0.18424641568506142,"score_spread":0.18135321841016602,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2331977246","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.96000123,0.000026280222,0.031698488,0.000077128636,0.0006171083,0.0002012692,0.000011195532,0.00029444994,0.007072847],"genre_scores_gemma":[0.9827059,0.00001580167,0.016613284,0.000098181685,0.0002312948,0.0000335849,0.000013444033,0.000079143254,0.00020937476],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9987023,0.000009175067,0.0003019532,0.0002846959,0.0002390673,0.0004628488],"domain_scores_gemma":[0.99930775,0.00014083066,0.000019231817,0.0003557837,0.00004692547,0.00012947548],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020438396,0.00025974022,0.00026826604,0.00010990735,0.000047295624,0.00005468897,0.00022557445,0.00022426379,0.00051936164],"category_scores_gemma":[0.00007302942,0.00021296575,0.000045482364,0.00023160987,0.00007894795,0.000094676936,0.000042911353,0.000719645,0.000055896347],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00020081169,0.00020951756,0.0071293064,0.00022962013,0.00016727236,0.00044063214,0.00064711925,0.376191,0.5960756,0.010018934,0.0019915346,0.006698654],"study_design_scores_gemma":[0.00071753334,0.000043483615,0.0031751117,0.00003143858,0.000021132266,0.00002138292,0.000045881483,0.9911894,0.0015509411,0.0017747576,0.001002973,0.00042595746],"about_ca_topic_score_codex":0.000056132936,"about_ca_topic_score_gemma":0.0021990142,"teacher_disagreement_score":0.6149984,"about_ca_system_score_codex":0.000043167674,"about_ca_system_score_gemma":0.000026070125,"threshold_uncertainty_score":0.86844915},"labels":[],"label_agreement":null},{"id":"W2332201333","doi":"10.2514/6.2015-2208","title":"Installation noise of a turbofan jet engine under an airfoil","year":2015,"lang":"en","type":"preprint","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Safran Electronics (Canada)","funders":"","keywords":"Turbofan; Reynolds-averaged Navier–Stokes equations; Airfoil; Jet engine; Noise (video); Jet (fluid); Jet noise; Turbulence; Euler equations; Acoustics; Turbojet; Aeroacoustics; Computer science; Mechanics; Physics; Aerospace engineering; Engineering","score_opus":0.019258270457326573,"score_gpt":0.2394432898392928,"score_spread":0.22018501938196622,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2332201333","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7476897,0.00019513776,0.20941362,0.000030383379,0.0013801396,0.00023955353,0.00012730963,0.0004583236,0.040465787],"genre_scores_gemma":[0.9876169,0.00008623782,0.011459472,0.000015901625,0.0002091901,0.000009740496,0.00029675092,0.00006971516,0.00023609764],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9990242,0.000013349227,0.00033616327,0.00022660858,0.00022065568,0.00017899247],"domain_scores_gemma":[0.99912083,0.000018971992,0.00005972687,0.0005394193,0.00014756992,0.00011347811],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00019076777,0.00026377477,0.00032203452,0.00011854768,0.000013493852,0.000030892217,0.00024348874,0.00032612853,0.00009350511],"category_scores_gemma":[0.00001900032,0.00025184435,0.0000733388,0.00007856041,0.000026362877,0.00006309958,0.00020080138,0.00041643812,0.000010174093],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000003101563,0.000026696367,0.00007363639,0.00018820446,0.000050173818,0.0000015208536,0.00012127726,0.9948644,0.0011393905,0.0014214201,0.0005479271,0.0015622479],"study_design_scores_gemma":[0.00017188989,0.000023707662,0.0005696209,0.00005668712,0.000036835463,0.0000013297874,0.00006161042,0.99078095,0.00020556402,0.0075028297,0.00028874085,0.00030024684],"about_ca_topic_score_codex":0.000065837754,"about_ca_topic_score_gemma":0.00015059063,"teacher_disagreement_score":0.23992714,"about_ca_system_score_codex":0.00012671911,"about_ca_system_score_gemma":0.00006445018,"threshold_uncertainty_score":0.9999934},"labels":[],"label_agreement":null},{"id":"W2333356901","doi":"10.2514/6.2009-3204","title":"Influence of Upwash Flow Disturbance on Flow-Induced Cavity Resonance","year":2009,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"","keywords":"Disturbance (geology); Flow (mathematics); Resonance (particle physics); Mechanics; Physics; Geology; Atomic physics","score_opus":0.005863012921193309,"score_gpt":0.2065117854618804,"score_spread":0.20064877254068708,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2333356901","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9825544,0.00011432147,0.006967531,0.00005252561,0.00013815855,0.000097186414,0.00002025914,0.00016895581,0.009886707],"genre_scores_gemma":[0.9920918,0.00006833426,0.0074007176,0.00013696688,0.000056571516,0.000003516015,0.000003857155,0.000015941741,0.0002222917],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99919105,0.0000074669356,0.00021837771,0.00017539042,0.00018330094,0.00022443426],"domain_scores_gemma":[0.9994774,0.000039874634,0.00002507226,0.0003512502,0.000049319216,0.000057122805],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00008539406,0.00015371054,0.00018577871,0.000032370608,0.000036456237,0.000012093453,0.00020805062,0.0000796996,0.000015395719],"category_scores_gemma":[0.000040733466,0.00014274893,0.0000455126,0.00015960565,0.000021013375,0.00007379638,0.000016430959,0.00019345392,0.000022112969],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000074534614,0.000032560703,0.00017419113,0.000019563693,0.000005068186,0.0000057496336,0.000044210654,0.9427948,0.016273767,0.0017558829,0.0006734935,0.03821328],"study_design_scores_gemma":[0.00018183407,0.00007900889,0.05970279,0.000070666836,0.0000057485327,0.0000012602873,0.0000032654348,0.92996806,0.007921498,0.0008521848,0.0009911883,0.00022251393],"about_ca_topic_score_codex":0.000009120454,"about_ca_topic_score_gemma":0.000011419038,"teacher_disagreement_score":0.0595286,"about_ca_system_score_codex":0.0000516325,"about_ca_system_score_gemma":0.000010139794,"threshold_uncertainty_score":0.58211327},"labels":[],"label_agreement":null},{"id":"W2333464096","doi":"10.2514/6.2011-3900","title":"Wake model effects on the prediction of turbulence-interaction broadband noise in a realistic compressor stage","year":2011,"lang":"en","type":"article","venue":"41st AIAA Fluid Dynamics Conference and Exhibit","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":10,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Compute Canada","keywords":"Wake; Gas compressor; Stage (stratigraphy); Turbulence; Noise (video); Broadband; Acoustics; Physics; Wake turbulence; Computer science; Aerospace engineering; Mechanics; Engineering; Geology; Optics","score_opus":0.03365097920267897,"score_gpt":0.2149425291050612,"score_spread":0.18129154990238222,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2333464096","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.93155706,0.00005756994,0.05638794,0.00003318143,0.00031748033,0.0003218931,0.00023621874,0.00007613688,0.011012543],"genre_scores_gemma":[0.9988539,0.0005116724,0.00031051596,0.000030901756,0.00003040789,0.00003659278,0.000048900994,0.00002748979,0.00014957564],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9990076,0.00003123469,0.00032409563,0.0002333458,0.00016573476,0.00023797998],"domain_scores_gemma":[0.99937654,0.00013177074,0.000060810235,0.00030152395,0.00006792387,0.00006141618],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015118274,0.00021554781,0.00024722004,0.000108297296,0.00006100455,0.000036563582,0.00017103498,0.00012269773,0.00002859747],"category_scores_gemma":[0.000042626372,0.00017567656,0.000044249406,0.00011081729,0.000080628146,0.00012343265,0.000047047604,0.00030653243,0.000004221904],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00029746577,0.00028504865,0.004296468,0.0013203414,0.00013257816,0.00003982132,0.0049670762,0.8017763,0.039844774,0.1366583,0.0004066042,0.009975214],"study_design_scores_gemma":[0.00031657793,0.00009293644,0.0026167962,0.00027977102,0.000023133207,0.0000026029952,0.0001530247,0.9931657,0.0009995482,0.0021864881,0.000010657418,0.00015281342],"about_ca_topic_score_codex":0.00012593927,"about_ca_topic_score_gemma":0.0002641403,"teacher_disagreement_score":0.19138934,"about_ca_system_score_codex":0.000076614415,"about_ca_system_score_gemma":0.000021627146,"threshold_uncertainty_score":0.7163882},"labels":[],"label_agreement":null},{"id":"W2333501865","doi":"10.2514/6.2005-3019","title":"Aeroacoustic Response of an Annular Duct with Coaxial Closed Side Branches","year":2005,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"","keywords":"Coaxial; Duct (anatomy); Acoustics; Computer science; Physics; Telecommunications; Anatomy; Medicine","score_opus":0.00473394597762888,"score_gpt":0.19498469049972308,"score_spread":0.1902507445220942,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2333501865","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9442565,0.000055337445,0.05296557,0.000040516086,0.0000994548,0.000107178515,0.000022611483,0.00020210566,0.0022507524],"genre_scores_gemma":[0.9743776,0.000011267229,0.025095683,0.000038766328,0.0001538338,0.000004721857,0.0000087461685,0.000046156438,0.0002632646],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99920267,0.000027811055,0.00021276559,0.0001552075,0.00017737495,0.00022414315],"domain_scores_gemma":[0.9994265,0.000090972026,0.000025784504,0.00031788368,0.00005323323,0.000085625965],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00022437057,0.00015676886,0.00019165705,0.00006873799,0.0000346839,0.000019122777,0.00015273318,0.000074615484,0.00007977223],"category_scores_gemma":[0.00003941657,0.00013257372,0.000033333363,0.00012532914,0.00006340757,0.00012793439,0.00001658806,0.00012640364,0.000013759767],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00032084616,0.00006657944,0.00009766376,0.000043379205,0.000044259803,0.000021874741,0.000218416,0.8338665,0.15955707,0.00031249778,0.0002560389,0.0051948964],"study_design_scores_gemma":[0.0007222044,0.00022307469,0.0045116176,0.000025829733,0.000041161347,0.000023157994,0.00014928046,0.9744634,0.018586019,0.00009614269,0.00085400534,0.0003041102],"about_ca_topic_score_codex":0.0000094946145,"about_ca_topic_score_gemma":0.00009143024,"teacher_disagreement_score":0.14097105,"about_ca_system_score_codex":0.0000393419,"about_ca_system_score_gemma":0.000028118946,"threshold_uncertainty_score":0.54061997},"labels":[],"label_agreement":null},{"id":"W2333652185","doi":"10.2514/6.2010-18","title":"Unsteady Numerical Simulation of a Round Jet with Impinging Microjets for Noise Suppresion","year":2010,"lang":"en","type":"article","venue":"48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":9,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"Université de Sherbrooke","keywords":"Jet (fluid); Jet noise; Noise (video); Acoustics; Physics; Computer simulation; Mechanics; Aerospace engineering; Computer science; Engineering","score_opus":0.012025195288456154,"score_gpt":0.2586892571629083,"score_spread":0.24666406187445214,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2333652185","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7393239,0.00013474336,0.25785586,0.001080232,0.00065627135,0.00048730205,0.000021709297,0.00015741344,0.00028252072],"genre_scores_gemma":[0.96585923,0.000043315966,0.03366977,0.000037821264,0.00024352958,0.000025766474,0.000014267237,0.000051699306,0.000054594206],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9981041,0.000038367456,0.00035450078,0.00044938197,0.00040774545,0.00064592995],"domain_scores_gemma":[0.9986263,0.0005783856,0.00022253035,0.00030059888,0.00011346541,0.00015873168],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0007886948,0.0003385228,0.0003316429,0.00012807072,0.0012001893,0.00026377896,0.00036921256,0.00015438045,0.000004156542],"category_scores_gemma":[0.00017587397,0.0002461125,0.000092140675,0.00055604905,0.0003498695,0.0005123364,0.00014940734,0.0003569958,0.0000014982611],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000056663208,0.000028071612,0.0034990693,0.000069256384,0.000025642392,7.696847e-7,0.00077419356,0.49413824,0.49783406,0.0017306642,0.0004899138,0.0013534672],"study_design_scores_gemma":[0.0008093784,0.00063484925,0.00041429664,0.00034000177,0.000086285414,0.000021315485,0.0015450219,0.9575042,0.03671512,0.0009690515,0.0004860592,0.0004743793],"about_ca_topic_score_codex":0.00009090404,"about_ca_topic_score_gemma":0.00025175384,"teacher_disagreement_score":0.463366,"about_ca_system_score_codex":0.00006188589,"about_ca_system_score_gemma":0.000069399386,"threshold_uncertainty_score":0.9999991},"labels":[],"label_agreement":null},{"id":"W2334115679","doi":"10.2514/6.2008-765","title":"Effect of Exit Velocity on Entrainment and Spreading of a Jet Issuing from an Asymmetric Nozzle With and Without a Sudden Expansion","year":2008,"lang":"en","type":"article","venue":"46th AIAA Aerospace Sciences Meeting and Exhibit","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Manitoba","funders":"Manitoba Hydro","keywords":"Entrainment (biomusicology); Nozzle; Jet (fluid); Mechanics; Materials science; Physics; Acoustics; Thermodynamics","score_opus":0.008336890231353832,"score_gpt":0.23384826339871326,"score_spread":0.22551137316735942,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2334115679","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99753547,0.00055225287,0.00075427315,0.000019989922,0.00006833872,0.00015644878,0.000012065522,0.000043052987,0.00085812167],"genre_scores_gemma":[0.994416,0.00047318445,0.00503759,0.000010393451,0.000033170774,0.000004292633,0.0000021036735,0.000016300955,0.000006980543],"study_design_codex":"observational","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99880636,0.00005348692,0.00019297228,0.00034821627,0.00033388252,0.00026507146],"domain_scores_gemma":[0.99933654,0.0002786438,0.00009265049,0.00014126986,0.000025451884,0.00012543851],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0007778676,0.00019935619,0.00034546465,0.00016654188,0.0002318995,0.000041413638,0.00010057129,0.00006254273,0.0000018840834],"category_scores_gemma":[0.00010754544,0.00014827696,0.000020305017,0.000397507,0.00038421658,0.00013604286,0.00005749502,0.00012789422,2.4205653e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00024376909,0.00010045776,0.7251306,0.0007076092,0.00009209893,0.000019208599,0.010441984,0.03821224,0.2038807,0.00020719947,0.000081307866,0.020882847],"study_design_scores_gemma":[0.002407745,0.00419295,0.050171927,0.001967899,0.00014635143,0.00005539075,0.0019798933,0.7474343,0.19068792,0.00009799642,0.000029707599,0.0008279257],"about_ca_topic_score_codex":0.00031563465,"about_ca_topic_score_gemma":0.00006201665,"teacher_disagreement_score":0.7092221,"about_ca_system_score_codex":0.000015526306,"about_ca_system_score_gemma":0.000014614109,"threshold_uncertainty_score":0.60465586},"labels":[],"label_agreement":null},{"id":"W2334322739","doi":"10.2514/6.2015-2205","title":"Detailed experimental investigation of the aeroacoustic field around a Controlled-Diffusion airfoil","year":2015,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":38,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Acoustics; Airfoil; Anechoic chamber; Noise (video); Microphone; Physics; Aeroacoustics; Mach number; Azimuth; Trailing edge; Computer science; Optics; Sound pressure; Mechanics","score_opus":0.013379769930060882,"score_gpt":0.212140146580495,"score_spread":0.1987603766504341,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2334322739","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9745534,0.0001565883,0.01543862,0.000063833955,0.0007178416,0.00021529038,0.0000021576784,0.000082357416,0.008769904],"genre_scores_gemma":[0.998505,0.000005896466,0.00089484226,0.0001048576,0.000073537405,0.0000198471,0.000002205661,0.000016214997,0.00037759033],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993486,0.000020317028,0.00022457524,0.000088634646,0.0001940051,0.00012387123],"domain_scores_gemma":[0.9995574,0.00007818849,0.000038153266,0.00020992939,0.000047245954,0.00006908757],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001329359,0.00010830371,0.00016993648,0.000027237274,0.000036691858,0.000017853503,0.00014831663,0.000070702205,0.00003757769],"category_scores_gemma":[0.000083874125,0.00007207405,0.00006359567,0.00009385474,0.000041323423,0.000050220722,0.000052153067,0.00010564541,0.0000076221304],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00014387013,0.00010436546,0.009943073,0.00008688171,0.00012586532,0.0000042115234,0.0016707159,0.35822526,0.61354834,0.0046462724,0.010919684,0.000581453],"study_design_scores_gemma":[0.0018591215,0.00005894326,0.0004135472,0.000024441799,0.000027541213,0.0000028165346,0.00060983695,0.96828514,0.027748313,0.00081202184,0.00003863925,0.000119648554],"about_ca_topic_score_codex":0.000016144702,"about_ca_topic_score_gemma":0.000039640443,"teacher_disagreement_score":0.61005986,"about_ca_system_score_codex":0.000056455203,"about_ca_system_score_gemma":0.000026418971,"threshold_uncertainty_score":0.29390943},"labels":[],"label_agreement":null},{"id":"W2334337896","doi":"10.2514/6.2009-3198","title":"Flow Features and Self-Noise of Airfoils Near Stall or in Stall","year":2009,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":81,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Center for Turbulence Research, Stanford University","keywords":"Stall (fluid mechanics); Airfoil; Acoustics; Computer science; Aerospace engineering; Physics; Engineering","score_opus":0.003776280541920831,"score_gpt":0.19789682748128476,"score_spread":0.19412054693936392,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2334337896","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9853416,0.00030272192,0.0033174339,0.00006595654,0.00009596445,0.00012490328,0.000018375029,0.00016576068,0.010567264],"genre_scores_gemma":[0.9725829,0.0002970198,0.026752686,0.00005171395,0.000022764025,0.000001386404,0.0000039277606,0.000014042189,0.00027355595],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99948615,0.000005414208,0.00015268064,0.00010410287,0.00008683613,0.00016483948],"domain_scores_gemma":[0.9997613,0.000028520099,0.000012049991,0.00013329338,0.000016943126,0.00004789462],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00007081003,0.00010812935,0.00015016262,0.0000431318,0.000016271964,0.000023693936,0.000076104676,0.000071262926,0.000047999725],"category_scores_gemma":[0.000013899464,0.00008714594,0.00001960975,0.00009649667,0.000016066484,0.000055454188,0.000018316943,0.000119028635,0.0000020407],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000047449565,0.00022522955,0.00042501665,0.0002450128,0.000053852367,0.00007764828,0.001187115,0.9340794,0.028019892,0.0027031952,0.005329509,0.027606675],"study_design_scores_gemma":[0.00036505892,0.00009486643,0.015230911,0.000027380665,0.000009107606,0.0000072701328,0.000054262975,0.9822944,0.00044974854,0.00054785877,0.0007530821,0.0001660771],"about_ca_topic_score_codex":0.00001634039,"about_ca_topic_score_gemma":0.00016196018,"teacher_disagreement_score":0.048214972,"about_ca_system_score_codex":0.000027186374,"about_ca_system_score_gemma":0.000012967476,"threshold_uncertainty_score":0.35537085},"labels":[],"label_agreement":null},{"id":"W2334741835","doi":"10.2514/6.2010-3887","title":"Direct aeroacoustics predictions of a low speed axial fan","year":2010,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":47,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Aeroacoustics; Computational aeroacoustics; Acoustics; Mechanical fan; Fan-in; Computer science; Aerospace engineering; Physics; Engineering; Electrical engineering; Algorithm; Sound pressure","score_opus":0.00426235603791567,"score_gpt":0.19349218786099814,"score_spread":0.18922983182308248,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2334741835","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6640844,0.0000113259875,0.1748417,0.000015040713,0.002984683,0.0001351788,0.00012086791,0.0004656636,0.15734115],"genre_scores_gemma":[0.9932541,0.000018900015,0.005782779,0.00000768531,0.0002604317,0.0000023699645,0.000010685255,0.000027931777,0.0006350684],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994423,0.0000029877674,0.00018087497,0.00009415089,0.000118966935,0.00016075866],"domain_scores_gemma":[0.99959105,0.00004440305,0.000017602315,0.00023145719,0.00005051209,0.0000649834],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000069921414,0.000101456404,0.00012976119,0.000051283423,0.000034404704,0.000013958079,0.00012273934,0.00009596032,0.00025363028],"category_scores_gemma":[0.000049808175,0.00009581968,0.000050492425,0.00010946664,0.00005022306,0.000035771627,0.000025196301,0.00021824887,0.000017078284],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000037235943,0.00007269341,0.00035753095,0.00008804011,0.000062197265,0.000003872828,0.00009879641,0.36058685,0.62948453,0.0034021898,0.0046777274,0.0011618506],"study_design_scores_gemma":[0.00014294543,0.00001764263,0.0009790396,0.000008439063,0.000023817673,0.0000034213285,0.000023347178,0.9916103,0.0064120633,0.00014235966,0.00051460287,0.00012205445],"about_ca_topic_score_codex":0.000011389327,"about_ca_topic_score_gemma":0.000100880665,"teacher_disagreement_score":0.6310234,"about_ca_system_score_codex":0.000011897081,"about_ca_system_score_gemma":0.000013338433,"threshold_uncertainty_score":0.39074135},"labels":[],"label_agreement":null},{"id":"W2335452561","doi":"10.2514/6.2003-3296","title":"Aeroacoustic Performance of Axial-Flow Fans in Self-Stimulated and Non-Self-Stimulated Domains: Influence of Reynolds Number on Axial-Flow Fans","year":2003,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Royal Military College of Canada","funders":"","keywords":"Reynolds number; Flow (mathematics); Axial compressor; Mechanics; Physics; Turbulence; Thermodynamics","score_opus":0.003430493379840462,"score_gpt":0.19733483303261462,"score_spread":0.19390433965277415,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2335452561","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9863727,0.00004011799,0.0068549654,0.00000666612,0.00026295707,0.00052040943,0.00005579742,0.0003009881,0.005585403],"genre_scores_gemma":[0.9763515,0.00045064656,0.022920141,0.000036200883,0.000027465989,0.000019353805,0.000019587256,0.000097098455,0.000078012235],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9974569,0.000054466876,0.0009725123,0.000467232,0.00042178825,0.00062709517],"domain_scores_gemma":[0.9986424,0.00024698846,0.00014586623,0.00060995517,0.00019628486,0.00015852472],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00041330376,0.0005060049,0.00071438286,0.00025614907,0.000081608356,0.000030416013,0.0002960514,0.00039989108,0.00010212967],"category_scores_gemma":[0.00012339363,0.00049769704,0.000093990086,0.0007998105,0.000118241485,0.00022633687,0.00006196055,0.0004998253,0.000024529982],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00004677278,0.00021242049,0.015023603,0.0004558254,0.00010978663,0.000017463526,0.0005661663,0.9736376,0.00936702,0.000222869,0.000050034134,0.00029045678],"study_design_scores_gemma":[0.0018580073,0.00021865137,0.022030825,0.00028814137,0.00008600081,0.000012913567,0.00004312228,0.9726624,0.0021162368,0.00009909634,0.000056159115,0.0005284555],"about_ca_topic_score_codex":0.00006212769,"about_ca_topic_score_gemma":0.00005473067,"teacher_disagreement_score":0.016065177,"about_ca_system_score_codex":0.0001647748,"about_ca_system_score_gemma":0.00007276394,"threshold_uncertainty_score":0.99974746},"labels":[],"label_agreement":null},{"id":"W2335499271","doi":"10.2514/6.2015-3123","title":"Experimental and numerical study of the noise generation in an outflow butterfly valve","year":2015,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Natural Sciences and Engineering Research Council of Canada; Consortium de Recherche et d’innovation en Aérospatiale au Québec; Compute Canada; Université de Sherbrooke","keywords":"Butterfly valve; Butterfly; Outflow; Noise (video); Computer science; Acoustics; Physics; Engineering; Mechanical engineering; Meteorology; Artificial intelligence","score_opus":0.02469875039232114,"score_gpt":0.25595965296556017,"score_spread":0.23126090257323903,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2335499271","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9935781,0.00003485056,0.0057323235,0.000007529269,0.00017813324,0.00011992388,0.0000011859577,0.000017209593,0.00033077403],"genre_scores_gemma":[0.9993371,3.4073597e-7,0.00056975236,0.00001453697,0.000045005992,0.0000070650412,0.0000014344054,0.000008938937,0.00001587552],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99966115,0.0000159933,0.00010282707,0.000071849994,0.000086443644,0.000061758255],"domain_scores_gemma":[0.9998249,0.000004253466,0.000008461094,0.00011702303,0.000012757419,0.000032635726],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0000620567,0.000054943208,0.000068307294,0.000015794867,0.00001210282,0.000013078662,0.00005992507,0.000021108177,0.000005212289],"category_scores_gemma":[0.0000049537443,0.000039412524,0.000010584933,0.000046599125,0.000009558057,0.000050505547,0.000031422864,0.00005048552,7.426045e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000006450777,0.00053094205,0.045469057,0.00000568479,0.000019209008,0.000002457454,0.007603655,0.8075657,0.13729928,0.00022333009,0.0003840204,0.000890223],"study_design_scores_gemma":[0.00034001045,0.00010243104,0.009311123,0.0000012235059,0.000003891477,7.2146656e-7,0.0014781418,0.98571396,0.002972836,0.0000148250165,0.000005586625,0.00005525956],"about_ca_topic_score_codex":0.00004387238,"about_ca_topic_score_gemma":0.000048739737,"teacher_disagreement_score":0.17814825,"about_ca_system_score_codex":0.000025832525,"about_ca_system_score_gemma":0.0000039957663,"threshold_uncertainty_score":0.1607196},"labels":[],"label_agreement":null},{"id":"W2335528110","doi":"10.2514/6.2013-2043","title":"Tonal Noise Control of Centrifugal Fan Using Flow Obstructions - Experimental and Numerical Approaches","year":2013,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Compute Canada","keywords":"Centrifugal fan; Aerodynamics; Acoustics; Noise (video); Blade (archaeology); Noise reduction; Inlet; Reduction (mathematics); Position (finance); Noise control; Flow (mathematics); Mechanical fan; Computer science; Engineering; Physics; Structural engineering; Mechanics; Aerospace engineering; Mechanical engineering; Mathematics; Artificial intelligence","score_opus":0.014826630070335437,"score_gpt":0.1978393037863234,"score_spread":0.18301267371598795,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2335528110","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.5756068,0.00012820224,0.42283174,0.000009869665,0.00016598086,0.00010737509,0.000014210145,0.000044900924,0.001090893],"genre_scores_gemma":[0.95924914,0.0000023514076,0.040624417,0.000008630934,0.00006631933,0.000008957867,0.000004003543,0.000016082542,0.000020104233],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99949497,0.0000063957436,0.00015658303,0.00010096237,0.0000873032,0.00015379387],"domain_scores_gemma":[0.99978536,0.00002244817,0.00001547174,0.00008837981,0.000016583755,0.00007174013],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000021708769,0.00010109496,0.00013842118,0.000028990302,0.000042523032,0.00002471099,0.000051637337,0.00004956064,0.00022505033],"category_scores_gemma":[0.000005308867,0.0000925014,0.000034348548,0.000047616628,0.000053286036,0.000089812,0.00002129802,0.00007835829,0.0000039654774],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000073105884,0.00010440455,0.0035226417,0.000045077137,0.00011301933,0.0000019187605,0.00027069513,0.5877709,0.4001443,0.0039339326,0.00017796566,0.003907865],"study_design_scores_gemma":[0.00029690852,0.000012532901,0.00125214,0.000004084911,0.000011925817,0.0000111380805,0.00024720374,0.9933079,0.0046482454,0.00008187329,0.00002023342,0.00010585083],"about_ca_topic_score_codex":0.000031552776,"about_ca_topic_score_gemma":5.017533e-7,"teacher_disagreement_score":0.405537,"about_ca_system_score_codex":0.00003004216,"about_ca_system_score_gemma":0.0000061692117,"threshold_uncertainty_score":0.37720975},"labels":[],"label_agreement":null},{"id":"W2337231262","doi":"10.1115/imece2014-38199","title":"Assessment of Surface-Based Aeroacoustic Noise From Blades of a Vertical-Axis Wind Turbine","year":2014,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Carleton University","funders":"","keywords":"Acoustics; Sound pressure; Turbine blade; Turbine; Noise (video); Vertical axis wind turbine; RADIUS; Plane (geometry); Aeroacoustics; Mechanics; Geology; Physics; Materials science; Engineering; Geometry; Aerospace engineering; Computer science; Mathematics","score_opus":0.006632575219260716,"score_gpt":0.21710768295095204,"score_spread":0.2104751077316913,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2337231262","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.69232994,0.000026621374,0.30347982,0.00001584104,0.00015480898,0.00007327561,0.000042600474,0.000060103495,0.0038169886],"genre_scores_gemma":[0.96633697,0.000009983099,0.033504125,0.000021893564,0.00003899529,0.0000015529293,0.000023480216,0.000031257532,0.000031750293],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9990346,0.000020762587,0.0003607191,0.000155481,0.00023841059,0.00019003153],"domain_scores_gemma":[0.9991575,0.00030089173,0.00003110711,0.00035970946,0.00007444943,0.000076380595],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015054095,0.0001573982,0.00032206607,0.00004168013,0.000016573918,0.00001038582,0.00016855139,0.00009016922,0.00029869334],"category_scores_gemma":[0.00005929235,0.00014036754,0.00007566972,0.0001161822,0.00007017944,0.000031109896,0.000031338746,0.00013021764,0.0000056886547],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000004162024,0.00006640133,0.00284154,0.000100486155,0.000044840137,7.5895355e-7,0.000014270066,0.7607132,0.23514816,0.000722249,0.00012058197,0.00022330062],"study_design_scores_gemma":[0.00045089133,0.000069518115,0.02836889,0.000051081017,0.000063057865,1.1157315e-7,0.000015202763,0.95871866,0.01178962,0.00029323896,0.00003322737,0.00014652601],"about_ca_topic_score_codex":0.000079764126,"about_ca_topic_score_gemma":0.000021204829,"teacher_disagreement_score":0.27400702,"about_ca_system_score_codex":0.0000395655,"about_ca_system_score_gemma":0.000027569904,"threshold_uncertainty_score":0.5724022},"labels":[],"label_agreement":null},{"id":"W2347032671","doi":"10.1121/1.4950579","title":"A study on minimizing the noise from a trailing edge by the use of optimized serrations","year":2016,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Carleton University","funders":"","keywords":"Trailing edge; Serration; Noise (video); Acoustics; Enhanced Data Rates for GSM Evolution; Flow (mathematics); Geometry; Mathematics; Mechanics; Physics; Materials science; Computer science; Telecommunications","score_opus":0.02788533829887473,"score_gpt":0.2440443631670432,"score_spread":0.21615902486816846,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2347032671","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.37883285,0.00023661075,0.61502296,0.0049665836,0.0004120634,0.00034282584,0.000110197194,0.000017971484,0.00005797551],"genre_scores_gemma":[0.9838812,0.0005270275,0.014920977,0.0004104351,0.00016240795,0.0000035225876,3.483092e-7,0.000028963044,0.000065165266],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.998498,0.00019345187,0.0005586647,0.00008162946,0.00046281714,0.00020539259],"domain_scores_gemma":[0.9955885,0.0033824788,0.00034393105,0.0005049494,0.00013018963,0.0000499785],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00059204816,0.00016612167,0.00033288272,0.000010539479,0.00023944183,0.0000219386,0.00085152773,0.000055515244,0.000023906405],"category_scores_gemma":[0.00039718408,0.00005707643,0.000370354,0.00019329332,0.0004987184,0.00007319868,0.00012382677,0.00048185568,0.0000014778202],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0001753201,0.00030055625,0.000048775448,0.000011472588,0.00081156014,7.509785e-7,0.0058414866,0.8273429,0.11154571,0.0000069689518,0.047814447,0.00610004],"study_design_scores_gemma":[0.0010628008,0.0003124876,0.00065713294,0.0001711832,0.0008094154,0.000009705279,0.008707159,0.9857726,0.00092321454,0.00023563647,0.0011827884,0.00015585471],"about_ca_topic_score_codex":0.000033542703,"about_ca_topic_score_gemma":0.0000013900726,"teacher_disagreement_score":0.6050483,"about_ca_system_score_codex":0.000046454603,"about_ca_system_score_gemma":0.00003815457,"threshold_uncertainty_score":0.23275092},"labels":[],"label_agreement":null},{"id":"W2372865606","doi":"10.1007/s00348-015-2103-7","title":"Effect of the driving algorithm on the turbulence generated by a random jet array","year":2016,"lang":"en","type":"article","venue":"Experiments in Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":35,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Turbulence; Physics; Isotropy; Reynolds number; Jet (fluid); Homogeneous isotropic turbulence; Mean flow; Gaussian; Turbulence kinetic energy; Flow (mathematics); Mechanics; Computational physics; Optics; Direct numerical simulation; Quantum mechanics","score_opus":0.004388283172994413,"score_gpt":0.22078687352313153,"score_spread":0.21639859035013712,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2372865606","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9706474,0.0004964127,0.025606258,0.000067138746,0.0009940322,0.0003347253,0.000023069719,0.000052040476,0.0017789386],"genre_scores_gemma":[0.9991169,0.00006807862,0.0003295085,0.00003635346,0.0000606076,0.00007076478,0.0000013523826,0.000028601782,0.00028782448],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9991338,0.000112658185,0.00020145894,0.00014540981,0.00019915507,0.00020751155],"domain_scores_gemma":[0.9992558,0.00032186412,0.000023712402,0.00036004063,0.000012699557,0.000025924523],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003461204,0.00016577766,0.00017131657,0.000024505784,0.000055818655,0.000015301832,0.00033937048,0.00006097269,0.000066575565],"category_scores_gemma":[0.00009127075,0.000071730836,0.000057183865,0.0001270831,0.00007040127,0.000034893,0.000045243203,0.00012158142,0.000011022406],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000013472049,0.000021078093,0.00025592028,0.000006302877,0.000026791393,0.0000010235135,0.00021834731,0.0013275053,0.98854953,0.00006816432,0.0018049808,0.0077068657],"study_design_scores_gemma":[0.0010687215,0.0000705748,0.00006777649,0.00015044771,0.0000056223366,6.8963544e-7,0.000012357955,0.08123007,0.9165803,0.000033049724,0.0006579406,0.00012244825],"about_ca_topic_score_codex":0.0000052065043,"about_ca_topic_score_gemma":7.336711e-7,"teacher_disagreement_score":0.07990256,"about_ca_system_score_codex":0.00009851344,"about_ca_system_score_gemma":0.000008560031,"threshold_uncertainty_score":0.29250985},"labels":[],"label_agreement":null},{"id":"W2378862251","doi":"10.1177/1475472x16630861","title":"Numerical assessment of the tonal noise of Counter-Rotating Open Rotors at approach","year":2016,"lang":"en","type":"article","venue":"International Journal of Aeroacoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":10,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Safran; École Centrale de Lyon; Compute Canada","keywords":"Rotor (electric); Aerodynamics; Vortex; Physics; Noise (video); Mechanics; Front (military); Acoustics; Chord (peer-to-peer); Helicopter rotor; Aerospace engineering; Computer science; Engineering; Meteorology","score_opus":0.011623381857338353,"score_gpt":0.2743577837076645,"score_spread":0.26273440185032615,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2378862251","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.44831985,0.000031006144,0.5443844,0.00017638369,0.002165885,0.00016876493,0.0001538762,0.000008472625,0.004591363],"genre_scores_gemma":[0.9701265,0.00004456078,0.0293986,0.000027545731,0.00022412749,0.0000034590134,0.0000022559382,0.000024774052,0.00014816246],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99818814,0.00003190361,0.00074773043,0.000092261645,0.0008021267,0.00013781562],"domain_scores_gemma":[0.9983684,0.00021621406,0.0005105083,0.00017352773,0.000671648,0.000059729995],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004067569,0.00013225096,0.00027213938,0.00007440959,0.000031802636,0.00003102549,0.0012270601,0.00006186652,0.00007570243],"category_scores_gemma":[0.0001654311,0.00007963043,0.00014676365,0.00008613089,0.00009550746,0.0001329986,0.0002826024,0.00018955034,8.7047937e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00007646082,0.00028441413,0.022267722,0.000075968,0.0006129873,0.000016954968,0.00019455847,0.8739905,0.09165009,0.0025281182,0.0024281286,0.005874119],"study_design_scores_gemma":[0.001837476,0.0001696817,0.0318427,0.0005856759,0.00012721591,0.0002080883,0.0001279451,0.95742047,0.0058935108,0.0007456084,0.0007656751,0.0002759751],"about_ca_topic_score_codex":0.000005583081,"about_ca_topic_score_gemma":0.0000018169343,"teacher_disagreement_score":0.52180666,"about_ca_system_score_codex":0.00026289493,"about_ca_system_score_gemma":0.00010772745,"threshold_uncertainty_score":0.32472348},"labels":[],"label_agreement":null},{"id":"W2394905731","doi":"10.1177/1475472x16630669","title":"The effect of upstream edge geometry on the acoustic resonance excitation in shallow rectangular cavities","year":2016,"lang":"en","type":"article","venue":"International Journal of Aeroacoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":19,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Guelph; Ontario Tech University","funders":"","keywords":"Resonance (particle physics); Vortex; Acoustic resonance; Mach number; Excited state; Excitation; Materials science; Physics; Vibration; Optics; Enhanced Data Rates for GSM Evolution; Geometry; Amplitude; Acoustics; Mechanics; Atomic physics; Telecommunications","score_opus":0.004733736576609895,"score_gpt":0.21648861377286838,"score_spread":0.2117548771962585,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2394905731","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.96828467,0.0005583676,0.027307237,0.0005215978,0.0025253352,0.00010970341,0.000055072578,0.000014742715,0.0006232546],"genre_scores_gemma":[0.99821633,0.0009654763,0.00024690913,0.000025170191,0.0003651065,0.000003983603,0.0000012358166,0.000026424548,0.00014933622],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99855137,0.000070337956,0.0005198389,0.00008280295,0.0005982173,0.00017745732],"domain_scores_gemma":[0.99658453,0.0026950638,0.00021503799,0.00017685432,0.00029343826,0.00003507744],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0008823882,0.0001497201,0.00019103088,0.00015686676,0.00004860147,0.000042549793,0.0006075138,0.000072716226,0.0000166138],"category_scores_gemma":[0.0013149604,0.00007277536,0.00010467057,0.00013585135,0.00012305265,0.00008504246,0.000037391725,0.00027632635,0.000004502319],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0008905895,0.00013992234,0.009791169,0.00011178059,0.00069750095,0.00027454374,0.0007179815,0.73919326,0.11695569,0.0082041845,0.008022084,0.11500129],"study_design_scores_gemma":[0.010585689,0.00455968,0.09783989,0.007551147,0.00061262987,0.0006179793,0.0022036997,0.7803843,0.05763888,0.027026715,0.009109401,0.001869989],"about_ca_topic_score_codex":0.0000031104444,"about_ca_topic_score_gemma":0.000025361727,"teacher_disagreement_score":0.1131313,"about_ca_system_score_codex":0.00022446323,"about_ca_system_score_gemma":0.000030959098,"threshold_uncertainty_score":0.2967693},"labels":[],"label_agreement":null},{"id":"W2396743501","doi":"10.2514/6.2016-2709","title":"FQUROH: a Flight Demonstration Project for Airframe Noise Reduction Technology - Concept and Current Status","year":2016,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":13,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Japan Aerospace Exploration Agency; Mitacs","keywords":"Airframe; Current (fluid); Noise reduction; Computer science; Aeronautics; Reduction (mathematics); Noise (video); Systems engineering; Aerospace engineering; Engineering; Electrical engineering; Artificial intelligence; Mathematics","score_opus":0.00917857436420512,"score_gpt":0.24348546589983477,"score_spread":0.23430689153562967,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2396743501","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.2285795,0.00063293485,0.76784074,0.00030777272,0.0008950952,0.0005548456,0.000060631835,0.0004566429,0.00067182805],"genre_scores_gemma":[0.9885424,0.0005452869,0.010547347,0.000003089148,0.000108311026,0.00007922726,0.0000093911385,0.000019438034,0.00014551284],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99946064,0.0000037683844,0.00013770175,0.0001486504,0.00004902629,0.00020023166],"domain_scores_gemma":[0.99977076,0.000025163328,0.000019729398,0.00010939034,0.00004428248,0.000030684772],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00004084026,0.00009765719,0.00009133881,0.000090257316,0.00004301651,0.00001698856,0.00004174506,0.00008673531,0.000009859911],"category_scores_gemma":[0.00003522422,0.00006919719,0.000019051431,0.00008938894,0.000064968255,0.0000869728,0.000014862174,0.00006499529,0.0000031225152],"study_design_candidate":"design_other","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000016691,0.000042061212,0.00028178486,0.00009204597,0.000040382634,8.7832683e-7,0.000209509,0.0013290008,0.17702802,0.046627946,0.0057123783,0.7686193],"study_design_scores_gemma":[0.003687222,0.00061707984,0.0008311589,0.00031762352,0.00014642783,0.000078551275,0.00073190604,0.7494018,0.062107358,0.03168973,0.1489983,0.0013928612],"about_ca_topic_score_codex":0.000002003449,"about_ca_topic_score_gemma":0.000006171511,"teacher_disagreement_score":0.76722646,"about_ca_system_score_codex":0.000052434418,"about_ca_system_score_gemma":0.000021622067,"threshold_uncertainty_score":0.28217795},"labels":[],"label_agreement":null},{"id":"W2398352932","doi":"10.2514/6.2016-2821","title":"A Novel Numerical Approach for Generation and Propagation of Rotor-Stator Interaction Noise","year":2016,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Windsor","funders":"","keywords":"Stator; Rotor (electric); Computer science; Noise (video); Engineering; Electrical engineering; Artificial intelligence","score_opus":0.017667711450165026,"score_gpt":0.2267682483728927,"score_spread":0.20910053692272768,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2398352932","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.103700876,0.0000056947765,0.8954981,0.000018254495,0.00010791138,0.00022350256,0.000014986006,0.000036404825,0.00039427375],"genre_scores_gemma":[0.90890545,0.000007730748,0.090830825,0.000005212474,0.00009123515,0.000056104585,0.000012610888,0.000011800291,0.00007901554],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99969095,0.0000024196597,0.00011822187,0.00008042085,0.00004616051,0.00006180079],"domain_scores_gemma":[0.99983776,0.000022540064,0.000020967458,0.000057205245,0.000040695064,0.000020858612],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00005370934,0.000053500487,0.000065153254,0.000024527579,0.000015694617,0.000008855923,0.000022016935,0.00003267123,0.000006579485],"category_scores_gemma":[0.000024180543,0.000036538124,0.00001579869,0.000027040935,0.00000985141,0.00009106823,0.000006815134,0.000020162648,5.3853205e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000008818723,0.00002647113,0.0000603713,0.000054288947,0.000011488947,2.3176659e-8,0.000033094348,0.01651662,0.9656442,0.0026247487,0.00022992799,0.014789983],"study_design_scores_gemma":[0.00024854377,0.000028330587,0.00013308124,0.000006380756,0.0000066671237,0.0000015325501,0.000013040393,0.9814764,0.017841805,0.000034341992,0.00015074352,0.00005909716],"about_ca_topic_score_codex":0.000002562815,"about_ca_topic_score_gemma":0.0000013227005,"teacher_disagreement_score":0.9649598,"about_ca_system_score_codex":0.000027738937,"about_ca_system_score_gemma":0.000004216962,"threshold_uncertainty_score":0.14899814},"labels":[],"label_agreement":null},{"id":"W2401360519","doi":"10.2514/6.2016-2818","title":"Influence of Distortion on Fan Tonal Noise","year":2016,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke; Safran Electronics (Canada)","funders":"Grand Équipement National De Calcul Intensif","keywords":"Distortion (music); Acoustics; Noise (video); Computer science; Physics; Telecommunications; Artificial intelligence; Bandwidth (computing)","score_opus":0.003457086945358178,"score_gpt":0.18448590044435478,"score_spread":0.1810288134989966,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2401360519","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.94787425,0.0000042073416,0.043758538,0.000022981427,0.000076639335,0.000022597365,0.000009308919,0.00005407124,0.008177418],"genre_scores_gemma":[0.9992744,0.000015160796,0.0003094201,0.000014111655,0.000023763685,0.0000018760982,7.464971e-7,0.000007247735,0.00035330214],"study_design_codex":"simulation_or_modeling","study_design_gemma":"observational","domain_scores_codex":[0.9997278,0.00000162689,0.00008537806,0.000049223014,0.00006974053,0.00006625967],"domain_scores_gemma":[0.9998314,0.000024153498,0.000009344846,0.000097128,0.000016606293,0.000021412716],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000026865979,0.000043743385,0.00004680261,0.000018196426,0.000007917938,0.0000018391592,0.000051179864,0.000023079743,0.000051047697],"category_scores_gemma":[0.000015570498,0.000028231962,0.00001598371,0.000026129594,0.000016384429,0.000033037333,0.000007888193,0.000023667275,0.00003194487],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000007988971,0.000026696162,0.0027533171,0.000032147233,0.000014836567,0.0000018461236,0.000034586676,0.50945413,0.44915572,0.02020748,0.00086582714,0.01744542],"study_design_scores_gemma":[0.0014383859,0.00035577282,0.50028497,0.00048039283,0.000038887873,0.0000054849875,0.000027607466,0.2871009,0.193238,0.008937172,0.007023029,0.0010694063],"about_ca_topic_score_codex":0.0000027321482,"about_ca_topic_score_gemma":0.0000055301,"teacher_disagreement_score":0.49753165,"about_ca_system_score_codex":0.000027545564,"about_ca_system_score_gemma":0.0000028126437,"threshold_uncertainty_score":0.115126595},"labels":[],"label_agreement":null},{"id":"W2403911445","doi":"10.2514/6.2016-2816","title":"Several noise control of the trailing-edge noise of a Controlled-Diffusion airfoil","year":2016,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":17,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Airfoil; Trailing edge; Noise (video); Acoustics; Diffusion; Noise control; Computer science; Physics; Noise reduction; Mechanics; Artificial intelligence","score_opus":0.0037884684640610697,"score_gpt":0.1786570178884671,"score_spread":0.17486854942440605,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2403911445","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.82426924,0.00011464195,0.1649581,0.00019566117,0.00059846864,0.00036663143,0.00008489693,0.00008055928,0.009331803],"genre_scores_gemma":[0.99824756,0.00005139124,0.00037049444,0.000044650147,0.00006668703,0.000012024503,5.842021e-7,0.000025227697,0.0011813937],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999076,0.000024125055,0.00039853796,0.00011552968,0.0001906666,0.00019515883],"domain_scores_gemma":[0.99924827,0.00020843306,0.00007745316,0.00032948394,0.00008754911,0.000048825805],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018207335,0.0001472689,0.00037468417,0.000039539133,0.000030312594,0.0000050152557,0.00024341153,0.00008761973,0.00014755121],"category_scores_gemma":[0.00010018934,0.00007330989,0.00019988748,0.00008290387,0.00008735191,0.00004247708,0.000038209848,0.00008525445,0.0000069662974],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00022067495,0.00011497733,0.0015389606,0.00010956245,0.00014904761,0.0000018109918,0.00015658802,0.056610383,0.9282436,0.00578117,0.00074581214,0.0063274307],"study_design_scores_gemma":[0.011609536,0.0000679527,0.0042043817,0.00015088702,0.00010050836,0.0000031628665,0.000034162127,0.972749,0.009745927,0.00055394723,0.00054610043,0.00023444048],"about_ca_topic_score_codex":0.000011990467,"about_ca_topic_score_gemma":0.000028347287,"teacher_disagreement_score":0.9184977,"about_ca_system_score_codex":0.000022943348,"about_ca_system_score_gemma":0.000023640834,"threshold_uncertainty_score":0.2989491},"labels":[],"label_agreement":null},{"id":"W2404597545","doi":"10.1115/imece2014-38371","title":"Turbulence Measurements in the Corner Wall Jet","year":2014,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of New Brunswick","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Turbulence; Jet (fluid); Mechanics; Reynolds number; Physics; Optics; Materials science","score_opus":0.01714428650468543,"score_gpt":0.20444641827988536,"score_spread":0.18730213177519991,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2404597545","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.69048154,0.000076047254,0.06257327,0.0002619119,0.00060845714,0.00017688141,0.0000019478991,0.00018153594,0.24563842],"genre_scores_gemma":[0.9986212,0.000011974657,0.0008647422,0.0003197897,0.00004016861,0.000006632455,0.0000015190326,0.0000094886545,0.0001244332],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99956775,0.000014059279,0.00008918768,0.000067900895,0.00012999358,0.0001311249],"domain_scores_gemma":[0.999759,0.0000356819,0.0000056145946,0.00017195048,0.00001163563,0.000016072341],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00029596282,0.00006666541,0.000056595898,0.000016888838,0.000017445771,0.000020614656,0.00018777681,0.000028190178,0.000049469265],"category_scores_gemma":[0.00002604075,0.000041387986,0.000015423491,0.00006240702,0.000010415185,0.000025955285,0.000011457509,0.00009846973,0.000056531724],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00000637714,0.00012949792,0.033582,0.00012623692,0.000049919134,0.0000074289937,0.0014225264,0.864736,0.009172912,0.02579095,0.039312758,0.02566337],"study_design_scores_gemma":[0.00012032916,0.000008973281,0.0065806336,0.000010162078,0.0000035755902,0.0000012091517,0.000021988903,0.987026,0.00009343252,0.0011180878,0.0049168924,0.00009873485],"about_ca_topic_score_codex":0.000014472407,"about_ca_topic_score_gemma":0.0001051311,"teacher_disagreement_score":0.3081397,"about_ca_system_score_codex":0.000016993003,"about_ca_system_score_gemma":0.0000019343886,"threshold_uncertainty_score":0.16877532},"labels":[],"label_agreement":null},{"id":"W2405258003","doi":"10.2514/6.2016-2770","title":"Review of landing gear acoustic research at Messier-Bugatti-Dowty","year":2016,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Safran Electronics (Canada)","funders":"Chinese Academy of Agricultural Sciences","keywords":"Landing gear; Computer science; Aerospace engineering; Moon landing; Acoustics; Aeronautics; Engineering; Physics","score_opus":0.03816410596101399,"score_gpt":0.31407706777425215,"score_spread":0.27591296181323816,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2405258003","genre_codex":"other","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.19641615,0.094021715,0.25786695,0.0019965656,0.0026100355,0.00166055,0.00025517453,0.001221172,0.44395167],"genre_scores_gemma":[0.9461927,0.04771561,0.0012121544,0.0000642371,0.00010612742,0.000015120561,0.000003858845,0.000041221905,0.0046489653],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989309,0.000035801622,0.00026425312,0.00015232262,0.00028257104,0.00033419955],"domain_scores_gemma":[0.9991302,0.00030249215,0.000022437187,0.0003452906,0.00011711493,0.000082445986],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00079680525,0.00010771003,0.00021642644,0.000071881695,0.000060432994,0.0000074694703,0.00021318262,0.00006441382,0.0014841106],"category_scores_gemma":[0.00024519622,0.00006812119,0.00005632995,0.0002039456,0.00006975291,0.000052303207,0.00012844436,0.00013584204,0.00025288636],"study_design_candidate":"not_applicable","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000014934868,0.00006703753,0.0013767784,0.021235961,0.0001628234,0.00003537558,0.00009738321,0.002668111,0.5803573,0.0072076307,0.3587547,0.028021947],"study_design_scores_gemma":[0.0038524861,0.0005107982,0.005346269,0.114810586,0.00039711947,0.00012959121,0.00023430497,0.5226079,0.04822478,0.009469618,0.2910051,0.0034114125],"about_ca_topic_score_codex":0.000005914029,"about_ca_topic_score_gemma":0.00001790263,"teacher_disagreement_score":0.74977654,"about_ca_system_score_codex":0.00015227508,"about_ca_system_score_gemma":0.000016205062,"threshold_uncertainty_score":0.9994287},"labels":[],"label_agreement":null},{"id":"W2406743161","doi":"10.2514/6.2016-2962","title":"Noise Prediction of a Simplified High-Lift Device","year":2016,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Mitacs; Compute Canada","keywords":"Lift (data mining); Computer science; Noise (video); Acoustics; Artificial intelligence; Physics; Data mining","score_opus":0.00790577809941755,"score_gpt":0.1870899555752779,"score_spread":0.17918417747586035,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2406743161","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6472417,0.000020622118,0.34050897,0.00005896838,0.0004466545,0.00006884674,0.000077713776,0.00023883225,0.011337673],"genre_scores_gemma":[0.99725103,0.00004441858,0.0021486662,0.00001563789,0.00007224772,0.000004404966,0.0000033132421,0.000016218586,0.00044404317],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99959666,0.0000032598368,0.00014378082,0.00007279821,0.00007774115,0.000105772495],"domain_scores_gemma":[0.9997235,0.00004512342,0.000014002586,0.00015135513,0.000032366912,0.000033648685],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00005036763,0.00006544371,0.000082893144,0.000029326602,0.000012044904,0.0000039611673,0.000070754206,0.000047934413,0.00014591239],"category_scores_gemma":[0.000018536482,0.000043837434,0.000022767425,0.000055088236,0.000015513213,0.00004873201,0.000016486942,0.000031858417,0.000034003115],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00001182482,0.00004511053,0.0020266068,0.00013056371,0.000086427055,0.0000029758824,0.00006714596,0.035599194,0.89725965,0.028820746,0.0074981973,0.02845154],"study_design_scores_gemma":[0.002261079,0.00017016772,0.046130717,0.0002400513,0.00010522149,0.000008378609,0.00007550624,0.85148203,0.076015726,0.008351208,0.014517724,0.0006422042],"about_ca_topic_score_codex":0.000009305247,"about_ca_topic_score_gemma":0.0000121729345,"teacher_disagreement_score":0.82124394,"about_ca_system_score_codex":0.000022442986,"about_ca_system_score_gemma":0.000005033612,"threshold_uncertainty_score":0.17876387},"labels":[],"label_agreement":null},{"id":"W2407092545","doi":"10.2514/6.2016-2950","title":"Turbofan broadband noise predictions using a 3-D ZDES rotor blade approach","year":2016,"lang":"en","type":"preprint","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":6,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke; Safran Electronics (Canada)","funders":"","keywords":"Turbulence; Reynolds-averaged Navier–Stokes equations; Turbofan; Aeroacoustics; Acoustics; Mechanics; Physics; Rotor (electric); Computational fluid dynamics; Duct (anatomy); Noise (video); Homogeneous isotropic turbulence; Detached eddy simulation; Aerospace engineering; Sound pressure; Engineering; Computer science; Direct numerical simulation; Reynolds number","score_opus":0.016839336139990554,"score_gpt":0.22718844281957756,"score_spread":0.210349106679587,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2407092545","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.055602524,0.00028516867,0.8812438,0.000019767593,0.0019491975,0.00065184897,0.00037717837,0.00091209286,0.05895837],"genre_scores_gemma":[0.95546067,0.00018664975,0.04118582,0.000019408819,0.0012692586,0.00008122837,0.00008459336,0.00015897481,0.0015534211],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9984922,0.000018260731,0.00038470983,0.00045649853,0.00023736042,0.00041096442],"domain_scores_gemma":[0.99899024,0.00003737397,0.000062039595,0.00068870035,0.00006621442,0.0001554278],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00011790072,0.00042944503,0.0003786113,0.00015239764,0.00010853261,0.00013350208,0.0003829862,0.0004885539,0.00014372167],"category_scores_gemma":[0.000023520082,0.0003545777,0.00017475174,0.00008521102,0.000069810856,0.00007152602,0.00037685773,0.0006714505,0.000020723559],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000034548866,0.00004279808,0.00013471318,0.00036573343,0.0001910458,0.000003915717,0.0001285952,0.99152035,0.004458556,0.00064935104,0.0020039836,0.0004974889],"study_design_scores_gemma":[0.00018556266,0.000007319137,0.00015410183,0.00016997031,0.00010081667,0.000010817091,0.000034075223,0.99602854,0.00015594064,0.0018030002,0.0008711619,0.0004786868],"about_ca_topic_score_codex":0.000030577616,"about_ca_topic_score_gemma":0.000008119218,"teacher_disagreement_score":0.8998581,"about_ca_system_score_codex":0.00024078818,"about_ca_system_score_gemma":0.000064408094,"threshold_uncertainty_score":0.9998906},"labels":[],"label_agreement":null},{"id":"W2409431362","doi":"10.2514/6.2016-3948","title":"The effect of acoustic excitation on the later stages of transition in a laminar separation bubble","year":2016,"lang":"en","type":"article","venue":"46th AIAA Fluid Dynamics Conference","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":6,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Waterloo","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Bubble; Laminar flow; Separation (statistics); Excitation; Acoustics; Transition (genetics); Materials science; Mechanics; Physics; Computer science; Engineering; Electrical engineering; Chemistry","score_opus":0.005909065204767816,"score_gpt":0.21882819306766998,"score_spread":0.21291912786290218,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2409431362","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.85131335,0.000027854552,0.14740972,0.00019782835,0.0001628417,0.0002679654,0.00006397076,0.000026493432,0.0005300015],"genre_scores_gemma":[0.999526,0.00021581883,0.00007360363,0.0000070785413,0.000015452906,0.00003717673,0.00001566529,0.000018362349,0.00009080466],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991095,0.00009264891,0.00030333563,0.00012736139,0.00018877197,0.00017840184],"domain_scores_gemma":[0.9987197,0.0008546857,0.00006311388,0.00026226405,0.00007975993,0.000020470896],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00047502504,0.00014540814,0.00017465882,0.000060797734,0.0000534313,0.000020909067,0.00018914191,0.00007873859,0.000013877173],"category_scores_gemma":[0.00010691322,0.00007613203,0.000045267887,0.0001298164,0.00010633939,0.00007753789,0.000014378693,0.00011501703,0.000005767499],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000248088,0.000047314756,0.0019321775,0.00035712647,0.00007477304,0.0000049940245,0.0011583252,0.41166022,0.50577164,0.058359616,0.0001259966,0.020259742],"study_design_scores_gemma":[0.00036162828,0.00026050914,0.0037137012,0.00019258788,0.000019271392,7.6346527e-7,0.00006490937,0.9877671,0.0058623445,0.0016435746,0.0000082265215,0.000105377156],"about_ca_topic_score_codex":0.000009292797,"about_ca_topic_score_gemma":0.0002560007,"teacher_disagreement_score":0.5761069,"about_ca_system_score_codex":0.00008139621,"about_ca_system_score_gemma":0.000019333365,"threshold_uncertainty_score":0.31045744},"labels":[],"label_agreement":null},{"id":"W2414179684","doi":"10.1061/(asce)hy.1943-7900.0001182","title":"Turbulent Jet Approach to Predict Expansion Head Loss at Submerged Outlets","year":2016,"lang":"en","type":"article","venue":"Journal of Hydraulic Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Alberta","funders":"","keywords":"Head (geology); Turbulence; Jet (fluid); Geology; Mechanics; Hydraulic head; Environmental science; Meteorology; Hydrology (agriculture); Marine engineering; Geotechnical engineering; Physics; Engineering; Geomorphology","score_opus":0.008075503996269395,"score_gpt":0.19934781196626333,"score_spread":0.19127230796999395,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2414179684","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7033404,0.000381795,0.29411536,0.00029559224,0.0010839752,0.0001095398,0.000008109018,0.0001548023,0.0005103783],"genre_scores_gemma":[0.9917315,0.00022284487,0.007247075,0.000041822033,0.0005604937,0.0000073989836,0.0000016528716,0.000081447964,0.00010575508],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99846053,0.000010888675,0.0005583617,0.00015704229,0.00039702008,0.00041617212],"domain_scores_gemma":[0.99921715,0.000051351242,0.00007947841,0.00025894397,0.00008171656,0.00031135386],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00031052766,0.000264348,0.00036367666,0.00021946669,0.0000383193,0.00002351075,0.00030230926,0.000105813626,0.000019323359],"category_scores_gemma":[0.00009228053,0.00018522447,0.00015559157,0.00017012208,0.000014081658,0.00015828919,0.00006881388,0.00025282227,0.000029044642],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000017891412,0.000035003544,0.00026765116,0.00007934084,0.00008251083,0.00007047352,0.00015105517,0.88417023,0.109171055,0.000062554325,0.004342284,0.0015499423],"study_design_scores_gemma":[0.001764483,0.00025338313,0.007153747,0.00080106326,0.000093379706,0.0010840221,0.000029423347,0.93812567,0.0143557,0.000054574077,0.035401117,0.0008834475],"about_ca_topic_score_codex":0.0000012031313,"about_ca_topic_score_gemma":0.0000013275031,"teacher_disagreement_score":0.28839108,"about_ca_system_score_codex":0.00033370865,"about_ca_system_score_gemma":0.000015121276,"threshold_uncertainty_score":0.75532347},"labels":[],"label_agreement":null},{"id":"W2472847087","doi":"","title":"ANCL - Aeroacoustics and Noise Control Laboratory at UOIT","year":2016,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":true,"ca_institutions":"Ontario Tech University","funders":"","keywords":"Aeroacoustics; Noise control; Noise (video); Control (management); Noise exposure; Computational aeroacoustics; Business; Engineering; Acoustics; Computer science; Economics; Telecommunications; Management; Noise reduction; Physics","score_opus":0.0027750505398190465,"score_gpt":0.15368392093652095,"score_spread":0.1509088703967019,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2472847087","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.82863593,0.001168504,0.15688519,0.0004241606,0.002368185,0.0003809896,0.0047023385,0.00041083994,0.0050238594],"genre_scores_gemma":[0.99642617,0.00046746028,0.001437325,0.00048486097,0.00031511686,0.000011812105,0.000010887519,0.00009321464,0.00075312995],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99872726,0.000012190318,0.00023698044,0.0002415448,0.0001500467,0.000631963],"domain_scores_gemma":[0.9985941,0.00012360715,0.000029951227,0.00035872043,0.000119574,0.00077403587],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000121624966,0.00025747682,0.00023448018,0.00013725943,0.0001641997,0.000046262547,0.00018182365,0.00021067561,0.00015688081],"category_scores_gemma":[0.00014521647,0.00022475838,0.00003302026,0.00013717574,0.00014804561,0.00007458822,0.000031050684,0.0001570861,0.00011457181],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000018670577,0.000022914257,0.0048476895,0.0002528548,0.00021638426,0.00051156577,0.00017450041,0.081627674,0.7577783,0.002722344,0.13636443,0.015462702],"study_design_scores_gemma":[0.0031524268,0.000114488896,0.034412865,0.00020800918,0.00040783064,0.00007617466,0.0001088623,0.89310247,0.00058975036,0.0010997999,0.064648174,0.0020791763],"about_ca_topic_score_codex":0.00025057138,"about_ca_topic_score_gemma":0.0038491136,"teacher_disagreement_score":0.8114748,"about_ca_system_score_codex":0.0006449978,"about_ca_system_score_gemma":0.0001646557,"threshold_uncertainty_score":0.91653806},"labels":[],"label_agreement":null},{"id":"W2478720943","doi":"10.1108/hff-04-2015-0143","title":"Effect of airfoil leading edge waviness on flow structures and noise","year":2016,"lang":"en","type":"article","venue":"International Journal of Numerical Methods for Heat &amp Fluid Flow","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":15,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"University of British Columbia","keywords":"Airfoil; Waviness; Leading edge; Aerodynamics; Mach number; Angle of attack; Transonic; Trailing edge; Reynolds number; Computational fluid dynamics; Aerospace engineering; Mechanics; Physics; Computer science; Acoustics; Engineering; Turbulence; Mechanical engineering","score_opus":0.013757646045539916,"score_gpt":0.342796662241049,"score_spread":0.32903901619550907,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2478720943","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.13219434,0.0003270121,0.86395186,0.00021293735,0.0030366275,0.00010058717,0.000059924918,0.000022102782,0.000094628114],"genre_scores_gemma":[0.57692635,0.00020077119,0.42201525,0.000043363223,0.0007161229,0.000007145723,0.0000038478915,0.000046069195,0.00004107434],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9986205,0.00014039777,0.0005568983,0.0001549082,0.00032077258,0.00020653679],"domain_scores_gemma":[0.9971701,0.0021781954,0.000092957525,0.00013881102,0.0002886076,0.00013130794],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0009626924,0.00021888025,0.00048609157,0.00019795829,0.00003582806,0.00003127019,0.00034002707,0.000104801766,0.000043117347],"category_scores_gemma":[0.0011378143,0.0001393102,0.00021970274,0.00008076524,0.00006821146,0.00012657252,0.00004658623,0.00019572972,0.0000024414778],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00042710194,0.000031581116,0.00020535187,0.00009575027,0.00028139938,0.000007636386,0.000059155318,0.05184452,0.25432804,0.00039158986,0.0005292155,0.6917987],"study_design_scores_gemma":[0.0033867822,0.0014478499,0.0009044623,0.0006890872,0.00016624684,0.0002772147,0.000007915552,0.87801856,0.09852245,0.0061451816,0.009954469,0.00047976436],"about_ca_topic_score_codex":0.0000015777019,"about_ca_topic_score_gemma":3.444906e-7,"teacher_disagreement_score":0.8261741,"about_ca_system_score_codex":0.00013316015,"about_ca_system_score_gemma":0.000018483446,"threshold_uncertainty_score":0.5680905},"labels":[],"label_agreement":null},{"id":"W2484810407","doi":"10.2514/6.2016-4801","title":"Numerical Investigation of the Effect of Wing Position on the Aeroacoustic Field of a Propeller","year":2016,"lang":"en","type":"article","venue":"52nd AIAA/SAE/ASEE Joint Propulsion Conference","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Carleton University","funders":"Pratt and Whitney Canada","keywords":"Propeller; Wing; Acoustics; Propulsor; Position (finance); Marine engineering; Aerospace engineering; Engineering; Field (mathematics); Aeronautics; Computer science; Physics; Mathematics","score_opus":0.013004399093189055,"score_gpt":0.2102289880899683,"score_spread":0.19722458899677922,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2484810407","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9830428,0.000021850248,0.014329095,0.0008058073,0.00033466856,0.00057281693,0.000023356823,0.000034578687,0.0008350689],"genre_scores_gemma":[0.9994734,0.000020995945,0.0002939717,0.000042760985,0.000043518958,0.000029212122,0.0000028427894,0.00002132244,0.00007201158],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9986485,0.0001453462,0.00047333422,0.00018554815,0.0003673321,0.00017993206],"domain_scores_gemma":[0.9987048,0.00044870476,0.0002165489,0.00044231434,0.00014166649,0.00004598502],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00038012714,0.00019073852,0.00030120046,0.000057884048,0.000067326946,0.000012385356,0.00026933517,0.00010800731,0.00010494896],"category_scores_gemma":[0.0004947189,0.00008671506,0.00011432095,0.00019181972,0.0001536641,0.00007212531,0.000074555246,0.00021509094,0.000007605345],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000045143588,0.000022519034,0.0011078379,0.00036369206,0.000028913124,8.474964e-7,0.0001447894,0.005009549,0.9826301,0.0015034906,0.0003680907,0.008775045],"study_design_scores_gemma":[0.0005659798,0.0009301346,0.018014282,0.0025699225,0.000082032326,0.000005525243,0.000038686172,0.07197753,0.9037063,0.0018752798,0.000021663987,0.00021263423],"about_ca_topic_score_codex":0.000019408442,"about_ca_topic_score_gemma":0.0000053726667,"teacher_disagreement_score":0.07892376,"about_ca_system_score_codex":0.000040338604,"about_ca_system_score_gemma":0.000039102888,"threshold_uncertainty_score":0.35361376},"labels":[],"label_agreement":null},{"id":"W2488615062","doi":"10.1121/1.4958916","title":"Tonal noise of a controlled-diffusion airfoil at low angle of attack and Reynolds number","year":2016,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":32,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Acoustics; Reynolds number; Physics; Anechoic chamber; Noise (video); Airfoil; Jet (fluid); Amplitude; Aeroacoustics; Mechanics; Turbulence; Sound pressure; Optics; Computer science","score_opus":0.005708533482359084,"score_gpt":0.21821619916704568,"score_spread":0.2125076656846866,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2488615062","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8990128,0.00030064577,0.09916684,0.0008459967,0.00021678463,0.00011446944,0.00004410825,0.000008235397,0.0002900909],"genre_scores_gemma":[0.99059737,0.0016395866,0.007360424,0.000100824465,0.00010112113,7.109559e-7,1.8193174e-7,0.00002069568,0.00017907674],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9986879,0.000056950714,0.00058370334,0.00006710521,0.00041499184,0.00018934939],"domain_scores_gemma":[0.9982854,0.0007767414,0.00041797137,0.0002556366,0.00019101976,0.00007323293],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004410351,0.00014102331,0.0005284792,0.000012131437,0.00006403321,0.0000037357443,0.00036218157,0.00008731092,0.000106492305],"category_scores_gemma":[0.00017647748,0.00006430129,0.00037857075,0.00012082327,0.00069808617,0.000044771587,0.00019719175,0.00020821307,0.0000017529834],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00072300166,0.00023784528,0.0012904526,0.00027951793,0.0005889654,0.0000015149855,0.000807246,0.078968905,0.8815669,0.0000246976,0.026985142,0.008525831],"study_design_scores_gemma":[0.0050893733,0.0004286114,0.005381784,0.00072730286,0.000733949,0.000100891535,0.0006611538,0.977281,0.0077326912,0.0008472484,0.0007436841,0.00027232204],"about_ca_topic_score_codex":0.000007926726,"about_ca_topic_score_gemma":6.199223e-7,"teacher_disagreement_score":0.8983121,"about_ca_system_score_codex":0.000064492546,"about_ca_system_score_gemma":0.000031331398,"threshold_uncertainty_score":0.26221305},"labels":[],"label_agreement":null},{"id":"W2504097591","doi":"10.1016/j.jsv.2016.06.035","title":"Cascade trailing-edge noise modeling using a mode-matching technique and the edge-dipole theory","year":2016,"lang":"en","type":"article","venue":"Journal of Sound and Vibration","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":14,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Trailing edge; Cascade; Physics; Acoustics; Noise (video); Dipole; Optics; Diffraction; Leading edge; Wake; Computational physics; Mechanics; Computer science; Engineering","score_opus":0.011470967063254076,"score_gpt":0.23679135961874842,"score_spread":0.22532039255549435,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2504097591","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.44111136,0.00036050464,0.5582709,0.00004326695,0.0000847593,0.000046746456,0.0000020289474,0.00000997057,0.00007052011],"genre_scores_gemma":[0.99275315,0.00029544413,0.0066398513,0.000025579036,0.00025806142,0.0000012953609,2.7092238e-7,0.000017313236,0.000009056473],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994473,0.000033340184,0.00026282747,0.00006209102,0.000093822455,0.00010060629],"domain_scores_gemma":[0.99965304,0.000121220626,0.00007746768,0.00006214169,0.000044272474,0.000041883424],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005834776,0.00009218987,0.00014300128,0.00005751351,0.00012972554,0.000078711775,0.00005848122,0.00006451991,0.0000028054194],"category_scores_gemma":[0.000037504546,0.000051041556,0.00004166852,0.00003782239,0.000053876447,0.000298585,0.000017780183,0.00015855615,2.395897e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00007825817,0.000011170218,0.000027954124,0.00005997001,0.000056573484,0.0000044762246,0.0013993246,0.6388021,0.33785304,0.014218952,0.000007770258,0.0074803843],"study_design_scores_gemma":[0.00045192314,0.000014583819,0.000008477922,0.00011874727,0.00003744953,0.00010552946,0.00017014758,0.9047535,0.0009068662,0.09334584,0.00000941379,0.000077496654],"about_ca_topic_score_codex":0.0000027880494,"about_ca_topic_score_gemma":0.0000026282084,"teacher_disagreement_score":0.55164176,"about_ca_system_score_codex":0.000024083909,"about_ca_system_score_gemma":0.000014299139,"threshold_uncertainty_score":0.20814142},"labels":[],"label_agreement":null},{"id":"W2506727889","doi":"10.1177/0957650915623669","title":"A numerical and experimental test-bed for low-speed fans","year":2016,"lang":"en","type":"article","venue":"Proceedings of the Institution of Mechanical Engineers Part A Journal of Power and Energy","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Airfoil; Mach number; Wake; Reynolds number; Trailing edge; Noise (video); Inviscid flow; Mechanics; Rotational speed; Rotation (mathematics); Engineering; Physics; Aerospace engineering; Geometry; Turbulence; Mathematics; Computer science; Mechanical engineering","score_opus":0.005309442615127472,"score_gpt":0.19876698723616668,"score_spread":0.1934575446210392,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2506727889","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.91484505,0.00071915315,0.08232057,0.00031515717,0.0011004189,0.00009277527,0.000027473794,0.000029143952,0.0005502303],"genre_scores_gemma":[0.9984077,0.0001667788,0.001294038,0.000016877026,0.00007668297,0.0000024911938,1.5505326e-7,0.00001290696,0.000022328806],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9992552,0.0000016609063,0.00036918375,0.000078862,0.00016323723,0.00013187535],"domain_scores_gemma":[0.99952936,0.000074010524,0.0001235303,0.000040132756,0.0001436739,0.000089274545],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016803246,0.000116681935,0.0002467649,0.00005895672,0.00003628949,0.000009724337,0.00013684256,0.00007673212,0.0000058952824],"category_scores_gemma":[0.00020681876,0.00007055711,0.000100204874,0.00007506787,0.00008099635,0.00012990498,0.000033443765,0.00007577074,5.8280506e-8],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000089923,0.00008745566,0.000027834987,0.00009666632,0.00009121484,6.55817e-7,0.00013239856,0.0046127625,0.91725177,0.07605345,0.0005412017,0.0010146531],"study_design_scores_gemma":[0.0028308393,0.00091975444,0.00006190236,0.000810534,0.00010907887,0.00013722616,0.00028478084,0.14413996,0.8428818,0.0028498096,0.004635444,0.00033888753],"about_ca_topic_score_codex":0.0000011904599,"about_ca_topic_score_gemma":1.4921375e-7,"teacher_disagreement_score":0.13952719,"about_ca_system_score_codex":0.000032418502,"about_ca_system_score_gemma":0.000015685691,"threshold_uncertainty_score":0.28772354},"labels":[],"label_agreement":null},{"id":"W2510660552","doi":"10.1063/1.4961199","title":"Large eddy simulation of the near-field vortex dynamics in starting square jet transitioning into steady state","year":2016,"lang":"en","type":"article","venue":"Physics of Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":20,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Windsor; University of Waterloo","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Physics; Vortex; Vortex ring; Mechanics; Jet (fluid); Turbulence; Vorticity; Reynolds number; Strouhal number; Nozzle; Classical mechanics; Reynolds stress; Large eddy simulation; Thermodynamics","score_opus":0.00628409178994941,"score_gpt":0.22687059298940349,"score_spread":0.22058650119945408,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2510660552","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.60164195,0.00001794705,0.3979079,0.00003770203,0.000106584856,0.000075507385,0.000054440345,0.00002015215,0.00013779239],"genre_scores_gemma":[0.9989295,0.0000126094465,0.000959794,0.000013919875,0.000036579233,0.0000035724916,0.00000770608,0.00002695504,0.000009387043],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992103,0.000021508673,0.00030012487,0.000106917585,0.00017738005,0.00018378705],"domain_scores_gemma":[0.9994289,0.00017981796,0.00005933652,0.00023181914,0.00007807364,0.000022006516],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016989144,0.00011483753,0.00017788618,0.00002443237,0.000046622838,0.000010751786,0.00014060634,0.000047974307,0.0000077742325],"category_scores_gemma":[0.000045633264,0.00008499318,0.0000707884,0.00017931833,0.000034711597,0.00013784473,0.00003566581,0.000119019045,0.000001358127],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000009112634,0.000040632065,0.005495819,0.00013202637,0.000021089822,5.0956055e-7,0.0016305664,0.95162976,0.03009597,0.0028897084,0.000007879564,0.0080469055],"study_design_scores_gemma":[0.0003110586,0.000027913655,0.00088693266,0.0001824152,0.00001179953,4.8266646e-8,0.0001792094,0.9832335,0.004082281,0.010969941,0.000008911026,0.00010597655],"about_ca_topic_score_codex":0.000027141688,"about_ca_topic_score_gemma":0.00019237195,"teacher_disagreement_score":0.39728752,"about_ca_system_score_codex":0.00009246326,"about_ca_system_score_gemma":0.000020037942,"threshold_uncertainty_score":0.34659213},"labels":[],"label_agreement":null},{"id":"W2516400425","doi":"10.11372/souonseigyo1977.31.102","title":"A Boeing Program for Aircraft Noise Reduction","year":2007,"lang":"en","type":"article","venue":"The journal of the INCE of Japan","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Boeing (Canada)","funders":"","keywords":"Aircraft noise; Reduction (mathematics); Noise reduction; Aeronautics; Noise (video); Acoustics; Computer science; Aerospace engineering; Engineering; Physics; Mathematics; Artificial intelligence; Geometry","score_opus":0.006910226100655397,"score_gpt":0.2399394226087929,"score_spread":0.2330291965081375,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2516400425","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9791164,0.00016793088,0.019032056,0.00022459298,0.00090486533,0.00017150081,0.000001976837,0.000017055905,0.00036362908],"genre_scores_gemma":[0.99329764,0.000046833255,0.0062171933,0.000009747946,0.00033520928,0.0000011159431,1.535089e-7,0.000016164213,0.000075965676],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99937636,0.000012125371,0.00029916447,0.000027923119,0.00014755456,0.00013689873],"domain_scores_gemma":[0.9994696,0.00007910996,0.00016901888,0.00015695057,0.000097789714,0.00002756725],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0010127217,0.00006659521,0.00011182207,0.000035651734,0.000070858114,0.000009669072,0.00032817185,0.000034608165,0.0000021660376],"category_scores_gemma":[0.00006264374,0.000037756374,0.000098167846,0.00009942273,0.00005568315,0.000058109952,0.000026167254,0.00019721019,3.9704884e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00023313369,0.00014347286,0.0005619612,0.00019186141,0.00022180262,0.0000011088568,0.0021394535,0.49168697,0.38719973,0.0006552709,0.002479159,0.11448606],"study_design_scores_gemma":[0.0027905472,0.0015262063,0.021284422,0.001526511,0.001012681,0.0012128123,0.0052882074,0.78648007,0.14639564,0.019244887,0.012394286,0.00084374857],"about_ca_topic_score_codex":0.0000062445374,"about_ca_topic_score_gemma":0.000012668334,"teacher_disagreement_score":0.29479307,"about_ca_system_score_codex":0.000052911797,"about_ca_system_score_gemma":0.000015765989,"threshold_uncertainty_score":0.15396602},"labels":[],"label_agreement":null},{"id":"W2525448906","doi":"10.1121/1.4963092","title":"Direct noise simulation of a canonical high lift device and comparison with an analytical model","year":2016,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":11,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Noise (video); Lift (data mining); Computer simulation; Numerical analysis; Computer science; Finite element method; Acoustics; Trailing edge; Compressibility; Diffraction; Near and far field; Mechanics; Physics; Mathematics; Mathematical analysis; Optics; Simulation; Structural engineering; Engineering","score_opus":0.01415131216833027,"score_gpt":0.2582671560241889,"score_spread":0.24411584385585866,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2525448906","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.3388924,0.000066296656,0.66043705,0.00043444324,0.00003633742,0.000051236577,0.00001483914,0.000008451825,0.000058913785],"genre_scores_gemma":[0.96938986,0.00016406269,0.03026161,0.0000870723,0.00006511786,3.4209398e-7,2.1840331e-7,0.000018864932,0.00001283224],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99892527,0.000055446413,0.00041909624,0.000072264105,0.00035854313,0.0001694019],"domain_scores_gemma":[0.9985328,0.0007464215,0.00021879011,0.00023564046,0.00016745391,0.00009894308],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00033421203,0.00012545331,0.00037930568,0.00001327864,0.000060296097,0.000008029959,0.00030195015,0.00006620587,0.000008240742],"category_scores_gemma":[0.00009283422,0.000054414326,0.00012228769,0.00013848796,0.00052190706,0.00007572748,0.000069119684,0.00024105617,2.69764e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000105714826,0.000062785766,0.00022847833,0.00003012364,0.00012619092,2.4625396e-7,0.00017959591,0.9860719,0.0093690595,0.00001656321,0.0003011925,0.0035081387],"study_design_scores_gemma":[0.00034411452,0.00024512355,0.00096222956,0.000091817616,0.0003270532,0.000006370989,0.00014949069,0.9972492,0.0002650498,0.0002416664,0.00003274109,0.00008514681],"about_ca_topic_score_codex":0.000017261425,"about_ca_topic_score_gemma":0.0000026431844,"teacher_disagreement_score":0.63049746,"about_ca_system_score_codex":0.00005077488,"about_ca_system_score_gemma":0.00005548316,"threshold_uncertainty_score":0.22189517},"labels":[],"label_agreement":null},{"id":"W2556102123","doi":"10.1016/j.euromechflu.2016.10.008","title":"Aeroacoustic study of an axial engine cooling module using lattice-Boltzmann simulations and the Ffowcs Williams and Hawkings’ analogy","year":2016,"lang":"en","type":"article","venue":"European Journal of Mechanics - B/Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":34,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Stator; Acoustics; Anechoic chamber; Rotor (electric); Noise (video); Sound pressure; Aerodynamics; Spectral density; Lattice Boltzmann methods; Engineering; Physics; Mechanics; Computer science; Mechanical engineering","score_opus":0.015923476411792002,"score_gpt":0.22902965046000703,"score_spread":0.21310617404821502,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2556102123","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.61349636,0.0002622887,0.3857457,0.000014818997,0.00032733087,0.000099173725,0.000012962562,0.000016185151,0.000025130867],"genre_scores_gemma":[0.99368495,0.00023967912,0.005670481,0.000016301316,0.00030570535,3.4681332e-7,9.711855e-7,0.00007054737,0.000010998306],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.998406,0.00025216932,0.00069382635,0.0001573424,0.0002679365,0.0002227598],"domain_scores_gemma":[0.998968,0.00024423943,0.00021054846,0.0002517804,0.00019784227,0.00012757826],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0014904465,0.00020256471,0.0003934993,0.00015795762,0.00014398718,0.000057243633,0.00025286045,0.000039877465,0.000010030262],"category_scores_gemma":[0.00020095037,0.0001328262,0.000058121725,0.00014218298,0.00006606258,0.00019880409,0.000105232524,0.0002610731,6.507429e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00016129922,0.00015687144,0.00012811995,0.00005532963,0.00036380094,0.0001293704,0.0015568677,0.9017876,0.08301052,0.0024652886,0.000017153736,0.010167778],"study_design_scores_gemma":[0.0028778946,0.00043567052,0.00034914116,0.00011918949,0.00029873406,0.00012694947,0.00029942297,0.9943269,0.00014582349,0.0008173593,0.00003157734,0.00017133493],"about_ca_topic_score_codex":0.0000031862855,"about_ca_topic_score_gemma":0.000006812961,"teacher_disagreement_score":0.38018858,"about_ca_system_score_codex":0.000035709745,"about_ca_system_score_gemma":0.000017027953,"threshold_uncertainty_score":0.5416495},"labels":[],"label_agreement":null},{"id":"W2559830481","doi":"10.1115/fedsm2016-7672","title":"Characteristics of Twin Jets in the Vicinity of a Free Surface","year":2016,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Manitoba","funders":"","keywords":"Turbulence; Mechanics; Reynolds number; Reynolds stress; Nozzle; Body orifice; Turbulence kinetic energy; Physics; Free surface; Entrainment (biomusicology); Optics; Materials science; Thermodynamics","score_opus":0.00867163985421504,"score_gpt":0.2037399206075156,"score_spread":0.19506828075330057,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2559830481","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97894186,0.000014019465,0.015180987,0.00012315119,0.000090243564,0.000057249435,0.000056611247,0.00001711408,0.0055187764],"genre_scores_gemma":[0.9988327,0.00009366009,0.000963051,0.000014499238,0.000021406293,8.5478837e-7,8.8408814e-7,0.000008276828,0.00006467969],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.9995583,0.00001205353,0.00019610007,0.000047125563,0.000094157826,0.00009221958],"domain_scores_gemma":[0.9995066,0.00015715709,0.000026408137,0.0002710356,0.000027003363,0.000011798269],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00019020036,0.00005786887,0.00012067855,0.000023632707,0.000005364875,0.0000023566986,0.00021953435,0.000036052104,0.000041360167],"category_scores_gemma":[0.00010694044,0.000031268988,0.000022680404,0.00009223495,0.000031987878,0.000021537597,0.000031062336,0.000051470408,0.0000031905167],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000044742486,0.00037671244,0.092838995,0.00068856566,0.000108455744,0.000024401934,0.0023643665,0.018780982,0.79048127,0.05973558,0.0046906862,0.029865244],"study_design_scores_gemma":[0.0019994238,0.00018096002,0.7027698,0.00040435774,0.000044602282,0.0000070053948,0.00036085083,0.2449562,0.033599395,0.0132203605,0.0018454588,0.0006115693],"about_ca_topic_score_codex":0.000028813129,"about_ca_topic_score_gemma":0.000052843752,"teacher_disagreement_score":0.7568819,"about_ca_system_score_codex":0.000014537313,"about_ca_system_score_gemma":0.000009565487,"threshold_uncertainty_score":0.12751123},"labels":[],"label_agreement":null},{"id":"W2560037457","doi":"10.1115/fedsm2016-7674","title":"Effects of Reynolds Number on Turbulent Characteristics of Surface Jet","year":2016,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Manitoba","funders":"","keywords":"Reynolds number; Turbulence; Mechanics; Jet (fluid); Magnetic Reynolds number; Reynolds-averaged Navier–Stokes equations; Reynolds stress; Physics; Reynolds decomposition; Reynolds stress equation model; Turbulence kinetic energy; Reynolds equation","score_opus":0.0034406734048948967,"score_gpt":0.19161026654753277,"score_spread":0.18816959314263787,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2560037457","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9815837,0.000012114413,0.012250846,0.000029648218,0.00030827304,0.00008145896,0.000021545866,0.000058097634,0.0056543243],"genre_scores_gemma":[0.9978205,0.00014106635,0.0012205946,0.000012343997,0.00003314908,0.000001512089,0.0000016560755,0.00002334429,0.00074586045],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9994618,0.0000075002877,0.00020152486,0.00008277915,0.00011932825,0.00012701222],"domain_scores_gemma":[0.9995154,0.00018488806,0.00003795341,0.00018726189,0.00004052447,0.0000339519],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000060647562,0.00010343621,0.0001895882,0.000015290465,0.000006990056,0.000002648707,0.00009564667,0.00006423547,0.0001090313],"category_scores_gemma":[0.000038088183,0.00006667607,0.000044162276,0.00004599044,0.000027458404,0.000021025773,0.00001940586,0.00004811316,0.000043657084],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000043868673,0.00024221052,0.008814216,0.0012890873,0.00017578335,0.00002537732,0.00013391812,0.0061466447,0.9434333,0.019287286,0.0076005273,0.012807825],"study_design_scores_gemma":[0.0018261415,0.00031987543,0.08257416,0.0011370224,0.000107925815,0.000008226869,0.00001470344,0.08749577,0.8202002,0.0012181873,0.0042839204,0.0008138382],"about_ca_topic_score_codex":0.0000036712286,"about_ca_topic_score_gemma":8.9389033e-7,"teacher_disagreement_score":0.12323302,"about_ca_system_score_codex":0.00002463636,"about_ca_system_score_gemma":0.0000047980375,"threshold_uncertainty_score":0.2718971},"labels":[],"label_agreement":null},{"id":"W2560455985","doi":"10.1115/fedsm2016-7673","title":"Reynolds Number Effects on the Characteristics of Twin Jets Interacting With a Free Surface","year":2016,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Manitoba","funders":"","keywords":"Reynolds number; Turbulence; Mechanics; Jet (fluid); Nozzle; Body orifice; Physics; Particle image velocimetry; Free surface; Thermodynamics; Mechanical engineering","score_opus":0.004814641670596489,"score_gpt":0.19143360201669457,"score_spread":0.1866189603460981,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2560455985","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9694202,0.0000035703085,0.016304173,0.00024395254,0.00036066413,0.00011207015,0.00001633875,0.000094406714,0.013444608],"genre_scores_gemma":[0.9975995,0.00001822195,0.0016751195,0.00004708753,0.000070321985,0.0000042529496,9.583168e-7,0.000035286183,0.00054924504],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99942636,0.000016382002,0.00015392697,0.00010440779,0.00013116686,0.00016772898],"domain_scores_gemma":[0.9985541,0.0009495007,0.000042763826,0.0003831106,0.000039532682,0.000031003463],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012614547,0.00012837895,0.00014602493,0.000012318726,0.000027892653,0.000016152273,0.00019857266,0.000045682875,0.00013364335],"category_scores_gemma":[0.00018816855,0.00006023035,0.000029308554,0.00006464354,0.000027120494,0.00004569881,0.000047564856,0.00011984346,0.000050825944],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0003338498,0.0003114113,0.06300132,0.0012187622,0.0009956458,0.00017185269,0.0017765347,0.014469497,0.71274406,0.054741308,0.045448884,0.10478686],"study_design_scores_gemma":[0.005367068,0.0010828145,0.08637222,0.008367162,0.00029754464,0.00010098836,0.00048659992,0.51234883,0.36829302,0.0038696325,0.01045554,0.0029585985],"about_ca_topic_score_codex":0.0000068932177,"about_ca_topic_score_gemma":0.000011376102,"teacher_disagreement_score":0.4978793,"about_ca_system_score_codex":0.000032854325,"about_ca_system_score_gemma":0.000006007352,"threshold_uncertainty_score":0.24561225},"labels":[],"label_agreement":null},{"id":"W2567377090","doi":"10.1016/j.cja.2016.12.010","title":"Experimental investigation on a cavity-step-actuated supersonic oscillating jet","year":2016,"lang":"en","type":"article","venue":"Chinese Journal of Aeronautics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":14,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"Natural Science Foundation of Jiangsu Province","keywords":"Supersonic speed; Jet (fluid); Wind tunnel; Nozzle; Mechanics; Supersonic wind tunnel; Schlieren; Amplitude; Physics; Optics; Acoustics; Materials science; Thermodynamics","score_opus":0.014187052076089699,"score_gpt":0.23082285963781887,"score_spread":0.21663580756172918,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2567377090","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9917632,0.00020008674,0.006410043,0.00016637739,0.0009118721,0.00006032682,0.000012752472,0.000052131447,0.00042323276],"genre_scores_gemma":[0.99625564,0.00006302237,0.0031620183,0.00006077087,0.0003655304,0.0000010483885,0.0000023527593,0.00004442615,0.000045223525],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989131,0.00002549791,0.00043640521,0.00009822464,0.00030746943,0.0002193026],"domain_scores_gemma":[0.99931896,0.00015287416,0.00013129899,0.00015834096,0.00009310247,0.00014540224],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023716096,0.0002175517,0.00026457,0.00011067172,0.00006810032,0.00003249401,0.00017708418,0.00009057082,0.00005124946],"category_scores_gemma":[0.0001789884,0.00012726986,0.000102477316,0.00014576653,0.000062260704,0.00017552711,0.000028892478,0.00024627807,0.000016677583],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000055012864,0.0000873454,0.009597217,0.0000516871,0.0001578872,0.00006947058,0.0011215365,0.027842095,0.9530279,0.0005923311,0.0014025538,0.0059949486],"study_design_scores_gemma":[0.008677468,0.0026236186,0.033924244,0.0019721696,0.00022393659,0.00075611763,0.00080972596,0.80438966,0.13737088,0.0045006834,0.002601841,0.002149632],"about_ca_topic_score_codex":0.0000013254454,"about_ca_topic_score_gemma":0.000003857342,"teacher_disagreement_score":0.815657,"about_ca_system_score_codex":0.00025604916,"about_ca_system_score_gemma":0.000039180693,"threshold_uncertainty_score":0.5189915},"labels":[],"label_agreement":null},{"id":"W2568135482","doi":"10.21205/deufmd.2017195523","title":"KAVİTE - KANAT KESİTİ ETKİLEŞİMİNİN AEROAKUSTİK ANALİZİ","year":2017,"lang":"tr","type":"article","venue":"Deu Muhendislik Fakultesi Fen ve Muhendislik","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Stantec (Canada)","funders":"","keywords":"Materials science","score_opus":0.01760649350512614,"score_gpt":0.25769159726683644,"score_spread":0.2400851037617103,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2568135482","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.69542426,0.01833575,0.015811933,0.003137855,0.039121352,0.005031708,0.010195296,0.0035381,0.20940377],"genre_scores_gemma":[0.9713408,0.0031697063,0.008533914,0.00058524736,0.004300726,0.00020170806,0.00091742084,0.0012078382,0.009742691],"study_design_codex":"not_applicable","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.98493135,0.00034034956,0.0032799991,0.0037012352,0.002666458,0.0050805886],"domain_scores_gemma":[0.98768836,0.00060976495,0.0019420556,0.006927012,0.0007495103,0.0020833095],"candidate_categories":["metaepi_narrow","sts","scholarly_communication","open_science","research_integrity","insufficient_payload"],"consensus_categories":["metaepi_narrow","research_integrity","insufficient_payload"],"category_scores_codex":[0.0018256236,0.0036505992,0.0032342265,0.0011326094,0.0045296936,0.0039150845,0.006808587,0.002237103,0.0034029128],"category_scores_gemma":[0.0011822551,0.004068664,0.0017776963,0.00092241284,0.0016431217,0.0021354249,0.0024640993,0.0039492473,0.0046289396],"study_design_candidate":"not_applicable","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0015754792,0.005876326,0.10571891,0.009134053,0.01569989,0.012341808,0.021719228,0.035049886,0.013650693,0.15707842,0.36724195,0.25491336],"study_design_scores_gemma":[0.015751584,0.0014914826,0.21604043,0.0038176621,0.0071313847,0.0007622309,0.007851784,0.4022268,0.0029192788,0.014024383,0.3095684,0.018414553],"about_ca_topic_score_codex":0.0018036,"about_ca_topic_score_gemma":0.0018386288,"teacher_disagreement_score":0.36717692,"about_ca_system_score_codex":0.0015234172,"about_ca_system_score_gemma":0.000470406,"threshold_uncertainty_score":0.9990582},"labels":[],"label_agreement":null},{"id":"W2580149798","doi":"10.1615/ichmt.2015.thmt-15.650","title":"Turbulent characteristics of surface attaching jet influenced by nozzle geometry","year":2015,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Manitoba","funders":"","keywords":"Nozzle; Reynolds number; Particle image velocimetry; Turbulence; Jet (fluid); Mechanics; Geometry; Entrainment (biomusicology); Physics; Reynolds stress; Materials science; Optics; Mathematics; Acoustics; Thermodynamics","score_opus":0.00963872697897313,"score_gpt":0.22486766440684505,"score_spread":0.2152289374278719,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2580149798","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.95641005,0.00011938963,0.04045736,0.000026924306,0.0003389994,0.00006425993,0.000056448178,0.00013875085,0.002387831],"genre_scores_gemma":[0.99503493,0.000043021006,0.0044717537,0.000044479784,0.000039746665,0.0000012768865,0.00003386962,0.000029712972,0.000301225],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99921066,0.00000828795,0.00027746573,0.00011177833,0.00019150392,0.00020030752],"domain_scores_gemma":[0.99952066,0.000032135566,0.000042184027,0.00021644823,0.000074649266,0.00011393842],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018775972,0.00013632799,0.00020355823,0.000034159773,0.000019390316,0.00002305564,0.00016751098,0.00007712779,0.000039711023],"category_scores_gemma":[0.000059755905,0.00012531262,0.000035203087,0.00012784486,0.00002584012,0.00007663302,0.000044978155,0.00015378244,0.000028205335],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000017950453,0.00018012305,0.030352777,0.00036399902,0.00018520269,0.000027365786,0.0008099338,0.7128703,0.20742412,0.001932346,0.040729858,0.005105996],"study_design_scores_gemma":[0.00042074718,0.000056359204,0.003802377,0.000040373678,0.00002620709,0.000007558908,0.00013162817,0.9836746,0.006410676,0.00015792402,0.00485608,0.0004155084],"about_ca_topic_score_codex":0.00003042631,"about_ca_topic_score_gemma":0.0000026892208,"teacher_disagreement_score":0.27080423,"about_ca_system_score_codex":0.000055894623,"about_ca_system_score_gemma":0.0000144900905,"threshold_uncertainty_score":0.51101005},"labels":[],"label_agreement":null},{"id":"W2586612119","doi":"10.1615/ichmt.2015.thmt-15.340","title":"Low Reynolds number effects on jets issuing from round and elliptic orifices","year":2015,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Manitoba","funders":"","keywords":"Reynolds number; Body orifice; Mechanics; Jet (fluid); Turbulence; Particle image velocimetry; Ellipse; Nozzle; Physics; Aspect ratio (aeronautics); Mathematics; Geometry; Mechanical engineering; Thermodynamics; Engineering","score_opus":0.008671003587064017,"score_gpt":0.21268981974842752,"score_spread":0.2040188161613635,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2586612119","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9624535,0.00019428965,0.008317758,0.000025250436,0.0009779913,0.00008714469,0.0000057734806,0.00022474116,0.027713573],"genre_scores_gemma":[0.9953162,0.000060857466,0.0033647267,0.00006150508,0.00030856126,0.000005402097,0.000009442852,0.000037419883,0.000835897],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99935997,0.000010902182,0.00011819538,0.0001745813,0.00014314978,0.00019322248],"domain_scores_gemma":[0.9994892,0.00015377442,0.000013816262,0.00019829176,0.00002236669,0.00012255921],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00009226171,0.00015049597,0.00014833399,0.00002341922,0.000032651962,0.000089798625,0.000088246976,0.00009249709,0.000045637466],"category_scores_gemma":[0.000036158173,0.00013337047,0.000019903433,0.00006154258,0.000015980777,0.00008849423,0.000028499302,0.00014076981,0.00023616954],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00016163007,0.00048753622,0.028958911,0.0016704785,0.0010354895,0.0007171508,0.006740041,0.57695395,0.08082926,0.038389742,0.08474268,0.17931314],"study_design_scores_gemma":[0.00080367527,0.000093649905,0.0021367606,0.0001870034,0.000051772262,0.0000065550844,0.00017239507,0.9771731,0.00793842,0.0048139147,0.00605043,0.0005723189],"about_ca_topic_score_codex":0.000051258237,"about_ca_topic_score_gemma":0.00003400385,"teacher_disagreement_score":0.40021917,"about_ca_system_score_codex":0.000054314645,"about_ca_system_score_gemma":0.0000059321874,"threshold_uncertainty_score":0.543869},"labels":[],"label_agreement":null},{"id":"W2587073992","doi":"10.2514/6.2017-0130","title":"A Discrete Adjoint Approach for Jet-Flap Interaction Noise Reduction","year":2017,"lang":"en","type":"article","venue":"58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":11,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Reduction (mathematics); Noise reduction; Jet noise; Noise (video); Jet (fluid); Acoustics; Computer science; Physics; Mathematics; Computer vision; Mechanics; Geometry","score_opus":0.015524466915566049,"score_gpt":0.25016108389158365,"score_spread":0.2346366169760176,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2587073992","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9189465,0.00013438285,0.06670749,0.00012281998,0.009391959,0.0011832231,0.0019097828,0.00036463712,0.0012391737],"genre_scores_gemma":[0.98093706,0.0003677276,0.01585988,0.000026347469,0.0011817119,0.00010841226,0.0011418624,0.00012775103,0.00024923382],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99711376,0.000059249367,0.00081209233,0.0008883404,0.00032064997,0.0008059046],"domain_scores_gemma":[0.9979202,0.000045224653,0.000462202,0.0010536469,0.00024871595,0.000269977],"candidate_categories":["metaepi_narrow","scholarly_communication"],"consensus_categories":[],"category_scores_codex":[0.00024650275,0.00080302596,0.0008844184,0.00016355509,0.0009072805,0.0013238974,0.0007617535,0.00042773475,0.00014562662],"category_scores_gemma":[0.00015878503,0.00070735306,0.00016495198,0.00005714644,0.00041214906,0.0007375132,0.00028167234,0.00043110628,0.000003830533],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0017166653,0.00006123699,0.00077957055,0.005447808,0.0012623478,0.000041875992,0.002603441,0.021577852,0.41194615,0.4001771,0.0020983259,0.15228763],"study_design_scores_gemma":[0.0023998758,0.000236896,0.04070259,0.00022819304,0.00033835342,0.00034481913,0.0006384229,0.88251233,0.01217844,0.05777154,0.00048260659,0.0021659262],"about_ca_topic_score_codex":0.00034229242,"about_ca_topic_score_gemma":0.00025352312,"teacher_disagreement_score":0.8609345,"about_ca_system_score_codex":0.0002358393,"about_ca_system_score_gemma":0.00005955081,"threshold_uncertainty_score":0.9997128},"labels":[],"label_agreement":null},{"id":"W2588558552","doi":"10.1063/1.4975155","title":"Free surface effects on the statistical properties of a submerged rectangular jet","year":2017,"lang":"en","type":"article","venue":"Physics of Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":10,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Manitoba","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Physics; Froude number; Turbulence; Mechanics; Nozzle; Turbulence kinetic energy; Reynolds number; Particle image velocimetry; Reynolds stress; Jet (fluid); Mean flow; Free surface; Optics; Flow (mathematics); Thermodynamics","score_opus":0.014971990971487676,"score_gpt":0.2169983560340597,"score_spread":0.20202636506257202,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2588558552","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98492926,0.00015178017,0.012784625,0.00008104921,0.00029586177,0.00015605293,0.00009579813,0.000031951422,0.0014735963],"genre_scores_gemma":[0.99869996,0.000049956965,0.0010998336,0.000007527636,0.00008825431,0.0000063530074,0.0000025533461,0.000027171,0.00001841172],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9993998,0.000021139937,0.0001453163,0.000093286355,0.00019442456,0.00014606124],"domain_scores_gemma":[0.99899995,0.00011032276,0.000042769334,0.0007640356,0.000055923298,0.000027001612],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00014145594,0.00011961005,0.0002052503,0.0000074344493,0.000087359105,0.000020544325,0.00044637712,0.000036652847,0.0000053507615],"category_scores_gemma":[0.00027517322,0.00008130213,0.000051420368,0.00002969597,0.0001313615,0.000045354525,0.00007956605,0.00013027144,0.0000039198676],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000024216926,0.00006576633,0.00038359442,0.0004406472,0.00011844827,0.0000030991955,0.00026213966,0.012493303,0.93441415,0.046879824,0.0021583831,0.0027564028],"study_design_scores_gemma":[0.00037929075,0.00012402984,0.002437713,0.00024112013,0.00005878014,3.0677668e-7,0.00002036681,0.3662807,0.6122687,0.017897872,0.000073695956,0.00021741579],"about_ca_topic_score_codex":0.000032370735,"about_ca_topic_score_gemma":0.0000043973378,"teacher_disagreement_score":0.3537874,"about_ca_system_score_codex":0.000014636102,"about_ca_system_score_gemma":0.000010999424,"threshold_uncertainty_score":0.33154047},"labels":[],"label_agreement":null},{"id":"W2588837130","doi":"10.1121/1.4976138","title":"Application of acoustic imaging techniques on snowmobile pass-by noise","year":2017,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":15,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Noise (video); Deconvolution; Acoustics; Beamforming; Microphone array; Computer science; Microphone; Acoustic emission; Synchronization (alternating current); Physics; Computer vision; Telecommunications; Algorithm","score_opus":0.004553512940417938,"score_gpt":0.23599813893402297,"score_spread":0.23144462599360502,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2588837130","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.014364013,0.00019548129,0.9831058,0.0011318707,0.00024789656,0.00018438073,0.00004077179,0.000029105753,0.00070071995],"genre_scores_gemma":[0.9835133,0.0006757075,0.015384599,0.00020313502,0.00016266794,0.0000032651524,6.291452e-7,0.000029362229,0.000027359549],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99885935,0.000032295655,0.0004468289,0.000077364886,0.00038816858,0.00019601999],"domain_scores_gemma":[0.9982042,0.0003112005,0.00059504557,0.00066153065,0.00017111664,0.000056948673],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004638934,0.00015060784,0.00031221996,0.0000147873925,0.00022854634,0.000023358054,0.0011018718,0.0000639356,0.0000110806905],"category_scores_gemma":[0.00018255042,0.00008820136,0.00028059623,0.00007937217,0.00064109784,0.00007423357,0.00014998352,0.00046926388,0.0000016845946],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00004599669,0.00015477842,0.00025612328,0.00014203039,0.00016805675,6.0944893e-7,0.00023467082,0.21812165,0.6608341,0.000018818842,0.04570707,0.07431614],"study_design_scores_gemma":[0.0001654033,0.000100252844,0.00085632707,0.00011783644,0.00021732302,0.000011660231,0.00026698085,0.9846944,0.011246821,0.0008600698,0.0013411044,0.00012179493],"about_ca_topic_score_codex":0.000024123798,"about_ca_topic_score_gemma":2.8571637e-7,"teacher_disagreement_score":0.96914923,"about_ca_system_score_codex":0.00007374485,"about_ca_system_score_gemma":0.000024933488,"threshold_uncertainty_score":0.35967472},"labels":[],"label_agreement":null},{"id":"W2589089093","doi":"10.1088/1674-1056/26/2/025205","title":"High sampling-rate measurement of turbulence velocity fluctuations in Mach 1.8 Laval jet using interferometric Rayleigh scattering","year":2017,"lang":"en","type":"article","venue":"Chinese Physics B","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":10,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Jet (fluid); Mach number; Turbulence; Physics; Rayleigh scattering; Interferometry; Mechanics; Computational physics; Optics","score_opus":0.035671226656550675,"score_gpt":0.27241691183104083,"score_spread":0.23674568517449016,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2589089093","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.85951227,0.00005898825,0.13946848,0.000015179457,0.0006200177,0.00010534515,0.000033040888,0.00004118964,0.00014547186],"genre_scores_gemma":[0.99383235,0.000040068815,0.005864248,0.000005358631,0.00019909994,0.000007664383,0.0000093087665,0.000039134433,0.000002787097],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99900997,0.000014915306,0.00030428276,0.00019783732,0.00024182853,0.00023119111],"domain_scores_gemma":[0.9991384,0.00004523171,0.000116792755,0.00052070495,0.0001313873,0.00004746107],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00032438556,0.00021123119,0.0003024814,0.0001216627,0.00014309071,0.000080724734,0.00041533905,0.000052873453,0.0000074832233],"category_scores_gemma":[0.0001885234,0.00019937726,0.00006713984,0.00028009235,0.00006691958,0.00019634973,0.00015684476,0.00022814167,0.0000046452806],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000007060521,0.00006818724,0.011592707,0.00019582741,0.000054057724,0.000002679174,0.00021613383,0.6468195,0.33786875,0.0003357404,0.000007805549,0.002831567],"study_design_scores_gemma":[0.00031435906,0.000011244131,0.13721892,0.0001507209,0.000019928042,7.835356e-7,0.0000064806472,0.8490997,0.0064797103,0.006461674,0.0000021748647,0.00023434256],"about_ca_topic_score_codex":0.00020917652,"about_ca_topic_score_gemma":0.00007067132,"teacher_disagreement_score":0.33138904,"about_ca_system_score_codex":0.00016646132,"about_ca_system_score_gemma":0.000026579819,"threshold_uncertainty_score":0.81303686},"labels":[],"label_agreement":null},{"id":"W2590774400","doi":"10.1121/1.4976072","title":"Time domain nearfield acoustical holography without wrap-around error and spectral leakage for forward propagation","year":2017,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Polytechnique Montréal","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Spectral leakage; Acoustics; Leakage (economics); Acoustic holography; Sound propagation; Propagation of uncertainty; Piston (optics); Microphone; Microphone array; Physics; Holography; Mathematics; Optics; Sound pressure; Fast Fourier transform; Wavefront; Algorithm","score_opus":0.009549906732769828,"score_gpt":0.24557200804336946,"score_spread":0.23602210131059964,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2590774400","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.1892178,0.00012600551,0.80738395,0.0022758946,0.00036781235,0.00028016177,0.00003078934,0.000021754002,0.00029580394],"genre_scores_gemma":[0.9172752,0.00022504469,0.08183436,0.00021474829,0.0003628758,0.0000029167218,6.216443e-7,0.000031512987,0.000052727024],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9987774,0.000041192252,0.00039481666,0.00010394021,0.0003757691,0.00030689125],"domain_scores_gemma":[0.9986084,0.00038656086,0.0003345971,0.00040765552,0.00016408539,0.00009870503],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00075649674,0.00018204875,0.00037697237,0.00001802775,0.0004667123,0.00007054164,0.0006746617,0.00012320423,0.000013491661],"category_scores_gemma":[0.0003190363,0.000104855615,0.00036653044,0.000071990915,0.0012436763,0.00012178134,0.00013273336,0.00051694876,0.0000013966994],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0011221693,0.0005123002,0.0015137485,0.0009930946,0.0025359518,0.000010996673,0.0038950269,0.4385474,0.42175645,0.00033326133,0.09443066,0.034348935],"study_design_scores_gemma":[0.0005496167,0.00030293848,0.0017097663,0.000067707915,0.000384928,0.00004992184,0.0007792181,0.9911269,0.00031513907,0.004129829,0.00042556177,0.0001584819],"about_ca_topic_score_codex":0.0000046252044,"about_ca_topic_score_gemma":7.461211e-7,"teacher_disagreement_score":0.7280574,"about_ca_system_score_codex":0.00004825237,"about_ca_system_score_gemma":0.000038718154,"threshold_uncertainty_score":0.4582377},"labels":[],"label_agreement":null},{"id":"W2593066711","doi":"10.1061/(asce)hy.1943-7900.0001307","title":"Numerical Modeling of Vertical Buoyant Jets Subjected to Lateral Confinement","year":2017,"lang":"en","type":"article","venue":"Journal of Hydraulic Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":42,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Ottawa","funders":"","keywords":"Froude number; Turbulence; Buoyancy; Jet (fluid); Mechanics; Meteorology; Mixing (physics); Flow (mathematics); Physics; Geology","score_opus":0.010409987280336385,"score_gpt":0.22665119884210128,"score_spread":0.2162412115617649,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2593066711","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7527935,0.00006972213,0.24586362,0.00009357868,0.0006406277,0.000053126478,0.0000023461437,0.000031196185,0.00045230918],"genre_scores_gemma":[0.9941122,0.000023559538,0.005555514,0.000015093712,0.00024421618,0.0000017130861,7.783386e-7,0.000039565955,0.0000073456545],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9987702,0.000005291965,0.00058517937,0.000089990295,0.00027728768,0.00027210274],"domain_scores_gemma":[0.99931407,0.000027303504,0.00007134385,0.0002776128,0.00011739798,0.00019225743],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020201036,0.00016787084,0.0003703672,0.00012979531,0.00005977911,0.000055857065,0.00038275734,0.00006966956,0.000021648379],"category_scores_gemma":[0.00014679032,0.00015650988,0.000116546675,0.000058823513,0.000013129156,0.00011397746,0.000055811957,0.00030989895,0.0000035245082],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000008760785,0.000019433495,0.00013861692,0.00005393345,0.000070461865,0.000044315693,0.00008355438,0.89267415,0.10641705,0.00015311105,0.00006220572,0.0002744326],"study_design_scores_gemma":[0.00037230627,0.00009068617,0.0020290075,0.00017211282,0.000032588,0.000042898417,0.000007079313,0.9900613,0.0068029338,0.000033198794,0.00018945268,0.00016646081],"about_ca_topic_score_codex":0.000014003817,"about_ca_topic_score_gemma":0.0000018093044,"teacher_disagreement_score":0.24131873,"about_ca_system_score_codex":0.000068684785,"about_ca_system_score_gemma":0.000017106006,"threshold_uncertainty_score":0.6382288},"labels":[],"label_agreement":null},{"id":"W2593290560","doi":"10.1155/2017/7061391","title":"Computational Acoustic Beamforming for Noise Source Identification for Small Wind Turbines","year":2017,"lang":"en","type":"article","venue":"International Scholarly Research Notices","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Defence Research and Development Canada; University of Waterloo","funders":"Natural Sciences and Engineering Research Council of Canada; Compute Canada","keywords":"Nacelle; Airfoil; Turbine; Acoustics; Beamforming; Noise (video); Wind power; Computer science; NACA airfoil; Small wind turbine; Aeroacoustics; Marine engineering; Aerospace engineering; Sound pressure; Meteorology; Engineering; Telecommunications; Physics; Reynolds number; Turbulence; Electrical engineering","score_opus":0.07329927709614566,"score_gpt":0.364607903149169,"score_spread":0.2913086260530234,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2593290560","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.38996106,0.000071019625,0.6060724,0.0007220155,0.0013141818,0.0006222911,0.00026207592,0.000081618164,0.0008933237],"genre_scores_gemma":[0.97405005,0.00001512152,0.022978228,0.00002167325,0.00088429864,0.00014752662,0.00019088291,0.00004741627,0.0016648364],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99843246,0.00001856991,0.00031476252,0.00028408325,0.00058940385,0.000360731],"domain_scores_gemma":[0.9972218,0.00082771,0.00010866726,0.0003075931,0.0014361795,0.00009800573],"candidate_categories":["scholarly_communication"],"consensus_categories":[],"category_scores_codex":[0.0015417802,0.00013667492,0.00012766589,0.00020724566,0.00097062805,0.0028029617,0.0011543402,0.00010319521,0.000020086138],"category_scores_gemma":[0.0027847402,0.00014136203,0.00009032168,0.000053235453,0.000120636476,0.0014089559,0.00014072373,0.0003468518,0.000026472677],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000058970152,0.0000517976,0.0009299812,0.00015526201,0.00013277656,0.0000017159579,0.00016041344,0.9652926,0.016773257,0.003662552,0.00090194517,0.011878744],"study_design_scores_gemma":[0.00053460686,0.0000383304,0.0061844923,0.00006243707,0.000017774928,0.0000018078774,0.00008389886,0.97588557,0.0004175751,0.008970223,0.0076362253,0.000167064],"about_ca_topic_score_codex":0.000028090877,"about_ca_topic_score_gemma":0.000077637116,"teacher_disagreement_score":0.5840889,"about_ca_system_score_codex":0.0001627815,"about_ca_system_score_gemma":0.00005197091,"threshold_uncertainty_score":0.99823225},"labels":[],"label_agreement":null},{"id":"W2604492971","doi":"10.1139/cjp-2016-0822","title":"Passive control of deep cavity shear layer flow at subsonic speed","year":2017,"lang":"en","type":"article","venue":"Canadian Journal of Physics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":12,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"C-Therm Technologies (Canada)","funders":"","keywords":"Physics; Cylinder; Particle image velocimetry; Mechanics; Flow control (data); Vorticity; Optics; Vortex; Turbulence; Potential flow around a circular cylinder; Acoustics; Geometry; Telecommunications; Open-channel flow; Engineering","score_opus":0.00906709990306098,"score_gpt":0.20307989301751972,"score_spread":0.19401279311445874,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2604492971","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9465317,0.00039974367,0.047989152,0.00019396775,0.0019186275,0.000106468025,0.0002201405,0.0000089151035,0.0026312573],"genre_scores_gemma":[0.99894726,0.000021271893,0.0004632961,0.000026742982,0.00046711817,3.022558e-7,0.0000019413048,0.000027617922,0.000044450477],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99930495,0.000010855759,0.00023431864,0.00006327753,0.00012720666,0.00025937974],"domain_scores_gemma":[0.9989494,0.000031309155,0.0001905844,0.00029461036,0.0001840773,0.0003499901],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00010232471,0.000117515156,0.00027275016,0.000040639297,0.00017007042,0.000049108658,0.00034308084,0.000066138906,0.000058052785],"category_scores_gemma":[0.00006568216,0.00011666541,0.00012866227,0.000032312822,0.00009781856,0.00012728502,0.000011335125,0.0002483008,0.000010110028],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000019240391,0.000020991489,0.008145796,0.000100543315,0.00039390585,0.00038455447,0.0006451203,0.93581074,0.010066738,0.00255925,0.0027338706,0.03911926],"study_design_scores_gemma":[0.0013303881,0.000085733365,0.02140625,0.00010469896,0.0001578747,0.00003653942,0.000047870413,0.9681432,0.0030428919,0.0034703428,0.0018362557,0.00033790132],"about_ca_topic_score_codex":0.0004932044,"about_ca_topic_score_gemma":0.010171524,"teacher_disagreement_score":0.052415535,"about_ca_system_score_codex":0.00024473446,"about_ca_system_score_gemma":0.00018757019,"threshold_uncertainty_score":0.56759495},"labels":[],"label_agreement":null},{"id":"W2604777015","doi":"10.1017/jfm.2015.427","title":"Laminar separation bubble development on an airfoil emitting tonal noise","year":2015,"lang":"en","type":"article","venue":"Journal of Fluid Mechanics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":131,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Waterloo","funders":"Natural Sciences and Engineering Research Council of Canada; Technische Universiteit Delft","keywords":"Airfoil; Laminar flow; Trailing edge; Reynolds number; Leading edge; Physics; Mechanics; Particle image velocimetry; Flow separation; Boundary layer; Bubble; Vortex; Acoustics; Vortex shedding; Turbulence","score_opus":0.02059705751750846,"score_gpt":0.2561570209388049,"score_spread":0.23555996342129643,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2604777015","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.80555606,0.00014076772,0.19182268,0.00003565861,0.0014996541,0.00005096632,0.0000027367275,0.000042874402,0.000848612],"genre_scores_gemma":[0.97249943,0.00004830147,0.02682212,0.00006825558,0.00042287668,0.0000015558013,0.000005628333,0.00003295182,0.00009889718],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99888295,0.000019888448,0.00042801865,0.00008479653,0.00039922306,0.00018514348],"domain_scores_gemma":[0.999319,0.000024586492,0.000106748164,0.00012476844,0.00023576734,0.00018913091],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0007715196,0.00013487169,0.0001821756,0.00009701578,0.00005294163,0.00004089861,0.00017402731,0.000087492044,0.00001115881],"category_scores_gemma":[0.00007367122,0.00012530363,0.000047706213,0.00009192046,0.0000038239405,0.00018080763,0.0000226374,0.00025568475,0.000020090061],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000052697647,0.00011363351,0.000017714727,0.00003427007,0.00006259132,0.000067309964,0.0010316427,0.88617074,0.09338504,0.0043500224,0.0034820463,0.01123231],"study_design_scores_gemma":[0.00046923925,0.0003300486,0.00002811619,0.000078737794,0.000022399236,0.000075238466,0.00025047766,0.97403353,0.017512042,0.0009695602,0.0060431743,0.00018742133],"about_ca_topic_score_codex":4.8167925e-7,"about_ca_topic_score_gemma":0.0000041092353,"teacher_disagreement_score":0.16694336,"about_ca_system_score_codex":0.00025163384,"about_ca_system_score_gemma":0.00012965717,"threshold_uncertainty_score":0.5109734},"labels":[],"label_agreement":null},{"id":"W2604797932","doi":"10.1017/jfm.2015.245","title":"Budgets of turbulent kinetic energy, Reynolds stresses, variance of temperature fluctuations and turbulent heat fluxes in a round jet","year":2015,"lang":"en","type":"article","venue":"Journal of Fluid Mechanics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":47,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Royal Military College of Canada; Université Laval","funders":"","keywords":"Physics; Turbulence; Turbulence kinetic energy; Kinetic energy; Reynolds number; Scalar (mathematics); Jet (fluid); Dissipation; Mechanics; Thermodynamics; Classical mechanics; Geometry","score_opus":0.009300149852908102,"score_gpt":0.21267655169221852,"score_spread":0.2033764018393104,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2604797932","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9446025,0.00902289,0.045059923,0.00027293467,0.00078780996,0.00011506962,0.000039547143,0.000016163269,0.0000831488],"genre_scores_gemma":[0.99188304,0.0028810597,0.0050388286,0.00002675229,0.0001142604,0.0000021348294,0.0000053105314,0.000027104621,0.000021486654],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9986658,0.000032524087,0.00067209563,0.00010755049,0.00034507806,0.00017693623],"domain_scores_gemma":[0.99913526,0.0000591397,0.00013857079,0.00019906831,0.00034403664,0.00012395812],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00034737866,0.00017305858,0.00040712475,0.0001866974,0.000017156795,0.000022538246,0.00019071541,0.00014415219,0.000007571464],"category_scores_gemma":[0.00010876372,0.00015112209,0.00006755816,0.00022103621,0.000019539882,0.000121456826,0.000039382965,0.0002522865,2.0743879e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000061246516,0.00019202879,0.000037504724,0.00023340528,0.00013166787,0.00008514979,0.0006522752,0.6158385,0.36716795,0.012551963,0.0023427405,0.000705572],"study_design_scores_gemma":[0.0015604933,0.00057663716,0.00027394117,0.0006728981,0.0001278683,0.00031100897,0.00030679742,0.94815296,0.037931174,0.008768089,0.0010207441,0.00029741143],"about_ca_topic_score_codex":0.000024867984,"about_ca_topic_score_gemma":0.00004647813,"teacher_disagreement_score":0.33231443,"about_ca_system_score_codex":0.000107325075,"about_ca_system_score_gemma":0.00009322107,"threshold_uncertainty_score":0.616258},"labels":[],"label_agreement":null},{"id":"W2605468331","doi":"10.2514/6.2011-3087","title":"Mean streamwise centreline velocity decay and entrainment in triangular and circular jets","year":2011,"lang":"en","type":"article","venue":"41st AIAA Fluid Dynamics Conference and Exhibit","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"St. Francis Xavier University; Dalhousie University","funders":"","keywords":"Entrainment (biomusicology); Mechanics; Physics; Jet (fluid); Acoustics","score_opus":0.019082513269070008,"score_gpt":0.19368683362215006,"score_spread":0.17460432035308004,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2605468331","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97939074,0.0011126163,0.017663164,0.00005175657,0.00013874366,0.00024387005,0.000064539825,0.0000763162,0.0012582486],"genre_scores_gemma":[0.99560887,0.0025608293,0.0016615043,0.000039367,0.00002884241,0.000012507202,0.000043039792,0.000031304822,0.000013713455],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9987267,0.000026595691,0.00033527857,0.00037546552,0.00014525319,0.00039065463],"domain_scores_gemma":[0.9994392,0.000034580014,0.000035273173,0.00023941394,0.000045704666,0.00020586216],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00022380098,0.00028945037,0.00032689492,0.00011006853,0.00007191505,0.000082133316,0.00011760882,0.00016350408,0.00004309331],"category_scores_gemma":[0.000018827912,0.000298647,0.000032494612,0.00009527057,0.0001363934,0.00011674511,0.0001385964,0.00024374097,0.000002352408],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0003453268,0.0009323018,0.18230532,0.0020420896,0.00071576744,0.0011698533,0.036171764,0.009955409,0.0549165,0.3343043,0.0001209926,0.3770204],"study_design_scores_gemma":[0.0009702855,0.000050615992,0.014721714,0.00009040015,0.000044069755,0.00001789906,0.0006216739,0.9786487,0.00043665525,0.003983725,0.000029766594,0.00038450002],"about_ca_topic_score_codex":0.0001078191,"about_ca_topic_score_gemma":0.0006540575,"teacher_disagreement_score":0.96869326,"about_ca_system_score_codex":0.000076821714,"about_ca_system_score_gemma":0.000026534834,"threshold_uncertainty_score":0.9999466},"labels":[],"label_agreement":null},{"id":"W2606480019","doi":"10.2514/6.2011-3568","title":"Novel Time-Resolved Pressure Measurements on an Airfoil at Low Reynolds Numbers","year":2011,"lang":"en","type":"article","venue":"41st AIAA Fluid Dynamics Conference and Exhibit","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Waterloo","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Reynolds number; Airfoil; Pressure measurement; Computer science; Mechanics; Physics; Meteorology; Turbulence","score_opus":0.034644990750150984,"score_gpt":0.20997036882043116,"score_spread":0.17532537807028017,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2606480019","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.90760815,0.00016086959,0.031327534,0.000040712293,0.00085800956,0.0004527033,0.0003397033,0.0005652719,0.058647033],"genre_scores_gemma":[0.99524266,0.00014357103,0.002142013,0.00010148562,0.00008977279,0.000026228376,0.00016692611,0.00009687861,0.0019904878],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9980904,0.000026219435,0.00038458267,0.0005388579,0.00038920477,0.0005707619],"domain_scores_gemma":[0.9988225,0.000028662424,0.000062420215,0.0006434157,0.0001557619,0.0002872255],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00024808847,0.00045559238,0.00038276662,0.00010785829,0.00020020393,0.0000999228,0.00039334653,0.0002979212,0.00036077067],"category_scores_gemma":[0.00002650296,0.0004642639,0.000081855265,0.00013344212,0.00013178184,0.00023512257,0.00013665266,0.000323867,0.0001555988],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0008968672,0.0019174392,0.015089385,0.0013135432,0.0016409036,0.0001344935,0.008950717,0.11751563,0.7552449,0.052548062,0.0067002303,0.038047846],"study_design_scores_gemma":[0.0007288568,0.00017100442,0.0019660832,0.00013693924,0.0000896661,0.000012650976,0.00008453674,0.9938877,0.0016017812,0.00036310908,0.0003207186,0.00063693244],"about_ca_topic_score_codex":0.00010265004,"about_ca_topic_score_gemma":0.000564329,"teacher_disagreement_score":0.8763721,"about_ca_system_score_codex":0.00015368639,"about_ca_system_score_gemma":0.000039435785,"threshold_uncertainty_score":0.9997809},"labels":[],"label_agreement":null},{"id":"W2616615040","doi":"10.1139/cjce-2016-0433","title":"Experimental and computational study of a high-Reynolds jet flow","year":2017,"lang":"en","type":"article","venue":"Canadian Journal of Civil Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Reynolds number; Jet (fluid); Pitot tube; Mechanics; Flow (mathematics); Flume; Turbulence; Large eddy simulation; Geology; Physics","score_opus":0.0072770301503589496,"score_gpt":0.20078894423090946,"score_spread":0.19351191408055052,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2616615040","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97838175,0.0004138068,0.020179104,0.000015084251,0.0006548066,0.000055769884,0.000017244576,0.0000090618105,0.00027339248],"genre_scores_gemma":[0.99824286,0.0000042587276,0.0015973494,0.0000030742533,0.00012063698,0.0000011821927,9.642317e-7,0.000024930741,0.0000047677254],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999417,0.0000037325967,0.0002441514,0.000059440204,0.000116646836,0.00015902895],"domain_scores_gemma":[0.99946606,0.000023504723,0.00007297024,0.00013893575,0.000059412887,0.0002391109],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00010704501,0.00011088701,0.00020605334,0.00015871965,0.000089591726,0.00007164966,0.00020282675,0.000039152645,0.00003315343],"category_scores_gemma":[0.000042408657,0.00011585153,0.000031715677,0.00003034907,0.000029308001,0.00013207328,0.000015196803,0.00015643793,4.3953716e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000013616893,0.00001116206,0.0015905827,0.000021696836,0.00006631717,0.00007322872,0.00049251533,0.996366,0.0007677192,0.00019063357,0.0001850044,0.00023375059],"study_design_scores_gemma":[0.0008070649,0.00015131732,0.036455333,0.00009032505,0.000026878746,0.00007667492,0.00024157747,0.9615428,0.00016503247,0.000109905326,0.00016044929,0.00017266556],"about_ca_topic_score_codex":0.0004147754,"about_ca_topic_score_gemma":0.012504525,"teacher_disagreement_score":0.03486475,"about_ca_system_score_codex":0.000070019814,"about_ca_system_score_gemma":0.00006134689,"threshold_uncertainty_score":0.6977818},"labels":[],"label_agreement":null},{"id":"W2618737763","doi":"10.1115/1.4036824","title":"Statistical Properties of Round, Square, and Elliptic Jets at Low and Moderate Reynolds Numbers","year":2017,"lang":"en","type":"article","venue":"Journal of Fluids Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":29,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Manitoba","funders":"","keywords":"Reynolds number; Jet (fluid); Physics; Mechanics; Nozzle; Geometry; Turbulence; Body orifice; Particle image velocimetry; Square (algebra); Classical mechanics; Mathematics; Thermodynamics; Mechanical engineering","score_opus":0.009509518546539504,"score_gpt":0.20205937460138967,"score_spread":0.19254985605485017,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2618737763","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9305629,0.0015056656,0.06737141,0.000014669988,0.00036200753,0.00004707429,0.00000945278,0.000017945684,0.00010883169],"genre_scores_gemma":[0.99180126,0.00089041376,0.007117137,0.000002764461,0.000105042454,0.0000010893974,4.6078782e-7,0.0000351605,0.00004669567],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992068,0.000005273636,0.00035314896,0.00008338844,0.00016819284,0.00018322947],"domain_scores_gemma":[0.99952966,0.000038103393,0.00007953287,0.00016735368,0.000071795774,0.000113563816],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018354334,0.00015011601,0.00029766842,0.000070199145,0.00008454962,0.00009931543,0.00013109445,0.000070764436,0.0000049246387],"category_scores_gemma":[0.00011475632,0.00013227019,0.00003441026,0.00002068852,0.00006687038,0.00021799796,0.00006501548,0.00020223239,6.8718015e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00006720731,0.0000276698,0.0020127897,0.0017094496,0.00018596691,0.00010764181,0.0004977561,0.6088924,0.38265193,0.0017755638,0.00014804896,0.0019236024],"study_design_scores_gemma":[0.0004412896,0.000072058574,0.004242258,0.00043939456,0.000050359056,0.0001523861,0.0000264018,0.9870151,0.0072210985,0.00007362039,0.000079197205,0.0001868185],"about_ca_topic_score_codex":0.000004344744,"about_ca_topic_score_gemma":0.0000027244737,"teacher_disagreement_score":0.37812275,"about_ca_system_score_codex":0.00005936778,"about_ca_system_score_gemma":0.00001140674,"threshold_uncertainty_score":0.5393822},"labels":[],"label_agreement":null},{"id":"W2620711026","doi":"10.2514/6.2017-3368","title":"Direct Numerical Simulation of Transitional Airfoil Noise","year":2017,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Engineering and Physical Sciences Research Council; Natural Sciences and Engineering Research Council of Canada; Compute Canada","keywords":"Airfoil; Noise (video); Computer science; Acoustics; Physics; Mechanics; Artificial intelligence","score_opus":0.010035778578587187,"score_gpt":0.23843965971413572,"score_spread":0.22840388113554855,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2620711026","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.19224171,0.00001838608,0.6890567,0.00004809459,0.0003258964,0.000049949565,0.00002924805,0.0001049635,0.11812508],"genre_scores_gemma":[0.99766386,0.0000070938368,0.0020990686,0.000007664048,0.000061019906,0.0000014349249,0.000005764386,0.000010221241,0.00014389909],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99969864,0.000002353582,0.000093875955,0.000054721724,0.00008133768,0.00006906543],"domain_scores_gemma":[0.9997385,0.000031230204,0.000016375383,0.00016547572,0.00002415422,0.000024234889],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000038675047,0.000050957977,0.00008015152,0.000014144229,0.000057758716,0.000014987586,0.000086318134,0.00003284276,0.00012975515],"category_scores_gemma":[0.00001933883,0.000047935697,0.000035632384,0.00001271735,0.000022488566,0.00005992912,0.000008493552,0.000040516756,0.000010526956],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000022348797,0.000009838459,0.00018814346,0.000013766109,0.000009317079,8.8124654e-7,0.000016359652,0.99405503,0.0027011097,0.00070151174,0.000085601576,0.0022161887],"study_design_scores_gemma":[0.000099129495,0.000005639833,0.006984975,0.0000063476346,0.000006534512,2.7970032e-7,0.0000022524277,0.9916721,0.0006296128,0.00021921672,0.0003133182,0.000060567076],"about_ca_topic_score_codex":0.0000063683156,"about_ca_topic_score_gemma":0.000003649455,"teacher_disagreement_score":0.8054221,"about_ca_system_score_codex":0.000010406564,"about_ca_system_score_gemma":0.000003943153,"threshold_uncertainty_score":0.1954761},"labels":[],"label_agreement":null},{"id":"W2620953108","doi":"10.2514/6.2017-3528","title":"Experimental investigation of the transient bleed valve noise","year":2017,"lang":"en","type":"preprint","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Safran Electronics (Canada)","funders":"","keywords":"Supersonic speed; Acoustics; Noise (video); Shock (circulatory); Sound pressure; Jet noise; Physics; Diaphragm (acoustics); Nozzle; Inlet; Jet (fluid); Mechanics; Materials science; Engineering; Computer science","score_opus":0.015919330813727997,"score_gpt":0.23149179978420253,"score_spread":0.21557246897047455,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2620953108","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9696639,0.00029897282,0.0088214185,0.000057081936,0.0024459779,0.0003250975,0.000049338913,0.00009708957,0.018241096],"genre_scores_gemma":[0.99801004,0.000029482133,0.0015658377,0.000016140053,0.00008566104,0.000023195586,0.00001750717,0.000030619583,0.00022150343],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993317,0.000010794303,0.00021808328,0.00015024169,0.0001744526,0.000114693285],"domain_scores_gemma":[0.99919754,0.000012151,0.000075605625,0.0006425087,0.00003251118,0.00003965538],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000083117884,0.00016915696,0.00018008964,0.000025796027,0.000057488454,0.000036240683,0.00044710134,0.00016745167,0.000039500268],"category_scores_gemma":[0.000008653212,0.00012699846,0.00019531413,0.000018676428,0.000093396615,0.000024531859,0.00020180314,0.0003036659,0.0000035546984],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000029012908,0.000027387045,0.00027275344,0.00036345795,0.00018228996,9.833839e-7,0.0016667303,0.7338783,0.2597652,0.0015218974,0.0019474571,0.0003706348],"study_design_scores_gemma":[0.00024192347,0.000012718322,0.012648122,0.00027266305,0.00009016351,0.0000012785131,0.000104786086,0.84061015,0.14313036,0.0024168552,0.00011023756,0.00036076093],"about_ca_topic_score_codex":0.000051706727,"about_ca_topic_score_gemma":0.000011749863,"teacher_disagreement_score":0.11663485,"about_ca_system_score_codex":0.0000640128,"about_ca_system_score_gemma":0.00003304568,"threshold_uncertainty_score":0.5178847},"labels":[],"label_agreement":null},{"id":"W2621186924","doi":"10.2514/6.2017-3215","title":"Aeroacoustics of an axial ducted low Mach-number stage: numerical and experimental investigation","year":2017,"lang":"en","type":"preprint","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke; Safran Electronics (Canada)","funders":"","keywords":"Mach number; Aeroacoustics; Stator; Computational aeroacoustics; Stall (fluid mechanics); Acoustics; Inlet; Mechanics; Computer simulation; Physics; Turbulence; Inflow; Static pressure; Computational fluid dynamics; Sound pressure; Engineering; Mechanical engineering","score_opus":0.014298422834122013,"score_gpt":0.2616683901424108,"score_spread":0.24736996730828875,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2621186924","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9598594,0.00008054552,0.035401464,0.000011049157,0.0012497205,0.00024528825,0.00019683181,0.00019811842,0.00275761],"genre_scores_gemma":[0.97240424,0.00005163077,0.026589708,0.000013145834,0.00027625606,0.000019600508,0.00024891607,0.00007491271,0.00032160606],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9987814,0.00002460491,0.0003693197,0.0003507427,0.00025028086,0.00022365722],"domain_scores_gemma":[0.9989681,0.000026438462,0.00013340729,0.00062134396,0.00007854396,0.00017213513],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00011577665,0.00032674358,0.0003930053,0.000050346378,0.00007892452,0.00012330862,0.00030596103,0.00037620688,0.00017410447],"category_scores_gemma":[0.000044691147,0.00034101077,0.000058191337,0.000030830786,0.00018357066,0.000101671074,0.00038000633,0.0005251938,0.000006034422],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000036852914,0.00019389685,0.0014046744,0.0013120912,0.00024199362,0.000044020835,0.0010130133,0.8728288,0.11752076,0.002166513,0.0010876555,0.0021497565],"study_design_scores_gemma":[0.0002859222,0.000029841845,0.001063322,0.00006858135,0.000043879474,0.0000065970175,0.0000934137,0.9843303,0.012886201,0.0007524683,0.000033799544,0.00040570335],"about_ca_topic_score_codex":0.00011901494,"about_ca_topic_score_gemma":0.000013137901,"teacher_disagreement_score":0.11150149,"about_ca_system_score_codex":0.00007778253,"about_ca_system_score_gemma":0.00005409637,"threshold_uncertainty_score":0.9999042},"labels":[],"label_agreement":null},{"id":"W2621291338","doi":"10.2514/6.2017-4181","title":"Comparison of Three Popular Methods for the Prediction of High Speed Propeller Noise","year":2017,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":9,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Carleton University","funders":"Pratt and Whitney Canada","keywords":"Propeller; Noise (video); Computer science; Acoustics; Marine engineering; Engineering; Artificial intelligence; Physics","score_opus":0.05694457121057943,"score_gpt":0.34308231032622644,"score_spread":0.286137739115647,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2621291338","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.076451845,0.00010601099,0.91937184,0.000049613478,0.00068698253,0.00032023533,0.00003148191,0.000034220953,0.0029477645],"genre_scores_gemma":[0.8955153,0.000019172665,0.10420059,0.0000018197198,0.00006445341,0.000006025628,0.0000046663235,0.000015695814,0.00017223044],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99953383,0.000006429114,0.00022411153,0.000071100876,0.00007350095,0.00009102975],"domain_scores_gemma":[0.9993267,0.00006664211,0.000083988525,0.0004402079,0.000065989625,0.000016459311],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024443323,0.00007234195,0.0001847134,0.000016925396,0.0000869514,0.000015368421,0.00025676063,0.000051932846,0.000022846913],"category_scores_gemma":[0.00008115672,0.00004658873,0.000055251974,0.00001871106,0.00005280418,0.000041430856,0.000043067474,0.00006802737,8.2403926e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00005418469,0.0001343559,0.018276667,0.0005181021,0.00038169493,2.377491e-7,0.00030928184,0.6819734,0.1397131,0.046939112,0.0035429853,0.10815685],"study_design_scores_gemma":[0.00020218852,0.000037262933,0.013857181,0.000014293445,0.000057120877,1.710611e-7,0.00002593674,0.97287804,0.009963337,0.002368593,0.00054816017,0.000047704092],"about_ca_topic_score_codex":0.0000702553,"about_ca_topic_score_gemma":0.000040172552,"teacher_disagreement_score":0.8190635,"about_ca_system_score_codex":0.000009998618,"about_ca_system_score_gemma":0.000004579647,"threshold_uncertainty_score":0.18998334},"labels":[],"label_agreement":null},{"id":"W2624365459","doi":"10.1007/s10494-017-9820-3","title":"PIV Measurements in the Near and Intermediate Field Regions of Jets Issuing from Eight Different Nozzle Geometries","year":2017,"lang":"en","type":"article","venue":"Flow Turbulence and Combustion","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":44,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Manitoba","funders":"","keywords":"Nozzle; Turbulence; Geometry; Jet (fluid); Body orifice; Physics; Mechanics; Particle image velocimetry; Reynolds number; Optics; Mathematics; Mechanical engineering; Thermodynamics","score_opus":0.019391367660847997,"score_gpt":0.22995688232163825,"score_spread":0.21056551466079024,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2624365459","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.993106,0.00056595483,0.005604412,0.00017258727,0.000313887,0.00008165838,0.000014222181,0.000012087261,0.0001291731],"genre_scores_gemma":[0.99886334,0.00082921627,0.0001930926,0.00003188776,0.000047584635,0.000006399261,0.000009350979,0.000006387146,0.000012723425],"study_design_codex":"observational","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995363,0.000010229886,0.00011901326,0.00010730139,0.00011995767,0.00010725162],"domain_scores_gemma":[0.99961287,0.0000720773,0.000042242365,0.00022916847,0.000019647165,0.000024023975],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000110741916,0.00009087154,0.00012063544,0.000035326004,0.0001498352,0.000099090525,0.00016534468,0.000055393164,0.0000083651885],"category_scores_gemma":[0.00008351686,0.00006738882,0.000017143288,0.000032239295,0.000068421716,0.00010302493,0.000052918254,0.00013788285,8.625431e-7],"study_design_candidate":"observational","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00021401676,0.0004036669,0.55362475,0.0010279407,0.00031782652,0.00005326347,0.015628144,0.06980805,0.017607966,0.0011630444,0.007062218,0.3330891],"study_design_scores_gemma":[0.0005186746,0.00007754145,0.30204698,0.00042821618,0.000045793826,0.0000022463837,0.00021914078,0.6921916,0.001529507,0.0025950554,0.0001465464,0.00019869675],"about_ca_topic_score_codex":0.00008066305,"about_ca_topic_score_gemma":0.00015075238,"teacher_disagreement_score":0.62238353,"about_ca_system_score_codex":0.000009812897,"about_ca_system_score_gemma":0.0000029887303,"threshold_uncertainty_score":0.27480364},"labels":[],"label_agreement":null},{"id":"W2625642555","doi":"","title":"Full-scale rotorcraft broadband noise prediction and its relevance to civil noise certification criteria","year":2013,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":6,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Bell Helicopter Textron (Canada)","funders":"","keywords":"Noise (video); Certification; Relevance (law); Scale (ratio); Broadband; Computer science; Acoustics; Telecommunications; Artificial intelligence; Political science; Geography; Cartography; Law; Physics","score_opus":0.008029857458219594,"score_gpt":0.21180136355162915,"score_spread":0.20377150609340955,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2625642555","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.93014646,0.00016495337,0.06318032,0.0002973366,0.0006243184,0.0005929637,0.00003622105,0.000360224,0.0045972248],"genre_scores_gemma":[0.99457884,0.00017181088,0.0031908506,0.00007306882,0.00017233928,0.00016133566,0.000017704848,0.000036983987,0.0015970527],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991957,0.000009216456,0.00022484307,0.0002320342,0.00012229082,0.0002159335],"domain_scores_gemma":[0.9994839,0.00003075489,0.000017626777,0.00022614749,0.0000928459,0.0001487568],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00007482039,0.00014834004,0.00012162922,0.00005834889,0.00006796302,0.000095280746,0.00009649972,0.00008728601,0.0003429513],"category_scores_gemma":[0.00003870576,0.00014565441,0.000022157803,0.00011589088,0.000013621786,0.00024035845,0.000036244914,0.000102297294,0.00021575238],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000011991459,0.00002717387,0.00031646396,0.00011544699,0.000014250967,7.301242e-7,0.00028149423,0.02896433,0.9445418,0.0001225587,0.02099548,0.0046082498],"study_design_scores_gemma":[0.00016752024,0.0000535631,0.016370187,0.000036519603,0.0000127164785,0.000004950088,0.00003010733,0.97536564,0.003918004,0.00020594678,0.0036215612,0.00021327466],"about_ca_topic_score_codex":0.000019229548,"about_ca_topic_score_gemma":0.00007717455,"teacher_disagreement_score":0.9464013,"about_ca_system_score_codex":0.000050129744,"about_ca_system_score_gemma":0.0000049748714,"threshold_uncertainty_score":0.5939615},"labels":[],"label_agreement":null},{"id":"W2626230095","doi":"10.1615/tsfp7.1450","title":"DIRECT SIMULATION OF TRAILING-EDGE NOISE GENERATED BY A CONTROLLED DIFFUSION AIRFOIL USING A LATTICE-BOLTZMANN METHOD","year":2011,"lang":"en","type":"article","venue":"Proceeding of Seventh International Symposium on Turbulence and Shear Flow Phenomena","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Airfoil; Trailing edge; Leading edge; Acoustics; Physics; Mechanics; Aerodynamics; Vortex; Boundary layer","score_opus":0.019628598914121238,"score_gpt":0.2533770520076578,"score_spread":0.23374845309353656,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2626230095","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9350135,0.0002644732,0.05748015,0.000028034647,0.00052934524,0.0003501613,0.000094760486,0.000072420145,0.0061671627],"genre_scores_gemma":[0.98966944,0.00017505066,0.009860166,0.000020439658,0.00012494107,0.000015240428,0.000020800755,0.000034024917,0.000079911464],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9987292,0.000015153681,0.0005028579,0.00025476696,0.0003063014,0.00019167364],"domain_scores_gemma":[0.9993733,0.00008337344,0.0001667496,0.00009096757,0.00021099455,0.00007461232],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003158239,0.00021286837,0.00037542067,0.00012888211,0.00006221903,0.000023851706,0.00018078974,0.00007955598,0.00004320327],"category_scores_gemma":[0.000037580172,0.00019816853,0.000080448146,0.00013048753,0.000046864378,0.0001629647,0.000043549735,0.0001343017,0.0000011871123],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00036253541,0.00025581935,0.00062090094,0.00021113169,0.00023881739,0.0000012290394,0.002435362,0.7354905,0.25720012,0.00049065775,0.000020449488,0.002672478],"study_design_scores_gemma":[0.0012584006,0.0001078321,0.00012576647,0.00018824336,0.000064592066,0.0000015801884,0.00008134103,0.9832099,0.014529878,0.00019636822,0.00004745491,0.0001886287],"about_ca_topic_score_codex":0.00002240946,"about_ca_topic_score_gemma":5.5586037e-7,"teacher_disagreement_score":0.24771942,"about_ca_system_score_codex":0.000054673972,"about_ca_system_score_gemma":0.000014357554,"threshold_uncertainty_score":0.8081078},"labels":[],"label_agreement":null},{"id":"W2646146168","doi":"10.2514/6.2017-3573","title":"Propeller Analysis Using Low &amp; High Fidelity Aero-acoustic Methods","year":2017,"lang":"en","type":"article","venue":"35th AIAA Applied Aerodynamics Conference","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Safran Electronics (Canada)","funders":"Horizon 2020 Framework Programme; Cleansky; European Commission","keywords":"Computer science; Propeller; Fidelity; Acoustics; Engineering; Marine engineering; Telecommunications; Physics","score_opus":0.031832889073524585,"score_gpt":0.30512202469065186,"score_spread":0.27328913561712725,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2646146168","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.3476822,0.000028207134,0.6446399,0.000018839957,0.00066719594,0.0003477272,0.00011264043,0.00028495354,0.0062183463],"genre_scores_gemma":[0.82392955,0.00011023041,0.17518684,0.000043390937,0.00015485301,0.000048466205,0.00014581592,0.000104922474,0.00027594838],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99685025,0.00006843094,0.00080237485,0.0008836015,0.00046391244,0.00093141396],"domain_scores_gemma":[0.99639285,0.00014429544,0.00035918833,0.0025012873,0.00028280632,0.00031954827],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0008559489,0.0006900431,0.0010047156,0.00026324397,0.00079368375,0.00070830854,0.0014740246,0.00039287,0.00031157437],"category_scores_gemma":[0.00017511995,0.0007020595,0.00026013012,0.00044722296,0.0003710848,0.00023470056,0.00045811312,0.00078920927,0.00009700559],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00002288486,0.00006471432,0.00041522516,0.00017369782,0.00067762745,0.000010520057,0.00014675308,0.8918114,0.08565996,0.010897168,0.000059730617,0.0100603225],"study_design_scores_gemma":[0.0003810694,0.000009238485,0.0063973283,0.000039077033,0.0007692241,0.0000036359525,0.00004463085,0.9878102,0.00026716825,0.0032368898,0.0001761188,0.0008654278],"about_ca_topic_score_codex":0.00019354661,"about_ca_topic_score_gemma":0.0011306772,"teacher_disagreement_score":0.47624734,"about_ca_system_score_codex":0.00027871653,"about_ca_system_score_gemma":0.00012580225,"threshold_uncertainty_score":0.9995431},"labels":[],"label_agreement":null},{"id":"W2674723473","doi":"10.1299/jsmefed.2004.142","title":"Jet noise reduction by a cross wire device in supersonic jet issuing from a Laval nozzle","year":2004,"lang":"en","type":"article","venue":"Ryuutai Kougaku Bumon Kouenkai kouen rombunshuu/Ryutai Kogaku Bumon Koenkai koen ronbunshu","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Jet (fluid); Nozzle; Jet noise; Supersonic speed; Noise (video); Reduction (mathematics); Physics; Acoustics; Materials science; Aerospace engineering; Mechanics; Engineering; Computer science; Mathematics; Geometry","score_opus":0.006997935615007841,"score_gpt":0.22708477918411066,"score_spread":0.22008684356910282,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2674723473","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97873753,0.004445288,0.002889082,0.001184413,0.0035532438,0.0022181268,0.0015606829,0.0024836592,0.0029279522],"genre_scores_gemma":[0.987586,0.0020247705,0.004528911,0.00046315405,0.0014419042,0.00047560615,0.0016027648,0.00093882706,0.00093804207],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.98677236,0.00038027114,0.0032201314,0.0033194174,0.00217725,0.0041305814],"domain_scores_gemma":[0.9942472,0.0003171724,0.0006652045,0.0028659992,0.00049439695,0.0014100431],"candidate_categories":["metaepi_narrow","scholarly_communication","research_integrity","insufficient_payload"],"consensus_categories":["metaepi_narrow","research_integrity"],"category_scores_codex":[0.0014020783,0.0029883957,0.0027778426,0.0011481467,0.0010087659,0.001201165,0.002756916,0.0017992624,0.00053055043],"category_scores_gemma":[0.00035516723,0.0032210741,0.0010192298,0.002669392,0.0007374373,0.0025012293,0.0007091465,0.0034439885,0.0009804893],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":true,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00091846404,0.0027914806,0.06930712,0.0012279407,0.0014518026,0.0015833874,0.009916275,0.527634,0.35960585,0.001940618,0.01718073,0.006442283],"study_design_scores_gemma":[0.05938906,0.003720435,0.11146758,0.0082403915,0.0030704464,0.0018149589,0.017245091,0.46784633,0.15229796,0.02296489,0.11867555,0.03326731],"about_ca_topic_score_codex":0.009187648,"about_ca_topic_score_gemma":0.004423881,"teacher_disagreement_score":0.20730789,"about_ca_system_score_codex":0.0033470641,"about_ca_system_score_gemma":0.0005520088,"threshold_uncertainty_score":0.99983567},"labels":[],"label_agreement":null},{"id":"W2690770139","doi":"10.1299/jsmefed.2003.45","title":"Experiment on Noise Characteristics of Supersonic Jets from a Laval Nozzle","year":2003,"lang":"en","type":"article","venue":"Ryuutai Kougaku Bumon Kouenkai kouen rombunshuu/Ryutai Kogaku Bumon Koenkai koen ronbunshu","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Nozzle; Supersonic speed; Jet noise; Noise (video); Jet (fluid); Acoustics; Materials science; Environmental science; Physics; Aerospace engineering; Mechanics; Engineering; Computer science","score_opus":0.007906295912372087,"score_gpt":0.20593892242546813,"score_spread":0.19803262651309606,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2690770139","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97155964,0.0018075295,0.0024459462,0.00026615293,0.004190196,0.0018695974,0.0016019626,0.0014404531,0.014818498],"genre_scores_gemma":[0.99029046,0.0014771441,0.004025536,0.00042564812,0.00079121854,0.0003201366,0.00066919357,0.0007562932,0.0012443574],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9890175,0.0004999004,0.0030266235,0.0023293109,0.0022029742,0.002923721],"domain_scores_gemma":[0.9935628,0.00058755174,0.00080149923,0.003253416,0.00052375847,0.001270965],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":["metaepi_narrow","insufficient_payload"],"category_scores_codex":[0.0010803511,0.0024894334,0.0028879133,0.0009002918,0.00062819076,0.00040387106,0.0020849954,0.0012206094,0.00136365],"category_scores_gemma":[0.00050222,0.0026119712,0.0011389554,0.0013139097,0.0005955621,0.00076269853,0.00038044862,0.0020510217,0.00082937017],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0019136465,0.00856072,0.055654485,0.0024703878,0.0053340746,0.0021023636,0.013064403,0.09962907,0.71288663,0.040383328,0.03617588,0.021825004],"study_design_scores_gemma":[0.02620021,0.006439005,0.080047615,0.004475679,0.003355985,0.00044720227,0.00930383,0.25091642,0.3884351,0.0093703745,0.19896744,0.022041159],"about_ca_topic_score_codex":0.000593391,"about_ca_topic_score_gemma":0.00017561227,"teacher_disagreement_score":0.32445157,"about_ca_system_score_codex":0.0011704965,"about_ca_system_score_gemma":0.0004011614,"threshold_uncertainty_score":0.9999486},"labels":[],"label_agreement":null},{"id":"W2732889288","doi":"10.4050/f-0073-2017-12286","title":"Atmospheric Absorption Model Effects on Civil Rotorcraft Noise Certification EPNL Values","year":2017,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Bell Helicopter Textron (Canada)","funders":"","keywords":"Certification; Atmospheric model; Absorption (acoustics); Noise (video); Aerospace engineering; Environmental science; Aeronautics; Remote sensing; Engineering; Computer science; Acoustics; Meteorology; Physics; Geology; Political science; Artificial intelligence; Law","score_opus":0.011616081179109849,"score_gpt":0.22911753411820435,"score_spread":0.2175014529390945,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2732889288","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.590243,0.000041923548,0.37035477,0.00010781778,0.0007968305,0.0003209871,0.0000053091626,0.0004249763,0.037704393],"genre_scores_gemma":[0.99014616,0.000078606005,0.0072867163,0.000042019376,0.00016989611,0.00005317751,0.000009509921,0.000045049866,0.0021688845],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993124,0.0000075707767,0.00014303655,0.00018919818,0.0001538621,0.00019392488],"domain_scores_gemma":[0.99916506,0.000036388552,0.00004293044,0.0006574591,0.00003441158,0.000063738094],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000100114055,0.00015749621,0.00012699801,0.000009231054,0.00021411765,0.000126717,0.00025355376,0.000096993994,0.0000355967],"category_scores_gemma":[0.000052995732,0.00014613508,0.00005303945,0.000026493935,0.000024895764,0.00014835905,0.00003308026,0.00012754856,0.00017951183],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000005879673,0.000023872968,0.00017085572,0.000076785735,0.00001738595,0.0000018396246,0.000053093292,0.95323944,0.029423479,0.0025685397,0.002078095,0.012340726],"study_design_scores_gemma":[0.00016432241,0.000023354485,0.0045410707,0.000034729295,0.000014994475,4.2959653e-7,0.000003251656,0.98925614,0.0026368822,0.0029815638,0.00015913109,0.00018414311],"about_ca_topic_score_codex":0.000013208782,"about_ca_topic_score_gemma":0.000020594687,"teacher_disagreement_score":0.39990315,"about_ca_system_score_codex":0.00008280865,"about_ca_system_score_gemma":0.0000074301306,"threshold_uncertainty_score":0.5959216},"labels":[],"label_agreement":null},{"id":"W2754484179","doi":"10.3390/ijtpp2030016","title":"Effect of Distortion on Turbofan Tonal Noise at Cutback with Hybrid Methods","year":2017,"lang":"en","type":"article","venue":"International Journal of Turbomachinery Propulsion and Power","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":12,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Office National d'études et de Recherches Aérospatiales; Safran Aircraft Engines; Grand Équipement National De Calcul Intensif","keywords":"Turbofan; Nacelle; Inlet; Duct (anatomy); Acoustics; Distortion (music); Aeroacoustics; Annulus (botany); Noise (video); Mechanical fan; Mechanics; Physics; Engineering; Aerospace engineering; Sound pressure; Computer science; Mechanical engineering; Materials science; Telecommunications","score_opus":0.004374511590186343,"score_gpt":0.2925739928122341,"score_spread":0.28819948122204775,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2754484179","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9895503,0.0001317753,0.0052774814,0.00019659732,0.0021002288,0.00007321493,0.00002767384,0.0000113995675,0.0026313514],"genre_scores_gemma":[0.99680614,0.000084834224,0.0026257823,0.000030291598,0.00019114291,0.0000013955085,0.0000070059064,0.00002198754,0.00023143686],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99904054,0.000053800122,0.00031933148,0.00010414484,0.00038270402,0.000099453224],"domain_scores_gemma":[0.99915075,0.00012009302,0.00032093984,0.00017582817,0.00014927471,0.00008311675],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00047428103,0.00015746799,0.00023920197,0.00010918053,0.00008296755,0.000060589755,0.00032440008,0.000044183646,0.00007314748],"category_scores_gemma":[0.00015417197,0.000099234225,0.00009810152,0.000014841641,0.000073347976,0.00015898317,0.000074837815,0.00024716134,0.0000025223987],"study_design_candidate":"design_other","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0097709345,0.0004918466,0.063499205,0.00042493222,0.0018010292,0.0009753043,0.000609883,0.075146616,0.22471513,0.0012647244,0.007071579,0.6142288],"study_design_scores_gemma":[0.015399279,0.011106476,0.24879965,0.0030467303,0.0006199405,0.0036182893,0.00003145247,0.34809366,0.3322927,0.0028470408,0.032054357,0.0020903952],"about_ca_topic_score_codex":0.000004905304,"about_ca_topic_score_gemma":0.0000022733343,"teacher_disagreement_score":0.6121384,"about_ca_system_score_codex":0.00008652261,"about_ca_system_score_gemma":0.000009624804,"threshold_uncertainty_score":0.40466544},"labels":[],"label_agreement":null},{"id":"W2758188329","doi":"10.1115/1.4037976","title":"Aeroacoustic Analysis of the Tonal Noise of a Large-Scale Radial Blower","year":2017,"lang":"en","type":"article","venue":"Journal of Fluids Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Volute; Noise (video); Acoustics; Scale (ratio); Aeroacoustics; Flow (mathematics); Computer science; Physics; Aerospace engineering; Mechanics; Impeller; Engineering; Sound pressure; Artificial intelligence","score_opus":0.004855755601049004,"score_gpt":0.21226132435223574,"score_spread":0.20740556875118674,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2758188329","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.85030913,0.00028946856,0.14781462,0.000019996523,0.0011896641,0.000042429645,0.000047319507,0.000011586506,0.00027576293],"genre_scores_gemma":[0.9956417,0.000082762555,0.0040017324,0.0000043461637,0.00021071782,8.07719e-7,8.4960874e-7,0.00002663023,0.000030450006],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9988056,0.0000075514054,0.00056899065,0.00007311414,0.00033834143,0.00020640358],"domain_scores_gemma":[0.9990371,0.00006577826,0.00022948315,0.00044280052,0.00014796175,0.00007687977],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00036789806,0.0001461187,0.00046574738,0.00023675172,0.00006321292,0.000028757877,0.00058871444,0.00008322479,0.00003913667],"category_scores_gemma":[0.00017413362,0.00011351184,0.00042742546,0.00022661158,0.00004377308,0.000116883464,0.000075908654,0.0002906862,4.103286e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000067793594,0.000027457289,0.0014940666,0.00006823771,0.00055644417,0.0000062014774,0.00014767302,0.87137115,0.12588397,0.00010496925,0.00012243562,0.00021061696],"study_design_scores_gemma":[0.00034615278,0.00002877467,0.043360453,0.00009856229,0.00088497036,0.000011111884,0.000024833473,0.95056736,0.004403087,0.000012171532,0.0001452237,0.000117282296],"about_ca_topic_score_codex":0.000003172746,"about_ca_topic_score_gemma":0.000007419553,"teacher_disagreement_score":0.14533255,"about_ca_system_score_codex":0.00005342632,"about_ca_system_score_gemma":0.000028878474,"threshold_uncertainty_score":0.46288785},"labels":[],"label_agreement":null},{"id":"W2759276811","doi":"10.1115/1.4038091","title":"Particle Image Velocimetry Investigation of the Coherent Structures in a Leading-Edge Slat Flow","year":2017,"lang":"en","type":"article","venue":"Journal of Fluids Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of New Brunswick","funders":"","keywords":"Reynolds number; Particle image velocimetry; Wind tunnel; Vortex; Mechanics; Cove; Flow visualization; Leading edge; Vortex generator; Physics; Turbulence; Geometry; Geology; Flow (mathematics); Mathematics","score_opus":0.009172099113292536,"score_gpt":0.2185999115945051,"score_spread":0.20942781248121256,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2759276811","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98118436,0.00037336204,0.017251173,0.000048839767,0.00097138894,0.000055464607,0.000004077024,0.000014400354,0.00009692717],"genre_scores_gemma":[0.9926527,0.000042876265,0.007118049,0.0000046519244,0.0001460094,0.0000010471794,2.7449445e-7,0.000023903058,0.000010498259],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991994,0.000008735611,0.00038654334,0.000057372163,0.00018620036,0.00016178701],"domain_scores_gemma":[0.99947834,0.000038171653,0.00011610064,0.00025137168,0.000060015034,0.00005600167],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024818524,0.00011427614,0.00020677691,0.00006834199,0.000049442984,0.00005583908,0.00035774347,0.000060319653,0.000008201339],"category_scores_gemma":[0.00019997978,0.000089144174,0.00008277103,0.00008500137,0.00004386976,0.00020303781,0.000051101433,0.00031338652,8.7461876e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000003246129,0.000004349251,0.0058975127,0.00009623003,0.000025973899,0.000008159128,0.00024230914,0.52747905,0.46480078,0.00026196006,0.0001233001,0.0010571574],"study_design_scores_gemma":[0.00033370228,0.000020668773,0.08530992,0.0001855327,0.000021307114,0.000017368218,0.000020293382,0.84276086,0.07086545,0.00031499728,0.000042391763,0.000107509484],"about_ca_topic_score_codex":0.000003203894,"about_ca_topic_score_gemma":0.000004703852,"teacher_disagreement_score":0.39393532,"about_ca_system_score_codex":0.00008521829,"about_ca_system_score_gemma":0.000020244046,"threshold_uncertainty_score":0.3635194},"labels":[],"label_agreement":null},{"id":"W2765354541","doi":"10.1115/pvp2017-65298","title":"Aeroacoustic Source of Multiple Cavities and Prediction of Self-Excited Oscillations","year":2017,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"","keywords":"Strouhal number; Piping; Acoustics; Oscillation (cell signaling); Amplitude; Mechanics; Flow (mathematics); Physics; Noise (video); Excited state; Optics; Turbulence; Computer science; Atomic physics","score_opus":0.00936973636537892,"score_gpt":0.1950540461194105,"score_spread":0.18568430975403158,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2765354541","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.89846396,0.000038286522,0.09667463,0.0000067242663,0.00016926779,0.00007304461,0.000064706954,0.00010082328,0.0044085626],"genre_scores_gemma":[0.9958336,0.0000725975,0.003825921,0.0000013846759,0.00003022545,0.0000023789364,0.000005801936,0.000012329428,0.00021579402],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99963254,0.0000032319936,0.0001507562,0.00006330983,0.000074678865,0.00007549179],"domain_scores_gemma":[0.9996099,0.00005217919,0.000048819536,0.00021540774,0.00004835198,0.000025383755],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000054356155,0.000062891784,0.000107106986,0.000040296763,0.00008954183,0.000016290705,0.00007352469,0.00004782469,0.00001084649],"category_scores_gemma":[0.00006141186,0.000060818595,0.000019643521,0.000021689299,0.000065096065,0.00006707177,0.00003251923,0.000047780686,4.873368e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000006341579,0.000059798844,0.09326172,0.0005475925,0.00015203818,8.1630793e-7,0.001187917,0.8233844,0.07663898,0.0017631885,0.0005972569,0.0023999675],"study_design_scores_gemma":[0.00017406022,0.000014558953,0.05881739,0.000018364924,0.000026606915,0.0000011706684,0.00011040652,0.9401297,0.00046939487,0.00009266529,0.00009699645,0.00004866138],"about_ca_topic_score_codex":0.00007131525,"about_ca_topic_score_gemma":0.000046967263,"teacher_disagreement_score":0.11674534,"about_ca_system_score_codex":0.000010697231,"about_ca_system_score_gemma":0.000005339639,"threshold_uncertainty_score":0.24801102},"labels":[],"label_agreement":null},{"id":"W2765501230","doi":"10.1115/fedsm2017-69419","title":"Comparison of Turbulent Jets Issuing From Various Sharp Contoured Nozzles","year":2017,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":9,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Manitoba","funders":"","keywords":"Turbulence; Nozzle; Physics; Reynolds number; Mechanics; Jet (fluid); Geometry; Body orifice; Particle image velocimetry; Ellipse; Aspect ratio (aeronautics); Equilateral triangle; Tuyere; Optics; Materials science; Mathematics; Mechanical engineering; Thermodynamics","score_opus":0.024590953796989896,"score_gpt":0.29501976520962564,"score_spread":0.27042881141263575,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2765501230","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8986576,0.0005312248,0.06850707,0.00011989617,0.00090343785,0.0001332691,0.000056655186,0.00019926182,0.030891582],"genre_scores_gemma":[0.9931625,0.000032859694,0.006359104,0.000014367497,0.00012214723,0.000003061996,0.000016390384,0.000025567433,0.00026401298],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99930304,0.000004739822,0.0002499006,0.0001320534,0.0001374198,0.00017284005],"domain_scores_gemma":[0.9992687,0.00006239803,0.00007446795,0.00049813284,0.000039482653,0.00005681664],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000061010312,0.0001295868,0.00027555585,0.00002320234,0.00011065105,0.00008244516,0.00036921675,0.00008452395,0.0002452478],"category_scores_gemma":[0.000058149366,0.000121516394,0.00005377583,0.000013026716,0.000040804374,0.000072232,0.00007086541,0.00013495151,0.00003156447],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00005103135,0.0004521533,0.058533598,0.00033932575,0.0009123514,0.00007213127,0.005669589,0.6092947,0.22099401,0.015074536,0.04287825,0.045728296],"study_design_scores_gemma":[0.00031171343,0.000016929976,0.011965155,0.000050086415,0.000031576936,6.9734807e-7,0.000121605524,0.9779798,0.006904291,0.00075770775,0.0016656216,0.00019482271],"about_ca_topic_score_codex":0.00033222468,"about_ca_topic_score_gemma":0.00029620083,"teacher_disagreement_score":0.36868507,"about_ca_system_score_codex":0.000025569003,"about_ca_system_score_gemma":0.000006107062,"threshold_uncertainty_score":0.49552947},"labels":[],"label_agreement":null},{"id":"W2766335472","doi":"10.1115/fedsm2017-69418","title":"Experimental-Numerical Analysis of Turbulent Incompressible Isothermal Jets","year":2017,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":6,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Manitoba","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Reynolds number; Turbulence; Mechanics; Jet (fluid); Physics; Particle image velocimetry; Turbulence kinetic energy; Mixing (physics); Reynolds stress equation model; Reynolds-averaged Navier–Stokes equations; Classical mechanics; K-omega turbulence model","score_opus":0.01300182107841582,"score_gpt":0.26230777777667785,"score_spread":0.24930595669826203,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2766335472","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8987655,0.00015442097,0.05914332,0.000026567543,0.00019829924,0.000054987304,0.000010661637,0.0000902033,0.041556053],"genre_scores_gemma":[0.9966613,0.000011713011,0.0029587124,0.000015762284,0.000030793908,0.00000493035,0.000004847645,0.000015741254,0.00029618986],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99947226,0.000004415064,0.00016363991,0.00010497015,0.000118992335,0.0001357248],"domain_scores_gemma":[0.9994038,0.000014006664,0.00004340503,0.00047326204,0.00001706649,0.000048508547],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000043524848,0.000094681425,0.00021625782,0.00007458032,0.00007577525,0.000041103696,0.0002842103,0.00004407669,0.00056928204],"category_scores_gemma":[0.0000060425537,0.00008378557,0.00010531204,0.00006850169,0.000041218093,0.00007009097,0.00006990321,0.00006143386,0.000009914438],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000008483618,0.00013344103,0.004480413,0.000025666262,0.0011685259,0.000013342695,0.00021652432,0.85415965,0.1344185,0.0027682164,0.00086514675,0.0017420653],"study_design_scores_gemma":[0.00011946092,0.00001210511,0.016325567,0.0000048286242,0.00010968062,4.837821e-7,0.000023500992,0.9634722,0.019564366,0.000026022517,0.00023310042,0.00010868174],"about_ca_topic_score_codex":0.000049083992,"about_ca_topic_score_gemma":0.0000060484363,"teacher_disagreement_score":0.11485414,"about_ca_system_score_codex":0.000022326913,"about_ca_system_score_gemma":0.000003556665,"threshold_uncertainty_score":0.6233239},"labels":[],"label_agreement":null},{"id":"W2772721293","doi":"","title":"Aeroacoustics and Aircraft Noise","year":2017,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"Carleton University","funders":"","keywords":"Aeroacoustics; Computational aeroacoustics; Aerodynamics; Noise (video); Aerospace engineering; Aircraft noise; Turbulence; Engineering; Noise reduction; Aeronautics; Acoustics; Computer science; Physics; Mechanics; Artificial intelligence; Sound pressure","score_opus":0.007704902267396303,"score_gpt":0.19759110902414748,"score_spread":0.18988620675675116,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2772721293","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.81165177,0.0006596693,0.11740879,0.00048650173,0.004696168,0.00037577542,0.000808749,0.00040655778,0.06350599],"genre_scores_gemma":[0.99351615,0.00035863882,0.004941126,0.0001665807,0.0003185838,0.000005604371,0.000012841996,0.00006713112,0.000613328],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99904174,0.0000041321923,0.00016386654,0.00018530776,0.000113658876,0.00049128185],"domain_scores_gemma":[0.9986012,0.000032166467,0.000033078886,0.00065393426,0.000064356675,0.0006152804],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000092896174,0.00020164027,0.00017620751,0.00009870878,0.00055240863,0.00028805484,0.0003777899,0.0001656073,0.00004545242],"category_scores_gemma":[0.00017435438,0.0002300186,0.000030164692,0.00003471678,0.00017560105,0.00010090595,0.000053625034,0.00026345544,0.00004637515],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000093645685,0.00004518848,0.0120537635,0.0007761972,0.00032870524,0.0014594529,0.00067702436,0.6428918,0.09362933,0.013943215,0.15838176,0.07580416],"study_design_scores_gemma":[0.00022971834,0.00001568658,0.045648217,0.000032189204,0.00007202283,0.000027338865,0.00005970264,0.9477444,0.00002839037,0.00094636733,0.0047576185,0.00043831952],"about_ca_topic_score_codex":0.0022037034,"about_ca_topic_score_gemma":0.008388843,"teacher_disagreement_score":0.3048526,"about_ca_system_score_codex":0.00015957493,"about_ca_system_score_gemma":0.00011392745,"threshold_uncertainty_score":0.93798864},"labels":[],"label_agreement":null},{"id":"W2774300954","doi":"10.4236/ojfd.2017.74036","title":"A Numerical Approach to Possible Identification of the Noisiest Zones of a Wall Surface with a Flow Interaction","year":2017,"lang":"en","type":"article","venue":"Open Journal of Fluid Dynamics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Natural Sciences and Engineering Research Council of Canada; Compute Canada","keywords":"Acoustics; Sound power; Singular value decomposition; Sound pressure; Noise (video); Aeroacoustics; Power (physics); Computational fluid dynamics; Physics; Surface (topology); Singular value; Computer science; Mechanics; Sound (geography); Mathematics; Geometry; Algorithm; Eigenvalues and eigenvectors","score_opus":0.012356844475069248,"score_gpt":0.2493199194180416,"score_spread":0.23696307494297236,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2774300954","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.73621196,0.000020384567,0.26125625,0.00017948971,0.00042184885,0.00019249751,0.000022148535,0.0000040378923,0.0016913847],"genre_scores_gemma":[0.97166073,0.000029973236,0.028094007,0.000007413697,0.000028819877,0.000001941699,0.000002728077,0.00002327786,0.00015108878],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99901444,0.000023438473,0.00050659216,0.00009232505,0.00024871482,0.0001145002],"domain_scores_gemma":[0.9986719,0.000032443044,0.00047158194,0.00047846895,0.0002888098,0.00005682626],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00041349162,0.00011258142,0.0002820656,0.000045326135,0.00010706612,0.00016306549,0.0010665153,0.000048319962,0.0000036846882],"category_scores_gemma":[0.0000916513,0.00007742475,0.0000751572,0.000113587856,0.00005347191,0.00035317522,0.00012505784,0.000202613,0.0000011716775],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000084419815,0.00009927997,0.0015004758,0.00006726653,0.00008429535,0.0000017079597,0.00032925184,0.98095393,0.014636762,0.00056678447,0.00010046158,0.0015753515],"study_design_scores_gemma":[0.0002835504,0.00008984268,0.008252662,0.00015774887,0.000047663973,0.00005375192,0.00017525222,0.98951125,0.0011961379,0.00011604972,0.000023945115,0.00009215468],"about_ca_topic_score_codex":0.000056743746,"about_ca_topic_score_gemma":0.000050679977,"teacher_disagreement_score":0.23544881,"about_ca_system_score_codex":0.00009818917,"about_ca_system_score_gemma":0.000052561067,"threshold_uncertainty_score":0.315729},"labels":[],"label_agreement":null},{"id":"W2784532368","doi":"10.22215/etd/2017-11724","title":"Computational Aeroacoustic Prediction of Propeller Noise Using Grid-Based and Grid-Free CFD Methods","year":2017,"lang":"en","type":"dissertation","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Carleton University","funders":"Pratt and Whitney Canada","keywords":"Propeller; Computational fluid dynamics; Noise (video); Harmonics; Vortex; Acoustics; Marine engineering; Grid; Cylinder; Engineering; Computer science; Aerospace engineering; Physics; Mechanical engineering; Meteorology; Electrical engineering; Mathematics; Geometry","score_opus":0.021113170836815045,"score_gpt":0.292023312918882,"score_spread":0.270910142082067,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2784532368","genre_codex":"methods","genre_gemma":"methods","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.09948723,0.0004915868,0.87336874,0.0000103075,0.005987706,0.0006801704,0.0010545239,0.00026023766,0.01865947],"genre_scores_gemma":[0.36511618,0.00015289296,0.62578607,0.000020391153,0.0010460987,0.000041223142,0.0049901567,0.00026870944,0.0025783004],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9987391,0.000033592944,0.0004519937,0.0002882996,0.00028691234,0.00020007361],"domain_scores_gemma":[0.9989429,0.00013032352,0.00019924199,0.00042864605,0.00022219417,0.000076660755],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0002940459,0.00031890784,0.00040815934,0.00018495308,0.00014700758,0.000070327806,0.00026669676,0.0003275332,0.00007219587],"category_scores_gemma":[0.00014229672,0.00031103787,0.00008794071,0.00007296225,0.000061408944,0.00009406635,0.000026675953,0.00031372797,0.0000016457058],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000020159767,0.000027774171,0.00005763891,0.0009855062,0.000100051126,0.0000027658973,0.000080318845,0.9859615,0.007727499,0.0001651331,0.0011706908,0.003700936],"study_design_scores_gemma":[0.000440553,0.000029235138,0.002340286,0.0002642866,0.00023251079,0.0000032085109,0.000053571966,0.9947911,0.0005333479,0.00093738746,0.00011007226,0.00026442748],"about_ca_topic_score_codex":0.00004878353,"about_ca_topic_score_gemma":0.00004344423,"teacher_disagreement_score":0.26562896,"about_ca_system_score_codex":0.000074300726,"about_ca_system_score_gemma":0.00011084156,"threshold_uncertainty_score":0.9999342},"labels":[],"label_agreement":null},{"id":"W2786642541","doi":"","title":"Performance Evaluation of an Innovative Sampling System for Closed Path Eddy Covariance Measurements","year":2016,"lang":"en","type":"article","venue":"32nd Conf. on Agricultural and Forest Meteorology/22nd Symp. Boundary Layers and Turbulence/ Third Conf. on Atmospheric Biogeosciences (20 – 24 June, 2016)","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Campbell Scientific (Canada)","funders":"","keywords":"Eddy covariance; Covariance; Path (computing); Environmental science; Sampling (signal processing); Computer science; Statistics; Mathematics; Filter (signal processing); Computer vision","score_opus":0.022946404230211135,"score_gpt":0.2300752216341433,"score_spread":0.20712881740393216,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2786642541","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9904677,0.0008082846,0.003380396,0.0002347585,0.0024590334,0.0010833131,0.00025400636,0.00014022237,0.0011722875],"genre_scores_gemma":[0.9926747,0.00046309046,0.005977199,0.00015112624,0.00015741464,0.00016148562,0.000052102074,0.000028040455,0.00033485686],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99669915,0.00013042732,0.00074650836,0.0008869445,0.00081483606,0.0007221426],"domain_scores_gemma":[0.99804336,0.00022368824,0.00039303428,0.00035900046,0.00074697344,0.00023395455],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0016328571,0.0005853607,0.00068030943,0.00004457017,0.00064557185,0.00019044372,0.0004703748,0.00032388337,0.000021433945],"category_scores_gemma":[0.00010667933,0.0003334636,0.000098980665,0.0005669611,0.00082354347,0.0005289575,0.000071036266,0.00024856403,0.00000837568],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0032316677,0.0010602791,0.036817197,0.002055477,0.0018683241,0.000023106633,0.004920429,0.103787266,0.2472448,0.08133606,0.0027778284,0.51487756],"study_design_scores_gemma":[0.009188824,0.0066253217,0.1467945,0.0020769686,0.00061872584,0.00012552066,0.002536433,0.81242496,0.0038528263,0.0036504043,0.009191188,0.0029143346],"about_ca_topic_score_codex":0.00007776647,"about_ca_topic_score_gemma":0.00011132856,"teacher_disagreement_score":0.70863765,"about_ca_system_score_codex":0.00015620708,"about_ca_system_score_gemma":0.00017660767,"threshold_uncertainty_score":0.9999117},"labels":[],"label_agreement":null},{"id":"W2786889285","doi":"10.1007/s00348-017-2486-8","title":"Effects of finite hot-wire spatial resolution on turbulence statistics and velocity spectra in a round turbulent free jet","year":2018,"lang":"en","type":"article","venue":"Experiments in Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":16,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Queen's University; University of Toronto","funders":"Natural Sciences and Engineering Research Council of Canada; Princeton University","keywords":"Turbulence; Dissipation; Physics; Jet (fluid); Turbulence kinetic energy; Length scale; Image resolution; Computational physics; Attenuation; Mechanics; Spectral line; Kolmogorov microscales; Optics; K-omega turbulence model; Thermodynamics","score_opus":0.00793004898392107,"score_gpt":0.2384590935578852,"score_spread":0.23052904457396411,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2786889285","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9473513,0.0005306617,0.050619736,0.000009783726,0.0005674708,0.0002627218,0.000048700185,0.00003819381,0.000571456],"genre_scores_gemma":[0.98874176,0.00016744254,0.010865472,0.000026194353,0.00011586938,0.000023229917,0.0000103213815,0.000026824688,0.000022882587],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99897057,0.000035214336,0.00029141933,0.00022555719,0.00021414981,0.00026311516],"domain_scores_gemma":[0.99949616,0.00014216443,0.000030055917,0.00025591542,0.0000257585,0.000049931237],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001354602,0.00018476362,0.00021738766,0.00011923719,0.00003449418,0.000019907353,0.00016672695,0.00010288662,0.000021943051],"category_scores_gemma":[0.00013384498,0.00019273613,0.00001728361,0.00013343766,0.000116463925,0.00005737173,0.00005687404,0.00019168308,0.0000056311956],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0015410878,0.0029444962,0.0106937755,0.0023820566,0.00033521943,0.0008745476,0.037819162,0.13097264,0.74390286,0.0274802,0.010445408,0.030608533],"study_design_scores_gemma":[0.0015561257,0.00046250632,0.027630966,0.00033236688,0.000009111083,0.000001991702,0.000051376774,0.89035046,0.077456675,0.0017254971,0.00010566268,0.00031725309],"about_ca_topic_score_codex":0.00017699492,"about_ca_topic_score_gemma":0.00012711217,"teacher_disagreement_score":0.75937784,"about_ca_system_score_codex":0.00023351825,"about_ca_system_score_gemma":0.000020826583,"threshold_uncertainty_score":0.78595513},"labels":[],"label_agreement":null},{"id":"W2787590512","doi":"","title":"Inter-comparison of Open and Closed-Path Eddy Covariance Fluxes Over an Irrigated Alfalfa Field in Davis, CA","year":2016,"lang":"en","type":"article","venue":"32nd Conf. on Agricultural and Forest Meteorology/22nd Symp. Boundary Layers and Turbulence/ Third Conf. on Atmospheric Biogeosciences (20 – 24 June, 2016)","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Campbell Scientific (Canada)","funders":"","keywords":"Eddy covariance; Path (computing); Environmental science; Hydrology (agriculture); Field (mathematics); Mathematics; Atmospheric sciences; Geology; Computer science; Geotechnical engineering; Ecosystem","score_opus":0.00907649028918945,"score_gpt":0.2372649944498309,"score_spread":0.22818850416064146,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2787590512","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9924114,0.0018409485,0.0006350161,0.0010167694,0.001474736,0.0006112973,0.00019017924,0.00008326209,0.0017364443],"genre_scores_gemma":[0.9941381,0.0017496134,0.0020678155,0.00061761995,0.000085336236,0.000048409052,0.000035555116,0.00002483791,0.0012326838],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.99703676,0.00011827078,0.00076154224,0.0009922612,0.000350637,0.0007405472],"domain_scores_gemma":[0.9985701,0.00031624912,0.00027178708,0.00039928083,0.00010574222,0.0003368832],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00050373847,0.0006206239,0.0008986737,0.000047423935,0.00038021954,0.0004188339,0.0007915168,0.00041144952,0.000117127674],"category_scores_gemma":[0.000069064336,0.0003553869,0.00008456109,0.00044317034,0.0011062723,0.0006906472,0.0002758448,0.0004445038,0.000010047478],"study_design_candidate":"observational","study_design_consensus":"observational","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0038840608,0.002354235,0.37705436,0.0009621496,0.0013404953,0.00028963276,0.009080815,0.009091183,0.11977399,0.17855425,0.042602174,0.25501266],"study_design_scores_gemma":[0.011311759,0.0138558075,0.55399877,0.0026229576,0.00046924545,0.00027858495,0.004583851,0.30231735,0.0030102383,0.028638043,0.07345783,0.0054555787],"about_ca_topic_score_codex":0.0014490542,"about_ca_topic_score_gemma":0.0023307654,"teacher_disagreement_score":0.29322618,"about_ca_system_score_codex":0.000053930347,"about_ca_system_score_gemma":0.000085440915,"threshold_uncertainty_score":0.9998898},"labels":[],"label_agreement":null},{"id":"W2788804074","doi":"","title":"Numerical Simulations of the Jet Ejected from the Outlet of the Laval Nozzle","year":2015,"lang":"en","type":"article","venue":"Institutional Repositories DataBase (IRDB)","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Maple; Nozzle; Jet (fluid); Rocket engine nozzle; Mechanics; Aerospace engineering; Environmental science; Physics; Engineering; Biology","score_opus":0.016363054336108306,"score_gpt":0.22572743951753607,"score_spread":0.20936438518142778,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2788804074","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9607191,0.00033080368,0.021416966,0.0005086294,0.0077787503,0.0003342092,0.005416124,0.00008419928,0.0034112309],"genre_scores_gemma":[0.9983792,0.0000071140753,0.0008654619,0.000037939037,0.00048317545,0.0000068375643,0.00016551562,0.000013094485,0.00004166427],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99883986,0.000053347456,0.00033205267,0.0001342663,0.0005091,0.00013140446],"domain_scores_gemma":[0.99865144,0.00028915645,0.00009610685,0.00070323807,0.00021247295,0.000047587015],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012258417,0.00013165742,0.00014759866,0.000013884959,0.00023203471,0.000025950321,0.000509952,0.00005964438,0.000011174614],"category_scores_gemma":[0.0007276868,0.0000701093,0.00008813966,0.00029452497,0.00033815566,0.00012834,0.00020637122,0.00024308507,0.0000033818742],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000028424285,0.000091056965,0.02553323,0.00002800824,0.0001365684,0.0000048425645,0.00044368493,0.91475326,0.016658787,0.03351083,0.008751429,0.00005988067],"study_design_scores_gemma":[0.0011276696,0.00004027918,0.07208402,0.00039350128,0.00027467162,0.000040815536,0.0003203479,0.80657226,0.0292654,0.002594183,0.08677622,0.00051062094],"about_ca_topic_score_codex":0.0007849928,"about_ca_topic_score_gemma":0.00023633988,"teacher_disagreement_score":0.108180985,"about_ca_system_score_codex":0.000087750035,"about_ca_system_score_gemma":0.00024718663,"threshold_uncertainty_score":0.28589743},"labels":[],"label_agreement":null},{"id":"W2790260663","doi":"","title":"Application of an Analytical Noise Models Using Numerical and Experimental Fan Data","year":2015,"lang":"en","type":"article","venue":"Espace ÉTS (ETS)","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Deutsche Forschungsgemeinschaft; Compute Canada; Université de Sherbrooke","keywords":"Noise (video); Trailing edge; Acoustics; Broadband; Range (aeronautics); Amplitude; Noise reduction; Inflow; Experimental data; Noise control; Leading edge; Noise measurement; Computer science; Engineering; Physics; Mathematics; Telecommunications; Mechanics; Structural engineering; Optics; Statistics; Aerospace engineering","score_opus":0.03978966206832023,"score_gpt":0.29908948175509276,"score_spread":0.2592998196867725,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2790260663","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.5537122,0.00013589405,0.44549668,0.000016945278,0.00006553572,0.000076539785,0.000032362692,0.00004678836,0.00041708985],"genre_scores_gemma":[0.9800981,0.0000050635817,0.019717371,0.000009905551,0.000077319746,0.0000029446617,0.00005024759,0.000027256037,0.000011754846],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999325,0.000012817516,0.00014265015,0.0002132641,0.00016109535,0.00014518017],"domain_scores_gemma":[0.9992872,0.000015748643,0.000025870664,0.00048723925,0.000027501846,0.00015645442],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00013238484,0.000110111454,0.00015415586,0.000039645704,0.00002421295,0.000025042016,0.0002032781,0.0000628829,0.0000040386867],"category_scores_gemma":[0.000015359772,0.00011288816,0.000013435325,0.0000975893,0.000045811135,0.00023853562,0.00014005521,0.000091737136,0.0000025697777],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000022324544,0.00009388305,0.00026062166,0.000021795538,0.00002636792,0.0000044682565,0.00055165676,0.9701446,0.024087334,0.0028826536,0.00020792663,0.0016963155],"study_design_scores_gemma":[0.00020992891,0.0000251434,0.000057942532,0.000005939828,0.000019395655,0.000006845491,0.0002819899,0.9980815,0.0008349527,0.00021199221,0.00013691274,0.00012745376],"about_ca_topic_score_codex":0.000042025473,"about_ca_topic_score_gemma":0.000006624324,"teacher_disagreement_score":0.42638597,"about_ca_system_score_codex":0.000048584312,"about_ca_system_score_gemma":0.000016271399,"threshold_uncertainty_score":0.46034458},"labels":[],"label_agreement":null},{"id":"W2791269623","doi":"10.1121/1.5027841","title":"Time domain nearfield acoustical holography with three-dimensional linear deconvolution","year":2018,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":16,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Polytechnique Montréal","funders":"","keywords":"Deconvolution; Tikhonov regularization; Acoustic holography; Piston (optics); Mathematics; Convolution (computer science); Extrapolation; Blind deconvolution; Mathematical analysis; Acoustics; Algorithm; Holography; Physics; Computer science; Inverse problem; Optics; Wavefront","score_opus":0.0056027108712719195,"score_gpt":0.20968431898401016,"score_spread":0.20408160811273823,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2791269623","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.18526326,0.00014525863,0.8126931,0.001087029,0.00038674157,0.000111432986,0.000016014956,0.000033584933,0.00026358283],"genre_scores_gemma":[0.84234005,0.00007090546,0.15630165,0.0006386013,0.00058817124,8.9459587e-7,6.702466e-7,0.00003375767,0.000025322937],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99848866,0.0000581474,0.0004193939,0.00009820781,0.0006152186,0.00032034234],"domain_scores_gemma":[0.9985235,0.0004682321,0.0002028172,0.00033034888,0.00036750687,0.000107629334],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006047447,0.00018880768,0.00032886365,0.000023667724,0.00021568606,0.000012455132,0.00055302505,0.0001283204,0.00012778961],"category_scores_gemma":[0.00010490131,0.000096879696,0.00030777836,0.00034333926,0.0018452553,0.00006306343,0.0001233902,0.00066431635,0.000016560698],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00043181021,0.00023584515,0.00024105253,0.00007569163,0.0009278782,0.0000069099365,0.0005254427,0.82896364,0.07206106,0.00003307088,0.09081281,0.0056848144],"study_design_scores_gemma":[0.00034135266,0.00049909315,0.00076613977,0.00007266911,0.0002619947,0.00010601598,0.00017446691,0.9955195,0.00025623356,0.001244564,0.00061523303,0.00014272907],"about_ca_topic_score_codex":0.000007646705,"about_ca_topic_score_gemma":0.0000018851309,"teacher_disagreement_score":0.6570768,"about_ca_system_score_codex":0.00006183598,"about_ca_system_score_gemma":0.00007094632,"threshold_uncertainty_score":0.67989194},"labels":[],"label_agreement":null},{"id":"W2794164972","doi":"10.1007/s00193-018-0806-4","title":"Identification of temporal and spatial signatures of broadband shock-associated noise","year":2018,"lang":"en","type":"article","venue":"Shock Waves","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":24,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Grand Équipement National De Calcul Intensif","keywords":"Physics; Supersonic speed; Mach number; Transonic; Jet (fluid); Shock wave; Shock (circulatory); Reynolds number; Mach reflection; Jet noise; Turbulence; Noise (video); Mach wave; Mechanics; Aerodynamics","score_opus":0.0052409101646876625,"score_gpt":0.2148936450308158,"score_spread":0.20965273486612812,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2794164972","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99230236,0.00023725136,0.006309761,0.000008611084,0.00030921644,0.0000833115,0.00008020218,0.000039750845,0.00062955904],"genre_scores_gemma":[0.99947834,0.000047304613,0.000214781,0.0000037996938,0.00009050886,0.0000016384497,0.000022159367,0.00001784417,0.00012363661],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99937963,0.000011604761,0.00026898528,0.000105804116,0.00012276164,0.00011121387],"domain_scores_gemma":[0.9996255,0.000034229077,0.00007717761,0.00013984917,0.00009364287,0.00002960883],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00011493174,0.00009231135,0.00015859456,0.000055304652,0.000032745287,0.000012121126,0.0000866913,0.000093579394,0.000022271237],"category_scores_gemma":[0.00006193656,0.00008994442,0.000030446558,0.000086231616,0.00010737635,0.000046041332,0.0000289657,0.00007555491,0.0000015155173],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00003121629,0.000083483996,0.013021209,0.0002400638,0.0001418023,0.0000018294007,0.001047408,0.008645963,0.9696824,0.0005798414,0.0012312077,0.005293556],"study_design_scores_gemma":[0.00047048877,0.00013118955,0.072997965,0.000087096836,0.000063959524,0.0000015088323,0.00012489945,0.82554424,0.09815877,0.002050668,0.00011388177,0.000255357],"about_ca_topic_score_codex":0.000051419887,"about_ca_topic_score_gemma":0.0001835023,"teacher_disagreement_score":0.8715236,"about_ca_system_score_codex":0.000016273729,"about_ca_system_score_gemma":0.000010178084,"threshold_uncertainty_score":0.3667827},"labels":[],"label_agreement":null},{"id":"W2795227631","doi":"10.1115/1.4039781","title":"Measurement of the Excitation Source of an Axisymmetric Shallow Cavity Shear Layer","year":2018,"lang":"en","type":"article","venue":"Journal of Pressure Vessel Technology","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"","keywords":"Acoustics; Mechanics; Sound pressure; Standing wave; Resonance (particle physics); Rotational symmetry; Turbulence; Acoustic resonance; Oscillation (cell signaling); Physics; Materials science; Atomic physics","score_opus":0.012119669239445808,"score_gpt":0.2273658255314792,"score_spread":0.2152461562920334,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2795227631","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.94329506,0.001350815,0.053954147,0.00018419694,0.0006712492,0.00010335777,0.0000058303926,0.00004104136,0.0003943236],"genre_scores_gemma":[0.9954789,0.000043187338,0.004322761,0.000006923601,0.00011160595,0.0000012588715,1.5200503e-7,0.000019743293,0.000015414693],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.998898,0.000035328558,0.00044915135,0.00008152744,0.00039059768,0.00014538437],"domain_scores_gemma":[0.99864274,0.000024782787,0.00031983494,0.00031646827,0.000664194,0.000031997413],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00059938023,0.000104214305,0.00026541806,0.0003457958,0.000038481612,0.000005829405,0.0004683821,0.00019908423,0.000010223048],"category_scores_gemma":[0.00027434918,0.00007702363,0.00007565859,0.0005648636,0.0001629553,0.00008827952,0.00005757603,0.0003363994,7.958463e-7],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000058781734,0.00034641835,0.0063413326,0.00045018486,0.0006463962,0.0000070752944,0.0005437735,0.100172214,0.8515392,0.0046506096,0.0011908798,0.034053136],"study_design_scores_gemma":[0.0030304182,0.002727883,0.10998591,0.0010177519,0.0012402408,0.00025156562,0.0011456024,0.44731674,0.37207535,0.02203393,0.038310207,0.0008644106],"about_ca_topic_score_codex":0.000007715596,"about_ca_topic_score_gemma":0.000016667502,"teacher_disagreement_score":0.47946385,"about_ca_system_score_codex":0.00003355929,"about_ca_system_score_gemma":0.00003815054,"threshold_uncertainty_score":0.31409323},"labels":[],"label_agreement":null},{"id":"W2796182680","doi":"10.1115/pvp2014-28508","title":"PIV Measurements of Aeroacoustic Sources of a Shallow Cavity in a Pipeline","year":2014,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"","keywords":"Strouhal number; Acoustics; Vorticity; Turbulence; Physics; Reynolds number; Acoustic source localization; Flow (mathematics); Mechanics; Sound (geography); Geology; Vortex","score_opus":0.0142791303858679,"score_gpt":0.20896955061951664,"score_spread":0.19469042023364874,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2796182680","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8701801,0.000050220533,0.118787706,0.000006632875,0.00011707188,0.00007636032,0.000006015221,0.000040109073,0.010735841],"genre_scores_gemma":[0.9956322,0.000009030268,0.004198748,0.000009448698,0.00002546816,0.0000033999495,0.0000022872468,0.000016987515,0.000102454425],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992466,0.000015394395,0.00030636427,0.000095483505,0.00018821734,0.00014795447],"domain_scores_gemma":[0.9996419,0.000048604743,0.000037923874,0.00018262942,0.000055373035,0.000033559838],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00034109695,0.00009887181,0.0002241983,0.000077512246,0.00000798328,0.0000037535278,0.00013578069,0.000055533517,0.000044088796],"category_scores_gemma":[0.00009465835,0.00009151329,0.00003926553,0.00010089864,0.000029607856,0.000026060925,0.000027350754,0.0000863914,0.000002900649],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00000856732,0.00010882442,0.039579522,0.0003349885,0.000026581401,0.0000010904561,0.00021720731,0.8862521,0.069539525,0.00021335029,0.00015513651,0.0035630947],"study_design_scores_gemma":[0.00037391487,0.000027598971,0.009070396,0.00006133314,0.000017765855,7.414978e-7,0.000033238448,0.9849274,0.0050716237,0.00027499374,0.000025555555,0.000115400566],"about_ca_topic_score_codex":0.000090682945,"about_ca_topic_score_gemma":0.00071320037,"teacher_disagreement_score":0.12545213,"about_ca_system_score_codex":0.000024343228,"about_ca_system_score_gemma":0.000007759454,"threshold_uncertainty_score":0.37318036},"labels":[],"label_agreement":null},{"id":"W2800450176","doi":"10.1016/j.ijheatfluidflow.2018.04.012","title":"Effects of offset height on the turbulent characteristics of a surface attaching jet","year":2018,"lang":"en","type":"article","venue":"International Journal of Heat and Fluid Flow","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":13,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Manitoba","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Reynolds number; Turbulence; Mechanics; Particle image velocimetry; Physics; Vortex; Offset (computer science); Reynolds stress; Boundary layer; Materials science; Optics","score_opus":0.005180134486832129,"score_gpt":0.21769169623233584,"score_spread":0.2125115617455037,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2800450176","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9871585,0.0002698898,0.010838837,0.00026170674,0.0011967089,0.00004650711,0.000027025642,0.0000048415445,0.00019602285],"genre_scores_gemma":[0.99813336,0.00037673823,0.0010028967,0.000065692024,0.00039758757,3.4931514e-7,0.0000023328923,0.000011307053,0.000009723886],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99923444,0.000019524829,0.00034066726,0.000049635,0.00027727042,0.00007847521],"domain_scores_gemma":[0.99935263,0.00022073847,0.00007643071,0.000069629605,0.00024611934,0.00003443063],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021603281,0.000090270085,0.00017606464,0.000055523888,0.000025119105,0.000017319573,0.00020190912,0.000038422746,0.000021848107],"category_scores_gemma":[0.0000606077,0.00005913435,0.00006814504,0.000033383825,0.00006221668,0.000049475602,0.000026924035,0.00014985779,0.0000017622222],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0010208385,0.0006306729,0.007865012,0.0005097877,0.0022584177,0.00027775508,0.0032317126,0.06955768,0.86009645,0.011445991,0.013803619,0.029302076],"study_design_scores_gemma":[0.0006200235,0.00040340048,0.0104076965,0.0005622105,0.00005336102,0.00010111216,0.000026533737,0.94803166,0.03817985,0.00044036636,0.0010436138,0.00013014456],"about_ca_topic_score_codex":0.0000029513017,"about_ca_topic_score_gemma":0.0000010438971,"teacher_disagreement_score":0.878474,"about_ca_system_score_codex":0.000027972368,"about_ca_system_score_gemma":0.000012379014,"threshold_uncertainty_score":0.24114287},"labels":[],"label_agreement":null},{"id":"W2803282037","doi":"10.1115/1.4040389","title":"Effect of the Separation Distance on the Aeroacoustic Source of Multiple Shallow Cavities","year":2018,"lang":"en","type":"article","venue":"Journal of Fluids Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"","keywords":"Particle image velocimetry; Acoustics; Interference (communication); Separation (statistics); Excitation; Physics; Sound pressure; Mechanics; Flow (mathematics); Standing wave; Upstream (networking); Range (aeronautics); Optics; Materials science; Engineering; Mathematics; Turbulence; Telecommunications","score_opus":0.004342432107803495,"score_gpt":0.20505314517935402,"score_spread":0.20071071307155053,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2803282037","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.81676024,0.00019752675,0.18182266,0.000016888554,0.00079805154,0.00008452204,0.0000062960858,0.000016114958,0.00029768745],"genre_scores_gemma":[0.9991642,0.000028757708,0.00043525294,0.000005748942,0.00026975264,0.0000021946812,3.0403552e-7,0.0000275654,0.00006622719],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991605,0.000025583802,0.00036250145,0.00005245213,0.00026249135,0.00013641482],"domain_scores_gemma":[0.9991062,0.00045556604,0.00010642268,0.0002077369,0.00009503492,0.00002902706],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00044644866,0.00013376643,0.00022226786,0.000056458437,0.00004358648,0.000013543472,0.00027269224,0.000051222432,0.000008895393],"category_scores_gemma":[0.0002976874,0.00007754511,0.00012755343,0.00014421898,0.000060465285,0.000055938475,0.000024352506,0.00024051055,9.3198304e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000020049782,0.0000074024933,0.00029415352,0.00014766066,0.000043430184,8.845678e-7,0.00020670518,0.81289464,0.1853726,0.0002082347,0.00023403308,0.0005701811],"study_design_scores_gemma":[0.00022220676,0.00026387826,0.0009834407,0.00029933744,0.000051401545,0.000010839455,0.00003084856,0.9268109,0.07090557,0.000009836886,0.00032819188,0.00008353225],"about_ca_topic_score_codex":0.0000016328802,"about_ca_topic_score_gemma":0.000003463303,"teacher_disagreement_score":0.18240395,"about_ca_system_score_codex":0.00005707561,"about_ca_system_score_gemma":0.000011022654,"threshold_uncertainty_score":0.3162198},"labels":[],"label_agreement":null},{"id":"W2803809847","doi":"10.1121/1.5038265","title":"Fast and accurate analytical modeling of broadband noise for a low-speed fan","year":2018,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":38,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Reynolds-averaged Navier–Stokes equations; Turbulence; Noise (video); Aeroacoustics; Acoustics; Flow (mathematics); Trailing edge; Computational fluid dynamics; Physics; Mechanics; Computer science; Sound pressure","score_opus":0.012683146284812768,"score_gpt":0.24734123380077538,"score_spread":0.23465808751596262,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2803809847","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.22020523,0.0001324346,0.7788727,0.0003914615,0.0001614278,0.0000980718,0.000024904353,0.0000074898717,0.000106229505],"genre_scores_gemma":[0.9744159,0.00038490133,0.024762342,0.00014337622,0.00024998316,4.0622513e-7,3.170826e-7,0.000022289962,0.000020464668],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99894017,0.000027028726,0.0004830595,0.000070189264,0.00026144285,0.0002181176],"domain_scores_gemma":[0.9988708,0.00035514648,0.00019795341,0.00021204202,0.0002836957,0.00008036263],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00043417467,0.000133138,0.00035587107,0.000016577706,0.00010815359,0.000014294118,0.00038651904,0.00007109098,0.000011535413],"category_scores_gemma":[0.00017451213,0.000075212236,0.0002691059,0.00015996826,0.0006413776,0.000053524775,0.0001036468,0.00028188378,4.4169045e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00011599032,0.00005034999,0.000028342865,0.00014221555,0.00026685323,2.1579487e-7,0.0007601397,0.9446184,0.047037356,0.000020846239,0.0027969875,0.0041622906],"study_design_scores_gemma":[0.0003586888,0.00017523003,0.00006871285,0.000092926464,0.00028607712,0.000017351445,0.0007009799,0.9969837,0.00044181207,0.0007424669,0.00004574485,0.00008630531],"about_ca_topic_score_codex":0.000007949638,"about_ca_topic_score_gemma":4.960885e-7,"teacher_disagreement_score":0.7542107,"about_ca_system_score_codex":0.00003130515,"about_ca_system_score_gemma":0.000033689572,"threshold_uncertainty_score":0.3067066},"labels":[],"label_agreement":null},{"id":"W2806246871","doi":"10.1017/jfm.2018.326","title":"The modified Myers boundary condition for swirling flow","year":2018,"lang":"en","type":"article","venue":"Journal of Fluid Mechanics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Agence Nationale de la Recherche","keywords":"Blasius boundary layer; Boundary layer; No-slip condition; Boundary layer thickness; Inviscid flow; Boundary (topology); External flow; Flow (mathematics); Boundary value problem; Boundary layer control; Mechanics; Different types of boundary conditions in fluid dynamics; Mathematical analysis; Physics; Mathematics","score_opus":0.009596331447796303,"score_gpt":0.2332470896986253,"score_spread":0.22365075825082897,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2806246871","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.052292183,0.00045138027,0.94246274,0.000102131075,0.0042501003,0.00010208501,0.000018724255,0.000029539628,0.0002911155],"genre_scores_gemma":[0.9870855,0.0004437075,0.01113194,0.000057568992,0.0011930359,0.000003468238,0.0000031973877,0.00003445162,0.00004710042],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992173,0.000009803046,0.00033918867,0.000057358964,0.00017736379,0.00019901566],"domain_scores_gemma":[0.9993192,0.0001152919,0.0000935998,0.00013146052,0.00027825052,0.00006222981],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005813687,0.00009839841,0.00013763053,0.000049067046,0.00024763425,0.00008058627,0.00020376075,0.00007309678,0.000008302715],"category_scores_gemma":[0.00011249631,0.00007345761,0.000111319714,0.00007441441,0.000023439196,0.00009654154,0.00001593556,0.00017903325,0.0000043115824],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00013621348,0.000031530108,5.0816914e-7,0.00007843809,0.00027888708,0.000012765106,0.00035304486,0.7121564,0.18451041,0.0471649,0.022528818,0.032748092],"study_design_scores_gemma":[0.00033247354,0.00016343202,0.0000015320751,0.000033047843,0.000041077346,0.000030228683,0.00008478013,0.9675798,0.0036476303,0.015908835,0.012089545,0.00008763512],"about_ca_topic_score_codex":2.0431034e-7,"about_ca_topic_score_gemma":0.0000041054495,"teacher_disagreement_score":0.93479335,"about_ca_system_score_codex":0.000090206675,"about_ca_system_score_gemma":0.0000449947,"threshold_uncertainty_score":0.29955143},"labels":[],"label_agreement":null},{"id":"W2808860434","doi":"10.1017/jfm.2018.429","title":"The impedance boundary condition for acoustics in swirling ducted flow","year":2018,"lang":"en","type":"article","venue":"Journal of Fluid Mechanics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Agence Nationale de la Recherche","keywords":"Mechanics; Duct (anatomy); Physics; Boundary value problem; Mean flow; Boundary layer; Turbulence","score_opus":0.006839907119953434,"score_gpt":0.2358533721160263,"score_spread":0.22901346499607286,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2808860434","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.22745796,0.0006306577,0.7678717,0.00007678451,0.0037409302,0.00012026165,0.000023664847,0.000023643268,0.00005443976],"genre_scores_gemma":[0.97997403,0.00092571916,0.01796261,0.000046433877,0.0010250509,0.000003941648,0.0000033769338,0.000035880705,0.000022960608],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99903315,0.000013501676,0.0004589664,0.00006982649,0.0001813085,0.00024324884],"domain_scores_gemma":[0.9991916,0.00016930592,0.00011301105,0.00014236596,0.00033026136,0.00005346188],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006735089,0.00011310844,0.00017163291,0.000073447496,0.0001563269,0.00006658009,0.0002205964,0.00008833143,0.000006364856],"category_scores_gemma":[0.00026712043,0.00008944746,0.00007779126,0.0001351252,0.000026468646,0.00010578741,0.000020204396,0.00026084174,0.0000027937115],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000096180935,0.000034817807,0.0000031356442,0.00008318976,0.00008876965,0.00002189671,0.0002994221,0.6037724,0.36720407,0.0061300052,0.0072148438,0.01505128],"study_design_scores_gemma":[0.00042200772,0.00015814406,0.000020629826,0.000069441085,0.00003110853,0.00004240504,0.0001137454,0.981247,0.0024671534,0.010969862,0.004354597,0.00010389433],"about_ca_topic_score_codex":3.7454723e-7,"about_ca_topic_score_gemma":0.00001155275,"teacher_disagreement_score":0.7525161,"about_ca_system_score_codex":0.00013975558,"about_ca_system_score_gemma":0.00007025202,"threshold_uncertainty_score":0.36475617},"labels":[],"label_agreement":null},{"id":"W2809730457","doi":"10.2514/6.2018-3795","title":"Improvement of the Near Wall Treatment in Large Eddy Simulation for Aeroacoustic Applications","year":2018,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Acoustics; Large eddy simulation; Eddy current; Computer science; Aerospace engineering; Engineering; Physics; Electrical engineering; Mechanics; Turbulence","score_opus":0.008347232688625049,"score_gpt":0.24678718099053543,"score_spread":0.23843994830191037,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2809730457","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.22774105,0.000014382052,0.7699501,0.000026371668,0.00013067892,0.0010369798,0.00004210348,0.000039853265,0.0010185249],"genre_scores_gemma":[0.9953272,0.000005484369,0.0041162046,0.000020192345,0.000058870915,0.00020733433,0.000008557953,0.000013787521,0.00024239751],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99960476,0.000002166304,0.0001388686,0.00007967704,0.000051736733,0.000122806],"domain_scores_gemma":[0.99968415,0.000049621303,0.000020055146,0.00019270723,0.00003849973,0.000014943201],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000058437923,0.00006760582,0.000072170034,0.000016669343,0.000050950228,0.000008385484,0.0000752642,0.000033191423,0.00002396497],"category_scores_gemma":[0.000007049182,0.000047000653,0.00003675587,0.00008068015,0.000020554486,0.000017044958,0.000014633023,0.00002393032,0.0000041471844],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000004178573,0.00007576116,0.00026224458,0.000028703707,0.000016291273,2.4888719e-8,0.00013299711,0.98637986,0.005986169,0.0013398315,0.00005068951,0.0057232534],"study_design_scores_gemma":[0.00047766705,0.00006329682,0.00062162994,0.000004306082,0.00001528675,3.815641e-8,0.000027428114,0.9948467,0.0009324111,0.00039116744,0.0025676636,0.000052409952],"about_ca_topic_score_codex":0.0000130596645,"about_ca_topic_score_gemma":0.00023685892,"teacher_disagreement_score":0.7675861,"about_ca_system_score_codex":0.00008936018,"about_ca_system_score_gemma":0.000012173745,"threshold_uncertainty_score":0.1916631},"labels":[],"label_agreement":null},{"id":"W2810060396","doi":"10.1121/1.5043088","title":"Sparse regularization for reconstructing transient sources with time domain nearfield acoustical holography","year":2018,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":16,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Polytechnique Montréal","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Tikhonov regularization; Regularization (linguistics); Time domain; Deconvolution; Acoustic holography; Inverse problem; Norm (philosophy); Signal reconstruction; Noise reduction; Algorithm; Mathematics; Acoustics; Physics; Computer science; Mathematical analysis; Signal processing; Near and far field; Optics; Artificial intelligence; Radar","score_opus":0.006309357324537686,"score_gpt":0.2029508570470999,"score_spread":0.1966414997225622,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2810060396","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.10658275,0.000058572885,0.89183086,0.0008141569,0.00028558713,0.00015713045,0.000016331775,0.000023291534,0.00023132158],"genre_scores_gemma":[0.73326516,0.000075813026,0.26588714,0.0002786338,0.00043452514,0.0000016209831,6.679076e-7,0.00003063261,0.00002578117],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9987983,0.000053536027,0.00041167633,0.00009048642,0.00037213127,0.00027387377],"domain_scores_gemma":[0.9986096,0.000535993,0.00023043563,0.00024085505,0.0003090036,0.000074134136],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00063865754,0.00015618277,0.0003000394,0.000022330083,0.00023332023,0.00002267614,0.00042187324,0.00010247966,0.00003450259],"category_scores_gemma":[0.0001368177,0.0000841722,0.00028692654,0.0002829482,0.0011295213,0.0000567061,0.000042026375,0.0003713605,0.0000012832514],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0006214047,0.00019272044,0.00021671581,0.00025018817,0.0012163061,0.00000236538,0.003931945,0.7173593,0.21406412,0.00009785928,0.03484994,0.02719712],"study_design_scores_gemma":[0.00043550108,0.0005102164,0.00015887425,0.00010525034,0.00038895398,0.00008970466,0.0013913098,0.99289185,0.0010600345,0.0020117867,0.000810467,0.00014603454],"about_ca_topic_score_codex":0.000002128134,"about_ca_topic_score_gemma":3.9774372e-7,"teacher_disagreement_score":0.6266824,"about_ca_system_score_codex":0.00004146083,"about_ca_system_score_gemma":0.000044981567,"threshold_uncertainty_score":0.41617683},"labels":[],"label_agreement":null},{"id":"W2810594978","doi":"10.1121/1.5044522","title":"Errata: Fast and accurate analytical modeling of broadband noise for a low-speed fan [J. Acoust. Soc. Am. <b>143</b>, 3103–3113 (2018)]","year":2018,"lang":"en","type":"erratum","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Broadband; Acoustics; Noise (video); Computer science; Physics; Telecommunications; Artificial intelligence","score_opus":0.014282251444361125,"score_gpt":0.2474544742241143,"score_spread":0.23317222277975316,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2810594978","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0054266923,0.0020683305,0.98302114,0.0009154641,0.0065888804,0.0005750219,0.00056479935,0.00004382985,0.0007958442],"genre_scores_gemma":[0.85531807,0.034159724,0.0857722,0.0014427423,0.012159254,0.000018718709,0.00009239227,0.0008484046,0.010188483],"study_design_codex":"not_applicable","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99643385,0.00010508055,0.001532156,0.00029469095,0.0009321502,0.0007020637],"domain_scores_gemma":[0.99642587,0.0007093477,0.0010437858,0.0007872059,0.0007806985,0.00025308732],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0010949614,0.0006274089,0.0015525923,0.00007587454,0.0002933145,0.000072805386,0.001517445,0.0006279791,0.000042611],"category_scores_gemma":[0.00047997257,0.0003886512,0.0010968436,0.00037870402,0.0014829704,0.00014199191,0.00045554954,0.0020593093,0.0000019554493],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00015942432,0.00009779253,0.0000034571542,0.00083947025,0.0009508908,0.0000013876254,0.00058090384,0.45538792,0.004399794,0.000004843518,0.5360956,0.0014785388],"study_design_scores_gemma":[0.0006682004,0.0003363487,0.000017925347,0.000699115,0.001753294,0.00005525997,0.0012243005,0.99140066,0.0000482171,0.00066370674,0.0027276934,0.0004052718],"about_ca_topic_score_codex":0.000028265746,"about_ca_topic_score_gemma":0.0000029004289,"teacher_disagreement_score":0.8972489,"about_ca_system_score_codex":0.00018295617,"about_ca_system_score_gemma":0.00029243412,"threshold_uncertainty_score":0.99985653},"labels":[],"label_agreement":null},{"id":"W2810851850","doi":"10.2514/6.2018-3282","title":"Using LES for combustion noise propagation to the far-field by considering the jet flow of a dual-stream nozzle","year":2018,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke; Safran Electronics (Canada)","funders":"Safran Aircraft Engines; Grand Équipement National De Calcul Intensif","keywords":"Nozzle; Dual (grammatical number); Jet (fluid); Jet noise; Acoustics; Combustion; Noise (video); Mechanics; Air stream; Jet stream; Flow (mathematics); Near and far field; Physics; Aerospace engineering; Materials science; Computer science; Environmental science; Engineering; Optics; Chemistry; Art","score_opus":0.020972548922343914,"score_gpt":0.2505912680620079,"score_spread":0.22961871913966397,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2810851850","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.2844814,0.000030301393,0.7137724,0.00035165227,0.00027135923,0.0003500709,0.000029644307,0.000050291717,0.0006628448],"genre_scores_gemma":[0.9822591,0.000009151946,0.017332178,0.00012718659,0.00014996681,0.000022323242,0.0000071942227,0.000019840625,0.00007304041],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99950236,0.00000988261,0.00016728874,0.00009219428,0.000090299254,0.00013795216],"domain_scores_gemma":[0.9995144,0.00015221437,0.000028629705,0.00018670045,0.00009544711,0.00002260075],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017737893,0.000093339106,0.000090529,0.000021061995,0.0001556727,0.000032019758,0.000092203685,0.000049402664,0.00002656599],"category_scores_gemma":[0.000110591885,0.000055930643,0.000033941415,0.00008641295,0.00003812232,0.00003972248,0.00003269885,0.00006962082,0.000003221346],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000029491368,0.000034819266,0.00023383494,0.00011865533,0.00006963063,4.3301938e-7,0.0010224377,0.64786285,0.2983233,0.0030526605,0.023552136,0.025699733],"study_design_scores_gemma":[0.00010327999,0.00005251256,0.000028398576,0.000025263196,0.000023060742,0.0000021651122,0.0002201857,0.9519119,0.045158066,0.00016539988,0.0022284393,0.00008131487],"about_ca_topic_score_codex":0.00006821056,"about_ca_topic_score_gemma":0.00029614984,"teacher_disagreement_score":0.69777775,"about_ca_system_score_codex":0.000023482664,"about_ca_system_score_gemma":0.000009734775,"threshold_uncertainty_score":0.22807854},"labels":[],"label_agreement":null},{"id":"W2883570416","doi":"10.1177/1475472x18785224","title":"Philip J Morris: Some history and professional achievements","year":2018,"lang":"en","type":"article","venue":"International Journal of Aeroacoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Honor; Classics; Library science; Sociology; Art history; History; Computer science","score_opus":0.008893642041900351,"score_gpt":0.23141570310008047,"score_spread":0.22252206105818012,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2883570416","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9010427,0.0013271751,0.060438126,0.00046338982,0.032136884,0.00010439905,0.000061578976,0.00007114045,0.004354629],"genre_scores_gemma":[0.9910734,0.00040988447,0.0050221104,0.0002865422,0.002474993,0.0000011049056,0.000004484823,0.000027048633,0.0007003883],"study_design_codex":"not_applicable","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99891335,0.000012180525,0.0003734991,0.00008473768,0.00047689694,0.0001393382],"domain_scores_gemma":[0.99915224,0.00005179697,0.00013302438,0.000086176435,0.0004826059,0.0000941407],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002246317,0.00012018136,0.0001399489,0.00014615689,0.00003252841,0.00002382831,0.00032364225,0.00007075296,0.00018166026],"category_scores_gemma":[0.00008919603,0.0001102169,0.000048132682,0.000028708191,0.000119886034,0.00019263124,0.00007252479,0.00026178098,0.000018700393],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0005211885,0.0010305183,0.006660061,0.00026348565,0.003132367,0.00088919734,0.003962865,0.094236426,0.19731505,0.021236531,0.6149998,0.055752523],"study_design_scores_gemma":[0.0031998581,0.0004540278,0.01118268,0.00055653247,0.000259352,0.00071228103,0.00045485,0.83542436,0.001437375,0.0116706025,0.13378781,0.0008602682],"about_ca_topic_score_codex":0.0000012320005,"about_ca_topic_score_gemma":0.0000017833177,"teacher_disagreement_score":0.74118793,"about_ca_system_score_codex":0.00028199572,"about_ca_system_score_gemma":0.000063227984,"threshold_uncertainty_score":0.44945148},"labels":[],"label_agreement":null},{"id":"W2883746298","doi":"","title":"Wind turbine aeroacoustic noise prediction using computational models and comparison to experimental measurements","year":2017,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":true,"ca_institutions":"University of Waterloo","funders":"","keywords":"Wind power; Turbine; Noise (video); Airfoil; Marine engineering; Acoustics; Predictive modelling; Engineering; Computational fluid dynamics; Environmental science; Aerospace engineering; Computer science; Physics; Electrical engineering; Machine learning","score_opus":0.054809242690575334,"score_gpt":0.2711678625592413,"score_spread":0.21635861986866597,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2883746298","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.74966455,0.00013692328,0.24770303,0.000028966766,0.0009658805,0.00023052168,0.00030009,0.00006149465,0.0009085282],"genre_scores_gemma":[0.9847228,0.0000054371108,0.014861379,0.0000835935,0.00020405465,0.0000048032825,0.00003259608,0.000053043055,0.000032287073],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99890214,0.000007835771,0.00024181949,0.00022574334,0.00024504378,0.00037743687],"domain_scores_gemma":[0.99896616,0.000016473805,0.00004611087,0.0003019469,0.000099559395,0.00056977145],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00010454804,0.000206452,0.0001992303,0.00013984977,0.00054046593,0.00023187291,0.00021997771,0.00010922618,0.000017330955],"category_scores_gemma":[0.000044740344,0.0002511785,0.000025194757,0.00004900941,0.000072973584,0.0001704097,0.0000497942,0.00016637791,0.000007752072],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000031061952,0.000012319917,0.001039912,0.000023317449,0.000030329737,0.0000089351515,0.0001829896,0.97485244,0.022351533,0.000050103215,0.0011470291,0.00029801216],"study_design_scores_gemma":[0.00029540143,0.000027009299,0.010718987,0.000045978013,0.000051876323,0.000010096432,0.00010984059,0.988222,0.00006966024,0.00018204824,0.000029378421,0.00023770837],"about_ca_topic_score_codex":0.0016580876,"about_ca_topic_score_gemma":0.0011595413,"teacher_disagreement_score":0.23505825,"about_ca_system_score_codex":0.0005420946,"about_ca_system_score_gemma":0.00011425481,"threshold_uncertainty_score":0.99999404},"labels":[],"label_agreement":null},{"id":"W2884047390","doi":"10.1177/1475472x18789005","title":"Advanced noise modeling for future propulsion systems","year":2018,"lang":"en","type":"article","venue":"International Journal of Aeroacoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":49,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Agence Nationale de la Recherche","keywords":"Turbomachinery; Airfoil; Acoustics; Noise (video); Turbofan; Rotor (electric); Solidity; Propulsion; Computer science; Aeroacoustics; Physics; Aerospace engineering; Mechanics; Engineering; Sound pressure","score_opus":0.008337794306489385,"score_gpt":0.2450104443787152,"score_spread":0.23667265007222582,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2884047390","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.20193918,0.00027722793,0.78183293,0.00010574663,0.015274161,0.000109992085,0.000055362834,0.00003564347,0.00036977258],"genre_scores_gemma":[0.9613637,0.00024861138,0.031434327,0.00003133211,0.006802123,0.0000041797343,0.000009040159,0.000039205697,0.00006749093],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9988838,0.000006670403,0.00047030646,0.00008573874,0.0003912293,0.00016227602],"domain_scores_gemma":[0.99807495,0.00003961958,0.0001380229,0.000100754274,0.0015723512,0.00007432639],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020239546,0.00012979913,0.0001720508,0.00012316609,0.000049699123,0.00007630697,0.0003766468,0.000087959066,0.000007836285],"category_scores_gemma":[0.00008860592,0.000113911585,0.00009091791,0.000055886758,0.000026346985,0.00014739498,0.000027786466,0.0001824439,0.000004399905],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00006256168,0.000024336814,0.000011697988,0.000031960903,0.00010273414,0.00001208864,0.000108170825,0.9818042,0.010430733,0.00070382433,0.0014521193,0.00525558],"study_design_scores_gemma":[0.00051615393,0.000114958195,0.000011484805,0.00011315495,0.000038337705,0.00008246248,0.00026390186,0.99471736,0.00022946957,0.0005877975,0.0031987005,0.00012619267],"about_ca_topic_score_codex":7.7119756e-7,"about_ca_topic_score_gemma":0.0000016709738,"teacher_disagreement_score":0.7594245,"about_ca_system_score_codex":0.00014281172,"about_ca_system_score_gemma":0.000036073554,"threshold_uncertainty_score":0.46451798},"labels":[],"label_agreement":null},{"id":"W2887084845","doi":"","title":"New Perspectives in Eddy Covariance Measurements Using Aircraft-Based Technology","year":2016,"lang":"en","type":"article","venue":"32nd Conf. on Agricultural and Forest Meteorology/22nd Symp. Boundary Layers and Turbulence/ Third Conf. on Atmospheric Biogeosciences (20 – 24 June, 2016)","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Agriculture and Agri-Food Canada","funders":"","keywords":"Eddy covariance; Covariance; Environmental science; Computer science; Remote sensing; Meteorology; Mathematics; Geology; Geography; Statistics","score_opus":0.01322668473918131,"score_gpt":0.20896378944541089,"score_spread":0.19573710470622957,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2887084845","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9776105,0.0047384575,0.009810603,0.0030338606,0.0023674003,0.0006808885,0.00009180348,0.00030826085,0.0013582112],"genre_scores_gemma":[0.98293763,0.0014474973,0.013352987,0.0004706364,0.00016495974,0.000048143986,0.000010430833,0.00003913312,0.0015285977],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99648714,0.00009308308,0.00063315046,0.0011852613,0.0005387944,0.001062541],"domain_scores_gemma":[0.9986528,0.00018185884,0.00022330877,0.00041335597,0.00016603392,0.00036261856],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00048192433,0.0007513777,0.00076240033,0.000102275444,0.0005603851,0.00026791156,0.00062811305,0.0005310737,0.00008970532],"category_scores_gemma":[0.000083041945,0.00044489995,0.00013086402,0.00092188537,0.0013944478,0.0003907598,0.00012190464,0.000515011,0.00003059282],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0026883036,0.0017204825,0.17778979,0.000685081,0.0016526087,0.0005374757,0.004345901,0.13385303,0.26688465,0.21187915,0.017133176,0.18083033],"study_design_scores_gemma":[0.027290689,0.011675649,0.2562035,0.004884602,0.0009936641,0.000955044,0.013386771,0.5135786,0.0056446027,0.05607821,0.096203975,0.0131047],"about_ca_topic_score_codex":0.00040192532,"about_ca_topic_score_gemma":0.000729795,"teacher_disagreement_score":0.37972558,"about_ca_system_score_codex":0.00020238283,"about_ca_system_score_gemma":0.00023678508,"threshold_uncertainty_score":0.99980026},"labels":[],"label_agreement":null},{"id":"W2887570707","doi":"10.1016/j.jsv.2018.07.036","title":"Experimental study of the noise radiated by an air flow discharge through diaphragms and perforated plates","year":2018,"lang":"en","type":"article","venue":"Journal of Sound and Vibration","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Université de Lyon; Agence Nationale de la Recherche","keywords":"Acoustics; Duct (anatomy); Supersonic speed; Sound pressure; Diaphragm (acoustics); Physics; Aeroacoustics; Optics; Noise (video); Materials science; Radiation; Shock (circulatory); Vortex shedding; Mechanics; Turbulence; Vibration","score_opus":0.008818478657470116,"score_gpt":0.2329831247454909,"score_spread":0.22416464608802078,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2887570707","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99552596,0.00025983996,0.0038088728,0.000015873464,0.0002514877,0.000083156636,0.000010420332,0.000007593776,0.000036794587],"genre_scores_gemma":[0.99953043,0.000034486715,0.00026645995,0.000014603977,0.00013431549,6.727773e-7,0.0000034981013,0.000010563509,0.0000049785676],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995537,0.000019692703,0.00020469257,0.000055318214,0.00010016851,0.0000664661],"domain_scores_gemma":[0.99976444,0.000014510129,0.00008155108,0.00006103927,0.000045633056,0.000032819138],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00008808981,0.000076436954,0.000111436355,0.000019688046,0.00010727754,0.00003863167,0.0000541889,0.00003089815,0.000009963001],"category_scores_gemma":[0.0000073097444,0.000050391143,0.00001571454,0.00006304776,0.000049430277,0.00033354337,0.000014488769,0.000089221096,1.936126e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00016555085,0.0011490998,0.02298708,0.00006310725,0.00026713344,0.0000042719785,0.030783804,0.056097087,0.88626033,0.00021881159,0.00094805035,0.0010556785],"study_design_scores_gemma":[0.001285217,0.0013327192,0.012608818,0.000033085966,0.000048457427,0.000023572857,0.0047265454,0.951768,0.027562393,0.00042145525,0.00004465104,0.00014510976],"about_ca_topic_score_codex":0.0000049627924,"about_ca_topic_score_gemma":0.000009229404,"teacher_disagreement_score":0.8956709,"about_ca_system_score_codex":0.000012051917,"about_ca_system_score_gemma":0.0000054450047,"threshold_uncertainty_score":0.20548911},"labels":[],"label_agreement":null},{"id":"W2887586616","doi":"10.1017/jfm.2018.546","title":"Transition in a separation bubble under tonal and broadband acoustic excitation","year":2018,"lang":"en","type":"article","venue":"Journal of Fluid Mechanics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":50,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Waterloo","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Airfoil; Bubble; Excitation; Physics; Acoustics; Vortex; Particle image velocimetry; Mechanics; Flow (mathematics); Mean flow; Turbulence","score_opus":0.00792294740505989,"score_gpt":0.23776536473026721,"score_spread":0.22984241732520733,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2887586616","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.4991983,0.0001275842,0.50019276,0.000041194777,0.00032902972,0.000032426295,0.0000022430656,0.0000075566177,0.00006889498],"genre_scores_gemma":[0.9965067,0.000249734,0.0029294542,0.00005302845,0.00023430414,8.963672e-7,0.0000023619739,0.000013686892,0.000009863114],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99941385,0.000013314892,0.00026632976,0.00005698286,0.00014453624,0.00010497302],"domain_scores_gemma":[0.9997215,0.000028783796,0.000046871806,0.000047421338,0.00011135454,0.000044062683],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00026302657,0.000076098215,0.00011866664,0.00011347364,0.00002984633,0.000027052618,0.000043865333,0.00007124237,0.000017863555],"category_scores_gemma":[0.000018672077,0.00007477223,0.000025758705,0.0001047831,0.000010284012,0.00017341314,0.000004889671,0.00013215556,0.0000022746106],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00005019373,0.000032771663,0.000004891564,0.000050750863,0.000029164825,0.000012552916,0.00084877416,0.43364885,0.5593166,0.0038134055,0.00041579764,0.0017762758],"study_design_scores_gemma":[0.00045674713,0.00017052954,0.00023906327,0.000058830472,0.000026188984,0.000064219326,0.00015610011,0.98392045,0.0014867466,0.013282417,0.000056528672,0.000082160484],"about_ca_topic_score_codex":0.0000012558095,"about_ca_topic_score_gemma":0.000039080118,"teacher_disagreement_score":0.5578298,"about_ca_system_score_codex":0.000075205615,"about_ca_system_score_gemma":0.000023132265,"threshold_uncertainty_score":0.3049123},"labels":[],"label_agreement":null},{"id":"W2889225512","doi":"10.1115/gt2018-75837","title":"Acoustic Properties of Perforated Liners With Perpendicular Arrangements of Narrow Slots","year":2018,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Siemens (Canada)","funders":"","keywords":"Perpendicular; Materials science; Pressure drop; Expansion chamber; Combustor; Mechanics; Absorption (acoustics); Stress (linguistics); Drop (telecommunication); Acoustics; Optics; Combustion; Physics; Composite material; Geometry; Mechanical engineering; Engineering","score_opus":0.008176488139708619,"score_gpt":0.17676836207957428,"score_spread":0.16859187393986566,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2889225512","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97722536,0.000092539805,0.018509904,0.0000070837464,0.00014377429,0.00013140772,0.000006416668,0.000073753115,0.0038097834],"genre_scores_gemma":[0.99649376,0.000012148352,0.0030461354,0.0000077070745,0.000046511388,0.000005560085,0.000003438393,0.00002995947,0.0003547849],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993635,0.0000065061,0.00019615782,0.00010243683,0.00017652083,0.00015490927],"domain_scores_gemma":[0.99956805,0.0000064855476,0.000037370934,0.00018113894,0.00017113397,0.000035837005],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000077970195,0.00012009602,0.00017540397,0.000057917307,0.00002696675,0.0000062994814,0.00012263721,0.000045740333,0.000108335495],"category_scores_gemma":[0.000015882948,0.0000840593,0.000025542176,0.00014806319,0.00014276704,0.000050741462,0.000019342857,0.00006417187,0.0000049708315],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000057484904,0.00007159275,0.0012009005,0.0005621414,0.00019745079,0.000004860358,0.0006173355,0.2519557,0.7438309,0.00017447576,0.0008402405,0.00048689792],"study_design_scores_gemma":[0.00038861533,0.00025712317,0.0003532953,0.00014410232,0.00006178794,0.0000032452444,0.00030676782,0.9044199,0.093785025,0.000026416692,0.00007344893,0.00018026576],"about_ca_topic_score_codex":0.000014716433,"about_ca_topic_score_gemma":0.000036406404,"teacher_disagreement_score":0.6524642,"about_ca_system_score_codex":0.000017737024,"about_ca_system_score_gemma":0.000018129898,"threshold_uncertainty_score":0.34278387},"labels":[],"label_agreement":null},{"id":"W2890563842","doi":"10.1088/1873-7005/aae16a","title":"Analogy between vortex waves and EM waves","year":2018,"lang":"en","type":"article","venue":"Fluid Dynamics Research","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Polytechnique Montréal","funders":"","keywords":"Physics; Analogy; Vortex; Mechanics; Classical mechanics; Philosophy","score_opus":0.03292054402194173,"score_gpt":0.32028892458959946,"score_spread":0.28736838056765773,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2890563842","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.96332467,0.000270133,0.020971268,0.000118924545,0.0003570515,0.0001938982,0.0001262156,0.00015420128,0.014483642],"genre_scores_gemma":[0.99522644,0.00038958306,0.0022126203,0.000012101623,0.00064335193,0.00001134374,0.00006906598,0.000072129136,0.0013633544],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9981112,0.00007433771,0.0002730182,0.00033894027,0.00046018124,0.00074231817],"domain_scores_gemma":[0.9987669,0.0002825002,0.000014065283,0.000453781,0.0002675652,0.00021518902],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00085652084,0.00019173071,0.00025219627,0.00032134922,0.00027821213,0.00014752908,0.00037097707,0.00019629899,0.00008892525],"category_scores_gemma":[0.00014484856,0.00019077603,0.000041682477,0.00046392973,0.00044521564,0.000098832395,0.00028298577,0.0005609346,0.00014437646],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00015080704,0.00032597577,0.090642214,0.0017555912,0.0016680359,0.00042456164,0.0075324695,0.020581743,0.061472405,0.29422316,0.03382515,0.48739788],"study_design_scores_gemma":[0.0001677547,0.00012711379,0.017610883,0.00002504334,0.000010127842,0.000007220964,0.00019514054,0.9732929,0.00010857315,0.0069249747,0.0013108079,0.00021947065],"about_ca_topic_score_codex":0.000033096574,"about_ca_topic_score_gemma":0.00050494383,"teacher_disagreement_score":0.95271116,"about_ca_system_score_codex":0.00016795733,"about_ca_system_score_gemma":0.00003762037,"threshold_uncertainty_score":0.777962},"labels":[],"label_agreement":null},{"id":"W2891313031","doi":"10.1016/j.jsv.2018.09.001","title":"Optimization of tonal noise control with flow obstruction","year":2018,"lang":"en","type":"article","venue":"Journal of Sound and Vibration","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":9,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Fonds de recherche du Québec – Nature et technologies; Natural Sciences and Engineering Research Council of Canada; Canada Foundation for Innovation","keywords":"Acoustics; Noise (video); Vortex; Aeroacoustics; Amplitude; Rotor (electric); Mechanics; Control theory (sociology); Physics; Mathematics; Optics; Sound pressure; Computer science","score_opus":0.004245516301862878,"score_gpt":0.1882541811311747,"score_spread":0.18400866482931183,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2891313031","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.35202962,0.000031004038,0.6475752,0.000015010807,0.00017800339,0.000020541556,0.0000027860967,0.0000045266947,0.00014329735],"genre_scores_gemma":[0.96914464,0.000030590723,0.030470222,0.000010358901,0.00033123657,1.9999202e-7,0.0000022186805,0.000006707048,0.000003796301],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996543,0.000005620797,0.00017224881,0.00002999753,0.00009397949,0.000043881162],"domain_scores_gemma":[0.9996899,0.000014768707,0.00009085335,0.000030556814,0.0001498387,0.000024112123],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00007526794,0.0000459523,0.00008532005,0.000043971897,0.000032527336,0.000022460927,0.000022678694,0.00003190997,0.00001786724],"category_scores_gemma":[0.000009877263,0.00003562922,0.000015257386,0.00004807941,0.000034064375,0.00019692954,0.0000020709635,0.00005335565,2.396126e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00004504021,0.0000074769205,0.00050654716,0.000016781485,0.00002591561,5.716637e-7,0.0001022928,0.9904025,0.0070660836,0.00022755918,0.000027150634,0.0015720454],"study_design_scores_gemma":[0.0004790829,0.0001998629,0.0015606291,0.000024467377,0.000028490953,0.00003288994,0.000042902684,0.9964541,0.00055472064,0.00055833126,0.000021303013,0.000043199336],"about_ca_topic_score_codex":3.9270054e-7,"about_ca_topic_score_gemma":0.0000025182133,"teacher_disagreement_score":0.6171151,"about_ca_system_score_codex":0.000013558526,"about_ca_system_score_gemma":0.000008997264,"threshold_uncertainty_score":0.14529175},"labels":[],"label_agreement":null},{"id":"W2893120794","doi":"10.1115/1.4041560","title":"The Effect of the Nozzle Top Lip Thickness on a Two-Dimensional Wall Jet","year":2018,"lang":"en","type":"article","venue":"Journal of Fluids Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Windsor; Western University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Nozzle; Jet (fluid); Reynolds number; Materials science; Mechanics; Wind tunnel; Optics; Composite material; Physics; Turbulence; Thermodynamics","score_opus":0.003403795476587451,"score_gpt":0.20432643469901285,"score_spread":0.2009226392224254,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2893120794","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99058056,0.000337387,0.0053452067,0.00011583451,0.0030384215,0.00008968908,0.0000035420542,0.00003159825,0.00045777074],"genre_scores_gemma":[0.99852407,0.000023763592,0.00067743653,0.00002233486,0.0006700418,0.000002069161,2.2608111e-7,0.00003673753,0.000043338827],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989517,0.000026383359,0.0003725516,0.000070131406,0.0003541645,0.00022511846],"domain_scores_gemma":[0.99905294,0.00043888224,0.000074224714,0.00026053193,0.000111943424,0.00006149073],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00066694967,0.00017207694,0.00023038569,0.00006449109,0.00009645304,0.00003058296,0.00039502425,0.000065475055,0.000011747489],"category_scores_gemma":[0.00020945468,0.0000906477,0.00016833952,0.00016408665,0.000052314957,0.000057008074,0.000053057458,0.0004445283,0.000005414193],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000059616024,0.000008265647,0.00024357962,0.00005925474,0.00008718302,0.0000073118986,0.0000824067,0.88193595,0.11491104,0.00051793334,0.0010962312,0.0009911924],"study_design_scores_gemma":[0.0006651963,0.00066508,0.0014804988,0.00033738394,0.00006387424,0.00009031801,0.0000063018533,0.9486143,0.045490425,0.00006564365,0.0023462716,0.00017467828],"about_ca_topic_score_codex":0.0000019967695,"about_ca_topic_score_gemma":0.0000023274267,"teacher_disagreement_score":0.06942062,"about_ca_system_score_codex":0.00007302144,"about_ca_system_score_gemma":0.000018837216,"threshold_uncertainty_score":0.3696506},"labels":[],"label_agreement":null},{"id":"W2895054269","doi":"","title":"Suppression of Flow-Excited Acoustic Resonance in Rectangular Cavities Using Spanwise High Frequency Vortex Generators","year":2018,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Ontario Tech University","funders":"","keywords":"Vortex; Vortex shedding; Acoustics; Duct (anatomy); Materials science; Acoustic resonance; Optics; Mechanics; Resonance (particle physics); Vortex generator; Flow (mathematics); Enhanced Data Rates for GSM Evolution; Static pressure; Physics; Turbulence; Resonator; Engineering; Anatomy; Reynolds number; Telecommunications; Atomic physics","score_opus":0.008491268364253844,"score_gpt":0.2144847309245251,"score_spread":0.20599346256027126,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2895054269","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9398918,0.00047896814,0.057525553,0.000005026606,0.0009222381,0.000121639205,0.00004618063,0.00011460417,0.00089396874],"genre_scores_gemma":[0.9623711,0.000092719274,0.037147377,0.000017562732,0.00022382216,0.0000050799463,0.000012300434,0.000049683702,0.0000803512],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99888515,0.000024702775,0.0003779906,0.00020996104,0.00019009775,0.0003121092],"domain_scores_gemma":[0.9994419,0.00004104668,0.000041372437,0.00032653866,0.00009222288,0.000056901383],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00013781108,0.00019175468,0.00025820642,0.00015189782,0.00005285025,0.000017829521,0.00017268259,0.00014496579,0.00018763838],"category_scores_gemma":[0.00005896321,0.00018273012,0.000040202118,0.00034048382,0.00010347895,0.00011023765,0.00004692293,0.00016038932,0.0000053741373],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000013069154,0.00003782256,0.0026511692,0.0001281627,0.000021521306,0.000036666774,0.000400401,0.31729144,0.6763071,0.0007959428,0.00040899412,0.0019076997],"study_design_scores_gemma":[0.00024697825,0.000029296343,0.0023737834,0.00015539894,0.000017550386,0.0000037181408,0.00006943301,0.97597003,0.019906169,0.00093559624,0.00005279712,0.00023922727],"about_ca_topic_score_codex":0.00034326036,"about_ca_topic_score_gemma":0.00047011123,"teacher_disagreement_score":0.6586786,"about_ca_system_score_codex":0.00011599228,"about_ca_system_score_gemma":0.000029646655,"threshold_uncertainty_score":0.74515176},"labels":[],"label_agreement":null},{"id":"W2895617529","doi":"","title":"Self-Excited Oscillations of Wiping Air Knives Part II: Suppression of Jet Oscillation","year":2018,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"","keywords":"Jet (fluid); Planar; Oscillation (cell signaling); Particle image velocimetry; Mechanics; Physics; Acoustics; Jet noise; Optics; Turbulence","score_opus":0.00799489964492032,"score_gpt":0.21546351007963413,"score_spread":0.20746861043471382,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2895617529","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.92002094,0.000034641474,0.04660879,0.000031030297,0.0005179948,0.00012272739,0.000031274532,0.00021237905,0.032420237],"genre_scores_gemma":[0.98832434,0.000045542354,0.011255893,0.000006717294,0.00012801104,0.0000017220452,0.000018503832,0.000017683926,0.00020161021],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993413,0.000010539678,0.000279082,0.00010389911,0.00013834261,0.00012679952],"domain_scores_gemma":[0.99951816,0.000050937826,0.00005908782,0.00019864761,0.00013914237,0.000034040197],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00009066359,0.000096327174,0.0001475857,0.000091077505,0.00007865071,0.0000043358677,0.00008478253,0.00007401744,0.00016240313],"category_scores_gemma":[0.000033689263,0.00008625765,0.00004184667,0.00020673785,0.00005586261,0.00009279008,0.000048761798,0.000054988013,0.0000056981976],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000031272295,0.0002899315,0.017898606,0.0007951609,0.00030363153,0.0000013219462,0.0041601914,0.608563,0.31978232,0.029983787,0.014709373,0.0034813827],"study_design_scores_gemma":[0.00016446915,0.00006843635,0.0046482217,0.000070409194,0.000020794736,7.3761106e-7,0.0000686817,0.9794653,0.010008736,0.0004173908,0.0049436954,0.00012310181],"about_ca_topic_score_codex":0.000008043816,"about_ca_topic_score_gemma":0.000020504382,"teacher_disagreement_score":0.3709023,"about_ca_system_score_codex":0.00002200945,"about_ca_system_score_gemma":0.000011925141,"threshold_uncertainty_score":0.35174847},"labels":[],"label_agreement":null},{"id":"W2895894736","doi":"10.1121/1.5067572","title":"Design and evaluation of a high-speed aeroacoustic wind tunnel","year":2018,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"Carleton University","funders":"","keywords":"Wind tunnel; Hypersonic wind tunnel; Supersonic wind tunnel; Anechoic chamber; Mach number; Subsonic and transonic wind tunnel; Aeroacoustics; Aerodynamics; Nozzle; Turbulence; Wind speed; Boundary layer; Noise (video); Jet (fluid); Aerospace engineering; Flow (mathematics); Airflow; Acoustics; Marine engineering; Meteorology; Mechanics; Engineering; Transonic; Physics; Mechanical engineering; Computer science; Sound pressure","score_opus":0.01908248166424069,"score_gpt":0.24752616619899273,"score_spread":0.22844368453475206,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2895894736","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.32258055,0.00027992052,0.67628634,0.00029171773,0.00032138548,0.00015585142,0.0000062946715,0.0000085426345,0.00006943429],"genre_scores_gemma":[0.94599307,0.00032986962,0.053331703,0.000104021245,0.00020910401,3.6890327e-7,2.1374447e-7,0.000020729185,0.000010918122],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9984831,0.00015200484,0.0004480743,0.00006807532,0.0006643364,0.00018440973],"domain_scores_gemma":[0.9983096,0.0005615152,0.00029618407,0.0002572385,0.0005144254,0.00006101629],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0016523831,0.0001333468,0.00030689032,0.000019107918,0.0001068313,0.0000106397,0.00039195715,0.00007470584,0.000045773402],"category_scores_gemma":[0.00025266604,0.000076262426,0.00014227642,0.00021890452,0.0008302911,0.0000542122,0.000091328715,0.00030311086,0.000001362035],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000045773646,0.000040258656,0.000009063635,0.000042448934,0.00020179145,1.5439996e-7,0.00072254846,0.88224536,0.105012104,0.0000058156647,0.00444501,0.0072296667],"study_design_scores_gemma":[0.0004311721,0.00022639474,0.0011773941,0.00007386053,0.00076342875,0.000024154173,0.0005366761,0.9930661,0.0012675484,0.0023278568,0.000021170323,0.00008428895],"about_ca_topic_score_codex":0.000012718093,"about_ca_topic_score_gemma":3.223321e-7,"teacher_disagreement_score":0.62341255,"about_ca_system_score_codex":0.000069684334,"about_ca_system_score_gemma":0.00007129977,"threshold_uncertainty_score":0.31098914},"labels":[],"label_agreement":null},{"id":"W2898220985","doi":"10.1115/fedsm2018-83269","title":"Nozzle Orientation Effects on the Turbulent Structure of Submerged Twin Jets","year":2018,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Ontario Tech University; University of Manitoba","funders":"","keywords":"Nozzle; Turbulence; Mechanics; Reynolds number; Materials science; Hydraulic diameter; Body orifice; Physics; Geometry; Engineering; Mathematics; Mechanical engineering; Thermodynamics","score_opus":0.004805686343928478,"score_gpt":0.20441276804157066,"score_spread":0.19960708169764219,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2898220985","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9888453,0.000012124354,0.00693721,0.00007097278,0.0007052758,0.00013287045,0.0000061862024,0.000060381284,0.0032296737],"genre_scores_gemma":[0.99893993,0.000005512044,0.00064746686,0.00009862434,0.00017820898,0.000002736464,0.0000056460894,0.00001565245,0.00010624868],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9995757,0.000011386436,0.00010138624,0.00007984998,0.000120280354,0.000111414905],"domain_scores_gemma":[0.99968,0.000055872777,0.000017723802,0.00018478264,0.000039608676,0.000022055701],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000047173882,0.000083162566,0.00007423248,0.000023194283,0.000038477603,0.000009181468,0.00009557212,0.000043071683,0.00019677036],"category_scores_gemma":[0.000030022251,0.000052545587,0.000024562489,0.000091937196,0.000027006046,0.000020358615,0.000012120064,0.0000827422,0.000019716645],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000031921776,0.00004292705,0.00056712114,0.00021021553,0.00013017649,0.000005261317,0.0013248562,0.06674434,0.8492622,0.050076187,0.022533474,0.009071313],"study_design_scores_gemma":[0.0003350481,0.00017256443,0.0072288513,0.0000463899,0.000027793467,0.0000021225262,0.00007723678,0.4763005,0.51139617,0.0031088367,0.0010868561,0.00021760138],"about_ca_topic_score_codex":0.0000059181325,"about_ca_topic_score_gemma":0.000026780259,"teacher_disagreement_score":0.40955618,"about_ca_system_score_codex":0.00002128726,"about_ca_system_score_gemma":0.0000036562076,"threshold_uncertainty_score":0.21544974},"labels":[],"label_agreement":null},{"id":"W2898477691","doi":"10.1115/fedsm2018-83495","title":"Comparative Evaluation of Single/Twin Round and Elliptic Jets Using Particle Image Velocimetry","year":2018,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Manitoba","funders":"","keywords":"Particle image velocimetry; Physics; Mechanics; Nozzle; Jet (fluid); Particle tracking velocimetry; Velocimetry; Skewness; Turbulence; Classical mechanics; Mathematics; Thermodynamics","score_opus":0.06738094550098028,"score_gpt":0.3117691861591661,"score_spread":0.24438824065818582,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2898477691","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9319174,0.00015652078,0.062769994,0.000004340519,0.0001495154,0.00010200861,0.000003432081,0.000038785223,0.0048580007],"genre_scores_gemma":[0.98550427,0.0000042289853,0.014382107,0.0000067977658,0.000067147,0.0000015636011,0.0000018271712,0.00001214326,0.000019941364],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99939716,0.000023775987,0.00016494964,0.0001003935,0.0001837053,0.0001300272],"domain_scores_gemma":[0.9996032,0.000041526764,0.00002633208,0.00011576923,0.00017730877,0.00003582346],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00029434016,0.00008391012,0.00013121458,0.00002925647,0.000044870925,0.000028217293,0.000044651562,0.000035552148,0.000107120504],"category_scores_gemma":[0.000026906915,0.00008111625,0.000015319076,0.0001190863,0.000105045816,0.000111611356,0.000024416611,0.00004520303,0.00001177898],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00000521602,0.000043623866,0.0003919022,0.000032664273,0.0000516354,5.491735e-7,0.000754592,0.040875033,0.955159,0.0005838546,0.000093587754,0.0020083177],"study_design_scores_gemma":[0.00021502281,0.000038269518,0.0016835377,0.000015046029,0.000057248944,0.0000020031064,0.00019427796,0.92784756,0.06935817,0.00048613633,0.000011146741,0.000091600945],"about_ca_topic_score_codex":0.000010399274,"about_ca_topic_score_gemma":0.000020999365,"teacher_disagreement_score":0.8869725,"about_ca_system_score_codex":0.00006547261,"about_ca_system_score_gemma":0.000012315275,"threshold_uncertainty_score":0.33078247},"labels":[],"label_agreement":null},{"id":"W2898854229","doi":"10.1016/j.jsv.2018.10.058","title":"Experimental investigation of the interplay between the sound field and the flow field in skewed low-pressure axial fans","year":2018,"lang":"en","type":"article","venue":"Journal of Sound and Vibration","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":39,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Turbulence; Acoustics; Sound pressure; Mechanical fan; Physics; Aerodynamics; Aeroacoustics; Mechanics; Noise (video); Turbulence kinetic energy; Jet (fluid); Vortex; Computer science","score_opus":0.007283202884532171,"score_gpt":0.24042437892471816,"score_spread":0.233141176040186,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2898854229","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9738742,0.00019849619,0.02475166,0.0005957408,0.00034707488,0.00007869292,0.0000030862495,0.0000027608824,0.00014826548],"genre_scores_gemma":[0.9992455,0.000020110805,0.0001736155,0.00013843323,0.0004095678,9.4910195e-7,6.944968e-7,0.000004954768,0.0000061229266],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99952906,0.000039650833,0.0002284159,0.000041417974,0.000103118706,0.00005832463],"domain_scores_gemma":[0.99956113,0.00022825752,0.00008857306,0.000073691575,0.0000311776,0.000017198412],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00026185825,0.00006084827,0.00010068773,0.000023250062,0.00008988232,0.00005893455,0.00010130276,0.000048957707,0.000009537777],"category_scores_gemma":[0.00006453744,0.00003057483,0.000031380114,0.000047780613,0.000116361625,0.00012535766,0.00003085237,0.000185251,1.4039465e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0019665905,0.00021464443,0.29502922,0.00084395235,0.0016687894,0.000012560101,0.17301002,0.09549243,0.3617771,0.028924145,0.010963093,0.030097455],"study_design_scores_gemma":[0.002865511,0.0005739637,0.038986314,0.00032434496,0.00017328987,0.000043151555,0.002967526,0.8182066,0.0800702,0.055332888,0.00019416444,0.00026204885],"about_ca_topic_score_codex":0.000009020794,"about_ca_topic_score_gemma":0.00003191711,"teacher_disagreement_score":0.7227142,"about_ca_system_score_codex":0.000007912497,"about_ca_system_score_gemma":0.000008438236,"threshold_uncertainty_score":0.124680534},"labels":[],"label_agreement":null},{"id":"W2898966767","doi":"10.1115/detc2018-85477","title":"Numerical Assessment of 2D Aeroacoustic Simulations for Landing Gear","year":2018,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto","funders":"","keywords":"Aerodynamics; Landing gear; Noise (video); Fluent; Flow (mathematics); Solver; Turbulence; Computational fluid dynamics; Computer simulation; Reynolds number; Cylinder; Acoustics; Computer science; Aerospace engineering; Engineering; Simulation; Mechanics; Physics; Mechanical engineering","score_opus":0.01490851487228394,"score_gpt":0.2908491301570058,"score_spread":0.27594061528472186,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2898966767","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.06772405,0.0000050971803,0.92237926,0.000011053771,0.00031243762,0.00011056369,0.00002901015,0.00008595968,0.009342581],"genre_scores_gemma":[0.93512994,0.0000023323012,0.06453296,0.0000123728505,0.00016078925,0.000006028235,0.00001155562,0.000018811783,0.00012519272],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995621,0.000003073725,0.00014793464,0.00007707526,0.00007621474,0.00013363181],"domain_scores_gemma":[0.99966055,0.00011528028,0.000015890257,0.00011593008,0.000059836562,0.000032516185],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00005964731,0.000066900204,0.00010480778,0.000035235338,0.00004765163,0.000010993563,0.00006662741,0.00003830393,0.00014857571],"category_scores_gemma":[0.000025328327,0.000061379695,0.000033581124,0.00007766083,0.000023640721,0.000028501414,0.000011941589,0.000046441484,0.000004123876],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000015974314,0.000022880173,0.00087393227,0.00005708024,0.000034598266,2.5662408e-7,0.000039213934,0.9763337,0.013724255,0.0073324335,0.0009297698,0.00065027893],"study_design_scores_gemma":[0.0001385989,0.000045104614,0.0010268955,0.000008309515,0.000018003,4.0977173e-7,0.00001601189,0.997424,0.0002646053,0.00054586143,0.00043502622,0.000077187746],"about_ca_topic_score_codex":0.0000032588143,"about_ca_topic_score_gemma":0.000005797542,"teacher_disagreement_score":0.8674059,"about_ca_system_score_codex":0.0000330594,"about_ca_system_score_gemma":0.0000103928005,"threshold_uncertainty_score":0.25029913},"labels":[],"label_agreement":null},{"id":"W2900516136","doi":"10.1115/1.4041989","title":"Experimental Investigation of Nozzle Spacing Effects on Characteristics of Round Twin Free Jets","year":2018,"lang":"en","type":"article","venue":"Journal of Fluids Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":43,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Manitoba","funders":"","keywords":"Nozzle; Turbulence; Mechanics; Particle image velocimetry; Reynolds number; Reynolds stress; Turbulence kinetic energy; Vorticity; Jet (fluid); Physics; Shear stress; Materials science; Optics; Vortex; Thermodynamics","score_opus":0.006610534278792954,"score_gpt":0.20598627983469808,"score_spread":0.19937574555590512,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2900516136","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9498981,0.00019680333,0.048337188,0.0000068587847,0.001337298,0.000058876005,0.000008701091,0.000026014983,0.00013011391],"genre_scores_gemma":[0.98959845,0.000021753938,0.009690344,0.0000079405245,0.0006313871,0.0000011266749,0.0000015720772,0.000041646843,0.000005793964],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99895126,0.000009822992,0.0005372405,0.00007193738,0.00026488077,0.00016488691],"domain_scores_gemma":[0.9993386,0.0001089757,0.00014725019,0.00019345363,0.000126258,0.000085415246],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00022109834,0.00016008044,0.00033335589,0.00020115785,0.000019661988,0.000014883593,0.00019547228,0.00007988339,0.000009149786],"category_scores_gemma":[0.00015289089,0.00015962674,0.00008853939,0.00013674948,0.00003529988,0.00012936069,0.00003361289,0.00020825124,0.0000015348654],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000016130682,0.000016626896,0.00027869502,0.00024558243,0.000052853695,0.000009808726,0.0003998584,0.028688446,0.96939766,0.00030296063,0.00014614794,0.0004452062],"study_design_scores_gemma":[0.00044601888,0.0004525906,0.0059300964,0.0005979657,0.00003288102,0.000020932479,0.000030388683,0.2141732,0.77808136,0.00004000305,0.0000438253,0.00015071566],"about_ca_topic_score_codex":0.000001798806,"about_ca_topic_score_gemma":2.7959936e-7,"teacher_disagreement_score":0.1913163,"about_ca_system_score_codex":0.000101045895,"about_ca_system_score_gemma":0.000017392616,"threshold_uncertainty_score":0.6509389},"labels":[],"label_agreement":null},{"id":"W2900632956","doi":"10.25071/10315/35214","title":"Numerical Investigations Of Aerodynamic Noise Due To Flow Past A Bluff Body","year":2018,"lang":"en","type":"article","venue":"Progress in Canadian Mechanical Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"University of Toronto; Taibah University","keywords":"Bluff; Aerodynamics; Noise (video); Flow (mathematics); Acoustics; Mechanics; Computer science; Marine engineering; Aerospace engineering; Engineering; Physics","score_opus":0.005337181758987971,"score_gpt":0.20904571489097687,"score_spread":0.2037085331319889,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2900632956","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7052518,0.00038900477,0.2878745,0.00089249655,0.0027917195,0.0010274239,0.0002178373,0.00061331975,0.00094191043],"genre_scores_gemma":[0.956774,0.0000045345605,0.04272951,0.00006864214,0.00023791948,0.00008684512,0.000014809451,0.000078194025,0.0000055267915],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9983568,0.000012732323,0.00041882857,0.0002753434,0.00019749875,0.00073878],"domain_scores_gemma":[0.9987067,0.000053645734,0.000022904707,0.00034124087,0.0000749758,0.00080056273],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00022718296,0.00024197817,0.000324092,0.0003979794,0.000045317658,0.000033524826,0.00035128833,0.00016614218,0.00005096448],"category_scores_gemma":[0.00016091253,0.0002834552,0.000058091813,0.0007591233,0.000051895,0.000071004375,0.000046754143,0.00032813806,0.000035189678],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":true,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000008674464,0.000053719417,0.0019197848,0.00028222494,0.00008097031,0.00015866004,0.0003510915,0.95904016,0.005939012,0.019234756,0.00037368905,0.01255728],"study_design_scores_gemma":[0.00014674076,0.000063084924,0.0023883798,0.00014060414,0.000010670208,0.000013143659,0.000007542072,0.99497235,0.00070959656,0.00023945904,0.0010035038,0.0003049093],"about_ca_topic_score_codex":0.002162743,"about_ca_topic_score_gemma":0.026345875,"teacher_disagreement_score":0.2515222,"about_ca_system_score_codex":0.00038124662,"about_ca_system_score_gemma":0.0001102564,"threshold_uncertainty_score":0.99996173},"labels":[],"label_agreement":null},{"id":"W2901604141","doi":"10.1007/s00348-020-2902-3","title":"Measurements of flow velocity and scalar concentration in turbulent multi-component jets: asymmetry and buoyancy effects","year":2020,"lang":"en","type":"preprint","venue":"Experiments in Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Victoria","funders":"Canadian Network for Research and Innovation in Machining Technology, Natural Sciences and Engineering Research Council of Canada","keywords":"Mechanics; Buoyancy; Turbulence; Particle image velocimetry; Physics; Jet (fluid); Nozzle; Body orifice; Neutral buoyancy; Reynolds number; Optics; Classical mechanics; Thermodynamics; Engineering","score_opus":0.02787049326004211,"score_gpt":0.26625922804209373,"score_spread":0.23838873478205164,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2901604141","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9774607,0.008627022,0.0118711945,0.000026452317,0.0009721885,0.0008068244,0.000023574752,0.000060658498,0.00015137925],"genre_scores_gemma":[0.9781219,0.0006363562,0.020968057,0.000029961891,0.00005166587,0.00008830449,0.000052916428,0.00004793625,0.0000029511616],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9983032,0.00007846876,0.00055809837,0.0004635739,0.00032181598,0.00027488093],"domain_scores_gemma":[0.99950415,0.000040486313,0.000055977132,0.00025840141,0.000033708387,0.00010726869],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00024273159,0.00036335728,0.00054309116,0.000108043845,0.000025239562,0.000039825067,0.00017577507,0.0002868399,0.0000055467303],"category_scores_gemma":[0.000067224806,0.00041069492,0.00004445057,0.0001059978,0.00006717198,0.000059966784,0.00031281245,0.0005030399,0.0000012789504],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00013199815,0.0010334578,0.051193744,0.005381082,0.00050139247,0.00014250937,0.011493909,0.24633019,0.66870964,0.00013265568,0.00022895179,0.014720483],"study_design_scores_gemma":[0.0018159183,0.00004382125,0.023511827,0.00079391716,0.000021292202,0.0000012744118,0.00004565757,0.90560097,0.06767314,0.000101313286,0.000009243451,0.00038163966],"about_ca_topic_score_codex":0.000059855203,"about_ca_topic_score_gemma":0.000010751738,"teacher_disagreement_score":0.65927076,"about_ca_system_score_codex":0.00034966826,"about_ca_system_score_gemma":0.000035555433,"threshold_uncertainty_score":0.9998345},"labels":[],"label_agreement":null},{"id":"W2902328516","doi":"10.1115/1.4042163","title":"Tonal Noise Prediction of a Modern Turbofan Engine With Large Upstream and Downstream Distortion","year":2018,"lang":"en","type":"article","venue":"Journal of Turbomachinery","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":26,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Safran Aircraft Engines; Grand Équipement National De Calcul Intensif","keywords":"Turbofan; Inlet; Distortion (music); Aeroacoustics; Noise (video); Acoustics; Annulus (botany); Impeller; Mechanics; Mechanical fan; Wake; Upstream (networking); Computational fluid dynamics; Dynamic mode decomposition; Physics; Engineering; Aerospace engineering; Computer science; Materials science; Sound pressure; Mechanical engineering; Telecommunications","score_opus":0.0029605992720083997,"score_gpt":0.17961410635343944,"score_spread":0.17665350708143104,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2902328516","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.92136735,0.00039207411,0.07699073,0.000025736701,0.00038674724,0.00004814284,0.00008534244,0.000028118568,0.0006757391],"genre_scores_gemma":[0.9964888,0.00010449167,0.0027759797,0.000009581916,0.00054763706,9.5175784e-7,0.000009309946,0.000025582307,0.000037643706],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991807,0.000011658956,0.00034777744,0.00008376369,0.00022838324,0.00014773822],"domain_scores_gemma":[0.999476,0.00002678372,0.00015457149,0.000121248624,0.00013183686,0.00008956011],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018618596,0.0001392459,0.00022516314,0.00012194215,0.000040363673,0.0000160291,0.000088716864,0.00006592341,0.00001911147],"category_scores_gemma":[0.000023195274,0.00010121157,0.00005781834,0.000090355905,0.000059518985,0.00015883715,0.000019550636,0.00022748215,5.65027e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0012957798,0.0011693509,0.17174242,0.00083327637,0.0015914206,0.00019379842,0.0034280627,0.4856839,0.16205001,0.00074135064,0.0058553256,0.1654153],"study_design_scores_gemma":[0.0014405237,0.0008098624,0.05647605,0.00021655609,0.00017031867,0.00039294004,0.000038964234,0.93668294,0.0021504783,0.0009926792,0.00042330948,0.00020537153],"about_ca_topic_score_codex":0.0000034491306,"about_ca_topic_score_gemma":0.000015607367,"teacher_disagreement_score":0.45099905,"about_ca_system_score_codex":0.000049033966,"about_ca_system_score_gemma":0.000020452691,"threshold_uncertainty_score":0.4127288},"labels":[],"label_agreement":null},{"id":"W2904473351","doi":"10.1177/1475472x18812798","title":"Modal analysis of the laminar boundary layer instability and tonal noise of an airfoil at Reynolds number 150,000","year":2018,"lang":"en","type":"article","venue":"International Journal of Aeroacoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":58,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Physics; Reynolds number; Airfoil; Mechanics; Boundary layer; Vortex; Vortex shedding; Turbulence; Lattice Boltzmann methods; Acoustics","score_opus":0.007788386799962314,"score_gpt":0.24881192007862918,"score_spread":0.24102353327866685,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2904473351","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98512965,0.000049834598,0.012143253,0.0000632097,0.0011872912,0.000040761977,0.0003081308,0.000008886974,0.0010689914],"genre_scores_gemma":[0.99555284,0.000074161915,0.003905384,0.000035923065,0.00031767177,5.8802556e-7,0.000008481056,0.000019406585,0.000085517655],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9983713,0.000036625614,0.00066608714,0.00011742882,0.00067034294,0.00013822119],"domain_scores_gemma":[0.99823016,0.00011112629,0.00031661004,0.00024203552,0.0010210981,0.0000789466],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00040485378,0.00014237028,0.00031766715,0.00015815918,0.00005545974,0.000030422718,0.0004913651,0.000100609985,0.00017950777],"category_scores_gemma":[0.00013258451,0.000111834386,0.00017967683,0.00025363668,0.00035200542,0.00014413755,0.00015530303,0.00022530729,0.0000010695662],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00039441194,0.00049424934,0.09885028,0.00010112294,0.004178988,0.000044249526,0.0017133733,0.805359,0.081950136,0.0012111256,0.0010614484,0.004641617],"study_design_scores_gemma":[0.0005644605,0.00013542552,0.17119752,0.00006690959,0.000821366,0.000097572774,0.00014997854,0.8212914,0.004099867,0.00084573805,0.0005498678,0.00017992781],"about_ca_topic_score_codex":0.000020608253,"about_ca_topic_score_gemma":0.00013832486,"teacher_disagreement_score":0.07785027,"about_ca_system_score_codex":0.00016498935,"about_ca_system_score_gemma":0.00006352348,"threshold_uncertainty_score":0.4560474},"labels":[],"label_agreement":null},{"id":"W2904858792","doi":"10.2514/1.c035113","title":"Design and Characterization of a High-Speed Subsonic Aeroacoustic Wind Tunnel","year":2018,"lang":"en","type":"article","venue":"Journal of Aircraft","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"Carleton University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Wind tunnel; Aerospace engineering; Aerodynamics; Subsonic and transonic wind tunnel; Characterization (materials science); Acoustics; Marine engineering; Engineering; Structural engineering; Geology; Transonic; Physics","score_opus":0.00869377545346853,"score_gpt":0.20004822880167997,"score_spread":0.19135445334821144,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2904858792","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.73774946,0.000056639674,0.26160583,0.00003309808,0.00045591866,0.000049705246,0.0000042282154,0.000012549993,0.00003257224],"genre_scores_gemma":[0.9917244,0.0001959584,0.0076575135,0.00001755001,0.0003406949,1.9271955e-7,0.0000016147434,0.000025047686,0.000037045687],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99926066,0.00001931481,0.00035983042,0.00006427104,0.00016062695,0.00013532235],"domain_scores_gemma":[0.99944496,0.000050619023,0.00014943838,0.00009826475,0.00018894306,0.00006776432],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00026356676,0.00010295553,0.00022407825,0.00010922646,0.000032161657,0.000021432577,0.00010871607,0.00006990441,0.000035319237],"category_scores_gemma":[0.000031409836,0.000092601316,0.000035955785,0.00011192324,0.00006358967,0.0001350265,0.000016769744,0.00014484659,0.0000036685758],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000044307497,0.000034697303,0.00017364822,0.00007024388,0.00008714227,0.000016331773,0.0003241103,0.052470647,0.9446393,0.0000749372,0.00019384449,0.0018707855],"study_design_scores_gemma":[0.0013340928,0.0008011985,0.05368923,0.00028098052,0.00020434978,0.00022117715,0.00005941641,0.92195743,0.019870149,0.0010496877,0.00020614997,0.00032612303],"about_ca_topic_score_codex":0.0000013298884,"about_ca_topic_score_gemma":0.0000011100698,"teacher_disagreement_score":0.92476916,"about_ca_system_score_codex":0.00003518879,"about_ca_system_score_gemma":0.000028969154,"threshold_uncertainty_score":0.3776172},"labels":[],"label_agreement":null},{"id":"W2906763941","doi":"10.5539/mer.v8n2p48","title":"Design of Next Generation Civil and Military Aircraft with Ultra-High Bypass Engine using Composites, Advanced Materials and Technology","year":2018,"lang":"en","type":"article","venue":"Mechanical Engineering Research","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Turbofan; Nacelle; Rotor (electric); Noise (video); Fuselage; Turboprop; Propulsive efficiency; Atmospheric duct; Payload (computing); Aerospace engineering; Blade (archaeology); Computer science; Engineering; Stator; Automotive engineering; Acoustics; Mechanical engineering; Propulsion; Physics; Artificial intelligence","score_opus":0.03125346843955326,"score_gpt":0.26058488365324445,"score_spread":0.2293314152136912,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2906763941","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.5647862,0.00040391556,0.43440256,0.00002358497,0.00008934729,0.0001898966,0.000010154987,0.00009089399,0.000003478433],"genre_scores_gemma":[0.8973472,0.00026515117,0.10219387,0.0000026717612,0.0001072735,0.000019954317,0.000007822486,0.000051422885,0.000004591225],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9988418,0.000032296524,0.00023875668,0.00025797816,0.00024106212,0.00038808622],"domain_scores_gemma":[0.9993262,0.00014656829,0.000014097501,0.00023675854,0.00018458771,0.00009177777],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005390878,0.0001730356,0.000269771,0.00026684534,0.00008414969,0.000028483564,0.00013748446,0.00016161115,0.000016024034],"category_scores_gemma":[0.000112583555,0.00016222375,0.00000853071,0.000400364,0.00012710576,0.000102668964,0.000075087715,0.00027990702,0.0000012389877],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000015882582,0.000009555826,0.0000020416355,0.00009892184,0.00002534795,0.0000057261873,0.000020339427,0.25598285,0.7425415,0.0006857073,0.0000073475658,0.00060482736],"study_design_scores_gemma":[0.00023732048,0.00023224641,0.000010448145,0.00007624422,0.000008774407,0.000019372506,0.000011731787,0.6554807,0.343676,0.00011479376,0.000015140823,0.00011720296],"about_ca_topic_score_codex":0.000019354791,"about_ca_topic_score_gemma":0.000009959071,"teacher_disagreement_score":0.39949787,"about_ca_system_score_codex":0.0000574364,"about_ca_system_score_gemma":0.000019038309,"threshold_uncertainty_score":0.6615292},"labels":[],"label_agreement":null},{"id":"W2907887292","doi":"10.3390/acoustics1010008","title":"Turbomachinery Noise Predictions: Present and Future","year":2019,"lang":"en","type":"article","venue":"Acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":90,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"École Centrale de Lyon; Compute Canada; National Aeronautics and Space Administration","keywords":"Turbomachinery; Reynolds-averaged Navier–Stokes equations; Turbine; Duct (anatomy); Cascade; Acoustics; Computational fluid dynamics; Noise (video); Gas compressor; Airfoil; Aeroacoustics; Lattice Boltzmann methods; Sound pressure; Mechanics; Physics; Engineering; Computer science; Mechanical engineering","score_opus":0.002920620466181729,"score_gpt":0.18477080071253252,"score_spread":0.1818501802463508,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2907887292","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9239305,0.0018006874,0.053265896,0.00023395386,0.004590746,0.0003489944,0.00012337022,0.000558667,0.015147138],"genre_scores_gemma":[0.99410045,0.0011069941,0.00263057,0.00004248902,0.0014699617,0.000007700032,0.000018816718,0.000040767325,0.00058222277],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99941397,0.000005424742,0.00013508736,0.0001356045,0.00012467853,0.00018521429],"domain_scores_gemma":[0.99959874,0.000045842928,0.000015186153,0.0002379844,0.00002984741,0.00007239826],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000050868424,0.00013213731,0.000118579555,0.000040770545,0.000040498202,0.000033898927,0.00009305681,0.00009976318,0.00006405121],"category_scores_gemma":[0.000006939604,0.00012367623,0.000025565047,0.00007666003,0.000022139948,0.000062642815,0.00004726633,0.0002114002,0.00004328605],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000058225696,0.000033989083,0.0021616153,0.00024360759,0.00007828254,0.000012853756,0.0001639137,0.9524466,0.01286317,0.0012331047,0.020679906,0.010077129],"study_design_scores_gemma":[0.00017129077,0.000022700446,0.0063212323,0.000011971371,0.000033238513,0.000012026659,0.00007587662,0.9759712,0.000018626783,0.00034645898,0.016861282,0.00015408645],"about_ca_topic_score_codex":0.0000022903425,"about_ca_topic_score_gemma":5.9700847e-7,"teacher_disagreement_score":0.07016993,"about_ca_system_score_codex":0.00002705278,"about_ca_system_score_gemma":0.000008171736,"threshold_uncertainty_score":0.5043371},"labels":[],"label_agreement":null},{"id":"W2910724385","doi":"10.2514/6.2019-2382","title":"Acoustic Atmospheric Propagation Model Validation with the NRC Convair 580","year":2019,"lang":"en","type":"article","venue":"AIAA Scitech 2019 Forum","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"National Research Council Canada","funders":"","keywords":"Atmospheric model; Environmental science; Model validation; Computer science; Atmospheric sciences; Meteorology; Remote sensing; Geology; Physics; Data science","score_opus":0.0031109838442521555,"score_gpt":0.17582858797570883,"score_spread":0.17271760413145668,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2910724385","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.43367165,0.0000620231,0.56081295,0.00040319486,0.0003677906,0.0005713334,0.000017926015,0.0002911922,0.003801915],"genre_scores_gemma":[0.99338907,0.000027030874,0.0039501926,0.0001336303,0.000046282723,0.000036957757,0.00003039247,0.0000620858,0.0023243309],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99889624,0.000010965853,0.0001666938,0.00021145125,0.0003687083,0.00034592117],"domain_scores_gemma":[0.9992979,0.000045152792,0.000054786633,0.00042760625,0.00012896201,0.000045593322],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00022975859,0.00018918238,0.00014658044,0.000016082371,0.0001159716,0.00008015497,0.0002573384,0.00009871611,0.000039384657],"category_scores_gemma":[0.0000147601495,0.00012833884,0.000040697367,0.00024411328,0.00004847821,0.00022266952,0.000048396712,0.0002238744,0.00024109331],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000071304707,0.000009396882,0.0003386823,0.00003485587,0.00002179729,6.8338767e-7,0.000052886106,0.9764878,0.013901399,0.0011616602,0.0068159136,0.0011677907],"study_design_scores_gemma":[0.0002554617,0.00006194995,0.00014846724,0.00002940087,0.000028112148,0.0000047956596,0.000102395075,0.99687713,0.00060093874,0.00085449015,0.00082018384,0.00021669581],"about_ca_topic_score_codex":0.0000072596126,"about_ca_topic_score_gemma":0.000024444762,"teacher_disagreement_score":0.5597174,"about_ca_system_score_codex":0.00011985006,"about_ca_system_score_gemma":0.000046997313,"threshold_uncertainty_score":0.5233506},"labels":[],"label_agreement":null},{"id":"W2912030641","doi":"10.1017/jfm.2018.988","title":"Curvature-induced deformations of the vortex rings generated at the exit of a rectangular duct","year":2019,"lang":"en","type":"article","venue":"Journal of Fluid Mechanics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":15,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Waterloo","funders":"","keywords":"Physics; Vortex; Mechanics; Vortex ring; Particle image velocimetry; Curvature; Vorticity; Intermittency; Classical mechanics; Turbulence; Optics; Geometry","score_opus":0.005614076216643831,"score_gpt":0.18606572481040684,"score_spread":0.180451648593763,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2912030641","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9899479,0.0005321992,0.0072940616,0.00009073452,0.0016034577,0.00013388607,0.00001632804,0.00000927885,0.00037216616],"genre_scores_gemma":[0.99875045,0.00027119048,0.00073976855,0.000031939548,0.000090845955,9.2758955e-7,0.0000012642121,0.000022834249,0.000090762944],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99894583,0.00003077957,0.0005158501,0.00005352561,0.00031766796,0.00013634618],"domain_scores_gemma":[0.9990441,0.000048229766,0.0002979634,0.00032062398,0.00025375414,0.000035288467],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004704498,0.000111141904,0.00023239244,0.00008108468,0.00004670633,0.0000105509835,0.0003612879,0.00009277439,0.000046146044],"category_scores_gemma":[0.00008441746,0.0000642362,0.00017086758,0.0003456996,0.000010975663,0.00008290107,0.00007014854,0.00031707584,0.0000041442727],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000009351587,0.000014373572,0.000021654228,0.000046105997,0.00010157294,0.0000012215363,0.00022594258,0.11889348,0.8774846,0.0022524884,0.0007423354,0.00020687288],"study_design_scores_gemma":[0.00037889887,0.000096730975,0.00021315325,0.00013740585,0.00012452701,0.0000980934,0.00014582547,0.69975585,0.29654154,0.0014315514,0.00095371954,0.00012271333],"about_ca_topic_score_codex":0.0000029416638,"about_ca_topic_score_gemma":0.000009853715,"teacher_disagreement_score":0.58094305,"about_ca_system_score_codex":0.00007745908,"about_ca_system_score_gemma":0.000044478184,"threshold_uncertainty_score":0.26194763},"labels":[],"label_agreement":null},{"id":"W2912079239","doi":"10.5004/dwt.2019.23477","title":"Experimental and numerical study of the characteristics of thermal and nonthermal offset buoyant jets discharged into stagnant water","year":2019,"lang":"en","type":"article","venue":"Desalination and Water Treatment","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":21,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Ottawa","funders":"","keywords":"Offset (computer science); Thermal; Mechanics; Environmental science; Nuclear engineering; Meteorology; Materials science; Physics; Engineering; Computer science","score_opus":0.005974901334222356,"score_gpt":0.2118454497242256,"score_spread":0.20587054839000324,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2912079239","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9993067,0.000052635194,0.00011520694,0.000038325463,0.00011907029,0.00031213058,0.000021065738,0.000010391439,0.000024476925],"genre_scores_gemma":[0.9998091,0.000013659288,0.000057484427,0.000006109865,0.000012467855,0.000016509919,0.00002144992,0.000013666937,0.00004956056],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9994889,0.000024409994,0.00018008743,0.00011256227,0.0000922111,0.000101820704],"domain_scores_gemma":[0.9998096,0.000010402646,0.000022950991,0.00010697254,0.000020588692,0.000029482993],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000053492546,0.0001177519,0.00017193609,0.000024273415,0.000041610594,0.000016075895,0.000034044253,0.000030892523,0.000017085087],"category_scores_gemma":[9.069394e-7,0.000054945318,0.00001803149,0.000013659857,0.00003272219,0.0000524052,0.00005017542,0.000033831293,0.0000011217983],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000052132884,0.0006024005,0.045880098,0.000064909735,0.00013665146,0.000003100512,0.019289192,0.0005337202,0.92944163,0.0001244717,0.0000014009674,0.0038702704],"study_design_scores_gemma":[0.0032533084,0.0010246033,0.18501131,0.000038327515,0.00011085139,0.000006829213,0.0017234248,0.121567376,0.68684375,0.00002949057,0.00012122189,0.000269482],"about_ca_topic_score_codex":0.000035756864,"about_ca_topic_score_gemma":0.0000017033291,"teacher_disagreement_score":0.24259788,"about_ca_system_score_codex":0.000024587043,"about_ca_system_score_gemma":0.000002035827,"threshold_uncertainty_score":0.2240605},"labels":[],"label_agreement":null},{"id":"W2919858753","doi":"10.1016/j.jsv.2019.02.032","title":"Azimuthal mode analysis of broadband shock-associated noise in an under-expanded axisymmetric jet","year":2019,"lang":"en","type":"article","venue":"Journal of Sound and Vibration","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":17,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Fonds de recherche du Québec – Nature et technologies; Canada Foundation for Innovation","keywords":"Physics; Jet (fluid); Mach number; Supersonic speed; Wavenumber; Jet noise; Shock (circulatory); Mach wave; Transonic; Mechanics; Noise (video); Azimuth; Turbulence; Computational physics; Shock wave; Amplitude; Aerodynamics; Optics","score_opus":0.01038250704836998,"score_gpt":0.2457155329060552,"score_spread":0.2353330258576852,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2919858753","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97310233,0.000120342265,0.026404891,0.000009096291,0.00013661612,0.000042435226,0.000014573835,0.000007070213,0.00016263226],"genre_scores_gemma":[0.9995209,0.00009386331,0.00029772814,0.0000111665595,0.000037227044,2.426395e-7,0.0000180898,0.000009878363,0.000010917211],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99926084,0.000023375,0.00037782075,0.00006940255,0.00016932726,0.00009921631],"domain_scores_gemma":[0.99957937,0.00006414407,0.00015000315,0.00007545197,0.000082681254,0.00004833998],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023011822,0.00008794825,0.00030003535,0.00052785175,0.00001844713,0.00004423036,0.00006577771,0.00008390492,0.000020853877],"category_scores_gemma":[0.00002023206,0.000075124146,0.00007401019,0.0006461009,0.00001136128,0.0002875071,0.000008426977,0.00014197263,4.3458894e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000233184,0.0000731228,0.13201308,0.000022897251,0.0002323162,0.0000017603829,0.0003076561,0.8484618,0.018131709,0.0002424901,0.00000674228,0.00048308208],"study_design_scores_gemma":[0.00047235072,0.00010293928,0.17250042,0.000017456821,0.00014676759,0.0000023562288,0.00018286111,0.8251619,0.00014484154,0.001190478,0.000001431,0.0000762205],"about_ca_topic_score_codex":0.000012311733,"about_ca_topic_score_gemma":0.00015315146,"teacher_disagreement_score":0.040487338,"about_ca_system_score_codex":0.00006115104,"about_ca_system_score_gemma":0.000014248966,"threshold_uncertainty_score":0.3063474},"labels":[],"label_agreement":null},{"id":"W2921494499","doi":"10.3390/jmse7030068","title":"The Hydrodynamic Noise Suppression of a Scaled Submarine Model by Leading-Edge Serrations","year":2019,"lang":"en","type":"article","venue":"Journal of Marine Science and Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":14,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"University of Alberta","keywords":"Noise (video); Leading edge; Vortex; Mechanics; Hull; Reynolds number; Chord (peer-to-peer); Physics; Water tunnel; Noise reduction; Enhanced Data Rates for GSM Evolution; Amplitude; Acoustics; Optics; Engineering; Marine engineering; Turbulence; Telecommunications; Computer science","score_opus":0.0033901436014338077,"score_gpt":0.19233588626486933,"score_spread":0.18894574266343553,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2921494499","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9837878,0.00011561773,0.014092819,0.00006498312,0.0005261209,0.000065231434,0.0000033075703,0.000016595019,0.0013275732],"genre_scores_gemma":[0.99728835,0.00031953063,0.002047497,0.0000049836754,0.00003622567,0.0000010970363,7.4292853e-7,0.000015059111,0.00028654313],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9990256,0.0000032438898,0.00032314486,0.000089466695,0.0003362398,0.00022230814],"domain_scores_gemma":[0.9994483,0.00006284778,0.000077332246,0.0001598544,0.00015850266,0.000093178314],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006503555,0.000109712906,0.0001788737,0.00013232719,0.00008715573,0.00005936794,0.00030681796,0.000034831868,0.0000066575894],"category_scores_gemma":[0.000101903264,0.00007874434,0.00004117506,0.00028851745,0.00007888666,0.0003067777,0.00014751048,0.00023368731,0.0000015771568],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000040573295,0.0000070444503,0.00041152394,0.00003736527,0.000008652621,7.4113353e-7,0.00004693278,0.7253676,0.27176186,0.00024247171,0.00020128203,0.0019104526],"study_design_scores_gemma":[0.0001882886,0.0000363315,0.0011990934,0.000043868098,0.000011437749,0.000021720422,0.000024232288,0.9963973,0.0016219666,0.00016284334,0.00020181204,0.000091069436],"about_ca_topic_score_codex":0.0000022171878,"about_ca_topic_score_gemma":0.000002772835,"teacher_disagreement_score":0.27102974,"about_ca_system_score_codex":0.00006242103,"about_ca_system_score_gemma":0.000046200275,"threshold_uncertainty_score":0.3211101},"labels":[],"label_agreement":null},{"id":"W2923214590","doi":"10.2514/1.j056658","title":"Evaluation of Acoustic Frequency Methods for the Prediction of Propeller Noise","year":2019,"lang":"en","type":"article","venue":"AIAA Journal","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":33,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Carleton University","funders":"Pratt and Whitney Canada; Carleton University; Pratt & Whitney","keywords":"Aerodynamics; Acoustics; Propeller; Noise (video); Mach number; Microphone; Range (aeronautics); Solver; Aeroacoustics; Computer science; Engineering; Sound pressure; Aerospace engineering; Marine engineering; Physics","score_opus":0.02999746725178898,"score_gpt":0.30913755977599866,"score_spread":0.2791400925242097,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2923214590","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.14267175,0.0007611094,0.853032,0.000028415976,0.0014400074,0.00037024627,0.000017461723,0.000010766092,0.001668275],"genre_scores_gemma":[0.96464646,0.00015119357,0.035000835,0.00000399759,0.00013890462,0.000009765227,0.0000017286964,0.000016143198,0.000030953463],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99925727,0.000056170247,0.00027246817,0.000050407893,0.00026835184,0.00009534444],"domain_scores_gemma":[0.999118,0.00016905893,0.00009871493,0.00013753607,0.00045573447,0.00002100047],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0022378438,0.000062317704,0.00010986747,0.000042041014,0.000035391895,0.000009819993,0.00011943188,0.00004547047,0.0001302571],"category_scores_gemma":[0.00020205307,0.00004164822,0.00006585248,0.000069588015,0.000018576344,0.00006502019,0.000009366208,0.00016036624,0.0000021303208],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000004686035,0.000013164662,0.0002222097,0.00005751468,0.00010205007,5.574749e-8,0.00013779482,0.7383035,0.21656704,0.00030483527,0.00020651499,0.04408067],"study_design_scores_gemma":[0.0003758165,0.00006713125,0.0016633725,0.000041531526,0.0002645215,0.000009456974,0.00006351253,0.9879375,0.0014931408,0.00796508,0.00007929248,0.00003964323],"about_ca_topic_score_codex":0.0000016252737,"about_ca_topic_score_gemma":0.0000011105103,"teacher_disagreement_score":0.82197475,"about_ca_system_score_codex":0.000054733235,"about_ca_system_score_gemma":0.00006181164,"threshold_uncertainty_score":0.1698365},"labels":[],"label_agreement":null},{"id":"W2935871243","doi":"10.22215/etd/2016-11518","title":"Numerical Predictions of Propeller-Wing Interaction Induced Noise in Cruise and Off-Design Conditions","year":2016,"lang":"en","type":"dissertation","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":6,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Carleton University","funders":"","keywords":"Propeller; Wing; Vortex; Mach number; Wake; Aerospace engineering; Computational fluid dynamics; Engineering; Advance ratio; Marine engineering; Physics; Acoustics; Structural engineering; Mechanics; Blade pitch; Turbine","score_opus":0.014980490668071814,"score_gpt":0.25650108525217513,"score_spread":0.24152059458410333,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2935871243","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.87216836,0.0002086705,0.067495614,0.00003734279,0.0029001925,0.0010604786,0.00011900922,0.00032827666,0.055682044],"genre_scores_gemma":[0.9976021,0.0002995695,0.00067901745,0.0000036601373,0.00007500023,0.000072943985,0.00017646623,0.000050207716,0.0010410266],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99913806,0.00002272333,0.00038300274,0.00018621258,0.00011902217,0.00015097191],"domain_scores_gemma":[0.99954426,0.000115828065,0.00007389566,0.0001457011,0.00006860971,0.00005168116],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00007906249,0.00019065871,0.00025437324,0.0002508505,0.00004440704,0.00001979757,0.00007755238,0.00022307235,0.00013800785],"category_scores_gemma":[0.000057428326,0.00016654297,0.000044294407,0.00013863498,0.000015683408,0.00012871031,0.000009158155,0.00030986752,0.000010478347],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00020047737,0.0004755877,0.00056323136,0.0017011253,0.00050440483,0.00003063612,0.0033433458,0.2894881,0.6591293,0.002457573,0.0044134986,0.037692685],"study_design_scores_gemma":[0.0007399311,0.00013070113,0.010263634,0.0013590734,0.0001165007,0.000008336168,0.0009764419,0.97655714,0.008058175,0.0009758358,0.00020720484,0.0006070454],"about_ca_topic_score_codex":0.000031213112,"about_ca_topic_score_gemma":0.00006073186,"teacher_disagreement_score":0.687069,"about_ca_system_score_codex":0.000089938716,"about_ca_system_score_gemma":0.00004035423,"threshold_uncertainty_score":0.67914253},"labels":[],"label_agreement":null},{"id":"W2937001726","doi":"10.1007/s10494-019-00023-1","title":"Effect of Nozzle Spacing on Turbulent Interaction of Low-Aspect-Ratio Twin Rectangular Jets","year":2019,"lang":"en","type":"article","venue":"Flow Turbulence and Combustion","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":29,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Manitoba","funders":"Natural Sciences and Engineering Research Council of Canada; University of Manitoba","keywords":"Nozzle; Turbulence; Particle image velocimetry; Reynolds number; Mechanics; Reynolds stress; Shear stress; Shear (geology); Aspect ratio (aeronautics); Turbulence kinetic energy; Optics; Physics; Materials science; Geometry; Mathematics; Thermodynamics; Composite material","score_opus":0.003534385351636969,"score_gpt":0.20788708985850488,"score_spread":0.2043527045068679,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2937001726","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99301344,0.00017152139,0.005082606,0.000015994941,0.00070085126,0.00023813668,0.000007440062,0.000053947144,0.00071606657],"genre_scores_gemma":[0.9994069,0.0001460577,0.00026416537,0.000010772989,0.000059486192,0.0000068484223,0.000019008678,0.000019681407,0.000067093926],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992412,0.00003101981,0.00024092515,0.00017152981,0.0001769199,0.00013845316],"domain_scores_gemma":[0.9995416,0.00009297093,0.000073008465,0.00021282244,0.000044992823,0.00003464514],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021295194,0.00015566275,0.00025066762,0.00009567843,0.000026271757,0.000014622103,0.000076250304,0.00009046365,0.000043674376],"category_scores_gemma":[0.000029653811,0.00014154198,0.000056807963,0.000118716904,0.000020413958,0.00011548589,0.000018828734,0.00018203721,0.000018840336],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00013209175,0.000042382024,0.00063518214,0.00086024345,0.000037438585,0.0000039649885,0.0002729401,0.91048276,0.074509144,0.00026282083,0.00026371205,0.012497336],"study_design_scores_gemma":[0.00038499446,0.00054210663,0.00060890004,0.00060398655,0.000028996194,0.0000066091793,0.00004609884,0.9024983,0.095021516,0.000082779305,0.000030976316,0.00014475128],"about_ca_topic_score_codex":0.000009096795,"about_ca_topic_score_gemma":0.000002293392,"teacher_disagreement_score":0.020512376,"about_ca_system_score_codex":0.000050099745,"about_ca_system_score_gemma":0.0000059877543,"threshold_uncertainty_score":0.5771915},"labels":[],"label_agreement":null},{"id":"W2944918111","doi":"10.2514/6.2019-2583","title":"Wavelet-based Procedure for the Identification of Signatures of the Azimuthal Modes for Broadband Shock-associated Noise","year":2019,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Broadband; Noise (video); Wavelet; Identification (biology); Azimuth; Computer science; Acoustics; Shock (circulatory); Speech recognition; Artificial intelligence; Physics; Telecommunications; Optics","score_opus":0.005900059327212209,"score_gpt":0.20846917349751265,"score_spread":0.20256911417030043,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2944918111","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.85623455,0.00014243115,0.14089948,0.0001288271,0.00036075627,0.0014978463,0.00034657514,0.000047849997,0.00034167114],"genre_scores_gemma":[0.9984898,0.0000049582045,0.00069384224,0.000023307777,0.00002400913,0.00006372954,0.000021551463,0.000023892911,0.0006548891],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994027,0.0000060877487,0.00025117304,0.000097040436,0.00012202198,0.00012098609],"domain_scores_gemma":[0.9992081,0.0003014978,0.00009429737,0.00023034067,0.00015480054,0.000010983432],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021590211,0.00008983182,0.00012819488,0.000020550002,0.00004756603,0.000013032252,0.00023286916,0.00008952459,0.000010366959],"category_scores_gemma":[0.00013810734,0.00005191098,0.000112821624,0.00008918849,0.000028661054,0.000026906122,0.000013316346,0.000070512375,3.929609e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000024170446,0.000037132566,0.00022090906,0.00038855654,0.00006910346,9.754291e-9,0.00008089487,0.67095137,0.32377598,0.0028413222,0.0011215969,0.0004889395],"study_design_scores_gemma":[0.00036592118,0.000020751297,0.0022575269,0.00002577872,0.000041539086,4.997814e-8,0.00006890696,0.9334163,0.063044764,0.00064041256,0.000050433937,0.00006763186],"about_ca_topic_score_codex":0.00000482561,"about_ca_topic_score_gemma":0.00003306011,"teacher_disagreement_score":0.2624649,"about_ca_system_score_codex":0.000024784787,"about_ca_system_score_gemma":0.000027518025,"threshold_uncertainty_score":0.21168683},"labels":[],"label_agreement":null},{"id":"W2945716003","doi":"10.2514/6.2019-2625","title":"Numerical Investigation of Noise Sources in a Single Airfoil Tip-Leakage Flow","year":2019,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Airfoil; Leakage (economics); Acoustics; Noise (video); Computer science; Mechanics; Materials science; Physics","score_opus":0.005485712205965425,"score_gpt":0.17134668825107743,"score_spread":0.16586097604511202,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2945716003","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97712994,0.00003643051,0.011653228,0.000025885276,0.00018591619,0.00007682041,0.0000031279935,0.00008082212,0.010807839],"genre_scores_gemma":[0.9933624,0.0000061301976,0.006294745,0.00003115136,0.000028049079,0.0000029595355,0.0000072399584,0.000019848416,0.0002474614],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994727,0.000008674013,0.00018545102,0.00009886705,0.00010272059,0.00013160126],"domain_scores_gemma":[0.9997456,0.00004063514,0.0000186831,0.00014164002,0.000016639335,0.000036814403],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0000766568,0.00008389762,0.00013574385,0.00006205968,0.000007246231,0.000010329145,0.00008682147,0.000060212176,0.00013205002],"category_scores_gemma":[0.000016324117,0.00008027213,0.000028253336,0.00015484368,0.000019527157,0.000059434737,0.00001791011,0.000100344536,0.00006279191],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000033723084,0.000026114292,0.020521339,0.00011537322,0.0000092127375,0.0000019008771,0.0003867793,0.888224,0.08837814,0.00042824895,0.00022633941,0.0016791823],"study_design_scores_gemma":[0.00018045612,0.000028313189,0.006766169,0.000033208256,0.0000031081336,8.4642534e-7,0.000054486416,0.98641187,0.0059279357,0.0003551071,0.00012884938,0.00010962456],"about_ca_topic_score_codex":0.000027243614,"about_ca_topic_score_gemma":0.000021664462,"teacher_disagreement_score":0.0981879,"about_ca_system_score_codex":0.000035793124,"about_ca_system_score_gemma":0.000007950037,"threshold_uncertainty_score":0.32734028},"labels":[],"label_agreement":null},{"id":"W2945785948","doi":"10.2514/6.2019-2466","title":"Explicit Differential Filtering on Unstructured Grids for Large-Eddy Simulations in Aeroacoustics Using an Approximate Deconvolution Model","year":2019,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"Fonds de Recherche du Québec - Santé; McGill University; Eli Lilly and Company","keywords":"Deconvolution; Aeroacoustics; Large eddy simulation; Computer science; Computational aeroacoustics; Unstructured grid; Computational fluid dynamics; Physics; Mechanics; Algorithm; Telecommunications; Turbulence","score_opus":0.02131408964721502,"score_gpt":0.25556555222829824,"score_spread":0.23425146258108323,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2945785948","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.49656612,0.0000019983258,0.50261295,0.0000011632583,0.00029914375,0.00022183872,0.00012330929,0.000082118466,0.000091378584],"genre_scores_gemma":[0.9465328,0.000003224199,0.05306551,0.000016819398,0.00009703464,0.000012654351,0.00016061023,0.00006023917,0.00005114415],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9990162,0.000007497522,0.00026853092,0.00023686634,0.00011430162,0.00035658042],"domain_scores_gemma":[0.9995665,0.00004194787,0.0000293643,0.0002676728,0.000035760397,0.0000587406],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000062545274,0.00019650078,0.0002003896,0.00012814233,0.00007001458,0.000051112904,0.00012517828,0.00013210179,0.000052747637],"category_scores_gemma":[0.0000119633105,0.00020132288,0.000049029994,0.000091242575,0.000006000999,0.00014983982,0.000033425786,0.00014757348,0.0000029337243],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000010319574,0.000036024154,0.00010582319,0.000060810038,0.000009806245,3.1759598e-7,0.00008637022,0.91132563,0.08376504,0.0044737286,0.000006941843,0.00011918907],"study_design_scores_gemma":[0.0006891494,0.000029969622,0.00013657312,0.000026997437,0.000017343384,0.0000011494175,0.000053071657,0.99666035,0.00056225236,0.0015659466,0.0000050693184,0.00025213553],"about_ca_topic_score_codex":0.0000052146793,"about_ca_topic_score_gemma":0.000061050974,"teacher_disagreement_score":0.44996664,"about_ca_system_score_codex":0.00014033732,"about_ca_system_score_gemma":0.000013161929,"threshold_uncertainty_score":0.82097083},"labels":[],"label_agreement":null},{"id":"W2946085962","doi":"10.2514/6.2019-2537","title":"LES and FW-H Prediction of Aeroacoustic Noise for a SD 7037 Airfoil for Wind Turbine Applications","year":2019,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Waterloo","funders":"Natural Sciences and Engineering Research Council of Canada; Compute Canada; TD Bank","keywords":"Airfoil; Turbine; Noise (video); Acoustics; Wind power; Environmental science; Aerospace engineering; Computer science; Physics; Engineering; Electrical engineering","score_opus":0.008876510936196739,"score_gpt":0.21097343507506036,"score_spread":0.20209692413886363,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2946085962","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.22978118,0.00010421822,0.7666258,0.000018001436,0.00014769586,0.00089992565,0.0003490252,0.000092121496,0.0019819785],"genre_scores_gemma":[0.9811184,0.000033034936,0.017674072,0.000008196161,0.00007880818,0.00016056772,0.000064779895,0.000028160386,0.0008339902],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99953246,0.0000014942123,0.00016595461,0.00012673918,0.00005307413,0.000120275545],"domain_scores_gemma":[0.9996249,0.00010282307,0.000024046452,0.00014830127,0.000066487795,0.000033404252],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00007007321,0.000089142624,0.00012693064,0.00003998627,0.000036793663,0.000010621528,0.00005986584,0.00006941366,0.00001938412],"category_scores_gemma":[0.000013382224,0.000084115425,0.000038190694,0.000041306223,0.000018953013,0.00003794602,0.000013409004,0.00004521063,0.000002073689],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00004159316,0.00011794773,0.0024359596,0.0028157115,0.00017346031,1.11525964e-7,0.00021193817,0.7530886,0.18678981,0.021264086,0.0027914406,0.030269355],"study_design_scores_gemma":[0.0005323602,0.00007316327,0.0014509169,0.000018039445,0.000054113843,9.160986e-7,0.000057689205,0.9933446,0.0005466983,0.0009420586,0.0028876178,0.000091842056],"about_ca_topic_score_codex":0.000005937018,"about_ca_topic_score_gemma":0.000012746071,"teacher_disagreement_score":0.75133723,"about_ca_system_score_codex":0.000021134145,"about_ca_system_score_gemma":0.0000068416653,"threshold_uncertainty_score":0.34301275},"labels":[],"label_agreement":null},{"id":"W2946528526","doi":"10.2514/6.2019-2451","title":"Acoustic and aerodynamic investigation of passive trailing-edge treatments for the Controlled-Diffusion airfoil","year":2019,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Airfoil; Aerodynamics; Trailing edge; Acoustics; Diffusion; Aerospace engineering; Physics; Computer science; Mechanics; Engineering","score_opus":0.005417516268785028,"score_gpt":0.1963547230810497,"score_spread":0.19093720681226467,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2946528526","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.96033984,0.00019291326,0.037237536,0.00005574342,0.00039839625,0.0008753022,0.00002922101,0.00006172698,0.00080930634],"genre_scores_gemma":[0.997998,0.00018490938,0.00092016585,0.000029852676,0.000037881182,0.00006732384,0.000018166891,0.000026500045,0.0007172188],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993761,0.000009800873,0.00022948187,0.0001356121,0.00009759872,0.00015141413],"domain_scores_gemma":[0.99925387,0.0004265279,0.000051649982,0.00017564034,0.000052228053,0.000040071725],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00010361424,0.00014122156,0.00024136833,0.000039300663,0.00005606686,0.000017629147,0.0000877974,0.00007370528,0.000024612773],"category_scores_gemma":[0.000036522044,0.00009050825,0.00006638972,0.000060133538,0.000048268143,0.00004760018,0.000019597568,0.00007078178,0.0000044877966],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00018205144,0.000059339378,0.0053269058,0.00043341098,0.00065847597,0.0000012762422,0.0007954067,0.53396237,0.43742007,0.0047786706,0.0004772862,0.015904749],"study_design_scores_gemma":[0.0027171357,0.00008736108,0.008247375,0.000027348613,0.00016096169,0.0000013067055,0.00013569102,0.98759407,0.0003976528,0.0005013251,0.000023581963,0.00010619784],"about_ca_topic_score_codex":0.000010254393,"about_ca_topic_score_gemma":0.000054932283,"teacher_disagreement_score":0.4536317,"about_ca_system_score_codex":0.00002802353,"about_ca_system_score_gemma":0.00001399748,"threshold_uncertainty_score":0.3690819},"labels":[],"label_agreement":null},{"id":"W2946699692","doi":"10.2514/6.2019-2714","title":"Fan Broadband Noise Computation at Transonic Regime","year":2019,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":9,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Transonic; Computation; Broadband; Computer science; Noise (video); Acoustics; Telecommunications; Aerospace engineering; Engineering; Aerodynamics; Physics; Artificial intelligence; Algorithm","score_opus":0.00440412181392785,"score_gpt":0.18998355948186035,"score_spread":0.1855794376679325,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2946699692","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.84696066,0.000072778166,0.09608121,0.000028796223,0.00041297244,0.0001099172,0.0000051500447,0.00021507348,0.056113463],"genre_scores_gemma":[0.99383384,0.000031816573,0.0016667405,0.000032553344,0.0000352854,0.0000020718744,0.000016684578,0.000023800492,0.0043572215],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99957395,0.0000036386189,0.00010209052,0.00010143379,0.00008171176,0.00013716712],"domain_scores_gemma":[0.9998057,0.000022401808,0.000008396033,0.000113415634,0.000013244871,0.000036876874],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000038421313,0.00008326383,0.00009035941,0.000025622758,0.00002309263,0.000016475671,0.000062123305,0.00004908669,0.00032692135],"category_scores_gemma":[0.0000014051279,0.00007925437,0.000033867705,0.000055544067,0.000008448646,0.000044311048,0.000010445266,0.00006923163,0.00045888472],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000061874352,0.0000131858305,0.0008996559,0.00008614931,0.00002965244,0.0000032409707,0.00017451719,0.94410914,0.04486202,0.0016407352,0.0032006404,0.0049748956],"study_design_scores_gemma":[0.0002755825,0.000016458587,0.0018400353,0.000009660432,0.0000073297347,0.000003449087,0.000013617898,0.99419516,0.0007509081,0.00024529878,0.0025036337,0.00013888461],"about_ca_topic_score_codex":0.000003955539,"about_ca_topic_score_gemma":0.000017169341,"teacher_disagreement_score":0.14687319,"about_ca_system_score_codex":0.0000559208,"about_ca_system_score_gemma":0.0000036965089,"threshold_uncertainty_score":0.5898188},"labels":[],"label_agreement":null},{"id":"W29479265","doi":"10.1093/pch/pxx136","title":"Microphone Array Applications in Cabins","year":2012,"lang":"en","type":"article","venue":"Paediatrics & Child Health","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Acoustics; Beamforming; Microphone; Fuselage; Noise (video); Microphone array; Sound transmission class; Reverberation; Aerodynamics; Engineering; Wind tunnel; Computer science; Aerospace engineering; Sound pressure; Electronic engineering; Physics","score_opus":0.006256108358140204,"score_gpt":0.226228007637729,"score_spread":0.2199718992795888,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W29479265","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.37758717,0.053357713,0.52821845,0.0020974504,0.0045759007,0.0021992547,0.00041269808,0.0010011825,0.030550145],"genre_scores_gemma":[0.9849891,0.004111039,0.009420785,0.00028064786,0.0010156835,0.000048490387,0.00006136618,0.000047825695,0.000025050314],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.99885947,0.000017232702,0.00030663118,0.00013249305,0.0001222649,0.00056189345],"domain_scores_gemma":[0.9994068,0.000057092922,0.00004434968,0.0002500557,0.000016122518,0.00022558351],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00031241565,0.00014272396,0.00018867906,0.00014909988,0.00011238608,0.000012675804,0.00014281545,0.000080817925,0.000016045791],"category_scores_gemma":[0.000015107987,0.00014957844,0.00004154813,0.0005043944,0.000014897711,0.00006155595,0.000021468686,0.00036976265,0.000080190475],"study_design_candidate":"observational","study_design_consensus":"observational","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000012894765,0.0020174542,0.72407955,0.0027097,0.00011082283,0.000005645128,0.01290882,0.13307051,0.0053099478,0.024178425,0.036529142,0.05906707],"study_design_scores_gemma":[0.0029268814,0.00014731243,0.52508676,0.00014575357,0.00009200115,0.000045928202,0.0014522237,0.030626886,0.0008017076,0.0025985767,0.43307897,0.0029969749],"about_ca_topic_score_codex":0.000057256482,"about_ca_topic_score_gemma":0.00008374163,"teacher_disagreement_score":0.6074019,"about_ca_system_score_codex":0.00023340396,"about_ca_system_score_gemma":0.000039040104,"threshold_uncertainty_score":0.6099632},"labels":[],"label_agreement":null},{"id":"W2951437859","doi":"10.82308/37645","title":"Towards the design of low-noise aircraft landing gears using the lattice Boltzmann method","year":2014,"lang":"en","type":"article","venue":"eScholarship@McGill (McGill)","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Héroux-Devtek; McGill University","keywords":"Wind tunnel; Aerodynamics; Landing gear; Lattice Boltzmann methods; Boundary layer; Noise (video); Airplane; Flow separation; Computational fluid dynamics; Aeroacoustics; Flow (mathematics); Reynolds number; Mechanics; Sound pressure; Airframe; Engineering; Acoustics; Physics; Aerospace engineering; Turbulence; Computer science","score_opus":0.02595152461540939,"score_gpt":0.24624560818630284,"score_spread":0.22029408357089345,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2951437859","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.88133794,0.0003122362,0.09495111,0.000081387516,0.0019294338,0.000982833,0.00029280025,0.0005446529,0.019567579],"genre_scores_gemma":[0.9530514,0.000085547814,0.046284843,0.00019841417,0.00009496457,0.000025005302,0.000005541651,0.00014239566,0.000111873094],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.997283,0.00054988643,0.0006000814,0.00039772943,0.0005369314,0.00063240994],"domain_scores_gemma":[0.9975837,0.0010453571,0.00016807896,0.00089510664,0.00016289721,0.0001448497],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0033190825,0.00042034494,0.00044453528,0.00011732919,0.0008255321,0.00008525032,0.0009224532,0.0002338043,0.000048178194],"category_scores_gemma":[0.00072614336,0.00029281873,0.0002053756,0.000481625,0.00012001843,0.00029055405,0.00025217744,0.00095428975,0.000032754106],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000026482698,0.00004825577,0.000028027402,0.00018230469,0.00020269683,0.000011180838,0.000027570788,0.73268837,0.16930123,0.061004985,0.000009773284,0.036469135],"study_design_scores_gemma":[0.00047313864,0.000056189907,0.00022094906,0.00016492275,0.00021397066,0.00004133088,0.00011081734,0.95068526,0.024074702,0.017628845,0.0057907463,0.0005391491],"about_ca_topic_score_codex":0.0000709877,"about_ca_topic_score_gemma":0.000027158623,"teacher_disagreement_score":0.21799688,"about_ca_system_score_codex":0.0002422662,"about_ca_system_score_gemma":0.000018463421,"threshold_uncertainty_score":0.9999524},"labels":[],"label_agreement":null},{"id":"W2953899826","doi":"","title":"Turbulent Energy Prediction for an External Flow Around Valeo Cooling Fan by V2-F Modelling and Improved K-? Low Reynolds Model","year":2019,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Turbulence; Mechanics; Reynolds number; Physics; Reynolds stress; Computational fluid dynamics; Turbulence kinetic energy; Wind tunnel; Classical mechanics","score_opus":0.0073832718028119795,"score_gpt":0.18229312056349717,"score_spread":0.1749098487606852,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2953899826","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.2845329,0.0002158377,0.7135545,0.000009127783,0.00053922023,0.00020131642,0.00071320485,0.000089541856,0.00014434618],"genre_scores_gemma":[0.97076464,0.00028076567,0.027722087,0.00013367164,0.00031493045,0.000028131199,0.00022164454,0.00011563424,0.0004185021],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99864346,0.0000073148494,0.0002907237,0.00034239588,0.00013425399,0.0005818616],"domain_scores_gemma":[0.99897695,0.00003601627,0.000040446957,0.00031930275,0.00010381792,0.0005234821],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00012700717,0.0002685409,0.0002274958,0.00012417127,0.00014344866,0.00013848016,0.00018540164,0.0002514461,0.000005997331],"category_scores_gemma":[0.000011083009,0.00031831636,0.00004944242,0.00007151299,0.00003116485,0.00017149776,0.000015637288,0.00021995045,0.0000017004601],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00000897708,0.00000831954,0.000021466522,0.00009289705,0.000023913804,0.0000019839972,0.000088751854,0.95991457,0.037654355,0.0001980787,0.0007693087,0.0012173703],"study_design_scores_gemma":[0.0003790099,0.000068689726,0.00001453147,0.00005335581,0.000057271125,0.00000975036,0.000060773706,0.99774045,0.00012747735,0.0009268046,0.00021738604,0.00034450376],"about_ca_topic_score_codex":0.0015266774,"about_ca_topic_score_gemma":0.0021790834,"teacher_disagreement_score":0.68623173,"about_ca_system_score_codex":0.0003797115,"about_ca_system_score_gemma":0.00013633509,"threshold_uncertainty_score":0.99992687},"labels":[],"label_agreement":null},{"id":"W2955194048","doi":"10.1007/s10494-019-00047-7","title":"Effects of Nozzle Geometry on Turbulent Characteristics and Structure of Surface Attaching Jets","year":2019,"lang":"en","type":"article","venue":"Flow Turbulence and Combustion","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":23,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Manitoba","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Nozzle; Turbulence; Mechanics; Reynolds number; Particle image velocimetry; Geometry; Jet (fluid); Vorticity; Materials science; Optics; Turbulence kinetic energy; Physics; Vortex; Mathematics; Thermodynamics","score_opus":0.0026647164811528954,"score_gpt":0.18429913024473063,"score_spread":0.18163441376357772,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2955194048","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99666756,0.0004512572,0.0022083528,0.000009005165,0.00039897623,0.00016489645,0.000037573995,0.00002965859,0.00003274386],"genre_scores_gemma":[0.9985394,0.0004577399,0.0008829061,0.000018197066,0.000032455515,6.8415784e-7,0.000019384368,0.000017485914,0.00003176577],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993648,0.0000121602,0.00019367028,0.00015210034,0.00014379215,0.00013348456],"domain_scores_gemma":[0.99961174,0.00009898502,0.00006460779,0.00014495973,0.000037643036,0.00004204007],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000063140156,0.00014294784,0.00024200993,0.000055614615,0.000027799855,0.000013920792,0.000070889255,0.00010241891,0.000012683755],"category_scores_gemma":[0.000021542226,0.00013295856,0.000024936473,0.000086757274,0.000033433626,0.00006601039,0.000030812105,0.00018168696,0.000001926167],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00007908482,0.0000931532,0.016802313,0.0048612035,0.00009561689,0.000011276407,0.0006169335,0.5998259,0.35503924,0.00097521296,0.00014635731,0.021453694],"study_design_scores_gemma":[0.00046481783,0.00019314402,0.06604254,0.0005473283,0.00004898044,0.000009065546,0.000028474436,0.9098548,0.02229715,0.00024308293,0.000036508485,0.00023406066],"about_ca_topic_score_codex":0.000004194972,"about_ca_topic_score_gemma":5.94561e-7,"teacher_disagreement_score":0.33274207,"about_ca_system_score_codex":0.000015734118,"about_ca_system_score_gemma":0.0000049478763,"threshold_uncertainty_score":0.5421893},"labels":[],"label_agreement":null},{"id":"W2960316029","doi":"10.1108/hff-09-2018-0479","title":"Cross-sectional reshaping of perturbed/unperturbed rectangular jets","year":2019,"lang":"en","type":"article","venue":"International Journal of Numerical Methods for Heat &amp Fluid Flow","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Waterloo","funders":"","keywords":"Vortex; Mechanics; Instability; Particle image velocimetry; Jet (fluid); Physics; Curvature; Inlet; Entrainment (biomusicology); Reynolds number; Turbulence; Amplitude; Classical mechanics; Geometry; Optics; Geology; Acoustics; Mathematics","score_opus":0.026348701887183523,"score_gpt":0.36578320649201496,"score_spread":0.33943450460483143,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2960316029","genre_codex":"methods","genre_gemma":"methods","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.1325335,0.001171818,0.8584639,0.00013415722,0.006956152,0.0001588265,0.00006643083,0.000037017468,0.00047818216],"genre_scores_gemma":[0.2949096,0.00013117802,0.7034843,0.00020431347,0.000976989,0.000008275904,0.000024705068,0.00006511742,0.0001955393],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99783826,0.00009912838,0.0010111195,0.00020693702,0.00057468686,0.00026986102],"domain_scores_gemma":[0.9974614,0.0010796316,0.00016011417,0.00020670556,0.0009548177,0.00013736564],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0012356658,0.00022351788,0.00048734128,0.00025617503,0.00004408073,0.00007414868,0.0006088615,0.00017483743,0.0003741335],"category_scores_gemma":[0.001017755,0.00020062126,0.00047048499,0.00015826098,0.000064594155,0.00022105638,0.00006454413,0.00039135144,0.000011892846],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0005457323,0.00016931348,0.006927695,0.0001431934,0.001013428,0.000013598991,0.00025487135,0.4588469,0.48251155,0.0010541794,0.0012999199,0.047219638],"study_design_scores_gemma":[0.0012116277,0.00022800744,0.0040013045,0.0001384929,0.000037342845,0.00025496318,0.000017306937,0.9457022,0.006412635,0.0033109956,0.038384683,0.00030044946],"about_ca_topic_score_codex":0.0000059372783,"about_ca_topic_score_gemma":4.4369833e-7,"teacher_disagreement_score":0.4868553,"about_ca_system_score_codex":0.000260946,"about_ca_system_score_gemma":0.000060946903,"threshold_uncertainty_score":0.81810975},"labels":[],"label_agreement":null},{"id":"W2964932413","doi":"10.3390/jmse7080246","title":"Multigene Genetic-Programming-Based Models for Initial Dilution of Laterally Confined Vertical Buoyant Jets","year":2019,"lang":"en","type":"article","venue":"Journal of Marine Science and Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":23,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Ottawa","funders":"Natural Sciences and Engineering Research Council of Canada; China Scholarship Council","keywords":"Genetic programming; Generalization; Dilution; Genetic algorithm; Jet (fluid); Mathematics; Computer science; Applied mathematics; Mechanics; Algorithm; Physics; Statistical physics; Mathematical optimization; Artificial intelligence; Mathematical analysis; Thermodynamics","score_opus":0.008622472179622002,"score_gpt":0.21767664769515752,"score_spread":0.2090541755155355,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2964932413","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.76471764,0.00003660533,0.23465057,0.000013830423,0.00041998902,0.0000904393,0.0000025976055,0.000014596598,0.000053704043],"genre_scores_gemma":[0.94509965,0.00002916931,0.054768823,0.0000086602395,0.00007409938,0.0000020514817,9.311324e-7,0.000013796723,0.0000028317752],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9990821,0.0000024145484,0.00032678497,0.000092590184,0.00026765044,0.00022846823],"domain_scores_gemma":[0.9994554,0.000053406817,0.000041787367,0.000092248265,0.00025643222,0.0001007146],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00039966515,0.000104007624,0.0001969506,0.00016459358,0.000028425486,0.000037535192,0.00016103071,0.000042152005,0.0000061108144],"category_scores_gemma":[0.000083085644,0.00009235368,0.000050041974,0.00015256145,0.000054604985,0.00016637288,0.000048693128,0.0001146413,3.2811963e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000017936116,0.000012824336,0.00014706583,0.00010054838,0.000011443394,0.0000029354826,0.00003127959,0.8423745,0.14695048,0.00022752475,0.0000034408347,0.010120021],"study_design_scores_gemma":[0.0005817792,0.00016866243,0.004329062,0.000052846484,0.000017751014,0.000014649837,0.000008535644,0.98786277,0.0066373744,0.00010712646,0.000112338144,0.00010709331],"about_ca_topic_score_codex":0.0000036741008,"about_ca_topic_score_gemma":0.0000014833258,"teacher_disagreement_score":0.18038197,"about_ca_system_score_codex":0.00004413042,"about_ca_system_score_gemma":0.00006446121,"threshold_uncertainty_score":0.3766074},"labels":[],"label_agreement":null},{"id":"W2966099225","doi":"10.1680/jencm.18.00034","title":"Characteristics of two-dimensional counter-flowing wall jets","year":2019,"lang":"en","type":"article","venue":"Proceedings of the Institution of Civil Engineers - Engineering and Computational Mechanics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Concordia University","funders":"","keywords":"Dilution; Jet (fluid); Mechanics; Mixing (physics); Penetration (warfare); Jet stream; Wake; Chemistry; Physics; Thermodynamics; Mathematics","score_opus":0.0039681226456447505,"score_gpt":0.17705833676255794,"score_spread":0.1730902141169132,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2966099225","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9573609,0.00012580084,0.04117765,0.00001927454,0.00080870243,0.00016170376,0.000041818883,0.0000728912,0.00023123977],"genre_scores_gemma":[0.9948361,0.000023344568,0.005051856,0.000008474512,0.00003384103,0.000004167024,0.000008046603,0.000026185713,0.000008010476],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99893034,0.0000015553438,0.00044056593,0.00013331974,0.00034053987,0.00015367469],"domain_scores_gemma":[0.99945015,0.0000636495,0.000097863,0.00007793907,0.0002647407,0.00004566225],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018842428,0.00018155729,0.00029746504,0.00013512536,0.000027334387,0.000011382577,0.0001904631,0.00007817015,0.000006187979],"category_scores_gemma":[0.0000548044,0.00017031799,0.00008837087,0.00021223561,0.00002935301,0.00012946226,0.00006532277,0.0001789691,8.166712e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000005880248,0.00001706177,0.000131645,0.0005817829,0.000057901245,1.4663928e-7,0.00007889528,0.8943168,0.040430453,0.06427168,0.000014453593,0.00009330121],"study_design_scores_gemma":[0.00035029452,0.00003626257,0.00067327917,0.00039512635,0.00003705328,0.000011323319,0.000014663499,0.99240327,0.0046552503,0.0012105077,0.000053368916,0.00015959419],"about_ca_topic_score_codex":0.0000028355928,"about_ca_topic_score_gemma":3.8691869e-7,"teacher_disagreement_score":0.09808648,"about_ca_system_score_codex":0.00004835733,"about_ca_system_score_gemma":0.000028381115,"threshold_uncertainty_score":0.6945366},"labels":[],"label_agreement":null},{"id":"W2970091142","doi":"10.1615/thmt-18.820","title":"DNS study of dual-plume interference in a wall-bounded turbulent flow","year":2018,"lang":"en","type":"article","venue":"Proceeding of THMT-18. Turbulence Heat and Mass Transfer 9 Proceedings of the Ninth International Symposium On Turbulence Heat and Mass Transfer","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Manitoba","funders":"","keywords":"Plume; Turbulence; Mixing (physics); Physics; Mechanics; Line source; Boundary layer; Direct numerical simulation; Line (geometry); Computational physics; Meteorology; Optics; Geometry; Reynolds number; Mathematics","score_opus":0.013890906311425073,"score_gpt":0.23356136889441415,"score_spread":0.21967046258298908,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2970091142","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9908613,0.00024067324,0.0018854429,0.0010875184,0.0008769361,0.0011610868,0.00007834101,0.000091707094,0.0037169994],"genre_scores_gemma":[0.9973169,0.0014699212,0.0006242733,0.00008308831,0.00017453119,0.00011812157,0.000005662771,0.000077670586,0.00012982229],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9963699,0.000018758941,0.001277399,0.00080821174,0.0008928127,0.0006329437],"domain_scores_gemma":[0.99862266,0.000106492,0.00005982948,0.0002187557,0.0007939238,0.00019832696],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0005965654,0.00067831716,0.0008769126,0.00039888525,0.00016815048,0.00012673825,0.0008774915,0.00027842872,0.00007760531],"category_scores_gemma":[0.000049276765,0.0005532019,0.0001789061,0.00056619284,0.0006148275,0.0005921719,0.00009139378,0.0007615941,0.0000012783249],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0021718869,0.0018016642,0.046149474,0.004267268,0.00090069656,0.000011366641,0.026218198,0.011931073,0.89437854,0.010300137,0.0003922092,0.0014774913],"study_design_scores_gemma":[0.0067444965,0.0044384585,0.006424587,0.0063992506,0.0005431669,0.0000954888,0.004583684,0.64616746,0.31632733,0.0060308496,0.0003467315,0.0018984962],"about_ca_topic_score_codex":0.00011925428,"about_ca_topic_score_gemma":0.000029250543,"teacher_disagreement_score":0.6342364,"about_ca_system_score_codex":0.00013556672,"about_ca_system_score_gemma":0.000051911928,"threshold_uncertainty_score":0.99969196},"labels":[],"label_agreement":null},{"id":"W2971044475","doi":"10.29252/jafm.13.01.29970","title":"Experiments and Large-Eddy Simulations of Lobed and Swirling Turbulent Thermal Jets for HVAC's Applications","year":2019,"lang":"en","type":"article","venue":"Journal of Applied Fluid Mechanics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":13,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Nozzle; Turbulence; Jet (fluid); Mechanics; Diffuser (optics); HVAC; Mixing (physics); Materials science; Thermal; Large eddy simulation; Physics; Air conditioning; Optics; Thermodynamics","score_opus":0.0065690233063317345,"score_gpt":0.22349008975833887,"score_spread":0.21692106645200712,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2971044475","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.57520896,0.00038426282,0.42370433,0.000013405482,0.00013131823,0.00037977507,0.000027373488,0.000013487391,0.0001370686],"genre_scores_gemma":[0.9842822,0.0001572658,0.015400881,0.00002059901,0.0000835309,0.0000122489755,0.0000054219845,0.000029402216,0.00000846543],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992757,0.000003158922,0.0003507407,0.0000931263,0.0001325907,0.00014469858],"domain_scores_gemma":[0.9995227,0.00007275006,0.00012072032,0.00012858404,0.00008905794,0.00006622403],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018314822,0.00011239552,0.00022302826,0.00007400991,0.00004721561,0.000019005287,0.00009475769,0.00007793017,0.000011258523],"category_scores_gemma":[0.000005780625,0.000106471205,0.000043424276,0.00005982717,0.000006942954,0.000052809264,0.000032799937,0.00011883272,8.1379767e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000038077185,0.000059570935,0.0000081342,0.00012326725,0.000093523355,6.1391694e-7,0.00034604507,0.33775738,0.63139457,0.028507885,0.000034326775,0.001636592],"study_design_scores_gemma":[0.0009657692,0.000062012594,0.000011152707,0.000027203881,0.000054993085,0.0000069776293,0.00024321755,0.9770327,0.016562527,0.0036334817,0.0012826767,0.00011723819],"about_ca_topic_score_codex":1.6306822e-7,"about_ca_topic_score_gemma":3.808612e-7,"teacher_disagreement_score":0.6392754,"about_ca_system_score_codex":0.000028894125,"about_ca_system_score_gemma":0.000015093906,"threshold_uncertainty_score":0.43417698},"labels":[],"label_agreement":null},{"id":"W2978454449","doi":"10.3390/w11102077","title":"Numerical Modeling of Multiple Inclined Dense Jets Discharged from Moderately Spaced Ports","year":2019,"lang":"en","type":"article","venue":"Water","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":25,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Ottawa","funders":"Natural Sciences and Engineering Research Council of Canada; China Scholarship Council","keywords":"Turbulence; Mechanics; Brine; Desalination; Mixing (physics); Numerical modeling; Computational fluid dynamics; Computer simulation; Dilution; Marine engineering; Physics; Engineering; Chemistry; Thermodynamics","score_opus":0.009036654500790223,"score_gpt":0.19462531005427974,"score_spread":0.18558865555348952,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2978454449","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9196061,0.000031076495,0.07920482,0.000029726687,0.00044639385,0.00011570906,0.000028774184,0.0000934376,0.00044398077],"genre_scores_gemma":[0.99590075,0.000008531049,0.0036785165,0.000021127762,0.00007350144,0.0000053424114,0.00009618246,0.000049380713,0.0001666608],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99917954,0.000010518028,0.00025315175,0.00017531755,0.00013734121,0.0002441411],"domain_scores_gemma":[0.99960274,0.000024437591,0.000017450498,0.00025579683,0.000041286152,0.000058280217],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00006742582,0.00014804988,0.00023651526,0.000035009776,0.000023818937,0.000021560067,0.00010138003,0.000090078276,0.00017675507],"category_scores_gemma":[0.000011817664,0.00010983602,0.00006102736,0.000031739637,0.000008795653,0.00008471805,0.000049000166,0.0001447053,0.00012135063],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00002116978,0.000017103564,0.0011500943,0.000021030512,0.000029203466,0.0000057941293,0.00030849635,0.87449527,0.12381579,0.000013319415,0.00004122464,0.000081489845],"study_design_scores_gemma":[0.00035173472,0.000010482575,0.00019202316,0.000019898302,0.000011443864,8.60509e-7,0.000019953095,0.9819061,0.016746217,0.00052505475,0.00004781075,0.00016837749],"about_ca_topic_score_codex":0.00009667587,"about_ca_topic_score_gemma":0.00001173997,"teacher_disagreement_score":0.10741086,"about_ca_system_score_codex":0.00002220404,"about_ca_system_score_gemma":0.0000051664306,"threshold_uncertainty_score":0.4478983},"labels":[],"label_agreement":null},{"id":"W2981381292","doi":"10.3390/app9214485","title":"Predicting Far-Field Noise Generated by a Landing Gear Using Multiple Two-Dimensional Simulations","year":2019,"lang":"en","type":"article","venue":"Applied Sciences","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto","funders":"Natural Sciences and Engineering Research Council of Canada; University of Toronto; Taibah University","keywords":"Strouhal number; Noise (video); Computational fluid dynamics; Near and far field; Acoustics; Cylinder; Flow (mathematics); Physics; Turbulence; Mathematics; Mechanics; Geometry; Computer science; Optics","score_opus":0.013562908158720141,"score_gpt":0.23719868217071424,"score_spread":0.2236357740119941,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2981381292","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98121166,0.000047643585,0.0156026585,0.000010476969,0.00036563422,0.0001412825,0.000021216658,0.00012758253,0.0024718668],"genre_scores_gemma":[0.992807,0.0000016014038,0.006985341,0.00006907985,0.00007578478,0.0000032231112,0.0000121890935,0.000014463951,0.00003135629],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99914885,0.0000057411257,0.00015808214,0.00021195425,0.00021944878,0.00025594514],"domain_scores_gemma":[0.9996003,0.00019224515,0.000030406043,0.000106791194,0.000019761259,0.000050506747],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017152676,0.000109311164,0.000107891006,0.000060234204,0.0002600426,0.000076416974,0.00015210808,0.000049543443,0.00006809793],"category_scores_gemma":[0.000023117042,0.00010142507,0.0000207249,0.0002859645,0.000041664127,0.00009054484,0.00004811437,0.00012427456,0.000022303282],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[9.131924e-7,0.000003992313,0.004847574,0.0000036188471,0.0000044804506,2.3345861e-7,0.00003593071,0.6526839,0.3420768,0.00015808314,0.000052358224,0.00013208707],"study_design_scores_gemma":[0.00019849352,0.000010065421,0.00007707897,0.000010606726,0.000006563037,0.000001179332,0.000054940145,0.99442244,0.0049077743,0.0001083794,0.00006577504,0.00013672301],"about_ca_topic_score_codex":0.000039598952,"about_ca_topic_score_gemma":0.000023628567,"teacher_disagreement_score":0.3417385,"about_ca_system_score_codex":0.000032153923,"about_ca_system_score_gemma":0.000021110714,"threshold_uncertainty_score":0.41359943},"labels":[],"label_agreement":null},{"id":"W2986853567","doi":"10.3390/jmse7110409","title":"Three-Dimensional Numerical Simulations of Buoyant Jets Discharged from a Rosette-Type Multiport Diffuser","year":2019,"lang":"en","type":"article","venue":"Journal of Marine Science and Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":28,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Ottawa","funders":"Natural Sciences and Engineering Research Council of Canada; China Scholarship Council","keywords":"Turbulence; Mechanics; Mixing (physics); Computer simulation; Diffuser (optics); Jet (fluid); Rosette (schizont appearance); Outfall; Physics; Simulation; Environmental science; Computer science; Optics; Environmental engineering; Biology","score_opus":0.005848726096744868,"score_gpt":0.20167139492087813,"score_spread":0.19582266882413327,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2986853567","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98685586,0.000060947183,0.012134973,0.00002632687,0.0007929275,0.00005404625,0.000008610109,0.00001747012,0.00004885736],"genre_scores_gemma":[0.9872082,0.000017920996,0.012647705,0.000009321537,0.0000917561,3.0177142e-7,0.0000023163873,0.000015186681,0.00000732555],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989802,0.0000020869807,0.00032417921,0.00010509054,0.00040381416,0.00018458068],"domain_scores_gemma":[0.99939483,0.00008703402,0.000072557654,0.00012888809,0.00020506258,0.00011162997],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002547932,0.000113112605,0.00023170735,0.00014913229,0.00003426098,0.000029430983,0.00017527645,0.00003620635,0.000058123293],"category_scores_gemma":[0.00014169887,0.000092653616,0.0000394592,0.00030153734,0.000041241856,0.00025342248,0.00011974135,0.00021473436,0.0000024826695],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000009275971,0.000019882205,0.012030625,0.000018597846,0.00002187964,0.0000054883494,0.000034177305,0.8296032,0.15719813,0.00005824765,0.000025604186,0.000974876],"study_design_scores_gemma":[0.0002673602,0.00005017415,0.07835054,0.000042481257,0.000014465765,0.000012804668,0.0000061137434,0.9201874,0.00074324943,0.000105098625,0.0001155672,0.00010476021],"about_ca_topic_score_codex":0.000015381489,"about_ca_topic_score_gemma":0.0000035258909,"teacher_disagreement_score":0.15645489,"about_ca_system_score_codex":0.00004122534,"about_ca_system_score_gemma":0.00004537094,"threshold_uncertainty_score":0.37783048},"labels":[],"label_agreement":null},{"id":"W2988665433","doi":"10.1017/jfm.2019.164","title":"An empirical expression for on the axis of a slightly heated turbulent round jet","year":2019,"lang":"en","type":"article","venue":"Journal of Fluid Mechanics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Royal Military College of Canada; Université Laval","funders":"","keywords":"Unicode; Physics; Computer science","score_opus":0.01532414417977573,"score_gpt":0.2568654378038719,"score_spread":0.24154129362409615,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2988665433","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8743103,0.0001275493,0.12422059,0.00021192853,0.00082395755,0.00018127209,0.000015055053,0.000016108761,0.00009323431],"genre_scores_gemma":[0.99574906,0.00010131131,0.003820702,0.000108521126,0.00016000202,0.0000026991468,0.000002515132,0.000030491045,0.000024726065],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99907595,0.000025967853,0.00039069806,0.000081975784,0.00026812864,0.00015729603],"domain_scores_gemma":[0.9992527,0.00014628124,0.000116047515,0.00024872698,0.00016403537,0.00007225087],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000454162,0.00012483077,0.0002445242,0.00006430151,0.00003407596,0.000022684415,0.0002663161,0.00009832626,0.000051544208],"category_scores_gemma":[0.000047765694,0.000075812655,0.00013493521,0.00007910428,0.0000050529234,0.0000793358,0.000015836471,0.00022734587,0.0000046118657],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00010950618,0.000104555074,0.000012096052,0.000055200337,0.000054072727,0.0000052055584,0.0001999393,0.121220805,0.86942893,0.00310896,0.005288884,0.00041181417],"study_design_scores_gemma":[0.00044261254,0.0008458684,0.000017337969,0.00013571086,0.000030260138,0.000021637641,0.00010428411,0.8870422,0.10698515,0.0021367038,0.0021340093,0.000104220795],"about_ca_topic_score_codex":4.3946568e-7,"about_ca_topic_score_gemma":6.254559e-7,"teacher_disagreement_score":0.7658214,"about_ca_system_score_codex":0.00006831612,"about_ca_system_score_gemma":0.000028332588,"threshold_uncertainty_score":0.30915505},"labels":[],"label_agreement":null},{"id":"W2990469972","doi":"10.1115/ajkfluids2019-5478","title":"The Effects of Nozzle Orientation on Mixing Characteristics of Elliptic Twin Free Jets","year":2019,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Manitoba","funders":"","keywords":"Nozzle; Turbulence; Jet (fluid); Mechanics; Plane (geometry); Physics; Particle image velocimetry; Reynolds number; Optics; Plane symmetry; Materials science; Geometry; Thermodynamics; Mathematics","score_opus":0.0025874072540822755,"score_gpt":0.18602943349479314,"score_spread":0.18344202624071088,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2990469972","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9862319,0.000034663168,0.007103118,0.0000074068344,0.0011541221,0.000157282,0.000006897002,0.000031226828,0.0052733705],"genre_scores_gemma":[0.998937,0.000067378096,0.00058811397,0.000009693191,0.000036663147,0.0000032435037,0.0000050180975,0.00001719648,0.00033566097],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994974,0.000008421375,0.00018831514,0.00006879551,0.00012864718,0.000108403205],"domain_scores_gemma":[0.9992595,0.000353807,0.000047520647,0.00028488968,0.00003647281,0.000017840892],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000087908746,0.00007588401,0.00012137003,0.000025929745,0.000019282583,0.000008806489,0.00014102433,0.000038520302,0.000014839715],"category_scores_gemma":[0.00010048764,0.000055682092,0.000033317014,0.00006465381,0.000017842478,0.000024409674,0.000024271169,0.00007642367,0.000019733445],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000055336197,0.00014943187,0.010162283,0.0027296422,0.00020247899,0.000006109842,0.0009601702,0.04324824,0.83507353,0.07631515,0.0014250749,0.02967256],"study_design_scores_gemma":[0.0008415352,0.00032466496,0.048158623,0.00030355863,0.000053486136,0.0000010174277,0.000118590215,0.85739934,0.09061155,0.0013343057,0.0005694245,0.00028391596],"about_ca_topic_score_codex":0.000004324889,"about_ca_topic_score_gemma":0.000003919207,"teacher_disagreement_score":0.8141511,"about_ca_system_score_codex":0.000019068091,"about_ca_system_score_gemma":0.0000048653833,"threshold_uncertainty_score":0.22706498},"labels":[],"label_agreement":null},{"id":"W2991338904","doi":"10.1115/ajkfluids2019-5463","title":"Experimental Investigation of Nozzle Orientation Effects on Mixing Characteristics of Elliptic Triple Free Jets","year":2019,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Manitoba","funders":"","keywords":"Nozzle; Turbulence; Mechanics; Plane (geometry); Physics; Materials science; Geometry; Optics; Mathematics; Thermodynamics","score_opus":0.005675687142094941,"score_gpt":0.2042180112431223,"score_spread":0.19854232410102737,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2991338904","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9932252,0.00003489649,0.0039934414,0.000004043882,0.0008436821,0.00020657896,0.000012106115,0.00004524317,0.0016347751],"genre_scores_gemma":[0.9973731,0.0000063167186,0.0023752898,0.0000120425875,0.000044522418,0.0000062703302,0.000033392713,0.000021235046,0.00012780569],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99939615,0.000013993295,0.00023972012,0.00009961599,0.0001514989,0.00009902724],"domain_scores_gemma":[0.99955267,0.00010217561,0.00006542934,0.0002155449,0.00003257356,0.00003159547],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000092853545,0.000096518306,0.00016623693,0.00006292545,0.000011856031,0.000006780076,0.0000930272,0.000053529493,0.00004255085],"category_scores_gemma":[0.000039923696,0.00009608718,0.00003428779,0.00008928057,0.000017218177,0.000060641818,0.000020872365,0.000064630374,0.000017696686],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000014614245,0.000022855926,0.0034863101,0.00030754504,0.000018210521,6.1004243e-7,0.0003172743,0.0039865994,0.98820317,0.0028073706,0.000108606924,0.0007268395],"study_design_scores_gemma":[0.0005550826,0.0001521672,0.02197363,0.00011347659,0.000013018013,4.333069e-7,0.00008288827,0.22015172,0.7566576,0.00016120235,0.000014153747,0.00012461946],"about_ca_topic_score_codex":0.000005650487,"about_ca_topic_score_gemma":9.827204e-7,"teacher_disagreement_score":0.23154555,"about_ca_system_score_codex":0.000040940293,"about_ca_system_score_gemma":0.000007249067,"threshold_uncertainty_score":0.39183214},"labels":[],"label_agreement":null},{"id":"W2991886677","doi":"","title":"Aeroacoustic prediction of an automotive cooling fan","year":2011,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Aerodynamics; Acoustics; Noise (video); Directivity; Mach number; Rotor (electric); Aeroacoustics; Sound pressure; Transonic; Polygon mesh; Microphone; Engineering; Acoustic radiation; Structural engineering; Aerospace engineering; Physics; Computer science; Mechanical engineering; Radiation; Optics; Electrical engineering","score_opus":0.016760954633796916,"score_gpt":0.1813656653767206,"score_spread":0.16460471074292368,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2991886677","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7760699,0.00007664307,0.20575206,0.0000031265063,0.0016776844,0.0002107843,0.0010884659,0.00029140903,0.014829961],"genre_scores_gemma":[0.99075794,0.000034879995,0.008803718,0.0000451968,0.0001581206,0.0000064589594,0.00006394127,0.000064879125,0.000064875705],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99898666,0.000012747159,0.00028431014,0.00017233586,0.00013424421,0.0004097162],"domain_scores_gemma":[0.99898756,0.000024796967,0.000039637147,0.00032238438,0.00017131507,0.00045432086],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012182814,0.00018023103,0.00018996319,0.00021126316,0.000081151426,0.000016533555,0.00023096442,0.00017029919,0.00014060584],"category_scores_gemma":[0.00007843084,0.00021025728,0.000040878997,0.00019971615,0.00008503285,0.00010564872,0.000013715714,0.00023185727,0.00001567139],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000015336258,0.000089704976,0.0009939064,0.0003154975,0.0001945042,0.0002026083,0.0035239118,0.91879565,0.062331066,0.002154392,0.0033447626,0.008038648],"study_design_scores_gemma":[0.00014925255,0.00007751436,0.02309153,0.000034555094,0.00009182573,0.000014179785,0.00040244643,0.9749627,0.00043210565,0.0004726528,0.000061755076,0.00020944697],"about_ca_topic_score_codex":0.0034086981,"about_ca_topic_score_gemma":0.0040988484,"teacher_disagreement_score":0.21468806,"about_ca_system_score_codex":0.00023382863,"about_ca_system_score_gemma":0.00016398919,"threshold_uncertainty_score":0.8574043},"labels":[],"label_agreement":null},{"id":"W2992056085","doi":"","title":"Minimizing Sonic Boom Noise to Meet Potential Regulatory Limits","year":2019,"lang":"en","type":"article","venue":"LA Referencia (Red Federada de Repositorios Institucionales de Publicaciones Científicas)","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Carleton University","funders":"","keywords":"Sonic boom; Supersonic speed; Acoustics; Aircraft noise; Noise (video); Sound pressure; Fuselage; Aerospace engineering; Shock (circulatory); Lift (data mining); Environmental science; Engineering; Physics; Computer science; Noise reduction","score_opus":0.01052561888165626,"score_gpt":0.2131225384562968,"score_spread":0.20259691957464054,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2992056085","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8494224,0.00048532613,0.016558452,0.0036000018,0.0046872273,0.00093724683,0.00009274949,0.0012300331,0.12298659],"genre_scores_gemma":[0.9913636,0.000068290195,0.0069630374,0.00019982066,0.0006876312,0.000099433724,0.000063665386,0.00012284156,0.00043171764],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"not_applicable","domain_scores_codex":[0.9969843,0.0000974794,0.0006460756,0.0006769547,0.00071937736,0.00087582535],"domain_scores_gemma":[0.99818236,0.000110121204,0.00013005022,0.00078449055,0.00023744913,0.00055551616],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00041456768,0.00049613114,0.000483522,0.000399544,0.0003189858,0.0002180476,0.0006708247,0.00046684768,0.00006446122],"category_scores_gemma":[0.00014593374,0.00053025066,0.00023252473,0.00051997666,0.000011910256,0.000336028,0.00019628642,0.0004841538,0.00008972249],"study_design_candidate":"not_applicable","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0001453172,0.0002741758,0.00038811972,0.00027377962,0.00028369148,0.0002014068,0.001011245,0.11137374,0.10395661,0.774545,0.005450465,0.0020964427],"study_design_scores_gemma":[0.0015055335,0.00011726845,0.005639378,0.0002901382,0.00012379054,0.00064079365,0.0003340046,0.1029819,0.003238916,0.0005836474,0.88318175,0.0013629051],"about_ca_topic_score_codex":3.6115978e-7,"about_ca_topic_score_gemma":0.00005044802,"teacher_disagreement_score":0.87773126,"about_ca_system_score_codex":0.00066932006,"about_ca_system_score_gemma":0.00021454669,"threshold_uncertainty_score":0.9997149},"labels":[],"label_agreement":null},{"id":"W2992846593","doi":"","title":"ACOUSTICS OF AERO-ACOUSTIC WIND TUNNELS – STATE OF THE ART","year":2017,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Aerospace; Acoustics; Engineering; Noise (video); Wind tunnel; Aerospace engineering; Emphasis (telecommunications); Jet noise; Aeroacoustics; Sound pressure; Aerodynamics; Jet (fluid); Marine engineering; Computer science; Telecommunications; Physics","score_opus":0.008358957524542127,"score_gpt":0.19918335123697054,"score_spread":0.1908243937124284,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2992846593","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9229507,0.00021244837,0.058124185,0.00013405045,0.004296221,0.00048829784,0.0021405646,0.000075969285,0.0115775615],"genre_scores_gemma":[0.9971331,0.0001898101,0.0012239788,0.00006383606,0.00015059652,0.0000033812362,0.000011682984,0.000085729866,0.0011379026],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9983839,0.000015964684,0.00050110545,0.00020287887,0.00031571928,0.00058044],"domain_scores_gemma":[0.9976871,0.000095716,0.00023465023,0.001388855,0.00024510693,0.00034857594],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00020305844,0.00028422184,0.0004091511,0.00012560457,0.00026725547,0.00007361044,0.0011317645,0.00016273862,0.00006551862],"category_scores_gemma":[0.00045221593,0.00025715816,0.0001283129,0.00013384239,0.0004632077,0.00009011399,0.00011612352,0.0003799638,0.00002139387],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000028885363,0.000014030933,0.000662471,0.00028369308,0.00007539423,0.000024080733,0.00014447207,0.8461377,0.14397863,0.00016877052,0.007215555,0.0012923027],"study_design_scores_gemma":[0.00041030336,0.00004771338,0.13015217,0.00022274026,0.0002585407,0.000015256783,0.00009880674,0.8647314,0.00077864196,0.0016804587,0.001079203,0.00052480516],"about_ca_topic_score_codex":0.0011383482,"about_ca_topic_score_gemma":0.0042197458,"teacher_disagreement_score":0.14319998,"about_ca_system_score_codex":0.00020832372,"about_ca_system_score_gemma":0.00039263448,"threshold_uncertainty_score":0.9999881},"labels":[],"label_agreement":null},{"id":"W2993067496","doi":"","title":"Jet noise prediction using a fully unstructured large eddy simulation solver","year":2011,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Jet noise; Strouhal number; Large eddy simulation; Nozzle; Aerodynamics; Unstructured grid; Acoustics; Jet (fluid); Boundary layer; Mechanics; Detached eddy simulation; Turbulence; Supersonic speed; Noise (video); Computational fluid dynamics; Physics; Engineering; Aerospace engineering; Computer science; Reynolds-averaged Navier–Stokes equations; Reynolds number","score_opus":0.01863643041352534,"score_gpt":0.20396710277039823,"score_spread":0.1853306723568729,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2993067496","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.45438626,0.000051170657,0.5402511,0.0000029501798,0.0018885477,0.00017788485,0.00073557923,0.00018117922,0.0023253094],"genre_scores_gemma":[0.98800933,0.000014232407,0.011344976,0.000088683875,0.0003378278,0.000003217904,0.00007842707,0.00006991003,0.0000533742],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989476,0.000009369175,0.00023326257,0.00017733016,0.0001350236,0.0004974232],"domain_scores_gemma":[0.9992214,0.000019635301,0.000032997355,0.00027007,0.000101345824,0.000354558],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00008780964,0.0002009202,0.0001500902,0.00018115625,0.00015409972,0.000037573172,0.00014504869,0.00021341152,0.00024467448],"category_scores_gemma":[0.00005057379,0.00022580578,0.000047467296,0.0001854321,0.00003264826,0.000111951595,0.000016623197,0.00023166412,0.000021665663],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000002834172,0.000006643259,0.0009882522,0.000033490564,0.000030870327,0.00003061073,0.00033795775,0.9901836,0.006864671,0.00024172808,0.0008117677,0.0004675923],"study_design_scores_gemma":[0.0002007982,0.000013883477,0.008583166,0.000018934817,0.00007615206,0.000007402825,0.00008323241,0.98966986,0.00003530059,0.00040751818,0.0006748463,0.00022888326],"about_ca_topic_score_codex":0.0014749691,"about_ca_topic_score_gemma":0.0049544675,"teacher_disagreement_score":0.5336231,"about_ca_system_score_codex":0.00041792367,"about_ca_system_score_gemma":0.00015040187,"threshold_uncertainty_score":0.92080927},"labels":[],"label_agreement":null},{"id":"W2993166778","doi":"","title":"Source localization of aircraft engines with circular microphone arrays","year":2011,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Jet engine; Anechoic chamber; Beamforming; Microphone; Microphone array; Acoustics; Noise (video); Turbofan; Jet noise; Aircraft noise; Engineering; Computer science; Aerospace engineering; Jet (fluid); Electronic engineering; Noise reduction; Artificial intelligence; Loudspeaker; Physics","score_opus":0.006961639473745194,"score_gpt":0.15429298947018263,"score_spread":0.14733134999643743,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2993166778","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.107760906,0.00014555236,0.8895665,0.000004554918,0.0002921085,0.000098183344,0.000060438593,0.000079253026,0.0019925125],"genre_scores_gemma":[0.9857849,0.000056442266,0.013835154,0.00005869138,0.000074957534,0.000004126074,0.000025385662,0.00006832451,0.00009203399],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99928737,0.000005445992,0.00017944607,0.00012454735,0.00010161974,0.0003016019],"domain_scores_gemma":[0.9993547,0.0000127502035,0.000028777282,0.0002575724,0.000108415916,0.00023776108],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000049821352,0.0001552583,0.00016194236,0.00014421892,0.000050548508,0.000011017987,0.00015563391,0.00010702936,0.00008227429],"category_scores_gemma":[0.00002071042,0.00015992434,0.000027880604,0.00022863889,0.00007508276,0.00003515637,0.0000080629325,0.0001237893,0.000014006493],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000024518476,0.00001072549,0.0009575973,0.00015036114,0.000052161806,0.0000314179,0.0006640748,0.96508497,0.03109322,0.00012495664,0.0011772405,0.0006508114],"study_design_scores_gemma":[0.00020929756,0.000044986315,0.0014355009,0.00006267761,0.00008609662,0.000022259397,0.00028922013,0.9932312,0.0021563666,0.00015254863,0.0019521513,0.00035769783],"about_ca_topic_score_codex":0.0029503277,"about_ca_topic_score_gemma":0.0029104368,"teacher_disagreement_score":0.878024,"about_ca_system_score_codex":0.0001147953,"about_ca_system_score_gemma":0.00011440745,"threshold_uncertainty_score":0.65215254},"labels":[],"label_agreement":null},{"id":"W2993647676","doi":"","title":"Evaluation of jet noise prediction capabilities of stochastic and statistical models","year":2011,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Jet noise; Turbulence; Reynolds-averaged Navier–Stokes equations; Noise (video); Statistical physics; Aerodynamics; Probabilistic logic; Field (mathematics); Physics; Mathematics; Mechanics; Computer science; Statistics","score_opus":0.030350562212657722,"score_gpt":0.211690756954488,"score_spread":0.18134019474183027,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2993647676","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.5174119,0.00014075612,0.4781765,0.0000015752286,0.00026620508,0.00016340983,0.0013327515,0.000019981931,0.0024869167],"genre_scores_gemma":[0.995427,0.00002080038,0.004459663,0.000003924564,0.000027814885,0.000008632558,0.000025040044,0.000020655258,0.0000064838828],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992448,0.000019308303,0.00023401031,0.000094782954,0.00024080729,0.00016627376],"domain_scores_gemma":[0.999299,0.000057515266,0.000029885106,0.00015301422,0.00029853798,0.00016203283],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003421905,0.000096268835,0.00014535453,0.00011231329,0.000024440647,0.000004630178,0.00006359557,0.00008168544,0.00007143201],"category_scores_gemma":[0.0001851772,0.00010481589,0.000014672876,0.0000629386,0.00012615578,0.00005167602,0.000008749365,0.00008526248,7.65818e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000002959376,0.000011801636,0.0001314093,0.0001449388,0.00004277347,0.0000012845053,0.0009861225,0.9852299,0.0025033355,0.008091758,0.00026306257,0.0025906607],"study_design_scores_gemma":[0.00014242948,0.00003589599,0.0062245145,0.000025902964,0.00021550457,0.0000023256769,0.00025172826,0.97574925,0.000031074804,0.01723844,8.8984837e-7,0.00008201801],"about_ca_topic_score_codex":0.003443696,"about_ca_topic_score_gemma":0.0034930012,"teacher_disagreement_score":0.4780151,"about_ca_system_score_codex":0.0001538014,"about_ca_system_score_gemma":0.00021359243,"threshold_uncertainty_score":0.52058613},"labels":[],"label_agreement":null},{"id":"W2993862764","doi":"","title":"Surface Dipole Strength Generated by Cylindrical Struts","year":2017,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"Rowan Williams Davies & Irwin (Canada)","funders":"","keywords":"Mechanics; Cylinder; Jet (fluid); Mach number; Physics; Laminar flow; Aerodynamic force; Dipole; Noise (video); Reynolds number; Flow (mathematics); Aerodynamics; Plane (geometry); Potential flow; Nozzle; Surface (topology); Geometry; Turbulence; Mathematics","score_opus":0.008898117741641934,"score_gpt":0.2102681088538643,"score_spread":0.20136999111222237,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2993862764","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9579448,0.0003116363,0.01720524,0.00018428602,0.0022189037,0.00014859659,0.0019261998,0.0001899815,0.019870332],"genre_scores_gemma":[0.99522805,0.00013817995,0.0022247636,0.000093203176,0.00023874287,0.0000023637847,0.00010731346,0.00007174592,0.0018956381],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99886715,0.000007909194,0.00019096553,0.00020577149,0.00014588506,0.000582324],"domain_scores_gemma":[0.998568,0.000028642058,0.000039856255,0.00065125455,0.00006869289,0.0006435377],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000070608345,0.00021643037,0.00018793206,0.00004398017,0.0004514182,0.0002715708,0.0005232453,0.00020430567,0.00014627639],"category_scores_gemma":[0.00010691476,0.00024431862,0.000039025774,0.000053344902,0.00009866751,0.00008149497,0.000037944745,0.00032100413,0.00011854542],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000027129288,0.000028125729,0.0017040002,0.00006253556,0.00012426627,0.00022231834,0.00007010231,0.57392514,0.10840481,0.0011267988,0.3072586,0.007070604],"study_design_scores_gemma":[0.00020320265,0.000013910685,0.0030808763,0.000012432644,0.000034868284,0.0000047298495,0.000023028802,0.9855286,0.00038762233,0.00011353597,0.010224965,0.00037221672],"about_ca_topic_score_codex":0.0051501696,"about_ca_topic_score_gemma":0.007883916,"teacher_disagreement_score":0.41160348,"about_ca_system_score_codex":0.00029334272,"about_ca_system_score_gemma":0.00016564454,"threshold_uncertainty_score":0.9963024},"labels":[],"label_agreement":null},{"id":"W2996407205","doi":"10.1115/1.4045619","title":"Turbulent Properties of Triple Elliptic Free Jets With Various Nozzle Orientation","year":2019,"lang":"en","type":"article","venue":"Journal of Fluids Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Manitoba","funders":"","keywords":"Nozzle; Turbulence; Physics; Mechanics; Plane (geometry); Reynolds number; Orientation (vector space); Transverse plane; Jet (fluid); Turbulence kinetic energy; Reynolds stress; Optics; Geometry; Materials science; Structural engineering; Mathematics; Engineering; Thermodynamics","score_opus":0.005133646949221848,"score_gpt":0.17039718860061684,"score_spread":0.16526354165139498,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2996407205","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.91572994,0.00089114625,0.08217469,0.00001636252,0.000891607,0.000105697414,0.0000026272282,0.00003839192,0.00014951712],"genre_scores_gemma":[0.99057543,0.00011192836,0.009055268,0.0000047027993,0.00012247096,0.0000018662672,8.738803e-7,0.000043126445,0.000084306805],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99906194,0.0000048965594,0.0004024845,0.00007246344,0.00028474105,0.00017346568],"domain_scores_gemma":[0.9995065,0.000018591101,0.000079910686,0.00019632565,0.0001367388,0.00006196195],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015703263,0.00014414112,0.00026518435,0.00014656885,0.000012782518,0.000021888784,0.00019963918,0.000054844913,0.000018314495],"category_scores_gemma":[0.00003274729,0.00011314754,0.00006625057,0.00014745176,0.000011090174,0.0001670979,0.000018533075,0.00022352862,0.0000041591475],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000018865263,0.000017257042,0.00014316756,0.00024398151,0.0000619923,0.000012528321,0.00023745435,0.74219257,0.2566272,0.00018921173,0.00010514432,0.00015066357],"study_design_scores_gemma":[0.0011072825,0.00031618524,0.00073046173,0.00046711872,0.00007249792,0.00015268257,0.00008770164,0.9543692,0.041912038,0.000027463504,0.00051971414,0.00023765661],"about_ca_topic_score_codex":0.0000022261445,"about_ca_topic_score_gemma":7.8201725e-7,"teacher_disagreement_score":0.21471515,"about_ca_system_score_codex":0.000086614375,"about_ca_system_score_gemma":0.000026738215,"threshold_uncertainty_score":0.46140227},"labels":[],"label_agreement":null},{"id":"W2996498632","doi":"","title":"Development and Testing of an Aeroacoustic Wind Tunnel Test Section","year":2019,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":6,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"Carleton University","funders":"","keywords":"Wind tunnel; Anechoic chamber; Airfoil; Trailing edge; Engineering; Aeroacoustics; Acoustics; Noise (video); Hypersonic wind tunnel; Structural engineering; Airplane; Subsonic and transonic wind tunnel; Marine engineering; Aerodynamics; Aerospace engineering; Transonic; Sound pressure; Physics; Computer science","score_opus":0.009192055393107712,"score_gpt":0.1776570549993911,"score_spread":0.1684649996062834,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2996498632","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9924451,0.000046473746,0.003300208,0.0000037022828,0.00067284575,0.00015071404,0.00006897902,0.00007778146,0.0032341792],"genre_scores_gemma":[0.97350395,0.000007670934,0.026104715,0.0000342492,0.00012866594,0.0000022404527,0.00002244715,0.000050072875,0.00014596565],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99912137,0.0000049352534,0.00024161584,0.00017714275,0.00011909375,0.00033583315],"domain_scores_gemma":[0.9992372,0.00010901497,0.00003532361,0.00020616184,0.00008932067,0.00032299204],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012332782,0.00016464191,0.00017164745,0.00015490518,0.000077548844,0.00003544895,0.000117650925,0.00012767267,0.000029847277],"category_scores_gemma":[0.00013235454,0.00019051728,0.000013091394,0.00019284077,0.000036058635,0.000076381446,0.000017891694,0.00019207054,0.000013883289],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000001439204,0.000021196409,0.005767175,0.00034463586,0.000031604235,0.000028872677,0.0004284786,0.6871734,0.29234186,0.000090945694,0.00025186775,0.013518503],"study_design_scores_gemma":[0.00018633009,0.000051653795,0.06533906,0.00006587672,0.000031980515,0.000027532247,0.00031006182,0.93285614,0.000271194,0.0000536716,0.0005076394,0.00029884186],"about_ca_topic_score_codex":0.0008179171,"about_ca_topic_score_gemma":0.0047154776,"teacher_disagreement_score":0.29207066,"about_ca_system_score_codex":0.00021902869,"about_ca_system_score_gemma":0.00021775093,"threshold_uncertainty_score":0.77690697},"labels":[],"label_agreement":null},{"id":"W2997223967","doi":"10.2514/6.2020-1726","title":"An Aeroacoustic Study of the Nose Landing Gear with Emphasis on Steering Actuators, Torque Link and Tow Hook","year":2020,"lang":"en","type":"article","venue":"AIAA Scitech 2020 Forum","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto","funders":"","keywords":"Freestream; Torque; Landing gear; Noise (video); Engineering; Actuator; Acoustics; Aerospace engineering; Computer science; Reynolds number; Physics; Electrical engineering; Turbulence","score_opus":0.006246365165254486,"score_gpt":0.1973052254246527,"score_spread":0.19105886025939822,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2997223967","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98217994,0.000046987567,0.016418083,0.00036697555,0.00019107925,0.00040146217,0.000028319282,0.00016253504,0.0002045953],"genre_scores_gemma":[0.9987357,0.000027892313,0.00086973404,0.00014748742,0.0001281531,0.000015314105,0.0000033491901,0.000057235324,0.0000150865835],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.998968,0.0000207025,0.00020375304,0.00026817335,0.00026392346,0.00027541374],"domain_scores_gemma":[0.9993999,0.000055523848,0.000047173122,0.0003366296,0.000029962737,0.00013078454],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000100058845,0.00020783141,0.00023056037,0.000039914048,0.00012938067,0.0000649293,0.00029033035,0.00007416254,0.000011816562],"category_scores_gemma":[0.00003596868,0.0001503626,0.000032905384,0.00030556848,0.000039264432,0.000106580796,0.00010446926,0.00029148642,0.00000281687],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00022129169,0.00042210234,0.059862014,0.0005183779,0.00056669326,0.00013886846,0.010495738,0.81423163,0.05619514,0.0008070037,0.0017402008,0.054800913],"study_design_scores_gemma":[0.0012976577,0.0018462221,0.006907573,0.00015910483,0.00013385242,0.000010284707,0.004317101,0.9822577,0.0017349361,0.00007803259,0.0007397487,0.0005177635],"about_ca_topic_score_codex":0.000016749627,"about_ca_topic_score_gemma":0.000083486186,"teacher_disagreement_score":0.16802606,"about_ca_system_score_codex":0.00004145554,"about_ca_system_score_gemma":0.000016138967,"threshold_uncertainty_score":0.6131609},"labels":[],"label_agreement":null},{"id":"W2997337391","doi":"10.22215/etd/2010-08916","title":"Design and construction of a scaled whirl tower facility","year":2010,"lang":"en","type":"dissertation","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Library and Archives Canada","funders":"","keywords":"Tower; Engineering; Humanities; Art; Civil engineering","score_opus":0.005216137391038828,"score_gpt":0.19998690890444137,"score_spread":0.19477077151340255,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2997337391","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8141714,0.00011936432,0.16846946,0.000002286396,0.001532487,0.00024972096,0.000045196903,0.0001167869,0.015293325],"genre_scores_gemma":[0.91166204,0.00027559977,0.0847316,0.0000030881122,0.000050284634,0.000019315872,0.0003678539,0.000032965105,0.0028572753],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99949116,0.000006115532,0.00019717879,0.0001263913,0.00008796573,0.0000911837],"domain_scores_gemma":[0.99968565,0.00003554489,0.00003692815,0.0001374894,0.000070871705,0.000033520653],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00008897822,0.00013914588,0.00019663181,0.000051245795,0.000021610094,0.000014510837,0.000055409484,0.00031189938,0.00023317865],"category_scores_gemma":[0.000020164563,0.0001341006,0.000029732193,0.000043351116,0.000032458054,0.000030262261,0.000005471789,0.0002662022,0.00000294163],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0002832102,0.000140445,0.0005963235,0.0045733503,0.0006696768,0.000011868251,0.0026942343,0.0490073,0.54134053,0.00791294,0.003822106,0.388948],"study_design_scores_gemma":[0.00075138465,0.00008436917,0.00277627,0.00018709376,0.0002453822,0.000017670985,0.00096317113,0.94851696,0.036622602,0.00770765,0.0010155593,0.001111885],"about_ca_topic_score_codex":0.000008513416,"about_ca_topic_score_gemma":0.00008269827,"teacher_disagreement_score":0.89950967,"about_ca_system_score_codex":0.000011550566,"about_ca_system_score_gemma":0.000016555756,"threshold_uncertainty_score":0.5468464},"labels":[],"label_agreement":null},{"id":"W2997389066","doi":"10.1299/jsmeenv.2019.29.j117","title":"Study on acoustic and flow induced noise characteristics of L-shaped duct with a shallow cavity","year":2019,"lang":"en","type":"article","venue":"The Proceedings of the Symposium on Environmental Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Cybernet Systems Corporation (Canada)","funders":"","keywords":"Duct (anatomy); Acoustics; Piping; Aerodynamics; Inflow; Inlet; Geology; Materials science; Physics; Engineering; Mechanics; Mechanical engineering; Geomorphology; Anatomy","score_opus":0.004095103535588234,"score_gpt":0.16251776056264722,"score_spread":0.158422657027059,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2997389066","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99872124,0.000009991433,0.000081951555,0.000031133924,0.00017581266,0.0006049251,0.000029183071,0.00004692907,0.00029881325],"genre_scores_gemma":[0.99965906,0.000026887617,0.00013421339,0.00001145303,0.000039615403,0.000020508074,0.0000014546856,0.00006630583,0.000040476672],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99901867,0.000003615573,0.00024266621,0.00020588051,0.00031503895,0.00021412483],"domain_scores_gemma":[0.9995762,0.000052273892,0.00009291625,0.00022183536,0.000009417292,0.000047362708],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016013709,0.0002634256,0.00028436963,0.00005426399,0.000048032103,0.00001935762,0.00032408544,0.000060277052,0.0000062323206],"category_scores_gemma":[0.000009714781,0.00016932149,0.000050746818,0.00009572688,0.00005061227,0.00006581604,0.00012892608,0.000325114,0.0000040970776],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00004045287,0.00012127801,0.005591071,0.00013037169,0.000082367704,7.233996e-7,0.00078290876,0.16391492,0.82916963,0.000047896476,0.0000014969787,0.00011689622],"study_design_scores_gemma":[0.00094295404,0.000956318,0.199443,0.00031339208,0.0001840796,0.000018058388,0.00083335163,0.7704989,0.02636275,0.00000945708,0.0000095414625,0.00042825053],"about_ca_topic_score_codex":0.0000023186574,"about_ca_topic_score_gemma":2.868144e-7,"teacher_disagreement_score":0.80280685,"about_ca_system_score_codex":0.000084871426,"about_ca_system_score_gemma":0.0000034611824,"threshold_uncertainty_score":0.690473},"labels":[],"label_agreement":null},{"id":"W2998188376","doi":"10.2514/6.2020-2044","title":"From Sparse Pressure Measurements to Prediction of Instantaneous Loads: A Test Case on Delta Wings in Axial and Transverse Gusts","year":2020,"lang":"en","type":"article","venue":"AIAA Scitech 2020 Forum","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Queen's University","funders":"","keywords":"Aerodynamics; Delta wing; Transverse plane; Vortex; Mechanics; Surface pressure; Angle of attack; Swept wing; Towing; Flow (mathematics); Aerodynamic force; Pressure measurement; Amplitude; Linear regression; Geometry; Mathematics; Structural engineering; Physics; Engineering; Optics; Meteorology; Statistics","score_opus":0.016366545588858455,"score_gpt":0.2056929524910975,"score_spread":0.18932640690223906,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2998188376","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9908251,0.00013705043,0.0059470367,0.00054622884,0.0002807824,0.00044044876,0.0012970661,0.00013643056,0.00038982194],"genre_scores_gemma":[0.9985966,0.000031643925,0.0010258448,0.00017189271,0.00009371955,0.000012745483,0.00002477948,0.000035025074,0.000007767388],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99890804,0.000011794616,0.0002900436,0.00028418106,0.00025364634,0.0002522817],"domain_scores_gemma":[0.99955416,0.000052321935,0.000030608735,0.00016840965,0.000035411285,0.0001590666],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00008773268,0.00018111705,0.00021968843,0.00006821635,0.000045057637,0.000025485764,0.00013065548,0.000115935465,0.000025977663],"category_scores_gemma":[0.00011770453,0.0001951967,0.0000347627,0.00029279085,0.000026427113,0.00008963776,0.000048336282,0.00022505668,0.0000066671437],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0005678082,0.0003199543,0.018587427,0.0005607891,0.00031161366,0.003970357,0.0077189165,0.59425503,0.34154013,0.000088562316,0.014824983,0.017254421],"study_design_scores_gemma":[0.0019074703,0.0008030786,0.001008642,0.00032984023,0.00013254695,0.000120718476,0.0008656147,0.9813681,0.0076182024,0.00016544934,0.0052245725,0.0004557364],"about_ca_topic_score_codex":0.00022901027,"about_ca_topic_score_gemma":0.0005336816,"teacher_disagreement_score":0.3871131,"about_ca_system_score_codex":0.000045542456,"about_ca_system_score_gemma":0.000013208216,"threshold_uncertainty_score":0.79598904},"labels":[],"label_agreement":null},{"id":"W2998641890","doi":"10.2514/6.2020-2037","title":"Streamwise Variation of the Unsteady Pressure Field in the Three-Dimensional Wall Jet","year":2020,"lang":"en","type":"article","venue":"AIAA Scitech 2020 Forum","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of New Brunswick","funders":"","keywords":"Jet (fluid); Mechanics; Turbulence; Reynolds number; Nozzle; Physics; Spectral line; Thermodynamics","score_opus":0.006721502658904176,"score_gpt":0.19366155186207407,"score_spread":0.1869400492031699,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2998641890","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9025142,0.00091170263,0.035659827,0.05228995,0.0015384364,0.0014541247,0.00023798709,0.0002776536,0.0051160925],"genre_scores_gemma":[0.9983605,0.000009755262,0.00043191583,0.001076452,0.00006510887,0.00001065728,0.0000073625524,0.000014872804,0.000023340419],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992272,0.000021942378,0.00019865952,0.00013155608,0.00024170896,0.00017891756],"domain_scores_gemma":[0.9995243,0.00012848884,0.00003932278,0.00025330935,0.000026049629,0.000028509156],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001370521,0.00011104324,0.00011862891,0.000016764296,0.000050471772,0.000019982646,0.0003962941,0.00008892691,0.000050571085],"category_scores_gemma":[0.00008022422,0.0000689411,0.000059659516,0.00029661934,0.000021622845,0.000058366844,0.00009247893,0.0002887168,0.0000070789524],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00006171802,0.00008180933,0.014866342,0.00018517226,0.00012506748,0.000014193367,0.001422446,0.91982967,0.012176945,0.010176208,0.03791374,0.003146704],"study_design_scores_gemma":[0.00021046097,0.00007506495,0.0070612514,0.000032347274,0.000029025334,0.0000014973369,0.000061205195,0.9860464,0.0004178979,0.0022709814,0.003684856,0.00010901166],"about_ca_topic_score_codex":0.000060296847,"about_ca_topic_score_gemma":0.00030680402,"teacher_disagreement_score":0.09584631,"about_ca_system_score_codex":0.000010993701,"about_ca_system_score_gemma":0.000017769698,"threshold_uncertainty_score":0.28113365},"labels":[],"label_agreement":null},{"id":"W3004926784","doi":"","title":"Aeroacoustic analysis of the tonal noise of a large-scale radial blower","year":2016,"lang":"en","type":"article","venue":"HAL (Le Centre pour la Communication Scientifique Directe)","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Acoustics; Noise (video); Scale (ratio); Computer science; Physics; Artificial intelligence","score_opus":0.004391141794561976,"score_gpt":0.18935023022889425,"score_spread":0.18495908843433226,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3004926784","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.64500684,0.00012030071,0.345645,0.0004687225,0.00014324923,0.00009145809,0.00017666904,0.000048475817,0.008299305],"genre_scores_gemma":[0.99309146,0.00009674337,0.00542578,0.000012811492,0.000008787009,0.00000656585,0.000017419243,0.00001798364,0.001322465],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99869263,0.00038223527,0.00032087057,0.00017125224,0.0002461039,0.00018692903],"domain_scores_gemma":[0.9977688,0.00062537636,0.00012439795,0.0009087288,0.00051338854,0.000059259677],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0012607279,0.00011446574,0.00022748503,0.00011856781,0.00007659536,0.000017823228,0.00052740757,0.00007234869,0.00019989519],"category_scores_gemma":[0.00036362917,0.00008018292,0.00020442257,0.00065073045,0.00015148046,0.000049381357,0.00015359257,0.000097617965,0.00000408972],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000033980716,0.0013817885,0.03928211,0.0002655291,0.0020739473,0.0000031218608,0.0121115735,0.0741298,0.7364941,0.08401062,0.0025029667,0.047710467],"study_design_scores_gemma":[0.00069825596,4.319006e-7,0.046977703,0.0004096517,0.0005365047,0.0000015958907,0.00008215341,0.8748488,0.07386256,0.0005476409,0.0017654885,0.0002692249],"about_ca_topic_score_codex":0.00004226526,"about_ca_topic_score_gemma":0.00080128334,"teacher_disagreement_score":0.80071896,"about_ca_system_score_codex":0.000040478702,"about_ca_system_score_gemma":0.000036058886,"threshold_uncertainty_score":0.32697648},"labels":[],"label_agreement":null},{"id":"W3004963651","doi":"10.1016/j.ijheatfluidflow.2019.108524","title":"A scale-dependent coherence analysis of turbulent round jets including the effects of shear layer manipulation","year":2020,"lang":"en","type":"article","venue":"International Journal of Heat and Fluid Flow","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto; Queen's University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Turbulence; Boundary layer; Mechanics; Physics; Aspect ratio (aeronautics); Jet (fluid); Optics; Length scale; Large eddy simulation; Scaling; Materials science; Geometry; Mathematics","score_opus":0.016043748464587594,"score_gpt":0.24809396135321887,"score_spread":0.23205021288863129,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3004963651","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.94289684,0.0006925959,0.055418357,0.00039593823,0.00043652154,0.00005836311,0.00001118369,0.000006298595,0.00008387915],"genre_scores_gemma":[0.9984896,0.00035495468,0.00092470594,0.00005999764,0.00015195504,8.8337777e-7,0.0000038905832,0.00000844617,0.0000055623336],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9990794,0.000019263085,0.00038378098,0.00006566152,0.00038183335,0.000070060734],"domain_scores_gemma":[0.99948084,0.00013407614,0.00007875935,0.000059625934,0.000198356,0.000048348036],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015736817,0.00008242072,0.00022268685,0.00011826998,0.000022292952,0.000026061967,0.0001975353,0.000037388414,0.000022070702],"category_scores_gemma":[0.000052447383,0.000055655306,0.000113784554,0.00013289801,0.000028047234,0.000091061534,0.000043911594,0.0001299159,5.051438e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000764108,0.00004172402,0.0070513207,0.00009757797,0.0016493825,0.00003754935,0.0012900985,0.8458728,0.13732763,0.00013124484,0.00018119256,0.0062430757],"study_design_scores_gemma":[0.00033471556,0.00007917519,0.009514285,0.00009271926,0.00031029322,0.000016024396,0.000050772946,0.98355067,0.0058166627,0.000098925666,0.00007258169,0.00006318734],"about_ca_topic_score_codex":0.000010967594,"about_ca_topic_score_gemma":0.000007759709,"teacher_disagreement_score":0.13767786,"about_ca_system_score_codex":0.000040658346,"about_ca_system_score_gemma":0.000011159012,"threshold_uncertainty_score":0.22695576},"labels":[],"label_agreement":null},{"id":"W3010766239","doi":"10.1007/978-981-15-2670-1_8","title":"Turbulent Round Jet Entrainment—A Historical Perspective","year":2020,"lang":"en","type":"book-chapter","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Queen's University","funders":"","keywords":"Entrainment (biomusicology); Perspective (graphical); Jet (fluid); Turbulence; Mechanics; History; Meteorology; Geology; Physics; Computer science; Acoustics; Artificial intelligence","score_opus":0.012821879554943558,"score_gpt":0.19484996759935172,"score_spread":0.18202808804440818,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3010766239","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0000039593615,0.0012825809,0.018837074,0.0006766786,0.001087811,0.00018806003,0.00004101561,0.0004251531,0.97745764],"genre_scores_gemma":[0.02111181,0.001704539,0.0037388578,0.00070487557,0.0021179207,0.000018094246,0.00009845372,0.00040460608,0.9701008],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"not_applicable","domain_scores_codex":[0.99883753,0.0000027146698,0.00026776036,0.00035690496,0.00030450552,0.00023056159],"domain_scores_gemma":[0.99943584,0.00003456713,0.000038804683,0.0002664334,0.000054839544,0.00016953482],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.000036588342,0.00041806023,0.00039627124,0.000057478122,0.00004014381,0.000039530994,0.00021686594,0.00030554732,0.0014871372],"category_scores_gemma":[0.000010394573,0.0004046567,0.00019769624,0.000017231097,0.000027350696,0.000031212116,0.00006309425,0.0006317793,0.00035388238],"study_design_candidate":"not_applicable","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000041248627,0.000010918591,3.6666114e-7,0.000055726345,0.00024772857,0.00016203408,0.00018198893,0.0025296095,0.0000797545,0.8684868,0.12778126,0.0004596769],"study_design_scores_gemma":[0.00016409409,0.000059343853,9.4820496e-7,0.000040351704,0.00012225563,0.000016104725,0.00003970758,0.05442269,0.000009041457,0.04231698,0.9021219,0.0006865775],"about_ca_topic_score_codex":0.000011603296,"about_ca_topic_score_gemma":0.000012834822,"teacher_disagreement_score":0.82616985,"about_ca_system_score_codex":0.0031677277,"about_ca_system_score_gemma":0.000027128683,"threshold_uncertainty_score":0.99984056},"labels":[],"label_agreement":null},{"id":"W3010952110","doi":"10.3390/w12030856","title":"CFD Modeling of Effluent Discharges: A Review of Past Numerical Studies","year":2020,"lang":"en","type":"review","venue":"Water","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":33,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Ottawa","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Computational fluid dynamics; Reynolds-averaged Navier–Stokes equations; Turbulence; Particle image velocimetry; Large eddy simulation; Mechanics; Lagrangian particle tracking; Jet (fluid); Meteorology; Environmental science; Aerospace engineering; Engineering; Physics","score_opus":0.04674027487046274,"score_gpt":0.31127091742253526,"score_spread":0.26453064255207254,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3010952110","genre_codex":"review","genre_gemma":"review","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"review","genre_consensus":"review","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0000026216858,0.99494267,0.0041193897,0.000027767455,0.00030140835,0.00032405587,0.00006751084,0.000039999286,0.00017459046],"genre_scores_gemma":[0.00016480529,0.9987258,0.0007406942,0.00001922859,0.00014347912,0.000049933227,0.000063594474,0.00007130116,0.000021164207],"study_design_codex":"systematic_review","study_design_gemma":"not_applicable","domain_scores_codex":[0.99853414,0.000031812957,0.000861903,0.00019151832,0.00018256628,0.0001980593],"domain_scores_gemma":[0.999493,0.000033990895,0.00008303576,0.0002764186,0.000066346525,0.000047216432],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001475448,0.0003127784,0.0021387015,0.000043331947,0.000013314659,0.0000047039275,0.00022866928,0.00009434043,0.00003277744],"category_scores_gemma":[0.00003097766,0.00018335086,0.00042013568,0.000100653335,0.000025691834,0.000022840944,0.0001461037,0.0002544999,0.000036261674],"study_design_candidate":"systematic_review","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[8.742873e-7,0.000019361623,2.576042e-7,0.8403049,0.0007245526,0.000009695516,0.00016279185,0.00877127,0.0000047350586,0.000065851054,0.0010193369,0.14891638],"study_design_scores_gemma":[0.000043591554,0.000025733387,9.6705755e-9,0.1656482,0.0009738388,0.000004983177,0.000010470166,0.07120202,0.0000030162234,0.000040625586,0.7617547,0.00029281696],"about_ca_topic_score_codex":8.671601e-7,"about_ca_topic_score_gemma":1.2081986e-7,"teacher_disagreement_score":0.76073533,"about_ca_system_score_codex":0.000047244575,"about_ca_system_score_gemma":0.000012966897,"threshold_uncertainty_score":0.7476831},"labels":[],"label_agreement":null},{"id":"W3013214124","doi":"10.15282/jmes.14.1.2020.10.0495","title":"Turbulent kinetic energy and self-sustaining tones: Experimental study of a rectangular impinging jet using high Speed 3D tomographic Particle Image Velocimetry","year":2020,"lang":"en","type":"article","venue":"JOURNAL OF MECHANICAL ENGINEERING AND SCIENCES","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":10,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Alberta","funders":"","keywords":"Particle image velocimetry; Turbulence kinetic energy; Turbulence; Acoustics; Jet (fluid); Aerodynamics; Physics; Aeroacoustics; Kinetic energy; Optics; Mechanics; Sound pressure; Classical mechanics","score_opus":0.011722401148568123,"score_gpt":0.22864327043336485,"score_spread":0.21692086928479673,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3013214124","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.96992856,0.0011090289,0.028676648,0.00003796145,0.00015800077,0.000047064852,7.4373327e-7,0.000038610895,0.0000034076666],"genre_scores_gemma":[0.980877,0.000097761316,0.018904205,0.0000145146505,0.00009029609,5.518301e-7,7.8491794e-8,0.000015437374,1.8792943e-7],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99892455,0.00002084041,0.00039434285,0.00014954273,0.00029341044,0.00021733023],"domain_scores_gemma":[0.9995734,0.000076103745,0.00008726168,0.00005856061,0.00004304562,0.00016162278],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003979349,0.0001454762,0.00029967865,0.00011134501,0.00007135229,0.00006612122,0.00014480851,0.000043102154,0.0000035198748],"category_scores_gemma":[0.000058569472,0.00012343074,0.000042739706,0.00038317742,0.000037779242,0.00014227869,0.00006597295,0.00014686544,3.1542648e-8],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000013962343,0.00013508044,0.00018834643,0.00008360631,0.00011355235,0.0000859974,0.0017103599,0.49160856,0.505008,0.0006251754,0.000002608161,0.00042477282],"study_design_scores_gemma":[0.00042877172,0.00083498016,0.00010527793,0.000069501184,0.000056509194,0.00007262429,0.002155593,0.9813339,0.01476575,0.000032893877,0.0000049961354,0.00013920678],"about_ca_topic_score_codex":0.000013712415,"about_ca_topic_score_gemma":4.4015007e-7,"teacher_disagreement_score":0.49024224,"about_ca_system_score_codex":0.000026064756,"about_ca_system_score_gemma":0.000014826965,"threshold_uncertainty_score":0.50333595},"labels":[],"label_agreement":null},{"id":"W3021373451","doi":"10.1063/5.0004717","title":"Prediction of “buzz-saw” noise propagation under nonuniform axial and radial flows","year":2020,"lang":"en","type":"article","venue":"AIP Advances","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"University of Guelph","keywords":"Shock (circulatory); Noise (video); Leading edge; Physics; RADIUS; Aerodynamics; Mechanics; Acoustics; Axial compressor; Wavefront; Trajectory; Transonic; Flow (mathematics); Computer science; Optics; Gas compressor","score_opus":0.010856305299984053,"score_gpt":0.19876726265494632,"score_spread":0.18791095735496227,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3021373451","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.79143405,0.00092861487,0.20444815,0.00017592587,0.00069825136,0.00022261281,0.000087367815,0.00017728747,0.0018277251],"genre_scores_gemma":[0.99628353,0.0006330075,0.0026961572,0.00003941561,0.00029591142,0.0000069315806,0.000020956137,0.00001627377,0.000007834941],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99951583,0.000005012375,0.00015977796,0.00011131918,0.00010512981,0.00010291866],"domain_scores_gemma":[0.9998035,0.000022319926,0.00002914628,0.00006578741,0.000025996736,0.000053269898],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000038721526,0.00008781515,0.00011060079,0.000022669265,0.00003383174,0.000011092496,0.00005572419,0.000044116783,0.000012380596],"category_scores_gemma":[0.000021824266,0.00008405488,0.000020628931,0.00008729176,0.000032662774,0.00020318652,0.00001682819,0.000086339605,0.0000036149304],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000055238277,0.0000289373,0.002430624,0.00042832986,0.000049998052,0.0000036981285,0.0006344848,0.86301833,0.087709084,0.0031264494,0.00023618106,0.042278655],"study_design_scores_gemma":[0.00032827543,0.000096125754,0.0024804221,0.000020118883,0.000019654932,0.0000017667618,0.00006827473,0.99147725,0.0013687147,0.00088834023,0.0031498899,0.00010114224],"about_ca_topic_score_codex":0.0000020304933,"about_ca_topic_score_gemma":0.000011267196,"teacher_disagreement_score":0.20484944,"about_ca_system_score_codex":0.000019631028,"about_ca_system_score_gemma":0.000009286804,"threshold_uncertainty_score":0.34276587},"labels":[],"label_agreement":null},{"id":"W3021743257","doi":"10.2514/6.2003-3104","title":"Study on Noise Characteristics of an Open Cavity with Cross-Correlation Analysis","year":2003,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Kootenay Association for Science & Technology","funders":"","keywords":"Correlation; Noise (video); Computer science; Acoustics; Physics; Artificial intelligence; Mathematics","score_opus":0.012664083428391123,"score_gpt":0.27273320490420994,"score_spread":0.2600691214758188,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3021743257","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.94596875,8.7746673e-7,0.043888614,7.709522e-7,0.00007684671,0.00020680722,0.000021650314,0.000039275907,0.009796405],"genre_scores_gemma":[0.99777,0.0000011625881,0.001954751,0.0000070027754,0.000010005489,0.000007922808,0.000024746725,0.000017663127,0.0002067565],"study_design_codex":"simulation_or_modeling","study_design_gemma":"observational","domain_scores_codex":[0.9994188,0.000019528383,0.00018943122,0.00014096442,0.00012988948,0.00010140923],"domain_scores_gemma":[0.9994972,0.000024757766,0.000040835308,0.00032855588,0.00006463605,0.000044022156],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00019932208,0.00010205581,0.0002080585,0.00007288244,0.000042033735,0.00007288567,0.0001579918,0.000037101185,0.00006762177],"category_scores_gemma":[0.000021334641,0.000082934355,0.00002129003,0.00031577784,0.000016662649,0.00011809655,0.000019141698,0.000089956295,0.000005021905],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000020877567,0.00039466307,0.31290427,0.000008620796,0.00029720267,0.000010014118,0.00026626542,0.6836043,0.00045315298,0.0014776479,0.000005758615,0.0005572383],"study_design_scores_gemma":[0.0002946598,0.0002344663,0.6377576,0.0000032243204,0.00019279649,5.487381e-7,0.00013036134,0.3610609,0.00015217747,0.00003364644,0.000011559791,0.00012809584],"about_ca_topic_score_codex":0.00004371842,"about_ca_topic_score_gemma":0.00018483291,"teacher_disagreement_score":0.3248533,"about_ca_system_score_codex":0.000029219489,"about_ca_system_score_gemma":0.000009375993,"threshold_uncertainty_score":0.3381965},"labels":[],"label_agreement":null},{"id":"W3024058683","doi":"10.3390/acoustics2020018","title":"Experimental and Analytical Investigation of the Tonal Trailing-Edge Noise Radiated by Low Reynolds Number Aerofoils","year":2020,"lang":"en","type":"article","venue":"Acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":49,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Trailing edge; Airfoil; Noise (video); Acoustics; Reynolds number; Laminar flow; Turbulence; Mechanics; Boundary layer; Bubble; Physics; Flow visualization; Flow (mathematics); Computer science","score_opus":0.009126484597520855,"score_gpt":0.2113302986701792,"score_spread":0.20220381407265833,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3024058683","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9855301,0.00014455938,0.013233654,0.00015048536,0.00021565915,0.00010828151,0.000097353644,0.00006789182,0.00045204908],"genre_scores_gemma":[0.99869895,0.000027462922,0.0008819389,0.0002027938,0.000100689926,0.00000365611,0.000022069742,0.000031050935,0.000031362702],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999242,0.000016026948,0.000246169,0.00014784354,0.00017711385,0.0001708173],"domain_scores_gemma":[0.99959457,0.00006301613,0.000037429185,0.00013952082,0.0000349995,0.00013046345],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000060126087,0.0001429726,0.00016460051,0.000011394722,0.000049279337,0.000022398426,0.00014436824,0.0000921942,0.000039049966],"category_scores_gemma":[0.00007362098,0.00012324014,0.000043329164,0.0001643235,0.00014995181,0.00004834368,0.00005578485,0.00019816901,0.0000058774003],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000108245995,0.000029059784,0.0028837603,0.00012302949,0.000059368456,0.000004788415,0.00076080806,0.061131425,0.92138404,0.00049811264,0.012817581,0.00029721917],"study_design_scores_gemma":[0.00029195932,0.000025824158,0.002361695,0.000022875021,0.000049790066,0.0000033236684,0.00011280955,0.9666947,0.030120824,0.000054729753,0.00010658003,0.0001549047],"about_ca_topic_score_codex":0.0000031337956,"about_ca_topic_score_gemma":3.7116115e-7,"teacher_disagreement_score":0.90556324,"about_ca_system_score_codex":0.000029614033,"about_ca_system_score_gemma":0.000022037264,"threshold_uncertainty_score":0.5025587},"labels":[],"label_agreement":null},{"id":"W3026286464","doi":"","title":"‘Butterfly acoustical skin’ – new method of reducing aero acoustical noise for a quiet propeller","year":2020,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Propeller; Acoustics; Airfoil; Noise (video); Butterfly; Wind tunnel; Scale (ratio); Marine engineering; Engineering; Aerospace engineering; Physics; Computer science; Biology; Ecology; Artificial intelligence","score_opus":0.018409192780607795,"score_gpt":0.24960319846086987,"score_spread":0.23119400568026208,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3026286464","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.008095777,0.00012037255,0.98669684,0.0007170835,0.00093049055,0.0006719333,0.00076374394,0.00018498593,0.0018187977],"genre_scores_gemma":[0.7099333,0.00004275315,0.28750217,0.0007976629,0.0011670645,0.00002376757,0.00006198658,0.00017178307,0.00029951445],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.997528,0.000028017168,0.00066489977,0.0004948673,0.00030599147,0.0009782049],"domain_scores_gemma":[0.99722075,0.0003264173,0.00007422132,0.00043882072,0.00022130845,0.0017184637],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0002351292,0.0004365076,0.0006157057,0.00016443148,0.0001237796,0.00007749142,0.0005204703,0.00037778856,0.00021412288],"category_scores_gemma":[0.0008007976,0.00046845805,0.00018660554,0.0003923137,0.00011213028,0.000088798115,0.00006719977,0.0005326578,0.00004199502],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00003280527,0.000020559663,0.000015934662,0.0005189367,0.00011573108,0.000047632304,0.00046623943,0.7752411,0.11251859,0.00058129936,0.099314526,0.01112665],"study_design_scores_gemma":[0.000582553,0.00014990258,0.00015866362,0.00006966009,0.00029222915,0.00001943848,0.00017728964,0.99278957,0.0007435787,0.00033912418,0.0041416897,0.0005362858],"about_ca_topic_score_codex":0.0014401783,"about_ca_topic_score_gemma":0.00042782823,"teacher_disagreement_score":0.70183754,"about_ca_system_score_codex":0.00028673615,"about_ca_system_score_gemma":0.00083081436,"threshold_uncertainty_score":0.9997767},"labels":[],"label_agreement":null},{"id":"W3028086876","doi":"10.1016/j.jsv.2020.115450","title":"Trailing-edge broadband noise prediction of an airfoil with boundary-layer tripping","year":2020,"lang":"en","type":"article","venue":"Journal of Sound and Vibration","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":45,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"German Academic Exchange Service London; Natural Sciences and Engineering Research Council of Canada; Engineering and Physical Sciences Research Council; Deutsche Forschungsgemeinschaft; Deutscher Akademischer Austauschdienst","keywords":"Airfoil; Boundary layer; Laminar flow; Leading edge; Acoustics; Trailing edge; Noise (video); Aerodynamics; Mechanics; Physics; Computer science","score_opus":0.0149160705134389,"score_gpt":0.21096475512515991,"score_spread":0.196048684611721,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3028086876","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7933081,0.00018065309,0.20607118,0.00005767824,0.00013177727,0.00003629255,0.000010357893,0.000014946553,0.00018901953],"genre_scores_gemma":[0.99676394,0.00007999048,0.0027221788,0.000036729663,0.000374024,3.2043792e-7,0.0000058890487,0.000013356739,0.0000035864255],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994486,0.000010375901,0.00027573944,0.000059678365,0.00013643097,0.00006920069],"domain_scores_gemma":[0.9996807,0.000016034524,0.00010709622,0.00004120017,0.00007552529,0.000079447425],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00011543783,0.00007562631,0.00014273162,0.000044324806,0.000052259413,0.000059148137,0.000043305903,0.000047532456,0.000008379425],"category_scores_gemma":[0.000016087515,0.00006156141,0.000027627253,0.00008180393,0.000027392152,0.00039671938,0.0000044157964,0.00014567036,2.3068556e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00040562113,0.00010619116,0.0040323404,0.0005351221,0.00021058109,0.000024211853,0.005615322,0.56979746,0.39953038,0.00047392977,0.0002545418,0.019014295],"study_design_scores_gemma":[0.0010658704,0.0007754976,0.0058040353,0.00008168812,0.00007556813,0.00005398615,0.00037430716,0.9877701,0.0029952817,0.00045494313,0.0004424139,0.0001063075],"about_ca_topic_score_codex":8.162789e-7,"about_ca_topic_score_gemma":0.0000041415956,"teacher_disagreement_score":0.41797265,"about_ca_system_score_codex":0.000011949301,"about_ca_system_score_gemma":0.00002289261,"threshold_uncertainty_score":0.25104016},"labels":[],"label_agreement":null},{"id":"W3029081388","doi":"10.3397/1/376818","title":"Study on acoustic and flow-induced noise characteristics of L-shaped duct with a shallow cavity","year":2020,"lang":"en","type":"article","venue":"Noise Control Engineering Journal","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Cybernet Systems Corporation (Canada)","funders":"","keywords":"Duct (anatomy); Acoustics; Piping; Geology; Inflow; Inlet; Engineering; Physics; Mechanical engineering; Geomorphology; Oceanography; Anatomy","score_opus":0.010212126011492153,"score_gpt":0.1956220180656359,"score_spread":0.18540989205414374,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3029081388","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7879172,0.00007214057,0.21121131,0.00006770603,0.0002823012,0.00026118167,0.000037108184,0.00011812395,0.000032905013],"genre_scores_gemma":[0.9978839,0.000037712012,0.0014936842,0.000055160952,0.00042257571,0.000012109835,0.0000025317856,0.000089346395,0.0000029732055],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9986335,0.000022287091,0.0004472234,0.00021514282,0.00033570014,0.0003461474],"domain_scores_gemma":[0.9991472,0.000118390504,0.00009826039,0.0001867865,0.00011703713,0.00033235713],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00021017918,0.0003388721,0.00056245615,0.00011027407,0.00006982631,0.00008303076,0.00020038337,0.00008845488,0.000013498546],"category_scores_gemma":[0.00015195283,0.00029725925,0.00007120929,0.00016091806,0.00001901813,0.000099982484,0.000027422475,0.0007487545,0.0000035843987],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0001489618,0.00009958337,0.0018270629,0.0001269501,0.00029473656,0.00032487966,0.000666018,0.86332995,0.1310456,0.000013713731,0.000013848219,0.0021087348],"study_design_scores_gemma":[0.0024261966,0.00068207306,0.0400004,0.00010126144,0.00018931495,0.00007666769,0.00008761788,0.9560402,0.000064938366,0.0000020042028,0.000021261547,0.0003080892],"about_ca_topic_score_codex":0.0000013638943,"about_ca_topic_score_gemma":0.0000016455564,"teacher_disagreement_score":0.20996669,"about_ca_system_score_codex":0.00006293479,"about_ca_system_score_gemma":0.000035392797,"threshold_uncertainty_score":0.99994797},"labels":[],"label_agreement":null},{"id":"W3032954165","doi":"10.1016/j.aej.2020.05.023","title":"Numerical modeling of inclined plane jets in a linearly stratified environment","year":2020,"lang":"en","type":"article","venue":"Alexandria Engineering Journal","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":12,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Ottawa","funders":"Natural Sciences and Engineering Research Council of Canada; China Scholarship Council","keywords":"Mechanics; Stratification (seeds); Turbulence; Stratified flow; Plane (geometry); Stratified flows; Mixing (physics); Homogeneous; Closure (psychology); Computational fluid dynamics; Environmental science; Statistical physics; Physics; Mathematics; Geometry","score_opus":0.012149405956415732,"score_gpt":0.18484940864382696,"score_spread":0.17270000268741123,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3032954165","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.32051128,0.0003143387,0.6784788,0.00015042002,0.00025163745,0.000078049045,0.000009923773,0.0000710407,0.00013456545],"genre_scores_gemma":[0.98147357,0.00027164165,0.017802421,0.000018411763,0.00037797785,0.000002912888,0.0000057433695,0.00004398879,0.0000033611166],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9988662,0.000009815342,0.0005164127,0.00012553869,0.00021580684,0.00026624667],"domain_scores_gemma":[0.99961066,0.00004804997,0.000042084554,0.00010556951,0.000015814934,0.00017779304],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00013686133,0.00017878336,0.00028561192,0.00011540182,0.000023798342,0.000031145868,0.0001821737,0.00009017813,0.000040728537],"category_scores_gemma":[0.00007866402,0.00018442125,0.00006912869,0.00015722973,0.000008864524,0.00009021723,0.00002711699,0.00055317854,0.000006778573],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000013348956,0.000015978469,0.00011645288,0.00005585216,0.000029679855,0.00004713612,0.00023640535,0.98535794,0.013661547,0.00011873291,0.00001947841,0.00032746838],"study_design_scores_gemma":[0.0005311709,0.00006172139,0.00018036435,0.000063948784,0.000010544664,0.000030118832,0.000021613047,0.99844503,0.00031850627,0.00003340848,0.00012648855,0.00017708173],"about_ca_topic_score_codex":0.0000042291185,"about_ca_topic_score_gemma":6.0226404e-7,"teacher_disagreement_score":0.6609623,"about_ca_system_score_codex":0.0000714206,"about_ca_system_score_gemma":0.000027428398,"threshold_uncertainty_score":0.752048},"labels":[],"label_agreement":null},{"id":"W3034589746","doi":"10.2514/6.2020-2539","title":"Aerodynamic and acoustic investigation of the liner-type porous treatment for the trailing-edge of the flat plate.","year":2020,"lang":"en","type":"article","venue":"AIAA AVIATION 2020 FORUM","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Trailing edge; Airfoil; Acoustics; Materials science; Particle image velocimetry; Boundary layer; Directivity; Noise (video); Aerodynamics; Mechanics; Physics; Composite material; Engineering; Turbulence; Computer science","score_opus":0.01320417604530153,"score_gpt":0.20850928263829546,"score_spread":0.19530510659299394,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3034589746","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9664309,0.00045119203,0.027005313,0.0040895925,0.00088294636,0.0008832116,0.00013506129,0.000051746752,0.000070064016],"genre_scores_gemma":[0.99919164,0.00013322469,0.00028024166,0.00017178462,0.000081721555,0.000019335135,0.000021048876,0.000024880841,0.000076092496],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99932945,0.000018518094,0.00027001926,0.00012085436,0.00012926625,0.00013191273],"domain_scores_gemma":[0.99940217,0.00017559169,0.00011464609,0.00021096221,0.00006418105,0.00003242865],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00008413329,0.00012591135,0.00014437437,0.000011544437,0.00011727775,0.000013806398,0.00017795392,0.000069403875,0.0000049853875],"category_scores_gemma":[0.00010811413,0.000069094734,0.000076809425,0.00021008453,0.00007230243,0.000043764485,0.000043893047,0.00009618692,0.0000010756377],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000046938094,0.000019100376,0.007828726,0.0002772023,0.0002082792,3.8194557e-7,0.002766037,0.7665863,0.2129136,0.0023746775,0.0015831557,0.0053956066],"study_design_scores_gemma":[0.000389733,0.000106525535,0.0104247695,0.000031207757,0.00013555319,0.0000013902054,0.00020806176,0.9834249,0.004228052,0.0006850066,0.0002771507,0.00008765277],"about_ca_topic_score_codex":0.000012083028,"about_ca_topic_score_gemma":0.00012775644,"teacher_disagreement_score":0.21683861,"about_ca_system_score_codex":0.000035913057,"about_ca_system_score_gemma":0.000037099402,"threshold_uncertainty_score":0.28176016},"labels":[],"label_agreement":null},{"id":"W3034633156","doi":"10.2514/6.2020-2514","title":"Large-Eddy Simulation of a Single Airfoil Tip-Leakage Flow","year":2020,"lang":"en","type":"article","venue":"AIAA AVIATION 2020 FORUM","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":6,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université du Québec; Université de Sherbrooke","funders":"","keywords":"Airfoil; Trailing edge; Leading edge; Mechanics; Turbulence; Aerodynamics; Large eddy simulation; Acoustics; Camber (aerodynamics); Leakage (economics); Vortex; Mach number; Reynolds number; Chord (peer-to-peer); Tip clearance; Physics; Materials science; Structural engineering; Engineering; Computer science","score_opus":0.008934182377998066,"score_gpt":0.2083524202016048,"score_spread":0.19941823782360674,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3034633156","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.08057125,0.00011034501,0.91546464,0.00077364186,0.0004634844,0.00018624701,0.00012767976,0.0002944683,0.0020082558],"genre_scores_gemma":[0.9967533,0.000016364345,0.0025379825,0.00029966977,0.00015757297,0.0000055426985,0.00012215532,0.000039886876,0.00006756547],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99914443,0.000012558431,0.00028765464,0.00015157317,0.0001900839,0.00021367555],"domain_scores_gemma":[0.9995972,0.000053644973,0.00006169716,0.0001462653,0.00006588714,0.000075300646],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00007086618,0.00012669958,0.00016329408,0.00003213325,0.000049369093,0.000020933181,0.0001108682,0.00008885148,0.00014040234],"category_scores_gemma":[0.00009571945,0.00014117219,0.00006870521,0.0002422116,0.000011540518,0.00013721701,0.000041957617,0.00011857456,0.00008723605],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00000728568,0.000029184977,0.0004273595,0.00006569975,0.00002290847,0.000002209486,0.0004544236,0.9829657,0.010996054,0.00048758896,0.0026397228,0.0019018815],"study_design_scores_gemma":[0.0003139552,0.00006149849,0.000352605,0.000014502976,0.000018517087,3.546343e-7,0.00014174246,0.9922859,0.001027442,0.00038230166,0.005258594,0.00014260027],"about_ca_topic_score_codex":0.0000013053093,"about_ca_topic_score_gemma":0.000010103334,"teacher_disagreement_score":0.916182,"about_ca_system_score_codex":0.00004272601,"about_ca_system_score_gemma":0.000010641629,"threshold_uncertainty_score":0.5756835},"labels":[],"label_agreement":null},{"id":"W3034671848","doi":"10.2514/6.2020-2607","title":"Large Eddy Simulation of an Outflow butterfly valve","year":2020,"lang":"en","type":"article","venue":"AIAA AVIATION 2020 FORUM","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université du Québec; Université de Sherbrooke","funders":"","keywords":"Butterfly valve; Aerodynamics; Acoustics; Noise (video); Schlieren; Transonic; Large eddy simulation; Wind tunnel; Aerospace engineering; Computer science; Mechanics; Physics; Engineering; Mechanical engineering; Turbulence","score_opus":0.007609323749449287,"score_gpt":0.22621268367967617,"score_spread":0.2186033599302269,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3034671848","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.2929181,0.000049205853,0.70506316,0.00050399,0.00040850675,0.00016669337,0.0001240131,0.00022249899,0.0005438611],"genre_scores_gemma":[0.9973319,0.000010660046,0.0018556667,0.00038644348,0.00018682721,0.0000048381676,0.00016442884,0.000033976088,0.000025229485],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99923486,0.000013363516,0.00025095983,0.00014371469,0.0001687973,0.00018832395],"domain_scores_gemma":[0.99961764,0.000033254444,0.00005471977,0.0001498719,0.000060506543,0.000084024],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00007433482,0.000112651294,0.00014153191,0.000027208069,0.000043553395,0.000020324173,0.00011606604,0.00007830582,0.0000905953],"category_scores_gemma":[0.000051066418,0.00012459149,0.00007263334,0.00016291592,0.000008403079,0.0001926941,0.000030857256,0.0001129922,0.000055124907],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000062080094,0.000021228643,0.0010509158,0.000041311112,0.000027342008,0.0000013815286,0.0005287176,0.9914888,0.0033938885,0.0007805579,0.0009302113,0.0017294314],"study_design_scores_gemma":[0.0002767579,0.00006549405,0.0015266644,0.0000073122483,0.000020688327,2.5901812e-7,0.000159905,0.9947579,0.00052929326,0.00060761045,0.0019175797,0.00013053016],"about_ca_topic_score_codex":0.0000020037942,"about_ca_topic_score_gemma":0.00000982303,"teacher_disagreement_score":0.70441383,"about_ca_system_score_codex":0.000026257838,"about_ca_system_score_gemma":0.0000091250195,"threshold_uncertainty_score":0.50806934},"labels":[],"label_agreement":null},{"id":"W3035448492","doi":"10.2514/6.2020-2541","title":"Numerical study of optimized airfoil trailing-edge serrations for broadband noise reduction","year":2020,"lang":"en","type":"article","venue":"AIAA AVIATION 2020 FORUM","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Airfoil; Reynolds-averaged Navier–Stokes equations; Trailing edge; Drag; Aerodynamics; Noise reduction; Shape optimization; Noise (video); Reduction (mathematics); Leading edge; Computational fluid dynamics; Acoustics; Mathematics; Mechanics; Physics; Structural engineering; Computer science; Engineering; Finite element method; Geometry","score_opus":0.013317677570740094,"score_gpt":0.23518529024317722,"score_spread":0.22186761267243713,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3035448492","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.2624705,0.00006465882,0.73309135,0.0015625841,0.0009020744,0.0010226368,0.000075777934,0.0002729502,0.00053744967],"genre_scores_gemma":[0.99455243,0.000014786982,0.0048851543,0.000057448906,0.0002023093,0.00008776999,0.000090112146,0.00003759932,0.00007235735],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99910426,0.000016708062,0.0003680513,0.00019293465,0.00014705023,0.00017098636],"domain_scores_gemma":[0.9995708,0.00004045449,0.000073142146,0.00013897462,0.00009660218,0.00008004137],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000076529854,0.00013191822,0.00021521444,0.000035309295,0.00009464072,0.000023955843,0.00010691278,0.00007077815,0.000036068348],"category_scores_gemma":[0.00007747717,0.00014322744,0.00007633177,0.00025032344,0.000012856106,0.000125994,0.000016299044,0.0001201819,0.000008804697],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00006069694,0.0001427641,0.00022184123,0.000066301014,0.00007724444,6.434156e-7,0.0019109932,0.9783945,0.010485665,0.00035222268,0.006566388,0.001720745],"study_design_scores_gemma":[0.0013373109,0.00029513822,0.00038209403,0.0000072742487,0.00006401666,0.000001164292,0.0011354226,0.99488777,0.00083699235,0.00014837786,0.0007460413,0.00015841068],"about_ca_topic_score_codex":0.0000068142012,"about_ca_topic_score_gemma":0.000004957565,"teacher_disagreement_score":0.73208195,"about_ca_system_score_codex":0.000028403461,"about_ca_system_score_gemma":0.000019666524,"threshold_uncertainty_score":0.58406454},"labels":[],"label_agreement":null},{"id":"W3035727109","doi":"10.2514/6.2020-2521","title":"Tip flow evolution in a turbofan rotor for broadband noise diagnostic","year":2020,"lang":"en","type":"article","venue":"AIAA AVIATION 2020 FORUM","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":9,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université du Québec; Université de Sherbrooke","funders":"","keywords":"Turbofan; Mechanics; Vortex; Leading edge; Boundary layer; Physics; Tip clearance; Acoustics; Duct (anatomy); Mean flow; Shock (circulatory); Leakage (economics); Materials science; Aerospace engineering; Engineering; Turbulence","score_opus":0.005439062950439926,"score_gpt":0.19690292472036303,"score_spread":0.1914638617699231,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3035727109","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.12874632,0.0003950744,0.86460924,0.0029367274,0.0010263568,0.0012680306,0.0002288125,0.00034389872,0.00044552475],"genre_scores_gemma":[0.99584514,0.000043035743,0.0031476016,0.00029026714,0.0002790857,0.00017299829,0.00013247132,0.000041856954,0.000047569043],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991506,0.000010355434,0.00025319675,0.00019311131,0.00012277113,0.0002699839],"domain_scores_gemma":[0.99956286,0.00015615398,0.00003412274,0.000116173345,0.000039297276,0.00009141967],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000073473006,0.00014021412,0.00015475099,0.000042996853,0.000051415213,0.000033526198,0.00011148264,0.00009526892,0.000036936355],"category_scores_gemma":[0.00039876613,0.00015639764,0.00006111304,0.0002235095,0.000010906067,0.0001319891,0.00002605337,0.00013561676,0.000058808317],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00006487991,0.00006725134,0.021021372,0.00033841128,0.000053023956,0.000013572379,0.00070873275,0.92360985,0.008470315,0.004040604,0.030947607,0.010664361],"study_design_scores_gemma":[0.00063813664,0.00006608822,0.011215412,0.000027223716,0.000016353268,7.799491e-7,0.000046651563,0.9813757,0.00013738032,0.0012648932,0.005016768,0.00019462965],"about_ca_topic_score_codex":0.000009107617,"about_ca_topic_score_gemma":0.000072792776,"teacher_disagreement_score":0.8670988,"about_ca_system_score_codex":0.00012871022,"about_ca_system_score_gemma":0.000019909687,"threshold_uncertainty_score":0.63777107},"labels":[],"label_agreement":null},{"id":"W3036489970","doi":"10.1177/0954406220934831","title":"Large-scale motion of submerged offset jets issuing from sharp-edged rectangular nozzles","year":2020,"lang":"en","type":"article","venue":"Proceedings of the Institution of Mechanical Engineers Part C Journal of Mechanical Engineering Science","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Memorial University of Newfoundland","funders":"","keywords":"Nozzle; Turbulence; Vortex; Mechanics; Reynolds number; Jet (fluid); Physics; Turbulence kinetic energy; Entrainment (biomusicology); Offset (computer science); Doppler effect; Reynolds stress; Acoustics; Thermodynamics","score_opus":0.010275120403341559,"score_gpt":0.2036505911515179,"score_spread":0.19337547074817635,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3036489970","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6455582,0.00023221425,0.3519182,0.00025691433,0.001646287,0.0001890591,0.00006323929,0.00007749334,0.000058449972],"genre_scores_gemma":[0.98084754,0.00011719341,0.018761288,0.000021380496,0.00021370027,0.0000031340398,0.0000017548867,0.00003220402,0.0000018027688],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9968965,0.000008837082,0.0012629732,0.00027658325,0.0011454554,0.00040964436],"domain_scores_gemma":[0.9982303,0.000080150116,0.0005085875,0.00018534873,0.00068737793,0.00030827304],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0014549061,0.0002844562,0.00068265566,0.00021062586,0.000080947764,0.000027556896,0.0012504626,0.00019355494,0.000020660958],"category_scores_gemma":[0.0023457804,0.00023572655,0.00031150872,0.001179925,0.00015024727,0.00048983813,0.00021328231,0.0007273347,0.00000118493],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000030484327,0.00004874503,0.000008747587,0.00018576154,0.00004967976,0.0000010926356,0.00021230667,0.2869088,0.69898546,0.013277952,0.000059628423,0.00023133632],"study_design_scores_gemma":[0.0004089603,0.000104361505,0.000044966968,0.00041868864,0.00007131654,0.000008997218,0.00012685308,0.5802907,0.41784737,0.00038521466,0.00013807845,0.00015451976],"about_ca_topic_score_codex":0.0000027489425,"about_ca_topic_score_gemma":5.92958e-7,"teacher_disagreement_score":0.3352894,"about_ca_system_score_codex":0.00013182341,"about_ca_system_score_gemma":0.000094828676,"threshold_uncertainty_score":0.96126497},"labels":[],"label_agreement":null},{"id":"W3039024119","doi":"10.1016/j.jsv.2020.115561","title":"On the role of turbulence distortion on leading-edge noise reduction by means of porosity","year":2020,"lang":"en","type":"article","venue":"Journal of Sound and Vibration","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":87,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Horizon 2020 Framework Programme; Gauss Centre for Supercomputing; European Commission","keywords":"Airfoil; Turbulence; Turbulence kinetic energy; Porosity; Mechanics; Materials science; Noise (video); Leading edge; Physics; Acoustics; Composite material","score_opus":0.007767891509106385,"score_gpt":0.19464472797310833,"score_spread":0.18687683646400194,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3039024119","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.96125835,0.0001399213,0.037956115,0.00018335994,0.0001409836,0.000036405516,0.000009872265,0.000005162102,0.00026985095],"genre_scores_gemma":[0.99965423,0.00009324028,0.00011486668,0.000021060967,0.000103590224,2.3241546e-7,0.0000026392113,0.000005629724,0.000004518624],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995782,0.000011891364,0.00020374989,0.00004121654,0.00012468603,0.000040303148],"domain_scores_gemma":[0.99971384,0.000029935516,0.00014365096,0.000041391104,0.000044311124,0.000026897575],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00010605561,0.000051037412,0.000094446565,0.000020763751,0.000034570505,0.000011968844,0.00004419419,0.00003184519,0.0000059968493],"category_scores_gemma":[0.000039440663,0.00003704054,0.00003208561,0.000051864747,0.000024230301,0.000098531586,0.0000042262345,0.0001182281,5.052527e-7],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00009777657,0.000074675765,0.000273752,0.00006927948,0.00003315216,4.5661508e-7,0.001457277,0.17253798,0.81657267,0.0046927137,0.001026628,0.0031636527],"study_design_scores_gemma":[0.00048813765,0.0014052846,0.0022171622,0.0002145189,0.00008872484,0.000013190503,0.00089525565,0.7595904,0.21884124,0.015755296,0.00029254818,0.00019823978],"about_ca_topic_score_codex":0.000001029005,"about_ca_topic_score_gemma":5.384078e-7,"teacher_disagreement_score":0.5977314,"about_ca_system_score_codex":0.00002128203,"about_ca_system_score_gemma":0.0000050555605,"threshold_uncertainty_score":0.15104693},"labels":[],"label_agreement":null},{"id":"W3046345056","doi":"","title":"Experimental investigation of nozzle geometry effect on the characteristics and structure of submerged twin jets","year":2020,"lang":"en","type":"dissertation","venue":"Mspace (University of Manitoba)","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Nozzle; Geometry; Mechanics; Mechanical engineering; Engineering; Physics; Mathematics","score_opus":0.006661581117594319,"score_gpt":0.1796124833937094,"score_spread":0.17295090227611506,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3046345056","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9988825,0.00009043127,0.00009179012,0.000027494394,0.00031000972,0.00019113562,0.00016174291,0.000020859392,0.00022409162],"genre_scores_gemma":[0.9993988,0.000045373396,0.00018929903,0.0000041482454,0.000028590031,1.6752936e-7,0.000282293,0.00002275992,0.000028523484],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.9994411,0.00003119467,0.00010794951,0.00013475912,0.0001960685,0.00008895996],"domain_scores_gemma":[0.999508,0.00006657575,0.00017964927,0.00015589304,0.000049643204,0.000040237166],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000052945594,0.00016509881,0.0003148235,0.00010204382,0.000054516135,0.0000056857903,0.00017529346,0.00016878304,0.0000099722965],"category_scores_gemma":[0.000028000528,0.00017191781,0.00006329899,0.00014083947,0.00007334279,0.0000388355,0.000032879907,0.00023720461,0.0000010825052],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00014752388,0.000018700384,0.008547139,0.0016063033,0.00020875828,0.000008831717,0.0017932776,0.0007546675,0.98527676,0.0007020599,0.00046833692,0.00046762178],"study_design_scores_gemma":[0.0008340152,0.00064144126,0.5867857,0.00066226773,0.0003809391,0.0000017885546,0.01772123,0.044483904,0.3476959,0.00011141229,0.00011471037,0.0005667072],"about_ca_topic_score_codex":0.000066440836,"about_ca_topic_score_gemma":0.0016197265,"teacher_disagreement_score":0.6375809,"about_ca_system_score_codex":0.00004027684,"about_ca_system_score_gemma":0.000013790883,"threshold_uncertainty_score":0.7010605},"labels":[],"label_agreement":null},{"id":"W3047909221","doi":"10.1016/j.jsv.2020.115620","title":"On the noise generated by a controlled-diffusion aerofoil at <mml:math xmlns:mml=\"http://www.w3.org/1998/Math/MathML\" altimg=\"si21.svg\"><mml:mrow><mml:mi>R</mml:mi><mml:msub><mml:mi>e</mml:mi><mml:mi>c</mml:mi></mml:msub><mml:mo linebreak=\"goodbreak\">=</mml:mo><mml:mn>1.5</mml:mn><mml:mo linebreak=\"goodbreak\">×</mml:mo><mml:msup><mml:mn>10</mml:mn><mml:mn>5</mml:mn></mml:msup></mml:mrow></mml:math>","year":2020,"lang":"lv","type":"article","venue":"Journal of Sound and Vibration","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":28,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Airfoil; Chord (peer-to-peer); Wake; Trailing edge; Noise (video); Reynolds number; Mach number; Leading edge; Physics; Acoustics; Turbulence; Mechanics; Computer science; Artificial intelligence; Database","score_opus":0.013760666136011146,"score_gpt":0.22026476697799413,"score_spread":0.20650410084198298,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3047909221","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7531894,0.005204323,0.008824461,0.003476778,0.0072698053,0.00023064697,0.0021881838,0.00073309004,0.21888334],"genre_scores_gemma":[0.9716116,0.005474609,0.003548468,0.003875047,0.0077665336,0.0013475838,0.0037960927,0.0020227127,0.00055731274],"study_design_codex":"not_applicable","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9800651,0.0012428,0.005237937,0.003423061,0.005425478,0.004605633],"domain_scores_gemma":[0.983594,0.0037240116,0.0055845305,0.003305516,0.0007802657,0.003011692],"candidate_categories":["metaepi_narrow","sts","scholarly_communication","research_integrity","insufficient_payload"],"consensus_categories":["metaepi_narrow","research_integrity","insufficient_payload"],"category_scores_codex":[0.0042597777,0.002396581,0.0011531459,0.0013096029,0.0046479367,0.0045450684,0.004165029,0.0052813124,0.21556015],"category_scores_gemma":[0.0038095608,0.004080026,0.004128277,0.002725446,0.0025610102,0.0033286163,0.0032528108,0.0049976297,0.002461302],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.006479858,0.0010758346,0.00002300808,0.0022855082,0.005085829,0.0027590967,0.0040910235,0.024003483,0.021583233,0.33601987,0.59271735,0.0038759066],"study_design_scores_gemma":[0.0078049814,0.004855708,0.000057048623,0.0024452936,0.0043938835,0.004143003,0.0031101678,0.18332234,0.7761429,0.0015306984,0.008364566,0.0038293933],"about_ca_topic_score_codex":0.0017413632,"about_ca_topic_score_gemma":0.002056424,"teacher_disagreement_score":0.7545597,"about_ca_system_score_codex":0.00009151974,"about_ca_system_score_gemma":0.0026553771,"threshold_uncertainty_score":0.99887717},"labels":[],"label_agreement":null},{"id":"W3086269337","doi":"10.3390/acoustics2030036","title":"Tonal-Noise Assessment of Quadrotor-Type UAV Using Source-Mode Expansions","year":2020,"lang":"en","type":"article","venue":"Acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":52,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Agence Nationale de la Recherche","keywords":"Lift (data mining); Acoustics; Aerodynamics; Noise (video); Thrust; Aeroacoustics; Parametric statistics; Ambient noise level; Computer science; Simulation; Engineering; Aerospace engineering; Physics; Sound pressure; Sound (geography); Mathematics","score_opus":0.02407401791216396,"score_gpt":0.2894959598908724,"score_spread":0.26542194197870844,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3086269337","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.4901399,0.000052203766,0.5085376,0.00002573332,0.00036836986,0.00011399314,0.00004405388,0.00012252017,0.0005956455],"genre_scores_gemma":[0.9527521,0.00007739387,0.046706792,0.00010155027,0.00024369934,0.0000034742588,0.00001844918,0.000065725566,0.000030828523],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99894613,0.000014200322,0.00033911786,0.00017511094,0.000263388,0.00026205753],"domain_scores_gemma":[0.99932516,0.00009044855,0.000058013855,0.00025648533,0.00011460284,0.0001553139],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00007024293,0.00018801508,0.0002660669,0.000043461612,0.00006666499,0.000021684893,0.00021291,0.000111788744,0.0000707695],"category_scores_gemma":[0.00009047123,0.00019939664,0.00006855705,0.00023621637,0.000047637255,0.000053721862,0.000089857655,0.00026669263,0.000008665272],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000002541341,0.000020121313,0.00046615655,0.00009643613,0.000033387783,0.0000063952198,0.00013723763,0.7607329,0.2374037,0.0002295726,0.00057238183,0.00029915612],"study_design_scores_gemma":[0.0001635136,0.00005335969,0.00056768,0.000035659774,0.00008886038,0.0000028728723,0.0001665624,0.9974743,0.00061222294,0.000105626495,0.00051323255,0.00021609236],"about_ca_topic_score_codex":0.000014070424,"about_ca_topic_score_gemma":0.0000017883342,"teacher_disagreement_score":0.46261218,"about_ca_system_score_codex":0.0000731259,"about_ca_system_score_gemma":0.00007521297,"threshold_uncertainty_score":0.8131159},"labels":[],"label_agreement":null},{"id":"W3087813909","doi":"10.3390/acoustics2030037","title":"Identification of Noise Sources in a Realistic Turbofan Rotor Using Large Eddy Simulation","year":2020,"lang":"en","type":"article","venue":"Acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":30,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Turbofan; Noise (video); Trailing edge; Aerodynamics; Rotor (electric); Acoustics; Leading edge; Aeroacoustics; Large eddy simulation; Mechanical fan; Helicopter rotor; Engineering; Physics; Aerospace engineering; Structural engineering; Vibration; Mechanics; Computer science; Sound pressure; Mechanical engineering; Turbulence","score_opus":0.016581045617699422,"score_gpt":0.25222955635701605,"score_spread":0.23564851073931664,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3087813909","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.52072024,0.000038337563,0.47885448,0.000007799554,0.00012568748,0.00011044978,0.00006567063,0.00005037336,0.000026945667],"genre_scores_gemma":[0.9971849,0.000021050419,0.0025478962,0.000025748564,0.0001505613,0.000003686833,0.000025781197,0.000034021294,0.00000639948],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99914616,0.000013212722,0.00038883422,0.00013087745,0.00015123088,0.00016965282],"domain_scores_gemma":[0.9995725,0.00008249098,0.00007620103,0.00015210004,0.00006339484,0.000053294603],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012179179,0.00011026008,0.00016093513,0.000060459057,0.00003021109,0.000021452986,0.00011834626,0.00008244786,0.00001112999],"category_scores_gemma":[0.00024903702,0.00012551753,0.0000305964,0.00023360738,0.000019651116,0.00006464215,0.00003123551,0.0001322581,0.0000047776903],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000004751401,0.000017148961,0.0006290651,0.00014390524,0.000007895352,0.0000034556883,0.0004071768,0.89623857,0.10226099,0.00008477964,0.000023134187,0.0001791044],"study_design_scores_gemma":[0.00018918149,0.000012354212,0.0022523056,0.000026911275,0.000038365673,3.8380668e-7,0.0001350435,0.9966231,0.0004245476,0.00013544374,0.000038981307,0.00012339988],"about_ca_topic_score_codex":0.000010407768,"about_ca_topic_score_gemma":0.0000064959227,"teacher_disagreement_score":0.4764646,"about_ca_system_score_codex":0.00005114586,"about_ca_system_score_gemma":0.000014743442,"threshold_uncertainty_score":0.51184565},"labels":[],"label_agreement":null},{"id":"W3088642828","doi":"10.1088/1742-6596/1618/4/042010","title":"Computational aeroacoustic prediction of trailing edge noise for small wind turbines","year":2020,"lang":"en","type":"article","venue":"Journal of Physics Conference Series","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Waterloo","funders":"","keywords":"Aeroacoustics; Acoustics; Trailing edge; Turbulence; Noise (video); Boundary layer; Computational fluid dynamics; Turbine; Inlet; Computational aeroacoustics; Laminar flow; Aerospace engineering; Engineering; Mechanics; Structural engineering; Computer science; Sound pressure; Mechanical engineering; Physics","score_opus":0.030663578719583875,"score_gpt":0.21373058933808403,"score_spread":0.18306701061850017,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3088642828","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.25117138,0.00005368572,0.747947,0.000101906946,0.00037042526,0.0000777277,0.00013393733,0.00002076581,0.00012319055],"genre_scores_gemma":[0.98246163,0.000040962583,0.01685986,0.000018836821,0.00057333056,0.0000012687016,0.000016802118,0.000019109691,0.000008176928],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992893,0.0000075581606,0.0003796237,0.00007006553,0.0001449188,0.000108536085],"domain_scores_gemma":[0.999202,0.00007705631,0.00016317068,0.000049553488,0.00044136765,0.00006686685],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00007383083,0.00011483753,0.0002505472,0.000026401516,0.00003619975,0.000030480121,0.00013049037,0.000043653155,0.0000074563045],"category_scores_gemma":[0.000055932796,0.000109897395,0.00009697466,0.00008676822,0.000053810665,0.00019747199,0.0000136462,0.000155719,5.228668e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000044471537,0.000022566683,0.0000877398,0.00028084457,0.000077379416,0.0000016371749,0.0008443578,0.93981445,0.04674188,0.0048011173,0.00013935473,0.0071441787],"study_design_scores_gemma":[0.000505924,0.00030588504,0.0007016225,0.000110882276,0.00009714667,0.000008944135,0.00039925508,0.97508186,0.0124044595,0.0101202475,0.00013890973,0.00012484509],"about_ca_topic_score_codex":3.4937167e-7,"about_ca_topic_score_gemma":7.185521e-7,"teacher_disagreement_score":0.7312903,"about_ca_system_score_codex":0.000013364018,"about_ca_system_score_gemma":0.000080623555,"threshold_uncertainty_score":0.44814858},"labels":[],"label_agreement":null},{"id":"W3089329526","doi":"10.33737/gpps20-tc-94","title":"Aeroacoustic Numerical Investigation of a Scaled Compressor Cascade","year":2020,"lang":"en","type":"article","venue":"Proceedings","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"Université de Sherbrooke","funders":"Leibniz-Gemeinschaft; Compute Canada","keywords":"Turbomachinery; Reynolds-averaged Navier–Stokes equations; Turbofan; Aerodynamics; Gas compressor; Engineering; Computational fluid dynamics; Stator; Turbocharger; Aeroacoustics; Axial compressor; Noise (video); Rotor (electric); Aerospace engineering; Mechanical engineering; Acoustics; Computer science; Sound pressure; Physics","score_opus":0.01374611722778208,"score_gpt":0.19321186916337085,"score_spread":0.17946575193558878,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3089329526","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9660702,0.0001211197,0.029538054,0.0002934811,0.00012039682,0.00015430605,0.000012911382,0.0003126034,0.003376938],"genre_scores_gemma":[0.9944837,0.000020084359,0.0051799,0.00013053733,0.00013171708,0.000010603714,0.0000040594205,0.000029474773,0.00000993412],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999354,0.0000015328499,0.00020708246,0.00013185544,0.00015260762,0.00015290093],"domain_scores_gemma":[0.99970937,0.00001925912,0.000038912458,0.000038202645,0.00007054199,0.00012372911],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000045976245,0.000110166235,0.00017317919,0.000027426584,0.000025367008,0.0000197244,0.0001362045,0.000063420805,0.000020545316],"category_scores_gemma":[0.00007284835,0.00011230625,0.000035927224,0.00022065773,0.000043670836,0.00008042704,0.0000352617,0.00016105444,0.000013783983],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000032766304,0.000026346012,0.0065074065,0.0022351318,0.00009673871,0.0000054141965,0.0045622196,0.06880394,0.9001643,0.0029864751,0.012558859,0.0020203975],"study_design_scores_gemma":[0.00017957378,0.000034447196,0.0011153575,0.00003151584,0.00002797117,0.00000300291,0.00007758383,0.9868466,0.010881768,0.00035567142,0.0003124478,0.00013401221],"about_ca_topic_score_codex":0.0000021219662,"about_ca_topic_score_gemma":1.12232506e-7,"teacher_disagreement_score":0.9180427,"about_ca_system_score_codex":0.00002041408,"about_ca_system_score_gemma":0.000007183444,"threshold_uncertainty_score":0.45797157},"labels":[],"label_agreement":null},{"id":"W3089658586","doi":"10.1063/5.0021121","title":"On the use of two-point velocity correlation in wall-pressure models for turbulent flow past a trailing edge under adverse pressure gradient","year":2020,"lang":"en","type":"article","venue":"Physics of Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":33,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Physics; Adverse pressure gradient; Pressure gradient; Turbulence; Airfoil; Trailing edge; Mechanics; Velocity gradient; Flow separation; Classical mechanics","score_opus":0.03960649742724289,"score_gpt":0.22757015707942724,"score_spread":0.18796365965218434,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3089658586","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.20717442,0.00010873154,0.79152083,0.00024326783,0.00015867653,0.0005022546,0.00016563451,0.0000415304,0.00008467012],"genre_scores_gemma":[0.9958711,0.00002499102,0.0038339016,0.00008137752,0.000090842164,0.000027198656,0.000028840794,0.00003376368,0.000007964778],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999168,0.000020667496,0.00028773164,0.00017052598,0.00018355115,0.00016954998],"domain_scores_gemma":[0.9993812,0.00021328202,0.000053935444,0.0002239777,0.000083305764,0.000044295117],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00010244844,0.00015889987,0.00023306445,0.000022046832,0.00003233927,0.000009797579,0.000161292,0.000059374368,0.0000048102693],"category_scores_gemma":[0.000031674295,0.00013574108,0.0001176855,0.00012867025,0.000037601527,0.0001371679,0.00003443849,0.00020061049,7.996736e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000034571294,0.00006573435,0.000014256316,0.00019172432,0.00008426891,4.0613511e-7,0.0012588133,0.9665217,0.004363086,0.026440974,0.00035277568,0.0006717162],"study_design_scores_gemma":[0.0003937554,0.00004562591,0.000059213024,0.000081615006,0.00008343815,1.4127794e-7,0.000041267333,0.9880251,0.00082016294,0.010220334,0.00010092582,0.00012841164],"about_ca_topic_score_codex":0.000013298353,"about_ca_topic_score_gemma":0.0000039927418,"teacher_disagreement_score":0.7886967,"about_ca_system_score_codex":0.000020418707,"about_ca_system_score_gemma":0.000014245491,"threshold_uncertainty_score":0.55353606},"labels":[],"label_agreement":null},{"id":"W3090974653","doi":"10.1115/1.4048684","title":"Particle Image Velocimetry Measurements of Turbulent Jets Issuing From Twin Elliptic Nozzles With Various Orientations","year":2020,"lang":"en","type":"article","venue":"Journal of Fluids Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Manitoba","funders":"","keywords":"Nozzle; Particle image velocimetry; Turbulence; Jet (fluid); Mechanics; Physics; Reynolds number; Reynolds stress; Plane (geometry); Optics; Materials science; Geometry; Mathematics; Thermodynamics","score_opus":0.014456212603985694,"score_gpt":0.20943375243613138,"score_spread":0.1949775398321457,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3090974653","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.63765454,0.0007454799,0.36118674,0.00006114989,0.0002068592,0.000049004553,0.000007644156,0.00004304931,0.000045546356],"genre_scores_gemma":[0.9443206,0.000053685057,0.05534437,0.000021220554,0.00020665034,0.0000014881288,0.0000024339822,0.000046783814,0.0000027752576],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99881464,0.000009220078,0.00049346016,0.00009891527,0.00037747258,0.00020629095],"domain_scores_gemma":[0.9994077,0.0000736838,0.00008602336,0.00011819335,0.00015236772,0.00016201288],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00013655038,0.00016764285,0.0002872011,0.00006617413,0.000026181211,0.00003657589,0.00018387592,0.000046966572,0.000034975797],"category_scores_gemma":[0.000112886875,0.0001533948,0.00007723559,0.0002452659,0.00001715282,0.00018531553,0.00002103769,0.0002607063,0.000005562703],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000011880837,0.000018916511,0.0005432358,0.0000705669,0.00013717354,0.00003088431,0.0007304856,0.59818363,0.39992842,0.000023516033,0.00007946532,0.00024179324],"study_design_scores_gemma":[0.0007905097,0.00016091422,0.0017148788,0.000212958,0.00017523758,0.000025986701,0.00020520431,0.86358684,0.13274448,0.000016214848,0.00012243172,0.00024431787],"about_ca_topic_score_codex":0.0000042055935,"about_ca_topic_score_gemma":7.4367637e-7,"teacher_disagreement_score":0.30666608,"about_ca_system_score_codex":0.00007871523,"about_ca_system_score_gemma":0.000025152678,"threshold_uncertainty_score":0.62552583},"labels":[],"label_agreement":null},{"id":"W3094895643","doi":"10.1063/5.0023833","title":"Characteristics of self-oscillating jets in a confined cavity","year":2020,"lang":"en","type":"article","venue":"Physics of Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":23,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Windsor","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Physics; Turbulence; Reynolds number; Mechanics; Jet (fluid); Nozzle; Vortex; Reynolds stress; Oscillation (cell signaling); Vortex ring; Square (algebra); Classical mechanics; Geometry; Thermodynamics","score_opus":0.012086582627659503,"score_gpt":0.2116083337108237,"score_spread":0.1995217510831642,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3094895643","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9792637,0.000029443605,0.018995436,0.000040606123,0.00009986413,0.0000782189,0.00006951216,0.000065955755,0.0013572572],"genre_scores_gemma":[0.9966887,0.00004552394,0.0030725996,0.00001891226,0.00013939674,0.0000018234598,0.00001023962,0.000021214864,0.0000015389372],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993632,0.000007710295,0.00028698018,0.00009341212,0.000120132005,0.00012860159],"domain_scores_gemma":[0.99968433,0.000048205955,0.00004625719,0.00012402072,0.000054731117,0.00004246175],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00006005347,0.00010136683,0.00026585482,0.000021949767,0.000009768953,0.0000049977602,0.00011402911,0.000042312615,0.0000050480985],"category_scores_gemma":[0.00005782027,0.00011461838,0.000045410736,0.00021395227,0.000024844563,0.00004067872,0.00004108185,0.000121748635,0.0000022635672],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00002157596,0.00014730303,0.018968625,0.0015184741,0.00010745445,0.000010637961,0.00413868,0.08047179,0.859704,0.017304072,0.00008490602,0.017522467],"study_design_scores_gemma":[0.00023313262,0.00003601734,0.0067169415,0.00004060244,0.000013760424,1.9327267e-7,0.000019391699,0.98443145,0.007563475,0.00074465096,0.000070724804,0.00012968831],"about_ca_topic_score_codex":0.000012479887,"about_ca_topic_score_gemma":0.0000012531925,"teacher_disagreement_score":0.90395963,"about_ca_system_score_codex":0.000023194085,"about_ca_system_score_gemma":0.000025940293,"threshold_uncertainty_score":0.4674002},"labels":[],"label_agreement":null},{"id":"W3096895608","doi":"10.1063/5.0026552","title":"Flow dynamics and azimuthal behavior of the self-excited acoustic modes in axisymmetric shallow cavities","year":2020,"lang":"en","type":"article","venue":"Physics of Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":20,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Ontario Tech University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Physics; Mechanics; Vortex; Excitation; Resonance (particle physics); Coupling (piping); Flow (mathematics); Acoustics; Classical mechanics; Atomic physics; Materials science","score_opus":0.009871805924475457,"score_gpt":0.20094110767633125,"score_spread":0.1910693017518558,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3096895608","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97231513,0.00018213561,0.026491895,0.000031575088,0.00013357856,0.0001686432,0.00019251568,0.000057809335,0.00042669568],"genre_scores_gemma":[0.99778366,0.00010255918,0.0019754919,0.000015781565,0.0000589237,0.000008854335,0.0000117602085,0.000036064645,0.00000690873],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99920124,0.000014231817,0.00026904073,0.00014039676,0.00019840086,0.0001767004],"domain_scores_gemma":[0.99958694,0.00007445272,0.000038801576,0.00019488689,0.00005546621,0.00004944173],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000057748573,0.00016117241,0.00027126988,0.000052630792,0.000023932791,0.000012846534,0.00023249493,0.000070635055,0.000004194633],"category_scores_gemma":[0.000032726486,0.00014441246,0.00007106707,0.0005122021,0.000077834986,0.00007929808,0.00010217865,0.0002026944,6.665612e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000091631255,0.00014373718,0.014178668,0.0006818672,0.00006700868,0.000004977287,0.0014375678,0.9237137,0.04887191,0.003674975,0.000033261287,0.0071831574],"study_design_scores_gemma":[0.00024225855,0.00003526169,0.009141455,0.00003233048,0.00006293228,8.3156624e-7,0.00016218732,0.9885271,0.0012182638,0.00043707594,0.0000015223703,0.00013878343],"about_ca_topic_score_codex":0.000028603146,"about_ca_topic_score_gemma":0.00004107924,"teacher_disagreement_score":0.06481339,"about_ca_system_score_codex":0.000050677354,"about_ca_system_score_gemma":0.000022684311,"threshold_uncertainty_score":0.58889693},"labels":[],"label_agreement":null},{"id":"W3103231494","doi":"10.11159/ffhmt20.184","title":"Effect of ambient turbulence on the evolution and mixing of passive scalar in turbulent jet","year":2020,"lang":"en","type":"article","venue":"Proceedings of the ... International Conference on Fluid Flow, Heat and Mass Transfer","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"McGill University","funders":"","keywords":"Turbulence; Scalar (mathematics); Jet (fluid); Mixing (physics); Physics; Mechanics; Statistical physics; Classical mechanics; Mathematics; Geometry; Quantum mechanics","score_opus":0.009837210121822322,"score_gpt":0.20602848605399643,"score_spread":0.19619127593217411,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3103231494","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.995393,0.0000632774,0.0009144961,0.0017841285,0.00012543554,0.00025114062,0.000033039152,0.000011345823,0.001424136],"genre_scores_gemma":[0.9995853,0.00023109608,0.000067856825,0.000054892047,0.000027390437,0.000015910908,0.0000014456031,0.000010567424,0.0000055493406],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99920076,0.000008942678,0.00024749443,0.00015625209,0.00027963633,0.000106894906],"domain_scores_gemma":[0.9996877,0.00008668875,0.000020091456,0.000050057904,0.00012007447,0.000035396428],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018600615,0.00014157058,0.00020039488,0.000053001284,0.000023810235,0.00001891164,0.0002451942,0.00005606954,0.000014132144],"category_scores_gemma":[0.00006236324,0.00008806815,0.00005525263,0.00008900622,0.000097349686,0.00006079972,0.00003078602,0.0001843658,3.8906822e-7],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00028783036,0.000034428882,0.0020423462,0.0004926945,0.0000691996,5.848096e-7,0.0008943812,0.0062628095,0.9194251,0.0694462,0.000087800014,0.0009566579],"study_design_scores_gemma":[0.0004851129,0.00031407195,0.0011852224,0.0005769304,0.000029034147,0.000001452828,0.000161144,0.74697727,0.24915655,0.0009944573,0.000014063434,0.00010470444],"about_ca_topic_score_codex":0.000012350772,"about_ca_topic_score_gemma":0.0000017697683,"teacher_disagreement_score":0.74071443,"about_ca_system_score_codex":0.000039044888,"about_ca_system_score_gemma":0.000009922062,"threshold_uncertainty_score":0.3591315},"labels":[],"label_agreement":null},{"id":"W3108856179","doi":"10.1121/1.5147474","title":"Spectral analysis of turbulent boundary layer pressure fluctuations collected by a MEMS microphone array","year":2020,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Turbulence; Boundary layer; Spectral density; Acoustics; Microphone array; Physics; Mach number; Optics; Microphone; Mechanics; Computer science; Sound pressure; Telecommunications","score_opus":0.007064569327247512,"score_gpt":0.21183734710233718,"score_spread":0.20477277777508968,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3108856179","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.10732154,0.001535996,0.88577795,0.004673104,0.00019411808,0.00015163275,0.00019769334,0.000022937178,0.00012502489],"genre_scores_gemma":[0.97179955,0.00081308384,0.026636105,0.0005407267,0.0001253046,8.001811e-7,0.000003634584,0.000023315073,0.00005745587],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99866706,0.00005747635,0.0005488307,0.00008043049,0.00044519536,0.00020102304],"domain_scores_gemma":[0.99887633,0.0002827952,0.00031438604,0.0002361752,0.00019071541,0.000099620105],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021053357,0.00014961658,0.0005043197,0.000024834855,0.000117246665,0.000016920301,0.00056854973,0.0000710589,0.00014550098],"category_scores_gemma":[0.00012197622,0.000089911155,0.00059829466,0.0010900584,0.00038920512,0.000036956866,0.00005974165,0.0004981839,0.0000010514661],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000025756652,0.000040817926,0.000013779408,0.000030329997,0.0019508662,2.719897e-7,0.00097230164,0.4695453,0.4842995,5.037499e-7,0.043012265,0.00010831004],"study_design_scores_gemma":[0.00025142677,0.00012199993,0.00062938116,0.000022678823,0.004005179,0.0000065758068,0.0006759473,0.97959256,0.01210114,0.000087919965,0.002387906,0.00011730205],"about_ca_topic_score_codex":0.000020288364,"about_ca_topic_score_gemma":8.57737e-7,"teacher_disagreement_score":0.86447805,"about_ca_system_score_codex":0.000049010916,"about_ca_system_score_gemma":0.00006523505,"threshold_uncertainty_score":0.36664706},"labels":[],"label_agreement":null},{"id":"W3110484132","doi":"10.3390/acoustics2040046","title":"Influence of Swept Blades on Low-Order Acoustic Prediction for Axial Fans","year":2020,"lang":"en","type":"article","venue":"Acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":17,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"H2020 Marie Skłodowska-Curie Actions; École Centrale de Lyon; European Commission; Université de Sherbrooke","keywords":"Airfoil; Noise (video); Acoustics; Trailing edge; Curvature; Aerodynamics; Rotation (mathematics); Blade (archaeology); Turbulence; Computational fluid dynamics; Sensitivity (control systems); Computer science; Physics; Mechanics; Structural engineering; Engineering; Mathematics; Geometry; Electronic engineering","score_opus":0.008352197205374529,"score_gpt":0.20880733088453557,"score_spread":0.20045513367916104,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3110484132","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.55181855,0.000024412564,0.44682205,0.000047026202,0.0002911149,0.00021965346,0.0003670824,0.00017286922,0.00023723725],"genre_scores_gemma":[0.99478877,0.000086165506,0.004322972,0.00021961042,0.0004262263,0.000025502164,0.00004024914,0.000064230895,0.000026277834],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989644,0.000006965888,0.00033693074,0.00020318273,0.00021560464,0.00027291107],"domain_scores_gemma":[0.9992661,0.00019177391,0.00005511414,0.00020263522,0.00017419584,0.00011021908],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000066929715,0.0001989549,0.00022881647,0.000046911387,0.00005968395,0.000019172514,0.00020557991,0.00014918351,0.000015577512],"category_scores_gemma":[0.00043087246,0.00020653044,0.00006261092,0.00020167058,0.00006274998,0.000066460954,0.00003319834,0.0002181427,0.000016260998],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000022836373,0.000021024816,0.0000671067,0.00032273296,0.000036459773,0.0000022387142,0.0001993349,0.8654334,0.13130435,0.00018914389,0.0019837974,0.0004175705],"study_design_scores_gemma":[0.00039411834,0.00024049269,0.0014685569,0.000061583865,0.000100660225,0.0000011106923,0.00008217147,0.9949898,0.001999018,0.00023615942,0.00023235964,0.00019394576],"about_ca_topic_score_codex":0.0000016088927,"about_ca_topic_score_gemma":0.0000014071805,"teacher_disagreement_score":0.44297022,"about_ca_system_score_codex":0.000043093234,"about_ca_system_score_gemma":0.000036230427,"threshold_uncertainty_score":0.8422067},"labels":[],"label_agreement":null},{"id":"W3112606248","doi":"10.1175/jtech-d-20-0174.1","title":"Effect of Acoustic Doppler Velocimeter Sampling Volume Size on Measurements of Turbulence","year":2020,"lang":"en","type":"article","venue":"Journal of Atmospheric and Oceanic Technology","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":16,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Sampling (signal processing); Turbulence; Doppler effect; Volume (thermodynamics); Acoustic Doppler velocimetry; Noise (video); Jet (fluid); Acoustics; Physics; Mechanics; Optics; Laser Doppler velocimetry; Blood flow; Computer science","score_opus":0.009565391866039066,"score_gpt":0.21841839302387522,"score_spread":0.20885300115783617,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3112606248","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9547464,0.0008961733,0.04382317,0.000103369726,0.00022914242,0.00007856053,0.0000035001713,0.000039366874,0.00008028149],"genre_scores_gemma":[0.98220193,0.00018484956,0.017501244,0.00003332697,0.000048668906,6.479832e-7,1.4039918e-7,0.00002330251,0.000005881285],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99905026,0.000017466906,0.00046188402,0.00010509987,0.00020069178,0.00016457187],"domain_scores_gemma":[0.999338,0.00015029375,0.0002355742,0.00012171069,0.00009449827,0.000059927566],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023700182,0.00015217761,0.0004588069,0.000012269762,0.00002055683,0.0000051471425,0.00022861916,0.00015474627,0.00003134323],"category_scores_gemma":[0.00038070098,0.0001228733,0.00007867547,0.00026185915,0.000089792615,0.000040314226,0.000047305366,0.00034649184,0.0000014589709],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00061396044,0.00014151326,0.021985434,0.0019557364,0.0010366961,0.00007786657,0.00047462195,0.4130322,0.46287102,0.00020379652,0.0017853761,0.09582178],"study_design_scores_gemma":[0.005126874,0.0134462295,0.009756142,0.0010723938,0.00095784693,0.00033201178,0.00039489075,0.8903751,0.075960144,0.0010272096,0.0006517483,0.0008994479],"about_ca_topic_score_codex":4.1454163e-7,"about_ca_topic_score_gemma":1.1380105e-7,"teacher_disagreement_score":0.47734284,"about_ca_system_score_codex":0.000033719953,"about_ca_system_score_gemma":0.000018450379,"threshold_uncertainty_score":0.5010628},"labels":[],"label_agreement":null},{"id":"W3116526468","doi":"10.22215/etd/2017-11820","title":"Aeroacoustic Optimization of Flat-Plate Serrated Trailing Edge Extensions for Broadband Noise Reduction","year":2017,"lang":"en","type":"dissertation","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Carleton University","funders":"","keywords":"Serration; Trailing edge; Noise reduction; Noise (video); Sawtooth wave; Acoustics; Reduction (mathematics); Mach number; Materials science; Structural engineering; Mechanics; Engineering; Mathematics; Geometry; Physics; Computer science","score_opus":0.013719037120943365,"score_gpt":0.2509658062242778,"score_spread":0.23724676910333442,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3116526468","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.13827783,0.000695492,0.8106989,0.000013427344,0.011794188,0.0018134915,0.00039384168,0.00061626895,0.03569653],"genre_scores_gemma":[0.9323113,0.000857445,0.03587689,0.0000033739389,0.00045051568,0.00010606005,0.0065038237,0.0002486854,0.023641888],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99875236,0.000008354187,0.0005114801,0.0003072357,0.00016205636,0.00025852496],"domain_scores_gemma":[0.9988293,0.000044915523,0.00023266667,0.00040931389,0.00041194508,0.000071825554],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00013874183,0.0003305407,0.00043831562,0.00018549518,0.00022073221,0.00006684483,0.00020116895,0.00048542765,0.00009069668],"category_scores_gemma":[0.000115754156,0.00034744543,0.00014616046,0.000098086995,0.00002774702,0.00014063806,0.0000070935603,0.0002616643,0.0000033816798],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00003926605,0.000015641164,4.609818e-7,0.00068788737,0.00008547668,9.751105e-7,0.00017516759,0.9203361,0.07493068,0.000091406815,0.00094928563,0.00268764],"study_design_scores_gemma":[0.00037056106,0.000034264856,0.000045677643,0.00038431946,0.00029708017,0.000004262209,0.00027432875,0.9927384,0.0052504907,0.0001342569,0.000101217454,0.00036510697],"about_ca_topic_score_codex":0.000016865259,"about_ca_topic_score_gemma":0.0000688842,"teacher_disagreement_score":0.79403347,"about_ca_system_score_codex":0.00004778816,"about_ca_system_score_gemma":0.00006890592,"threshold_uncertainty_score":0.9998978},"labels":[],"label_agreement":null},{"id":"W3118904974","doi":"10.3390/jmse9010061","title":"Buoyant Jets in Cross-Flows: Review, Developments, and Applications","year":2021,"lang":"en","type":"article","venue":"Journal of Marine Science and Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":32,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Wilfrid Laurier University; University of Ottawa","funders":"","keywords":"Mixing (physics); Jet (fluid); Mechanics; Outfall; Environmental science; Vortex; Flow (mathematics); Current (fluid); Meteorology; Physics; Geology; Oceanography; Environmental engineering","score_opus":0.005576269944192648,"score_gpt":0.22931114129770172,"score_spread":0.22373487135350908,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3118904974","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.95541674,0.013059447,0.02820545,0.00026799797,0.0005067578,0.00015294057,0.0000030025542,0.000039159164,0.0023484956],"genre_scores_gemma":[0.92593926,0.03786604,0.035906095,0.00008207691,0.00014250992,0.000006797461,0.0000010011743,0.00001561654,0.00004062053],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99930274,0.00000204719,0.00026025999,0.000087264605,0.00019300415,0.00015468289],"domain_scores_gemma":[0.9996284,0.000024307119,0.000028876275,0.00007438696,0.00015632053,0.000087667475],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005751962,0.00007427496,0.00014181976,0.00014691331,0.000039116392,0.00006173566,0.00010703102,0.000019877125,0.0000050971707],"category_scores_gemma":[0.00019498082,0.000069397196,0.000013355354,0.0005139076,0.000035831996,0.00020138473,0.00012536754,0.00015986814,4.837471e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000044666263,0.000064101776,0.01895734,0.002899089,0.0000543095,0.00026495435,0.0002337733,0.47573626,0.0964504,0.003509396,0.0002157866,0.4016101],"study_design_scores_gemma":[0.00097423577,0.000047073947,0.23800835,0.0021776222,0.000040754763,0.0015360622,0.000094390714,0.7008667,0.0021123122,0.00090040156,0.052517865,0.0007242494],"about_ca_topic_score_codex":0.0000010539794,"about_ca_topic_score_gemma":0.0000029798675,"teacher_disagreement_score":0.40088585,"about_ca_system_score_codex":0.00007098084,"about_ca_system_score_gemma":0.00010147525,"threshold_uncertainty_score":0.28299353},"labels":[],"label_agreement":null},{"id":"W3119513293","doi":"10.1007/s13272-020-00484-5","title":"CFD-based prediction of wall-pressure spectra under a turbulent boundary layer with adverse pressure gradient","year":2021,"lang":"en","type":"article","venue":"CEAS Aeronautical Journal","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure; Université de Sherbrooke","funders":"Horizon 2020; Canadian Network for Research and Innovation in Machining Technology, Natural Sciences and Engineering Research Council of Canada","keywords":"Turbulence; Boundary layer; Direct numerical simulation; Airfoil; Mechanics; Computational fluid dynamics; Pressure gradient; Turbulence modeling; Statistical physics; Physics; Wind tunnel; Adverse pressure gradient; Flow separation; Classical mechanics; Reynolds number","score_opus":0.01018194260158959,"score_gpt":0.2068171236100554,"score_spread":0.1966351810084658,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3119513293","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.74485123,0.0062165293,0.24154012,0.0018178131,0.0017367468,0.0003594672,0.00021237516,0.0002670652,0.0029986338],"genre_scores_gemma":[0.99413085,0.0001308976,0.0050504347,0.00012922751,0.00025736835,0.000004440086,0.000025325806,0.00005287725,0.0002185818],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99836,0.000051141997,0.0004047171,0.00022477067,0.0005529525,0.00040646302],"domain_scores_gemma":[0.99908656,0.000056100238,0.00007165012,0.0002945861,0.00021199368,0.00027912782],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018255606,0.0002382976,0.00029613802,0.00006347937,0.00013192545,0.000064870976,0.0001805328,0.00015209339,0.00055919826],"category_scores_gemma":[0.000026912223,0.00019742595,0.00014344038,0.00016407954,0.00013447605,0.0001098768,0.000033666554,0.00075920747,0.0000067326687],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00010386443,0.00029377986,0.00084137416,0.00020513883,0.00066840963,0.00039456235,0.000114456874,0.9842462,0.0069672987,0.0033864134,0.0021688347,0.000609655],"study_design_scores_gemma":[0.0018709205,0.00027587652,0.01754754,0.000337959,0.0007472031,0.00073398784,0.00012375321,0.95400006,0.0022988075,0.0015786674,0.02012755,0.00035764885],"about_ca_topic_score_codex":0.0000016910645,"about_ca_topic_score_gemma":0.000008627435,"teacher_disagreement_score":0.2492796,"about_ca_system_score_codex":0.00009539523,"about_ca_system_score_gemma":0.00019676532,"threshold_uncertainty_score":0.80507964},"labels":[],"label_agreement":null},{"id":"W3123715913","doi":"10.22215/etd/2018-12858","title":"The Design, Fabrication, and Commissioning of a High-Speed Aeroacoustic Wind Tunnel for Studies of Surface Pressure Fluctuations Beneath Turbulent Boundary Layers","year":2018,"lang":"en","type":"dissertation","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Wind tunnel; Hypersonic wind tunnel; Turbulence; Boundary layer; Supersonic wind tunnel; Engineering; Mach number; Wind speed; Duct (anatomy); Aerodynamics; Aerospace engineering; Wind gradient; Boiler blowdown; Static pressure; Marine engineering; Computational fluid dynamics; Transonic; Mechanical engineering; Meteorology; Wind profile power law; Inlet; Physics","score_opus":0.02043136768708731,"score_gpt":0.268920761327905,"score_spread":0.24848939364081768,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3123715913","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.71550375,0.024412686,0.2538162,0.00013012109,0.0022394366,0.0026857331,0.00039260724,0.00018184788,0.0006376474],"genre_scores_gemma":[0.969535,0.0018043809,0.024970563,0.0000046039004,0.00008394075,0.000024223156,0.000280935,0.00006945491,0.0032268786],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99881846,0.000026724936,0.0005204853,0.00021308658,0.00022786196,0.00019338306],"domain_scores_gemma":[0.9977868,0.0007665108,0.00023029737,0.00031013883,0.00086085056,0.00004536588],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003533595,0.00026183427,0.00041880613,0.000059777285,0.0003535364,0.000042853208,0.00022088301,0.00017169317,0.000010304755],"category_scores_gemma":[0.00032665412,0.00019537471,0.000067430396,0.00012435965,0.00013755565,0.000051566858,0.000026632566,0.00014526126,4.2536107e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00008844438,0.000043258617,0.000015195461,0.0018823361,0.001293665,3.0952526e-7,0.0042804256,0.95643824,0.020954384,0.001316606,0.01218998,0.0014971687],"study_design_scores_gemma":[0.0005854284,0.00018329108,0.002299682,0.0005843995,0.0010872949,0.000001583121,0.006808228,0.9771215,0.004791107,0.004850977,0.0012181706,0.00046839385],"about_ca_topic_score_codex":0.000022950746,"about_ca_topic_score_gemma":0.000081908984,"teacher_disagreement_score":0.25403127,"about_ca_system_score_codex":0.000037429465,"about_ca_system_score_gemma":0.00008012452,"threshold_uncertainty_score":0.79671496},"labels":[],"label_agreement":null},{"id":"W3128724451","doi":"10.22215/etd/2006-07735","title":"Trailing edge flap control of dynamic stall on helicopter rotor blades","year":2006,"lang":"en","type":"dissertation","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Carleton University; Canadian Heritage; Library and Archives Canada","funders":"","keywords":"Stall (fluid mechanics); Trailing edge; Rotor (electric); Engineering; Computer science; Aerospace engineering; Mechanical engineering; Structural engineering","score_opus":0.003250346813878867,"score_gpt":0.20886795490078303,"score_spread":0.20561760808690416,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3128724451","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8194982,0.0006037024,0.036670126,0.000008592886,0.0025546346,0.0009193013,0.0004395718,0.0004266095,0.13887928],"genre_scores_gemma":[0.9890828,0.00006805175,0.0008594564,0.000017244,0.0001374789,0.000045318793,0.00095282856,0.00012573607,0.008711069],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9987664,0.000009490053,0.0004707831,0.00024379468,0.00023645637,0.0002730821],"domain_scores_gemma":[0.999436,0.00007591754,0.000090058114,0.00026967304,0.00007923937,0.000049083614],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.000076775716,0.00035924377,0.00045343506,0.00016312211,0.000032756674,0.000031316828,0.00019989727,0.00036054707,0.00015099341],"category_scores_gemma":[0.0000144907135,0.0003467922,0.0001722031,0.0000740408,0.000016988914,0.000036896156,0.000005142928,0.00036181454,0.000030143532],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00017622417,0.00024546418,0.000038431263,0.003153724,0.0006013678,0.00002803962,0.00046778016,0.67163247,0.2861664,0.004091858,0.0021549172,0.031243302],"study_design_scores_gemma":[0.00071926875,0.00009608902,0.0013996775,0.00035722496,0.00013176899,8.1629196e-7,0.00016689186,0.9922632,0.003223966,0.00023625686,0.00078671344,0.000618106],"about_ca_topic_score_codex":0.000028641593,"about_ca_topic_score_gemma":0.0006214092,"teacher_disagreement_score":0.32063073,"about_ca_system_score_codex":0.00007021527,"about_ca_system_score_gemma":0.000025685547,"threshold_uncertainty_score":0.99989843},"labels":[],"label_agreement":null},{"id":"W3129285050","doi":"10.1002/9781119756743.ch8","title":"An Efficient Far‐Field Noise Prediction Framework for the Next Generation of Aircraft Landing Gear Designs","year":2021,"lang":"en","type":"other","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto","funders":"","keywords":"Landing gear; Noise (video); Near and far field; Computer science; Field (mathematics); Experimental data; Computer simulation; Algorithm; Aerospace engineering; Engineering; Simulation; Mathematics; Artificial intelligence; Physics","score_opus":0.04668599873267707,"score_gpt":0.2650868926251844,"score_spread":0.21840089389250736,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3129285050","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.00034926072,0.0008042499,0.98428,0.000018404968,0.0016222426,0.00035182023,0.00007060844,0.00016427768,0.012339172],"genre_scores_gemma":[0.48207322,0.0033091935,0.43914494,0.000307956,0.008651384,0.00035489767,0.0009832889,0.0015766456,0.06359847],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993775,0.0000119560955,0.00017583434,0.0001652913,0.00012638408,0.00014303038],"domain_scores_gemma":[0.99942863,0.00014028342,0.000046423258,0.00032138385,0.000031547424,0.000031749565],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00011364436,0.00015495504,0.00016614656,0.000063567524,0.000053165706,0.000046580513,0.00013512367,0.00032006757,0.00067214906],"category_scores_gemma":[0.000043183416,0.00011957485,0.00007163418,0.0000805634,0.000012824873,0.000012863579,0.000015209727,0.00018526286,0.0000020040752],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000002703889,0.000030145866,0.000020984658,0.00019713635,0.00010918217,8.4419753e-7,0.00008628223,0.9377116,0.012651477,0.004989217,0.042035047,0.0021653965],"study_design_scores_gemma":[0.000072697716,0.00003916679,0.000009740001,0.000119959666,0.0000565267,7.1526904e-7,0.00005814098,0.98947567,0.00055092387,0.000063590494,0.009427439,0.00012545213],"about_ca_topic_score_codex":0.00002736486,"about_ca_topic_score_gemma":0.000077317265,"teacher_disagreement_score":0.545135,"about_ca_system_score_codex":0.000030414698,"about_ca_system_score_gemma":0.000015269985,"threshold_uncertainty_score":0.7359561},"labels":[],"label_agreement":null},{"id":"W3130700783","doi":"10.1016/b978-0-12-820644-7.00023-2","title":"Mixing of inclined dense jets: a numerical modeling","year":2021,"lang":"en","type":"book-chapter","venue":"Elsevier eBooks","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Ottawa","funders":"","keywords":"Mechanics; Froude number; Turbulence; Jet (fluid); Nozzle; Dimensionless quantity; Mixing (physics); Plume; Vortex; Physics; Flow (mathematics); Meteorology; Thermodynamics","score_opus":0.013541666927923584,"score_gpt":0.21933088846700427,"score_spread":0.2057892215390807,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3130700783","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0005645634,0.0027604694,0.014170499,0.000007826162,0.0007450549,0.00020572095,0.00006380837,0.00016437855,0.9813177],"genre_scores_gemma":[0.09807283,0.0007102644,0.015876912,0.00009861977,0.00078286516,0.000025210922,0.000099987235,0.0004639197,0.8838694],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9983709,0.000010454505,0.00068868697,0.00032937565,0.00030864176,0.0002919674],"domain_scores_gemma":[0.9990403,0.0000756384,0.00010583212,0.0005267617,0.00014166531,0.00010979404],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00014955585,0.00042866627,0.0007285756,0.0001227403,0.00005181517,0.000028585759,0.00025475593,0.00040479566,0.00012347737],"category_scores_gemma":[0.000033763125,0.0004650558,0.0003054088,0.00001776373,0.000046366113,0.000022050344,0.00016891326,0.0006747539,0.000023073595],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000009364271,0.000010954839,0.0000012786311,0.000695512,0.00038709462,0.00017120899,0.00023323543,0.15117295,0.0008585272,0.008250432,0.00005484213,0.8381546],"study_design_scores_gemma":[0.00020675141,0.000020933978,2.4546688e-7,0.0010736876,0.00018634903,0.000021650125,0.000013073736,0.9021687,0.00005456627,0.006384611,0.08924998,0.0006194769],"about_ca_topic_score_codex":4.178321e-7,"about_ca_topic_score_gemma":0.0000069806624,"teacher_disagreement_score":0.83753514,"about_ca_system_score_codex":0.000108021704,"about_ca_system_score_gemma":0.000069957474,"threshold_uncertainty_score":0.9997801},"labels":[],"label_agreement":null},{"id":"W3131373906","doi":"10.3390/en14041170","title":"Effect of Upstream Side Flow of Wind Turbine on Aerodynamic Noise: Simulation Using Open-Loop Vibration in the Rod in Rod-Airfoil Configuration","year":2021,"lang":"en","type":"article","venue":"Energies","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":9,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Waterloo","funders":"","keywords":"Airfoil; Strouhal number; Turbine; Aerodynamics; Noise (video); Turbine blade; Vibration; Acoustics; Lift (data mining); Trailing edge; Wind tunnel; Structural engineering; Potential flow; Leading edge; Lift coefficient; Engineering; Mechanics; Reynolds number; Physics; Turbulence; Aerospace engineering; Computer science","score_opus":0.009851735899772873,"score_gpt":0.2573142974943203,"score_spread":0.2474625615945474,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3131373906","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99625564,0.00009508591,0.002387761,0.000024315894,0.00019613806,0.00019225776,0.000013946907,0.00001712985,0.00081770716],"genre_scores_gemma":[0.9992368,0.000031095795,0.00054563483,0.000011148164,0.00004114079,0.0000070990272,0.000084132356,0.000021322869,0.000021614567],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99904984,0.00014073343,0.00035514386,0.00015265729,0.00017535836,0.00012628929],"domain_scores_gemma":[0.9992104,0.00040192652,0.000075289354,0.00025318854,0.000047598445,0.000011587744],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003787681,0.00014277032,0.0002489338,0.00010422428,0.000028122708,0.00003898198,0.00015723628,0.00008455804,0.000012343008],"category_scores_gemma":[0.00016607922,0.00011905612,0.00003739955,0.00032723622,0.00002451168,0.00016956484,0.00003403454,0.00013666076,8.433015e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000029234707,0.000033284105,0.00030351826,0.00008127502,0.000009722273,0.000005261051,0.00024736382,0.8652209,0.13113165,0.0002798105,0.0000027497515,0.0026552384],"study_design_scores_gemma":[0.00056806154,0.00008245525,0.005354771,0.00015232395,0.000016404556,0.0000011232206,0.000105830586,0.9231946,0.07032715,0.00009282203,0.0000042456372,0.00010020323],"about_ca_topic_score_codex":0.00009704855,"about_ca_topic_score_gemma":0.0005059957,"teacher_disagreement_score":0.06080451,"about_ca_system_score_codex":0.00007219326,"about_ca_system_score_gemma":0.000028452536,"threshold_uncertainty_score":0.4854968},"labels":[],"label_agreement":null},{"id":"W3140704679","doi":"","title":"The Effect of Non-Equilibrium Condensation on Supersonic Air Flows over Rectangular Cavities","year":2007,"lang":"en","type":"article","venue":"热科学学报：英文版","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Supersonic speed; Condensation; Mechanics; Choked flow; Physics; Meteorology; Thermodynamics; Materials science; Environmental science","score_opus":0.0025874999045817438,"score_gpt":0.2077559884771523,"score_spread":0.20516848857257056,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3140704679","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99040776,0.0001988058,0.0014188882,0.000020173313,0.0008797418,0.00020301297,0.000018735478,0.000103512255,0.006749358],"genre_scores_gemma":[0.9992229,0.00001817819,0.00010434229,0.000022410433,0.00021492304,0.000008572056,0.000012985254,0.000045381195,0.00035034667],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9990538,0.00002346374,0.00023448537,0.00014052856,0.00023603534,0.00031169297],"domain_scores_gemma":[0.9992405,0.00037672796,0.000035429457,0.00027676343,0.000028635679,0.000041911444],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00053249655,0.00017893645,0.00019815756,0.00006228084,0.00009407701,0.000021803306,0.0001707075,0.00011508096,0.000024664703],"category_scores_gemma":[0.000050894512,0.00013508547,0.00009827275,0.00013255751,0.0000589319,0.000056212528,0.000027427754,0.00021505798,0.000023007584],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00045173362,0.0000612463,0.0045096385,0.0008764788,0.00045203825,0.0000931556,0.005754198,0.23191212,0.7191417,0.0039917547,0.008421868,0.024334071],"study_design_scores_gemma":[0.0014256354,0.0008537816,0.0180863,0.00015220091,0.00011387601,0.000012028388,0.00075320405,0.8539404,0.11949229,0.00019711004,0.004321225,0.00065194175],"about_ca_topic_score_codex":0.000043959793,"about_ca_topic_score_gemma":0.00012713585,"teacher_disagreement_score":0.6220283,"about_ca_system_score_codex":0.000100486424,"about_ca_system_score_gemma":0.000008300787,"threshold_uncertainty_score":0.55086255},"labels":[],"label_agreement":null},{"id":"W3148288363","doi":"","title":"Optimization and Testing of Flat-Plate Trailing-Edge Serration Geometry for Reducing Airfoil Self-Noise","year":2020,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"Carleton University","funders":"","keywords":"Serration; Trailing edge; Wind tunnel; Airfoil; Anechoic chamber; NACA airfoil; Noise (video); Engineering; Acoustics; Aeroacoustics; Structural engineering; Aerospace engineering; Turbulence; Physics; Sound pressure; Reynolds number; Mechanics; Computer science","score_opus":0.014448566831018276,"score_gpt":0.19410662194827427,"score_spread":0.179658055117256,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3148288363","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.36531273,0.00015480809,0.6327496,0.00010036212,0.00037665156,0.00027113364,0.0002502087,0.00015669236,0.0006278156],"genre_scores_gemma":[0.8651044,0.000046135385,0.1344371,0.00009014458,0.0001992441,0.000005977532,0.000053554908,0.000049284394,0.000014158399],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999229,0.000005395875,0.00026066173,0.00016952812,0.00007522783,0.00026014587],"domain_scores_gemma":[0.9993104,0.00009713312,0.000049311748,0.00010652764,0.00013379141,0.0003028354],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000100432015,0.00014033224,0.00017142334,0.00010993089,0.00010092599,0.000038487706,0.00008855793,0.00012248397,0.00000845966],"category_scores_gemma":[0.00036138413,0.00017370009,0.000024944435,0.0002812247,0.000023481032,0.00007618201,0.000011337384,0.00013623711,9.80442e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000015698718,0.0000020859623,0.00009494717,0.00032956823,0.000020763759,0.0000031846816,0.00035153463,0.9689566,0.027924467,0.00006871572,0.00047518694,0.00177141],"study_design_scores_gemma":[0.00019267453,0.00004248981,0.000268246,0.000040399715,0.00006933223,0.0000034134086,0.000103265476,0.9986012,0.00034344764,0.00003321083,0.00012435908,0.00017794847],"about_ca_topic_score_codex":0.00025767644,"about_ca_topic_score_gemma":0.00021666457,"teacher_disagreement_score":0.49979168,"about_ca_system_score_codex":0.00008701867,"about_ca_system_score_gemma":0.00014133875,"threshold_uncertainty_score":0.70832837},"labels":[],"label_agreement":null},{"id":"W3149164910","doi":"10.4236/jfcmv.2021.92002","title":"Application of Rainbow Schlieren Deflectometry for Jets from Round Laval Nozzles Followed by Cylindrical Ducts","year":2021,"lang":"en","type":"article","venue":"Journal of Flow Control Measurement &amp Visualization","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Nozzle; Schlieren; Jet (fluid); Duct (anatomy); Mach number; Flow visualization; Mechanics; Optics; Schlieren imaging; Physics; Materials science; Flow (mathematics); Anatomy","score_opus":0.018528848529244798,"score_gpt":0.262610558921567,"score_spread":0.24408171039232218,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3149164910","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.08756852,0.0023664928,0.90881735,0.000091313195,0.0007103854,0.00027510125,0.00009556953,0.000030618372,0.00004465257],"genre_scores_gemma":[0.9885404,0.00020252093,0.010604215,0.000053999956,0.00039379214,0.000016098573,0.0001257985,0.00004931058,0.0000138807945],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9978037,0.00008640719,0.00085740804,0.00017757571,0.0008592928,0.00021560042],"domain_scores_gemma":[0.9976035,0.00017712278,0.00038847068,0.00020013419,0.0015241527,0.00010665613],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0008752683,0.00019705715,0.00047684324,0.00016190317,0.0000682061,0.0000678708,0.0001744805,0.00015284405,0.000017223001],"category_scores_gemma":[0.0008569223,0.00019508254,0.00019202926,0.00033408342,0.000020396335,0.00016506825,0.000013578402,0.00015625329,0.0000018336709],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0001595208,0.00025090206,0.001594372,0.00010710568,0.00048526577,0.0000027109672,0.00010343945,0.09711263,0.8908186,0.0002057465,0.0032960752,0.0058636446],"study_design_scores_gemma":[0.0054429555,0.0001607008,0.0015929841,0.00017472943,0.00048425296,0.000010313879,0.000050553714,0.94443536,0.04168498,0.0008154964,0.004818145,0.0003295539],"about_ca_topic_score_codex":0.0000055881023,"about_ca_topic_score_gemma":0.000041984735,"teacher_disagreement_score":0.9009719,"about_ca_system_score_codex":0.00024708072,"about_ca_system_score_gemma":0.00012701002,"threshold_uncertainty_score":0.7955235},"labels":[],"label_agreement":null},{"id":"W3153859653","doi":"10.1063/5.0048582","title":"Control of the self-sustained shear layer oscillations over rectangular cavities using high-frequency vortex generators","year":2021,"lang":"en","type":"article","venue":"Physics of Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":30,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Ontario Tech University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Physics; Wind tunnel; Excitation; Vortex; Particle image velocimetry; Resonance (particle physics); Acoustic resonance; Acoustics; Vortex generator; Wake; Vortex shedding; Flapping; Mechanics; Reynolds number; Leading edge; Flow control (data); Optics; Resonator; Turbulence; Atomic physics; Telecommunications","score_opus":0.007749743571060123,"score_gpt":0.21032584103570923,"score_spread":0.2025760974646491,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3153859653","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.94245833,0.00033004905,0.055814352,0.000025753261,0.00052599114,0.00010796502,0.0001332473,0.000051479896,0.000552821],"genre_scores_gemma":[0.99198973,0.000029872936,0.0076852813,0.000022697996,0.00020725396,0.0000034227016,0.000007572148,0.000035999423,0.000018190027],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992048,0.00003076203,0.00025835395,0.00011881105,0.00021559585,0.00017165634],"domain_scores_gemma":[0.99928296,0.00005354421,0.00004781307,0.00037305188,0.00021250482,0.00003010401],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000074213924,0.00013284129,0.00023321487,0.000021939908,0.000072013325,0.000015126353,0.00013438164,0.00006153635,0.000021370372],"category_scores_gemma":[0.0000318545,0.000118914824,0.00011899718,0.00027624078,0.00005398884,0.00007799366,0.00004089712,0.00011719924,5.9828614e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000013934131,0.000036787438,0.001532604,0.0001034303,0.000160239,0.000002731324,0.00024072667,0.30771828,0.63803035,0.051972896,0.00006143163,0.000139141],"study_design_scores_gemma":[0.0004865418,0.000014431829,0.0016854828,0.000052699354,0.00019177773,0.0000015543271,0.00011049372,0.9223487,0.061488453,0.013300649,0.0000761157,0.00024312508],"about_ca_topic_score_codex":0.00005131842,"about_ca_topic_score_gemma":0.0000065808554,"teacher_disagreement_score":0.6146304,"about_ca_system_score_codex":0.00008020541,"about_ca_system_score_gemma":0.000101944825,"threshold_uncertainty_score":0.48492056},"labels":[],"label_agreement":null},{"id":"W3154016978","doi":"10.1063/5.0045967","title":"Airfoil flow receptivity to simulated tonal noise emissions","year":2021,"lang":"en","type":"article","venue":"Physics of Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":16,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Waterloo","funders":"","keywords":"Airfoil; Physics; Vortex shedding; Acoustics; Bubble; Flow separation; Mechanics; Reynolds number; Noise (video); Particle image velocimetry; Boundary layer; Mean flow; Trailing edge; Turbulence","score_opus":0.01052809472107824,"score_gpt":0.2333131243614041,"score_spread":0.22278502964032587,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3154016978","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.73830545,0.00010743579,0.2499257,0.00016114314,0.000839371,0.000102787046,0.00019029676,0.00020474705,0.010163077],"genre_scores_gemma":[0.9869843,0.000032712847,0.012364293,0.000049766546,0.00019933391,0.0000029448834,0.00004540262,0.00003542595,0.0002858232],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99926937,0.000011874949,0.0001805298,0.00016183539,0.00017693102,0.00019943983],"domain_scores_gemma":[0.9993411,0.00006777067,0.000012413504,0.00031666982,0.00014443828,0.000117609576],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000059406753,0.00013484198,0.00019958003,0.000020046693,0.000043804233,0.000014802344,0.00012897377,0.000059244132,0.00010716815],"category_scores_gemma":[0.00006224901,0.00014748705,0.00008765097,0.00021646677,0.000020507108,0.00005700876,0.00008460685,0.00015221936,0.0000408598],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000029281487,0.000053567448,0.00006151167,0.00003471529,0.000029033687,0.0000047451113,0.00010422052,0.6716378,0.31716937,0.0008833521,0.0013334875,0.0086852955],"study_design_scores_gemma":[0.00015886631,0.000018534658,0.00032185556,0.000052568783,0.000020959016,8.915527e-7,0.0000157822,0.949073,0.04612511,0.0018938894,0.0021225323,0.0001960076],"about_ca_topic_score_codex":0.000003808556,"about_ca_topic_score_gemma":0.00000302671,"teacher_disagreement_score":0.2774352,"about_ca_system_score_codex":0.000041930383,"about_ca_system_score_gemma":0.00003754733,"threshold_uncertainty_score":0.60143477},"labels":[],"label_agreement":null},{"id":"W3159681769","doi":"10.1103/physrevfluids.6.054501","title":"Positively buoyant jets: Semiturbulent to fully turbulent regimes","year":2021,"lang":"en","type":"article","venue":"Physical Review Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":29,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université Laval","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Turbulence; Laminar flow; Mechanics; Jet (fluid); Physics; Dissipation; Velocimetry; Particle image velocimetry; RADIUS; Thermodynamics","score_opus":0.007969553464690584,"score_gpt":0.2563119522985886,"score_spread":0.24834239883389803,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3159681769","genre_codex":"review","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.40724012,0.40876952,0.10000975,0.024116088,0.0032018342,0.0029970238,0.00038776742,0.0020635638,0.051214322],"genre_scores_gemma":[0.91187096,0.07351128,0.0059957365,0.0059861047,0.0011036112,0.00018571323,0.00015135978,0.00016018313,0.0010350356],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.99862236,0.000039388073,0.00030246185,0.00034299438,0.0003165395,0.00037625065],"domain_scores_gemma":[0.99905425,0.00007785242,0.000021066158,0.00046760877,0.00014383005,0.00023541649],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.000118146745,0.0002749353,0.0005001607,0.000024521642,0.000053856496,0.000043500102,0.00022507887,0.00003808613,0.00008377506],"category_scores_gemma":[0.00012072357,0.00024677985,0.00022156337,0.0003375458,0.000023564546,0.00006191064,0.000115572904,0.00024692368,0.00049169327],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000024680845,0.0011665942,0.00004546495,0.011902065,0.00078841334,0.0011212982,0.00094864983,0.045264047,0.33897296,0.08144761,0.41191489,0.10640334],"study_design_scores_gemma":[0.00059964193,0.00026586698,0.00079198636,0.011291143,0.0006470037,0.00015165353,0.000054850767,0.25940815,0.02372881,0.004136668,0.6967455,0.0021787437],"about_ca_topic_score_codex":0.0000017114634,"about_ca_topic_score_gemma":0.0000011783114,"teacher_disagreement_score":0.50463086,"about_ca_system_score_codex":0.00011663287,"about_ca_system_score_gemma":0.00003738315,"threshold_uncertainty_score":0.99999845},"labels":[],"label_agreement":null},{"id":"W3162313066","doi":"10.1063/5.0051226","title":"Shear layer synchronization of aerodynamically isolated opposite cavities due to acoustic resonance excitation","year":2021,"lang":"en","type":"article","venue":"Physics of Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":9,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Ontario Tech University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Physics; Mechanics; Resonance (particle physics); Excitation; Vortex; Acoustic resonance; Reynolds number; Acoustic wave; Acoustics; Turbulence; Atomic physics","score_opus":0.008053880370991202,"score_gpt":0.21842298536990712,"score_spread":0.21036910499891592,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3162313066","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.40321562,0.00024481333,0.59569126,0.000021707921,0.00019409638,0.000077952136,0.0000699033,0.00004886678,0.000435756],"genre_scores_gemma":[0.9900714,0.00009056763,0.009541709,0.000021942922,0.00008214715,0.000007621069,0.000076931916,0.000041717904,0.00006595432],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991486,0.000018799798,0.00030400342,0.00015779784,0.0002013539,0.00016942596],"domain_scores_gemma":[0.9992545,0.00007035538,0.00003672955,0.00025928902,0.00033065744,0.00004842219],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00006552098,0.0001346203,0.0002482656,0.00003861748,0.00003109781,0.000016200689,0.00011868543,0.00006753198,0.000014900264],"category_scores_gemma":[0.000054416527,0.00015860044,0.0000563485,0.0003669798,0.00003584318,0.000109579545,0.00004669071,0.00009986236,0.000006858313],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000007809536,0.00003767666,0.00006298937,0.00019209272,0.0000297548,0.0000054734187,0.0003416222,0.51215917,0.48009324,0.002400787,0.00011496972,0.004554397],"study_design_scores_gemma":[0.0001630985,0.000054030606,0.0022441559,0.00014504138,0.000038683047,0.000002052385,0.000044458564,0.98375845,0.011793114,0.0015493217,0.00003351685,0.0001741032],"about_ca_topic_score_codex":0.00001020838,"about_ca_topic_score_gemma":0.0000133817,"teacher_disagreement_score":0.58685577,"about_ca_system_score_codex":0.0000610545,"about_ca_system_score_gemma":0.000041625906,"threshold_uncertainty_score":0.6467538},"labels":[],"label_agreement":null},{"id":"W3164304948","doi":"10.11159/ffhmt21.138","title":"Comparison of Experimental and Theoretical Characteristics of LinearWaves in the Submerged Air Jet","year":2021,"lang":"en","type":"article","venue":"Proceedings of the ... International Conference on Fluid Flow, Heat and Mass Transfer","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"Russian Science Foundation","keywords":"Jet (fluid); Mechanics; Acoustics; Physics","score_opus":0.017451855486458185,"score_gpt":0.2580101909062933,"score_spread":0.2405583354198351,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3164304948","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9944296,0.0001134935,0.0004674597,0.00040609285,0.00017127041,0.0000932255,0.000059151138,0.000006280292,0.0042534377],"genre_scores_gemma":[0.9993988,0.00022012592,0.00028776433,0.00003097491,0.000029846677,0.000007319272,0.0000061778633,0.000009170586,0.0000098206965],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9992706,0.000006373925,0.0002942279,0.00011197265,0.00022592505,0.000090865855],"domain_scores_gemma":[0.9997169,0.000041081206,0.000014630626,0.00005521668,0.00015058253,0.000021612734],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00013676126,0.00010885757,0.00021691345,0.000037297923,0.00001931619,0.00001942484,0.0002048453,0.00005491817,0.000043489115],"category_scores_gemma":[0.000029965884,0.000073463816,0.00004498473,0.000060366314,0.00018182641,0.000044107648,0.000030383666,0.00015059147,1.4970624e-7],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000048168935,0.00008168339,0.005032744,0.00008277531,0.000029662258,3.472043e-7,0.0010686514,0.00006544126,0.72536904,0.26797217,0.000022006696,0.00022730354],"study_design_scores_gemma":[0.00046650937,0.0000881258,0.0075603626,0.00022138939,0.000029369607,0.000004659705,0.0017262301,0.4368186,0.5505099,0.0024112745,0.0000378438,0.00012569768],"about_ca_topic_score_codex":0.0000024874842,"about_ca_topic_score_gemma":0.0000015768296,"teacher_disagreement_score":0.43675315,"about_ca_system_score_codex":0.000010809445,"about_ca_system_score_gemma":0.000012169172,"threshold_uncertainty_score":0.29957676},"labels":[],"label_agreement":null},{"id":"W3164549964","doi":"10.1088/1742-6596/1909/1/012010","title":"Analytical Modeling of Modulated Rotating-Blade Noise : the Skipping Rope and the Darrieus Wind Turbine","year":2021,"lang":"en","type":"article","venue":"Journal of Physics Conference Series","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Agence Nationale de la Recherche","keywords":"Rope; Spectrogram; Airfoil; Aerodynamics; Stall (fluid mechanics); Acoustics; Turbine; Wind power; Noise (video); Marine engineering; Context (archaeology); Engineering; Computer science; Aerospace engineering; Structural engineering; Geology; Speech recognition; Artificial intelligence; Physics; Electrical engineering","score_opus":0.013254912426243819,"score_gpt":0.21603130096428086,"score_spread":0.20277638853803703,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3164549964","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8583526,0.00043359597,0.13996974,0.0004931589,0.00020032209,0.000054748645,0.000008840594,0.000010229083,0.000476782],"genre_scores_gemma":[0.99804175,0.00038062586,0.0013353167,0.000023015555,0.0001771176,5.696366e-7,0.000001708105,0.000016462078,0.000023411081],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99908835,0.000045625613,0.00041543035,0.00007942521,0.00022604146,0.000145113],"domain_scores_gemma":[0.9990553,0.000118982425,0.00014234819,0.00018021862,0.00045719626,0.000045922854],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000264711,0.00013113981,0.0003181039,0.00001912055,0.0000966399,0.000099436205,0.00019168542,0.000040499846,0.000010442047],"category_scores_gemma":[0.00013966432,0.00007809299,0.00009035436,0.00016090757,0.00019046653,0.00019322417,0.000072690695,0.0003897752,3.182765e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000353967,0.0000133122485,0.00008656282,0.000048669237,0.0001584999,0.000012183058,0.0013246735,0.96329826,0.008449015,0.021061257,0.000010840819,0.0055013383],"study_design_scores_gemma":[0.00041154225,0.000029756971,0.00017458684,0.00012718588,0.000096182725,0.00003884657,0.00086260954,0.98056936,0.0027943437,0.01478976,0.000014569063,0.00009128143],"about_ca_topic_score_codex":0.0000048180855,"about_ca_topic_score_gemma":0.0000074709133,"teacher_disagreement_score":0.13968919,"about_ca_system_score_codex":0.000012884769,"about_ca_system_score_gemma":0.00009083318,"threshold_uncertainty_score":0.31845397},"labels":[],"label_agreement":null},{"id":"W3164804625","doi":"10.1088/1742-6596/1909/1/012005","title":"Sweep-angle effect on low-order acoustic prediction for low-speed fans","year":2021,"lang":"en","type":"article","venue":"Journal of Physics Conference Series","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Noise (video); Airfoil; Acoustics; Automotive industry; Computational fluid dynamics; Trailing edge; Computer science; Physics; Simulation; Mechanics; Engineering; Aerospace engineering","score_opus":0.008988473527202933,"score_gpt":0.22072318192228096,"score_spread":0.21173470839507802,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3164804625","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.5222306,0.00007444343,0.47410852,0.00009183625,0.002082886,0.00015706786,0.00011954161,0.00006184055,0.0010732232],"genre_scores_gemma":[0.99772686,0.000115702016,0.0010644813,0.00003095366,0.0007687731,0.0000055597857,0.000025114685,0.00004078872,0.00022178442],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99904096,0.000024761597,0.0003361852,0.0001249596,0.0002457587,0.00022740038],"domain_scores_gemma":[0.9988841,0.00015716632,0.000121138895,0.00017697256,0.000581766,0.00007887149],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00014484474,0.00019772166,0.00034153464,0.00004105942,0.00008297812,0.000102249636,0.00014644224,0.0000877796,0.000034526918],"category_scores_gemma":[0.00013799101,0.00017920054,0.00014670713,0.00015457235,0.00004566859,0.00027087532,0.00002235811,0.0003126007,0.0000064856577],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00012540528,0.00012336925,0.000064590924,0.0005295627,0.00024600577,0.000042698834,0.0004621105,0.55594283,0.40204832,0.0056116516,0.0009937935,0.033809625],"study_design_scores_gemma":[0.0019187474,0.0017725833,0.00094218936,0.0009240061,0.00032525815,0.000071480084,0.0005721457,0.51020026,0.46941382,0.012509261,0.00077264215,0.0005776114],"about_ca_topic_score_codex":6.351385e-7,"about_ca_topic_score_gemma":0.0000060981724,"teacher_disagreement_score":0.4754962,"about_ca_system_score_codex":0.00007042108,"about_ca_system_score_gemma":0.00012542964,"threshold_uncertainty_score":0.7307586},"labels":[],"label_agreement":null},{"id":"W3165471595","doi":"10.1088/1742-6596/1909/1/012006","title":"Identification of Noise Sources in a Realistic Turbofan Rotor Using Large Eddy Simulation","year":2021,"lang":"en","type":"article","venue":"Journal of Physics Conference Series","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Turbofan; Acoustics; Noise (video); Aerodynamics; Rotor (electric); Trailing edge; Leading edge; Large eddy simulation; Physics; Helicopter rotor; Vortex; Frequency domain; Amplitude; Dynamic mode decomposition; Aeroacoustics; Blade (archaeology); Mechanics; Aerospace engineering; Vibration; Engineering; Structural engineering; Computer science; Turbulence; Optics; Sound pressure","score_opus":0.01792677841617344,"score_gpt":0.2596621382008514,"score_spread":0.24173535978467794,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3165471595","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6707862,0.00006270471,0.3288336,0.000009098905,0.00020706093,0.000034392848,0.00002189353,0.0000063362977,0.00003869279],"genre_scores_gemma":[0.9982654,0.000062984436,0.0014860632,0.0000032494745,0.00014389503,7.366067e-7,0.000006511566,0.000013373632,0.00001777305],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999164,0.000024933073,0.0004643403,0.00006459744,0.00017328547,0.00010884228],"domain_scores_gemma":[0.99917763,0.000046775498,0.00023443747,0.00011540265,0.00039691536,0.00002883321],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016250502,0.00008725634,0.00021333325,0.00005175682,0.000027584168,0.000048922313,0.00009278576,0.000042973883,0.000012121477],"category_scores_gemma":[0.000090335336,0.00008999512,0.000053862193,0.00017141686,0.000028107708,0.00030676342,0.000020537385,0.0001506625,5.189667e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000096457,0.000037312384,0.0005295335,0.000093663395,0.000020067486,0.000008845261,0.0006894776,0.82527477,0.16801333,0.0034218398,0.000002418012,0.0018991221],"study_design_scores_gemma":[0.00023182768,0.000023586483,0.0027680984,0.00017543041,0.00003760949,0.0000072642065,0.00068966864,0.92678416,0.061774787,0.0073563037,0.000036053127,0.00011522509],"about_ca_topic_score_codex":0.000004266112,"about_ca_topic_score_gemma":0.000025446057,"teacher_disagreement_score":0.32747918,"about_ca_system_score_codex":0.000044289558,"about_ca_system_score_gemma":0.00008365475,"threshold_uncertainty_score":0.36698946},"labels":[],"label_agreement":null},{"id":"W3168245730","doi":"10.1017/jfm.2021.418","title":"The exchanges between the mainstream in an open channel and a recirculating flow on its side at large Froude numbers","year":2021,"lang":"en","type":"article","venue":"Journal of Fluid Mechanics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University; York University","funders":"","keywords":"Froude number; Open-channel flow; Flow (mathematics); Mechanics; Channel (broadcasting); Mainstream; Computer science; Physics; Telecommunications","score_opus":0.028241537782020383,"score_gpt":0.26505284373594024,"score_spread":0.23681130595391986,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3168245730","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98699075,0.0013930955,0.009267733,0.00063881575,0.0008350969,0.00019131659,0.000050044164,0.000016615673,0.0006165262],"genre_scores_gemma":[0.9967476,0.0015616874,0.0011200293,0.00012200815,0.0003371792,0.0000042894508,0.0000056807344,0.00003978305,0.00006170584],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9988889,0.000084913765,0.00036752087,0.00012597391,0.00024781591,0.0002848443],"domain_scores_gemma":[0.99919903,0.00026151695,0.00010471736,0.00023749688,0.00010107999,0.000096173855],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0011248158,0.0001469435,0.00024253456,0.0000407667,0.00023568983,0.00012937254,0.00040638464,0.00009116596,0.000010373168],"category_scores_gemma":[0.00018294311,0.00009688055,0.000050143142,0.00015334254,0.000007992513,0.00014717139,0.00022983234,0.00040926173,0.0000022019085],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00020509685,0.0003096917,0.001320567,0.0002574244,0.0006894718,0.0011185813,0.007720296,0.754224,0.12375454,0.016594348,0.0031985836,0.09060739],"study_design_scores_gemma":[0.0006107143,0.00010265428,0.00058917137,0.00018335792,0.00003898111,0.000081029786,0.0009100833,0.9916805,0.0018002285,0.002596564,0.0012528667,0.00015386156],"about_ca_topic_score_codex":0.0000024402627,"about_ca_topic_score_gemma":0.00041194013,"teacher_disagreement_score":0.23745649,"about_ca_system_score_codex":0.00014952371,"about_ca_system_score_gemma":0.00003454662,"threshold_uncertainty_score":0.3950674},"labels":[],"label_agreement":null},{"id":"W3170464410","doi":"10.1615/tsfp2.1820","title":"LARGE EDDY SIMULATION OF THE NEAR FIELD OF ROUND JETS WITH VORTEX-GENERATING TABS","year":2001,"lang":"en","type":"article","venue":"Proceeding of Second Symposium on Turbulence and Shear Flow Phenomena","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Queen's University","funders":"","keywords":"Nozzle; Large eddy simulation; Vortex; Turbulence; Jet (fluid); Entrainment (biomusicology); Mechanics; Vortex ring; Braid; Field (mathematics); Physics; Materials science; Thermodynamics; Acoustics; Mathematics","score_opus":0.007437285427639365,"score_gpt":0.21409480520495516,"score_spread":0.2066575197773158,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3170464410","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9931144,0.00017038248,0.003524104,0.00003788338,0.00013937023,0.00016715028,0.00002091515,0.000019785271,0.0028060032],"genre_scores_gemma":[0.998502,0.0000752409,0.0011738566,0.00004047018,0.00008587448,0.000005085703,0.000002705844,0.000022451954,0.00009231763],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99913204,0.0000053059807,0.00029581875,0.0001657201,0.00020382047,0.00019729514],"domain_scores_gemma":[0.9995196,0.000069640824,0.000114941904,0.00014974408,0.0001050103,0.000041077463],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017342043,0.00015121278,0.00024035164,0.00004845148,0.00009620937,0.000027208853,0.00014182599,0.00006181994,0.000045295477],"category_scores_gemma":[0.000016985363,0.00011283511,0.00003963029,0.00017184379,0.000058031437,0.00013321034,0.00003800943,0.00016247293,4.8672e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00003134772,0.000048458052,0.0039762445,0.00041727826,0.000044237408,5.4106647e-7,0.0021941115,0.9554813,0.0364736,0.00045822913,0.000020587768,0.00085408],"study_design_scores_gemma":[0.00031184027,0.00020352862,0.0005692163,0.00020459056,0.00002449054,0.000002262556,0.00031644994,0.99171233,0.00623534,0.00018325748,0.0000979424,0.00013871989],"about_ca_topic_score_codex":0.0000036606436,"about_ca_topic_score_gemma":0.000005212973,"teacher_disagreement_score":0.036231074,"about_ca_system_score_codex":0.000016771672,"about_ca_system_score_gemma":0.000019772848,"threshold_uncertainty_score":0.46012822},"labels":[],"label_agreement":null},{"id":"W3175024409","doi":"10.1177/1475472x211023873","title":"Influence of the liner-type treatment on the trailing-edge noise generated by a flat plate","year":2021,"lang":"en","type":"article","venue":"International Journal of Aeroacoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Trailing edge; Noise (video); Physics; Acoustics; Optics; Dipole; Airfoil; Wind tunnel; Anechoic chamber; Materials science; Scattering; Directivity; Geometry; Mechanics; Antenna (radio); Mathematics","score_opus":0.010944151868659383,"score_gpt":0.22979931090810396,"score_spread":0.21885515903944458,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3175024409","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99268055,0.00027660298,0.0043982295,0.00047511264,0.0016586896,0.00005250088,0.00010777508,0.000011024768,0.0003395348],"genre_scores_gemma":[0.99787545,0.0006134402,0.0007010042,0.00016977573,0.00029683838,0.0000010535065,0.000008168636,0.000022347658,0.00031191928],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989005,0.0000294951,0.00043358782,0.00008045522,0.0004350746,0.00012091156],"domain_scores_gemma":[0.99856895,0.00019394356,0.0001754122,0.00018215048,0.00083340204,0.000046158977],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001327477,0.00014019944,0.0001632093,0.000041019557,0.000045136843,0.000044542987,0.00043298258,0.0000664158,0.000028263832],"category_scores_gemma":[0.00024304561,0.00008256435,0.00011523014,0.00014507514,0.000054965494,0.00004508524,0.000039601648,0.000269671,0.0000038365433],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000020921316,0.000054183914,0.00006270814,0.000005043108,0.00022746573,0.000059030757,0.00011281395,0.8113079,0.18579431,0.0002616648,0.001556688,0.00053727184],"study_design_scores_gemma":[0.0009838659,0.00022606248,0.0010090793,0.00028105904,0.00018015034,0.00029079695,0.00012386174,0.8438266,0.14804174,0.000371569,0.00443624,0.00022896127],"about_ca_topic_score_codex":0.0000032045746,"about_ca_topic_score_gemma":0.0000073205824,"teacher_disagreement_score":0.03775258,"about_ca_system_score_codex":0.00012493362,"about_ca_system_score_gemma":0.00011564209,"threshold_uncertainty_score":0.33668765},"labels":[],"label_agreement":null},{"id":"W3176009340","doi":"10.2514/6.2015-2686","title":"Aeroacoustic Simulations of a Simplified High-Lift Device Accounting for Installations Effects","year":2015,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Mitacs; Compute Canada","keywords":"Lift (data mining); Marine engineering; Computer science; Environmental science; Acoustics; Engineering; Physics","score_opus":0.018930311532665965,"score_gpt":0.2477233940656213,"score_spread":0.22879308253295533,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3176009340","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.42442533,0.000028353845,0.5719932,0.000015192515,0.00034974905,0.00029566925,0.000076252334,0.00016424153,0.0026520293],"genre_scores_gemma":[0.97596574,0.0000018623545,0.023733579,0.00002996578,0.00008579422,0.000020847343,0.00006953897,0.00002878402,0.000063879655],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993228,0.0000065458557,0.00024702694,0.00011256873,0.00012383297,0.00018726081],"domain_scores_gemma":[0.99905,0.00047167685,0.000039298626,0.00018233806,0.00018533808,0.00007133501],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00011529755,0.00011946604,0.00017003981,0.0000797268,0.000053906042,0.000025108982,0.0001034105,0.000075049546,0.0000122113],"category_scores_gemma":[0.0002920104,0.00011954034,0.00004180366,0.00018452434,0.000018374516,0.00009941653,0.000028138786,0.00007098078,0.000007442243],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000027244428,0.000016834587,0.0001281162,0.00013423226,0.000030617088,2.9447546e-7,0.00007485605,0.9868079,0.0068710917,0.004772591,0.00062774756,0.0005330256],"study_design_scores_gemma":[0.00049887,0.000025662142,0.00032800945,0.000020459933,0.000054541943,5.236977e-7,0.00005377356,0.99568254,0.00055316626,0.0021867212,0.00045210816,0.00014360728],"about_ca_topic_score_codex":0.000018474857,"about_ca_topic_score_gemma":0.000079975594,"teacher_disagreement_score":0.55154043,"about_ca_system_score_codex":0.000048685204,"about_ca_system_score_gemma":0.0000323836,"threshold_uncertainty_score":0.48747134},"labels":[],"label_agreement":null},{"id":"W3176189635","doi":"10.1515/ijnsns-2020-0071","title":"Dynamic characteristics of supersonic turbulent free jets from four types of circular nozzles","year":2021,"lang":"en","type":"article","venue":"International Journal of Nonlinear Sciences and Numerical Simulation","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Nozzle; Supersonic speed; Mechanics; Turbulence; Jet (fluid); Physics; Materials science; Classical mechanics; Thermodynamics","score_opus":0.013868239056213106,"score_gpt":0.26204252239588693,"score_spread":0.24817428333967384,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3176189635","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9010943,0.00046645195,0.09772173,0.00015092756,0.00044565683,0.000016102154,0.00007029181,0.0000039936713,0.000030542407],"genre_scores_gemma":[0.9857596,0.00033885802,0.013756294,0.000016580143,0.000109073015,1.0716905e-7,0.000010835443,0.000005472992,0.0000031675977],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991014,0.000014087533,0.00036127874,0.0000755538,0.00038092674,0.0000667587],"domain_scores_gemma":[0.9991451,0.0001870428,0.00015832936,0.00005993112,0.00041332043,0.000036266734],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012752095,0.000064043066,0.00016690722,0.00006360235,0.000021484155,0.00002635788,0.00020527311,0.000036663165,0.000038485075],"category_scores_gemma":[0.00022302572,0.000054966076,0.000057237354,0.00011680468,0.00006990339,0.00011067358,0.000038176182,0.00008293891,4.6487423e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000024097119,0.00008024841,0.0061101955,0.000031520492,0.00013631849,0.000040514988,0.00020069981,0.9596107,0.013813673,0.00009827749,0.000006224836,0.019847512],"study_design_scores_gemma":[0.00020888251,0.00004888166,0.020240176,0.000068974594,0.000021226275,0.000016691953,0.00003968778,0.97797513,0.0004784595,0.00068651803,0.00015906777,0.00005631919],"about_ca_topic_score_codex":0.000009691055,"about_ca_topic_score_gemma":0.0000026639134,"teacher_disagreement_score":0.08466531,"about_ca_system_score_codex":0.00002712531,"about_ca_system_score_gemma":0.00005051878,"threshold_uncertainty_score":0.22414516},"labels":[],"label_agreement":null},{"id":"W3183288673","doi":"10.2514/6.2021-2289","title":"Experimental and Analytical Investigation of the Distortion of Turbulence Interacting with a Porous Airfoil","year":2021,"lang":"en","type":"article","venue":"AIAA AVIATION 2021 FORUM","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"European Commission","keywords":"Airfoil; Turbulence; Porosity; Mechanics; Turbulence kinetic energy; Acoustics; Noise (video); Distortion (music); Physics; Materials science; Composite material; Computer science","score_opus":0.004824526458557909,"score_gpt":0.19886698428065266,"score_spread":0.19404245782209475,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3183288673","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98587984,0.000107980944,0.013374703,0.00013198974,0.0002001762,0.00004490715,0.000008484086,0.000009066258,0.00024284722],"genre_scores_gemma":[0.99927056,0.000008697614,0.00061971904,0.000015423666,0.000014595233,0.000003308083,0.000013462282,0.000008279982,0.000045960292],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995552,0.000013074536,0.00016484038,0.000080670085,0.000117694784,0.00006852167],"domain_scores_gemma":[0.99970996,0.00003613805,0.000065717635,0.00010921847,0.00005980454,0.000019143177],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00004771492,0.000056404835,0.0000819332,0.000018102546,0.000030606185,0.000009203604,0.000037332644,0.000028724857,0.00001990808],"category_scores_gemma":[0.00004542283,0.000045111672,0.00002028313,0.00012917697,0.000041500152,0.000084429535,0.0000322165,0.00006932607,3.7809576e-7],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000039030212,0.00011792821,0.28885537,0.00032986593,0.00018167708,0.0000103046095,0.0039702896,0.09748067,0.58873755,0.010426804,0.00049291784,0.009357586],"study_design_scores_gemma":[0.00031839652,0.000061990744,0.059173428,0.00024920166,0.00004643754,0.000017922435,0.0018276202,0.65453833,0.28311977,0.0004669341,0.000028932454,0.00015103893],"about_ca_topic_score_codex":0.000008523115,"about_ca_topic_score_gemma":0.000020469723,"teacher_disagreement_score":0.5570577,"about_ca_system_score_codex":0.00003665434,"about_ca_system_score_gemma":0.000017903354,"threshold_uncertainty_score":0.18396007},"labels":[],"label_agreement":null},{"id":"W3187671956","doi":"10.1115/1.4039920","title":"Particle Image Velocimetry Measurements of Aeroacoustic Sources of a Shallow Cavity in a Pipeline","year":2018,"lang":"en","type":"article","venue":"Journal of Pressure Vessel Technology","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"","keywords":"Particle image velocimetry; Strouhal number; Acoustics; Sound power; Acoustic source localization; Reynolds number; Aeroacoustics; Velocimetry; Physics; Mechanics; Geology; Acoustic wave; Sound pressure; Sound (geography); Turbulence","score_opus":0.011992522445877608,"score_gpt":0.23998587139860805,"score_spread":0.22799334895273043,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3187671956","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97087556,0.0017941955,0.0266186,0.000085990316,0.0002806121,0.00008428892,0.00001238453,0.000038566082,0.00020978854],"genre_scores_gemma":[0.99122375,0.000074001786,0.008576579,0.000005399091,0.000077072466,0.0000018782678,3.0966322e-7,0.00002332536,0.000017686756],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9986313,0.00002808713,0.00072282105,0.00010615439,0.00027554296,0.00023610085],"domain_scores_gemma":[0.99891496,0.000050602284,0.00032094045,0.0002492924,0.00042049916,0.00004368687],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00057966297,0.00013698178,0.00045750264,0.00036049282,0.000019826108,0.0000066684956,0.0004161397,0.00020843322,0.00003072001],"category_scores_gemma":[0.00035579441,0.00012569028,0.00006825682,0.00044729392,0.00026112888,0.00009596814,0.00007495365,0.00036775155,0.0000017278818],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000074380405,0.00031844268,0.043815225,0.00039785923,0.00026211576,0.000039419567,0.00042460553,0.02237224,0.9278272,0.00012619904,0.00039287278,0.0039494545],"study_design_scores_gemma":[0.0024729888,0.0007308597,0.014641886,0.00059791055,0.00045576517,0.0001398055,0.0005694749,0.3198752,0.6568041,0.0027927246,0.0005155333,0.000403758],"about_ca_topic_score_codex":0.000010211915,"about_ca_topic_score_gemma":0.000038516057,"teacher_disagreement_score":0.29750296,"about_ca_system_score_codex":0.000029264429,"about_ca_system_score_gemma":0.000038613667,"threshold_uncertainty_score":0.51255006},"labels":[],"label_agreement":null},{"id":"W3190434546","doi":"10.2514/1.j060163","title":"ACAT1 Fan Stage Broadband Noise Prediction Using Large-Eddy Simulation and Analytical Models","year":2022,"lang":"en","type":"article","venue":"AIAA Journal","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":22,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure; Université de Sherbrooke","funders":"Horizon 2020 Framework Programme","keywords":"Stage (stratigraphy); Broadband; Noise (video); Acoustics; Large eddy simulation; Environmental science; Computer science; Meteorology; Geology; Physics; Telecommunications; Artificial intelligence; Turbulence","score_opus":0.023772858852627147,"score_gpt":0.26202318295421173,"score_spread":0.2382503241015846,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3190434546","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.5648884,0.0001286975,0.43429527,0.000013948205,0.00030705688,0.00004281795,0.00006094574,0.000033688957,0.00022915295],"genre_scores_gemma":[0.99827063,0.000059840473,0.0012870868,0.000029021618,0.00022236227,0.0000015552872,0.000011015794,0.00002786454,0.000090621215],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99916583,0.000028925424,0.00022895138,0.00010732882,0.00025225527,0.00021667904],"domain_scores_gemma":[0.9996907,0.00003446683,0.000043323507,0.00009245979,0.000036078934,0.00010296218],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00030896172,0.000101880345,0.00011544354,0.00010126059,0.0003904437,0.000082884806,0.00007765098,0.000043520133,0.00014403313],"category_scores_gemma":[0.000013851392,0.000107978114,0.000041452702,0.00011330499,0.000014814751,0.00022583926,0.00006422386,0.00049305195,7.56425e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000008763828,0.000017895187,0.0007726755,0.00000958307,0.000030306837,0.000016110384,0.00018702206,0.99703205,0.00087104295,0.00032380325,0.00009652999,0.0006341954],"study_design_scores_gemma":[0.00037296617,0.00003449252,0.00063776836,0.000008099443,0.00004063698,0.00007305033,0.00016798997,0.9967777,0.0000063576836,0.0011490447,0.0006248879,0.00010699004],"about_ca_topic_score_codex":0.0000024044311,"about_ca_topic_score_gemma":0.000001436568,"teacher_disagreement_score":0.4333822,"about_ca_system_score_codex":0.00015108647,"about_ca_system_score_gemma":0.0000206583,"threshold_uncertainty_score":0.44032198},"labels":[],"label_agreement":null},{"id":"W3197983132","doi":"10.1016/j.jsv.2021.116423","title":"Parametric study on state-of-the-art analytical models for fan broadband interaction noise predictions","year":2021,"lang":"en","type":"article","venue":"Journal of Sound and Vibration","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":19,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke; École de Technologie Supérieure","funders":"Horizon 2020 Framework Programme; Centre Lyonnais d'Acoustique, Université de Lyon; Université de Lyon; Airbus; Natural Sciences and Engineering Research Council of Canada; Université de Sherbrooke; European Commission; FP7 Coherent Development of Research Policies; Agence Nationale de la Recherche; National Aeronautics and Space Administration","keywords":"Reynolds-averaged Navier–Stokes equations; Turbulence; Computation; Noise (video); Parametric statistics; Airfoil; Wake; Cascade; Mean flow; Parametric model; Aeroacoustics; Computational fluid dynamics; Computer science; Simulation; Acoustics; Mechanics; Engineering; Physics; Mathematics; Algorithm; Sound pressure","score_opus":0.022566660452201445,"score_gpt":0.2683300670704814,"score_spread":0.24576340661827994,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3197983132","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.61221194,0.00002544441,0.3871743,0.000033151293,0.0003500844,0.0000676195,0.000008580962,0.0000039113274,0.00012494487],"genre_scores_gemma":[0.99923736,0.000037038706,0.0005620544,0.000011030523,0.00009405119,0.0000015973109,0.000002685707,0.000007897065,0.00004627199],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994789,0.00001564413,0.00026618305,0.00005346928,0.00012821071,0.000057588437],"domain_scores_gemma":[0.9995932,0.00009785489,0.0000826842,0.00006602957,0.00012890676,0.000031299773],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012370832,0.000056313213,0.0001111929,0.00008007209,0.000056917608,0.00005066971,0.00003460137,0.000025135532,0.0000027251965],"category_scores_gemma":[0.00006240694,0.000042933498,0.000057049016,0.00015022978,0.000011212765,0.00018403048,0.000008286634,0.00013012665,2.2605957e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000031365267,0.0001505024,0.0009679907,0.000024572175,0.00008067081,0.0000014082567,0.0002356187,0.994894,0.0013303052,0.00036920374,0.00025358604,0.0016607281],"study_design_scores_gemma":[0.00038027077,0.00023380505,0.0052504744,0.00002873677,0.00007205904,0.000013250741,0.00028527912,0.9886424,0.00036525645,0.0046202047,0.00006315138,0.000045096956],"about_ca_topic_score_codex":4.1875185e-7,"about_ca_topic_score_gemma":0.000007300151,"teacher_disagreement_score":0.38702542,"about_ca_system_score_codex":0.00003265944,"about_ca_system_score_gemma":0.000016589504,"threshold_uncertainty_score":0.17507774},"labels":[],"label_agreement":null},{"id":"W3201363867","doi":"10.1177/1475472x211043339","title":"Swirling mean flow effects on locally reacting interstage liner","year":2021,"lang":"en","type":"article","venue":"International Journal of Aeroacoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Mechanics; Transmission loss; Physics; Duct (anatomy); Attenuation; Axial compressor; Parametric statistics; Optics; Mathematics; Thermodynamics","score_opus":0.0066020399960872245,"score_gpt":0.22524477150301891,"score_spread":0.2186427315069317,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3201363867","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.3081669,0.00022004418,0.675172,0.00030453547,0.0114654815,0.000052926862,0.000029454122,0.00007329391,0.0045153904],"genre_scores_gemma":[0.9672798,0.00025018267,0.029995449,0.00028259226,0.0019488159,8.1220776e-7,0.000012667643,0.000052722397,0.00017693774],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99847203,0.000026360363,0.0005401029,0.00012939492,0.00062711345,0.00020501671],"domain_scores_gemma":[0.998367,0.00037546843,0.00016437694,0.00015702589,0.0008245194,0.000111597285],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002817221,0.00018538411,0.0002383145,0.00016248565,0.000038162263,0.00012517227,0.0003796997,0.00010010118,0.000040378214],"category_scores_gemma":[0.0005309182,0.00017909822,0.0001574749,0.00010547488,0.000022593313,0.000121178935,0.00007050513,0.00062608975,0.000016017202],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00003443424,0.000066825385,0.000053384218,0.000044924145,0.00034431144,0.0016053629,0.00025693665,0.93026614,0.038993057,0.00032534028,0.0017693408,0.026239963],"study_design_scores_gemma":[0.0008036928,0.0001087497,0.00011375966,0.0006298543,0.00008807028,0.00043353467,0.00029029828,0.98037475,0.014293404,0.0005137734,0.0020862692,0.00026386743],"about_ca_topic_score_codex":9.279993e-7,"about_ca_topic_score_gemma":0.000006767797,"teacher_disagreement_score":0.65911293,"about_ca_system_score_codex":0.0002648432,"about_ca_system_score_gemma":0.00007160357,"threshold_uncertainty_score":0.7303414},"labels":[],"label_agreement":null},{"id":"W3201882004","doi":"10.1115/fedsm2021-65225","title":"Frequency Response of Synthetic Jets Emanating From an Array of Circular Orifices","year":2021,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto","funders":"University of Toronto","keywords":"Body orifice; Synthetic jet; Acoustics; Excitation; Jet (fluid); Helmholtz resonator; Physics; Optics; Mechanics; Resonator; Actuator; Engineering; Electrical engineering","score_opus":0.008815835339396068,"score_gpt":0.2242713266595742,"score_spread":0.21545549132017813,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3201882004","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9482863,0.00033249677,0.047751762,0.000020126807,0.00022245657,0.000035043897,0.00004477545,0.000059593585,0.003247447],"genre_scores_gemma":[0.9783203,0.00003215123,0.021532884,0.000007774273,0.000030500323,0.0000019558365,0.000013760985,0.000023873257,0.000036819667],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99925095,0.000049249946,0.00028381776,0.00014671739,0.00014860113,0.00012067701],"domain_scores_gemma":[0.9992604,0.00019317989,0.000044286433,0.0003689805,0.000091682945,0.000041463365],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021427548,0.00009502915,0.00019439824,0.000043503565,0.000019970768,0.000010992636,0.00013704419,0.00006590412,0.00028745967],"category_scores_gemma":[0.0001720962,0.0000964619,0.000051779225,0.00013253262,0.00003180796,0.000061556435,0.000015512855,0.000086534026,0.0000035593152],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000004085806,0.000029748711,0.00073452375,0.000068467154,0.000044230375,0.000017449132,0.00028398054,0.025073761,0.97207487,0.0012089525,0.000007289109,0.00045264157],"study_design_scores_gemma":[0.0002675361,0.000049887272,0.009681451,0.00019944845,0.00007845684,0.000006328827,0.0014718097,0.332289,0.64822984,0.0073197167,0.000049798684,0.00035671474],"about_ca_topic_score_codex":0.000058764363,"about_ca_topic_score_gemma":0.00004164953,"teacher_disagreement_score":0.32384503,"about_ca_system_score_codex":0.000020200345,"about_ca_system_score_gemma":0.000028200226,"threshold_uncertainty_score":0.39336023},"labels":[],"label_agreement":null},{"id":"W3210043672","doi":"10.32920/ryerson.14663562.v1","title":"Supersonic Windtunnel Noise Attenuation","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Wind tunnel; Supersonic wind tunnel; Acoustics; Aerodynamics; Silencer; Hypersonic wind tunnel; Sound pressure; Noise (video); Supersonic speed; Sound power; Acoustic attenuation; Transonic; Shock wave; Nozzle; Attenuation; Aeroacoustics; Physics; Engineering; Sound (geography); Computer science; Optics; Aerospace engineering; Mechanics; Inlet","score_opus":0.011608593298238615,"score_gpt":0.20915608502274616,"score_spread":0.19754749172450753,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3210043672","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.69536227,0.00076106127,0.26749206,0.00013842333,0.0041159377,0.00023890127,0.000051314055,0.00069021044,0.031149836],"genre_scores_gemma":[0.9899082,0.00040514395,0.008066484,0.00005275644,0.00031107973,0.000024498422,0.00029295054,0.00006557953,0.0008732868],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991528,0.000009684349,0.00020642852,0.0002610731,0.00016295878,0.00020709974],"domain_scores_gemma":[0.99939656,0.00002397068,0.000019384508,0.0004334546,0.000066962915,0.00005964808],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00008553585,0.00022287936,0.00022205668,0.000054416047,0.000030764073,0.00012190306,0.00019552857,0.00029436356,0.00038636138],"category_scores_gemma":[0.000020476315,0.00024028825,0.00011559627,0.00006421883,0.000014945093,0.00004228972,0.00022632624,0.00056133716,0.00005267173],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[5.8283143e-7,0.000015326117,0.0001383285,0.00025082316,0.00008271236,0.000018450266,0.0002143973,0.99088335,0.0038586475,0.0003494967,0.0020197032,0.0021681944],"study_design_scores_gemma":[0.000085677726,0.000003225381,0.0008334749,0.000084718326,0.000039319784,0.0000028202776,0.00014849116,0.9975213,0.0002718737,0.00040745872,0.00027406265,0.0003275922],"about_ca_topic_score_codex":0.000024123152,"about_ca_topic_score_gemma":0.00005316044,"teacher_disagreement_score":0.29454598,"about_ca_system_score_codex":0.0001299135,"about_ca_system_score_gemma":0.000047102443,"threshold_uncertainty_score":0.97986704},"labels":[],"label_agreement":null},{"id":"W3210939917","doi":"10.1016/j.jsv.2021.116534","title":"Sound localization and quantification analysis of an automotive engine cooling module","year":2021,"lang":"en","type":"article","venue":"Journal of Sound and Vibration","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":24,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"European Commission; Budapesti Műszaki és Gazdaságtudományi Egyetem","keywords":"Acoustics; Microphone; Aerodynamics; Radiator (engine cooling); Noise (video); Heat exchanger; Turbulence; Internal combustion engine cooling; Beamforming; Sound transmission class; Directivity; Engineering; Physics; Mechanics; Computer science; Mechanical engineering; Sound pressure; Electrical engineering; Electronic engineering; Combustion; Chemistry; Combustion chamber","score_opus":0.011350819889736213,"score_gpt":0.23993673968754606,"score_spread":0.22858591979780984,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3210939917","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.5106787,0.00020609885,0.48901087,0.000008192602,0.000061135965,0.000011635995,0.000005142607,0.000004881071,0.000013334894],"genre_scores_gemma":[0.99572134,0.00024023009,0.003906324,0.000010739794,0.00006677091,2.0676072e-7,0.00004298737,0.0000073892634,0.0000039906217],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994873,0.000018767088,0.00027540562,0.00006453227,0.000102746555,0.00005124982],"domain_scores_gemma":[0.9995055,0.000035446043,0.00011603857,0.000060392722,0.00024464718,0.000037929884],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000177556,0.00005808594,0.00016036644,0.00014227466,0.000046156947,0.00006092183,0.000023865634,0.00004663696,0.0000075526063],"category_scores_gemma":[0.00004767048,0.000056335062,0.000031763102,0.00027237434,0.000019672847,0.00027440832,0.000006234976,0.00006717549,8.5141664e-8],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000067591286,0.000023990679,0.0012119289,0.000037650374,0.00018827445,0.0000021963037,0.00041842886,0.98055166,0.01483727,0.0009381297,0.000003955454,0.0017797796],"study_design_scores_gemma":[0.00013321085,0.00003409101,0.011458604,0.000015330603,0.0002809442,0.0000104052215,0.000272426,0.98359144,0.0021037806,0.0020356425,0.000008325312,0.00005582914],"about_ca_topic_score_codex":0.0000015099366,"about_ca_topic_score_gemma":0.000022070144,"teacher_disagreement_score":0.48510453,"about_ca_system_score_codex":0.000017328588,"about_ca_system_score_gemma":0.000010645449,"threshold_uncertainty_score":0.22972772},"labels":[],"label_agreement":null},{"id":"W3215169953","doi":"10.1016/j.jsv.2021.116635","title":"On a three-dimensional investigation of airfoil turbulence-impingement noise and its reduction by leading-edge tubercles","year":2021,"lang":"en","type":"article","venue":"Journal of Sound and Vibration","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":19,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"H2020 Marie Skłodowska-Curie Actions; Horizon 2020 Framework Programme; Centre Lyonnais d'Acoustique, Université de Lyon; Agence Nationale de la Recherche; Université de Lyon; European Commission","keywords":"Airfoil; Turbulence; Nozzle; Mechanics; Physics; Acoustics; Noise reduction; Leading edge; Jet (fluid); Anechoic chamber; Noise (video); Aeroacoustics; Computer science; Sound pressure","score_opus":0.01172214337351557,"score_gpt":0.21666730833340314,"score_spread":0.20494516495988757,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3215169953","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9916049,0.0009664828,0.0068662725,0.00015880502,0.00029324173,0.000035029232,0.000006334677,0.000007106493,0.00006178479],"genre_scores_gemma":[0.99872786,0.00023071916,0.00087455346,0.000023757744,0.0001133156,5.6426813e-7,0.000007822854,0.000008230628,0.00001320503],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99943316,0.000013040521,0.00024761565,0.00007025898,0.00017427982,0.000061644816],"domain_scores_gemma":[0.9996352,0.00003226765,0.00009821548,0.000037942707,0.00014982061,0.000046549485],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016950957,0.00007169325,0.00011574005,0.000044204193,0.00005231109,0.000034457236,0.000021974573,0.000049044025,0.000008522925],"category_scores_gemma":[0.00004216136,0.00006654934,0.00002253326,0.00006625154,0.000023903074,0.0001990052,0.000010368325,0.0001125891,5.41836e-7],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00003471955,0.000040886836,0.00065284857,0.00019898286,0.00007053374,0.000004069763,0.00046211958,0.10834007,0.88331443,0.0020226766,0.001278918,0.0035797223],"study_design_scores_gemma":[0.0009089641,0.00037878245,0.008815505,0.0005178538,0.00009756917,0.00016659668,0.00017840393,0.8628391,0.10178695,0.02400077,0.000059710444,0.00024982286],"about_ca_topic_score_codex":9.864822e-7,"about_ca_topic_score_gemma":0.0000041938083,"teacher_disagreement_score":0.7815275,"about_ca_system_score_codex":0.00003480137,"about_ca_system_score_gemma":0.00002344941,"threshold_uncertainty_score":0.27138034},"labels":[],"label_agreement":null},{"id":"W352400371","doi":"","title":"MULTISPECTRUM ANALYSIS OF METHANE FROM 4100 TO 4635 CM$^{-1}$: SELF- AND AIR-BROADENING COEFFICIENTS (WIDTH AND SHIFTS)","year":2005,"lang":"en","type":"article","venue":"The Knowledge Bank (The Ohio State University)","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Jet propulsion; Research council; Atmospheric research; National laboratory; Research center; Aeronautics; Methane; Aerospace engineering; Engineering; Meteorology; Environmental science; Physics; Political science; Engineering physics; Law; Chemistry","score_opus":0.006292339999655706,"score_gpt":0.19840117291916817,"score_spread":0.19210883291951247,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W352400371","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.96466213,0.00041674115,0.029211624,0.00014983313,0.00011286267,0.00019511905,0.00010730353,0.000113653245,0.0050307135],"genre_scores_gemma":[0.9967416,0.00031204635,0.0019376632,0.000019826257,0.00004214164,5.991549e-7,0.000010709162,0.000024714649,0.0009106893],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99908507,0.000072395815,0.00017610806,0.0002512418,0.00013476411,0.00028042262],"domain_scores_gemma":[0.9991305,0.00029374848,0.00005350476,0.0003470782,0.000061951774,0.00011323474],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00022086357,0.00020135874,0.00031524268,0.00037147684,0.00015520363,0.000024967292,0.00037425038,0.00005728255,0.000045174682],"category_scores_gemma":[0.000020540512,0.00015798004,0.00007763289,0.0011030689,0.000102321865,0.00008379363,0.0002501197,0.00019942332,0.000020213152],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0001307856,0.00021015831,0.0019681866,0.00007958935,0.004225928,0.00003288151,0.03638525,0.88576245,0.007859089,0.004165626,0.00036212508,0.058817934],"study_design_scores_gemma":[0.0006432568,0.000040101848,0.010199361,0.000031334235,0.0014351903,0.0000011161155,0.0007123493,0.96875346,0.0006834335,0.00011374588,0.01706997,0.00031667066],"about_ca_topic_score_codex":0.000055297412,"about_ca_topic_score_gemma":0.00096233503,"teacher_disagreement_score":0.08299102,"about_ca_system_score_codex":0.00011094147,"about_ca_system_score_gemma":0.000016069811,"threshold_uncertainty_score":0.6442239},"labels":[],"label_agreement":null},{"id":"W4200251590","doi":"10.1017/jfm.2021.1018","title":"Experimental investigation of aerofoil tonal noise at low Mach number","year":2021,"lang":"en","type":"article","venue":"Journal of Fluid Mechanics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":32,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Airfoil; Trailing edge; Physics; Mach number; Acoustics; Aeroacoustics; Leading edge; Wake; Particle image velocimetry; Reynolds number; Mechanics; Chord (peer-to-peer); Noise (video); Aerodynamics; Sound pressure; Turbulence; Computer science","score_opus":0.008061705203221175,"score_gpt":0.21669050349008406,"score_spread":0.2086287982868629,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4200251590","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9758079,0.00062498776,0.021836298,0.00003423096,0.0012907785,0.000030668816,0.000014682935,0.000014269777,0.00034615063],"genre_scores_gemma":[0.99153674,0.0001913458,0.007865908,0.00005489201,0.0001994966,0.000001016013,0.0000078983,0.00002910262,0.00011362432],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9989798,0.000020306903,0.00045284716,0.00007779896,0.0003253455,0.00014392071],"domain_scores_gemma":[0.99939495,0.00003244202,0.00012197457,0.00013583894,0.00020738914,0.00010741303],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018648252,0.00011699495,0.00022336363,0.000039428585,0.00003269571,0.0000152114435,0.00012342037,0.000089572284,0.00029056886],"category_scores_gemma":[0.00003637557,0.000117946496,0.00012303596,0.0001188846,0.000012719554,0.00009969118,0.00005848934,0.00018501775,0.000011981872],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000012400927,0.00003129769,0.00006105023,0.000047799454,0.00005073477,0.000052663683,0.00018532154,0.028720025,0.967297,0.0017984951,0.0016012146,0.00014199014],"study_design_scores_gemma":[0.000394023,0.000042204425,0.000049292466,0.00008345669,0.0000302804,0.00023267626,0.0001345088,0.28193733,0.71610016,0.0006944647,0.00018935221,0.000112254624],"about_ca_topic_score_codex":6.892169e-7,"about_ca_topic_score_gemma":0.0000016898224,"teacher_disagreement_score":0.2532173,"about_ca_system_score_codex":0.00017624369,"about_ca_system_score_gemma":0.00006659129,"threshold_uncertainty_score":0.48097187},"labels":[],"label_agreement":null},{"id":"W4200484023","doi":"10.1177/0309524x211060548","title":"Experimental investigation of NACA-0012 airfoil instability noise with sawtooth trailing edges","year":2021,"lang":"en","type":"article","venue":"Wind Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Carleton University","funders":"","keywords":"Sawtooth wave; Airfoil; NACA airfoil; Trailing edge; Physics; Noise (video); Serration; Acoustics; Angle of attack; Instability; Reynolds number; Mechanics; Optics; Materials science; Aerodynamics; Turbulence; Engineering; Computer science; Telecommunications","score_opus":0.007876752716581793,"score_gpt":0.18137707451536492,"score_spread":0.17350032179878314,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4200484023","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9745761,0.0005970308,0.023495497,0.000013176611,0.00033544694,0.00007297817,0.000014054626,0.00019275551,0.0007029485],"genre_scores_gemma":[0.9890737,0.000015615124,0.010699002,0.000007457421,0.000106813815,0.0000074301697,0.000021278282,0.000052270712,0.000016440188],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99916947,0.0000073285696,0.00024489866,0.00018350067,0.00016679332,0.00022799837],"domain_scores_gemma":[0.999564,0.000036732097,0.000023872524,0.00023527436,0.000050610357,0.00008949252],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000091015645,0.0001847129,0.00021252244,0.000057463738,0.00003140954,0.000022125541,0.00009246436,0.00007902118,0.000030383124],"category_scores_gemma":[0.000026383881,0.00019299927,0.000047148435,0.00022876123,0.000045282864,0.00013599967,0.00003058999,0.00019006622,0.0000023234657],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000023286436,0.000012691881,0.0006468919,0.00014853764,0.0000266896,0.0000073172155,0.00039941634,0.6043115,0.39381248,0.00026338763,0.000008745696,0.0003599675],"study_design_scores_gemma":[0.0003631458,0.000031231997,0.0063950806,0.00014640823,0.000021246928,0.000015936155,0.00031110892,0.5208231,0.4713284,0.000021645546,0.00023333242,0.0003093449],"about_ca_topic_score_codex":0.0000045245183,"about_ca_topic_score_gemma":0.0000050928656,"teacher_disagreement_score":0.08348844,"about_ca_system_score_codex":0.000068687244,"about_ca_system_score_gemma":0.0000336731,"threshold_uncertainty_score":0.7870282},"labels":[],"label_agreement":null},{"id":"W4205200631","doi":"10.7901/2169-3358-2021.1.1141666","title":"Hydrodynamics and Mixing Characteristics in Different Sized Aspirator Bottles for the Water Accommodated Fraction (WAF) Tests","year":2021,"lang":"en","type":"article","venue":"International Oil Spill Conference Proceedings","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Bedford Institute of Oceanography; Fisheries and Oceans Canada","funders":"","keywords":"Aspirator; Mixing (physics); Fraction (chemistry); Materials science; Mechanics; Environmental science; Chromatography; Chemistry; Physics; Thermodynamics","score_opus":0.012869490163162927,"score_gpt":0.23320283656363727,"score_spread":0.22033334640047433,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4205200631","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99069524,0.000041938354,0.0062813554,0.0011109614,0.00075809663,0.00009849317,0.00005541844,0.00007925744,0.0008792415],"genre_scores_gemma":[0.9983126,0.0003591229,0.0006379182,0.000097837015,0.00022004417,0.000078302946,0.000095287614,0.000032476193,0.0001664089],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9990245,0.0000027826738,0.00032218703,0.00023329393,0.00018407675,0.0002331682],"domain_scores_gemma":[0.9993285,0.00012517221,0.000056998462,0.00007652643,0.0003659282,0.00004685937],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00013222023,0.00019724632,0.00021034088,0.000069715636,0.00007954709,0.00026513802,0.00021773393,0.00009747535,0.00004041848],"category_scores_gemma":[0.00019640136,0.00012749445,0.000043710646,0.00006142403,0.00004038352,0.00016897316,0.00010171569,0.00025082845,0.0000039079396],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00014649524,0.00022243158,0.060549203,0.0006318513,0.00043840424,0.000030335681,0.0017665447,0.00202492,0.82014495,0.02138696,0.00031861468,0.09233927],"study_design_scores_gemma":[0.00050805707,0.000017412764,0.025913391,0.00012523822,0.000027886881,0.000013000056,0.00018128278,0.96478534,0.0038392534,0.0021937583,0.0021589636,0.00023643915],"about_ca_topic_score_codex":0.000009234557,"about_ca_topic_score_gemma":0.00006358847,"teacher_disagreement_score":0.9627604,"about_ca_system_score_codex":0.00012171079,"about_ca_system_score_gemma":0.000019218734,"threshold_uncertainty_score":0.5199073},"labels":[],"label_agreement":null},{"id":"W4205750851","doi":"10.22215/etd/2021-14704","title":"Aerodynamic and Aeroacoustic Analyses of Vertical-Axis Wind Turbines","year":2021,"lang":"en","type":"dissertation","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Carleton University","funders":"","keywords":"Vertical axis wind turbine; Aerodynamics; Wake; Turbine; Wind power; Noise (video); Marine engineering; Aerospace engineering; Vortex; Torque; Engineering; Computational fluid dynamics; Vertical axis; Acoustics; Wind tunnel; Physics; Mechanics; Computer science; Electrical engineering","score_opus":0.012863240556672992,"score_gpt":0.2672415912788733,"score_spread":0.25437835072220033,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4205750851","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9792875,0.0029111365,0.002183207,0.000004379524,0.0009609403,0.00012130519,0.000045616016,0.000114524904,0.014371396],"genre_scores_gemma":[0.9937017,0.001190024,0.0013586227,0.000007712858,0.00007893891,0.0000055926844,0.0007732937,0.00008128638,0.00280286],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99879754,0.000013521904,0.0004387385,0.000290097,0.00022809124,0.00023199245],"domain_scores_gemma":[0.99931335,0.00011014938,0.00003917902,0.00031015542,0.0001441611,0.00008299539],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.000061015766,0.00033115366,0.0005484719,0.00014867268,0.00003773883,0.00004236149,0.0001402897,0.0003149179,0.00022679735],"category_scores_gemma":[0.00009081777,0.00031418534,0.00011672266,0.00022568202,0.000040986633,0.000046418485,0.000025782407,0.00028808785,0.0000049282603],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00004607662,0.0001538425,0.00037359365,0.0067000906,0.0016061718,0.00009107275,0.00065257103,0.2612782,0.7174458,0.001479324,0.001891948,0.008281322],"study_design_scores_gemma":[0.00038116405,0.000058138794,0.017011689,0.0005251817,0.0010156122,0.000008843838,0.001270657,0.9707424,0.0074949083,0.00051048194,0.000058646336,0.00092227105],"about_ca_topic_score_codex":0.000048108228,"about_ca_topic_score_gemma":0.00047554757,"teacher_disagreement_score":0.70995086,"about_ca_system_score_codex":0.000035645855,"about_ca_system_score_gemma":0.00003927279,"threshold_uncertainty_score":0.99993104},"labels":[],"label_agreement":null},{"id":"W4206909643","doi":"10.22215/etd/2021-14700","title":"Experimental and Numerical Investigation of Bio-Inspired Airfoil Trailing-Edge Designs for Noise Reduction","year":2021,"lang":"en","type":"dissertation","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Carleton University","funders":"","keywords":"Sawtooth wave; Airfoil; Serration; Trailing edge; Aerodynamics; Noise (video); Acoustics; Wing; Leading edge; Engineering; Noise reduction; Aeroacoustics; Structural engineering; Physics; Aerospace engineering; Computer science; Sound pressure","score_opus":0.019229698595242522,"score_gpt":0.25327555533915436,"score_spread":0.23404585674391185,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4206909643","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.94999546,0.0010312455,0.045775387,0.000009879251,0.001442619,0.0003746729,0.00004411093,0.00012786778,0.0011987421],"genre_scores_gemma":[0.98352623,0.000058260568,0.013666044,0.0000050586577,0.00015534043,0.00008581811,0.0015963183,0.00006857042,0.0008383635],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99915344,0.000011134823,0.00033523265,0.00023893523,0.000119279044,0.00014199257],"domain_scores_gemma":[0.9996082,0.000032280594,0.00007281365,0.0001285408,0.000090901965,0.000067271816],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00006919089,0.00021309391,0.00028023947,0.00008731593,0.000052649186,0.000027153574,0.0000634477,0.00025349378,0.00002902918],"category_scores_gemma":[0.000025000076,0.00023373602,0.00008298657,0.00011215746,0.000029531137,0.00006413242,0.0000069761886,0.00012660376,7.844037e-7],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000024093819,0.0000252277,0.000012986209,0.00051268854,0.000059234797,7.6913466e-7,0.0010952246,0.004096578,0.9908977,0.00059768,0.00039800914,0.0022798025],"study_design_scores_gemma":[0.00038769958,0.000101223726,0.00035606336,0.00015728152,0.000097655466,0.0000046405858,0.0026559394,0.3208427,0.6747368,0.0002114262,0.00007814809,0.00037042607],"about_ca_topic_score_codex":0.00001241507,"about_ca_topic_score_gemma":0.0000074436507,"teacher_disagreement_score":0.31674615,"about_ca_system_score_codex":0.000046285022,"about_ca_system_score_gemma":0.00004818248,"threshold_uncertainty_score":0.9531478},"labels":[],"label_agreement":null},{"id":"W4207077983","doi":"10.22215/etd/2021-14822","title":"Experimental Wind Tunnel Testing and Numerical Optimization Studies for Airfoil Trailing Edge Noise Reduction","year":2021,"lang":"en","type":"dissertation","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Carleton University","funders":"","keywords":"Airfoil; Serration; Wind tunnel; Trailing edge; Anechoic chamber; Noise (video); Engineering; Acoustics; NACA airfoil; Noise reduction; Leading edge; Subsonic and transonic wind tunnel; Structural engineering; Aerospace engineering; Transonic; Aerodynamics; Physics; Computer science; Mechanics; Turbulence; Reynolds number","score_opus":0.02594250011736057,"score_gpt":0.2795030821000933,"score_spread":0.25356058198273274,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4207077983","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7815484,0.014576945,0.18567793,0.000026228749,0.008364788,0.0011306931,0.0000625545,0.00072139147,0.007891102],"genre_scores_gemma":[0.8719115,0.00029169628,0.12446484,0.000007138432,0.0005970828,0.000091354974,0.00077852333,0.00012680757,0.0017310044],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9990562,0.000008268154,0.00031283527,0.0003107657,0.000115326344,0.00019660077],"domain_scores_gemma":[0.99949867,0.000108653454,0.0000599398,0.00010626508,0.0001757814,0.00005067272],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.000064885375,0.00026869273,0.00031850056,0.000071197865,0.00015765776,0.00006719473,0.00005489741,0.00018599269,0.000017194296],"category_scores_gemma":[0.00016668448,0.00028796608,0.000060125123,0.00012748159,0.000018137118,0.00009333077,0.000015305523,0.000174583,6.291766e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000012841881,0.00003013868,0.000003232983,0.00049950567,0.00011820611,0.0000022394456,0.0012000906,0.92141956,0.072663985,0.00007256535,0.00024683028,0.003730805],"study_design_scores_gemma":[0.0002653773,0.00004526514,0.000047421894,0.00022048716,0.000095611365,0.000010323999,0.011478363,0.9795923,0.007813202,0.000040349634,0.000025888003,0.00036537662],"about_ca_topic_score_codex":0.0000048800953,"about_ca_topic_score_gemma":0.0000047909284,"teacher_disagreement_score":0.09036319,"about_ca_system_score_codex":0.000080697006,"about_ca_system_score_gemma":0.00002735291,"threshold_uncertainty_score":0.99995726},"labels":[],"label_agreement":null},{"id":"W4210248727","doi":"10.1063/5.0071023","title":"The dynamics of an axisymmetric turbulent jet in ambient turbulence interpreted from the passive scalar field statistics","year":2022,"lang":"en","type":"article","venue":"Physics of Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":17,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Physics; Turbulence; Entrainment (biomusicology); Scalar (mathematics); Jet (fluid); Mechanics; Turbulence kinetic energy; Classical mechanics; Geometry","score_opus":0.005170452816178433,"score_gpt":0.21075387051333508,"score_spread":0.20558341769715666,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4210248727","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.83158875,0.00037208537,0.16546874,0.00021116521,0.00065549527,0.000246014,0.0012917595,0.000032402473,0.00013359862],"genre_scores_gemma":[0.9979696,0.00017059849,0.0015810172,0.000054459906,0.000051007268,0.000029494591,0.00011121444,0.000026079066,0.000006474073],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9988675,0.00006656682,0.00035966124,0.00015231714,0.00034974358,0.00020419554],"domain_scores_gemma":[0.9985495,0.0007816952,0.00008192547,0.0004804769,0.00007310438,0.000033265325],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018735159,0.00014598061,0.00020445994,0.00003688726,0.000107811764,0.000021428454,0.0006393619,0.000033902572,0.000017786704],"category_scores_gemma":[0.00009276689,0.00010781886,0.000060909908,0.00041590838,0.00008035217,0.00005040964,0.00020453893,0.00039434843,8.176573e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000088737135,0.00036847297,0.0019917737,0.00009140794,0.00021774576,0.000020762047,0.003036613,0.8357409,0.0070210705,0.056569576,0.0023994567,0.092453465],"study_design_scores_gemma":[0.00015898481,0.00013557376,0.0010804172,0.000022107353,0.000023850564,6.255947e-7,0.00044050912,0.9821515,0.0014969098,0.01428944,0.00007896772,0.00012113238],"about_ca_topic_score_codex":0.00027008372,"about_ca_topic_score_gemma":0.00012058861,"teacher_disagreement_score":0.16638091,"about_ca_system_score_codex":0.0001299207,"about_ca_system_score_gemma":0.000027182989,"threshold_uncertainty_score":0.43967253},"labels":[],"label_agreement":null},{"id":"W4210355909","doi":"10.4236/aast.2022.71001","title":"Aeroacoustic Investigation of Trailing-Edge Finlets","year":2022,"lang":"en","type":"article","venue":"Advances in Aerospace Science and Technology","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Carleton University","funders":"","keywords":"Airfoil; Trailing edge; Angle of attack; Wind tunnel; Noise (video); Acoustics; Noise reduction; Reduction (mathematics); Subsonic and transonic wind tunnel; Enhanced Data Rates for GSM Evolution; Aerodynamics; Materials science; Physics; Mechanics; Engineering; Geometry; Computer science; Transonic; Mathematics; Telecommunications","score_opus":0.003930986664476241,"score_gpt":0.21041732649485803,"score_spread":0.20648633983038178,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4210355909","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99298286,0.0024003522,0.0029215033,0.00024487881,0.00038862225,0.00011556004,0.00000869306,0.00012385407,0.0008136799],"genre_scores_gemma":[0.99589276,0.00050726766,0.0035122114,0.00002216977,0.0000064139394,0.000032667816,0.0000010596285,0.000008674877,0.00001674655],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99915904,0.000006232015,0.00016055955,0.00021018558,0.0002241992,0.00023975824],"domain_scores_gemma":[0.99964863,0.00004550764,0.000040260664,0.00018163059,0.000053932206,0.000030023848],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00036539364,0.00008538388,0.00013351515,0.00037146808,0.00014891231,0.000008150402,0.0003165331,0.000041944648,0.000008199937],"category_scores_gemma":[0.00014998051,0.000092682574,0.000008311633,0.0018508636,0.00091768353,0.00020056411,0.00015593383,0.00025110596,6.742322e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000045655383,0.000028308961,0.016348245,0.000105132545,0.000004300635,0.000013354228,0.00052929105,0.56205124,0.33289126,0.048054673,0.000059633996,0.03990999],"study_design_scores_gemma":[0.00061007205,0.00030896137,0.0021891713,0.000055367138,0.0000128725,0.000039608552,0.0024778969,0.920042,0.023892201,0.046634264,0.0032597224,0.00047786479],"about_ca_topic_score_codex":0.0000020112545,"about_ca_topic_score_gemma":0.00003033422,"teacher_disagreement_score":0.35799074,"about_ca_system_score_codex":0.000066008484,"about_ca_system_score_gemma":0.000050863942,"threshold_uncertainty_score":0.37794858},"labels":[],"label_agreement":null},{"id":"W4210665188","doi":"10.1016/j.jsv.2022.116762","title":"Surface pressure spectrum variation with Mach number on a CD airfoil","year":2022,"lang":"en","type":"article","venue":"Journal of Sound and Vibration","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":19,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"General Fusion (Canada); Université de Sherbrooke","funders":"Australian Research Council","keywords":"Mach number; Airfoil; Reynolds number; Mach wave; Boundary layer; Wavenumber; Amplitude; Physics; Mechanics; Trailing edge; Sound pressure; Acoustics; Leading edge; Optics; Turbulence","score_opus":0.005361662914798901,"score_gpt":0.19893418119474962,"score_spread":0.19357251827995073,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4210665188","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.940035,0.00008015597,0.058225114,0.00017787071,0.00033240297,0.00004752225,0.000010846834,0.000016881015,0.0010742355],"genre_scores_gemma":[0.9981757,0.000027264543,0.0014804791,0.00003723001,0.00016055699,6.667012e-7,0.0000040417676,0.000013067875,0.00010103696],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99952984,0.000017768118,0.00014007093,0.00005123314,0.00019060253,0.00007048178],"domain_scores_gemma":[0.99979806,0.000024944813,0.000076202654,0.00004882551,0.000023468048,0.000028471954],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015097608,0.00006355075,0.000084407926,0.00002587813,0.00010990898,0.00005079611,0.000042791446,0.000021711432,0.00010392815],"category_scores_gemma":[0.0000043791356,0.00005327371,0.000018563222,0.00006969753,0.0000070588026,0.00012777024,0.000010271606,0.00020952245,0.0000013015555],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00006404098,0.000029283896,0.00091338507,0.000022580258,0.000053378837,0.000007504106,0.00035715432,0.9922722,0.0028090016,0.0030138413,0.0003040574,0.000153554],"study_design_scores_gemma":[0.0006569751,0.000485033,0.009365135,0.000020515774,0.000074107236,0.00016638049,0.00018679792,0.98102075,0.000104081235,0.005764524,0.0020010767,0.00015461333],"about_ca_topic_score_codex":0.0000022049003,"about_ca_topic_score_gemma":0.000005109115,"teacher_disagreement_score":0.058140684,"about_ca_system_score_codex":0.000034587054,"about_ca_system_score_gemma":0.000012204765,"threshold_uncertainty_score":0.2172439},"labels":[],"label_agreement":null},{"id":"W4211131378","doi":"10.1063/5.0079921","title":"Circular turbulent wall jets in quiescent and coflowing surroundings","year":2022,"lang":"en","type":"article","venue":"Physics of Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Physics; Mechanics; Jet (fluid); Turbulence; Entrainment (biomusicology)","score_opus":0.009260677595422189,"score_gpt":0.20452336137184718,"score_spread":0.195262683776425,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4211131378","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99421215,0.00055847137,0.004561992,0.00006119054,0.00020406244,0.00008841041,0.000011176546,0.000042233092,0.0002603227],"genre_scores_gemma":[0.9994423,0.00012642273,0.00028753016,0.000026283971,0.00005390884,0.000014112953,0.000012027741,0.000027077062,0.0000103849525],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993059,0.000013045601,0.00017783571,0.00012565732,0.00019706473,0.00018050584],"domain_scores_gemma":[0.9997606,0.000029118692,0.000015813795,0.00014632974,0.000014691976,0.000033393666],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015927496,0.00010389025,0.00016428872,0.000055785535,0.000052356507,0.000012928738,0.00012254904,0.00001948419,0.000009723224],"category_scores_gemma":[0.000008320656,0.00012625499,0.000042157117,0.00018786029,0.000024721425,0.000057479712,0.00009758881,0.00018199488,9.000335e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000011581306,0.00019439725,0.0072708996,0.00044850665,0.00008787671,0.00003713723,0.0027462635,0.7134657,0.25169116,0.017682083,0.00032059135,0.006043805],"study_design_scores_gemma":[0.000453599,0.000044433968,0.0028958083,0.00003959859,0.000016860015,0.000005732643,0.00016768948,0.9861515,0.0022488034,0.0063979165,0.0013064372,0.00027158987],"about_ca_topic_score_codex":0.000031608848,"about_ca_topic_score_gemma":0.0000013477363,"teacher_disagreement_score":0.27268586,"about_ca_system_score_codex":0.0001516424,"about_ca_system_score_gemma":0.000016013631,"threshold_uncertainty_score":0.5148529},"labels":[],"label_agreement":null},{"id":"W4213241436","doi":"10.1063/5.0072554","title":"Flow features of shallow cylindrical cavities subject to grazing flow","year":2022,"lang":"en","type":"article","venue":"Physics of Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto","funders":"Natural Sciences and Engineering Research Council of Canada; Bombardier","keywords":"Physics; Mechanics; Flow (mathematics); Hele-Shaw flow; Flapping; Mean flow; Flow visualization; Optics; Asymmetry; Amplitude; Open-channel flow; Orientation (vector space); Reynolds number; Geometry; Turbulence; Thermodynamics; Wing","score_opus":0.009077112158672735,"score_gpt":0.21734842811034427,"score_spread":0.20827131595167153,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4213241436","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.89051414,0.0006612524,0.09888285,0.000085298656,0.0015334039,0.00030243647,0.0006655639,0.00020504673,0.0071500074],"genre_scores_gemma":[0.9866348,0.000023571245,0.012949993,0.000031955882,0.00018144542,0.000026625974,0.000038332008,0.0000481037,0.00006516785],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99897933,0.000019648609,0.0002475406,0.00015876518,0.0003555705,0.00023911956],"domain_scores_gemma":[0.99948096,0.000079133904,0.000027485077,0.0002933908,0.000058631653,0.000060385784],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012894216,0.00016203066,0.00029982545,0.00006646711,0.000082691244,0.000011765238,0.00031458566,0.000035870995,0.000032169108],"category_scores_gemma":[0.000022879483,0.00018114965,0.00013438602,0.00029307796,0.00003809952,0.000052318694,0.00018345601,0.00025909906,0.000002906948],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000013713527,0.000060034552,0.00018471798,0.00010684508,0.000060527487,0.0000043656623,0.0008588076,0.92084074,0.064259924,0.002889486,0.0013812565,0.009339568],"study_design_scores_gemma":[0.00023026414,0.00014150064,0.001226624,0.000028985933,0.000040511433,0.0000033097028,0.0002119297,0.98383105,0.009822874,0.003659449,0.00051443244,0.000289063],"about_ca_topic_score_codex":0.000025051702,"about_ca_topic_score_gemma":0.000013011142,"teacher_disagreement_score":0.09612066,"about_ca_system_score_codex":0.00006980411,"about_ca_system_score_gemma":0.000024991154,"threshold_uncertainty_score":0.7387068},"labels":[],"label_agreement":null},{"id":"W4220891058","doi":"10.1063/5.0083241","title":"Artificial neural networks modeling of wall pressure spectra beneath turbulent boundary layers","year":2022,"lang":"en","type":"article","venue":"Physics of Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":43,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"École Centrale de Lyon; Université de Sherbrooke","keywords":"Artificial neural network; Boundary layer; Turbulence; Pressure gradient; Adverse pressure gradient; Sensitivity (control systems); Boundary (topology); Physics; Range (aeronautics); Flow (mathematics); Spectral line; Set (abstract data type); Machine learning; Artificial intelligence; Flow separation; Mechanics; Computer science; Aerospace engineering; Mathematical analysis; Mathematics; Engineering","score_opus":0.012159575737501078,"score_gpt":0.20936400457492388,"score_spread":0.1972044288374228,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4220891058","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7711338,0.0013005695,0.22577798,0.00004439268,0.00070950226,0.00016964764,0.00009681455,0.00010345244,0.00066388835],"genre_scores_gemma":[0.998684,0.000044057815,0.0008887997,0.000018008262,0.00025715286,0.000011239518,0.00003958395,0.000044508335,0.000012634637],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99901056,0.000016440377,0.00030667888,0.00015207715,0.00027995044,0.0002342859],"domain_scores_gemma":[0.9995832,0.000024923154,0.000040935956,0.0002647588,0.000045503388,0.000040699062],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000113766284,0.00014864128,0.00023967143,0.00003101161,0.00009539746,0.000014409335,0.00025223428,0.00003617153,0.00003419124],"category_scores_gemma":[0.0000032390487,0.00017229744,0.000121798286,0.00015027513,0.000036538055,0.00006442483,0.00009852753,0.000311302,4.1145657e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000014648367,0.000059886843,0.000030922558,0.000058297297,0.000075438424,0.0000027083095,0.00025767053,0.9855019,0.009278464,0.003154816,0.0001563182,0.001408953],"study_design_scores_gemma":[0.00008391787,0.000056657664,0.000011560156,0.000008359893,0.000059014925,0.0000014149807,0.00004418372,0.99437773,0.0006277605,0.0044686277,0.00010600647,0.00015475323],"about_ca_topic_score_codex":0.000024631108,"about_ca_topic_score_gemma":0.000001981106,"teacher_disagreement_score":0.22755027,"about_ca_system_score_codex":0.000037602873,"about_ca_system_score_gemma":0.00001891053,"threshold_uncertainty_score":0.7026085},"labels":[],"label_agreement":null},{"id":"W4220971174","doi":"10.1063/5.0084060","title":"The third golden age of aeroacoustics","year":2022,"lang":"en","type":"article","venue":"Physics of Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":66,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Computational aeroacoustics; Aeroacoustics; Airfoil; Physics; Jet noise; Noise (video); Trailing edge; Airframe; Acoustics; Aerospace engineering; Supersonic speed; Aerodynamics; Wind tunnel; Mechanics; Computer science; Engineering; Sound pressure","score_opus":0.009437695543355577,"score_gpt":0.20900126574399752,"score_spread":0.19956357020064194,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4220971174","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7147884,0.001468333,0.2389868,0.00012064304,0.0028858692,0.00041401866,0.0004910987,0.0002443046,0.04060052],"genre_scores_gemma":[0.99849397,0.00010974346,0.0010272801,0.000011281754,0.00009999741,0.000013009629,0.00001604739,0.000026910984,0.00020174302],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992926,0.000013953262,0.00021029336,0.00007389031,0.00025860002,0.00015062444],"domain_scores_gemma":[0.9994687,0.00011568749,0.000035740337,0.0003129213,0.000044799748,0.00002218529],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015672769,0.00008962621,0.00014709034,0.000014453309,0.00011049686,0.000008620019,0.00034633564,0.000018633711,0.000010239498],"category_scores_gemma":[0.000016340848,0.000079266065,0.00007544675,0.00015807815,0.00007554001,0.00002434165,0.000147102,0.00018418072,0.0000018034505],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000067933997,0.00005851634,0.00007610301,0.00008483063,0.00008938468,0.0000040286022,0.00045724472,0.7782809,0.16615817,0.04420642,0.0052767294,0.0053008418],"study_design_scores_gemma":[0.0002046357,0.00007831571,0.00023355067,0.000010150922,0.000053579817,0.0000013628396,0.00027924764,0.9661496,0.0039298045,0.022123074,0.006751653,0.00018500719],"about_ca_topic_score_codex":0.0000075184435,"about_ca_topic_score_gemma":0.0000013930606,"teacher_disagreement_score":0.2837056,"about_ca_system_score_codex":0.000033259057,"about_ca_system_score_gemma":0.000015440719,"threshold_uncertainty_score":0.32323763},"labels":[],"label_agreement":null},{"id":"W4224943438","doi":"10.3390/jmse10050590","title":"Numerical Study on the Effect of Port Orientation on Multiple Inclined Dense Jets","year":2022,"lang":"en","type":"article","venue":"Journal of Marine Science and Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":16,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Wilfrid Laurier University; University of Ottawa","funders":"Natural Sciences and Engineering Research Council of Canada; Mitacs","keywords":"Dilution; Turbulence; Outfall; Mechanics; Dispersion (optics); Mixing (physics); Jet (fluid); Orientation (vector space); Normalization (sociology); Physics; Environmental science; Simulation; Mathematics; Computer science; Optics; Geometry; Thermodynamics","score_opus":0.006413111861988927,"score_gpt":0.22533642614965887,"score_spread":0.21892331428766995,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4224943438","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99809927,0.0000071168242,0.001014679,0.00003368968,0.00056482124,0.00010501791,0.0000011993033,0.000012576559,0.0001616518],"genre_scores_gemma":[0.9997453,0.000004519982,0.00016294126,0.000011291915,0.000055444296,0.00000509413,2.8922577e-7,0.000010095279,0.0000050377876],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99901354,0.000017588178,0.00023159689,0.000079257006,0.0005304339,0.00012759173],"domain_scores_gemma":[0.9994018,0.00032189302,0.00006468663,0.00010839378,0.000052064337,0.00005117301],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.001428269,0.0000877782,0.00014732042,0.00016365871,0.00011769834,0.000020389845,0.0001977839,0.000009796073,0.000011053909],"category_scores_gemma":[0.0005016113,0.00005953019,0.00003142369,0.000371855,0.000026060125,0.00006985626,0.000112374706,0.00028575372,3.4495716e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00003860954,0.000035974557,0.011742629,0.000013486251,0.000015955828,0.00002151736,0.00019297839,0.97573495,0.009281324,0.000048770045,0.000036431764,0.0028373674],"study_design_scores_gemma":[0.0005762567,0.002039155,0.08010751,0.000017039933,0.000020763333,0.000041944953,0.00021319627,0.9145269,0.0022530938,0.00001448988,0.00009050864,0.00009915767],"about_ca_topic_score_codex":0.0000033899278,"about_ca_topic_score_gemma":2.5338477e-7,"teacher_disagreement_score":0.06836488,"about_ca_system_score_codex":0.00008373817,"about_ca_system_score_gemma":0.00001736572,"threshold_uncertainty_score":0.24275707},"labels":[],"label_agreement":null},{"id":"W4225592327","doi":"10.22215/etd/2021-14855","title":"Modelling of Wall Pressure Fluctuations Induced by Turbulent Boundary Layer Flow","year":2021,"lang":"en","type":"dissertation","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Carleton University","funders":"","keywords":"Turbulence; Spectral density; Boundary layer; Pressure gradient; Adverse pressure gradient; Mechanics; Range (aeronautics); Boundary (topology); Flow (mathematics); Wind tunnel; Physics; Statistical physics; Meteorology; Mathematics; Materials science; Flow separation; Statistics; Mathematical analysis","score_opus":0.01456120657503584,"score_gpt":0.22721200730840205,"score_spread":0.2126508007333662,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4225592327","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.65689665,0.011287519,0.27228624,0.000064996486,0.0039136894,0.00077091594,0.00052339846,0.00053848414,0.0537181],"genre_scores_gemma":[0.9618152,0.0008454741,0.010887977,0.000023318258,0.00012958888,0.000042415064,0.0070676156,0.00015316613,0.019035263],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9988664,0.000010906728,0.00039729656,0.00023983521,0.0002824483,0.00020312438],"domain_scores_gemma":[0.99933505,0.000034503697,0.00006529129,0.00031188258,0.00019592543,0.00005734712],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.000064361,0.0002720064,0.00033346022,0.000078087134,0.00006136212,0.000056239365,0.00018302012,0.00039633646,0.00039606035],"category_scores_gemma":[0.000011619881,0.00028885953,0.00011834835,0.00012428651,0.000008002692,0.000060845206,0.000013602525,0.00043073084,0.0000075296493],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000029198375,0.00002709915,3.6544552e-7,0.00041907516,0.00019231207,0.0000017975148,0.00046603708,0.97632617,0.017586282,0.00019191294,0.004065297,0.00072073797],"study_design_scores_gemma":[0.00009784815,0.000008837342,0.000005559944,0.00013029923,0.00014923699,6.5592917e-7,0.00017780233,0.9923834,0.0033772232,0.00029719228,0.003081923,0.00028997945],"about_ca_topic_score_codex":0.00006159373,"about_ca_topic_score_gemma":0.00009440114,"teacher_disagreement_score":0.30491853,"about_ca_system_score_codex":0.000038008107,"about_ca_system_score_gemma":0.000081615945,"threshold_uncertainty_score":0.99995637},"labels":[],"label_agreement":null},{"id":"W4229454438","doi":"10.3390/fluids7050161","title":"Advances in the Prediction of the Statistical Properties of Wall-Pressure Fluctuations under Turbulent Boundary Layers","year":2022,"lang":"en","type":"article","venue":"Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Centre Lyonnais d'Acoustique, Université de Lyon; Agence Nationale de la Recherche","keywords":"Boundary layer; Turbulence; Mechanics; Mach number; Compressibility; Airfoil; Physics; Boundary layer thickness; Spectral density; Compressible flow; Statistical physics; Mathematics; Statistics","score_opus":0.009914843004668328,"score_gpt":0.20752821714488134,"score_spread":0.19761337414021302,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4229454438","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.94503415,0.0077206655,0.040932693,0.00084284064,0.0012966028,0.0006661101,0.000683018,0.00007341282,0.002750535],"genre_scores_gemma":[0.9995561,0.000115670126,0.00016726008,0.000033720185,0.00002025057,0.000038342434,0.000011520106,0.000008844554,0.00004826399],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99940455,0.000046879602,0.00016723105,0.00006070499,0.00023829447,0.00008233144],"domain_scores_gemma":[0.9997484,0.000040218354,0.000016940714,0.00016599646,0.000020553456,0.000007855358],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001353829,0.000054718395,0.000072902076,0.00002368774,0.00009029439,0.000007021171,0.00019292283,0.000017726077,0.000058353413],"category_scores_gemma":[0.000022738039,0.000034123754,0.000024260531,0.00012579586,0.00007883761,0.000041173786,0.000044939636,0.00016163572,3.5833614e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000061591536,0.000035092155,0.00023752014,0.00008200117,0.000017302433,4.440441e-7,0.0011481328,0.97850215,0.011518895,0.006860002,0.0011794397,0.0004128459],"study_design_scores_gemma":[0.00016341124,0.00004969778,0.0075867795,0.000027984926,0.00004040573,0.0000042223173,0.0012423508,0.97680134,0.00045336815,0.002905522,0.010659275,0.000065638786],"about_ca_topic_score_codex":0.000012214749,"about_ca_topic_score_gemma":0.000014525831,"teacher_disagreement_score":0.054522004,"about_ca_system_score_codex":0.00003102784,"about_ca_system_score_gemma":0.000026701391,"threshold_uncertainty_score":0.13915263},"labels":[],"label_agreement":null},{"id":"W4229642551","doi":"10.32920/14640087","title":"Airfoil Performance at Low Reynolds Numbers in the Presence of Periodic Disturbances","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University; University of Toronto; University of New Brunswick","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Airfoil; Reynolds number; Wake; Mechanics; Wind tunnel; Boundary layer; Lift (data mining); Physics; Drag; Vortex; Angle of attack; Vortex generator; Flow separation; Acoustics; Relative wind; Starting vortex; Lift-to-drag ratio; Aerodynamics; Turbulence; Vortex ring; Computer science","score_opus":0.006885650351629162,"score_gpt":0.20268756798411625,"score_spread":0.19580191763248708,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4229642551","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9766056,0.00091692887,0.0012708078,0.000043545064,0.0010446851,0.00018775386,0.00002443539,0.000061661005,0.01984456],"genre_scores_gemma":[0.9959527,0.0020649887,0.0010303003,0.000024508749,0.00007764742,0.0000537706,0.000044951346,0.000027754288,0.00072335196],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9987734,0.000029240397,0.00036148375,0.00027991692,0.00030707938,0.0002489095],"domain_scores_gemma":[0.9990861,0.00009237633,0.000063380205,0.00068442774,0.000045213194,0.000028525126],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002390395,0.0002418873,0.00031767436,0.00004352029,0.00004784692,0.00006334171,0.0006653831,0.00019898548,0.000120662255],"category_scores_gemma":[0.00003466779,0.00018299106,0.00010323716,0.00011553934,0.000112934824,0.000056177643,0.00044182836,0.0006152303,0.0000058536407],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000005495225,0.000037619997,0.009744428,0.0017140246,0.000038686332,0.000019315818,0.0027139564,0.98279136,0.00041872947,0.00021822161,0.0011672956,0.0011308555],"study_design_scores_gemma":[0.0001341639,0.000014279592,0.02323451,0.00064650417,0.000023103743,0.000008008946,0.00086229097,0.97357464,0.00056091434,0.00006861564,0.00049255363,0.0003804117],"about_ca_topic_score_codex":0.00009649933,"about_ca_topic_score_gemma":0.00051161496,"teacher_disagreement_score":0.019347103,"about_ca_system_score_codex":0.00013001205,"about_ca_system_score_gemma":0.000043958018,"threshold_uncertainty_score":0.74621594},"labels":[],"label_agreement":null},{"id":"W4232644502","doi":"10.32920/14640087.v1","title":"Airfoil Performance at Low Reynolds Numbers in the Presence of Periodic Disturbances","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University; University of Toronto; University of New Brunswick","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Airfoil; Reynolds number; Wake; Mechanics; Boundary layer; Drag; Lift (data mining); Wind tunnel; Vortex; Flow separation; Physics; Angle of attack; Acoustics; Vortex generator; Relative wind; Aerodynamics; Turbulence; Computer science","score_opus":0.006885650351629162,"score_gpt":0.20268756798411625,"score_spread":0.19580191763248708,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4232644502","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9766056,0.00091692887,0.0012708078,0.000043545064,0.0010446851,0.00018775386,0.00002443539,0.000061661005,0.01984456],"genre_scores_gemma":[0.9959527,0.0020649887,0.0010303003,0.000024508749,0.00007764742,0.0000537706,0.000044951346,0.000027754288,0.00072335196],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9987734,0.000029240397,0.00036148375,0.00027991692,0.00030707938,0.0002489095],"domain_scores_gemma":[0.9990861,0.00009237633,0.000063380205,0.00068442774,0.000045213194,0.000028525126],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002390395,0.0002418873,0.00031767436,0.00004352029,0.00004784692,0.00006334171,0.0006653831,0.00019898548,0.000120662255],"category_scores_gemma":[0.00003466779,0.00018299106,0.00010323716,0.00011553934,0.000112934824,0.000056177643,0.00044182836,0.0006152303,0.0000058536407],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000005495225,0.000037619997,0.009744428,0.0017140246,0.000038686332,0.000019315818,0.0027139564,0.98279136,0.00041872947,0.00021822161,0.0011672956,0.0011308555],"study_design_scores_gemma":[0.0001341639,0.000014279592,0.02323451,0.00064650417,0.000023103743,0.000008008946,0.00086229097,0.97357464,0.00056091434,0.00006861564,0.00049255363,0.0003804117],"about_ca_topic_score_codex":0.00009649933,"about_ca_topic_score_gemma":0.00051161496,"teacher_disagreement_score":0.019347103,"about_ca_system_score_codex":0.00013001205,"about_ca_system_score_gemma":0.000043958018,"threshold_uncertainty_score":0.74621594},"labels":[],"label_agreement":null},{"id":"W4233695389","doi":"10.1063/5.0051226.2","title":"10.1063/5.0051226.2","year":2021,"lang":"en","type":"dataset","venue":"Default Digital Object Group","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Ontario Institute of Technology","funders":"","keywords":"Mechanics; Physics; Excitation; Resonance (particle physics); Vortex; Acoustic resonance; Reynolds number; Acoustics; Turbulence; Atomic physics","score_opus":0.005077928682538386,"score_gpt":0.1978229574490914,"score_spread":0.192745028766553,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4233695389","genre_codex":"dataset","genre_gemma":"dataset","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"dataset","genre_consensus":"dataset","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.00010848701,0.0010005367,0.00043239005,0.000005461666,0.0016269094,0.00018587732,0.97608966,0.00038929912,0.0201614],"genre_scores_gemma":[0.0011124164,0.0003480318,0.00010623244,0.000055165947,0.0008229009,0.00004517227,0.9940057,0.00015008998,0.0033543385],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.99771106,0.000014999319,0.00054191414,0.00057260913,0.00049573445,0.00066367193],"domain_scores_gemma":[0.9983909,0.00014800814,0.00008605441,0.0010821387,0.00008585453,0.00020704564],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.00009151177,0.0006962691,0.00067123416,0.00017663479,0.00008554511,0.0007134476,0.00065942336,0.0006016176,0.002066589],"category_scores_gemma":[0.0001744123,0.0007327103,0.00033098058,0.00040124773,0.000074398275,0.00027798387,0.00028549525,0.00084145425,0.0047523575],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000050020435,0.00006698221,6.868662e-7,0.0002942935,0.00015363528,0.0003251335,0.0000044612184,0.0018200653,0.000012702691,0.00001144148,0.993226,0.004079593],"study_design_scores_gemma":[0.00021535132,0.00005685244,0.0000070932674,0.00014714123,0.00007734962,0.000056199173,0.000017257249,0.005378715,0.0000058681353,0.000094642935,0.99309784,0.0008456841],"about_ca_topic_score_codex":0.000015650205,"about_ca_topic_score_gemma":0.00007389869,"teacher_disagreement_score":0.017916014,"about_ca_system_score_codex":0.00019298367,"about_ca_system_score_gemma":0.000052974436,"threshold_uncertainty_score":0.9995124},"labels":[],"label_agreement":null},{"id":"W4235135930","doi":"10.1155/2012/153204","title":"Prediction of Turbulent Boundary Layer Induced Noise in the Cabin of a BWB Aircraft","year":2012,"lang":"en","type":"article","venue":"Shock and Vibration","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":10,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Victoria","funders":"Fundação para a Ciência e a Tecnologia","keywords":"Boundary layer; Turbulence; Noise (video); Range (aeronautics); Acoustics; Aircraft noise; Sound pressure; Volume (thermodynamics); Flow (mathematics); Boundary (topology); Aerospace engineering; Engineering; Mechanics; Physics; Computer science; Mathematics; Noise reduction","score_opus":0.018040491493636703,"score_gpt":0.22078158587591212,"score_spread":0.20274109438227542,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4235135930","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99236983,0.00017751943,0.006677452,0.000037969323,0.00015498685,0.00009946727,0.000010432016,0.00001223624,0.0004601176],"genre_scores_gemma":[0.9996121,0.00004175662,0.00022807135,0.0000146875145,0.000070842296,0.0000069733546,0.000014765698,0.0000059699423,0.00000482708],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996487,0.000014504674,0.00014326366,0.000039513685,0.00008004189,0.0000740107],"domain_scores_gemma":[0.9998534,0.00001920044,0.000021890057,0.000077577046,0.000013756859,0.000014181059],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00014905269,0.00004850709,0.00006562486,0.00003562856,0.000020083473,0.0000067068113,0.000033109634,0.000047352263,0.0000055431556],"category_scores_gemma":[0.000009148272,0.000037626436,0.000013709536,0.00007052803,0.000012467693,0.000114309674,0.000007935451,0.000070410984,4.5681938e-7],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000037710783,0.00025855802,0.045222607,0.0004409048,0.00004837584,0.0000012070597,0.013401853,0.07265978,0.8544724,0.0045532137,0.0009435991,0.007959804],"study_design_scores_gemma":[0.00042182248,0.000100935926,0.26517105,0.000059381564,0.000030229674,0.000005900696,0.00055990054,0.7179202,0.01464468,0.000566927,0.00040265673,0.00011635607],"about_ca_topic_score_codex":0.000013679682,"about_ca_topic_score_gemma":0.000016432708,"teacher_disagreement_score":0.8398277,"about_ca_system_score_codex":0.000012658786,"about_ca_system_score_gemma":0.0000071022446,"threshold_uncertainty_score":0.15343615},"labels":[],"label_agreement":null},{"id":"W4235394574","doi":"10.32920/ryerson.14663562","title":"Supersonic Windtunnel Noise Attenuation","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Wind tunnel; Acoustics; Silencer; Aerodynamics; Supersonic wind tunnel; Noise (video); Sound pressure; Hypersonic wind tunnel; Supersonic speed; Acoustic attenuation; Sound power; Transonic; Aeroacoustics; Shock wave; Attenuation; Nozzle; Physics; Engineering; Sound (geography); Computer science; Aerospace engineering; Optics; Mechanics; Inlet","score_opus":0.011608593298238615,"score_gpt":0.20915608502274616,"score_spread":0.19754749172450753,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4235394574","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.69536227,0.00076106127,0.26749206,0.00013842333,0.0041159377,0.00023890127,0.000051314055,0.00069021044,0.031149836],"genre_scores_gemma":[0.9899082,0.00040514395,0.008066484,0.00005275644,0.00031107973,0.000024498422,0.00029295054,0.00006557953,0.0008732868],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991528,0.000009684349,0.00020642852,0.0002610731,0.00016295878,0.00020709974],"domain_scores_gemma":[0.99939656,0.00002397068,0.000019384508,0.0004334546,0.000066962915,0.00005964808],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00008553585,0.00022287936,0.00022205668,0.000054416047,0.000030764073,0.00012190306,0.00019552857,0.00029436356,0.00038636138],"category_scores_gemma":[0.000020476315,0.00024028825,0.00011559627,0.00006421883,0.000014945093,0.00004228972,0.00022632624,0.00056133716,0.00005267173],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[5.8283143e-7,0.000015326117,0.0001383285,0.00025082316,0.00008271236,0.000018450266,0.0002143973,0.99088335,0.0038586475,0.0003494967,0.0020197032,0.0021681944],"study_design_scores_gemma":[0.000085677726,0.000003225381,0.0008334749,0.000084718326,0.000039319784,0.0000028202776,0.00014849116,0.9975213,0.0002718737,0.00040745872,0.00027406265,0.0003275922],"about_ca_topic_score_codex":0.000024123152,"about_ca_topic_score_gemma":0.00005316044,"teacher_disagreement_score":0.29454598,"about_ca_system_score_codex":0.0001299135,"about_ca_system_score_gemma":0.000047102443,"threshold_uncertainty_score":0.97986704},"labels":[],"label_agreement":null},{"id":"W4236409929","doi":"10.1121/1.4790578","title":"Effects of a boundary layer trip in the prediction of noise from flow past tandem cylinders","year":2013,"lang":"en","type":"article","venue":"Proceedings of meetings on acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"Héroux-Devtek; Compute Canada; McGill University","keywords":"Boundary layer; Turbulence; Wind tunnel; Mechanics; Acoustics; Wake; Computational fluid dynamics; Noise (video); Vortex shedding; Physics; Reynolds number; Computer science","score_opus":0.006015186341112044,"score_gpt":0.18629268585126937,"score_spread":0.18027749951015734,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4236409929","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9943407,0.000116215,0.0022888375,0.000044503453,0.00027353712,0.0005024822,0.000053015974,0.00005777096,0.0023229173],"genre_scores_gemma":[0.9948947,0.00017550576,0.0046343356,0.000042645075,0.00015257903,0.00003978569,0.000007449813,0.00004298497,0.000010002865],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9985124,0.0000069379416,0.000584941,0.00018844611,0.0004564494,0.00025081745],"domain_scores_gemma":[0.9988701,0.00040234608,0.0002436125,0.000107668355,0.00032842642,0.000047862293],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00034019392,0.00021494826,0.00037050655,0.00014581681,0.000036919468,0.000032717937,0.0003403321,0.00018289423,0.000010077543],"category_scores_gemma":[0.00047264426,0.0001765892,0.00007661959,0.00031713845,0.00011278113,0.000116509975,0.000043075772,0.0003444326,0.0000025077788],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000042583415,0.0002809458,0.0076877703,0.0015448614,0.00009655934,0.0000016226028,0.0024615815,0.042360965,0.93782943,0.00019184292,0.0049065715,0.0025952705],"study_design_scores_gemma":[0.0014267678,0.00031880196,0.047464173,0.0009478166,0.000194132,0.0000019543904,0.0017444724,0.90236664,0.043076262,0.0021139858,0.00007448635,0.00027053585],"about_ca_topic_score_codex":0.0000392728,"about_ca_topic_score_gemma":0.000001264017,"teacher_disagreement_score":0.89475316,"about_ca_system_score_codex":0.0000517837,"about_ca_system_score_gemma":0.000017712184,"threshold_uncertainty_score":0.7201098},"labels":[],"label_agreement":null},{"id":"W4236941157","doi":"10.1063/5.0051226.13","title":"10.1063/5.0051226.13","year":2021,"lang":"en","type":"dataset","venue":"Default Digital Object Group","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Ontario Institute of Technology","funders":"","keywords":"Mechanics; Physics; Excitation; Resonance (particle physics); Vortex; Acoustics; Reynolds number; Acoustic resonance; Turbulence; Atomic physics","score_opus":0.005129882607962208,"score_gpt":0.19819277594651993,"score_spread":0.19306289333855772,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4236941157","genre_codex":"dataset","genre_gemma":"dataset","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"dataset","genre_consensus":"dataset","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.00019167736,0.0009393058,0.0004456317,0.0000063394477,0.0018144337,0.00021332507,0.97605824,0.00040473347,0.01992632],"genre_scores_gemma":[0.001746279,0.00034087052,0.000097226904,0.00006248004,0.0009209962,0.000050934224,0.9932422,0.00016489257,0.0033741076],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.9975427,0.000016348247,0.00058331597,0.00061570265,0.0005302127,0.0007117134],"domain_scores_gemma":[0.99828345,0.0001602426,0.00009513096,0.0011429826,0.00009274087,0.00022548197],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.00009774086,0.0007469078,0.00071955286,0.00018863237,0.000091647424,0.00075699866,0.0007110422,0.0006447832,0.002105944],"category_scores_gemma":[0.0001867277,0.00078565883,0.0003546672,0.0003799481,0.00007995265,0.00030741905,0.0003173717,0.0008934428,0.0048950217],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000057982406,0.00007269095,0.0000011360311,0.0003184545,0.00016735999,0.00035009728,0.000005374846,0.0024860103,0.000013661026,0.000009597971,0.99293387,0.0036359536],"study_design_scores_gemma":[0.0002471245,0.00006138368,0.000012041068,0.00015747281,0.00008471588,0.000059772505,0.000019814572,0.0065697264,0.000006012488,0.00010588191,0.99176604,0.000910037],"about_ca_topic_score_codex":0.000026061662,"about_ca_topic_score_gemma":0.00014018039,"teacher_disagreement_score":0.01718398,"about_ca_system_score_codex":0.00020022447,"about_ca_system_score_gemma":0.00005701124,"threshold_uncertainty_score":0.99945945},"labels":[],"label_agreement":null},{"id":"W4238459107","doi":"10.1063/1.3026074.1","title":"10.1063/1.3026074.1","year":2008,"lang":"en","type":"dataset","venue":"Default Digital Object Group","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Concordia University","funders":"","keywords":"Diffuser (optics); Mechanics; Particle image velocimetry; Body orifice; Nozzle; Volumetric flow rate; Acoustics; Flow (mathematics); Reynolds number; Materials science; Impeller; Inlet; Backflow; Progressive cavity pump; Flow velocity; Optics; Physics; Variable displacement pump; Mechanical engineering; Engineering; Radial piston pump; Turbulence; Thermodynamics","score_opus":0.005679318086970971,"score_gpt":0.19205242822840884,"score_spread":0.18637311014143787,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4238459107","genre_codex":"dataset","genre_gemma":"dataset","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"dataset","genre_consensus":"dataset","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.00016966183,0.0005726088,0.0003736921,0.000003509889,0.0013253338,0.00025433835,0.97226816,0.0005346115,0.024498073],"genre_scores_gemma":[0.001914914,0.0007221275,0.000105626554,0.000048748603,0.0008135007,0.000047636928,0.9931389,0.00016866006,0.003039896],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.99761456,0.000011558207,0.0005731588,0.0005430884,0.0005355306,0.0007221059],"domain_scores_gemma":[0.99845237,0.00014159473,0.00009943129,0.0010146182,0.000065999804,0.00022600348],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.00006923586,0.0007661024,0.0006709994,0.0002363149,0.00011884415,0.00035736634,0.0007876461,0.0006474297,0.001126444],"category_scores_gemma":[0.00012852137,0.00078574906,0.00032291844,0.0003160806,0.000121815676,0.00032597015,0.00022186394,0.00085262704,0.008696723],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000083345085,0.000065395914,0.0000010833405,0.00018399484,0.00012229751,0.00028782376,0.000007000795,0.0021601594,0.0000053913195,0.0000068976033,0.99380666,0.0033449568],"study_design_scores_gemma":[0.00025061326,0.000093954455,0.000012222859,0.00008593666,0.00005250237,0.00011370615,0.0000063544635,0.0056697032,0.0000029390435,0.00007682253,0.99272007,0.0009151554],"about_ca_topic_score_codex":0.000022021923,"about_ca_topic_score_gemma":0.00004377667,"teacher_disagreement_score":0.021458177,"about_ca_system_score_codex":0.00020282608,"about_ca_system_score_gemma":0.00004117018,"threshold_uncertainty_score":0.9997867},"labels":[],"label_agreement":null},{"id":"W4239462260","doi":"10.1121/1.4799638","title":"Industrial Fan Noise Control using Flow Obstructions","year":2013,"lang":"en","type":"article","venue":"Proceedings of meetings on acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Institut de recherche Robert-Sauvé en santé et en sécurité du travail; Université de Sherbrooke","funders":"","keywords":"Duct (anatomy); Noise control; Noise (video); Acoustics; Engineering; Noise reduction; Active noise control; Mechanical fan; Computer science; Electrical engineering; Physics","score_opus":0.012773679066089214,"score_gpt":0.198197802315067,"score_spread":0.18542412324897778,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4239462260","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9820361,0.000026575248,0.009953724,0.000054428165,0.0010135224,0.00043789233,0.000062705214,0.00030440398,0.0061106104],"genre_scores_gemma":[0.9770417,0.000030704625,0.02209881,0.00005508478,0.00060230785,0.000025165313,0.0000037532084,0.00008631589,0.000056162906],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9984163,0.0000028421493,0.00052242866,0.0002487126,0.00036777504,0.0004419234],"domain_scores_gemma":[0.99888027,0.00010646351,0.00017453832,0.00011354127,0.0005660991,0.00015911789],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00020350878,0.00029663747,0.0003638763,0.00017501797,0.00012834003,0.00011318307,0.00029269067,0.0002659156,0.00007161656],"category_scores_gemma":[0.0005320793,0.000304474,0.00008651709,0.0003120907,0.000098830176,0.00020031791,0.0000464765,0.00048873556,0.000024321007],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00001754568,0.000067121626,0.0015620522,0.00018505477,0.00009473997,0.0000010243418,0.00014785031,0.32714364,0.6590433,0.0007867694,0.006745817,0.004205076],"study_design_scores_gemma":[0.0008062981,0.00007440956,0.000472718,0.00015231103,0.00011963639,0.000009060755,0.00034228055,0.99257284,0.0042534736,0.0006916884,0.00015980341,0.00034549955],"about_ca_topic_score_codex":0.00001821632,"about_ca_topic_score_gemma":2.7571986e-7,"teacher_disagreement_score":0.6654292,"about_ca_system_score_codex":0.00011964551,"about_ca_system_score_gemma":0.00002396911,"threshold_uncertainty_score":0.99994075},"labels":[],"label_agreement":null},{"id":"W4240048038","doi":"10.1121/1.4799211","title":"Effects of Scalloping Depth on the Sound Generated by Turbofan Engine Lobed Mixers","year":2013,"lang":"en","type":"article","venue":"Proceedings of meetings on acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"","keywords":"Turbofan; Mach number; Acoustics; Nozzle; Noise (video); Aeroacoustics; Jet engine; Computer science; Noise reduction; Solver; Sound pressure; Engineering; Aerospace engineering; Physics; Artificial intelligence","score_opus":0.0043727114702891735,"score_gpt":0.1800785227951319,"score_spread":0.17570581132484273,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4240048038","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9922629,0.00013303265,0.002547291,0.00012340053,0.00030640737,0.00052954647,0.00001425052,0.00017333304,0.0039098356],"genre_scores_gemma":[0.9960299,0.00019740596,0.0032598914,0.00015668891,0.00012767703,0.00004512284,0.000006149861,0.00009378675,0.00008339182],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9984021,0.000005675181,0.00047411883,0.00025532968,0.00044161294,0.00042111584],"domain_scores_gemma":[0.9986715,0.00043778535,0.00021124502,0.0001283413,0.00044674703,0.00010440937],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0002887773,0.00033812065,0.0003763786,0.00011380853,0.000089021996,0.000073277486,0.0004257671,0.00017836282,0.000016660662],"category_scores_gemma":[0.0007806085,0.00026505793,0.00008087969,0.00033808622,0.00011362406,0.000081588594,0.000060852362,0.0004021256,0.000014152088],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000013794035,0.000087268854,0.00015680736,0.0008473715,0.00009045566,6.24913e-7,0.00018467943,0.028729517,0.95059323,0.0010141546,0.017079446,0.0012026263],"study_design_scores_gemma":[0.00061441655,0.000284635,0.0007394642,0.0006446965,0.00012934051,0.000002308549,0.00029044494,0.5909918,0.4045173,0.0011662571,0.00012795469,0.0004914075],"about_ca_topic_score_codex":0.000011587287,"about_ca_topic_score_gemma":3.5766152e-7,"teacher_disagreement_score":0.56226224,"about_ca_system_score_codex":0.00007568712,"about_ca_system_score_gemma":0.000011142184,"threshold_uncertainty_score":0.99998015},"labels":[],"label_agreement":null},{"id":"W4240089570","doi":"10.1063/5.0051226.1","title":"10.1063/5.0051226.1","year":2021,"lang":"en","type":"dataset","venue":"Default Digital Object Group","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Ontario Institute of Technology","funders":"","keywords":"Mechanics; Physics; Excitation; Resonance (particle physics); Vortex; Acoustics; Acoustic resonance; Reynolds number; Turbulence; Atomic physics","score_opus":0.00508051735085661,"score_gpt":0.19783578090511686,"score_spread":0.19275526355426026,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4240089570","genre_codex":"dataset","genre_gemma":"dataset","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"dataset","genre_consensus":"dataset","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.00011163347,0.0009927774,0.00043703613,0.000005611531,0.0016152444,0.00018966818,0.9766989,0.00038344713,0.019565728],"genre_scores_gemma":[0.0011158057,0.0003523244,0.000109865636,0.00005631202,0.0008162562,0.000045218196,0.9941812,0.00015016757,0.0031728288],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.9977069,0.0000148182535,0.0005436469,0.0005727276,0.0004966241,0.00066527573],"domain_scores_gemma":[0.998391,0.00014689851,0.00008611923,0.0010813187,0.00008557127,0.00020910468],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.0000905794,0.00069799594,0.0006744057,0.00017632968,0.000084506966,0.00070436974,0.0006632768,0.0006068735,0.0020966623],"category_scores_gemma":[0.00017127051,0.0007341273,0.0003323218,0.0004073872,0.000073779585,0.00028224566,0.00029045064,0.0008359329,0.004779727],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000050845583,0.00006723936,7.15183e-7,0.00029705177,0.00015399834,0.00033039696,0.0000043172026,0.0017749981,0.000013777345,0.000011060327,0.9932429,0.004098448],"study_design_scores_gemma":[0.00021736164,0.0000568459,0.0000076726865,0.00014407503,0.00007762922,0.000056239605,0.000016723556,0.005348856,0.0000061310175,0.00009717186,0.99312323,0.0008480763],"about_ca_topic_score_codex":0.000015245189,"about_ca_topic_score_gemma":0.000074286734,"teacher_disagreement_score":0.017482366,"about_ca_system_score_codex":0.00019206916,"about_ca_system_score_gemma":0.00005321012,"threshold_uncertainty_score":0.999511},"labels":[],"label_agreement":null},{"id":"W4240239653","doi":"10.1115/1.4051113","title":"Prediction of the Acoustic Reflection in a Realistic Aeroengine Intake With Three Numerical Methods to Analyze Fan Flutter","year":2021,"lang":"en","type":"article","venue":"Journal of Turbomachinery","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":9,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Safran Electronics (Canada)","funders":"","keywords":"Flutter; Reflection (computer programming); Acoustics; Computer science; Structural engineering; Engineering; Aerospace engineering; Aerodynamics; Physics","score_opus":0.01373798928235009,"score_gpt":0.26736036695953497,"score_spread":0.2536223776771849,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4240239653","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.3641756,0.00015272108,0.63430905,0.00021216852,0.00073709054,0.00006300143,0.000014286221,0.000015734087,0.00032036076],"genre_scores_gemma":[0.9568906,0.000023018601,0.042723976,0.000066293265,0.00023204318,0.0000026197174,0.0000027565056,0.000028427048,0.000030264875],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99885046,0.00008680089,0.0005235893,0.00010903945,0.00026562798,0.00016449693],"domain_scores_gemma":[0.99928784,0.00011944451,0.00013601959,0.00022816,0.000152775,0.0000757532],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00043907788,0.00014103088,0.0003141564,0.0001658607,0.00003016218,0.000020940426,0.00016622833,0.000068753405,0.000020745429],"category_scores_gemma":[0.0002627126,0.00009234503,0.000104199295,0.0006682964,0.00002073648,0.000077536315,0.0000401136,0.00054045144,4.3670673e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000046832134,0.000044940916,0.0048314934,0.000051751205,0.00008965672,0.000048661528,0.00011374865,0.9094425,0.08170457,0.00003671548,0.0003819149,0.0032072328],"study_design_scores_gemma":[0.0005211942,0.00019206859,0.11145354,0.0002768741,0.00018506238,0.00048216074,0.00005661123,0.88352513,0.002299177,0.0006814803,0.0001785167,0.00014817054],"about_ca_topic_score_codex":0.000018869761,"about_ca_topic_score_gemma":0.00023842404,"teacher_disagreement_score":0.592715,"about_ca_system_score_codex":0.00015813057,"about_ca_system_score_gemma":0.000054040047,"threshold_uncertainty_score":0.3765721},"labels":[],"label_agreement":null},{"id":"W4240455765","doi":"10.1063/5.0051226.6","title":"10.1063/5.0051226.6","year":2021,"lang":"en","type":"dataset","venue":"Default Digital Object Group","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Ontario Institute of Technology","funders":"","keywords":"Mechanics; Physics; Excitation; Resonance (particle physics); Acoustics; Vortex; Reynolds number; Acoustic resonance; Turbulence; Atomic physics","score_opus":0.005077928682538386,"score_gpt":0.1978229574490914,"score_spread":0.192745028766553,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4240455765","genre_codex":"dataset","genre_gemma":"dataset","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"dataset","genre_consensus":"dataset","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0001141856,0.0009909485,0.00043279343,0.000005547368,0.0016164867,0.00018968293,0.9767538,0.00038319468,0.019513369],"genre_scores_gemma":[0.0011371734,0.00035181514,0.000108912376,0.000056279936,0.00081867893,0.00004521831,0.99415904,0.00015013928,0.0031727133],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.9977067,0.000014820251,0.00054365984,0.00057277817,0.00049671193,0.0006653405],"domain_scores_gemma":[0.99839085,0.00014694635,0.00008612622,0.0010813713,0.00008558628,0.00020912688],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.00009060513,0.00069802743,0.00067313854,0.00017633733,0.00008451964,0.0007045283,0.00066309754,0.00060697907,0.0021170352],"category_scores_gemma":[0.00017137293,0.00073415285,0.00033233693,0.00040745008,0.00007378651,0.00028229164,0.00029034851,0.0008368641,0.004790254],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000050858976,0.000067209694,7.455983e-7,0.00029675476,0.00015197786,0.00033020147,0.0000043305145,0.001775426,0.000013221571,0.000011234882,0.99337256,0.0039712247],"study_design_scores_gemma":[0.00021738143,0.00005684784,0.000007844224,0.00014532036,0.00007754542,0.000056229816,0.000016747868,0.0052673263,0.000006035901,0.00009730552,0.9932032,0.00084819295],"about_ca_topic_score_codex":0.00001533563,"about_ca_topic_score_gemma":0.0000750483,"teacher_disagreement_score":0.017405277,"about_ca_system_score_codex":0.00019216382,"about_ca_system_score_gemma":0.000053228,"threshold_uncertainty_score":0.99951094},"labels":[],"label_agreement":null},{"id":"W4240955173","doi":"10.1007/978-94-007-0753-5_100116","title":"Aircraft Noise","year":2014,"lang":"en","type":"book-chapter","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Brandon University; University of Northern British Columbia","funders":"","keywords":"Noise (video); Aircraft noise; Computer science; Aeronautics; Acoustics; Aerospace engineering; Engineering; Physics; Artificial intelligence; Noise reduction","score_opus":0.006217499443858734,"score_gpt":0.1767010242702609,"score_spread":0.17048352482640217,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4240955173","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0000071518853,0.00013955454,0.098548144,0.000014393624,0.00080097764,0.00006563527,0.000020295283,0.00041116113,0.8999927],"genre_scores_gemma":[0.007815348,0.0002807057,0.0024546403,0.00009487154,0.0005176682,0.0000028190655,0.000039126906,0.00015334971,0.9886415],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"not_applicable","domain_scores_codex":[0.9993901,8.382718e-7,0.00017698092,0.00015261679,0.00012419632,0.00015521552],"domain_scores_gemma":[0.9995337,0.000025352738,0.000018586705,0.00032998557,0.000025535555,0.00006685636],"candidate_categories":["insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.00004374482,0.00024920842,0.00022979054,0.00005554438,0.000021140295,0.000020770727,0.00016027954,0.00028545898,0.0016618723],"category_scores_gemma":[0.0000035566582,0.00024154315,0.000095288655,0.0000059419344,0.0000243511,0.000010785836,0.000038293758,0.0003005011,0.0013114355],"study_design_candidate":"not_applicable","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[8.578168e-7,0.0000019297097,9.704538e-7,0.0001517609,0.00009315927,0.00001836363,0.000009264137,0.036013406,0.000119376375,0.8431687,0.103674755,0.016747499],"study_design_scores_gemma":[0.000058789563,0.000009387783,0.000001866336,0.000050526345,0.000031795607,0.0000035443923,4.1745412e-7,0.17845997,0.0000067507385,0.013467396,0.8075355,0.00037400535],"about_ca_topic_score_codex":0.0000010349364,"about_ca_topic_score_gemma":0.000012286778,"teacher_disagreement_score":0.82970124,"about_ca_system_score_codex":0.000043234497,"about_ca_system_score_gemma":0.0000068479544,"threshold_uncertainty_score":0.9994662},"labels":[],"label_agreement":null},{"id":"W4242214852","doi":"10.2172/883301","title":"CFD Simulation of Flow Tones from Grazing Flow past a Deep Cavity","year":2006,"lang":"en","type":"report","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lockheed Martin (Canada)","funders":"Lehigh University; Rensselaer Polytechnic Institute; U.S. Department of Energy","keywords":"Dimensionless quantity; Vorticity; Flow (mathematics); Scale (ratio); Oscillation (cell signaling); Wavelength; Mechanics; Computational fluid dynamics; Physics; Transverse plane; Acoustics; Vortex; Optics; Engineering; Structural engineering","score_opus":0.013848098696984194,"score_gpt":0.2427668071157246,"score_spread":0.2289187084187404,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4242214852","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.02251209,0.0009620433,0.90883464,0.0000050790873,0.0035045564,0.00029903077,0.0007258059,0.00042351207,0.062733226],"genre_scores_gemma":[0.9626862,0.0003485068,0.03245148,0.000005610757,0.0016005978,0.00001339212,0.0017276359,0.0001537291,0.0010128511],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9981115,0.000014070286,0.00067423086,0.0003196538,0.0005958716,0.00028469178],"domain_scores_gemma":[0.9988501,0.00018228895,0.00014678523,0.00047233645,0.00028617313,0.00006231533],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00020646733,0.00038942942,0.00062822294,0.00013119903,0.000049738115,0.000040239764,0.00019380335,0.00050268526,0.00013870352],"category_scores_gemma":[0.00007031691,0.0003872044,0.00021067381,0.00014340045,0.00003118017,0.00006698633,0.00006881081,0.00039538043,0.00001376892],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000018405821,0.000020224723,0.0005331054,0.0002339448,0.000094841904,0.000012274053,0.000023731474,0.9816808,0.00021548384,0.000004536169,0.00219753,0.014981647],"study_design_scores_gemma":[0.00011884664,0.000008742411,0.0020125525,0.00014576963,0.00012904774,0.0000019893087,0.00000847113,0.9917617,0.00004786369,0.0002999337,0.0050654076,0.00039969734],"about_ca_topic_score_codex":0.0009931163,"about_ca_topic_score_gemma":0.0022106145,"teacher_disagreement_score":0.9401741,"about_ca_system_score_codex":0.00025813698,"about_ca_system_score_gemma":0.00007005326,"threshold_uncertainty_score":0.99985796},"labels":[],"label_agreement":null},{"id":"W4243321758","doi":"10.1016/j.bone.2018.07.024","title":"Letter to the Editor","year":2018,"lang":"en","type":"letter","venue":"Bone","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Ottawa; University of Calgary; University of Manitoba; Memorial University of Newfoundland; University of British Columbia","funders":"","keywords":"Jet (fluid); Beam (structure); Physics; Mechanics; Acoustic streaming; Particle image velocimetry; Plane (geometry); Field (mathematics); Compressibility; Optics; Vector field; Flow (mathematics); Reflection (computer programming); Near and far field; Classical mechanics; Acoustics; Geometry; Turbulence; Mathematics; Ultrasonic sensor","score_opus":0.006136977170010188,"score_gpt":0.19208508321063003,"score_spread":0.18594810604061984,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4243321758","genre_codex":"commentary","genre_gemma":"commentary","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"commentary","genre_consensus":"commentary","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.00010579801,0.00014260043,0.0132164685,0.9214117,0.052712627,0.00028147284,0.000168212,0.0002504358,0.0117106885],"genre_scores_gemma":[0.00017534374,0.000009446173,0.00077367877,0.6295139,0.36012334,0.000030822,0.000049054514,0.000087130364,0.009237301],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.99917126,0.000009220667,0.00014505858,0.00016404346,0.000216261,0.00029414098],"domain_scores_gemma":[0.99937755,0.000045170927,0.000017446877,0.00049954664,0.000031764273,0.000028534203],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00008567256,0.00019595369,0.00016214067,0.000043056185,0.000051751067,0.000057351248,0.00031186864,0.0003853282,0.00018720559],"category_scores_gemma":[0.000018722953,0.00014074553,0.00006410826,0.0000672093,0.000027830238,0.000015231032,0.000069819085,0.0009786653,0.0023567823],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[3.092114e-7,9.609032e-7,1.8821942e-7,0.000030096242,0.000018301243,0.00003771351,0.00002469993,0.0007691244,0.000051090858,0.000003125915,0.99883926,0.00022512552],"study_design_scores_gemma":[0.000028523677,0.000009225178,0.0000040865407,0.000026891665,0.000017851646,0.0000032875328,6.5949644e-7,0.0058817416,0.000008122277,0.0000459489,0.9937724,0.0002012812],"about_ca_topic_score_codex":0.000003214875,"about_ca_topic_score_gemma":0.000008558267,"teacher_disagreement_score":0.30741072,"about_ca_system_score_codex":0.00004684989,"about_ca_system_score_gemma":0.000006809948,"threshold_uncertainty_score":0.99842},"labels":[],"label_agreement":null},{"id":"W4243849243","doi":"10.1016/j.jfluidstructs.2003.08.015","title":"Preface","year":2003,"lang":"en","type":"article","venue":"Journal of Fluids and Structures","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"","keywords":"Duct (anatomy); Acoustics; Laminar flow; Classification of discontinuities; Aeroacoustics; Noise control; Noise (video); Noise reduction; Physics; Engineering; Mechanics; Computer science; Sound pressure; Mathematics","score_opus":0.00486054570744062,"score_gpt":0.20039934643855317,"score_spread":0.19553880073111254,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4243849243","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97900707,0.003031723,0.01315969,0.000013825525,0.00064827304,0.000018043256,0.00000254396,0.0000099643985,0.0041088504],"genre_scores_gemma":[0.9925182,0.00045735235,0.006869377,0.000016954478,0.00008649186,9.284925e-8,1.06028104e-7,0.000008111981,0.00004333409],"study_design_codex":"bench_or_experimental","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.9996612,0.0000068821864,0.00014475675,0.00003004565,0.000080047175,0.00007703805],"domain_scores_gemma":[0.99983597,0.00001552967,0.000021962065,0.000046389898,0.000030778723,0.000049351787],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000077151504,0.000060495084,0.00010198728,0.000031932923,0.000025358282,0.00002440865,0.000047211695,0.00003585109,0.00003729552],"category_scores_gemma":[0.00002716522,0.000044245247,0.00002934153,0.000028877532,0.000016543245,0.00004258632,0.0000039919564,0.00012320663,2.7065846e-7],"study_design_candidate":"theoretical_or_conceptual","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000041371255,0.000037869042,0.0064589055,0.00034355713,0.0005436172,0.00019803908,0.0014603604,0.25561097,0.3778372,0.2572669,0.035087727,0.065113455],"study_design_scores_gemma":[0.0045180633,0.0010229389,0.09498101,0.00024263986,0.00039524824,0.0044666603,0.001168829,0.17038374,0.045862213,0.40428278,0.27080694,0.0018689283],"about_ca_topic_score_codex":2.2225169e-7,"about_ca_topic_score_gemma":4.656836e-7,"teacher_disagreement_score":0.33197498,"about_ca_system_score_codex":0.000009165836,"about_ca_system_score_gemma":0.000007673476,"threshold_uncertainty_score":0.18042688},"labels":[],"label_agreement":null},{"id":"W4244297137","doi":"10.1007/978-1-4614-5491-5_200130","title":"Jet-Type Rectifier","year":2015,"lang":"en","type":"book-chapter","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Waterloo","funders":"","keywords":"Jet (fluid); Rectifier (neural networks); Physics; Mechanics; Computer science; Artificial intelligence","score_opus":0.028896632139958914,"score_gpt":0.22159839180314655,"score_spread":0.19270175966318764,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4244297137","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.000011203357,0.0007798733,0.0022470264,0.000015821066,0.002657886,0.00008237293,0.000020086281,0.00039735646,0.99378836],"genre_scores_gemma":[0.0019103893,0.00050375855,0.001521173,0.00003032253,0.0004978449,0.0000014611779,0.000059629037,0.00014724254,0.9953282],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.9993359,0.0000011899913,0.00017371782,0.00016334966,0.00016835319,0.00015749369],"domain_scores_gemma":[0.9994338,0.000019392295,0.000020148225,0.00033094655,0.00010463697,0.00009104146],"candidate_categories":["insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.00007760118,0.00025600835,0.00023405181,0.000060634058,0.000018410248,0.000023695135,0.00014968116,0.000353501,0.002858742],"category_scores_gemma":[0.000011634327,0.00023292101,0.00006023869,0.000015295689,0.000023015862,0.000023308923,0.000044086388,0.00038204034,0.0013119162],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000032142354,0.0000030248302,0.0000010927449,0.00006229461,0.00013359233,0.000035041772,0.000020881378,0.011619594,0.000066808425,0.30587143,0.6718632,0.010319846],"study_design_scores_gemma":[0.000051415347,0.00001712023,4.967226e-7,0.000034949902,0.000031558495,0.0000058803334,0.0000017910727,0.026268195,0.000005059549,0.04129335,0.93195075,0.00033946024],"about_ca_topic_score_codex":0.0000025038737,"about_ca_topic_score_gemma":0.00003386828,"teacher_disagreement_score":0.2645781,"about_ca_system_score_codex":0.00010274972,"about_ca_system_score_gemma":0.000025932288,"threshold_uncertainty_score":0.9994657},"labels":[],"label_agreement":null},{"id":"W4244836171","doi":"10.1007/978-3-642-40371-2_5","title":"Self-Excited Oscillations of Two Opposing Planar Jets","year":2013,"lang":"en","type":"book-chapter","venue":"Lecture notes in mechanical engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"","keywords":"Oscillation (cell signaling); Physics; Particle image velocimetry; Planar; Jet (fluid); Excited state; Excitation; Flow (mathematics); Mechanics; Phase (matter); Optics; Acoustics; Atomic physics; Chemistry; Quantum mechanics","score_opus":0.00787204677490857,"score_gpt":0.20105897985957283,"score_spread":0.19318693308466425,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4244836171","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0006841511,0.00094007375,0.9798181,0.000031598873,0.001165339,0.00044464,0.00007423543,0.00064465683,0.016197193],"genre_scores_gemma":[0.8401436,0.0006001087,0.15735225,0.00005382856,0.0006675571,0.000030883977,0.00013983529,0.00050923054,0.00050266273],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9982904,0.000006600944,0.0006458654,0.00034561285,0.00029880562,0.00041270792],"domain_scores_gemma":[0.998915,0.0003753325,0.00008502303,0.00043689564,0.000065823224,0.00012193659],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00013327872,0.0005392851,0.0006670317,0.00034780632,0.000030167028,0.000034177094,0.00030801268,0.0006586814,0.00017331551],"category_scores_gemma":[0.0001223196,0.0005803063,0.0001673682,0.00012367846,0.00001789622,0.000061584506,0.00006683758,0.0011469551,0.000027458567],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000001543418,0.000008142932,8.725526e-7,0.000338815,0.000105357554,0.00001818809,0.000043709122,0.9337039,0.009693892,0.053728554,0.000017187826,0.0023398164],"study_design_scores_gemma":[0.00025563678,0.000026734815,0.000002942443,0.0005028695,0.00006933588,0.000012779567,4.2156873e-7,0.9783593,0.00092799414,0.017103218,0.0021744133,0.0005643505],"about_ca_topic_score_codex":0.000008062014,"about_ca_topic_score_gemma":0.000023541013,"teacher_disagreement_score":0.8394595,"about_ca_system_score_codex":0.00022816584,"about_ca_system_score_gemma":0.00002373663,"threshold_uncertainty_score":0.99966484},"labels":[],"label_agreement":null},{"id":"W4244861686","doi":"10.1063/5.0051226.8","title":"10.1063/5.0051226.8","year":2021,"lang":"en","type":"dataset","venue":"Default Digital Object Group","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Ontario Institute of Technology","funders":"","keywords":"Mechanics; Excitation; Physics; Resonance (particle physics); Vortex; Acoustics; Reynolds number; Acoustic resonance; Turbulence; Atomic physics","score_opus":0.005077928682538386,"score_gpt":0.1978229574490914,"score_spread":0.192745028766553,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4244861686","genre_codex":"dataset","genre_gemma":"dataset","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"dataset","genre_consensus":"dataset","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.00011169848,0.0010018975,0.00042807413,0.000005558775,0.0016194747,0.00019006908,0.9781682,0.000425672,0.01804938],"genre_scores_gemma":[0.0011385587,0.00034716458,0.00010859681,0.00005635477,0.00081904593,0.000045336652,0.9942885,0.00016195986,0.0030344645],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.9977089,0.000014802331,0.0005433235,0.0005721363,0.00049620756,0.00066462415],"domain_scores_gemma":[0.99839413,0.00014517613,0.00008606521,0.0010801627,0.000085518266,0.00020896312],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.00009048997,0.00069757336,0.00067264313,0.00017604142,0.00008444006,0.0007032985,0.0006618241,0.0006065895,0.0020424807],"category_scores_gemma":[0.00017109927,0.0007337276,0.00033216973,0.00040685755,0.00007381747,0.0002817384,0.0002894311,0.00083609443,0.0050783306],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000005141699,0.0000672279,7.4383547e-7,0.00029664207,0.00015381759,0.00033029605,0.0000044097837,0.0017471684,0.000013106028,0.000011300044,0.9933268,0.0040433537],"study_design_scores_gemma":[0.00021677354,0.000058137935,0.000007807839,0.00014524965,0.000077456796,0.00005619955,0.000016493263,0.0052478253,0.0000060613906,0.00009827802,0.99322647,0.0008432319],"about_ca_topic_score_codex":0.000015219611,"about_ca_topic_score_gemma":0.00007716062,"teacher_disagreement_score":0.016120344,"about_ca_system_score_codex":0.0001919357,"about_ca_system_score_gemma":0.0000531823,"threshold_uncertainty_score":0.99951136},"labels":[],"label_agreement":null},{"id":"W4246477084","doi":"10.1007/978-1-4615-0407-8_2","title":"Turbulent Jets","year":2003,"lang":"en","type":"book-chapter","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"","keywords":"Turbulence; Jet (fluid); Mechanics; Reynolds number; Entrainment (biomusicology); Eddy; Physics; Laminar flow; Classical mechanics","score_opus":0.009072233439323974,"score_gpt":0.1819660821329582,"score_spread":0.17289384869363422,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4246477084","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.000008639742,0.000556491,0.007978279,0.000029456265,0.0007669434,0.00008676604,0.000014694345,0.0002582202,0.99030054],"genre_scores_gemma":[0.0010805328,0.0009168028,0.0020846464,0.00021605512,0.00017350195,0.0000030614515,0.00003087701,0.00013831226,0.9953562],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"not_applicable","domain_scores_codex":[0.999385,8.677236e-7,0.00017217797,0.00014984664,0.00013112438,0.00016097778],"domain_scores_gemma":[0.99960834,0.000017145261,0.000016305616,0.00027245283,0.000023715525,0.00006205151],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00003323354,0.00025022452,0.00019701685,0.00004860789,0.000019946452,0.000020298825,0.00011384251,0.00026597275,0.0026432099],"category_scores_gemma":[0.0000033462545,0.00024140351,0.00008797978,0.0000067423543,0.00001791143,0.000013928158,0.000017053204,0.00029716972,0.00065580284],"study_design_candidate":"not_applicable","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[6.265402e-7,0.0000045411552,3.1458444e-7,0.00010630727,0.00013261856,0.0000586007,0.000016628926,0.02810534,0.00004751847,0.6640499,0.3034089,0.0040686806],"study_design_scores_gemma":[0.000057347144,0.000007993282,3.6764138e-7,0.000042547497,0.000029756095,0.000014622988,0.0000013235784,0.032204725,0.000012335901,0.020070752,0.94717664,0.00038159764],"about_ca_topic_score_codex":3.989567e-7,"about_ca_topic_score_gemma":0.0000037382783,"teacher_disagreement_score":0.6439792,"about_ca_system_score_codex":0.00006863353,"about_ca_system_score_gemma":0.000006128039,"threshold_uncertainty_score":0.9982685},"labels":[],"label_agreement":null},{"id":"W4247581117","doi":"10.22215/etd/2007-07776","title":"Feasibility study and design of an actively controlled tip for helicopter rotor blades","year":2007,"lang":"en","type":"dissertation","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Library and Archives Canada","funders":"","keywords":"Rotor (electric); Engineering; Humanities; Mechanical engineering; Art","score_opus":0.026819536994261137,"score_gpt":0.31882283309134074,"score_spread":0.2920032960970796,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4247581117","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.88506687,0.00008462843,0.108279765,6.784508e-7,0.0003187998,0.004727165,0.00005087027,0.000082330924,0.0013889121],"genre_scores_gemma":[0.98788625,0.000017339316,0.01064123,0.0000042462793,0.00007401939,0.0002505095,0.00010136328,0.000060050304,0.00096496975],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9990042,0.000026336362,0.00038648417,0.00025694168,0.00014676864,0.00017928214],"domain_scores_gemma":[0.99922615,0.00025336345,0.00008690889,0.00021102412,0.00015978467,0.000062767554],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00048240623,0.00025470834,0.0005657575,0.00010196869,0.000041747357,0.000031280793,0.000116565534,0.00021753104,0.00002868125],"category_scores_gemma":[0.00008049876,0.00022063851,0.000073169555,0.000047603105,0.000015603135,0.000063639134,0.000006777023,0.00014686925,6.6637705e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.06411959,0.012219147,0.004612378,0.013157552,0.0101808505,0.0000627446,0.024479004,0.3071747,0.4037427,0.0025600425,0.0013591828,0.1563321],"study_design_scores_gemma":[0.009532578,0.0012473478,0.01467754,0.00007374155,0.00047710634,8.671731e-7,0.004537077,0.96415377,0.0038741294,0.00072379585,0.00001539013,0.00068663206],"about_ca_topic_score_codex":0.000014469986,"about_ca_topic_score_gemma":0.00025067435,"teacher_disagreement_score":0.6569791,"about_ca_system_score_codex":0.000046036865,"about_ca_system_score_gemma":0.000024897225,"threshold_uncertainty_score":0.8997377},"labels":[],"label_agreement":null},{"id":"W4248925257","doi":"10.22215/etd/2017-12146","title":"Evaluation of Acoustic Frequency Methods Coupled to Blade Element Momentum Theory for the Prediction of Propeller Noise","year":2017,"lang":"en","type":"dissertation","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Carleton University","funders":"","keywords":"Aerodynamics; Propeller; Noise (video); Acoustics; Range (aeronautics); Microphone; Mach number; Chord (peer-to-peer); Solver; Blade (archaeology); Engineering; Computer science; Structural engineering; Marine engineering; Aerospace engineering; Sound pressure; Physics; Artificial intelligence","score_opus":0.033486870807530635,"score_gpt":0.33968063019118794,"score_spread":0.3061937593836573,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4248925257","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.02280949,0.0006610539,0.9533212,0.000017713557,0.0030714213,0.0038180486,0.00027205204,0.000062821266,0.015966162],"genre_scores_gemma":[0.96702534,0.00032072107,0.025738005,0.0000064753817,0.00021797966,0.0012264729,0.00065841066,0.00011346049,0.00469312],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9983243,0.000080093916,0.00057357154,0.00021223343,0.0006244332,0.00018541169],"domain_scores_gemma":[0.997928,0.00026512603,0.000271031,0.0005670607,0.00092894706,0.00003979161],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0034818435,0.00023542836,0.0003278456,0.00011544199,0.00009793544,0.000022817905,0.00035205725,0.00018699389,0.00025177063],"category_scores_gemma":[0.000654939,0.00017015942,0.00012498663,0.0000710433,0.000025081303,0.000049615588,0.000015437507,0.00017017909,0.0000020201633],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00005569683,0.000059253576,0.000004590069,0.0008908439,0.0006297737,8.024114e-8,0.00081152824,0.65829545,0.29113397,0.0027030397,0.0006650767,0.04475067],"study_design_scores_gemma":[0.00039500272,0.00010137756,0.00048105782,0.00016202709,0.0016262585,1.435074e-7,0.0006112146,0.97972465,0.008306753,0.008360802,0.00007677629,0.00015391246],"about_ca_topic_score_codex":0.0000255456,"about_ca_topic_score_gemma":0.0001237059,"teacher_disagreement_score":0.9442159,"about_ca_system_score_codex":0.00016051835,"about_ca_system_score_gemma":0.00015094712,"threshold_uncertainty_score":0.69389},"labels":[],"label_agreement":null},{"id":"W4251363633","doi":"10.1063/5.0048582.6","title":"10.1063/5.0048582.6","year":2021,"lang":"en","type":"dataset","venue":"Default Digital Object Group","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Ontario Institute of Technology","funders":"","keywords":"Excitation; Resonance (particle physics); Wind tunnel; Acoustic resonance; Acoustics; Wake; Particle image velocimetry; Vortex; Leading edge; Materials science; Flapping; Vortex shedding; Mechanics; Vortex generator; Reynolds number; Optics; Physics; Structural engineering; Engineering; Turbulence; Atomic physics","score_opus":0.005066727996708143,"score_gpt":0.19766858512963006,"score_spread":0.1926018571329219,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4251363633","genre_codex":"dataset","genre_gemma":"dataset","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"dataset","genre_consensus":"dataset","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.000116271236,0.000926011,0.00044207805,0.0000054302996,0.0016236013,0.00019041458,0.9778125,0.00038288132,0.018500762],"genre_scores_gemma":[0.0012764022,0.0003149179,0.00010821272,0.00005523827,0.000793109,0.000045239558,0.9941325,0.00014808893,0.0031262524],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.9977132,0.00001473751,0.00054177106,0.0005723354,0.0004969447,0.0006610038],"domain_scores_gemma":[0.9983929,0.00014536855,0.00008556194,0.0010793201,0.00008885507,0.00020804399],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.000089257825,0.00069608365,0.000672084,0.00017734,0.000083366554,0.00070772285,0.000666573,0.0006074319,0.00202822],"category_scores_gemma":[0.00017520963,0.0007345975,0.00033368287,0.00036832254,0.00007440858,0.0002836129,0.00028845275,0.0008354997,0.004566478],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000050293206,0.00006390961,7.4889107e-7,0.0003030314,0.0001537724,0.00033853995,0.000004423672,0.00184549,0.000013277304,0.0000117590835,0.9934502,0.003809817],"study_design_scores_gemma":[0.00021331788,0.000058951136,0.000007839308,0.00014845128,0.00007823144,0.00005778592,0.000017013881,0.0050165835,0.0000059032836,0.00009678254,0.99344987,0.0008492773],"about_ca_topic_score_codex":0.000016781609,"about_ca_topic_score_gemma":0.000080897,"teacher_disagreement_score":0.016319988,"about_ca_system_score_codex":0.00019755337,"about_ca_system_score_gemma":0.000055313318,"threshold_uncertainty_score":0.9995105},"labels":[],"label_agreement":null},{"id":"W4253383226","doi":"10.1121/1.4799200","title":"A robust numerical approach for the prediction of turbofan engine noise","year":2013,"lang":"en","type":"article","venue":"Proceedings of meetings on acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"Compute Canada","keywords":"Turbofan; Jet engine; Takeoff; Jet noise; Turbulence; Acoustics; Nozzle; Noise (video); Computational fluid dynamics; Computer science; Large eddy simulation; Jet (fluid); Intermittency; Simulation; Engineering; Aerospace engineering; Mechanics; Physics","score_opus":0.013047846091878765,"score_gpt":0.18662061751612483,"score_spread":0.17357277142424607,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4253383226","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.3739645,0.0001676529,0.6137227,0.00016788825,0.0005732921,0.0016634865,0.00018147434,0.0003667272,0.009192322],"genre_scores_gemma":[0.92572004,0.000114536204,0.07361645,0.000026017424,0.00024327893,0.00013801611,0.000010634797,0.0000646923,0.00006631121],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99873954,0.0000015065955,0.00045503123,0.00020049092,0.00030811585,0.00029534084],"domain_scores_gemma":[0.99883765,0.00021892194,0.00016761568,0.0001175773,0.00058643013,0.000071824456],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002770637,0.00021714317,0.00029061484,0.00008504433,0.00007284092,0.00003799755,0.00033546716,0.00013968146,0.000011731384],"category_scores_gemma":[0.0004800694,0.00016634619,0.00009378021,0.00024603674,0.000082844126,0.000092602735,0.000047266294,0.0002537222,0.0000018285581],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00002783104,0.00015026897,0.00035120596,0.0011051934,0.00010719482,6.976786e-8,0.00029383754,0.80115473,0.17904985,0.0012384834,0.012789759,0.0037315795],"study_design_scores_gemma":[0.0003055632,0.00014349027,0.00074527576,0.00006696132,0.00010917104,0.0000024560516,0.00041248061,0.9927317,0.0049614157,0.00024700392,0.00013336539,0.00014111606],"about_ca_topic_score_codex":0.000007050832,"about_ca_topic_score_gemma":3.3673935e-8,"teacher_disagreement_score":0.55175555,"about_ca_system_score_codex":0.00004315342,"about_ca_system_score_gemma":0.000010419246,"threshold_uncertainty_score":0.6783401},"labels":[],"label_agreement":null},{"id":"W4254237032","doi":"10.1115/1.862ama_ch8","title":"An Efficient Far-Field Noise Prediction Framework for the Next Generation of Aircraft Landing Gear Designs","year":2021,"lang":"en","type":"book-chapter","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto","funders":"","keywords":"Airframe; Turbofan; Aircraft noise; Landing gear; Noise (video); Aerospace engineering; Jet engine; Jet noise; Jet (fluid); Engineering; Aeronautics; Automotive engineering; Acoustics; Computer science; Noise reduction; Physics","score_opus":0.054864310072375876,"score_gpt":0.2520803507321847,"score_spread":0.19721604065980883,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4254237032","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.00061414955,0.0005236615,0.9848804,0.000029573926,0.0013492431,0.0003637422,0.000089211804,0.00010784392,0.012042197],"genre_scores_gemma":[0.80303323,0.0029278402,0.15145503,0.00029952478,0.004672575,0.00013703873,0.000739639,0.00039901197,0.036336135],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991854,0.0000054368115,0.00028509917,0.0002017712,0.0001746935,0.00014764049],"domain_scores_gemma":[0.9991704,0.00026757692,0.000058165224,0.00036728656,0.00009448834,0.000042043714],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015461865,0.00020125277,0.00020643216,0.000055105244,0.00010180923,0.00006337207,0.00014654103,0.0003855749,0.00021656246],"category_scores_gemma":[0.000041327396,0.00016194185,0.00011963227,0.000024710927,0.0000179282,0.00003308293,0.000023476738,0.0003118482,0.000003315038],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000004672884,0.000010051936,0.0000031578943,0.00008550008,0.000088283006,0.0000013195609,0.000077765486,0.8354354,0.0068054474,0.15369333,0.0007651308,0.003029962],"study_design_scores_gemma":[0.00007224139,0.00006965767,0.000004766006,0.00010877697,0.00010331052,0.0000016200026,0.000032793043,0.99408907,0.0007175263,0.0015497344,0.0030855355,0.00016495593],"about_ca_topic_score_codex":0.0000044085464,"about_ca_topic_score_gemma":0.000021448162,"teacher_disagreement_score":0.83342534,"about_ca_system_score_codex":0.000057424993,"about_ca_system_score_gemma":0.000022956556,"threshold_uncertainty_score":0.6603797},"labels":[],"label_agreement":null},{"id":"W4254989839","doi":"10.1063/5.0048582.5","title":"10.1063/5.0048582.5","year":2021,"lang":"en","type":"dataset","venue":"Default Digital Object Group","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Ontario Institute of Technology","funders":"","keywords":"Excitation; Resonance (particle physics); Wind tunnel; Acoustic resonance; Acoustics; Wake; Particle image velocimetry; Materials science; Vortex; Leading edge; Flapping; Vortex shedding; Mechanics; Vortex generator; Reynolds number; Optics; Physics; Structural engineering; Turbulence; Engineering; Atomic physics","score_opus":0.005076337502701541,"score_gpt":0.19773461886271812,"score_spread":0.1926582813600166,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4254989839","genre_codex":"dataset","genre_gemma":"dataset","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"dataset","genre_consensus":"dataset","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.000116390154,0.000926298,0.0004408589,0.000005425263,0.0016375495,0.00019045314,0.9779865,0.00038294212,0.018313557],"genre_scores_gemma":[0.0013022221,0.00031485042,0.000108256,0.000055280514,0.0007977101,0.000045245426,0.9941028,0.00014808208,0.0031255917],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.9977132,0.000014737616,0.0005417869,0.00057231914,0.00049694034,0.0006609958],"domain_scores_gemma":[0.9983927,0.00014538612,0.00008553798,0.0010793244,0.00008899572,0.00020803513],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.00008925792,0.0006960681,0.0006720761,0.00017731906,0.000083390114,0.0007077754,0.000666751,0.0006074206,0.00202419],"category_scores_gemma":[0.00017548428,0.0007345853,0.00033368653,0.00036823394,0.00007440466,0.0002835837,0.00028848503,0.0008355232,0.0045623346],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000005035207,0.00006391432,7.130286e-7,0.00030273624,0.00015579753,0.00033871242,0.000004445824,0.00194797,0.000013400009,0.000011674621,0.9933123,0.0038432896],"study_design_scores_gemma":[0.00021342542,0.00005908758,0.000007776066,0.00014844847,0.000078258025,0.000057790057,0.00001714721,0.0049634087,0.0000058526634,0.00009673387,0.9935028,0.000849252],"about_ca_topic_score_codex":0.00001673912,"about_ca_topic_score_gemma":0.00008080893,"teacher_disagreement_score":0.016116235,"about_ca_system_score_codex":0.00019744204,"about_ca_system_score_gemma":0.000055313798,"threshold_uncertainty_score":0.9995105},"labels":[],"label_agreement":null},{"id":"W4256289100","doi":"10.1063/5.0026552.2","title":"10.1063/5.0026552.2","year":2020,"lang":"en","type":"dataset","venue":"Default Digital Object Group","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Ontario Institute of Technology","funders":"","keywords":"Excitation; Mechanics; Vortex; Physics; Resonance (particle physics); Acoustics; Coupling (piping); Flow (mathematics); Trailing edge; Reynolds number; Turbulence; Materials science; Atomic physics","score_opus":0.006052908467327483,"score_gpt":0.1947890998202256,"score_spread":0.18873619135289812,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4256289100","genre_codex":"dataset","genre_gemma":"dataset","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"dataset","genre_consensus":"dataset","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.000033876408,0.00025092068,0.00059849187,0.000012167351,0.0011358887,0.00025075517,0.98140126,0.00059360394,0.01572303],"genre_scores_gemma":[0.0022253643,0.00017437538,0.00009274485,0.000105085805,0.0009492589,0.000040545532,0.995049,0.00016182833,0.0012018083],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.99782103,0.000011603239,0.0005327202,0.000554222,0.00047725902,0.0006031735],"domain_scores_gemma":[0.9986943,0.00012567952,0.00009181524,0.00075997465,0.000049241957,0.00027900017],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.00006378541,0.00071105245,0.00065709604,0.00014826153,0.00007653214,0.0005521272,0.000792711,0.00052636745,0.0010300815],"category_scores_gemma":[0.00017140133,0.0007356704,0.0002980953,0.00033586367,0.00007601046,0.00027581435,0.00027271485,0.0008973719,0.018752825],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000010415535,0.00003912696,5.051077e-7,0.00031114704,0.00013695964,0.00019492823,0.000007738643,0.0015156852,0.000010714374,0.000014102677,0.9944227,0.0033360142],"study_design_scores_gemma":[0.00022345656,0.00011617432,0.0000053739323,0.00008154481,0.00007555513,0.000025444833,0.000010863568,0.010929946,0.0000033205795,0.00012608187,0.9875711,0.0008311138],"about_ca_topic_score_codex":0.0000113599,"about_ca_topic_score_gemma":0.000027280237,"teacher_disagreement_score":0.017722743,"about_ca_system_score_codex":0.00015168289,"about_ca_system_score_gemma":0.00003365336,"threshold_uncertainty_score":0.9998831},"labels":[],"label_agreement":null},{"id":"W4280599179","doi":"10.1007/978-981-19-0507-0_7","title":"Numerical Simulations of 15-Degree Inclined Dense Jets in Stagnate Water Over a Sloped Bottom","year":2022,"lang":"en","type":"book-chapter","venue":"Lecture notes in civil engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Ottawa","funders":"","keywords":"Froude number; Mechanics; Dilution; Turbulence; Reynolds-averaged Navier–Stokes equations; Plume; Jet (fluid); Mixing (physics); Environmental science; Geology; Flow (mathematics); Meteorology; Physics; Thermodynamics","score_opus":0.011172132843859359,"score_gpt":0.21275065884938732,"score_spread":0.20157852600552795,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4280599179","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0672689,0.0048357053,0.87428623,0.0002997082,0.0051444527,0.0025089013,0.0011345311,0.0014945294,0.043027062],"genre_scores_gemma":[0.9960746,0.0001714346,0.0025809065,0.000032634725,0.00021597299,0.00002586425,0.00019087466,0.00028605812,0.0004216484],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99784344,0.000014051125,0.0007911608,0.00041590407,0.00039588998,0.00053954794],"domain_scores_gemma":[0.99883884,0.0004742246,0.00006982605,0.00049324456,0.000042167267,0.00008170539],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00018630725,0.0005986062,0.0007599112,0.0008271455,0.000035107794,0.000023957718,0.00033262043,0.00051244383,0.0010771182],"category_scores_gemma":[0.00020140012,0.0005999817,0.00016564639,0.00021922801,0.000028700899,0.00007957972,0.00019105019,0.0018244612,0.000006442013],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000012961055,0.000018101222,0.00007703852,0.00028764745,0.0000698414,0.000111365654,0.00028645655,0.99459594,0.0025856555,0.0008994339,0.000009882489,0.0010456656],"study_design_scores_gemma":[0.00053568115,0.00003470257,0.00014934377,0.00028451026,0.000033957556,0.0000067153915,7.423348e-7,0.98938775,0.00032456816,0.0029150888,0.0056343894,0.0006925413],"about_ca_topic_score_codex":0.00005676775,"about_ca_topic_score_gemma":0.0007817317,"teacher_disagreement_score":0.9288057,"about_ca_system_score_codex":0.0005466595,"about_ca_system_score_gemma":0.00005098267,"threshold_uncertainty_score":0.999836},"labels":[],"label_agreement":null},{"id":"W4282542916","doi":"10.2514/6.2022-2816","title":"Acoustic Investigation of the Transonic RAE 2822 Airfoil with Large-Eddy Simulation","year":2022,"lang":"en","type":"article","venue":"28th AIAA/CEAS Aeroacoustics 2022 Conference","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure; Université de Sherbrooke","funders":"","keywords":"Airfoil; Acoustics; Mach number; Physics; Trailing edge; Transonic; Chord (peer-to-peer); Leading edge; Relative wind; Noise (video); Mechanics; Angle of attack; Aerospace engineering; Aerodynamics; Computer science; Engineering","score_opus":0.009308454220051936,"score_gpt":0.19153131653217526,"score_spread":0.1822228623121233,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4282542916","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.47868103,0.00017394671,0.5174413,0.00008615981,0.0010944682,0.0006211341,0.0006175792,0.00024417686,0.0010402334],"genre_scores_gemma":[0.9976403,0.000062350424,0.0014312381,0.0001469744,0.0000918056,0.00009819135,0.00010326652,0.000096544776,0.0003292989],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9974381,0.00013314933,0.00055470254,0.00040919663,0.0009193304,0.0005455223],"domain_scores_gemma":[0.998452,0.00023133338,0.00020287902,0.0007156508,0.0002580441,0.00014005981],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0004574059,0.00037510088,0.00037901397,0.00013225344,0.0005235276,0.000060329246,0.0007060576,0.00011352785,0.0007098725],"category_scores_gemma":[0.00009059297,0.00032814615,0.00011504694,0.000806464,0.0001856716,0.00012385883,0.0002093914,0.0008755955,0.0000081855615],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000029868763,0.00005113201,0.0008152057,0.00016090946,0.00006725999,0.00000743521,0.0006617265,0.98287404,0.012782656,0.0016159996,0.00037449098,0.0005593036],"study_design_scores_gemma":[0.0007219747,0.00013937808,0.0028771034,0.000059759088,0.00020790883,0.000011931254,0.00067244587,0.9929123,0.00034525743,0.0009432375,0.0006963766,0.00041233565],"about_ca_topic_score_codex":0.000017404785,"about_ca_topic_score_gemma":0.00013688,"teacher_disagreement_score":0.5189593,"about_ca_system_score_codex":0.00024101802,"about_ca_system_score_gemma":0.00030957116,"threshold_uncertainty_score":0.99991703},"labels":[],"label_agreement":null},{"id":"W4282548726","doi":"10.2514/6.2022-2985","title":"Investigation of Curle's Dipolar Sources on a Porous Airfoil Interacting with Incoming Turbulence","year":2022,"lang":"en","type":"article","venue":"28th AIAA/CEAS Aeroacoustics 2022 Conference","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Gauss Centre for Supercomputing; European Commission","keywords":"Airfoil; Mechanics; Reynolds number; Turbulence; Wake; Physics; Mach number; Reynolds stress; Vortex","score_opus":0.011730730635202967,"score_gpt":0.18906327575092005,"score_spread":0.17733254511571708,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4282548726","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.94538534,0.00025504472,0.049830917,0.000067392524,0.001028148,0.0003218034,0.00024008246,0.00028269485,0.0025885669],"genre_scores_gemma":[0.9948872,0.0000730898,0.0043983883,0.0001601335,0.00010968654,0.00007510502,0.00006894917,0.00009429908,0.00013318965],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99760264,0.000098470904,0.0005645001,0.00046381782,0.00077530113,0.00049526716],"domain_scores_gemma":[0.998433,0.00037994422,0.0002845777,0.0005401544,0.00019569526,0.00016660948],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00043369495,0.00039658512,0.00042577385,0.00023264565,0.0003926362,0.00009174518,0.00061558984,0.00008628395,0.00025879632],"category_scores_gemma":[0.0001859682,0.00040871283,0.00006794294,0.0005185572,0.0001648691,0.0001586063,0.00030589092,0.0010812337,0.000007753836],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00007845622,0.000061001574,0.0029055455,0.0002657074,0.00011045495,0.000061663064,0.002084392,0.9643096,0.023011325,0.0028575067,0.0005433757,0.0037110127],"study_design_scores_gemma":[0.00051580096,0.000473028,0.00066747447,0.00032439068,0.00011173515,0.00004872448,0.0021566756,0.9917995,0.0019177845,0.0007885025,0.0005676719,0.00062873896],"about_ca_topic_score_codex":0.0000714887,"about_ca_topic_score_gemma":0.00004542641,"teacher_disagreement_score":0.04950181,"about_ca_system_score_codex":0.00024284796,"about_ca_system_score_gemma":0.0001730213,"threshold_uncertainty_score":0.99983644},"labels":[],"label_agreement":null},{"id":"W4282573435","doi":"10.2514/6.2022-2894","title":"Flow-field and Noise Characterization of a Controlled-Diffusion Airfoil","year":2022,"lang":"en","type":"article","venue":"28th AIAA/CEAS Aeroacoustics 2022 Conference","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":9,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Strouhal number; Airfoil; Stall (fluid mechanics); Reynolds number; Flow separation; Physics; Boundary layer; Aerodynamics; Mechanics; Anechoic chamber; Noise (video); Acoustics; Turbulence; Computer science","score_opus":0.005591471970554196,"score_gpt":0.18315777393095625,"score_spread":0.17756630196040205,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4282573435","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7628521,0.00020937726,0.23143776,0.000118924356,0.0013176649,0.00052026147,0.0005236298,0.00019119908,0.0028291359],"genre_scores_gemma":[0.9970788,0.0006650118,0.0012356793,0.00016308538,0.00010154843,0.00011090153,0.00015952218,0.000056842266,0.00042862253],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99824893,0.000064008564,0.0005270706,0.00033139947,0.00046990186,0.00035870136],"domain_scores_gemma":[0.99900275,0.00016329884,0.00014972517,0.00038481347,0.00015858411,0.00014082166],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00031018548,0.00028930107,0.0005086576,0.00016051682,0.0002530585,0.000058195033,0.00031579714,0.00010543207,0.0007727584],"category_scores_gemma":[0.00013187758,0.00031375664,0.000084910076,0.00027764202,0.000066390196,0.00008620375,0.0003223206,0.00050108676,0.0000044969756],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0002998016,0.00022092825,0.0006883601,0.00035898792,0.00014565146,0.00004093135,0.0007911798,0.16445377,0.8072193,0.005404807,0.001079125,0.01929715],"study_design_scores_gemma":[0.0015711833,0.00017901207,0.00086425553,0.000033183584,0.00010285921,0.000015139918,0.000201421,0.994762,0.0006168498,0.0003965417,0.0009232165,0.00033434125],"about_ca_topic_score_codex":0.000014325123,"about_ca_topic_score_gemma":0.000010746622,"teacher_disagreement_score":0.8303082,"about_ca_system_score_codex":0.00007699559,"about_ca_system_score_gemma":0.000088519286,"threshold_uncertainty_score":0.99993145},"labels":[],"label_agreement":null},{"id":"W4282586356","doi":"10.2514/6.2022-2948","title":"Aeroacoustic investigation of an Urban-Air-Mobility ducted fan","year":2022,"lang":"en","type":"article","venue":"28th AIAA/CEAS Aeroacoustics 2022 Conference","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Anechoic chamber; Acoustics; Wind tunnel; Aeroacoustics; Subsonic and transonic wind tunnel; Directivity; Rotor (electric); Sound pressure; Noise (video); Aerospace engineering; Physics; Engineering; Transonic; Aerodynamics; Computer science; Electrical engineering","score_opus":0.011690878203802659,"score_gpt":0.2031918110836955,"score_spread":0.19150093287989284,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4282586356","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8725216,0.00026025815,0.120840445,0.000054452143,0.0017541795,0.00070796016,0.0012584913,0.0006434464,0.0019591658],"genre_scores_gemma":[0.9927991,0.000065915585,0.0056624752,0.00013430386,0.00019605609,0.00016969106,0.0005774227,0.00012750534,0.0002675017],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9963948,0.0002186628,0.00092861714,0.00072775973,0.0010053435,0.0007248138],"domain_scores_gemma":[0.99751025,0.00024763562,0.00025479385,0.0011788205,0.0004234585,0.00038502706],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0007531761,0.0005326539,0.0006196419,0.0002704138,0.00044959655,0.00006903164,0.0009914926,0.00018292814,0.0009906779],"category_scores_gemma":[0.00027133772,0.0006358721,0.00013913318,0.00090595515,0.00032579325,0.0002430919,0.00039982825,0.0010787986,0.000013920101],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000044176566,0.00022447815,0.0010863871,0.00032433565,0.0001013096,0.000037639475,0.00088230905,0.8740997,0.114506856,0.0048516714,0.0025159554,0.0013252186],"study_design_scores_gemma":[0.0005710405,0.00030578382,0.0037743945,0.000038777674,0.00016011347,0.000022386937,0.00096743216,0.98817796,0.0016248164,0.003150197,0.0004736162,0.00073349266],"about_ca_topic_score_codex":0.00006267711,"about_ca_topic_score_gemma":0.00004249689,"teacher_disagreement_score":0.120277524,"about_ca_system_score_codex":0.00037057512,"about_ca_system_score_gemma":0.00034190353,"threshold_uncertainty_score":0.9999226},"labels":[],"label_agreement":null},{"id":"W4282587439","doi":"10.2514/6.2022-2861","title":"Wall-Resolved LES of a Linear Compressor Cascade with Moving Endwall","year":2022,"lang":"en","type":"article","venue":"28th AIAA/CEAS Aeroacoustics 2022 Conference","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Adiabatic wall; Aerodynamics; Cascade; Mechanics; Vortex; Acoustics; Physics; Noise (video); Chord (peer-to-peer); Mach number; Compressible flow; Directivity; Large eddy simulation; Gas compressor; Compressibility; Boundary layer; Turbulence; Engineering; Computer science","score_opus":0.014689769815665662,"score_gpt":0.2067175626737007,"score_spread":0.19202779285803503,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4282587439","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.49555165,0.0010760189,0.4917159,0.0001143565,0.0009427597,0.000726612,0.0010466257,0.00058140425,0.00824467],"genre_scores_gemma":[0.987747,0.00023613755,0.010871737,0.00008182696,0.00010489413,0.000107635264,0.00011663965,0.00012541929,0.00060869113],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9974148,0.00008075498,0.00058103935,0.00047477148,0.0008088029,0.00063980126],"domain_scores_gemma":[0.9984918,0.00021055614,0.00017816546,0.0006791445,0.00024236782,0.00019792066],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0003055876,0.00043902165,0.00055511866,0.0001825155,0.00042518144,0.0000566902,0.0008215639,0.000122033794,0.0009402921],"category_scores_gemma":[0.000069283924,0.00045068434,0.00010988675,0.000429679,0.00017909602,0.000084984975,0.0004246913,0.0010230535,0.0000079061065],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00007069178,0.000142244,0.0004308074,0.00034148432,0.000178085,0.00009829694,0.00069492316,0.9564777,0.034900393,0.0030379125,0.0012813489,0.0023460945],"study_design_scores_gemma":[0.0006957746,0.0002173549,0.00034047948,0.000070715025,0.00014340068,0.000039168735,0.0007757843,0.9914265,0.00074676506,0.00022687844,0.0047469395,0.00057020143],"about_ca_topic_score_codex":0.00016493916,"about_ca_topic_score_gemma":0.00013011755,"teacher_disagreement_score":0.49219537,"about_ca_system_score_codex":0.00017957075,"about_ca_system_score_gemma":0.00017285647,"threshold_uncertainty_score":0.999973},"labels":[],"label_agreement":null},{"id":"W4282588736","doi":"10.2514/6.2022-2859","title":"Aeroacoustic investigation of automotive engine cooling modules using the Lattice-Boltzmann Method","year":2022,"lang":"en","type":"article","venue":"28th AIAA/CEAS Aeroacoustics 2022 Conference","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Overheating (electricity); Automotive engineering; Acoustics; Noise (video); Duct (anatomy); Automotive engine; Wind tunnel; Computation; Mach number; Anechoic chamber; Automotive industry; Mechanical engineering; Engineering; Computer science; Aerospace engineering; Electrical engineering; Physics","score_opus":0.025385546908868958,"score_gpt":0.249622120256783,"score_spread":0.22423657334791403,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4282588736","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.21843551,0.00045706122,0.7778466,0.000070899536,0.0013956677,0.0004894535,0.00050739053,0.00027914825,0.00051830045],"genre_scores_gemma":[0.93220574,0.00010399993,0.06687114,0.0001526764,0.00020055966,0.000084935484,0.00011069139,0.00012453632,0.00014572876],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99673957,0.00028361092,0.0008243532,0.0005375597,0.00092412,0.0006908082],"domain_scores_gemma":[0.9974216,0.00075129693,0.00030644934,0.0008091848,0.0005168907,0.00019454317],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0011837628,0.00050457864,0.000588661,0.00025720004,0.00067529286,0.000105491716,0.0009243985,0.00014440627,0.00038249308],"category_scores_gemma":[0.00038849594,0.0004890729,0.00015851708,0.0009241807,0.0002551211,0.0001533997,0.0005090461,0.0011927385,0.0000057134716],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000018092354,0.000038558323,0.00009883896,0.0001665094,0.00014132081,0.000017697335,0.0009988543,0.9624037,0.03097166,0.003521271,0.00040981566,0.0012136695],"study_design_scores_gemma":[0.00037440791,0.00008529056,0.0003959214,0.00006123963,0.0003547332,0.000036486832,0.0017336424,0.9919303,0.0013940285,0.0029427526,0.00017386851,0.00051731605],"about_ca_topic_score_codex":0.00007232793,"about_ca_topic_score_gemma":0.000020025345,"teacher_disagreement_score":0.7137702,"about_ca_system_score_codex":0.0003524694,"about_ca_system_score_gemma":0.00025485625,"threshold_uncertainty_score":0.9997561},"labels":[],"label_agreement":null},{"id":"W4282982892","doi":"10.4271/2022-01-0934","title":"Effects of Boundary Layer and Local Volumetric Cells Refinements on Compressor Direct Noise Computation","year":2022,"lang":"en","type":"article","venue":"SAE International Journal of Advances and Current Practices in Mobility","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Volvo (Canada)","funders":"","keywords":"Turbocharger; Gas compressor; Noise (video); Acoustics; Computer science; Computational fluid dynamics; Computation; Grid; Engineering; Mechanical engineering; Physics; Aerospace engineering; Algorithm; Mathematics; Geometry","score_opus":0.010727868293123523,"score_gpt":0.3034218275920519,"score_spread":0.2926939592989284,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4282982892","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9771691,0.014683756,0.005333243,0.000031013013,0.0024523202,0.00010886085,0.000034492925,0.0000058548203,0.00018138123],"genre_scores_gemma":[0.9929457,0.0063334536,0.0006316888,0.000011991908,0.000057853707,0.0000057760853,0.000004153663,0.000006505792,0.0000029177818],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989696,0.00007752736,0.0003680305,0.00011415389,0.00039207118,0.00007857403],"domain_scores_gemma":[0.9988373,0.0005198037,0.0004531059,0.000047510035,0.000108211934,0.00003407678],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00044089672,0.00008812006,0.00016880741,0.00015788233,0.000042744672,0.000030921154,0.0001463588,0.000015617961,0.000011969737],"category_scores_gemma":[0.00014099212,0.000083661995,0.00003387321,0.00010603993,0.000057513953,0.00032493292,0.00008837331,0.00033163125,1.7761823e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00031218727,0.00073327206,0.008618721,0.0005243394,0.000095252835,0.000024232677,0.00018646689,0.6816242,0.0023639516,0.000054820684,0.000084505606,0.30537808],"study_design_scores_gemma":[0.0045680804,0.0013329408,0.14040686,0.00054444466,0.00015198403,0.000065946915,0.000617226,0.7760296,0.0020911815,0.0035662202,0.07015425,0.00047125408],"about_ca_topic_score_codex":0.000007044911,"about_ca_topic_score_gemma":0.000009210333,"teacher_disagreement_score":0.30490682,"about_ca_system_score_codex":0.000108500426,"about_ca_system_score_gemma":0.000017210452,"threshold_uncertainty_score":0.34116372},"labels":[],"label_agreement":null},{"id":"W4283690577","doi":"10.3390/fluids7070218","title":"Recent Advances in Passive Acoustic Localization Methods via Aircraft and Wake Vortex Aeroacoustics","year":2022,"lang":"en","type":"article","venue":"Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":14,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Waterloo","funders":"","keywords":"Aeroacoustics; Acoustics; Wake; Vortex; Beamforming; Noise (video); Wake turbulence; Computer science; Aerospace engineering; Physics; Engineering; Telecommunications; Meteorology; Sound pressure; Artificial intelligence","score_opus":0.006865787904208205,"score_gpt":0.2530370149254175,"score_spread":0.24617122702120933,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4283690577","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.008228266,0.0076210047,0.98163265,0.00003665639,0.0012453961,0.0001851084,0.00003898999,0.00014043307,0.0008715204],"genre_scores_gemma":[0.9486419,0.015101176,0.035463512,0.00018764075,0.000157737,0.00010432277,0.00007418197,0.000094980416,0.00017456841],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99892575,0.00007774233,0.00028892467,0.00023192819,0.0001985856,0.0002770904],"domain_scores_gemma":[0.99955595,0.00011364147,0.000027308888,0.00019116976,0.000042645366,0.00006928191],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00028138832,0.00017373051,0.00020600132,0.00011447559,0.00012875513,0.000022936236,0.00013758185,0.00006413391,0.00017918657],"category_scores_gemma":[0.000077787205,0.00019407833,0.000024887257,0.00037080902,0.000042120162,0.0000941786,0.00012200798,0.00030471454,0.0000039407687],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000004925072,0.000021452639,0.00022558602,0.00005424589,0.000010518121,0.000017301034,0.00014716286,0.86773103,0.006037853,0.00015837888,0.0004178725,0.12517366],"study_design_scores_gemma":[0.00023050419,0.000048490754,0.0003713148,0.000011413742,0.000027864298,0.000012437841,0.00016886865,0.96304226,0.00010983798,0.0014925139,0.034259878,0.00022459353],"about_ca_topic_score_codex":0.0000029243763,"about_ca_topic_score_gemma":0.000030810705,"teacher_disagreement_score":0.94616914,"about_ca_system_score_codex":0.00020281246,"about_ca_system_score_gemma":0.000020318155,"threshold_uncertainty_score":0.79142845},"labels":[],"label_agreement":null},{"id":"W4283732722","doi":"10.1038/s41598-022-15026-8","title":"Mitigation of jet cross-flow induced vibrations using an innovative biomimetic nozzle design inspired by shark gill geometry","year":2022,"lang":"en","type":"article","venue":"Scientific Reports","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":16,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Polytechnique Montréal","funders":"Framatome; Natural Sciences and Engineering Research Council of Canada","keywords":"Nozzle; Baffle; Jet (fluid); Mixing (physics); Mechanics; Flow (mathematics); Coolant; Materials science; Mechanical engineering; Physics; Engineering","score_opus":0.026604276261553237,"score_gpt":0.26373499022089664,"score_spread":0.2371307139593434,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4283732722","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.86787647,0.0000443811,0.12815396,0.0000054917764,0.0033098655,0.00027141903,0.00008489205,0.0000974696,0.00015604371],"genre_scores_gemma":[0.9845354,7.1948006e-7,0.014825198,0.000010715788,0.00002759867,0.000031497213,0.00043874842,0.000036929374,0.00009317249],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9981091,0.000055914687,0.00064385415,0.0004424232,0.00049571303,0.0002530152],"domain_scores_gemma":[0.99879086,0.000038368256,0.0002562975,0.0005560746,0.0002849273,0.000073490686],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0013277546,0.0001555947,0.00019153711,0.00037891843,0.0005742058,0.00019783412,0.00017874707,0.00006410852,0.0001925155],"category_scores_gemma":[0.00012531338,0.0001747268,0.000045047756,0.0023334138,0.00014243725,0.00033703377,0.00010231918,0.00019041666,0.0000013087123],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000001512347,0.000050342827,0.00030836783,0.000013247515,0.000014226677,0.000014346332,0.00022955157,0.44485596,0.55356205,0.000021849357,0.0005808329,0.0003477257],"study_design_scores_gemma":[0.000099502206,0.000041121988,0.00032485812,0.000011132527,0.000013520394,0.000031120628,0.00007842508,0.868021,0.12986921,0.0008285973,0.0004764027,0.00020508115],"about_ca_topic_score_codex":0.000017169727,"about_ca_topic_score_gemma":0.0000023042041,"teacher_disagreement_score":0.42369282,"about_ca_system_score_codex":0.00017178556,"about_ca_system_score_gemma":0.0001313423,"threshold_uncertainty_score":0.7125152},"labels":[],"label_agreement":null},{"id":"W4283743366","doi":"10.1121/10.0012188","title":"Semi-empirical wall pressure spectral modeling for zero and favorable pressure gradient flows","year":2022,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Carleton University","funders":"","keywords":"Pressure gradient; Spectral density; Adverse pressure gradient; Turbulence; Mechanics; Range (aeronautics); Boundary layer; Density gradient; Power (physics); Materials science; Physics; Thermodynamics; Flow separation; Mathematics; Statistics","score_opus":0.0124413532020709,"score_gpt":0.23253555575950885,"score_spread":0.22009420255743795,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4283743366","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.06603004,0.0030664965,0.92775303,0.0020913328,0.00053639105,0.0003115454,0.00010792698,0.000030083294,0.00007315488],"genre_scores_gemma":[0.96552044,0.0005580236,0.03316046,0.00040669114,0.0001725346,0.000006657343,0.0000011709868,0.00003856778,0.00013547658],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9986053,0.00007461876,0.00042932722,0.000109466,0.0004561526,0.0003251011],"domain_scores_gemma":[0.9990343,0.0003442472,0.00016554844,0.00026248067,0.0000987726,0.00009468722],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00063109834,0.00017142038,0.00035524412,0.000015711581,0.00037351027,0.000021279751,0.00060768845,0.00005960307,0.000032415344],"category_scores_gemma":[0.00007507429,0.00010605143,0.00041455374,0.00015687717,0.00016343404,0.00005501511,0.0002514153,0.0007850515,1.9793238e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000556145,0.00005556279,0.000022405384,0.000104114486,0.0003708807,4.4106437e-7,0.0007534309,0.97136784,0.0041069877,0.000016067566,0.022618677,0.0005280058],"study_design_scores_gemma":[0.00032282,0.0001945305,0.000019022164,0.00002332631,0.00069535204,0.000047650727,0.0006459973,0.98692846,0.00004266706,0.0031972178,0.0077568237,0.00012614005],"about_ca_topic_score_codex":0.0000141025,"about_ca_topic_score_gemma":4.0154706e-7,"teacher_disagreement_score":0.89949036,"about_ca_system_score_codex":0.00006073659,"about_ca_system_score_gemma":0.000046625777,"threshold_uncertainty_score":0.4324652},"labels":[],"label_agreement":null},{"id":"W4285225475","doi":"10.1007/978-981-19-1065-4_34","title":"Numerical Simulation of Turbulent Offset Dense Jet Flow","year":2022,"lang":"en","type":"book-chapter","venue":"Lecture notes in civil engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Ottawa","funders":"","keywords":"Turbulence; Mechanics; Reynolds number; Large eddy simulation; Jet (fluid); Turbulence kinetic energy; K-epsilon turbulence model; Reynolds stress; Direct numerical simulation; Computer simulation; Physics","score_opus":0.007523607089037368,"score_gpt":0.19969736343526118,"score_spread":0.1921737563462238,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4285225475","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.00060151087,0.0023146917,0.98282856,0.000036618858,0.001505989,0.00036935904,0.00015217515,0.00039437073,0.011796714],"genre_scores_gemma":[0.9945858,0.0002529533,0.0041649803,0.000025429199,0.0002963477,0.000018648318,0.00019296302,0.00025050645,0.00021233755],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99843323,0.000007074871,0.0005353985,0.00031881325,0.0003768711,0.0003285853],"domain_scores_gemma":[0.9989666,0.0004322452,0.00007907851,0.00041238253,0.000040329505,0.00006941405],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00012949725,0.0005005274,0.000586271,0.00032486,0.000029102073,0.000016817743,0.00024731836,0.00040128367,0.00078774075],"category_scores_gemma":[0.00012113998,0.0005595721,0.00018173775,0.00011908797,0.000019204654,0.0000466422,0.000073557305,0.0011583907,0.000007441218],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000061324845,0.000008559274,0.00000786143,0.00031481532,0.00006754861,0.000051504947,0.000102668506,0.995594,0.00020173364,0.00067257066,0.000041570416,0.002931025],"study_design_scores_gemma":[0.00016764842,0.00003187373,0.000013465746,0.00020806228,0.00004143287,0.0000121642515,3.7626506e-7,0.9822248,0.000081408354,0.0013587486,0.0153637575,0.0004962603],"about_ca_topic_score_codex":0.0000063646035,"about_ca_topic_score_gemma":0.0000452727,"teacher_disagreement_score":0.99398434,"about_ca_system_score_codex":0.0003473782,"about_ca_system_score_gemma":0.000023726785,"threshold_uncertainty_score":0.9996856},"labels":[],"label_agreement":null},{"id":"W4285306397","doi":"10.1007/978-981-19-1065-4_10","title":"Experimental Study of Sand-Water Coaxial Jets with Low Velocity Ratio","year":2022,"lang":"en","type":"book-chapter","venue":"Lecture notes in civil engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lakehead University","funders":"","keywords":"Coaxial; Nozzle; Jet (fluid); Turbulence; Reynolds number; Mechanics; Particle (ecology); Volumetric flow rate; Core (optical fiber); Sauter mean diameter; Materials science; Optics; Physics; Geology; Thermodynamics","score_opus":0.006265813916645538,"score_gpt":0.19241870669727984,"score_spread":0.1861528927806343,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4285306397","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.45130244,0.003807162,0.45987275,0.000032723237,0.0060577514,0.004062692,0.00029474337,0.0014960298,0.0730737],"genre_scores_gemma":[0.9985469,0.000025952471,0.0006294887,0.000009207422,0.0002176086,0.000061215476,0.00007225828,0.0002321659,0.00020519947],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99837655,0.000008269251,0.00044766476,0.0003746439,0.00042466004,0.0003682308],"domain_scores_gemma":[0.99934316,0.00010518116,0.000054048134,0.00040547515,0.000030258381,0.000061887935],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00011464541,0.0005649274,0.0006213999,0.00026142405,0.000051313054,0.000028090337,0.00027650828,0.00025182072,0.0007697754],"category_scores_gemma":[0.000015238311,0.0005043334,0.00008494924,0.000069774884,0.00002971806,0.00006184017,0.00014001537,0.0010411144,0.0000037955697],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000022205153,0.000082210616,0.000015932359,0.00018138303,0.00014710397,0.000096846205,0.0013477824,0.98799103,0.009645882,0.00019260785,0.000009779831,0.00026721705],"study_design_scores_gemma":[0.0025335662,0.0011480657,0.00005468854,0.000544937,0.00016290795,0.00004093561,0.000047110054,0.9533811,0.037566535,0.0003329215,0.0020543116,0.0021329296],"about_ca_topic_score_codex":0.000021814632,"about_ca_topic_score_gemma":0.00021314806,"teacher_disagreement_score":0.5472444,"about_ca_system_score_codex":0.00031050324,"about_ca_system_score_gemma":0.000021268675,"threshold_uncertainty_score":0.99974084},"labels":[],"label_agreement":null},{"id":"W4287877634","doi":"10.3390/w14152312","title":"Vertical Dense Effluent Discharge Modelling in Shallow Waters","year":2022,"lang":"en","type":"article","venue":"Water","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Ottawa","funders":"","keywords":"Froude number; Outfall; Dilution; Turbulence; Effluent; Jet (fluid); Mechanics; Environmental science; Range (aeronautics); Flow (mathematics); Current (fluid); Plume; Splash; Geology; Meteorology; Materials science; Physics; Environmental engineering; Oceanography; Thermodynamics","score_opus":0.008112924512962414,"score_gpt":0.18073604038472801,"score_spread":0.1726231158717656,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4287877634","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9850124,0.000025696872,0.013750192,0.000097623575,0.00044465825,0.00007286888,0.000007663555,0.00007599565,0.00051290815],"genre_scores_gemma":[0.99926007,0.000007969273,0.0003909396,0.00005861528,0.000035491696,0.000036783265,0.000025334071,0.000032524615,0.00015225857],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992563,0.0000137773795,0.00015368377,0.00012949118,0.00013645702,0.0003102757],"domain_scores_gemma":[0.99981004,0.0000083422865,0.0000021807716,0.0001317933,0.0000047909334,0.000042875676],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012340344,0.00009503038,0.00009715651,0.00005080291,0.000060124676,0.000021129888,0.00011704834,0.000025714011,0.0002644128],"category_scores_gemma":[0.0000012211974,0.000074649855,0.000035145622,0.000039117782,0.000010447062,0.000039564573,0.00010526439,0.00022576141,0.00006052835],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000059360978,0.000019322615,0.00063587615,0.000013558128,0.000007837562,0.00003313423,0.0005151915,0.9897193,0.008669142,0.00021851818,0.00010163942,0.000060560586],"study_design_scores_gemma":[0.00018100007,0.000011207207,0.0001118112,0.0000041428725,0.0000051540155,0.000004010556,0.00003950756,0.995993,0.0013251317,0.0005155141,0.0016747211,0.00013477921],"about_ca_topic_score_codex":0.000012621522,"about_ca_topic_score_gemma":0.000005145268,"teacher_disagreement_score":0.01424769,"about_ca_system_score_codex":0.00010414409,"about_ca_system_score_gemma":0.0000023288592,"threshold_uncertainty_score":0.3044133},"labels":[],"label_agreement":null},{"id":"W4289543171","doi":"","title":"Monte-carlo computation of wall-pressure spectra under turbulent boundary layers for trailing-edge noise prediction","year":2018,"lang":"en","type":"preprint","venue":"HAL (Le Centre pour la Communication Scientifique Directe)","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Trailing edge; Turbulence; Monte Carlo method; Noise (video); Computation; Boundary layer; Mechanics; Statistical physics; Physics; Acoustics; Computational physics; Materials science; Computer science; Mathematics; Algorithm; Artificial intelligence","score_opus":0.011962779993875386,"score_gpt":0.21970580752936347,"score_spread":0.2077430275354881,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4289543171","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.24893254,0.0015502042,0.74166834,0.0009974496,0.0008899951,0.0008438779,0.0004759986,0.00040706294,0.004234545],"genre_scores_gemma":[0.954478,0.0004759257,0.043457147,0.00002557648,0.00008695721,0.00007896167,0.0005435095,0.00009610397,0.00075777667],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99762136,0.00049351656,0.000656202,0.00054446625,0.00035879153,0.0003256831],"domain_scores_gemma":[0.99649316,0.0004654504,0.00031305308,0.0010439216,0.001559306,0.00012510741],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0019242334,0.00036046706,0.00041706147,0.00017225667,0.00020748317,0.00019573746,0.000680692,0.00039248474,0.00003331533],"category_scores_gemma":[0.00023771962,0.00041558084,0.00025683024,0.0001742598,0.00021549164,0.000099974466,0.00027560606,0.0005254393,0.0000052674814],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00003742899,0.00043726966,0.00027378017,0.0017761692,0.0005561359,0.0000018506412,0.0074333823,0.962191,0.0069845393,0.007126588,0.0051246993,0.008057179],"study_design_scores_gemma":[0.0004733475,0.0000013215755,0.0012237845,0.0010607463,0.00015692007,0.0000033151155,0.000061436156,0.9845288,0.0050076707,0.0042174575,0.0029342119,0.00033102228],"about_ca_topic_score_codex":0.00014207966,"about_ca_topic_score_gemma":0.0003416544,"teacher_disagreement_score":0.7055455,"about_ca_system_score_codex":0.00013476578,"about_ca_system_score_gemma":0.00014657094,"threshold_uncertainty_score":0.9998296},"labels":[],"label_agreement":null},{"id":"W4291476105","doi":"10.1088/1361-6501/ac86e4","title":"A new experimental setup for time-resolved measurements of interactions between gas jets and flexible surfaces","year":2022,"lang":"en","type":"article","venue":"Measurement Science and Technology","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"Deutsche Forschungsgemeinschaft","keywords":"Nozzle; Bar (unit); Supersonic speed; Jet (fluid); Materials science; Surface (topology); Optics; Plane (geometry); Mechanics; Inlet; Range (aeronautics); Acoustics; Physics; Geometry; Mechanical engineering; Composite material","score_opus":0.039628740252560565,"score_gpt":0.26577330767989327,"score_spread":0.2261445674273327,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4291476105","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9848108,0.0012331619,0.01112547,0.0004869415,0.00038123378,0.00054113654,0.000035057146,0.00023651858,0.0011496454],"genre_scores_gemma":[0.995733,0.000008096163,0.00412978,0.000007461507,0.000014394226,0.00005163482,0.0000019394581,0.000011302178,0.000042345786],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9987358,0.000007399076,0.0001816721,0.0002265529,0.00060783024,0.0002407656],"domain_scores_gemma":[0.99954814,0.000016187412,0.00004308508,0.00015801059,0.00017523595,0.000059340524],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00092828856,0.000106419306,0.00016158061,0.00028399567,0.0003280082,0.000024603461,0.00024114651,0.000030642208,0.000031687956],"category_scores_gemma":[0.00008544762,0.000110743415,0.000016138381,0.0004634263,0.00019841397,0.0001021359,0.00017322857,0.00011620373,9.2764816e-7],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000062972667,0.000029597726,0.0023347693,0.00001837109,0.00003282827,3.0353897e-7,0.00010830364,0.0010561041,0.9849602,0.00029347488,0.0010299431,0.010129788],"study_design_scores_gemma":[0.0015608474,0.00073384354,0.0011277869,0.000057849957,0.000086137705,0.000016256043,0.0013006354,0.08680809,0.8947974,0.0032914248,0.009707657,0.00051206956],"about_ca_topic_score_codex":0.000013852322,"about_ca_topic_score_gemma":0.000010336337,"teacher_disagreement_score":0.09016281,"about_ca_system_score_codex":0.00021180375,"about_ca_system_score_gemma":0.00009156234,"threshold_uncertainty_score":0.45159853},"labels":[],"label_agreement":null},{"id":"W4294025852","doi":"10.1007/s12206-022-0812-4","title":"Numerical simulation and analysis of the aerodynamic noise of a nautilus-inspired bionic multiblade centrifugal fan","year":2022,"lang":"en","type":"article","venue":"Journal of Mechanical Science and Technology","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":12,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Saskatchewan","funders":"","keywords":"Volute; Aerodynamics; Centrifugal fan; Impeller; Detached eddy simulation; Noise (video); Reynolds-averaged Navier–Stokes equations; Engineering; Acoustics; Sound pressure; Computational fluid dynamics; Mechanics; Mechanical engineering; Computer science; Aerospace engineering; Physics; Inlet","score_opus":0.005578518321014427,"score_gpt":0.2273084578005599,"score_spread":0.22172993947954547,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4294025852","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98345214,0.00017461994,0.01584604,0.0002862851,0.00015400529,0.000055780245,0.0000098496275,0.000012157311,0.000009111726],"genre_scores_gemma":[0.99903053,0.00006092849,0.00088440446,0.000011445994,0.0000062075496,8.796028e-7,2.6967874e-7,0.0000041160024,0.0000012229085],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.998976,0.00001963445,0.0003612418,0.000108036,0.00038691456,0.00014819665],"domain_scores_gemma":[0.9994148,0.000067820234,0.0001983014,0.00014442798,0.00012962721,0.000045045505],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005862985,0.00006766715,0.00026086989,0.0004952798,0.00012810796,0.0000076009137,0.00035691916,0.000061548926,0.00001148634],"category_scores_gemma":[0.00025131722,0.000048360158,0.00006277389,0.0025754822,0.00026743367,0.00005772964,0.00019338181,0.00028897738,4.197846e-8],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000017559692,0.000074235395,0.0025714845,0.000015167183,0.00012799089,0.0000047655267,0.00006779463,0.61178625,0.36839417,0.0043613072,0.000002871896,0.012576442],"study_design_scores_gemma":[0.00020891627,0.0001505555,0.005083223,0.000008233065,0.00014361284,0.00001869505,0.00010945465,0.9904845,0.002669609,0.0010429788,0.00002969049,0.000050535815],"about_ca_topic_score_codex":0.0000046887885,"about_ca_topic_score_gemma":0.0000065384634,"teacher_disagreement_score":0.3786983,"about_ca_system_score_codex":0.00007300073,"about_ca_system_score_gemma":0.00005173526,"threshold_uncertainty_score":0.197207},"labels":[],"label_agreement":null},{"id":"W4298205206","doi":"","title":"Extensions and limitations of analytical airfoil broadband noise models","year":2009,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Airfoil; Broadband; Noise (video); Acoustics; Computer science; Telecommunications; Physics; Aerospace engineering; Engineering; Artificial intelligence","score_opus":0.03020372843374829,"score_gpt":0.22755693415360279,"score_spread":0.19735320571985449,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4298205206","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.52420896,0.00027288205,0.33598283,0.00027247914,0.000089334535,0.00008122607,0.00001267146,0.00014349067,0.13893613],"genre_scores_gemma":[0.9899618,0.0004247448,0.009235263,0.000053062737,0.000016292432,7.673089e-7,0.0000029851312,0.0000070653728,0.0002980236],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996316,0.0000027075148,0.00012858196,0.00007400042,0.00006515267,0.000097980075],"domain_scores_gemma":[0.99970186,0.00007949891,0.0000075124126,0.0001144985,0.000038970382,0.000057682293],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000035317837,0.000064587395,0.0001004351,0.000042432755,0.00002495657,0.000009523242,0.00003934266,0.000039291328,0.000008911762],"category_scores_gemma":[0.000034430144,0.000058179437,0.000024579109,0.000077978075,0.000025951776,0.00005569421,0.000009119129,0.00006399602,0.00000213731],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000002212087,0.00003704572,0.000024631374,0.000010462403,0.0000172625,0.0000028750635,0.0000971816,0.8754422,0.0038479334,0.102238744,0.0017430459,0.016536372],"study_design_scores_gemma":[0.00009667488,0.000021382824,0.0018929692,0.000007611248,0.000019548348,0.000002529237,0.000028934826,0.98661363,0.00004853821,0.0110750375,0.00012269427,0.00007045312],"about_ca_topic_score_codex":0.0000019603074,"about_ca_topic_score_gemma":0.000009276346,"teacher_disagreement_score":0.46575284,"about_ca_system_score_codex":0.0000069150087,"about_ca_system_score_gemma":0.000005072016,"threshold_uncertainty_score":0.23724887},"labels":[],"label_agreement":null},{"id":"W4298425936","doi":"10.1615/tsfp7.1520","title":"INCOMPLETE SIMILARITY OF A PLANE TURBULENT WALL JET","year":2011,"lang":"en","type":"article","venue":"Proceeding of Seventh International Symposium on Turbulence and Shear Flow Phenomena","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Saskatchewan","funders":"","keywords":"Jet (fluid); Turbulence; Physics; Plane (geometry); Mechanics; Reynolds number; Similarity (geometry); Geometry; Mathematics; Image (mathematics); Computer science","score_opus":0.01869223539123787,"score_gpt":0.21416893291307926,"score_spread":0.19547669752184138,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4298425936","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97393584,0.00016850067,0.0019473777,0.00026184955,0.00065347593,0.00025567264,0.00012903128,0.000092956456,0.022555271],"genre_scores_gemma":[0.995912,0.0003294598,0.0034915605,0.000053428706,0.00011227719,0.000011852994,0.000020074058,0.000023666214,0.000045692454],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9988886,0.000004606007,0.00038467356,0.00021412676,0.00031343751,0.00019454378],"domain_scores_gemma":[0.99956024,0.000028807543,0.00009857388,0.00011036748,0.00012311507,0.00007890651],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017458311,0.00018727414,0.00024117705,0.00010160665,0.000037694022,0.000015571932,0.000289248,0.000059705566,0.000098289805],"category_scores_gemma":[0.000012007955,0.00017531839,0.00005572467,0.00008127664,0.00007649927,0.00012530446,0.00006599687,0.00017251073,0.0000046015552],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0023222405,0.005117051,0.12586872,0.008381486,0.004388829,0.0001107284,0.06786629,0.38474876,0.20277879,0.15398128,0.0050053415,0.039430484],"study_design_scores_gemma":[0.00082468044,0.00044125973,0.006141939,0.0005625565,0.000057797934,0.000021224849,0.00024472282,0.9709486,0.013007571,0.0061841263,0.0010454083,0.0005201246],"about_ca_topic_score_codex":0.000025938054,"about_ca_topic_score_gemma":0.0000012743486,"teacher_disagreement_score":0.5861998,"about_ca_system_score_codex":0.00005057534,"about_ca_system_score_gemma":0.000010565528,"threshold_uncertainty_score":0.7149276},"labels":[],"label_agreement":null},{"id":"W4299846381","doi":"","title":"Aeroacoustic Study of an Axial Ring Fan using Lattice-Boltzmann Simulations and the Ffowcs-Williams and Hawkings Analogy","year":2016,"lang":"en","type":"preprint","venue":"HAL (Le Centre pour la Communication Scientifique Directe)","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Lattice Boltzmann methods; Analogy; Physics; Mechanics; Computer science; Aerospace engineering; Statistical physics; Engineering","score_opus":0.013284454518550017,"score_gpt":0.23365796331378935,"score_spread":0.22037350879523934,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4299846381","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8200881,0.00035686363,0.17727052,0.0001730403,0.00019211535,0.00045639405,0.00006934638,0.00009582213,0.0012978242],"genre_scores_gemma":[0.99118495,0.00017017551,0.008339949,0.00000898209,0.000037260284,0.000016669814,0.00004677822,0.000055185003,0.00014005846],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99733794,0.0012084441,0.00049978436,0.0004513516,0.00025049862,0.0002519683],"domain_scores_gemma":[0.9965854,0.0013307062,0.00025068727,0.0011489838,0.00057590526,0.0001083056],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.002123887,0.00028603495,0.00041808083,0.00015172736,0.0003317555,0.00021777095,0.00052019855,0.00018699258,0.000009159454],"category_scores_gemma":[0.00045778125,0.00023738165,0.00006192876,0.00015696467,0.0003589189,0.000111978894,0.00080959074,0.0004502698,5.193653e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0001202885,0.0019105369,0.020439826,0.0017250271,0.0015002742,0.000024951543,0.08703219,0.6769124,0.03545861,0.10334923,0.00005075655,0.0714759],"study_design_scores_gemma":[0.001066357,9.0497343e-7,0.003690345,0.000503709,0.00017436597,0.000005987247,0.00030603277,0.98961794,0.000344885,0.0039818706,0.000037200225,0.0002704],"about_ca_topic_score_codex":0.0006052811,"about_ca_topic_score_gemma":0.0024778473,"teacher_disagreement_score":0.31270555,"about_ca_system_score_codex":0.000060016337,"about_ca_system_score_gemma":0.00004457144,"threshold_uncertainty_score":0.96801424},"labels":[],"label_agreement":null},{"id":"W4300247867","doi":"","title":"Optimization of tonal noise control with flow obstruction","year":2017,"lang":"en","type":"article","venue":"HAL (Le Centre pour la Communication Scientifique Directe)","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Noise (video); Computer science; Flow (mathematics); Acoustics; Flow control (data); Control (management); Control theory (sociology); Speech recognition; Physics; Telecommunications; Artificial intelligence; Mechanics","score_opus":0.0050245360932915754,"score_gpt":0.18333502129460935,"score_spread":0.1783104852013178,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4300247867","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.098504305,0.00006841573,0.8776227,0.00046089594,0.00014663003,0.00012322096,0.0000351334,0.00009741009,0.022941278],"genre_scores_gemma":[0.88701373,0.00008401001,0.11234224,0.0000067301553,0.000014268841,0.0000093073195,0.000045729423,0.000022970122,0.0004609948],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99915093,0.00017929793,0.00019525274,0.00016060623,0.00017331867,0.00014062117],"domain_scores_gemma":[0.99810886,0.00016977856,0.00014787946,0.0008527456,0.00066090736,0.0000598481],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0007119128,0.00011440466,0.0001448914,0.00004653737,0.00025366558,0.00012574959,0.000392302,0.000066998015,0.00006129771],"category_scores_gemma":[0.00027447913,0.00011236899,0.000043359556,0.000066823195,0.00013694464,0.00016531322,0.000055326414,0.00012130923,0.000003857936],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000016097218,0.00009620363,0.0030583288,0.00007116887,0.000067102636,0.0000020114614,0.00076338794,0.94529134,0.0074136653,0.017947176,0.00013566091,0.025137883],"study_design_scores_gemma":[0.00054002134,3.0600094e-7,0.0045252643,0.00017268199,0.000021286252,0.0000040339664,0.000016904123,0.987414,0.006691928,0.00021640514,0.00027224238,0.00012491512],"about_ca_topic_score_codex":0.00006471466,"about_ca_topic_score_gemma":0.00021869363,"teacher_disagreement_score":0.7885094,"about_ca_system_score_codex":0.000035323174,"about_ca_system_score_gemma":0.000027128033,"threshold_uncertainty_score":0.45822746},"labels":[],"label_agreement":null},{"id":"W4300531948","doi":"","title":"Trailing Edge Noise Computation of a Fan Blade Profile","year":2008,"lang":"en","type":"article","venue":"HAL (Le Centre pour la Communication Scientifique Directe)","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Blade (archaeology); Trailing edge; Computation; Noise (video); Computer science; Acoustics; Enhanced Data Rates for GSM Evolution; Structural engineering; Engineering; Physics; Telecommunications; Artificial intelligence; Algorithm","score_opus":0.009831144449010063,"score_gpt":0.19871682740069022,"score_spread":0.18888568295168015,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4300531948","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.54391474,0.00023981289,0.42905006,0.00015214128,0.000097451324,0.00012888391,0.000021695463,0.00017069085,0.02622453],"genre_scores_gemma":[0.9626695,0.00017088241,0.03615254,0.0000096560925,0.000012304016,0.000011379871,0.00006411425,0.000029565215,0.00088008575],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99885243,0.0003000475,0.00029937975,0.00018384396,0.00018219142,0.0001821127],"domain_scores_gemma":[0.9986549,0.0002809941,0.00008837848,0.0004133198,0.0004888098,0.00007358449],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00074522465,0.00012758974,0.00016585598,0.00008292018,0.00014577279,0.000028041984,0.00027795465,0.000074777854,0.000032830816],"category_scores_gemma":[0.00013332831,0.00014281498,0.000070991264,0.000260694,0.00011750848,0.00008646096,0.00006758537,0.00016534599,0.000017055154],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000026740325,0.0013948928,0.009662855,0.00097611285,0.00027319728,0.000033183274,0.05117962,0.14098464,0.4774484,0.08884038,0.0036627785,0.2255172],"study_design_scores_gemma":[0.00032733602,3.3144008e-7,0.0044658766,0.00025642122,0.000013695207,0.0000118086045,0.00008341703,0.92003185,0.07352726,0.00031305163,0.0007675287,0.00020144993],"about_ca_topic_score_codex":0.00004489208,"about_ca_topic_score_gemma":0.00007824109,"teacher_disagreement_score":0.7790472,"about_ca_system_score_codex":0.000031431005,"about_ca_system_score_gemma":0.00004077144,"threshold_uncertainty_score":0.5823826},"labels":[],"label_agreement":null},{"id":"W4300585751","doi":"10.1615/tsfp10.540","title":"Merging of coherent structures in a separation bubble","year":2017,"lang":"en","type":"article","venue":"Proceeding of Tenth International Symposium on Turbulence and Shear Flow Phenomena","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Waterloo","funders":"","keywords":"Airfoil; Vortex; Laminar flow; Physics; Reynolds number; Particle image velocimetry; Bubble; Mechanics; Wind tunnel; Flow separation; Vortex shedding; Flow visualization; Angle of attack; Particle tracking velocimetry; Acoustics; Aerodynamics; Classical mechanics; Flow (mathematics); Boundary layer; Turbulence","score_opus":0.012096924130187283,"score_gpt":0.2614286732470526,"score_spread":0.24933174911686531,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4300585751","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9854021,0.00009989139,0.00084299914,0.00019699894,0.0005916549,0.00013296177,0.000026681908,0.000021126727,0.012685581],"genre_scores_gemma":[0.9981605,0.00022459285,0.0014287467,0.000007776658,0.000106840394,0.000009903333,0.0000064106384,0.000012116462,0.00004310938],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99929446,0.0000021492326,0.00025120444,0.00014462888,0.00018781042,0.00011972948],"domain_scores_gemma":[0.99966407,0.000015266774,0.00010732329,0.00010598817,0.000074911746,0.00003245531],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00011402272,0.00010883969,0.00015569333,0.00008172029,0.00005975289,0.000051751267,0.00024818635,0.000035820078,0.000019382334],"category_scores_gemma":[0.000024628287,0.00010257354,0.000027982207,0.000030334586,0.00005594816,0.00017205061,0.000055813478,0.00010492743,9.254371e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00014088022,0.00019495715,0.0538653,0.0007461285,0.0002222041,0.000004443534,0.0031066155,0.7588253,0.12465117,0.040927384,0.00025220384,0.017063381],"study_design_scores_gemma":[0.00036902685,0.00006152681,0.00919106,0.00024036833,0.000009859429,0.0000014943142,0.00009982008,0.9799565,0.006489732,0.00333684,0.00010341553,0.00014036709],"about_ca_topic_score_codex":0.000027365932,"about_ca_topic_score_gemma":0.0000030405804,"teacher_disagreement_score":0.22113116,"about_ca_system_score_codex":0.000044226315,"about_ca_system_score_gemma":0.000007304059,"threshold_uncertainty_score":0.41828278},"labels":[],"label_agreement":null},{"id":"W4300827152","doi":"","title":"Direct Noise Prediction and Control of an Installed Large Low-speed Radial Fan","year":2016,"lang":"en","type":"article","venue":"HAL (Le Centre pour la Communication Scientifique Directe)","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Noise (video); Speed skating; Computer science; Acoustics; Physics; Simulation; Artificial intelligence","score_opus":0.0038905433478399762,"score_gpt":0.17908362644614637,"score_spread":0.1751930830983064,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4300827152","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7427851,0.00018261257,0.24444503,0.00031377646,0.00014932481,0.00018503044,0.00023818483,0.00020197881,0.011498942],"genre_scores_gemma":[0.9969782,0.000308328,0.0020911586,0.000013618161,0.00002278043,0.000008877838,0.000048305676,0.000030951673,0.000497743],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9985819,0.0005148427,0.00028356182,0.00022910215,0.00017451766,0.00021608763],"domain_scores_gemma":[0.9983833,0.00043893539,0.00008391771,0.00059508183,0.00037324394,0.00012551353],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0014942469,0.00014297018,0.00020168263,0.00008366724,0.00010953831,0.000049459188,0.00024811833,0.000096145544,0.00005117702],"category_scores_gemma":[0.0003736155,0.00012348882,0.000052404124,0.00013305151,0.00010718743,0.00017583647,0.000068461086,0.000097007294,0.0000050017566],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00005124427,0.0005428103,0.0053104386,0.00014516615,0.00013991259,0.0000050700896,0.0033269124,0.0010290436,0.89289165,0.028683675,0.00023972642,0.06763435],"study_design_scores_gemma":[0.0038867106,0.0000023504901,0.0171591,0.0006428514,0.000056404955,0.000007294676,0.000070452974,0.8614139,0.11244883,0.0006242418,0.003296983,0.00039087527],"about_ca_topic_score_codex":0.000038740473,"about_ca_topic_score_gemma":0.00030529962,"teacher_disagreement_score":0.8603849,"about_ca_system_score_codex":0.00004362689,"about_ca_system_score_gemma":0.000025392152,"threshold_uncertainty_score":0.50357276},"labels":[],"label_agreement":null},{"id":"W4300997066","doi":"10.1615/tsfp6.1530","title":"ANALYSIS OF SECOND MOMENT CLOSURE MODELING FOR A RECTANGULAR SURFACE JET USING DNS DATA","year":2009,"lang":"en","type":"article","venue":"Proceeding of Sixth International Symposium on Turbulence and Shear Flow Phenomena","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Western University; University of Calgary; Queen's University","funders":"","keywords":"Reynolds-averaged Navier–Stokes equations; Mechanics; Jet (fluid); Turbulence; Vorticity; Anisotropy; Reynolds number; Dissipation; Surface (topology); Physics; Moment (physics); Statistical physics; Geometry; Mathematics; Classical mechanics; Vortex; Optics; Thermodynamics","score_opus":0.028505984397558855,"score_gpt":0.2682607536753497,"score_spread":0.23975476927779082,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4300997066","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9450923,0.00022990834,0.0527623,0.00012847889,0.00022245565,0.00018830234,0.0005380824,0.00003218342,0.000805975],"genre_scores_gemma":[0.9866395,0.00018004782,0.012857827,0.000031581807,0.00012489044,0.0000031304917,0.00011995601,0.000018473434,0.000024621573],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99880666,0.0000034880995,0.0004062807,0.00030738593,0.00028555273,0.00019065752],"domain_scores_gemma":[0.99942666,0.000036184574,0.00009123917,0.0002027118,0.00018545809,0.000057747802],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00030460863,0.00017431483,0.0003304737,0.00016793342,0.000051713574,0.000039264884,0.00037582664,0.000057974074,0.000021093494],"category_scores_gemma":[0.00001785411,0.0001708655,0.000075849275,0.00024194353,0.000025369023,0.00019746456,0.00006218762,0.00011143805,2.4188972e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000037167378,0.000052246258,0.000778045,0.000102730664,0.00046396875,3.4805626e-7,0.0004134482,0.9660034,0.030744607,0.0008234509,0.00002428219,0.00055630686],"study_design_scores_gemma":[0.00023375194,0.00008829753,0.00013177918,0.00010630751,0.00022048468,8.985279e-7,0.00009565462,0.9973075,0.0009985064,0.000592692,0.00005925427,0.00016490066],"about_ca_topic_score_codex":0.000007412982,"about_ca_topic_score_gemma":0.000001683637,"teacher_disagreement_score":0.041547157,"about_ca_system_score_codex":0.000069475915,"about_ca_system_score_gemma":0.000014789154,"threshold_uncertainty_score":0.6967693},"labels":[],"label_agreement":null},{"id":"W4301703123","doi":"","title":"Tonal Noise Prediction of a Modern Turbofan Engine with Large Upstream and Downstream Distortion","year":2017,"lang":"en","type":"article","venue":"HAL (Le Centre pour la Communication Scientifique Directe)","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Turbofan; Upstream (networking); Downstream (manufacturing); Distortion (music); Noise (video); Computer science; Upstream and downstream (DNA); Acoustics; Environmental science; Engineering; Aerospace engineering; Telecommunications; Physics; Artificial intelligence","score_opus":0.004832540933835302,"score_gpt":0.17993765754528135,"score_spread":0.17510511661144604,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4301703123","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.667514,0.00018077399,0.3197421,0.00025170553,0.00007195671,0.00011164596,0.00014039027,0.00010407695,0.011883324],"genre_scores_gemma":[0.9904498,0.00022370937,0.008597421,0.0000033478884,0.000014624018,0.000011978622,0.00011040459,0.000023463419,0.0005652473],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99918383,0.000112352,0.00018566895,0.00019154524,0.00016499608,0.00016158124],"domain_scores_gemma":[0.9986002,0.000103399354,0.0001184819,0.000781416,0.0003177446,0.000078768215],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006775783,0.00012898979,0.0001422721,0.000050340495,0.00024415046,0.00009768288,0.0002638386,0.00006873196,0.000019829822],"category_scores_gemma":[0.00015012735,0.00012188945,0.000035254587,0.000053664833,0.00012180658,0.0001571319,0.00009858852,0.00013671332,0.0000015478266],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00010624121,0.0017688276,0.18896021,0.00089396257,0.0004971543,0.000019465473,0.01607182,0.0285154,0.089788094,0.07425149,0.00096792553,0.5981594],"study_design_scores_gemma":[0.0007779848,0.000001292675,0.06338387,0.0004425275,0.00004465287,0.000010102091,0.00003859873,0.917269,0.015865108,0.0012050194,0.00076270715,0.00019913304],"about_ca_topic_score_codex":0.000073109375,"about_ca_topic_score_gemma":0.000522956,"teacher_disagreement_score":0.8887536,"about_ca_system_score_codex":0.00003654418,"about_ca_system_score_gemma":0.00001993596,"threshold_uncertainty_score":0.49705073},"labels":[],"label_agreement":null},{"id":"W4301935083","doi":"10.1615/tsfp7.1070","title":"A POD INVESTIGATION OF THE THREE-DIMENSIONAL WALL JET NEAR FIELD","year":2011,"lang":"en","type":"article","venue":"Proceeding of Seventh International Symposium on Turbulence and Shear Flow Phenomena","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of New Brunswick","funders":"","keywords":"Vorticity; Vortex; Jet (fluid); Physics; Particle image velocimetry; Turbulence; Mechanics; Reynolds number; Vector field; Geometry; Classical mechanics; Optics; Mathematics","score_opus":0.01376013984971735,"score_gpt":0.2004144346116835,"score_spread":0.18665429476196616,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4301935083","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.992683,0.000059735572,0.0004627852,0.00039307948,0.0005735366,0.00014401451,0.000022330643,0.000029373474,0.0056321677],"genre_scores_gemma":[0.9971354,0.000033253556,0.0025768687,0.00011217836,0.00007903422,0.000009139294,0.000004738261,0.000014853617,0.00003452878],"study_design_codex":"observational","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991913,0.000003884361,0.00025991318,0.00014675627,0.0002761375,0.00012201152],"domain_scores_gemma":[0.9996421,0.000032780965,0.00008102351,0.000095054886,0.00010400326,0.00004506742],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012783949,0.000123376,0.00012752498,0.00004060146,0.000056249857,0.000015562398,0.00024096103,0.000049597842,0.000053843574],"category_scores_gemma":[0.00001818042,0.00009526716,0.000048988728,0.000085927524,0.00008301188,0.00010759832,0.00006781956,0.00014559073,0.0000025123416],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0012266801,0.0009731703,0.3747379,0.0022708955,0.0016361161,0.000009941247,0.03152549,0.32678145,0.1375574,0.09648162,0.0035544494,0.023244882],"study_design_scores_gemma":[0.00033729148,0.00025328138,0.015351464,0.0003930973,0.000029954821,0.000004769633,0.000053871223,0.95922714,0.01567483,0.008320935,0.000139651,0.00021370269],"about_ca_topic_score_codex":0.00003348783,"about_ca_topic_score_gemma":0.0000032322725,"teacher_disagreement_score":0.6324457,"about_ca_system_score_codex":0.000029283186,"about_ca_system_score_gemma":0.000016997612,"threshold_uncertainty_score":0.3884882},"labels":[],"label_agreement":null},{"id":"W4303438120","doi":"10.2514/1.j061917","title":"Hilbert–Huang Spectral Analysis of Cavity Flows Incorporating Fluidic Spoilers","year":2022,"lang":"en","type":"article","venue":"AIAA Journal","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":6,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Geomechanica (Canada)","funders":"","keywords":"Acoustics; Fluidics; Mach number; Aeroacoustics; Mechanics; Physics; Materials science; Optics; Sound pressure; Engineering; Aerospace engineering","score_opus":0.006599447491006612,"score_gpt":0.20110689764925083,"score_spread":0.19450745015824422,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4303438120","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9841803,0.0003107855,0.013071998,0.00005667695,0.000786285,0.00004487026,0.000052880856,0.0000454634,0.0014507541],"genre_scores_gemma":[0.99699455,0.000058688263,0.002636179,0.000030437148,0.00018139774,0.0000035797104,0.000017694609,0.00002880599,0.000048689468],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9987527,0.000050505223,0.00043621083,0.00012170468,0.00037854028,0.00026029715],"domain_scores_gemma":[0.9994594,0.000057678037,0.00013462365,0.0001950766,0.000048072154,0.000105190986],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005390083,0.00013898149,0.00031858427,0.00037068152,0.00027687053,0.00003779701,0.0002752738,0.000036375037,0.0006941867],"category_scores_gemma":[0.000029338667,0.00014668111,0.00025737297,0.0009069653,0.000026101368,0.00009220059,0.00008569819,0.00063819013,0.000002805439],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000006090667,0.000025221156,0.005288645,0.000009720158,0.000623535,0.000064474996,0.00020808137,0.97674775,0.01475113,0.00042619486,0.00056677766,0.0012823932],"study_design_scores_gemma":[0.00019210653,0.000043360214,0.004822392,0.0000071454624,0.0004766969,0.00005416056,0.00024000404,0.99267983,0.00021088634,0.0006587597,0.00043354038,0.00018114239],"about_ca_topic_score_codex":0.000029104785,"about_ca_topic_score_gemma":0.000045959816,"teacher_disagreement_score":0.01593207,"about_ca_system_score_codex":0.00023521174,"about_ca_system_score_gemma":0.000042012434,"threshold_uncertainty_score":0.76008576},"labels":[],"label_agreement":null},{"id":"W4308326463","doi":"","title":"Unsteady lift and flow velocity evaluation for subsonic fans using inverse aeroacoustic models","year":2005,"lang":"en","type":"article","venue":"HAL (Le Centre pour la Communication Scientifique Directe)","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Lift (data mining); Mechanics; Inverse; Flow (mathematics); Inverse method; Geology; Aerospace engineering; Acoustics; Physics; Engineering; Computer science; Mathematics; Geometry; Applied mathematics","score_opus":0.021698990254172944,"score_gpt":0.22830367586705708,"score_spread":0.20660468561288414,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4308326463","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.32631966,0.00035589596,0.6692216,0.00029789214,0.000101222424,0.00031127658,0.000041309795,0.00012696542,0.0032241833],"genre_scores_gemma":[0.8288131,0.00018974744,0.1705182,0.000032042837,0.00002965486,0.000032424134,0.000094032155,0.000037690876,0.0002531059],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99841833,0.0004987789,0.00027778573,0.00028775405,0.00024448225,0.00027286005],"domain_scores_gemma":[0.99794966,0.0005426535,0.00007574944,0.00053220865,0.00078881875,0.00011088412],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0032960528,0.00017729924,0.00017232416,0.00008804787,0.00025459714,0.00012900651,0.00024721608,0.00011592522,0.000030530442],"category_scores_gemma":[0.0004509554,0.00020297687,0.00006213079,0.00018609379,0.00008401515,0.00023568624,0.00008634389,0.00016828808,0.000005129842],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000052901682,0.000082307415,0.0000654249,0.000082426646,0.00003995614,3.452345e-7,0.0028787814,0.9256412,0.006311978,0.007455921,0.00028410423,0.057152297],"study_design_scores_gemma":[0.00049197656,2.512114e-7,0.00013985757,0.00014255219,0.000067998924,0.00000370061,0.000076724515,0.994651,0.0018275743,0.0018755359,0.0005133567,0.00020944403],"about_ca_topic_score_codex":0.00006089072,"about_ca_topic_score_gemma":0.0011863376,"teacher_disagreement_score":0.50249344,"about_ca_system_score_codex":0.0001915335,"about_ca_system_score_gemma":0.000075876065,"threshold_uncertainty_score":0.82771564},"labels":[],"label_agreement":null},{"id":"W4309729092","doi":"10.3390/ijtpp7040034","title":"Effect of Sweep on Axial Fan Noise Sources Using the Lattice Boltzmann Method","year":2022,"lang":"en","type":"article","venue":"International Journal of Turbomachinery Propulsion and Power","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":19,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure; Université de Sherbrooke","funders":"Université de Sherbrooke","keywords":"Vortex; Mechanical fan; Lattice Boltzmann methods; Physics; Aerodynamics; Noise (video); Mechanics; Acoustics; Lattice (music); Sound pressure; Computer science","score_opus":0.006448208163412914,"score_gpt":0.2775624246124587,"score_spread":0.2711142164490458,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4309729092","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9891697,0.00029670665,0.006959638,0.00028146838,0.0026162788,0.000080549384,0.000031024774,0.0000112720545,0.000553327],"genre_scores_gemma":[0.99808234,0.000028317314,0.0014400893,0.000117851545,0.00024271922,0.0000017220524,0.0000029913967,0.000020032481,0.0000639627],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9987965,0.0001696802,0.00033326301,0.000081782506,0.00052238884,0.00009635648],"domain_scores_gemma":[0.99928147,0.00030635664,0.00018879076,0.00009265903,0.000086689724,0.000044028908],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0008930516,0.00012436441,0.0001844525,0.00014666554,0.00010137566,0.00003682724,0.00033993623,0.000030804964,0.00011520672],"category_scores_gemma":[0.00009752945,0.00007713834,0.000119077165,0.00006737047,0.000029283678,0.00006851992,0.000118579126,0.00045578033,6.029302e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.001059993,0.00014254947,0.0022790967,0.00006524936,0.00050403964,0.00013810312,0.0011513714,0.8629464,0.07566837,0.0010662554,0.0009699793,0.054008607],"study_design_scores_gemma":[0.0020274534,0.0015398818,0.002677134,0.00014959618,0.00017397088,0.0008582781,0.00019525812,0.9715209,0.008408502,0.0010411731,0.011060832,0.00034701405],"about_ca_topic_score_codex":0.000013626662,"about_ca_topic_score_gemma":7.4493994e-7,"teacher_disagreement_score":0.108574525,"about_ca_system_score_codex":0.000056599103,"about_ca_system_score_gemma":0.000012020163,"threshold_uncertainty_score":0.31456104},"labels":[],"label_agreement":null},{"id":"W4312877442","doi":"10.4050/f-0077-2021-16686","title":"Aeroacoustic Measurements from the Aerodynamic and Acoustic Rotorprop Test (AART) in the National Full-Scale Aerodynamics Complex (NFAC) 40- by 80-Foot Wind Tunnel ","year":2021,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lockheed Martin (Canada)","funders":"","keywords":"Aerodynamics; Wind tunnel; Propeller; Wing; Propulsor; Mach number; Acoustics; Marine engineering; Aerospace engineering; Engineering; Physics","score_opus":0.02436864408953318,"score_gpt":0.22913600042384807,"score_spread":0.2047673563343149,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4312877442","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9715628,0.00063782936,0.01935935,0.00078115915,0.0006650916,0.00080308167,0.001130407,0.00020289204,0.0048573604],"genre_scores_gemma":[0.99626285,0.00013302096,0.0017181429,0.0007632946,0.00024898333,0.00006247278,0.00049090316,0.0000840783,0.00023623538],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99715656,0.00012848049,0.00059622363,0.0005587456,0.0009773175,0.0005826911],"domain_scores_gemma":[0.99798095,0.0010711143,0.00007961352,0.00051547604,0.00023688407,0.0001159629],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0007050772,0.00046273103,0.00037150685,0.000060859893,0.00031775725,0.0003009035,0.00063964137,0.00019706173,0.00024950158],"category_scores_gemma":[0.00037042337,0.00033332236,0.00009305727,0.00046024588,0.00018874007,0.00014845323,0.00017040024,0.0006695215,0.000039338625],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000022465756,0.00044633923,0.005931803,0.000097205826,0.00018667275,0.000032164153,0.0006208894,0.47041854,0.49511775,0.00015605909,0.026289798,0.0006803294],"study_design_scores_gemma":[0.0007890707,0.00003926401,0.13685966,0.000056114775,0.00008290186,0.00003893952,0.0006843204,0.8597106,0.00003955647,0.0006966449,0.0005198957,0.00048306127],"about_ca_topic_score_codex":0.0001190398,"about_ca_topic_score_gemma":0.009878415,"teacher_disagreement_score":0.49507818,"about_ca_system_score_codex":0.00028573195,"about_ca_system_score_gemma":0.00009468881,"threshold_uncertainty_score":0.9999119},"labels":[],"label_agreement":null},{"id":"W4320182854","doi":"10.3397/in_2022_0416","title":"Active Sound Power Attenuation with a Ring of Harmonic Acoustic Pneumatic Sources fOr Destructive Interference (RHAPSODI) and near field in-duct microphones","year":2023,"lang":"en","type":"article","venue":"NOISE-CON proceedings","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Acoustics; Sound power; Duct (anatomy); Microphone; Active noise control; Secondary source; Engineering; Loudspeaker; Computer science; Physics; Noise reduction","score_opus":0.010253410981318697,"score_gpt":0.2201769349537306,"score_spread":0.20992352397241193,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4320182854","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99507177,0.000044154836,0.004068192,0.000036238704,0.00012786762,0.0003645263,0.000015464311,0.00009722606,0.00017453209],"genre_scores_gemma":[0.9982572,0.000039747465,0.0015317551,0.000012769742,0.000023588167,0.000071449474,0.000003874884,0.00003978364,0.000019835617],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991915,0.0000025536153,0.00023037098,0.00022888515,0.00009712621,0.00024955644],"domain_scores_gemma":[0.9995194,0.00016315976,0.00008471253,0.00006472114,0.00012698489,0.0000410018],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001192674,0.00017676574,0.00023811488,0.00014241807,0.00006735012,0.00006842833,0.00011684296,0.00008568618,0.000006676941],"category_scores_gemma":[0.00012660126,0.00016567466,0.000028658535,0.0002822593,0.00007859789,0.00019003655,0.00004529384,0.00017564597,0.00000287797],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0005088263,0.00005435956,0.02176496,0.0027241958,0.0002453109,0.0000064283972,0.032723147,0.026525145,0.9094862,0.00090440596,0.00015645768,0.004900578],"study_design_scores_gemma":[0.002332983,0.00079940556,0.05140008,0.0012942265,0.00016833468,0.000039240713,0.012297668,0.8614074,0.060488112,0.008877597,0.000019210838,0.0008757575],"about_ca_topic_score_codex":0.000014224975,"about_ca_topic_score_gemma":0.00002234289,"teacher_disagreement_score":0.84899807,"about_ca_system_score_codex":0.000057869904,"about_ca_system_score_gemma":0.000019106423,"threshold_uncertainty_score":0.67560166},"labels":[],"label_agreement":null},{"id":"W4320807713","doi":"10.17223/19988621/78/4","title":"Investigation of acoustic characteristics of a single supersonic jet flowing into a flooded space","year":2022,"lang":"en","type":"article","venue":"Vestnik Tomskogo gosudarstvennogo universiteta Matematika i mekhanika","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Supersonic speed; Jet (fluid); Nozzle; Mach number; Mechanics; Amplitude; Physics; Sound pressure; Compressible flow; Overall pressure ratio; Acoustics; Compressibility; Materials science; Optics; Thermodynamics","score_opus":0.009325416430986265,"score_gpt":0.1740213197728479,"score_spread":0.16469590334186163,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4320807713","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98789424,0.0002987637,0.008873842,0.000060275208,0.0008289697,0.00045875538,0.00030575765,0.000256114,0.0010232856],"genre_scores_gemma":[0.9937783,0.00006630496,0.0056306394,0.000027652972,0.000058087597,0.000014390822,0.00016199601,0.000110523746,0.0001521009],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99745166,0.00015423208,0.00084085704,0.00039436345,0.0006829401,0.00047595138],"domain_scores_gemma":[0.99849683,0.00020043789,0.00027705723,0.0006720522,0.00018367852,0.00016994757],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0004972053,0.00042945673,0.0008298516,0.00055200956,0.0002649827,0.000039966828,0.0006870622,0.00013758264,0.00029038786],"category_scores_gemma":[0.000087134744,0.0005084982,0.00021479563,0.0010304627,0.0001828763,0.00037239466,0.0003790257,0.00041805024,0.000015343572],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000059958726,0.000121286954,0.0011484151,0.0022688736,0.00031713242,0.00007918787,0.006498279,0.06051002,0.92506766,0.003136679,0.00056127156,0.00023125633],"study_design_scores_gemma":[0.0037851594,0.0015752529,0.0034435797,0.0014359603,0.0015233452,0.00016645216,0.019086797,0.85380834,0.107240655,0.0033293338,0.0019195819,0.002685538],"about_ca_topic_score_codex":0.00006173016,"about_ca_topic_score_gemma":0.000028881452,"teacher_disagreement_score":0.817827,"about_ca_system_score_codex":0.000500012,"about_ca_system_score_gemma":0.00011757787,"threshold_uncertainty_score":0.99973667},"labels":[],"label_agreement":null},{"id":"W4322741930","doi":"10.3390/app13053145","title":"Analysis of Upstream Turbulence Impact on Wall Heat Transfer in an Acoustic Liner with Large-Eddy Simulations","year":2023,"lang":"en","type":"article","venue":"Applied Sciences","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Grand Équipement National De Calcul Intensif","keywords":"Turbulence; Mechanics; Large eddy simulation; Heat transfer; Boundary layer; Jet (fluid); Scale (ratio); Physics","score_opus":0.012554977378736072,"score_gpt":0.2685555020355974,"score_spread":0.25600052465686135,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4322741930","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9865405,0.000006438272,0.012596894,0.000012898606,0.000029295335,0.00010081982,0.00007236439,0.00008529906,0.0005555112],"genre_scores_gemma":[0.99965745,0.0000117243,0.0002440756,0.000016477283,0.000012916559,0.00000831657,0.00003070709,0.0000108873555,0.0000074648415],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99909085,0.0000073757597,0.00016839901,0.00021417886,0.00025059402,0.000268606],"domain_scores_gemma":[0.9996048,0.00013534885,0.0000067804053,0.00018058474,0.00001933235,0.000053160165],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023281993,0.00012204739,0.00020143234,0.00043422257,0.000072769886,0.000030579286,0.000212313,0.000042799704,0.000040795487],"category_scores_gemma":[0.000005796462,0.00008495932,0.00004214493,0.0027506934,0.000091121445,0.000071876886,0.000009680987,0.00009838368,0.0000051238603],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000057264524,0.00003290494,0.0059397365,0.0000064761393,0.00003951101,0.0000015732522,0.00036155916,0.9863704,0.0067919176,0.00032351268,0.0000042715496,0.0001224011],"study_design_scores_gemma":[0.000117629745,0.00007226055,0.023416948,0.000010166788,0.00007455426,1.03487096e-7,0.00017222471,0.9756718,0.00026383103,0.000085556785,0.0000018704709,0.00011300068],"about_ca_topic_score_codex":0.000027862534,"about_ca_topic_score_gemma":0.0008525481,"teacher_disagreement_score":0.017477212,"about_ca_system_score_codex":0.00002797007,"about_ca_system_score_gemma":0.000022819306,"threshold_uncertainty_score":0.34645405},"labels":[],"label_agreement":null},{"id":"W4323926537","doi":"10.1016/j.euromechflu.2023.03.003","title":"Effects of bulb seal on slat flow dynamics and slat tones","year":2023,"lang":"en","type":"article","venue":"European Journal of Mechanics - B/Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":9,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Fiducie de Recherche sur la Foret des Cantons-de-l'Est","keywords":"Seal (emblem); Flow (mathematics); Bulb; Dynamics (music); Geology; Acoustics; Mechanics; Art; Physics; Biology; Visual arts","score_opus":0.00604703932793451,"score_gpt":0.19514789328240578,"score_spread":0.18910085395447127,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4323926537","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7624504,0.0008501373,0.22989674,0.00015900182,0.0038888215,0.00018199346,0.000052662734,0.00016901056,0.0023512372],"genre_scores_gemma":[0.9940569,0.0015981166,0.0037021914,0.000036418267,0.00031600287,4.9564164e-7,0.0000070307,0.000118151926,0.00016472835],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9985218,0.000118263895,0.0005616741,0.0001470106,0.0003625331,0.00028871803],"domain_scores_gemma":[0.999191,0.00020087407,0.00013109496,0.00020919096,0.00011056493,0.00015730166],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0010164767,0.0002343052,0.0003835946,0.00024810364,0.000058939117,0.000043348962,0.00031088566,0.0000594483,0.000012841099],"category_scores_gemma":[0.00014284832,0.00021520865,0.00014046124,0.00026543453,0.0000224378,0.00008845037,0.000113511654,0.00043702105,0.000037025085],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00025907243,0.00021704182,0.00011207885,0.0018672328,0.0010085886,0.0042419164,0.0015698338,0.4689898,0.3350461,0.044278078,0.012377663,0.13003258],"study_design_scores_gemma":[0.0007844584,0.0005339047,0.00044191506,0.0003144979,0.00009525945,0.00008581045,0.00005326305,0.99342626,0.0026846875,0.0009794076,0.00036436968,0.00023617821],"about_ca_topic_score_codex":4.0118167e-7,"about_ca_topic_score_gemma":0.0000017965373,"teacher_disagreement_score":0.5244365,"about_ca_system_score_codex":0.00006243714,"about_ca_system_score_gemma":0.000016451995,"threshold_uncertainty_score":0.8775954},"labels":[],"label_agreement":null},{"id":"W4362473377","doi":"10.1017/jfm.2023.157","title":"On the effect of adverse pressure gradients on wall-pressure statistics in a controlled-diffusion aerofoil turbulent boundary layer","year":2023,"lang":"en","type":"article","venue":"Journal of Fluid Mechanics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":20,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"General Fusion (Canada); École de Technologie Supérieure; Université de Sherbrooke","funders":"Mitacs","keywords":"Mechanics; Boundary layer; Reynolds number; Physics; Airfoil; Turbulence; Trailing edge; Materials science","score_opus":0.00599488262289738,"score_gpt":0.21960949314395448,"score_spread":0.2136146105210571,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4362473377","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99172807,0.0004962851,0.0051698615,0.00015657912,0.0017001478,0.00046582805,0.00011188716,0.000039880397,0.00013147558],"genre_scores_gemma":[0.9988332,0.00063656823,0.00015208754,0.00006477574,0.0000905252,0.0000099732515,0.0000064520195,0.0000470056,0.0001594371],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9982342,0.00013361202,0.00060406263,0.0001236287,0.00062069733,0.00028380376],"domain_scores_gemma":[0.9985541,0.0007673631,0.00021134716,0.0002760939,0.00010759669,0.00008350482],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0011619793,0.00023328554,0.00053938566,0.00021984556,0.00006654243,0.000017371736,0.00032928376,0.00013710294,0.000043830885],"category_scores_gemma":[0.00042091365,0.00014917125,0.00017484499,0.000230822,0.000016429505,0.00004926655,0.000049994967,0.0006128643,0.000013587108],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0012032035,0.00011185313,0.000036758905,0.00030232038,0.00043317807,0.00022267018,0.00031068374,0.9461473,0.02760337,0.0072555128,0.015378291,0.0009948313],"study_design_scores_gemma":[0.0035924225,0.0010847745,0.00011429506,0.00038132924,0.00022340174,0.000012966955,0.00003591126,0.989093,0.0017596454,0.0020243018,0.0015343394,0.00014359805],"about_ca_topic_score_codex":0.0000032117246,"about_ca_topic_score_gemma":0.0000066648763,"teacher_disagreement_score":0.042945687,"about_ca_system_score_codex":0.000066463355,"about_ca_system_score_gemma":0.000031322896,"threshold_uncertainty_score":0.60830265},"labels":[],"label_agreement":null},{"id":"W4362666036","doi":"10.1007/s10652-023-09919-z","title":"Reynolds flux modeling; new numerical insights into inclined dense jets","year":2023,"lang":"en","type":"article","venue":"Environmental Fluid Mechanics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Wilfrid Laurier University; University of Ottawa","funders":"Compute Canada","keywords":"Turbulence; Scalar (mathematics); Physics; Turbulence modeling; Mechanics; Large eddy simulation; Reynolds number; Statistical physics; Flux (metallurgy); Vector field; Context (archaeology); Classical mechanics; Geometry; Mathematics; Geology; Materials science","score_opus":0.0087251804799502,"score_gpt":0.19848638564662593,"score_spread":0.18976120516667574,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4362666036","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.62731284,0.00038882298,0.3699952,0.00006045606,0.0011169901,0.0001887953,0.000015645754,0.00064243743,0.00027881685],"genre_scores_gemma":[0.993622,0.00097221305,0.0037933544,0.000108615495,0.00026823513,0.000016858314,0.00020133646,0.0001232421,0.00089415273],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99849457,0.00001790283,0.0003597655,0.00035115136,0.00035739582,0.0004192469],"domain_scores_gemma":[0.99925745,0.000034873556,0.000022963728,0.0004301602,0.000003943508,0.0002506093],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00011099021,0.00030229546,0.0002503547,0.000110040055,0.00013467715,0.000031196327,0.00028892313,0.00021047599,0.00022870563],"category_scores_gemma":[0.000023411973,0.00032382243,0.00010345055,0.00023192698,0.000014365502,0.00011114911,0.00026503517,0.00029480393,0.0011646316],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000007913048,0.000030665007,0.000004283032,0.000013593792,0.000036042846,0.000047842557,0.0003995382,0.8362215,0.15482156,0.001013334,0.0034524973,0.0039512436],"study_design_scores_gemma":[0.00032999332,0.000053204712,0.0000111521595,0.000014999588,0.000026334974,0.0000058787887,0.00010913512,0.98296416,0.0035109743,0.008502359,0.0041130143,0.00035878137],"about_ca_topic_score_codex":0.000011065081,"about_ca_topic_score_gemma":0.0000061730875,"teacher_disagreement_score":0.36630917,"about_ca_system_score_codex":0.00027295868,"about_ca_system_score_gemma":0.000017222941,"threshold_uncertainty_score":0.9999214},"labels":[],"label_agreement":null},{"id":"W4366139317","doi":"10.1515/tjj-2022-0073","title":"Effect of zero penetration angle chevrons in supersonic jet noise and screech tone mitigation","year":2023,"lang":"en","type":"article","venue":"International Journal of Turbo and Jet Engines","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Mach number; Supersonic speed; Physics; Nozzle; Acoustics; Schlieren; Noise (video); Penetration (warfare); Optics; Schlieren imaging; Mechanics; Engineering","score_opus":0.004473665508924468,"score_gpt":0.24611320484382204,"score_spread":0.24163953933489757,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4366139317","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99743366,0.00049422926,0.0012367286,0.0001337381,0.0004989456,0.000050274484,0.000019182306,0.00001678201,0.000116436466],"genre_scores_gemma":[0.9985318,0.0009243789,0.0003476759,0.000006505183,0.00014271843,0.0000019862641,0.00001538605,0.000011319251,0.000018226696],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99941933,0.000016467786,0.00024374263,0.000060545142,0.0001771632,0.0000827508],"domain_scores_gemma":[0.9996421,0.00014783617,0.000052492305,0.000038828748,0.00008351579,0.000035239504],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00031487865,0.000089920555,0.00015240487,0.00020226096,0.000011885799,0.000027607242,0.000086848864,0.000049844646,0.0000070331166],"category_scores_gemma":[0.00009685409,0.000075097254,0.00003719361,0.00010880051,0.000023747218,0.00015353401,0.000019316794,0.000118123455,8.332661e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00029926142,0.000105787534,0.18541591,0.0006592588,0.0006058227,0.00025569985,0.0019870766,0.367604,0.36299607,0.0019165629,0.0020554864,0.07609907],"study_design_scores_gemma":[0.0024526312,0.0004596693,0.16195668,0.0005187634,0.00007149184,0.00017098367,0.00014766505,0.80031693,0.032035165,0.0012993546,0.0002791003,0.0002915548],"about_ca_topic_score_codex":0.000009653217,"about_ca_topic_score_gemma":0.000020092933,"teacher_disagreement_score":0.43271294,"about_ca_system_score_codex":0.00002911854,"about_ca_system_score_gemma":0.000009030262,"threshold_uncertainty_score":0.30623773},"labels":[],"label_agreement":null},{"id":"W4366382521","doi":"10.4050/f-0077-2021-16887","title":"Fast Multi-Objective Aeroacoustic Optimization of Propeller Blades ","year":2021,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":6,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Aerodynamics; Noise (video); Propeller; Airfoil; Computer science; Pareto principle; Rotor (electric); Parametric statistics; Trailing edge; Engineering; Acoustics; Marine engineering; Aerospace engineering; Structural engineering; Mechanical engineering; Artificial intelligence; Mathematics","score_opus":0.009337860097536644,"score_gpt":0.20662664527084068,"score_spread":0.19728878517330403,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4366382521","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.016168687,0.00010776309,0.9673085,0.000008923696,0.00025079577,0.0000835231,0.00001280599,0.000110207526,0.01594879],"genre_scores_gemma":[0.86299646,0.000092888775,0.13544685,0.0000111973195,0.000032849257,0.00000506828,0.000016926204,0.00002639398,0.0013713941],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99950564,0.000009073515,0.00015821286,0.0001152586,0.00008957518,0.00012224069],"domain_scores_gemma":[0.9996485,0.000025393843,0.00001768346,0.0001448379,0.00013227064,0.000031292493],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00003890827,0.00009286891,0.00012248312,0.000032269803,0.00002310066,0.000015024206,0.000060084425,0.000056527417,0.00028922863],"category_scores_gemma":[0.000041335563,0.000086546774,0.0000349513,0.00015629151,0.000024931982,0.00004790589,0.000030957704,0.00008385268,0.0000110351275],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000001018605,0.000034032142,0.000051274266,0.000049289138,0.000030643314,0.0000047050657,0.00011222236,0.98653716,0.012144642,0.00021785912,0.00013274651,0.00068440643],"study_design_scores_gemma":[0.00017798904,0.000008893137,0.00018131171,0.000018991417,0.000018834919,0.0000034295092,0.00026449084,0.9923747,0.006797862,0.000022379076,0.000023964732,0.00010716473],"about_ca_topic_score_codex":0.0000030236683,"about_ca_topic_score_gemma":0.000016822809,"teacher_disagreement_score":0.84682775,"about_ca_system_score_codex":0.000028629243,"about_ca_system_score_gemma":0.000020522493,"threshold_uncertainty_score":0.35292748},"labels":[],"label_agreement":null},{"id":"W4375843630","doi":"10.4271/2023-01-1042","title":"Feedforward Harmonic Suppression for Noise Control of Piezoelectrically Driven Synthetic Jet Actuators","year":2023,"lang":"en","type":"article","venue":"SAE International Journal of Advances and Current Practices in Mobility","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"","keywords":"Span (engineering); Actuator; Acoustics; Control theory (sociology); Structural engineering; Engineering; Physics; Electrical engineering; Computer science; Control (management)","score_opus":0.01477548965184692,"score_gpt":0.32089488870619376,"score_spread":0.3061193990543468,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4375843630","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9348467,0.0039782636,0.058069054,0.00026433577,0.002457522,0.00021610406,0.00009376702,0.000019439773,0.00005482497],"genre_scores_gemma":[0.9862964,0.0125140585,0.0010196371,0.000006157601,0.00013211876,0.0000119889455,0.0000060869825,0.00001087656,0.000002648746],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9988401,0.00003642183,0.00053946103,0.00012747239,0.00030941283,0.00014714435],"domain_scores_gemma":[0.9982185,0.0008127313,0.00054939045,0.000089553985,0.00027656593,0.000053294778],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00064853753,0.00011228982,0.00023957147,0.00016150033,0.000023886656,0.000033164546,0.00028415208,0.00004196193,0.000011972714],"category_scores_gemma":[0.0010245739,0.000091642185,0.00009769712,0.00012160686,0.000050422394,0.00051502534,0.000036908496,0.00026496078,7.188941e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00095199194,0.0005695775,0.038515013,0.0006961264,0.0003169544,0.000019864414,0.0003825343,0.24146993,0.0104578845,0.00073855394,0.00031188707,0.7055697],"study_design_scores_gemma":[0.00274859,0.00040003928,0.02286836,0.0005544704,0.00013367757,0.000032308446,0.0002796838,0.937417,0.0008402028,0.011560838,0.022881959,0.00028292803],"about_ca_topic_score_codex":0.0000017625218,"about_ca_topic_score_gemma":0.000012341803,"teacher_disagreement_score":0.70528674,"about_ca_system_score_codex":0.00007719223,"about_ca_system_score_gemma":0.00003870573,"threshold_uncertainty_score":0.37370598},"labels":[],"label_agreement":null},{"id":"W4379805635","doi":"10.2514/6.2023-4052","title":"Flow-field and Noise Characterization of a Controlled-Diffusion Airfoil under stall","year":2023,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Airfoil; Stall (fluid mechanics); Boundary layer; Flow separation; Wind tunnel; Reynolds number; Trailing edge; Mechanics; Angle of attack; Physics; Leading edge; Acoustics; Aerodynamics; Mean flow; Turbulence","score_opus":0.005027464733712754,"score_gpt":0.19235741513190938,"score_spread":0.1873299503981966,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4379805635","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.92479885,0.000011220023,0.07204374,0.00009453895,0.00022219132,0.0001110834,0.000013871391,0.00018207986,0.002522448],"genre_scores_gemma":[0.99861306,0.00033255076,0.00029360745,0.00005649747,0.000038589285,0.000007518599,0.000032243763,0.000017557279,0.00060838176],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995683,0.0000051527036,0.00015561405,0.00007930287,0.00008212604,0.000109514105],"domain_scores_gemma":[0.99977076,0.000058338646,0.000017539223,0.00009591178,0.000024195007,0.00003324176],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000076498945,0.000076593606,0.00014838987,0.000063781794,0.000022686363,0.000013466561,0.000041361523,0.000059172777,0.000072060124],"category_scores_gemma":[0.0000195661,0.000066352426,0.000026472177,0.00011089944,0.000009946247,0.000041652653,0.00003397716,0.000056024084,0.000010749205],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000026024552,0.000014190418,0.0001660969,0.000080251215,0.00003012605,0.0000024351896,0.00010691322,0.03755316,0.9548764,0.0016084845,0.00027164232,0.0052642752],"study_design_scores_gemma":[0.00075798325,0.000022774055,0.0048041083,0.000016036456,0.000011200081,6.0407365e-7,0.000035745194,0.99258053,0.0013050918,0.00026963945,0.00011697901,0.000079322206],"about_ca_topic_score_codex":0.000004582794,"about_ca_topic_score_gemma":0.000009929835,"teacher_disagreement_score":0.95502734,"about_ca_system_score_codex":0.000008312434,"about_ca_system_score_gemma":0.0000046737705,"threshold_uncertainty_score":0.27057734},"labels":[],"label_agreement":null},{"id":"W4379877348","doi":"10.2514/6.2023-3641","title":"Numerical investigation of aerodynamics and aeroacoustics of helical Darrieus wind turbines","year":2023,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Wake; Aerodynamics; Turbine; Vortex; Aeroacoustics; Large eddy simulation; Mechanics; Acoustics; Noise (video); Trailing edge; Structural engineering; Physics; Engineering; Sound pressure; Aerospace engineering; Turbulence; Computer science","score_opus":0.008192327530807592,"score_gpt":0.20278751002624573,"score_spread":0.19459518249543814,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4379877348","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9729557,0.000044306937,0.025672944,0.000038793696,0.00022950079,0.00008095432,0.000037992493,0.00016086448,0.0007789665],"genre_scores_gemma":[0.99462223,0.00013374723,0.005060611,0.000012378626,0.000044441073,0.0000018392851,0.00003154034,0.000027222903,0.00006601414],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99924034,0.000009887667,0.00030514604,0.00012116169,0.00016593176,0.000157509],"domain_scores_gemma":[0.9995409,0.00011505161,0.00003850044,0.00016383678,0.000066445806,0.00007526814],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012406186,0.00011789156,0.00021516517,0.00008941542,0.000021498221,0.000008469759,0.00009354116,0.00009700611,0.000012786569],"category_scores_gemma":[0.00008118187,0.00011119222,0.000032372493,0.0003535527,0.00011738742,0.00004314365,0.000046249537,0.000109842345,0.0000040880195],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000008477358,0.000017079228,0.008608741,0.0005317506,0.00006740084,0.0000058233295,0.0003217804,0.8513897,0.13058119,0.005352915,0.001249784,0.0018653561],"study_design_scores_gemma":[0.00013854043,0.000034336957,0.016647346,0.000024443474,0.00002132386,0.0000029422743,0.000075201984,0.9797847,0.0018166561,0.0013135836,0.000023888582,0.000116979994],"about_ca_topic_score_codex":0.000011261171,"about_ca_topic_score_gemma":0.0000061607584,"teacher_disagreement_score":0.12876453,"about_ca_system_score_codex":0.000013942316,"about_ca_system_score_gemma":0.000014942222,"threshold_uncertainty_score":0.45342872},"labels":[],"label_agreement":null},{"id":"W4379878611","doi":"10.2514/6.2023-4524","title":"Aeroacoustics of drones","year":2023,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Anechoic chamber; Directivity; Acoustics; Drone; Noise (video); Signature (topology); Aeroacoustics; Microphone; Noise measurement; Computer science; Physics; Loudspeaker; Noise reduction; Antenna (radio); Telecommunications; Artificial intelligence; Mathematics","score_opus":0.0061417766093788415,"score_gpt":0.18596035729691818,"score_spread":0.17981858068753934,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4379878611","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7802051,0.0000398336,0.15221545,0.000025925616,0.00086000306,0.00006143217,0.000023619548,0.000942225,0.06562642],"genre_scores_gemma":[0.9969294,0.00010082204,0.002032653,0.0000054331595,0.000037166352,0.0000018519047,0.000006305701,0.000015825006,0.0008705377],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996943,0.0000013090323,0.00009413942,0.000041546195,0.000066658744,0.000102034435],"domain_scores_gemma":[0.9998292,0.000029172455,0.0000035925357,0.00010226825,0.00001598743,0.000019819243],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000046765745,0.00004610989,0.00006701728,0.00004312649,0.000010625885,0.0000037675084,0.000064989355,0.000029330518,0.00006109407],"category_scores_gemma":[0.000011742231,0.000043098138,0.000019812678,0.00017147341,0.000014603802,0.000014019409,0.000019227204,0.00003844112,0.00008520956],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[5.533762e-7,0.0000065177815,0.00020354976,0.00008913593,0.000021355218,0.0000049536598,0.000060896644,0.92206985,0.045699533,0.010732703,0.018283792,0.0028271535],"study_design_scores_gemma":[0.000043681415,0.0000056462736,0.0008415482,0.0000048385664,0.000005278853,5.0151414e-7,0.000056435838,0.9958799,0.0013569017,0.0011257875,0.00061887875,0.00006061555],"about_ca_topic_score_codex":0.0000015711206,"about_ca_topic_score_gemma":0.0000034991242,"teacher_disagreement_score":0.21672432,"about_ca_system_score_codex":0.0000060292323,"about_ca_system_score_gemma":0.0000027476558,"threshold_uncertainty_score":0.1757491},"labels":[],"label_agreement":null},{"id":"W4379930507","doi":"10.2514/6.2023-4481","title":"Experimental and Computational Characterization of Canonical Side-Edge Noise","year":2023,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke; Institute for Christian Studies; University of Toronto","funders":"","keywords":"Aerodynamics; Airfoil; Vortex; Trailing edge; Acoustics; Noise (video); Detached eddy simulation; Leading edge; Physics; Mechanics; Computational fluid dynamics; Computer science; Reynolds-averaged Navier–Stokes equations","score_opus":0.008809978821192324,"score_gpt":0.2276059570683663,"score_spread":0.21879597824717398,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4379930507","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97107506,0.000009199982,0.02710337,0.000018138813,0.00012532642,0.000038460585,0.000020137762,0.00010456714,0.0015057579],"genre_scores_gemma":[0.9988873,0.000008333694,0.00086490746,0.000011780444,0.000025506752,0.0000032913645,0.00008316344,0.000009941179,0.00010578138],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997272,0.0000025503289,0.00009483974,0.00005358431,0.0000588264,0.00006301258],"domain_scores_gemma":[0.9998987,0.000020069609,0.000008027944,0.00003726267,0.0000120433615,0.000023897346],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000027946657,0.000043182667,0.000058224166,0.00003056297,0.000015386187,0.0000073171605,0.00002569415,0.000023634071,0.000031619194],"category_scores_gemma":[0.0000033025788,0.00004342346,0.000010481387,0.00007062059,0.000018625795,0.00003098705,0.000021461587,0.000027492884,0.000010176037],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000001572056,0.00001090857,0.00045804828,0.000022376178,0.000009783436,0.0000015616657,0.00010954679,0.07208343,0.9226082,0.0040212865,0.000111430454,0.00056186196],"study_design_scores_gemma":[0.00010330732,0.000009337052,0.03407975,0.000004809352,0.0000020207247,0.0000013489941,0.000026476588,0.9585605,0.0069677886,0.00010469825,0.00008434964,0.000055596836],"about_ca_topic_score_codex":0.0000017409153,"about_ca_topic_score_gemma":9.4397285e-7,"teacher_disagreement_score":0.9156404,"about_ca_system_score_codex":0.000010647954,"about_ca_system_score_gemma":0.0000059280433,"threshold_uncertainty_score":0.17707573},"labels":[],"label_agreement":null},{"id":"W4381057223","doi":"10.3397/nc_2023_01_1042","title":"Feedforward Harmonic Suppression for Noise Control of Piezoelectric Synthetic Jet Actuators","year":2023,"lang":"en","type":"article","venue":"NOISE-CON proceedings","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"","keywords":"Acoustics; Synthetic jet; Feed forward; Harmonics; Actuator; Microphone; Engineering; Active noise control; Noise control; Harmonic; Noise (video); Loudspeaker; Noise reduction; Computer science; Electrical engineering; Physics; Control engineering","score_opus":0.008738470814510907,"score_gpt":0.21810637764940566,"score_spread":0.20936790683489476,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4381057223","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9658065,0.00014192188,0.03018665,0.00015129765,0.0007167057,0.0008260075,0.00012498333,0.0007519666,0.0012939686],"genre_scores_gemma":[0.9983377,0.00016564295,0.0007459272,0.000037659218,0.00015377735,0.0001866554,0.000020737874,0.000118603595,0.00023328682],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99839795,0.0000036425256,0.00043882206,0.00032565487,0.00024905842,0.00058486086],"domain_scores_gemma":[0.9992078,0.00018106516,0.00011235719,0.00015979419,0.0002056193,0.00013339888],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0003494253,0.0002999111,0.0004334886,0.00030769053,0.00010356219,0.00005455782,0.00033471646,0.00020191373,0.000037316335],"category_scores_gemma":[0.00026571637,0.00027898178,0.0001817781,0.00059220265,0.000052482195,0.00016173159,0.00004307293,0.00023469403,0.000048464757],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0003351119,0.00015591574,0.0071833464,0.0032423446,0.0004308965,0.00000687205,0.0013862309,0.011684277,0.8625822,0.007823682,0.045169212,0.05999989],"study_design_scores_gemma":[0.0014030894,0.0001695006,0.0011834801,0.00016083173,0.0001591099,0.0000053473846,0.00013994405,0.9616714,0.029472068,0.002117366,0.0030749994,0.00044286807],"about_ca_topic_score_codex":0.000003067367,"about_ca_topic_score_gemma":5.907703e-7,"teacher_disagreement_score":0.9499871,"about_ca_system_score_codex":0.000091646725,"about_ca_system_score_gemma":0.00003131683,"threshold_uncertainty_score":0.99996626},"labels":[],"label_agreement":null},{"id":"W4381513950","doi":"10.1016/j.jsv.2023.117888","title":"Large Eddy Simulation of the ACAT1 fan stage for broadband noise prediction","year":2023,"lang":"en","type":"article","venue":"Journal of Sound and Vibration","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":12,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure; Université du Québec à Montréal","funders":"Agence Nationale de la Recherche","keywords":"Duct (anatomy); Stator; Aerodynamics; Large eddy simulation; Noise (video); Acoustics; Aeroacoustics; Rotor (electric); Turbulence; Computational fluid dynamics; Mechanics; Physics; Engineering; Sound pressure; Computer science; Mechanical engineering","score_opus":0.01318402155764314,"score_gpt":0.2505276825553127,"score_spread":0.23734366099766957,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4381513950","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.65226895,0.000032307944,0.34715417,0.000024883167,0.00035962646,0.000068750334,0.000045811084,0.000010921935,0.000034571844],"genre_scores_gemma":[0.9994006,0.000054617154,0.00024102321,0.000008581952,0.00021864768,8.8696555e-7,0.000009691704,0.000008753443,0.0000571684],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995839,0.000007264781,0.00021005103,0.00003358639,0.00010163802,0.000063534215],"domain_scores_gemma":[0.9997104,0.000060458253,0.00009645452,0.00004691792,0.00006738391,0.000018383122],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002114789,0.0000447748,0.00007364886,0.000048409765,0.00006785517,0.000024949846,0.000038091912,0.00004253638,0.00000348577],"category_scores_gemma":[0.000042802185,0.000032592576,0.000040928026,0.00009109734,0.000009896568,0.00016011477,0.000008369355,0.00006872315,2.6900958e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000012839282,0.000009392059,0.0011595994,0.000070877686,0.00001821618,1.6176382e-7,0.0003751928,0.97823405,0.018852873,0.00035379775,0.00018435925,0.0007286638],"study_design_scores_gemma":[0.0003391299,0.00004767119,0.011869953,0.000024734874,0.000021618482,0.0000010759162,0.00017158594,0.984431,0.0005837498,0.0019479153,0.0005287731,0.000032772503],"about_ca_topic_score_codex":2.4285134e-7,"about_ca_topic_score_gemma":0.0000031091304,"teacher_disagreement_score":0.34713167,"about_ca_system_score_codex":0.000014718761,"about_ca_system_score_gemma":0.000008065741,"threshold_uncertainty_score":0.13290867},"labels":[],"label_agreement":null},{"id":"W4383032579","doi":"10.1016/j.enganabound.2023.06.035","title":"A comprehensive multi-objective optimization study for the aerodynamic noise mitigation of a small wind turbine","year":2023,"lang":"en","type":"article","venue":"Engineering Analysis with Boundary Elements","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":14,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Calgary","funders":"Materials and Energy Research Center","keywords":"Aerodynamics; Noise (video); Turbine; Turbine blade; Wind power; Inertia; Computer science; Noise control; Power (physics); Noise reduction; Acoustics; Environmental science; Control theory (sociology); Aerospace engineering; Engineering; Physics; Electrical engineering","score_opus":0.010022927148574966,"score_gpt":0.22791837980438728,"score_spread":0.2178954526558123,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4383032579","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.4777426,0.00010003653,0.5212747,0.0000054481957,0.00013497613,0.0005302019,0.00006326413,0.00014563031,0.0000031547463],"genre_scores_gemma":[0.9815888,0.00005709231,0.017786995,0.0000036414265,0.000045779525,0.00013045447,0.00028003822,0.000060826293,0.000046380705],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99882776,0.00001801396,0.00039313588,0.00024759094,0.00023680732,0.00027667006],"domain_scores_gemma":[0.9991575,0.00018019462,0.00009178107,0.0003247371,0.00019998445,0.00004579084],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024018549,0.00023769298,0.00033925488,0.00040710944,0.00015087932,0.000060776092,0.00019111797,0.000040499315,0.000006682179],"category_scores_gemma":[0.00003694744,0.00019165094,0.0001282212,0.0017075429,0.0000327253,0.0000733415,0.00003912,0.000155027,0.0000018253925],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000015959838,0.00005946322,0.00427666,0.00008827776,0.0025637823,0.0000021104522,0.0005272957,0.9912774,0.0006950841,0.000005628354,0.000011578593,0.00047678547],"study_design_scores_gemma":[0.0008626301,0.00009661283,0.050012317,0.000026552469,0.0011626139,3.8380162e-7,0.00045411178,0.947085,0.000030872423,0.0000026983985,0.00007084658,0.0001953658],"about_ca_topic_score_codex":0.000021828027,"about_ca_topic_score_gemma":0.00012931201,"teacher_disagreement_score":0.50384617,"about_ca_system_score_codex":0.000098884855,"about_ca_system_score_gemma":0.000023088092,"threshold_uncertainty_score":0.7815298},"labels":[],"label_agreement":null},{"id":"W4383316265","doi":"10.2514/6.2023-3634.c1","title":"Correction: Computational Aeroacoustic Predictions of the 30P30N High-Lift Airfoil","year":2023,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke; University of Toronto","funders":"","keywords":"Airfoil; Lift (data mining); Computer science; Acoustics; Computational fluid dynamics; Aerospace engineering; Marine engineering; Engineering; Physics; Data mining","score_opus":0.0055417117435507274,"score_gpt":0.18981669914311922,"score_spread":0.1842749873995685,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4383316265","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.25301963,0.00002869715,0.6975259,0.00032179512,0.01648712,0.00023789013,0.00014029795,0.0014210618,0.030817604],"genre_scores_gemma":[0.9955837,0.000017130773,0.0008540379,0.000024178984,0.00013183022,0.000011199936,0.000025690153,0.000020022979,0.003332178],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994215,0.000008603428,0.00017302943,0.000087879416,0.00018143054,0.00012757597],"domain_scores_gemma":[0.9996051,0.00013044539,0.000020283143,0.00015853214,0.000056415756,0.00002920164],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000070849885,0.00008003444,0.000086474836,0.00005320527,0.00010214813,0.000011919517,0.00012570035,0.00004851832,0.00012330439],"category_scores_gemma":[0.00003554169,0.000062473024,0.000051141804,0.00044216093,0.00004790737,0.00003160305,0.00004340917,0.00013330633,0.00005924373],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[5.593842e-7,0.0000080445925,0.00020634748,0.000015487502,0.000021762624,4.8572525e-7,0.0000323617,0.9425211,0.00021148818,0.0020684544,0.054576036,0.00033786215],"study_design_scores_gemma":[0.00009308484,0.000008592152,0.019798819,0.000016406806,0.000018248073,0.000004021883,0.000060433846,0.97810566,0.000054027834,0.0013204666,0.00045413655,0.000066109904],"about_ca_topic_score_codex":0.0000150528,"about_ca_topic_score_gemma":0.000029631068,"teacher_disagreement_score":0.7425641,"about_ca_system_score_codex":0.000034691922,"about_ca_system_score_gemma":0.00002138899,"threshold_uncertainty_score":0.25475758},"labels":[],"label_agreement":null},{"id":"W4383879155","doi":"10.29169/1927-5129.2023.19.09","title":"Sensitivity Analysis of Wind Turbine Broadband Noise Estimation to Semi-Empirical Models Parameters","year":2023,"lang":"en","type":"article","venue":"Journal of Basic & Applied Sciences","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Noise (video); Sensitivity (control systems); Wind power; Turbine; Boundary layer; Turbulence kinetic energy; Environmental science; Turbulence; Acoustics; Meteorology; Computer science; Mechanics; Engineering; Physics; Electronic engineering; Aerospace engineering","score_opus":0.02708418915141011,"score_gpt":0.27351350022871834,"score_spread":0.24642931107730823,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4383879155","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.83428556,0.000013227517,0.16471873,0.00011574465,0.0001521963,0.000054636177,0.00001110677,0.000022585475,0.0006262474],"genre_scores_gemma":[0.98854536,0.000018465782,0.011334935,0.000045465786,0.000036303045,8.318415e-7,0.0000020928007,0.00000744753,0.000009092028],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99872977,0.000017539867,0.00040539427,0.0001352325,0.0005120356,0.00020004237],"domain_scores_gemma":[0.9993147,0.0002509505,0.00013566189,0.000116698066,0.00007329152,0.00010866075],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0012829246,0.00010769825,0.00035335607,0.00061126414,0.00007021184,0.000046682737,0.00017071023,0.000047383663,0.000006113783],"category_scores_gemma":[0.00006077224,0.0000878985,0.000118007694,0.0023454926,0.000103067454,0.00013911164,0.00003469793,0.00014284346,0.0000041478293],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000072133257,0.000013100578,0.00028594414,0.000010591204,0.000104846,0.0000066405023,0.00032156653,0.9753074,0.020961432,0.00010839889,0.0003519889,0.0025208849],"study_design_scores_gemma":[0.000094892,0.000041440642,0.005159892,0.00001794026,0.00019248622,0.000004209671,0.00014229452,0.9916937,0.0014551826,0.0010920144,0.000009813591,0.000096137854],"about_ca_topic_score_codex":0.0000058221012,"about_ca_topic_score_gemma":0.000013196698,"teacher_disagreement_score":0.15425983,"about_ca_system_score_codex":0.000048799404,"about_ca_system_score_gemma":0.000040396888,"threshold_uncertainty_score":0.35843968},"labels":[],"label_agreement":null},{"id":"W4384163490","doi":"10.1016/j.jfluidstructs.2023.103949","title":"Aeroacoustics and shear layer characteristics of confined cavities subject to low Mach number flow","year":2023,"lang":"en","type":"article","venue":"Journal of Fluids and Structures","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Ontario Tech University","funders":"","keywords":"Strouhal number; Aeroacoustics; Mach number; Mechanics; Physics; Vortex shedding; Particle image velocimetry; Optics; Acoustics; Flow visualization; Sound pressure; Flow (mathematics); Reynolds number; Turbulence","score_opus":0.007747605768967567,"score_gpt":0.22710696371178649,"score_spread":0.2193593579428189,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4384163490","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9941037,0.00016891533,0.0046114447,0.000042965894,0.00066038215,0.000052299278,0.00013477208,0.000021645728,0.00020384506],"genre_scores_gemma":[0.99440235,0.00072616147,0.0044643343,0.000036418303,0.00026386554,6.28135e-7,0.000004946264,0.000025283443,0.000076039534],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99917597,0.000011832686,0.0003707237,0.00007865643,0.0001880551,0.00017476041],"domain_scores_gemma":[0.99953955,0.00007733376,0.00005879876,0.000092150585,0.000118229866,0.00011392695],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015510689,0.0001430227,0.000333818,0.00010588534,0.000047405276,0.000051113224,0.00008764341,0.0000851564,0.000042553787],"category_scores_gemma":[0.0000680717,0.00011726612,0.000046472844,0.00011402343,0.000054289358,0.000044435594,0.00003751808,0.00019003273,0.0000010866157],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00040877346,0.00006105991,0.026152307,0.0028911247,0.001038589,0.0005917101,0.006841411,0.173685,0.6370905,0.0068924376,0.037221067,0.10712603],"study_design_scores_gemma":[0.0016161468,0.000494168,0.3420726,0.00039281446,0.0003167762,0.0005210661,0.0010678989,0.63798654,0.0066658654,0.0054172636,0.0025723875,0.00087643723],"about_ca_topic_score_codex":0.0000047674375,"about_ca_topic_score_gemma":0.0000028901084,"teacher_disagreement_score":0.6304246,"about_ca_system_score_codex":0.000014148593,"about_ca_system_score_gemma":0.000018388037,"threshold_uncertainty_score":0.47819737},"labels":[],"label_agreement":null},{"id":"W4385690203","doi":"10.1121/10.0020561","title":"Amplitude modulation of acoustic waves in accelerating flows quantified using acoustic black and white hole analogues","year":2023,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Polytechnique Montréal","funders":"Deutsche Forschungsgemeinschaft","keywords":"Acoustics; Physics; Amplitude; Acoustic wave equation; Acoustic wave; Acoustic radiation; Modulation (music); Amplitude modulation; Flow (mathematics); Helmholtz free energy; Mechanics; Frequency modulation; Optics; Computer science; Telecommunications; Radiation; Radio frequency","score_opus":0.027463307396052055,"score_gpt":0.2608652188842576,"score_spread":0.23340191148820558,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4385690203","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6705781,0.000073343566,0.32889038,0.00012629495,0.00017581291,0.000102021004,0.000016744294,0.000017749624,0.000019531166],"genre_scores_gemma":[0.977808,0.0006616191,0.021316163,0.000051206214,0.000116535266,6.888727e-7,0.0000017936931,0.000033737302,0.000010255668],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9983104,0.00008981262,0.0007618801,0.000111317575,0.0004194326,0.00030715184],"domain_scores_gemma":[0.99851835,0.00064366625,0.00035483882,0.00026837876,0.000151476,0.00006328639],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0008174575,0.00019039662,0.0004706498,0.00007105927,0.00011695982,0.000027179163,0.0003935788,0.0001035316,0.000008747823],"category_scores_gemma":[0.00028216818,0.00012438852,0.0002038054,0.00067279424,0.00042877803,0.00011069429,0.00017203765,0.0004932365,9.1326433e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000014443294,0.000021298154,0.00039874495,0.00014773794,0.00007218232,9.425485e-7,0.0009071866,0.71719855,0.2802223,0.000001742127,0.0002390953,0.00077578047],"study_design_scores_gemma":[0.00025421643,0.0000575419,0.014308431,0.00020054585,0.00018865411,0.000009624691,0.0024959191,0.98159134,0.00025671313,0.00050851016,0.0000034737384,0.00012502082],"about_ca_topic_score_codex":0.00002991132,"about_ca_topic_score_gemma":0.0000070154506,"teacher_disagreement_score":0.3075742,"about_ca_system_score_codex":0.00007461821,"about_ca_system_score_gemma":0.00004331804,"threshold_uncertainty_score":0.50724167},"labels":[],"label_agreement":null},{"id":"W4386560420","doi":"10.3390/aerospace10090791","title":"Recent Advances in Airfoil Self-Noise Passive Reduction","year":2023,"lang":"en","type":"article","venue":"Aerospace","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":21,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Carleton University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Airfoil; Morphing; Noise reduction; Noise (video); Computer science; Reduction (mathematics); Noise control; Computation; Trailing edge; Emphasis (telecommunications); Engineering; Aerospace engineering; Artificial intelligence; Telecommunications; Algorithm; Structural engineering","score_opus":0.005190117465206628,"score_gpt":0.21956133150236684,"score_spread":0.21437121403716022,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4386560420","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97503,0.0042087203,0.0019507828,0.0010314767,0.0038597207,0.00029457803,0.000017443224,0.002214866,0.011392413],"genre_scores_gemma":[0.93928325,0.058541577,0.0011918687,0.00001680164,0.0001754451,0.00004226338,0.000020552736,0.000045492732,0.00068276084],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99933064,0.000009509588,0.00012787599,0.00015589152,0.00012381484,0.00025224604],"domain_scores_gemma":[0.9997153,0.000023984558,0.00001938582,0.00016742396,0.000028588644,0.000045309404],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000086261374,0.00011138885,0.00011007343,0.00006962199,0.00003836564,0.000018127143,0.000088993234,0.00006451857,0.00002026412],"category_scores_gemma":[0.000025765294,0.00011813838,0.000023596625,0.00051013206,0.000015413698,0.00013251556,0.000028593176,0.00016225225,0.00016043155],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000054664806,0.000029670811,0.00050890143,0.000074451025,0.00001638683,0.000029582687,0.00067452237,0.9101058,0.0064912844,0.0008853709,0.013067981,0.06811058],"study_design_scores_gemma":[0.0006448498,0.000052266023,0.0060419096,0.0001072222,0.000019950598,0.000011877136,0.0010357553,0.7377405,0.0023117464,0.0019128028,0.24952124,0.0005998871],"about_ca_topic_score_codex":0.000003054197,"about_ca_topic_score_gemma":0.000055851826,"teacher_disagreement_score":0.23645326,"about_ca_system_score_codex":0.00013658784,"about_ca_system_score_gemma":0.000010834449,"threshold_uncertainty_score":0.48175433},"labels":[],"label_agreement":null},{"id":"W4386860934","doi":"10.1063/5.0166646","title":"Aeroacoustic investigation of airfoil at near-stall conditions","year":2023,"lang":"en","type":"article","venue":"Physics of Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":10,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Airfoil; Stall (fluid mechanics); Physics; Relative wind; Flow separation; Acoustics; Angle of attack; NACA airfoil; Reynolds number; Mechanics; Aeroacoustics; Aerodynamics; Turbulence; Sound pressure","score_opus":0.013994383284219888,"score_gpt":0.22378663771926155,"score_spread":0.20979225443504165,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4386860934","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98553437,0.000030740437,0.012506283,0.00001985346,0.00025786547,0.00007458878,0.00019622476,0.00016531916,0.0012147392],"genre_scores_gemma":[0.9985252,0.00004202705,0.0010408976,0.00000891653,0.0000679992,0.0000098374885,0.00018390933,0.000031133328,0.000090089416],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99937356,0.0000074518052,0.00021447695,0.00009399245,0.00016404585,0.00014647002],"domain_scores_gemma":[0.999535,0.0000988948,0.000034411656,0.00021040098,0.0000762241,0.00004505669],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00007058085,0.0000991475,0.00015932447,0.000034815177,0.000049410683,0.0000070759597,0.000111034286,0.000046441826,0.000022151085],"category_scores_gemma":[0.000026456948,0.00011209352,0.000062380364,0.00033179895,0.00013016515,0.000064360494,0.00005208193,0.00007611972,0.000047851154],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000001053839,0.000007889271,0.00030989212,0.00015409387,0.00002970271,8.3860806e-7,0.00024497474,0.5748603,0.4191239,0.0031684102,0.0019263669,0.0001725864],"study_design_scores_gemma":[0.00013884425,0.00002414969,0.0037246721,0.000041653107,0.00003547783,3.3463567e-7,0.00002835971,0.9657398,0.017735098,0.012360489,0.000051616335,0.00011953679],"about_ca_topic_score_codex":0.0000072300077,"about_ca_topic_score_gemma":0.0000029781713,"teacher_disagreement_score":0.4013888,"about_ca_system_score_codex":0.000036057823,"about_ca_system_score_gemma":0.000020296337,"threshold_uncertainty_score":0.45710412},"labels":[],"label_agreement":null},{"id":"W4387231110","doi":"10.3390/app131910893","title":"Advances in Riblets Design","year":2023,"lang":"en","type":"article","venue":"Applied Sciences","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":13,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"National Research Council Canada; Carleton University","funders":"","keywords":"Drag; Boundary layer; Turbulence; Marine engineering; Aerospace engineering; Wind tunnel; Mechanical engineering; Noise control; Aviation; Engineering; Noise (video); Computer science; Acoustics; Mechanics; Noise reduction; Physics","score_opus":0.018413490053280683,"score_gpt":0.24298772391320234,"score_spread":0.22457423385992165,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4387231110","genre_codex":"other","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.3997758,0.0009890589,0.19288589,0.00014785165,0.0015020648,0.00047620476,0.000006574627,0.0014609572,0.40275562],"genre_scores_gemma":[0.99483496,0.0005128943,0.0045466046,0.000018337727,0.000028765158,0.000023943447,8.802186e-7,0.0000067161886,0.000026907554],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994161,0.0000037946756,0.00009023176,0.00012774787,0.0001357489,0.00022637384],"domain_scores_gemma":[0.9998089,0.000089496636,0.000007803368,0.000066873166,0.0000035195999,0.00002341238],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00036813936,0.00006176224,0.00006772577,0.00011251656,0.000066852386,0.000028999311,0.00019664362,0.000024151917,0.000012763326],"category_scores_gemma":[0.000009756318,0.0000549256,0.000008761171,0.0008672178,0.000084684645,0.000080862796,0.000023118895,0.000059810558,0.00013240127],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[4.854161e-7,0.0000022724757,0.00008683179,0.000007823153,5.385094e-7,0.000003034448,0.00007294063,0.97008026,0.0047291736,0.010764455,0.0004075765,0.0138446065],"study_design_scores_gemma":[0.000078955156,0.000010170351,0.0006025233,0.000009517998,0.0000010350115,5.413299e-7,0.00019684744,0.9704127,0.0009991447,0.02551068,0.0020405124,0.00013738993],"about_ca_topic_score_codex":8.8947917e-7,"about_ca_topic_score_gemma":0.000011700443,"teacher_disagreement_score":0.59505916,"about_ca_system_score_codex":0.000013233091,"about_ca_system_score_gemma":0.000010046975,"threshold_uncertainty_score":0.2239801},"labels":[],"label_agreement":null},{"id":"W4387725503","doi":"10.48550/arxiv.2310.10574","title":"Near-Field Aeroacoustic Shape Optimization at Low Reynolds Numbers","year":2023,"lang":"en","type":"preprint","venue":"arXiv (Cornell University)","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Fonds de recherche du Québec – Nature et technologies; Natural Sciences and Engineering Research Council of Canada","keywords":"Airfoil; Reynolds number; Sound pressure; Lift-to-drag ratio; Acoustics; Mach number; Lift coefficient; Drag coefficient; Physics; Drag; Noise (video); Aeroacoustics; Noise reduction; Lift (data mining); NACA airfoil; Mechanics; Computer science; Turbulence","score_opus":0.034124601562745875,"score_gpt":0.16852742657943812,"score_spread":0.13440282501669223,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4387725503","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.572639,0.000031037245,0.42075145,0.000023995799,0.0020943326,0.00026666472,0.00008313492,0.0010440992,0.003066276],"genre_scores_gemma":[0.9931231,0.00083285756,0.0018643031,0.0000427671,0.00015309424,0.0000021711185,0.00018262376,0.00013967429,0.00365938],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9984568,0.000029356206,0.00024956826,0.0007071038,0.000108692046,0.00044851672],"domain_scores_gemma":[0.99870795,0.0001470213,0.000099487566,0.00077990995,0.00009563961,0.00016997421],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00013040137,0.0004112652,0.00035381352,0.00015468482,0.0001930395,0.00009378145,0.00061003014,0.00061871094,0.0004284076],"category_scores_gemma":[0.00006443738,0.00054467225,0.00019669988,0.00042904058,0.00007917397,0.0000988827,0.0008314742,0.00074446376,0.0003100541],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000016499935,0.000018042108,0.00052860583,0.0002466572,0.00011502848,0.00022584644,0.00007514831,0.99495715,0.000048175545,0.000616909,0.0030649973,0.00008693384],"study_design_scores_gemma":[0.00024239557,0.00001887801,0.00014185384,0.0001475523,0.0001505643,0.0000025109473,0.000054238335,0.99761117,0.00002110937,0.0009690264,0.00009468162,0.0005460171],"about_ca_topic_score_codex":0.00007674795,"about_ca_topic_score_gemma":0.0001069819,"teacher_disagreement_score":0.42048413,"about_ca_system_score_codex":0.0005907685,"about_ca_system_score_gemma":0.00006197053,"threshold_uncertainty_score":0.9997005},"labels":[],"label_agreement":null},{"id":"W4388023497","doi":"10.18280/ts.400506","title":"Predicting Flow-Induced Noise Based on an Improved Four-Dimensional Acoustic Analogy Model and Multi-Domain Feature Analysis","year":2023,"lang":"en","type":"article","venue":"Traitement du signal","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"Natural Science Foundation of Ningxia Province","keywords":"Noise (video); Acoustics; Frequency domain; Sound pressure; Mathematical analysis; Time domain; Acoustic wave equation; Mathematics; Physics; Computer science; Acoustic wave; Artificial intelligence","score_opus":0.01650354775750999,"score_gpt":0.22982377100337842,"score_spread":0.21332022324586844,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4388023497","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6914424,0.000009726593,0.30764976,0.000060824696,0.000106937005,0.00020640936,0.00015836889,0.00031883336,0.000046777855],"genre_scores_gemma":[0.9763321,0.000004920088,0.022923212,0.00014571824,0.00013307821,0.00004431216,0.00031314357,0.00006353834,0.000039974537],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.998376,0.00004594608,0.00030973798,0.0004487569,0.00034160656,0.0004779416],"domain_scores_gemma":[0.9993012,0.00013087029,0.00005175361,0.00023584932,0.000062289044,0.00021804249],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.000418358,0.00032430678,0.00034613893,0.0004294834,0.00019100374,0.00006362761,0.00015551675,0.00016794381,0.000057818266],"category_scores_gemma":[0.000018730074,0.0003172627,0.00013320091,0.0006232685,0.00003230109,0.00009579709,0.000044238415,0.00033593515,0.0000058686765],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00003284326,0.00006222745,0.00053639465,0.00003671251,0.00022592829,0.000030146417,0.00012989712,0.87752044,0.11993758,0.000012021468,0.00009431689,0.001381481],"study_design_scores_gemma":[0.0011066826,0.00014064628,0.0068934304,0.000022139213,0.00035225114,0.0000017316848,0.00006285604,0.99095124,0.00008988754,0.00005236871,0.000004077639,0.00032267006],"about_ca_topic_score_codex":0.000009716442,"about_ca_topic_score_gemma":0.00012922773,"teacher_disagreement_score":0.28488973,"about_ca_system_score_codex":0.000090273796,"about_ca_system_score_gemma":0.000034595207,"threshold_uncertainty_score":0.99992794},"labels":[],"label_agreement":null},{"id":"W4388280665","doi":"10.1139/tcsme-2023-0028","title":"Numerical investigation of the velocity and spreading characteristics of non-circular turbulent jets at different Reynolds numbers","year":2023,"lang":"en","type":"article","venue":"Transactions of the Canadian Society for Mechanical Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Turbulence; Reynolds number; Mechanics; Jet (fluid); Physics; Turbulence kinetic energy; Laminar flow; Anemometer; Classical mechanics","score_opus":0.008389259615020924,"score_gpt":0.18731095756734117,"score_spread":0.17892169795232024,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4388280665","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8922399,0.000017853776,0.10665578,0.00016227378,0.00044857108,0.00025962657,0.00017306964,0.00003685563,0.0000060606085],"genre_scores_gemma":[0.9986205,0.00003732706,0.001230531,0.0000136927365,0.000019244491,0.00001839674,0.0000075940266,0.000030803138,0.000021906677],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992621,0.0000058689207,0.00027216887,0.000105397594,0.00014661213,0.0002078776],"domain_scores_gemma":[0.99947846,0.00009541281,0.000050927323,0.0002222029,0.000040029652,0.000112952315],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012177506,0.00012353131,0.00021462259,0.000031248303,0.00012123273,0.000006254352,0.00018915722,0.00012979351,0.0000049171754],"category_scores_gemma":[0.000033547483,0.00010052502,0.00030255923,0.00026413935,0.00005599905,0.000026951231,0.000012816649,0.00018555584,2.0113609e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000004816033,0.000012748306,0.00029151948,0.0015091237,0.00039540112,3.5672753e-7,0.001278993,0.77784747,0.21647966,0.0011313375,0.00019356856,0.00085502694],"study_design_scores_gemma":[0.0001424228,0.000011637219,0.005444257,0.000115356925,0.00008975112,0.0000023492246,0.000041492684,0.96464807,0.029218793,0.00011878051,0.00006058243,0.000106519365],"about_ca_topic_score_codex":0.00060823926,"about_ca_topic_score_gemma":0.00065889343,"teacher_disagreement_score":0.18726087,"about_ca_system_score_codex":0.0002570945,"about_ca_system_score_gemma":0.000034689932,"threshold_uncertainty_score":0.40992916},"labels":[],"label_agreement":null},{"id":"W4388537262","doi":"10.3397/no_2023_0083","title":"Numerical Simulation of Aeroacoustics Generated by Flow around 30P30N High-lift Aerofoil using Hybrid CFD/BEM approach","year":2023,"lang":"en","type":"article","venue":"NOISE-CON proceedings","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Cybernet Systems Corporation (Canada)","funders":"","keywords":"Airfoil; Computational fluid dynamics; Physics; Acoustics; Boundary element method; Aeroacoustics; Lift (data mining); Mechanics; Angle of attack; Finite element method; Sound pressure; Aerodynamics; Computer science","score_opus":0.015921587950418276,"score_gpt":0.22693624700804974,"score_spread":0.21101465905763145,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4388537262","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8279858,0.00006901757,0.16932248,0.000016991029,0.0006076699,0.00027930058,0.00014016425,0.0006780188,0.00090051536],"genre_scores_gemma":[0.98690724,0.00005280887,0.011993134,0.00003764206,0.0003717786,0.0000232569,0.00025965637,0.00016276455,0.00019170277],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99784046,0.00000894145,0.00062790664,0.0004645001,0.0004533908,0.00060481677],"domain_scores_gemma":[0.99907094,0.000079623926,0.00015182614,0.00019393173,0.00033919746,0.00016445213],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0003089556,0.0004013253,0.00048880687,0.00020570363,0.00015634227,0.00012215949,0.0003026838,0.00022922225,0.000023013266],"category_scores_gemma":[0.00013128102,0.0004352006,0.00010202569,0.0008906087,0.00008143453,0.00025667742,0.000079810765,0.00039053935,0.000029420176],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000014286537,0.000045437944,0.00022895838,0.00026863746,0.000060724717,0.0000025396323,0.00014066418,0.8541697,0.14049008,0.00012649107,0.0038161648,0.0006362927],"study_design_scores_gemma":[0.00047776435,0.00004101863,0.00011673484,0.000045350418,0.00008980759,0.000007284066,0.00013315293,0.99060005,0.007459174,0.00022953632,0.00034863796,0.0004514843],"about_ca_topic_score_codex":0.00002430925,"about_ca_topic_score_gemma":2.97493e-7,"teacher_disagreement_score":0.15892142,"about_ca_system_score_codex":0.00017957321,"about_ca_system_score_gemma":0.000036161007,"threshold_uncertainty_score":0.99981},"labels":[],"label_agreement":null},{"id":"W4388764480","doi":"10.1038/s41598-023-47469-y","title":"Mitigation of PWR fuel assembly vibrations using bio-inspired nozzles","year":2023,"lang":"en","type":"article","venue":"Scientific Reports","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Polytechnique Montréal","funders":"Framatome; Natural Sciences and Engineering Research Council of Canada","keywords":"Nozzle; Jet (fluid); Mixing (physics); Flow (mathematics); Materials science; Volumetric flow rate; Rod; Mechanics; Mechanical engineering; Engineering; Physics","score_opus":0.01665444841498278,"score_gpt":0.24326410933867187,"score_spread":0.2266096609236891,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4388764480","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97402215,0.000050041723,0.017016737,0.00001999403,0.0068736337,0.00012344541,0.000011221169,0.0002903199,0.0015924689],"genre_scores_gemma":[0.9963863,0.000007687728,0.003046289,0.0000023003017,0.000058453326,0.000005479511,0.000109724344,0.000021826057,0.00036195357],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9988797,0.0000085038955,0.00039248038,0.000243421,0.00028512735,0.00019080914],"domain_scores_gemma":[0.9992993,0.000023080509,0.00010017767,0.0004145911,0.00011140243,0.000051477546],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00050163467,0.00009050174,0.00011778876,0.00021828602,0.00014423259,0.000111152745,0.0000769683,0.000056819936,0.000019762594],"category_scores_gemma":[0.000086072316,0.000094734016,0.000058922342,0.0008635304,0.00009115186,0.000149092,0.000036029425,0.000058454618,0.000016258606],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[2.6773174e-7,0.0000103165985,0.00075549126,0.00007502566,0.00001386932,0.000047985763,0.0001767697,0.2988669,0.69661295,0.00026025748,0.0026991996,0.00048096542],"study_design_scores_gemma":[0.000040126328,0.0000046635923,0.0019248085,0.000049483468,0.00001983587,0.00002156477,0.00008943368,0.9499724,0.040137645,0.0063719475,0.0012213715,0.00014675126],"about_ca_topic_score_codex":0.0000065697354,"about_ca_topic_score_gemma":0.000023996363,"teacher_disagreement_score":0.6564753,"about_ca_system_score_codex":0.000036140318,"about_ca_system_score_gemma":0.000050157963,"threshold_uncertainty_score":0.3863141},"labels":[],"label_agreement":null},{"id":"W4388901689","doi":"10.5772/intechopen.1002433","title":"Early Advancements in Turbulence-Generated Noise Modelling: A Review","year":2023,"lang":"en","type":"review","venue":"IntechOpen eBooks","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of British Columbia","funders":"","keywords":"Turbulence; Reynolds-averaged Navier–Stokes equations; Noise (video); Airfoil; Physics; Computational fluid dynamics; Turbulence kinetic energy; K-epsilon turbulence model; Acoustics; Statistical physics; Aerospace engineering; Mechanics; Computer science; Engineering","score_opus":0.07334432012929439,"score_gpt":0.3169120242706677,"score_spread":0.24356770414137335,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4388901689","genre_codex":"review","genre_gemma":"review","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"review","genre_consensus":"review","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0000044887547,0.98138845,0.005803936,0.0000021351723,0.00073678116,0.0016984964,0.00014663785,0.00038473774,0.009834354],"genre_scores_gemma":[0.000017719578,0.9954642,0.00073738146,0.000037331676,0.00010942308,0.000709988,0.00012976918,0.00025625227,0.0025379187],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9975539,0.00005378884,0.0011377071,0.00049151055,0.0002633195,0.0004997947],"domain_scores_gemma":[0.9989403,0.000071274124,0.00015412527,0.0006650001,0.000064683416,0.000104648854],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0003579758,0.0006222993,0.0017245162,0.0002916437,0.000037347647,0.00007102479,0.00082077715,0.0003355672,0.000032479744],"category_scores_gemma":[0.00003903211,0.00056909985,0.00030039388,0.00036437684,0.000035834863,0.00005667671,0.00019864677,0.0010313982,0.0005573491],"study_design_candidate":"design_other","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000013394964,0.000015353284,1.3029388e-7,0.0647756,0.00016277032,0.00013278173,0.00003549608,0.019962855,0.0000024840847,0.00013821023,0.0007907802,0.9139822],"study_design_scores_gemma":[0.00009463938,0.000014940732,1.8675722e-8,0.17271566,0.00017858103,0.0000064530386,0.0000020938503,0.06231151,0.0000012737501,0.00019341058,0.7638706,0.0006108456],"about_ca_topic_score_codex":0.000030168947,"about_ca_topic_score_gemma":0.000023018787,"teacher_disagreement_score":0.9133714,"about_ca_system_score_codex":0.000285512,"about_ca_system_score_gemma":0.000096427255,"threshold_uncertainty_score":0.99967605},"labels":[],"label_agreement":null},{"id":"W4389273272","doi":"10.3397/in_2023_0302","title":"Producing a High Level Harmonic Acoustic Pressure Field with Harmonic Acoustic Pneumatic Source (HAPS): Experimental Validation of the Harmonic Distortion Reduction","year":2023,"lang":"en","type":"article","venue":"NOISE-CON proceedings","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Acoustics; Harmonics; Harmonic; Sound pressure; Anechoic chamber; Distortion (music); Total harmonic distortion; Noise (video); Phase distortion; Physics; Electrical engineering; Phase (matter); Engineering; Voltage; Computer science; Amplifier","score_opus":0.015081081276583428,"score_gpt":0.2174869158655053,"score_spread":0.2024058345889219,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4389273272","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98965615,0.00021416631,0.0073129116,0.00018757458,0.0009939978,0.0008814252,0.000026354404,0.0005963309,0.00013109352],"genre_scores_gemma":[0.99800426,0.00006391238,0.0003323356,0.000021273474,0.00023924728,0.0002176836,0.000029631192,0.00013113195,0.00096053194],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9978584,0.000015998277,0.00055989256,0.0005277568,0.0005271863,0.000510764],"domain_scores_gemma":[0.99902177,0.00006217809,0.00027779135,0.00034591922,0.0002005968,0.00009174316],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00034516217,0.0003894679,0.0003636713,0.00018348698,0.00028725056,0.00011912084,0.00040424624,0.00019338299,0.000054059186],"category_scores_gemma":[0.00015705849,0.0003230388,0.00011477691,0.00075545884,0.00010263694,0.00040456772,0.00012276713,0.0005040077,0.000023361205],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000050829814,0.00006381883,0.00034680113,0.00087852974,0.00011933416,0.0000011187177,0.0032172767,0.16781187,0.8247601,0.000037302783,0.0020537009,0.00065935304],"study_design_scores_gemma":[0.0008259931,0.0002516957,0.0063628983,0.00064191595,0.0004636429,0.000048085847,0.001541935,0.31577066,0.6731933,0.00021696194,0.00008403063,0.00059887517],"about_ca_topic_score_codex":0.000055203407,"about_ca_topic_score_gemma":0.0000054793372,"teacher_disagreement_score":0.15156676,"about_ca_system_score_codex":0.00024532198,"about_ca_system_score_gemma":0.00006672303,"threshold_uncertainty_score":0.99992216},"labels":[],"label_agreement":null},{"id":"W4389540952","doi":"10.17118/11143/20978","title":"A comparison of single-time and spectral linear stochastic field pressureestimation in the flow over a backward-facing step","year":2023,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of New Brunswick","funders":"","keywords":"Estimation; Computer science; Flow (mathematics); Stochastic process; Field (mathematics); Algorithm; Mathematics; Statistics; Engineering; Geometry","score_opus":0.017590549787610932,"score_gpt":0.26429718038485417,"score_spread":0.24670663059724324,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4389540952","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.83213896,0.000048844453,0.16614068,0.00005717766,0.0001069558,0.00016474247,0.000010820698,0.00010763177,0.0012242296],"genre_scores_gemma":[0.99439764,0.0000032127152,0.0054589007,0.000012746964,0.000040307656,0.000004193426,0.0000101572205,0.000012233449,0.000060580864],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99945235,0.000012224841,0.00018686985,0.000086583415,0.00012265219,0.0001393119],"domain_scores_gemma":[0.9995843,0.0002496158,0.000018994628,0.00011818564,0.000011319975,0.000017549437],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000148535,0.00008371379,0.00014659972,0.000062466774,0.000022147422,0.000020804935,0.000081681246,0.00005078428,0.000041708015],"category_scores_gemma":[0.0000604636,0.00006608606,0.00002102265,0.00017184789,0.000015577456,0.000046575125,0.00002561106,0.00012577136,0.000010887604],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000043390282,0.00001696421,0.00031019212,0.00004933126,0.000010701696,0.0000016893118,0.00062552525,0.98998916,0.0063667344,0.00010176187,0.0008128358,0.0017107843],"study_design_scores_gemma":[0.00015049712,0.000040108094,0.0026874635,0.00003931382,0.000012772688,0.0000011272048,0.00009539398,0.9965039,0.00025765115,0.000118521326,0.000017596049,0.00007564791],"about_ca_topic_score_codex":0.00002000457,"about_ca_topic_score_gemma":0.00008028994,"teacher_disagreement_score":0.16225874,"about_ca_system_score_codex":0.000011412555,"about_ca_system_score_gemma":0.000003821498,"threshold_uncertainty_score":0.26949114},"labels":[],"label_agreement":null},{"id":"W4389541022","doi":"10.17118/11143/20960","title":"An experimental study of buoyant jets : effects ofviscoplasticity","year":2023,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université Laval","funders":"","keywords":"Viscoplasticity; Physics; Mechanics; Computer science; Finite element method; Thermodynamics","score_opus":0.00862575477340989,"score_gpt":0.2543108481988776,"score_spread":0.24568509342546774,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4389541022","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9937505,0.000012132434,0.0038197592,8.872885e-7,0.00044217237,0.00019111123,0.000004141202,0.00038054126,0.0013987387],"genre_scores_gemma":[0.99957174,0.000003148128,0.0002942244,0.0000033478589,0.000037796202,0.0000174067,0.000004796103,0.000024821542,0.00004272625],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99944323,0.000012597149,0.00013655631,0.00011476369,0.00013793114,0.00015494101],"domain_scores_gemma":[0.9996755,0.000060906645,0.00001090585,0.00018660679,0.000013164992,0.0000529305],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0000669902,0.000098164084,0.00014094656,0.000060144655,0.00002907773,0.00001158368,0.0001138515,0.000030409674,0.00003755753],"category_scores_gemma":[0.000010178199,0.00008860856,0.000019236182,0.00016129565,0.000012869624,0.000045274523,0.000037679332,0.0000633166,0.00003054322],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000012222932,0.00096162024,0.0017837022,0.00010176641,0.00006578814,0.00005009307,0.0018683195,0.57051265,0.42290375,0.0004951798,0.00070991303,0.00053501566],"study_design_scores_gemma":[0.00045767587,0.0008016161,0.006576954,0.000011214209,0.000012828591,7.5186824e-7,0.0014478642,0.9489132,0.04159534,0.000034029585,0.0000071725985,0.00014134125],"about_ca_topic_score_codex":0.000018410652,"about_ca_topic_score_gemma":0.000029340488,"teacher_disagreement_score":0.3813084,"about_ca_system_score_codex":0.000018344357,"about_ca_system_score_gemma":0.0000034788463,"threshold_uncertainty_score":0.36133522},"labels":[],"label_agreement":null},{"id":"W4389541074","doi":"10.17118/11143/20856","title":"Aeroacoustic investigation of a ducted tail rotor using theLattice-Boltzmann Method","year":2023,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Alliance de recherche numérique du Canada; Natural Sciences and Engineering Research Council of Canada; Mitacs","keywords":"Lattice Boltzmann methods; Rotor (electric); Physics; Computer science; Acoustics; Aerospace engineering; Mechanics; Engineering","score_opus":0.026873572146712058,"score_gpt":0.265735571812052,"score_spread":0.23886199966533994,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4389541074","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6035584,0.00002492988,0.3942924,0.000021441114,0.00037434138,0.00016743022,0.000016490616,0.00045596773,0.0010885578],"genre_scores_gemma":[0.8979217,0.000017074892,0.101551495,0.000019943436,0.00009117108,0.000012053268,0.000021931664,0.000049568644,0.00031506235],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99914294,0.000028704946,0.00028111826,0.00014723581,0.00017477927,0.00022523834],"domain_scores_gemma":[0.9994064,0.00018288798,0.000041838706,0.00022757282,0.00007521875,0.00006607857],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00030746404,0.00013693875,0.0001849267,0.00015481355,0.000047147325,0.000019265259,0.00012931658,0.00009341251,0.00007197791],"category_scores_gemma":[0.00011186678,0.00013093253,0.000050449213,0.00060096383,0.00003747152,0.00008186154,0.00004581583,0.0001331676,0.000037249156],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000013991869,0.0000032629805,0.0001699641,0.000104142506,0.000034994075,0.0000031706518,0.0001648165,0.75048125,0.24727257,0.0009851301,0.00030179205,0.00047752602],"study_design_scores_gemma":[0.0001334748,0.000011177933,0.0010631484,0.00003344479,0.000048118614,0.0000025154548,0.00013941976,0.99188435,0.004567623,0.0019289088,0.000039097253,0.00014869976],"about_ca_topic_score_codex":0.000027882581,"about_ca_topic_score_gemma":0.000007935357,"teacher_disagreement_score":0.29436326,"about_ca_system_score_codex":0.00004709086,"about_ca_system_score_gemma":0.000024431141,"threshold_uncertainty_score":0.5339274},"labels":[],"label_agreement":null},{"id":"W4389541103","doi":"10.17118/11143/20855","title":"Investigating the noise sources of the transonic RAE 2822 airfoil","year":2023,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure; Université de Sherbrooke","funders":"Alliance de recherche numérique du Canada","keywords":"Airfoil; Transonic; Noise (video); Computer science; Acoustics; Aerospace engineering; Physics; Artificial intelligence; Engineering; Aerodynamics","score_opus":0.009584807823471968,"score_gpt":0.19598015634010527,"score_spread":0.1863953485166333,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4389541103","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9901913,0.00006130573,0.0014415603,0.0004274284,0.00032602437,0.00008812173,0.0000081992,0.00021794056,0.007238143],"genre_scores_gemma":[0.99876976,0.00004585801,0.0002445631,0.000077649005,0.000059748014,0.0000073595006,0.0000011773732,0.00002211202,0.00077175634],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994618,0.000014805626,0.00015361488,0.000070748996,0.00013773913,0.00016128975],"domain_scores_gemma":[0.9995875,0.000117645584,0.000018922934,0.0002376659,0.000014746814,0.00002355676],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001968478,0.0000813124,0.000082250044,0.000019557398,0.00010027185,0.00001672619,0.00029067096,0.000036911562,0.000049022095],"category_scores_gemma":[0.000044243436,0.000043479715,0.00006644362,0.00031962653,0.00008523259,0.000021995738,0.000043452834,0.00015694754,0.000028725226],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[3.370154e-7,0.0000043323794,0.0017031059,0.00008133872,0.0000341524,6.9493785e-7,0.0013336312,0.9667567,0.019429673,0.0042264443,0.0026328724,0.0037966955],"study_design_scores_gemma":[0.00008726863,0.0000048549414,0.008178013,0.000030717667,0.000016400361,0.0000013524684,0.00045241695,0.9848402,0.003215527,0.0016431008,0.0014422887,0.000087839035],"about_ca_topic_score_codex":0.000022205191,"about_ca_topic_score_gemma":0.00008224232,"teacher_disagreement_score":0.018083498,"about_ca_system_score_codex":0.000010676201,"about_ca_system_score_gemma":0.000011972141,"threshold_uncertainty_score":0.17730513},"labels":[],"label_agreement":null},{"id":"W4389541132","doi":"10.17118/11143/20863","title":"Computational aeroacoustic noise predictions of a 30P30N three-elementhigh-lift device","year":2023,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"Université de Sherbrooke; York University; University of Toronto","funders":"","keywords":"Lift (data mining); Acoustics; Noise (video); Computer science; Aerospace engineering; Physics; Engineering","score_opus":0.012583392705372714,"score_gpt":0.23002216781515974,"score_spread":0.21743877510978704,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4389541132","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.1658981,0.000030316603,0.8259257,0.000070011265,0.00056323357,0.00014996353,0.00014377561,0.0006846978,0.0065342234],"genre_scores_gemma":[0.9898901,0.00002592897,0.009542183,0.00002489271,0.00008405569,0.000020737283,0.00010421453,0.000029706325,0.00027819286],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991993,0.000005400111,0.00025958827,0.00012166543,0.0002172685,0.00019681455],"domain_scores_gemma":[0.99958587,0.00011010546,0.000023787574,0.00014865959,0.000074194526,0.00005740394],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000111329566,0.00010997554,0.00012877003,0.000113875045,0.00006213093,0.000014822379,0.0001224998,0.00005297031,0.00018590229],"category_scores_gemma":[0.000016831355,0.00011040381,0.00004735649,0.00039487774,0.000033697215,0.00005071567,0.000045529832,0.00010665306,0.0001219824],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000011633493,0.000016706254,0.0005649129,0.0000663938,0.000049711194,0.0000024563376,0.00004454856,0.9876748,0.00075754966,0.0052706446,0.0050474056,0.0005037462],"study_design_scores_gemma":[0.00017720606,0.000017487764,0.00867882,0.000019304445,0.00003054157,0.0000015477927,0.00004773586,0.988599,0.00003329728,0.001731782,0.0005551404,0.00010815432],"about_ca_topic_score_codex":0.000012867786,"about_ca_topic_score_gemma":0.00006897268,"teacher_disagreement_score":0.823992,"about_ca_system_score_codex":0.00003263387,"about_ca_system_score_gemma":0.000021410735,"threshold_uncertainty_score":0.45021367},"labels":[],"label_agreement":null},{"id":"W4389541373","doi":"10.17118/11143/20851","title":"Direct numerical simulation of installation effects on self noise of acontrolled diffusion airfoil","year":2023,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure; Université de Sherbrooke","funders":"","keywords":"Airfoil; Noise (video); Diffusion; Computer science; Computer simulation; Simulation; Acoustics; Mechanics; Physics; Artificial intelligence","score_opus":0.004425027724144705,"score_gpt":0.2137932887961732,"score_spread":0.2093682610720285,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4389541373","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9491444,0.00000900048,0.040704686,0.000008294435,0.0002491128,0.00018421681,0.0000055643277,0.0003264008,0.00936833],"genre_scores_gemma":[0.99934524,0.000028319148,0.00043907034,0.0000066469747,0.00004471964,0.00000572797,0.000015972695,0.000022139724,0.00009215907],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993828,0.000018259103,0.00022068151,0.00009457482,0.00017392612,0.00010973876],"domain_scores_gemma":[0.99933606,0.00041985494,0.00004100779,0.000136266,0.000038329414,0.00002847406],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000102586055,0.00009620294,0.0002112067,0.00010936865,0.000020003292,0.000003877277,0.000053537155,0.00006850312,0.000013773789],"category_scores_gemma":[0.00008191628,0.0000834611,0.00006121448,0.0002752559,0.0000067641167,0.00003364649,0.000021348622,0.00005777407,0.0000122243655],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000015819782,0.000028118098,0.00034868286,0.00011442452,0.000023964198,9.624018e-7,0.00007360529,0.93939567,0.0556461,0.00013188951,0.00004892104,0.0041718483],"study_design_scores_gemma":[0.0006105203,0.00007264304,0.010810454,0.00003701761,0.000018153007,5.318408e-8,0.000005846569,0.9829167,0.005323898,0.000074591655,0.00005092901,0.0000791527],"about_ca_topic_score_codex":0.0000062999225,"about_ca_topic_score_gemma":0.0000021946823,"teacher_disagreement_score":0.0503222,"about_ca_system_score_codex":0.000030659587,"about_ca_system_score_gemma":0.0000050959884,"threshold_uncertainty_score":0.3403445},"labels":[],"label_agreement":null},{"id":"W4389541390","doi":"10.17118/11143/20852","title":"Acoustic far-field prediction of a controlled diffusion airfoilself-noise","year":2023,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"National Cancer Institute; Natural Sciences and Engineering Research Council of Canada; National Computational Infrastructure; Alliance de recherche numérique du Canada; Agence Nationale de la Recherche; Australian Government","keywords":"Airfoil; Noise (video); Acoustics; Diffusion; Near and far field; Computer science; Aerospace engineering; Physics; Engineering; Optics; Artificial intelligence","score_opus":0.005986238115003584,"score_gpt":0.19806382783817847,"score_spread":0.19207758972317487,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4389541390","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.76703244,0.00007080829,0.20626403,0.00006774183,0.0012983283,0.0003477421,0.000043262695,0.0012627168,0.023612902],"genre_scores_gemma":[0.997789,0.0003453124,0.00032461397,0.000029653473,0.000087491,0.000026992788,0.000017665763,0.000026718504,0.0013525507],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99925435,0.000008512627,0.00027119255,0.000112554284,0.00016385563,0.0001895631],"domain_scores_gemma":[0.9995296,0.00016663504,0.000026408625,0.00018611204,0.00004159574,0.000049635448],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00013737632,0.00011378766,0.00022738904,0.000112843794,0.00003785839,0.00001154255,0.000099762765,0.000097559685,0.0001145969],"category_scores_gemma":[0.00010250664,0.00009733295,0.00007983925,0.0002413768,0.000012991059,0.00004069547,0.0000380365,0.00011564887,0.00004321357],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000743943,0.000057270725,0.0008269568,0.00019844135,0.00011373913,0.000011617686,0.000158821,0.6508809,0.32550052,0.0012161172,0.016109044,0.004852196],"study_design_scores_gemma":[0.0012446337,0.000054551747,0.0015089107,0.000022017257,0.000039946735,0.00000117581,0.000072804745,0.99572194,0.00067670655,0.00029634486,0.00027684766,0.00008411201],"about_ca_topic_score_codex":0.000009464214,"about_ca_topic_score_gemma":0.000016391581,"teacher_disagreement_score":0.34484106,"about_ca_system_score_codex":0.000022683429,"about_ca_system_score_gemma":0.0000084587045,"threshold_uncertainty_score":0.39691228},"labels":[],"label_agreement":null},{"id":"W4389584823","doi":"10.17118/11143/20884","title":"Near-field aero-acoustic shape optimization at low Reynoldsnumber","year":2023,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Concordia University","funders":"","keywords":"Reynolds number; Acoustics; Field (mathematics); Shape optimization; Computer science; Mechanics; Physics; Engineering; Mathematics; Structural engineering; Finite element method; Turbulence","score_opus":0.006534664454600245,"score_gpt":0.20611738739551838,"score_spread":0.19958272294091814,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4389584823","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.78789234,0.00005537783,0.18109731,0.00021541798,0.0018848539,0.00023624959,0.000019307516,0.0025746834,0.026024453],"genre_scores_gemma":[0.98826605,0.00024626288,0.006418632,0.00022079481,0.00016952248,0.000018034196,0.00006074394,0.00007154734,0.004528416],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991911,0.0000057213156,0.00018145081,0.00017122724,0.00015105431,0.00029945053],"domain_scores_gemma":[0.9995526,0.00009029928,0.000014908132,0.00023905301,0.000029201494,0.00007391089],"candidate_categories":["insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.00007908372,0.00014377938,0.00012427599,0.00004652972,0.00010784679,0.00005942131,0.00012853202,0.00012239642,0.0019764209],"category_scores_gemma":[0.000053397944,0.00014436012,0.000045961315,0.0002815399,0.00001888818,0.000096807016,0.000086451764,0.00012539989,0.0008882462],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000023468983,0.0000049688674,0.000081920356,0.000037518585,0.000013247609,0.000012987287,0.000034658013,0.9667849,0.0022683167,0.00021365816,0.029646581,0.0008989253],"study_design_scores_gemma":[0.000117898184,0.00001352988,0.00014703869,0.000015904185,0.0000114511395,0.0000031957309,0.00001952334,0.9982644,0.0002739984,0.000075347794,0.00086977944,0.00018795328],"about_ca_topic_score_codex":0.00000613161,"about_ca_topic_score_gemma":0.000019185938,"teacher_disagreement_score":0.20037371,"about_ca_system_score_codex":0.00006627199,"about_ca_system_score_gemma":0.000008931911,"threshold_uncertainty_score":0.9998897},"labels":[],"label_agreement":null},{"id":"W4389584831","doi":"10.17118/11143/20893","title":"Large Eddy Simulation of self-excited diametral acoustic mode inrectangular cavities","year":2023,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Ontario Institute of Technology","funders":"","keywords":"Mode (computer interface); Excited state; Acoustics; Large eddy simulation; Materials science; Mechanics; Physics; Computer science; Atomic physics; Turbulence","score_opus":0.007254754275592657,"score_gpt":0.23852992295705544,"score_spread":0.23127516868146278,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4389584831","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.66744006,0.000029028884,0.32987836,0.000003931201,0.0003162608,0.00009210761,0.00006885647,0.0008151754,0.0013562144],"genre_scores_gemma":[0.9977636,0.000046456393,0.0016753417,0.000012164988,0.00007912202,0.0000071581594,0.00006174416,0.000042008756,0.00031240273],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992456,0.000010067827,0.00020969115,0.00010979112,0.00016463027,0.00026023833],"domain_scores_gemma":[0.9995737,0.00013978843,0.000020670317,0.00017569416,0.000047405505,0.00004275466],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001134089,0.00012160129,0.00016153645,0.00015728157,0.00003883859,0.000015433709,0.00009706603,0.000088035245,0.00006376001],"category_scores_gemma":[0.000048091457,0.000121891826,0.000053842334,0.0004227876,0.000014516339,0.000073063165,0.0000335265,0.00010415425,0.000029743618],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000014153557,0.000016831833,0.00016907766,0.00009024527,0.00003673127,0.0000037141808,0.0004837369,0.9915474,0.006623371,0.0005303853,0.00038623327,0.00011086286],"study_design_scores_gemma":[0.00016216021,0.000014540707,0.0006539777,0.000012158249,0.000025166142,3.533758e-7,0.00030087717,0.9976334,0.00037209014,0.0005531218,0.00013199514,0.00014013896],"about_ca_topic_score_codex":0.000013047981,"about_ca_topic_score_gemma":0.000047712143,"teacher_disagreement_score":0.33032355,"about_ca_system_score_codex":0.000044018012,"about_ca_system_score_gemma":0.000009321773,"threshold_uncertainty_score":0.49706042},"labels":[],"label_agreement":null},{"id":"W4389584912","doi":"10.17118/11143/20871","title":"Wall-resolved large-eddy simulation of supercritical airfoil side-edgenoise","year":2023,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto; Université de Sherbrooke","funders":"École de technologie supérieure","keywords":"Airfoil; Supercritical fluid; Noise (video); Large eddy simulation; Acoustics; Enhanced Data Rates for GSM Evolution; Mechanics; Detached eddy simulation; Eddy current; Physics; Materials science; Computational fluid dynamics; Computer science; Turbulence; Reynolds-averaged Navier–Stokes equations; Telecommunications; Thermodynamics","score_opus":0.012895076020408682,"score_gpt":0.25186200816370635,"score_spread":0.23896693214329767,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4389584912","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7293711,0.000047077618,0.25841188,0.00008799897,0.00044342765,0.00012292303,0.00004023607,0.000739958,0.010735419],"genre_scores_gemma":[0.9981859,0.000039544728,0.0012285435,0.000046670462,0.00007491525,0.0000056160407,0.00004444982,0.000039753853,0.0003346487],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99914986,0.000009621141,0.00024954398,0.00012930788,0.00017198663,0.00028968795],"domain_scores_gemma":[0.99947345,0.00017027077,0.0000039719484,0.00021557936,0.00006638873,0.000070359325],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015802181,0.000115681854,0.00015843107,0.00008523987,0.00003950261,0.0000141447645,0.00011483401,0.00009681279,0.00018662108],"category_scores_gemma":[0.00009180864,0.00011378079,0.00006379607,0.00024951913,0.000024211382,0.00006139983,0.00004774054,0.00011588569,0.00017264971],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000027517174,0.000020893633,0.00017599903,0.00007345021,0.000018937899,0.0000080316595,0.00010060679,0.9792953,0.014644014,0.003880486,0.00113421,0.0006453228],"study_design_scores_gemma":[0.00020732642,0.000015361515,0.0010551759,0.000012946251,0.000014269171,4.1437596e-7,0.00008416576,0.9951204,0.0009012075,0.00071047375,0.0017437506,0.00013447276],"about_ca_topic_score_codex":0.0000071696163,"about_ca_topic_score_gemma":0.00003197091,"teacher_disagreement_score":0.2688148,"about_ca_system_score_codex":0.00002800791,"about_ca_system_score_gemma":0.000009447698,"threshold_uncertainty_score":0.4639846},"labels":[],"label_agreement":null},{"id":"W4390451705","doi":"10.1177/1475472x231225628","title":"Supersonic jet noise and screech tone suppression using cross-wire","year":2023,"lang":"en","type":"article","venue":"International Journal of Aeroacoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Nozzle; Strouhal number; Supersonic speed; Acoustics; Jet (fluid); Physics; Sound pressure; Noise (video); Mach number; Shock (circulatory); Schlieren imaging; Jet noise; Schlieren; Mechanics; Computer science; Turbulence","score_opus":0.01745822576005184,"score_gpt":0.3054249021978505,"score_spread":0.28796667643779866,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4390451705","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9533574,0.00018437742,0.042668976,0.00009070924,0.0031464326,0.000041066105,0.00008263536,0.00006457481,0.0003638273],"genre_scores_gemma":[0.9914131,0.00068684475,0.0070029777,0.00003212918,0.00068685564,5.739777e-7,0.000012699281,0.00003995552,0.00012486201],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9987743,0.000011811657,0.00040297463,0.00010206199,0.00050539075,0.00020347584],"domain_scores_gemma":[0.99917835,0.0001079951,0.00009955453,0.0001019566,0.00040545393,0.00010666549],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002775978,0.00014727157,0.00018349038,0.00018482644,0.00006254728,0.0001443995,0.0003182704,0.000100032616,0.000053586245],"category_scores_gemma":[0.00015245377,0.00013472277,0.00007589654,0.0001430063,0.00006808752,0.00020638554,0.00010309784,0.00030404818,0.000008830866],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000037657104,0.000031138366,0.004606868,0.000042530173,0.00019781145,0.00037508586,0.00019299862,0.8694646,0.118314154,0.00019870554,0.003880176,0.0026582994],"study_design_scores_gemma":[0.00056909537,0.000036864618,0.0060466737,0.0001457082,0.000047209083,0.00031490313,0.00015574774,0.99040294,0.0011477639,0.00044772323,0.00051557395,0.00016977204],"about_ca_topic_score_codex":0.000004237281,"about_ca_topic_score_gemma":0.0000020856469,"teacher_disagreement_score":0.12093839,"about_ca_system_score_codex":0.00011937015,"about_ca_system_score_gemma":0.000040141163,"threshold_uncertainty_score":0.54938346},"labels":[],"label_agreement":null},{"id":"W4390986271","doi":"10.2514/1.j063328","title":"Multispecies Flow Indirect-Noise Modeling Re-Examined with a Helicopter-Engine Application","year":2024,"lang":"en","type":"article","venue":"AIAA Journal","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Nozzle; Isentropic process; Noise (video); Large eddy simulation; Statistical physics; Mechanics; Jet engine; Acoustics; Physics; Turbulence; Computer science; Thermodynamics","score_opus":0.008147004943530997,"score_gpt":0.20197708763407066,"score_spread":0.19383008269053967,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4390986271","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.18562669,0.0013572776,0.81053096,0.00011830858,0.00051047717,0.00009507868,0.0000127272,0.00029987856,0.0014485972],"genre_scores_gemma":[0.9734252,0.0005619845,0.025080163,0.000023170041,0.0006614519,0.000015909267,0.0000123496,0.00006804198,0.00015172415],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99910486,0.000009705316,0.0002494029,0.00015950992,0.00021635511,0.0002601497],"domain_scores_gemma":[0.9996035,0.00003952795,0.000021301947,0.00016713195,0.00006132372,0.0001071863],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018641421,0.00017930756,0.0001602926,0.00015335908,0.00010752923,0.00022433395,0.00015190835,0.00007285206,0.000058082074],"category_scores_gemma":[0.000012952334,0.00014691587,0.00005537976,0.00022130544,0.000017668774,0.00018387212,0.000021058071,0.00050697004,0.000045923214],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000066254474,0.000010287313,0.00002397924,0.00005521172,0.00007154776,0.000050574854,0.0002867285,0.95675373,0.0047739423,0.00009721812,0.00043154077,0.037438627],"study_design_scores_gemma":[0.00018964813,0.000033627377,0.00006295907,0.000156805,0.000039035174,0.00016059174,0.00006822971,0.99662673,0.00022421476,0.00035129365,0.0018881535,0.00019870412],"about_ca_topic_score_codex":0.0000033982867,"about_ca_topic_score_gemma":0.000019683926,"teacher_disagreement_score":0.7877985,"about_ca_system_score_codex":0.00012229937,"about_ca_system_score_gemma":0.0000262895,"threshold_uncertainty_score":0.59910554},"labels":[],"label_agreement":null},{"id":"W4390989582","doi":"10.2139/ssrn.4699082","title":"Characterisation of Noise Sources in Two- and Three-Element High-Lift Airfoil Configurations","year":2024,"lang":"en","type":"preprint","venue":"SSRN Electronic Journal","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke; University of Toronto","funders":"","keywords":"Cove; Airfoil; Acoustics; Wind tunnel; Lift (data mining); Aerodynamics; Angle of attack; Noise (video); Anechoic chamber; Sound pressure; Geology; Mechanics; Physics; Computer science","score_opus":0.004951086800101975,"score_gpt":0.22361330188451417,"score_spread":0.2186622150844122,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4390989582","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.96928906,0.0044808495,0.024561735,0.00025037327,0.0008220944,0.0001937102,0.000054975753,0.000051897958,0.00029527477],"genre_scores_gemma":[0.9913159,0.007929827,0.00020828769,0.000007597243,0.0003521366,0.000018866474,0.000048462283,0.00005040715,0.00006850589],"study_design_codex":"simulation_or_modeling","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.99821144,0.000024689964,0.000541312,0.00020497404,0.0002064583,0.0008111472],"domain_scores_gemma":[0.99954766,0.000032267657,0.00014031015,0.00017350989,0.00005747414,0.00004876357],"candidate_categories":["research_integrity"],"consensus_categories":[],"category_scores_codex":[0.000755238,0.00024099539,0.00031918887,0.00024355315,0.000049276376,0.00009353114,0.00018510403,0.00012886163,0.000022174232],"category_scores_gemma":[0.000015922771,0.00023847815,0.00007880943,0.00009118356,0.000036744535,0.000048123457,0.00014069697,0.0031116665,0.000004993232],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000036988145,0.00010793574,0.0027512081,0.00093119,0.0010477477,0.000020042256,0.0014147497,0.67997605,0.019765813,0.23970403,0.000067124,0.054177154],"study_design_scores_gemma":[0.0006363203,0.000093866365,0.0046072323,0.00049777917,0.00018475346,0.0000719771,0.0004662937,0.4363018,0.00029224175,0.55624163,0.00013286623,0.00047325803],"about_ca_topic_score_codex":0.00014206811,"about_ca_topic_score_gemma":0.004333255,"teacher_disagreement_score":0.3165376,"about_ca_system_score_codex":0.00063244876,"about_ca_system_score_gemma":0.00056592084,"threshold_uncertainty_score":0.9991882},"labels":[],"label_agreement":null},{"id":"W4391028430","doi":"10.61782/fa.2023.0652","title":"Nonlinear behaviour of lossy acoustic black holes","year":2024,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université du Québec à Montréal; École de Technologie Supérieure","funders":"Defence Science and Technology Laboratory","keywords":"Lossy compression; Nonlinear system; Acoustics; Computer science; Physics; Artificial intelligence","score_opus":0.0075372874973374335,"score_gpt":0.22614872962805668,"score_spread":0.21861144213071926,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4391028430","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7055305,0.00043373575,0.2794807,0.0000304141,0.0008680677,0.000084095576,0.00009095821,0.0005184718,0.012963038],"genre_scores_gemma":[0.99383,0.00011813637,0.0047382945,0.000008565988,0.00012972976,0.0000019867366,0.000011049917,0.000037755864,0.0011244534],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994868,0.000002513869,0.00016405391,0.00010412243,0.000103562124,0.00013897031],"domain_scores_gemma":[0.9997488,0.000035865727,0.0000059949875,0.00014802211,0.00002322901,0.000038079972],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00005757389,0.000099207085,0.00010939212,0.00005751975,0.000010535239,0.00002923221,0.000100533936,0.00006197155,0.00016981487],"category_scores_gemma":[0.00000836794,0.000087972454,0.000054133056,0.00011944969,0.000079281286,0.00004111318,0.0000257967,0.00013228162,0.000108799846],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000025989416,0.00007237142,0.00051376264,0.0010370746,0.00012597443,0.00010691798,0.00031517592,0.88009447,0.09165743,0.010276701,0.010336003,0.0054614944],"study_design_scores_gemma":[0.000042063548,0.000015964053,0.00012394153,0.000056970457,0.0000370969,0.0000034750653,0.0000531469,0.99663246,0.0020810005,0.00037408381,0.00046499117,0.00011481549],"about_ca_topic_score_codex":0.00000382214,"about_ca_topic_score_gemma":0.000010364182,"teacher_disagreement_score":0.2882995,"about_ca_system_score_codex":0.000021058126,"about_ca_system_score_gemma":0.000012112131,"threshold_uncertainty_score":0.35874125},"labels":[],"label_agreement":null},{"id":"W4391028888","doi":"10.61782/fa.2023.0405","title":"Informed Source Separation for Turbofan Broadband Noise Using Non-Negative Matrix Factorization","year":2024,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Safran Electronics (Canada)","funders":"","keywords":"Non-negative matrix factorization; Broadband; Source separation; Turbofan; Matrix decomposition; Noise (video); Separation (statistics); Computer science; Matrix (chemical analysis); Factorization; Speech recognition; Algorithm; Artificial intelligence; Telecommunications; Engineering; Materials science; Physics; Machine learning","score_opus":0.011270712623693712,"score_gpt":0.290713536768064,"score_spread":0.27944282414437027,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4391028888","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.12964024,0.000038637394,0.867069,0.000009249569,0.0007362236,0.00026650858,0.000031196283,0.00022675113,0.001982223],"genre_scores_gemma":[0.9840634,0.000026101809,0.014224336,0.0000107518335,0.00023986444,0.00001642067,0.00006575314,0.000041140254,0.0013122737],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99944997,0.0000026166172,0.00017864454,0.00011727051,0.00009060949,0.00016086883],"domain_scores_gemma":[0.9996868,0.00012823934,0.000014595029,0.0000863462,0.000044675147,0.00003934626],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000053573065,0.00012507917,0.00009897287,0.0000802562,0.0000634406,0.00014020473,0.000054032178,0.000082303755,0.00003111415],"category_scores_gemma":[0.00003958606,0.00011531011,0.00004792276,0.00015570056,0.000011519767,0.0002332656,0.000012576395,0.000078550445,0.000014690873],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000005234608,0.000004494667,0.000038514845,0.0003139887,0.00004430405,6.614542e-7,0.000809779,0.95652235,0.03829581,0.0011429255,0.0012518639,0.0015700563],"study_design_scores_gemma":[0.00013453673,0.000016052501,0.0000548306,0.00004795416,0.000026443062,0.0000014868954,0.00007725179,0.99180114,0.004440975,0.00058069243,0.002662204,0.00015643665],"about_ca_topic_score_codex":0.000013420183,"about_ca_topic_score_gemma":0.000032415206,"teacher_disagreement_score":0.8544231,"about_ca_system_score_codex":0.00012850584,"about_ca_system_score_gemma":0.00004191553,"threshold_uncertainty_score":0.47022098},"labels":[],"label_agreement":null},{"id":"W4391300476","doi":"10.2514/6.2024-2868","title":"A semi-analytical model for Mach reflection in axisymmetric overexpanded jets.","year":2024,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"","keywords":"Reflection (computer programming); Rotational symmetry; Mach reflection; Physics; Mach number; Mechanics; Optics; Computer science; Mach wave","score_opus":0.026400811303870567,"score_gpt":0.29001916288203067,"score_spread":0.2636183515781601,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4391300476","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.032565642,0.00022021196,0.9395386,0.000060395803,0.00037311026,0.00016125542,0.000019127187,0.0003431785,0.026718473],"genre_scores_gemma":[0.99095696,0.000061241546,0.0052754297,0.000029829378,0.000075415264,0.000032368152,0.000012812147,0.000036057823,0.0035198939],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99934554,0.0000030851033,0.00018134643,0.00016824796,0.00009477811,0.00020699025],"domain_scores_gemma":[0.99974984,0.00008123551,0.000004122137,0.00010757409,0.000016743152,0.000040499282],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001390219,0.000103462815,0.000121619814,0.00025378226,0.000017445189,0.000055796532,0.00006393596,0.00009387018,0.000032736112],"category_scores_gemma":[0.00003440251,0.00009531111,0.000067383815,0.00047117492,0.0000073473684,0.00006377181,0.000015696573,0.00016369305,0.000015600011],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000053755393,0.000015932048,0.00002153739,0.0001450008,0.000033731645,0.0000048214183,0.000057415793,0.9515139,0.0013133119,0.036857698,0.0044589485,0.0055723256],"study_design_scores_gemma":[0.0001317419,0.000013084632,0.000019648885,0.000019327086,0.000018909543,0.0000027921778,0.000009847607,0.9901574,0.00007021717,0.008833745,0.00059973425,0.00012352312],"about_ca_topic_score_codex":0.0000077503555,"about_ca_topic_score_gemma":0.00005934729,"teacher_disagreement_score":0.9583913,"about_ca_system_score_codex":0.00016445384,"about_ca_system_score_gemma":0.000017339506,"threshold_uncertainty_score":0.38866743},"labels":[],"label_agreement":null},{"id":"W4391325177","doi":"10.2514/6.2024-1485","title":"Effect of struts and central tower on aerodynamics and aeroacoustics of vertical axis wind turbines using mid-fidelity and high-fidelity methods","year":2024,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"European Commission; Trent University; Nottingham Trent University","keywords":"Aerodynamics; Aeroacoustics; Wind power; Vertical axis; Tower; Fidelity; Computational aeroacoustics; Aerospace engineering; Horizontal axis; Tower crane; Computer science; Marine engineering; Acoustics; Engineering; Structural engineering; Physics; Electrical engineering; Engineering drawing; Telecommunications","score_opus":0.008788396518915638,"score_gpt":0.28452285160390667,"score_spread":0.275734455084991,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4391325177","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.88735574,0.00080306234,0.1108556,0.000013282032,0.0005270798,0.00016975864,0.00007796386,0.00006927893,0.00012824804],"genre_scores_gemma":[0.96907777,0.00030025432,0.030504985,0.00000883228,0.000055307508,0.0000011019403,0.0000070582305,0.0000353698,0.000009325641],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9986903,0.000087797525,0.0004348004,0.00032049508,0.00017727847,0.00028929676],"domain_scores_gemma":[0.99872285,0.00083655136,0.000024029585,0.00022507289,0.000055052868,0.0001364423],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00057285524,0.00026972478,0.00047272508,0.000085660904,0.000040664643,0.000052139083,0.00007159729,0.0001788036,0.00001527929],"category_scores_gemma":[0.00022050439,0.00022166058,0.000051238472,0.000139512,0.00021382119,0.000085730964,0.0001078232,0.0002611773,1.2916405e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00028949772,0.000109380904,0.0063349055,0.007749147,0.00062742486,0.000042627213,0.00048647806,0.30411303,0.59316814,0.008284878,0.000118476106,0.07867602],"study_design_scores_gemma":[0.0003133915,0.00022262546,0.009078648,0.00016646532,0.00020872854,0.000010621543,0.000023266788,0.9797225,0.009310681,0.0007257948,0.000007859322,0.00020939206],"about_ca_topic_score_codex":0.00008797261,"about_ca_topic_score_gemma":0.00001979162,"teacher_disagreement_score":0.6756095,"about_ca_system_score_codex":0.000054415854,"about_ca_system_score_gemma":0.000018423063,"threshold_uncertainty_score":0.90390563},"labels":[],"label_agreement":null},{"id":"W4391388868","doi":"10.61782/fa.2023.0428","title":"Noise Estimation Framework for Advanced Air Mobility","year":2024,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Miller Group (Canada)","funders":"Nuclear Safety and Security Commission; National Aeronautics and Space Administration","keywords":"Computer science; Noise (video); Estimation; Acoustics; Artificial intelligence; Engineering; Physics; Systems engineering","score_opus":0.0062413246347460555,"score_gpt":0.2550865247045084,"score_spread":0.24884520006976232,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4391388868","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.03979281,0.00019756741,0.95641774,0.00007201157,0.0007819464,0.00017812896,0.000022294838,0.00066936424,0.0018681608],"genre_scores_gemma":[0.7271348,0.000016775475,0.27253503,0.000021293805,0.000061495615,0.000045897952,0.000010830957,0.000019491077,0.00015437957],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99962205,0.0000014927342,0.00010218471,0.00011116361,0.000049104732,0.00011400238],"domain_scores_gemma":[0.9996757,0.00014346796,0.0000035117982,0.00013333125,0.000016254284,0.00002772475],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0000672075,0.00007319751,0.00006487149,0.000021876634,0.000024000567,0.0000250517,0.000053302847,0.000060551876,0.000047335496],"category_scores_gemma":[0.00005739768,0.00006690062,0.000040541905,0.000076277276,0.000009334126,0.00007075925,0.000009378428,0.000094785195,0.000031963733],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000016661498,0.000006321754,0.0000027128724,0.00023278751,0.000009971662,6.6257405e-7,0.00003410657,0.8765875,0.00087651185,0.08093687,0.0006195621,0.040691286],"study_design_scores_gemma":[0.000032031414,0.0000098044475,0.000054225635,0.000053469037,0.000006578015,4.248881e-7,0.000010094306,0.9212304,0.00044671615,0.07640012,0.0016747322,0.00008142199],"about_ca_topic_score_codex":6.9161706e-7,"about_ca_topic_score_gemma":0.0000022560155,"teacher_disagreement_score":0.687342,"about_ca_system_score_codex":0.000044780216,"about_ca_system_score_gemma":0.0000065429563,"threshold_uncertainty_score":0.27281278},"labels":[],"label_agreement":null},{"id":"W4391440875","doi":"10.1051/aacus/2023062","title":"Experimental and numerical observation of flow-acoustics feedback phenomena due to two diaphragms in tandem inserted in a rectangular duct","year":2024,"lang":"en","type":"article","venue":"Acta Acustica","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Simon Fraser University; University of Toronto; Compute Canada","keywords":"Duct (anatomy); Acoustics; Tandem; Flow (mathematics); Mechanics; Computer science; Materials science; Physics; Engineering; Aerospace engineering; Anatomy","score_opus":0.010707649237066418,"score_gpt":0.23986021296293436,"score_spread":0.22915256372586795,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4391440875","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.960888,0.0005454159,0.037119973,0.00009267698,0.0004610584,0.00024522148,0.000025970645,0.00010080063,0.00052088196],"genre_scores_gemma":[0.99049795,0.000043992466,0.009177215,0.00004609209,0.00011281695,0.000033147106,0.000021323181,0.00005087612,0.000016580338],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989078,0.000021670468,0.00036695073,0.00025651054,0.00016279485,0.00028425624],"domain_scores_gemma":[0.999546,0.00014691037,0.000016947095,0.00017741843,0.000021717931,0.00009101055],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015062514,0.00019493458,0.00029662397,0.00018983126,0.000018964638,0.00004509423,0.00012581075,0.00009041763,0.00003726041],"category_scores_gemma":[0.00011286463,0.00019915585,0.000029104156,0.00061480503,0.0000338774,0.000109592635,0.00007422032,0.00024505498,0.000006348549],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00003408668,0.00015177888,0.0011850877,0.0002547339,0.000062160114,0.00025130852,0.003104688,0.12631156,0.85976315,0.0010187187,0.00058016606,0.0072825598],"study_design_scores_gemma":[0.00034136465,0.00005952118,0.011706348,0.00016687273,0.000020834856,0.00001102228,0.00029069307,0.98529106,0.0014364368,0.00023137215,0.0002085259,0.00023595976],"about_ca_topic_score_codex":0.000036851696,"about_ca_topic_score_gemma":0.000013395512,"teacher_disagreement_score":0.85897946,"about_ca_system_score_codex":0.00018118996,"about_ca_system_score_gemma":0.000026557907,"threshold_uncertainty_score":0.81213397},"labels":[],"label_agreement":null},{"id":"W4391734097","doi":"10.1121/10.0024751","title":"Acoustic pressure modulation driven by spatially non-uniform flow","year":2024,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Polytechnique Montréal","funders":"","keywords":"Acoustics; Acoustic wave; Sound pressure; Acoustic wave equation; Modulation (music); Physics; Flow (mathematics); Particle velocity; Ion acoustic wave; Mechanics","score_opus":0.004639931647006502,"score_gpt":0.21032399803349985,"score_spread":0.20568406638649336,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4391734097","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0070162606,0.0006976833,0.9901132,0.00088386016,0.0007962905,0.00013051105,0.0000684771,0.00004232174,0.00025141734],"genre_scores_gemma":[0.9655011,0.0009473709,0.032825194,0.0001593742,0.0003604193,0.0000012329921,0.0000020281368,0.00004266752,0.00016061256],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9986989,0.000034654535,0.00044998358,0.00008495877,0.00048983784,0.00024166403],"domain_scores_gemma":[0.9990766,0.00035275248,0.00013454068,0.00023647601,0.00012371597,0.00007589205],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00034189952,0.00017641422,0.0002822346,0.000018412124,0.000116623574,0.000042291766,0.00058577536,0.000106529886,0.00005735365],"category_scores_gemma":[0.00007207177,0.00009921648,0.00034813947,0.0002565861,0.00026442282,0.00010390388,0.000106971915,0.00068152114,0.0000055525666],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000009880433,0.000022478882,0.0000069746156,0.00014363724,0.00027573592,8.806195e-7,0.00038532357,0.89116734,0.05210914,0.0000026092362,0.04824238,0.007633599],"study_design_scores_gemma":[0.000119646065,0.00008111164,0.0001553208,0.00014359184,0.00047148633,0.000021872595,0.00013709212,0.99599135,0.00022761368,0.00042434255,0.002109881,0.00011666399],"about_ca_topic_score_codex":0.000009265531,"about_ca_topic_score_gemma":9.129088e-7,"teacher_disagreement_score":0.9584848,"about_ca_system_score_codex":0.000076503566,"about_ca_system_score_gemma":0.000058110847,"threshold_uncertainty_score":0.40459305},"labels":[],"label_agreement":null},{"id":"W4392649179","doi":"10.1063/5.0190336","title":"Investigation of pulsed direct-current plasma jets in a turbulent boundary layer","year":2024,"lang":"en","type":"article","venue":"Physics of Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"National Key Research and Development Program of China; National Science and Technology Major Project; National Natural Science Foundation of China; University of Guelph","keywords":"Physics; Boundary layer; Turbulence; Plasma; Mechanics; Current (fluid); Jet (fluid); Nuclear physics; Thermodynamics","score_opus":0.01839095368546618,"score_gpt":0.23925630087800184,"score_spread":0.22086534719253567,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4392649179","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98819447,0.0018538055,0.0075536137,0.00005069111,0.000676644,0.00011954151,0.00004928865,0.00009395475,0.0014079985],"genre_scores_gemma":[0.99915445,0.00023117271,0.0003960331,0.00000381465,0.00013708678,0.000010940113,0.000026697817,0.000027494581,0.000012313264],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993179,0.0000101310925,0.0002507691,0.0001218256,0.00016729654,0.00013211342],"domain_scores_gemma":[0.99971324,0.00005436777,0.000016783057,0.00014840128,0.000034610497,0.000032590968],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00009764941,0.000113350696,0.00017585981,0.00008629589,0.0000106168945,0.00001805422,0.00009793339,0.000039359093,0.000005083697],"category_scores_gemma":[0.0000132572995,0.00011663777,0.000059591355,0.0003089568,0.000052660198,0.00009112244,0.000026744567,0.00015268243,0.0000059640133],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000013205421,0.00008322599,0.00093623035,0.0025169847,0.00012481946,0.000011992523,0.0024778526,0.37128076,0.54515815,0.015351758,0.0016805315,0.060364515],"study_design_scores_gemma":[0.00013084833,0.000020755237,0.0004457324,0.00031515412,0.000016308062,4.807369e-7,0.000008178497,0.94422936,0.043177795,0.010804973,0.0007265367,0.00012388594],"about_ca_topic_score_codex":0.000011046126,"about_ca_topic_score_gemma":0.000004530097,"teacher_disagreement_score":0.5729486,"about_ca_system_score_codex":0.00007145745,"about_ca_system_score_gemma":0.00006100909,"threshold_uncertainty_score":0.47563502},"labels":[],"label_agreement":null},{"id":"W4392764232","doi":"10.3390/ijtpp9010011","title":"Turbomachinery Noise Review","year":2024,"lang":"en","type":"article","venue":"International Journal of Turbomachinery Propulsion and Power","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":22,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Centre National de la Recherche Scientifique; Agence Nationale de la Recherche","keywords":"Turbomachinery; Propulsion; Rotor (electric); Stator; Aerodynamics; Noise (video); Computer science; Emphasis (telecommunications); Aerospace engineering; Jet propulsion; Fidelity; Systems engineering; High fidelity; Engineering; Control engineering; Mechanical engineering; Electrical engineering; Telecommunications","score_opus":0.0039669519690976075,"score_gpt":0.2453018693479876,"score_spread":0.24133491737888998,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4392764232","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.47519338,0.41481006,0.019563615,0.013914089,0.046102114,0.000487182,0.00019752629,0.000519189,0.029212845],"genre_scores_gemma":[0.97365767,0.023567403,0.0010811643,0.0006398654,0.00056392147,0.0000019449724,0.000010149821,0.00003622337,0.0004416531],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.99886525,0.000022837618,0.00047440096,0.00011622258,0.0003993004,0.00012201772],"domain_scores_gemma":[0.99950975,0.000071744675,0.00006547545,0.00009682899,0.00015221024,0.00010396889],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003345153,0.00016712402,0.00021593014,0.0001955004,0.000023378814,0.00011733634,0.00027388087,0.000058726157,0.00027077188],"category_scores_gemma":[0.00008969067,0.00011704863,0.0001479432,0.00009463647,0.000029678116,0.00023859368,0.000057665286,0.00043854225,0.000021472979],"study_design_candidate":"not_applicable","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0001578537,0.00025104455,0.0013388682,0.0033567597,0.0017248691,0.0036897578,0.00065643614,0.015470147,0.041434657,0.0093787955,0.31898984,0.603551],"study_design_scores_gemma":[0.0009241247,0.0002496014,0.0026879772,0.010920742,0.00024688386,0.0040095705,0.00002516491,0.35424086,0.00044393982,0.0068161073,0.61855745,0.0008775694],"about_ca_topic_score_codex":0.0000019733086,"about_ca_topic_score_gemma":6.3286325e-7,"teacher_disagreement_score":0.6026734,"about_ca_system_score_codex":0.000052894375,"about_ca_system_score_gemma":0.000023997944,"threshold_uncertainty_score":0.47731045},"labels":[],"label_agreement":null},{"id":"W4392768580","doi":"10.1063/5.0196818","title":"Effect of turbulent coflows on the dynamics of turbulent twin jets","year":2024,"lang":"en","type":"article","venue":"Physics of Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":9,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"","keywords":"Physics; Turbulence; Mechanics; Dynamics (music); Computational fluid dynamics; Classical mechanics; Statistical physics","score_opus":0.006788296902983471,"score_gpt":0.22757079676050776,"score_spread":0.2207824998575243,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4392768580","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97734267,0.0007234338,0.018710982,0.00015895793,0.00059749524,0.0002961463,0.00012614793,0.00008985931,0.0019543315],"genre_scores_gemma":[0.9994041,0.00015257843,0.0001816946,0.000011389566,0.000116865966,0.000013614277,0.000024192635,0.00005076164,0.00004482956],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99897957,0.0000352537,0.0003335475,0.00015321742,0.0003154989,0.00018289054],"domain_scores_gemma":[0.9989901,0.00045947277,0.000039656254,0.00041986333,0.000057311183,0.000033578417],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003082828,0.0002066329,0.0003372732,0.000048861846,0.000020000114,0.000013200973,0.0002846518,0.00006727425,0.000019838795],"category_scores_gemma":[0.000026812644,0.00014660416,0.0002045097,0.00022522111,0.00009230682,0.000040622694,0.000048217204,0.00023303997,0.000010134962],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00006301852,0.00018590748,0.0000722266,0.0036839035,0.0005715129,0.000016907476,0.00079683313,0.67128295,0.10703181,0.1843884,0.003248988,0.028657578],"study_design_scores_gemma":[0.0001329911,0.00027473574,0.000030484309,0.00032389778,0.000081940205,0.0000013336606,0.000011979542,0.9367453,0.059574675,0.0025708638,0.00012461419,0.00012721906],"about_ca_topic_score_codex":0.000009703975,"about_ca_topic_score_gemma":0.0000014141698,"teacher_disagreement_score":0.26546234,"about_ca_system_score_codex":0.000069987684,"about_ca_system_score_gemma":0.000017863105,"threshold_uncertainty_score":0.59783435},"labels":[],"label_agreement":null},{"id":"W4393323271","doi":"10.1051/e3sconf/202450701067","title":"Acoustic analysis of chevron nozzle: A CFD approach","year":2024,"lang":"en","type":"article","venue":"E3S Web of Conferences","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Horizon College and Seminary","funders":"","keywords":"Chevron (anatomy); Computational fluid dynamics; Nozzle; Mechanical engineering; Engineering; Acoustics; Geology; Aerospace engineering; Physics","score_opus":0.012105900884503395,"score_gpt":0.23009993585360186,"score_spread":0.21799403496909847,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4393323271","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6933392,0.0021590865,0.16467471,0.000022288845,0.00072183984,0.00013983888,0.00018864473,0.0002539219,0.1385004],"genre_scores_gemma":[0.99835956,0.0002450212,0.0011170525,0.000002527501,0.000045087596,0.00000695336,0.00003172275,0.0000139883405,0.00017806959],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99921525,0.000010043215,0.00028673178,0.00015091273,0.00019474384,0.00014232795],"domain_scores_gemma":[0.9995864,0.00009940177,0.000033158278,0.00018662494,0.0000579325,0.000036457794],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001491893,0.00012458646,0.00034263666,0.0003005222,0.00001331296,0.00003098975,0.00019895953,0.00007689361,0.00023478748],"category_scores_gemma":[0.000022628565,0.0001078506,0.0001321286,0.0007025722,0.00008023821,0.00004742247,0.000026732232,0.00012578386,0.0000041679996],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000055666655,0.00006722392,0.0018090489,0.0010971795,0.0028028581,0.000006721717,0.00053998927,0.89961845,0.04178574,0.0406709,0.000860796,0.010735503],"study_design_scores_gemma":[0.00004514975,0.00002023085,0.0020897847,0.00004999823,0.0006749397,5.12255e-7,0.00015568829,0.99540097,0.00046588897,0.00028814754,0.00069548225,0.00011319508],"about_ca_topic_score_codex":0.000020561001,"about_ca_topic_score_gemma":0.000048463284,"teacher_disagreement_score":0.30502033,"about_ca_system_score_codex":0.000014286621,"about_ca_system_score_gemma":0.00014697472,"threshold_uncertainty_score":0.439802},"labels":[],"label_agreement":null},{"id":"W4393347424","doi":"10.2139/ssrn.4778663","title":"Installation Effects on Airfoil Self-Noise Estimated by Direct Numerical Simulations","year":2024,"lang":"en","type":"preprint","venue":"SSRN Electronic Journal","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Airfoil; Noise (video); Acoustics; Computer science; Mechanics; Physics; Artificial intelligence","score_opus":0.004206214191919587,"score_gpt":0.22859664060611146,"score_spread":0.22439042641419188,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4393347424","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8036772,0.015436565,0.15829073,0.0004400056,0.006655146,0.00093254313,0.00025822557,0.002695828,0.011613765],"genre_scores_gemma":[0.9947991,0.0033382187,0.00055366126,0.000025407797,0.0006098171,0.00001704346,0.0001592163,0.0001752051,0.00032236718],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9971725,0.00006436632,0.00044127688,0.0003732283,0.00038407245,0.001564566],"domain_scores_gemma":[0.9992051,0.00018233992,0.000104748746,0.00030724477,0.00007055778,0.00013001398],"candidate_categories":["metaepi_narrow","research_integrity"],"consensus_categories":[],"category_scores_codex":[0.00045579346,0.0004739857,0.0004095692,0.00022594575,0.00016041157,0.00021137513,0.0003045707,0.00039658762,0.000015473053],"category_scores_gemma":[0.000074806856,0.00046315638,0.00021008814,0.00023367246,0.000015580481,0.000052878295,0.00016492432,0.0065907757,0.000078403194],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000100643965,0.000050731105,0.00004715654,0.00019805737,0.00053586304,0.000012882987,0.00006183208,0.98211545,0.000802132,0.0035099213,0.0008855999,0.011770303],"study_design_scores_gemma":[0.00023934418,0.000117822034,0.00005393477,0.0002806056,0.00021872134,0.000037945298,0.000009555264,0.9135733,0.0001297972,0.084300995,0.0005972529,0.00044071928],"about_ca_topic_score_codex":0.000012773284,"about_ca_topic_score_gemma":0.000039520834,"teacher_disagreement_score":0.19112188,"about_ca_system_score_codex":0.0027800088,"about_ca_system_score_gemma":0.0007474607,"threshold_uncertainty_score":0.999782},"labels":[],"label_agreement":null},{"id":"W4393850424","doi":"10.34185/1991-7848.itmm.2023.01.045","title":"COMPUTER SIMULATION OF THE NON-STATIONARY PROCESS OF THE SUPERSONIC OVEREXPANDED JET DEVELOPMENT","year":2024,"lang":"en","type":"article","venue":"International scientific and technical conference Information technologies in metallurgy and machine building","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Mathematics","score_opus":0.009613397190924564,"score_gpt":0.24597334062024503,"score_spread":0.23635994342932048,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4393850424","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6998108,0.000093219925,0.29853636,0.00018500723,0.0005389214,0.00016759276,0.000018864883,0.00010942579,0.00053979777],"genre_scores_gemma":[0.99744165,0.00003413603,0.002480878,0.000005480586,0.0000036603494,0.000010924698,0.000009281561,0.000002802927,0.000011193692],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993008,0.0000057427483,0.0003176454,0.00009066258,0.00021036265,0.000074837095],"domain_scores_gemma":[0.99967664,0.00007591311,0.000057249348,0.00010416762,0.0000783425,0.0000076697],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002685666,0.00007888544,0.00009001897,0.00015436909,0.000072785064,0.00008166395,0.00029877402,0.00007261037,0.000008540555],"category_scores_gemma":[0.00009319303,0.000047872985,0.000026527337,0.00027410465,0.00024669882,0.0003225254,0.00020675223,0.00018263765,3.1080063e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000014284273,0.00004146768,0.004597358,0.00059623056,0.00009611238,7.8928394e-7,0.0013045812,0.48791644,0.010184238,0.16504036,0.000067516354,0.33014065],"study_design_scores_gemma":[0.000079225705,0.0000053679687,0.004711012,0.00019781332,0.0000053237154,0.000003852674,0.00012786768,0.9838274,0.0039996617,0.0062916074,0.0006871073,0.00006375805],"about_ca_topic_score_codex":0.0000030221802,"about_ca_topic_score_gemma":0.000011657156,"teacher_disagreement_score":0.49591097,"about_ca_system_score_codex":0.00003178317,"about_ca_system_score_gemma":0.000035601744,"threshold_uncertainty_score":0.19522037},"labels":[],"label_agreement":null},{"id":"W4395110905","doi":"10.1063/5.0204050","title":"Aeroacoustic investigation of a ducted wind turbine employing bio-inspired airfoil profiles","year":2024,"lang":"en","type":"article","venue":"Physics of Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":11,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lakehead University","funders":"","keywords":"Physics; Airfoil; Turbine; Aerospace engineering; Computational fluid dynamics; Marine engineering; Mechanics; Meteorology; Engineering","score_opus":0.012621005647346655,"score_gpt":0.21872441997481692,"score_spread":0.20610341432747026,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4395110905","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9613693,0.000698901,0.036477547,0.000028907709,0.0005706301,0.00014705118,0.00009493987,0.00027070913,0.000342031],"genre_scores_gemma":[0.9955736,0.00006101714,0.0039503905,0.0000064717888,0.00024545408,0.0000080262935,0.00006432636,0.00005998112,0.000030729083],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9990822,0.000011722479,0.00033714672,0.00017456165,0.00021507505,0.00017925978],"domain_scores_gemma":[0.9994866,0.00008899452,0.000033716373,0.00023705592,0.00010342753,0.00005018929],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00010119052,0.00017377072,0.0002440985,0.00008459371,0.00002753558,0.00002361468,0.0001469564,0.00007147625,0.0000103979555],"category_scores_gemma":[0.00003900151,0.00017483522,0.000084416555,0.00044618966,0.00010539168,0.00013937039,0.000039491177,0.00015902084,0.0000082085235],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000033319889,0.00001935145,0.00034318937,0.0011534574,0.00011042271,0.00000333564,0.00055130816,0.15316969,0.838243,0.0035107036,0.0003416465,0.0025505475],"study_design_scores_gemma":[0.00013626929,0.00004619083,0.0008691684,0.00035641956,0.00009036355,0.0000010674911,0.000032181593,0.90838075,0.08348851,0.0063767913,0.000029198083,0.00019311924],"about_ca_topic_score_codex":0.000012885248,"about_ca_topic_score_gemma":0.0000011452433,"teacher_disagreement_score":0.75521106,"about_ca_system_score_codex":0.000042061754,"about_ca_system_score_gemma":0.000047321693,"threshold_uncertainty_score":0.7129574},"labels":[],"label_agreement":null},{"id":"W4396494601","doi":"10.2514/1.j063650","title":"Near-Field Aeroacoustic Shape Optimization at Low Reynolds Numbers","year":2024,"lang":"en","type":"article","venue":"AIAA Journal","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Concordia University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Reynolds number; Acoustics; Mechanics; Field (mathematics); Physics; Geometry; Mathematics; Turbulence","score_opus":0.004219431987734233,"score_gpt":0.2043323294214538,"score_spread":0.20011289743371957,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4396494601","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.40993977,0.0015141413,0.57353294,0.00040716826,0.0057194657,0.00010009147,0.000013943062,0.0004543687,0.008318138],"genre_scores_gemma":[0.98738647,0.0008026713,0.010357223,0.00012489062,0.00060492853,0.0000029356831,0.000008083697,0.00006732239,0.00064550294],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991123,0.000011648863,0.00025133693,0.00013370383,0.00020966837,0.0002813356],"domain_scores_gemma":[0.99958974,0.00008568757,0.000022706281,0.00013399367,0.00004196589,0.00012588283],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00016551765,0.00015064685,0.00012487135,0.00006707036,0.00017944838,0.0003243127,0.00015460083,0.000121280376,0.0017644807],"category_scores_gemma":[0.000043934873,0.00014318252,0.00008805846,0.00018015777,0.000023511204,0.00016554959,0.00003991963,0.0004914079,0.00014785814],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000039806328,0.0000062910017,0.00005467689,0.000057653033,0.000051304614,0.00013740153,0.00015038461,0.9707562,0.0009813035,0.00011059173,0.021802006,0.005888261],"study_design_scores_gemma":[0.00010761771,0.000029846764,0.0000361169,0.00013183914,0.000040928073,0.0003393078,0.00002763814,0.99658215,0.00008050636,0.00021390061,0.0022383893,0.00017177932],"about_ca_topic_score_codex":0.0000022668094,"about_ca_topic_score_gemma":0.000004411806,"teacher_disagreement_score":0.57744664,"about_ca_system_score_codex":0.00021275874,"about_ca_system_score_gemma":0.00003705582,"threshold_uncertainty_score":0.9991481},"labels":[],"label_agreement":null},{"id":"W4397004526","doi":"10.2514/1.j063714","title":"Large-Eddy Simulation and Aeroacoustic Prediction of Supercritical Airfoil Side-Edge Noise","year":2024,"lang":"en","type":"article","venue":"AIAA Journal","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":9,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke; University of Toronto","funders":"Natural Sciences and Engineering Research Council of Canada; Alliance de recherche numérique du Canada; Bombardier","keywords":"Airfoil; Acoustics; Large eddy simulation; Noise (video); Supercritical fluid; Detached eddy simulation; Aeroacoustics; Enhanced Data Rates for GSM Evolution; Physics; Aerospace engineering; Geology; Computational fluid dynamics; Computer science; Mechanics; Engineering; Turbulence; Reynolds-averaged Navier–Stokes equations; Telecommunications; Artificial intelligence","score_opus":0.009859325408470482,"score_gpt":0.24096515923577733,"score_spread":0.23110583382730684,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4397004526","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.5877674,0.001126155,0.4091828,0.000048678296,0.0011285417,0.000043998585,0.00006134319,0.00009223345,0.0005488324],"genre_scores_gemma":[0.998168,0.00031982883,0.0009594023,0.000014763252,0.00046821727,0.0000014962815,0.00000762831,0.00003210996,0.0000285717],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992172,0.000015910959,0.00028547752,0.00010395003,0.00017931142,0.00019816606],"domain_scores_gemma":[0.999599,0.00014182538,0.0000068622744,0.000083871935,0.00006790836,0.0001005426],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025080878,0.00010925421,0.0001314817,0.000104818566,0.000073311865,0.000084570216,0.000057844314,0.00008977577,0.0000651805],"category_scores_gemma":[0.000077822166,0.00010223781,0.000052856976,0.00010588513,0.000035346646,0.00018494311,0.000022004202,0.00037142696,0.000008762285],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000067914325,0.00003125424,0.0004711508,0.0002882185,0.00007286628,0.00006421348,0.00043824743,0.972299,0.019949002,0.001997412,0.0008478021,0.0035340355],"study_design_scores_gemma":[0.00018412147,0.000047443285,0.00197568,0.00013935659,0.00007540807,0.00012722886,0.00010603639,0.99482256,0.00010333763,0.001818598,0.0005138402,0.0000863705],"about_ca_topic_score_codex":7.4025075e-7,"about_ca_topic_score_gemma":0.0000019029495,"teacher_disagreement_score":0.41040057,"about_ca_system_score_codex":0.00005239848,"about_ca_system_score_gemma":0.000022413453,"threshold_uncertainty_score":0.41691372},"labels":[],"label_agreement":null},{"id":"W4399152540","doi":"10.2514/6.2024-3150","title":"Influence of the Rotor Blade Pitch Angle on the Far-Field Noise Emissions of a Ducted Tail Rotor","year":2024,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"École de Technologie Supérieure; Université de Sherbrooke","funders":"","keywords":"Rotor (electric); Noise (video); Blade (archaeology); Acoustics; Blade pitch; Physics; Aerospace engineering; Engineering; Computer science; Mechanical engineering","score_opus":0.005718942755401643,"score_gpt":0.20759139722045455,"score_spread":0.20187245446505292,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4399152540","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9913677,0.00009761076,0.0015585052,0.0005743883,0.00024874325,0.0003377322,0.00003307341,0.000100107405,0.0056821345],"genre_scores_gemma":[0.9985234,0.000036973423,0.00019907956,0.000112339454,0.00004754073,0.000035333207,7.9162936e-7,0.000021586451,0.0010229584],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99935305,0.00001424721,0.00021220333,0.00011004055,0.00017415358,0.00013629215],"domain_scores_gemma":[0.9992489,0.00025331764,0.000023005885,0.00039619004,0.000044844033,0.00003374485],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00009682786,0.000110130364,0.00011300888,0.00003230618,0.000044972458,0.000017661907,0.0003169232,0.000072008035,0.0001869097],"category_scores_gemma":[0.00019226952,0.00005753274,0.000080122976,0.00026992924,0.000040415616,0.00003258386,0.0000729356,0.00024912725,0.000011055145],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000009308036,0.000050674436,0.00034677127,0.00023518424,0.00008576858,0.000003800914,0.0006016099,0.35590842,0.61560994,0.016245617,0.009893944,0.0010089643],"study_design_scores_gemma":[0.00015134811,0.00009732111,0.0072099296,0.0005571097,0.00006036782,0.0000036446622,0.00027220108,0.86911345,0.112806626,0.001409383,0.008054745,0.00026385518],"about_ca_topic_score_codex":0.000038843344,"about_ca_topic_score_gemma":0.000024018653,"teacher_disagreement_score":0.51320505,"about_ca_system_score_codex":0.000021705973,"about_ca_system_score_gemma":0.000031866624,"threshold_uncertainty_score":0.2346117},"labels":[],"label_agreement":null},{"id":"W4399162972","doi":"10.2514/6.2024-3389","title":"Data-Driven Acceleration and Sensitivity Study of an Acoustic Cascade Response Model","year":2024,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Cascade; Acceleration; Sensitivity (control systems); Computer science; Physics; Engineering; Electronic engineering","score_opus":0.03470974136359383,"score_gpt":0.28754121017142087,"score_spread":0.25283146880782703,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4399162972","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8102763,0.000024650264,0.1890824,0.0000090303665,0.00009704142,0.000118724594,0.000122047866,0.0001539281,0.000115848445],"genre_scores_gemma":[0.99647397,0.000016113665,0.0033415132,0.000005860521,0.000035586763,0.0000026872442,0.000027897659,0.000023165661,0.000073210205],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99943477,0.00003848995,0.00013683687,0.00019275575,0.00010420664,0.00009294003],"domain_scores_gemma":[0.9994814,0.00011694827,0.00000713227,0.0003350889,0.00001960326,0.000039841158],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003591353,0.00008936111,0.000107759915,0.000058589678,0.000029552417,0.00005873498,0.000062177685,0.000043420194,0.0000052063924],"category_scores_gemma":[0.00003039276,0.00008188613,0.000007598186,0.00007548931,0.000014572631,0.0002463416,0.00008724296,0.00011318619,0.0000016861912],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000164725,0.00003921347,0.0000091288575,0.00003952033,0.000024834919,0.00004156459,0.0004290674,0.9153842,0.082708105,0.0000583834,0.00013046507,0.0011190944],"study_design_scores_gemma":[0.000100133584,0.000063756575,0.0005562932,0.0000103259135,0.000041936575,0.000014866329,0.00029243095,0.99863744,0.00012643897,0.000054430846,0.000008451188,0.000093513234],"about_ca_topic_score_codex":0.000019634543,"about_ca_topic_score_gemma":0.00060649496,"teacher_disagreement_score":0.18619764,"about_ca_system_score_codex":0.00002069686,"about_ca_system_score_gemma":0.000016269365,"threshold_uncertainty_score":0.33392194},"labels":[],"label_agreement":null},{"id":"W4399163041","doi":"10.2514/6.2024-3276","title":"Laser-Induced Plasma Studies in the UTIAS Hybrid Anechoic Wind Tunnel","year":2024,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke; Institute for Christian Studies; University of Toronto","funders":"","keywords":"Anechoic chamber; Wind tunnel; Plasma; Laser; Acoustics; Materials science; Aerospace engineering; Physics; Optics; Engineering","score_opus":0.041747423415587175,"score_gpt":0.28260014436052927,"score_spread":0.2408527209449421,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4399163041","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9869992,0.00051383907,0.0003694472,0.00018831508,0.0012152186,0.00011909175,0.000012963608,0.0002704379,0.010311468],"genre_scores_gemma":[0.99887425,0.00023622822,0.00021482665,0.000072794544,0.0001676425,0.00001052292,0.0000047291296,0.000027758719,0.00039122233],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993351,0.000013810011,0.0001599445,0.00015217962,0.00012829654,0.00021062938],"domain_scores_gemma":[0.99954695,0.00022048329,0.000004980136,0.00019256714,0.0000127988205,0.000022209793],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021315731,0.00013643809,0.00012484362,0.00006958335,0.000037593152,0.00006700672,0.00017826211,0.00003561192,0.000037472986],"category_scores_gemma":[0.000030740994,0.00009046487,0.00004107992,0.00018872984,0.000025564006,0.000065690365,0.000037789334,0.00027098507,0.00011065172],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000014949342,0.00021820611,0.0004932127,0.001789997,0.0012147696,0.0044959197,0.012147658,0.6283642,0.03563301,0.035796273,0.14623062,0.13360117],"study_design_scores_gemma":[0.00011331108,0.000020819387,0.00022739131,0.00007114136,0.000019466135,0.00003806395,0.0009742152,0.9939585,0.0005661439,0.0014201734,0.0024135832,0.00017723658],"about_ca_topic_score_codex":0.000007218192,"about_ca_topic_score_gemma":0.00012311844,"teacher_disagreement_score":0.36559424,"about_ca_system_score_codex":0.000054615248,"about_ca_system_score_gemma":0.000009751307,"threshold_uncertainty_score":0.36890504},"labels":[],"label_agreement":null},{"id":"W4399163300","doi":"10.2514/6.2024-3141","title":"Turbulent Boundary Layer Trailing Edge Noise in the UTIAS Hybrid Anechoic Wind Tunnel","year":2024,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke; Institute for Christian Studies; University of Toronto","funders":"","keywords":"Wind tunnel; Trailing edge; Anechoic chamber; Boundary layer; Acoustics; Noise (video); Turbulence; Boundary layer suction; Aerospace engineering; Marine engineering; Physics; Geology; Flow separation; Computer science; Mechanics; Engineering; Boundary layer control","score_opus":0.013501111612687897,"score_gpt":0.22920346826967372,"score_spread":0.21570235665698584,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4399163300","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9569558,0.0028234755,0.012457072,0.000608956,0.0013519941,0.00023574616,0.00002270253,0.00043373767,0.025110502],"genre_scores_gemma":[0.9984356,0.00014596853,0.00044235255,0.00020910952,0.0002756558,0.000009044909,0.000013496739,0.000043028846,0.00042574052],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99912834,0.000014881299,0.00021080037,0.00019752386,0.00016547854,0.00028300085],"domain_scores_gemma":[0.999586,0.000110014065,0.000005967385,0.00024647763,0.000010754097,0.000040798226],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002879932,0.00016360484,0.00012106569,0.00008355476,0.000053848824,0.00020225666,0.00023236871,0.000052200565,0.000167378],"category_scores_gemma":[0.000013139915,0.00011718426,0.00006987024,0.00018620145,0.00003082273,0.00009466503,0.000027318392,0.00040987632,0.000114565686],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000010245088,0.0001355869,0.00020607332,0.0006715725,0.00014999647,0.001694636,0.003778867,0.8845639,0.024932915,0.014081205,0.043136545,0.026638458],"study_design_scores_gemma":[0.00011643246,0.000013383709,0.00088784576,0.0000715996,0.000019038083,0.000073822026,0.00018716215,0.96602523,0.00021829175,0.0014186351,0.030747399,0.00022115099],"about_ca_topic_score_codex":0.000013258645,"about_ca_topic_score_gemma":0.000054211163,"teacher_disagreement_score":0.08146134,"about_ca_system_score_codex":0.000052713836,"about_ca_system_score_gemma":0.000026634567,"threshold_uncertainty_score":0.47786355},"labels":[],"label_agreement":null},{"id":"W4399215805","doi":"10.3390/aerospace11060446","title":"The Derivation of an Empirical Model to Estimate the Power Spectral Density of Turbulent Boundary Layer Wall Pressure in Aircraft Using Machine Learning Regression Techniques","year":2024,"lang":"en","type":"article","venue":"Aerospace","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Carleton University","funders":"","keywords":"Boundary layer; Turbulence; Spectral density; Boundary (topology); Regression analysis; Regression; Power (physics); Mechanics; Mathematics; Physics; Statistics; Mathematical analysis; Thermodynamics","score_opus":0.014750945986421569,"score_gpt":0.3085844512749139,"score_spread":0.29383350528849234,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4399215805","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.93566895,0.00057143497,0.06280576,0.0005061589,0.000085596905,0.00017168849,0.0000045583633,0.00012365586,0.0000622248],"genre_scores_gemma":[0.97970587,0.00004823352,0.020083793,0.000020151007,0.000018649236,0.0000048434235,0.0000038056146,0.00003170757,0.000082923914],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992575,0.000034594686,0.00020241234,0.00014548172,0.00018506958,0.00017494652],"domain_scores_gemma":[0.9995995,0.00006738536,0.000032671804,0.00022752435,0.000041110343,0.00003181244],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00034789246,0.00012604722,0.00014085871,0.000041359606,0.00009318907,0.00005150471,0.00015678228,0.00007516355,0.0000026692394],"category_scores_gemma":[0.00004187681,0.00007825935,0.000041009625,0.00016959636,0.00004804464,0.00008687266,0.00007012031,0.00034094037,4.8275825e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000015337568,0.000014235899,0.0016093946,0.00005552536,0.000015974681,0.000005191845,0.0009391406,0.9078987,0.08866096,0.00024090352,0.00012987902,0.0004147608],"study_design_scores_gemma":[0.000037046553,0.000037356236,0.001669242,0.00016537354,0.000018355902,0.0000060705406,0.000031005933,0.97938746,0.017703371,0.0005065382,0.00034896214,0.00008918573],"about_ca_topic_score_codex":0.00006947155,"about_ca_topic_score_gemma":0.00020980187,"teacher_disagreement_score":0.0714888,"about_ca_system_score_codex":0.00006152035,"about_ca_system_score_gemma":0.000027444414,"threshold_uncertainty_score":0.31913236},"labels":[],"label_agreement":null},{"id":"W4399271163","doi":"10.2514/6.2024-3348","title":"Noise Radiation and Dynamics of Slat Cove Vortices Revisited in Light of a Parametric LBM Study","year":2024,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Cove; Parametric statistics; Noise (video); Vortex; Physics; Radiation; Acoustics; Dynamics (music); Optics; Computer science; Mechanics; Geology; Mathematics; Artificial intelligence","score_opus":0.004099334351870178,"score_gpt":0.22116046980458343,"score_spread":0.21706113545271324,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4399271163","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9890437,0.001730135,0.006794331,0.000018454686,0.00013674425,0.00021373705,0.000018110872,0.00004856396,0.0019961824],"genre_scores_gemma":[0.99892414,0.00042261905,0.0005455035,0.0000021834496,0.000012569617,0.0000041051544,0.0000067592205,0.000014664487,0.00006748264],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99939877,0.000011757916,0.00029339612,0.000109516805,0.00010263557,0.00008391961],"domain_scores_gemma":[0.99969167,0.000120972974,0.000025155714,0.00011835194,0.000022633536,0.00002122808],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017596461,0.000080465434,0.00017970428,0.0002731327,0.000005982613,0.000019913761,0.000055271652,0.00004462113,0.000012989646],"category_scores_gemma":[0.00005504785,0.000071916475,0.000021601032,0.0006550093,0.000011246844,0.00006781115,0.000022713433,0.00008797993,0.0000013449227],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000047600974,0.00068284135,0.22696057,0.0049052425,0.0006180729,0.00008854951,0.0048079514,0.6001946,0.012675999,0.039128553,0.0004331424,0.1094569],"study_design_scores_gemma":[0.00015531438,0.000058363334,0.013029502,0.000058684713,0.000037917533,6.5307916e-7,0.0001838787,0.985977,0.00012417727,0.00026448382,0.00003508826,0.00007493403],"about_ca_topic_score_codex":0.00003618318,"about_ca_topic_score_gemma":0.000113009984,"teacher_disagreement_score":0.38578242,"about_ca_system_score_codex":0.000042046388,"about_ca_system_score_gemma":0.000007024994,"threshold_uncertainty_score":0.29326686},"labels":[],"label_agreement":null},{"id":"W4399271203","doi":"10.2514/6.2024-3067","title":"On the Noise Mechanisms of a Controlled Diffusion Airfoil at Pre-Stall","year":2024,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure; Université de Sherbrooke","funders":"","keywords":"Stall (fluid mechanics); Airfoil; Computer science; Acoustics; Aerospace engineering; Physics; Engineering","score_opus":0.004060464191329437,"score_gpt":0.18750630453334843,"score_spread":0.183445840342019,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4399271203","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7015991,0.0001819207,0.2470854,0.00023986645,0.00090057164,0.0003793158,0.000027444727,0.0003511916,0.049235187],"genre_scores_gemma":[0.9952523,0.000057196412,0.0003525974,0.000064390384,0.000031301235,0.000025021556,0.0000033213937,0.00002856669,0.0041853115],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994428,0.000009789339,0.00016421064,0.000106049265,0.00015136674,0.00012579572],"domain_scores_gemma":[0.9994885,0.0002582125,0.000010928217,0.00019952763,0.00001488826,0.000027959204],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001382585,0.000109654364,0.0001531722,0.00003552101,0.000035963156,0.00002298893,0.000115033356,0.000052269905,0.00052374037],"category_scores_gemma":[0.000029876916,0.000061642495,0.00009220677,0.00007130466,0.000015676458,0.000016973856,0.00005353493,0.00011167736,0.000051248735],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000073023606,0.00003598567,0.0000011926941,0.00012390006,0.000106688145,0.000011441216,0.00019489772,0.14165582,0.34420535,0.5083157,0.0044084666,0.00086758554],"study_design_scores_gemma":[0.00038633743,0.000040750572,0.00001799443,0.000053750144,0.000023995484,0.0000011897968,0.000018360406,0.98081094,0.0031536997,0.015096734,0.00031599886,0.00008023478],"about_ca_topic_score_codex":0.000005470962,"about_ca_topic_score_gemma":0.00002163098,"teacher_disagreement_score":0.83915514,"about_ca_system_score_codex":0.000045047767,"about_ca_system_score_gemma":0.000005939744,"threshold_uncertainty_score":0.57345897},"labels":[],"label_agreement":null},{"id":"W4399271208","doi":"10.2514/6.2024-3094","title":"Large-Eddy Simulation and Broadband Acoustic Prediction of a Helicopter Rotor in Forward Flight","year":2024,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure; Université de Sherbrooke","funders":"","keywords":"Broadband; Acoustics; Aerospace engineering; Rotor (electric); Large eddy simulation; Aerodynamics; Computer science; Physics; Engineering; Meteorology; Telecommunications; Electrical engineering","score_opus":0.006773488851618213,"score_gpt":0.22976975338569697,"score_spread":0.22299626453407875,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4399271208","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.5387032,0.00039446817,0.45881224,0.000010141733,0.00034876197,0.00016794032,0.000054820353,0.00014083613,0.0013676073],"genre_scores_gemma":[0.99898624,0.00007466151,0.00061991025,0.0000074084514,0.00006972312,0.000011274237,0.000011771211,0.00001935246,0.00019963323],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995084,0.0000044874473,0.00017844584,0.00011012961,0.00008104635,0.000117532305],"domain_scores_gemma":[0.99981517,0.000057904967,0.000007027848,0.000077389675,0.000015821814,0.000026666059],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00009450125,0.0000811066,0.00009860332,0.00010271975,0.000012269574,0.000026031052,0.000028957256,0.000068620735,0.00005713415],"category_scores_gemma":[0.0000139594895,0.000072978495,0.00002093289,0.00011272345,0.000009762481,0.000096700816,0.000016762684,0.00008966649,0.000004984536],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000037448413,0.000011396311,0.0006067557,0.00028353115,0.00001772787,0.0000037852028,0.00026887582,0.98970693,0.007302268,0.00032618616,0.00016999613,0.0012988056],"study_design_scores_gemma":[0.00016911166,0.000021853357,0.0019242261,0.00008216341,0.00001611558,0.0000012929531,0.000036648078,0.9964495,0.00019743647,0.00027599433,0.00076126924,0.000064432206],"about_ca_topic_score_codex":0.000003846417,"about_ca_topic_score_gemma":0.0000370424,"teacher_disagreement_score":0.46028307,"about_ca_system_score_codex":0.000031946824,"about_ca_system_score_gemma":0.0000056668346,"threshold_uncertainty_score":0.29759768},"labels":[],"label_agreement":null},{"id":"W4399271226","doi":"10.2514/6.2024-3005","title":"Noise Emission from the Flap Profile of a Two-Element 30P30N High-Lift Airfoil","year":2024,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke; Institute for Christian Studies; University of Toronto","funders":"","keywords":"Airfoil; Lift (data mining); Acoustics; Noise (video); Aerospace engineering; Marine engineering; Geology; Computer science; Physics; Engineering","score_opus":0.005773511968019548,"score_gpt":0.21665145094106616,"score_spread":0.21087793897304663,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4399271226","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.88140786,0.0015706333,0.08454396,0.0006927643,0.0026118467,0.0003912292,0.00033314535,0.0007050259,0.027743515],"genre_scores_gemma":[0.9938561,0.00009006787,0.0041677975,0.000041544674,0.00025041503,0.00001866902,0.000045109515,0.00003437565,0.0014959371],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992967,0.000009722397,0.00021266578,0.00014783244,0.0001746872,0.00015835301],"domain_scores_gemma":[0.99954855,0.000107550426,0.000012583236,0.00026617752,0.000022032424,0.00004310117],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.000116499425,0.00012289187,0.00011995436,0.000023028171,0.00003518144,0.000039742645,0.00017672003,0.00004527806,0.0009221262],"category_scores_gemma":[0.000012293594,0.00007721079,0.000055721935,0.00011240226,0.000020646537,0.000039445735,0.00007022778,0.00015875507,0.00007874149],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000019508385,0.000118153206,0.0007205285,0.0006065235,0.0004818384,0.00005376272,0.00179355,0.23830019,0.45319214,0.06030087,0.18669802,0.057714924],"study_design_scores_gemma":[0.00016023955,0.000017675971,0.00023316438,0.00013109687,0.000038106926,6.5847576e-7,0.0000697156,0.96906126,0.012901776,0.001939565,0.01530887,0.00013788161],"about_ca_topic_score_codex":0.00012874631,"about_ca_topic_score_gemma":0.00004131919,"teacher_disagreement_score":0.73076105,"about_ca_system_score_codex":0.000038099704,"about_ca_system_score_gemma":0.000019680067,"threshold_uncertainty_score":0.9999912},"labels":[],"label_agreement":null},{"id":"W4399271248","doi":"10.2514/6.2024-3139","title":"Tonal Aeroacoustic Sources of a Cambered Airfoil Using Wavelet Beamforming","year":2024,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke; University of Toronto","funders":"","keywords":"Airfoil; Acoustics; Beamforming; Wavelet; Computer science; Physics; Engineering; Aerospace engineering; Artificial intelligence; Telecommunications","score_opus":0.009563529858735294,"score_gpt":0.21739323130852536,"score_spread":0.20782970144979007,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4399271248","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7227853,0.00045221945,0.26861656,0.000008494,0.0005929355,0.00005591145,0.00002754476,0.000269063,0.007191977],"genre_scores_gemma":[0.9780691,0.00003332296,0.021236822,0.000011036145,0.00014733385,0.0000025497347,0.0000059107915,0.00004505787,0.00044883197],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99922913,0.0000042426755,0.00024199263,0.00013574501,0.0001612259,0.00022764243],"domain_scores_gemma":[0.99970734,0.000067938825,0.00001309202,0.00013522412,0.000025970981,0.00005044477],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001064293,0.00013921065,0.00016249769,0.00009921162,0.000036495796,0.00004291094,0.00010238847,0.00007098924,0.00015573319],"category_scores_gemma":[0.000013446705,0.00012619823,0.00007223634,0.00018436268,0.00003661193,0.00008013672,0.000040480438,0.00015076759,0.000011892362],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000023692921,0.000013125851,0.000055433014,0.0006126957,0.00011493696,0.000037545284,0.00035381218,0.9253188,0.06254804,0.003874809,0.00047978625,0.006588652],"study_design_scores_gemma":[0.000057981888,0.000011076728,0.000029746003,0.000116535855,0.00004397265,0.00003553752,0.00012491761,0.99667186,0.0019256573,0.00033131754,0.00049538416,0.0001560237],"about_ca_topic_score_codex":0.00003505355,"about_ca_topic_score_gemma":0.00001787524,"teacher_disagreement_score":0.25528383,"about_ca_system_score_codex":0.00006176896,"about_ca_system_score_gemma":0.00002976392,"threshold_uncertainty_score":0.51462144},"labels":[],"label_agreement":null},{"id":"W4399271251","doi":"10.2514/6.2024-3322","title":"Installation and Manufacturing Effects of Propeller Trailing Edge Serrations","year":2024,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke; École de Technologie Supérieure","funders":"","keywords":"Trailing edge; Propeller; Marine engineering; Computer science; Engineering; Structural engineering","score_opus":0.00461450701658989,"score_gpt":0.1923888373124453,"score_spread":0.1877743302958554,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4399271251","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.86790574,0.00042589556,0.11248387,0.000012983342,0.00038418118,0.00011216478,0.0000017965612,0.0001781999,0.018495204],"genre_scores_gemma":[0.9975667,0.00007573996,0.0019276439,0.0000029199948,0.000040519557,0.0000031928207,0.0000028298434,0.000013806622,0.00036662945],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99975246,0.0000023125217,0.0000830623,0.000063166146,0.000040155966,0.000058813126],"domain_scores_gemma":[0.99988884,0.000038415743,0.0000035690884,0.00004735696,0.0000051959905,0.000016645277],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00003105436,0.00005240794,0.000052432264,0.000041865216,0.00001752312,0.000025750544,0.000019656582,0.000029160976,0.000015543861],"category_scores_gemma":[0.0000042461697,0.000044956585,0.000013588922,0.0000327686,0.000009285275,0.00006765864,0.000010287915,0.000060878258,0.0000036330462],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000024058502,0.000022087821,0.00010331265,0.005630498,0.00015750978,0.000020512965,0.0020395834,0.55518544,0.29511303,0.025054982,0.0008009771,0.11586968],"study_design_scores_gemma":[0.00004637939,0.00000844694,0.0007008259,0.000084538515,0.000012692512,0.0000018999904,0.00001972127,0.97054195,0.027338931,0.00034295648,0.0008338905,0.000067790636],"about_ca_topic_score_codex":0.0000018170136,"about_ca_topic_score_gemma":0.000009597347,"teacher_disagreement_score":0.4153565,"about_ca_system_score_codex":0.0000075519383,"about_ca_system_score_gemma":0.0000040454033,"threshold_uncertainty_score":0.18332763},"labels":[],"label_agreement":null},{"id":"W4399271260","doi":"10.2514/6.2024-3006","title":"Flap Side Edge Aeroacoustics of the 30P30N High-Lift Airfoil","year":2024,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"Université de Sherbrooke; University of Toronto","funders":"","keywords":"Airfoil; Aeroacoustics; Lift (data mining); Acoustics; Computer science; Aerospace engineering; Engineering; Physics","score_opus":0.004156008212308747,"score_gpt":0.1823817010992646,"score_spread":0.17822569288695586,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4399271260","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.5082396,0.0017252171,0.33300617,0.00051383046,0.012901882,0.00034689746,0.00018227889,0.0013673704,0.14171673],"genre_scores_gemma":[0.99378103,0.00010896866,0.0026365137,0.000049103422,0.00023975779,0.0000052432283,0.000004302401,0.000049688348,0.0031253884],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992542,0.000008171109,0.00022346286,0.0001347503,0.00017761499,0.00020176891],"domain_scores_gemma":[0.9994759,0.000099592595,0.000012163014,0.00033709002,0.000033336608,0.00004193647],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00010266349,0.00014063333,0.00014038908,0.00004098177,0.000039224433,0.000040413684,0.00025137322,0.000086699016,0.00012234913],"category_scores_gemma":[0.000031322063,0.0000959978,0.000088110886,0.00021817433,0.00005477273,0.00004122824,0.00008494459,0.00023641453,0.00006431847],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000019758531,0.000028001756,0.000072832605,0.00061318977,0.00014836458,0.000019718247,0.00019919715,0.80664515,0.052409172,0.09041373,0.04044439,0.009004259],"study_design_scores_gemma":[0.00007373606,0.000011739713,0.00045859042,0.000085941865,0.000058229383,0.000005298077,0.00004562057,0.98494047,0.0042897207,0.0027956066,0.0070613325,0.0001737026],"about_ca_topic_score_codex":0.000018525978,"about_ca_topic_score_gemma":0.000043812448,"teacher_disagreement_score":0.4855414,"about_ca_system_score_codex":0.000044575463,"about_ca_system_score_gemma":0.000028175531,"threshold_uncertainty_score":0.39146766},"labels":[],"label_agreement":null},{"id":"W4399271306","doi":"10.2514/6.2024-3004","title":"Performance Evaluation of Far-Field Noise Prediction Models for High-Lift Devices Using Reynolds-Averaged Navier-Stokes Simulations","year":2024,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"Université de Sherbrooke; University of Toronto","funders":"","keywords":"Lift (data mining); Reynolds number; Computational fluid dynamics; Reynolds-averaged Navier–Stokes equations; Field (mathematics); Noise (video); Computer science; Near and far field; Mechanics; Aerospace engineering; Physics; Mathematics; Engineering; Turbulence; Optics; Artificial intelligence; Data mining","score_opus":0.03326150169349454,"score_gpt":0.2778472773999421,"score_spread":0.24458577570644754,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4399271306","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6423672,0.000222466,0.3557296,0.000008428327,0.0005519483,0.00031018708,0.00007191357,0.00018674262,0.0005514942],"genre_scores_gemma":[0.9875063,0.000094132556,0.012087512,0.000009256952,0.00012448948,0.000035517267,0.00006314932,0.000031627853,0.000048034293],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991705,0.0000118970665,0.0002794704,0.0001478018,0.00025320603,0.00013713219],"domain_scores_gemma":[0.9995065,0.0001308837,0.00002515825,0.00015117206,0.00016030273,0.000026012704],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00030921822,0.00011506437,0.00011906865,0.0001034718,0.000082142935,0.00004017744,0.00007306273,0.000092300186,0.00005819081],"category_scores_gemma":[0.000026954658,0.00011175066,0.000046384255,0.00013750643,0.000010375561,0.00035223225,0.0000149842235,0.00010007869,0.000001948834],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000038808003,0.000010734057,0.00012434987,0.00024456292,0.00003964949,9.102669e-8,0.00010437798,0.9772678,0.008523246,0.00085450534,0.00006304349,0.012763781],"study_design_scores_gemma":[0.00018459721,0.00004097443,0.00039035885,0.0001334102,0.00016663126,6.8842127e-7,0.000017637796,0.99543583,0.0025779174,0.0008765562,0.00006274758,0.0001126446],"about_ca_topic_score_codex":0.000015174352,"about_ca_topic_score_gemma":0.000032606793,"teacher_disagreement_score":0.3451391,"about_ca_system_score_codex":0.00009298797,"about_ca_system_score_gemma":0.000034285393,"threshold_uncertainty_score":0.45570597},"labels":[],"label_agreement":null},{"id":"W4399271316","doi":"10.2514/6.2024-3160","title":"Aeroacoustic Performances of the ECL5 UHBR Turbofan Model With Serrated OGVs: Design, Predictions and Comparisons With Measurements","year":2024,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Safran Electronics (Canada)","funders":"Office National d'études et de Recherches Aérospatiales; European Commission; Cleansky; Abu Dhabi Education Council","keywords":"Turbofan; 3d printer; Computer science; Acoustics; Engineering; Aerospace engineering; Mechanical engineering; Physics","score_opus":0.026141511985967262,"score_gpt":0.19917868043677278,"score_spread":0.17303716845080552,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4399271316","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.17003064,0.00025901987,0.8251948,0.00003763019,0.00015131349,0.0002365373,0.000023353672,0.00022069615,0.0038460183],"genre_scores_gemma":[0.9858519,0.000048003025,0.013657102,0.000009327612,0.000019308545,0.000020473502,0.0000031580782,0.000030402714,0.00036033322],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993291,0.0000099259705,0.00014478626,0.00013776244,0.000220332,0.00015808098],"domain_scores_gemma":[0.9996825,0.000025170839,0.000016708442,0.00017074466,0.00006031973,0.000044574346],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000103877916,0.00014528779,0.00013128237,0.000045093962,0.000108998334,0.00005282391,0.00010899625,0.000041966756,0.000010591053],"category_scores_gemma":[0.0000035269188,0.00007937824,0.000017107364,0.00023849517,0.00008943554,0.000100923666,0.00002193647,0.0001781164,0.0000011557582],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000008746638,0.000013370524,0.00089644315,0.00011405502,0.000121828285,6.450553e-7,0.000205746,0.99574727,0.0013376178,0.00011882419,0.0013566577,0.000078806945],"study_design_scores_gemma":[0.0001520919,0.00006273323,0.0007748752,0.00017330557,0.00013575712,0.000009451132,0.00015657442,0.9979314,0.00041367352,0.00004767007,0.000024371386,0.000118080214],"about_ca_topic_score_codex":0.000010749994,"about_ca_topic_score_gemma":0.00011490376,"teacher_disagreement_score":0.81582123,"about_ca_system_score_codex":0.000032218155,"about_ca_system_score_gemma":0.00005359203,"threshold_uncertainty_score":0.32369506},"labels":[],"label_agreement":null},{"id":"W4399271322","doi":"10.2514/6.2024-3047","title":"A Numerical and Analytical Approach of the Sound-Scattering Effects in Rotor-Strut Interaction Noise of Small-Size Drones","year":2024,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Natural Sciences and Engineering Research Council of Canada; Alliance de recherche numérique du Canada","keywords":"Aerodynamics; Noise (video); Rotor (electric); Acoustics; Physics; Cylinder; Scattering; Mechanics; Computer science; Engineering; Optics; Mechanical engineering","score_opus":0.007744316160464592,"score_gpt":0.2217065903468226,"score_spread":0.21396227418635802,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4399271322","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9041778,0.00008557098,0.09298562,0.000020706177,0.00028121995,0.00014751879,0.0000020596742,0.000039608025,0.0022598915],"genre_scores_gemma":[0.99736565,0.000008107598,0.0025197905,0.000005220195,0.000030060117,0.000012189695,6.683332e-7,0.000016078671,0.000042244348],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995072,0.000013995395,0.00018747564,0.00011283035,0.00007535769,0.0001031723],"domain_scores_gemma":[0.9996394,0.00019791708,0.000012873418,0.000118159,0.000008783645,0.000022894885],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00008581317,0.00008859292,0.00015438262,0.000046438898,0.000009483627,0.000020384045,0.00007099374,0.000049073475,0.00000972663],"category_scores_gemma":[0.000040204966,0.000063225794,0.00004660126,0.00016249738,0.000041213538,0.00004030454,0.000048031256,0.00016508548,8.093019e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000047547986,0.00020493087,0.03081018,0.007368289,0.0003125711,0.000017964088,0.0014135044,0.851261,0.06999095,0.023106094,0.00013627196,0.0153306965],"study_design_scores_gemma":[0.00008729436,0.00001736582,0.010978257,0.00011287785,0.00001985458,0.000007974517,0.000050079307,0.9876616,0.0005443924,0.00044211367,0.000011177374,0.00006702939],"about_ca_topic_score_codex":0.000031725926,"about_ca_topic_score_gemma":0.000009846549,"teacher_disagreement_score":0.13640058,"about_ca_system_score_codex":0.000033320666,"about_ca_system_score_gemma":0.0000059279196,"threshold_uncertainty_score":0.2578273},"labels":[],"label_agreement":null},{"id":"W4399271337","doi":"10.2514/6.2024-3128","title":"A Data-Driven Method for Stall Noise Predictions","year":2024,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Stall (fluid mechanics); Computer science; Noise (video); Artificial intelligence; Aerospace engineering; Engineering","score_opus":0.02627848298010176,"score_gpt":0.30050506366261454,"score_spread":0.27422658068251277,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4399271337","genre_codex":"methods","genre_gemma":"methods","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0002813205,0.00016237934,0.98504126,0.00009193585,0.00096458633,0.00014532135,0.0015126594,0.0007396667,0.011060875],"genre_scores_gemma":[0.15548569,0.00012946402,0.83985126,0.00004941491,0.00054035615,0.000076233075,0.00054163026,0.000080571845,0.0032453917],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995584,0.000003163496,0.00010343237,0.00015369146,0.000054905486,0.00012639318],"domain_scores_gemma":[0.99954695,0.00011079407,0.0000029261682,0.0002862331,0.00001462513,0.000038475882],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000109992456,0.000072006565,0.000068702255,0.000039474467,0.000030022531,0.000060675808,0.00016961839,0.000039651914,0.000089551875],"category_scores_gemma":[0.000017725462,0.000063954496,0.000030381065,0.000077399054,0.000006846675,0.000095926676,0.000057836223,0.00008469314,0.000026687509],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000015961194,0.000013527837,0.000002503683,0.00025287416,0.0001583084,0.000005913543,0.00007540424,0.7790699,0.0071850005,0.030557828,0.16551274,0.017164383],"study_design_scores_gemma":[0.000041363077,0.000008302916,0.000007785727,0.000012333543,0.0000359305,0.0000025869392,0.000015495687,0.8590551,0.00002063611,0.0009581331,0.1397732,0.00006913846],"about_ca_topic_score_codex":0.000004326497,"about_ca_topic_score_gemma":0.000041286617,"teacher_disagreement_score":0.15520437,"about_ca_system_score_codex":0.000025760235,"about_ca_system_score_gemma":0.000013645183,"threshold_uncertainty_score":0.26079887},"labels":[],"label_agreement":null},{"id":"W4399271345","doi":"10.2514/6.2024-3345","title":"On the Phase Relation in Aeroacoustic Feedback Loops","year":2024,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Relation (database); Phase (matter); Acoustics; Control theory (sociology); Computer science; Physics; Artificial intelligence; Control (management)","score_opus":0.009027474066342195,"score_gpt":0.22963090122489765,"score_spread":0.22060342715855547,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4399271345","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7440063,0.0002687506,0.15785138,0.00038678444,0.0011933501,0.00018644918,0.000011676165,0.00045486566,0.095640466],"genre_scores_gemma":[0.9986194,0.00003901085,0.00024311506,0.00005853215,0.000063344676,0.0000094910465,0.000005899214,0.000023035702,0.0009381823],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995811,0.0000070334468,0.00011369965,0.00009492007,0.0000837239,0.00011954454],"domain_scores_gemma":[0.9996553,0.0001875281,0.0000033657088,0.00012948923,0.0000058635746,0.000018467572],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012852844,0.000078580975,0.000053188636,0.000053514817,0.000021659629,0.00005172089,0.00007030317,0.000045107656,0.00030203455],"category_scores_gemma":[0.000030242461,0.000052606127,0.00002307401,0.0001853758,0.000012389174,0.00004028302,0.000009900286,0.00022067325,0.00026634848],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000033989093,0.000028067177,0.000008197342,0.000048083104,0.000015939862,0.000026971242,0.00014389445,0.83477366,0.0032596819,0.14278674,0.011311998,0.0075933784],"study_design_scores_gemma":[0.00010801323,0.0000152199,0.0000896513,0.000048006703,0.0000060078146,0.0000015228544,0.000030844425,0.9927524,0.00005971052,0.0061889207,0.0006264276,0.0000733164],"about_ca_topic_score_codex":0.0000030930262,"about_ca_topic_score_gemma":0.000016281581,"teacher_disagreement_score":0.2546131,"about_ca_system_score_codex":0.00005975942,"about_ca_system_score_gemma":0.00000642005,"threshold_uncertainty_score":0.34234595},"labels":[],"label_agreement":null},{"id":"W4399271413","doi":"10.2514/6.2024-3363","title":"Large Eddy Simulation of Airfoil Tip Noise at Various Angles of Attack","year":2024,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke; University of Toronto","funders":"","keywords":"Airfoil; Acoustics; Noise (video); Large eddy simulation; Angle of attack; Computer science; Aerospace engineering; Marine engineering; Geology; Mechanics; Physics; Engineering; Aerodynamics; Turbulence; Artificial intelligence","score_opus":0.009708045412631284,"score_gpt":0.24588401583588188,"score_spread":0.2361759704232506,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4399271413","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7648928,0.00053835387,0.22169691,0.000010842957,0.00049200543,0.00007720327,0.00008261911,0.00019287759,0.0120163495],"genre_scores_gemma":[0.9974748,0.000044724333,0.0012922728,0.000006470927,0.000052757892,0.0000014979776,0.000018102413,0.000025560645,0.0010838042],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994883,0.000004274179,0.00019407224,0.00008974535,0.00010832587,0.00011527507],"domain_scores_gemma":[0.9996977,0.00008551734,0.000014162638,0.00014462574,0.000033790977,0.000024218689],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000079622965,0.00008137915,0.00012161661,0.000053363576,0.000014104727,0.000008019511,0.00006430957,0.000060839604,0.00022908008],"category_scores_gemma":[0.000014268217,0.00007402007,0.0000524174,0.00011534133,0.0000145365275,0.000042262378,0.000039809962,0.00006198922,0.000030799296],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000022221977,0.000016608958,0.00013117,0.0002774791,0.000031177315,0.0000033811352,0.00017544441,0.98816806,0.007995882,0.0016790454,0.0007975177,0.0007220281],"study_design_scores_gemma":[0.000086105945,0.00001619664,0.00036318085,0.000041180283,0.000020488425,7.3006294e-7,0.000018276216,0.9955661,0.00096543034,0.00019323736,0.0026496786,0.00007938517],"about_ca_topic_score_codex":0.000005241981,"about_ca_topic_score_gemma":0.000044440145,"teacher_disagreement_score":0.23258199,"about_ca_system_score_codex":0.00003674657,"about_ca_system_score_gemma":0.00000768585,"threshold_uncertainty_score":0.30184507},"labels":[],"label_agreement":null},{"id":"W4399271428","doi":"10.2514/6.2024-3362","title":"Computational Aeroacoustic Prediction of Tonal Noise for Low Reynolds Number Airfoils","year":2024,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Waterloo","funders":"","keywords":"Airfoil; Reynolds number; Noise (video); Acoustics; Computer science; Computational fluid dynamics; Speech recognition; Mechanics; Physics; Turbulence; Artificial intelligence","score_opus":0.006765515559938656,"score_gpt":0.22258949243178355,"score_spread":0.2158239768718449,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4399271428","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.08702596,0.0000680565,0.9041744,0.000030730833,0.0011655347,0.00014960833,0.00039287348,0.00031928893,0.006673555],"genre_scores_gemma":[0.9771184,0.000014873056,0.021794673,0.000015275633,0.00020581765,0.000025103183,0.000118442644,0.000032265092,0.0006751948],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993782,0.0000030074484,0.00021916046,0.00012621611,0.00014007515,0.0001333302],"domain_scores_gemma":[0.99967426,0.00013344908,0.000010078941,0.00008130258,0.000064303495,0.000036580965],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000092143026,0.000096784555,0.00010639088,0.000044046465,0.000025221492,0.000027260248,0.0000626203,0.00006947011,0.00019327423],"category_scores_gemma":[0.000014317857,0.00009304977,0.00006925156,0.0001040003,0.000024747402,0.00006775934,0.000012905968,0.00008296115,0.000027907003],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000036498702,0.000016553611,0.000065676926,0.0004069661,0.000053194373,0.0000016336046,0.000042447216,0.9721264,0.0021474364,0.011792515,0.011709144,0.001634385],"study_design_scores_gemma":[0.00013258372,0.000018797371,0.00043900812,0.000067143534,0.00003056169,0.000006902244,0.000012685127,0.99380857,0.00019044778,0.004499594,0.00071054994,0.00008318062],"about_ca_topic_score_codex":0.000002018466,"about_ca_topic_score_gemma":0.0000018814158,"teacher_disagreement_score":0.8900924,"about_ca_system_score_codex":0.000055037035,"about_ca_system_score_gemma":0.0000258045,"threshold_uncertainty_score":0.37944597},"labels":[],"label_agreement":null},{"id":"W4399271429","doi":"10.2514/6.2024-3046","title":"LBM and iLES Comparison for the Aaerodynamic and Acoustic Characteristics of a Low-speed Rotor","year":2024,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Rotor (electric); Computer science; Acoustics; Electrical engineering; Physics; Engineering","score_opus":0.0072336697342894945,"score_gpt":0.2294517143901441,"score_spread":0.22221804465585462,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4399271429","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.83171165,0.0014411756,0.16517411,0.000061433464,0.0006229128,0.00041233198,0.00017330798,0.0001505067,0.00025255783],"genre_scores_gemma":[0.99855113,0.00036015606,0.0007353604,0.000013249173,0.00009777686,0.000018427467,0.000012509032,0.000034024066,0.00017739396],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994187,0.0000044146273,0.000222978,0.00013229797,0.00007290364,0.00014874614],"domain_scores_gemma":[0.9993836,0.0004016566,0.00001818932,0.00012942869,0.000029086563,0.0000379871],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001212866,0.00012899592,0.00019561693,0.000039430004,0.000049718325,0.00007777704,0.00007964469,0.000059111553,0.000014404754],"category_scores_gemma":[0.000036554993,0.0000902747,0.00003234496,0.000061516526,0.000075952936,0.00003793609,0.00003870462,0.000114057824,0.0000016497903],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00013188345,0.00018450156,0.004272663,0.016999276,0.0013344049,0.000027382728,0.003615816,0.18231559,0.5725331,0.051357534,0.010500325,0.15672754],"study_design_scores_gemma":[0.000112114736,0.000031495998,0.003491883,0.00008510715,0.00007354733,0.000004120093,0.000115412106,0.9952546,0.00013476916,0.00023221475,0.00035012583,0.000114663344],"about_ca_topic_score_codex":0.0000064688293,"about_ca_topic_score_gemma":0.000031673397,"teacher_disagreement_score":0.8129389,"about_ca_system_score_codex":0.000016423448,"about_ca_system_score_gemma":0.000009037668,"threshold_uncertainty_score":0.36812955},"labels":[],"label_agreement":null},{"id":"W4399271432","doi":"10.2514/6.2024-3326","title":"Advanced Measurement and Analysis Techniques for Aircraft Core Noise: Application on the BEARCAT Turboshaft Research Test Bench","year":2024,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Safran Electronics (Canada)","funders":"","keywords":"Test bench; Noise (video); Core (optical fiber); Computer science; Aerospace engineering; Test (biology); Noise measurement; Test equipment; Aeronautics; Engineering; Automotive engineering; Telecommunications; Noise reduction; Embedded system; Artificial intelligence; Geology","score_opus":0.043130879243784406,"score_gpt":0.3190201297286768,"score_spread":0.27588925048489243,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4399271432","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.03291742,0.0014603555,0.9458635,0.0024939592,0.00012938846,0.0021792501,0.00013711247,0.000984023,0.01383502],"genre_scores_gemma":[0.9928997,0.0002190793,0.0058781435,0.000037006812,0.000071901464,0.00053808856,0.000024784205,0.000028927965,0.00030234875],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9990546,0.000009019725,0.0001441511,0.00023586779,0.00034940505,0.00020695307],"domain_scores_gemma":[0.9990332,0.0004524878,0.000007538425,0.00029820102,0.00016719922,0.000041354033],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0009635729,0.00010853887,0.00011169352,0.00017390527,0.00012653723,0.00008987572,0.00015141252,0.00005884043,0.000020029398],"category_scores_gemma":[0.00012330424,0.00007362112,0.00005586833,0.00057877414,0.000045942754,0.00003645059,0.00003709409,0.00022498108,0.000007933997],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000029604995,0.00017222484,0.0011215608,0.0010116948,0.001111508,0.0000052738765,0.0005241108,0.064471684,0.46033543,0.11029937,0.039784722,0.3211328],"study_design_scores_gemma":[0.000034566612,0.00006133573,0.0004839815,0.000036909656,0.000080271675,4.1595436e-7,0.00005082846,0.9781152,0.005832003,0.0039532487,0.011237614,0.00011363377],"about_ca_topic_score_codex":0.000008854126,"about_ca_topic_score_gemma":0.000070651484,"teacher_disagreement_score":0.9599823,"about_ca_system_score_codex":0.00012839075,"about_ca_system_score_gemma":0.000014206453,"threshold_uncertainty_score":0.30021822},"labels":[],"label_agreement":null},{"id":"W4399271447","doi":"10.2514/6.2024-3116","title":"On the Numerical Investigation of the Tip Leakage Noise Sources of a Stationary Aerofoil","year":2024,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure; Université de Sherbrooke","funders":"","keywords":"Airfoil; Leakage (economics); Acoustics; Noise (video); Computer science; Mechanics; Physics; Artificial intelligence","score_opus":0.007705559764202023,"score_gpt":0.1920354294288524,"score_spread":0.18432986966465037,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4399271447","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97332764,0.000100062694,0.02002056,0.0004706955,0.00024516942,0.00008018812,0.000019382576,0.000059523627,0.0056767785],"genre_scores_gemma":[0.99918914,0.000012057986,0.00035729946,0.000065459906,0.000026752665,0.0000051486068,0.0000025574711,0.000012701245,0.0003288776],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995905,0.0000159885,0.00013500036,0.000058163758,0.00014026742,0.00006008097],"domain_scores_gemma":[0.99956757,0.00024882163,0.000015740134,0.00013660903,0.000018113182,0.000013150992],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000099812576,0.000057084446,0.00005899815,0.000021191105,0.000024858546,0.000010598495,0.00011346705,0.000026324753,0.00007158489],"category_scores_gemma":[0.000036448157,0.00002988869,0.000040530096,0.00015662753,0.000059522878,0.00002396685,0.000022698556,0.000107106796,0.000008798934],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00000518314,0.000021126609,0.00086615974,0.00028995247,0.00008410684,0.0000021174749,0.0018252981,0.69429433,0.03860323,0.24999857,0.010982515,0.0030274142],"study_design_scores_gemma":[0.000028913502,0.000015444564,0.0029748874,0.00006359299,0.000012460819,8.899548e-7,0.00012345897,0.98242843,0.0056473245,0.00846173,0.00019371176,0.000049166574],"about_ca_topic_score_codex":0.000010615535,"about_ca_topic_score_gemma":0.0000036559302,"teacher_disagreement_score":0.2881341,"about_ca_system_score_codex":0.00001399766,"about_ca_system_score_gemma":0.00001549459,"threshold_uncertainty_score":0.12188254},"labels":[],"label_agreement":null},{"id":"W4399489757","doi":"10.1088/1742-6596/2767/7/072022","title":"Numerical Prediction of Tonal Aeroacoustic Noise Produced by Small Wind Turbines","year":2024,"lang":"en","type":"article","venue":"Journal of Physics Conference Series","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Waterloo","funders":"","keywords":"Airfoil; Aeroacoustics; Acoustics; Propeller; Noise (video); Trailing edge; Wind tunnel; Reynolds number; Computational fluid dynamics; Sound pressure; Engineering; Physics; Computer science; Aerospace engineering; Structural engineering; Mechanics; Marine engineering; Turbulence","score_opus":0.012471060662346352,"score_gpt":0.2024353019081683,"score_spread":0.18996424124582195,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4399489757","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.74597496,0.00091778784,0.24975461,0.00015928711,0.0023223266,0.000109635424,0.00018098111,0.00009564495,0.00048478626],"genre_scores_gemma":[0.9979581,0.0002480178,0.0010817077,0.0000053112417,0.00056779856,0.0000014853185,0.000010430643,0.00002898852,0.00009815801],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9990753,0.000013865191,0.00040514057,0.000109953515,0.00023992555,0.00015583096],"domain_scores_gemma":[0.9994189,0.000048299302,0.00009265997,0.000116337884,0.0002575273,0.00006627652],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00011612269,0.00015955369,0.0002731083,0.000049558246,0.000028508675,0.00007550762,0.00016222199,0.000061464634,0.000027804534],"category_scores_gemma":[0.000035290446,0.00013695018,0.00009816162,0.00017042621,0.00007230589,0.0003040408,0.000019310159,0.0003263993,0.0000029354687],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000045852266,0.00009669187,0.00017277365,0.0007163826,0.00027264474,0.000025975993,0.00070809736,0.18966,0.77857846,0.0048229448,0.0029690843,0.021931088],"study_design_scores_gemma":[0.00046883622,0.00072812074,0.0012079527,0.0009873032,0.00033572942,0.00012663871,0.00034837896,0.70377487,0.27973878,0.009992923,0.0017851808,0.00050527183],"about_ca_topic_score_codex":0.0000017187525,"about_ca_topic_score_gemma":5.3703303e-7,"teacher_disagreement_score":0.5141149,"about_ca_system_score_codex":0.000041482755,"about_ca_system_score_gemma":0.000107340624,"threshold_uncertainty_score":0.5584666},"labels":[],"label_agreement":null},{"id":"W4399596002","doi":"10.4271/2024-01-2937","title":"HVAC Blower: A Steady State RANS Noise Prediction Method","year":2024,"lang":"en","type":"article","venue":"SAE International Journal of Advances and Current Practices in Mobility","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Volvo (Canada)","funders":"","keywords":"Reynolds-averaged Navier–Stokes equations; HVAC; Noise (video); Engineering; Automotive engineering; Computer science; Air conditioning; Computational fluid dynamics; Mechanical engineering; Aerospace engineering","score_opus":0.0143233142440203,"score_gpt":0.35242494544580566,"score_spread":0.3381016312017854,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4399596002","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7505549,0.070710026,0.1604147,0.00038409114,0.016296623,0.00020551287,0.00022742245,0.00007624063,0.0011304952],"genre_scores_gemma":[0.95346403,0.04182734,0.0042726034,0.00000843414,0.0003813586,0.0000061748146,0.000006327324,0.000013796633,0.000019946327],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9987813,0.000060222977,0.00052126375,0.0001620242,0.00035302815,0.00012215874],"domain_scores_gemma":[0.99910426,0.00036204836,0.00022237115,0.00008445757,0.00016968629,0.00005715243],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0010747295,0.00012177313,0.00016307975,0.0001503744,0.000021109865,0.00014275142,0.00020819603,0.000033328142,0.000034074754],"category_scores_gemma":[0.00023277284,0.00010392781,0.00006976036,0.00010825116,0.0000371147,0.0013470836,0.000039789968,0.00054567296,0.0000017428823],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00017153521,0.0002631642,0.00518824,0.00048257137,0.00022465439,0.000085490545,0.00087501167,0.28105697,0.001632952,0.0005453191,0.00017208775,0.709302],"study_design_scores_gemma":[0.0008361514,0.00016438683,0.008445324,0.00076504995,0.000099721365,0.00020857604,0.00044932845,0.7769777,0.00012980128,0.01957747,0.19210105,0.00024540268],"about_ca_topic_score_codex":0.0000056343897,"about_ca_topic_score_gemma":0.00005570865,"teacher_disagreement_score":0.7090566,"about_ca_system_score_codex":0.00013270917,"about_ca_system_score_gemma":0.000040987812,"threshold_uncertainty_score":0.4238053},"labels":[],"label_agreement":null},{"id":"W4400090520","doi":"10.1063/5.0208973","title":"A review on free miscible buoyant jets","year":2024,"lang":"en","type":"review","venue":"Physics of Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":20,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université Laval","funders":"Natural Sciences and Engineering Research Council of Canada; Canada Research Chairs; Canada Foundation for Innovation; Petroleum Technology Alliance Canada","keywords":"Physics; Mechanics; Classical mechanics","score_opus":0.03609053014913529,"score_gpt":0.30493763919245653,"score_spread":0.26884710904332126,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4400090520","genre_codex":"review","genre_gemma":"review","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"review","genre_consensus":"review","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[3.040317e-7,0.98992425,0.00089809514,0.000011608433,0.0010408703,0.00042741207,0.0004619091,0.00017313889,0.0070624254],"genre_scores_gemma":[0.000003867956,0.9983632,0.00052166457,0.000036806814,0.0005211178,0.00007378449,0.00011430983,0.00017819674,0.00018705314],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9985327,0.00002138777,0.0006027992,0.00031480798,0.00025987058,0.0002684109],"domain_scores_gemma":[0.9986884,0.000085691434,0.00007275451,0.0010349705,0.00004734627,0.0000708338],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00016460232,0.0005100611,0.0016664106,0.0000726674,0.000021826783,0.000025797379,0.0006663744,0.00016001161,0.00002688865],"category_scores_gemma":[0.000038088718,0.0004032748,0.00068700523,0.0004188116,0.00003805151,0.00003312801,0.00016184634,0.0005795097,0.0003195185],"study_design_candidate":"not_applicable","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[2.1527671e-7,0.00003023013,5.8135305e-9,0.33458006,0.00026427995,0.000009149728,0.000009072661,0.00030001442,0.000005624864,0.004879523,0.09456104,0.5653608],"study_design_scores_gemma":[0.00003319981,0.000025374906,7.729357e-9,0.15979037,0.0014316313,0.0000031615696,3.956891e-7,0.004332799,0.0000024254425,0.002442111,0.83159655,0.0003419891],"about_ca_topic_score_codex":0.000002269654,"about_ca_topic_score_gemma":5.809123e-7,"teacher_disagreement_score":0.7370355,"about_ca_system_score_codex":0.000093165974,"about_ca_system_score_gemma":0.00007134136,"threshold_uncertainty_score":0.9998419},"labels":[],"label_agreement":null},{"id":"W4400287751","doi":"10.1121/10.0027419","title":"Aircraft noise contours—From everything for everyone to nothing for anyone","year":2024,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"University of Windsor","funders":"","keywords":"Nothing; Noise (video); Computer science; Philosophy; Artificial intelligence; Epistemology","score_opus":0.009199151994621837,"score_gpt":0.24096226928071335,"score_spread":0.2317631172860915,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4400287751","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.012620025,0.0016190812,0.98060167,0.0032372396,0.0013631348,0.00032036222,0.00016651336,0.000044247317,0.000027746644],"genre_scores_gemma":[0.706884,0.00034316207,0.2896295,0.0016466734,0.0011617766,0.000010202474,0.0000021735796,0.00007938069,0.00024309204],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99874705,0.000023869356,0.0004867977,0.00010879659,0.00032735686,0.000306145],"domain_scores_gemma":[0.9973927,0.0019629416,0.000117951415,0.0002515491,0.00017293096,0.00010190164],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006036603,0.00017585063,0.0003688295,0.000022189204,0.00015153683,0.000052442734,0.00059187243,0.000087621316,0.00001368841],"category_scores_gemma":[0.00033456963,0.00010537171,0.00056885934,0.00019755491,0.00014454118,0.000099095785,0.00010234429,0.000428527,0.0000023084947],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00009519352,0.000036918405,0.000004603075,0.00024821653,0.00053042907,9.557747e-7,0.0028860662,0.7244273,0.13050674,0.000015748785,0.13125622,0.009991644],"study_design_scores_gemma":[0.000267256,0.00014775957,0.000065378605,0.00030407088,0.00044948608,0.000010721519,0.0008097914,0.98066807,0.0009205035,0.0014691561,0.014741219,0.00014660251],"about_ca_topic_score_codex":0.000019648392,"about_ca_topic_score_gemma":7.4720623e-7,"teacher_disagreement_score":0.694264,"about_ca_system_score_codex":0.00013528623,"about_ca_system_score_gemma":0.00005933388,"threshold_uncertainty_score":0.42969337},"labels":[],"label_agreement":null},{"id":"W4400289008","doi":"10.1121/10.0026991","title":"Acoustic characterization and optimization of a subsonic closed loop wind tunnel","year":2024,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Carleton University","funders":"","keywords":"Wind tunnel; Acoustics; Loop (graph theory); Characterization (materials science); Aerospace engineering; Subsonic and transonic wind tunnel; Physics; Control theory (sociology); Environmental science; Engineering; Computer science; Aerodynamics; Mathematics; Optics; Transonic","score_opus":0.006334970067184094,"score_gpt":0.20917862762182152,"score_spread":0.20284365755463743,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4400289008","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.1396989,0.00056806253,0.85874146,0.00045504092,0.00037681396,0.000089398454,0.000026304051,0.000018809436,0.000025219102],"genre_scores_gemma":[0.9825163,0.002869937,0.014292331,0.0000987268,0.0001458395,4.0244663e-7,0.0000021422823,0.000029051607,0.000045261197],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999035,0.000041664618,0.00042682633,0.00006545009,0.0002818451,0.00014918436],"domain_scores_gemma":[0.99918944,0.000307841,0.00017120985,0.0001661573,0.00011800843,0.000047361384],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00033931376,0.00012368479,0.00025531204,0.000024732286,0.0000622199,0.000022914768,0.000263581,0.00007422025,0.00002840096],"category_scores_gemma":[0.00008370991,0.000072997864,0.00017562686,0.00029599926,0.00032047526,0.00008941696,0.00006838811,0.00034813935,6.4102153e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000139566955,0.000020330657,0.000011124817,0.00019111874,0.00013283188,5.7108883e-7,0.00036904996,0.82407326,0.16973396,0.0000066708353,0.00047080987,0.0049763075],"study_design_scores_gemma":[0.00013497005,0.000077029224,0.00070673507,0.00018726743,0.00033738662,0.000029382554,0.00027485,0.9975809,0.00038812732,0.00011521201,0.00009164127,0.00007648908],"about_ca_topic_score_codex":0.000002981187,"about_ca_topic_score_gemma":1.5452378e-7,"teacher_disagreement_score":0.8444491,"about_ca_system_score_codex":0.000052174462,"about_ca_system_score_gemma":0.000050299146,"threshold_uncertainty_score":0.29767665},"labels":[],"label_agreement":null},{"id":"W4400289224","doi":"10.1121/10.0026986","title":"Computational optimization of trailing-edge designs to reduce airfoil self-noise","year":2024,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Carleton University","funders":"","keywords":"Airfoil; Trailing edge; Noise (video); Computer science; Acoustics; Aerospace engineering; Engineering; Structural engineering; Physics; Artificial intelligence","score_opus":0.01142285600110196,"score_gpt":0.24404104538809135,"score_spread":0.2326181893869894,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4400289224","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.012316386,0.00033992238,0.9854834,0.0011356559,0.00043625457,0.00009353095,0.000023989924,0.000033625027,0.00013722364],"genre_scores_gemma":[0.70735943,0.00027314003,0.2920322,0.00014295941,0.00014651958,6.751764e-7,8.0942084e-7,0.0000225847,0.000021634105],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989172,0.00004653927,0.00044796002,0.000065745655,0.0003705747,0.00015195609],"domain_scores_gemma":[0.9989824,0.00050520845,0.00011351312,0.000149975,0.00017935288,0.000069528694],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00043154386,0.00011616528,0.00023286334,0.000025678222,0.000067781955,0.000017395896,0.00039892423,0.00005613115,0.000029937572],"category_scores_gemma":[0.00009012055,0.00007074243,0.00026414156,0.0003710446,0.00016917575,0.0000526071,0.000063870444,0.0003387689,0.0000021335834],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000014417254,0.000038700244,0.0000019791453,0.00010816213,0.0001724302,5.386113e-7,0.0009100007,0.97496897,0.009985693,0.000023034236,0.010903534,0.0028725616],"study_design_scores_gemma":[0.00010143739,0.00009552357,0.000052260228,0.00013031338,0.00021947396,0.000022273642,0.00034069875,0.99773765,0.00045130475,0.00046773287,0.0003042897,0.000077045195],"about_ca_topic_score_codex":0.0000027342676,"about_ca_topic_score_gemma":6.103836e-8,"teacher_disagreement_score":0.6950431,"about_ca_system_score_codex":0.00006724332,"about_ca_system_score_gemma":0.000088807166,"threshold_uncertainty_score":0.28847927},"labels":[],"label_agreement":null},{"id":"W4400894584","doi":"10.1080/09377255.2024.2374655","title":"Evolution of underwater noise emission prediction technology for ship-propulsor combinations in an industry environment","year":2024,"lang":"en","type":"article","venue":"Ship Technology Research","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Transport Canada; Bundesministerium für Wirtschaft und Klimaschutz","keywords":"Propulsor; Marine engineering; Propulsion; Computational fluid dynamics; Noise (video); Large eddy simulation; Underwater; Aerospace engineering; Turbulence; Engineering; Field (mathematics); Fidelity; Cavitation; Computer science; Acoustics; Meteorology; Geology; Artificial intelligence; Oceanography; Telecommunications; Geography","score_opus":0.03183554312764428,"score_gpt":0.3184376837488136,"score_spread":0.2866021406211693,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4400894584","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9747225,0.00067597866,0.021523388,0.0014073291,0.00020581807,0.0006189092,0.000065359454,0.0005408475,0.00023987214],"genre_scores_gemma":[0.99775094,0.00007964989,0.0015172709,9.725666e-7,0.000034664867,0.00033972866,0.000035219557,0.000041979685,0.00019957656],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99871576,0.0000331121,0.00028807274,0.00031384677,0.000222394,0.0004268307],"domain_scores_gemma":[0.99939317,0.00007543116,0.000014865182,0.00038524406,0.00008736553,0.000043950804],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00068176235,0.00012150863,0.00015459988,0.0018749818,0.00009455276,0.000020689291,0.00033188664,0.0011515039,0.000023944509],"category_scores_gemma":[0.000122191,0.00012004688,0.000025358342,0.0012179432,0.00034429383,0.000105492814,0.00012993749,0.0015589398,0.000012712448],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00005366606,0.0006427631,0.06613225,0.0010729523,0.00008815353,0.000040220148,0.00033269526,0.045920417,0.62937766,0.22387871,0.00063993206,0.031820577],"study_design_scores_gemma":[0.0004353764,0.00041316682,0.0021664617,0.00021976641,0.000013439753,0.00001049375,0.0008329526,0.769435,0.019063756,0.20606218,0.0011785111,0.00016887713],"about_ca_topic_score_codex":0.000004665227,"about_ca_topic_score_gemma":0.000021360851,"teacher_disagreement_score":0.7235146,"about_ca_system_score_codex":0.00055938057,"about_ca_system_score_gemma":0.00006791785,"threshold_uncertainty_score":0.88814527},"labels":[],"label_agreement":null},{"id":"W4401255341","doi":"10.1121/10.0028125","title":"Erratum: An experimental study of the wall-pressure fluctuations beneath low Reynolds number turbulent boundary layers [J. Acoust. Soc. Am. <b>141</b>, 1257–1268 (2017)]","year":2024,"lang":"en","type":"erratum","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Carleton University","funders":"","keywords":"Reynolds number; Turbulence; Mechanics; Physics; Boundary (topology); Boundary layer; Mathematics; Mathematical analysis","score_opus":0.01001874044240813,"score_gpt":0.2571170416085904,"score_spread":0.24709830116618225,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4401255341","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.54980844,0.0611063,0.10336373,0.020962995,0.2260786,0.010957311,0.003621534,0.0011095152,0.022991573],"genre_scores_gemma":[0.980915,0.0027946406,0.0036300165,0.00058147765,0.0021138142,0.000019974106,0.000022185377,0.0002954151,0.00962745],"study_design_codex":"not_applicable","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99538606,0.00031850286,0.0014043114,0.00035622373,0.0019020472,0.00063286425],"domain_scores_gemma":[0.9964946,0.0003165992,0.0009626562,0.0015703526,0.0004509715,0.00020483154],"candidate_categories":["metaepi_narrow","research_integrity"],"consensus_categories":[],"category_scores_codex":[0.0008727196,0.00072764093,0.0011748644,0.00005309033,0.0005730447,0.00013413205,0.00303573,0.0005711251,0.00017502236],"category_scores_gemma":[0.00011973446,0.0004008223,0.001269764,0.00058156316,0.0011743652,0.00016772945,0.00078787294,0.004090174,0.000008765933],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000042316733,0.0007458523,0.000009813744,0.00028243696,0.0016362637,0.0000065861764,0.005722531,0.22488102,0.004993881,0.000005352483,0.7614084,0.00026557254],"study_design_scores_gemma":[0.00081429933,0.0008925523,0.00038383997,0.0009930875,0.0047688177,0.00019063387,0.020550428,0.94235504,0.00021407503,0.0008699533,0.02718238,0.000784915],"about_ca_topic_score_codex":0.00012556299,"about_ca_topic_score_gemma":0.000011885836,"teacher_disagreement_score":0.734226,"about_ca_system_score_codex":0.00039913447,"about_ca_system_score_gemma":0.0004781291,"threshold_uncertainty_score":0.9998444},"labels":[],"label_agreement":null},{"id":"W4401346599","doi":"10.1007/978-3-031-55924-2_22","title":"Scaling of Turbulence Moments in Compressible Axisymmetric Jets","year":2024,"lang":"en","type":"book-chapter","venue":"Springer proceedings in physics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Calgary","funders":"","keywords":"Scaling; Rotational symmetry; Turbulence; Compressibility; Physics; Mechanics; Statistical physics; Classical mechanics; Mathematics; Geometry","score_opus":0.011739260751270717,"score_gpt":0.21241160541241225,"score_spread":0.20067234466114153,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4401346599","genre_codex":"other","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.041193407,0.0034361759,0.00059503724,0.000007743523,0.0016048432,0.0005408674,0.0000676158,0.0002789509,0.95227534],"genre_scores_gemma":[0.98207706,0.0015766397,0.0018517624,0.000009474907,0.00046081396,0.000027485268,0.0000115450075,0.00026387582,0.013721313],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9982376,7.8480736e-7,0.00059411966,0.0004231299,0.00038018584,0.00036414163],"domain_scores_gemma":[0.9995167,0.00004301704,0.00012610489,0.00017385349,0.00008468798,0.000055585773],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0001680453,0.00042746728,0.0005735275,0.0005104496,0.000016808583,0.000055099466,0.0003948072,0.00029947827,0.00001387216],"category_scores_gemma":[0.000018620689,0.0004875285,0.000113265785,0.0003561637,0.00006554246,0.00013308287,0.00023439233,0.0010260692,0.000033395827],"study_design_candidate":"theoretical_or_conceptual","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000023287872,0.00016640064,0.0013983357,0.014183256,0.00032397042,0.0000944194,0.0016643155,0.17339192,0.005214402,0.76164407,0.0006702374,0.04122538],"study_design_scores_gemma":[0.0005826886,0.00005188273,0.00030520788,0.010758158,0.000113302696,0.000004437069,0.000055644872,0.68131495,0.0023652802,0.29677898,0.0061118975,0.0015575759],"about_ca_topic_score_codex":0.000007674337,"about_ca_topic_score_gemma":0.0000026425892,"teacher_disagreement_score":0.9408837,"about_ca_system_score_codex":0.00026408987,"about_ca_system_score_gemma":0.000021115371,"threshold_uncertainty_score":0.99975765},"labels":[],"label_agreement":null},{"id":"W4401942762","doi":"10.1115/gt2024-129341","title":"Effect of Gerlach Cross-Section on S-Duct Inlet Performance in High Subsonic Flow","year":2024,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Defence Research and Development Canada; Royal Military College of Canada","funders":"","keywords":"Inlet; Duct (anatomy); Cross section (physics); Flow (mathematics); Mechanics; Section (typography); Computer science; Physics; Mechanical engineering; Engineering; Anatomy; Medicine","score_opus":0.003831603445370599,"score_gpt":0.2282219854900783,"score_spread":0.2243903820447077,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4401942762","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9916289,0.00015324652,0.002571723,0.0000056892477,0.0017110726,0.00010415417,0.000007319964,0.00019163667,0.003626277],"genre_scores_gemma":[0.99912536,0.0001162907,0.00023789458,0.000004222506,0.0001480991,0.000012534783,0.000009615951,0.000030201038,0.00031575293],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993959,0.000012952515,0.00017447046,0.00013902568,0.00011155782,0.00016607878],"domain_scores_gemma":[0.999712,0.00010123934,0.0000073622514,0.00014775657,0.000010595343,0.000021035627],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00029240767,0.00012033359,0.00014075908,0.00012090186,0.000017575368,0.000036482215,0.00007756998,0.00008454594,0.00007965157],"category_scores_gemma":[0.000014330268,0.00009996144,0.000039694984,0.00023220254,0.000019238209,0.00008460552,0.000014973607,0.00025084795,0.000046384226],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000021189462,0.000008807111,0.0055188187,0.000754348,0.00001843526,0.000008947686,0.000054988668,0.97147655,0.0032694854,0.00060678757,0.0001607864,0.018100854],"study_design_scores_gemma":[0.0001738637,0.00020627197,0.012801228,0.000097482305,0.0000061158034,0.000003151985,0.0000014354033,0.9795887,0.0067761727,0.000031604483,0.00020796715,0.00010601546],"about_ca_topic_score_codex":0.000012697873,"about_ca_topic_score_gemma":0.000024542313,"teacher_disagreement_score":0.017994838,"about_ca_system_score_codex":0.00010468601,"about_ca_system_score_gemma":0.000007716205,"threshold_uncertainty_score":0.40763095},"labels":[],"label_agreement":null},{"id":"W4402188119","doi":"10.21203/rs.3.rs-4870938/v1","title":"RETRACTED: Experimental Investigation of Positively Buoyant Surface Jet in Confluence Regions","year":2024,"lang":"en","type":"preprint","venue":"Research Square","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":true,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Ottawa","funders":"","keywords":"Confluence; Jet (fluid); Surface (topology); Mechanics; Geometry; Mathematics; Physics; Computer science","score_opus":0.04692944580322176,"score_gpt":0.3515888640712459,"score_spread":0.3046594182680241,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4402188119","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99303776,0.0028205214,0.00022694348,0.00014771508,0.00039904602,0.00061195955,0.00038978012,0.00012937534,0.0022368971],"genre_scores_gemma":[0.9980939,0.0005076187,0.00095190026,0.000004315714,0.000087103814,0.000056923393,0.00014028336,0.00007148604,0.00008644445],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99782914,0.00014872442,0.00041721686,0.00042101438,0.00075604714,0.00042782922],"domain_scores_gemma":[0.998858,0.0002424517,0.000042093263,0.00045945751,0.00027102293,0.0001270121],"candidate_categories":["metaepi_narrow","research_integrity"],"consensus_categories":[],"category_scores_codex":[0.0009049998,0.00023795808,0.00031946204,0.00035672064,0.000047437876,0.00009144988,0.00037346964,0.00045095666,0.000029786162],"category_scores_gemma":[0.00013347546,0.0002477657,0.000086270215,0.00051109056,0.00024084166,0.000050290113,0.00070445536,0.0028713292,0.000029179],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00003731938,0.00011478402,0.0044114925,0.005469921,0.00013792385,0.00041905348,0.005220666,0.3500673,0.6181353,0.012160446,0.0036401611,0.00018566863],"study_design_scores_gemma":[0.00033873646,0.0001788397,0.018463237,0.007957502,0.000022923472,0.00001394554,0.0019799573,0.8379768,0.117077954,0.015108458,0.00014578167,0.0007358276],"about_ca_topic_score_codex":0.00041917135,"about_ca_topic_score_gemma":0.000088467976,"teacher_disagreement_score":0.5010573,"about_ca_system_score_codex":0.00050154363,"about_ca_system_score_gemma":0.0002300221,"threshold_uncertainty_score":0.99999744},"labels":[],"label_agreement":null},{"id":"W4402392148","doi":"10.1063/5.0223543","title":"Jet mixing optimization using a flexible nozzle, distributed actuators, and machine learning","year":2024,"lang":"en","type":"article","venue":"Physics of Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of New Brunswick","funders":"Basic and Applied Basic Research Foundation of Guangdong Province; National Natural Science Foundation of China","keywords":"Physics; Nozzle; Mixing (physics); Jet (fluid); Actuator; Aerospace engineering; Mechanics; Mechanical engineering; Artificial intelligence; Thermodynamics; Computer science","score_opus":0.01376535530201099,"score_gpt":0.23036337977440347,"score_spread":0.2165980244723925,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4402392148","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.06720425,0.00095916406,0.9310215,0.000009304682,0.00021613187,0.000053014643,0.00008225867,0.00022302705,0.00023133185],"genre_scores_gemma":[0.97543865,0.00025988743,0.023988914,0.000002976738,0.00012750406,0.0000020082468,0.00012331684,0.000044892135,0.00001184758],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994566,0.000008208698,0.00015455099,0.00012968028,0.000104309554,0.0001466914],"domain_scores_gemma":[0.9997692,0.000050894007,0.00001494025,0.00009541604,0.000031444906,0.000038116374],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00007894883,0.00012980972,0.00015005551,0.000041801934,0.000055625816,0.000060649327,0.000060322276,0.000045366476,0.000010367117],"category_scores_gemma":[0.000018031724,0.00013213267,0.000040006384,0.00022911158,0.000028645816,0.00014659329,0.000060077233,0.00017170691,0.0000013918223],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000016809036,0.000007717893,0.00019393479,0.00019797742,0.00004519085,0.000002307019,0.000126543,0.97504854,0.017094225,0.0021320793,0.000033304266,0.0051164697],"study_design_scores_gemma":[0.00007807341,0.0000132037685,0.000013353628,0.00010520072,0.000041847863,0.0000023229238,0.000013712286,0.9960382,0.0021921706,0.0011815354,0.00018710397,0.00013329368],"about_ca_topic_score_codex":0.0000130225435,"about_ca_topic_score_gemma":5.8795405e-7,"teacher_disagreement_score":0.9082344,"about_ca_system_score_codex":0.00004101028,"about_ca_system_score_gemma":0.000012695105,"threshold_uncertainty_score":0.5388214},"labels":[],"label_agreement":null},{"id":"W4402455273","doi":"10.11159/htff24.189","title":"Plane Jet Vectoring near a Flat Plate using Secondary Suction Flow","year":2024,"lang":"en","type":"article","venue":"Proceedings of the World Congress on Mechanical, Chemical, and Material Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Suction; Jet (fluid); Mechanics; Plane (geometry); Flow (mathematics); Physics; Materials science; Geometry; Mathematics","score_opus":0.005984624248500986,"score_gpt":0.19484118159320568,"score_spread":0.1888565573447047,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4402455273","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99391437,0.000053053725,0.000045229728,0.000034791858,0.0050990204,0.0001643036,0.00005979427,0.00041348787,0.00021597881],"genre_scores_gemma":[0.9945961,0.0000800312,0.0046234233,0.0000102736985,0.0005142662,0.000015308406,0.0000056050326,0.000092518465,0.000062426014],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9988515,0.000001964725,0.00033394655,0.00029453408,0.0001946362,0.00032346087],"domain_scores_gemma":[0.999653,0.00005279163,0.000042320742,0.000117553,0.0000396994,0.000094671814],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00015042546,0.00029622644,0.00031503462,0.00010170978,0.000077929995,0.00028879396,0.0002432394,0.00012628413,0.000036502097],"category_scores_gemma":[0.000037227997,0.0002473145,0.00008436479,0.00023521758,0.00004645073,0.00017523991,0.00015118327,0.00040145696,0.0000021189483],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000025376163,0.0000058860774,0.0000015628219,0.00095450063,0.00006501324,0.0000025475015,0.000011205577,0.0177158,0.97836304,0.0021870632,0.0002749772,0.00039304348],"study_design_scores_gemma":[0.00010223959,0.000010411208,0.0000011195334,0.0005234011,0.000036600773,0.000014821149,0.000005122526,0.46852794,0.52922124,0.00015503782,0.0012353514,0.00016668062],"about_ca_topic_score_codex":0.0000043239697,"about_ca_topic_score_gemma":7.909774e-7,"teacher_disagreement_score":0.45081216,"about_ca_system_score_codex":0.00008812643,"about_ca_system_score_gemma":0.000012742643,"threshold_uncertainty_score":0.9999979},"labels":[],"label_agreement":null},{"id":"W4402596910","doi":"10.1134/s1063771023601474","title":"Analysis of Aeroacoustic Characteristics of a Supersonic Jet at Designed Conditions Based on Numerical Simulation Data","year":2024,"lang":"en","type":"article","venue":"Acoustical Physics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Supersonic speed; Jet (fluid); Aerospace engineering; Acoustics; Mechanics; Physics; Engineering","score_opus":0.024474492353131084,"score_gpt":0.28037417259110714,"score_spread":0.25589968023797605,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4402596910","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.12745477,0.00002424186,0.8685344,0.000010057484,0.00025658598,0.00012255389,0.0032191682,0.00013645228,0.00024179734],"genre_scores_gemma":[0.9959231,0.000013120915,0.0020926748,0.000028546341,0.00012251684,0.000006787218,0.0017474144,0.000052775726,0.000013046915],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9985971,0.000030486992,0.00044267235,0.000321479,0.00036275003,0.0002455142],"domain_scores_gemma":[0.9976169,0.001429106,0.000048334277,0.00072212244,0.00009256628,0.00009098542],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00014236788,0.00022005862,0.0004993092,0.00016152003,0.000049012357,0.000025843163,0.00029082113,0.000114676084,0.00016751884],"category_scores_gemma":[0.00019602885,0.00021182097,0.00016551896,0.00082105387,0.00012193509,0.000091570815,0.00008300407,0.00021596832,0.000021474212],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000219632,0.00012248436,0.00021878105,0.0002574563,0.00051936606,0.000010108121,0.000041579635,0.9823657,0.014509006,0.00063379743,0.00020430026,0.0010954011],"study_design_scores_gemma":[0.00011812264,0.000068710935,0.002834926,0.0000718192,0.0025427102,2.8356664e-7,0.000010728,0.9938026,0.0001487163,0.00018395187,0.000019680752,0.00019776663],"about_ca_topic_score_codex":0.0000038976714,"about_ca_topic_score_gemma":0.000001982538,"teacher_disagreement_score":0.86846834,"about_ca_system_score_codex":0.00011445936,"about_ca_system_score_gemma":0.00004941625,"threshold_uncertainty_score":0.86378086},"labels":[],"label_agreement":null},{"id":"W4402598324","doi":"10.1063/5.0224877","title":"Effects of axisymmetric confinement on vortical structures emanating from round turbulent jets","year":2024,"lang":"en","type":"article","venue":"Physics of Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Windsor","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Physics; Turbulence; Rotational symmetry; Mechanics; Vortex; Jet (fluid); Classical mechanics","score_opus":0.006974212667926227,"score_gpt":0.22456275876718004,"score_spread":0.21758854609925382,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4402598324","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9252562,0.0015481744,0.07098297,0.000020473071,0.0007709635,0.00014915336,0.00004248153,0.000093244846,0.0011363326],"genre_scores_gemma":[0.9977674,0.00007348317,0.0018397268,0.000012218401,0.00023967179,0.0000064695714,0.000017388751,0.000033581415,0.000010057978],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99913484,0.000010030149,0.00025786506,0.00015970347,0.0002801328,0.00015741774],"domain_scores_gemma":[0.99930483,0.0004189683,0.000020913583,0.00017770911,0.000036534388,0.00004106212],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000051494255,0.00015403981,0.00023573326,0.000069244415,0.00001744505,0.000024584515,0.00013375538,0.00005132852,0.000020616271],"category_scores_gemma":[0.000050222086,0.00014123497,0.00009261822,0.00022016367,0.00003821251,0.000036393765,0.00003541887,0.00016351341,0.0000066298085],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000016442309,0.00019950877,0.00007570224,0.0026573204,0.0007703576,0.000039376115,0.00084570906,0.22299667,0.46658948,0.22965296,0.0013713375,0.07478513],"study_design_scores_gemma":[0.00022672575,0.000106525586,0.0011144786,0.0002564641,0.00011474554,3.6437856e-7,0.000020099103,0.8373827,0.13285282,0.027612468,0.00012361039,0.00018902922],"about_ca_topic_score_codex":0.000026416936,"about_ca_topic_score_gemma":9.28691e-7,"teacher_disagreement_score":0.614386,"about_ca_system_score_codex":0.000044361022,"about_ca_system_score_gemma":0.000011873142,"threshold_uncertainty_score":0.5759395},"labels":[],"label_agreement":null},{"id":"W4402602649","doi":"10.1007/978-981-97-6211-8_24","title":"Flow Around Surface-Mounted Low-Aspect-Ratio Square Blocks","year":2024,"lang":"en","type":"book-chapter","venue":"Lecture notes in mechanical engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Saskatchewan","funders":"","keywords":"Square (algebra); Flow (mathematics); Surface (topology); Geometry; Aspect ratio (aeronautics); Geology; Mathematics; Materials science; Composite material","score_opus":0.005557078544772394,"score_gpt":0.20218739027544386,"score_spread":0.19663031173067147,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4402602649","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0012490811,0.0059399744,0.96699345,0.00017064181,0.0051888186,0.0006642324,0.00022815952,0.0019354123,0.017630214],"genre_scores_gemma":[0.97791207,0.0006108843,0.012082175,0.00008417724,0.0016694908,0.000033507098,0.00021582162,0.0008882682,0.006503628],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99733865,0.0000056212207,0.0007673464,0.0007353885,0.00046375796,0.00068921805],"domain_scores_gemma":[0.99871165,0.0003203526,0.000051831987,0.00067149836,0.00006224131,0.00018241964],"candidate_categories":["metaepi_narrow","research_integrity"],"consensus_categories":["research_integrity"],"category_scores_codex":[0.00019889952,0.001003194,0.00088309194,0.00029062293,0.000048118414,0.00016130297,0.00045490736,0.0012996714,0.0003131587],"category_scores_gemma":[0.00014999826,0.0010523027,0.00031696816,0.00019124104,0.000024546103,0.00006850836,0.00016268078,0.0029101814,0.0001559846],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000005353158,0.000008522631,2.5387266e-7,0.00058276975,0.00015867938,0.00024416015,0.000051445233,0.97777325,0.0043238187,0.0153001435,0.000092690774,0.0014589201],"study_design_scores_gemma":[0.00020361556,0.000042356387,3.6508766e-7,0.0012410254,0.00010521108,0.00003215681,0.0000018476767,0.9730957,0.0010004179,0.01769234,0.0055485805,0.0010363533],"about_ca_topic_score_codex":0.000020934913,"about_ca_topic_score_gemma":0.00036362148,"teacher_disagreement_score":0.976663,"about_ca_system_score_codex":0.0007627241,"about_ca_system_score_gemma":0.00006147904,"threshold_uncertainty_score":0.99999684},"labels":[],"label_agreement":null},{"id":"W4403005183","doi":"10.1017/jfm.2024.665","title":"A generalized wall-pressure spectral model for non-equilibrium boundary layers","year":2024,"lang":"en","type":"article","venue":"Journal of Fluid Mechanics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Office of Naval Research; College of Engineering, Michigan State University; Alliance de recherche numérique du Canada; Université de Sherbrooke; Michigan State University","keywords":"Mechanics; Boundary layer; Boundary (topology); Materials science; Thermodynamics; Physics; Mathematical analysis; Mathematics","score_opus":0.011080680608710935,"score_gpt":0.2355489138217241,"score_spread":0.22446823321301318,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4403005183","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.09440135,0.0037348971,0.8974935,0.00024137151,0.0035389024,0.00016427095,0.00008149452,0.00010412894,0.0002400806],"genre_scores_gemma":[0.9526798,0.0007227668,0.04497227,0.00010566417,0.00086847896,0.00000637863,0.0000069372704,0.00010986918,0.00052783225],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9988594,0.000007387646,0.0004426101,0.00012835424,0.0002542811,0.0003079839],"domain_scores_gemma":[0.99950457,0.000043414064,0.00005004981,0.0001667558,0.00010722418,0.00012801279],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00036880982,0.00019097066,0.0003000164,0.00013778248,0.0000418066,0.00014626604,0.00027544147,0.00013460139,0.000024928058],"category_scores_gemma":[0.000021417552,0.0001724759,0.00029546648,0.00011547247,0.000009151174,0.00020694431,0.000031482108,0.0003527186,0.0000045380198],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000029236522,0.000012709101,1.7257256e-7,0.00022135524,0.00022132431,0.000040843297,0.00015807318,0.74330765,0.23140313,0.0067648944,0.017293476,0.0005471135],"study_design_scores_gemma":[0.00040039298,0.00009339366,2.6830563e-7,0.000102646765,0.00019937416,0.00008091293,0.000016188365,0.97086835,0.0027029996,0.01604855,0.009298678,0.00018822221],"about_ca_topic_score_codex":6.549803e-7,"about_ca_topic_score_gemma":0.0000023047123,"teacher_disagreement_score":0.85827845,"about_ca_system_score_codex":0.00010414896,"about_ca_system_score_gemma":0.00014099179,"threshold_uncertainty_score":0.70333636},"labels":[],"label_agreement":null},{"id":"W4403286590","doi":"10.1016/j.jsv.2024.118771","title":"Shape considerations for the design of propellers with trailing edge serrations","year":2024,"lang":"en","type":"article","venue":"Journal of Sound and Vibration","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"Université de Sherbrooke; École de Technologie Supérieure","funders":"Natural Sciences and Engineering Research Council of Canada; Fonds de recherche du Québec – Nature et technologies; Alliance de recherche numérique du Canada; Université de Sherbrooke","keywords":"Trailing edge; Enhanced Data Rates for GSM Evolution; Marine engineering; Structural engineering; Engineering; Aerospace engineering; Acoustics; Mathematics; Physics; Telecommunications","score_opus":0.03373772619851089,"score_gpt":0.24062959811872098,"score_spread":0.20689187192021008,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4403286590","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.033010624,0.000704824,0.96557254,0.00026040192,0.00021393337,0.00013735112,0.00000653039,0.000010620403,0.00008318978],"genre_scores_gemma":[0.9800887,0.00012649687,0.01959969,0.000013118934,0.0001444842,0.000002776013,9.772629e-7,0.000009147746,0.000014611119],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996889,0.0000066490716,0.00016985819,0.000032188174,0.00005923611,0.000043153603],"domain_scores_gemma":[0.9995486,0.00029717895,0.00003384228,0.000030170579,0.00007467409,0.000015491412],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017608063,0.0000450336,0.00006520319,0.000031307576,0.00008472681,0.000094795105,0.000021834288,0.000021721522,0.000009880573],"category_scores_gemma":[0.000029088711,0.000026580285,0.000022542128,0.000049989234,0.000025655747,0.00016284427,0.0000019623112,0.0000760126,1.66479e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000009882747,0.000007211807,0.000008821654,0.000083770254,0.00008696686,0.0000013760276,0.0009244379,0.9718431,0.01695279,0.007899431,0.00053019775,0.0016519825],"study_design_scores_gemma":[0.00010668556,0.00008998931,0.000046981964,0.00005113281,0.00006280571,0.00003230093,0.00029410023,0.9936403,0.0003686459,0.0051259575,0.00014447529,0.000036597066],"about_ca_topic_score_codex":1.8139221e-7,"about_ca_topic_score_gemma":0.00000429944,"teacher_disagreement_score":0.94707805,"about_ca_system_score_codex":0.0000072678363,"about_ca_system_score_gemma":0.00004081222,"threshold_uncertainty_score":0.108391255},"labels":[],"label_agreement":null},{"id":"W4403684527","doi":"10.1016/j.apacoust.2024.110354","title":"Characterization of noise sources in two- and three-element high-lift airfoil configurations","year":2024,"lang":"en","type":"article","venue":"Applied Acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke; University of Toronto","funders":"Natural Sciences and Engineering Research Council of Canada; Ontario Research Foundation; Bombardier","keywords":"Airfoil; Lift (data mining); Acoustics; Aerospace engineering; Noise (video); Engineering; Structural engineering; Computer science; Physics; Artificial intelligence","score_opus":0.0047843311088263205,"score_gpt":0.20529929871748348,"score_spread":0.20051496760865717,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4403684527","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.72890896,0.00007339855,0.26953575,0.000027217351,0.00027285173,0.0001558653,0.00010645759,0.00010733132,0.0008122038],"genre_scores_gemma":[0.99786377,0.00019413742,0.0015978107,0.000020090092,0.00012436582,0.000029465034,0.00011304326,0.00003525166,0.000022077864],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993006,0.0000032756611,0.0002740276,0.00014666334,0.00011884936,0.00015658812],"domain_scores_gemma":[0.9997305,0.000058729765,0.000024319894,0.00012742013,0.00002229052,0.000036720667],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00009000595,0.00013124934,0.00015660915,0.000100765305,0.000030505133,0.00004914763,0.00007156542,0.000053328175,0.000029660203],"category_scores_gemma":[0.0000062209574,0.0001343414,0.000015932877,0.00016472953,0.000043378986,0.00004234337,0.000029445195,0.00014607693,0.000007868372],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000002654359,0.000017707785,0.00011170779,0.000233749,0.000026823496,0.0000043246805,0.00024085435,0.19267353,0.77148354,0.029578745,0.000036402824,0.0055899634],"study_design_scores_gemma":[0.00023600625,0.000011982531,0.0048605357,0.00006565407,0.000052041454,0.0000014208665,0.000074336014,0.9871308,0.0050731334,0.0020167592,0.00029352668,0.00018380534],"about_ca_topic_score_codex":0.000010884071,"about_ca_topic_score_gemma":0.000043658838,"teacher_disagreement_score":0.79445726,"about_ca_system_score_codex":0.000032965312,"about_ca_system_score_gemma":0.00001709586,"threshold_uncertainty_score":0.5478284},"labels":[],"label_agreement":null},{"id":"W4404004162","doi":"10.31857/s0320791924030111","title":"Analysis of aeroacoustic characteristics of a supersonic jet at designed conditions based on numerical simulation","year":2024,"lang":"en","type":"article","venue":"Акустический журнал","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Supersonic speed; Jet (fluid); Acoustics; Computer simulation; Mechanics; Aerospace engineering; Physics; Structural engineering; Engineering","score_opus":0.009919046908965232,"score_gpt":0.245663991714037,"score_spread":0.23574494480507177,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4404004162","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6432449,0.000068604946,0.3547133,0.000014578149,0.00031222287,0.00013281347,0.0008183632,0.00015629941,0.0005388958],"genre_scores_gemma":[0.998648,0.000015120665,0.0007367458,0.00002312572,0.000051080813,0.00001446602,0.0004041634,0.000046489593,0.00006080796],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99880695,0.000031040232,0.00043876912,0.00022349297,0.0002856239,0.00021409923],"domain_scores_gemma":[0.9988809,0.00058723224,0.00005444997,0.00032466918,0.00008033989,0.00007236533],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001469436,0.00019773829,0.00044045845,0.00045593895,0.00004637346,0.000022150643,0.00012800239,0.00011523952,0.00045835556],"category_scores_gemma":[0.00008546981,0.00019386025,0.00024087241,0.0008201112,0.00006214987,0.000047251153,0.000021237955,0.0001495808,0.000023990602],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000020108526,0.000057708556,0.0012377995,0.00019893976,0.0004359044,0.000011086745,0.00012876472,0.98026973,0.016703658,0.00030366748,0.00009571766,0.0005368856],"study_design_scores_gemma":[0.00013296117,0.0000747777,0.015674768,0.00008426848,0.0010897656,4.814328e-7,0.000017209102,0.9822182,0.0004355382,0.00002866415,0.00006869518,0.00017463615],"about_ca_topic_score_codex":0.0000059063514,"about_ca_topic_score_gemma":0.000008768896,"teacher_disagreement_score":0.35540307,"about_ca_system_score_codex":0.00016145897,"about_ca_system_score_gemma":0.000036613186,"threshold_uncertainty_score":0.79053915},"labels":[],"label_agreement":null},{"id":"W4404240149","doi":"10.3390/en17225597","title":"Flow Separation Control and Aeroacoustic Effects of a Leading-Edge Slat over a Wind Turbine Blade","year":2024,"lang":"en","type":"article","venue":"Energies","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure; Université du Québec à Montréal","funders":"","keywords":"Separation (statistics); Blade (archaeology); Turbine; Turbine blade; Flow separation; Flow (mathematics); Flow control (data); Leading edge; Marine engineering; Acoustics; Enhanced Data Rates for GSM Evolution; Aerodynamics; Materials science; Engineering; Geology; Environmental science; Aerospace engineering; Mechanics; Mechanical engineering; Physics; Computer science; Telecommunications; Boundary layer","score_opus":0.002654754775295259,"score_gpt":0.20909642696354053,"score_spread":0.20644167218824527,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4404240149","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9634912,0.0057693,0.02875997,0.000017207572,0.0009197543,0.000110518835,0.000022338985,0.00020949113,0.0007002009],"genre_scores_gemma":[0.9986889,0.0002243446,0.00045872421,0.0000140196935,0.00017752642,0.000009241332,0.0000083548375,0.000033777636,0.000385143],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994581,0.000010004409,0.0001446595,0.00013657333,0.00010086003,0.00014984733],"domain_scores_gemma":[0.9996293,0.00019641308,0.0000125578745,0.00011234157,0.0000148232575,0.00003454921],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00005839746,0.00013820206,0.00019214256,0.000078659694,0.000026287003,0.000054222077,0.000051909177,0.00007470036,0.000010588297],"category_scores_gemma":[0.000032367512,0.0001258214,0.00004108553,0.00010311517,0.000042634896,0.00009161,0.000017742788,0.00011403881,0.000006731597],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000044623725,0.000005695142,0.000027235083,0.0005417713,0.000076857985,0.000018417308,0.00028901317,0.8475541,0.14744437,0.0010068741,0.0013174457,0.0017137901],"study_design_scores_gemma":[0.00029095318,0.00003967374,0.0004831706,0.00015451894,0.00008468493,0.000005124323,0.000011216327,0.9937598,0.004136076,0.00034067527,0.0005586308,0.00013547248],"about_ca_topic_score_codex":0.0000045246916,"about_ca_topic_score_gemma":0.0000087708695,"teacher_disagreement_score":0.14620574,"about_ca_system_score_codex":0.000028134806,"about_ca_system_score_gemma":0.000009982557,"threshold_uncertainty_score":0.5130848},"labels":[],"label_agreement":null},{"id":"W4405416348","doi":"10.1007/978-3-031-78151-3_3","title":"The Effect of Background Turbulence on the Dynamics of Turbulent Jets and Entrainment Processes Across the Turbulent/Turbulent Interface","year":2024,"lang":"en","type":"book-chapter","venue":"IUTAM bookseries","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"","keywords":"Turbulence; Entrainment (biomusicology); Mechanics; Physics; Acoustics","score_opus":0.008381682113210996,"score_gpt":0.23092230305573958,"score_spread":0.22254062094252858,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4405416348","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6219343,0.1409636,0.002610625,0.014253359,0.0074690757,0.011731251,0.0033206665,0.0012386267,0.19647849],"genre_scores_gemma":[0.92726964,0.011409111,0.000038527087,0.000088847046,0.00023357022,0.00015982281,0.00003804489,0.00027017103,0.06049226],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"not_applicable","domain_scores_codex":[0.99745125,0.00003972621,0.00078589085,0.00049101585,0.0007057617,0.00052635215],"domain_scores_gemma":[0.9968312,0.0016865213,0.0002930416,0.0009691229,0.00014034414,0.00007979623],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00068013964,0.0008294854,0.00068590103,0.000049427137,0.00034306585,0.00028038258,0.00095204875,0.00030818617,0.00004169979],"category_scores_gemma":[0.00008456437,0.00041453293,0.00024903583,0.0000693293,0.0013117963,0.00007185294,0.00035162867,0.0010142212,0.000020080019],"study_design_candidate":"theoretical_or_conceptual","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0011401888,0.000114602284,0.00003515499,0.021793962,0.0057108654,0.00021907482,0.018136147,0.10934644,0.0009502747,0.8092283,0.0133191375,0.020005818],"study_design_scores_gemma":[0.0021704903,0.005978704,0.000094459225,0.021482382,0.0030644801,0.0008560264,0.0076199635,0.34815282,0.033034604,0.10498604,0.46707192,0.0054881205],"about_ca_topic_score_codex":0.0000088972665,"about_ca_topic_score_gemma":0.00010472531,"teacher_disagreement_score":0.7042423,"about_ca_system_score_codex":0.00022650162,"about_ca_system_score_gemma":0.000054123437,"threshold_uncertainty_score":0.99983066},"labels":[],"label_agreement":null},{"id":"W4406398425","doi":"10.1016/0967-0653(93)95668-v","title":"10.1016/0967-0653(93)95668-v","year":2000,"lang":"en","type":"article","venue":"Time to knit","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Reduction (mathematics); Noise reduction; Flow (mathematics); Planar; Noise (video); Acoustics; Materials science; Mechanics; Computer science; Physics; Mathematics; Geometry; Artificial intelligence; Computer graphics (images)","score_opus":0.003032541136601945,"score_gpt":0.14536738184541423,"score_spread":0.14233484070881228,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4406398425","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0008557589,0.000052868174,0.00007290736,0.000032460295,0.0000071569675,0.00010457193,0.000029664434,0.00037024473,0.99847436],"genre_scores_gemma":[0.001456581,0.0000010468345,0.0005817856,0.0000143435345,0.0002008049,0.000012863091,0.000022385053,0.000054951364,0.9976552],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.999276,0.0000071805816,0.00015816824,0.00015336565,0.00012122172,0.00028405662],"domain_scores_gemma":[0.9995453,0.00002647546,0.000008064464,0.00027646168,0.000019793728,0.00012395506],"candidate_categories":["insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.00007258412,0.00015284572,0.0001443439,0.00004575541,0.00004781957,0.00004029818,0.00020530066,0.00007233878,0.99248475],"category_scores_gemma":[0.000011499696,0.00016187345,0.000048113106,0.0001388162,0.000016246824,0.000054881355,0.000025383655,0.00014059155,0.9927773],"study_design_candidate":"not_applicable","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000087618055,0.00001928844,3.9839836e-8,0.000015751008,0.000025247351,0.000009761149,0.000015764337,0.13897142,0.00016085317,0.0000048990264,0.2038109,0.6569573],"study_design_scores_gemma":[0.000088351284,0.000026264106,0.0000057197954,0.0000110596475,0.000010674973,0.000003846268,4.7145284e-7,0.13841979,0.00002959066,0.000017688002,0.86119884,0.00018769436],"about_ca_topic_score_codex":0.000004151479,"about_ca_topic_score_gemma":1.9275613e-7,"teacher_disagreement_score":0.657388,"about_ca_system_score_codex":0.000047938895,"about_ca_system_score_gemma":0.0000071989994,"threshold_uncertainty_score":0.66010076},"labels":[],"label_agreement":null},{"id":"W4406532766","doi":"10.1016/0967-0653(94)93858-x","title":"10.1016/0967-0653(94)93858-x","year":2000,"lang":"en","type":"article","venue":"Time to knit","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Acoustics; Environmental science; Power (physics); Dual (grammatical number); Boundary layer; Layer (electronics); Remote sensing; Geology; Materials science; Physics; Art; Mechanics","score_opus":0.0034321534328955695,"score_gpt":0.1510354233784052,"score_spread":0.14760326994550962,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4406532766","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0009339427,0.000073342606,0.00007426748,0.000034315464,0.0000073103897,0.00010579499,0.000031936324,0.00038872397,0.9983504],"genre_scores_gemma":[0.0015482747,0.0000010984371,0.0005776659,0.000016573476,0.0002029768,0.000012900336,0.000021675041,0.000056178946,0.99756265],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.99925804,0.000007513576,0.00015937007,0.00015525128,0.00013011202,0.00028972316],"domain_scores_gemma":[0.99953705,0.000027446005,0.00000813692,0.00028055836,0.000020916112,0.00012590869],"candidate_categories":["insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.00007512147,0.00015352017,0.00014602063,0.000046433626,0.000049285456,0.000039845654,0.00020924606,0.00007466362,0.9922104],"category_scores_gemma":[0.000012740365,0.00016365957,0.000048951457,0.00014640628,0.000016689555,0.000053761025,0.00002527387,0.00014463635,0.9929915],"study_design_candidate":"not_applicable","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000008283093,0.000018021234,3.137688e-8,0.000014374256,0.00002344079,0.00000960622,0.000014704236,0.11531048,0.0001453408,0.0000039712336,0.24204582,0.6424059],"study_design_scores_gemma":[0.00009172289,0.000026894182,0.0000053610484,0.000011926432,0.000011065685,0.000004042144,4.556192e-7,0.13431895,0.000028887103,0.000019102483,0.8652903,0.00019131687],"about_ca_topic_score_codex":0.0000043225987,"about_ca_topic_score_gemma":2.746181e-7,"teacher_disagreement_score":0.6422146,"about_ca_system_score_codex":0.000046581205,"about_ca_system_score_gemma":0.0000071711966,"threshold_uncertainty_score":0.6673844},"labels":[],"label_agreement":null},{"id":"W4406999635","doi":"10.1016/j.jsv.2025.118978","title":"Installation effects on airfoil self-noise estimated by direct numerical simulations","year":2025,"lang":"en","type":"article","venue":"Journal of Sound and Vibration","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure; Université de Sherbrooke","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Airfoil; Noise (video); Acoustics; Direct numerical simulation; Mechanics; Physics; Environmental science; Aerospace engineering; Marine engineering; Engineering; Computer science; Reynolds number; Turbulence","score_opus":0.004788885615491642,"score_gpt":0.23276925966471623,"score_spread":0.22798037404922458,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4406999635","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7540851,0.00018957052,0.24351153,0.00008732169,0.0003797229,0.00006310513,0.0000060971674,0.00005211295,0.0016254027],"genre_scores_gemma":[0.997962,0.000060242724,0.0017998908,0.00005563101,0.000080815094,5.48334e-7,0.000010725089,0.000008523829,0.000021599082],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99956995,0.000015665724,0.00020005647,0.00005296719,0.000093957104,0.00006742071],"domain_scores_gemma":[0.99967104,0.00014700987,0.000054986787,0.000045466084,0.000047818856,0.000033676577],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00007105506,0.00007645914,0.000114891016,0.000084859,0.000075697855,0.00006252615,0.00003123517,0.000055594628,0.0000037793884],"category_scores_gemma":[0.000050093364,0.00006780226,0.00002672019,0.00012628283,0.0000069232406,0.00015348586,0.0000058534233,0.000118184544,0.0000010149014],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000019632042,0.00005214022,0.001854926,0.00009009272,0.000069777176,0.0000025342097,0.00010553018,0.96693814,0.021193516,0.0007659458,0.0011646971,0.0077430625],"study_design_scores_gemma":[0.0003260613,0.00007634361,0.004902193,0.00007017039,0.00003933006,0.0000022496492,0.000006687569,0.9912872,0.0012044739,0.0016062931,0.0004100593,0.00006898572],"about_ca_topic_score_codex":6.456418e-7,"about_ca_topic_score_gemma":8.653428e-7,"teacher_disagreement_score":0.24387689,"about_ca_system_score_codex":0.000052260035,"about_ca_system_score_gemma":0.000011953365,"threshold_uncertainty_score":0.27648962},"labels":[],"label_agreement":null},{"id":"W4407414528","doi":"10.2514/6.2025-1682","title":"The Effect of Axisymmetric Nozzle Forcing on Turbulent Three-Dimensional Wall Jet Development","year":2025,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of New Brunswick","funders":"","keywords":"Rotational symmetry; Nozzle; Turbulence; Mechanics; Jet (fluid); Forcing (mathematics); Physics; Aerospace engineering; Classical mechanics; Atmospheric sciences; Engineering; Thermodynamics","score_opus":0.004217310537993651,"score_gpt":0.2053433506656961,"score_spread":0.20112604012770244,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4407414528","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.95439565,0.00042056374,0.021947501,0.0001406861,0.0007743929,0.00031283905,0.0000018710313,0.00013436213,0.021872137],"genre_scores_gemma":[0.9978396,0.000013251115,0.0013501563,0.000046501184,0.000016025944,0.000018901052,0.0000039135953,0.000014355324,0.00069725275],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992781,0.000010284838,0.0002214231,0.00011460386,0.00018061137,0.0001949729],"domain_scores_gemma":[0.9992192,0.00051601115,0.000019702122,0.00019096522,0.000027196787,0.000026927983],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002935339,0.00013733038,0.00014835823,0.00010098925,0.000111536174,0.000017731689,0.00016051804,0.00005077345,0.000015094623],"category_scores_gemma":[0.000050889907,0.00008159735,0.00005293504,0.00024556054,0.000017567128,0.000014943061,0.000041497173,0.00013192868,0.000017142842],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00013135497,0.00004534528,0.0035527954,0.00031537956,0.00035774955,0.000008528909,0.000044070504,0.8863142,0.0022500078,0.015461353,0.011616319,0.07990286],"study_design_scores_gemma":[0.0004401658,0.00015784414,0.004292765,0.000112441885,0.000022815117,9.0384674e-7,0.0000037371576,0.9650144,0.02271738,0.0003494087,0.0067210007,0.00016715292],"about_ca_topic_score_codex":0.000010381345,"about_ca_topic_score_gemma":0.000067192406,"teacher_disagreement_score":0.079735704,"about_ca_system_score_codex":0.00009353917,"about_ca_system_score_gemma":0.000018893155,"threshold_uncertainty_score":0.33274433},"labels":[],"label_agreement":null},{"id":"W4407782581","doi":"10.2514/1.j064364","title":"Gradient-Free Aeroacoustic Shape Optimization Using Large Eddy Simulation","year":2025,"lang":"en","type":"article","venue":"AIAA Journal","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Concordia University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Airfoil; Freestream; Lift coefficient; Drag coefficient; Shape optimization; Mach number; Lift-to-drag ratio; Reynolds number; Drag; Physics; Acoustics; Mechanics; Turbulence; Finite element method","score_opus":0.008977434531407327,"score_gpt":0.24582227788305724,"score_spread":0.2368448433516499,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4407782581","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.1340512,0.00023251818,0.8632615,0.000032622967,0.0014827218,0.000066186985,0.000010881919,0.000079377365,0.00078294304],"genre_scores_gemma":[0.96713144,0.00009879294,0.032325123,0.00006959997,0.00026459608,0.0000011295791,0.000008453274,0.000027844624,0.00007303271],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991715,0.000017825192,0.00028131375,0.00010265736,0.00015758279,0.00026911194],"domain_scores_gemma":[0.9995311,0.000057988684,0.000050359104,0.00019281227,0.00010255372,0.00006521526],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020710689,0.00012954039,0.00013037129,0.00016446586,0.00023449576,0.000110178684,0.00020524945,0.00008499064,0.000184792],"category_scores_gemma":[0.00011909562,0.000133621,0.000060751852,0.0002379905,0.000013892196,0.00017004948,0.0000535903,0.00029839028,0.000004272114],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000037758869,0.000017842236,0.00024564468,0.000021611178,0.000037739235,0.00000875643,0.000042798616,0.99691784,0.0003784227,0.00034988884,0.00052670547,0.0014489838],"study_design_scores_gemma":[0.00050653145,0.000010380211,0.00024566817,0.00007025978,0.00006379757,0.000017090608,0.000043388223,0.99721825,0.000010988944,0.0014570457,0.0002294738,0.00012710578],"about_ca_topic_score_codex":0.0000010121952,"about_ca_topic_score_gemma":0.0000025373056,"teacher_disagreement_score":0.83308023,"about_ca_system_score_codex":0.00016224255,"about_ca_system_score_gemma":0.000031111736,"threshold_uncertainty_score":0.54489064},"labels":[],"label_agreement":null},{"id":"W4407905785","doi":"10.3233/978-1-61499-063-5-138","title":"European Aviation Noise Research Network (X-NOISE)","year":2012,"lang":"en","type":"book-chapter","venue":"IOS Press eBooks","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Noise (video); Aviation; Aeronautics; Environmental science; Acoustics; Computer science; Telecommunications; Aerospace engineering; Engineering; Physics; Artificial intelligence","score_opus":0.05571856845116855,"score_gpt":0.2609152100665923,"score_spread":0.20519664161542375,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4407905785","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.000057275705,0.0024195248,0.0033316333,0.000003932095,0.0013890567,0.00044472676,0.00006968976,0.00038768206,0.99189645],"genre_scores_gemma":[0.122539416,0.0008350535,0.00087093015,0.000039412666,0.0063643847,0.000040345083,0.00012983358,0.00060703146,0.8685736],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"not_applicable","domain_scores_codex":[0.99787647,0.000063559426,0.0004135902,0.0003398029,0.0005385098,0.0007680535],"domain_scores_gemma":[0.9986753,0.00012676202,0.00007991045,0.00076292985,0.00015884347,0.00019629142],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00089689065,0.0004070362,0.0003296889,0.00011101823,0.0001867399,0.00011350393,0.000486087,0.0003572952,0.00009469588],"category_scores_gemma":[0.000017048467,0.00043698095,0.00012847481,0.000009730557,0.00010388918,0.00004765234,0.00031967988,0.0013309189,0.0003824036],"study_design_candidate":"not_applicable","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000029579844,0.00002243424,0.000008615176,0.00070299424,0.0004172155,0.00014553191,0.0007037088,0.06658478,0.0011965808,0.73338664,0.07680398,0.11999796],"study_design_scores_gemma":[0.00020601074,0.000028564496,0.00005017803,0.00043757723,0.00009830893,0.000007643596,0.0000023184173,0.022298273,0.000054289692,0.010447932,0.96562856,0.00074032013],"about_ca_topic_score_codex":0.000011808981,"about_ca_topic_score_gemma":0.000013603296,"teacher_disagreement_score":0.8888246,"about_ca_system_score_codex":0.00013594386,"about_ca_system_score_gemma":0.00001977142,"threshold_uncertainty_score":0.9998082},"labels":[],"label_agreement":null},{"id":"W4408179807","doi":"10.1016/j.ijheatmasstransfer.2025.126867","title":"LIF measurement of turbulent horizontal dense jets in stagnant ambient","year":2025,"lang":"en","type":"article","venue":"International Journal of Heat and Mass Transfer","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Ottawa","funders":"","keywords":"Turbulence; Mechanics; Materials science; Jet (fluid); Environmental science; Meteorology; Atmospheric sciences; Physics","score_opus":0.007631700246244835,"score_gpt":0.2201592951760483,"score_spread":0.21252759492980344,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4408179807","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9168413,0.0011100943,0.08005126,0.00047911383,0.0010285354,0.000057692007,0.000011013125,0.000005334644,0.00041565395],"genre_scores_gemma":[0.99840784,0.0011626803,0.0003123774,0.000026765469,0.0000682069,0.0000014546564,9.498297e-7,0.0000066267894,0.000013094705],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99912053,0.000010085239,0.00036846517,0.000055888875,0.00035477083,0.00009028206],"domain_scores_gemma":[0.9996806,0.000020964642,0.000010649329,0.000040453124,0.00021243637,0.000034934325],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021908498,0.00008022069,0.00015029208,0.00022314682,0.000008584023,0.000016455875,0.00012174005,0.000031236905,0.0000101542955],"category_scores_gemma":[0.000014170762,0.00006879086,0.00006285958,0.00005344098,0.000019771927,0.000054607517,0.000007720411,0.0001413742,2.3277435e-7],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00058397173,0.0004718946,0.008718148,0.0002912623,0.0010854317,0.0005510838,0.00092227827,0.18196914,0.7650362,0.011580093,0.0005972005,0.028193269],"study_design_scores_gemma":[0.021927575,0.0017705518,0.121390045,0.007483804,0.00050119904,0.0005733645,0.0013986123,0.4930036,0.30097786,0.019036913,0.030356878,0.0015796154],"about_ca_topic_score_codex":0.000012332351,"about_ca_topic_score_gemma":0.000045428813,"teacher_disagreement_score":0.46405837,"about_ca_system_score_codex":0.0001620842,"about_ca_system_score_gemma":0.00005293367,"threshold_uncertainty_score":0.280521},"labels":[],"label_agreement":null},{"id":"W4408468927","doi":"10.2139/ssrn.5179883","title":"On the Effect of Frequency Dependence and Anisotropy On Surface Pressure Spectra Towards Improved Modelling Of Trailing Edge Noise","year":2025,"lang":"en","type":"preprint","venue":"SSRN Electronic Journal","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto","funders":"","keywords":"Trailing edge; Anisotropy; Noise (video); Spectral line; Enhanced Data Rates for GSM Evolution; Frequency dependence; Acoustics; Materials science; Condensed matter physics; Physics; Mechanics; Nuclear magnetic resonance; Optics; Engineering; Computer science; Telecommunications","score_opus":0.006881595428187667,"score_gpt":0.2142285517025186,"score_spread":0.20734695627433092,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4408468927","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6848333,0.0069047497,0.30615583,0.000046306657,0.0005147646,0.0004209201,0.00008128869,0.000039936436,0.0010029009],"genre_scores_gemma":[0.98923874,0.009291687,0.0011845536,0.0000047264325,0.00012053569,0.000006361177,0.000004123282,0.000045881003,0.00010340034],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99770266,0.00011147904,0.00051449327,0.00031490266,0.0003338343,0.0010226103],"domain_scores_gemma":[0.99883944,0.0003438717,0.0002428648,0.00042868312,0.00008984805,0.00005530937],"candidate_categories":["metaepi_narrow","research_integrity"],"consensus_categories":[],"category_scores_codex":[0.0015989802,0.0004117908,0.0005819489,0.00010578125,0.00010159567,0.00004451317,0.0005894331,0.00029980182,0.000007898049],"category_scores_gemma":[0.00009406295,0.00030506554,0.00022160186,0.00010678547,0.00006227538,0.00004141606,0.00010823717,0.0048713805,4.3782129e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000081086364,0.000018664907,0.00003295243,0.00044121518,0.0004415098,0.0000018256393,0.00009882648,0.95870477,0.008018121,0.030115774,0.0000037487937,0.002041516],"study_design_scores_gemma":[0.00040849877,0.00058576127,0.000015485031,0.0005972207,0.00025790202,0.000015601794,0.00004961134,0.90865755,0.007413522,0.0817495,0.000002375886,0.00024695933],"about_ca_topic_score_codex":0.00008119476,"about_ca_topic_score_gemma":0.000063398766,"teacher_disagreement_score":0.30497128,"about_ca_system_score_codex":0.0002864783,"about_ca_system_score_gemma":0.0006650486,"threshold_uncertainty_score":0.99994016},"labels":[],"label_agreement":null},{"id":"W4409146450","doi":"10.1063/5.0259952","title":"Analysis and mitigation of post-bore noises in modeling mixed flows in closed conduits","year":2025,"lang":"en","type":"article","venue":"Physics of Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Ottawa; Environment and Climate Change Canada","funders":"","keywords":"Physics; Electrical conduit; Mechanics; Statistical physics; Mechanical engineering","score_opus":0.006572075711258166,"score_gpt":0.22633596228116803,"score_spread":0.21976388656990986,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4409146450","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.91073745,0.0001870427,0.08864998,0.00001235937,0.000064001,0.00006886539,0.00003520668,0.000012089097,0.00023298607],"genre_scores_gemma":[0.9974043,0.00007944218,0.0024458712,0.00000632874,0.000010559691,0.0000048528223,0.000035670044,0.000008532671,0.000004489321],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99941903,0.000011064121,0.00028370073,0.00010603158,0.00008129632,0.00009889804],"domain_scores_gemma":[0.99970686,0.00005136419,0.0000202989,0.0001331087,0.00007397737,0.000014382229],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00009231494,0.00008775529,0.000266592,0.00020439479,0.000008719858,0.000006009763,0.00007545303,0.000050055038,0.0000014406802],"category_scores_gemma":[0.000026455078,0.00009937964,0.000051078026,0.0006551377,0.000021089549,0.00006780525,0.000027269107,0.000086511376,1.4494648e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000049647897,0.000028157367,0.005795659,0.00014249537,0.000081463426,5.3083284e-7,0.00021996653,0.8479253,0.14040256,0.0013492199,0.000002171315,0.004047498],"study_design_scores_gemma":[0.00026750556,0.000007985173,0.006392856,0.00007126845,0.00007800907,2.2208775e-8,0.00006969846,0.98066634,0.008284163,0.004086515,6.552814e-7,0.000074982265],"about_ca_topic_score_codex":0.00008843079,"about_ca_topic_score_gemma":0.0003186544,"teacher_disagreement_score":0.13274102,"about_ca_system_score_codex":0.000024671828,"about_ca_system_score_gemma":0.000016294653,"threshold_uncertainty_score":0.40525842},"labels":[],"label_agreement":null},{"id":"W4409305202","doi":"10.24135/ijcmr.v11i1.141","title":"Piano Dreamscapes Ice-Flow Isolation - A case study in binaural mixing for multi-speaker arrays","year":2025,"lang":"en","type":"article","venue":"International Journal of Creative Media Research","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Concordia University","funders":"","keywords":"Piano; Binaural recording; Mixing (physics); Isolation (microbiology); Acoustics; Flow (mathematics); Speech recognition; Computer science; Geology; Physics; Mechanics; Biology","score_opus":0.07198303855685297,"score_gpt":0.4072547385842656,"score_spread":0.33527170002741263,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4409305202","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8050038,0.00019972802,0.1922705,0.0002028184,0.0011012314,0.0003731985,0.000029193505,0.000012762066,0.00080676563],"genre_scores_gemma":[0.98525655,0.00007885768,0.014069298,0.000009570072,0.00033241024,0.000038038437,0.0000075345315,0.000020207435,0.0001875358],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9983393,0.00012577063,0.00051637937,0.00013913236,0.00062796293,0.00025144266],"domain_scores_gemma":[0.9973072,0.0010302772,0.00007560167,0.00009535953,0.0014216099,0.00006997507],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0015771176,0.00012583112,0.0002243617,0.0009869945,0.00007214177,0.00010948064,0.0003656945,0.00006306841,0.000040561277],"category_scores_gemma":[0.0012487255,0.00011256083,0.00008424105,0.00032653922,0.00006957714,0.00023261439,0.00006858999,0.00056506426,0.0000028017505],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.002143473,0.0037687356,0.11485452,0.00029003303,0.0033141363,0.016812576,0.05997808,0.62407225,0.024470465,0.0048006834,0.0048417603,0.1406533],"study_design_scores_gemma":[0.0029014375,0.00016533234,0.008213732,0.00023071088,0.000021344016,0.00016535773,0.011919631,0.9746512,0.000338578,0.0009722834,0.00030128568,0.00011908169],"about_ca_topic_score_codex":0.000098597295,"about_ca_topic_score_gemma":0.0009427375,"teacher_disagreement_score":0.350579,"about_ca_system_score_codex":0.00046720973,"about_ca_system_score_gemma":0.00012448298,"threshold_uncertainty_score":0.45900974},"labels":[],"label_agreement":null},{"id":"W4410436665","doi":"10.1063/5.0264550","title":"Flow characteristics of three-dimensional offset jet over surface-mounted ribs using large-eddy simulation","year":2025,"lang":"en","type":"article","venue":"Physics of Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Dalhousie University","funders":"","keywords":"Physics; Offset (computer science); Large eddy simulation; Mechanics; Jet (fluid); Flow (mathematics); Detached eddy simulation; Vortex; Rib cage; Computational fluid dynamics; Turbulence; Reynolds-averaged Navier–Stokes equations; Structural engineering","score_opus":0.01181207598368777,"score_gpt":0.262875123899706,"score_spread":0.25106304791601824,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4410436665","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6783964,0.00005518684,0.32056233,0.0000041477233,0.00039072343,0.00008077772,0.00038889877,0.00003674318,0.0000848199],"genre_scores_gemma":[0.99246377,0.000008527897,0.0072269975,0.000018837742,0.000088234265,9.6686e-7,0.00015223137,0.000028354176,0.000012082445],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9990556,0.000010954905,0.0003822976,0.00013928792,0.00022162602,0.0001901867],"domain_scores_gemma":[0.9993082,0.00012053229,0.000068903035,0.00027566342,0.000197647,0.0000289971],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000120646306,0.00017122547,0.00032447255,0.000046585094,0.000046703644,0.000011254769,0.00012629021,0.000089746056,0.000024344587],"category_scores_gemma":[0.00003193197,0.0001825666,0.00009392084,0.00024969366,0.00004330074,0.00010012449,0.000072738294,0.00014108222,0.0000025673962],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000013844288,0.00007214249,0.0024037703,0.0001531647,0.00008338799,6.80339e-7,0.000045645833,0.9171506,0.077939674,0.0014199006,0.00008822828,0.00062892283],"study_design_scores_gemma":[0.0003293855,0.000013732113,0.005088126,0.00011849061,0.0000651742,1.3153254e-7,0.0000038086257,0.98991,0.0027134456,0.001518462,0.00009404314,0.00014521339],"about_ca_topic_score_codex":0.000016030805,"about_ca_topic_score_gemma":0.000004186272,"teacher_disagreement_score":0.3140674,"about_ca_system_score_codex":0.000057215893,"about_ca_system_score_gemma":0.000038384584,"threshold_uncertainty_score":0.74448496},"labels":[],"label_agreement":null},{"id":"W4412068278","doi":"10.3390/fluids10070177","title":"Experimental Investigation of the Entrainment Mechanism in Circular and Lobed Hemispherical Jets","year":2025,"lang":"en","type":"article","venue":"Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"SAIT Polytechnic","funders":"","keywords":"Entrainment (biomusicology); Mechanism (biology); Mechanics; Physics; Optics; Acoustics","score_opus":0.004254884354616991,"score_gpt":0.19388106815982173,"score_spread":0.18962618380520474,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4412068278","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9869904,0.00034547554,0.011446991,0.00004407277,0.00021506807,0.00009227248,0.0000024007475,0.000017790882,0.00084556156],"genre_scores_gemma":[0.999175,0.000014430952,0.0007028228,0.000058903166,0.000009648756,0.000009653459,0.0000014877425,0.000005766496,0.000022287031],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9996627,0.000009406004,0.000111971545,0.000069699396,0.00006999241,0.00007623462],"domain_scores_gemma":[0.99986154,0.000011614193,0.0000064692204,0.00009826026,0.000005270998,0.00001684464],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000055765093,0.00005625884,0.000069753325,0.000013779561,0.000015601716,0.0000062235404,0.00006407753,0.000039701987,0.000012580811],"category_scores_gemma":[0.000008837479,0.00004821434,0.000016689884,0.00008864741,0.000031222382,0.000015277274,0.000039925282,0.000060713613,4.2213085e-7],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[9.3430265e-7,0.000008998956,0.0008038467,0.000034269673,0.000008543887,8.6714067e-7,0.00028144242,0.002039153,0.98866487,0.0078903595,0.00010977077,0.0001569435],"study_design_scores_gemma":[0.00031982665,0.000011007689,0.005737666,0.00006702544,0.000008209782,0.0000010492598,0.0001753816,0.47013417,0.5181964,0.0051686005,0.00009436745,0.00008628444],"about_ca_topic_score_codex":0.0000046107084,"about_ca_topic_score_gemma":0.0000011118631,"teacher_disagreement_score":0.47046846,"about_ca_system_score_codex":0.00005802735,"about_ca_system_score_gemma":0.000009244739,"threshold_uncertainty_score":0.19661237},"labels":[],"label_agreement":null},{"id":"W4412345684","doi":"10.1121/10.0037183","title":"Characterization of micro-scale gas leaks using an optomechanical ultrasound sensor","year":2025,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"The Metabolomics Innovation Centre; University of Alberta","funders":"Natural Sciences and Engineering Research Council of Canada; Emissions Reduction Alberta; Government of Alberta","keywords":"Acoustics; Microphone; Broadband; Ultrasound; Acoustic sensor; Ultrasonic sensor; Energy (signal processing); Physics; Gas leak; Materials science; Optics; Sound pressure; Chemistry","score_opus":0.007818609497282058,"score_gpt":0.236977783077414,"score_spread":0.22915917358013194,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4412345684","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.52212954,0.00003239652,0.4773022,0.00017669343,0.00024771833,0.00005468617,0.000017527393,0.000007973282,0.000031267846],"genre_scores_gemma":[0.951316,0.0004697569,0.047804106,0.00022638742,0.00013144838,3.0849984e-7,0.0000015190284,0.000020880552,0.000029609711],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99887073,0.00007643882,0.0005231418,0.00006984444,0.00026991463,0.00018995944],"domain_scores_gemma":[0.99891907,0.0002927258,0.00027003654,0.0002832146,0.00018224168,0.00005271381],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00039913703,0.00013303458,0.0003369103,0.000023079803,0.00010286749,0.0000144367095,0.00048793567,0.000096777425,0.000020458388],"category_scores_gemma":[0.0000870811,0.000082889695,0.00026816153,0.00029536613,0.00032402723,0.000071789276,0.000083755134,0.00041721325,4.558288e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000022459184,0.00006962022,0.00005699096,0.00006206192,0.00011051771,1.8552363e-7,0.00022841219,0.118030116,0.8800163,0.0000051015854,0.00019490627,0.0012032766],"study_design_scores_gemma":[0.00021997248,0.00007969576,0.00077931845,0.00013765058,0.00034361208,0.000034277295,0.0008283224,0.9426779,0.054339536,0.00033660658,0.0001203245,0.00010278174],"about_ca_topic_score_codex":0.000008441175,"about_ca_topic_score_gemma":2.6126938e-7,"teacher_disagreement_score":0.8256768,"about_ca_system_score_codex":0.000074994314,"about_ca_system_score_gemma":0.00005054533,"threshold_uncertainty_score":0.33801436},"labels":[],"label_agreement":null},{"id":"W4412699862","doi":"10.11159/ffhmt25.165","title":"Comparative Study of RANS and LES for Transient Flow Characteristics in an EC Fan","year":2025,"lang":"en","type":"article","venue":"Proceedings of the ... International Conference on Fluid Flow, Heat and Mass Transfer","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"Korea Institute of Energy Technology Evaluation and Planning; Ministry of Trade, Industry and Energy","keywords":"Reynolds-averaged Navier–Stokes equations; Transient (computer programming); Transient flow; Flow (mathematics); Computer science; Marine engineering; Mechanics; Computational fluid dynamics; Physics; Engineering; Meteorology; Surge","score_opus":0.026327273323664666,"score_gpt":0.26602572213454606,"score_spread":0.2396984488108814,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4412699862","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98951846,0.00002420363,0.0077229347,0.00020056312,0.0002264391,0.00047826863,0.00014079153,0.000014847522,0.0016735016],"genre_scores_gemma":[0.9992881,0.00011461745,0.00046640536,0.000016838816,0.000019904694,0.000045545217,0.000007375965,0.000009633193,0.000031612606],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992707,0.0000043222753,0.00030080118,0.00017080519,0.00014506883,0.000108318534],"domain_scores_gemma":[0.9996553,0.000037822705,0.000011106063,0.000050597704,0.00021673516,0.00002841331],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012514721,0.00014369165,0.0002749444,0.000106356594,0.000039381175,0.00003844461,0.00021193334,0.000056732082,0.0000076786255],"category_scores_gemma":[0.00000892366,0.00011692547,0.0000366229,0.00006833629,0.00006529352,0.000084863255,0.000013974889,0.00012743211,5.4592032e-8],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0007552751,0.0006499376,0.010984503,0.00071087555,0.00030568615,5.5764247e-7,0.012255038,0.004759753,0.8956498,0.067782946,0.000074969146,0.00607067],"study_design_scores_gemma":[0.0015212867,0.00027652248,0.010939835,0.00027045945,0.00006147153,5.1542725e-7,0.0024696894,0.96876764,0.014277159,0.0012165998,0.00004629636,0.00015251579],"about_ca_topic_score_codex":0.00001057829,"about_ca_topic_score_gemma":0.00006765165,"teacher_disagreement_score":0.9640079,"about_ca_system_score_codex":0.000023621978,"about_ca_system_score_gemma":0.000013743697,"threshold_uncertainty_score":0.47680822},"labels":[],"label_agreement":null},{"id":"W4412700125","doi":"10.11159/ffhmt25.170","title":"Application of Singular Value Decomposition and Autoencoder for Supersonic Flow over Backward Facing Step","year":2025,"lang":"en","type":"article","venue":"Proceedings of the ... International Conference on Fluid Flow, Heat and Mass Transfer","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Autoencoder; Singular value decomposition; Supersonic speed; Decomposition; Flow (mathematics); Choked flow; Value (mathematics); Computer science; Algorithm; Artificial intelligence; Engineering; Physics; Aerospace engineering; Mechanics; Deep learning","score_opus":0.0083609993511453,"score_gpt":0.2362333688127912,"score_spread":0.2278723694616459,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4412700125","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.5738877,0.00009104557,0.42147473,0.00044939754,0.0003120529,0.0003845711,0.00010753837,0.000034125766,0.0032588583],"genre_scores_gemma":[0.9911046,0.00017560764,0.008522781,0.00005135845,0.00003165913,0.000036020265,0.0000133238045,0.000013831899,0.0000508103],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992976,0.000002330521,0.00023718308,0.00018241553,0.00016411665,0.000116311385],"domain_scores_gemma":[0.9996629,0.000037955102,0.000012363702,0.000057640016,0.00020219499,0.000026982336],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012754637,0.00013650436,0.00017622375,0.000086138854,0.000054950087,0.00004561678,0.0001765806,0.00008070676,0.000009386244],"category_scores_gemma":[0.000013358119,0.000117295815,0.00006448967,0.00006524129,0.000061125014,0.00010491825,0.000022482267,0.00010097816,2.1937355e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000871169,0.000030117551,0.0005130084,0.00040361946,0.00012063296,4.8391094e-8,0.00025275286,0.009673971,0.82473683,0.15833692,0.00012828717,0.005716671],"study_design_scores_gemma":[0.0004940037,0.00003149297,0.00046969255,0.00022354383,0.000053380045,8.508166e-7,0.000074451855,0.9554639,0.03750996,0.0054174433,0.0001579156,0.00010337589],"about_ca_topic_score_codex":0.000009945097,"about_ca_topic_score_gemma":0.0000031127572,"teacher_disagreement_score":0.94578993,"about_ca_system_score_codex":0.00004559295,"about_ca_system_score_gemma":0.000016941207,"threshold_uncertainty_score":0.47831842},"labels":[],"label_agreement":null},{"id":"W4412975945","doi":"10.1121/10.0037432","title":"Nonlinear vibration characterization of the synthetic jet actuator to reduce noise levels","year":2025,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"","keywords":"Acoustics; Vibration; Piezoelectricity; Synthetic jet; Overtone; Noise (video); Nonlinear system; Actuator; Laser Doppler vibrometer; Jet (fluid); Materials science; Jet noise; Control theory (sociology); Mechanics; Engineering; Physics; Computer science; Electrical engineering; Optoelectronics","score_opus":0.007695904707946366,"score_gpt":0.23203252755238532,"score_spread":0.22433662284443895,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4412975945","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.3978317,0.000030084266,0.59715605,0.0039925007,0.00064777356,0.00018002288,0.00005067386,0.000010984312,0.00010018828],"genre_scores_gemma":[0.98226815,0.00014170406,0.016664369,0.0006982603,0.00013458639,0.0000012975555,6.4917475e-7,0.000017254488,0.00007373584],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989263,0.00006935779,0.00046823054,0.00006338517,0.00032177902,0.00015094403],"domain_scores_gemma":[0.9988948,0.00027219238,0.00025848325,0.00035228705,0.00018033103,0.00004191026],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00035930565,0.00012419748,0.00025837778,0.000019293748,0.00011489132,0.000014124573,0.00065577816,0.00006705645,0.00002035909],"category_scores_gemma":[0.00029466924,0.000062513696,0.00026420032,0.00040306442,0.00022243084,0.000053939842,0.00014691093,0.00033408686,0.0000014007818],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000026036705,0.00005011463,0.000018289416,0.00006441294,0.00011139207,7.186877e-8,0.00048572195,0.10334611,0.88971084,0.000012036581,0.0013809389,0.004794036],"study_design_scores_gemma":[0.00017732779,0.00006577867,0.0041768868,0.0002676005,0.00029471793,0.0000062460067,0.0003790293,0.9390506,0.05452192,0.00029009473,0.0006716263,0.00009818475],"about_ca_topic_score_codex":0.0000041074913,"about_ca_topic_score_gemma":2.5324442e-7,"teacher_disagreement_score":0.8357045,"about_ca_system_score_codex":0.00007345636,"about_ca_system_score_gemma":0.00007869886,"threshold_uncertainty_score":0.25492343},"labels":[],"label_agreement":null},{"id":"W4412976015","doi":"10.1121/10.0037377","title":"Shape optimization of a synthetic jet actuator enclosure for aerodynamic efficiency and noise reduction using COMSOL Multiphysics","year":2025,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"McGill University","funders":"","keywords":"Multiphysics; Enclosure; Synthetic jet; Aerodynamics; Actuator; Reduction (mathematics); Acoustics; Computational fluid dynamics; Mechanical engineering; Engineering; Jet noise; Optimal design; Computer science; Structural engineering; Finite element method; Aerospace engineering; Nozzle; Physics; Electrical engineering; Mathematics","score_opus":0.006645282440867623,"score_gpt":0.23028595257878334,"score_spread":0.22364067013791572,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4412976015","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.23986743,0.00019566804,0.7592648,0.00022028488,0.00024950522,0.00016683647,0.000017513537,0.000007786274,0.000010142804],"genre_scores_gemma":[0.8814667,0.0005054937,0.117915235,0.000035398767,0.000054991135,0.0000011176814,5.691417e-7,0.000015667092,0.000004818126],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99911106,0.000040523635,0.0004301877,0.00007074719,0.00019856387,0.00014892418],"domain_scores_gemma":[0.99887854,0.0004100068,0.0002876728,0.00018694178,0.00020447613,0.000032337623],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00034195196,0.00012634123,0.00030591205,0.000023962757,0.00012976555,0.00001042144,0.00028004928,0.00007034679,0.0000046492364],"category_scores_gemma":[0.00018587259,0.00007796776,0.00026351892,0.0002454173,0.00039437198,0.00005127972,0.00007119557,0.0002363965,5.2493604e-8],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000033296867,0.000054191813,0.00001089436,0.00023901957,0.00011004973,3.8972143e-8,0.000254828,0.9114598,0.08454791,0.000010974799,0.00019123123,0.0030877853],"study_design_scores_gemma":[0.00027016236,0.00007425842,0.000073337935,0.0002388462,0.0004896408,0.000009349874,0.0006068802,0.9971071,0.0007391604,0.00031239493,0.000007748573,0.000071114744],"about_ca_topic_score_codex":0.000004887142,"about_ca_topic_score_gemma":1.1936442e-7,"teacher_disagreement_score":0.6415993,"about_ca_system_score_codex":0.00007273711,"about_ca_system_score_gemma":0.00005249637,"threshold_uncertainty_score":0.3179433},"labels":[],"label_agreement":null},{"id":"W4412987548","doi":"10.1016/j.jsv.2025.119336","title":"The effect of the leading-edge separation bubble vortex shedding on the far field noise of a Controlled Diffusion airfoil: A DNS study","year":2025,"lang":"en","type":"article","venue":"Journal of Sound and Vibration","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Alliance de recherche numérique du Canada; Natural Sciences and Engineering Research Council of Canada; Government of Western Australia; Agence Nationale de la Recherche; National Computational Infrastructure","keywords":"Airfoil; Bubble; Vortex shedding; Near and far field; Separation (statistics); Vortex; Noise (video); Leading edge; Mechanics; Acoustics; Physics; Diffusion; Mathematics; Reynolds number; Computer science; Optics; Turbulence; Thermodynamics","score_opus":0.004283372533397312,"score_gpt":0.24762585729635164,"score_spread":0.24334248476295434,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4412987548","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.979038,0.0001832536,0.019162856,0.0002613199,0.00043215926,0.000326024,0.0000011632509,0.000004629117,0.00059061445],"genre_scores_gemma":[0.9997218,0.000072290706,0.000015400967,0.000032133663,0.00006616224,0.000004396589,2.519101e-7,0.000005408295,0.00008212343],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992812,0.000088383706,0.00035347845,0.00004773129,0.0001618443,0.00006733277],"domain_scores_gemma":[0.99875045,0.000871339,0.00018974113,0.00011754121,0.000058883703,0.000012053228],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00069388846,0.00008224122,0.00020553308,0.000043077263,0.00019338021,0.00005459553,0.00011759718,0.00004126697,0.000002300159],"category_scores_gemma":[0.00024287771,0.00003613303,0.00008955148,0.00011062784,0.00002603754,0.00006518075,0.000022299155,0.00018118128,2.1511961e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.003394744,0.00047231882,0.04342308,0.00041575986,0.0014023873,0.0000048317393,0.0065368083,0.47592595,0.42707562,0.020891262,0.0030660147,0.017391235],"study_design_scores_gemma":[0.003982336,0.0016111765,0.0127139,0.00027077968,0.000331109,0.0000041223598,0.0008695205,0.9677636,0.009863403,0.0023127198,0.00016595094,0.00011139957],"about_ca_topic_score_codex":0.0000025522468,"about_ca_topic_score_gemma":0.000028001154,"teacher_disagreement_score":0.49183765,"about_ca_system_score_codex":0.000021740438,"about_ca_system_score_gemma":0.00001247836,"threshold_uncertainty_score":0.14873439},"labels":[],"label_agreement":null},{"id":"W4413043132","doi":"10.1016/j.jsv.2025.119363","title":"Experimental estimation of the sound power radiated from panels excited by a turbulent boundary layer","year":2025,"lang":"en","type":"article","venue":"Journal of Sound and Vibration","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Université de Lyon; Institut National des Sciences Appliquées de Lyon; Naval Group; Agence Nationale de la Recherche; Université de Sherbrooke","keywords":"Acoustics; Boundary layer; Sound (geography); Effective radiated power; Sound power; Excited state; Power (physics); Turbulence; Boundary (topology); Physics; Mechanics; Mathematics; Mathematical analysis; Atomic physics","score_opus":0.006944244578198834,"score_gpt":0.23019721695470835,"score_spread":0.2232529723765095,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4413043132","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.87275714,0.0010148913,0.125535,0.00009300665,0.00039328728,0.00005473346,0.000014695222,0.000008243036,0.00012897832],"genre_scores_gemma":[0.9992851,0.000030209732,0.00053558085,0.000063978485,0.000040338313,7.520626e-7,0.000010229711,0.000007520282,0.000026289494],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994635,0.000017323035,0.0002821532,0.00005058848,0.00012318722,0.000063258674],"domain_scores_gemma":[0.9997195,0.00004152891,0.0001068683,0.00006891858,0.000040210933,0.00002297129],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00008231961,0.00007642933,0.000117786185,0.000044798344,0.000067680034,0.000073166615,0.00006609747,0.00005660557,0.000022994158],"category_scores_gemma":[0.000016997607,0.00005647011,0.00004424631,0.000085599975,0.000034966066,0.00016886186,0.000013276803,0.00011625958,3.8337967e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000922191,0.00018310713,0.0015148683,0.000068736335,0.00031760603,0.000004204057,0.0025570453,0.30912313,0.67825806,0.0012752669,0.0049742297,0.0016314841],"study_design_scores_gemma":[0.0010201888,0.00009011597,0.010628416,0.00014201568,0.000073368756,0.000012994112,0.000547134,0.9456259,0.02765288,0.013655316,0.00040265164,0.00014903884],"about_ca_topic_score_codex":0.00000444822,"about_ca_topic_score_gemma":8.569419e-7,"teacher_disagreement_score":0.6506052,"about_ca_system_score_codex":0.000047180965,"about_ca_system_score_gemma":0.000017920156,"threshold_uncertainty_score":0.23027842},"labels":[],"label_agreement":null},{"id":"W4413391597","doi":"10.1115/omae2025-156118","title":"LES Analysis of Vortex-Vortex Interaction and Associated Acoustic Signatures","year":2025,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Vortex; Acoustics; Physics; Computer science; Mechanics","score_opus":0.005859750894557293,"score_gpt":0.24376051092020576,"score_spread":0.23790076002564847,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4413391597","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.88379496,0.00021324576,0.0982865,0.000012258646,0.00024086027,0.00004915653,0.000021059286,0.000111129244,0.0172708],"genre_scores_gemma":[0.99897957,0.00009003943,0.00028239356,0.000017117596,0.000007376104,0.0000023098316,0.000021540645,0.0000075864227,0.00059206167],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995516,0.000009071706,0.00017879118,0.00009926704,0.00006882877,0.00009242206],"domain_scores_gemma":[0.99967897,0.00012366356,0.000027618775,0.00010127421,0.000049731505,0.000018750115],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00007719224,0.000085938125,0.00019789702,0.00025320373,0.000029819983,0.000018277655,0.000057438014,0.00009122109,0.00008449841],"category_scores_gemma":[0.000060334743,0.00008010362,0.00006023211,0.00049453054,0.000019581628,0.000035267734,0.000023293518,0.00012789753,4.979684e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000038167896,0.000027536511,0.0035826454,0.000050754592,0.0018839282,0.0000014919261,0.000058500686,0.9641242,0.02211268,0.0028932279,0.00038444833,0.0048767724],"study_design_scores_gemma":[0.00007883864,0.0000063289617,0.058918897,0.00001895093,0.00076276925,6.964156e-8,0.00009622035,0.9395771,0.0001822174,0.0002478195,0.000038755203,0.00007200319],"about_ca_topic_score_codex":0.00007802921,"about_ca_topic_score_gemma":0.0006966108,"teacher_disagreement_score":0.11518458,"about_ca_system_score_codex":0.000044621425,"about_ca_system_score_gemma":0.000004876091,"threshold_uncertainty_score":0.3266531},"labels":[],"label_agreement":null},{"id":"W4413409630","doi":"10.1017/jfm.2025.10475","title":"Self-preservation scaling of turbulence in free axisymmetric compressible jets","year":2025,"lang":"en","type":"article","venue":"Journal of Fluid Mechanics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Calgary","funders":"","keywords":"Turbulence; Mechanics; Rotational symmetry; Compressibility; Physics; Scaling; K-epsilon turbulence model; Jet (fluid); Compressible flow; Geometry; Mathematics","score_opus":0.005823685412069994,"score_gpt":0.215159932922796,"score_spread":0.20933624751072602,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4413409630","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.39110807,0.006815722,0.59776485,0.00015126265,0.002559482,0.00012454296,0.0000123659365,0.000042603926,0.0014211228],"genre_scores_gemma":[0.96849597,0.0018985537,0.029467806,0.00002595718,0.00006413555,0.0000010611648,8.07188e-7,0.000013929439,0.00003179703],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989787,0.000019900397,0.000555105,0.00006632582,0.0002309776,0.00014904376],"domain_scores_gemma":[0.99934214,0.00010687611,0.00012203627,0.00020389525,0.00018824762,0.00003680361],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000515865,0.00009397189,0.00024362042,0.00045090792,0.000018152854,0.000016975953,0.00038237986,0.000098361495,0.0000066382436],"category_scores_gemma":[0.00023975334,0.000094079645,0.00006795469,0.00071250956,0.0000050886824,0.00019204665,0.00007269808,0.00028650212,5.853889e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000023150653,0.00014225497,0.00015524584,0.0006532272,0.00010224978,0.000027456927,0.0001710542,0.90868443,0.0567589,0.024650216,0.0026056943,0.0060261134],"study_design_scores_gemma":[0.00047784916,0.00003327118,0.00012798718,0.00034363565,0.000028801805,0.00000658462,0.00003739211,0.9740888,0.00849656,0.015767599,0.0005174514,0.00007410293],"about_ca_topic_score_codex":0.0000047979815,"about_ca_topic_score_gemma":0.000005253111,"teacher_disagreement_score":0.57738787,"about_ca_system_score_codex":0.00010506783,"about_ca_system_score_gemma":0.00004846329,"threshold_uncertainty_score":0.38364568},"labels":[],"label_agreement":null},{"id":"W4413454982","doi":"10.1016/j.ast.2026.112412","title":"VAE‑based surrogate model of rotor aerodynamic load distribution for noise prediction","year":2025,"lang":"en","type":"article","venue":"Aerospace Science and Technology","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Nexen (Canada)","funders":"","keywords":"Aerodynamics; Rotor (electric); Noise (video); Computer science; Surrogate model; Distribution (mathematics); Control theory (sociology); Aerospace engineering; Engineering; Artificial intelligence; Mathematics; Machine learning; Mechanical engineering; Mathematical analysis","score_opus":0.00429045462660622,"score_gpt":0.2120926005862121,"score_spread":0.2078021459596059,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4413454982","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6106812,0.000094525036,0.3876475,0.00045170073,0.00026240989,0.0002927136,0.000169326,0.00022099065,0.00017962373],"genre_scores_gemma":[0.99586576,0.000051685747,0.0039010781,0.000013429964,0.000006128259,0.00006643653,0.0000126712475,0.000007427978,0.000075405325],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99919,0.0000021821625,0.00015850148,0.00023451724,0.00015601974,0.0002588315],"domain_scores_gemma":[0.99933606,0.000028912225,0.00003466804,0.00024618485,0.0003238023,0.000030395491],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00030190605,0.00010553325,0.0001454196,0.0001688504,0.00014755806,0.000019491008,0.00022340674,0.0001405508,6.6480544e-7],"category_scores_gemma":[0.00020634045,0.00010551528,0.000022283144,0.0008855886,0.00055644417,0.00010289527,0.000057727833,0.0001107769,5.390902e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000014915899,0.000042861284,0.0017678493,0.00016741501,0.000015053705,3.709372e-7,0.0000232999,0.2477127,0.69133955,0.052099757,0.0005805217,0.0062357076],"study_design_scores_gemma":[0.00030865576,0.000047227968,0.00034240243,0.00003413198,0.000017282342,4.814244e-7,0.000032970318,0.97475654,0.019932522,0.004317667,0.00012977178,0.00008032785],"about_ca_topic_score_codex":0.0000049947275,"about_ca_topic_score_gemma":0.000033625707,"teacher_disagreement_score":0.72704387,"about_ca_system_score_codex":0.00017048066,"about_ca_system_score_gemma":0.00018060638,"threshold_uncertainty_score":0.4302788},"labels":[],"label_agreement":null},{"id":"W4413478808","doi":"10.1016/j.jaerosci.2025.106672","title":"Aerosol discharge velocity and particle size characteristics of a low powered e-cigarette by phase Doppler anemometer","year":2025,"lang":"en","type":"article","venue":"Journal of Aerosol Science","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Carleton University","funders":"Mitacs","keywords":"Anemometer; Aerosol; Environmental science; Doppler effect; Phase (matter); Particle (ecology); Atmospheric sciences; Meteorology; Materials science; Mechanics; Physics; Geology; Turbulence; Oceanography","score_opus":0.004889927748337256,"score_gpt":0.2384001633804543,"score_spread":0.23351023563211704,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4413478808","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9896455,0.00016738391,0.008950402,0.0002061911,0.0007293462,0.00008560999,0.00006874775,0.000015794982,0.00013104855],"genre_scores_gemma":[0.99826616,0.00017153996,0.0013241642,0.000098889825,0.000045723857,0.0000015191741,8.0237334e-7,0.000010740286,0.00008047282],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9985905,0.000014163895,0.0005410728,0.00015337151,0.00038779125,0.00031305174],"domain_scores_gemma":[0.9991174,0.00012375068,0.00019096659,0.00019293312,0.0002126221,0.00016233268],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005881543,0.00014459387,0.0003115875,0.00006123622,0.00011040424,0.00010078441,0.00036449425,0.000056521665,0.000036682202],"category_scores_gemma":[0.0003366121,0.00012172363,0.00006225025,0.00046070694,0.00031878275,0.0003367811,0.000085189306,0.00025373138,0.0000010495678],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000030995223,0.00012630217,0.00060735416,0.00007703953,0.00002951524,0.000008692276,0.0002165706,0.00015787072,0.99511534,0.000055873534,0.0012782399,0.0022961863],"study_design_scores_gemma":[0.003563781,0.0005263651,0.0045073675,0.0005409357,0.00013704925,0.00007369859,0.00020354311,0.257975,0.7315562,0.00014560414,0.00016487099,0.00060560816],"about_ca_topic_score_codex":0.0000018192864,"about_ca_topic_score_gemma":0.0000011504841,"teacher_disagreement_score":0.2635592,"about_ca_system_score_codex":0.0000648787,"about_ca_system_score_gemma":0.00008278419,"threshold_uncertainty_score":0.49637455},"labels":[],"label_agreement":null},{"id":"W4413768421","doi":"10.1016/j.jsv.2025.119376","title":"Influence of angle of attack on airfoil tip noise","year":2025,"lang":"en","type":"article","venue":"Journal of Sound and Vibration","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"University of Toronto; Université de Sherbrooke","funders":"Natural Sciences and Engineering Research Council of Canada; Ontario Research Foundation; Bombardier","keywords":"Airfoil; Angle of attack; Acoustics; Noise (video); Aerospace engineering; Physics; Engineering; Computer science; Aerodynamics; Artificial intelligence","score_opus":0.009185754632677732,"score_gpt":0.2444320147122297,"score_spread":0.23524626007955196,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4413768421","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98252,0.0001308304,0.016338423,0.000030276165,0.000106487045,0.000020100542,0.0000036497931,0.0000033921258,0.0008468721],"genre_scores_gemma":[0.9992148,0.000105860134,0.00059261895,0.000022179827,0.00003752466,1.3952256e-7,6.20741e-7,0.0000034404497,0.000022791328],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99962234,0.0000052045343,0.00022849157,0.000027440843,0.00007726852,0.000039219933],"domain_scores_gemma":[0.9997356,0.0000386353,0.00008581899,0.000046791814,0.00007768509,0.000015475596],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00009088662,0.000041961557,0.00010492934,0.00006879509,0.0000152381435,0.000008920695,0.000041202653,0.000033380853,0.0000027474534],"category_scores_gemma":[0.00003040823,0.000035927686,0.000025345667,0.000072586554,0.00001981305,0.00009362882,0.0000066663833,0.00007418706,2.8395652e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000022219067,0.000028917948,0.002346871,0.0001568742,0.00003069832,0.0000011008186,0.00013182627,0.9221362,0.07137407,0.0021318153,0.00023739581,0.0014020059],"study_design_scores_gemma":[0.001667064,0.00076319335,0.16339044,0.0011363853,0.00014177147,0.000017567629,0.0002946064,0.77208376,0.042119145,0.017306298,0.00079997454,0.00027981677],"about_ca_topic_score_codex":8.9160375e-7,"about_ca_topic_score_gemma":0.0000020119155,"teacher_disagreement_score":0.16104357,"about_ca_system_score_codex":0.00001206869,"about_ca_system_score_gemma":0.0000123931295,"threshold_uncertainty_score":0.14650886},"labels":[],"label_agreement":null},{"id":"W4415015764","doi":"10.1016/j.jsv.2025.119492","title":"Far-Field Aeroacoustic Shape Optimization using Large Eddy Simulation","year":2025,"lang":"en","type":"article","venue":"Journal of Sound and Vibration","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Concordia University","funders":"Fonds de recherche du Québec – Nature et technologies; Alliance de recherche numérique du Canada; Fonds de recherche du Québec; Natural Sciences and Engineering Research Council of Canada; Osteoporosis Canada","keywords":"Airfoil; Shape optimization; Lift coefficient; Lift (data mining); Lift-to-drag ratio; NACA airfoil; Drag; Drag coefficient; Large eddy simulation","score_opus":0.010145900587692148,"score_gpt":0.257324408673207,"score_spread":0.24717850808551484,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4415015764","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.25786835,0.00017609773,0.7413391,0.000018634664,0.0003882808,0.00003479534,0.0000017291572,0.000012940451,0.00016006563],"genre_scores_gemma":[0.9856298,0.000091489244,0.014010667,0.00008654261,0.00015827145,2.2111281e-7,0.0000036777749,0.000008450795,0.000010890293],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99951637,0.00000986175,0.0002535418,0.000049737948,0.000088852255,0.00008164726],"domain_scores_gemma":[0.9996917,0.00007270232,0.00007395657,0.00004464693,0.000091585636,0.000025403428],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00014168967,0.00006960911,0.00010274191,0.00010915996,0.00008648462,0.00007802365,0.000037256883,0.000070541566,0.00002802375],"category_scores_gemma":[0.00006201325,0.00006621252,0.000028660332,0.0001142318,0.0000065932454,0.0002629624,0.000010417841,0.000115884104,2.8348884e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000008258207,0.000011315163,0.00030966653,0.00003494602,0.00001968486,0.000001082574,0.000055399727,0.9951838,0.0019141904,0.0004856275,0.000027422439,0.0019485588],"study_design_scores_gemma":[0.00024227852,0.000029115885,0.00028513398,0.00004566768,0.000047614856,0.0000041683365,0.00007894636,0.99804777,0.00005854619,0.001044785,0.000055374276,0.00006057136],"about_ca_topic_score_codex":5.731731e-7,"about_ca_topic_score_gemma":0.0000019833526,"teacher_disagreement_score":0.72776145,"about_ca_system_score_codex":0.000037231977,"about_ca_system_score_gemma":0.000015617192,"threshold_uncertainty_score":0.2700068},"labels":[],"label_agreement":null},{"id":"W4415328802","doi":"10.1007/jhep11(2025)038","title":"A method for correcting the substructure of multiprong jets using the Lund jet plane","year":2025,"lang":"en","type":"article","venue":"Journal of High Energy Physics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Institute of Particle Physics","funders":"Institut National de Physique Nucléaire et de Physique des Particules; Agencia Estatal de Investigación; Fonds pour la Formation à la Recherche dans l’Industrie et dans l’Agriculture; Qatar National Research Fund; Ministry of Higher Education, Science, Research and Innovation, Thailand; Ministry of Science and ICT, South Korea; Ministry of Science,Technology and Research; Latvijas Zinātnes Padome; European Regional Development Fund; Centre National de la Recherche Scientifique; Türkiye Enerji, Nükleer ve Maden Araştırma Kurumu; National Academy of Sciences of Ukraine; U.S. Department of Energy; Fundação Carlos Chagas Filho de Amparo à Pesquisa do Estado do Rio de Janeiro; Ministry of Education, India; Benemérita Universidad Autónoma de Puebla; Türkiye Bilimsel ve Teknolojik Araştırma Kurumu; Fundação de Amparo à Pesquisa do Estado do Rio Grande do Sul; National Natural Science Foundation of China; National Science and Technology Development Agency; A.G. Leventis Foundation; Fonds De La Recherche Scientifique - FNRS; Conselho Nacional de Desenvolvimento Científico e Tecnológico; Bulgarian National Science Fund; Bundesministerium für Bildung und Forschung; Ministerio de Economía y Competitividad; Alexander von Humboldt-Stiftung; Secretaría de Educación Superior, Ciencia, Tecnología e Innovación; Consejo Nacional de Ciencia y Tecnología; Beijing Municipal Science and Technology Commission; Austrian Science Fund; Ministerstvo Školství, Mládeže a Tělovýchovy; Fundação para a Ciência e a Tecnologia; Universidad Autónoma de San Luis Potosí; Kavli Foundation; Coordenação de Aperfeiçoamento de Pessoal de Nível Superior; European Commission; Fundação de Amparo à Pesquisa do Estado de São Paulo; National Science Foundation; Science Foundation Ireland; Hellenic Foundation for Research and Innovation; Nvidia; Department of Science and Technology, Ministry of Science and Technology, India; Nemzeti Kutatási Fejlesztési és Innovációs Hivatal; Shota Rustaveli National Science Foundation; Deutsche Forschungsgemeinschaft; Centro de Investigación y de Estudios Avanzados del Instituto Politécnico Nacional; CERN; Science and Technology Facilities Council; Welch Foundation; Fundamental Research Funds for the Central Universities; Fonds Wetenschappelijk Onderzoek; Weston Havens Foundation; Magyar Tudományos Akadémia; National Science Council; Pakistan Atomic Energy Commission; Fonds National de la Recherche Luxembourg; Alfred P. Sloan Foundation","keywords":"Substructure; Large Hadron Collider; Jet (fluid); Calibration; Luminosity; Plane (geometry); Quark","score_opus":0.009998867776641789,"score_gpt":0.2550954009215014,"score_spread":0.2450965331448596,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4415328802","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.11630831,0.0002784201,0.88189906,0.000048989674,0.0012612846,0.00004759514,0.000014490265,0.00000857525,0.00013329586],"genre_scores_gemma":[0.96238357,0.00002905857,0.03700577,0.000049580012,0.00046820706,0.0000017691491,0.0000021394746,0.000021162426,0.0000387671],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99929285,0.000033301967,0.00032522643,0.00006282012,0.00014025737,0.00014555543],"domain_scores_gemma":[0.99888754,0.00056796544,0.00021732715,0.00015896099,0.00014891081,0.000019318546],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00026701324,0.00012433136,0.00024662976,0.00003308889,0.000118909134,0.000027340191,0.00026696554,0.00005663929,0.0000015686712],"category_scores_gemma":[0.00004036338,0.000069954905,0.00013188268,0.00016484314,0.00003285491,0.000054484695,0.000032240994,0.0002513693,2.607526e-8],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000017936805,0.000010782538,0.000032031086,0.000044020595,0.00019380497,0.0000016728551,0.00016606906,0.9310014,0.0081871245,0.042758096,0.0002692446,0.01731777],"study_design_scores_gemma":[0.00038819292,0.000030709645,0.00010495577,0.000109844914,0.00019293721,0.00003701155,0.00025005138,0.92665374,0.022830388,0.048404146,0.00089520647,0.00010281681],"about_ca_topic_score_codex":0.000039700324,"about_ca_topic_score_gemma":0.000040972962,"teacher_disagreement_score":0.84607524,"about_ca_system_score_codex":0.00004980849,"about_ca_system_score_gemma":0.00003861203,"threshold_uncertainty_score":0.28526783},"labels":[],"label_agreement":null},{"id":"W4415788412","doi":"10.1016/j.jsv.2025.119515","title":"Virtualization-based acoustic imaging for low-frequency source localization","year":2025,"lang":"en","type":"article","venue":"Journal of Sound and Vibration","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Institut de recherche Robert-Sauvé en santé et en sécurité du travail; Université de Sherbrooke; École de Technologie Supérieure","funders":"Mitacs; Institut de Recherche Robert-Sauvé en Santé et en Sécurité du Travail","keywords":"Acoustic holography; Interpolation (computer graphics); Microphone; Spherical harmonics; Beamforming; Harmonics; Anechoic chamber; Parametric statistics","score_opus":0.00424792854858227,"score_gpt":0.2211428545794965,"score_spread":0.21689492603091423,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4415788412","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.03096739,0.0002715889,0.96796316,0.00008272817,0.00045141662,0.00008070917,0.0000044936673,0.000025386084,0.00015313618],"genre_scores_gemma":[0.9960272,0.000034950262,0.0035547758,0.00018574564,0.00014307266,0.0000019816994,0.00001452656,0.000013251422,0.00002453553],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99948925,0.000008890158,0.00028272232,0.00005651882,0.00008152059,0.0000811116],"domain_scores_gemma":[0.9995959,0.00008957375,0.00008178768,0.000050731374,0.00015412614,0.000027878848],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001488384,0.00007572526,0.0001045864,0.00012416256,0.0000983417,0.00008986829,0.00004898091,0.000040813567,0.0000049793402],"category_scores_gemma":[0.000090642534,0.00007211695,0.000036175326,0.000118606426,0.00001991794,0.00017814366,0.0000044382473,0.00006496984,2.746856e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000008259473,0.0000132593,0.0008024281,0.00015699957,0.000016309494,5.8797997e-7,0.00007896038,0.98413855,0.009533821,0.0022464548,0.0003414567,0.002662901],"study_design_scores_gemma":[0.00039594554,0.000022307493,0.00019420621,0.000096210744,0.0000433115,0.0000024941405,0.000095720345,0.98945516,0.0003566887,0.009064381,0.00020312621,0.00007044483],"about_ca_topic_score_codex":6.498881e-7,"about_ca_topic_score_gemma":0.000003683198,"teacher_disagreement_score":0.96505976,"about_ca_system_score_codex":0.00004609974,"about_ca_system_score_gemma":0.00003406658,"threshold_uncertainty_score":0.2940844},"labels":[],"label_agreement":null},{"id":"W4416251990","doi":"10.1109/waspaa66052.2025.11231017","title":"Physics-Informed Transfer Learning for Data-Driven Sound Source Reconstruction in Near-Field Acoustic Holography","year":2025,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Centre for Interdisciplinary Research in Music Media and Technology","funders":"","keywords":"Acoustic holography; Transfer of learning; Convolutional neural network; Generalization; Artificial neural network; Acoustic source localization; Transfer function; Sound (geography); Holography","score_opus":0.01387969289271251,"score_gpt":0.25039291826226234,"score_spread":0.23651322536954983,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4416251990","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.250481,0.00002425526,0.74514,0.000028931407,0.00041341543,0.00018603654,0.000009155331,0.00017493,0.003542281],"genre_scores_gemma":[0.99026984,0.00006554917,0.009162832,0.000065630295,0.00006485311,0.000028624856,0.000070156406,0.000022844917,0.00024967507],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992284,0.000008236812,0.00024152298,0.00020477171,0.000062810635,0.00025426465],"domain_scores_gemma":[0.9994221,0.0002508315,0.0000112985945,0.00026032532,0.000027110531,0.000028378716],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00010899327,0.00013824568,0.00017576749,0.000092413546,0.000097005395,0.0000696339,0.00021926367,0.000119556695,0.000024655259],"category_scores_gemma":[0.00006940589,0.0001431212,0.00006008391,0.0002685849,0.000040209507,0.00016485635,0.000036968082,0.00029328192,0.0000036928686],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000013189341,0.000011709052,0.0025090585,0.00013956588,0.00005009656,6.143955e-7,0.00011651685,0.9382411,0.00111996,0.0005760741,0.00044183034,0.056780268],"study_design_scores_gemma":[0.0004232675,0.000026861533,0.00027682615,0.000045441397,0.000035340352,0.0000016476133,0.00022048558,0.9960905,0.00011939085,0.0013985172,0.0012040865,0.0001576369],"about_ca_topic_score_codex":0.000019746423,"about_ca_topic_score_gemma":0.00028404695,"teacher_disagreement_score":0.73978883,"about_ca_system_score_codex":0.00003963075,"about_ca_system_score_gemma":0.000031531188,"threshold_uncertainty_score":0.58363134},"labels":[],"label_agreement":null},{"id":"W4416274948","doi":"","title":"Contrôle Actif d’un Bruit Tonal Multimodal Propagé en Ecoulement avec des Sources Harmoniques Acoustiques Pneumatiques (HAPS)","year":2025,"lang":"fr","type":"article","venue":"HAL (Le Centre pour la Communication Scientifique Directe)","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Noise (video); Field (mathematics); Sound (geography); Current (fluid)","score_opus":0.005797489635289644,"score_gpt":0.2176745535793841,"score_spread":0.21187706394409445,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4416274948","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.3555576,0.0088911755,0.58081424,0.012924032,0.000729039,0.00082779507,0.00020997686,0.00069173955,0.039354376],"genre_scores_gemma":[0.79812026,0.006947587,0.1705989,0.00015797645,0.000079109726,0.00013666056,0.0001761152,0.00009837377,0.023685],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99384457,0.0031528007,0.00093704014,0.0007717631,0.0004608273,0.0008329805],"domain_scores_gemma":[0.9945935,0.002132689,0.000301248,0.0012570248,0.0014517839,0.00026376173],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0047081285,0.00061742833,0.00059649325,0.0002565247,0.00073499564,0.00074657897,0.0011962592,0.00044294892,0.00061423227],"category_scores_gemma":[0.0012928521,0.000693712,0.0002794652,0.00045781847,0.00058105675,0.00044928296,0.0006757925,0.00086079974,0.000051296345],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000047257618,0.0018245393,0.004749796,0.001602586,0.00090160035,0.000043200806,0.041931458,0.0055517517,0.051186632,0.26730576,0.004468414,0.620387],"study_design_scores_gemma":[0.0010810386,0.0000034268196,0.007073556,0.00450288,0.00024694245,0.0000236445,0.0008511774,0.7220414,0.20663564,0.019223226,0.037320003,0.0009970657],"about_ca_topic_score_codex":0.0022885166,"about_ca_topic_score_gemma":0.004526189,"teacher_disagreement_score":0.7164897,"about_ca_system_score_codex":0.0006313724,"about_ca_system_score_gemma":0.0003180519,"threshold_uncertainty_score":0.9995514},"labels":[],"label_agreement":null},{"id":"W4416274987","doi":"","title":"Flow-induced noise produced by ducted single and double-diaphragm configurations","year":2025,"lang":"fr","type":"article","venue":"HAL (Le Centre pour la Communication Scientifique Directe)","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Noise (video); Session (web analytics); Background noise; Noise reduction","score_opus":0.008607817693803666,"score_gpt":0.207315300128476,"score_spread":0.19870748243467232,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4416274987","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.42565012,0.0129761975,0.3949543,0.052673582,0.0019458956,0.0010883231,0.00027423774,0.0005815471,0.1098558],"genre_scores_gemma":[0.9136839,0.0013077549,0.03523397,0.00010730785,0.000046821264,0.00006586792,0.000375103,0.00007406507,0.04910524],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9971633,0.0009642896,0.0005433183,0.000622742,0.00023195047,0.0004743876],"domain_scores_gemma":[0.996369,0.000804665,0.00014511122,0.0012105514,0.0012712238,0.00019944801],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0016589493,0.00035314215,0.0003369815,0.00016979712,0.0004750135,0.0004825964,0.0005051904,0.00028310245,0.00018626367],"category_scores_gemma":[0.00067381596,0.00043538245,0.000096894895,0.00074027845,0.00023890108,0.00024003978,0.00025452307,0.0004931017,0.000045990426],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000016276208,0.0007634669,0.00021641476,0.00037878958,0.00018802566,0.0000056928793,0.0032741271,0.0017451688,0.70533955,0.19127765,0.013293463,0.08350136],"study_design_scores_gemma":[0.0015876534,9.784393e-7,0.0008414348,0.0016115363,0.0001636937,0.000009913483,0.00013414552,0.6210025,0.29770222,0.0018134429,0.07447659,0.0006558924],"about_ca_topic_score_codex":0.0006260716,"about_ca_topic_score_gemma":0.0007069595,"teacher_disagreement_score":0.61925733,"about_ca_system_score_codex":0.00019617518,"about_ca_system_score_gemma":0.00017036781,"threshold_uncertainty_score":0.9998098},"labels":[],"label_agreement":null},{"id":"W4416275456","doi":"","title":"Une petite antenne sphérique avec peu de microphones peut-elle localiser des sources sonores basses fréquence ?","year":2025,"lang":"fr","type":"article","venue":"HAL (Le Centre pour la Communication Scientifique Directe)","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke; École de Technologie Supérieure; Institut de recherche Robert-Sauvé en santé et en sécurité du travail; McGill University","funders":"","keywords":"Microphone; SIGNAL (programming language); Work (physics); Line (geometry)","score_opus":0.006922688842870841,"score_gpt":0.21380396831552156,"score_spread":0.20688127947265073,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4416275456","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.32542944,0.01771587,0.6222768,0.017146569,0.0005861392,0.00024289549,0.00010340334,0.0002486168,0.01625027],"genre_scores_gemma":[0.7636821,0.012583912,0.14934151,0.00017577581,0.00007124495,0.000038957653,0.000100652294,0.000092616705,0.073913194],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9961697,0.001601639,0.0005917186,0.0006134812,0.00024456027,0.0007789177],"domain_scores_gemma":[0.99534816,0.0016998585,0.00018199443,0.0012692797,0.0012688705,0.00023185671],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.002568793,0.00044883342,0.00042271437,0.00020462496,0.00070229697,0.00052308064,0.0010731617,0.00030814784,0.00032729807],"category_scores_gemma":[0.0011225815,0.00051762396,0.00021397918,0.0009832678,0.000871933,0.00024465015,0.00048363666,0.0006114606,0.00008089019],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":true,"about_ca_topic_consensus":true,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00006081978,0.001956765,0.03759279,0.004297831,0.00073356775,0.00015714778,0.044442676,0.073923714,0.235899,0.44723725,0.0125629725,0.14113547],"study_design_scores_gemma":[0.0007919107,0.000001496554,0.013226971,0.007820257,0.00018672965,0.00005651091,0.0014062457,0.75023276,0.12205721,0.021785352,0.08142928,0.0010052657],"about_ca_topic_score_codex":0.0074676853,"about_ca_topic_score_gemma":0.018262776,"teacher_disagreement_score":0.67630905,"about_ca_system_score_codex":0.00032099173,"about_ca_system_score_gemma":0.00030364952,"threshold_uncertainty_score":0.99972755},"labels":[],"label_agreement":null},{"id":"W4416630922","doi":"10.1063/5.0295587","title":"Vorticity shedding and acoustic resonance excitation in a tube array with different compactness","year":2025,"lang":"en","type":"article","venue":"Physics of Fluids","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Ontario Tech University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Acoustic resonance; Vortex shedding; Vorticity; Vortex; Particle image velocimetry; Jet (fluid); Transverse plane; Resonance (particle physics); Excitation","score_opus":0.006773324497677408,"score_gpt":0.22421642773407216,"score_spread":0.21744310323639476,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4416630922","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6853925,0.00016648826,0.31384522,0.000011036747,0.00006733108,0.00006733674,0.000006885839,0.000024811736,0.00041841783],"genre_scores_gemma":[0.99876326,0.000066711786,0.001096693,0.000009512276,0.000023899383,0.000010343088,0.000004463012,0.000013233854,0.000011883131],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994859,0.000008640003,0.00015755465,0.00011537084,0.00009518114,0.00013736926],"domain_scores_gemma":[0.99971324,0.00008682912,0.000016154507,0.00012659971,0.000034898716,0.000022290238],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000049466486,0.000112784575,0.00019570783,0.000043281278,0.000024382516,0.000015385502,0.000070108494,0.000029600566,0.0000011623805],"category_scores_gemma":[0.000015539936,0.00010155121,0.000016561444,0.00018321518,0.00004991924,0.000069083086,0.000016913265,0.00011349188,2.0319287e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000054634995,0.00016952724,0.034346662,0.0010001863,0.000076861514,0.0000046070677,0.00118735,0.5199697,0.412093,0.019381214,0.000060209204,0.011656061],"study_design_scores_gemma":[0.00039518223,0.000025748386,0.109598726,0.00031888648,0.00002710761,3.0299014e-7,0.00007300549,0.87766504,0.004480325,0.007268809,0.000007065837,0.00013980834],"about_ca_topic_score_codex":0.000011353758,"about_ca_topic_score_gemma":0.000035189278,"teacher_disagreement_score":0.40761268,"about_ca_system_score_codex":0.000044659377,"about_ca_system_score_gemma":0.0000101902115,"threshold_uncertainty_score":0.41411382},"labels":[],"label_agreement":null},{"id":"W4416960243","doi":"","title":"Méthode rapide pour la prédiction de bruit de rotor installé à faible nombre de Reynolds","year":2025,"lang":"fr","type":"article","venue":"HAL (Le Centre pour la Communication Scientifique Directe)","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Noise (video); Rotor (electric); Strouhal number; Turbine","score_opus":0.009365698673065142,"score_gpt":0.22280460889233464,"score_spread":0.2134389102192695,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4416960243","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.060721546,0.0029017217,0.8256957,0.01484875,0.0005981045,0.00036089175,0.00008145386,0.00034138153,0.09445045],"genre_scores_gemma":[0.52118653,0.0033068187,0.37423941,0.00032071513,0.00009645535,0.000109618755,0.000114368006,0.00011021126,0.10051589],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9944987,0.0033342903,0.00056616374,0.00052267686,0.0002530163,0.00082509575],"domain_scores_gemma":[0.9957273,0.001784523,0.00018665615,0.001261862,0.0007608916,0.00027875905],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0066894796,0.0003722034,0.00034767055,0.0002482355,0.00043211243,0.00043146888,0.0009077413,0.00050429744,0.0001935555],"category_scores_gemma":[0.0018316759,0.0004817823,0.00021021823,0.00070354,0.00022244852,0.00028449722,0.00040371294,0.0008335953,0.000055988345],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000031986736,0.0010289561,0.007207232,0.0010608094,0.00032751038,0.00004810984,0.008295314,0.045307342,0.09011953,0.6768258,0.020543491,0.14920391],"study_design_scores_gemma":[0.0009112121,8.4844396e-7,0.0059651276,0.0025339797,0.0001423257,0.000050781346,0.00027671005,0.78802216,0.029054033,0.019304156,0.15322454,0.00051411294],"about_ca_topic_score_codex":0.002145708,"about_ca_topic_score_gemma":0.0022010636,"teacher_disagreement_score":0.7427148,"about_ca_system_score_codex":0.0010865516,"about_ca_system_score_gemma":0.000829683,"threshold_uncertainty_score":0.99976337},"labels":[],"label_agreement":null},{"id":"W4416964864","doi":"","title":"Sound Zones : mesure des fonctions de transfert à l’aide d’un microphone ambisonique d’ordre élevé","year":2025,"lang":"fr","type":"article","venue":"HAL (Le Centre pour la Communication Scientifique Directe)","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Microphone; Sound (geography); Noise (video); Function (biology); Field (mathematics)","score_opus":0.00830876986718201,"score_gpt":0.21018237819635388,"score_spread":0.20187360832917187,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4416964864","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.22772527,0.006704756,0.7183189,0.0101475725,0.00072806794,0.00027422272,0.00013642145,0.00026380902,0.035701003],"genre_scores_gemma":[0.74263114,0.007935618,0.22055405,0.0001189934,0.000050715393,0.00005910007,0.0001166453,0.000085532265,0.028448207],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9958194,0.0020658064,0.00060048746,0.00055739534,0.00022823263,0.0007287077],"domain_scores_gemma":[0.99601686,0.0012762805,0.00010002205,0.001284234,0.0010926417,0.00022994932],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0031586834,0.00042243904,0.0004046435,0.00020372047,0.0008788899,0.0003802353,0.00081305794,0.00041636144,0.00038882592],"category_scores_gemma":[0.00072609045,0.00052124436,0.00028103392,0.00092170987,0.00051761,0.00020971593,0.00022425843,0.0007735599,0.00005188941],"study_design_candidate":"theoretical_or_conceptual","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00004168421,0.002197214,0.012174795,0.0020342823,0.000983514,0.00005551446,0.030000204,0.017130135,0.13961616,0.46741608,0.007515788,0.3208346],"study_design_scores_gemma":[0.0027848785,0.0000032924881,0.03710802,0.0073865135,0.00080276985,0.00014459358,0.0018594452,0.4930025,0.22595343,0.13666469,0.092196316,0.002093566],"about_ca_topic_score_codex":0.003064539,"about_ca_topic_score_gemma":0.012287897,"teacher_disagreement_score":0.51490587,"about_ca_system_score_codex":0.000458476,"about_ca_system_score_gemma":0.00028519717,"threshold_uncertainty_score":0.9997239},"labels":[],"label_agreement":null},{"id":"W4417038454","doi":"10.3390/jmse13122309","title":"Influence of a Sloped Bottom on a 60-Degree Inclined Dense Jet Discharged into a Stationary Environment: A Large Eddy Simulation Study","year":2025,"lang":"en","type":"article","venue":"Journal of Marine Science and Engineering","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Wilfrid Laurier University; University of Ottawa","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Jet (fluid); Mixing (physics); Dilution; Reynolds-averaged Navier–Stokes equations; Large eddy simulation; Kinematics; Turbulence","score_opus":0.006324291375900381,"score_gpt":0.23700236504863476,"score_spread":0.23067807367273438,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4417038454","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9725385,0.00003928304,0.027051076,0.000027740974,0.00013217842,0.00012767989,0.000003416393,0.000017552582,0.000062628016],"genre_scores_gemma":[0.99483377,0.00006721378,0.005022813,0.000016050415,0.000032861983,0.0000024359467,8.0542236e-7,0.000010379895,0.0000136602785],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99885005,0.000009940965,0.00042495318,0.00012409576,0.00040932433,0.0001816325],"domain_scores_gemma":[0.99943435,0.00013159822,0.000089456225,0.00014189057,0.00012867636,0.00007403635],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0008829547,0.00013221198,0.0002138533,0.00040365692,0.00008323748,0.000034379722,0.00020253111,0.00003152111,0.000005022569],"category_scores_gemma":[0.00037251483,0.00011461633,0.00003083466,0.00042348556,0.000044591256,0.00030621295,0.00016757127,0.00024358106,7.2901815e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000024510591,0.000088127956,0.004993901,0.000059915204,0.000028909386,0.00001394284,0.0004750516,0.97709495,0.014905564,0.00011809892,0.000005199693,0.002191817],"study_design_scores_gemma":[0.0005882145,0.00014569965,0.13669865,0.00008573244,0.00002633811,0.0000031301356,0.00015708344,0.86179024,0.00017519422,0.00015052433,0.00007733025,0.00010189254],"about_ca_topic_score_codex":0.000005244091,"about_ca_topic_score_gemma":0.0000033427589,"teacher_disagreement_score":0.13170475,"about_ca_system_score_codex":0.00010646159,"about_ca_system_score_gemma":0.00005675213,"threshold_uncertainty_score":0.46739182},"labels":[],"label_agreement":null},{"id":"W4417095480","doi":"10.1016/j.apacoust.2025.111175","title":"Aeroacoustic impact of heat exchanger installation in an industrial engine cooling module","year":2025,"lang":"en","type":"article","venue":"Applied Acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Heat exchanger; Internal combustion engine cooling; Heat engine; Water cooling; Jet engine","score_opus":0.015104204504616775,"score_gpt":0.2485313507434855,"score_spread":0.23342714623886873,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4417095480","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.76671773,0.000069127535,0.23036192,0.0000026848031,0.00042975982,0.00028485092,0.000060970688,0.00012420413,0.001948723],"genre_scores_gemma":[0.99723965,0.0000758862,0.002291884,0.000014379531,0.00019675963,0.000023286579,0.0000878948,0.00004790534,0.000022345635],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.998795,0.000011701135,0.0004497036,0.00021925823,0.0001725407,0.0003518137],"domain_scores_gemma":[0.99938786,0.00010434438,0.000037149377,0.00033174126,0.000065400454,0.000073486975],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00019490965,0.00024873862,0.00035098972,0.00031456907,0.00004160358,0.000032178985,0.00019633994,0.00027481187,0.000030088619],"category_scores_gemma":[0.000045630764,0.00026015198,0.00006112184,0.00056886254,0.0000446168,0.00007802745,0.00005640185,0.00038804844,0.0000031365812],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00003371927,0.000060711976,0.0004988981,0.00007269552,0.000038846298,0.0000030172016,0.00009224539,0.9086993,0.08474247,0.0004376294,0.00019874804,0.0051217494],"study_design_scores_gemma":[0.00079609326,0.00004383575,0.0039964146,0.000072108036,0.000055092958,7.094442e-7,0.00007785759,0.99361914,0.00050815544,0.00059178355,0.000011986315,0.00022683699],"about_ca_topic_score_codex":0.0000320321,"about_ca_topic_score_gemma":0.00002617801,"teacher_disagreement_score":0.2305219,"about_ca_system_score_codex":0.00027165102,"about_ca_system_score_gemma":0.000074008036,"threshold_uncertainty_score":0.9999851},"labels":[],"label_agreement":null},{"id":"W4417501046","doi":"10.3390/ijtpp11010001","title":"The Characterization of the Installation Effects on the Flow and Sound Field of Automotive Cooling Modules","year":2025,"lang":"en","type":"article","venue":"International Journal of Turbomachinery Propulsion and Power","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"Université de Sherbrooke","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Duct (anatomy); Aeroacoustics; Aerodynamics; Trailing edge; Thrust; Jet engine; Vibration; Vortex; Rotor (electric); Internal flow","score_opus":0.0029846661850144755,"score_gpt":0.22152636123480596,"score_spread":0.21854169504979148,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4417501046","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9890432,0.00012695983,0.0075499867,0.0014360718,0.0013875378,0.00008469942,0.000009954994,0.0000036857864,0.0003579152],"genre_scores_gemma":[0.9994701,0.00017860107,0.00008746519,0.00015193103,0.00005630143,8.962779e-7,0.0000015341723,0.0000047509648,0.000048386406],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99946404,0.00003717679,0.0002339148,0.00004182858,0.00017969424,0.000043328993],"domain_scores_gemma":[0.99925494,0.00035013253,0.00014540993,0.00006854874,0.00016969974,0.000011247593],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020848078,0.00006509631,0.00008514435,0.000052439762,0.00006494818,0.000033483364,0.00015549014,0.000030936717,0.00000388126],"category_scores_gemma":[0.0002490764,0.00003032977,0.000043055654,0.000045894012,0.000037443704,0.000053655695,0.000047948102,0.00016709263,7.385157e-8],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0011949136,0.00022836502,0.021007065,0.00038802435,0.001513649,0.000017535609,0.0029611222,0.12505503,0.412984,0.044198353,0.0015068923,0.38894504],"study_design_scores_gemma":[0.0007813163,0.00018342155,0.16437554,0.0009026828,0.000061462015,0.000028240142,0.00007903111,0.7788003,0.03970047,0.01382909,0.0011201818,0.00013826569],"about_ca_topic_score_codex":0.0000016803046,"about_ca_topic_score_gemma":0.0000020464745,"teacher_disagreement_score":0.6537453,"about_ca_system_score_codex":0.00001541236,"about_ca_system_score_gemma":0.000008269824,"threshold_uncertainty_score":0.1236812},"labels":[],"label_agreement":null},{"id":"W630781715","doi":"10.1016/0967-0653(93)90020-8","title":"10.1016/0967-0653(93)90020-8","year":2000,"lang":"en","type":"article","venue":"Time to knit","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Oceanography; Geology; Environmental science","score_opus":0.0030797766605169213,"score_gpt":0.1452401239980953,"score_spread":0.14216034733757837,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W630781715","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0009288986,0.00006688439,0.0000734215,0.000035363715,0.0000070975393,0.00010538788,0.00003186224,0.00038869592,0.99836236],"genre_scores_gemma":[0.0015502775,0.0000011550542,0.00058320514,0.000016597307,0.00020232408,0.000012683216,0.00002154554,0.000056103094,0.9975561],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.99926203,0.0000074420427,0.00015880773,0.00015500437,0.0001294816,0.00028720294],"domain_scores_gemma":[0.99954045,0.000027023478,0.00000812067,0.00027687885,0.000020517373,0.00012700577],"candidate_categories":["insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.00007259562,0.00015476966,0.0001461307,0.00004490174,0.00004864563,0.000039605395,0.00020847027,0.00007421408,0.9931125],"category_scores_gemma":[0.00001251334,0.00016327263,0.000048755443,0.00014593542,0.00001658197,0.000053776854,0.00002554375,0.00014434337,0.9931887],"study_design_candidate":"not_applicable","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000008184326,0.00001795836,3.5560827e-8,0.000014667972,0.0000235089,0.000009630423,0.000015349942,0.1182783,0.00014437106,0.000004394839,0.24945192,0.6320317],"study_design_scores_gemma":[0.00009027416,0.000026747652,0.000005596248,0.000011639054,0.000010926023,0.0000039843962,4.6197786e-7,0.1459608,0.00002861951,0.000017647806,0.8536551,0.000188226],"about_ca_topic_score_codex":0.000004015124,"about_ca_topic_score_gemma":2.57824e-7,"teacher_disagreement_score":0.63184345,"about_ca_system_score_codex":0.00004570442,"about_ca_system_score_gemma":0.0000069382118,"threshold_uncertainty_score":0.6658065},"labels":[],"label_agreement":null},{"id":"W6884566240","doi":"10.1051/lhb/1968023/pdf","title":"Reattached wall jets","year":2010,"lang":"en","type":"article","venue":"Springer Link (Chiba Institute of Technology)","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"University of Alberta","keywords":"Deformation (meteorology); Feature (linguistics); Closure (psychology); Work (physics)","score_opus":0.007880109893546696,"score_gpt":0.21958794913019036,"score_spread":0.21170783923664366,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6884566240","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9758458,0.00013044257,0.0054117185,0.0006450921,0.0031375259,0.0001778336,0.000011481406,0.0012612967,0.013378809],"genre_scores_gemma":[0.94482106,0.00010918892,0.05465936,0.000021242819,0.00019398902,0.0000196208,0.000006976553,0.000049983617,0.000118597],"study_design_codex":"bench_or_experimental","study_design_gemma":"not_applicable","domain_scores_codex":[0.9988762,0.000001942062,0.00036764314,0.00026073455,0.0001415727,0.00035191493],"domain_scores_gemma":[0.999001,0.00001009729,0.00006531703,0.0007831249,0.00007268556,0.00006775543],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00013324653,0.00023627745,0.00029733058,0.0003576825,0.000067898596,0.000016819029,0.0006028904,0.0005305364,0.00004073014],"category_scores_gemma":[0.00011649003,0.00024070733,0.000091269234,0.00037836688,0.0003245614,0.0001236539,0.00015764458,0.0009774632,0.000066173845],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00000720304,0.00009019027,0.005741861,0.00019989963,0.00017089232,0.00004772337,0.00005936207,0.01074147,0.7795191,0.12553813,0.00043883786,0.07744534],"study_design_scores_gemma":[0.0017814392,0.00017040793,0.008659612,0.00026443534,0.00017573439,0.00009761194,0.000035808982,0.19366156,0.23321873,0.023077771,0.5370626,0.001794337],"about_ca_topic_score_codex":0.000011490246,"about_ca_topic_score_gemma":0.00010920414,"teacher_disagreement_score":0.54630035,"about_ca_system_score_codex":0.00003196415,"about_ca_system_score_gemma":0.000030050705,"threshold_uncertainty_score":0.981576},"labels":[],"label_agreement":null},{"id":"W6920699033","doi":"10.6084/m9.figshare.20528779.v1","title":"Photosensitizing properties of dissolved organic carbon in Canadian prairie pothole wetland ponds change in response to sunlight","year":2022,"lang":"en","type":"article","venue":"Figshare","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Dissolved organic carbon; Wetland; Absorbance; Carbon cycle; Sunlight; Total organic carbon; Surface water; Carbon fibers; Fluorescence","score_opus":0.021454529199122847,"score_gpt":0.21150416697756724,"score_spread":0.19004963777844439,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6920699033","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97423285,0.00019553989,7.924348e-8,0.0001719411,0.000078246805,0.00031976428,0.024532616,0.000035428828,0.0004335235],"genre_scores_gemma":[0.9975084,9.914138e-7,0.000012544284,0.00007307961,0.000028343326,0.00023760881,0.002040769,0.00004210442,0.00005614472],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99916863,0.000044154098,0.00017821412,0.00014451651,0.00012837334,0.00033607802],"domain_scores_gemma":[0.99964356,0.000032870525,0.000019230401,0.00017623871,0.000023629676,0.00010447391],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00013948907,0.00011616409,0.0001609045,0.00032023483,0.000039855833,0.000014255405,0.00015109696,0.00004736432,0.0028927391],"category_scores_gemma":[0.00027914727,0.00012975936,0.00001955745,0.00046002233,0.000002813349,0.000037338854,0.00009865444,0.0002172219,0.0000120944915],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":true,"about_ca_topic_consensus":true,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0002753375,0.000074123076,0.003967745,0.0007050688,0.000029763125,0.0010469368,0.015927618,0.06694505,0.9024725,0.000009258583,0.008094982,0.0004516316],"study_design_scores_gemma":[0.0014118478,0.00028092266,0.103355035,0.003630357,0.00001428796,0.00004670166,0.001915758,0.8185076,0.03126455,0.000018123728,0.03810082,0.0014539945],"about_ca_topic_score_codex":0.011756679,"about_ca_topic_score_gemma":0.38448125,"teacher_disagreement_score":0.87120795,"about_ca_system_score_codex":0.00043848934,"about_ca_system_score_gemma":0.000110589244,"threshold_uncertainty_score":0.99801874},"labels":[],"label_agreement":null},{"id":"W6939149206","doi":"10.60692/pgxnb-6tw55","title":"A review of acoustic imaging methods using phased microphone arrays","year":2019,"lang":"en","type":"article","venue":"Greater South Information System","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure","funders":"","keywords":"Microphone; Phased array; Optoacoustic imaging; Aeroacoustics; Microphone array; Bioacoustics","score_opus":0.019722764852885433,"score_gpt":0.24774135953022586,"score_spread":0.22801859467734042,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6939149206","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0819011,0.00044879082,0.9138012,0.0000027404014,0.0008983654,0.00035636002,0.000068017136,0.00016265427,0.0023607903],"genre_scores_gemma":[0.96374345,0.000015325066,0.036066364,0.00008593951,0.000036825008,0.000009174867,0.000010870611,0.00002096705,0.000011064294],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9988855,0.000034604556,0.00066326733,0.000083029016,0.00014393561,0.00018966994],"domain_scores_gemma":[0.9992765,0.0000109812845,0.00019095423,0.00033563742,0.00014000933,0.000045871748],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00048072168,0.00016189028,0.0003357653,0.00014372898,0.00003070453,0.000037347145,0.00013963765,0.000048404327,0.00004027995],"category_scores_gemma":[0.000016592317,0.00014662156,0.00008341908,0.00022032367,0.00001343942,0.00027112864,0.000022973232,0.00009564484,0.00014104662],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000039592807,0.000007922901,0.009524848,0.25587237,0.00038361855,0.000006443352,0.028928874,0.58818114,0.10937813,0.00011070922,0.00063651614,0.006929803],"study_design_scores_gemma":[0.00044814433,0.0000074591285,0.000118178476,0.007121477,0.00007298213,0.000040242357,0.001297734,0.9864286,0.003935109,6.7414527e-7,0.00029296093,0.0002363912],"about_ca_topic_score_codex":0.0000018916483,"about_ca_topic_score_gemma":1.1179902e-8,"teacher_disagreement_score":0.8818424,"about_ca_system_score_codex":0.000114776834,"about_ca_system_score_gemma":0.000018588016,"threshold_uncertainty_score":0.5979054},"labels":[],"label_agreement":null},{"id":"W6958230496","doi":"10.6084/m9.figshare.24079648.v1","title":"Additional file 1 of Evaluating the impact of continuing professional development courses on physician behavioral intention: a pre-post study with follow-up at six months","year":2023,"lang":"en","type":"article","venue":"Figshare","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université Laval; Centres Intégré Universitaires de Santé et de Services Sociaux","funders":"","keywords":"Continuing professional development; Professional development; Data collection; MEDLINE; Continuing education","score_opus":0.03465059072305794,"score_gpt":0.31762899316083354,"score_spread":0.2829784024377756,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6958230496","genre_codex":"dataset","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.4326234,0.0000025727024,2.761938e-7,0.0000010312531,0.00004615554,0.00029333172,0.56685436,0.00004020685,0.00013866623],"genre_scores_gemma":[0.6498147,5.8266217e-8,0.00008645779,0.0000020366529,0.000032900294,0.0007427491,0.34862077,0.000022965824,0.00067736476],"study_design_codex":"not_applicable","study_design_gemma":"observational","domain_scores_codex":[0.99905705,0.000023809424,0.00022372836,0.00013438698,0.00038935797,0.00017165202],"domain_scores_gemma":[0.9990316,0.0004168276,0.00012432598,0.00015275781,0.00024410742,0.000030371],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.000053640586,0.00014656316,0.00016744917,0.000049747414,0.00009917818,0.000013371599,0.00015508919,0.00003670691,0.4524953],"category_scores_gemma":[0.000282369,0.00009735645,0.000080863596,0.00018957247,0.000010556809,0.000050042738,0.0000996386,0.0001381249,0.0001160007],"study_design_candidate":"not_applicable","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00006494426,0.00017436138,0.00011414212,0.000065670734,0.00008877319,0.0000052028536,0.001263986,0.032728862,0.0003002426,4.3032108e-7,0.96138126,0.0038121124],"study_design_scores_gemma":[0.0016222475,0.002843288,0.55999273,0.01735071,0.00008211839,0.000004489055,0.0048226453,0.4081883,0.00031610657,0.000009909853,0.004103636,0.00066381844],"about_ca_topic_score_codex":0.0000047039707,"about_ca_topic_score_gemma":0.000073583135,"teacher_disagreement_score":0.95727766,"about_ca_system_score_codex":0.00009486602,"about_ca_system_score_gemma":0.000083769846,"threshold_uncertainty_score":0.54800516},"labels":[],"label_agreement":null},{"id":"W6968138146","doi":"10.5281/zenodo.1336049","title":"Application Of De-Laval Nozzle Transonic Flow Field Computation Approaches","year":2014,"lang":"en","type":"article","venue":"Zenodo (CERN European Organization for Nuclear Research)","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Transonic; Throat; Nozzle; Supersonic speed; Computation; RADIUS; Flow (mathematics); Field (mathematics)","score_opus":0.01862821317909377,"score_gpt":0.20530901346502203,"score_spread":0.18668080028592826,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6968138146","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.028364029,0.000022542308,0.94376135,0.00010032249,0.000049011767,0.00015947594,0.00003402397,0.0004123522,0.027096922],"genre_scores_gemma":[0.9947577,0.00002645205,0.004321284,0.000018295583,0.00007354039,5.01947e-8,0.00035512677,0.00041606132,0.000031465253],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99933374,0.00006098097,0.00016056746,0.0001419507,0.00013838471,0.00016436393],"domain_scores_gemma":[0.9996037,0.000028335504,0.000032310807,0.00017722638,0.00010057513,0.000057850295],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003379995,0.000077560486,0.00009227064,0.00007361634,0.00028287823,0.0000879663,0.00030188123,0.00005453405,0.0002480468],"category_scores_gemma":[0.000094707844,0.00008857126,0.00003053928,0.00017843107,0.000038874343,0.00006506373,0.00007973486,0.00013882417,0.00022359447],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00001638694,0.000066024964,0.000006960623,0.0002085278,0.000030762796,5.216467e-7,0.0008719892,0.38905042,0.015943779,0.0067790397,0.009268581,0.577757],"study_design_scores_gemma":[0.00017941774,0.00007000563,0.00020585935,0.000009634796,0.000009215846,0.000008170961,0.000050455394,0.93271255,0.0011347883,0.0005366417,0.06499361,0.00008966452],"about_ca_topic_score_codex":0.0000056611157,"about_ca_topic_score_gemma":4.363849e-7,"teacher_disagreement_score":0.9663937,"about_ca_system_score_codex":0.000049606748,"about_ca_system_score_gemma":0.0000011326844,"threshold_uncertainty_score":0.3611831},"labels":[],"label_agreement":null},{"id":"W6979730412","doi":"","title":"Acoustic Characterization of a Low-Speed Closed Loop Wind Tunnel","year":2024,"lang":"en","type":"other","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Plenum space; Microphone; Wind tunnel; Closed loop; Volume (thermodynamics); Flutter; Characterization (materials science)","score_opus":0.005705303171506887,"score_gpt":0.18703648042889312,"score_spread":0.18133117725738623,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6979730412","genre_codex":"other","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"other","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.037488967,0.0037995412,0.045943663,0.000099449,0.025680123,0.0024589938,0.030776123,0.0025539831,0.85119915],"genre_scores_gemma":[0.53787124,0.0011570633,0.00045904564,0.00014601283,0.0017708624,0.000008952114,0.0013059815,0.0026514926,0.45462933],"study_design_codex":"not_applicable","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9984343,0.0000111234185,0.00041430938,0.00034203957,0.00023821241,0.0005600096],"domain_scores_gemma":[0.99885476,0.000021963828,0.00010090736,0.00053144427,0.00007268987,0.0004182149],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.000076745775,0.00047869736,0.00051747414,0.00073025323,0.000027749504,0.00006748148,0.00034953354,0.0007072641,0.0011184417],"category_scores_gemma":[0.000049381582,0.00055173424,0.000109314555,0.00036312526,0.000096599826,0.000026994901,0.000033332133,0.0005129739,0.00049314485],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000026249083,0.000021888396,0.000006612843,0.004248426,0.0003763849,0.00030868602,0.000135749,0.047599014,0.35423782,0.00021677827,0.5917063,0.0011397359],"study_design_scores_gemma":[0.00041975107,0.000047567955,0.0005248021,0.0025489854,0.0007759732,0.000022411343,0.00007364286,0.9124269,0.00008200954,0.00022516861,0.081212215,0.0016405623],"about_ca_topic_score_codex":0.0015157191,"about_ca_topic_score_gemma":0.008030752,"teacher_disagreement_score":0.8648279,"about_ca_system_score_codex":0.00035699276,"about_ca_system_score_gemma":0.00034992816,"threshold_uncertainty_score":0.99979466},"labels":[],"label_agreement":null},{"id":"W6984870479","doi":"","title":"Interview no. 1508","year":2009,"lang":"en","type":"article","venue":"scholarworks - UTEP (The University of Texas at El Paso)","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Product (mathematics); Negotiation; Work (physics); Vendor; Aerospace; Bachelor; Outsourcing; Software; Las vegas; Software development; Suite","score_opus":0.006635592238382419,"score_gpt":0.18202439104464804,"score_spread":0.17538879880626562,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6984870479","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7905094,0.0036497822,0.07660172,0.002147662,0.0022501266,0.0006922406,0.00008546634,0.000788673,0.123274915],"genre_scores_gemma":[0.99284005,0.0008062387,0.0023122716,0.00021115849,0.00009907319,8.76532e-8,0.000015028933,0.000020725764,0.0036953534],"study_design_codex":"simulation_or_modeling","study_design_gemma":"not_applicable","domain_scores_codex":[0.9991009,0.00004501417,0.00015717877,0.00019390165,0.00019777582,0.00030520794],"domain_scores_gemma":[0.99921155,0.00005471122,0.00005667951,0.0004897064,0.000093757655,0.00009357535],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003096745,0.00018160608,0.0002270338,0.00006157467,0.0002501219,0.000027226057,0.0006819083,0.00014793749,0.00055896747],"category_scores_gemma":[0.00003245359,0.0001724465,0.00016246153,0.00020532159,0.00010234643,0.0001877941,0.00018615733,0.0005026168,0.0005661493],"study_design_candidate":"not_applicable","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0002725915,0.0006031257,0.0059452923,0.00068959774,0.0011812815,0.0003911257,0.002704524,0.34603804,0.019326111,0.011808771,0.33545884,0.27558067],"study_design_scores_gemma":[0.0018406041,0.000269685,0.06898234,0.00064269174,0.00035333307,0.00003170171,0.0004680728,0.33999115,0.00037560324,0.0023333177,0.5834849,0.0012266258],"about_ca_topic_score_codex":0.000009447736,"about_ca_topic_score_gemma":0.000030185887,"teacher_disagreement_score":0.27435404,"about_ca_system_score_codex":0.0001429306,"about_ca_system_score_gemma":0.000011945865,"threshold_uncertainty_score":0.7276893},"labels":[],"label_agreement":null},{"id":"W6984890800","doi":"","title":"","year":2021,"lang":"en","type":"other","venue":"Directory of Open access Books (OAPEN Foundation)","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Diaspora; Relation (database); State (computer science); Reproduction; South asia","score_opus":0.05406006403388638,"score_gpt":0.3658784409166036,"score_spread":0.31181837688271724,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6984890800","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.001817904,0.00092569273,0.006781242,0.00003381747,0.0033714322,0.0016952372,0.000029155934,0.0006339835,0.9847115],"genre_scores_gemma":[0.054420445,0.003532816,0.009752812,0.0002692807,0.0010934691,0.00073994976,0.004019721,0.0036762934,0.9224952],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9963767,0.00012401407,0.0011633995,0.0009854522,0.0007172507,0.0006331836],"domain_scores_gemma":[0.996987,0.00020089778,0.0006821607,0.0016410534,0.00024356811,0.00024530527],"candidate_categories":["metaepi_narrow","scholarly_communication","open_science","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0004582948,0.0009615848,0.0016493454,0.0006573751,0.00017778589,0.0029034128,0.0062153856,0.00033529598,0.03151613],"category_scores_gemma":[0.00012763827,0.0011123156,0.00027736684,0.00053453573,0.0002558527,0.0013658167,0.00266913,0.00062790903,0.00011632072],"study_design_candidate":"not_applicable","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00014171524,0.00090681616,0.0076678037,0.009985374,0.007330497,0.00038587567,0.0004421285,0.049671873,0.018891577,0.08020611,0.30269,0.52168024],"study_design_scores_gemma":[0.001080161,0.000023067518,0.0045643817,0.0019122718,0.0002018598,0.000008582243,0.000047370188,0.011597182,0.0007798616,0.00092231086,0.9770563,0.0018066305],"about_ca_topic_score_codex":0.0015595845,"about_ca_topic_score_gemma":0.003507377,"teacher_disagreement_score":0.67436635,"about_ca_system_score_codex":0.00027491688,"about_ca_system_score_gemma":0.00032670642,"threshold_uncertainty_score":0.9991615},"labels":[],"label_agreement":null},{"id":"W6987797096","doi":"","title":"Turbulence Distortion Effect on Leading Edge Noise from Wind Turbine Blades","year":2023,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"Gandhi Institute of Technology and Management","keywords":"Turbulence kinetic energy; Turbulence; Distortion (music); Noise (video); Aerodynamics; Leading edge; K-epsilon turbulence model; Turbine; K-omega turbulence model","score_opus":0.007322062838314641,"score_gpt":0.2029351449387573,"score_spread":0.19561308210044268,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6987797096","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98883677,0.00012004559,0.0045775636,0.000063752115,0.0025322502,0.00017866965,0.0005853691,0.00041853986,0.0026870572],"genre_scores_gemma":[0.9980721,0.00008178634,0.00018370032,0.000113475035,0.0005818615,0.00000874502,0.00026274484,0.00008489787,0.00061071955],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99880713,0.000015449801,0.0001959706,0.000257403,0.0001793931,0.0005446434],"domain_scores_gemma":[0.99900395,0.0001959054,0.0000246377,0.00033934717,0.000031631287,0.00040451545],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00012337657,0.0002446333,0.00021716686,0.00023621353,0.00014873156,0.000070127986,0.00023271545,0.00016971557,0.00006985092],"category_scores_gemma":[0.00017610715,0.0002619778,0.00005793733,0.0003598101,0.000050640072,0.00005828622,0.000020528269,0.00034425256,0.0006958979],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000005157578,0.00000714173,0.0005322607,0.000086772205,0.00004542631,0.0002208071,0.0001839496,0.9163808,0.0442709,0.00011584256,0.03103393,0.007116965],"study_design_scores_gemma":[0.0002476961,0.00010342981,0.019804448,0.00014800733,0.00007652164,0.0000027561375,0.000040411553,0.9754702,0.00062001805,0.00034308367,0.0026492449,0.00049417175],"about_ca_topic_score_codex":0.0016640977,"about_ca_topic_score_gemma":0.0028566595,"teacher_disagreement_score":0.059089363,"about_ca_system_score_codex":0.0005629544,"about_ca_system_score_gemma":0.000067868976,"threshold_uncertainty_score":0.99998325},"labels":[],"label_agreement":null},{"id":"W6991118204","doi":"","title":"Experimental Study on a Notched Nozzle for Jet Noise Reduction","year":2015,"lang":"en","type":"article","venue":"Institutional Repositories DataBase (IRDB)","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Nozzle; Jet (fluid); Noise (video); Noise reduction; Reduction (mathematics)","score_opus":0.03393883755922368,"score_gpt":0.28363248803979224,"score_spread":0.24969365048056857,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6991118204","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9463324,0.0001879888,0.034982514,0.000046245215,0.012959773,0.0008498049,0.00064608274,0.00035618164,0.003639036],"genre_scores_gemma":[0.9931444,0.0000036930637,0.004004374,0.000017262319,0.0019254843,0.0002607576,0.00049179426,0.000034971526,0.000117263735],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99867004,0.00001775455,0.0003105167,0.00032662507,0.00043507727,0.00023996223],"domain_scores_gemma":[0.9991598,0.000045693745,0.000045336288,0.0004221198,0.00016301978,0.00016402661],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020603697,0.00023380129,0.0001901893,0.00007806515,0.0002524858,0.00009049599,0.0001823925,0.00006972687,0.000005583963],"category_scores_gemma":[0.00015992363,0.00022827437,0.0000616041,0.00014416942,0.00008786055,0.00036557077,0.000072797215,0.00016707167,0.000028028235],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.001412619,0.0054951864,0.0016900746,0.0002189057,0.0006041869,0.0003978619,0.0045185154,0.39724624,0.4346573,0.088274464,0.06493657,0.00054805935],"study_design_scores_gemma":[0.014438063,0.0049301176,0.0021538658,0.00060167065,0.00046061512,0.00072366145,0.014861017,0.35859856,0.37226933,0.0011988423,0.22590479,0.0038594357],"about_ca_topic_score_codex":0.00005163124,"about_ca_topic_score_gemma":0.000011223713,"teacher_disagreement_score":0.16096821,"about_ca_system_score_codex":0.0004410026,"about_ca_system_score_gemma":0.00012748604,"threshold_uncertainty_score":0.93087584},"labels":[],"label_agreement":null},{"id":"W6996504767","doi":"","title":"In-situ Measurement of Acoustic Impedance in Presence of Grazing Flow","year":2023,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Nacelle; Acoustic impedance; Electrical impedance; Sound pressure; Noise control; Mechanical impedance; Noise (video)","score_opus":0.014029887036864065,"score_gpt":0.21244927397741062,"score_spread":0.19841938694054656,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6996504767","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97763324,0.00033258102,0.01808639,0.000044432738,0.0011482618,0.0002801657,0.00014951103,0.000060626655,0.0022647658],"genre_scores_gemma":[0.9984699,0.00025100235,0.0011311941,0.00001681246,0.000045983077,0.000011299226,0.0000067775795,0.000037494538,0.000029531422],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99864227,0.000014484304,0.00042199524,0.00015800502,0.00028635803,0.0004768831],"domain_scores_gemma":[0.99932164,0.00008957109,0.00004235061,0.00027926234,0.00011036114,0.00015684395],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00041264363,0.00014839212,0.00026868054,0.00050229457,0.0000190738,0.000008246931,0.00026133299,0.000109632565,0.000009478363],"category_scores_gemma":[0.00034669568,0.00017965215,0.000036545513,0.0008494162,0.000058435224,0.000059076076,0.00002944054,0.00022602137,0.000009298146],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":true,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000014759656,0.000006532186,0.00083478383,0.00025349858,0.000008569435,0.00006597048,0.00019102485,0.7936054,0.20297565,0.00008675489,0.0010464379,0.00092389697],"study_design_scores_gemma":[0.00020653925,0.000014452829,0.03254608,0.00022557835,0.000014120565,0.0000017247495,0.00017554176,0.9654902,0.0007102644,0.00039334584,0.00004693828,0.00017518578],"about_ca_topic_score_codex":0.0031893568,"about_ca_topic_score_gemma":0.15540831,"teacher_disagreement_score":0.20226538,"about_ca_system_score_codex":0.00041809125,"about_ca_system_score_gemma":0.0002572062,"threshold_uncertainty_score":0.8600033},"labels":[],"label_agreement":null},{"id":"W6999293315","doi":"","title":"Computational fluid dynamics in mesoscopic nozzles","year":2016,"lang":"en","type":"dissertation","venue":"eScholarship@McGill (McGill)","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"McGill University","funders":"","keywords":"Hagen–Poiseuille equation; Nozzle; Solver; Computational fluid dynamics; Mesoscopic physics; Speedup; Python (programming language)","score_opus":0.006595719928807922,"score_gpt":0.21441910888195923,"score_spread":0.2078233889531513,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6999293315","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.86026853,0.00034019924,0.00003560629,0.0000102950735,0.0034341267,0.0005015694,0.002925559,0.00052173604,0.13196239],"genre_scores_gemma":[0.99072486,0.00042427384,0.0020055575,0.0000519832,0.000083061284,0.00010526118,0.0027818773,0.00035171537,0.0034713864],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99674803,0.00008691957,0.0009850464,0.00075523095,0.0006608801,0.0007639156],"domain_scores_gemma":[0.9985353,0.0002817452,0.00018941627,0.0005437956,0.00022588557,0.00022386643],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0003986475,0.0008189615,0.00075679546,0.0005415551,0.00037046423,0.00007800769,0.0006742308,0.00090175524,0.00021255732],"category_scores_gemma":[0.00020611293,0.00085618783,0.00023579465,0.00042046385,0.000049002272,0.00037015395,0.000083336614,0.0013032516,0.00034138566],"study_design_candidate":"theoretical_or_conceptual","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00013052997,0.0003072079,0.00027051885,0.0020547092,0.00060271024,0.0003156144,0.000019523955,0.15560281,0.016403046,0.55133486,0.000043267304,0.2729152],"study_design_scores_gemma":[0.0049789143,0.00026713702,0.0072031324,0.005011259,0.0004803133,0.000070771064,0.000620768,0.5885468,0.010164011,0.35763094,0.017706629,0.007319293],"about_ca_topic_score_codex":0.00005764387,"about_ca_topic_score_gemma":0.0027446363,"teacher_disagreement_score":0.43294403,"about_ca_system_score_codex":0.0021480806,"about_ca_system_score_gemma":0.000048719052,"threshold_uncertainty_score":0.9993889},"labels":[],"label_agreement":null},{"id":"W7000394924","doi":"","title":"Experimental Study of Three-Dimensional Turbulent Offset Jets and Wall Jets","year":2010,"lang":"en","type":"dissertation","venue":"Mspace (University of Manitoba)","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Turbulence; Reynolds number; Turbulence kinetic energy; Offset (computer science); Particle image velocimetry; Vortex; Jet (fluid); Reynolds stress","score_opus":0.009909340037459654,"score_gpt":0.1996508432696827,"score_spread":0.18974150323222302,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7000394924","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99824935,0.00028587162,0.00004227199,0.000022209697,0.0004942811,0.00029656253,0.000033978184,0.000047881582,0.0005275769],"genre_scores_gemma":[0.99896353,0.000028512883,0.0006474986,0.0000025080903,0.000025182128,5.318755e-7,0.00014019413,0.000033773773,0.00015825297],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.99915135,0.000013132782,0.00013046009,0.00023696988,0.0003130264,0.00015504142],"domain_scores_gemma":[0.9994379,0.000028967466,0.00012664034,0.00024568362,0.00009188189,0.00006890524],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00006366025,0.00022650638,0.00034944754,0.00014804951,0.000100888814,0.000009242123,0.00022896631,0.00025349858,0.000021589602],"category_scores_gemma":[0.000004090226,0.00029217277,0.000072420924,0.000072585965,0.000050468774,0.00007221669,0.00006964146,0.00035539136,0.000005541294],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":true,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0026128462,0.014894852,0.06152136,0.006473253,0.0062296083,0.0017314837,0.046834636,0.13826317,0.6699145,0.0019438971,0.036693163,0.012887247],"study_design_scores_gemma":[0.00510227,0.0016949398,0.50697803,0.0006187954,0.00083498977,0.00002501194,0.118419155,0.35707587,0.0057623857,0.000214977,0.0013897484,0.0018837914],"about_ca_topic_score_codex":0.0008428688,"about_ca_topic_score_gemma":0.21103996,"teacher_disagreement_score":0.6641521,"about_ca_system_score_codex":0.000054782442,"about_ca_system_score_gemma":0.000020199002,"threshold_uncertainty_score":0.99995303},"labels":[],"label_agreement":null},{"id":"W7000539694","doi":"","title":"Extended Optimization Study and Panel Parameter Study for Noise Radiation Reduction of an Aircraft Panel Excited by Turbulent Flow","year":2017,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Reduction (mathematics); Turbulence; Excited state; Noise reduction; Noise (video); Flow (mathematics); Radiation","score_opus":0.019623027174506067,"score_gpt":0.23998035751240046,"score_spread":0.2203573303378944,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7000539694","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8686888,0.000049367303,0.12896624,0.000030543346,0.000601664,0.0012209325,0.00036512606,0.000053311705,0.000023981169],"genre_scores_gemma":[0.99139655,0.000053163072,0.008010573,0.000014097642,0.0001439253,0.00007163592,0.00017123083,0.000062268016,0.000076545286],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989335,0.000026611879,0.00031516087,0.00028039634,0.00015083846,0.00029349077],"domain_scores_gemma":[0.9988709,0.00003970182,0.000108523884,0.00055161386,0.00014758315,0.00028166862],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021852668,0.00020629592,0.00024311666,0.00014547365,0.00031250977,0.00014999683,0.00021943967,0.00012226202,0.000009288304],"category_scores_gemma":[0.0001793028,0.000233095,0.000029406832,0.00006356507,0.00005532827,0.00019844678,0.000017549479,0.00013034856,5.9411286e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000015984579,0.00020019451,0.00044378338,0.0000497516,0.00008533963,0.000010073374,0.0008925543,0.9833065,0.0025372729,0.0000036087831,0.0008897509,0.011565183],"study_design_scores_gemma":[0.00093756255,0.00034247918,0.022431193,0.000010721127,0.00018102248,0.0000050745844,0.0011589451,0.9745788,0.000029423803,0.00005262889,0.000026241922,0.0002459316],"about_ca_topic_score_codex":0.0020894385,"about_ca_topic_score_gemma":0.001403436,"teacher_disagreement_score":0.122707725,"about_ca_system_score_codex":0.00018592707,"about_ca_system_score_gemma":0.000065338325,"threshold_uncertainty_score":0.9505338},"labels":[],"label_agreement":null},{"id":"W7001109105","doi":"","title":"Insertion Loss and Wind Induced Noise Results for Secondary Wind Screens","year":2017,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Insertion loss; Microphone; Wind power; Noise (video); Sound pressure; Noise reduction; Wind gradient; Noise barrier","score_opus":0.015407888646654275,"score_gpt":0.2241861360643064,"score_spread":0.20877824741765214,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7001109105","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98590106,0.000061429244,0.004185601,0.00028376194,0.0010328608,0.00030339818,0.0017679775,0.000059496517,0.0064044283],"genre_scores_gemma":[0.9972472,0.000058214904,0.0017271372,0.00015354625,0.00038361244,0.0000039630636,0.000089987,0.000056022185,0.00028029305],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99903953,0.0000049956566,0.0002189465,0.00022138069,0.00008654997,0.00042862564],"domain_scores_gemma":[0.9988484,0.00005487658,0.00005737919,0.00050725613,0.000093312236,0.0004387878],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015903401,0.00018488051,0.00017408218,0.0001081315,0.0004962369,0.00020353287,0.00025890046,0.00021396493,0.000008586695],"category_scores_gemma":[0.0003097118,0.00021473001,0.00003441498,0.000035708304,0.00008659406,0.00013782944,0.0000331182,0.0002578175,0.000008522722],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":true,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00029263826,0.00009229771,0.0059466623,0.0017296509,0.00069567893,0.0009155244,0.002487899,0.32877478,0.3630518,0.006672559,0.13037047,0.15897003],"study_design_scores_gemma":[0.0019700201,0.000104482024,0.22283214,0.000106528045,0.00011424614,0.000026480713,0.00013108405,0.7628911,0.00021721398,0.0013569504,0.009493577,0.0007561824],"about_ca_topic_score_codex":0.0027123173,"about_ca_topic_score_gemma":0.019637516,"teacher_disagreement_score":0.43411633,"about_ca_system_score_codex":0.00020596443,"about_ca_system_score_gemma":0.00020033558,"threshold_uncertainty_score":0.99825156},"labels":[],"label_agreement":null},{"id":"W7001402196","doi":"","title":"Jet reconstruction in the DØ experiment trigger system","year":2006,"lang":"en","type":"dissertation","venue":"eScholarship@McGill (McGill)","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Jet (fluid); Noise (video); Tracking (education); Control system","score_opus":0.00825689548951412,"score_gpt":0.208277906805323,"score_spread":0.20002101131580888,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7001402196","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.83607876,0.0005407416,0.0000031413724,0.0000030350327,0.004231333,0.00070609455,0.0004686979,0.0004016367,0.15756658],"genre_scores_gemma":[0.996143,0.0001709742,0.00051198166,0.000023667144,0.00015019478,0.00033500852,0.000817805,0.00022187218,0.0016255039],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9969035,0.0001855363,0.001004467,0.00064088055,0.000638176,0.0006274854],"domain_scores_gemma":[0.9986435,0.00015139446,0.00023707894,0.0007402055,0.00012632119,0.00010148141],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00076571153,0.0007348733,0.000653166,0.00036251917,0.00046496937,0.00012298982,0.00065518945,0.00079273694,0.000055712535],"category_scores_gemma":[0.00007171905,0.0006464726,0.00027815407,0.00048945536,0.000032368473,0.00028837548,0.000034952598,0.0015912572,0.00011941027],"study_design_candidate":"theoretical_or_conceptual","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0002467304,0.0005617229,0.00009660932,0.004958366,0.00072944484,0.00062503497,0.000119940225,0.055411715,0.09728467,0.45841828,0.0002508917,0.38129658],"study_design_scores_gemma":[0.012488008,0.001099512,0.008718281,0.018492453,0.0031429948,0.002065008,0.03816563,0.24012014,0.34377074,0.051358335,0.25672194,0.023856938],"about_ca_topic_score_codex":0.00021490743,"about_ca_topic_score_gemma":0.001371405,"teacher_disagreement_score":0.40705997,"about_ca_system_score_codex":0.0012996164,"about_ca_system_score_gemma":0.000021051537,"threshold_uncertainty_score":0.9995987},"labels":[],"label_agreement":null},{"id":"W7009376980","doi":"","title":"Dynamics of Harmonic Active Sound Control with a Harmonic Acoustic Pneumatic Source","year":2023,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Association Nationale de la Recherche et de la Technologie","keywords":"Secondary source; Turbofan; Active noise control; Loudspeaker; Microphone; Controller (irrigation); Noise (video); Harmonic; Sound pressure","score_opus":0.006988763678460298,"score_gpt":0.190637973137503,"score_spread":0.1836492094590427,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7009376980","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.71597654,0.00008328637,0.2802579,0.000146771,0.0005255107,0.00043759326,0.0010985227,0.00040181557,0.0010720637],"genre_scores_gemma":[0.99834144,0.00011155043,0.0005607591,0.00009436519,0.00009628461,0.000038629776,0.00013781205,0.00017327147,0.00044587615],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9980543,0.000023063374,0.00040549703,0.0002898772,0.0003152382,0.0009119877],"domain_scores_gemma":[0.9984323,0.00026880947,0.00009472181,0.0005093544,0.00017229537,0.0005225375],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00016990225,0.00036985392,0.0004679103,0.00045048026,0.00016439873,0.000064539134,0.00041094492,0.00021354052,0.000068430585],"category_scores_gemma":[0.0001267742,0.00037946308,0.00008930263,0.00079531997,0.00018692839,0.00008891839,0.000030137255,0.00047939728,0.00010439161],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":true,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00001506499,0.000012703114,0.0002372345,0.00029784584,0.00023075215,0.000112146285,0.0003121848,0.9892591,0.0057374807,0.00036754936,0.0013631175,0.0020547789],"study_design_scores_gemma":[0.0006948543,0.00007707481,0.0038397843,0.00009499351,0.00025277748,0.00002597396,0.0007631475,0.9927479,0.00003140754,0.00097393803,0.00005845123,0.0004397228],"about_ca_topic_score_codex":0.0013502175,"about_ca_topic_score_gemma":0.021686636,"teacher_disagreement_score":0.2823649,"about_ca_system_score_codex":0.0008846631,"about_ca_system_score_gemma":0.0004428358,"threshold_uncertainty_score":0.9998657},"labels":[],"label_agreement":null},{"id":"W7009425188","doi":"","title":"Effect of Duct Height on the Magnitude of Acoustic Resonance for Single Cylinder in Cross-flow","year":2017,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"Ontario Tech University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Magnitude (astronomy); Duct (anatomy); Cylinder; Resonance (particle physics); Acoustic resonance","score_opus":0.012523243505297441,"score_gpt":0.2485819063956539,"score_spread":0.23605866289035646,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7009425188","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9852689,0.00025553332,0.007444525,0.00006834751,0.0010643603,0.0006059866,0.000787678,0.000022747008,0.0044819154],"genre_scores_gemma":[0.9985476,0.000038592403,0.0010294442,0.000042661974,0.00013022486,0.0000283014,0.000009306016,0.000055354016,0.0001185267],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99894804,0.000020290041,0.00030290755,0.00017212075,0.00014840193,0.00040825052],"domain_scores_gemma":[0.9984327,0.0005315066,0.00009633178,0.0007018805,0.00011121904,0.00012637206],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00042372002,0.00019677331,0.0002976666,0.00010606933,0.00016873778,0.000054879485,0.0005464277,0.00015306321,0.000022160328],"category_scores_gemma":[0.0010345688,0.00016201682,0.00007789777,0.00007405899,0.00021802561,0.000047286492,0.000027879614,0.00022941107,0.0000037868688],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000052252763,0.000027007836,0.001373303,0.00048732682,0.0000352985,0.000034510795,0.000084676954,0.9536508,0.03495866,0.00073945516,0.001450808,0.0071059573],"study_design_scores_gemma":[0.00064488506,0.00029305415,0.01702553,0.00020258217,0.000055064495,0.0000031743991,0.000012554788,0.97743195,0.003487639,0.0003881256,0.00021824603,0.00023718523],"about_ca_topic_score_codex":0.0008828039,"about_ca_topic_score_gemma":0.006393296,"teacher_disagreement_score":0.03147102,"about_ca_system_score_codex":0.0001978475,"about_ca_system_score_gemma":0.00010611059,"threshold_uncertainty_score":0.6606854},"labels":[],"label_agreement":null},{"id":"W7011406691","doi":"","title":"Measurement of acoustic resistance of perforated plates subjected to a pulsated grazing flow","year":2021,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Flow resistance; Flow (mathematics); Acoustic emission; Resistance (ecology)","score_opus":0.009669888453859897,"score_gpt":0.18724759271984504,"score_spread":0.17757770426598513,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7011406691","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.85062295,0.0011337727,0.14354809,0.00007821427,0.001094523,0.0003449334,0.00096844713,0.0001333203,0.0020757408],"genre_scores_gemma":[0.9915348,0.0000754066,0.008045828,0.000046137302,0.000052744723,0.00000806892,0.000054348708,0.00006551799,0.00011713533],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9984372,0.000022219225,0.00047890257,0.00022417869,0.000353024,0.00048442473],"domain_scores_gemma":[0.9980615,0.000047927067,0.000059864804,0.00040340822,0.0010257614,0.00040154034],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00021273411,0.00022111164,0.000366496,0.00023348167,0.000071129594,0.00002525226,0.00021611436,0.00014907033,0.0000580672],"category_scores_gemma":[0.00057355396,0.0002640657,0.000060386537,0.0008775893,0.00004912231,0.000036959616,0.000026541002,0.00021207581,0.000007726637],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":true,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000005375415,0.000010160431,0.00013000137,0.00024428073,0.000060041162,0.00005329005,0.00009543847,0.5109825,0.48666805,0.00003238798,0.0015215102,0.00019691093],"study_design_scores_gemma":[0.00035454953,0.00003740064,0.0069489167,0.0005070911,0.00015849037,0.0000078526045,0.00027970996,0.9612011,0.029614354,0.00012817419,0.00031870094,0.00044369558],"about_ca_topic_score_codex":0.0007070038,"about_ca_topic_score_gemma":0.06378245,"teacher_disagreement_score":0.45705372,"about_ca_system_score_codex":0.0004923395,"about_ca_system_score_gemma":0.00069252047,"threshold_uncertainty_score":0.99998116},"labels":[],"label_agreement":null},{"id":"W7015139952","doi":"","title":"A semi-analytical model for Mach reflection in axisymmetric steady overexpanded jets","year":2024,"lang":"en","type":"dissertation","venue":"eScholarship@McGill (McGill)","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"McGill University","keywords":"Reflection (computer programming); Mach number; Mach reflection; Rotational symmetry; Work (physics)","score_opus":0.023928854984822605,"score_gpt":0.2737185610688881,"score_spread":0.24978970608406548,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7015139952","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.89084834,0.0008089438,0.00018537312,0.000008307811,0.0040202495,0.0015490107,0.002833416,0.000950203,0.09879618],"genre_scores_gemma":[0.9820089,0.00038641377,0.0013726555,0.000046498455,0.000104554405,0.00038539918,0.0017048682,0.0004905968,0.013500129],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.996119,0.00006242432,0.0011236074,0.0010862364,0.0006865067,0.0009222148],"domain_scores_gemma":[0.99844724,0.0002706877,0.00015841846,0.0006192364,0.00024382058,0.00026057794],"candidate_categories":["metaepi_narrow","research_integrity"],"consensus_categories":["research_integrity"],"category_scores_codex":[0.0007555451,0.0008887294,0.00093287847,0.0013324075,0.000304738,0.00015848425,0.0005042404,0.0013104229,0.000045478082],"category_scores_gemma":[0.00051043386,0.0009993517,0.00048065287,0.0013961069,0.000022735414,0.00034049357,0.0000790062,0.0023357305,0.00011449635],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00049382186,0.0004785749,0.000015510688,0.0065697236,0.0012849268,0.00017908646,0.000068904716,0.61014557,0.042627994,0.22719269,0.00021368847,0.110729516],"study_design_scores_gemma":[0.0007207955,0.00007820172,0.00004720873,0.0004877389,0.00039506907,0.00001145858,0.00009089933,0.94645745,0.0016004584,0.046361636,0.0026785238,0.0010705682],"about_ca_topic_score_codex":0.000055956116,"about_ca_topic_score_gemma":0.0018423205,"teacher_disagreement_score":0.33631188,"about_ca_system_score_codex":0.0018966058,"about_ca_system_score_gemma":0.00005822973,"threshold_uncertainty_score":0.9999861},"labels":[],"label_agreement":null},{"id":"W7015266394","doi":"","title":"Simulation numérique de l’atténuation sonore d’un protecteur auditif de type casque anti-bruit","year":2017,"lang":"fr","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Institut de recherche Robert-Sauvé en santé et en sécurité du travail","funders":"","keywords":"Context (archaeology); Subject (documents); Feature (linguistics)","score_opus":0.016874274217675192,"score_gpt":0.27087092913698824,"score_spread":0.25399665491931306,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7015266394","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.44025448,0.00018957058,0.5492893,0.0010575136,0.0012376028,0.00038927,0.000025940002,0.0001410352,0.007415338],"genre_scores_gemma":[0.96857935,0.00022134419,0.024145478,0.000053351498,0.00092793634,0.000023246559,0.000026744305,0.0000879388,0.0059345993],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.998612,0.00006087729,0.0003061569,0.00028642826,0.00016348502,0.00057106715],"domain_scores_gemma":[0.99870485,0.0001384789,0.00015723932,0.0006410706,0.00020192323,0.00015644458],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0005088212,0.00027501205,0.00023594704,0.000058356647,0.00050725794,0.0003590207,0.00034637362,0.00043087298,0.00062404515],"category_scores_gemma":[0.0007873121,0.00031674694,0.000081553466,0.00007755711,0.00007763948,0.00035354166,0.00009932455,0.0004649656,0.00021018503],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000066572425,0.00004880091,0.003981749,0.00019946517,0.00005682385,0.000050114908,0.00057047367,0.96017534,0.007930711,0.009444626,0.00030204022,0.017233191],"study_design_scores_gemma":[0.00029144195,0.000040702813,0.022514572,0.000131892,0.000034104098,0.00001822441,0.00008108856,0.9635373,0.001984762,0.007856693,0.003147625,0.00036164542],"about_ca_topic_score_codex":0.00078251667,"about_ca_topic_score_gemma":0.00065480435,"teacher_disagreement_score":0.5283249,"about_ca_system_score_codex":0.0004714792,"about_ca_system_score_gemma":0.00014819078,"threshold_uncertainty_score":0.9999285},"labels":[],"label_agreement":null},{"id":"W7015602796","doi":"","title":"Turboshaft engine performance comparison between CVT and fixed ratio transmission for a variable speed rotor helicopter","year":2013,"lang":"en","type":"article","venue":"Research Padua  Archive (University of Padua)","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Airframe; Continuously variable transmission; Rotor (electric); Rotational speed; Turbine; Control theory (sociology); Variable (mathematics); Power (physics); Propulsion","score_opus":0.029128057389588638,"score_gpt":0.25658133226415064,"score_spread":0.22745327487456202,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7015602796","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.43337926,0.000060391572,0.56423885,0.00017851482,0.00003469519,0.0008105393,0.00012060619,0.00005744083,0.0011196936],"genre_scores_gemma":[0.88971883,0.00025212904,0.10924928,0.0000041978265,0.00008172286,0.0000043206182,0.0001053607,0.0000293326,0.0005548115],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99870014,0.00006996198,0.00016502697,0.00025390115,0.00033273257,0.00047823583],"domain_scores_gemma":[0.998847,0.00048051882,0.000034648572,0.00022800027,0.00018334443,0.00022645811],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00043574892,0.00015787676,0.0003135453,0.00023771901,0.00030817278,0.000039857605,0.00030532046,0.00009280215,0.00013257336],"category_scores_gemma":[0.000035779543,0.00017597254,0.00006404869,0.00020621144,0.00018891567,0.00024490224,0.00012290655,0.00041148887,0.00002306729],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00023953298,0.0001880117,0.0084853,0.0027081035,0.0003856795,0.000008741583,0.004824433,0.03750522,0.7578081,0.0006855066,0.01966973,0.16749167],"study_design_scores_gemma":[0.0008770308,0.00023378876,0.012159717,0.0001440152,0.000023670187,8.558123e-7,0.00036496363,0.97932255,0.0012917398,0.0009166879,0.0044695246,0.00019545243],"about_ca_topic_score_codex":0.0001307712,"about_ca_topic_score_gemma":0.00001482387,"teacher_disagreement_score":0.94181734,"about_ca_system_score_codex":0.000053702257,"about_ca_system_score_gemma":0.00004072822,"threshold_uncertainty_score":0.7175952},"labels":[],"label_agreement":null},{"id":"W7018678190","doi":"","title":"Effect of nozzle geometry on mixing characteristics of turbulent free orifice jets","year":2017,"lang":"en","type":"dissertation","venue":"Mspace (University of Manitoba)","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Winnipeg; University of Manitoba","funders":"","keywords":"Nucleofection; Gestational period; TSG101; Liquation; Diafiltration; Hemopericardium","score_opus":0.006081596184172982,"score_gpt":0.19684067676684142,"score_spread":0.19075908058266844,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7018678190","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99173427,0.000097853095,0.00045150623,0.000012142007,0.0010500132,0.00020391101,0.00022211779,0.00004248235,0.006185703],"genre_scores_gemma":[0.99813414,0.00026235497,0.00035504898,9.4866766e-7,0.00006880715,2.776085e-7,0.0002970981,0.00004583366,0.0008355098],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.9990721,0.000029233559,0.00016933652,0.00020832552,0.00033360618,0.000187431],"domain_scores_gemma":[0.9985244,0.00014976457,0.00044054302,0.0006879308,0.00014345576,0.000053859854],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00021173128,0.00026096805,0.0006358488,0.0002676443,0.00012202001,0.000014359346,0.00070064416,0.00032853012,0.000010947367],"category_scores_gemma":[0.000099927274,0.0003305665,0.000189716,0.000095233496,0.0000757843,0.00006928535,0.000053291802,0.0003514685,0.000009743105],"study_design_candidate":"observational","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.007926179,0.0021397087,0.068111144,0.15672159,0.008777309,0.0019113016,0.009307258,0.078741096,0.3673885,0.0059202984,0.041034658,0.25202098],"study_design_scores_gemma":[0.005384013,0.0031240215,0.78484416,0.009412517,0.0031135683,0.000012493638,0.008913501,0.1174964,0.058108766,0.00020098677,0.006423294,0.0029662973],"about_ca_topic_score_codex":0.0003357685,"about_ca_topic_score_gemma":0.008909616,"teacher_disagreement_score":0.716733,"about_ca_system_score_codex":0.000093987495,"about_ca_system_score_gemma":0.000028402757,"threshold_uncertainty_score":0.99991465},"labels":[],"label_agreement":null},{"id":"W7034502494","doi":"","title":"Tonal Noise Prediction Of Serrated Trailing-Edge Airfoils","year":2023,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"Carleton University","funders":"","keywords":"Serration; Sawtooth wave; Airfoil; Amplitude; Noise (video); Wind tunnel; Vortex shedding","score_opus":0.012055515494521381,"score_gpt":0.19302383342027038,"score_spread":0.180968317925749,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7034502494","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.96667504,0.00008448488,0.017409446,0.00006213095,0.0026702464,0.00020139398,0.0025676903,0.0005469423,0.0097826095],"genre_scores_gemma":[0.9983524,0.000094376424,0.0004836243,0.000040229676,0.00020275,0.0000071514,0.00022500343,0.000051546776,0.00054288545],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99908507,0.000006798421,0.00024760398,0.0001339328,0.0001394434,0.00038714847],"domain_scores_gemma":[0.9993373,0.000039885846,0.000022674467,0.00020700158,0.00009424889,0.00029889937],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012025315,0.00013836984,0.0001546163,0.0002456183,0.000066838,0.000018489738,0.0001576697,0.00015253702,0.00008685718],"category_scores_gemma":[0.00007052562,0.0001633126,0.000044986322,0.0005034129,0.000048850867,0.000043446576,0.000012265615,0.00019330262,0.000071011455],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00000150777,0.000005390045,0.00036308903,0.00013407048,0.000039845214,0.00004265884,0.00016838429,0.89416784,0.07763228,0.00040052133,0.025502767,0.0015416442],"study_design_scores_gemma":[0.00013981525,0.000019213374,0.018758016,0.00003843365,0.000033906217,0.000004420739,0.000100121455,0.9788481,0.00018037611,0.00017463024,0.0015608585,0.00014211795],"about_ca_topic_score_codex":0.0007130107,"about_ca_topic_score_gemma":0.0025039355,"teacher_disagreement_score":0.084680244,"about_ca_system_score_codex":0.00013539413,"about_ca_system_score_gemma":0.00019973396,"threshold_uncertainty_score":0.66596943},"labels":[],"label_agreement":null},{"id":"W7037814882","doi":"","title":"Evaluation of aircrew noise exposure and hearing protection solutions in CH- 147F Chinook Helicopter Cabin","year":2017,"lang":"en","type":"article","venue":"NPARC","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Aircrew; Noise (video); Attenuation; Lift (data mining); Noise exposure; Sound pressure; Noise level; Aircraft noise","score_opus":0.03871486510071686,"score_gpt":0.2572370498172845,"score_spread":0.21852218471656765,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7037814882","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9842777,0.00010189157,0.0054808403,0.00008040006,0.00020664993,0.00028397303,0.000006298293,0.000030985193,0.009531209],"genre_scores_gemma":[0.9989174,0.000041030537,0.00089376804,0.0000028719887,0.000055743763,0.00004520122,0.0000020694738,0.00001311328,0.000028805614],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99941254,0.000021099797,0.00014101077,0.000103724306,0.00019251084,0.00012910496],"domain_scores_gemma":[0.9996286,0.000007322671,0.000035196903,0.00023563292,0.00006680767,0.000026407108],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006043517,0.0000733415,0.000097777905,0.00005615335,0.00011664263,0.000032861324,0.00007491075,0.00006315,0.00003285799],"category_scores_gemma":[0.00010321305,0.00007779074,0.000018447998,0.000029523148,0.00003359981,0.00011573684,0.000042099196,0.00013280327,0.0000030413078],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000010176579,0.00006071512,0.004437077,0.00020028131,0.000044323733,0.0000020305367,0.0007674584,0.20123821,0.58432066,0.00091853127,0.00008879028,0.2079117],"study_design_scores_gemma":[0.000382601,0.000020173236,0.07519958,0.00006744558,0.000024122844,0.0000021218877,0.00001852521,0.9200794,0.0013393027,0.0027534424,0.00002783867,0.00008546168],"about_ca_topic_score_codex":0.000057025696,"about_ca_topic_score_gemma":0.00025982855,"teacher_disagreement_score":0.71884114,"about_ca_system_score_codex":0.000074951524,"about_ca_system_score_gemma":0.000018348137,"threshold_uncertainty_score":0.31722143},"labels":[],"label_agreement":null},{"id":"W7037857089","doi":"","title":"Experimental and Computational Approach for Jet Noise Mitigation by Mixing Control Devices","year":2015,"lang":"en","type":"article","venue":"Institutional Repositories DataBase (IRDB)","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Mixing (physics); Noise (video); Jet (fluid); Control (management); Control system","score_opus":0.01256966546069726,"score_gpt":0.23770001863382895,"score_spread":0.22513035317313168,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7037857089","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.14351048,0.0022857985,0.8494247,0.000027870836,0.0015259145,0.00031774584,0.0016190837,0.00013370063,0.0011546554],"genre_scores_gemma":[0.93975693,0.000006581689,0.056520876,0.00004102399,0.00059686945,0.000106573876,0.0029398724,0.0000196812,0.0000115866205],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9990157,0.00001435998,0.00025567954,0.0002393018,0.00029771382,0.00017727491],"domain_scores_gemma":[0.99942905,0.000096321026,0.000048027978,0.00012658801,0.00015398847,0.00014599884],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015944995,0.00017484727,0.00015455318,0.000041959032,0.00024327538,0.0001202635,0.00010141107,0.000057830453,0.0000015406041],"category_scores_gemma":[0.00008155918,0.00017748866,0.000033398424,0.00007255987,0.00013802495,0.00047328664,0.000039260227,0.000106487016,0.0000018379009],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00023294082,0.00038519403,0.006522297,0.0005545832,0.00029494351,0.000024817835,0.0005927754,0.7326127,0.08139665,0.1433478,0.033374924,0.0006603361],"study_design_scores_gemma":[0.0014244759,0.000040096515,0.0002620678,0.000052710027,0.00004019049,0.000059116293,0.00016732114,0.97892267,0.0027826743,0.00045660144,0.0154705215,0.000321583],"about_ca_topic_score_codex":0.000019236546,"about_ca_topic_score_gemma":0.0000020786958,"teacher_disagreement_score":0.79624647,"about_ca_system_score_codex":0.00016042219,"about_ca_system_score_gemma":0.00009056661,"threshold_uncertainty_score":0.7237778},"labels":[],"label_agreement":null},{"id":"W7065843376","doi":"","title":"Experimental Modal Analysis of a Half-Scale Model Rear Twin-Engine Mounted Aircraft Fuselage Section","year":2018,"lang":"en","type":"dissertation","venue":"QSpace (Queen's University Library)","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Modal testing; Modal; Modal analysis; Mode (computer interface); Modal matrix; Work (physics)","score_opus":0.0038482342509076634,"score_gpt":0.18738719757353814,"score_spread":0.18353896332263048,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7065843376","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.96227914,0.000040886553,0.022289002,0.00015628192,0.0006631921,0.00027547497,0.00041819646,0.0005519167,0.013325906],"genre_scores_gemma":[0.9278156,0.00017326811,0.0077649914,0.000009678756,0.00013740401,0.0000021003214,0.0031615638,0.00013185246,0.06080351],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9985521,0.000034618595,0.0002687408,0.00047040338,0.0003329447,0.0003411929],"domain_scores_gemma":[0.9990707,0.000028669,0.00015468238,0.00050437497,0.00008573293,0.00015581989],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00003641801,0.000447814,0.0006465177,0.0010602169,0.00013287022,0.00004572973,0.00041773546,0.0005517165,0.00033735714],"category_scores_gemma":[0.0000051127768,0.0005695276,0.00040278,0.0012205065,0.000061719285,0.0006661076,0.000087764616,0.00046157805,0.000011042916],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0002610493,0.00021127473,0.00025681104,0.0003130786,0.0022532442,0.0000491258,0.0031583537,0.95594823,0.006107923,0.0004373551,0.030943945,0.0000596199],"study_design_scores_gemma":[0.00043360607,0.00009177153,0.0007378394,0.00009870499,0.0014336564,1.6632711e-7,0.0025250895,0.97252494,0.01877129,0.000040857547,0.0026252824,0.0007167976],"about_ca_topic_score_codex":0.0009678117,"about_ca_topic_score_gemma":0.00023652824,"teacher_disagreement_score":0.047477603,"about_ca_system_score_codex":0.00023225426,"about_ca_system_score_gemma":0.00008372862,"threshold_uncertainty_score":0.99967563},"labels":[],"label_agreement":null},{"id":"W7070555505","doi":"","title":"Phased microphone array measurements of a bombardier aircraft scaled model","year":2013,"lang":"en","type":"article","venue":"NPARC","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Microphone array; Beamforming; Microphone; Calibration; Noise (video); Phased array; Directivity; Noise-canceling microphone; Aeroacoustics","score_opus":0.014236720317319722,"score_gpt":0.20776148750378315,"score_spread":0.19352476718646341,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7070555505","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.5127685,0.000070846254,0.43576866,0.00004922143,0.000304092,0.00024211113,0.000023029343,0.00011991051,0.050653618],"genre_scores_gemma":[0.9184223,0.000012525223,0.08115034,0.0000286588,0.000042185606,0.000025937918,0.000004480861,0.00003487038,0.00027873798],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992203,0.000007798212,0.00021931139,0.00012488743,0.00020130446,0.00022638869],"domain_scores_gemma":[0.9995448,0.000011583906,0.000025857982,0.00024936616,0.00009486218,0.000073529416],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00009054571,0.00013201547,0.00018982738,0.00004609295,0.000027138467,0.000015081623,0.0001531911,0.00006671657,0.00032526942],"category_scores_gemma":[0.000015226889,0.00012864258,0.000066278764,0.00008520976,0.000034651468,0.000060364757,0.000012964651,0.00011148221,0.00008365493],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000022970703,0.000031639855,0.0000762673,0.000037660127,0.000038519804,3.218718e-7,0.00005909117,0.07091156,0.9244899,0.000011212774,0.0032794836,0.0010620555],"study_design_scores_gemma":[0.0006164937,0.00001697411,0.00014325538,0.0000342874,0.00002593264,0.0000010979958,0.000011576049,0.65512073,0.3404021,0.0033030633,0.000116070434,0.0002084376],"about_ca_topic_score_codex":0.000005728491,"about_ca_topic_score_gemma":0.0000025035436,"teacher_disagreement_score":0.58420914,"about_ca_system_score_codex":0.00004258584,"about_ca_system_score_gemma":0.000014423963,"threshold_uncertainty_score":0.52458924},"labels":[],"label_agreement":null},{"id":"W7096396606","doi":"","title":"STUDY AND COMPARISON OF RESULTS OF EXPERIMENTAL AND NUMERICAL SOLUTIONS FOR HYDRAULIC ANALOGY","year":2016,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Supersonic speed; Aerodynamics; Choked flow; Compressibility; Compressible flow; Flow (mathematics); Supercritical flow; Sonic boom; Mach number","score_opus":0.026935061712597158,"score_gpt":0.29127180645905437,"score_spread":0.2643367447464572,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7096396606","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8798868,0.00017714298,0.11885958,0.000027858607,0.000054101813,0.00014195229,0.000038960898,0.00001735764,0.00079623784],"genre_scores_gemma":[0.99828094,0.0000068030536,0.001658011,0.0000020036523,0.000010781384,0.0000072808,0.0000013555024,0.0000064683913,0.000026339238],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99960536,0.0000054547622,0.00018321993,0.000076610915,0.000039458406,0.00008990826],"domain_scores_gemma":[0.99976677,0.00009644513,0.000021223339,0.00007441748,0.000015334148,0.000025795369],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00006322274,0.000050278,0.000144029,0.000025322646,0.000020595058,0.0000020807315,0.000030340385,0.00002264575,0.0000034887278],"category_scores_gemma":[0.000017803115,0.00003572792,0.000012726558,0.00002639371,0.000043632037,0.000019481471,0.000033248878,0.000017556544,1.7330444e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00029429636,0.0018962293,0.033107582,0.00014364666,0.00041527307,0.0000024804754,0.0055829147,0.010827034,0.8950178,0.015665235,0.006614445,0.030433053],"study_design_scores_gemma":[0.004057326,0.0012876849,0.018146405,0.000027324351,0.000052715674,0.0000032295916,0.0031292138,0.9521242,0.020240385,0.00033669316,0.00036867455,0.00022614823],"about_ca_topic_score_codex":0.000014828465,"about_ca_topic_score_gemma":0.000011538108,"teacher_disagreement_score":0.9412972,"about_ca_system_score_codex":0.000007721931,"about_ca_system_score_gemma":0.0000023594964,"threshold_uncertainty_score":0.14569424},"labels":[],"label_agreement":null},{"id":"W7096399297","doi":"","title":"Table of Contents","year":2007,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Bruit; Table (database); Noise (video); National standard","score_opus":0.007675681363540377,"score_gpt":0.20470540244399835,"score_spread":0.19702972108045796,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7096399297","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.3713413,0.000059061185,0.37192172,0.0000032863136,0.00031700212,0.00003100146,0.0000037408772,0.00008155687,0.25624135],"genre_scores_gemma":[0.99541795,0.000010313333,0.0036284123,0.000010871357,0.000018389645,2.2891636e-7,0.0000010987776,0.000006599761,0.00090612995],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997665,4.000066e-7,0.000081835715,0.000025919293,0.00004199065,0.00008334929],"domain_scores_gemma":[0.99988455,0.0000135489245,0.00000507289,0.000061171464,0.00001686539,0.000018810184],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000060232618,0.00002901749,0.00004598831,0.00001543906,0.0000053961276,0.000001887478,0.000040232284,0.000019712243,0.00008467474],"category_scores_gemma":[0.000005725122,0.00002622589,0.000010429031,0.000043962576,0.0000075500643,0.00001460983,0.000006915945,0.000028048189,0.0000095632495],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00001470498,0.00010353218,0.012045277,0.0002233718,0.00013648803,0.00002599437,0.00019539692,0.17690453,0.65635467,0.100398295,0.02301619,0.030581547],"study_design_scores_gemma":[0.0005125569,0.00003616504,0.011331437,0.000025935897,0.000014624366,0.0000039215247,0.00019191526,0.8910805,0.07868728,0.001469618,0.016368408,0.00027765916],"about_ca_topic_score_codex":0.000007126803,"about_ca_topic_score_gemma":0.000018184588,"teacher_disagreement_score":0.71417594,"about_ca_system_score_codex":0.0000051871316,"about_ca_system_score_gemma":9.205301e-7,"threshold_uncertainty_score":0.10694607},"labels":[],"label_agreement":null},{"id":"W7100297150","doi":"","title":"Proceedings of the 2002 Fluids Engineering Division Summer Meeting July 14 - 18, 2002, Montreal, Quebec, Canada","year":2002,"lang":"en","type":"article","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Flow (mathematics); Division (mathematics); Field (mathematics); Quadratic equation; Estimation","score_opus":0.0066145126077029525,"score_gpt":0.1646139798091798,"score_spread":0.15799946720147684,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7100297150","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.62324905,0.002246066,0.0044577466,0.0003630921,0.0026443857,0.0006861696,0.000076426986,0.0006298729,0.36564717],"genre_scores_gemma":[0.9854293,0.00011435753,0.00082636246,0.00004412932,0.000104877516,0.000008602954,0.000001099264,0.000060245748,0.013411021],"study_design_codex":"not_applicable","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9987556,0.0000027539234,0.00034142504,0.00018032388,0.00034314196,0.000376796],"domain_scores_gemma":[0.99953187,0.000054074502,0.000042865682,0.0001817721,0.0001005767,0.00008883928],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00009708767,0.00022613976,0.00021229137,0.000047041907,0.00007808241,0.00004301563,0.0003082591,0.00008769433,0.0005104932],"category_scores_gemma":[0.0000789872,0.00017508175,0.000067379835,0.00025473023,0.000021046222,0.00010629435,0.00008388194,0.00024238418,0.000013585943],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":true,"about_ca_topic_consensus":true,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[9.996949e-7,0.000024294619,0.00056370784,0.00020228235,0.000046734327,0.0000034131021,0.00013169022,0.286677,0.021326132,0.0002506521,0.6892273,0.0015458302],"study_design_scores_gemma":[0.00017083397,0.0000063197053,0.0022118166,0.00011824157,0.00002414366,0.0000021247533,0.00004018853,0.97639966,0.002991822,0.0000064611327,0.017755888,0.00027252582],"about_ca_topic_score_codex":0.11201304,"about_ca_topic_score_gemma":0.28983304,"teacher_disagreement_score":0.68972266,"about_ca_system_score_codex":0.00015895568,"about_ca_system_score_gemma":0.000017634035,"threshold_uncertainty_score":0.89390016},"labels":[],"label_agreement":null},{"id":"W7105647213","doi":"10.7868/s3034500625040078","title":"Features of background acoustic disturbances in high-speed wind tunnels","year":2025,"lang":"en","type":"article","venue":"Акустический журнал / Acoustical Physics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Supersonic speed; Mach number; Transonic; Aeroacoustics; Wind tunnel; Boundary layer; Compressible flow; Acoustic wave; Supersonic wind tunnel","score_opus":0.007733916224334626,"score_gpt":0.23412183467014216,"score_spread":0.22638791844580755,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7105647213","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.55022275,0.0010530849,0.4250083,0.00011609506,0.0027335463,0.00057985634,0.0002856476,0.00038037726,0.019620346],"genre_scores_gemma":[0.9966665,0.00014163308,0.0021238283,0.00010210544,0.00036376622,0.000010844388,0.000049150538,0.0000695627,0.0004726256],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99779075,0.000039331968,0.0006482208,0.00045399333,0.00040929692,0.00065841095],"domain_scores_gemma":[0.9986119,0.0004943371,0.00007426445,0.0005633782,0.00013250222,0.00012362009],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0001889183,0.00046047926,0.00073205517,0.00014740395,0.000081809085,0.00007227607,0.00051446474,0.00026919442,0.000041264502],"category_scores_gemma":[0.000121807185,0.00045421437,0.00014950914,0.0008501264,0.00030266188,0.00018237258,0.00015548116,0.00071229413,0.00002083236],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000050535335,0.00030435313,0.00049214927,0.00069993956,0.00014658901,0.000031870582,0.000109315966,0.91159785,0.04498318,0.028417211,0.0036948256,0.009472204],"study_design_scores_gemma":[0.0017719097,0.000115078874,0.045440156,0.0006251768,0.00032099243,0.0000039543884,0.00039166553,0.87663084,0.0034675733,0.06992591,0.00026318463,0.001043539],"about_ca_topic_score_codex":0.000043397024,"about_ca_topic_score_gemma":0.00004111144,"teacher_disagreement_score":0.44644374,"about_ca_system_score_codex":0.00020117697,"about_ca_system_score_gemma":0.00007765433,"threshold_uncertainty_score":0.99979097},"labels":[],"label_agreement":null},{"id":"W7106287642","doi":"10.1134/s1063771025600664","title":"Features of Background Acoustic Disturbances in High-Speed Wind Tunnels","year":2025,"lang":"en","type":"article","venue":"Acoustical Physics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Supersonic speed; Mach number; Transonic; Wind tunnel; Boundary layer; Aeroacoustics; Compressible flow; Turbulence; Acoustic wave","score_opus":0.007689065041994448,"score_gpt":0.23408523303139228,"score_spread":0.22639616798939782,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7106287642","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.57095826,0.00052825233,0.40902594,0.00007279368,0.0017185484,0.00031229516,0.00012420413,0.00020201357,0.017057715],"genre_scores_gemma":[0.99783045,0.000084718864,0.0015150021,0.00006046672,0.00019507512,0.0000041870903,0.000020961483,0.000032490552,0.00025666057],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9988373,0.000016944348,0.00034584443,0.00023666413,0.00020835003,0.00035488326],"domain_scores_gemma":[0.99919575,0.00034011333,0.000033117758,0.0003105484,0.00006279118,0.000057680565],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00009289195,0.00023622846,0.00039852288,0.00006749762,0.00004004439,0.00003225373,0.00027589148,0.00014085368,0.000020839903],"category_scores_gemma":[0.00006908828,0.00022890762,0.000074182404,0.00047505254,0.00016270347,0.000096897194,0.0000790281,0.00038867118,0.000010180237],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00002108402,0.0001581098,0.00030951254,0.0003840202,0.00007649418,0.000014490565,0.00005762182,0.9285971,0.035832077,0.025953509,0.0025538641,0.006042141],"study_design_scores_gemma":[0.00093474635,0.00005704846,0.045136105,0.00031204792,0.00017261424,0.00000146684,0.00020406971,0.8754057,0.0020539018,0.07508885,0.00011162731,0.00052179745],"about_ca_topic_score_codex":0.000028019791,"about_ca_topic_score_gemma":0.000020360483,"teacher_disagreement_score":0.4268722,"about_ca_system_score_codex":0.00009428296,"about_ca_system_score_gemma":0.00003471665,"threshold_uncertainty_score":0.9334582},"labels":[],"label_agreement":null},{"id":"W7116683018","doi":"10.18280/mmep.121118","title":"Analytical Investigation of Air Flow in a Continuous Closed-Circuit Supersonic Wind Tunnel","year":2025,"lang":"","type":"article","venue":"Mathematical Modelling and Engineering Problems","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Supersonic wind tunnel; Wind tunnel; Airflow; Supersonic speed; Flow (mathematics); Choked flow","score_opus":0.016839633507395382,"score_gpt":0.20288253183626195,"score_spread":0.18604289832886656,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7116683018","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.42447257,0.0010344124,0.57311016,0.00007631927,0.00020209735,0.0003491627,0.000015828631,0.00009224958,0.0006472009],"genre_scores_gemma":[0.9772879,0.00037710293,0.021979392,0.000015611342,0.000054497206,0.000024505429,0.000009722914,0.00008032073,0.0001709795],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9971867,0.000029790654,0.0012801618,0.000508856,0.00029735037,0.00069711014],"domain_scores_gemma":[0.9987791,0.00044986204,0.00007562643,0.000405057,0.000088800174,0.00020153879],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00078485534,0.0005206665,0.0010071937,0.00046988245,0.00006218705,0.00007854202,0.0002487087,0.0004476399,0.000018554487],"category_scores_gemma":[0.00015346977,0.00056448387,0.00015284363,0.0006729683,0.00014020049,0.00013728667,0.00010251554,0.00083415164,0.000007008851],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000067821206,0.00007890929,0.00017649896,0.0059364187,0.00013076511,0.0000075169264,0.0018131473,0.9407837,0.0008935544,0.049548607,0.000009422044,0.0006146817],"study_design_scores_gemma":[0.0006405167,0.00005477384,0.00016871445,0.003951659,0.00016551447,0.000007448662,0.00011939371,0.94977564,0.000083468214,0.044565015,0.00001911859,0.00044872108],"about_ca_topic_score_codex":0.000021210064,"about_ca_topic_score_gemma":0.000003855039,"teacher_disagreement_score":0.5528153,"about_ca_system_score_codex":0.00015069754,"about_ca_system_score_gemma":0.000065339664,"threshold_uncertainty_score":0.99968064},"labels":[],"label_agreement":null},{"id":"W7117299423","doi":"10.1016/j.ijheatfluidflow.2025.110207","title":"Direct numerical simulation of installation effects on airfoil noise","year":2025,"lang":"en","type":"article","venue":"International Journal of Heat and Fluid Flow","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"École de Technologie Supérieure; Université de Sherbrooke","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Airfoil; Trailing edge; Boundary layer; Reynolds number; Boundary layer thickness; Turbulence; Angle of attack; Direct numerical simulation; Reynolds stress; Noise (video)","score_opus":0.004021756833079732,"score_gpt":0.23591036757335399,"score_spread":0.23188861074027425,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7117299423","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7598764,0.0004920098,0.23124808,0.0001906813,0.0024734777,0.00006461344,0.000011716249,0.000020845177,0.0056222323],"genre_scores_gemma":[0.9986598,0.00016831484,0.0008699012,0.000058236208,0.000200109,6.445308e-7,0.000004078543,0.0000075835965,0.000031359785],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999395,0.000012905429,0.0002709486,0.000054163294,0.00020675207,0.00006023085],"domain_scores_gemma":[0.9995238,0.00020108453,0.000032459116,0.000048411574,0.00016547786,0.000028756876],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000104057624,0.00007602432,0.0001433745,0.00016908952,0.0000177058,0.00001971832,0.0000915295,0.000046150028,0.000008938757],"category_scores_gemma":[0.000079051475,0.00006726342,0.00005810699,0.00006560277,0.000013522697,0.0000812635,0.000016134045,0.00010213544,0.0000010841923],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000072172465,0.000026387817,0.00068437477,0.000031169835,0.00010096963,0.000009758183,0.000045594574,0.95556206,0.0132006835,0.00030577657,0.00023724498,0.029723784],"study_design_scores_gemma":[0.0004643383,0.00007056248,0.004735152,0.00018735717,0.000020067584,0.0000046854047,0.0000045234597,0.9896961,0.003578712,0.00031316688,0.0008704948,0.00005485181],"about_ca_topic_score_codex":0.0000018399534,"about_ca_topic_score_gemma":7.9117643e-7,"teacher_disagreement_score":0.23878343,"about_ca_system_score_codex":0.00006037155,"about_ca_system_score_gemma":0.000015324633,"threshold_uncertainty_score":0.27429226},"labels":[],"label_agreement":null},{"id":"W7126317553","doi":"","title":"Optimisation et test de la géométrie de la dentelure du bord de fuite des plaques planes pour réduire le bruit propre aux ailes","year":2020,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Trailing edge; Wind tunnel; Anechoic chamber; Serration; Airfoil; Noise (video); NACA airfoil; Microphone; Aeroacoustics","score_opus":0.008431846162694597,"score_gpt":0.2186850777797879,"score_spread":0.2102532316170933,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7126317553","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7909844,0.00043604203,0.20070918,0.0010183774,0.00012458417,0.00022568546,0.0006955106,0.00037165615,0.0054345527],"genre_scores_gemma":[0.97709745,0.00050477555,0.020997614,0.0007052379,0.0003690707,0.000017181195,0.00008334149,0.00009646685,0.00012886799],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9988878,0.000069568945,0.000194541,0.00019062743,0.000117770935,0.00053970976],"domain_scores_gemma":[0.998678,0.0004390511,0.00003548003,0.00015591405,0.000070763694,0.0006207411],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00027457913,0.00023481244,0.0001782933,0.0000871856,0.00019867925,0.00022978372,0.00027889805,0.0002955711,0.000037938975],"category_scores_gemma":[0.0009644305,0.00027445043,0.00004781707,0.0001513298,0.00016441796,0.00009901519,0.000030302166,0.00043064423,0.00001218341],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000063560374,0.000025952773,0.014202443,0.0003185553,0.000057842688,0.000566973,0.0028455968,0.9224841,0.025573365,0.002163487,0.028880322,0.002875001],"study_design_scores_gemma":[0.0003302212,0.00003693033,0.018811192,0.00010082392,0.00008489567,0.00014153626,0.0009886024,0.96880496,0.00031857027,0.0017288387,0.008231221,0.00042219236],"about_ca_topic_score_codex":0.005021618,"about_ca_topic_score_gemma":0.010362581,"teacher_disagreement_score":0.18611303,"about_ca_system_score_codex":0.00054373156,"about_ca_system_score_gemma":0.0014914862,"threshold_uncertainty_score":0.9999708},"labels":[],"label_agreement":null},{"id":"W7132906065","doi":"","title":"The Measurement and Application of Trailing-Edge Noise in the UTIAS Hybrid Anechoic Wind Tunnel","year":2024,"lang":"","type":"dissertation","venue":"TSpace","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Airfoil; Anechoic chamber; Wind tunnel; Aerodynamics; Noise (video); Angle of attack; Aeroacoustics; NACA airfoil; Boundary layer","score_opus":0.014766581806868016,"score_gpt":0.2728999406752801,"score_spread":0.2581333588684121,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7132906065","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.96292955,0.01975613,0.0054688,0.0009608923,0.0014652979,0.0019454205,0.000040267452,0.00005429872,0.007379344],"genre_scores_gemma":[0.99664015,0.0024686612,0.00009806392,0.000014782663,0.00018113166,0.00009411117,0.00007729275,0.00008198938,0.00034382445],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9978617,0.00006189936,0.0006119994,0.00045851737,0.00064058707,0.00036532865],"domain_scores_gemma":[0.99864435,0.00031611236,0.00018165809,0.0006409771,0.00015919162,0.000057710564],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0014894225,0.0004268087,0.0003616986,0.00012041448,0.00020430544,0.00015436103,0.00050014706,0.00020022294,0.000009809344],"category_scores_gemma":[0.0001455419,0.00030545294,0.00012034444,0.00035856979,0.0001045822,0.000041646977,0.000042913358,0.00086908654,0.000018056122],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00037808603,0.00048947014,0.00028867784,0.010480174,0.0009322091,0.000054342072,0.14629984,0.46339294,0.23779497,0.03624414,0.001424491,0.10222067],"study_design_scores_gemma":[0.00041971877,0.00007874044,0.006501051,0.00073979236,0.00041701907,0.000010952101,0.014392372,0.969327,0.0009527932,0.0039978037,0.002615038,0.0005477327],"about_ca_topic_score_codex":0.00017326868,"about_ca_topic_score_gemma":0.0015505992,"teacher_disagreement_score":0.50593406,"about_ca_system_score_codex":0.00012758681,"about_ca_system_score_gemma":0.00009257868,"threshold_uncertainty_score":0.99993974},"labels":[],"label_agreement":null},{"id":"W7133074981","doi":"","title":"Computational Aeroacoustic Predictions of the 30P30N High-Lift Airfoil using RANS Simulations","year":2025,"lang":"","type":"dissertation","venue":"TSpace","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Reynolds-averaged Navier–Stokes equations; Wind tunnel; Airfoil; Turbulence; Freestream; Aeroacoustics; Turbulence kinetic energy; Noise (video); Mach number","score_opus":0.013213351867339027,"score_gpt":0.28746520881808135,"score_spread":0.27425185695074233,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7133074981","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.41295078,0.00042933458,0.5743188,0.00023413246,0.006588643,0.0009042843,0.001163773,0.00011470668,0.003295545],"genre_scores_gemma":[0.98314,0.000085509244,0.008536357,0.000022985807,0.00029563735,0.000019946801,0.0009771086,0.00011089003,0.0068115476],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9971956,0.00010259042,0.0010088276,0.0005203952,0.0006958437,0.00047676306],"domain_scores_gemma":[0.9972202,0.0008748563,0.00043965882,0.0007304596,0.0006246706,0.00011014413],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00016439059,0.0006214864,0.0006774215,0.0003358618,0.0008021444,0.00008523394,0.0005813229,0.0005859978,0.0004053665],"category_scores_gemma":[0.00030874755,0.00062166946,0.00038326817,0.0011529935,0.00014521973,0.00010006934,0.00011304763,0.0009873484,0.000008568528],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000020378053,0.000113516595,0.00014183196,0.000909469,0.00039921905,0.0000011477674,0.001967027,0.98742044,0.0032868886,0.005396588,0.00020140948,0.00014210459],"study_design_scores_gemma":[0.0006284532,0.000024482104,0.0030858049,0.0011963852,0.0013080119,0.0000027459184,0.0009874123,0.9896503,0.00012609918,0.0024628274,0.00006699445,0.00046047638],"about_ca_topic_score_codex":0.00051523966,"about_ca_topic_score_gemma":0.0005391253,"teacher_disagreement_score":0.57018924,"about_ca_system_score_codex":0.00039117475,"about_ca_system_score_gemma":0.00071523205,"threshold_uncertainty_score":0.9996235},"labels":[],"label_agreement":null},{"id":"W7151307806","doi":"10.70675/2e0a95d6z6265z421fzb056z76c9ebe196b1","title":"Aerodynamic and acoustic investigation of automotive fan-driven cooling systems","year":2021,"lang":"","type":"dissertation","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Bruit; Noise (video); Aeroacoustics; High speed train; Diffuser (optics)","score_opus":0.007578744172517096,"score_gpt":0.21732874046783332,"score_spread":0.2097499962953162,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7151307806","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9178208,0.00339723,0.07076821,0.000015741029,0.0042744083,0.00087546324,0.00023033388,0.00013367787,0.0024841262],"genre_scores_gemma":[0.9901657,0.0023104788,0.002605202,0.000010998418,0.00023601599,0.000052277752,0.001993343,0.00019818768,0.0024278027],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99635893,0.00012773101,0.001526371,0.00084838935,0.000569026,0.0005695277],"domain_scores_gemma":[0.9970014,0.0005372953,0.00061757426,0.0005436551,0.0010342795,0.0002657834],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00032889922,0.0008542029,0.0013079932,0.00038774958,0.00020710837,0.00022510547,0.00030524604,0.00096298056,0.000111758694],"category_scores_gemma":[0.00036968355,0.0009795334,0.00019157774,0.00056857476,0.00017245949,0.00021347613,0.00010812343,0.0008967693,0.000011677925],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000017831191,0.000026836384,0.0006510601,0.0066646305,0.0004770537,0.000021295366,0.002238529,0.8765995,0.110890545,0.0021477132,0.00004092506,0.00022406076],"study_design_scores_gemma":[0.00044143866,0.000086687905,0.0085636955,0.0032184497,0.00072037184,0.000019849427,0.005526593,0.97942466,0.0009523003,0.00019501308,0.0000025468667,0.0008483874],"about_ca_topic_score_codex":0.00036762847,"about_ca_topic_score_gemma":0.0008446067,"teacher_disagreement_score":0.10993825,"about_ca_system_score_codex":0.00028381034,"about_ca_system_score_gemma":0.00029832852,"threshold_uncertainty_score":0.9992655},"labels":[],"label_agreement":null},{"id":"W7160903110","doi":"10.1121/10.0041262","title":"Study on aircraft noise calculation model for helicopters and advanced air mobility","year":2025,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"International Civil Aviation Organization","funders":"","keywords":"Aircraft noise; Noise (video); Rotor (electric); Position (finance); Point (geometry); Airplane; Noise measurement","score_opus":0.009461987576967913,"score_gpt":0.26020174300795673,"score_spread":0.2507397554309888,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7160903110","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.3060587,0.000068511574,0.6928533,0.000601662,0.00012217705,0.00024215253,0.000010957479,0.000010196608,0.000032367083],"genre_scores_gemma":[0.9771206,0.00012358907,0.022284204,0.00038227023,0.00003323325,0.000004173323,2.2992116e-7,0.00001148726,0.000040228817],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992549,0.000030618903,0.00031457836,0.000071360606,0.00019224524,0.0001363224],"domain_scores_gemma":[0.99917156,0.00035414152,0.00010647236,0.00022350301,0.00010791881,0.000036385718],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003708861,0.0001109467,0.00022989117,0.0000134604625,0.000117667725,0.0000067648352,0.00025102292,0.000043337706,8.024725e-7],"category_scores_gemma":[0.00011861841,0.00006415584,0.00018096811,0.00012074987,0.00017646252,0.000037304002,0.000067806875,0.00026179588,1.4175441e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00006688143,0.00010811747,0.000054286073,0.000049471626,0.000104402316,7.2959494e-8,0.0005012907,0.9861794,0.0056971665,0.0000064790734,0.0012081297,0.0060242685],"study_design_scores_gemma":[0.00044588855,0.00015795596,0.0026093072,0.000057692192,0.00017802107,0.0000011545449,0.00106763,0.99442786,0.00013042346,0.0008315036,0.000031226573,0.00006135438],"about_ca_topic_score_codex":0.0000033421225,"about_ca_topic_score_gemma":4.563585e-7,"teacher_disagreement_score":0.6710619,"about_ca_system_score_codex":0.00007459669,"about_ca_system_score_gemma":0.000027376862,"threshold_uncertainty_score":0.26161996},"labels":[],"label_agreement":null},{"id":"W7161757897","doi":"10.82308/20574","title":"Computational fluid dynamics in mesoscopic nozzles","year":2016,"lang":"en","type":"dissertation","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Hagen–Poiseuille equation; Computational fluid dynamics; Nozzle; Mesoscopic physics; Solver; Compressibility; Transonic; Compressible flow; Fluid dynamics","score_opus":0.003643722562132392,"score_gpt":0.21680232116702555,"score_spread":0.21315859860489317,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7161757897","genre_codex":"other","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.42635113,0.0006126007,0.08196199,0.0000616575,0.005323492,0.00043868143,0.00027395372,0.00059908256,0.4843774],"genre_scores_gemma":[0.980947,0.00021606586,0.0037666939,0.000018726694,0.00013248916,0.000028526509,0.002508881,0.000102089645,0.012279525],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99913937,0.0000064758997,0.0002970265,0.00018072785,0.00017044296,0.0002059303],"domain_scores_gemma":[0.9996791,0.00006725432,0.000028663571,0.00013847384,0.000047000747,0.000039496645],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00005524757,0.00022760176,0.00023309459,0.00016852014,0.000027131646,0.000027668513,0.00016336962,0.00025362094,0.00023256606],"category_scores_gemma":[0.000013499549,0.00020365283,0.000051439554,0.00009271761,0.000011226204,0.000046089743,0.00000998578,0.00020413239,0.00009611727],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000267171,0.00008992799,0.0013550832,0.0013209664,0.00021334164,0.000058732952,0.0003907073,0.7894623,0.0010399469,0.15188853,0.0052634114,0.04889031],"study_design_scores_gemma":[0.00020646253,0.000007706493,0.0018946613,0.00019549788,0.000011661043,9.5365704e-7,0.00013833048,0.98937064,0.00005030056,0.0076452335,0.00016278111,0.0003157843],"about_ca_topic_score_codex":0.0000148277795,"about_ca_topic_score_gemma":0.0016976084,"teacher_disagreement_score":0.5545959,"about_ca_system_score_codex":0.00032806877,"about_ca_system_score_gemma":0.000039455885,"threshold_uncertainty_score":0.8304722},"labels":[],"label_agreement":null},{"id":"W81798676","doi":"10.1007/978-1-4419-9507-0_12","title":"High Intensity Noise Generation for Extremely Large Reverberant Room Test Applications","year":2011,"lang":"en","type":"book-chapter","venue":"Conference proceedings of the Society for Experimental Mechanics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University; National Research Council Canada","funders":"National Aeronautics and Space Administration","keywords":"Aerospace; Engineering; Sound pressure; Noise (video); Power (physics); Electrical engineering; Aerospace engineering; Computer science; Telecommunications","score_opus":0.02861294626319887,"score_gpt":0.22237115302501725,"score_spread":0.19375820676181837,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W81798676","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0037835422,0.0024193402,0.9584438,0.00017550358,0.0037337977,0.010490615,0.005233693,0.000557666,0.015162043],"genre_scores_gemma":[0.9317776,0.0006237007,0.04488888,0.00015434355,0.00077839935,0.0013234424,0.0002810991,0.00027616275,0.019896394],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99873286,4.3166554e-7,0.00041960643,0.00037457873,0.00019095607,0.00028155342],"domain_scores_gemma":[0.99877554,0.000029544257,0.0002761858,0.00021960028,0.00063392456,0.000065225955],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00016717546,0.00038922956,0.00043273505,0.000023099641,0.00024926054,0.000051409705,0.0005138598,0.00041194842,0.00003516876],"category_scores_gemma":[0.00002339538,0.00035574083,0.00077899656,0.00003150791,0.00004432255,0.00009686641,0.00018684,0.00026577845,0.000002583917],"study_design_candidate":"theoretical_or_conceptual","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000012873684,0.00006509589,4.756236e-7,0.00036259458,0.0001913011,2.005675e-8,0.0006523622,0.00003052564,0.38756415,0.6023184,0.008391729,0.00041048572],"study_design_scores_gemma":[0.00089090125,0.00026331114,4.7032276e-7,0.00037229774,0.0004957108,0.000004674483,0.0006283369,0.53593355,0.2965156,0.14435683,0.01959044,0.00094785506],"about_ca_topic_score_codex":0.0000019959102,"about_ca_topic_score_gemma":0.0000020863083,"teacher_disagreement_score":0.927994,"about_ca_system_score_codex":0.00021611017,"about_ca_system_score_gemma":0.00004042104,"threshold_uncertainty_score":0.99988943},"labels":[],"label_agreement":null},{"id":"W909481505","doi":"10.1007/s12206-015-0420-7","title":"Design and testing of low-divergence elliptical-jet nozzles","year":2015,"lang":"en","type":"article","venue":"Journal of Mechanical Science and Technology","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":16,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Dalhousie University","funders":"Dalhousie University","keywords":"Nozzle; Jet (fluid); Divergence (linguistics); Fabrication; Machining; Materials science; Mechanics; Mechanical engineering; Geometry; Physics; Engineering; Mathematics","score_opus":0.02604475649993842,"score_gpt":0.2368808878468464,"score_spread":0.21083613134690798,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W909481505","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.78345674,0.00029225182,0.21572219,0.00019136231,0.00019630215,0.000038667033,5.726268e-7,0.000025544325,0.00007636969],"genre_scores_gemma":[0.91824096,0.00013475012,0.08159063,0.000007682223,0.000020190833,4.0908597e-7,1.3083898e-8,0.000003964919,0.0000014092144],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992359,0.000006930392,0.00024605665,0.00008998827,0.00025284314,0.00016827186],"domain_scores_gemma":[0.9992571,0.000099835546,0.00007528628,0.00008227631,0.00036455184,0.000120984994],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0010001537,0.00006698048,0.0001708081,0.00016881776,0.000042026903,0.000015503596,0.00025766483,0.000087707245,0.000002205916],"category_scores_gemma":[0.0012555133,0.000050078186,0.0000095346695,0.0005582381,0.0003647406,0.00010771644,0.0001087018,0.00019925022,6.9966893e-7],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000133964,0.000047442983,0.0009067679,0.00004457379,0.000017457878,0.00006631773,0.00005814561,0.008856966,0.90787166,0.027416855,0.00013859362,0.05456184],"study_design_scores_gemma":[0.00032031455,0.0006117519,0.00009163868,0.00010138565,0.000023382614,0.00041879565,0.00019235995,0.81628674,0.11468721,0.06703627,0.000092692375,0.00013745487],"about_ca_topic_score_codex":8.338955e-7,"about_ca_topic_score_gemma":4.801293e-7,"teacher_disagreement_score":0.8074298,"about_ca_system_score_codex":0.000027394444,"about_ca_system_score_gemma":0.00007424608,"threshold_uncertainty_score":0.20421292},"labels":[],"label_agreement":null},{"id":"W961076052","doi":"10.1007/978-3-540-39507-2_33","title":"Analysis of Sound Sources for a Generic Car Mirror","year":2006,"lang":"en","type":"book-chapter","venue":"","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Bombardier (Canada)","funders":"","keywords":"Sound pressure; Acoustics; Aeroacoustics; Noise (video); Transient (computer programming); Engineering; Reynolds-averaged Navier–Stokes equations; Flow (mathematics); Aerospace engineering; Sound (geography); Marine engineering; Computer science; Computational fluid dynamics; Physics; Mechanics; Artificial intelligence","score_opus":0.014784128034925112,"score_gpt":0.21165976061284988,"score_spread":0.1968756325779248,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W961076052","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0057648458,0.0009929106,0.22316815,0.0000041873454,0.00031424413,0.00026413097,0.0008907712,0.00016527761,0.7684355],"genre_scores_gemma":[0.21437675,0.0002291847,0.018813228,0.000033052354,0.00024131997,0.00003169593,0.0009644579,0.00025244488,0.76505786],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991688,0.0000011377825,0.00033923602,0.00019002675,0.00013661494,0.00016414441],"domain_scores_gemma":[0.9994684,0.000060814993,0.00007773439,0.00028615992,0.00007121538,0.00003568786],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000053943928,0.00025123917,0.00055260037,0.00031424506,0.000026089141,0.000016519418,0.0001564578,0.00024617242,0.00023484517],"category_scores_gemma":[0.0000034070915,0.00024156731,0.00044943223,0.000065792454,0.00003758668,0.000013092771,0.000023722445,0.00010282851,0.000004610313],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000057599054,0.000014570037,0.00008444655,0.00046020132,0.0064362464,0.000005435064,0.00005954791,0.93895423,0.0010290773,0.040913075,0.01106324,0.0009741386],"study_design_scores_gemma":[0.000120722296,0.000023491315,0.000053453055,0.00001995156,0.003927134,5.596901e-7,0.00000794805,0.9304155,0.000033893346,0.004021169,0.060900003,0.00047614763],"about_ca_topic_score_codex":0.000036197293,"about_ca_topic_score_gemma":0.00033856343,"teacher_disagreement_score":0.2086119,"about_ca_system_score_codex":0.000046755675,"about_ca_system_score_gemma":0.000009523295,"threshold_uncertainty_score":0.98508286},"labels":[],"label_agreement":null},{"id":"W984552799","doi":"10.1016/j.jsv.2015.06.003","title":"Design of multi-modal obstruction to control tonal fan noise using modulation principles","year":2015,"lang":"en","type":"article","venue":"Journal of Sound and Vibration","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Acoustics; Modal; Noise control; Noise (video); Modulation (music); Engineering; Structural engineering; Physics; Computer science; Noise reduction; Materials science; Artificial intelligence","score_opus":0.0512385047232341,"score_gpt":0.2613943211310817,"score_spread":0.21015581640784758,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W984552799","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.47990137,0.000026632999,0.519827,0.000007607796,0.00018391959,0.000041732917,0.0000019289514,0.0000039614124,0.000005842709],"genre_scores_gemma":[0.93417066,0.0000061070064,0.0656297,0.00000752712,0.00017344054,3.391544e-7,0.0000013292105,0.000008325309,0.000002552349],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994665,0.000017003718,0.00027429374,0.00004286188,0.00013739886,0.00006196603],"domain_scores_gemma":[0.99960786,0.000022466378,0.00011332897,0.00003747956,0.00015296307,0.00006591009],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023045685,0.000061534985,0.000115661554,0.00007727667,0.0000289741,0.00003155781,0.00003152416,0.00004420514,0.0000015393591],"category_scores_gemma":[0.000044077216,0.000055955814,0.000020966425,0.000053066815,0.000011425218,0.00023803274,0.000005607818,0.000065608336,2.652706e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000029878243,0.000009351217,0.00056192593,0.000010355251,0.000014091655,5.970439e-7,0.00025658146,0.8549725,0.14315909,0.0001459318,0.00000326217,0.00083642284],"study_design_scores_gemma":[0.0005538446,0.00008049413,0.0048520216,0.000021572625,0.000021095686,0.000021239957,0.000103793114,0.99255496,0.00092033885,0.0008065043,0.0000062198933,0.000057927813],"about_ca_topic_score_codex":0.000002360385,"about_ca_topic_score_gemma":0.0000022639,"teacher_disagreement_score":0.45426932,"about_ca_system_score_codex":0.000055923112,"about_ca_system_score_gemma":0.000021767248,"threshold_uncertainty_score":0.22818118},"labels":[],"label_agreement":null}]}