{"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.17682275,0.0003056205,0.8197192,0.00007192802,0.000060269962,0.000065262146,0.00017726679,0.0012723746,0.0015053443],"genre_scores_gemma":[0.8998406,0.00021203309,0.09789001,0.000029941362,0.000028587965,0.00006433287,0.00034500594,0.00008538714,0.0015040596],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99986494,0.000018546685,0.0000063131047,0.000034387565,0.00004921232,0.00002653484],"domain_scores_gemma":[0.9996656,0.00014366244,0.00005222537,0.000016550866,0.00008551522,0.00003646412],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00036600375,0.00069387717,0.00037567597,0.0011305318,0.00025716232,0.00055752636,0.00048487747,0.00077188696,0.0013147998],"category_scores_gemma":[0.0010109147,0.00023674495,0.00041416686,0.00036374904,0.0002196541,0.00041347195,0.00034586334,0.00040002493,0.000538435],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00037579364,0.00013769347,0.012193923,0.00014561412,0.0000799975,0.00028768685,0.00009617909,0.73165226,0.06379889,0.0014937373,0.0009798934,0.18875842],"study_design_scores_gemma":[0.0000024022258,0.000043923366,0.0015762111,0.0000034418008,0.0000050065773,0.000033735298,0.000021434362,0.9955048,0.0023157888,0.00027292923,0.00021432573,0.0000060481343],"about_ca_topic_score_codex":0.0029040787,"about_ca_topic_score_gemma":0.0027530822,"teacher_disagreement_score":0.0029040787,"about_ca_system_score_codex":0.0003475818,"about_ca_system_score_gemma":0.00050709007,"threshold_uncertainty_score":0.005774319},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9523181,0.0002405318,0.03960672,0.00011452711,0.000052193463,0.00006390475,0.00013907562,0.00019662397,0.007268309],"genre_scores_gemma":[0.9954502,0.00006501102,0.003706819,0.000008037537,0.000006154594,0.000013817233,0.0000369872,0.000010351373,0.0007025979],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997662,0.00006516293,0.000010206417,0.000031972788,0.00009463084,0.00003177263],"domain_scores_gemma":[0.9992403,0.0005083572,0.000065416425,0.000034604218,0.00010860456,0.00004273344],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00043603,0.00054925325,0.000505405,0.0004335034,0.00039609853,0.00046122604,0.00037189067,0.00060153974,0.0016346718],"category_scores_gemma":[0.0011488118,0.00014166589,0.00038930387,0.00024973444,0.0009543742,0.0003390349,0.0003677103,0.00028301185,0.00020078733],"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":[0.0013287439,0.00035953065,0.0087762745,0.00038687946,0.000032035023,0.0024123758,0.0005688308,0.6082747,0.34343272,0.0077244136,0.0007350394,0.025968442],"study_design_scores_gemma":[0.00011046211,0.00073263876,0.007571041,0.000030433828,0.00001559132,0.00052263145,0.00013278582,0.94794834,0.040814504,0.0013320419,0.00074539747,0.000044183853],"about_ca_topic_score_codex":0.0019763533,"about_ca_topic_score_gemma":0.001072438,"teacher_disagreement_score":0.0019763533,"about_ca_system_score_codex":0.0003044182,"about_ca_system_score_gemma":0.0003778864,"threshold_uncertainty_score":0.0054684877},"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":"methods","genre_gemma":"methods","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.09905654,0.0003359906,0.89443874,0.00025174997,0.0000834063,0.0000771837,0.000088103356,0.00028269266,0.00538571],"genre_scores_gemma":[0.9313197,0.0003994287,0.06377154,0.00006125761,0.00007537346,0.00014495358,0.00009636744,0.000065859305,0.004065556],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996885,0.000073757394,0.000014800404,0.000048115016,0.0001382669,0.00003657808],"domain_scores_gemma":[0.9995603,0.00018117414,0.0000489816,0.000034795354,0.00015308554,0.000021668024],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0007551832,0.00066166086,0.0006450176,0.00066842703,0.0006411441,0.0008627188,0.0013518719,0.0013088195,0.0007897493],"category_scores_gemma":[0.0019751028,0.00063151063,0.0007489923,0.0003622696,0.000942123,0.00092487806,0.00077019515,0.0008047214,0.00021112408],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000066360817,0.000022154072,0.00026707433,0.000014169117,0.0000075004427,0.000025034233,0.00001763254,0.9923051,0.0014485347,0.0027490128,0.00005961713,0.0030775666],"study_design_scores_gemma":[8.3953034e-7,0.0000040060963,0.000022120272,7.1731694e-7,7.326411e-7,0.0000014773078,0.0000016801555,0.99963105,0.00009837793,0.000191014,0.000046784517,0.0000011425345],"about_ca_topic_score_codex":0.01938791,"about_ca_topic_score_gemma":0.011216534,"teacher_disagreement_score":0.01938791,"about_ca_system_score_codex":0.00095162896,"about_ca_system_score_gemma":0.0020250336,"threshold_uncertainty_score":0.03855008},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99717665,0.00024057852,0.0018446262,0.000028481712,0.00001852623,0.0000126493915,0.000026908196,0.000038293747,0.00061324827],"genre_scores_gemma":[0.9990515,0.00006818567,0.00056123827,0.000017347602,0.000004420996,0.000004675906,0.000025982372,0.000006094217,0.0002604319],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9995388,0.000053457585,0.000029722712,0.00007145281,0.0002064669,0.0001001765],"domain_scores_gemma":[0.9990177,0.00046135264,0.00016172642,0.00007035095,0.00020982594,0.0000790471],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00039210063,0.00034570726,0.00030794734,0.00029011298,0.00026510036,0.00038195623,0.0003136365,0.00028269604,0.00082694367],"category_scores_gemma":[0.0019086584,0.0001994627,0.0002674196,0.00014060113,0.0004714226,0.0004273961,0.0005201312,0.00054357224,0.00014916355],"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":[0.0002496711,0.000037552538,0.0025092727,0.000041598876,0.0000052679893,0.00009403624,0.00008276877,0.00095288316,0.99070346,0.00009397043,0.000023288589,0.005206181],"study_design_scores_gemma":[0.000018503533,0.00077368924,0.026509337,0.0000053180866,0.000012686887,0.000092303955,0.00007549207,0.0051800227,0.9668992,0.00006389471,0.00035085587,0.000018644107],"about_ca_topic_score_codex":0.0015002006,"about_ca_topic_score_gemma":0.0010487405,"teacher_disagreement_score":0.0015002006,"about_ca_system_score_codex":0.00041088418,"about_ca_system_score_gemma":0.00017108554,"threshold_uncertainty_score":0.0029829144},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9598089,0.0012759349,0.033456843,0.00008417007,0.000102672086,0.00004836819,0.00007618403,0.0004203259,0.0047267256],"genre_scores_gemma":[0.97837466,0.00081739784,0.014762839,0.00009271698,0.000042068605,0.000031612068,0.00027769335,0.00012121011,0.00547969],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9995192,0.00007088557,0.000021808995,0.000057756493,0.00022025466,0.0001099797],"domain_scores_gemma":[0.9986407,0.0005175849,0.00012384646,0.00013759584,0.0004884681,0.00009178209],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00031995217,0.00055833725,0.0006216061,0.00042823865,0.00039466083,0.000491934,0.0003370966,0.0005560931,0.0027449646],"category_scores_gemma":[0.0013295391,0.00016790247,0.00038289427,0.0003597977,0.0004570991,0.000516335,0.00066083,0.0005099152,0.0009548559],"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":[0.0005095587,0.00005932086,0.0009814048,0.00012635133,0.000016136857,0.00020570194,0.00025721622,0.0006007578,0.9596129,0.0001245167,0.00022995865,0.037276223],"study_design_scores_gemma":[0.00002947176,0.0010608949,0.0154730985,0.000018128338,0.000060690392,0.00048100957,0.00021754263,0.0051486497,0.9743949,0.00009490448,0.0029839592,0.000036721103],"about_ca_topic_score_codex":0.0022269948,"about_ca_topic_score_gemma":0.002594379,"teacher_disagreement_score":0.0027449646,"about_ca_system_score_codex":0.00012778,"about_ca_system_score_gemma":0.00028766034,"threshold_uncertainty_score":0.00918287},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99813473,0.00019325185,0.0009541299,0.000018630142,0.000024005953,0.000007671812,0.00003579893,0.000039980114,0.0005916973],"genre_scores_gemma":[0.99757403,0.00010415285,0.0017520561,0.000012087491,0.00001062591,0.000007664096,0.00007492768,0.00001622257,0.00044833578],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99949956,0.00012893029,0.000045682016,0.000092777365,0.00012965086,0.000103403945],"domain_scores_gemma":[0.99779594,0.001230044,0.00014695783,0.0001800778,0.000546644,0.0001003983],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0011029588,0.00039305814,0.0002918655,0.00032660575,0.0002383262,0.0005373355,0.00035311814,0.00039344243,0.0018564686],"category_scores_gemma":[0.0031476454,0.00020985908,0.00020453421,0.00022154223,0.0001984775,0.00058700616,0.00019241912,0.00027709416,0.00021543691],"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":[0.013060282,0.001655018,0.07312638,0.00047389342,0.00014497993,0.0006771532,0.0002849611,0.03296078,0.78175175,0.00077377213,0.0010239691,0.09406709],"study_design_scores_gemma":[0.00018495457,0.006801195,0.07104375,0.000027659953,0.0002459922,0.0004215498,0.000101838916,0.027320253,0.89106935,0.00012588111,0.0025867485,0.00007077552],"about_ca_topic_score_codex":0.0007574864,"about_ca_topic_score_gemma":0.0013096125,"teacher_disagreement_score":0.0018564686,"about_ca_system_score_codex":0.00033928044,"about_ca_system_score_gemma":0.00021709932,"threshold_uncertainty_score":0.006210506},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0030871942,0.000093955736,0.9962574,0.000011820071,0.000013033152,0.000011495115,0.000012452105,0.000105313986,0.0004073651],"genre_scores_gemma":[0.088878825,0.0002068874,0.9047436,0.00003842758,0.000032733868,0.00014149782,0.00012965883,0.000056738798,0.00577161],"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9996244,0.00009877841,0.000017074175,0.0000647586,0.00017199534,0.000023114339],"domain_scores_gemma":[0.9996604,0.0001300451,0.00003262551,0.000056356348,0.00010738164,0.00001320447],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00063995214,0.0004773467,0.00060028146,0.0009926396,0.00026259635,0.00073207135,0.0008481895,0.0006647719,0.0024608313],"category_scores_gemma":[0.0007600721,0.00029589335,0.00045383614,0.00054073805,0.0003778603,0.00096928736,0.0008761808,0.0005255152,0.0008085157],"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":[0.00017353283,0.0001196206,0.0010092099,0.00027467357,0.00016415959,0.00015291451,0.00020908673,0.14578965,0.10078177,0.09657219,0.0015265625,0.6532267],"study_design_scores_gemma":[0.000011575353,0.00007674477,0.000444238,0.000009815269,0.000013807455,0.00011766696,0.00002499072,0.97427285,0.009893868,0.011143295,0.003966485,0.000024685325],"about_ca_topic_score_codex":0.0008665114,"about_ca_topic_score_gemma":0.0012660736,"teacher_disagreement_score":0.0024608313,"about_ca_system_score_codex":0.00024241512,"about_ca_system_score_gemma":0.0005009555,"threshold_uncertainty_score":0.0082322955},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9264728,0.00011483872,0.072135456,0.000024138055,0.000009132836,0.000005991316,0.000022360207,0.00013160838,0.0010836883],"genre_scores_gemma":[0.9975515,0.00003052718,0.0019715177,0.0000023046891,0.0000012671591,0.000004030777,0.000014940745,0.000006265607,0.00041747815],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999223,0.000017783794,0.0000029242199,0.000020629206,0.000025294965,0.000011036755],"domain_scores_gemma":[0.999882,0.000060571565,0.000024277579,0.000008874896,0.000013869749,0.000010418898],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00014867735,0.00032520352,0.00019332078,0.0002469742,0.00019115953,0.00026333044,0.0002261058,0.0003308658,0.00044598788],"category_scores_gemma":[0.00033709948,0.00016615013,0.00030311613,0.000093503324,0.00037643145,0.0002634422,0.00019997878,0.00018960818,0.00008395135],"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":[0.00020269527,0.00006774734,0.0128107555,0.000080933074,0.000033122687,0.0003586323,0.0002206044,0.77281857,0.1980231,0.0015664767,0.00013958773,0.0136777],"study_design_scores_gemma":[0.0000021788546,0.000039648872,0.0036080629,0.0000024357141,0.0000039211977,0.000014102096,0.000014880315,0.99069995,0.0054453863,0.00011071792,0.00005376913,0.0000049442624],"about_ca_topic_score_codex":0.0022155768,"about_ca_topic_score_gemma":0.0013868746,"teacher_disagreement_score":0.0022155768,"about_ca_system_score_codex":0.00019294916,"about_ca_system_score_gemma":0.000138958,"threshold_uncertainty_score":0.0044053197},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98566425,0.00018858313,0.011972633,0.000017992403,0.000037711412,0.000036367983,0.00003624956,0.000066985885,0.0019791625],"genre_scores_gemma":[0.9944804,0.00018392885,0.0037110967,0.000024112343,0.000017848573,0.000015551139,0.00006918282,0.000013919838,0.001484002],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9996301,0.000054733267,0.000014064631,0.000055532502,0.00017989134,0.00006556933],"domain_scores_gemma":[0.9987729,0.00075938326,0.00012618808,0.000053404194,0.00019859824,0.000089436384],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00039704161,0.0005584568,0.00050418044,0.00044438566,0.00023243317,0.00031397215,0.00035990626,0.0003477484,0.0013503412],"category_scores_gemma":[0.0013081583,0.00020984707,0.00021952242,0.0003443346,0.00057108566,0.00023859197,0.00040991802,0.0003147949,0.00017113873],"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":[0.0010344072,0.000045252415,0.0017415766,0.00014399675,0.000011922668,0.00048353974,0.0001327875,0.0027806212,0.98270804,0.00025971918,0.000045925597,0.010612147],"study_design_scores_gemma":[0.00009575082,0.0039523155,0.050204653,0.00006604327,0.000113445116,0.001136958,0.00037164122,0.026090717,0.9161388,0.00042712028,0.0013355762,0.00006684154],"about_ca_topic_score_codex":0.0006056504,"about_ca_topic_score_gemma":0.0007015015,"teacher_disagreement_score":0.0013503412,"about_ca_system_score_codex":0.00027126813,"about_ca_system_score_gemma":0.00020707281,"threshold_uncertainty_score":0.0045173764},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.022299243,0.00053784694,0.95287853,0.00073182763,0.00059087045,0.00079728913,0.0002874243,0.0023393752,0.019537667],"genre_scores_gemma":[0.22045001,0.0008336274,0.73978996,0.00062781764,0.0004509116,0.0012461675,0.0010826188,0.000656587,0.03486235],"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9957146,0.00046821838,0.0001884441,0.0003417651,0.0030605183,0.00022641086],"domain_scores_gemma":[0.99436694,0.0004703843,0.0003631492,0.00043662934,0.00392763,0.00043523312],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.005613304,0.0006568297,0.00067089987,0.0016667362,0.000804238,0.001728435,0.0023623316,0.0012053783,0.0058107576],"category_scores_gemma":[0.0039047678,0.0006372717,0.00055287004,0.00053934136,0.0006867923,0.001865702,0.0014137668,0.0012642352,0.0030701212],"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":[0.0007815848,0.00050638244,0.009368304,0.00061642955,0.000056377074,0.0010387796,0.000840874,0.029032025,0.3703092,0.027611222,0.023656609,0.5361823],"study_design_scores_gemma":[0.0004908285,0.0057337815,0.017546503,0.00028296775,0.00015865244,0.0040340694,0.00044915616,0.17305106,0.2261179,0.005105518,0.566601,0.00042858472],"about_ca_topic_score_codex":0.0028439034,"about_ca_topic_score_gemma":0.004680252,"teacher_disagreement_score":0.0058107576,"about_ca_system_score_codex":0.0009264894,"about_ca_system_score_gemma":0.0026243224,"threshold_uncertainty_score":0.029686332},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.025050247,0.00062154053,0.934233,0.00085331354,0.00043277454,0.0000872529,0.0003238628,0.00032174416,0.038076352],"genre_scores_gemma":[0.7942755,0.0017571903,0.09496971,0.0004570844,0.00051873736,0.00029826997,0.0005495453,0.0004113324,0.10676256],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99980575,0.000046908586,0.000008690549,0.00003975033,0.00007453415,0.000024456793],"domain_scores_gemma":[0.9997634,0.00007380585,0.000032459728,0.000019988744,0.000085919986,0.000024439763],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024755366,0.0010852726,0.00070857967,0.00058421376,0.00074531836,0.0010093272,0.0017994299,0.0023956946,0.0035402807],"category_scores_gemma":[0.0012487884,0.00066403486,0.00075286365,0.00058503146,0.0013419776,0.0013620744,0.0012932707,0.0013809878,0.0013900269],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000015811707,0.000017631395,0.00015774106,0.000034755234,0.000009633836,0.00012135976,0.000059406844,0.9468813,0.002404577,0.044981208,0.0010103002,0.004306288],"study_design_scores_gemma":[0.000004046063,0.000005248874,0.00004920505,0.000002268493,0.0000031563195,0.000020089756,0.000007503722,0.9951514,0.00010817686,0.0037130378,0.0009282953,0.000007484233],"about_ca_topic_score_codex":0.02031713,"about_ca_topic_score_gemma":0.013317419,"teacher_disagreement_score":0.02031713,"about_ca_system_score_codex":0.0011110827,"about_ca_system_score_gemma":0.0010110235,"threshold_uncertainty_score":0.040397763},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.12878266,0.000650027,0.86725605,0.00009827277,0.00008676976,0.000036198762,0.00012477342,0.0006556944,0.0023095636],"genre_scores_gemma":[0.4677296,0.0013581086,0.52819663,0.000059681453,0.00005702975,0.00003940729,0.00049634074,0.00032022825,0.0017429539],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996257,0.00011599164,0.00002112391,0.000054944787,0.00014490717,0.00003741923],"domain_scores_gemma":[0.99898523,0.0003766876,0.00006857626,0.00018202233,0.0003221766,0.00006529348],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0009930899,0.0005515153,0.00042110757,0.0007174303,0.00017504685,0.0007286026,0.00040125012,0.00037448795,0.0011789701],"category_scores_gemma":[0.0024079117,0.00018560197,0.00036736412,0.0006781643,0.0003605452,0.0012771514,0.0006295618,0.0004515639,0.0002587632],"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":[0.0012663102,0.00019867858,0.008650314,0.0005857247,0.00014158878,0.00022378267,0.0003679747,0.11109244,0.082811534,0.013250198,0.0021518036,0.7792597],"study_design_scores_gemma":[0.000035424444,0.0001619354,0.0061401846,0.000032287102,0.000026918262,0.00023763653,0.0001034379,0.96792847,0.021983784,0.0016686447,0.0016398736,0.000041441366],"about_ca_topic_score_codex":0.0009833571,"about_ca_topic_score_gemma":0.0014843174,"teacher_disagreement_score":0.0011789701,"about_ca_system_score_codex":0.00015849032,"about_ca_system_score_gemma":0.0003817493,"threshold_uncertainty_score":0.0052520037},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.996214,0.000985072,0.0018511894,0.000025628648,0.00002288496,0.00005096724,0.00009926801,0.00003878807,0.0007122115],"genre_scores_gemma":[0.9899322,0.0011561757,0.0074852766,0.000054269152,0.000015754516,0.00006573134,0.0001340657,0.000070949936,0.0010855586],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.999044,0.0002706793,0.000107941036,0.0001551827,0.00027765406,0.00014465446],"domain_scores_gemma":[0.9961319,0.0026622096,0.00041181312,0.000181174,0.0004750029,0.00013788803],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0010773173,0.0006515699,0.0005857554,0.0003080225,0.00025124117,0.000517803,0.00030591886,0.00036634834,0.0012709044],"category_scores_gemma":[0.0033107293,0.00041033875,0.00035229215,0.00038849955,0.00035972736,0.0005709983,0.00030053811,0.0006270927,0.00018776754],"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":[0.0020164961,0.00012881921,0.0017468779,0.00018840721,0.00003260945,0.00007030997,0.00014096603,0.000598351,0.98782897,0.00005419787,0.000072516115,0.007121561],"study_design_scores_gemma":[0.000037194015,0.001354046,0.010343443,0.000009497204,0.000056331806,0.000053720207,0.00006158618,0.0013631162,0.9860216,0.000018530363,0.0006601737,0.000020862797],"about_ca_topic_score_codex":0.0009223067,"about_ca_topic_score_gemma":0.00131604,"teacher_disagreement_score":0.0012709044,"about_ca_system_score_codex":0.00024693957,"about_ca_system_score_gemma":0.00039477187,"threshold_uncertainty_score":0.005697489},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9710489,0.00012034681,0.02093205,0.00006557574,0.000019932768,0.00003559261,0.0001478512,0.00015637495,0.00747347],"genre_scores_gemma":[0.9970855,0.000032614615,0.0018938342,0.0000067058804,0.00000307734,0.0000101214455,0.000074284726,0.00001351938,0.0008803171],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999064,0.000025091593,0.0000033315905,0.000011533807,0.000036099274,0.000017462813],"domain_scores_gemma":[0.9996519,0.00022287735,0.000024079614,0.000015400417,0.00005890233,0.000026878333],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002230324,0.00038201647,0.0003156806,0.00039273564,0.00033161166,0.00040404618,0.000387367,0.0004814636,0.0015237551],"category_scores_gemma":[0.00069164764,0.000106935986,0.00035862037,0.00021865757,0.0005593278,0.00014728493,0.00028595843,0.00024303976,0.00015082894],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00016069598,0.000074135576,0.0040449835,0.000059353726,0.0000138403875,0.000347905,0.00007551174,0.963229,0.026285935,0.0013537805,0.00017249849,0.0041824733],"study_design_scores_gemma":[0.000013892484,0.000057506793,0.0018727484,0.0000032003552,0.000002784869,0.000022496695,0.00001924191,0.9958275,0.0018834303,0.0001488647,0.0001435703,0.000004803505],"about_ca_topic_score_codex":0.010925836,"about_ca_topic_score_gemma":0.004806152,"teacher_disagreement_score":0.010925836,"about_ca_system_score_codex":0.00044824363,"about_ca_system_score_gemma":0.00036192322,"threshold_uncertainty_score":0.021724463},"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":"review","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"review","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.46375698,0.18615168,0.15617765,0.06105243,0.0030302065,0.0001294913,0.005351895,0.0038270403,0.12052262],"genre_scores_gemma":[0.9370751,0.030312877,0.0217413,0.00071621273,0.00079697865,0.000023905723,0.0020779243,0.000085994434,0.0071699047],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9990121,0.00019877464,0.000079066485,0.00018733885,0.00043301834,0.00008968546],"domain_scores_gemma":[0.9966112,0.0008349019,0.0004420872,0.00016104,0.001705355,0.00024549535],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.003772545,0.00057406427,0.00038638522,0.0011902392,0.00031387908,0.0021132736,0.0012874888,0.0010624323,0.0026382655],"category_scores_gemma":[0.00463081,0.00020860782,0.00032617137,0.0010119895,0.00055414176,0.0020675815,0.0005330706,0.00069614773,0.0012471902],"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":[0.00069142174,0.000363223,0.16794023,0.0007193448,0.00013414933,0.00015849207,0.00016865169,0.07513157,0.0027080067,0.009170421,0.028269053,0.7145455],"study_design_scores_gemma":[0.00008924238,0.00065741007,0.13285434,0.0016081478,0.00025177575,0.0004110755,0.0017951548,0.74429184,0.007818953,0.022978235,0.087069415,0.00017436719],"about_ca_topic_score_codex":0.01437828,"about_ca_topic_score_gemma":0.01247873,"teacher_disagreement_score":0.01437828,"about_ca_system_score_codex":0.0011260996,"about_ca_system_score_gemma":0.0012860781,"threshold_uncertainty_score":0.028589189},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9902282,0.0001627792,0.008903408,0.000019724339,0.000017009183,0.000012237244,0.000008043816,0.000070918184,0.0005776758],"genre_scores_gemma":[0.99663216,0.00005347422,0.003127494,0.0000054730967,0.0000030650974,0.000004790124,0.000004710623,0.0000062980967,0.00016257138],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998265,0.000048062215,0.000010542212,0.00002993078,0.000048355447,0.000036613703],"domain_scores_gemma":[0.9992029,0.00043966892,0.00017204697,0.000055695957,0.00007888816,0.000050949373],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003657957,0.0002670094,0.00027364443,0.00016571912,0.00015442182,0.00024826464,0.0002311961,0.00027715336,0.00048921595],"category_scores_gemma":[0.000777888,0.00015506885,0.00016205292,0.000072011935,0.0004330996,0.00021500804,0.00032760992,0.00017657298,0.00009831929],"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":[0.00031280288,0.000041226496,0.0009202134,0.00011269897,0.00000584483,0.00022013135,0.0000922454,0.006737654,0.9825722,0.00017168437,0.000044426954,0.008768768],"study_design_scores_gemma":[0.000052501306,0.002116376,0.0050452836,0.0000220588,0.000036801164,0.00018796063,0.00010884801,0.059425842,0.93197185,0.00009346196,0.00091183756,0.000027227812],"about_ca_topic_score_codex":0.0002132392,"about_ca_topic_score_gemma":0.00021919908,"teacher_disagreement_score":0.00048921595,"about_ca_system_score_codex":0.000090995694,"about_ca_system_score_gemma":0.00015938097,"threshold_uncertainty_score":0.0019345284},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.998439,0.000016867385,0.00057601574,0.000010192189,0.000007353518,0.00000950203,0.00004491569,0.000031981057,0.00086411636],"genre_scores_gemma":[0.998543,0.000013630271,0.0005676164,0.0000086426035,0.000005010147,0.000005050618,0.00012691326,0.0000127761305,0.0007173089],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.9997023,0.000048975104,0.000012735872,0.00004843884,0.00012014251,0.00006742437],"domain_scores_gemma":[0.999509,0.00007998854,0.000045837278,0.000030552943,0.00019593071,0.00013875509],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00037391146,0.0002700818,0.00029349228,0.0009814831,0.0007647171,0.00041584944,0.00030935332,0.0005829408,0.001232918],"category_scores_gemma":[0.00065589853,0.00025277046,0.00016620258,0.0003671052,0.0003209362,0.00020832598,0.00040209386,0.00028804594,0.00024603336],"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":[0.0037866873,0.0017231817,0.26280472,0.0003037596,0.00014405955,0.014535423,0.0040320284,0.01565785,0.6319292,0.0009385087,0.0020297267,0.062114768],"study_design_scores_gemma":[0.00017349915,0.004887216,0.8590234,0.00013244186,0.00013877431,0.009360106,0.0034156146,0.053391356,0.063629895,0.00068270316,0.0049882415,0.00017679749],"about_ca_topic_score_codex":0.0029086636,"about_ca_topic_score_gemma":0.007956679,"teacher_disagreement_score":0.0029086636,"about_ca_system_score_codex":0.00017627943,"about_ca_system_score_gemma":0.00020052772,"threshold_uncertainty_score":0.0057834387},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.18580487,0.00013050919,0.8124534,0.00007045144,0.000020202086,0.00003322208,0.000045427,0.00018210807,0.0012598225],"genre_scores_gemma":[0.953016,0.00005451966,0.046450626,0.000012587231,0.000010505527,0.00003409824,0.000061370396,0.00003298922,0.00032738026],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9990404,0.00024518807,0.000049914936,0.00017782189,0.00042602548,0.00006060988],"domain_scores_gemma":[0.9964677,0.0024974858,0.00037640234,0.00021997227,0.00035652658,0.000081878265],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.002139903,0.0007538979,0.0003961726,0.00096065627,0.00037812386,0.00074383477,0.00091805885,0.0007023431,0.0003086934],"category_scores_gemma":[0.005846052,0.00030171315,0.00057803775,0.00030357885,0.00094289804,0.00096046727,0.00093618553,0.0007419594,0.000033016313],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000102867976,0.00005110135,0.0014828283,0.000060633447,0.000035374833,0.000068810565,0.00011802794,0.9429783,0.023889165,0.017007537,0.00010822583,0.014097195],"study_design_scores_gemma":[0.0000022113304,0.000012429396,0.00026311638,0.0000024882177,0.0000026697633,0.0000054224715,0.0000034984942,0.99617285,0.0027350609,0.0007465732,0.000046115012,0.0000075772423],"about_ca_topic_score_codex":0.0033885094,"about_ca_topic_score_gemma":0.0016920932,"teacher_disagreement_score":0.0033885094,"about_ca_system_score_codex":0.000767095,"about_ca_system_score_gemma":0.00068139733,"threshold_uncertainty_score":0.011317015},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9290631,0.00062871067,0.065720275,0.000076730525,0.000063752734,0.00006555165,0.00007312041,0.00021182379,0.004096947],"genre_scores_gemma":[0.98680264,0.00013886011,0.011086632,0.000024395184,0.000010638822,0.000027989465,0.000039947456,0.00001881988,0.0018500226],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9994567,0.00013644011,0.000020691617,0.00011223257,0.00020253427,0.0000714028],"domain_scores_gemma":[0.9991227,0.00039940517,0.00019925408,0.00008826412,0.000120970864,0.00006937001],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005981905,0.00032483265,0.00023835189,0.00022114106,0.00026397346,0.00034472666,0.00037349144,0.00048582474,0.0012091248],"category_scores_gemma":[0.0011635786,0.00032288345,0.0001828362,0.00016863282,0.0004942825,0.000653392,0.0006307097,0.000274794,0.0001700424],"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":[0.0007031709,0.0001485869,0.003247331,0.00023700479,0.000021931224,0.0005978608,0.00041824594,0.034743637,0.93542594,0.0054205763,0.00027561132,0.018760124],"study_design_scores_gemma":[0.00021074593,0.0034033773,0.02603127,0.00009227354,0.000048875936,0.0016415932,0.000636474,0.33526996,0.6187479,0.0052454737,0.008485544,0.00018648303],"about_ca_topic_score_codex":0.00041806872,"about_ca_topic_score_gemma":0.0004207631,"teacher_disagreement_score":0.0012091248,"about_ca_system_score_codex":0.00016944291,"about_ca_system_score_gemma":0.0001978221,"threshold_uncertainty_score":0.0040448904},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.907593,0.0005524272,0.08736312,0.00015392072,0.00008758002,0.000053746127,0.000047065274,0.00046497592,0.0036842586],"genre_scores_gemma":[0.9883938,0.00014132157,0.010502469,0.000019564492,0.00001495237,0.000023832827,0.000012904311,0.000022561799,0.00086857984],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99991214,0.000016567394,0.00000397597,0.0000197651,0.000029220177,0.000018416284],"domain_scores_gemma":[0.99968815,0.00013869951,0.00008767713,0.000020629255,0.000030400523,0.000034418525],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020227731,0.0002611918,0.00028103447,0.00010979372,0.00013148726,0.00024942198,0.00041894743,0.0002295008,0.0010471407],"category_scores_gemma":[0.00032463728,0.00016968996,0.00010623014,0.00006082163,0.00046333837,0.00023427024,0.00033145555,0.00028417257,0.00028742515],"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":[0.00011449985,0.000019043257,0.00011056548,0.00005272745,0.000003000275,0.00003768257,0.000046369496,0.004303959,0.9901052,0.00075238897,0.00009092033,0.004363666],"study_design_scores_gemma":[0.00016557536,0.0014674928,0.0018901521,0.000032956723,0.000024901867,0.00008308685,0.00006976872,0.26774395,0.72316045,0.00083906506,0.0044817254,0.000040743107],"about_ca_topic_score_codex":0.00021769133,"about_ca_topic_score_gemma":0.00033405112,"teacher_disagreement_score":0.0010471407,"about_ca_system_score_codex":0.00017949527,"about_ca_system_score_gemma":0.00015861852,"threshold_uncertainty_score":0.0035030246},"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":"methods","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.46636593,0.00029141898,0.5264042,0.00013119634,0.00006820118,0.00009114367,0.0002580406,0.0008525437,0.0055372985],"genre_scores_gemma":[0.9820458,0.00011830874,0.014749915,0.000024518453,0.000016103273,0.000069643844,0.00019791986,0.000047660214,0.002730001],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997079,0.00004763409,0.000019810066,0.000060002,0.00013370169,0.000031022646],"domain_scores_gemma":[0.9995963,0.00015937757,0.000065335604,0.000029537692,0.00013246678,0.00001696032],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00065213005,0.00096269394,0.0006904073,0.00035274398,0.00030228295,0.0007335498,0.0010505369,0.00073096884,0.00067216833],"category_scores_gemma":[0.0009326627,0.00030462636,0.0007895153,0.00017411697,0.00026400012,0.0005792491,0.00041510756,0.0005546892,0.00032713552],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000058936497,0.000025649835,0.0013249273,0.000015911195,0.000010581678,0.00004473914,0.000019515113,0.9883591,0.0059780926,0.00046019824,0.00007799185,0.0036244527],"study_design_scores_gemma":[0.000003583742,0.000017029024,0.0002235463,0.000001194064,0.0000034365817,0.0000047492485,0.000001349804,0.99887675,0.0007763109,0.000056736786,0.000033007436,0.0000024312305],"about_ca_topic_score_codex":0.009629873,"about_ca_topic_score_gemma":0.006133666,"teacher_disagreement_score":0.009629873,"about_ca_system_score_codex":0.000539877,"about_ca_system_score_gemma":0.00067984,"threshold_uncertainty_score":0.019147635},"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":"commentary","genre_gemma":"commentary","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"commentary","genre_consensus":"commentary","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.01958017,0.0063609197,0.04230434,0.74956393,0.15731193,0.00022698958,0.0017947067,0.002931714,0.019925334],"genre_scores_gemma":[0.23703974,0.0065028137,0.02119196,0.5925998,0.081172794,0.0004991815,0.00086001545,0.0019956143,0.058138102],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.99818784,0.000446816,0.00012425963,0.0002557108,0.00088392914,0.00010152052],"domain_scores_gemma":[0.9931751,0.0038504929,0.00045386833,0.00041441488,0.0017985464,0.0003076931],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0025490944,0.0006070857,0.00076846906,0.0004198646,0.0015510522,0.0013043458,0.0028827568,0.00399994,0.00991653],"category_scores_gemma":[0.016394941,0.0002826182,0.0007150403,0.0006292783,0.0021657734,0.0017686001,0.0012371241,0.0042105545,0.0038332262],"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":[0.00043005557,0.00006597399,0.0020650877,0.0004866828,0.00008108566,0.0015181849,0.00059393956,0.010600301,0.0033618545,0.016647156,0.94607824,0.018071374],"study_design_scores_gemma":[0.0002370575,0.00027928787,0.006963396,0.0006081878,0.0001289512,0.0008856591,0.00069546973,0.06374485,0.013353478,0.045021746,0.8678,0.0002818235],"about_ca_topic_score_codex":0.009002718,"about_ca_topic_score_gemma":0.006844747,"teacher_disagreement_score":0.00991653,"about_ca_system_score_codex":0.0014218756,"about_ca_system_score_gemma":0.00082176086,"threshold_uncertainty_score":0.033174157},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.89985687,0.00013146263,0.09030382,0.00014262297,0.000090352674,0.00013730601,0.0008604547,0.0005244877,0.007952682],"genre_scores_gemma":[0.9807087,0.00009258952,0.016779011,0.00001567152,0.00000924506,0.00009864849,0.00027264102,0.000033179487,0.0019902245],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998165,0.00002732225,0.0000124811295,0.000027963615,0.00006912928,0.00004663637],"domain_scores_gemma":[0.9994186,0.0003254974,0.000040673654,0.00004240959,0.00012680402,0.0000461001],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003666037,0.0004513715,0.00060527155,0.00048001183,0.0004158074,0.00045914002,0.0005143052,0.00072635704,0.0015415304],"category_scores_gemma":[0.0011917317,0.0002287094,0.0003981996,0.00044940197,0.00055487803,0.00024786068,0.00043163175,0.0005371074,0.00018603499],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00008782674,0.000046021803,0.0015625792,0.000035679925,0.000007859524,0.00017725152,0.000074424504,0.9748906,0.017124632,0.0019786211,0.0002271557,0.0037871944],"study_design_scores_gemma":[0.000021714568,0.00003852684,0.0008631361,0.0000043756067,0.0000030262552,0.000025057321,0.000014757549,0.99427223,0.0041379924,0.00023851551,0.00037116717,0.000009436692],"about_ca_topic_score_codex":0.010036702,"about_ca_topic_score_gemma":0.0036309808,"teacher_disagreement_score":0.010036702,"about_ca_system_score_codex":0.00056748034,"about_ca_system_score_gemma":0.0009530793,"threshold_uncertainty_score":0.019956589},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.14825544,0.042040005,0.7955882,0.0005535103,0.000868565,0.0007800419,0.00026400373,0.0020387592,0.009611444],"genre_scores_gemma":[0.3580855,0.021757869,0.6034926,0.0003766591,0.00061225967,0.0009388237,0.00051155826,0.00040013215,0.013824474],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99843115,0.00038404044,0.000098096265,0.00029192943,0.00071438967,0.000080464786],"domain_scores_gemma":[0.99833447,0.00063153193,0.00022946572,0.00018882718,0.00054383185,0.0000718655],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0014483484,0.0011464003,0.0010971543,0.0018001985,0.0004674599,0.0007999967,0.0008777162,0.0008430001,0.003242494],"category_scores_gemma":[0.0021606106,0.00083625247,0.0006846273,0.00079868425,0.00057179865,0.000956745,0.00053071283,0.0009076076,0.0014778438],"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":[0.0003943524,0.00021958922,0.0012167025,0.0012687728,0.000032792403,0.00012241062,0.00018243758,0.0014119528,0.79173976,0.0008100125,0.00069208693,0.20190915],"study_design_scores_gemma":[0.000113018345,0.0021023275,0.008544251,0.0002709515,0.00018871983,0.0007966419,0.00020582258,0.013763905,0.94265187,0.0007905871,0.030426089,0.00014579037],"about_ca_topic_score_codex":0.00075437187,"about_ca_topic_score_gemma":0.0012314544,"teacher_disagreement_score":0.003242494,"about_ca_system_score_codex":0.00036250902,"about_ca_system_score_gemma":0.00035903187,"threshold_uncertainty_score":0.010847211},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.95936865,0.0006983332,0.036591347,0.00013161321,0.00002121625,0.000059832146,0.0013232386,0.0002492997,0.001556361],"genre_scores_gemma":[0.99215674,0.00033095674,0.00459685,0.000012651407,0.000029286502,0.000028120323,0.002182988,0.00005054958,0.0006118395],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999858,0.000023241084,0.000012555093,0.00003451359,0.00004367026,0.000028105975],"domain_scores_gemma":[0.99910647,0.0004900423,0.00015174766,0.00007033882,0.00013011244,0.00005135851],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00054747507,0.00031246862,0.00048502703,0.0011842292,0.0002652389,0.00090102386,0.00024167156,0.00044027227,0.00085239444],"category_scores_gemma":[0.0018599187,0.0002495683,0.00036849038,0.00085420196,0.0007104832,0.0006442914,0.00027698773,0.00036866957,0.00028508028],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00047175668,0.0002886494,0.21628341,0.00024521854,0.00011224781,0.00043558478,0.00031917228,0.657247,0.054493982,0.008579587,0.0030460686,0.058477283],"study_design_scores_gemma":[0.000013290874,0.00011506622,0.14750355,0.000024349658,0.000009933807,0.00015907481,0.00008439469,0.84290946,0.005754606,0.0021275673,0.0012438048,0.000054842614],"about_ca_topic_score_codex":0.009828867,"about_ca_topic_score_gemma":0.0039718794,"teacher_disagreement_score":0.009828867,"about_ca_system_score_codex":0.0003572624,"about_ca_system_score_gemma":0.0004936718,"threshold_uncertainty_score":0.01954329},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.32054862,0.028164431,0.6253413,0.00027433995,0.00043137718,0.00011215466,0.00011354435,0.00062526105,0.024389071],"genre_scores_gemma":[0.9560391,0.0120584555,0.024535976,0.00004576175,0.00014208129,0.00005816159,0.0000862282,0.00005437971,0.006979807],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99979645,0.000036998248,0.00001016326,0.000042039934,0.00009583674,0.000018631321],"domain_scores_gemma":[0.9996637,0.00018225455,0.000070925365,0.000020421383,0.00004949321,0.000013221173],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00019422092,0.0003727466,0.00049745856,0.00037205996,0.00024673034,0.00057935214,0.00036881177,0.00044262965,0.0015792158],"category_scores_gemma":[0.0006579787,0.00022383001,0.00034047366,0.0004165193,0.0005504146,0.0008223876,0.000446486,0.00042971878,0.00030630876],"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":[0.000246484,0.000095992364,0.0042173956,0.0024081063,0.00009872595,0.0019317097,0.0006569326,0.2272237,0.48419964,0.06715521,0.0014113969,0.2103547],"study_design_scores_gemma":[0.000084236526,0.0011328795,0.01779014,0.00027540736,0.00016657785,0.0061889323,0.0005891989,0.6511593,0.17988987,0.068635635,0.07389864,0.00018910646],"about_ca_topic_score_codex":0.00030722478,"about_ca_topic_score_gemma":0.00020087791,"teacher_disagreement_score":0.0015792158,"about_ca_system_score_codex":0.00023528293,"about_ca_system_score_gemma":0.00015715159,"threshold_uncertainty_score":0.0052830577},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9725602,0.00060673745,0.0067350212,0.000324604,0.00012104744,0.000033822675,0.000068738824,0.0002298784,0.01931997],"genre_scores_gemma":[0.99674904,0.00011271316,0.0006781862,0.00003647192,0.000043931017,0.000006397759,0.000039838196,0.000039477465,0.002293795],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99981815,0.000053503027,0.000006331331,0.00003420447,0.000054385913,0.000033453598],"domain_scores_gemma":[0.99842036,0.00077338127,0.0001599711,0.00007013176,0.00028498005,0.0002912311],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00034113973,0.00049053115,0.0004921244,0.0008923405,0.0007086425,0.0009300108,0.00042647426,0.00059676345,0.00257756],"category_scores_gemma":[0.002603402,0.00034858647,0.0002284335,0.00038513285,0.0011727917,0.0013516408,0.0006266189,0.0007666591,0.00032115137],"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":[0.006597721,0.0016092764,0.011490767,0.0003661954,0.00009943008,0.0029771957,0.0007168968,0.5209881,0.3823983,0.043540042,0.0031572622,0.02605888],"study_design_scores_gemma":[0.0005238303,0.00092059583,0.043135878,0.000060155257,0.00007752596,0.0006325129,0.0003029871,0.9050991,0.036319412,0.010667591,0.0020072637,0.00025312157],"about_ca_topic_score_codex":0.0023467063,"about_ca_topic_score_gemma":0.0011307773,"teacher_disagreement_score":0.00257756,"about_ca_system_score_codex":0.00054637203,"about_ca_system_score_gemma":0.00036045446,"threshold_uncertainty_score":0.008622825},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99906987,0.000057957805,0.00032103498,0.000012431506,0.000009801042,0.0000022118177,0.000016466021,0.000019723004,0.0004905701],"genre_scores_gemma":[0.99971384,0.000030171826,0.00007047508,0.0000042685797,0.0000041434882,0.0000010511445,0.000015050427,0.000005969332,0.00015496749],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99987614,0.000021624039,0.000007569686,0.000017119242,0.000026195674,0.00005127573],"domain_scores_gemma":[0.9986118,0.0008773819,0.00012418904,0.000060290615,0.000113612,0.00021273422],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00028015222,0.00029181264,0.00037969914,0.00034315538,0.00037191992,0.0006001996,0.00029535868,0.000383665,0.0020525],"category_scores_gemma":[0.0018011986,0.00020058795,0.00030457292,0.00018120234,0.0005445425,0.00041346587,0.00054308184,0.000565443,0.00017536661],"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":[0.0070049497,0.00017378361,0.008254934,0.00011697104,0.00006606022,0.001467998,0.00023706039,0.041480634,0.92802334,0.0006403332,0.00019202476,0.01234194],"study_design_scores_gemma":[0.00012231225,0.002690654,0.06114181,0.000022286105,0.00012560077,0.0004400968,0.00044404238,0.11236653,0.82174236,0.0002592256,0.0005634939,0.00008165574],"about_ca_topic_score_codex":0.0010145275,"about_ca_topic_score_gemma":0.0006183859,"teacher_disagreement_score":0.0020525,"about_ca_system_score_codex":0.00024074844,"about_ca_system_score_gemma":0.00019289069,"threshold_uncertainty_score":0.0068662763},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9964064,0.000092533475,0.0027805788,0.000016821441,0.000013049106,0.000019044459,0.00007478226,0.000033072898,0.0005636894],"genre_scores_gemma":[0.99297994,0.00017479951,0.0059742136,0.000016905811,0.000015825388,0.00003638005,0.00013008878,0.000010151494,0.00066156994],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99973017,0.00002773001,0.000012913965,0.000078157966,0.00009870411,0.000052338884],"domain_scores_gemma":[0.9993956,0.00018433025,0.00014415057,0.00006446874,0.0001258873,0.000085451524],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004539395,0.00033169484,0.00036393633,0.0002683628,0.0004747782,0.0002908968,0.0002851768,0.00044319857,0.0011016567],"category_scores_gemma":[0.0006863722,0.00014871592,0.0001491698,0.00026635596,0.0006869982,0.00035133894,0.00040213027,0.00045645447,0.00013160768],"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":[0.00016705632,0.000144593,0.0012136187,0.000048810904,0.0000032113635,0.00011049058,0.00011309396,0.0006393467,0.9950212,0.00018017022,0.000037723115,0.0023206735],"study_design_scores_gemma":[0.00008073026,0.0047106817,0.052090555,0.000035588673,0.000034131812,0.00054931245,0.00037918173,0.019209746,0.92024344,0.00029683078,0.0023100686,0.000059703914],"about_ca_topic_score_codex":0.00037824558,"about_ca_topic_score_gemma":0.000341075,"teacher_disagreement_score":0.0011016567,"about_ca_system_score_codex":0.00015335812,"about_ca_system_score_gemma":0.00025293394,"threshold_uncertainty_score":0.0036853552},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.111063324,0.00016289824,0.8807192,0.000052536696,0.000019473482,0.0002115001,0.00026144538,0.00059596216,0.0069136405],"genre_scores_gemma":[0.5280684,0.0002230318,0.4672561,0.00004624781,0.000015308335,0.0007045182,0.0002908697,0.00024989696,0.0031456382],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998048,0.000041577696,0.0000117847285,0.000017459308,0.000109582026,0.000014852466],"domain_scores_gemma":[0.9992162,0.00044766252,0.00006776416,0.00008005789,0.00016834978,0.000019968584],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00089871656,0.0005600194,0.0006233479,0.0005734515,0.0003919629,0.0005703907,0.0010520733,0.00066592405,0.0025233799],"category_scores_gemma":[0.001593727,0.0004582913,0.00038146824,0.0003256863,0.000422407,0.00060090853,0.00047732575,0.000777419,0.0004894485],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000696686,0.000115808274,0.0008650023,0.00039178447,0.0000197989,0.00014880775,0.00018221285,0.8867974,0.04219705,0.017836813,0.0005219204,0.050853714],"study_design_scores_gemma":[0.000015529777,0.000029826455,0.000127408,0.00000764628,0.0000023448445,0.000018367118,0.000018080087,0.9946896,0.0033575012,0.0012475956,0.0004800934,0.000005946048],"about_ca_topic_score_codex":0.0014181304,"about_ca_topic_score_gemma":0.0015052711,"teacher_disagreement_score":0.0025233799,"about_ca_system_score_codex":0.00042344048,"about_ca_system_score_gemma":0.0013711427,"threshold_uncertainty_score":0.008441567},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.96937895,0.00014962816,0.026653808,0.000019939484,0.000020054804,0.00002556301,0.00004318428,0.00011354985,0.0035953096],"genre_scores_gemma":[0.9982864,0.00004716915,0.0009871707,0.0000026897155,0.000005704254,0.0000046246164,0.000036186677,0.000009123347,0.0006209902],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997663,0.000049723734,0.0000055042487,0.000020983993,0.00013014759,0.000027383847],"domain_scores_gemma":[0.99939084,0.0003208415,0.000026365224,0.000019924397,0.00020569742,0.000036260346],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002326704,0.00028245413,0.00020254093,0.00048353925,0.00025414937,0.00018237981,0.000159913,0.00015867842,0.0010732762],"category_scores_gemma":[0.00091006345,0.00009904858,0.00015513673,0.00022176796,0.0003624233,0.00020727981,0.00015783955,0.0002218037,0.00017988197],"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":[0.0015712585,0.00035385782,0.026918918,0.00016858036,0.00004268656,0.0016362088,0.0006285843,0.08045695,0.83748096,0.0032402899,0.00055319926,0.046948455],"study_design_scores_gemma":[0.00012861723,0.0023839336,0.0737638,0.00003259918,0.000039790753,0.001767559,0.00036321036,0.6123421,0.3044372,0.0013227501,0.0033632738,0.00005521502],"about_ca_topic_score_codex":0.0022327937,"about_ca_topic_score_gemma":0.0011539694,"teacher_disagreement_score":0.0022327937,"about_ca_system_score_codex":0.00017835105,"about_ca_system_score_gemma":0.00012140799,"threshold_uncertainty_score":0.0044395924},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9912788,0.00010908777,0.0071557784,0.000022288064,0.000006538428,0.00000784672,0.000018816716,0.000050834795,0.0013501447],"genre_scores_gemma":[0.9975979,0.00003602648,0.0019952343,0.000008270189,0.0000037285731,0.0000075771404,0.000011948331,0.00000714619,0.0003322254],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99987435,0.000026932556,0.000004040271,0.00002829078,0.000039578783,0.000026825255],"domain_scores_gemma":[0.9996611,0.00013179048,0.00009330785,0.00002836849,0.000057045283,0.000028357941],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002264469,0.00024243732,0.00017840887,0.00019384778,0.00015341955,0.00015673542,0.00019240886,0.00018732689,0.0011260418],"category_scores_gemma":[0.0004506918,0.00019203551,0.000101153084,0.00008949464,0.0003242633,0.00021037959,0.0003661521,0.00020227654,0.00014196163],"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":[0.000091118345,0.000006678441,0.0006728928,0.000033883043,0.0000020309305,0.000056180677,0.00007007312,0.00071660464,0.9951349,0.00029438254,0.000031295836,0.002889903],"study_design_scores_gemma":[0.00006902674,0.00056043814,0.018106487,0.000016739266,0.000012571255,0.00027567518,0.00008525111,0.03598379,0.9428416,0.0004374756,0.0015879314,0.000023000015],"about_ca_topic_score_codex":0.00016998015,"about_ca_topic_score_gemma":0.00015992734,"teacher_disagreement_score":0.0011260418,"about_ca_system_score_codex":0.00015598473,"about_ca_system_score_gemma":0.00008025803,"threshold_uncertainty_score":0.0037670135},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99308914,0.000080868405,0.005941652,0.0000211624,0.0000064317032,0.000010494007,0.000046814203,0.0000875631,0.00071599067],"genre_scores_gemma":[0.9985782,0.000032068107,0.0010554784,0.0000075649305,0.0000023881807,0.00000661393,0.000032217664,0.000014628292,0.00027099054],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997949,0.000031481995,0.000013246283,0.000038208444,0.00007252666,0.000049588485],"domain_scores_gemma":[0.9983701,0.0010243938,0.0001472616,0.00006992821,0.0002898557,0.00009855057],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025119112,0.00039997132,0.000417951,0.00050930015,0.00034290977,0.0002861559,0.00018364497,0.00033750822,0.001028742],"category_scores_gemma":[0.0016049715,0.00014814101,0.00019978016,0.00020461399,0.0004139837,0.00036191527,0.00031666688,0.0003002715,0.00021432115],"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":[0.0015075266,0.00015278811,0.010303165,0.00021409176,0.000016301998,0.00080081547,0.00038135203,0.018769752,0.9384554,0.0002561698,0.00019756454,0.028945062],"study_design_scores_gemma":[0.00006806112,0.0016848944,0.10475314,0.000056745193,0.000056624212,0.0010362589,0.0005262477,0.051252674,0.83939517,0.00030604776,0.00077640865,0.00008767889],"about_ca_topic_score_codex":0.0014458308,"about_ca_topic_score_gemma":0.0021092282,"teacher_disagreement_score":0.0014458308,"about_ca_system_score_codex":0.00021655935,"about_ca_system_score_gemma":0.00017556452,"threshold_uncertainty_score":0.0034415126},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99254626,0.00011777169,0.006411419,0.000026685777,0.000008810389,0.000016613752,0.00004543444,0.00006102862,0.0007660134],"genre_scores_gemma":[0.99595547,0.000040808016,0.0035687792,0.0000080239815,0.0000074424734,0.000009957305,0.00006160281,0.0000068221116,0.00034096473],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998747,0.00001085442,0.000009246758,0.000033717664,0.00004160349,0.000029857158],"domain_scores_gemma":[0.99942374,0.00013360889,0.0001935171,0.000035711684,0.00013196845,0.000081526865],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021157408,0.00032757243,0.00025344812,0.0008946711,0.0005628992,0.000540095,0.00016990335,0.00042259027,0.00047728914],"category_scores_gemma":[0.00049511576,0.00017800786,0.00020409258,0.0005471814,0.0005625123,0.00032129284,0.00024390746,0.00023706861,0.00007716347],"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":[0.001400245,0.00024784904,0.031900294,0.00011967973,0.000024625291,0.0019491548,0.00039123095,0.045378778,0.89706117,0.0034448637,0.0005216027,0.017560655],"study_design_scores_gemma":[0.00020646438,0.0009487413,0.09093522,0.000026405094,0.000046725898,0.0011713643,0.00034370538,0.66075766,0.24243289,0.0014048297,0.0016134792,0.0001124574],"about_ca_topic_score_codex":0.0020310325,"about_ca_topic_score_gemma":0.0010293061,"teacher_disagreement_score":0.0020310325,"about_ca_system_score_codex":0.00038047167,"about_ca_system_score_gemma":0.0004428213,"threshold_uncertainty_score":0.0040383935},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.303441,0.002813947,0.51771593,0.0028117632,0.0012309848,0.00007843651,0.00035928102,0.00072013814,0.17082858],"genre_scores_gemma":[0.94296485,0.00059146556,0.015859665,0.00022098269,0.0003663667,0.000030264253,0.000112364294,0.00008727919,0.039766815],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998933,0.000023155222,0.0000022818842,0.000032475586,0.000033832643,0.000014920949],"domain_scores_gemma":[0.9998727,0.000047462992,0.000013985361,0.00001461926,0.000023689134,0.000027608456],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018489877,0.00028556449,0.00033477228,0.00025790904,0.00026316955,0.0005788371,0.0006145247,0.00074999087,0.005158209],"category_scores_gemma":[0.00087140425,0.00018129202,0.0002551981,0.00023080186,0.0006647596,0.0005661845,0.000685123,0.0006020565,0.0006761405],"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":[0.0003178826,0.000042312415,0.000626931,0.00012618862,0.00004231649,0.0003202247,0.000116471005,0.059479874,0.07277096,0.817272,0.0045736805,0.044311233],"study_design_scores_gemma":[0.00019484117,0.00017835453,0.0027554827,0.000029908084,0.000052154304,0.00073635933,0.00009052682,0.64795774,0.012388185,0.31558177,0.019907309,0.00012739775],"about_ca_topic_score_codex":0.00025565323,"about_ca_topic_score_gemma":0.00014564881,"teacher_disagreement_score":0.005158209,"about_ca_system_score_codex":0.00025863494,"about_ca_system_score_gemma":0.00029939902,"threshold_uncertainty_score":0.017255962},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9964804,0.00068451336,0.0014066085,0.00006171387,0.00004493292,0.000015024756,0.00015112857,0.000058551566,0.0010973174],"genre_scores_gemma":[0.99739766,0.00020580861,0.0009749681,0.00003157628,0.0000343319,0.000012369401,0.000111574605,0.00009977703,0.0011319073],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99929833,0.00018871392,0.00006453196,0.0001408633,0.00012314114,0.00018435888],"domain_scores_gemma":[0.99043244,0.0073921694,0.00050456,0.00069090223,0.0005288767,0.00045118717],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0008189229,0.00040407834,0.00048857986,0.00027250696,0.00055719324,0.0009282075,0.00050597044,0.00050067983,0.0027381359],"category_scores_gemma":[0.0042612385,0.0005801581,0.00022247639,0.00026460266,0.00064404984,0.0007772256,0.00045917238,0.00056461606,0.00032684996],"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":[0.00444956,0.00019454779,0.0019238926,0.000056813125,0.00001138256,0.00011814906,0.00014448837,0.0006598576,0.98731005,0.00015283676,0.00013643222,0.0048419596],"study_design_scores_gemma":[0.000051303785,0.0011569163,0.0078115915,0.000006838443,0.00002061456,0.000072565665,0.000052879823,0.002120091,0.98802894,0.000053585056,0.0006036655,0.000020854752],"about_ca_topic_score_codex":0.0007911247,"about_ca_topic_score_gemma":0.00093430316,"teacher_disagreement_score":0.0027381359,"about_ca_system_score_codex":0.00034997505,"about_ca_system_score_gemma":0.00046360257,"threshold_uncertainty_score":0.009160042},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.030446561,0.00009580829,0.9654795,0.00007901761,0.00003093955,0.000037485515,0.000039713148,0.0004101849,0.0033807983],"genre_scores_gemma":[0.40957516,0.00067498995,0.58337164,0.000042550484,0.00003876557,0.00009315611,0.00020678785,0.00011703141,0.00587989],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998753,0.000019253026,0.000005362304,0.000007756287,0.00008669544,0.000005634565],"domain_scores_gemma":[0.9997105,0.00016507984,0.000022783723,0.00002982101,0.000060921542,0.000010880743],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003294657,0.000434829,0.00026629935,0.0002790837,0.00014830045,0.0005809778,0.0003485466,0.0003543882,0.002530974],"category_scores_gemma":[0.00077128777,0.00023077345,0.00039596716,0.00026679412,0.00055110856,0.00054680783,0.000547384,0.0005630195,0.0005477186],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0003289011,0.00011595877,0.0013027602,0.00050184585,0.000036172136,0.00070064364,0.00045034837,0.39493197,0.3348371,0.060551357,0.0013429688,0.20489997],"study_design_scores_gemma":[0.000022743883,0.00008080451,0.0002876672,0.000017793529,0.000006453608,0.00028313333,0.00004485647,0.9455749,0.049309757,0.0029348994,0.0014164594,0.000020634969],"about_ca_topic_score_codex":0.0008474188,"about_ca_topic_score_gemma":0.0006571681,"teacher_disagreement_score":0.002530974,"about_ca_system_score_codex":0.00021912657,"about_ca_system_score_gemma":0.00058255624,"threshold_uncertainty_score":0.008466899},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99853146,0.00016637355,0.0006880564,0.000009254887,0.000009904503,0.0000115315,0.000039513114,0.000031860145,0.0005121425],"genre_scores_gemma":[0.99876416,0.00016132557,0.0005916135,0.000011236491,0.0000020771863,0.000007729498,0.00011767305,0.000012483507,0.000331767],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99977845,0.00003241258,0.000018607509,0.000040325063,0.00006276832,0.00006744958],"domain_scores_gemma":[0.99962294,0.00014333718,0.00005969316,0.00002543784,0.00008597783,0.00006250553],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00027531377,0.00053822075,0.0002981997,0.00032410136,0.0002034807,0.0005644366,0.00032388174,0.0003433689,0.0010129107],"category_scores_gemma":[0.00083032396,0.00024645316,0.00016831378,0.00021932178,0.00022601483,0.00037617196,0.00035845354,0.0003141569,0.00027217044],"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":[0.0021642575,0.0002724801,0.016361207,0.00026997135,0.00006447365,0.0008088833,0.00014871589,0.016130686,0.9451499,0.00011606651,0.00018811645,0.018325265],"study_design_scores_gemma":[0.0000858689,0.010451765,0.065650314,0.000049083603,0.0001674185,0.00059678033,0.00039162373,0.010328318,0.91048884,0.00008337586,0.0016147287,0.000091993235],"about_ca_topic_score_codex":0.0005582892,"about_ca_topic_score_gemma":0.0006314339,"teacher_disagreement_score":0.0010129107,"about_ca_system_score_codex":0.00015368177,"about_ca_system_score_gemma":0.00016522354,"threshold_uncertainty_score":0.0033885837},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.40238547,0.0016251494,0.57464004,0.00067093567,0.00014528597,0.00006820498,0.00013185489,0.0005007395,0.019832304],"genre_scores_gemma":[0.9767322,0.0007038677,0.018393962,0.000033867036,0.00008249732,0.0000304294,0.00011319996,0.000066574314,0.0038433191],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997707,0.000035033114,0.0000074168033,0.000045971174,0.000118014614,0.000022927166],"domain_scores_gemma":[0.9989507,0.00039928878,0.00011114115,0.00005839276,0.0004382796,0.000042282983],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00036060516,0.00030187517,0.0002588604,0.00066221284,0.00022130748,0.0005577259,0.00045564436,0.00051189645,0.0019793608],"category_scores_gemma":[0.002064502,0.00022295013,0.00028603317,0.000541026,0.0004349194,0.0012695955,0.0003047536,0.00046816003,0.00035001038],"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":[0.00046527485,0.00009145664,0.013657614,0.00058551534,0.00006901034,0.0013046815,0.0014971249,0.07283539,0.63609767,0.11838677,0.0022837857,0.15272573],"study_design_scores_gemma":[0.00006574628,0.00030681738,0.017044062,0.00005675819,0.000056902514,0.0024577542,0.0003945766,0.75916106,0.18550181,0.026214566,0.008609634,0.00013032819],"about_ca_topic_score_codex":0.00044832478,"about_ca_topic_score_gemma":0.00017471868,"teacher_disagreement_score":0.0019793608,"about_ca_system_score_codex":0.0002969469,"about_ca_system_score_gemma":0.00022817553,"threshold_uncertainty_score":0.006621599},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6813515,0.0002586011,0.31270278,0.00002798752,0.00001709799,0.000036881782,0.00001875928,0.00057444716,0.0050119343],"genre_scores_gemma":[0.9971246,0.000030481013,0.002520594,0.0000024111766,0.000002971868,0.0000052824694,0.0000051570414,0.000009930774,0.0002985045],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998747,0.000033297743,0.0000039912297,0.000024039362,0.000041450265,0.00002255676],"domain_scores_gemma":[0.9994759,0.00030007685,0.000089966066,0.000038964692,0.00006966613,0.00002539711],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023599043,0.00043740674,0.00029474124,0.00021786161,0.00025956356,0.00039596437,0.00050890277,0.00016571296,0.0010610825],"category_scores_gemma":[0.00060978567,0.000111102934,0.00022784728,0.00008985825,0.0003497212,0.00029299603,0.00038595006,0.00018435076,0.00014924807],"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":[0.0006040088,0.00021645128,0.00502537,0.00026676524,0.00004701426,0.00023601948,0.00021612538,0.7211031,0.1876601,0.001894748,0.00020075694,0.082529545],"study_design_scores_gemma":[0.00006520397,0.00066240283,0.0041755736,0.000019143896,0.00008270845,0.000111147776,0.00007097959,0.9118405,0.08125668,0.0006897121,0.0009970091,0.000028991757],"about_ca_topic_score_codex":0.0013094161,"about_ca_topic_score_gemma":0.00199508,"teacher_disagreement_score":0.0013094161,"about_ca_system_score_codex":0.00019709197,"about_ca_system_score_gemma":0.00018047642,"threshold_uncertainty_score":0.003549695},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9987325,0.00010123386,0.0007948113,0.0000072982352,0.000009046372,0.0000021429103,0.000017511915,0.000051437746,0.00028392606],"genre_scores_gemma":[0.9992505,0.000031839423,0.00032150056,0.0000034932016,0.00000473818,0.00000145294,0.000025259464,0.000009718387,0.00035150658],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997433,0.000044391603,0.000010490759,0.000060018945,0.00008953198,0.000052349107],"domain_scores_gemma":[0.9991543,0.00026114765,0.00016741078,0.00008672907,0.00025333394,0.00007700261],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00031019235,0.0003538224,0.00034681373,0.0002730099,0.0002634128,0.00026257333,0.0004118968,0.00045583528,0.0012843166],"category_scores_gemma":[0.00084827637,0.00020526451,0.00028307148,0.00020619528,0.00025568297,0.00031927176,0.00020858693,0.00024297487,0.00020280124],"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":[0.00076779706,0.000055290664,0.0035665755,0.00006764425,0.000026508138,0.00020441195,0.000113977534,0.0027139043,0.98732054,0.00008965356,0.000096570904,0.0049772356],"study_design_scores_gemma":[0.000019109944,0.0026172574,0.018778957,0.000008691679,0.00008143097,0.0003489129,0.00008322629,0.010242747,0.9671811,0.00002789628,0.0005980316,0.00001277906],"about_ca_topic_score_codex":0.00033621863,"about_ca_topic_score_gemma":0.00046802795,"teacher_disagreement_score":0.0012843166,"about_ca_system_score_codex":0.00019446368,"about_ca_system_score_gemma":0.0001067641,"threshold_uncertainty_score":0.004296541},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9765272,0.00014574901,0.015412315,0.00014039557,0.000049426664,0.00012361763,0.0004619917,0.00017880072,0.0069604395],"genre_scores_gemma":[0.9924712,0.00006953162,0.005879818,0.000024214625,0.000010035873,0.000050880895,0.00019302058,0.00001723505,0.0012839818],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998054,0.00003751519,0.000014441659,0.000035277266,0.000052777454,0.000054609533],"domain_scores_gemma":[0.9990791,0.0005168673,0.00009721935,0.000079384445,0.00010047795,0.00012689749],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00039776368,0.00047773612,0.0007873857,0.0006227292,0.0007318081,0.0009898352,0.00091565744,0.0018115824,0.0018783252],"category_scores_gemma":[0.0013414162,0.0003076633,0.0006288646,0.0006042701,0.0011478716,0.0006226181,0.0008248719,0.000678974,0.00016600791],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00022808426,0.00021192341,0.004533571,0.00005048598,0.000029127928,0.00072284637,0.00012360736,0.98593986,0.0036551892,0.001876629,0.00030896786,0.0023196624],"study_design_scores_gemma":[0.0000402633,0.000114865645,0.00090059655,0.0000063734055,0.000007260902,0.00004404655,0.000042380932,0.9977247,0.0006831696,0.0002225162,0.00020245052,0.000011310967],"about_ca_topic_score_codex":0.010109623,"about_ca_topic_score_gemma":0.004116664,"teacher_disagreement_score":0.010109623,"about_ca_system_score_codex":0.00071399333,"about_ca_system_score_gemma":0.00081217114,"threshold_uncertainty_score":0.020101607},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9920671,0.00032952227,0.006191139,0.000014580179,0.00002440042,0.000012284886,0.000037439695,0.00009350845,0.0012300456],"genre_scores_gemma":[0.9974583,0.00011258626,0.0015289224,0.00002056758,0.000017184759,0.000006172228,0.00012507635,0.000023874105,0.0007072801],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99980205,0.000012796827,0.000008610315,0.000033138775,0.00010428069,0.00003916124],"domain_scores_gemma":[0.9994306,0.00016297936,0.00012331671,0.000037489976,0.00013908283,0.00010652953],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001817228,0.00020850144,0.00034948724,0.0005719897,0.00028085316,0.00089365087,0.00023191207,0.00038604758,0.0009800484],"category_scores_gemma":[0.0007019362,0.00017876714,0.0003050853,0.00029529055,0.00033925782,0.0005464249,0.00031611937,0.00032348183,0.00020659615],"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":[0.00086442684,0.00007087512,0.021239698,0.00010692908,0.00003951625,0.0036282092,0.00042801703,0.005639317,0.95209706,0.00044649103,0.00017027062,0.015269315],"study_design_scores_gemma":[0.00018024442,0.0036123495,0.4844399,0.00008022912,0.00021024072,0.005797347,0.0016960267,0.10759738,0.3891064,0.0010155209,0.0059962496,0.0002680987],"about_ca_topic_score_codex":0.0006517662,"about_ca_topic_score_gemma":0.000452555,"teacher_disagreement_score":0.0009800484,"about_ca_system_score_codex":0.00018450357,"about_ca_system_score_gemma":0.00016047084,"threshold_uncertainty_score":0.003278613},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.22078258,0.00048436745,0.76913965,0.00010732308,0.00011162519,0.0000394485,0.000022220953,0.0006575616,0.008655262],"genre_scores_gemma":[0.9905489,0.00008811954,0.008135356,0.0000138575515,0.000022057951,0.00001457651,0.000009767903,0.0000133082995,0.0011540337],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99982375,0.00003671795,0.0000070238007,0.000036548157,0.000072646646,0.000023234059],"domain_scores_gemma":[0.9996014,0.00017954117,0.000053203676,0.000020729894,0.00012689302,0.000018247927],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00033314282,0.00063736766,0.00030717175,0.00027802194,0.0002925193,0.00043623,0.0004607084,0.00021973581,0.0010058834],"category_scores_gemma":[0.0006629773,0.00011032456,0.00019461632,0.00010085393,0.00035427723,0.00027211907,0.00041313804,0.00023709438,0.00013397814],"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":[0.00076842465,0.000276054,0.0016018965,0.00033958166,0.000049108214,0.00015792571,0.00019418434,0.26084745,0.47064114,0.009609556,0.00078331184,0.25473133],"study_design_scores_gemma":[0.00007891442,0.0007055981,0.0014217573,0.000028225631,0.000060792376,0.000080182064,0.0000471073,0.86034137,0.13069053,0.002628743,0.0038939267,0.000022805643],"about_ca_topic_score_codex":0.00077667885,"about_ca_topic_score_gemma":0.0012570554,"teacher_disagreement_score":0.0010058834,"about_ca_system_score_codex":0.00029979035,"about_ca_system_score_gemma":0.00021180678,"threshold_uncertainty_score":0.0033650398},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9752319,0.000092678376,0.021881822,0.0001120239,0.00003286434,0.00003685264,0.00008252423,0.00018351595,0.0023458197],"genre_scores_gemma":[0.99480397,0.000036128222,0.0042453017,0.00001360809,0.000010223568,0.000012397114,0.00007097429,0.000015176635,0.00079219684],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999192,0.000018631725,0.000003911512,0.00001892744,0.000020908272,0.000018468174],"domain_scores_gemma":[0.99940884,0.00033856407,0.000058164154,0.000025146668,0.00008418995,0.00008513298],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00030547997,0.00053789583,0.0004580349,0.00044533343,0.00058319344,0.0007272679,0.0005362383,0.0009111141,0.0007295979],"category_scores_gemma":[0.0010539558,0.00049436756,0.00038520573,0.0002750244,0.00083041686,0.00041908922,0.00040187812,0.0005396506,0.000115268456],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00016698115,0.00009151452,0.0034645936,0.000016760901,0.000009341417,0.00009699814,0.00003107241,0.98691076,0.005813124,0.0006634932,0.00013239171,0.0026030361],"study_design_scores_gemma":[0.0000098039345,0.00003333361,0.00053893914,6.938488e-7,0.0000013213191,0.0000031111217,0.000004929107,0.9989435,0.00040706483,0.000043561555,0.000011720465,0.0000020387538],"about_ca_topic_score_codex":0.013115735,"about_ca_topic_score_gemma":0.0048331306,"teacher_disagreement_score":0.013115735,"about_ca_system_score_codex":0.0005982592,"about_ca_system_score_gemma":0.001075945,"threshold_uncertainty_score":0.02607876},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9969664,0.000028122306,0.0027940897,0.000006138345,0.0000020622265,0.0000025820573,0.0000133685635,0.000017758231,0.00016959662],"genre_scores_gemma":[0.99907076,0.000012710784,0.0008164985,0.0000030860767,0.0000019137542,0.0000019826318,0.0000181091,0.0000050027948,0.000069906586],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99987125,0.000016362594,0.0000084706635,0.000025153287,0.000041943484,0.00003681268],"domain_scores_gemma":[0.9993543,0.00020953924,0.0002195475,0.000040036062,0.00008362603,0.00009296899],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025762172,0.0001464472,0.0001925555,0.000513659,0.0001647244,0.00048965804,0.00013711896,0.0001710376,0.00035523385],"category_scores_gemma":[0.0007011743,0.00020998779,0.00013236016,0.00019355706,0.0005156103,0.00037750546,0.00030925393,0.00031116596,0.000057983627],"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":[0.00043230096,0.000051508723,0.012034,0.000029669009,0.00001125882,0.0004114723,0.00020924017,0.0045826333,0.9731204,0.0008112162,0.000055687728,0.008250553],"study_design_scores_gemma":[0.00011686829,0.00068210845,0.42270273,0.000024388715,0.000047657573,0.0011956218,0.0005589335,0.113263376,0.45871073,0.0019818218,0.0005924328,0.0001234115],"about_ca_topic_score_codex":0.0002910158,"about_ca_topic_score_gemma":0.00025148704,"teacher_disagreement_score":0.000513659,"about_ca_system_score_codex":0.00016248507,"about_ca_system_score_gemma":0.00015110978,"threshold_uncertainty_score":0.0013625026},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9974644,0.000025868909,0.0009174671,0.000052522682,0.0000108719,0.0000129496175,0.00007730686,0.00006433778,0.001374297],"genre_scores_gemma":[0.9990866,0.0000146816765,0.0005117037,0.000013586829,0.0000033227755,0.0000069111265,0.00006120622,0.000009001181,0.00029302397],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99993014,0.000015047755,0.0000039524693,0.000010184229,0.000014919494,0.00002581129],"domain_scores_gemma":[0.99958736,0.00016846131,0.000045170997,0.000021778142,0.00004184397,0.00013544096],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002371715,0.00032167474,0.0003394885,0.00025971132,0.0004206356,0.0005152173,0.0004171062,0.00053617696,0.0010027841],"category_scores_gemma":[0.0009161479,0.0002236248,0.000360913,0.00019582867,0.00051610277,0.00040671905,0.00036375842,0.00049793936,0.00008724695],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0008221425,0.00037302138,0.008484239,0.000048072165,0.000055831842,0.00039992362,0.000118018375,0.96679515,0.018279504,0.0013085845,0.00046720775,0.0028483502],"study_design_scores_gemma":[0.00009319229,0.00016303507,0.0051467516,0.0000035302028,0.000010943325,0.0000183534,0.000044496646,0.99243486,0.0017777735,0.00016766472,0.00012775931,0.00001172178],"about_ca_topic_score_codex":0.012635153,"about_ca_topic_score_gemma":0.0072880974,"teacher_disagreement_score":0.012635153,"about_ca_system_score_codex":0.0006365536,"about_ca_system_score_gemma":0.00044644516,"threshold_uncertainty_score":0.025123179},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.54804534,0.0002645126,0.43820757,0.0003735026,0.0001291283,0.00012006033,0.0002739087,0.0007712964,0.0118147805],"genre_scores_gemma":[0.9573158,0.00012002733,0.039104447,0.00004737203,0.000020719086,0.00009217985,0.00012116534,0.00008739548,0.0030908745],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99985826,0.000039684503,0.0000066127086,0.000014808453,0.000057004436,0.000023661403],"domain_scores_gemma":[0.99951446,0.0002540818,0.000044921813,0.000016728462,0.00011826814,0.000051515985],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00056452595,0.00041713938,0.0006496815,0.00037300345,0.0004659267,0.0007635116,0.0007119831,0.00071308727,0.0010492802],"category_scores_gemma":[0.0012290452,0.0003136978,0.0003652133,0.00026572437,0.0006001413,0.00039314845,0.00039267933,0.0005096139,0.00026991114],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00004499487,0.0000235088,0.00064961,0.000017789325,0.000005571914,0.000036518875,0.000019910734,0.99239653,0.0029724855,0.001918855,0.00010049604,0.0018137465],"study_design_scores_gemma":[0.00000297687,0.00000351233,0.000042991163,6.9505774e-7,4.2087646e-7,0.0000013074896,0.0000014320427,0.99967194,0.00016326828,0.00009072294,0.000019403691,0.0000013903721],"about_ca_topic_score_codex":0.023000127,"about_ca_topic_score_gemma":0.0077262474,"teacher_disagreement_score":0.023000127,"about_ca_system_score_codex":0.00084031624,"about_ca_system_score_gemma":0.0016901136,"threshold_uncertainty_score":0.0457325},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0020271651,0.000051400333,0.9966299,0.000035071378,0.00004397162,0.000015839418,0.000017125285,0.0002490604,0.00093049626],"genre_scores_gemma":[0.06430731,0.000085106636,0.9270382,0.00011790266,0.00007997331,0.0001926663,0.00016991573,0.00025581138,0.0077531235],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996226,0.00008057925,0.000018671763,0.000059673217,0.00018768282,0.00003072587],"domain_scores_gemma":[0.9994677,0.00023927803,0.000025826579,0.000058277576,0.00017233055,0.00003668755],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00065051607,0.0008688138,0.0008308751,0.0006525867,0.0005289919,0.0008778266,0.0015697276,0.0017291921,0.006638773],"category_scores_gemma":[0.0013500109,0.00056259194,0.0007658165,0.00064109,0.00050899736,0.0010530023,0.0016382586,0.000997493,0.0022556086],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00032480923,0.00015233799,0.000440075,0.00013866552,0.00012561132,0.0000990512,0.00008865904,0.5224947,0.020861804,0.025022607,0.0054187397,0.42483303],"study_design_scores_gemma":[0.000029458088,0.000036145644,0.000051646737,0.0000041669314,0.0000074203363,0.000023967214,0.000004797147,0.9941624,0.0014010464,0.00264659,0.0016238611,0.000008534201],"about_ca_topic_score_codex":0.002204618,"about_ca_topic_score_gemma":0.00318046,"teacher_disagreement_score":0.006638773,"about_ca_system_score_codex":0.00033203527,"about_ca_system_score_gemma":0.0007222054,"threshold_uncertainty_score":0.02220887},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.018135158,0.00004297318,0.95818186,0.0000438368,0.000040270435,0.00021430067,0.00045524043,0.020592388,0.0022940065],"genre_scores_gemma":[0.22760531,0.00019503369,0.759787,0.0000613087,0.000027649447,0.0006146417,0.0044290326,0.003402603,0.0038773252],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99842215,0.0002344821,0.00015661535,0.00021533792,0.0008578463,0.000113512775],"domain_scores_gemma":[0.99746084,0.00085489627,0.00010219525,0.0006724129,0.00080109434,0.000108658125],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0022254824,0.001558953,0.0008651856,0.0019711403,0.00053714786,0.0017898824,0.0015392386,0.00076756073,0.0068428544],"category_scores_gemma":[0.004270219,0.00088487356,0.0011396289,0.0009365224,0.00041540884,0.0012012961,0.0017932457,0.001226379,0.0020169136],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0004942314,0.00054639665,0.0073126764,0.0003485645,0.00021345737,0.00056310307,0.00044233634,0.514259,0.06111963,0.010382627,0.0074424376,0.39687562],"study_design_scores_gemma":[0.000048249593,0.000103752136,0.00087762764,0.00004226447,0.000028235438,0.0000668467,0.00003554951,0.96156317,0.025772216,0.0022486784,0.009160068,0.000053364205],"about_ca_topic_score_codex":0.006238787,"about_ca_topic_score_gemma":0.0040144837,"teacher_disagreement_score":0.0068428544,"about_ca_system_score_codex":0.00084814016,"about_ca_system_score_gemma":0.0019512149,"threshold_uncertainty_score":0.02289164},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9783831,0.00016822679,0.017345982,0.00003798006,0.000041750947,0.00027567634,0.00007300302,0.00007505028,0.0035991909],"genre_scores_gemma":[0.99002445,0.00014811059,0.008184177,0.000030757245,0.000015343587,0.00007549571,0.00015889309,0.0000230502,0.0013396235],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99860364,0.00048715502,0.00011207894,0.0001088015,0.0006092334,0.00007901223],"domain_scores_gemma":[0.99583215,0.0022687293,0.00053410034,0.00020511025,0.00081926427,0.0003406635],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0017763501,0.00063285336,0.00026616507,0.00045817025,0.00018584864,0.0007433826,0.00046002102,0.00044195176,0.003234278],"category_scores_gemma":[0.0106378775,0.00026730972,0.0005156121,0.0001206913,0.00037436673,0.0005647396,0.001297127,0.0005263454,0.00026287517],"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":[0.00681756,0.0014687983,0.04110735,0.0015118632,0.0002241495,0.0006445303,0.0053256755,0.014751862,0.8524008,0.0015915633,0.00078210275,0.073373765],"study_design_scores_gemma":[0.00092423457,0.04955129,0.39313155,0.00068859337,0.0010777491,0.003382485,0.008861536,0.11141001,0.41305172,0.0023947444,0.014783583,0.00074246596],"about_ca_topic_score_codex":0.000413206,"about_ca_topic_score_gemma":0.00056988833,"teacher_disagreement_score":0.003234278,"about_ca_system_score_codex":0.00025652858,"about_ca_system_score_gemma":0.00019187262,"threshold_uncertainty_score":0.010819674},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.95765305,0.00050105003,0.035548057,0.00014657938,0.0000853701,0.00003475481,0.00003822096,0.0001541995,0.0058386484],"genre_scores_gemma":[0.9934923,0.0001033917,0.004857925,0.00001893471,0.00003122592,0.000013719431,0.000013146497,0.000018594315,0.0014506951],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99966216,0.00011352636,0.000011969928,0.00006316904,0.00010296796,0.0000462379],"domain_scores_gemma":[0.9989679,0.0005235317,0.0002304491,0.00006691629,0.00013765089,0.000073530115],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00051012397,0.0005361036,0.0004935744,0.00031137367,0.0003426281,0.000666413,0.00067492627,0.00067361956,0.0017164765],"category_scores_gemma":[0.0008767804,0.00044512507,0.00032836132,0.00025074603,0.00091957866,0.00063155574,0.0006049129,0.00037173062,0.00043341765],"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":[0.00083572936,0.00013793414,0.0012111892,0.00011710003,0.000046396606,0.00045262979,0.00028319878,0.019876985,0.96351075,0.006986827,0.00032147017,0.0062198127],"study_design_scores_gemma":[0.00031440155,0.0011370245,0.0057979263,0.000040016756,0.00011240908,0.0005532056,0.00027218467,0.47292382,0.5148172,0.0019280912,0.002007333,0.00009641329],"about_ca_topic_score_codex":0.00046077342,"about_ca_topic_score_gemma":0.00053842936,"teacher_disagreement_score":0.0017164765,"about_ca_system_score_codex":0.00034510248,"about_ca_system_score_gemma":0.00025604255,"threshold_uncertainty_score":0.0057421327},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9947702,0.00027137893,0.004358577,0.000014454802,0.00003973693,0.000024915707,0.00003848759,0.00004746047,0.0004347393],"genre_scores_gemma":[0.9923866,0.00025784818,0.0066397707,0.000031195425,0.000024985842,0.00003470122,0.0000976631,0.00004618565,0.00048116504],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9990984,0.00014296688,0.00011543182,0.0001522522,0.00034764336,0.00014336433],"domain_scores_gemma":[0.9965406,0.0019482244,0.00056958024,0.0003296677,0.00045829886,0.00015351688],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00069326744,0.0005469692,0.0005996324,0.00027534447,0.00032019874,0.00078180444,0.00033675047,0.00043538978,0.0011206446],"category_scores_gemma":[0.0030773894,0.00028478578,0.00026303937,0.0003076492,0.000478915,0.00062883704,0.00052563596,0.0006624979,0.0002004115],"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":[0.00088751677,0.00014734837,0.002174864,0.00008022814,0.0000071769455,0.00013971703,0.0000992536,0.0011005647,0.9906865,0.00011319032,0.000028004923,0.0045356643],"study_design_scores_gemma":[0.00005335561,0.0021310903,0.013983744,0.000020440513,0.00003713525,0.00016708879,0.00006497227,0.0074043875,0.9754034,0.00010709491,0.0005787674,0.000048526752],"about_ca_topic_score_codex":0.00019044545,"about_ca_topic_score_gemma":0.00021262262,"teacher_disagreement_score":0.0011206446,"about_ca_system_score_codex":0.00021184214,"about_ca_system_score_gemma":0.00017895919,"threshold_uncertainty_score":0.0037489533},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8006007,0.00018790776,0.18910913,0.00017425927,0.000119609234,0.00012387296,0.00031758507,0.00076866406,0.008598153],"genre_scores_gemma":[0.9449078,0.000091876114,0.05211502,0.000027302709,0.000017797889,0.00012645709,0.00022051184,0.000048739694,0.002444516],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99987245,0.000027118022,0.0000056509834,0.000015164409,0.00004923438,0.0000303803],"domain_scores_gemma":[0.9996352,0.00017487346,0.000034180863,0.000028127353,0.000056159857,0.00007145336],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002535013,0.00048239907,0.0005898327,0.00037029022,0.0005518416,0.000624748,0.00077957107,0.0010113573,0.0013895578],"category_scores_gemma":[0.0009062298,0.00022021274,0.00031778225,0.0003579649,0.00065437757,0.0004602028,0.0005842633,0.0004729642,0.00015671345],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000108745924,0.00009508074,0.0021484916,0.000034495224,0.000024040472,0.00019456068,0.00012769559,0.97521454,0.010869731,0.0035734135,0.00042829505,0.007181014],"study_design_scores_gemma":[0.000014796541,0.00002114028,0.00017921046,0.0000011574381,0.0000019380632,0.0000108063405,0.000008541869,0.99870634,0.0006779828,0.0002075975,0.00016722611,0.0000032802384],"about_ca_topic_score_codex":0.0048334957,"about_ca_topic_score_gemma":0.0028598977,"teacher_disagreement_score":0.0048334957,"about_ca_system_score_codex":0.00032801367,"about_ca_system_score_gemma":0.0006754726,"threshold_uncertainty_score":0.0096107125},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.019333318,0.0034259066,0.9604416,0.00072520156,0.00026278564,0.000049973805,0.00022280474,0.00077785476,0.014760507],"genre_scores_gemma":[0.84031177,0.009466873,0.12792766,0.0005602299,0.0008214585,0.00031366735,0.00048205937,0.0004035885,0.019712718],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99900013,0.00030924045,0.000054760312,0.000117556476,0.0004261926,0.000092055445],"domain_scores_gemma":[0.99830294,0.0009377551,0.00012926836,0.00020540689,0.00036437187,0.000060263574],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0009819644,0.0012472544,0.0010673515,0.0012109696,0.00048380802,0.0016040128,0.0032811875,0.0015784559,0.0018269],"category_scores_gemma":[0.0041900915,0.0005100077,0.0011878359,0.00066999445,0.0010147106,0.0023911404,0.0011690474,0.001300356,0.0012483966],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00003708646,0.000054265372,0.00063191,0.00018382967,0.00004600719,0.00012386477,0.00009726708,0.9124963,0.0015662424,0.053710863,0.0013870165,0.029665338],"study_design_scores_gemma":[0.0000045882225,0.000027806043,0.00007205978,0.00004187355,0.000010858991,0.00004715451,0.000021086187,0.9769274,0.0003717056,0.019357746,0.0031043263,0.000013467928],"about_ca_topic_score_codex":0.004171807,"about_ca_topic_score_gemma":0.0017499129,"teacher_disagreement_score":0.004171807,"about_ca_system_score_codex":0.00061997754,"about_ca_system_score_gemma":0.00088107254,"threshold_uncertainty_score":0.008295059},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7261342,0.0003536108,0.23679614,0.00041520258,0.00023587084,0.000291882,0.001896327,0.0015220874,0.03235472],"genre_scores_gemma":[0.93517274,0.00016246346,0.05790238,0.0001003198,0.000028874858,0.000250687,0.0014733918,0.00017627893,0.0047327834],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996997,0.00006602407,0.000021380449,0.000036369645,0.00012549305,0.000051060626],"domain_scores_gemma":[0.9994286,0.00023940654,0.00007037278,0.000057723446,0.00015116802,0.00005262621],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00036379482,0.00069520756,0.0005673984,0.000527111,0.0003523464,0.00075081934,0.0009875816,0.0008059304,0.0018590974],"category_scores_gemma":[0.0014878814,0.00023755961,0.0005831103,0.0005457818,0.00048736602,0.00052805996,0.0006847937,0.0005888099,0.0002886282],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000054640215,0.00004426702,0.00091016025,0.000027863827,0.000013205643,0.00006850426,0.00004519236,0.9906247,0.0024695613,0.0028764198,0.00035085602,0.0025146657],"study_design_scores_gemma":[0.000011196179,0.0000137354,0.0001822786,0.0000024540032,0.0000016651668,0.0000047352837,0.000009774984,0.9986721,0.00050411094,0.00036592854,0.0002282036,0.0000037490915],"about_ca_topic_score_codex":0.012843866,"about_ca_topic_score_gemma":0.005981606,"teacher_disagreement_score":0.012843866,"about_ca_system_score_codex":0.0005832231,"about_ca_system_score_gemma":0.00071982964,"threshold_uncertainty_score":0.025538206},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99450666,0.000050012077,0.0045442265,0.000022151407,0.000010904089,0.000010497766,0.000019611325,0.00005521106,0.000780657],"genre_scores_gemma":[0.9984901,0.000027976472,0.001068702,0.000004870548,0.000004585035,0.00000531985,0.000020992014,0.000007911804,0.00036943477],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998505,0.000031517542,0.000005669499,0.000023655015,0.000048250015,0.00004027566],"domain_scores_gemma":[0.99973685,0.00013635022,0.000039499966,0.000016760481,0.000040719602,0.000029780304],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00028299456,0.00040956298,0.0004495228,0.00041284907,0.00032608616,0.0003174982,0.00028585485,0.00036101276,0.0008274134],"category_scores_gemma":[0.00052086345,0.00013477991,0.00029479802,0.0001889871,0.0006810546,0.00033489102,0.00036002483,0.00028429262,0.00009890569],"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":[0.0024628828,0.0006319629,0.023717036,0.00032880896,0.00006381242,0.004914755,0.001001734,0.25822055,0.67305064,0.002662003,0.00064145285,0.032304324],"study_design_scores_gemma":[0.000107356216,0.0012079234,0.03639621,0.000026887526,0.000041658197,0.00051573606,0.0003797349,0.83908427,0.120915174,0.00067895034,0.0005805482,0.00006556148],"about_ca_topic_score_codex":0.0017068004,"about_ca_topic_score_gemma":0.0010564065,"teacher_disagreement_score":0.0017068004,"about_ca_system_score_codex":0.00023995645,"about_ca_system_score_gemma":0.00018472342,"threshold_uncertainty_score":0.0033937097},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99716103,0.00013289043,0.0017398201,0.000017645118,0.000020412806,0.000008145847,0.000037789276,0.000030271405,0.00085199653],"genre_scores_gemma":[0.99918526,0.00003223279,0.0004159618,0.0000045498787,0.000008770739,0.0000036474673,0.000042533862,0.000011065916,0.0002959395],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9996271,0.00008396671,0.000028105647,0.00007229533,0.00007614783,0.00011238207],"domain_scores_gemma":[0.9991321,0.00041154455,0.00013443892,0.0000478119,0.00011046396,0.00016366341],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005807497,0.00047763003,0.0004558516,0.0012142857,0.00089812675,0.0019862007,0.00039516436,0.000488748,0.0018372989],"category_scores_gemma":[0.0014500618,0.0003896596,0.00046891236,0.0005054575,0.0010262736,0.00091134285,0.0009219821,0.000604057,0.00017324572],"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":[0.010382585,0.0004280338,0.013161348,0.00015865066,0.00010066232,0.00055619434,0.0006722774,0.013706123,0.9407742,0.008662553,0.00026094407,0.011136466],"study_design_scores_gemma":[0.00090934616,0.0018818054,0.043032214,0.000042686257,0.00021350924,0.00031268422,0.0006309802,0.16560271,0.7826207,0.0036189372,0.00093581306,0.00019854122],"about_ca_topic_score_codex":0.00073745876,"about_ca_topic_score_gemma":0.00034163342,"teacher_disagreement_score":0.0019862007,"about_ca_system_score_codex":0.00057976146,"about_ca_system_score_gemma":0.00028559144,"threshold_uncertainty_score":0.006146431},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.45929646,0.006633095,0.4928102,0.0006526448,0.00024130018,0.00023094428,0.00008707376,0.00034079893,0.039707508],"genre_scores_gemma":[0.9737583,0.0016804794,0.017539585,0.0000702519,0.000105994586,0.000056935853,0.000027754219,0.000030022176,0.00673068],"study_design_codex":"simulation_or_modeling","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.9999088,0.000025764897,0.00000382542,0.0000149927155,0.000027522909,0.000019047662],"domain_scores_gemma":[0.99981695,0.00007695329,0.000043047457,0.000010828205,0.00004178582,0.000010382949],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024651355,0.00039057707,0.00036409614,0.00063096284,0.0004960329,0.00062865997,0.0003984975,0.00052054605,0.00097206497],"category_scores_gemma":[0.0009100292,0.00019993319,0.00039095216,0.0002446549,0.0013480033,0.00064914644,0.0003582759,0.0004660633,0.0001573327],"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":[0.00026127018,0.0004158017,0.005496739,0.0005970681,0.000055795106,0.002884061,0.0013980205,0.40210906,0.17785354,0.34999642,0.002218486,0.056713663],"study_design_scores_gemma":[0.0000246781,0.00015680723,0.0011595344,0.000023716224,0.000014428019,0.00046617145,0.00010876044,0.972421,0.0073417225,0.014781057,0.0034686392,0.000033534507],"about_ca_topic_score_codex":0.0015310629,"about_ca_topic_score_gemma":0.00056710106,"teacher_disagreement_score":0.0015310629,"about_ca_system_score_codex":0.0006118375,"about_ca_system_score_gemma":0.0004936083,"threshold_uncertainty_score":0.0044392347},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98348075,0.00008213104,0.015434285,0.000050055532,0.000024899955,0.000028343911,0.000022727367,0.0001116687,0.00076509407],"genre_scores_gemma":[0.9939622,0.000031836513,0.0056894803,0.000010866953,0.0000049647415,0.0000122047795,0.000022715669,0.000012540764,0.00025318153],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99979633,0.00007639846,0.000015120943,0.0000249085,0.000049750175,0.000037509202],"domain_scores_gemma":[0.99904615,0.0005770018,0.00010758711,0.00004519884,0.000119126475,0.00010499999],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0008045162,0.00047581256,0.00041424978,0.0003944605,0.0004038897,0.00060420326,0.00051353633,0.00092227245,0.0003794661],"category_scores_gemma":[0.0018738235,0.0003018182,0.00050758646,0.0001918236,0.00058980327,0.000465811,0.00047715154,0.00063762045,0.00007237765],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00015428397,0.00008283103,0.0034272156,0.000025814317,0.000013329207,0.00011703271,0.00003830848,0.9848887,0.007469122,0.0002117122,0.000043505053,0.0035281735],"study_design_scores_gemma":[0.0000070441183,0.00006100285,0.00033975925,0.0000020988568,0.0000027608799,0.0000065086215,0.0000098952405,0.99817824,0.001352968,0.000021853599,0.0000147481405,0.0000031441448],"about_ca_topic_score_codex":0.014577748,"about_ca_topic_score_gemma":0.007941498,"teacher_disagreement_score":0.014577748,"about_ca_system_score_codex":0.00045923868,"about_ca_system_score_gemma":0.0008772501,"threshold_uncertainty_score":0.028985798},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9919699,0.000059199614,0.0070412937,0.000020798168,0.000008042302,0.00001711385,0.000025771962,0.00005132283,0.00080659526],"genre_scores_gemma":[0.99898463,0.000021129035,0.0007961572,0.000005180555,0.000002192372,0.0000058089336,0.00001901536,0.0000070403353,0.00015881968],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99959594,0.00008751208,0.000013617838,0.000059938433,0.00017849129,0.00006458148],"domain_scores_gemma":[0.9976895,0.0015997418,0.00015938315,0.00009031613,0.0003489345,0.00011220018],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00039798574,0.00035997885,0.0003561482,0.00032617975,0.00025732198,0.00026905685,0.00025338263,0.00030006745,0.0009242187],"category_scores_gemma":[0.001981154,0.0001522743,0.00019486777,0.00014983241,0.0005719943,0.00030089795,0.0002854371,0.00023822646,0.00015856075],"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":[0.001378116,0.0000899589,0.006566525,0.0001498744,0.000016027283,0.00073110027,0.00040988796,0.01481274,0.95750725,0.0005104722,0.00012148176,0.017706536],"study_design_scores_gemma":[0.000090073816,0.0012719495,0.0598671,0.00003307121,0.000043081764,0.00071450806,0.0002865803,0.099282116,0.8373671,0.0003780723,0.0005965392,0.000069782844],"about_ca_topic_score_codex":0.00080125814,"about_ca_topic_score_gemma":0.0007726796,"teacher_disagreement_score":0.0009242187,"about_ca_system_score_codex":0.00024607257,"about_ca_system_score_gemma":0.00013431559,"threshold_uncertainty_score":0.0030918717},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9782296,0.00006217061,0.02026206,0.000037766433,0.00007491916,0.00011041744,0.00010381764,0.00022933506,0.0008901042],"genre_scores_gemma":[0.99616677,0.000031184463,0.0030154497,0.000014864787,0.000010255876,0.00005092018,0.000056914614,0.000025856774,0.0006279009],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9986492,0.000303044,0.00007466664,0.00021116334,0.00051067694,0.00025131783],"domain_scores_gemma":[0.99711454,0.0013026284,0.0002866153,0.00024305524,0.00082542014,0.00022781333],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0011917435,0.0010118922,0.0005252776,0.00055600086,0.0008672254,0.0004924083,0.00097366807,0.0009282089,0.0024901005],"category_scores_gemma":[0.0036149875,0.000324898,0.00034471366,0.0002343473,0.0011686172,0.00056245306,0.00082635647,0.00039782646,0.00027026032],"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":[0.007163247,0.0014189129,0.005692035,0.0004715077,0.00004117541,0.00027040852,0.00073182624,0.010611924,0.945446,0.00086829386,0.00031306702,0.02697166],"study_design_scores_gemma":[0.00051508006,0.011106366,0.025422897,0.000060844628,0.00015637965,0.00024742418,0.00022348393,0.05833872,0.9006254,0.00031429782,0.0028928032,0.000096208474],"about_ca_topic_score_codex":0.0018661018,"about_ca_topic_score_gemma":0.0015504454,"teacher_disagreement_score":0.0024901005,"about_ca_system_score_codex":0.00045127686,"about_ca_system_score_gemma":0.0005540681,"threshold_uncertainty_score":0.008330226},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9973386,0.000042909105,0.0013502188,0.00001449627,0.0000051616225,0.000007449981,0.000023360868,0.000032384825,0.0011854349],"genre_scores_gemma":[0.9991074,0.000010088393,0.00040754242,0.0000030913773,0.0000023263567,0.0000031928555,0.000022595881,0.0000049895225,0.00043879735],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999509,0.000007550698,0.0000012152262,0.000008519861,0.000012812789,0.000019102728],"domain_scores_gemma":[0.9998894,0.00003676163,0.000011789841,0.000008688865,0.000024410228,0.000028899178],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012159335,0.00017219056,0.00026416001,0.0003517956,0.00043292213,0.00023655606,0.00025918815,0.0002713641,0.0014408763],"category_scores_gemma":[0.00036047903,0.00015005673,0.00023808339,0.00023342189,0.0003173929,0.000353086,0.0003977504,0.0003521254,0.000087970184],"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":[0.0012568845,0.00018475605,0.02883606,0.00007650753,0.000106467945,0.0014554532,0.0008793182,0.03489643,0.9156894,0.0037214127,0.0005521235,0.0123451585],"study_design_scores_gemma":[0.000208618,0.0012942798,0.25211802,0.000015526071,0.00010955939,0.00059993414,0.0010685313,0.56647485,0.17330678,0.0012226115,0.0034928764,0.00008843861],"about_ca_topic_score_codex":0.003061517,"about_ca_topic_score_gemma":0.0025201256,"teacher_disagreement_score":0.003061517,"about_ca_system_score_codex":0.00020880085,"about_ca_system_score_gemma":0.00017639832,"threshold_uncertainty_score":0.0060873628},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99330336,0.00012509043,0.0015581235,0.000046937952,0.000028732873,0.00004109076,0.0011343261,0.00009213893,0.0036701958],"genre_scores_gemma":[0.9959806,0.00009996697,0.0022739798,0.000019742925,0.000009594665,0.000026914882,0.0010192661,0.00002162286,0.00054831087],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997509,0.000040084968,0.0000294623,0.000041513966,0.00007045766,0.00006764787],"domain_scores_gemma":[0.9994655,0.00017404888,0.000071517585,0.00003764559,0.00013499933,0.00011631755],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000378059,0.00069025723,0.0010061907,0.000669733,0.0006386653,0.0012802857,0.00071934,0.0009888795,0.0012678282],"category_scores_gemma":[0.0011136412,0.00028399948,0.00042686862,0.001006821,0.0008676821,0.00043155334,0.0003721345,0.00050171796,0.00012449158],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0008059306,0.00043359245,0.019634655,0.00014438079,0.00009252715,0.0011876756,0.00020989859,0.9466883,0.022705559,0.0035737962,0.00091702753,0.003606705],"study_design_scores_gemma":[0.00010904088,0.00025324058,0.014397578,0.000023849707,0.00001409467,0.00009143225,0.00012000321,0.98118985,0.0028343806,0.00040855425,0.00052197906,0.00003595128],"about_ca_topic_score_codex":0.020108901,"about_ca_topic_score_gemma":0.011312805,"teacher_disagreement_score":0.020108901,"about_ca_system_score_codex":0.0013437547,"about_ca_system_score_gemma":0.00090366934,"threshold_uncertainty_score":0.03998375},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99478096,0.00019873872,0.0044932845,0.000017954384,0.000009605489,0.000012842438,0.0000068481827,0.000037290763,0.000442451],"genre_scores_gemma":[0.99820733,0.00008669068,0.001520792,0.000009731147,0.000005608645,0.000005304672,0.00000998597,0.0000067335204,0.00014789397],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99937516,0.00009722535,0.000030171072,0.00011302662,0.000260832,0.00012368405],"domain_scores_gemma":[0.9991769,0.00040847337,0.00021879208,0.000042370066,0.00008696078,0.00006641165],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00040114953,0.0005267208,0.0005078173,0.00030891507,0.00039058801,0.0006342911,0.00040886295,0.00045019452,0.0010029428],"category_scores_gemma":[0.0015122498,0.00034309208,0.00026454436,0.0001702296,0.00074987934,0.00066668674,0.0007789618,0.00039070775,0.00010769325],"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":[0.00026414005,0.00004150882,0.0012342702,0.00009736046,0.000016872564,0.00019464527,0.00008952679,0.0050938926,0.9870863,0.000114876086,0.000017999982,0.0057486575],"study_design_scores_gemma":[0.00008481807,0.0015044876,0.026990484,0.00001480736,0.00007054569,0.00035116373,0.00020958667,0.040061735,0.92984915,0.00013847364,0.0006701505,0.000054761145],"about_ca_topic_score_codex":0.0007230851,"about_ca_topic_score_gemma":0.00058229227,"teacher_disagreement_score":0.0010029428,"about_ca_system_score_codex":0.00034548764,"about_ca_system_score_gemma":0.00021200378,"threshold_uncertainty_score":0.0033551455},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99105513,0.00010945274,0.0077782567,0.000015565372,0.000010776976,0.000009740746,0.000017915889,0.000071059156,0.00093210314],"genre_scores_gemma":[0.9982652,0.00004035648,0.0014414676,0.00000904401,0.0000030554859,0.000006941204,0.000015582957,0.0000052842265,0.00021298675],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99981815,0.000027843276,0.000009595684,0.000047358037,0.000049309707,0.00004769516],"domain_scores_gemma":[0.99968195,0.00009502457,0.000114857205,0.000020488742,0.000047141348,0.00004046073],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025354407,0.000190831,0.00027810677,0.0002867354,0.0002565266,0.00040889432,0.00027508184,0.00045232015,0.0010255211],"category_scores_gemma":[0.00064214796,0.00021242304,0.00021237948,0.00019356646,0.00059786707,0.0004312283,0.00057415734,0.00035419487,0.00018000517],"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":[0.00020119727,0.000030195033,0.002222094,0.00005454823,0.000007818537,0.00024772383,0.00009135058,0.0042551886,0.98826873,0.00076323317,0.00004659892,0.0038113284],"study_design_scores_gemma":[0.00008696778,0.0012675303,0.02306215,0.000027064252,0.00003542801,0.00033794602,0.00027968842,0.10217895,0.86979413,0.0010158154,0.0018637141,0.000050548402],"about_ca_topic_score_codex":0.00025079673,"about_ca_topic_score_gemma":0.00019420835,"teacher_disagreement_score":0.0010255211,"about_ca_system_score_codex":0.00020243516,"about_ca_system_score_gemma":0.00015647992,"threshold_uncertainty_score":0.0034307241},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6118001,0.00067327684,0.3839149,0.00017416196,0.00009059201,0.00006290889,0.00022075046,0.00028559603,0.0027778049],"genre_scores_gemma":[0.9562719,0.000304366,0.04204392,0.00002417181,0.000047014404,0.00003154051,0.00022213277,0.000021649976,0.0010333754],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999249,0.000010023081,0.000004506913,0.000014312028,0.000036269274,0.000010029708],"domain_scores_gemma":[0.9998572,0.00005192664,0.000023567938,0.000011127472,0.00004579574,0.000010387131],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001839841,0.00026686562,0.000187646,0.0006971466,0.00015634434,0.00021236208,0.00018573385,0.00018639151,0.0005247789],"category_scores_gemma":[0.00049515325,0.00006279805,0.00020949783,0.0004400562,0.00022682201,0.00033250407,0.00023210542,0.00024411408,0.00010068999],"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":[0.00038469266,0.00021743843,0.008451148,0.00046448346,0.00006421616,0.0014500989,0.00073774427,0.105232276,0.41289508,0.011307732,0.0019483017,0.45684674],"study_design_scores_gemma":[0.00001068315,0.00026826424,0.02720319,0.000030182522,0.000023950044,0.0004198208,0.0002717388,0.92313176,0.04121788,0.0044696173,0.0029104026,0.000042456013],"about_ca_topic_score_codex":0.0006389761,"about_ca_topic_score_gemma":0.00046116294,"teacher_disagreement_score":0.0006971466,"about_ca_system_score_codex":0.00009937545,"about_ca_system_score_gemma":0.00014522224,"threshold_uncertainty_score":0.0017555952},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99711466,0.00013988285,0.0021836592,0.000008061448,0.000010291788,0.000011052086,0.000024591433,0.00004304352,0.00046458901],"genre_scores_gemma":[0.9983229,0.000068606845,0.0014247034,0.00000539525,0.0000033824422,0.000005014114,0.000017424536,0.000011020992,0.00014146452],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99965143,0.0000694377,0.00002565574,0.00008609564,0.00009772899,0.00006974598],"domain_scores_gemma":[0.99810994,0.0011427893,0.0003539288,0.00014267582,0.0001499601,0.000100699],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00039914384,0.00057074666,0.0004591989,0.0002771457,0.00026014328,0.00046418054,0.0005327566,0.00040282708,0.0015677887],"category_scores_gemma":[0.0013939183,0.0003287544,0.00019269048,0.0001318349,0.00056371297,0.0003526816,0.0004260933,0.00038601152,0.00023593125],"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":[0.00057749223,0.000044035365,0.00079191127,0.00009968179,0.000007061722,0.00019365235,0.000065875276,0.002527468,0.99255884,0.00012835063,0.000022255403,0.0029833196],"study_design_scores_gemma":[0.000044095472,0.0013756517,0.005334899,0.00001229209,0.00002928251,0.00012949605,0.000075841286,0.0077493433,0.9848856,0.00004341912,0.00029643864,0.000023744204],"about_ca_topic_score_codex":0.0002451824,"about_ca_topic_score_gemma":0.00032891083,"teacher_disagreement_score":0.0015677887,"about_ca_system_score_codex":0.00020069776,"about_ca_system_score_gemma":0.00014724533,"threshold_uncertainty_score":0.005244732},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6906815,0.00037375357,0.30329603,0.00005667282,0.000048513077,0.00010138223,0.00006044141,0.0008318461,0.004549891],"genre_scores_gemma":[0.9929986,0.00007157205,0.0056688474,0.0000085104175,0.000006373504,0.000013303554,0.00002798328,0.000014977285,0.0011899027],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99970394,0.000043978762,0.000013746903,0.00006816543,0.000120232224,0.000049910854],"domain_scores_gemma":[0.9996741,0.000108790235,0.000077629295,0.000025907702,0.00008960651,0.00002400128],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00037971453,0.00063129904,0.0003884001,0.00036964862,0.00034523627,0.0003599004,0.000454992,0.00022738782,0.0009162692],"category_scores_gemma":[0.00056488626,0.00016112122,0.00029673037,0.00014640405,0.00048012464,0.0002608046,0.00036370815,0.00015378541,0.00013519861],"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":[0.0010851164,0.0004089375,0.01618268,0.0005378043,0.00005274689,0.00036997488,0.000527003,0.32962456,0.55206364,0.0032638262,0.0005000054,0.09538368],"study_design_scores_gemma":[0.00009386701,0.0014545071,0.018463392,0.000038851307,0.00010270247,0.00013195424,0.00012842561,0.8420263,0.13002169,0.00090683514,0.0065631587,0.00006840142],"about_ca_topic_score_codex":0.012316646,"about_ca_topic_score_gemma":0.0118353,"teacher_disagreement_score":0.012316646,"about_ca_system_score_codex":0.0006918843,"about_ca_system_score_gemma":0.00059758616,"threshold_uncertainty_score":0.02448988},"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":"methods","genre_gemma":"methods","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.026845684,0.00011648528,0.9701732,0.00011843086,0.000059259743,0.00012366385,0.000028403028,0.0009435915,0.0015913066],"genre_scores_gemma":[0.18431947,0.00026260348,0.8115891,0.00011479761,0.000041915177,0.00022340493,0.00007124615,0.00015736574,0.003220125],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9996277,0.00006239029,0.000021104623,0.00010776726,0.00015231309,0.000028748831],"domain_scores_gemma":[0.9994056,0.00015612136,0.000067831774,0.00016851374,0.00018428113,0.000017625081],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006525708,0.0006759272,0.00049337046,0.0004940081,0.00053555943,0.00075934303,0.0011719514,0.00057887356,0.0021100391],"category_scores_gemma":[0.0013742809,0.0003233517,0.0003847837,0.0004739399,0.00061744306,0.0011842145,0.00057251845,0.001290954,0.0012417453],"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":[0.00014237131,0.00028534868,0.0015041748,0.00031346147,0.000024136723,0.00012471323,0.00036084323,0.005879651,0.7199014,0.020994714,0.0010536854,0.24941547],"study_design_scores_gemma":[0.00007614244,0.0006435941,0.0038433084,0.00006756817,0.000073348696,0.000650985,0.0001497731,0.20436001,0.76178485,0.009311542,0.018933797,0.00010504571],"about_ca_topic_score_codex":0.0007349209,"about_ca_topic_score_gemma":0.001168661,"teacher_disagreement_score":0.0021100391,"about_ca_system_score_codex":0.00030595507,"about_ca_system_score_gemma":0.0009003548,"threshold_uncertainty_score":0.0070587397},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98590255,0.000091488706,0.012374946,0.000045212044,0.000026551097,0.000056589317,0.00019631145,0.00013300375,0.0011733624],"genre_scores_gemma":[0.99637383,0.00005852515,0.0029384813,0.00000846324,0.0000028962227,0.000033049306,0.00007325502,0.000009418208,0.00050211576],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99988055,0.000012762073,0.000005973785,0.0000350393,0.000041874766,0.000023889805],"domain_scores_gemma":[0.9997557,0.00010849625,0.000037753827,0.000032253316,0.000040522333,0.000025248335],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024351968,0.0004160421,0.00067570346,0.00024024055,0.000403227,0.00064506003,0.00051625434,0.0006570898,0.0012848598],"category_scores_gemma":[0.0004290307,0.00019665703,0.0004983876,0.0001690385,0.0005029886,0.00030730476,0.00038684224,0.0005007894,0.00012023836],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0005174619,0.00050256774,0.004970712,0.00018783884,0.000051534444,0.0005442785,0.00020678715,0.49915,0.486152,0.0010853146,0.00031690812,0.006314587],"study_design_scores_gemma":[0.0000834806,0.0006629198,0.00425014,0.000008153126,0.000022279812,0.00003342128,0.000048023758,0.9431354,0.051219128,0.00017973369,0.00032806705,0.000029341725],"about_ca_topic_score_codex":0.0043519605,"about_ca_topic_score_gemma":0.0019152737,"teacher_disagreement_score":0.0043519605,"about_ca_system_score_codex":0.00040262492,"about_ca_system_score_gemma":0.0003928834,"threshold_uncertainty_score":0.008653283},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9895008,0.00056475756,0.0076496163,0.000028312948,0.000020974045,0.00001224653,0.000032458294,0.000090688656,0.0021001648],"genre_scores_gemma":[0.9974878,0.0001616683,0.0018271158,0.000010676174,0.000010917715,0.0000050811714,0.000054095883,0.000037961807,0.0004047937],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997867,0.00004316627,0.000016536651,0.00004551699,0.00006024015,0.000047876954],"domain_scores_gemma":[0.9991824,0.00040809732,0.00017239805,0.000050947987,0.000105609986,0.00008051627],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025834932,0.00034328067,0.0003941322,0.0005439506,0.0003262071,0.00075430505,0.0001397401,0.00025781093,0.00075791206],"category_scores_gemma":[0.001504342,0.00027656445,0.0002036818,0.0001653091,0.000468162,0.0005373555,0.00040835093,0.00030928783,0.0001987034],"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":[0.0009728525,0.00010938925,0.014048003,0.00012136009,0.000018466126,0.0008261852,0.00025612154,0.015281311,0.94681346,0.00081339077,0.00012955493,0.020609884],"study_design_scores_gemma":[0.00014067262,0.0012874305,0.29206276,0.000070931615,0.000097006414,0.0015174132,0.00028909522,0.09035132,0.61023915,0.0010968125,0.002682711,0.00016473845],"about_ca_topic_score_codex":0.0003362351,"about_ca_topic_score_gemma":0.00034366184,"teacher_disagreement_score":0.00075791206,"about_ca_system_score_codex":0.00016964515,"about_ca_system_score_gemma":0.000121553836,"threshold_uncertainty_score":0.0025354624},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9927441,0.00006777399,0.005047073,0.000014061262,0.000030984575,0.000041252584,0.00024606197,0.0001277064,0.0016809135],"genre_scores_gemma":[0.99401736,0.000066657805,0.0049268086,0.000019402894,0.0000052174296,0.000020837439,0.00026216803,0.000014265529,0.000667232],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997316,0.000015578249,0.000009916672,0.00004272902,0.00013007656,0.00007019334],"domain_scores_gemma":[0.9996594,0.00006953627,0.000028962133,0.00003966628,0.00013482927,0.00006762343],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018758516,0.00037453827,0.00032645382,0.00033606414,0.00049489585,0.0002055534,0.00024910565,0.00036916652,0.001994162],"category_scores_gemma":[0.00059816084,0.00013309118,0.00023161352,0.00018397885,0.00027314137,0.00024235457,0.00037451184,0.00047744543,0.00028363746],"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":[0.00019879185,0.00005247289,0.0043905694,0.000053754145,0.0000064279197,0.0004901623,0.0001373227,0.0010689427,0.98166627,0.00010802983,0.00017880205,0.01164846],"study_design_scores_gemma":[0.000060847833,0.0022335155,0.0732074,0.0000393941,0.000032433116,0.00088484085,0.00038569752,0.016438939,0.904128,0.00020255511,0.002339046,0.000047205438],"about_ca_topic_score_codex":0.0012011348,"about_ca_topic_score_gemma":0.0010750971,"teacher_disagreement_score":0.001994162,"about_ca_system_score_codex":0.00014725937,"about_ca_system_score_gemma":0.00024349388,"threshold_uncertainty_score":0.0066711307},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99516666,0.00013863374,0.003170265,0.000021081229,0.00002377872,0.000019101637,0.000029174835,0.00008064147,0.0013507932],"genre_scores_gemma":[0.99838364,0.000083917235,0.0012332764,0.000008655095,0.000005105796,0.000009859312,0.00002541854,0.000019159677,0.00023090855],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.99963,0.000054049444,0.000025194748,0.00010262222,0.00008659939,0.00010160885],"domain_scores_gemma":[0.99851495,0.00047657214,0.00036596396,0.0000994491,0.00025400694,0.000289112],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000540777,0.00040001865,0.00040851018,0.0003037135,0.0004832759,0.00072767376,0.0004953192,0.0005044545,0.0021620193],"category_scores_gemma":[0.002018816,0.0004481934,0.0002756029,0.00025775708,0.0006217483,0.0007450564,0.00067125156,0.00050314754,0.0004776585],"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":[0.00055795757,0.00016772203,0.0025263603,0.00011234688,0.000021761562,0.0003221241,0.00014165117,0.013610579,0.9786557,0.0008359121,0.00013310615,0.0029146874],"study_design_scores_gemma":[0.000109095956,0.0016601272,0.014966266,0.000035676356,0.00010493147,0.00031991597,0.0004032336,0.1011757,0.8790931,0.0003989362,0.0016603378,0.00007268155],"about_ca_topic_score_codex":0.000984241,"about_ca_topic_score_gemma":0.00087289186,"teacher_disagreement_score":0.0021620193,"about_ca_system_score_codex":0.00030795764,"about_ca_system_score_gemma":0.00036114856,"threshold_uncertainty_score":0.007232666},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99364245,0.000039688664,0.003548334,0.0000972077,0.000015507896,0.000022074822,0.00017205001,0.000085634194,0.0023769815],"genre_scores_gemma":[0.99702793,0.000019717092,0.0020772067,0.000016053644,0.0000031819955,0.000010875997,0.00009388521,0.0000127054,0.0007384292],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999915,0.00001524882,0.0000052981013,0.000013871477,0.000021958427,0.000028678298],"domain_scores_gemma":[0.9995414,0.0002588213,0.000040550214,0.000021310381,0.000055682634,0.00008237667],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024122154,0.00033756628,0.00042730014,0.00032039903,0.0005172133,0.0006478933,0.0004022729,0.00085388863,0.0012648737],"category_scores_gemma":[0.0009864771,0.00022171067,0.00030673426,0.0002780344,0.0006772681,0.0003636785,0.00038519345,0.0005198343,0.00008329444],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00036013976,0.00016235217,0.0103327315,0.000046576777,0.00002463236,0.0005775988,0.00020795598,0.96649253,0.015533176,0.0016539373,0.00041754756,0.0041907607],"study_design_scores_gemma":[0.000021063475,0.0000544714,0.0021171907,0.0000033942151,0.0000032389123,0.000018702862,0.000032865293,0.99632484,0.0011702602,0.00012567008,0.00012053839,0.000007776789],"about_ca_topic_score_codex":0.014412412,"about_ca_topic_score_gemma":0.0071256277,"teacher_disagreement_score":0.014412412,"about_ca_system_score_codex":0.0007554246,"about_ca_system_score_gemma":0.0007260245,"threshold_uncertainty_score":0.02865702},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.036343567,0.00042563747,0.950457,0.0007324741,0.0000921608,0.00013669228,0.00020055728,0.00023556763,0.011376332],"genre_scores_gemma":[0.8527676,0.00036623504,0.13184828,0.0003110465,0.00009652179,0.00059535855,0.0002611766,0.00019158304,0.013562413],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999238,0.00027043358,0.000029422594,0.00019964422,0.0001348551,0.00012766145],"domain_scores_gemma":[0.9980813,0.0013812929,0.00015167336,0.00004063504,0.0002646371,0.00008047081],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0021112754,0.0015813562,0.0019914072,0.0006000798,0.00057367457,0.0017178465,0.00081746996,0.0021833437,0.0060259006],"category_scores_gemma":[0.003941103,0.0008002044,0.00065684563,0.00044415018,0.0015671275,0.0009795005,0.0012617206,0.0017741777,0.00065119157],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00012690353,0.0000396986,0.00025550966,0.00009421195,0.000032929944,0.00006600423,0.00006099924,0.982061,0.0014466057,0.007090495,0.0010888502,0.0076368186],"study_design_scores_gemma":[0.000030782852,0.000039280505,0.00013979453,0.000006862886,0.00000794047,0.000008119452,0.000018364564,0.9972486,0.00032567405,0.0018217585,0.00034451642,0.00000826217],"about_ca_topic_score_codex":0.006810563,"about_ca_topic_score_gemma":0.0026948252,"teacher_disagreement_score":0.006810563,"about_ca_system_score_codex":0.0012689813,"about_ca_system_score_gemma":0.0015719346,"threshold_uncertainty_score":0.020158708},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9430694,0.00021919573,0.030745704,0.00031222106,0.0001214897,0.000059281385,0.00027853303,0.00017250067,0.025021572],"genre_scores_gemma":[0.9937569,0.000074229465,0.0033008088,0.000030248671,0.000016732041,0.000015793608,0.00012317699,0.00002008153,0.0026619735],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998276,0.000021742675,0.000011119485,0.000028412342,0.000059496266,0.000051647497],"domain_scores_gemma":[0.99967945,0.00012162644,0.000044968623,0.000023927178,0.000065235,0.000064883454],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020671476,0.0004466371,0.0006436111,0.00044259444,0.00096069195,0.0014733747,0.0007663271,0.001231665,0.0016762576],"category_scores_gemma":[0.0009177606,0.00033852344,0.00056200556,0.00048059903,0.0011263137,0.0004762888,0.0005591239,0.0006545818,0.00020915554],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00006580786,0.000090405854,0.0015872327,0.000017557106,0.000008937717,0.00010093757,0.000052846743,0.988881,0.004173622,0.0027924965,0.00020976774,0.002019403],"study_design_scores_gemma":[0.000009816559,0.000019320378,0.0006238934,0.0000018344268,0.000002403028,0.0000091728425,0.000022661947,0.99840194,0.0005921628,0.00019973509,0.00011092299,0.000006153817],"about_ca_topic_score_codex":0.025215749,"about_ca_topic_score_gemma":0.011520969,"teacher_disagreement_score":0.025215749,"about_ca_system_score_codex":0.0010107023,"about_ca_system_score_gemma":0.0012104132,"threshold_uncertainty_score":0.050137937},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.56047004,0.00034688425,0.43397138,0.00029926884,0.00006105972,0.000031029285,0.00042372695,0.0003612048,0.004035303],"genre_scores_gemma":[0.9108892,0.0003644084,0.08702052,0.000021213078,0.000049340037,0.000022402182,0.0005808377,0.000052975847,0.0009992669],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.99994934,0.000007164448,0.0000016210897,0.0000097995535,0.000022020165,0.000009988526],"domain_scores_gemma":[0.9999455,0.000010362658,0.000010135493,0.000008795488,0.00001798763,0.0000071951376],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017345298,0.00032204142,0.00018510252,0.0004705617,0.0001564526,0.00028139135,0.00012748512,0.00013436837,0.0003509483],"category_scores_gemma":[0.000353843,0.000110179986,0.00021041169,0.0003026339,0.00015421772,0.00026872585,0.0001569397,0.00030865308,0.000070079564],"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":[0.00026069005,0.00009843853,0.034737725,0.00014293453,0.00008178309,0.0002451008,0.00014084655,0.18403368,0.3969736,0.024898479,0.0019661007,0.3564207],"study_design_scores_gemma":[0.000015995485,0.000063459935,0.05988945,0.000013456414,0.000020509036,0.00009753829,0.000064845015,0.90019476,0.03324042,0.0035541544,0.0028237093,0.00002179194],"about_ca_topic_score_codex":0.0021463905,"about_ca_topic_score_gemma":0.0024705727,"teacher_disagreement_score":0.0021463905,"about_ca_system_score_codex":0.00017580207,"about_ca_system_score_gemma":0.00038183862,"threshold_uncertainty_score":0.004267752},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99469614,0.000053623397,0.0048883976,0.000007653947,0.0000034298994,0.0000039404554,0.000031106698,0.000029802568,0.00028586015],"genre_scores_gemma":[0.9968714,0.000045443863,0.0027656283,0.0000051378947,0.0000034696536,0.0000049081896,0.000083811225,0.0000063944935,0.00021376264],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999598,0.0000040795603,0.0000019354204,0.0000073922038,0.000015944852,0.000010830496],"domain_scores_gemma":[0.9998983,0.000024311848,0.00002002808,0.0000077021405,0.000020034537,0.000029616749],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000112263,0.00015841612,0.00023946713,0.00042535856,0.0002024554,0.00045388888,0.0001077519,0.00018174187,0.0003065162],"category_scores_gemma":[0.00023482014,0.00010852684,0.0001282106,0.00019604876,0.00036010257,0.00023632208,0.0001865453,0.00025282011,0.00005510404],"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":[0.00030311992,0.00012400538,0.011644679,0.000043455075,0.000017473183,0.0007338228,0.0001863511,0.018634321,0.9505268,0.00205806,0.00012902329,0.015598963],"study_design_scores_gemma":[0.0001613118,0.00093717774,0.31653473,0.000033902263,0.000045162877,0.0011706826,0.00035367487,0.36176786,0.31422445,0.0029730098,0.001664066,0.00013393255],"about_ca_topic_score_codex":0.0005024574,"about_ca_topic_score_gemma":0.00035263423,"teacher_disagreement_score":0.0005024574,"about_ca_system_score_codex":0.00014868047,"about_ca_system_score_gemma":0.00017652872,"threshold_uncertainty_score":0.0010787845},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.048590973,0.0006043612,0.84345984,0.0006887233,0.000412186,0.00036990762,0.017266935,0.009835211,0.07877188],"genre_scores_gemma":[0.5683527,0.0013099964,0.34721255,0.0003553586,0.00019990983,0.0012882424,0.0257805,0.0026586503,0.052842084],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997693,0.00004039282,0.000012946508,0.000040202245,0.00010541042,0.000031843745],"domain_scores_gemma":[0.99966216,0.00009991415,0.000042509462,0.0000394148,0.00013060102,0.000025373613],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003403844,0.0008705134,0.00069187244,0.0005041322,0.0005566945,0.0011599875,0.0017618388,0.0012592437,0.010993079],"category_scores_gemma":[0.0012868146,0.00045982024,0.0007554694,0.0005014773,0.00028094288,0.0010401807,0.00084652175,0.0010444477,0.003608189],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000051137904,0.000030091049,0.0011057887,0.00008265578,0.000019353238,0.00005062095,0.00003394296,0.95912313,0.0014767117,0.015488409,0.009466037,0.013072154],"study_design_scores_gemma":[0.000019791138,0.000013934873,0.00014884434,0.000010081195,0.0000055590717,0.000013403824,0.000005714221,0.9874878,0.0005226692,0.0020317337,0.009733376,0.0000071240347],"about_ca_topic_score_codex":0.016653784,"about_ca_topic_score_gemma":0.009592263,"teacher_disagreement_score":0.016653784,"about_ca_system_score_codex":0.000613348,"about_ca_system_score_gemma":0.0015043475,"threshold_uncertainty_score":0.03677559},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9949791,0.000032100532,0.0036084908,0.000058499543,0.00001268973,0.00001109441,0.000010428517,0.000056722798,0.0012308668],"genre_scores_gemma":[0.99933064,0.000009436846,0.00025665015,0.000004446433,0.0000022841284,0.0000018998678,0.0000034952948,0.000005602799,0.00038546126],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998902,0.0000308658,0.0000046202663,0.000015364198,0.000029911742,0.000028933368],"domain_scores_gemma":[0.99949265,0.00025970765,0.000042131174,0.00003120404,0.00007412821,0.000100158206],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018342918,0.0002598862,0.0005581367,0.00031403173,0.000555655,0.00037996875,0.00037087064,0.0005802822,0.0022768225],"category_scores_gemma":[0.0009107127,0.00028728787,0.0002714759,0.00021802679,0.0008486515,0.0004538718,0.00078906445,0.0006428163,0.00019744069],"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":[0.0023515958,0.0005276158,0.014017715,0.00009178079,0.000056713274,0.0075230864,0.00085616077,0.3164722,0.63628757,0.0045801797,0.00072317943,0.016512154],"study_design_scores_gemma":[0.00023128699,0.0010187145,0.02375273,0.000011911284,0.00004520175,0.00084858626,0.0004902123,0.9107021,0.060502972,0.0015436929,0.00078120804,0.00007150322],"about_ca_topic_score_codex":0.0026215757,"about_ca_topic_score_gemma":0.001287471,"teacher_disagreement_score":0.0026215757,"about_ca_system_score_codex":0.0002943551,"about_ca_system_score_gemma":0.0002599293,"threshold_uncertainty_score":0.0076166987},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8944742,0.00012610941,0.0899278,0.00015954273,0.000064977816,0.00012107023,0.00062550115,0.0009510387,0.013549898],"genre_scores_gemma":[0.98416686,0.0000758375,0.012219428,0.000011793708,0.000007720007,0.000035780933,0.00028746796,0.000045783454,0.0031493902],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998596,0.000024139621,0.000008124888,0.000027151105,0.000056480098,0.00002452884],"domain_scores_gemma":[0.99954176,0.00024073324,0.00003736403,0.000023175311,0.00012706297,0.000029962033],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003192529,0.00053475937,0.00038345845,0.0005181415,0.00061424036,0.0006758538,0.00041865,0.000728504,0.0015371147],"category_scores_gemma":[0.0009808457,0.00031543057,0.00051355467,0.00027569963,0.00041201993,0.00041371406,0.0003453676,0.00052835094,0.00040256063],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000041264033,0.000044307097,0.0030948129,0.000016508358,0.000005184065,0.00004418734,0.000028481592,0.988145,0.0034114593,0.00038121434,0.00018259668,0.0046050283],"study_design_scores_gemma":[0.0000038864396,0.000012893921,0.0006727864,0.0000016861769,0.0000013204407,0.000004548364,0.0000064754995,0.9981804,0.0009884412,0.000049310078,0.00007507081,0.000003157177],"about_ca_topic_score_codex":0.04802399,"about_ca_topic_score_gemma":0.013285759,"teacher_disagreement_score":0.04802399,"about_ca_system_score_codex":0.0011425267,"about_ca_system_score_gemma":0.0012425836,"threshold_uncertainty_score":0.095488966},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9922821,0.0001309616,0.0063019465,0.00003201056,0.00001729921,0.000030999137,0.00014231673,0.0000834479,0.0009789567],"genre_scores_gemma":[0.99151844,0.00024263293,0.006935148,0.000020489255,0.000015020109,0.000056043064,0.0001302598,0.000027054999,0.001054871],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99960965,0.000057723828,0.000026834166,0.00008626093,0.00015023742,0.00006927243],"domain_scores_gemma":[0.99930966,0.0002991524,0.000104403436,0.000077851095,0.00016057615,0.000048403148],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005675304,0.00035147832,0.00058280915,0.00045384027,0.0007262782,0.00048186438,0.00024458423,0.00036074215,0.0012538227],"category_scores_gemma":[0.000792904,0.0002215188,0.00020147004,0.00071594986,0.00045911552,0.0003664435,0.0005148096,0.00045246506,0.0003468908],"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":[0.00029664254,0.00019176406,0.0021760284,0.00010574847,0.000006979758,0.00015142756,0.00045987946,0.0011462583,0.9872846,0.00032431015,0.00012012174,0.0077363024],"study_design_scores_gemma":[0.00011693674,0.0035750358,0.019344287,0.000038402442,0.000040151874,0.00024572818,0.0005523814,0.022714583,0.95015806,0.00023619755,0.0028962777,0.000082100334],"about_ca_topic_score_codex":0.0008742319,"about_ca_topic_score_gemma":0.00080465496,"teacher_disagreement_score":0.0012538227,"about_ca_system_score_codex":0.0002260877,"about_ca_system_score_gemma":0.00023328926,"threshold_uncertainty_score":0.0041944385},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9844674,0.0001343307,0.014224492,0.000022980372,0.000015072893,0.000025418523,0.00014614341,0.0001148012,0.0008494832],"genre_scores_gemma":[0.9947653,0.00006817751,0.004647563,0.000008336909,0.0000106544385,0.000015103824,0.00020655085,0.00001424258,0.00026398158],"study_design_codex":"observational","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9995771,0.00009690643,0.00002081612,0.00007055286,0.00019164578,0.000042928747],"domain_scores_gemma":[0.9994715,0.00024878513,0.00006849098,0.000028827022,0.00015195765,0.000030490757],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005020478,0.00028191903,0.00025234284,0.0011184978,0.00021863257,0.0003753942,0.00021764546,0.0003636535,0.0002519147],"category_scores_gemma":[0.0029061588,0.00018284263,0.00015138942,0.0006047376,0.00016518353,0.0003340785,0.00031170988,0.00018488872,0.00020229469],"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":[0.0015927049,0.0003050973,0.4538021,0.0002957588,0.00010850158,0.000940692,0.00075262366,0.041975494,0.32565522,0.00093741703,0.0008377183,0.1727967],"study_design_scores_gemma":[0.000050542676,0.00032023992,0.7046852,0.000058835984,0.00009582756,0.00079496554,0.00022545061,0.2101695,0.08193872,0.00044188177,0.0011786334,0.000040106665],"about_ca_topic_score_codex":0.0040209177,"about_ca_topic_score_gemma":0.0060192524,"teacher_disagreement_score":0.0040209177,"about_ca_system_score_codex":0.00025010496,"about_ca_system_score_gemma":0.00019394336,"threshold_uncertainty_score":0.007995069},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8452162,0.0002538773,0.14512567,0.0001290067,0.0000653652,0.00004445361,0.00014719758,0.0007739023,0.00824425],"genre_scores_gemma":[0.9916855,0.00006472761,0.0073831673,0.0000148626805,0.0000070306364,0.0000108509585,0.00006147686,0.000057763235,0.0007146661],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999589,0.00012157149,0.000017374226,0.00007716493,0.00013829349,0.000056480163],"domain_scores_gemma":[0.99909496,0.00049401994,0.000101039856,0.00009356242,0.00016741488,0.000049009064],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00068067113,0.0008529791,0.0005992051,0.00039236146,0.00032430812,0.00051321334,0.0006287064,0.00078338495,0.00076945167],"category_scores_gemma":[0.0020015475,0.00038932005,0.0004853776,0.00017742628,0.0004122743,0.0004984893,0.0004204337,0.00048261735,0.00026164844],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00011708914,0.000062723404,0.003637338,0.00003350443,0.000012484649,0.00015579975,0.000053345437,0.9645694,0.02134582,0.00068552874,0.0001431919,0.009183844],"study_design_scores_gemma":[0.0000038466546,0.00004204504,0.0008108326,0.0000063924003,0.0000044626227,0.000012895847,0.0000067089723,0.9934876,0.00542701,0.000072252595,0.000119846256,0.000006015146],"about_ca_topic_score_codex":0.008813949,"about_ca_topic_score_gemma":0.006450305,"teacher_disagreement_score":0.008813949,"about_ca_system_score_codex":0.00040819586,"about_ca_system_score_gemma":0.0007061182,"threshold_uncertainty_score":0.017525315},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.954268,0.00034432707,0.041723836,0.000046298155,0.000024036766,0.0000128586435,0.000039471663,0.00013541606,0.0034059347],"genre_scores_gemma":[0.9967805,0.00011194156,0.0026216134,0.0000073936126,0.000010976631,0.0000039777246,0.000040311184,0.000010874127,0.00041241743],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99991,0.000010550848,0.0000026400728,0.000013769393,0.00004530065,0.000017771164],"domain_scores_gemma":[0.9997043,0.00014568654,0.000029895089,0.000021881227,0.00006963854,0.000028643368],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016172737,0.00029314664,0.00019382965,0.00032951374,0.00022850036,0.00026824616,0.0001994123,0.00020943572,0.00049111084],"category_scores_gemma":[0.0006789494,0.00010471948,0.00021790688,0.00030993248,0.00042304833,0.00026583663,0.0002757304,0.00021126805,0.00007448779],"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":[0.00097147166,0.00019651187,0.013796153,0.00019407136,0.000063562555,0.001372296,0.0004198887,0.3846975,0.5122762,0.019735944,0.00092576194,0.06535065],"study_design_scores_gemma":[0.000048601833,0.00014675531,0.010845036,0.000010702217,0.0000159313,0.000324509,0.00007284666,0.9293963,0.054790583,0.003659425,0.0006592684,0.000030028508],"about_ca_topic_score_codex":0.0013701081,"about_ca_topic_score_gemma":0.00069244695,"teacher_disagreement_score":0.0013701081,"about_ca_system_score_codex":0.00033145933,"about_ca_system_score_gemma":0.00017782126,"threshold_uncertainty_score":0.00272429},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6286487,0.000491771,0.3564336,0.00024267103,0.000117753414,0.00020633636,0.0007794758,0.0018369332,0.011242826],"genre_scores_gemma":[0.9780757,0.000110177614,0.020857811,0.000019170444,0.0000145551485,0.000043352484,0.00030201697,0.00006698772,0.0005102399],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998388,0.00002364389,0.000012605528,0.00003540173,0.000057370693,0.0000321179],"domain_scores_gemma":[0.99945635,0.00024444712,0.00005394254,0.00005068882,0.00013391481,0.0000606752],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004819124,0.000846333,0.0005315712,0.0009270785,0.00046406174,0.0011042751,0.00045525623,0.00069317827,0.00077977875],"category_scores_gemma":[0.0020826892,0.00032075023,0.00064305286,0.0002808339,0.00039360806,0.0006311433,0.0004480716,0.00070611516,0.00036344366],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00017347482,0.00017444235,0.043152362,0.00006624641,0.000035277448,0.00030057464,0.00011144152,0.8729488,0.038738158,0.0047170524,0.0011203977,0.0384617],"study_design_scores_gemma":[0.000003412557,0.00000919925,0.0028690787,0.0000041762387,0.0000019829386,0.000007097899,0.000006102547,0.99522144,0.0015965805,0.00016537259,0.00010965772,0.0000059315803],"about_ca_topic_score_codex":0.010047658,"about_ca_topic_score_gemma":0.0059110047,"teacher_disagreement_score":0.010047658,"about_ca_system_score_codex":0.00085398013,"about_ca_system_score_gemma":0.0007836441,"threshold_uncertainty_score":0.019978344},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.14240804,0.00022438189,0.8535898,0.000072919676,0.00019425896,0.00011414919,0.000116903975,0.0015701024,0.0017094053],"genre_scores_gemma":[0.5050691,0.00038700248,0.4891034,0.00009487164,0.00009111908,0.00019650917,0.00037489305,0.00024410058,0.0044390433],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9994573,0.000050052673,0.000020167563,0.00009962178,0.0003326114,0.000040202118],"domain_scores_gemma":[0.9989974,0.00032306323,0.0001116052,0.00013469014,0.00040002403,0.000033229495],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00047874107,0.0005627794,0.0005018507,0.0007431248,0.000396849,0.0005100379,0.0005465827,0.00061069796,0.000647344],"category_scores_gemma":[0.0024395124,0.00032144636,0.00040013075,0.00059766223,0.0003023092,0.00025361852,0.00035914467,0.000644655,0.0007642644],"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":[0.00031645107,0.00015428934,0.0029084191,0.00017870979,0.00006689134,0.0001366839,0.00015602009,0.0052751806,0.77397114,0.0005139926,0.00058125326,0.21574098],"study_design_scores_gemma":[0.00006478376,0.0005468636,0.035057195,0.000028523635,0.00018730845,0.0010710945,0.00008499974,0.17298995,0.78170687,0.00046203614,0.0076778783,0.00012259319],"about_ca_topic_score_codex":0.0014591292,"about_ca_topic_score_gemma":0.002370574,"teacher_disagreement_score":0.0014591292,"about_ca_system_score_codex":0.00017994441,"about_ca_system_score_gemma":0.0005538553,"threshold_uncertainty_score":0.002901256},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.93528265,0.00021876034,0.058055058,0.0001580489,0.00008340721,0.000055133747,0.000098158016,0.00019829409,0.005850399],"genre_scores_gemma":[0.98102427,0.000087405744,0.017314842,0.000018803463,0.00000780035,0.000043298496,0.000045996687,0.000021184836,0.0014363668],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99991596,0.000018897457,0.000004331737,0.0000077093455,0.00003617575,0.000016984313],"domain_scores_gemma":[0.99969864,0.00018232942,0.00003553615,0.000015744474,0.000037549988,0.000030217729],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00027058026,0.00027852232,0.00039263009,0.00024330126,0.0003869335,0.00050163764,0.00042089308,0.0004900979,0.0009277835],"category_scores_gemma":[0.0007918284,0.00022330819,0.00030529246,0.00020252394,0.0004326783,0.00031838816,0.0003233172,0.00032851033,0.00012275895],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000086636675,0.00005804614,0.0017541051,0.00003251705,0.000009485075,0.00009494528,0.000047872385,0.98096806,0.012946728,0.0010328519,0.00008578557,0.0028829433],"study_design_scores_gemma":[0.0000064707515,0.000017533155,0.00017571797,0.0000014374148,0.0000014162558,0.000005678908,0.0000069905946,0.9985335,0.0011080565,0.000064003776,0.000076908975,0.0000022087397],"about_ca_topic_score_codex":0.0068729343,"about_ca_topic_score_gemma":0.004396373,"teacher_disagreement_score":0.0068729343,"about_ca_system_score_codex":0.00045142876,"about_ca_system_score_gemma":0.0008866878,"threshold_uncertainty_score":0.013665855},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99330115,0.00012608591,0.0048355823,0.000033387685,0.0000115235625,0.00002597685,0.000033707358,0.00006073108,0.0015719407],"genre_scores_gemma":[0.9983398,0.000054736327,0.0010984486,0.000010486237,0.0000042215734,0.000006449266,0.000039044044,0.000006159182,0.00044075615],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997223,0.00003189617,0.000009320198,0.000043196935,0.00010412491,0.00008916917],"domain_scores_gemma":[0.99969244,0.00009868005,0.00006079913,0.000021823116,0.000057930738,0.000068326175],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00027535472,0.00035067773,0.0006678635,0.00034664088,0.0005751295,0.00076687685,0.00049293425,0.00083826215,0.0010636628],"category_scores_gemma":[0.00058267865,0.00025552922,0.0004150221,0.00030282122,0.0006737608,0.0003686162,0.0005972972,0.00053411676,0.00015975906],"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":[0.0009301909,0.0004241239,0.01295516,0.00016178851,0.00009492525,0.0058503454,0.00050698477,0.1264214,0.8392903,0.0043498618,0.00042717974,0.008587727],"study_design_scores_gemma":[0.00019661196,0.0019084302,0.05099893,0.000027582244,0.00008186757,0.001312979,0.00063896494,0.7650222,0.17720586,0.0010558165,0.0014173461,0.00013330304],"about_ca_topic_score_codex":0.002464214,"about_ca_topic_score_gemma":0.00088137935,"teacher_disagreement_score":0.002464214,"about_ca_system_score_codex":0.00044107673,"about_ca_system_score_gemma":0.0004405418,"threshold_uncertainty_score":0.0048998},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9907465,0.00021719902,0.008434697,0.000026337875,0.000024801724,0.000024726436,0.000047109774,0.00006103642,0.00041764555],"genre_scores_gemma":[0.9922306,0.00017719163,0.0072868112,0.000011427033,0.0000111980435,0.000021437889,0.000056353638,0.000011224966,0.00019374161],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99962604,0.000050441875,0.00002364657,0.000055389257,0.00019282059,0.000051763996],"domain_scores_gemma":[0.9986934,0.000694543,0.00023501959,0.000121637946,0.00017904192,0.000076326614],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005321453,0.0004452339,0.00060756324,0.0002705604,0.0004307184,0.0002666639,0.00047223977,0.00038736107,0.0005450615],"category_scores_gemma":[0.0018052377,0.00017184546,0.0002530987,0.00030620513,0.0008124293,0.00030238874,0.00037582873,0.0003870761,0.00008012123],"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":[0.00037227088,0.0002850603,0.004149633,0.00026651067,0.000015732643,0.00033338304,0.00032467366,0.013699248,0.9656623,0.0003592629,0.00012188524,0.014409966],"study_design_scores_gemma":[0.00010355853,0.003908795,0.046670746,0.000037924074,0.000070440656,0.0008088458,0.0004571117,0.14846896,0.7976129,0.0004075115,0.001347793,0.00010546698],"about_ca_topic_score_codex":0.00032511333,"about_ca_topic_score_gemma":0.00038636956,"teacher_disagreement_score":0.00060756324,"about_ca_system_score_codex":0.00014950288,"about_ca_system_score_gemma":0.00018565789,"threshold_uncertainty_score":0.002814293},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7582148,0.00035991945,0.23813401,0.00008333706,0.00003872788,0.00002594657,0.00007735754,0.00065970735,0.002406191],"genre_scores_gemma":[0.99305564,0.000096323514,0.006112121,0.000008236861,0.0000061279375,0.000015641552,0.000051173327,0.000022723103,0.00063198735],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998832,0.000028939456,0.0000045708857,0.000023793034,0.000039945477,0.000019676285],"domain_scores_gemma":[0.99974376,0.00013587775,0.00004483119,0.000009190157,0.00004483876,0.000021572383],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00026620107,0.0008104858,0.00035526213,0.00047242327,0.00028440513,0.0004386421,0.00032705723,0.0005492778,0.00028062833],"category_scores_gemma":[0.0006251992,0.0002480212,0.00040416795,0.00016716715,0.00041800315,0.0003105057,0.00026832035,0.00026598113,0.00010753952],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00005276158,0.00003502225,0.002582389,0.000032173244,0.000008893809,0.00006165577,0.000033359815,0.97833645,0.0134286685,0.0004001859,0.00009581316,0.0049326294],"study_design_scores_gemma":[0.0000015074118,0.000013732976,0.00044041706,0.0000012505276,0.0000015334574,0.0000037171994,0.0000037444252,0.99847215,0.0009814457,0.000050628092,0.000027742857,0.0000021028611],"about_ca_topic_score_codex":0.0089517515,"about_ca_topic_score_gemma":0.004857199,"teacher_disagreement_score":0.0089517515,"about_ca_system_score_codex":0.00036038968,"about_ca_system_score_gemma":0.0004553233,"threshold_uncertainty_score":0.017799318},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9948372,0.00011705768,0.004331909,0.000011562713,0.0000112606285,0.000012777999,0.000042213003,0.000043023872,0.0005930147],"genre_scores_gemma":[0.9971624,0.00009706782,0.002383708,0.00000676591,0.000005385546,0.000008038089,0.000057759775,0.000008091573,0.00027075087],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.99975103,0.000019444351,0.000011803801,0.00003549503,0.000117032956,0.00006524403],"domain_scores_gemma":[0.9996517,0.00012522304,0.000057804926,0.00003404031,0.00007669844,0.00005450541],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025849493,0.00024701774,0.0005119413,0.00030252023,0.00044186242,0.00055384106,0.0002026872,0.0002954257,0.00051244034],"category_scores_gemma":[0.0004460096,0.00020434319,0.00023912649,0.00022664886,0.0005873935,0.0003428954,0.0003501494,0.00041243818,0.00008998447],"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":[0.0002807996,0.00008827498,0.003959247,0.0000810736,0.000015310135,0.0005456533,0.0002697479,0.005815793,0.983371,0.0004094726,0.00008224759,0.005081335],"study_design_scores_gemma":[0.00008344653,0.0020167553,0.05393047,0.00002480806,0.00003908111,0.00061420014,0.0006216435,0.085598044,0.85531485,0.00044717177,0.0012128317,0.000096726675],"about_ca_topic_score_codex":0.00062516704,"about_ca_topic_score_gemma":0.0004597547,"teacher_disagreement_score":0.00062516704,"about_ca_system_score_codex":0.00014185243,"about_ca_system_score_gemma":0.00020925884,"threshold_uncertainty_score":0.0017143488},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9966001,0.00008463714,0.0028050125,0.0000079894635,0.000011152063,0.000015934242,0.000060461192,0.00004020722,0.00037455154],"genre_scores_gemma":[0.99709845,0.000089047244,0.0021426815,0.000007657725,0.000009052595,0.000015352718,0.00006734548,0.000017976023,0.0005525273],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99961615,0.00006517167,0.000021453146,0.00009501343,0.00014217409,0.000060069313],"domain_scores_gemma":[0.99915886,0.0004347065,0.000120156365,0.00009879948,0.00012763745,0.000059786882],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004140887,0.00040244532,0.00045908923,0.00028784142,0.00040740706,0.0003110835,0.00040222824,0.0004006105,0.0013815771],"category_scores_gemma":[0.0006866441,0.00019754501,0.0003308825,0.00024158428,0.0006161691,0.00032982207,0.0003578956,0.0005106615,0.0001679952],"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":[0.00066935964,0.00024156862,0.0025216732,0.00010325748,0.000012805757,0.00018083202,0.00024288932,0.0013036361,0.98965865,0.000081354614,0.000041425657,0.004942461],"study_design_scores_gemma":[0.00009998858,0.004619133,0.027236281,0.000014376106,0.000045217,0.00023847746,0.00031310762,0.008219713,0.9583758,0.00005635117,0.00074588734,0.00003565002],"about_ca_topic_score_codex":0.0003796724,"about_ca_topic_score_gemma":0.0003647957,"teacher_disagreement_score":0.0013815771,"about_ca_system_score_codex":0.00018337322,"about_ca_system_score_gemma":0.00014552817,"threshold_uncertainty_score":0.0046218038},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9961584,0.000119122466,0.0033332326,0.000007226338,0.0000061981564,0.000006304542,0.000011226398,0.00005678039,0.0003014826],"genre_scores_gemma":[0.9977404,0.000048946302,0.0020556091,0.0000057597235,0.0000023127927,0.0000033899635,0.000010096373,0.0000095382375,0.00012395413],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997781,0.00004239754,0.000015119889,0.000053867967,0.0000526002,0.000057915484],"domain_scores_gemma":[0.99913687,0.0003624216,0.00023346602,0.00008220453,0.00012144606,0.00006354643],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002797377,0.00037809234,0.00025842,0.0002010473,0.00014116481,0.00027702603,0.0002591733,0.000252703,0.0006266602],"category_scores_gemma":[0.0009010741,0.00024292161,0.00017643801,0.000077869394,0.000304769,0.0002658858,0.0003800651,0.00021111662,0.00014004223],"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":[0.0002169497,0.000017356677,0.0019394855,0.00007189616,0.0000054667316,0.00014509773,0.00005246679,0.002317352,0.98996407,0.000065675806,0.000020063257,0.005184174],"study_design_scores_gemma":[0.000020824296,0.0016568302,0.025644448,0.000014239655,0.000057919846,0.00027325982,0.00013282054,0.012966467,0.95850724,0.00005236121,0.000646231,0.000027328913],"about_ca_topic_score_codex":0.00022494035,"about_ca_topic_score_gemma":0.0003465885,"teacher_disagreement_score":0.0006266602,"about_ca_system_score_codex":0.000099646844,"about_ca_system_score_gemma":0.00010996095,"threshold_uncertainty_score":0.002096355},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9788643,0.00034100024,0.009620524,0.00043290952,0.00016346927,0.00006882665,0.00032847008,0.0005023318,0.009678122],"genre_scores_gemma":[0.9945492,0.00008921467,0.00421791,0.00007625399,0.000019858266,0.000018907118,0.00015384688,0.00013267781,0.00074214186],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994572,0.00023056923,0.000041900894,0.00006851725,0.00009163839,0.000110118235],"domain_scores_gemma":[0.99020946,0.008071532,0.00034903118,0.00025589895,0.00073328754,0.0003807649],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0011927702,0.0007500413,0.00088283594,0.00075689616,0.0012138531,0.0014790525,0.0010576859,0.0019002245,0.0032001173],"category_scores_gemma":[0.00820024,0.0006450235,0.00066648,0.00057385175,0.0011404831,0.001179683,0.00074386696,0.0014962943,0.0002751933],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0009626614,0.00054868736,0.0059555364,0.00014869953,0.0000660136,0.00022243096,0.00019623456,0.97652644,0.007703565,0.0007260925,0.0006177916,0.0063259564],"study_design_scores_gemma":[0.000054016342,0.0001846766,0.0010682011,0.000012385181,0.000025638767,0.000009463131,0.000063934014,0.994584,0.0037470234,0.00009424949,0.00014375072,0.0000126611],"about_ca_topic_score_codex":0.023396809,"about_ca_topic_score_gemma":0.014584065,"teacher_disagreement_score":0.023396809,"about_ca_system_score_codex":0.0006260316,"about_ca_system_score_gemma":0.0008332657,"threshold_uncertainty_score":0.046521246},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99536586,0.000120540026,0.0037688436,0.000020527294,0.000014431547,0.000017462538,0.00006617462,0.00005029794,0.0005758562],"genre_scores_gemma":[0.99432087,0.0001164568,0.0049538487,0.0000147946,0.000012345411,0.000024368315,0.000086256114,0.000017934104,0.00045313913],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9996449,0.000030741387,0.000015502339,0.00010574183,0.0001349077,0.00006829581],"domain_scores_gemma":[0.9984762,0.0007664051,0.00022380814,0.00008351559,0.00037560784,0.0000744662],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006344664,0.00033103584,0.00032292103,0.0003334345,0.0005628352,0.0004312075,0.0003822316,0.00041358452,0.00089164614],"category_scores_gemma":[0.0013722903,0.0001894049,0.00018139301,0.00035393558,0.0006261524,0.0003595205,0.00029637924,0.0006873708,0.000071888295],"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":[0.00020030653,0.00008321488,0.001021955,0.00003374546,0.000003419882,0.00007233269,0.00014152101,0.0008843537,0.994642,0.00019957054,0.00004723262,0.0026702827],"study_design_scores_gemma":[0.00002431149,0.0011038581,0.0067607835,0.0000066421712,0.000013368457,0.00008454429,0.00006977329,0.012925702,0.9784703,0.00006401609,0.0004560342,0.000020663574],"about_ca_topic_score_codex":0.0013535202,"about_ca_topic_score_gemma":0.0009696647,"teacher_disagreement_score":0.0013535202,"about_ca_system_score_codex":0.00052955846,"about_ca_system_score_gemma":0.00031804654,"threshold_uncertainty_score":0.0038422346},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98449475,0.00017996361,0.0139443595,0.000019956598,0.000023056637,0.00004807648,0.00008592312,0.00010540119,0.0010986334],"genre_scores_gemma":[0.98000425,0.00020478168,0.01863152,0.000010095609,0.000010884417,0.000052783624,0.00012373229,0.000018009147,0.00094391475],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997235,0.000035027253,0.000024050492,0.00004810908,0.00011784911,0.000051461444],"domain_scores_gemma":[0.9993068,0.0002664487,0.00012256329,0.000093794464,0.0001428356,0.000067498695],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00071855995,0.0003934227,0.00041416605,0.00035061018,0.0005234131,0.00036977994,0.00038159062,0.00034460373,0.0012778589],"category_scores_gemma":[0.0009211488,0.00017924438,0.00021848857,0.00042925062,0.0006814198,0.0003376427,0.0003689723,0.0003768115,0.00015250941],"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":[0.0004990555,0.00033462577,0.0048284163,0.00017903294,0.000012031763,0.0005172717,0.00047107582,0.015211301,0.96521753,0.0010967758,0.00015977185,0.011473101],"study_design_scores_gemma":[0.000099690784,0.003160945,0.018917924,0.000034746008,0.000044758803,0.00036306446,0.00030556758,0.11658651,0.8577362,0.0004606623,0.002199093,0.00009079365],"about_ca_topic_score_codex":0.0007026912,"about_ca_topic_score_gemma":0.0005303472,"teacher_disagreement_score":0.0012778589,"about_ca_system_score_codex":0.0001825484,"about_ca_system_score_gemma":0.00032336186,"threshold_uncertainty_score":0.0042749047},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9849814,0.00010166502,0.011802901,0.000021586236,0.000007268779,0.0000065396403,0.000020616068,0.000069866415,0.0029882395],"genre_scores_gemma":[0.99849844,0.000030274881,0.0010034665,0.0000029479304,0.0000023141747,0.0000030310891,0.000013385072,0.000009868065,0.0004364109],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99988234,0.000019623127,0.0000040776695,0.00002553175,0.00004845856,0.000019884908],"domain_scores_gemma":[0.99951947,0.00019206195,0.00010283797,0.000045229008,0.000094844356,0.000045622757],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023826235,0.0002329752,0.00017520631,0.0002649859,0.00015009566,0.0002762261,0.0001922163,0.00020537883,0.0014665422],"category_scores_gemma":[0.0007995687,0.00020557025,0.00011072304,0.00011779602,0.00045106933,0.00024479488,0.0003055251,0.00029103248,0.0002125541],"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":[0.00025256895,0.000040309103,0.0059882607,0.0000834884,0.000013437783,0.0003110935,0.0005606689,0.021030644,0.94864064,0.005798962,0.00020341355,0.017076578],"study_design_scores_gemma":[0.000058389796,0.0005008919,0.031357314,0.000034899174,0.000023544388,0.00064656115,0.00030997003,0.64766324,0.31566018,0.0019799327,0.0016889864,0.00007612045],"about_ca_topic_score_codex":0.00022046275,"about_ca_topic_score_gemma":0.00015576908,"teacher_disagreement_score":0.0014665422,"about_ca_system_score_codex":0.00012483275,"about_ca_system_score_gemma":0.00009656098,"threshold_uncertainty_score":0.0049060583},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8511704,0.0002873571,0.14681393,0.000062221894,0.000052921176,0.000055559005,0.00015639195,0.00046114734,0.00094004103],"genre_scores_gemma":[0.82129115,0.00019682103,0.17712788,0.000038432863,0.0000253221,0.00006694359,0.00010385141,0.000031652387,0.0011178919],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99955887,0.000081366066,0.000023285547,0.00014179008,0.00015327305,0.00004154179],"domain_scores_gemma":[0.9992804,0.00018694508,0.0002149657,0.00010630893,0.00016959984,0.00004169928],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00040064068,0.00055511313,0.00037680453,0.0003747581,0.0001198638,0.0003243483,0.00052874745,0.0005127325,0.0008786651],"category_scores_gemma":[0.0011317353,0.00035563522,0.00017636149,0.00032628208,0.0003343041,0.00058416673,0.0005282354,0.00020797072,0.00031262715],"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":[0.00013008331,0.000017770628,0.0009369407,0.000052138952,0.000006895485,0.000036416768,0.000065769105,0.0007830116,0.98751104,0.00008731957,0.000044114968,0.010328536],"study_design_scores_gemma":[0.000040517614,0.0008152582,0.011033621,0.000014423171,0.000035046585,0.00045033442,0.00013418146,0.024024768,0.96175724,0.00014864848,0.0014836531,0.0000624125],"about_ca_topic_score_codex":0.0002471405,"about_ca_topic_score_gemma":0.00040086076,"teacher_disagreement_score":0.0008786651,"about_ca_system_score_codex":0.0001294163,"about_ca_system_score_gemma":0.00013729677,"threshold_uncertainty_score":0.002939403},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9840866,0.00007387186,0.010041281,0.00010990596,0.000038961498,0.000012311766,0.000041550033,0.00012285699,0.005472588],"genre_scores_gemma":[0.99791855,0.000016381082,0.0008592628,0.000013323151,0.000011952286,0.0000031862292,0.000027202148,0.000017952178,0.0011322625],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99991405,0.000011487943,0.0000028441434,0.000020103735,0.000032157215,0.000019345247],"domain_scores_gemma":[0.999848,0.00004476362,0.000022524517,0.0000134844995,0.000026195263,0.0000449699],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000106609565,0.00027355392,0.00034374703,0.00028575948,0.0002775693,0.00047245814,0.000366635,0.0005812628,0.0017295667],"category_scores_gemma":[0.0004999895,0.0002063542,0.00021958353,0.00017848187,0.0007357873,0.00039340003,0.0005658088,0.0004441407,0.00014808621],"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":[0.0019749696,0.0004204458,0.011877176,0.00022450727,0.00019876474,0.005884657,0.0013928717,0.19784535,0.7200699,0.016424507,0.0020708907,0.04161596],"study_design_scores_gemma":[0.0001385603,0.00045504147,0.03761476,0.000015506914,0.000056315417,0.000914378,0.00042973208,0.92651546,0.029227812,0.0029954195,0.0015444154,0.000092596754],"about_ca_topic_score_codex":0.00044618285,"about_ca_topic_score_gemma":0.0002614133,"teacher_disagreement_score":0.0017295667,"about_ca_system_score_codex":0.0001994163,"about_ca_system_score_gemma":0.00014955949,"threshold_uncertainty_score":0.0057860017},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99670285,0.00006057998,0.002591949,0.000010725275,0.0000068009317,0.000009259327,0.000078230296,0.00007618727,0.0004635292],"genre_scores_gemma":[0.9985001,0.000026000667,0.001065138,0.000007355132,0.0000032654389,0.0000031696784,0.00013151483,0.000009348384,0.00025428212],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999081,0.0000069081734,0.0000055694954,0.000016989283,0.00004569637,0.000016766198],"domain_scores_gemma":[0.99928313,0.00030373855,0.00010556484,0.000031456606,0.00013109396,0.00014514462],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001517506,0.00016580844,0.00026392663,0.0005147434,0.00022865205,0.00045023917,0.00015452832,0.00028363283,0.00095036766],"category_scores_gemma":[0.00064338447,0.00010888353,0.00018456235,0.00043628615,0.00025888017,0.0001858148,0.00019828304,0.0002415253,0.00010564353],"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":[0.0015795669,0.00022338568,0.073855266,0.00011169046,0.000054578504,0.0061647077,0.0007057739,0.029157087,0.8653857,0.000661562,0.00037339277,0.02172726],"study_design_scores_gemma":[0.000100321275,0.0024749974,0.72313035,0.000033829976,0.000074238415,0.0043768706,0.0010641938,0.1756724,0.09022928,0.0005743518,0.002088821,0.00018032358],"about_ca_topic_score_codex":0.0010306053,"about_ca_topic_score_gemma":0.00077523023,"teacher_disagreement_score":0.0010306053,"about_ca_system_score_codex":0.00014632926,"about_ca_system_score_gemma":0.00014138587,"threshold_uncertainty_score":0.0031793118},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97076076,0.00010865887,0.026646154,0.00007144218,0.000045197114,0.000015434256,0.000015036228,0.00012086704,0.0022163554],"genre_scores_gemma":[0.99596316,0.000027799475,0.00313472,0.000008837043,0.00000700017,0.000007766289,0.000004711499,0.000012959088,0.0008330785],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998634,0.00003330013,0.0000048261563,0.000029184162,0.000038164737,0.000031231873],"domain_scores_gemma":[0.99954337,0.00023641132,0.00010212988,0.000035955047,0.00004628684,0.00003583113],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00027749498,0.0002502736,0.00024416484,0.0000936186,0.00017273834,0.00026824232,0.00054596935,0.00026915947,0.0012818567],"category_scores_gemma":[0.00047397785,0.00018323811,0.00013894899,0.00005081282,0.00046035045,0.00030526394,0.00031378362,0.00029659152,0.00021285813],"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":[0.00036860356,0.000059654754,0.00012977637,0.000047760088,0.0000048831944,0.000028598379,0.000054971475,0.0040513715,0.9908494,0.0009857512,0.000054637236,0.0033646217],"study_design_scores_gemma":[0.00014404925,0.0011209862,0.0009519454,0.000012685434,0.00002192848,0.000033709537,0.00003543567,0.1277043,0.86864424,0.00026386938,0.0010475924,0.000019204972],"about_ca_topic_score_codex":0.0002507183,"about_ca_topic_score_gemma":0.00032445966,"teacher_disagreement_score":0.0012818567,"about_ca_system_score_codex":0.00021884676,"about_ca_system_score_gemma":0.00016751963,"threshold_uncertainty_score":0.004288256},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98933196,0.000043994205,0.009967524,0.000024322686,0.000006750875,0.000005531537,0.0000068081713,0.000049171707,0.00056402746],"genre_scores_gemma":[0.99793637,0.000017164424,0.0017751206,0.000005267962,0.0000020305156,0.000006331371,0.000003657836,0.000003418774,0.000250702],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99994695,0.000011106981,0.0000017066488,0.000011856878,0.000016665714,0.000011729575],"domain_scores_gemma":[0.99974805,0.00013294606,0.0000428941,0.00001668078,0.000025791163,0.00003362913],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017128354,0.00014019507,0.00017766177,0.0000722252,0.00014031424,0.00013870093,0.00016257093,0.00017399318,0.000519707],"category_scores_gemma":[0.00034095213,0.00008063239,0.000095704956,0.000033605123,0.00036364052,0.00010143339,0.00022555824,0.00014634641,0.00007774697],"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":[0.00016109926,0.000021765829,0.0003963187,0.00002315478,0.0000024096103,0.00010139282,0.00009208768,0.0049288566,0.9895391,0.00029944273,0.000030258365,0.0044040536],"study_design_scores_gemma":[0.00013564489,0.0015854058,0.013758014,0.00002990769,0.000030124556,0.0002577495,0.00016434585,0.34205693,0.6391703,0.00095148245,0.0018170144,0.000043126543],"about_ca_topic_score_codex":0.00045461048,"about_ca_topic_score_gemma":0.0003805582,"teacher_disagreement_score":0.000519707,"about_ca_system_score_codex":0.000121360994,"about_ca_system_score_gemma":0.00011620698,"threshold_uncertainty_score":0.0017385483},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9378016,0.00021677624,0.05230542,0.00019862612,0.000047693276,0.000053275555,0.00016667844,0.00025638862,0.008953531],"genre_scores_gemma":[0.98613095,0.00005621832,0.01218908,0.00001762066,0.0000062201457,0.00006156024,0.000063196625,0.000022870214,0.0014523079],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99985135,0.000040502335,0.000006909679,0.000017550503,0.000043389096,0.000040276],"domain_scores_gemma":[0.9992687,0.00041656205,0.00009082924,0.00004475074,0.000119734636,0.00005950947],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00045209643,0.00037453594,0.000677805,0.00038078352,0.0005930089,0.0005937786,0.00072223874,0.0010300748,0.0011835339],"category_scores_gemma":[0.0015941641,0.00032953324,0.0004562165,0.0003794294,0.00092203036,0.000378839,0.0005921007,0.00051741843,0.00011241029],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000055197183,0.000030666888,0.0010458286,0.000033255146,0.0000102433305,0.000087142405,0.0000692995,0.9916289,0.0035267526,0.0019947258,0.000120896664,0.0013971502],"study_design_scores_gemma":[0.000009179596,0.000015595955,0.00015796894,0.0000028663296,0.0000018578777,0.000006223695,0.000009229095,0.9990522,0.00047724397,0.00017476549,0.00008961809,0.0000032594455],"about_ca_topic_score_codex":0.0075518033,"about_ca_topic_score_gemma":0.0029768026,"teacher_disagreement_score":0.0075518033,"about_ca_system_score_codex":0.00072676246,"about_ca_system_score_gemma":0.0008360596,"threshold_uncertainty_score":0.015015662},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9959204,0.000035720877,0.0027311777,0.000025923826,0.000023265795,0.000010264689,0.00011495331,0.000053184678,0.0010849959],"genre_scores_gemma":[0.9983089,0.000028088694,0.0012438789,0.000012115236,0.000010114533,0.000007029792,0.00007994204,0.000012126298,0.00029771752],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.99973744,0.000033090808,0.000012359154,0.00005163678,0.000112262926,0.00005318271],"domain_scores_gemma":[0.9994319,0.00017641162,0.00006147802,0.00006342205,0.00019108508,0.00007562633],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023788803,0.00020775113,0.00028843372,0.00039083607,0.0005699562,0.00058447634,0.00038406265,0.0004648341,0.0009167145],"category_scores_gemma":[0.000870542,0.00022873314,0.00015959768,0.00045773198,0.00058617454,0.0005978511,0.00032532105,0.0004949447,0.00014396112],"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":[0.0019431746,0.0003367649,0.005137685,0.000035107776,0.000016574315,0.00025247913,0.00032686853,0.003229281,0.979529,0.0006297702,0.00023644959,0.0083268965],"study_design_scores_gemma":[0.0005784258,0.0031652802,0.09395579,0.000017460252,0.00008260072,0.0006016421,0.0006907324,0.09537595,0.8029435,0.00091137766,0.0015475707,0.00012964629],"about_ca_topic_score_codex":0.001578558,"about_ca_topic_score_gemma":0.0015916176,"teacher_disagreement_score":0.001578558,"about_ca_system_score_codex":0.0002995258,"about_ca_system_score_gemma":0.00026225534,"threshold_uncertainty_score":0.0031387806},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99340516,0.000032246153,0.005846396,0.000011559509,0.000007667128,0.0000075875946,0.000023664372,0.000039019636,0.00062667875],"genre_scores_gemma":[0.9988544,0.000015379637,0.0008343125,0.000003406258,0.0000039867386,0.0000030462095,0.000026868212,0.000004654236,0.00025415458],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999186,0.0000125680135,0.0000035924643,0.000012762218,0.000034862373,0.000017666498],"domain_scores_gemma":[0.99976844,0.000095703814,0.000034027275,0.00001793327,0.000057168563,0.000026660064],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001453508,0.00014695933,0.00016700034,0.00054492644,0.00018890982,0.00019808843,0.00012007177,0.0002069088,0.00081954076],"category_scores_gemma":[0.00050287566,0.000066881184,0.00010994239,0.00016546318,0.00028606015,0.00012911271,0.00013813154,0.00014028978,0.000069167334],"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":[0.00073159975,0.00020227073,0.015048935,0.000112206755,0.000027732467,0.0006903891,0.00040449615,0.020382982,0.9185708,0.0010152883,0.00024503068,0.04256838],"study_design_scores_gemma":[0.00008296919,0.0024664071,0.24861172,0.000045374138,0.00005589509,0.0009557035,0.00057617854,0.45109794,0.29272544,0.0008272288,0.0024652372,0.000089806534],"about_ca_topic_score_codex":0.0005899061,"about_ca_topic_score_gemma":0.00039892018,"teacher_disagreement_score":0.00081954076,"about_ca_system_score_codex":0.00010255438,"about_ca_system_score_gemma":0.000073314804,"threshold_uncertainty_score":0.0027416348},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9741166,0.000109551474,0.023305513,0.00011241969,0.0000996616,0.000027358657,0.000033400607,0.0001241916,0.0020713035],"genre_scores_gemma":[0.99502486,0.000037128237,0.0035278033,0.000012439273,0.000015884767,0.00000739576,0.000012383417,0.000010610083,0.001351453],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997216,0.00004027335,0.000021104432,0.00006848735,0.00010045573,0.00004806107],"domain_scores_gemma":[0.9990025,0.0005636217,0.000105518084,0.0001182123,0.00013578619,0.000074411226],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00045783128,0.00038483777,0.0004981395,0.00028241024,0.0005826051,0.00082567084,0.00052841037,0.00044567615,0.0015767382],"category_scores_gemma":[0.0010073277,0.000199445,0.00025946085,0.0001430131,0.00079478644,0.00060071325,0.00033957037,0.00048055296,0.00008635591],"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":[0.0016629256,0.00030372062,0.0005190547,0.000073263436,0.000015060339,0.00018829815,0.00016819066,0.027603345,0.9455622,0.0030042892,0.00015692155,0.020742672],"study_design_scores_gemma":[0.0002836672,0.002762993,0.0029499736,0.000009961298,0.000037737624,0.0000976828,0.00006555268,0.4358542,0.5553356,0.0016061665,0.00094031525,0.00005621362],"about_ca_topic_score_codex":0.0009629292,"about_ca_topic_score_gemma":0.0005113249,"teacher_disagreement_score":0.0015767382,"about_ca_system_score_codex":0.00027729556,"about_ca_system_score_gemma":0.00029329312,"threshold_uncertainty_score":0.0052747726},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.96305084,0.00049265585,0.03248819,0.00013542415,0.000035002107,0.000047074842,0.00013516648,0.00013314444,0.003482504],"genre_scores_gemma":[0.9662,0.00041595666,0.030520897,0.00006056158,0.000035438527,0.0000638708,0.00010985335,0.00007490276,0.0025185258],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.9998375,0.000025132682,0.00000608595,0.000038435606,0.000055012588,0.00003773575],"domain_scores_gemma":[0.9992643,0.0003422122,0.00011871467,0.000066232766,0.00011720132,0.00009131156],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00034265537,0.00041170538,0.0002614694,0.00047102012,0.0003189192,0.000585471,0.0003741944,0.000604313,0.0020636567],"category_scores_gemma":[0.00075018674,0.00040481729,0.00013106829,0.0002971395,0.00065309904,0.0006127701,0.0005411787,0.0005249565,0.00020542486],"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":[0.00016321802,0.000038121023,0.00018223903,0.000021637921,0.0000035772866,0.000038071834,0.000033067852,0.00070719625,0.9963361,0.00036457018,0.000048085003,0.0020640632],"study_design_scores_gemma":[0.000082366736,0.00028046744,0.0060685254,0.000018535511,0.000026866173,0.00036912586,0.00008037282,0.033278886,0.95839685,0.0005455358,0.0008258599,0.000026624579],"about_ca_topic_score_codex":0.00066191505,"about_ca_topic_score_gemma":0.0006632898,"teacher_disagreement_score":0.0020636567,"about_ca_system_score_codex":0.00035510008,"about_ca_system_score_gemma":0.0003697253,"threshold_uncertainty_score":0.0069036484},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8705455,0.0003097258,0.124153696,0.00009774652,0.00004255922,0.00010998219,0.000052898013,0.00029341088,0.0043944507],"genre_scores_gemma":[0.98343277,0.00011418336,0.015340585,0.000022118234,0.000005909836,0.00006639278,0.000036346533,0.000028256758,0.00095348695],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998516,0.000025821571,0.000010295944,0.000040526105,0.000040341132,0.000031562937],"domain_scores_gemma":[0.9996958,0.00014695512,0.000074516276,0.000012440741,0.000045594265,0.000024784964],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004123751,0.00067168067,0.00043154223,0.0002932498,0.00019066529,0.0008553898,0.00031659805,0.000509273,0.00093975355],"category_scores_gemma":[0.0010648014,0.00039154448,0.00021223514,0.00017425782,0.00035327487,0.00037410273,0.0005491747,0.00035251537,0.00012494171],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0005789602,0.0002586142,0.0012090283,0.00022971559,0.00004830273,0.00030680504,0.00014182022,0.702916,0.26439467,0.0028987916,0.00028014925,0.026737036],"study_design_scores_gemma":[0.000071881004,0.000766329,0.0009029287,0.000011217764,0.00001596741,0.0000342835,0.000027941938,0.93612224,0.060726248,0.0005797434,0.00072215457,0.000019115045],"about_ca_topic_score_codex":0.00074106647,"about_ca_topic_score_gemma":0.00069933286,"teacher_disagreement_score":0.00093975355,"about_ca_system_score_codex":0.00038476402,"about_ca_system_score_gemma":0.0003581779,"threshold_uncertainty_score":0.0031437874},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97579795,0.00020449141,0.023136605,0.000021455415,0.00001334268,0.000025043024,0.00002729885,0.000087157765,0.000686659],"genre_scores_gemma":[0.9933816,0.00012518858,0.006200241,0.0000070451465,0.00000873053,0.000012102266,0.000042940483,0.0000110350875,0.00021102812],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99981946,0.00002020699,0.0000067562146,0.000047286303,0.000083615814,0.000022563172],"domain_scores_gemma":[0.9993498,0.00034883438,0.00010350733,0.00004869874,0.00007242368,0.00007670336],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00035828818,0.00042510583,0.00037369906,0.0004386011,0.00046794701,0.00051433506,0.00042971244,0.00036132368,0.00050415855],"category_scores_gemma":[0.0010926968,0.00019481425,0.00021767763,0.00035106708,0.0007544632,0.0007404146,0.0004074236,0.0005913684,0.000083443985],"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":[0.00041476986,0.0002179807,0.0074403156,0.000104246225,0.000016047165,0.0006794623,0.00021603986,0.016185,0.9569039,0.002671926,0.00008056462,0.015069688],"study_design_scores_gemma":[0.00012541206,0.0029953814,0.06827978,0.000028604965,0.00004863071,0.0015615764,0.00029115577,0.50458306,0.41783577,0.0020403527,0.0020891218,0.000121186145],"about_ca_topic_score_codex":0.00096374564,"about_ca_topic_score_gemma":0.00056813116,"teacher_disagreement_score":0.00096374564,"about_ca_system_score_codex":0.0003268082,"about_ca_system_score_gemma":0.00019126838,"threshold_uncertainty_score":0.002371192},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99616975,0.00015640905,0.0030298948,0.000018348861,0.000003508597,0.000012978265,0.000027145132,0.000031670144,0.00055024045],"genre_scores_gemma":[0.9980519,0.000033282686,0.0016935742,0.0000072874213,0.0000025429015,0.00000878517,0.000042167812,0.000006282815,0.00015422051],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999342,0.000009385321,0.0000043396562,0.000012263446,0.000018577604,0.000021233333],"domain_scores_gemma":[0.99967027,0.000084577056,0.00008366571,0.00002426443,0.000066082466,0.00007105135],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00014266768,0.00012110147,0.00014457149,0.00037285977,0.0002618558,0.0004704224,0.00019247198,0.000133249,0.00038838788],"category_scores_gemma":[0.00074140093,0.0001287693,0.0001923773,0.00014110276,0.00051477994,0.00032261852,0.00042853615,0.00017610086,0.0000619227],"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":[0.00047601497,0.00009737091,0.026876695,0.000106512125,0.000023961331,0.0006795398,0.0007875038,0.021661056,0.93553954,0.0034388567,0.00021349048,0.010099452],"study_design_scores_gemma":[0.00031115365,0.0010297657,0.16557543,0.00007525508,0.000055678378,0.0012569707,0.0009003414,0.30852354,0.5122377,0.006660303,0.0032381609,0.00013570442],"about_ca_topic_score_codex":0.0009832432,"about_ca_topic_score_gemma":0.00080000045,"teacher_disagreement_score":0.0009832432,"about_ca_system_score_codex":0.00037317254,"about_ca_system_score_gemma":0.00020136786,"threshold_uncertainty_score":0.002707541},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.40868136,0.00092953915,0.5766186,0.00023579953,0.000053387063,0.00021045754,0.0004282583,0.0012966217,0.011545967],"genre_scores_gemma":[0.96306795,0.0004469499,0.033124913,0.0000299874,0.00001804904,0.00025043334,0.00024788093,0.00006969361,0.0027441161],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997223,0.0000963235,0.000014775349,0.00003696588,0.0001007587,0.00002886452],"domain_scores_gemma":[0.99916124,0.0005005532,0.00010370991,0.00005215652,0.00016487068,0.000017462851],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000728227,0.0007987444,0.0008200137,0.0005053583,0.00047529195,0.00073019986,0.0010242737,0.0014087968,0.0011569071],"category_scores_gemma":[0.0017813457,0.00031587417,0.0007843748,0.0003140449,0.0006641602,0.00047598334,0.0005793786,0.0006114367,0.00031036272],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000026372216,0.000040875897,0.00039036546,0.000053669668,0.00000805507,0.00004916296,0.00006072217,0.99156255,0.0033712974,0.0010303638,0.00008851181,0.0033180446],"study_design_scores_gemma":[0.0000041257917,0.000015000262,0.00006917118,0.000003569009,0.0000018745454,0.000005812875,0.00000786311,0.9991535,0.00052658137,0.00011672465,0.0000929943,0.0000027106987],"about_ca_topic_score_codex":0.011286042,"about_ca_topic_score_gemma":0.0051692585,"teacher_disagreement_score":0.011286042,"about_ca_system_score_codex":0.0005058675,"about_ca_system_score_gemma":0.0008496378,"threshold_uncertainty_score":0.022440732},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.94812703,0.00017486868,0.049300123,0.00003995017,0.000022463315,0.000019893463,0.00002030491,0.00009686931,0.0021984135],"genre_scores_gemma":[0.9982895,0.000021853824,0.0014564272,0.000005658348,0.000010104359,0.0000030854549,0.000015249083,0.000010729438,0.00018740896],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99971837,0.00004931588,0.000018656785,0.00007678355,0.000095903866,0.000040849147],"domain_scores_gemma":[0.99818355,0.0005011058,0.0005234263,0.00025855127,0.00031830388,0.0002149951],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00041910418,0.00019208166,0.00036990634,0.00085818564,0.00030326933,0.0013329674,0.00039254536,0.0003729197,0.00058713485],"category_scores_gemma":[0.0031654611,0.00021587634,0.0002481236,0.00025368624,0.0012833256,0.0009946878,0.0007331497,0.00036269636,0.00009322075],"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":[0.0025176697,0.0004915802,0.124475166,0.00026357677,0.00023400565,0.004954346,0.0022447743,0.17142451,0.3739409,0.22517887,0.0013366921,0.09293798],"study_design_scores_gemma":[0.00009994708,0.00036892554,0.0706425,0.00002022782,0.000042802047,0.0014579241,0.00032579896,0.832767,0.03175376,0.06096771,0.0014569887,0.00009628853],"about_ca_topic_score_codex":0.00027635385,"about_ca_topic_score_gemma":0.00011123588,"teacher_disagreement_score":0.0013329674,"about_ca_system_score_codex":0.00027310438,"about_ca_system_score_gemma":0.00019499972,"threshold_uncertainty_score":0.002216518},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9904337,0.00021819492,0.007582957,0.000086153974,0.000051275027,0.000037261318,0.00015990496,0.0002990525,0.0011315184],"genre_scores_gemma":[0.99621505,0.00009779493,0.0027316364,0.00005135822,0.000015960153,0.000028028819,0.000116686104,0.00021085564,0.00053277914],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99927515,0.00020050054,0.000051665844,0.00013428657,0.00015075915,0.00018757682],"domain_scores_gemma":[0.99470574,0.0036319953,0.00038172363,0.0004371605,0.00061231264,0.00023103566],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0010132293,0.00055906124,0.00071637746,0.00037296128,0.0008289555,0.00074305077,0.00041946032,0.0009597172,0.0022914645],"category_scores_gemma":[0.0058404617,0.00048662192,0.00027419027,0.00038071713,0.00089733844,0.001157526,0.000759181,0.00059718534,0.0003641369],"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":[0.005633392,0.00030514383,0.0041936,0.0001938022,0.000022142247,0.0004856331,0.00039196998,0.007214073,0.97221166,0.00044850286,0.00032280982,0.008577285],"study_design_scores_gemma":[0.00011449123,0.0030005674,0.014415243,0.000025204266,0.00005486993,0.0002106043,0.00023563519,0.017624242,0.9628708,0.00016101661,0.0012336985,0.00005369137],"about_ca_topic_score_codex":0.0010110062,"about_ca_topic_score_gemma":0.0014545969,"teacher_disagreement_score":0.0022914645,"about_ca_system_score_codex":0.00048144063,"about_ca_system_score_gemma":0.00041145153,"threshold_uncertainty_score":0.0076657534},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99691606,0.00005284743,0.0023833576,0.000010195428,0.0000048455468,0.000008193249,0.000050889274,0.00014993708,0.00042365893],"genre_scores_gemma":[0.9981421,0.00003542034,0.0013552073,0.000016127562,0.0000016364631,0.000007026205,0.000079235084,0.000035286623,0.00032791702],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99936706,0.00012414485,0.00005644662,0.00013991287,0.00020308104,0.00010933712],"domain_scores_gemma":[0.99831885,0.0005572732,0.00047934832,0.00020496323,0.0003287232,0.00011086967],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006697726,0.00068511744,0.00033723947,0.0003702948,0.000247067,0.0006088188,0.0005361611,0.00066692947,0.0018002308],"category_scores_gemma":[0.0017718424,0.00039807736,0.0002495207,0.0003589193,0.00044052125,0.0004586514,0.00055449863,0.00035764714,0.0007054933],"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":[0.0008620232,0.0000908367,0.0072649787,0.0000797051,0.000021608965,0.0003330339,0.00016188882,0.0154663585,0.96727276,0.00012893493,0.00011209787,0.008205829],"study_design_scores_gemma":[0.000053293432,0.0040408676,0.02785507,0.000018710627,0.00006605257,0.0006031216,0.00022147142,0.020822491,0.94519633,0.000071076174,0.0009796093,0.00007192072],"about_ca_topic_score_codex":0.000348431,"about_ca_topic_score_gemma":0.0004022158,"teacher_disagreement_score":0.0018002308,"about_ca_system_score_codex":0.0003053175,"about_ca_system_score_gemma":0.00014945326,"threshold_uncertainty_score":0.0060223937},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7279647,0.00033890628,0.26550168,0.00018393376,0.0002655047,0.00014743693,0.00003779455,0.00059974776,0.004960276],"genre_scores_gemma":[0.98064613,0.000060155286,0.018461745,0.0000230618,0.000028371613,0.000018757124,0.000007738939,0.000024689469,0.0007292273],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99963677,0.00009303315,0.000014955253,0.0000767551,0.00012891823,0.000049609775],"domain_scores_gemma":[0.99856865,0.0008583765,0.00012778684,0.00016616251,0.00017276997,0.000106272935],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0007472795,0.0005001988,0.0004585974,0.0004702151,0.00061914045,0.00050606736,0.0007326559,0.0008205875,0.0017470373],"category_scores_gemma":[0.0018430268,0.0003045053,0.0003060653,0.00020698555,0.00087337353,0.00065774703,0.0006316268,0.00046715344,0.0001574708],"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":[0.0026687812,0.0008732514,0.0028597093,0.00019389558,0.000054627115,0.00025364038,0.00039163503,0.022682365,0.8743129,0.00816445,0.00028644133,0.08725837],"study_design_scores_gemma":[0.0006612221,0.007073079,0.008889794,0.000038678234,0.00017849382,0.00045290522,0.00008746952,0.546455,0.42935804,0.0028479155,0.003814956,0.00014250868],"about_ca_topic_score_codex":0.0006550549,"about_ca_topic_score_gemma":0.0004866878,"teacher_disagreement_score":0.0017470373,"about_ca_system_score_codex":0.00029085937,"about_ca_system_score_gemma":0.00022997898,"threshold_uncertainty_score":0.0058444142},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.96958065,0.00033201606,0.02149918,0.00028652474,0.0000578175,0.00010714074,0.000062969535,0.00017369178,0.007900135],"genre_scores_gemma":[0.9891439,0.00010122501,0.009153355,0.000033581786,0.000012894168,0.000016546337,0.0000264326,0.00001675141,0.0014952727],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99955815,0.00007037908,0.000017015438,0.00010038463,0.00017041656,0.00008363416],"domain_scores_gemma":[0.9991009,0.00042169506,0.00012316591,0.000096551405,0.00012881252,0.00012880417],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00065330794,0.000391618,0.0007777502,0.0007633694,0.0012902613,0.001719373,0.00084685936,0.0020527772,0.0012855595],"category_scores_gemma":[0.002156796,0.00036553302,0.00057006435,0.000352011,0.0018326481,0.0009964824,0.00076674053,0.0006963471,0.00020431141],"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":[0.0019874147,0.0015923763,0.014249621,0.0005654552,0.00010684171,0.01928309,0.0020270846,0.5558789,0.31683558,0.0507048,0.0013453313,0.035423502],"study_design_scores_gemma":[0.00028959263,0.0010061539,0.006989523,0.000048229267,0.000043751686,0.0029612007,0.000527156,0.9376966,0.044250317,0.0037345847,0.0023661063,0.00008691715],"about_ca_topic_score_codex":0.004240699,"about_ca_topic_score_gemma":0.0017141323,"teacher_disagreement_score":0.004240699,"about_ca_system_score_codex":0.00095457985,"about_ca_system_score_gemma":0.0009956895,"threshold_uncertainty_score":0.008432031},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.112057954,0.00028054704,0.88360095,0.000084297695,0.000066439236,0.00010733047,0.0000543622,0.00050202577,0.003246097],"genre_scores_gemma":[0.7361102,0.00032640382,0.26079535,0.000053872525,0.000043715598,0.000076071556,0.000097265634,0.00005958279,0.0024375187],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99975556,0.000054371983,0.000011036998,0.000033484383,0.00012547517,0.00002005997],"domain_scores_gemma":[0.999398,0.00038883497,0.000064875334,0.000086910295,0.00003901951,0.00002222618],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002971851,0.0003287055,0.0002897274,0.00029816676,0.00013323757,0.0004727803,0.0004496321,0.00035491886,0.0009589503],"category_scores_gemma":[0.0010786159,0.00015553234,0.00028633792,0.00020737886,0.00062663475,0.00068547763,0.0006650292,0.00032874595,0.00016268955],"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":[0.00039344365,0.0001530254,0.0013360553,0.00030588577,0.000041154737,0.00049154344,0.00027406117,0.15827152,0.6087941,0.027019553,0.0005683932,0.2023513],"study_design_scores_gemma":[0.00009592043,0.00051732024,0.0012590733,0.000019620078,0.000024814832,0.0006294211,0.000074748095,0.7040321,0.28357473,0.004881894,0.0048150714,0.00007527675],"about_ca_topic_score_codex":0.00020694254,"about_ca_topic_score_gemma":0.00020652327,"teacher_disagreement_score":0.0009589503,"about_ca_system_score_codex":0.00022340231,"about_ca_system_score_gemma":0.00020374396,"threshold_uncertainty_score":0.0032079816},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7628076,0.00028612552,0.23234135,0.000112394264,0.00004487946,0.000042759923,0.0002151902,0.0002734411,0.00387621],"genre_scores_gemma":[0.97650754,0.00015323299,0.022122132,0.00001024853,0.0000114952045,0.000011529833,0.00012308497,0.000037052516,0.0010236261],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99995494,0.000007805034,0.0000020151404,0.000012323551,0.000013854184,0.000009107692],"domain_scores_gemma":[0.9999006,0.00002991174,0.000018237553,0.000016563632,0.000018908288,0.00001575201],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001492445,0.00027837526,0.00027060608,0.0003696141,0.00019861154,0.00065656146,0.00017126983,0.00021944332,0.0008588683],"category_scores_gemma":[0.00039065134,0.00015038016,0.00028451713,0.00024278546,0.00046040484,0.0004517501,0.00037203322,0.00038532604,0.00007009547],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0003244883,0.00018038729,0.027242579,0.00018209846,0.000090065354,0.0009032612,0.00054951437,0.61954474,0.2047829,0.027077157,0.0014257805,0.11769703],"study_design_scores_gemma":[0.000006429211,0.000035979465,0.009781166,0.000006599249,0.000005058097,0.00007272822,0.00005373424,0.98148525,0.00603706,0.0018005891,0.00069959025,0.00001589995],"about_ca_topic_score_codex":0.0029333364,"about_ca_topic_score_gemma":0.0019237577,"teacher_disagreement_score":0.0029333364,"about_ca_system_score_codex":0.0002325868,"about_ca_system_score_gemma":0.0003169396,"threshold_uncertainty_score":0.0058324933},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99741423,0.000089852445,0.0021604048,0.0000054328593,0.00000638816,0.000008940654,0.000016399557,0.000024447438,0.00027382065],"genre_scores_gemma":[0.9971289,0.000063116386,0.0024588013,0.0000062820945,0.000002226713,0.000004891745,0.000024443567,0.000006960094,0.00030424588],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997403,0.000046899793,0.000018920246,0.00004853478,0.0000904006,0.000054899225],"domain_scores_gemma":[0.99935585,0.00016048376,0.00016963303,0.00007753046,0.00014145295,0.00009512484],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004823373,0.00029681387,0.00029888653,0.00027753174,0.00019621968,0.00045962958,0.00026453883,0.00029645668,0.0005056197],"category_scores_gemma":[0.0010596486,0.0002081211,0.00029920271,0.00021781589,0.00042883816,0.0003171409,0.00028495392,0.00021840986,0.00016787846],"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":[0.0006341115,0.00009187854,0.007078709,0.00010248628,0.00001611234,0.00033286057,0.00014609461,0.012937756,0.9688376,0.00032173525,0.00005831762,0.009442275],"study_design_scores_gemma":[0.000099098994,0.0044302763,0.060325287,0.000031393392,0.000084546045,0.0008459718,0.0006019799,0.09070651,0.84076494,0.00017993194,0.0018719152,0.00005810665],"about_ca_topic_score_codex":0.00078368996,"about_ca_topic_score_gemma":0.0011168874,"teacher_disagreement_score":0.00078368996,"about_ca_system_score_codex":0.00021092588,"about_ca_system_score_gemma":0.00018742589,"threshold_uncertainty_score":0.0025508404},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9978277,0.000057983594,0.0018393525,0.000005046614,0.000006308635,0.00000721529,0.000008779294,0.000017896751,0.00022965434],"genre_scores_gemma":[0.9968149,0.000055543773,0.0027762742,0.000007377006,0.0000045760644,0.000007143285,0.000031411786,0.0000056782897,0.0002970849],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997588,0.000018794117,0.000008450419,0.00005306428,0.00010834706,0.00005259773],"domain_scores_gemma":[0.9995388,0.00013231674,0.00012622439,0.000041235686,0.000094717114,0.00006676994],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024612065,0.00032811565,0.00035172602,0.00034203607,0.000344268,0.0006162208,0.0002713108,0.00040955163,0.00067441806],"category_scores_gemma":[0.00071993767,0.00027313823,0.00015376929,0.00029742176,0.00060536445,0.00044313268,0.00038844493,0.00068771286,0.000093204755],"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":[0.0001101997,0.00004611232,0.001261852,0.00002467165,0.0000028422514,0.00011506394,0.00006705958,0.00068866863,0.9950513,0.00012661587,0.000009731978,0.0024958905],"study_design_scores_gemma":[0.000053498396,0.0021072284,0.056706544,0.0000125002125,0.000036430098,0.00037310825,0.00041309424,0.019582868,0.91932863,0.00017737207,0.0011629638,0.000045870587],"about_ca_topic_score_codex":0.0003811867,"about_ca_topic_score_gemma":0.00036861107,"teacher_disagreement_score":0.00067441806,"about_ca_system_score_codex":0.00022852694,"about_ca_system_score_gemma":0.00015723913,"threshold_uncertainty_score":0.002256155},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9988751,0.000022153008,0.0009460247,0.0000050787503,0.0000056304048,0.0000019231077,0.000017293947,0.0000200528,0.000106801745],"genre_scores_gemma":[0.9995509,0.000016624483,0.0003428164,0.000002626019,0.00000120771,0.0000011799136,0.000019004812,0.0000025119955,0.000063020736],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998622,0.000013057452,0.000010884584,0.000028802946,0.00004427629,0.000040809267],"domain_scores_gemma":[0.99879897,0.0005865907,0.00019444083,0.000076213495,0.00021637,0.00012747254],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00022726406,0.0001648212,0.00022402171,0.00018508274,0.0001546713,0.0002542165,0.00015311514,0.00016569068,0.00046446265],"category_scores_gemma":[0.0014429297,0.0001219639,0.00009371301,0.00011217301,0.00027662484,0.00022889438,0.00022767288,0.0002632308,0.00006277937],"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":[0.0018320581,0.00019196444,0.029564224,0.0000870631,0.000026429934,0.0009638325,0.00026333437,0.031993054,0.9114752,0.00030112584,0.00017667213,0.02312509],"study_design_scores_gemma":[0.000038572263,0.0011612573,0.12690532,0.00002131321,0.000050126306,0.00023781855,0.00037332243,0.2511117,0.61948824,0.00015293472,0.00040912465,0.00005032974],"about_ca_topic_score_codex":0.0015861674,"about_ca_topic_score_gemma":0.0010891955,"teacher_disagreement_score":0.0015861674,"about_ca_system_score_codex":0.00016293624,"about_ca_system_score_gemma":0.00023833913,"threshold_uncertainty_score":0.003153801},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.39220527,0.00023935965,0.6030902,0.00016242953,0.00007034631,0.00008860743,0.00018191227,0.0015880923,0.0023738032],"genre_scores_gemma":[0.70120907,0.00017661575,0.2970451,0.000042866654,0.000017677356,0.00008616369,0.00014052031,0.000043979155,0.0012380615],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997079,0.00009875925,0.00001735516,0.000051607094,0.00010149095,0.000022847871],"domain_scores_gemma":[0.9993956,0.00031901087,0.0000630686,0.00005966035,0.000118584525,0.000044177028],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005625005,0.00047800806,0.00053686404,0.0003519722,0.00021742022,0.00045580225,0.00040618435,0.00072555314,0.0013090239],"category_scores_gemma":[0.0011010672,0.0004106201,0.00029821083,0.0002922425,0.0005187918,0.00074135006,0.0008118017,0.0002894618,0.00028837018],"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":[0.0008350187,0.00024400168,0.004085821,0.00024034976,0.00005375378,0.0006962223,0.0004927496,0.24455015,0.670144,0.0024890758,0.0006152933,0.07555361],"study_design_scores_gemma":[0.00015809778,0.0005929052,0.0043136873,0.000047244386,0.000026947831,0.00047509538,0.00015694243,0.8911426,0.10003451,0.0013820836,0.00157122,0.00009868347],"about_ca_topic_score_codex":0.0008176847,"about_ca_topic_score_gemma":0.0011519804,"teacher_disagreement_score":0.0013090239,"about_ca_system_score_codex":0.0001543784,"about_ca_system_score_gemma":0.0004620901,"threshold_uncertainty_score":0.0043791533},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9983291,0.00013556016,0.0011525975,0.0000130222215,0.000009664723,0.000004232876,0.0000133415015,0.000023746969,0.00031871238],"genre_scores_gemma":[0.99891543,0.000079710364,0.0006594466,0.000009718817,0.000005545341,0.0000044202293,0.000020926422,0.0000118476855,0.00029279725],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99951136,0.00008464058,0.000033247095,0.00009699326,0.00017927881,0.000094437084],"domain_scores_gemma":[0.9987936,0.0006838382,0.00020794637,0.000068960886,0.00012343135,0.00012218533],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00039880362,0.00053166394,0.0005048619,0.00016178597,0.00022324134,0.00052002684,0.00026669138,0.00040879048,0.0020159052],"category_scores_gemma":[0.0010515007,0.00034654108,0.00025227835,0.00014640782,0.0003116451,0.0002703624,0.00041710955,0.00036276504,0.00033085348],"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":[0.00021552974,0.000012613922,0.00027996782,0.000019676914,0.000007974118,0.000060656053,0.00002754506,0.0004362888,0.9983171,0.000019700008,0.000007638016,0.000595286],"study_design_scores_gemma":[0.000027246779,0.0004712266,0.0061531616,0.0000044034628,0.000032783402,0.000082820006,0.000038711118,0.0069326,0.9860103,0.000010723099,0.00022569114,0.000010367306],"about_ca_topic_score_codex":0.00046009774,"about_ca_topic_score_gemma":0.0004364563,"teacher_disagreement_score":0.0020159052,"about_ca_system_score_codex":0.00022214107,"about_ca_system_score_gemma":0.0001477032,"threshold_uncertainty_score":0.006743908},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99708015,0.00007560886,0.0014224997,0.000023522864,0.000011612944,0.000016152848,0.00010493708,0.00004041258,0.0012250091],"genre_scores_gemma":[0.9979018,0.000054265216,0.0010876346,0.000010772692,0.000010099924,0.000010602098,0.00008285125,0.000013935742,0.00082812266],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998957,0.00001207123,0.0000039418874,0.000029259068,0.000028785484,0.000030274632],"domain_scores_gemma":[0.9991602,0.00042751193,0.000118132564,0.00009062324,0.00011264045,0.00009086789],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021239975,0.00021554253,0.00025373002,0.00024693296,0.0007201219,0.0002901296,0.00049517286,0.0004311693,0.0028629561],"category_scores_gemma":[0.00059339614,0.00022392711,0.00018882823,0.00019259847,0.0008837597,0.00047401196,0.00039544134,0.00065570977,0.00024080262],"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":[0.0014105255,0.00031640736,0.0017704697,0.0000523117,0.000009768122,0.0002652724,0.00016589687,0.0006406519,0.9929178,0.0005016455,0.00010423733,0.0018449693],"study_design_scores_gemma":[0.00029604914,0.0052086175,0.056774896,0.000021724654,0.00006554456,0.00073501584,0.0006300396,0.013963611,0.9199857,0.00054013135,0.0017232415,0.00005552052],"about_ca_topic_score_codex":0.000553626,"about_ca_topic_score_gemma":0.00044607124,"teacher_disagreement_score":0.0028629561,"about_ca_system_score_codex":0.0001576619,"about_ca_system_score_gemma":0.00018825404,"threshold_uncertainty_score":0.009577572},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9941525,0.000032835447,0.005147094,0.000009310023,0.000007107213,0.00000877637,0.00002256515,0.000040157654,0.0005796572],"genre_scores_gemma":[0.99752074,0.000019274758,0.0021643578,0.0000050601147,0.0000017600894,0.0000050508916,0.000029005621,0.0000064186447,0.00024830806],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997209,0.00006442844,0.0000137868,0.00004639539,0.00011859122,0.000035906465],"domain_scores_gemma":[0.99949956,0.0002023717,0.00006239765,0.00006914765,0.0001296684,0.00003686545],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000425105,0.0003442306,0.00034745215,0.00020107011,0.00020391635,0.00021998714,0.0001819888,0.00029356676,0.00070910965],"category_scores_gemma":[0.0008566182,0.00013630577,0.00017318774,0.000089276095,0.0004317698,0.00019376256,0.00017986124,0.00012758959,0.00022378647],"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":[0.0010559411,0.00018376246,0.012416329,0.00011005656,0.000023926616,0.00059021474,0.00015480755,0.057946227,0.90463793,0.0004627264,0.00018742385,0.022230523],"study_design_scores_gemma":[0.00019637351,0.0076175905,0.055879146,0.000035293895,0.000062964566,0.0010653307,0.00026443147,0.3930859,0.5388348,0.00049136917,0.0023926364,0.000074223295],"about_ca_topic_score_codex":0.0003737224,"about_ca_topic_score_gemma":0.00034035195,"teacher_disagreement_score":0.00070910965,"about_ca_system_score_codex":0.00016261976,"about_ca_system_score_gemma":0.00015144286,"threshold_uncertainty_score":0.0023722053},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.17384128,0.001278806,0.8192161,0.00022290439,0.00025374556,0.000168996,0.000108232045,0.000667116,0.004242838],"genre_scores_gemma":[0.54070747,0.0010743866,0.4558968,0.00010092894,0.00010383675,0.00013348476,0.00007070983,0.000033733948,0.0018786419],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997913,0.000040473027,0.0000104118735,0.00003495461,0.00011166513,0.000011260067],"domain_scores_gemma":[0.999597,0.00022169432,0.000028895964,0.000035262176,0.00010203352,0.000015221062],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002555538,0.00030216685,0.00021426783,0.00022951963,0.00012738074,0.00020654258,0.0002433718,0.00029859404,0.0006763706],"category_scores_gemma":[0.0010011571,0.00021054855,0.00015904743,0.00017424484,0.0002129706,0.00028312573,0.00022255383,0.00016740338,0.00026844113],"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":[0.000057083063,0.000021148931,0.0008572334,0.00013269982,0.000008933866,0.00016890634,0.000045598474,0.0067488737,0.8969438,0.00094708265,0.00024086972,0.09382774],"study_design_scores_gemma":[0.000046657915,0.0010685549,0.008420898,0.000030485993,0.00004379583,0.0016188286,0.00007877568,0.14193542,0.8282079,0.0016331475,0.016851816,0.0000636617],"about_ca_topic_score_codex":0.0002677783,"about_ca_topic_score_gemma":0.00056840415,"teacher_disagreement_score":0.0006763706,"about_ca_system_score_codex":0.0001419554,"about_ca_system_score_gemma":0.00021035249,"threshold_uncertainty_score":0.002262652},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99445194,0.00011251583,0.0034376201,0.000032542805,0.000031992662,0.000015433357,0.00010098828,0.00005430941,0.0017626238],"genre_scores_gemma":[0.9981824,0.000049983628,0.0012227185,0.000005387036,0.0000043201017,0.0000036482156,0.0000489194,0.000003985645,0.00047870225],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998729,0.000012878124,0.0000055617897,0.000022199516,0.000043463962,0.00004288154],"domain_scores_gemma":[0.999754,0.00009397229,0.00002324425,0.0000312069,0.000052524298,0.000044993296],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015546681,0.0003144784,0.00034140048,0.0002348114,0.0004494039,0.00039527984,0.00029374677,0.00039029456,0.0014314717],"category_scores_gemma":[0.00031819972,0.00022361585,0.00019429094,0.00018127821,0.0005557839,0.00035811114,0.00043817924,0.00046849417,0.00015885312],"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":[0.0007860703,0.00009866999,0.0043486482,0.000070981,0.000013227935,0.0006268674,0.00022846354,0.008515796,0.97826743,0.00093714724,0.00017355182,0.005933123],"study_design_scores_gemma":[0.00011126654,0.002291977,0.04728685,0.000024907244,0.000030158926,0.0006819712,0.0005166084,0.12318249,0.82359135,0.0006689622,0.0015454688,0.00006803851],"about_ca_topic_score_codex":0.0007311019,"about_ca_topic_score_gemma":0.00065395114,"teacher_disagreement_score":0.0014314717,"about_ca_system_score_codex":0.00018311638,"about_ca_system_score_gemma":0.00029115373,"threshold_uncertainty_score":0.0047887564},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.06296563,0.00035632963,0.9320893,0.00018538997,0.000101328726,0.00008963027,0.00010131268,0.00050845253,0.003602569],"genre_scores_gemma":[0.8180939,0.0003636189,0.17816164,0.00007189612,0.000083778184,0.00031916008,0.0001665623,0.00017112964,0.0025683143],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99961543,0.000115930416,0.000021335487,0.00004833132,0.00016480066,0.00003410829],"domain_scores_gemma":[0.99918836,0.00039114256,0.00011860098,0.00006280801,0.00020123593,0.00003781237],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0011076054,0.0008222093,0.0008663421,0.00061993196,0.00052436866,0.0010646253,0.0012331171,0.0015452126,0.0010866295],"category_scores_gemma":[0.0029373248,0.00049646,0.0009333765,0.0003051743,0.0010132196,0.0006609232,0.0010073953,0.0011487145,0.00029148397],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000018436756,0.000013757597,0.00021990585,0.000017396722,0.000012185719,0.000028459439,0.000009907761,0.99170035,0.0026518577,0.0028286038,0.000053074087,0.0024461122],"study_design_scores_gemma":[0.0000011446575,0.000003691527,0.0000140609645,6.5495374e-7,6.901098e-7,9.565185e-7,5.2754444e-7,0.9997003,0.000120455705,0.00013295037,0.000023543418,9.557945e-7],"about_ca_topic_score_codex":0.0074181026,"about_ca_topic_score_gemma":0.0024946565,"teacher_disagreement_score":0.0074181026,"about_ca_system_score_codex":0.0007238235,"about_ca_system_score_gemma":0.0015282285,"threshold_uncertainty_score":0.014749825},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.47153494,0.0008256257,0.5218927,0.00011697619,0.00020655923,0.00022834585,0.0004006039,0.00080884126,0.003985378],"genre_scores_gemma":[0.8100223,0.00066198764,0.18739904,0.000045215158,0.00009338772,0.00016071067,0.00031480374,0.000057237394,0.0012452308],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99925536,0.00008796884,0.000032626638,0.00016356423,0.00038921836,0.00007128467],"domain_scores_gemma":[0.9995104,0.00010163293,0.000078718505,0.000052885658,0.00021014536,0.000046091413],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005657465,0.0004940467,0.0006430464,0.0008430395,0.00027802354,0.0006609726,0.00057266804,0.00037865216,0.000618571],"category_scores_gemma":[0.0008979684,0.00037921587,0.00019999115,0.0006593877,0.0004708123,0.0008541779,0.00082500157,0.0005594808,0.0002285738],"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":[0.00010614633,0.000035694608,0.0016534552,0.00009047404,0.00001979863,0.0000679183,0.00006477781,0.0014232647,0.9662229,0.0016302879,0.00027284626,0.028412445],"study_design_scores_gemma":[0.00006210362,0.0005727008,0.0068192077,0.000018772986,0.000057679525,0.0003201991,0.00012055024,0.08630267,0.8998137,0.0014604112,0.0043760245,0.00007587921],"about_ca_topic_score_codex":0.00085418404,"about_ca_topic_score_gemma":0.0008323689,"teacher_disagreement_score":0.00085418404,"about_ca_system_score_codex":0.00028288102,"about_ca_system_score_gemma":0.00067743595,"threshold_uncertainty_score":0.002992034},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.87172693,0.00009832721,0.11734055,0.00019076795,0.00005594737,0.00007071176,0.000349061,0.00058246596,0.009585387],"genre_scores_gemma":[0.96902776,0.00007539543,0.027407462,0.000027116455,0.000008044494,0.000070886104,0.0002328761,0.00004673237,0.0031035522],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99991345,0.000022082504,0.0000052559303,0.000011078332,0.000033034856,0.00001514669],"domain_scores_gemma":[0.9996045,0.00021715913,0.000044608183,0.000026315714,0.00007679699,0.00003069222],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020365909,0.00034029485,0.000368137,0.00022923552,0.0003218404,0.00042193133,0.0005462994,0.0008105429,0.0017756274],"category_scores_gemma":[0.0007306896,0.00017478949,0.00028137257,0.00026733137,0.00046793316,0.0003466764,0.0004136196,0.00043102214,0.0001765634],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000051411313,0.00004635076,0.00093602185,0.000024671133,0.0000067661663,0.00010707111,0.00005595316,0.9904255,0.0050907764,0.0010911161,0.00014059851,0.002023748],"study_design_scores_gemma":[0.0000046231703,0.000008896067,0.00007800835,8.636021e-7,6.408437e-7,0.0000054827365,0.0000057635466,0.99921906,0.0005317503,0.000059678317,0.00008358792,0.0000016021223],"about_ca_topic_score_codex":0.0064372486,"about_ca_topic_score_gemma":0.002759363,"teacher_disagreement_score":0.0064372486,"about_ca_system_score_codex":0.00037362197,"about_ca_system_score_gemma":0.0006210722,"threshold_uncertainty_score":0.012799561},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97720397,0.00018345371,0.020648856,0.00003271213,0.000030072262,0.000011474904,0.0000682327,0.00028003135,0.0015411653],"genre_scores_gemma":[0.9938134,0.00009245053,0.0052031414,0.000013321506,0.000008013264,0.000006096587,0.00013159472,0.000027472463,0.00070441235],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99986815,0.000028041173,0.00001004911,0.00001708725,0.000053955242,0.00002274784],"domain_scores_gemma":[0.9997503,0.00010726223,0.000054228305,0.000016791553,0.000037761583,0.000033670352],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00028571728,0.00035893504,0.0003020485,0.00029718084,0.00029869736,0.0011150541,0.00024222751,0.00039006205,0.0007171897],"category_scores_gemma":[0.00062522123,0.00015242858,0.00033559639,0.00030699288,0.00039229842,0.00039483563,0.000420485,0.00036045737,0.00016784773],"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":[0.0018639484,0.0001430203,0.0075376076,0.00011786876,0.000034812776,0.00092083216,0.00029817852,0.08847766,0.8782602,0.0027898923,0.0003128403,0.019243155],"study_design_scores_gemma":[0.00030186918,0.0010866887,0.017600572,0.000032854437,0.000069146896,0.00028764099,0.0001694344,0.6700517,0.30713394,0.0012386437,0.0019403503,0.00008713953],"about_ca_topic_score_codex":0.001722855,"about_ca_topic_score_gemma":0.00081023714,"teacher_disagreement_score":0.001722855,"about_ca_system_score_codex":0.00036769416,"about_ca_system_score_gemma":0.00029825376,"threshold_uncertainty_score":0.0034257174},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9751175,0.00015621253,0.0031334308,0.00035154825,0.00019154717,0.000059817627,0.0010003797,0.00040651456,0.01958299],"genre_scores_gemma":[0.99666744,0.000045459663,0.0013546519,0.00004910662,0.00002638403,0.000012201813,0.00053281756,0.00006736209,0.0012445308],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997291,0.000051796396,0.0000221151,0.000055861925,0.000074847674,0.00006622958],"domain_scores_gemma":[0.99887735,0.00046714232,0.00007980575,0.0000950764,0.00024669926,0.00023391032],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00033496926,0.0006764679,0.0008692005,0.00077409897,0.0010581843,0.0016366497,0.0007412244,0.0017176707,0.0034821266],"category_scores_gemma":[0.0021986596,0.00042308524,0.000465481,0.0007593214,0.0015480584,0.00089833594,0.0005281533,0.0013115179,0.00030287346],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0015990903,0.0007026619,0.019416736,0.00016863758,0.00009157612,0.0016711074,0.00034842658,0.9238402,0.026903735,0.014116775,0.0037280393,0.0074129626],"study_design_scores_gemma":[0.00012243871,0.000092344235,0.0065306993,0.000011475192,0.0000111867075,0.000073202675,0.000092739516,0.9881379,0.0034691165,0.0008761686,0.00055777153,0.000025048066],"about_ca_topic_score_codex":0.021832766,"about_ca_topic_score_gemma":0.007747541,"teacher_disagreement_score":0.021832766,"about_ca_system_score_codex":0.0018048553,"about_ca_system_score_gemma":0.0011673304,"threshold_uncertainty_score":0.043411374},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99493897,0.0001573622,0.003040813,0.000046773832,0.000030075867,0.0000043201894,0.000020754891,0.000064473505,0.0016964765],"genre_scores_gemma":[0.999413,0.00002941254,0.0002543673,0.0000054851453,0.000006324035,0.0000014640067,0.0000065492573,0.000017266057,0.00026620398],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998528,0.0000350072,0.0000044228836,0.000024012004,0.000022587781,0.000061170555],"domain_scores_gemma":[0.9975942,0.00178851,0.00012101086,0.00009436638,0.00016044793,0.00024148925],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00046976286,0.00030845185,0.00042365046,0.00039008903,0.00056526705,0.00069160416,0.00030852243,0.00041082487,0.0039241207],"category_scores_gemma":[0.0027361054,0.00028751724,0.00035251386,0.000109477885,0.0009445228,0.0005552499,0.0005313863,0.00051313656,0.00020428648],"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":[0.005062661,0.00026006892,0.00520445,0.00018847623,0.00007498826,0.00057353184,0.00047220476,0.06805779,0.8926539,0.004414069,0.00051660545,0.022521228],"study_design_scores_gemma":[0.00026789092,0.0021513863,0.02919877,0.000055613335,0.00023219199,0.00036397777,0.00037322557,0.4926083,0.47165498,0.001905391,0.0010298246,0.00015842765],"about_ca_topic_score_codex":0.0005975702,"about_ca_topic_score_gemma":0.00037625822,"teacher_disagreement_score":0.0039241207,"about_ca_system_score_codex":0.00023610385,"about_ca_system_score_gemma":0.00024438958,"threshold_uncertainty_score":0.013127506},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98881173,0.00052807474,0.007920616,0.000017164393,0.00001047221,0.000022187141,0.000068181325,0.00006342906,0.0025581168],"genre_scores_gemma":[0.9936452,0.0002930381,0.0052293846,0.000011356329,0.000007914352,0.000010030378,0.0000904153,0.000016913089,0.00069575635],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99991894,0.000007116767,0.0000034011096,0.000022241436,0.000028205779,0.000019945499],"domain_scores_gemma":[0.99970907,0.00006953595,0.00006911085,0.000021933667,0.000082986895,0.000047341317],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00013758049,0.00016814376,0.00017100561,0.0003716477,0.00024842733,0.0005036746,0.00022438212,0.00018279871,0.00068250776],"category_scores_gemma":[0.00037247286,0.00015282152,0.00017271642,0.00031618177,0.00027008593,0.00031974787,0.00022151056,0.00031118642,0.00012333928],"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":[0.00023063313,0.000049526494,0.015773643,0.00009409059,0.000009364563,0.0011788583,0.00024062234,0.0021387222,0.96121126,0.0012061354,0.00010617479,0.017760932],"study_design_scores_gemma":[0.000043476433,0.0010902074,0.23565087,0.00003935061,0.000056099056,0.002772569,0.00076238456,0.066946685,0.6865619,0.0011041563,0.0049148267,0.000057563037],"about_ca_topic_score_codex":0.0007621671,"about_ca_topic_score_gemma":0.00039333687,"teacher_disagreement_score":0.0007621671,"about_ca_system_score_codex":0.00011287636,"about_ca_system_score_gemma":0.00021006288,"threshold_uncertainty_score":0.0022832155},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9921828,0.00017247115,0.0064036855,0.000023547485,0.000043171978,0.000019860936,0.00005361742,0.00013245645,0.000968334],"genre_scores_gemma":[0.998009,0.00006647158,0.0014261488,0.000014046725,0.0000057981265,0.0000030945646,0.000053459007,0.000034955512,0.00038685472],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99878794,0.00026922068,0.00007406987,0.00020886601,0.00048066746,0.00017929262],"domain_scores_gemma":[0.9970407,0.0016970003,0.00030920046,0.00024596823,0.0005452385,0.00016194387],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00077305775,0.0007016647,0.00059314596,0.00045286832,0.00048147666,0.0009858895,0.00065137376,0.00068614003,0.0017080602],"category_scores_gemma":[0.0054578297,0.00038233036,0.00042948863,0.00020130316,0.00055486715,0.0005990275,0.00052087515,0.00035093407,0.00043582977],"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":[0.0024094733,0.00022026974,0.017902432,0.0002397778,0.00004410182,0.00070846995,0.00039308146,0.03223559,0.9171078,0.00027937934,0.00015954438,0.02830014],"study_design_scores_gemma":[0.00011247522,0.012122402,0.07710242,0.000044101325,0.00033917962,0.0013680246,0.00057490537,0.045898553,0.85993516,0.00026379764,0.0021157677,0.00012323298],"about_ca_topic_score_codex":0.0017456939,"about_ca_topic_score_gemma":0.0020449988,"teacher_disagreement_score":0.0017456939,"about_ca_system_score_codex":0.0003149285,"about_ca_system_score_gemma":0.00027959826,"threshold_uncertainty_score":0.005714059},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.995282,0.00013528888,0.0032449628,0.000017377988,0.000022097545,0.000011224686,0.00002135282,0.000031646177,0.0012340999],"genre_scores_gemma":[0.99806565,0.00010035305,0.0012285656,0.000019970981,0.0000110597575,0.000007949348,0.00003498224,0.0000064974133,0.0005248908],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992512,0.00006987781,0.000028325936,0.0001474921,0.000334182,0.00016897173],"domain_scores_gemma":[0.9988857,0.0005778937,0.00016804934,0.000057917892,0.00020229082,0.0001081407],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002556481,0.00036532208,0.00045331122,0.0003267699,0.00020504872,0.0005688583,0.00033862542,0.00041583832,0.0011540536],"category_scores_gemma":[0.0017277958,0.0002700872,0.00020197898,0.0002709564,0.00056420587,0.0003323735,0.0008450219,0.00042547108,0.00014064551],"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":[0.00035707542,0.00003319844,0.0011815362,0.000053903765,0.000010126614,0.00023518996,0.000080798374,0.001872855,0.99094594,0.0001228075,0.00002476502,0.005081741],"study_design_scores_gemma":[0.000108874636,0.0025024517,0.0421057,0.000028392113,0.000051460236,0.00080482464,0.00041146798,0.030239195,0.9214922,0.0003293667,0.0018627596,0.000063440035],"about_ca_topic_score_codex":0.00048033343,"about_ca_topic_score_gemma":0.00040969887,"teacher_disagreement_score":0.0011540536,"about_ca_system_score_codex":0.00021396426,"about_ca_system_score_gemma":0.0001541354,"threshold_uncertainty_score":0.003860712},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.55474395,0.0006671216,0.44144362,0.00015524974,0.00016129955,0.00007238136,0.000054027805,0.0006504973,0.0020518214],"genre_scores_gemma":[0.9713803,0.00015135117,0.02770527,0.000021307966,0.000024149122,0.000028075277,0.000023087485,0.000015842652,0.00065062096],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998584,0.000028589975,0.00001209574,0.0000227109,0.000061454724,0.000016723623],"domain_scores_gemma":[0.999619,0.00018841421,0.00009036007,0.000019597108,0.00006272515,0.000020007406],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00029484776,0.00026754072,0.00016987434,0.00014656036,0.00011419042,0.00027912762,0.0002747437,0.00018186512,0.0004840029],"category_scores_gemma":[0.00083933875,0.0000829642,0.0001184639,0.00008734976,0.0002635859,0.00019615496,0.00021504759,0.00020654887,0.00005659068],"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":[0.00024766027,0.000049571412,0.00024473362,0.00020011832,0.000008896212,0.00008851306,0.00008273655,0.010102996,0.9557858,0.0011670305,0.00014811999,0.031873815],"study_design_scores_gemma":[0.000105615196,0.0009892298,0.0015302923,0.000019438774,0.000028893226,0.00020409704,0.000035036574,0.13862026,0.85336953,0.00048668895,0.004584255,0.000026680258],"about_ca_topic_score_codex":0.00012123687,"about_ca_topic_score_gemma":0.00015070803,"teacher_disagreement_score":0.0004840029,"about_ca_system_score_codex":0.000103115395,"about_ca_system_score_gemma":0.00012482429,"threshold_uncertainty_score":0.0016191006},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97456837,0.00042107428,0.021971313,0.000025015235,0.000031167194,0.000020553043,0.000048358306,0.00013749512,0.0027767008],"genre_scores_gemma":[0.9957379,0.00008284586,0.003595684,0.000009006741,0.0000081030485,0.00000574801,0.00003851096,0.000017835424,0.00050445634],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996512,0.000049035225,0.0000136669,0.00007139252,0.00016395267,0.00005071969],"domain_scores_gemma":[0.9987118,0.0004284721,0.00034263023,0.00011059602,0.00031129198,0.000095194715],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0007106317,0.00023637933,0.00040168889,0.00039384412,0.00032024024,0.0008824231,0.00036756942,0.0003901227,0.0009737223],"category_scores_gemma":[0.0019516551,0.0002658186,0.00030151533,0.0002762543,0.00049211364,0.00055158604,0.00032424758,0.0004125912,0.00025350394],"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":[0.000679645,0.00004538517,0.0022436874,0.00004883549,0.000011834519,0.00015434924,0.00018295877,0.0059673507,0.97651666,0.0019738993,0.00008648932,0.01208894],"study_design_scores_gemma":[0.00008457617,0.0009880727,0.013315722,0.000021547443,0.00003474331,0.00060228177,0.00014462636,0.0787913,0.9031433,0.00086830946,0.0019347498,0.000070784685],"about_ca_topic_score_codex":0.00018399148,"about_ca_topic_score_gemma":0.00011120544,"teacher_disagreement_score":0.0009737223,"about_ca_system_score_codex":0.0003442987,"about_ca_system_score_gemma":0.00021668285,"threshold_uncertainty_score":0.0037582517},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99548835,0.00009514708,0.004014887,0.000006040564,0.000004372185,0.000006044413,0.00005825295,0.000030542324,0.00029633156],"genre_scores_gemma":[0.9974226,0.00007250536,0.0019423687,0.000009273032,0.0000033557071,0.000008169824,0.0002744852,0.000017731723,0.00024959675],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999859,0.000007504521,0.000012711439,0.000020672802,0.000072407456,0.000027697582],"domain_scores_gemma":[0.99935573,0.0001592707,0.00017639782,0.000038466394,0.00017785019,0.00009226711],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021598318,0.00022260475,0.0002812607,0.00043931746,0.00020884923,0.0009413676,0.00017114638,0.00024680447,0.00038164793],"category_scores_gemma":[0.0008386596,0.0001941913,0.00018954021,0.0004340426,0.0002990955,0.00038049888,0.00024214071,0.0003066223,0.00008112554],"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":[0.00091845304,0.00010442097,0.062253855,0.00009155762,0.000026132793,0.00072552584,0.00036941326,0.00894024,0.9083283,0.0010994168,0.00012078566,0.017021967],"study_design_scores_gemma":[0.00011903379,0.0010631193,0.5707597,0.0000306799,0.0000823928,0.0014087656,0.00037950056,0.10723653,0.31556433,0.0012455657,0.0019099684,0.00020043162],"about_ca_topic_score_codex":0.0005155118,"about_ca_topic_score_gemma":0.00032803902,"teacher_disagreement_score":0.0009413676,"about_ca_system_score_codex":0.00023738551,"about_ca_system_score_gemma":0.00019003262,"threshold_uncertainty_score":0.0017223954},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98932403,0.00005003714,0.00973808,0.000014197619,0.0000086603595,0.0000065398012,0.0000079116735,0.000032439653,0.00081810105],"genre_scores_gemma":[0.9976413,0.000032604796,0.0019487884,0.0000034367824,0.0000051281413,0.0000048300476,0.000011105439,0.000004024337,0.00034872923],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999162,0.00001868015,0.0000047876006,0.000014222836,0.000028662611,0.000017492652],"domain_scores_gemma":[0.99977225,0.00009263176,0.0000621218,0.000012515691,0.00003240471,0.000028150855],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001638275,0.00027434662,0.00029782156,0.00049098814,0.00023873532,0.00041817073,0.0001869363,0.00022812356,0.0003554037],"category_scores_gemma":[0.0005255605,0.00017023903,0.00024461944,0.00023997911,0.0006355685,0.00026376316,0.00041271414,0.00016465326,0.00005507966],"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":[0.0006830848,0.00019633782,0.024688538,0.00013788926,0.000069139955,0.001588017,0.00043629835,0.43411478,0.49148592,0.009235117,0.00032977216,0.037035137],"study_design_scores_gemma":[0.000052805834,0.00026491398,0.009590752,0.0000069172183,0.000023366794,0.00016729742,0.000075567616,0.9514312,0.037108198,0.000867037,0.00039192502,0.000020114718],"about_ca_topic_score_codex":0.000904451,"about_ca_topic_score_gemma":0.0004403239,"teacher_disagreement_score":0.000904451,"about_ca_system_score_codex":0.00027412857,"about_ca_system_score_gemma":0.00022697433,"threshold_uncertainty_score":0.0019888878},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.5939869,0.00007366485,0.403587,0.000065077984,0.000019980567,0.00003262872,0.000064066415,0.00026010672,0.0019104185],"genre_scores_gemma":[0.9476353,0.00004888327,0.051877987,0.000008643729,0.000008970073,0.00001504444,0.0000627788,0.000031701926,0.0003108056],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997886,0.000057372567,0.000011640003,0.00004423011,0.000071929964,0.00002616729],"domain_scores_gemma":[0.9994659,0.00021568064,0.000065338725,0.000104757986,0.000103233644,0.00004523819],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00048993184,0.00024827482,0.00031624688,0.0004221089,0.0002552105,0.00052507536,0.0001928037,0.00016679712,0.00042086295],"category_scores_gemma":[0.0023625551,0.00015133488,0.0002714565,0.00037817002,0.0005012137,0.000302081,0.000609156,0.00039857998,0.00006075021],"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":[0.0015046404,0.0003108148,0.017060377,0.00025250105,0.00011735952,0.0009450129,0.0006117677,0.3100036,0.3678688,0.039571907,0.0007110388,0.2610422],"study_design_scores_gemma":[0.000032304924,0.00012641681,0.011018197,0.0000058961273,0.0000075114463,0.00021075284,0.000061237944,0.95168865,0.031885047,0.0043456024,0.00059621036,0.00002219614],"about_ca_topic_score_codex":0.00064890215,"about_ca_topic_score_gemma":0.00039712846,"teacher_disagreement_score":0.00064890215,"about_ca_system_score_codex":0.00017499544,"about_ca_system_score_gemma":0.00032698896,"threshold_uncertainty_score":0.0025910735},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.992148,0.00006651139,0.004137458,0.000056155553,0.000014407957,0.000006124684,0.000016880502,0.00007883093,0.0034756458],"genre_scores_gemma":[0.9987005,0.000012525689,0.000578026,0.000006406844,0.0000070388633,0.0000019935117,0.000007490895,0.000008421613,0.0006775148],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99987423,0.000034913697,0.0000044999197,0.00002567874,0.00003243662,0.000028181663],"domain_scores_gemma":[0.9994796,0.000246212,0.000064172105,0.00003656681,0.00007902854,0.00009445443],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00026373798,0.00027776044,0.0004510741,0.00023753129,0.00043346846,0.00042689283,0.00040920547,0.000597209,0.00138952],"category_scores_gemma":[0.00069864304,0.000252275,0.00018193536,0.00014378196,0.0009447658,0.00042460745,0.000650473,0.0004159971,0.00027139697],"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":[0.004477501,0.00044592816,0.015954012,0.00019309517,0.00004080551,0.004597074,0.0017943642,0.100317605,0.8380418,0.010724319,0.0012776208,0.022135913],"study_design_scores_gemma":[0.00020917009,0.0008214034,0.031551916,0.00004330405,0.000045715606,0.0013642453,0.00059528346,0.8201257,0.14131862,0.0021228653,0.0017242872,0.00007750558],"about_ca_topic_score_codex":0.0006880937,"about_ca_topic_score_gemma":0.00037599824,"teacher_disagreement_score":0.00138952,"about_ca_system_score_codex":0.00025318484,"about_ca_system_score_gemma":0.00020519659,"threshold_uncertainty_score":0.004648447},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9987544,0.0001695987,0.0007498147,0.000009851203,0.0000033992876,0.0000056025965,0.00001739344,0.000016685413,0.0002732303],"genre_scores_gemma":[0.99865925,0.00012573686,0.00089953316,0.000010602355,0.0000031324967,0.0000068174595,0.000043050662,0.000009119324,0.00024269601],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997733,0.0000388307,0.000016072998,0.000040221195,0.00007885509,0.000052596286],"domain_scores_gemma":[0.99959046,0.00016949917,0.00010315744,0.000022663751,0.00006342751,0.000050803264],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020303941,0.00026149332,0.00020524139,0.00024715016,0.00019247565,0.0005044941,0.00018966894,0.00017507722,0.00051156303],"category_scores_gemma":[0.0006380499,0.00017430203,0.00015828582,0.00015196462,0.00024623473,0.00021207717,0.00043075948,0.00035753634,0.0000740511],"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":[0.0001032326,0.0000171911,0.0015607695,0.000020486063,0.0000030724184,0.000047829348,0.00006119591,0.00021302939,0.99639136,0.000044255303,0.000010396456,0.0015271755],"study_design_scores_gemma":[0.000007862193,0.0003612183,0.012457831,0.0000056389217,0.000010443305,0.00006242685,0.000069397545,0.0037101575,0.9830289,0.000024306248,0.0002553235,0.000006548941],"about_ca_topic_score_codex":0.0010968148,"about_ca_topic_score_gemma":0.00091627013,"teacher_disagreement_score":0.0010968148,"about_ca_system_score_codex":0.00026256355,"about_ca_system_score_gemma":0.00014564798,"threshold_uncertainty_score":0.0021808147},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.92910826,0.00047562004,0.06185586,0.0001956298,0.0001972926,0.00006472712,0.00007891738,0.00056741777,0.007456408],"genre_scores_gemma":[0.99736685,0.00006459356,0.0014631065,0.00002363657,0.00000971755,0.000014518845,0.000021175321,0.00001373922,0.0010226201],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99981517,0.00002661769,0.000010140069,0.000033339325,0.000089587884,0.000025164161],"domain_scores_gemma":[0.99958056,0.00017374619,0.00004924094,0.00002344493,0.0001335757,0.000039443465],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023539692,0.0003434157,0.00027094968,0.00026210185,0.00033641036,0.00029645808,0.0003617528,0.00022162823,0.0009730593],"category_scores_gemma":[0.0005988517,0.00009545313,0.00016662116,0.00008018911,0.00025076853,0.00018602273,0.00024919474,0.00015997414,0.00015602504],"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":[0.0013739145,0.00025859175,0.003172459,0.00037171817,0.000030421454,0.0005745864,0.000388441,0.031443086,0.90321934,0.00087723735,0.00089446764,0.05739568],"study_design_scores_gemma":[0.00015730537,0.0014891649,0.014387426,0.000053478318,0.00008407858,0.000252739,0.00017574702,0.510748,0.46874282,0.0006679023,0.0031630753,0.000078324505],"about_ca_topic_score_codex":0.00083402783,"about_ca_topic_score_gemma":0.00090857275,"teacher_disagreement_score":0.0009730593,"about_ca_system_score_codex":0.0002689727,"about_ca_system_score_gemma":0.00017305404,"threshold_uncertainty_score":0.0032551885},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9973937,0.00009519083,0.0022234812,0.000004802882,0.000004182329,0.000008404925,0.000022913353,0.000024192208,0.00022316695],"genre_scores_gemma":[0.9988236,0.000086266205,0.00069121417,0.000008396234,0.0000026198047,0.0000046789423,0.00003765806,0.00000897507,0.00033659243],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997855,0.000015282394,0.0000095972655,0.00003789871,0.0001006358,0.000051114705],"domain_scores_gemma":[0.9989819,0.0005188138,0.00015653422,0.00005750653,0.00016168377,0.00012350279],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00028145735,0.0002735135,0.00027896932,0.00030112034,0.00019466439,0.0006027464,0.00022234977,0.0002930776,0.0010074793],"category_scores_gemma":[0.0013712948,0.00019064877,0.00019963984,0.00021803408,0.00040423998,0.0005481296,0.00047034485,0.00033500887,0.00013652911],"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":[0.00043682553,0.000030903382,0.004076346,0.00004031856,0.00000690353,0.00016406474,0.00011183431,0.0014405348,0.9882117,0.00006578483,0.0000138024725,0.005401012],"study_design_scores_gemma":[0.0000877437,0.003687509,0.1039621,0.000021352933,0.00006398787,0.00034016877,0.0004841611,0.026057567,0.86408746,0.00023429532,0.00091940875,0.000054159696],"about_ca_topic_score_codex":0.000853887,"about_ca_topic_score_gemma":0.0011343884,"teacher_disagreement_score":0.0010074793,"about_ca_system_score_codex":0.00021848983,"about_ca_system_score_gemma":0.0001903888,"threshold_uncertainty_score":0.003370285},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9911618,0.000097572716,0.0060929963,0.000049906364,0.0000118910075,0.000007579317,0.000020723754,0.00006826826,0.0024891759],"genre_scores_gemma":[0.9986749,0.000013293826,0.0005820723,0.0000071177215,0.000003782595,0.0000028280065,0.000010991368,0.00000984471,0.00069498306],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99991703,0.000021250655,0.0000024605915,0.000018578949,0.000017553899,0.000023062306],"domain_scores_gemma":[0.9996685,0.00015301672,0.00004429267,0.000032584485,0.000046508314,0.000055136738],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002496218,0.00022929063,0.00026960918,0.00028438045,0.00025227954,0.0003006797,0.00044391234,0.00041370222,0.002085221],"category_scores_gemma":[0.000667172,0.00022960782,0.00018014769,0.000110246416,0.000680212,0.0004312751,0.00047378635,0.00038168978,0.00022081996],"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":[0.00146666,0.00016902473,0.006047253,0.00016991136,0.00004625579,0.0013448757,0.0018764217,0.020486053,0.9379337,0.015130458,0.00075077807,0.014578564],"study_design_scores_gemma":[0.00040347668,0.0012579731,0.045699812,0.00008391843,0.0000809527,0.0012946653,0.0012728568,0.741594,0.19363523,0.011441322,0.0030573774,0.000178434],"about_ca_topic_score_codex":0.00023594857,"about_ca_topic_score_gemma":0.00021232644,"teacher_disagreement_score":0.002085221,"about_ca_system_score_codex":0.00015734727,"about_ca_system_score_gemma":0.00010355133,"threshold_uncertainty_score":0.0069757104},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9942971,0.000102783844,0.0045887385,0.000013332414,0.000019809524,0.0000111236395,0.000018011733,0.000041303803,0.00090780447],"genre_scores_gemma":[0.9974566,0.000053641295,0.001942009,0.000009577229,0.000004867168,0.0000047030107,0.00001215241,0.0000058156566,0.0005107542],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999485,0.000005323217,0.000003864864,0.000008778594,0.00001615983,0.000017323086],"domain_scores_gemma":[0.9998165,0.00006015893,0.000059753133,0.000016580287,0.000029361176,0.00001780667],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001129038,0.00019680278,0.00013033408,0.00016355887,0.00007507791,0.00018418964,0.00014137427,0.0001362933,0.0012242262],"category_scores_gemma":[0.0002738895,0.0000935448,0.00010452026,0.00007339364,0.00018173909,0.00011532289,0.00014265395,0.00013283544,0.00012523262],"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":[0.00020620694,0.000015923613,0.00070437073,0.000055212713,0.000003632672,0.000046533205,0.000040781368,0.00085473264,0.9896374,0.000082976316,0.000030132645,0.008321978],"study_design_scores_gemma":[0.000045597237,0.0010721721,0.00827635,0.000007430934,0.000017522643,0.00011015097,0.00004130126,0.01479673,0.97431684,0.000043127104,0.0012619529,0.000010708538],"about_ca_topic_score_codex":0.00032926945,"about_ca_topic_score_gemma":0.00049977435,"teacher_disagreement_score":0.0012242262,"about_ca_system_score_codex":0.00009888014,"about_ca_system_score_gemma":0.00008231046,"threshold_uncertainty_score":0.004095435},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9931545,0.00008036644,0.0060246415,0.0000070400574,0.000007809342,0.000009924427,0.00006190375,0.000053047697,0.0006006728],"genre_scores_gemma":[0.9966342,0.000050648185,0.0026712278,0.000008946971,0.0000064185447,0.000015120718,0.00020008204,0.000036679714,0.00037658948],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997788,0.000018453207,0.000015423217,0.000036568686,0.00011373034,0.000037053],"domain_scores_gemma":[0.99941504,0.00016311833,0.00015343496,0.000053019125,0.00011839337,0.00009694386],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00027282984,0.0002864305,0.0003597077,0.00051137607,0.000301168,0.00089360104,0.00017964406,0.00024519503,0.001109213],"category_scores_gemma":[0.0006988981,0.00025552945,0.00019318094,0.0004048223,0.00049710093,0.00034495842,0.00034487344,0.0003276655,0.00013553603],"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":[0.00086170906,0.00009823341,0.009110737,0.0000524625,0.000012821934,0.0004943827,0.00021167647,0.005048422,0.97379875,0.0008476698,0.00009714027,0.00936609],"study_design_scores_gemma":[0.0002212489,0.0017047647,0.18145292,0.000040207513,0.00006457897,0.0017358417,0.0005272137,0.07670327,0.73448014,0.0009921346,0.0018752842,0.00020238412],"about_ca_topic_score_codex":0.00021608328,"about_ca_topic_score_gemma":0.00018610968,"teacher_disagreement_score":0.001109213,"about_ca_system_score_codex":0.00019488428,"about_ca_system_score_gemma":0.0001554837,"threshold_uncertainty_score":0.0037106872},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.821066,0.0001231041,0.17319314,0.00012566819,0.000049741397,0.0000556594,0.000083939776,0.00062750495,0.0046752975],"genre_scores_gemma":[0.99049395,0.000043062093,0.008697629,0.000006838612,0.000005031912,0.000018182378,0.000045946934,0.000015922325,0.00067345443],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999206,0.000022291248,0.000004556754,0.000009709207,0.00003045275,0.00001249584],"domain_scores_gemma":[0.99983144,0.00006884117,0.000019576893,0.000014779457,0.000047859376,0.000017436476],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024841074,0.00053147116,0.0003611992,0.0002912187,0.00030953743,0.00037274303,0.00038872776,0.00033435348,0.00047694214],"category_scores_gemma":[0.00057665654,0.00016801649,0.00039935453,0.00018683849,0.0003811311,0.00032348398,0.00028389445,0.00033219293,0.00010209676],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00008510203,0.000033340293,0.0047364766,0.000015087904,0.000013928581,0.0001264494,0.000031245963,0.97933733,0.008012018,0.0016881695,0.00014359139,0.005777233],"study_design_scores_gemma":[0.0000024965466,0.000014648397,0.00027352574,4.6272459e-7,0.0000010190786,0.0000053770827,0.0000030660874,0.9987974,0.00078198133,0.00006652434,0.0000518356,0.0000016048067],"about_ca_topic_score_codex":0.014875272,"about_ca_topic_score_gemma":0.007438132,"teacher_disagreement_score":0.014875272,"about_ca_system_score_codex":0.00033547517,"about_ca_system_score_gemma":0.0007394785,"threshold_uncertainty_score":0.029577374},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7287918,0.0003134878,0.253079,0.00029342755,0.00032815005,0.0007508279,0.00066818425,0.0020828801,0.013692258],"genre_scores_gemma":[0.92736447,0.00013216579,0.06598444,0.00006547949,0.000019097333,0.00034592583,0.00047126753,0.00012540897,0.005491699],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9983418,0.00039085833,0.00010610703,0.00016313503,0.0008937878,0.000104305094],"domain_scores_gemma":[0.99761707,0.00051728246,0.00021822064,0.00035176813,0.0011949982,0.00010069575],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0024975212,0.0006558254,0.00074356433,0.0005833466,0.0006157646,0.00076396944,0.0010640357,0.0011494795,0.002103454],"category_scores_gemma":[0.003955986,0.00042747005,0.0003829083,0.00029205313,0.00071597134,0.0005193504,0.00060969096,0.000622758,0.0013762593],"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":[0.000946924,0.00066210364,0.015758894,0.00077150547,0.00005253281,0.0009683466,0.0009800368,0.49706918,0.37806004,0.0036724685,0.0032207281,0.09783728],"study_design_scores_gemma":[0.00020444368,0.0033115565,0.012942845,0.00008243352,0.00004681193,0.0003213732,0.00029787899,0.7972462,0.1701695,0.000568704,0.014705673,0.000102577746],"about_ca_topic_score_codex":0.002902109,"about_ca_topic_score_gemma":0.0031941372,"teacher_disagreement_score":0.002902109,"about_ca_system_score_codex":0.0007238297,"about_ca_system_score_gemma":0.0009171815,"threshold_uncertainty_score":0.01320833},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.002737227,0.000023893328,0.99620146,0.000021485987,0.0000094716615,0.00001358449,0.000009189184,0.00007152208,0.000912244],"genre_scores_gemma":[0.17243399,0.00022158517,0.8224364,0.000051640098,0.00007387613,0.00010777727,0.00010344447,0.00008759331,0.004483627],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99976045,0.00005210316,0.0000129450855,0.000038085003,0.00012086099,0.000015500907],"domain_scores_gemma":[0.99961144,0.00020407281,0.00003988811,0.00006827042,0.00006125881,0.000015025553],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003990491,0.00046721936,0.0003351641,0.00035060116,0.00018929802,0.0006495827,0.00051810715,0.00051021023,0.0022330573],"category_scores_gemma":[0.0011249755,0.00027025773,0.0005691824,0.0002636872,0.00058570685,0.0007022052,0.0007465161,0.00058520405,0.00043590393],"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":[0.00013115552,0.00009174635,0.0003966853,0.00018000019,0.000034829198,0.00016201321,0.00017009341,0.5042695,0.1464543,0.075272,0.0007404893,0.27209717],"study_design_scores_gemma":[0.000020443655,0.00008375243,0.0000964527,0.000009506675,0.000007821335,0.00012909369,0.000014503637,0.9649799,0.023380833,0.007955428,0.0033079395,0.000014275266],"about_ca_topic_score_codex":0.00026615846,"about_ca_topic_score_gemma":0.00024138558,"teacher_disagreement_score":0.0022330573,"about_ca_system_score_codex":0.0002488571,"about_ca_system_score_gemma":0.00033302914,"threshold_uncertainty_score":0},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9334854,0.00017329612,0.060752433,0.00012515883,0.000096462565,0.0000684022,0.00025636898,0.00039569568,0.0046467516],"genre_scores_gemma":[0.98735666,0.00006695847,0.01096072,0.000015116252,0.000014067501,0.000015309688,0.000092837276,0.000038392573,0.0014398005],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997131,0.00002943372,0.000011302639,0.00004655921,0.0001444255,0.000055085377],"domain_scores_gemma":[0.9994443,0.000284313,0.00002726799,0.000049809176,0.00013693102,0.000057342695],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000289941,0.0003063044,0.00040996724,0.0004958948,0.00064419775,0.0007295676,0.0005692388,0.00051570864,0.0012673711],"category_scores_gemma":[0.0007708663,0.0003038406,0.00034643142,0.00030680798,0.00072515296,0.0006845774,0.00060297304,0.00047522833,0.00022349456],"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":[0.001259723,0.00041022978,0.0037434099,0.00013306181,0.000047730704,0.00096751656,0.0005150837,0.037573583,0.919859,0.0032236944,0.00070647686,0.031560563],"study_design_scores_gemma":[0.00019128216,0.00076432206,0.019507207,0.000018686527,0.0000368677,0.00048522232,0.0003580898,0.43060878,0.5440407,0.0022944831,0.0015849964,0.00010938925],"about_ca_topic_score_codex":0.0025426669,"about_ca_topic_score_gemma":0.0020893458,"teacher_disagreement_score":0.0025426669,"about_ca_system_score_codex":0.0003143019,"about_ca_system_score_gemma":0.0005385297,"threshold_uncertainty_score":0.0050557256},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99200684,0.00011406792,0.0068367627,0.000022074748,0.00001169259,0.000009651315,0.00008793923,0.000099600984,0.0008113082],"genre_scores_gemma":[0.9988034,0.000059168327,0.00084836636,0.000004694626,0.0000024696249,0.000005585932,0.000089696565,0.000022712155,0.0001639926],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.99981576,0.000024172703,0.000013470557,0.00004202832,0.00004761134,0.00005705395],"domain_scores_gemma":[0.99868006,0.000765021,0.00016927309,0.0000964568,0.00016943977,0.00011976777],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004962684,0.00030494368,0.00037645194,0.00033449824,0.00039975063,0.00084572606,0.00022181659,0.0002786073,0.00097648473],"category_scores_gemma":[0.0028876984,0.00026828964,0.00029230633,0.00025027813,0.00043263723,0.0006224189,0.0004613461,0.00046091137,0.00014918148],"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":[0.0020825956,0.00030722082,0.034594562,0.00018716013,0.000054918135,0.0010218724,0.0006202102,0.18689407,0.7495519,0.0019017013,0.00034502568,0.022438757],"study_design_scores_gemma":[0.00007961607,0.0015896715,0.063679025,0.000044057277,0.00006695234,0.00027161377,0.00038045674,0.5253707,0.40714622,0.0005092785,0.00077682815,0.00008561382],"about_ca_topic_score_codex":0.0016879338,"about_ca_topic_score_gemma":0.0010224442,"teacher_disagreement_score":0.0016879338,"about_ca_system_score_codex":0.00033080237,"about_ca_system_score_gemma":0.00029138505,"threshold_uncertainty_score":0.0033562183},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9835016,0.0002351691,0.012457666,0.000080668564,0.000012419226,0.000018479603,0.000048732883,0.00004727607,0.0035979808],"genre_scores_gemma":[0.9977585,0.00007942656,0.001085504,0.000008991993,0.000008229796,0.0000068848735,0.000029352284,0.0000074585496,0.0010156486],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998648,0.000014806883,0.000005132801,0.00002759892,0.0000619106,0.000025820338],"domain_scores_gemma":[0.99943715,0.00020816253,0.00015174867,0.000026106678,0.0001232411,0.000053548883],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023068306,0.00054798985,0.0002751474,0.00041795138,0.00056723214,0.00086313114,0.00022748996,0.00034156896,0.0005291654],"category_scores_gemma":[0.0014687155,0.0001762218,0.00019346093,0.00021408137,0.0011017323,0.0004204716,0.00043314256,0.00032889674,0.00010476453],"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":[0.0019041327,0.0003093611,0.022436457,0.00018663384,0.00007709395,0.0020641931,0.00090002094,0.34697056,0.57989484,0.02663639,0.00061617343,0.018004114],"study_design_scores_gemma":[0.00006874103,0.00037008798,0.0074379863,0.000013212949,0.000017641434,0.00028944341,0.00013958364,0.9273508,0.06154529,0.0022852519,0.00044267546,0.000039205093],"about_ca_topic_score_codex":0.0034597225,"about_ca_topic_score_gemma":0.0013542139,"teacher_disagreement_score":0.0034597225,"about_ca_system_score_codex":0.0004963907,"about_ca_system_score_gemma":0.0003621586,"threshold_uncertainty_score":0.006879151},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9961367,0.000030254416,0.0033733784,0.000004720916,0.0000042872257,0.0000063695147,0.000020169417,0.000011276843,0.0004127499],"genre_scores_gemma":[0.99844676,0.0000324419,0.0012766344,0.0000037433942,0.0000033615208,0.0000036878475,0.000035726618,0.0000040413106,0.00019359324],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.99984825,0.000016904583,0.0000046676455,0.00003229918,0.000074263226,0.000023665001],"domain_scores_gemma":[0.99960285,0.00017472227,0.00006716431,0.000025273357,0.00009568578,0.000034284585],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020896575,0.00017610338,0.00015845707,0.00030814618,0.00017046872,0.00027460596,0.00013078252,0.00014849982,0.0007122095],"category_scores_gemma":[0.00087158533,0.00010499315,0.0000788997,0.00027130693,0.00035190882,0.00023549254,0.00011806445,0.00028664575,0.000096688505],"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":[0.00047968508,0.00006343911,0.0061792126,0.000032962223,0.000005919243,0.000112514856,0.00011577733,0.0029236434,0.9744012,0.00047827247,0.000031051906,0.0151762655],"study_design_scores_gemma":[0.00006567821,0.0030748022,0.1535721,0.000020872958,0.00003781324,0.00034812494,0.0003417566,0.05401682,0.786931,0.0004649678,0.0010640479,0.00006200558],"about_ca_topic_score_codex":0.0005105912,"about_ca_topic_score_gemma":0.0004034223,"teacher_disagreement_score":0.0007122095,"about_ca_system_score_codex":0.00014601635,"about_ca_system_score_gemma":0.00012319165,"threshold_uncertainty_score":0.0023825765},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9935452,0.00008729241,0.0033925197,0.000052631378,0.000019572346,0.0001146048,0.00091547245,0.00019648811,0.0016762972],"genre_scores_gemma":[0.9903756,0.00013887783,0.0063137966,0.00007444796,0.000020359776,0.00008341499,0.0009891775,0.000032262833,0.0019720588],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.9996898,0.000031433297,0.000010325219,0.00008132009,0.00013646099,0.0000505725],"domain_scores_gemma":[0.99977213,0.0000321694,0.000018163875,0.000010242673,0.00012551615,0.00004188213],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003479069,0.0006947069,0.00042357514,0.0010712873,0.00079051394,0.00030189301,0.0004877932,0.00043968845,0.0011817624],"category_scores_gemma":[0.00030303205,0.00019204704,0.0001846389,0.00061582687,0.00021239367,0.00017077522,0.00024677152,0.00035247992,0.00031161748],"study_design_candidate":"observational","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":[0.0008373215,0.0006630338,0.05607725,0.00013762173,0.0001449139,0.001110845,0.0012384414,0.011664889,0.87868345,0.00024145996,0.0022274745,0.046973404],"study_design_scores_gemma":[0.00016344123,0.0022186749,0.80326444,0.000031350504,0.0001409661,0.00035041268,0.0005520141,0.01825219,0.17087087,0.000038565784,0.0040034363,0.00011365272],"about_ca_topic_score_codex":0.164817,"about_ca_topic_score_gemma":0.40285587,"teacher_disagreement_score":0.835183,"about_ca_system_score_codex":0.001093607,"about_ca_system_score_gemma":0.0013512373,"threshold_uncertainty_score":0.32771534},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99138534,0.000111454756,0.006799815,0.000024517964,0.000024338742,0.000006567974,0.000008718354,0.000027329655,0.0016120146],"genre_scores_gemma":[0.9979584,0.000035965368,0.0013150261,0.000011724874,0.000008245665,0.000004018938,0.000015909556,0.0000056007693,0.00064508285],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997799,0.000020903544,0.0000076283072,0.00004486352,0.00009825548,0.00004858885],"domain_scores_gemma":[0.99974924,0.00009216086,0.000064430875,0.000018575302,0.000040851963,0.000034603523],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00013733197,0.00023223867,0.00031878785,0.00019914343,0.00017923208,0.00049122877,0.00028083226,0.00037878047,0.00073629525],"category_scores_gemma":[0.0005745353,0.00018332043,0.00020352416,0.00013001074,0.00049266557,0.000357723,0.00068776566,0.00029259242,0.00009906522],"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":[0.0003484426,0.00004188984,0.0020152815,0.00007576985,0.000025709714,0.0006556953,0.00019301071,0.0085464,0.97545177,0.0016381209,0.0000829411,0.010924932],"study_design_scores_gemma":[0.00015844656,0.0011619088,0.030749582,0.000029026798,0.00007677987,0.001325532,0.0006436822,0.30344948,0.6564877,0.0017656304,0.004058925,0.000093284965],"about_ca_topic_score_codex":0.00017435288,"about_ca_topic_score_gemma":0.00013722465,"teacher_disagreement_score":0.00073629525,"about_ca_system_score_codex":0.00014248946,"about_ca_system_score_gemma":0.00011129624,"threshold_uncertainty_score":0.002463162},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97939175,0.00004342382,0.019628845,0.000025651447,0.000008091331,0.000010912765,0.000018316201,0.00005700626,0.000816153],"genre_scores_gemma":[0.9980837,0.000020755882,0.0013574071,0.0000030076196,0.0000015412514,0.000006803466,0.000010537978,0.0000049601076,0.0005112339],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99992657,0.000011108247,0.000002464838,0.00002373403,0.000019800553,0.000016322087],"domain_scores_gemma":[0.99984145,0.00006210843,0.000032553682,0.000013113913,0.000023130144,0.000027581173],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001580097,0.00044416182,0.00044100484,0.0002046409,0.00030213717,0.00047225534,0.0005531286,0.0005694347,0.00069835014],"category_scores_gemma":[0.0004158518,0.00026831703,0.00032149418,0.00009043695,0.00065694074,0.00031706897,0.0004893846,0.000358985,0.00007270727],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00025001515,0.0001365905,0.0068092216,0.00009825961,0.000033893422,0.0009978233,0.0003194981,0.7441725,0.23997931,0.0032585773,0.00013093406,0.0038133103],"study_design_scores_gemma":[0.000008158426,0.00007404041,0.0007970151,0.0000017689662,0.0000044768735,0.000025613243,0.000023656907,0.9955449,0.0033064862,0.00013581695,0.000072083705,0.0000059264503],"about_ca_topic_score_codex":0.0044409824,"about_ca_topic_score_gemma":0.0018720814,"teacher_disagreement_score":0.0044409824,"about_ca_system_score_codex":0.0003393626,"about_ca_system_score_gemma":0.0005639008,"threshold_uncertainty_score":0.008830309},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9924374,0.000074976844,0.0047606216,0.00005328288,0.00001630068,0.000044050936,0.00044623617,0.00022162152,0.0019454701],"genre_scores_gemma":[0.99819034,0.000032291817,0.0010420333,0.000012314752,0.000002786237,0.000026800157,0.0001956659,0.000022725331,0.00047510758],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99984,0.000025155334,0.00001867985,0.00002996866,0.000055518267,0.00003059954],"domain_scores_gemma":[0.9987206,0.00085207715,0.00008065162,0.000066224326,0.00019629592,0.0000841636],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00039771816,0.00040936703,0.0005223488,0.00052512065,0.00044771066,0.0004928192,0.00051564525,0.0011706437,0.0017344954],"category_scores_gemma":[0.0016288931,0.00028357716,0.00047649705,0.00028889056,0.00051788596,0.00046359395,0.0003316964,0.00043570157,0.00027931132],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.001421069,0.0003690591,0.023322396,0.00028711298,0.000082518214,0.0012048087,0.0008117241,0.8605435,0.09403388,0.00093860575,0.0011260101,0.015859352],"study_design_scores_gemma":[0.000075492055,0.00042098662,0.013065795,0.000022684168,0.000031829008,0.00013539285,0.00023541723,0.9655141,0.019690314,0.00024287142,0.0005118574,0.000053318203],"about_ca_topic_score_codex":0.0059098587,"about_ca_topic_score_gemma":0.002904776,"teacher_disagreement_score":0.0059098587,"about_ca_system_score_codex":0.00039229635,"about_ca_system_score_gemma":0.0003258792,"threshold_uncertainty_score":0.0117509365},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.360901,0.00033763296,0.6184829,0.00023083853,0.00012265185,0.0002296159,0.00026543142,0.0007672697,0.018662667],"genre_scores_gemma":[0.97133183,0.00014548982,0.02536612,0.00002609581,0.000027119722,0.00013283825,0.00010956694,0.00006110976,0.0027998784],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997938,0.000053656142,0.000009574527,0.00003901435,0.00007713821,0.000026844233],"domain_scores_gemma":[0.9995919,0.00019076896,0.00003872906,0.000030753596,0.00011309005,0.000034771772],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004205676,0.00084116025,0.000633949,0.00047106028,0.00040686832,0.00051854335,0.0011630334,0.0010987734,0.002019333],"category_scores_gemma":[0.0010355632,0.00031500746,0.0006556751,0.00021377704,0.00044237403,0.0005668917,0.00059802725,0.00062591524,0.00038179365],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000040122235,0.000038676953,0.0004857806,0.000022373233,0.000007406503,0.0000654703,0.000024912299,0.9908981,0.004439907,0.0012876583,0.00009139049,0.0025981935],"study_design_scores_gemma":[0.0000016116425,0.000010624897,0.00004603618,8.8267944e-7,9.333896e-7,0.0000031274012,0.0000015787772,0.99957496,0.00026561206,0.000050438095,0.00004276957,0.0000013802631],"about_ca_topic_score_codex":0.010204622,"about_ca_topic_score_gemma":0.004978954,"teacher_disagreement_score":0.010204622,"about_ca_system_score_codex":0.0005964209,"about_ca_system_score_gemma":0.0009708248,"threshold_uncertainty_score":0.020290434},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.19314276,0.00016512506,0.7976693,0.00015870294,0.00007236491,0.00008368043,0.00027895102,0.0010166625,0.0074124425],"genre_scores_gemma":[0.6594799,0.00019020632,0.33418626,0.0000777662,0.000027322336,0.00013616048,0.0004010585,0.00016712859,0.00533426],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99993503,0.000009350914,0.000003176368,0.000010828626,0.000027410993,0.000014117157],"domain_scores_gemma":[0.9997782,0.000088082634,0.000023776925,0.000022560997,0.00006051695,0.000026852826],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002659601,0.00030431314,0.00046618056,0.00025703682,0.00018370748,0.00040557125,0.0005561424,0.0005088244,0.0019218662],"category_scores_gemma":[0.0006698125,0.00022407,0.0003507349,0.00020403576,0.00045156755,0.0003069051,0.00044374753,0.00041228236,0.00027265665],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0001130699,0.000036271522,0.0016315244,0.00008351775,0.000026999187,0.00034032177,0.00009940088,0.9230444,0.04035579,0.012318218,0.0012027927,0.020747734],"study_design_scores_gemma":[0.000019748408,0.000017246794,0.00019947677,0.000003395943,0.000002405564,0.000033575016,0.000010822999,0.9964747,0.0020195495,0.00044361476,0.0007718495,0.000003628322],"about_ca_topic_score_codex":0.0034832438,"about_ca_topic_score_gemma":0.0029603916,"teacher_disagreement_score":0.0034832438,"about_ca_system_score_codex":0.00020316453,"about_ca_system_score_gemma":0.0007221341,"threshold_uncertainty_score":0.0069259405},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.3092798,0.00013441104,0.6891842,0.00014619136,0.000029048166,0.00003555541,0.00008880749,0.0002779073,0.00082409254],"genre_scores_gemma":[0.91209245,0.00004818785,0.0869687,0.00002349373,0.0000084492385,0.000031922933,0.00010653122,0.000051521172,0.00066870183],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99908483,0.00039204254,0.00004390427,0.000106144085,0.00031598055,0.000057022295],"domain_scores_gemma":[0.9966241,0.0023153238,0.00020309423,0.00030109505,0.00050469104,0.000051723895],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0018388097,0.00048315316,0.00048269556,0.00035078707,0.00052946,0.00066794915,0.0007619181,0.0006121732,0.0005790598],"category_scores_gemma":[0.0053924336,0.00031334208,0.00042172783,0.00037200536,0.00058854936,0.0012304162,0.0005317268,0.0006366953,0.00006758928],"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":[0.0012506677,0.00012266454,0.00303706,0.00013328399,0.00008923499,0.00007189981,0.0002615748,0.84427214,0.052215878,0.01082276,0.00037294356,0.08734987],"study_design_scores_gemma":[0.0000078730545,0.000046731548,0.00091731705,0.0000030096728,0.000011146825,0.000010097147,0.000017926912,0.9758995,0.021846704,0.0010362332,0.00018548126,0.000017966515],"about_ca_topic_score_codex":0.0025991474,"about_ca_topic_score_gemma":0.0023007942,"teacher_disagreement_score":0.0025991474,"about_ca_system_score_codex":0.0007452083,"about_ca_system_score_gemma":0.00048019833,"threshold_uncertainty_score":0.009724617},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9988036,0.00007648953,0.00082947046,0.0000070861806,0.0000039436286,0.0000054366255,0.000049910916,0.000019866713,0.00020420193],"genre_scores_gemma":[0.99849474,0.0000873406,0.00076997397,0.0000070885308,0.0000018821647,0.000007465178,0.00012221752,0.000013634682,0.0004955232],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998692,0.0000094167,0.000004767784,0.000032841315,0.00004249066,0.000041261752],"domain_scores_gemma":[0.99969494,0.00009828828,0.00007221133,0.000019370947,0.00008433244,0.000030809024],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020262206,0.00022058617,0.00026853124,0.000252545,0.00026494975,0.00034784852,0.00019212176,0.00033579802,0.0014174181],"category_scores_gemma":[0.00038040837,0.00014186406,0.00014287829,0.00018373097,0.00039189844,0.0003061021,0.000251547,0.00049617304,0.00016614806],"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":[0.00020705139,0.000022871936,0.0020669214,0.000023015782,0.0000043176474,0.0001116162,0.000104866915,0.0005300864,0.99532133,0.000078882935,0.000023884926,0.001505244],"study_design_scores_gemma":[0.000017814331,0.00093049044,0.024896543,0.000007318842,0.000015185558,0.000080312144,0.00019668251,0.006533511,0.9666003,0.0000775807,0.00062438997,0.000019888757],"about_ca_topic_score_codex":0.0017015517,"about_ca_topic_score_gemma":0.0016908137,"teacher_disagreement_score":0.0017015517,"about_ca_system_score_codex":0.00033048025,"about_ca_system_score_gemma":0.0002057899,"threshold_uncertainty_score":0.004741788},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99461657,0.0001442541,0.0038135273,0.000023510258,0.00004221846,0.000022857877,0.00006366413,0.00007894625,0.0011945025],"genre_scores_gemma":[0.9944364,0.000155643,0.003838792,0.00001817089,0.00001854112,0.000017010136,0.000100828875,0.000039796665,0.0013749531],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9991456,0.00006486576,0.000041139272,0.00018365918,0.00036779317,0.00019691995],"domain_scores_gemma":[0.99814403,0.00062505744,0.00030639564,0.00037762066,0.0004000316,0.00014684026],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00065281405,0.0008842899,0.00073639833,0.00031787527,0.00080389896,0.0008385849,0.0010015101,0.0011507027,0.0035753897],"category_scores_gemma":[0.0020580862,0.0005468701,0.00028735417,0.00079888676,0.0012286806,0.0010280688,0.0011567175,0.0011548563,0.00052337867],"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":[0.0012570292,0.0003493002,0.0013109193,0.00014015881,0.000010870613,0.0002461783,0.00021859002,0.002761743,0.98649615,0.0005963553,0.00012331753,0.006489391],"study_design_scores_gemma":[0.00012465681,0.00414981,0.0077142776,0.000018929231,0.000042840893,0.00021649746,0.00022343076,0.013845554,0.9718085,0.00030203752,0.0015116547,0.000041854953],"about_ca_topic_score_codex":0.00030591537,"about_ca_topic_score_gemma":0.00031273116,"teacher_disagreement_score":0.0035753897,"about_ca_system_score_codex":0.00035671412,"about_ca_system_score_gemma":0.0003239781,"threshold_uncertainty_score":0.011960864},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99875367,0.00012998415,0.0009503172,0.000004165717,0.00001190745,0.000005003425,0.000009618883,0.00001695047,0.00011832191],"genre_scores_gemma":[0.9986333,0.00008854963,0.001063478,0.0000059019258,0.0000056707895,0.0000033074616,0.00001317637,0.0000063809803,0.00018008941],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997292,0.00005102475,0.000022561073,0.00007342829,0.0000653322,0.00005844195],"domain_scores_gemma":[0.9991775,0.00026064762,0.00031210788,0.00009446948,0.00007282381,0.00008249398],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00028223096,0.0004982539,0.00029485085,0.00012144007,0.00018002164,0.0003250374,0.00029726472,0.00028315812,0.00049408706],"category_scores_gemma":[0.0007408999,0.00019351259,0.00018693347,0.000073119445,0.00030735898,0.00026582446,0.00020649137,0.00016906318,0.000079664125],"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":[0.00080196845,0.000075353804,0.000915517,0.00009243801,0.000013416208,0.0001407781,0.000041408468,0.0014004523,0.9939195,0.00003679845,0.000013334139,0.0025489933],"study_design_scores_gemma":[0.000036987458,0.00423978,0.011228349,0.0000081025555,0.00006791347,0.00013168772,0.000054550754,0.005019703,0.97875655,0.000010988874,0.00042623386,0.000019198193],"about_ca_topic_score_codex":0.00030469926,"about_ca_topic_score_gemma":0.00032662443,"teacher_disagreement_score":0.0004982539,"about_ca_system_score_codex":0.0001370016,"about_ca_system_score_gemma":0.000082484104,"threshold_uncertainty_score":0.0016528964},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8699375,0.00017407948,0.12850711,0.000033251166,0.000012566336,0.00002801375,0.000074612624,0.00012473568,0.0011082089],"genre_scores_gemma":[0.97933674,0.000071961025,0.020157829,0.000006306754,0.000008850264,0.000008802923,0.000064396954,0.000013560501,0.00033139344],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99982554,0.00002552816,0.000007853359,0.000030831212,0.00008335613,0.000026960513],"domain_scores_gemma":[0.99960333,0.00020113739,0.00005965534,0.000031254105,0.00007124872,0.00003337851],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00031948643,0.00019550946,0.0002626086,0.00062371785,0.00016249172,0.0004588821,0.00016580685,0.00017965092,0.00037967783],"category_scores_gemma":[0.0010731928,0.00015764537,0.00017105178,0.0002465916,0.00043908783,0.0005805491,0.00026693888,0.00019076622,0.00005183068],"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":[0.00044685235,0.00022834413,0.027898377,0.00024252228,0.00008758163,0.0006985988,0.00033942398,0.08566234,0.76726663,0.008163833,0.0002979149,0.10866759],"study_design_scores_gemma":[0.000043138418,0.00043921068,0.06717024,0.0000149247535,0.000030896626,0.00033908026,0.00016857286,0.8154763,0.11259382,0.0028197425,0.00084964914,0.000054504562],"about_ca_topic_score_codex":0.00045094747,"about_ca_topic_score_gemma":0.00043070098,"teacher_disagreement_score":0.00062371785,"about_ca_system_score_codex":0.00018164692,"about_ca_system_score_gemma":0.00020824456,"threshold_uncertainty_score":0.0016896129},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9909376,0.00012753031,0.008149985,0.000012578163,0.000015386766,0.000009756194,0.000030573872,0.000052919946,0.00066366233],"genre_scores_gemma":[0.997195,0.00006450788,0.0022783,0.00000681955,0.0000061402206,0.0000063123593,0.000045858247,0.000015960595,0.00038111123],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9996226,0.000090062975,0.000025289506,0.000053176598,0.00014049665,0.00006839559],"domain_scores_gemma":[0.99742883,0.0014070144,0.0002132445,0.00012802682,0.00069428905,0.00012869926],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00064098835,0.0004922858,0.00028596117,0.00056554325,0.00023121043,0.00026101506,0.0001556886,0.00024643508,0.0012289134],"category_scores_gemma":[0.0024315235,0.00017015755,0.00020871447,0.00021261757,0.0003800713,0.00029358128,0.00015087424,0.0001550724,0.00022096779],"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":[0.0011778174,0.00013102088,0.009381303,0.00014652024,0.00002733947,0.0002595347,0.00026787026,0.0061909487,0.9493925,0.00021311027,0.000100252764,0.032711685],"study_design_scores_gemma":[0.00009425236,0.00432732,0.048142396,0.000030159474,0.00009616909,0.0008813672,0.00032891298,0.022745071,0.92060775,0.0001928474,0.0024849402,0.00006890733],"about_ca_topic_score_codex":0.00041229476,"about_ca_topic_score_gemma":0.0004779577,"teacher_disagreement_score":0.0012289134,"about_ca_system_score_codex":0.00014337234,"about_ca_system_score_gemma":0.00011439531,"threshold_uncertainty_score":0.0041110516},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9836293,0.00044079078,0.005430588,0.0001264867,0.000031196603,0.000023507437,0.000049839437,0.00010453097,0.010163808],"genre_scores_gemma":[0.99809366,0.00007704229,0.00055108365,0.000010238592,0.000010644126,0.000006173504,0.000021526655,0.000033331537,0.0011962333],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999113,0.000016883787,0.000003753085,0.000016852659,0.000020861124,0.000030420973],"domain_scores_gemma":[0.9991035,0.00052388647,0.00010696164,0.00003464478,0.00009781161,0.00013322997],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017233855,0.00035300726,0.000435583,0.0005001051,0.00070351845,0.001115095,0.00041044847,0.00042717042,0.001526271],"category_scores_gemma":[0.0011726349,0.00042281512,0.00022406745,0.0002114841,0.0008667797,0.00060331885,0.0005342779,0.00071368855,0.00022140605],"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":[0.0046266606,0.00068085373,0.018119594,0.00022058442,0.0000616084,0.004909928,0.0009059312,0.3135417,0.6078228,0.028130038,0.0015000984,0.019480273],"study_design_scores_gemma":[0.00042175635,0.001060405,0.0730202,0.00004083114,0.00013267926,0.0010646138,0.00040223822,0.76865226,0.14838554,0.004276166,0.0023245765,0.00021880245],"about_ca_topic_score_codex":0.0024543155,"about_ca_topic_score_gemma":0.001292114,"teacher_disagreement_score":0.0024543155,"about_ca_system_score_codex":0.0006041497,"about_ca_system_score_gemma":0.0004776521,"threshold_uncertainty_score":0.005105853},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9988933,0.000047813235,0.0008443938,0.000013536958,0.00001147799,0.00002173902,0.000036930614,0.000007362998,0.00012349915],"genre_scores_gemma":[0.9976349,0.00012594757,0.0016467066,0.000020290263,0.00001290776,0.000027911117,0.00007543724,0.0000072482103,0.0004486431],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9996588,0.00005225989,0.00003414088,0.000067771485,0.00009622446,0.000090940295],"domain_scores_gemma":[0.998892,0.000534935,0.00019108788,0.00007701227,0.00015146802,0.00015342604],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006146292,0.00045520935,0.00046817565,0.00027026443,0.00060130045,0.00058161886,0.00029446065,0.00047123907,0.0005806883],"category_scores_gemma":[0.0013019169,0.00018810405,0.00045395488,0.00021348048,0.0006475964,0.00054931134,0.00050878583,0.0010445726,0.00007828478],"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":[0.0016037964,0.002017142,0.0053636804,0.00006764751,0.00002329181,0.00018265021,0.0002573458,0.003363377,0.981964,0.00020992958,0.00005593508,0.004891286],"study_design_scores_gemma":[0.00036903223,0.025517995,0.0332188,0.000024042338,0.00009942053,0.00018387994,0.00030258027,0.042970546,0.8964253,0.00024336543,0.0005772602,0.00006783293],"about_ca_topic_score_codex":0.0029091837,"about_ca_topic_score_gemma":0.0022768213,"teacher_disagreement_score":0.0029091837,"about_ca_system_score_codex":0.0004133021,"about_ca_system_score_gemma":0.00037965248,"threshold_uncertainty_score":0.0057845116},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9967025,0.00008196984,0.0026938554,0.00001217208,0.0000064974492,0.000007008715,0.00001688006,0.000021379174,0.0004577366],"genre_scores_gemma":[0.9992605,0.000046666748,0.00054390146,0.0000080947375,0.000001915352,0.0000021869669,0.0000108747445,0.000004870412,0.0001210456],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99981946,0.000033911736,0.000013176053,0.000026940583,0.000057075275,0.000049394203],"domain_scores_gemma":[0.99907386,0.0005934116,0.00011419881,0.00005294793,0.00009125011,0.00007426794],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00047111846,0.00035510008,0.00031370166,0.00022852125,0.00024144033,0.00054379815,0.00018264992,0.00027003212,0.0007993147],"category_scores_gemma":[0.0012848912,0.0001722592,0.00031153669,0.0001505407,0.0005484923,0.0002915707,0.00057545985,0.0003266478,0.00010236523],"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":[0.0025299536,0.00016356986,0.020036746,0.00015532557,0.00004234136,0.00069273904,0.00027894895,0.15821488,0.801473,0.00061051303,0.00007710807,0.015724871],"study_design_scores_gemma":[0.0001997044,0.003289283,0.061059244,0.000042970783,0.0001300833,0.0002912818,0.00041108744,0.23589432,0.69742763,0.00040995993,0.00073806796,0.0001063872],"about_ca_topic_score_codex":0.0008728469,"about_ca_topic_score_gemma":0.0009697782,"teacher_disagreement_score":0.0008728469,"about_ca_system_score_codex":0.00040665644,"about_ca_system_score_gemma":0.000207249,"threshold_uncertainty_score":0.0029504895},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97862417,0.00047024596,0.018602569,0.000032545584,0.000033005806,0.000032244334,0.00006975871,0.00012884285,0.0020065769],"genre_scores_gemma":[0.99601954,0.00011378217,0.0031431073,0.000011215577,0.000005549932,0.000013678735,0.00008559358,0.00001073864,0.00059671607],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998907,0.000011160665,0.000003953817,0.000028778284,0.000030364781,0.000035036446],"domain_scores_gemma":[0.99944764,0.00018646297,0.00014615283,0.00005240005,0.00007366259,0.000093649025],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018338581,0.00012433238,0.00024248702,0.00030673953,0.00022006182,0.00040563583,0.00015947917,0.00019257478,0.0007995497],"category_scores_gemma":[0.00062439765,0.00014204964,0.00015135796,0.00013814867,0.0003524613,0.00027903184,0.00026422727,0.0003036252,0.00012205582],"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":[0.0001638455,0.00006623474,0.0050252136,0.000071962226,0.000011176516,0.0003914239,0.00014154866,0.0034931763,0.97284627,0.0037657737,0.00019219727,0.013831276],"study_design_scores_gemma":[0.00009911069,0.0012833617,0.046692137,0.000030427285,0.000026082413,0.0011911485,0.00017564182,0.07070958,0.8691859,0.0030016736,0.0075552077,0.00004968328],"about_ca_topic_score_codex":0.0001347438,"about_ca_topic_score_gemma":0.00008346866,"teacher_disagreement_score":0.0007995497,"about_ca_system_score_codex":0.00024805384,"about_ca_system_score_gemma":0.00014398199,"threshold_uncertainty_score":0.0026746988},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99718803,0.00019865824,0.000888883,0.000027752398,0.000028317558,0.0000039195256,0.00005569688,0.00002904529,0.0015797452],"genre_scores_gemma":[0.9992415,0.00008358812,0.00022684628,0.000011291232,0.0000052158744,0.000001412653,0.000021580987,0.000019802239,0.00038873294],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997851,0.000037935253,0.000013517552,0.00003563932,0.00005223171,0.00007561772],"domain_scores_gemma":[0.9986744,0.00082155946,0.000179101,0.00008427117,0.00015199873,0.00008868527],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00033512292,0.0003050856,0.0003445898,0.00021727597,0.00025239552,0.0007306127,0.00029785337,0.00038252192,0.0038448262],"category_scores_gemma":[0.0014200717,0.00035076766,0.0002411153,0.00022011934,0.0004510646,0.0004979925,0.00034902376,0.00034021912,0.0002182325],"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":[0.0027384225,0.00011515986,0.0018814452,0.00016289097,0.0000373633,0.0005083146,0.00013209076,0.015573204,0.9720685,0.00036534906,0.0001546455,0.0062626116],"study_design_scores_gemma":[0.000105029954,0.0010502945,0.015436021,0.000032290147,0.00013848308,0.0001955407,0.00023364977,0.024880989,0.9571665,0.00009519155,0.00061724114,0.00004872896],"about_ca_topic_score_codex":0.00048539686,"about_ca_topic_score_gemma":0.0005060006,"teacher_disagreement_score":0.0038448262,"about_ca_system_score_codex":0.0002591602,"about_ca_system_score_gemma":0.00020073164,"threshold_uncertainty_score":0.0128622055},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9954983,0.00008100701,0.0033911925,0.000025091906,0.000013200456,0.000007759408,0.000105509374,0.000120778735,0.0007572866],"genre_scores_gemma":[0.9986749,0.000038190985,0.0008769726,0.0000072378807,0.000016685217,0.0000045768793,0.000089219255,0.000009574809,0.0002826578],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996662,0.00003472107,0.000011411553,0.000093190225,0.00015216565,0.000042315605],"domain_scores_gemma":[0.9987,0.00051916874,0.0002970249,0.00007189866,0.00028216364,0.00012968435],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003053271,0.00037186284,0.00043658464,0.0011385368,0.0002452537,0.0006343551,0.00028731965,0.00035602055,0.0013702373],"category_scores_gemma":[0.0015680022,0.00034890432,0.0001790114,0.000700387,0.00043887045,0.0007346135,0.00055284426,0.0008055361,0.00029476595],"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":[0.0027497492,0.00044163296,0.12779178,0.0002735754,0.000121366626,0.0027301204,0.0013590921,0.03069486,0.75377315,0.0010861967,0.00070522487,0.0782732],"study_design_scores_gemma":[0.00007094126,0.0010565779,0.80750054,0.000031552885,0.000055633926,0.0012224322,0.00049219804,0.10342792,0.08480758,0.0005500688,0.0006150089,0.00016952338],"about_ca_topic_score_codex":0.00088695396,"about_ca_topic_score_gemma":0.000782038,"teacher_disagreement_score":0.0013702373,"about_ca_system_score_codex":0.00016462345,"about_ca_system_score_gemma":0.00012772008,"threshold_uncertainty_score":0.004583955},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.30438945,0.00073099375,0.6851578,0.00010392354,0.0001357702,0.00005690556,0.00012367016,0.00047272834,0.00882873],"genre_scores_gemma":[0.9762725,0.00030532683,0.021020772,0.000019795532,0.000026600126,0.000020640768,0.00007524259,0.000064510066,0.0021945965],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99993324,0.000015341111,0.000002712258,0.0000121564935,0.000026928496,0.000009611452],"domain_scores_gemma":[0.9998697,0.000067171226,0.000015438085,0.000011133558,0.000025998692,0.000010447146],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00014268211,0.00053247815,0.00023983546,0.00015360604,0.00017188267,0.00025978737,0.00022477099,0.00020490645,0.0016482703],"category_scores_gemma":[0.0005077433,0.00011963303,0.00016824831,0.00011184458,0.0002624099,0.00022723612,0.00024553775,0.0001757062,0.00015305194],"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":[0.0015793972,0.00009681201,0.0010367663,0.0003176748,0.00005895416,0.00021087506,0.00018430075,0.120732084,0.6441296,0.003834348,0.00089741504,0.22692177],"study_design_scores_gemma":[0.000059071044,0.00027412164,0.0061117695,0.000020014135,0.00004973228,0.00018122308,0.0000503487,0.8783316,0.11004375,0.0015700529,0.0032761432,0.000032078722],"about_ca_topic_score_codex":0.0009436013,"about_ca_topic_score_gemma":0.0013765543,"teacher_disagreement_score":0.0016482703,"about_ca_system_score_codex":0.000107881344,"about_ca_system_score_gemma":0.00013138348,"threshold_uncertainty_score":0.0055140257},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.728114,0.0008582584,0.25681135,0.00047253896,0.00014764379,0.00009893804,0.00014926496,0.0003630577,0.012984868],"genre_scores_gemma":[0.9867555,0.00022219575,0.008985135,0.00007099379,0.00005038488,0.000029614152,0.00007358169,0.00003902408,0.0037735815],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996275,0.00004931497,0.00001549861,0.00008787471,0.00015483653,0.000064994216],"domain_scores_gemma":[0.99935097,0.00018288725,0.00021404127,0.000050307957,0.00013476839,0.00006704335],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003889948,0.00043988507,0.0005617595,0.0006916388,0.00032542157,0.0015765032,0.00073177106,0.000789913,0.00088203256],"category_scores_gemma":[0.0018538816,0.00039574623,0.00062965835,0.00037316754,0.000969563,0.0016241255,0.0009824211,0.00092637114,0.00020487013],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00019778154,0.0001264731,0.012107486,0.00015523983,0.00007796865,0.0027353694,0.00084979,0.48506078,0.07071312,0.39891952,0.0020991266,0.026957264],"study_design_scores_gemma":[0.000021624668,0.00003605698,0.0038307128,0.0000066948264,0.000007794463,0.00028855694,0.000051486208,0.97777224,0.0027432404,0.014523129,0.0006671197,0.000051501185],"about_ca_topic_score_codex":0.004417734,"about_ca_topic_score_gemma":0.0016433186,"teacher_disagreement_score":0.004417734,"about_ca_system_score_codex":0.0008845414,"about_ca_system_score_gemma":0.0007303607,"threshold_uncertainty_score":0.008784056},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.983573,0.00006194643,0.01441705,0.000050184844,0.000007416213,0.000020999109,0.00003647409,0.00020267646,0.0016302831],"genre_scores_gemma":[0.9981749,0.000022346647,0.001424503,0.0000045834263,0.0000023990451,0.0000072816288,0.000012429897,0.000008294258,0.00034334665],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99983406,0.00002745859,0.0000037067823,0.000029300294,0.00008637662,0.000019026613],"domain_scores_gemma":[0.99966586,0.0001371054,0.00006445161,0.000019550442,0.00007679159,0.000036279805],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017508323,0.00028426823,0.0002853155,0.00015724466,0.0002138066,0.00022159844,0.00024155433,0.00028525863,0.00056533766],"category_scores_gemma":[0.00059396005,0.00023116963,0.00012923415,0.00012231423,0.0005513894,0.00023447761,0.00044861974,0.00025250408,0.00013857178],"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":[0.0001746808,0.000034851662,0.0015240936,0.00006304805,0.000008147598,0.00041781995,0.00017592477,0.010797578,0.9817563,0.00068972906,0.00010877314,0.004248947],"study_design_scores_gemma":[0.0003230764,0.001977286,0.027340364,0.000040713967,0.000060160495,0.0014192638,0.0003094611,0.3241214,0.63960814,0.0017500041,0.002940428,0.00010970046],"about_ca_topic_score_codex":0.0007049889,"about_ca_topic_score_gemma":0.00048746177,"teacher_disagreement_score":0.0007049889,"about_ca_system_score_codex":0.00030033733,"about_ca_system_score_gemma":0.00033502452,"threshold_uncertainty_score":0.0021790862},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.098314896,0.0031764263,0.88871807,0.0008357352,0.00021543894,0.000074914526,0.00012559637,0.00029912902,0.008239801],"genre_scores_gemma":[0.89656276,0.003433277,0.09134539,0.00020340766,0.0003354908,0.00012356867,0.00019748781,0.00016404697,0.0076345843],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998727,0.00005335227,0.0000054990205,0.000020544723,0.000036309324,0.000011614147],"domain_scores_gemma":[0.9995158,0.00029131077,0.000046454403,0.000021260548,0.000084905645,0.00004022487],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00053036015,0.00085259875,0.00043293124,0.00048640743,0.00027786376,0.00083838956,0.00094332703,0.0013259281,0.0009117788],"category_scores_gemma":[0.0023464966,0.00046961237,0.0006347065,0.00035201316,0.0009441755,0.0010102812,0.0007196434,0.0010284509,0.00050322164],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000292968,0.00005037276,0.0011909838,0.00006365958,0.0000123272575,0.00008049912,0.000044543725,0.975715,0.0019227865,0.007990132,0.0005668411,0.012333644],"study_design_scores_gemma":[0.0000020320836,0.00000888294,0.00012254993,0.000004442027,0.0000012610421,0.000005285124,0.000003917209,0.9964856,0.00016365449,0.0029979155,0.00020274671,0.0000017733363],"about_ca_topic_score_codex":0.0071661263,"about_ca_topic_score_gemma":0.0031437087,"teacher_disagreement_score":0.0071661263,"about_ca_system_score_codex":0.00036622208,"about_ca_system_score_gemma":0.00072794734,"threshold_uncertainty_score":0.014248788},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.50129735,0.00017471799,0.49287906,0.00011566439,0.00006370979,0.000040963136,0.00007323427,0.0005876326,0.0047676563],"genre_scores_gemma":[0.9638885,0.00005793385,0.033110242,0.000016967913,0.000018749213,0.000013950903,0.00007108568,0.000059653168,0.0027629759],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999918,0.000017226545,0.0000027368928,0.0000132920295,0.00003550685,0.000013221334],"domain_scores_gemma":[0.9997205,0.00013669145,0.000023852339,0.000012777297,0.000076553035,0.000029698278],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002087927,0.00050750136,0.00032469796,0.00033882016,0.00025263795,0.00042156628,0.00030950995,0.0005397533,0.0006579762],"category_scores_gemma":[0.0009724786,0.00015987549,0.00025300172,0.00013884291,0.0003019952,0.0003637664,0.00022837534,0.000292359,0.00014160524],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00041298906,0.00006323929,0.0047569396,0.00007420391,0.000021071211,0.00043108794,0.00010930948,0.90579206,0.04712586,0.006681958,0.00048972486,0.034041595],"study_design_scores_gemma":[0.0000048945585,0.000012796227,0.0002371357,0.0000013635841,9.3848877e-7,0.000016225757,0.000004963342,0.9974789,0.001895861,0.00024936456,0.00009554423,0.0000020854034],"about_ca_topic_score_codex":0.004703557,"about_ca_topic_score_gemma":0.0025540786,"teacher_disagreement_score":0.004703557,"about_ca_system_score_codex":0.00034836523,"about_ca_system_score_gemma":0.0004142241,"threshold_uncertainty_score":0.009352326},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9921256,0.0002641271,0.0050455886,0.00011423563,0.00002584934,0.000013725797,0.000037026377,0.00007707295,0.002296774],"genre_scores_gemma":[0.997654,0.00013757976,0.0010897191,0.00002621902,0.0000167303,0.000007124727,0.00006645376,0.000023924835,0.0009782618],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.9994647,0.0001216749,0.000015372927,0.0000743578,0.00018849708,0.00013544165],"domain_scores_gemma":[0.9990295,0.0005620652,0.00007181423,0.000059094527,0.00018233931,0.00009519032],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0007295955,0.00083362265,0.0007000076,0.00065445673,0.00070022146,0.00076011266,0.00045685426,0.00073004054,0.00091221166],"category_scores_gemma":[0.0012441474,0.00041479548,0.00043844205,0.0004106009,0.0014578076,0.00092054904,0.00094796944,0.0008403195,0.00021306035],"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":[0.0011042649,0.00013869122,0.0025426967,0.000051640996,0.000037953694,0.00033051783,0.0004931281,0.02375913,0.9650203,0.0030158907,0.00030352865,0.0032022195],"study_design_scores_gemma":[0.00035569,0.0009864352,0.015796041,0.00001859768,0.00004444234,0.0004996484,0.00046988725,0.21307622,0.76515657,0.0025196942,0.0009305774,0.00014613973],"about_ca_topic_score_codex":0.0025431472,"about_ca_topic_score_gemma":0.0013476156,"teacher_disagreement_score":0.0025431472,"about_ca_system_score_codex":0.0006573322,"about_ca_system_score_gemma":0.00031946483,"threshold_uncertainty_score":0.0050566792},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7488051,0.0010263389,0.21149133,0.0005406169,0.00015589283,0.000105863204,0.00027264192,0.0014319215,0.03617038],"genre_scores_gemma":[0.9873652,0.0001698899,0.009692345,0.000024479703,0.000011591006,0.000027341315,0.00006633604,0.000033431494,0.0026094306],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999887,0.000016741542,0.0000042290553,0.000010572553,0.000056952547,0.000024549077],"domain_scores_gemma":[0.999762,0.00010522966,0.000025315161,0.000017344862,0.000071534305,0.000018686265],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002186676,0.00026225232,0.00032885408,0.0003554974,0.0003663335,0.00037317292,0.00045216968,0.00054977933,0.0016303299],"category_scores_gemma":[0.0010037419,0.00014286018,0.00031526614,0.00028354875,0.0004395376,0.00032744816,0.00031320858,0.00037104005,0.00014104317],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00026771054,0.00012287298,0.0037445796,0.00036345006,0.000027699767,0.0011139733,0.00038253306,0.8239035,0.1225005,0.017881844,0.0014306327,0.028260753],"study_design_scores_gemma":[0.000009018171,0.000035351026,0.00048493722,0.0000057689927,0.0000028827212,0.000049030637,0.000030524756,0.99319226,0.0052445317,0.00048470165,0.00045529683,0.000005588722],"about_ca_topic_score_codex":0.0038768086,"about_ca_topic_score_gemma":0.0017323672,"teacher_disagreement_score":0.0038768086,"about_ca_system_score_codex":0.0004949279,"about_ca_system_score_gemma":0.00053052296,"threshold_uncertainty_score":0.00770849},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9991279,0.000006465434,0.00066279393,0.0000033839594,0.0000019652005,0.000011343058,0.000025062112,0.000008037253,0.00015319805],"genre_scores_gemma":[0.9980878,0.000021376798,0.0013971524,0.0000067809524,0.0000016337809,0.000010792605,0.00012517809,0.0000067810106,0.0003424472],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99978787,0.000031207634,0.000008270926,0.000044741977,0.00009588639,0.000032054268],"domain_scores_gemma":[0.99968266,0.00008272955,0.000023210032,0.000023464236,0.00013573773,0.000052215],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003250402,0.0004130985,0.00046888803,0.00040964363,0.0004424491,0.00020386289,0.00036028767,0.00032605973,0.0006530527],"category_scores_gemma":[0.00041066567,0.00016513251,0.00029852003,0.00018278146,0.00021671798,0.00017550727,0.00022252752,0.00022216013,0.00013924915],"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":[0.0020317377,0.0016196588,0.047986493,0.00015214698,0.00006194834,0.0009350714,0.0009493701,0.0348399,0.8881701,0.00020436315,0.0003155809,0.02273361],"study_design_scores_gemma":[0.00026096564,0.025983311,0.49749726,0.000054153556,0.00024127297,0.0013492072,0.0021823999,0.17693028,0.29347593,0.00017876358,0.0016802857,0.00016614946],"about_ca_topic_score_codex":0.008634826,"about_ca_topic_score_gemma":0.016224945,"teacher_disagreement_score":0.008634826,"about_ca_system_score_codex":0.000260177,"about_ca_system_score_gemma":0.00030089566,"threshold_uncertainty_score":0.017169178},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.1304479,0.00031036083,0.8609501,0.00009555802,0.00015665739,0.00012219096,0.00006378614,0.0025965297,0.0052568824],"genre_scores_gemma":[0.9289028,0.00011177041,0.06504088,0.00005279434,0.00007903744,0.00012431062,0.000057249756,0.000048951595,0.005582203],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997662,0.000036676567,0.000012458775,0.000051010775,0.000112314985,0.00002132103],"domain_scores_gemma":[0.9997532,0.000080624675,0.000033034034,0.000021675472,0.000094380324,0.000017126249],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00034798682,0.00053720287,0.00041372786,0.00024611785,0.00037639253,0.000405754,0.00074591313,0.00027113265,0.0036842912],"category_scores_gemma":[0.00042125717,0.00015150078,0.00015927476,0.00009425656,0.000257218,0.00034720293,0.00036076232,0.0002603383,0.00046983178],"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":[0.00094847055,0.00015815473,0.00074788305,0.0003597936,0.000026527325,0.00019798944,0.0002551731,0.0141146965,0.7006853,0.0033853254,0.0012438677,0.2778768],"study_design_scores_gemma":[0.00040262393,0.0037588102,0.005814549,0.00009512129,0.00015516364,0.0009014423,0.00010016331,0.52040327,0.43535206,0.0014652463,0.03145439,0.00009705699],"about_ca_topic_score_codex":0.0008103746,"about_ca_topic_score_gemma":0.0010752933,"teacher_disagreement_score":0.0036842912,"about_ca_system_score_codex":0.00018352103,"about_ca_system_score_gemma":0.00019019286,"threshold_uncertainty_score":0.012325168},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9337279,0.00023852762,0.039948307,0.000699128,0.00028924306,0.00014437494,0.00075150945,0.0004066915,0.023794211],"genre_scores_gemma":[0.96891564,0.00012815495,0.016844936,0.00012761589,0.000052915366,0.00005266104,0.0005290911,0.00005894349,0.013289956],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998579,0.000016801947,0.00000959927,0.00003786854,0.000041505584,0.000036284004],"domain_scores_gemma":[0.99970907,0.00009943404,0.000036127036,0.000024689347,0.000047516085,0.000083093255],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002126867,0.0007581262,0.00089103886,0.00065650675,0.0010962606,0.001434314,0.0007722007,0.0022517305,0.00579645],"category_scores_gemma":[0.00078868476,0.0004997951,0.0005888419,0.00050028245,0.0013160626,0.0010500366,0.001292426,0.0009540716,0.00052055495],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0011885853,0.0007238858,0.0066375346,0.00014986165,0.00008635319,0.002916065,0.000338686,0.8934809,0.071254075,0.01054859,0.0019451523,0.0107303],"study_design_scores_gemma":[0.00012925484,0.00029469442,0.004541343,0.000021002223,0.000024054352,0.00018403871,0.00014907621,0.98183113,0.010724191,0.0010295989,0.0010127745,0.00005885008],"about_ca_topic_score_codex":0.005210179,"about_ca_topic_score_gemma":0.0035306315,"teacher_disagreement_score":0.00579645,"about_ca_system_score_codex":0.0007056086,"about_ca_system_score_gemma":0.0013112437,"threshold_uncertainty_score":0.01939112},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.003255301,0.00051222014,0.97595507,0.00028895747,0.00019987326,0.0001412033,0.00022149581,0.0003686469,0.019057175],"genre_scores_gemma":[0.14763972,0.0009828964,0.8293416,0.0005854742,0.00020309094,0.0011987721,0.0006171191,0.0009106284,0.01852069],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9987664,0.00038126993,0.00007655842,0.00009389477,0.000590049,0.00009177893],"domain_scores_gemma":[0.99902725,0.0003888248,0.00007832528,0.00011508121,0.0003277071,0.000062724626],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0012505214,0.00071702624,0.00085555285,0.0005539419,0.0006718167,0.0014591458,0.0016777297,0.0013688906,0.011701609],"category_scores_gemma":[0.0041591795,0.00045287175,0.0006822278,0.0005245186,0.0010350124,0.0013755378,0.0015663883,0.0026525522,0.006801847],"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":[0.00011273976,0.0001488297,0.00050535996,0.0003616786,0.000021279046,0.00025575643,0.00024764257,0.20061316,0.02953127,0.6862519,0.009080069,0.07287038],"study_design_scores_gemma":[0.000082677194,0.000055488315,0.000151387,0.00011314016,0.000012734459,0.00017622551,0.000059243466,0.85916847,0.007536267,0.09371224,0.038886473,0.000045572768],"about_ca_topic_score_codex":0.002075098,"about_ca_topic_score_gemma":0.0010800919,"teacher_disagreement_score":0.011701609,"about_ca_system_score_codex":0.00064010004,"about_ca_system_score_gemma":0.00178066,"threshold_uncertainty_score":0.039145768},"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":"methods","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.062973924,0.00019298635,0.92569923,0.0003331522,0.00030624654,0.0001586497,0.00026863837,0.003028246,0.0070389295],"genre_scores_gemma":[0.35141253,0.0001987015,0.6424023,0.00029593494,0.000071274524,0.00022517674,0.00034993078,0.00020612402,0.004838048],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994609,0.00010264205,0.000052315856,0.00013017895,0.0002088063,0.000045172346],"domain_scores_gemma":[0.9984125,0.00029279888,0.00020647966,0.00039943197,0.0006308403,0.00005798195],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00037812837,0.0006535735,0.00030694314,0.00040422127,0.00017268745,0.0005102093,0.0006039773,0.00043751264,0.0044613816],"category_scores_gemma":[0.003141338,0.0003094781,0.0003562628,0.0006589391,0.00034263462,0.00076944433,0.00048935285,0.00043800066,0.0019293884],"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":[0.0010823591,0.0001277232,0.0029321362,0.0002206884,0.000042223204,0.00031840333,0.00014314882,0.030722937,0.6013652,0.006205669,0.0032668817,0.35357255],"study_design_scores_gemma":[0.00030485936,0.0043120035,0.010368115,0.00007834374,0.00013503563,0.004812002,0.00016678889,0.31137106,0.56914926,0.0069797416,0.09206984,0.00025306435],"about_ca_topic_score_codex":0.00071551744,"about_ca_topic_score_gemma":0.001173061,"teacher_disagreement_score":0.0044613816,"about_ca_system_score_codex":0.0003210234,"about_ca_system_score_gemma":0.00048564046,"threshold_uncertainty_score":0.014924824},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99442923,0.000067249544,0.004386246,0.00004058369,0.000006140125,0.000006299843,0.00003632629,0.000043281405,0.0009846345],"genre_scores_gemma":[0.99836963,0.000026614436,0.0012117586,0.0000075354446,0.0000047302487,0.0000036912784,0.000049198836,0.0000049147507,0.00032197716],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999629,0.0000037887091,0.0000010551211,0.0000112334565,0.000010539951,0.000010462936],"domain_scores_gemma":[0.9998697,0.000036656656,0.000025924714,0.000005096478,0.0000337238,0.00002884929],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000113200156,0.000119273194,0.00023671763,0.00030816055,0.00023301807,0.00042634358,0.00014128763,0.0002425631,0.00054562185],"category_scores_gemma":[0.00034015035,0.000083961124,0.00011972957,0.00015005602,0.0003711039,0.00016855919,0.00011854671,0.0002510709,0.00006818389],"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":[0.0006627188,0.00013623165,0.02094627,0.000059692375,0.000018549044,0.0010020803,0.00020858445,0.055199955,0.89730495,0.007174503,0.00043895585,0.0168475],"study_design_scores_gemma":[0.00017113212,0.0009475827,0.1644856,0.000020825704,0.000031278953,0.00037248875,0.00023038339,0.74743927,0.08213951,0.002758012,0.0013132573,0.00009060451],"about_ca_topic_score_codex":0.0023173774,"about_ca_topic_score_gemma":0.0011644203,"teacher_disagreement_score":0.0023173774,"about_ca_system_score_codex":0.0004889822,"about_ca_system_score_gemma":0.00031991498,"threshold_uncertainty_score":0.004607737},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99789315,0.00009118392,0.0016113549,0.000007922103,0.0000057146804,0.000013925099,0.0000253776,0.000015090778,0.00033634115],"genre_scores_gemma":[0.99749833,0.00008925831,0.0018235473,0.000019405443,0.0000050178664,0.000014913529,0.00006240803,0.000011120602,0.0004760493],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996045,0.000049630704,0.000024449888,0.00007678483,0.00014083122,0.00010385224],"domain_scores_gemma":[0.9992895,0.00030105354,0.00013322632,0.0000486102,0.00016694472,0.000060674673],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00036106145,0.00040379784,0.00036612593,0.00022742577,0.00021854525,0.0004072139,0.00025915727,0.0003080337,0.0008907299],"category_scores_gemma":[0.0012047425,0.00024888225,0.0002937291,0.00017943283,0.0003668696,0.00044652921,0.0005142086,0.00048304815,0.00013067594],"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":[0.00015541779,0.000030157255,0.0010406595,0.000024719113,0.0000036739373,0.000050397615,0.00006212572,0.00035605454,0.99596965,0.000036310325,0.000011783672,0.0022590489],"study_design_scores_gemma":[0.000020148194,0.0017675636,0.014369116,0.000007980527,0.000015970318,0.00014219145,0.00008628156,0.0058075883,0.97733104,0.0000412563,0.00039295485,0.000017953585],"about_ca_topic_score_codex":0.0011482817,"about_ca_topic_score_gemma":0.0005946046,"teacher_disagreement_score":0.0011482817,"about_ca_system_score_codex":0.0002700939,"about_ca_system_score_gemma":0.00014216916,"threshold_uncertainty_score":0.002979815},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.2657388,0.00028784614,0.7052663,0.00064674194,0.00014513898,0.00010156132,0.00033559455,0.00061959814,0.026858352],"genre_scores_gemma":[0.9048158,0.00028771054,0.07558526,0.00016379548,0.00011609533,0.00013816461,0.0002539773,0.00016597155,0.018473128],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99991643,0.000020392445,0.000004075316,0.000015518046,0.00002933472,0.000014273224],"domain_scores_gemma":[0.999828,0.000048015787,0.000033157365,0.000010394229,0.000060826693,0.000019601224],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002534341,0.000546584,0.00051156234,0.00039540703,0.0003565003,0.0007094976,0.00056177157,0.0010415065,0.0018060412],"category_scores_gemma":[0.0009418031,0.00022510471,0.0005612719,0.00026564763,0.00074357,0.00036500045,0.0006727047,0.00072836614,0.00020865358],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000090837784,0.000034538065,0.00076929183,0.00008628882,0.00002024294,0.00033891655,0.00016692863,0.9268669,0.01825865,0.0417208,0.0011899008,0.010456683],"study_design_scores_gemma":[0.000015067827,0.000026026604,0.00027141927,0.0000037502712,0.000003860825,0.000028207864,0.000022601418,0.9962064,0.00075936044,0.0022587145,0.00039660995,0.00000795788],"about_ca_topic_score_codex":0.0054752305,"about_ca_topic_score_gemma":0.0043779155,"teacher_disagreement_score":0.0054752305,"about_ca_system_score_codex":0.0004920393,"about_ca_system_score_gemma":0.0010007785,"threshold_uncertainty_score":0.010886729},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.86227113,0.00042498801,0.13119808,0.00028087344,0.00009006341,0.000078800804,0.00026276283,0.0004883909,0.0049049216],"genre_scores_gemma":[0.99491525,0.000080470076,0.0040193684,0.000015209647,0.000017079527,0.0000216076,0.000103582934,0.000027721724,0.000799662],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99989045,0.000024853278,0.000004206592,0.000028854622,0.000025206025,0.00002652813],"domain_scores_gemma":[0.9995652,0.0002292603,0.000076427124,0.000009825747,0.000073613104,0.00004571151],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00031098624,0.0008084367,0.0003925328,0.0004138466,0.00041673894,0.0006144078,0.0005444431,0.0010434347,0.0007311926],"category_scores_gemma":[0.0011505038,0.00031563034,0.00039320003,0.00018150998,0.00058784685,0.0004838869,0.00031610884,0.0004305269,0.00014914335],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000028618275,0.00003128252,0.0021988994,0.00001461312,0.000004602631,0.00005238607,0.00001712951,0.99343455,0.0021895508,0.00050386565,0.00012830447,0.0013961847],"study_design_scores_gemma":[0.0000019034828,0.000007477012,0.0003902886,8.066113e-7,6.339514e-7,0.0000020219925,0.000002487397,0.99939203,0.00013718999,0.000047128662,0.000016204065,0.0000017960562],"about_ca_topic_score_codex":0.029354718,"about_ca_topic_score_gemma":0.009902668,"teacher_disagreement_score":0.029354718,"about_ca_system_score_codex":0.00073597074,"about_ca_system_score_gemma":0.00077909906,"threshold_uncertainty_score":0.05836773},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.996405,0.000053992346,0.0027156672,0.000008768969,0.000011028885,0.000013044149,0.000030310885,0.000032903095,0.00072929094],"genre_scores_gemma":[0.99820244,0.000032242173,0.000809396,0.000006778834,0.0000070254364,0.000011101368,0.00004446518,0.000015525431,0.0008709211],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9994981,0.00015838284,0.000018252167,0.000088034285,0.00014596825,0.000091242735],"domain_scores_gemma":[0.9987213,0.0007199496,0.00006657918,0.00010082575,0.000328405,0.00006293331],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004714774,0.00045399077,0.00043059833,0.00035476562,0.00077839935,0.00025911749,0.0004741374,0.0005842009,0.0021995772],"category_scores_gemma":[0.0012574764,0.00025228944,0.00023203925,0.0002082245,0.0006692455,0.0003570348,0.00031542094,0.00033602686,0.00024897436],"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":[0.0023792558,0.00049462053,0.0063288314,0.000096712836,0.000020692081,0.00019927611,0.00043906394,0.001833293,0.97901136,0.00021699027,0.00011741973,0.008862504],"study_design_scores_gemma":[0.00013308499,0.004278096,0.03717034,0.000019980986,0.00005990218,0.0004962143,0.00027555344,0.014009208,0.9420371,0.00010271847,0.001382412,0.000035499972],"about_ca_topic_score_codex":0.0010892246,"about_ca_topic_score_gemma":0.0009971652,"teacher_disagreement_score":0.0021995772,"about_ca_system_score_codex":0.00029835245,"about_ca_system_score_gemma":0.00019671273,"threshold_uncertainty_score":0.007358372},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9432213,0.00026385614,0.05225681,0.000050109527,0.000040722403,0.00006976425,0.00004314643,0.0003324279,0.0037219],"genre_scores_gemma":[0.98189306,0.000103217775,0.017134089,0.00002018574,0.000010875099,0.000035493904,0.000032260472,0.000029134351,0.0007417964],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9994708,0.000058321286,0.000018446746,0.00013602045,0.00024569102,0.00007071037],"domain_scores_gemma":[0.9991416,0.00025564214,0.00016281357,0.00006353055,0.000263613,0.00011285513],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00059823075,0.00026469675,0.000531423,0.00082256546,0.00050629175,0.00069441035,0.0006948258,0.0006041324,0.001175706],"category_scores_gemma":[0.0011154212,0.00026384185,0.00030992512,0.00033675964,0.0006565646,0.00074769196,0.0008240502,0.0004833072,0.00043858436],"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":[0.00037747988,0.00009539117,0.00437463,0.000095837066,0.000010626396,0.0008396133,0.00037472096,0.0027316443,0.9788214,0.0013921125,0.00010839865,0.010778206],"study_design_scores_gemma":[0.0000806105,0.0011065626,0.02155206,0.00004460838,0.000049552225,0.0011060224,0.0011401926,0.09307045,0.8767798,0.0017079336,0.0032883347,0.000073943724],"about_ca_topic_score_codex":0.00034859692,"about_ca_topic_score_gemma":0.00043596563,"teacher_disagreement_score":0.001175706,"about_ca_system_score_codex":0.00022388058,"about_ca_system_score_gemma":0.0003633113,"threshold_uncertainty_score":0.0039331317},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9754287,0.0005026161,0.02166252,0.000058767968,0.00008000931,0.000035109897,0.00008404566,0.00023621686,0.0019120187],"genre_scores_gemma":[0.990004,0.00018533667,0.0067523727,0.000025721083,0.000015631154,0.000016829736,0.00010148313,0.00003490519,0.0028637506],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998117,0.00001370874,0.000013232288,0.000050850238,0.00008477008,0.000025743584],"domain_scores_gemma":[0.99973065,0.000037900896,0.0001137612,0.000038179685,0.000060647933,0.000018758064],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016383312,0.0002938064,0.00017575295,0.00016188627,0.000113452596,0.000305461,0.00036597953,0.00022062864,0.0011094549],"category_scores_gemma":[0.00021493813,0.000117153824,0.000098406716,0.00011400589,0.00019401993,0.00026173374,0.00025055223,0.0002359164,0.00020888768],"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":[0.00014399034,0.0000301046,0.00030131784,0.00004469964,0.0000043743803,0.000057781566,0.000021695858,0.00071208813,0.99289083,0.00025923035,0.00008730408,0.0054464373],"study_design_scores_gemma":[0.000015429292,0.00061213085,0.0022176118,0.0000032828746,0.000011850802,0.000060753202,0.000013106826,0.006282122,0.98810834,0.0000490974,0.0026185482,0.000007748294],"about_ca_topic_score_codex":0.00031373068,"about_ca_topic_score_gemma":0.00042927108,"teacher_disagreement_score":0.0011094549,"about_ca_system_score_codex":0.00023636105,"about_ca_system_score_gemma":0.0001017009,"threshold_uncertainty_score":0.003711462},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9981558,0.00003765435,0.0010671278,0.000020303201,0.000009445296,0.000011485343,0.00003825918,0.000062442785,0.00059761136],"genre_scores_gemma":[0.99892104,0.000017403328,0.0006465823,0.000009025853,0.0000053672397,0.000006588195,0.000044508608,0.000012352394,0.000337103],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99972934,0.000031936233,0.000016492864,0.00004963472,0.000119433025,0.000053269836],"domain_scores_gemma":[0.99969196,0.00010442545,0.00004322752,0.000021770433,0.00007021037,0.00006846351],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00033692695,0.00045835308,0.0006183547,0.00051275495,0.0010403721,0.0005220041,0.00054771313,0.00065817847,0.000983925],"category_scores_gemma":[0.00057918293,0.0003616628,0.00030040377,0.00026756927,0.00046418273,0.0005705033,0.00066801853,0.00086136593,0.00019797287],"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":[0.0021250022,0.00019180044,0.007719878,0.000036206482,0.000025454943,0.0002473066,0.00028564176,0.001516951,0.98210365,0.00018291501,0.00008188427,0.0054833805],"study_design_scores_gemma":[0.00023033342,0.0021876018,0.06882673,0.000013332028,0.00007338282,0.00033837964,0.00027734798,0.039636753,0.8875379,0.0001364662,0.000686115,0.000055606728],"about_ca_topic_score_codex":0.0014228142,"about_ca_topic_score_gemma":0.001247511,"teacher_disagreement_score":0.0014228142,"about_ca_system_score_codex":0.00030393768,"about_ca_system_score_gemma":0.00028439672,"threshold_uncertainty_score":0.0032915473},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99680007,0.00015295132,0.0025859806,0.000010223197,0.000015341187,0.000010836182,0.00002821668,0.000038890994,0.00035740732],"genre_scores_gemma":[0.99876297,0.000084562686,0.0009438815,0.00001584123,0.0000057962793,0.0000060072243,0.000046025416,0.000009548342,0.00012540355],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9995919,0.00008975335,0.000028834373,0.000064945496,0.00013780428,0.000086800654],"domain_scores_gemma":[0.99928504,0.00021992582,0.00015093802,0.00005359652,0.00012297064,0.00016757917],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00037868824,0.00056225475,0.00053298473,0.00037928368,0.0003979482,0.0007870278,0.0002031401,0.00019641062,0.00044532708],"category_scores_gemma":[0.00073819916,0.00016460211,0.00026160502,0.00024557684,0.0003466085,0.00022888654,0.00038155663,0.00034545833,0.00007260189],"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":[0.0013025126,0.00011611686,0.0039134715,0.00006838949,0.000028454577,0.0003140698,0.00007421053,0.0030196235,0.9871738,0.00021224875,0.000045655477,0.0037314729],"study_design_scores_gemma":[0.00014224893,0.0038282424,0.06320828,0.00003344958,0.000091367925,0.0003206334,0.00016170942,0.029727327,0.9014283,0.0001649525,0.0008360558,0.000057339475],"about_ca_topic_score_codex":0.0010300748,"about_ca_topic_score_gemma":0.000733112,"teacher_disagreement_score":0.0010300748,"about_ca_system_score_codex":0.00026027302,"about_ca_system_score_gemma":0.00020391596,"threshold_uncertainty_score":0.0020481944},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9981863,0.00003407756,0.0015294431,0.0000025720647,0.0000021709332,0.000003313607,0.000017267279,0.000017484319,0.00020743758],"genre_scores_gemma":[0.99767524,0.000039772065,0.0019320664,0.000003850598,0.0000021133046,0.0000055210908,0.000067651075,0.000010018831,0.0002638343],"study_design_codex":"bench_or_experimental","study_design_gemma":"not_applicable","domain_scores_codex":[0.9999286,0.0000056947447,0.000003478413,0.000010525818,0.00002433829,0.000027409718],"domain_scores_gemma":[0.9997259,0.000076422795,0.00007752338,0.00001659495,0.000041194777,0.000062406536],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016882572,0.00017312665,0.0001542695,0.00023433033,0.00015788259,0.00044216515,0.00009681961,0.00011723316,0.00030899988],"category_scores_gemma":[0.0002931581,0.00012047467,0.00014156097,0.00014098844,0.00026063435,0.0002474161,0.00020987129,0.00023740994,0.00005907421],"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":[0.00019479326,0.000021476657,0.0036325704,0.000012626041,0.0000039600045,0.00012906692,0.000085604675,0.000847794,0.9925055,0.00032542404,0.00002353956,0.0022176674],"study_design_scores_gemma":[0.000035605088,0.00042925845,0.078391284,0.000009422127,0.000018408544,0.0002958638,0.00015644277,0.01630447,0.9032137,0.00031424122,0.0007968486,0.000034437897],"about_ca_topic_score_codex":0.0002229344,"about_ca_topic_score_gemma":0.0002973472,"teacher_disagreement_score":0.00044216515,"about_ca_system_score_codex":0.0001483116,"about_ca_system_score_gemma":0.00010842256,"threshold_uncertainty_score":0.0010761023},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9622724,0.00014124697,0.0323912,0.000081603845,0.000015559475,0.000042870557,0.000087635264,0.00022168012,0.0047457977],"genre_scores_gemma":[0.9960265,0.000030419178,0.0036044435,0.000005001607,0.000002833094,0.000013706161,0.000025606505,0.000011081946,0.0002802909],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997906,0.0000574323,0.000012111957,0.000020008702,0.00008735733,0.000032445318],"domain_scores_gemma":[0.9988053,0.00078515214,0.00008461096,0.00006771272,0.0002049542,0.000052325235],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00045243942,0.00031450752,0.0005719654,0.00033659354,0.00037967943,0.00042611727,0.0003736116,0.0003961709,0.0009405494],"category_scores_gemma":[0.0014655621,0.0001769296,0.0002601599,0.0002899222,0.00043263767,0.0004037322,0.00036490735,0.00033775685,0.000090350586],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00032483033,0.00021503927,0.0050570923,0.00011797415,0.000034826066,0.00035589776,0.00020957367,0.8950906,0.08760649,0.0029470427,0.00018406777,0.0078566335],"study_design_scores_gemma":[0.00002470053,0.00006972053,0.0011156977,0.0000032274902,0.0000035435955,0.00002291727,0.000017574599,0.99178725,0.0066495137,0.00017045073,0.00012728058,0.000008116145],"about_ca_topic_score_codex":0.0034124122,"about_ca_topic_score_gemma":0.0016760541,"teacher_disagreement_score":0.0034124122,"about_ca_system_score_codex":0.00028107897,"about_ca_system_score_gemma":0.00042788425,"threshold_uncertainty_score":0.0067851543},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98750186,0.000027863327,0.011959003,0.000008290816,0.0000028909174,0.000009950146,0.000071646784,0.00008933151,0.0003291035],"genre_scores_gemma":[0.9961461,0.00002366117,0.0036481123,0.0000014709001,0.0000013407484,0.0000056224862,0.00008715676,0.0000066627595,0.00007988219],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998915,0.000015711119,0.0000032814887,0.000023864815,0.00005359577,0.000011857656],"domain_scores_gemma":[0.9995043,0.0002852353,0.00004895434,0.000042337655,0.000084248924,0.000034897548],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00033475153,0.00033915738,0.00024392422,0.0004389964,0.00020064093,0.00025636575,0.00030687673,0.00042879645,0.00030086839],"category_scores_gemma":[0.0008234376,0.0001927276,0.00017529738,0.00019249106,0.0002809035,0.0002339372,0.00012549944,0.00026597304,0.000102304926],"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":[0.0005580071,0.0002640846,0.09145843,0.00020448254,0.000037466663,0.00029649923,0.00038580078,0.083761916,0.7772557,0.00026700422,0.00023743452,0.04527321],"study_design_scores_gemma":[0.000030625157,0.00088047405,0.25468346,0.000018439825,0.000033302247,0.00026162714,0.00015735679,0.57717776,0.16627464,0.00014428623,0.00029326192,0.000044893273],"about_ca_topic_score_codex":0.0013763707,"about_ca_topic_score_gemma":0.0013585447,"teacher_disagreement_score":0.0013763707,"about_ca_system_score_codex":0.00015367093,"about_ca_system_score_gemma":0.00014795976,"threshold_uncertainty_score":0.0027367473},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99875915,0.000031538373,0.0009921832,0.000008818266,0.0000047502253,0.000014241703,0.000024929,0.000018556975,0.0001459011],"genre_scores_gemma":[0.9979038,0.000040258437,0.0017976421,0.0000066380035,0.0000041514377,0.000016798625,0.000029545894,0.000005352466,0.00019575696],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997125,0.000035092162,0.000013360053,0.0000647994,0.00009029546,0.000083866085],"domain_scores_gemma":[0.9991566,0.00036195194,0.00011872758,0.000114166236,0.0001314306,0.00011712556],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00048597736,0.00033303388,0.0004167624,0.00017701247,0.0005096311,0.0003075844,0.0003834038,0.00044502347,0.0008463286],"category_scores_gemma":[0.001031911,0.0002481033,0.00018246558,0.00015431187,0.00078141445,0.00027736722,0.0004828704,0.0003533079,0.00008538631],"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":[0.00038355193,0.00012731,0.002235717,0.000057111232,0.0000069353264,0.000114593044,0.00019723896,0.0019512064,0.9922369,0.000102855236,0.00003766332,0.002548823],"study_design_scores_gemma":[0.00023116627,0.009707903,0.042626254,0.00003430558,0.000051334704,0.00023384794,0.00026292983,0.035107102,0.9104256,0.00011745678,0.0011436279,0.000058358535],"about_ca_topic_score_codex":0.0009435114,"about_ca_topic_score_gemma":0.00092627667,"teacher_disagreement_score":0.0009435114,"about_ca_system_score_codex":0.00024099303,"about_ca_system_score_gemma":0.00029119925,"threshold_uncertainty_score":0.0028312206},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.07832129,0.0012028359,0.86404395,0.0004972158,0.0001753739,0.00007136425,0.00018069065,0.00027579663,0.05523155],"genre_scores_gemma":[0.8766028,0.0020661964,0.08804887,0.00040639323,0.00018449382,0.00012776845,0.0002886529,0.00024259908,0.032031994],"study_design_codex":"simulation_or_modeling","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.99983597,0.000044495067,0.0000059919184,0.00003958832,0.000048770315,0.000025196936],"domain_scores_gemma":[0.99981314,0.00005782154,0.000028539647,0.000025733802,0.000059560465,0.000015231309],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004588742,0.0009358957,0.00036413208,0.000502462,0.0002853579,0.0007306948,0.00056927896,0.00087637996,0.0035206103],"category_scores_gemma":[0.0009605016,0.00021230093,0.00056373497,0.00029107687,0.0008598353,0.00093869277,0.00075337867,0.0008086344,0.0014342682],"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":[0.00018403644,0.00008496574,0.000958222,0.00026986323,0.000026037837,0.0009855328,0.0002503958,0.4805324,0.04573877,0.43352574,0.0045463922,0.032897644],"study_design_scores_gemma":[0.00000561803,0.000032587257,0.00021219936,0.000022829598,0.0000045106253,0.00014329195,0.000026239268,0.9765609,0.0019321046,0.018354595,0.0026907485,0.000014403955],"about_ca_topic_score_codex":0.001767374,"about_ca_topic_score_gemma":0.0009857429,"teacher_disagreement_score":0.0035206103,"about_ca_system_score_codex":0.00041485523,"about_ca_system_score_gemma":0.00045688933,"threshold_uncertainty_score":0.01177758},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.011679269,0.001856085,0.93134016,0.0009824404,0.00069098565,0.000098777564,0.00021098205,0.00010965319,0.0530317],"genre_scores_gemma":[0.4349734,0.0045499494,0.43873772,0.0018777646,0.0020484654,0.00060898607,0.0005447384,0.00028890194,0.116370186],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.9997962,0.000042871623,0.000010496959,0.000052143154,0.0000832983,0.000015002726],"domain_scores_gemma":[0.9997986,0.00006612613,0.000026958629,0.00001915299,0.0000759252,0.000013269773],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00036395906,0.0006554083,0.00037198374,0.00048284832,0.0003092722,0.001002648,0.00093857694,0.0011748425,0.004790618],"category_scores_gemma":[0.0008100901,0.00023253822,0.0004215974,0.00033843907,0.00067765097,0.0013742507,0.00091390935,0.0010443124,0.0011794217],"study_design_candidate":"theoretical_or_conceptual","study_design_consensus":"theoretical_or_conceptual","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00003165468,0.000053684802,0.00035620382,0.00030823666,0.000015735824,0.000454787,0.00014810839,0.08404043,0.023300493,0.8345532,0.008068842,0.048668697],"study_design_scores_gemma":[0.000020354546,0.00011027168,0.00089194725,0.0000676935,0.000021881351,0.0005639143,0.00009354299,0.80506647,0.00644237,0.12474033,0.06193445,0.00004691465],"about_ca_topic_score_codex":0.0014427821,"about_ca_topic_score_gemma":0.0011066993,"teacher_disagreement_score":0.004790618,"about_ca_system_score_codex":0.00042993165,"about_ca_system_score_gemma":0.0006699555,"threshold_uncertainty_score":0.01602614},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9371061,0.0011757086,0.059312273,0.000047784193,0.000042658387,0.0000285095,0.000036014473,0.00031418868,0.0019367018],"genre_scores_gemma":[0.9869249,0.0002555546,0.012376065,0.000016713115,0.000012810467,0.000009278566,0.000029460378,0.000030622847,0.0003446214],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997141,0.00007132297,0.000016012742,0.000054961958,0.00010660019,0.000037123813],"domain_scores_gemma":[0.99941826,0.0003115508,0.0000960474,0.000036846497,0.00011338647,0.000023943843],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005330614,0.0003235571,0.00039269973,0.0004560187,0.00022872488,0.0003720022,0.00057796773,0.00023649925,0.00090557814],"category_scores_gemma":[0.0010147212,0.00012834552,0.0003106496,0.0002475742,0.00019604202,0.00032089153,0.000213796,0.0001382239,0.000092558184],"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":[0.0014119261,0.0005399556,0.01854151,0.0005230735,0.00008313293,0.00030977986,0.00021833829,0.118445136,0.64167726,0.0017384742,0.00039175124,0.21611968],"study_design_scores_gemma":[0.0003725853,0.010960289,0.056987807,0.00010039327,0.00039929725,0.0010163467,0.00027397575,0.30151802,0.61410403,0.0011001376,0.013037197,0.00013000246],"about_ca_topic_score_codex":0.00055538333,"about_ca_topic_score_gemma":0.0006118087,"teacher_disagreement_score":0.00090557814,"about_ca_system_score_codex":0.00015427348,"about_ca_system_score_gemma":0.00016683768,"threshold_uncertainty_score":0.0030294657},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7097084,0.0005905694,0.27893415,0.0005654989,0.00017634651,0.0001501441,0.00022196613,0.0007704519,0.008882453],"genre_scores_gemma":[0.93644595,0.00021098704,0.060438108,0.000055137658,0.000037771693,0.000097747026,0.000098633514,0.000071751325,0.0025440382],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998969,0.000032076787,0.000006350383,0.000010930983,0.00003803927,0.000015812579],"domain_scores_gemma":[0.9997435,0.00013798088,0.000025982796,0.000028779812,0.000033068165,0.000030688],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024423536,0.00040174022,0.0005697097,0.00013995892,0.0002934836,0.00072689477,0.0004943494,0.00061244576,0.0013262591],"category_scores_gemma":[0.00056816824,0.00020345181,0.00028116314,0.00015030877,0.00048527188,0.00047169274,0.00037606314,0.0006795903,0.00015469168],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00018012829,0.00014849898,0.0024536834,0.00014237707,0.000026578075,0.00014713102,0.00010490251,0.93494904,0.046738207,0.0050395504,0.0004652908,0.009604526],"study_design_scores_gemma":[0.000027978484,0.00007155398,0.000372615,0.000004142113,0.0000042000534,0.000014456817,0.000012391519,0.9918413,0.0067248214,0.00039300587,0.0005274206,0.0000061015094],"about_ca_topic_score_codex":0.0020444375,"about_ca_topic_score_gemma":0.0017175024,"teacher_disagreement_score":0.0020444375,"about_ca_system_score_codex":0.0002837029,"about_ca_system_score_gemma":0.00043128477,"threshold_uncertainty_score":0.004436791},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.4013279,0.0001974329,0.5869625,0.00015360804,0.00010048856,0.00007032166,0.00024593313,0.0019028857,0.009038953],"genre_scores_gemma":[0.8768799,0.000105324754,0.11986356,0.000032390355,0.00001746046,0.000053856624,0.00024001439,0.00015110258,0.0026564598],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998981,0.000014696292,0.0000062157965,0.000010241267,0.000059646074,0.000011206716],"domain_scores_gemma":[0.9996954,0.00009614434,0.000025326684,0.000029031453,0.00014563774,0.000008472445],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021897095,0.00040483542,0.0003310305,0.0006686134,0.00039811913,0.0005033137,0.00037725794,0.00036069786,0.00235019],"category_scores_gemma":[0.00061156234,0.0001578951,0.00037773332,0.0002875622,0.00022840867,0.00042241183,0.00029272158,0.00042739225,0.00031617336],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00015819214,0.00014645654,0.006170451,0.00014445654,0.00003703686,0.0002568711,0.00022152187,0.7051929,0.15738237,0.008000352,0.0019671293,0.120322265],"study_design_scores_gemma":[0.000007421423,0.00001749336,0.0007681422,0.0000038079886,0.000002604484,0.00003112651,0.000012620763,0.98998207,0.008126727,0.00027076592,0.0007667213,0.000010639421],"about_ca_topic_score_codex":0.007765619,"about_ca_topic_score_gemma":0.00545337,"teacher_disagreement_score":0.007765619,"about_ca_system_score_codex":0.00033042478,"about_ca_system_score_gemma":0.0006864596,"threshold_uncertainty_score":0.015440822},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.010064248,0.0011596131,0.96986246,0.00039325038,0.00034766004,0.00004210799,0.000060288385,0.0000874447,0.01798296],"genre_scores_gemma":[0.5051348,0.003823619,0.40391007,0.0011115657,0.0016129733,0.00037170094,0.0002711807,0.00023784357,0.0835262],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.9997831,0.00005224177,0.000010533474,0.000045225883,0.000094846764,0.0000141243845],"domain_scores_gemma":[0.99981517,0.00007471056,0.000028026,0.000016404018,0.00005330694,0.0000124322405],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00042929157,0.0007485054,0.0003773315,0.00051740755,0.00027932142,0.0008464496,0.001026283,0.0014045715,0.0034760777],"category_scores_gemma":[0.0009679828,0.00027154476,0.0005490245,0.000391798,0.00075661554,0.0016017769,0.0009097955,0.0012037427,0.0008374171],"study_design_candidate":"theoretical_or_conceptual","study_design_consensus":"theoretical_or_conceptual","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00003462289,0.000044104778,0.00022723741,0.00019268603,0.000018172881,0.0005947582,0.00019273454,0.101973645,0.02658872,0.83186257,0.003247381,0.035023335],"study_design_scores_gemma":[0.00001919814,0.00010462589,0.00032275025,0.00003048448,0.000016877711,0.00037720482,0.0000588894,0.87249815,0.0035549842,0.10645575,0.016528836,0.00003232861],"about_ca_topic_score_codex":0.0006042568,"about_ca_topic_score_gemma":0.0005944649,"teacher_disagreement_score":0.0034760777,"about_ca_system_score_codex":0.00039335634,"about_ca_system_score_gemma":0.00043814207,"threshold_uncertainty_score":0.011628628},"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":"review","genre_gemma":"review","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"review","genre_consensus":"review","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0021422864,0.82789075,0.139304,0.0029730154,0.0046251905,0.00009422824,0.0001699298,0.0005642744,0.022236304],"genre_scores_gemma":[0.018320309,0.8511156,0.11255846,0.0014444428,0.0043762126,0.00022589369,0.00045112584,0.00044262988,0.011065414],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9985576,0.00029456348,0.0002009906,0.0001746468,0.0007102383,0.00006190878],"domain_scores_gemma":[0.9955713,0.002221121,0.00012397363,0.00023094361,0.0017334182,0.00011922121],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0016520654,0.0011508978,0.0017187456,0.002505002,0.0008084198,0.0018289941,0.0016175198,0.0015955353,0.006464222],"category_scores_gemma":[0.0058676302,0.0007650236,0.0011230032,0.0054004467,0.0007800991,0.0019712923,0.0012356567,0.0023338655,0.0035263544],"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":[0.00009385951,0.00008768891,0.00078367646,0.0065578893,0.0001520493,0.00030915576,0.00019772575,0.028194118,0.0051405593,0.043281596,0.053993568,0.8612082],"study_design_scores_gemma":[0.000031329342,0.00011497904,0.0009722531,0.001986796,0.000078684476,0.00072689366,0.00008562243,0.029344602,0.002827287,0.025349885,0.9383897,0.00009198077],"about_ca_topic_score_codex":0.0020146412,"about_ca_topic_score_gemma":0.0017172833,"teacher_disagreement_score":0.006464222,"about_ca_system_score_codex":0.0005880561,"about_ca_system_score_gemma":0.0014715568,"threshold_uncertainty_score":0.021624923},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.96777064,0.00012584365,0.028034076,0.00010900503,0.000046734716,0.000056104614,0.000099714525,0.0001560831,0.003601778],"genre_scores_gemma":[0.99147695,0.00005503085,0.007106158,0.000016737044,0.000011018446,0.000025992176,0.00006579072,0.000015529626,0.0012266723],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99988055,0.000026034975,0.000005273239,0.000010745124,0.000043674372,0.000033773667],"domain_scores_gemma":[0.99952877,0.00029095612,0.000045421744,0.000019607582,0.00006614367,0.000049182778],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00030620425,0.00037352598,0.0005287701,0.00039306586,0.00052077806,0.00052772585,0.00044145004,0.00082517735,0.0010249775],"category_scores_gemma":[0.0010779441,0.00018467553,0.00037851592,0.00020170223,0.0007597013,0.00033941923,0.0004473427,0.00039146107,0.000092339906],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00017316273,0.000068012014,0.0022272628,0.000056965127,0.000013104814,0.00030148833,0.000107554355,0.97202784,0.0197108,0.0012982524,0.00013586722,0.003879606],"study_design_scores_gemma":[0.00002278062,0.00004903473,0.00046602453,0.000003416521,0.0000029103237,0.000016950606,0.000020930403,0.9971199,0.00203371,0.00015505038,0.00010457391,0.000004668539],"about_ca_topic_score_codex":0.0065642586,"about_ca_topic_score_gemma":0.0024558322,"teacher_disagreement_score":0.0065642586,"about_ca_system_score_codex":0.00054839294,"about_ca_system_score_gemma":0.0006774922,"threshold_uncertainty_score":0.013052106},"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":"review","genre_gemma":"review","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"review","genre_consensus":"review","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0053092404,0.9884403,0.0019365817,0.001674922,0.00029744813,0.000016170872,0.000015741249,0.000035588084,0.0022739978],"genre_scores_gemma":[0.046566803,0.9445112,0.004537152,0.000982932,0.0015405277,0.000035332392,0.00007563687,0.000025309264,0.0017250903],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.998741,0.00023855583,0.0001821987,0.00027392115,0.00045087517,0.00011350723],"domain_scores_gemma":[0.99319357,0.0038628436,0.0008400349,0.00011768284,0.0016987275,0.00028707608],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.003646037,0.0008313642,0.0016336465,0.0019969265,0.0005354765,0.0025269468,0.0018128133,0.0032316826,0.003870051],"category_scores_gemma":[0.0036304924,0.00049018057,0.0008695476,0.0018059803,0.0015275627,0.0023550035,0.00076586823,0.0014147075,0.0010227935],"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":[0.0004899844,0.00070254627,0.0024266667,0.010729463,0.000117035284,0.0001582542,0.00023021727,0.0023043463,0.0060741547,0.0023342823,0.0030689926,0.9713641],"study_design_scores_gemma":[0.00033495223,0.013105798,0.040537134,0.021663021,0.0022489915,0.0038756314,0.0042521907,0.0130259255,0.058524612,0.013731392,0.82818246,0.0005178988],"about_ca_topic_score_codex":0.0021310668,"about_ca_topic_score_gemma":0.0019418944,"teacher_disagreement_score":0.003870051,"about_ca_system_score_codex":0.00077706086,"about_ca_system_score_gemma":0.0021240807,"threshold_uncertainty_score":0.019282281},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9320641,0.0005436963,0.04635737,0.0011841459,0.00010152679,0.000058115853,0.00012794789,0.0002709804,0.019292045],"genre_scores_gemma":[0.99517596,0.000076187156,0.0011171852,0.000029946208,0.000044854587,0.000015991885,0.00003074971,0.000023081127,0.0034860673],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997223,0.00006791043,0.000009454096,0.00005647784,0.00010079138,0.00004308798],"domain_scores_gemma":[0.9984315,0.0007822668,0.00027750953,0.000054897464,0.00030805747,0.00014566517],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00050423597,0.00081276346,0.00061542465,0.0006519482,0.0010090383,0.0020807667,0.00057397754,0.0010695354,0.0013296087],"category_scores_gemma":[0.0032207174,0.0004308176,0.0003137893,0.00033449984,0.0023638331,0.001208971,0.0014351973,0.0010343386,0.00024042661],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.002432183,0.00030142616,0.0049400423,0.00022290854,0.000089456786,0.0008272285,0.0005937219,0.8007073,0.09095082,0.086254366,0.0015558675,0.011124661],"study_design_scores_gemma":[0.000057320223,0.00010092771,0.0009980464,0.0000056148406,0.00000750528,0.00004337979,0.0000502472,0.9907487,0.0036708529,0.0041594584,0.0001337219,0.000024101537],"about_ca_topic_score_codex":0.0075857076,"about_ca_topic_score_gemma":0.0018909808,"teacher_disagreement_score":0.0075857076,"about_ca_system_score_codex":0.0012490251,"about_ca_system_score_gemma":0.0009504818,"threshold_uncertainty_score":0.015083075},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.24666843,0.001046745,0.7217433,0.0010207104,0.00019644383,0.00010298571,0.00017123287,0.0004286756,0.028621454],"genre_scores_gemma":[0.9319232,0.0004478921,0.04954214,0.00014694159,0.00012259316,0.00011983292,0.00009002855,0.00010014966,0.01750717],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998542,0.000051057807,0.000005653015,0.000021250637,0.000046733232,0.000021182368],"domain_scores_gemma":[0.99969256,0.00013729747,0.0000787538,0.00001737831,0.000048384903,0.000025576739],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00038862936,0.0005845978,0.0005971979,0.00067718874,0.00033093928,0.00081255514,0.00061665644,0.0009044661,0.0019993274],"category_scores_gemma":[0.0012096813,0.00030547354,0.0004924973,0.0002799146,0.001316645,0.0007484861,0.0009967207,0.0009307492,0.00029609373],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0001038875,0.00007586118,0.00123634,0.00020237366,0.00004142634,0.00041309354,0.0003461256,0.7743729,0.017780272,0.18826997,0.0014090538,0.015748745],"study_design_scores_gemma":[0.0000063393763,0.000016742315,0.00021785106,0.000006764791,0.0000024808078,0.000032273627,0.000023454208,0.9919728,0.0005368176,0.0067341235,0.00043929068,0.000010940681],"about_ca_topic_score_codex":0.0035616527,"about_ca_topic_score_gemma":0.0024534035,"teacher_disagreement_score":0.0035616527,"about_ca_system_score_codex":0.0007761909,"about_ca_system_score_gemma":0.00074781873,"threshold_uncertainty_score":0.0070818067},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.91838914,0.00021725114,0.06943312,0.00018573937,0.0000485651,0.000074897485,0.00030326482,0.00060493324,0.010742996],"genre_scores_gemma":[0.9929436,0.000055429355,0.00558848,0.000014882074,0.000007662557,0.00003935894,0.00012728554,0.00004786103,0.0011753904],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998641,0.000037410777,0.0000054712546,0.00001588679,0.000045919864,0.000031236897],"domain_scores_gemma":[0.9995048,0.00025416294,0.000052490675,0.000020947717,0.00012678339,0.000040796975],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000359516,0.0006629877,0.0003908495,0.0007815322,0.00040010115,0.00049663486,0.0004771684,0.00089394295,0.0009876488],"category_scores_gemma":[0.0012907363,0.00020856448,0.0003677846,0.00029272717,0.00040974768,0.00032572763,0.00033659945,0.00040881266,0.00016126368],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00006211695,0.00003415668,0.002395475,0.00003154792,0.000007949876,0.00011181466,0.00004653742,0.9907952,0.0026997365,0.0013376913,0.0001622942,0.0023156037],"study_design_scores_gemma":[0.0000020201185,0.0000051433644,0.00023746358,0.0000013803892,7.011702e-7,0.0000025602164,0.0000048583956,0.9993231,0.00032137893,0.000066483604,0.000033313765,0.0000015693392],"about_ca_topic_score_codex":0.015837511,"about_ca_topic_score_gemma":0.005183466,"teacher_disagreement_score":0.015837511,"about_ca_system_score_codex":0.00056673144,"about_ca_system_score_gemma":0.0005593861,"threshold_uncertainty_score":0.031490684},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9902367,0.000016686288,0.008985737,0.000011802486,0.0000029769046,0.000008184587,0.000104292405,0.000075550066,0.00055796106],"genre_scores_gemma":[0.9993438,0.000009095097,0.00043389952,0.0000014402862,0.0000012478613,0.000004267415,0.00008493801,0.000007649014,0.00011375927],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99988973,0.000013466711,0.0000049262253,0.00002468192,0.00004168764,0.000025560053],"domain_scores_gemma":[0.99942625,0.00030813567,0.00009332063,0.000045688466,0.00007674465,0.00004989575],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023381614,0.0002830723,0.00021680271,0.0004325527,0.00017601709,0.00023047485,0.00027754443,0.00019908288,0.0009996826],"category_scores_gemma":[0.00084310654,0.00016541743,0.00022559395,0.00023917461,0.0005487122,0.00018579638,0.00023241586,0.00027457034,0.00009296296],"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":[0.0007815047,0.00017692114,0.04329587,0.00013107438,0.00006458925,0.0010449678,0.00027467858,0.37940088,0.554274,0.0034939388,0.00032693445,0.0167346],"study_design_scores_gemma":[0.0000128441025,0.00023143418,0.078414194,0.0000053293275,0.000014192862,0.00014494652,0.000075115124,0.8530749,0.067384236,0.0004909158,0.00011460998,0.00003723532],"about_ca_topic_score_codex":0.0018596674,"about_ca_topic_score_gemma":0.00075874163,"teacher_disagreement_score":0.0018596674,"about_ca_system_score_codex":0.00024192562,"about_ca_system_score_gemma":0.0002138329,"threshold_uncertainty_score":0.0036976933},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.70343953,0.00023790558,0.28441298,0.00023026626,0.000117031945,0.00012681523,0.0003753303,0.00073098147,0.010329196],"genre_scores_gemma":[0.9544888,0.00010712146,0.042563997,0.000029019535,0.000017136212,0.00010710378,0.00016330986,0.000054146338,0.002469181],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99985707,0.000040948744,0.0000064158357,0.000011950268,0.00006182687,0.000021755262],"domain_scores_gemma":[0.9996049,0.0002464776,0.000030531784,0.000019013109,0.00006276711,0.000036374593],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00036710032,0.00033049725,0.0006779268,0.00032923147,0.00044670035,0.0006455173,0.0006138924,0.0005730538,0.0011924113],"category_scores_gemma":[0.0010199997,0.000290022,0.0003947803,0.00035179593,0.0005716436,0.00044049372,0.00044544917,0.00048440354,0.0002144219],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00007106919,0.00003789815,0.0009085447,0.000028694047,0.000010557128,0.00006227504,0.000037712005,0.98728186,0.0076841777,0.0015922753,0.00008887454,0.0021960232],"study_design_scores_gemma":[0.000014312237,0.000010251689,0.00009117845,0.000001371951,0.0000011898468,0.0000044971766,0.0000043782265,0.9988625,0.00074610586,0.00019391891,0.00006760052,0.0000028022387],"about_ca_topic_score_codex":0.008901408,"about_ca_topic_score_gemma":0.0034738157,"teacher_disagreement_score":0.008901408,"about_ca_system_score_codex":0.0006504609,"about_ca_system_score_gemma":0.0010873879,"threshold_uncertainty_score":0.017699182},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98797137,0.00006876239,0.0112531325,0.000019538607,0.000006555758,0.000019160441,0.000031557527,0.000054467993,0.00057545],"genre_scores_gemma":[0.9970927,0.000053820047,0.002356525,0.0000062972404,0.0000018391548,0.000012600566,0.000033214157,0.00001123186,0.00043188522],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999143,0.000017856695,0.0000064989895,0.000017624065,0.000025663221,0.000018068045],"domain_scores_gemma":[0.9997024,0.00015436155,0.000045302135,0.000031047217,0.000043561817,0.000023229799],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002830318,0.0004897331,0.00028106236,0.00020272333,0.00023987913,0.0005729776,0.000344497,0.00046244528,0.00054017396],"category_scores_gemma":[0.0006351229,0.00026010038,0.00033282788,0.00013776637,0.0003316316,0.00050176197,0.00033089574,0.00041154923,0.00009924382],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00030531385,0.00018512872,0.00991038,0.00008837798,0.000019495757,0.00022920575,0.000111489804,0.6273211,0.35474738,0.0007190415,0.00008706159,0.006275924],"study_design_scores_gemma":[0.000026433014,0.00030026076,0.0044155433,0.000004662982,0.0000099582585,0.000029333138,0.000020282381,0.9389623,0.055962685,0.00012358831,0.00013155743,0.000013346875],"about_ca_topic_score_codex":0.0040200297,"about_ca_topic_score_gemma":0.0021495782,"teacher_disagreement_score":0.0040200297,"about_ca_system_score_codex":0.000429391,"about_ca_system_score_gemma":0.00029676154,"threshold_uncertainty_score":0.007993281},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99208903,0.000121914076,0.007319196,0.000015676302,0.000017708942,0.000015851001,0.000011368212,0.00005746601,0.0003516695],"genre_scores_gemma":[0.9967824,0.000044628327,0.0028569147,0.000011316818,0.0000075958615,0.000011097444,0.0000118944245,0.000009727688,0.00026436755],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99955803,0.000073791394,0.000030265619,0.00008927618,0.00016159045,0.00008699694],"domain_scores_gemma":[0.9985287,0.00053054444,0.00039826994,0.0001542252,0.00026600825,0.0001221159],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00051903044,0.00046581344,0.00048091132,0.00021197346,0.00023051244,0.00035110657,0.0003362122,0.00025446725,0.00062414363],"category_scores_gemma":[0.0012112159,0.00018760502,0.0001365799,0.0001126729,0.00059127115,0.0003538985,0.0005879082,0.00025181985,0.00009486404],"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":[0.00039600738,0.000042635766,0.00039195703,0.000044426666,0.0000040126633,0.000051100607,0.00006918133,0.0009444773,0.99438125,0.00012162956,0.000022538292,0.0035307417],"study_design_scores_gemma":[0.00007764893,0.0022684676,0.004740028,0.000011576307,0.000027131508,0.00015772639,0.00004942431,0.012492629,0.9790608,0.000107133565,0.0009729923,0.00003448899],"about_ca_topic_score_codex":0.00027721943,"about_ca_topic_score_gemma":0.00023617274,"teacher_disagreement_score":0.00062414363,"about_ca_system_score_codex":0.00014736585,"about_ca_system_score_gemma":0.00021279704,"threshold_uncertainty_score":0.0027449727},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.461947,0.00018714851,0.5059002,0.0002683628,0.00012227842,0.00012819117,0.0006493665,0.0030839439,0.027713474],"genre_scores_gemma":[0.8813759,0.00008852769,0.1148721,0.000041604584,0.000023828972,0.00012712574,0.0004032949,0.00025486044,0.002812818],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998512,0.000029384913,0.000006038712,0.000016913229,0.00007403885,0.000022326676],"domain_scores_gemma":[0.99945396,0.0002379642,0.000040028906,0.000054732445,0.00016683707,0.00004652255],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00039499393,0.0007083302,0.00074009673,0.00076257694,0.0007608022,0.0006387627,0.0007602905,0.00066400383,0.0028089616],"category_scores_gemma":[0.0011314243,0.000290782,0.00044170153,0.0006531177,0.00062597636,0.00044201428,0.00079025293,0.00039480868,0.00042853368],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000852724,0.000058156216,0.0010524903,0.000044049586,0.00001271016,0.00014676379,0.00009545886,0.96986085,0.0053027817,0.0070354166,0.0006850543,0.015620927],"study_design_scores_gemma":[0.00001013546,0.000007515115,0.00013700224,0.0000021973008,0.0000012091915,0.000015234335,0.000009939934,0.997561,0.0010969455,0.00086360186,0.00029221794,0.0000030791275],"about_ca_topic_score_codex":0.0060702446,"about_ca_topic_score_gemma":0.0053602597,"teacher_disagreement_score":0.0060702446,"about_ca_system_score_codex":0.00060382736,"about_ca_system_score_gemma":0.0009702547,"threshold_uncertainty_score":0.012069821},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.11955849,0.0014927471,0.86000204,0.00076711574,0.00027375357,0.00008480102,0.00026431275,0.0006954821,0.01686125],"genre_scores_gemma":[0.91851866,0.0014374761,0.0642437,0.0002350943,0.00025879766,0.00028007262,0.00023457293,0.00041929778,0.014372383],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998072,0.00003613117,0.0000101587275,0.000049147384,0.00005674492,0.00004073109],"domain_scores_gemma":[0.9996574,0.00010930172,0.00006328228,0.00005409497,0.00006318386,0.000052743177],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004605172,0.00091252715,0.0009438409,0.0005679649,0.0004757865,0.0014965158,0.0019859832,0.0017904788,0.0010451046],"category_scores_gemma":[0.001215164,0.00046801657,0.0012540264,0.0004109357,0.001394352,0.0023462554,0.0013696398,0.0013750887,0.00040922518],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00007670427,0.00007737543,0.0012139644,0.000111475994,0.000054973876,0.0002584265,0.00017662143,0.835221,0.016976926,0.13697934,0.0012068145,0.0076463334],"study_design_scores_gemma":[0.0000032280852,0.0000092159235,0.00013838547,0.0000031702464,0.000004476682,0.000012493879,0.0000049956907,0.9911607,0.00021752267,0.007972778,0.0004648795,0.000008189623],"about_ca_topic_score_codex":0.004315788,"about_ca_topic_score_gemma":0.0015528225,"teacher_disagreement_score":0.004315788,"about_ca_system_score_codex":0.0010195567,"about_ca_system_score_gemma":0.0007807401,"threshold_uncertainty_score":0.00858134},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.992002,0.00007891855,0.0068873977,0.000035413952,0.000009569342,0.0000058407245,0.000009623494,0.000084388244,0.0008868132],"genre_scores_gemma":[0.9987602,0.00002118247,0.0010052628,0.0000048302522,0.0000020336208,0.000003051429,0.0000043316973,0.000007138697,0.00019194608],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99985766,0.000039074483,0.000006340681,0.00002106162,0.0000363958,0.00003950353],"domain_scores_gemma":[0.99896026,0.0007214231,0.00010750218,0.00005147033,0.000076954915,0.0000823781],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00043210867,0.00031626318,0.0004414749,0.00021960196,0.00049890386,0.0004891572,0.0002544772,0.00041866198,0.0010015526],"category_scores_gemma":[0.0017481353,0.0002444814,0.0002870133,0.000082140934,0.00089348777,0.0004484812,0.0006544493,0.0004228532,0.00009730043],"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":[0.0012103132,0.00013016287,0.0054994775,0.00018530068,0.000045390836,0.0007264046,0.00057440164,0.37359917,0.5954054,0.0041050166,0.00026913537,0.018249769],"study_design_scores_gemma":[0.00006006764,0.0010028532,0.005585491,0.000021304775,0.00003729333,0.00021602924,0.000109939065,0.86275727,0.12901016,0.00071042177,0.0004378518,0.000051313356],"about_ca_topic_score_codex":0.0010399761,"about_ca_topic_score_gemma":0.0006310771,"teacher_disagreement_score":0.0010399761,"about_ca_system_score_codex":0.0002672292,"about_ca_system_score_gemma":0.0003652317,"threshold_uncertainty_score":0.003350556},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9877758,0.00010139473,0.0092039425,0.0001159278,0.00006016584,0.000017661805,0.00010539091,0.00020237091,0.002417324],"genre_scores_gemma":[0.99603575,0.00005038558,0.0027612366,0.000013215924,0.000011451541,0.000006783966,0.000091746755,0.000014229414,0.0010151592],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998317,0.00002391385,0.0000100778425,0.00002566198,0.0000870669,0.000021547325],"domain_scores_gemma":[0.99944717,0.00027210102,0.000035820307,0.00003873457,0.00016275715,0.00004336225],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021247852,0.00029123898,0.00039508505,0.00059398776,0.00045302548,0.000338291,0.00024253833,0.00042209364,0.00081567717],"category_scores_gemma":[0.000849168,0.00014023787,0.00026548607,0.00019235272,0.00058203924,0.00026312115,0.00027210533,0.00023184421,0.00015695527],"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":[0.0010987194,0.00028880173,0.032971606,0.00019604123,0.00004876972,0.004408588,0.0010255128,0.23082897,0.68785334,0.0027695026,0.0014732477,0.037036926],"study_design_scores_gemma":[0.00008987091,0.0007340099,0.041946832,0.000040646803,0.000042566742,0.000947969,0.0004169773,0.77630824,0.17588289,0.00080184,0.0026954925,0.0000926394],"about_ca_topic_score_codex":0.0040319534,"about_ca_topic_score_gemma":0.0020420155,"teacher_disagreement_score":0.0040319534,"about_ca_system_score_codex":0.0004358694,"about_ca_system_score_gemma":0.0003814533,"threshold_uncertainty_score":0.008017004},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98951656,0.00039648617,0.007913478,0.000032883203,0.000026376723,0.00004445305,0.0002525238,0.00009638732,0.0017208308],"genre_scores_gemma":[0.99218655,0.00035467843,0.0062240944,0.000017569573,0.000017763508,0.00005530038,0.0002924782,0.000018705727,0.0008328695],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99983156,0.00001277684,0.000014202359,0.00004115166,0.0000654898,0.0000349169],"domain_scores_gemma":[0.9996278,0.00012239428,0.0000850252,0.000033326338,0.00010007761,0.000031264946],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00028591455,0.00024961468,0.00017719281,0.00028836413,0.00025529665,0.0002496963,0.00024151565,0.00020384908,0.0016789376],"category_scores_gemma":[0.0004529011,0.00012231681,0.000121713776,0.00028091314,0.00026203238,0.00033127388,0.00018939967,0.00031072187,0.00015261154],"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":[0.00011370952,0.000043914915,0.0013606464,0.00007627902,0.0000029314397,0.000084875355,0.00009950094,0.0004950391,0.9923609,0.0002510851,0.000105941624,0.0050053117],"study_design_scores_gemma":[0.000014906013,0.0004418581,0.013510463,0.000009972611,0.000014286756,0.00013838439,0.000073160016,0.005602765,0.97843117,0.000088062436,0.0016555709,0.000019404524],"about_ca_topic_score_codex":0.00064377947,"about_ca_topic_score_gemma":0.0007148818,"teacher_disagreement_score":0.0016789376,"about_ca_system_score_codex":0.00024588985,"about_ca_system_score_gemma":0.00019506761,"threshold_uncertainty_score":0.0056166053},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9951616,0.00008386991,0.0043297852,0.000005806826,0.0000034544164,0.000005735399,0.000086196844,0.000024187519,0.00029943392],"genre_scores_gemma":[0.9958263,0.000077638855,0.0035351764,0.0000067423675,0.0000044055682,0.000008025757,0.0002946804,0.00001111812,0.00023590261],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999187,0.000004681813,0.0000047847734,0.000018155626,0.000036527483,0.000017215421],"domain_scores_gemma":[0.999864,0.000031038322,0.00003461651,0.000010772834,0.000036190813,0.000023358456],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012418852,0.00020055658,0.00019297474,0.0005117284,0.00017781362,0.0006032858,0.00011987432,0.00020513244,0.0005020533],"category_scores_gemma":[0.00026015023,0.00017262965,0.00013924344,0.00038397717,0.0002618498,0.0002819252,0.00018030389,0.00026496666,0.00007604351],"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":[0.00030152878,0.00006131833,0.020404652,0.000057592802,0.000010721397,0.00046478782,0.00020252803,0.009735512,0.95332503,0.000971395,0.000092621034,0.014372424],"study_design_scores_gemma":[0.000074345655,0.0003901654,0.46553314,0.000026729513,0.00004030563,0.00090520945,0.00041976685,0.20830016,0.32067087,0.0011263215,0.0023945735,0.000118452845],"about_ca_topic_score_codex":0.0006853796,"about_ca_topic_score_gemma":0.00050817785,"teacher_disagreement_score":0.0006853796,"about_ca_system_score_codex":0.00024909235,"about_ca_system_score_gemma":0.00024175891,"threshold_uncertainty_score":0.0018072724},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99424064,0.00014097583,0.0043949247,0.000017628963,0.0000130908675,0.000007302359,0.000068417066,0.00010662799,0.0010105348],"genre_scores_gemma":[0.99792,0.00007865699,0.0013463813,0.000010148684,0.0000078401345,0.0000044861167,0.00024082675,0.000023672741,0.0003681144],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999206,0.0000074217296,0.0000049103455,0.000016026655,0.000022866838,0.000028125673],"domain_scores_gemma":[0.9996406,0.00009127376,0.00004984999,0.000030375053,0.00009850569,0.00008942526],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017745893,0.00027780546,0.00028216426,0.000786192,0.00018157247,0.000654116,0.00018534606,0.00022201506,0.0013436025],"category_scores_gemma":[0.00042193633,0.00016825313,0.00037813184,0.00039485705,0.00044582042,0.0003632627,0.0003056591,0.00027749603,0.00015641518],"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":[0.0032093737,0.0005237518,0.05910593,0.00026574513,0.00019655794,0.002295752,0.001114553,0.11469009,0.73538274,0.005057916,0.0010035028,0.07715411],"study_design_scores_gemma":[0.00031272127,0.0013656102,0.51888937,0.00005656325,0.00012405838,0.00071284064,0.0009902534,0.41489258,0.058332812,0.0024707075,0.001617211,0.00023518021],"about_ca_topic_score_codex":0.0016883324,"about_ca_topic_score_gemma":0.00076279056,"teacher_disagreement_score":0.0016883324,"about_ca_system_score_codex":0.00023274496,"about_ca_system_score_gemma":0.00022337207,"threshold_uncertainty_score":0.004494846},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9986965,0.00002242014,0.0008239913,0.000011994572,0.000009556524,0.0000038404646,0.000058161124,0.000029785253,0.0003437079],"genre_scores_gemma":[0.9993862,0.000012405119,0.00032890175,0.000006518754,0.0000062394047,0.000003777179,0.000071923096,0.000008883091,0.00017522882],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.9996265,0.000031080617,0.000020843809,0.00008356907,0.00016186682,0.000076095144],"domain_scores_gemma":[0.9994079,0.00020765045,0.00007530728,0.000048120688,0.0001413259,0.0001197785],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00037571392,0.00030258545,0.000648767,0.0007640546,0.0009746816,0.0008392832,0.00051850535,0.0006051917,0.0006359199],"category_scores_gemma":[0.0012570489,0.00028924635,0.00029471202,0.00044301254,0.0009136952,0.00052826334,0.00058493443,0.0006527163,0.000113371694],"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":[0.0037991493,0.0003001749,0.03046086,0.000044560886,0.000043821696,0.00068309944,0.0010057366,0.0047780876,0.9478668,0.0005595916,0.00017364508,0.010284464],"study_design_scores_gemma":[0.00046221528,0.0030717808,0.47338706,0.000028324,0.0001582313,0.0010245126,0.0010915743,0.075265296,0.4434119,0.0005340225,0.001305091,0.00026002416],"about_ca_topic_score_codex":0.0035957699,"about_ca_topic_score_gemma":0.002458876,"teacher_disagreement_score":0.0035957699,"about_ca_system_score_codex":0.0005007996,"about_ca_system_score_gemma":0.00036342183,"threshold_uncertainty_score":0.0071496964},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6756458,0.0007893251,0.31740844,0.0002271109,0.00028374745,0.00012416045,0.000055968143,0.00053919625,0.004926188],"genre_scores_gemma":[0.9722474,0.00022243163,0.02639078,0.000052217278,0.00004661682,0.000059815186,0.00003021006,0.000034822075,0.000915697],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997665,0.000050015566,0.000022773136,0.000039370974,0.00009229165,0.000029114259],"domain_scores_gemma":[0.999345,0.0003409654,0.00017214318,0.000036609545,0.00005489762,0.000050306026],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00039012902,0.00035401288,0.0002191627,0.00016155474,0.00017761452,0.00051066297,0.00038105846,0.00022683997,0.0007722585],"category_scores_gemma":[0.0010319926,0.00014869294,0.000162958,0.00007493564,0.0004466618,0.0002808427,0.000406316,0.00036386956,0.000105581596],"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":[0.00036941786,0.0000610113,0.0003233582,0.0001787459,0.000016230182,0.00014291302,0.0001023677,0.01000829,0.9658939,0.0030405691,0.0001419524,0.01972123],"study_design_scores_gemma":[0.00023077049,0.0014814975,0.0013561317,0.000029178229,0.000042631455,0.00026764508,0.000077616074,0.11512308,0.86855125,0.0017577512,0.011031857,0.000050489558],"about_ca_topic_score_codex":0.000057575722,"about_ca_topic_score_gemma":0.0001204873,"teacher_disagreement_score":0.0007722585,"about_ca_system_score_codex":0.00010914018,"about_ca_system_score_gemma":0.00015055147,"threshold_uncertainty_score":0.0025835037},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.96346307,0.000119792545,0.032166276,0.00007714416,0.000020556508,0.000045688757,0.0006374359,0.00043425328,0.0030358424],"genre_scores_gemma":[0.9918745,0.00007357072,0.0067304196,0.000009993043,0.000006231786,0.000027419572,0.0003043657,0.00003395058,0.0009394837],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99982905,0.000027706688,0.00001574875,0.000024306733,0.0000827846,0.000020286156],"domain_scores_gemma":[0.99962866,0.00020904023,0.00003102513,0.0000393017,0.00006871728,0.0000231882],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025105104,0.0004896137,0.00040148446,0.0004925353,0.0003383776,0.0006281165,0.00021458553,0.00038581743,0.00093476754],"category_scores_gemma":[0.0006749153,0.00014430362,0.00027343683,0.0003499752,0.0005256267,0.00049188174,0.0003077099,0.00031303693,0.00014284451],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0005510672,0.00023895492,0.023218287,0.00023243172,0.000050429946,0.00094585377,0.00078944257,0.5202462,0.4231179,0.0031483523,0.0007561135,0.026705008],"study_design_scores_gemma":[0.000024198573,0.00016063046,0.013693165,0.000011600575,0.000010103448,0.000074419164,0.0001651373,0.9457399,0.038903475,0.00031803467,0.00086326874,0.000036075926],"about_ca_topic_score_codex":0.0029463698,"about_ca_topic_score_gemma":0.0015547052,"teacher_disagreement_score":0.0029463698,"about_ca_system_score_codex":0.00026595427,"about_ca_system_score_gemma":0.00027888716,"threshold_uncertainty_score":0.005858481},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.93927336,0.000021253167,0.06032992,0.000011648952,0.0000027799238,0.000004421334,0.00001788304,0.00007010419,0.00026859055],"genre_scores_gemma":[0.9908839,0.00001200289,0.008973979,0.0000021960225,0.0000020797788,0.0000029664388,0.000028460043,0.000004410755,0.0000899116],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99991477,0.000019121415,0.000003419347,0.00001667742,0.000033699984,0.000012255597],"domain_scores_gemma":[0.99966764,0.0001872472,0.000053577376,0.00001982244,0.000043594548,0.000028014436],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025728298,0.00014644134,0.00014176684,0.00036985026,0.00011589315,0.000269602,0.00015111656,0.00017786551,0.00020484708],"category_scores_gemma":[0.00094277586,0.00012475302,0.00011929072,0.0001701324,0.00036846683,0.00024871976,0.00019235235,0.00016512621,0.00003877812],"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":[0.00063894805,0.00015005394,0.030348742,0.0000756032,0.000048219194,0.0004409641,0.00025385764,0.42868555,0.47847885,0.0038510375,0.00020856962,0.05681965],"study_design_scores_gemma":[0.000011263561,0.00007431562,0.018908568,0.000003005973,0.000005583796,0.00005947733,0.000034363995,0.95416516,0.026317423,0.00032514517,0.000074365955,0.000021319393],"about_ca_topic_score_codex":0.0010654284,"about_ca_topic_score_gemma":0.0007793631,"teacher_disagreement_score":0.0010654284,"about_ca_system_score_codex":0.00012358934,"about_ca_system_score_gemma":0.00016295022,"threshold_uncertainty_score":0.0021184683},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9845095,0.00011779147,0.014871773,0.000017762359,0.0000147990295,0.000010443686,0.000012330455,0.00009560565,0.0003500309],"genre_scores_gemma":[0.9939949,0.00004575435,0.0057478594,0.000005307438,0.0000031207305,0.000009594182,0.000010160553,0.0000062808435,0.0001770715],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99987507,0.000018501436,0.000009053033,0.000030745738,0.00004239401,0.000024144141],"domain_scores_gemma":[0.9995752,0.00013786046,0.00015114392,0.000044982073,0.00006536264,0.000025477168],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00030177904,0.0002702794,0.00026917513,0.00014053879,0.00012455677,0.0001757769,0.00029449433,0.00022982116,0.00026669214],"category_scores_gemma":[0.0004738033,0.00013441553,0.00018635968,0.000065554035,0.00035676124,0.00020136709,0.0002637209,0.00015116944,0.0000767891],"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":[0.000121649595,0.000026894679,0.0005105678,0.00005346259,0.0000041354647,0.00008840817,0.000055838736,0.006185744,0.98895824,0.00016605043,0.000026626889,0.0038023337],"study_design_scores_gemma":[0.00005332592,0.0009827642,0.0034439655,0.000009524728,0.000017393266,0.000099756566,0.000040643776,0.12398402,0.8702543,0.00007989907,0.001011202,0.000023264554],"about_ca_topic_score_codex":0.00031596512,"about_ca_topic_score_gemma":0.0003081832,"teacher_disagreement_score":0.00031596512,"about_ca_system_score_codex":0.000105803214,"about_ca_system_score_gemma":0.00014444072,"threshold_uncertainty_score":0.001595974},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0081130685,0.00005574472,0.99113464,0.000032312146,0.000015738688,0.000020308586,0.0000151329195,0.00016912779,0.00044386068],"genre_scores_gemma":[0.12677321,0.00022171752,0.87049043,0.000052166615,0.000027577735,0.000111466805,0.000092596594,0.000057975656,0.0021729511],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9996742,0.00008191699,0.000018319126,0.00007798599,0.00013003426,0.000017594917],"domain_scores_gemma":[0.99969244,0.00016033034,0.0000324211,0.000025728337,0.00007660587,0.000012527337],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00051728403,0.001157106,0.0006796696,0.0005801581,0.00029926436,0.00049882324,0.0005002472,0.0011627133,0.0011504634],"category_scores_gemma":[0.0011015392,0.00040369623,0.00080175465,0.00035269104,0.0004311514,0.0008476368,0.0006150154,0.0005110258,0.00057734427],"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":[0.00028148945,0.000106556836,0.0016294181,0.0003652509,0.00009549043,0.0002479868,0.00027943664,0.21535799,0.43061158,0.006903554,0.0007929343,0.34332836],"study_design_scores_gemma":[0.00002400628,0.00011529898,0.0010227038,0.000025456795,0.00003116689,0.0002454984,0.000058201756,0.94329643,0.051128246,0.0019107389,0.0020948858,0.000047390993],"about_ca_topic_score_codex":0.00078881363,"about_ca_topic_score_gemma":0.0013183878,"teacher_disagreement_score":0.0011627133,"about_ca_system_score_codex":0.00020485917,"about_ca_system_score_gemma":0.00055719004,"threshold_uncertainty_score":0.003848672},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8400138,0.0001521917,0.14474171,0.00015299047,0.000070257156,0.00013922372,0.00015325054,0.00047640508,0.0141001465],"genre_scores_gemma":[0.96809477,0.000055580906,0.030261995,0.000018311552,0.0000074554678,0.00009951323,0.0000737513,0.000027954711,0.0013606854],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99991846,0.000018149633,0.000004495641,0.000007822873,0.0000335685,0.00001736067],"domain_scores_gemma":[0.99981743,0.00007835376,0.00001487471,0.000016284392,0.000040670955,0.000032444546],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023176064,0.00029986154,0.0003680191,0.00031282005,0.00036349893,0.00045635045,0.0006031653,0.00060481916,0.0011913021],"category_scores_gemma":[0.00054247706,0.00020338042,0.00022846421,0.00022392263,0.00043661048,0.00031114044,0.00047684734,0.00032851065,0.00015526504],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00013417761,0.00012691111,0.0014268844,0.000056963625,0.00002017785,0.00019213842,0.00018891947,0.9430219,0.03601977,0.0064358255,0.00033131757,0.012044965],"study_design_scores_gemma":[0.000015281747,0.000024166036,0.00013408103,0.0000021070664,0.00000171116,0.0000096255,0.000009455283,0.9980683,0.0012603744,0.000285892,0.00018598983,0.0000029498544],"about_ca_topic_score_codex":0.0037683481,"about_ca_topic_score_gemma":0.0016679442,"teacher_disagreement_score":0.0037683481,"about_ca_system_score_codex":0.00039833496,"about_ca_system_score_gemma":0.0007060818,"threshold_uncertainty_score":0.0074928403},"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":"methods","genre_gemma":"methods","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0008828543,0.00010676548,0.99478346,0.000050394174,0.000087355205,0.0000051449624,0.000013592245,0.00011090394,0.003959462],"genre_scores_gemma":[0.078994706,0.00055383495,0.88349444,0.00018199006,0.00023074608,0.000074569434,0.00021834101,0.00059636147,0.035655025],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997403,0.0000556609,0.000011378556,0.000038572245,0.0001417136,0.000012477072],"domain_scores_gemma":[0.99980396,0.00010083259,0.000009946933,0.00002098056,0.000054200973,0.000010152146],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00045491874,0.00084400404,0.00065100385,0.00037697426,0.00025670326,0.0008239598,0.0006506882,0.0009275984,0.0036179738],"category_scores_gemma":[0.0006709897,0.0003633496,0.00066940597,0.000312699,0.0006209654,0.001039477,0.0009766481,0.0013422379,0.0016576753],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000095002775,0.00015136859,0.00016412589,0.00030201898,0.000078661884,0.00014794993,0.00012654853,0.37347957,0.070971355,0.21831347,0.013260418,0.3229096],"study_design_scores_gemma":[0.000009373788,0.000030651663,0.000091159854,0.000019757692,0.000013381196,0.00012422676,0.000014805054,0.92435914,0.009232569,0.055243988,0.010838445,0.000022476666],"about_ca_topic_score_codex":0.00034142568,"about_ca_topic_score_gemma":0.0006034335,"teacher_disagreement_score":0.0036179738,"about_ca_system_score_codex":0.0001868588,"about_ca_system_score_gemma":0.00033147546,"threshold_uncertainty_score":0.012103319},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.88944846,0.0010652771,0.0670878,0.00011145599,0.000084897976,0.000086105494,0.00066454447,0.00047993462,0.040971417],"genre_scores_gemma":[0.9931666,0.0001929084,0.0027214733,0.000024053612,0.00001913264,0.000020968335,0.0004316077,0.00003195862,0.0033912333],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.9995751,0.00004590042,0.000016236118,0.000048742062,0.00026364086,0.000050349914],"domain_scores_gemma":[0.9985728,0.0005719869,0.00007007769,0.000039222392,0.00069773826,0.000048119568],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021186778,0.00017690363,0.00015201258,0.0010077487,0.00018447402,0.00041062088,0.0001752531,0.00029745692,0.0037610857],"category_scores_gemma":[0.0014379546,0.0000988923,0.00010337383,0.0007048576,0.000118391275,0.00029169553,0.00016336824,0.00022863461,0.0008763941],"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":[0.00087302655,0.00017676242,0.029741557,0.00039570386,0.000057820944,0.0009935574,0.00070413266,0.039131355,0.6896617,0.0036050954,0.0019046171,0.23275469],"study_design_scores_gemma":[0.0001248628,0.0018450323,0.40082678,0.00014480001,0.000104355335,0.005276202,0.0014018052,0.24454032,0.3136769,0.0038480796,0.02802361,0.00018724866],"about_ca_topic_score_codex":0.0021375439,"about_ca_topic_score_gemma":0.0011743887,"teacher_disagreement_score":0.0037610857,"about_ca_system_score_codex":0.00016880575,"about_ca_system_score_gemma":0.00016824863,"threshold_uncertainty_score":0.012582064},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98132986,0.00011720787,0.017257571,0.000020766498,0.0000070342226,0.000008723296,0.000014431154,0.00006154372,0.0011828401],"genre_scores_gemma":[0.9958442,0.000030059395,0.003674657,0.0000049354935,0.0000019585361,0.0000063404427,0.00000794617,0.000004741441,0.0004252735],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999372,0.0000130983435,0.0000027766384,0.000017638158,0.000016596021,0.000012763478],"domain_scores_gemma":[0.99983037,0.00006081025,0.000043482094,0.000018922132,0.000025127181,0.000021225136],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020285521,0.00014477054,0.00017102977,0.00014956176,0.00017278362,0.00022967023,0.0002589629,0.0002460601,0.00082959834],"category_scores_gemma":[0.0003198875,0.00017634685,0.00012211053,0.000081931124,0.00056994264,0.00019179525,0.00031066174,0.00014690707,0.00012372223],"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":[0.00031162807,0.000044121356,0.004523701,0.00012839319,0.000027866932,0.00082491245,0.00049507566,0.052718025,0.9266515,0.004487453,0.00022439435,0.009563053],"study_design_scores_gemma":[0.00008811371,0.00074328546,0.009982459,0.00003076458,0.000033260567,0.0006581195,0.00030489278,0.7920104,0.1929027,0.0015428797,0.0016451412,0.000057977708],"about_ca_topic_score_codex":0.00033917194,"about_ca_topic_score_gemma":0.00021756352,"teacher_disagreement_score":0.00082959834,"about_ca_system_score_codex":0.00011755981,"about_ca_system_score_gemma":0.00015154252,"threshold_uncertainty_score":0.0027753115},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9909121,0.0000768564,0.008086442,0.000016049327,0.000005934555,0.0000064937353,0.000015052553,0.000038204005,0.00084282627],"genre_scores_gemma":[0.9961593,0.000028113074,0.003494254,0.0000052215664,0.0000013499912,0.0000069407647,0.00001126592,0.0000042459455,0.00028925057],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999441,0.000008177879,0.0000029829725,0.00001731825,0.000013321768,0.000014021618],"domain_scores_gemma":[0.9998173,0.000058481557,0.000050787177,0.000023895405,0.000025498848,0.00002410782],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020403635,0.00015454821,0.00016949364,0.0001335091,0.00017521234,0.0002351302,0.0002603964,0.0002376772,0.00079462817],"category_scores_gemma":[0.0002728137,0.00017866184,0.00017836668,0.00007799886,0.0004698381,0.0001992232,0.00031974664,0.00016143847,0.000113436916],"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":[0.0002773552,0.000056727065,0.0049567986,0.00013647131,0.000027421554,0.00064913696,0.00043755778,0.05100319,0.9311597,0.003809109,0.00018955224,0.007296992],"study_design_scores_gemma":[0.000096109135,0.0008083285,0.012255996,0.000032148593,0.000038409995,0.00048557538,0.00033212625,0.7647473,0.21839201,0.0012452063,0.0015007927,0.000066002576],"about_ca_topic_score_codex":0.00040370776,"about_ca_topic_score_gemma":0.00029326795,"teacher_disagreement_score":0.00079462817,"about_ca_system_score_codex":0.00011774638,"about_ca_system_score_gemma":0.00017848969,"threshold_uncertainty_score":0.002658248},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9971186,0.00008390943,0.0023971521,0.000007603983,0.0000041812077,0.0000053365357,0.000017448769,0.000059692517,0.00030612317],"genre_scores_gemma":[0.9992933,0.000025704729,0.0005896333,0.0000036881736,0.0000018198486,0.000004097398,0.000009626265,0.000009123609,0.000062846964],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997222,0.00006647965,0.000014314013,0.00005384811,0.00007977604,0.000063474545],"domain_scores_gemma":[0.99699914,0.0021145744,0.00035840602,0.00015595098,0.00020712252,0.0001647232],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00041655527,0.00032517905,0.00036135846,0.00020897234,0.00018434372,0.00039699452,0.00026815257,0.00030009032,0.0008891853],"category_scores_gemma":[0.0016431567,0.00023824534,0.00020377485,0.000100923775,0.0006146676,0.00032683063,0.00046189807,0.0002592057,0.00012427809],"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":[0.0004930632,0.00003350071,0.0016976711,0.00007391255,0.000009910349,0.00012816025,0.000111206,0.0070562507,0.98593,0.000086268104,0.000023060102,0.004356994],"study_design_scores_gemma":[0.00008212159,0.0038285172,0.030110875,0.000028384085,0.000081705606,0.00022749613,0.00024910946,0.042598546,0.92190844,0.00017442285,0.00064154126,0.00006894127],"about_ca_topic_score_codex":0.0002636437,"about_ca_topic_score_gemma":0.0002623231,"teacher_disagreement_score":0.0008891853,"about_ca_system_score_codex":0.0001432589,"about_ca_system_score_gemma":0.00016220612,"threshold_uncertainty_score":0.0029746294},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.12041719,0.00046390595,0.86794287,0.00041062475,0.00015636816,0.00015497902,0.00028033194,0.0015277133,0.008646068],"genre_scores_gemma":[0.5664948,0.000626212,0.4204733,0.00011048397,0.000092489674,0.0005022626,0.0004300667,0.0005791337,0.010691213],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998479,0.00004093642,0.000008871021,0.000021662729,0.000065479006,0.000015176999],"domain_scores_gemma":[0.99949896,0.00029165362,0.000057735113,0.000040083964,0.000082521314,0.000028891835],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004984603,0.0005352038,0.00075596623,0.0004923689,0.00060380204,0.0010112985,0.00086545595,0.00096961524,0.0031419727],"category_scores_gemma":[0.001244937,0.00054631295,0.0007606047,0.00034578057,0.0006516954,0.0010289276,0.0008529539,0.00091018534,0.00053777103],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00005648836,0.00008361035,0.0011558201,0.00011905875,0.000039946073,0.00009523692,0.0001502084,0.9532563,0.009867989,0.013389694,0.0010334996,0.02075225],"study_design_scores_gemma":[0.000006326129,0.0000035384273,0.000052660234,0.0000020620105,0.0000010315605,0.0000040875616,0.0000034119128,0.9986299,0.00038908457,0.0005432566,0.00036208748,0.0000026234795],"about_ca_topic_score_codex":0.008106193,"about_ca_topic_score_gemma":0.006289142,"teacher_disagreement_score":0.008106193,"about_ca_system_score_codex":0.00067428855,"about_ca_system_score_gemma":0.0016973902,"threshold_uncertainty_score":0.01611805},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9947056,0.000039488015,0.004742907,0.00000902888,0.000003554287,0.000007582016,0.000015043005,0.000076977776,0.000399861],"genre_scores_gemma":[0.9985337,0.0000146695365,0.0012385694,0.000001863072,0.000002063527,0.0000039768015,0.000016214639,0.000008445894,0.0001805457],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998627,0.000038641287,0.000005447064,0.000023735978,0.000044005803,0.000025468871],"domain_scores_gemma":[0.9995608,0.0002519631,0.000048187114,0.000032486343,0.00007246129,0.000034191617],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00041785036,0.00033555145,0.00037106161,0.0005211048,0.00029099916,0.00021201713,0.00029832087,0.00028420915,0.00085434923],"category_scores_gemma":[0.0008965886,0.00013141255,0.00019324616,0.00015511217,0.00059618277,0.00031735323,0.00026891066,0.000199178,0.00014295352],"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":[0.0015746237,0.00046120008,0.03127557,0.00029514087,0.00004085739,0.0015965424,0.0008086698,0.1911054,0.73250526,0.001811909,0.00031129405,0.038213577],"study_design_scores_gemma":[0.00011512752,0.0019501689,0.0481749,0.000025270054,0.00003655207,0.0004413529,0.00020497333,0.6026844,0.34494096,0.0007092081,0.0006495193,0.00006770373],"about_ca_topic_score_codex":0.00073713314,"about_ca_topic_score_gemma":0.00064024195,"teacher_disagreement_score":0.00085434923,"about_ca_system_score_codex":0.00019669566,"about_ca_system_score_gemma":0.00009238915,"threshold_uncertainty_score":0.0028580427},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99807787,0.00007119959,0.0015716265,0.000007952965,0.000009168081,0.00000563526,0.000010431587,0.000020743591,0.00022537977],"genre_scores_gemma":[0.99906737,0.00007586077,0.00068889896,0.0000064906058,0.000009250824,0.0000034886402,0.000013884802,0.00001053431,0.00012417535],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998192,0.000040956333,0.00001710872,0.000032142543,0.000054636646,0.00003591664],"domain_scores_gemma":[0.9994105,0.0003735211,0.00011192907,0.000033131764,0.000034684588,0.0000362686],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003163959,0.00030004885,0.00034084843,0.00025690428,0.00027026367,0.0004896445,0.00015347032,0.00020361636,0.0007668027],"category_scores_gemma":[0.00094451156,0.00019138165,0.00021065919,0.00015840994,0.00052847207,0.00037787488,0.00031597566,0.00028006648,0.00008635665],"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":[0.0010101728,0.00008607674,0.0022053788,0.000084308886,0.000016093778,0.00022923695,0.00012809322,0.003771496,0.9853157,0.00018470385,0.000018766252,0.006950083],"study_design_scores_gemma":[0.000078965226,0.0019577157,0.01800334,0.000009009881,0.00005515033,0.00019475778,0.00007014283,0.020638138,0.9584099,0.00016259607,0.00039686525,0.000023488992],"about_ca_topic_score_codex":0.00014166062,"about_ca_topic_score_gemma":0.00008588723,"teacher_disagreement_score":0.0007668027,"about_ca_system_score_codex":0.00014110276,"about_ca_system_score_gemma":0.00009567475,"threshold_uncertainty_score":0.0025652647},"labels":[],"label_agreement":null},{"id":"W2254629731","doi":"10.4271/2004-01-0855","title":"Detection of Obstructions in Automotive Manifolds by Aeroacoustic Means<xref ref-type=\"fn\" rid=\"FN1\">*</xref>","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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6989457,0.0013163514,0.29483426,0.00014243429,0.000099270575,0.0001251901,0.00013221336,0.0017857957,0.0026188549],"genre_scores_gemma":[0.92240244,0.00038887063,0.075583875,0.000041840918,0.00003410549,0.000044069413,0.000091839436,0.000045013752,0.0013679777],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99945384,0.00008989976,0.00001681827,0.00008311483,0.000315454,0.000040850297],"domain_scores_gemma":[0.99882144,0.00055355584,0.00018203605,0.00009253449,0.00029965767,0.000050651695],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00038831757,0.00043795875,0.00041275247,0.0010184592,0.0002387902,0.00026825513,0.00036876538,0.00050102454,0.00064796366],"category_scores_gemma":[0.0014346527,0.00022897645,0.00018432122,0.0002947165,0.0005953154,0.0004464994,0.00046305603,0.00038888675,0.00027176776],"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":[0.0002561733,0.0000475,0.007978679,0.00013249043,0.000015691274,0.00043299986,0.00017247116,0.001302866,0.93434423,0.0003287972,0.00032715168,0.054660857],"study_design_scores_gemma":[0.000046754794,0.00096896244,0.0600341,0.000030274003,0.00006155134,0.0025770268,0.00014167132,0.023435522,0.9079825,0.0004571113,0.0041903337,0.000074176656],"about_ca_topic_score_codex":0.0005837991,"about_ca_topic_score_gemma":0.0010892396,"teacher_disagreement_score":0.0010184592,"about_ca_system_score_codex":0.00019864886,"about_ca_system_score_gemma":0.00022167599,"threshold_uncertainty_score":0.0021676421},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99612,0.000057550078,0.0027335049,0.000022544198,0.0000053337644,0.000011300564,0.000025753356,0.0000250336,0.0009991805],"genre_scores_gemma":[0.99828786,0.000042768504,0.0013141041,0.0000070190863,0.000004731088,0.0000063322113,0.00003249709,0.000007739308,0.00029690907],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999057,0.000015165983,0.000004052213,0.000020561063,0.000020630909,0.00003383548],"domain_scores_gemma":[0.9996972,0.00012762332,0.000062599065,0.000020387293,0.00004503135,0.000047219914],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021002184,0.00035107008,0.00055452564,0.00034073877,0.00051138387,0.0004845058,0.0003367028,0.00045451926,0.0008691338],"category_scores_gemma":[0.0007711492,0.00019861438,0.000411897,0.00020471078,0.0007865307,0.00036026174,0.000404335,0.0003696934,0.000074017065],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00043234002,0.0002109866,0.0133452155,0.0002053232,0.00009013812,0.0013943495,0.00046010132,0.6969987,0.27388155,0.0053404644,0.00023082754,0.0074100257],"study_design_scores_gemma":[0.00007242833,0.00032740665,0.009532072,0.000011941168,0.000027162489,0.00009917081,0.00015006996,0.96469826,0.024343165,0.00033955948,0.0003732605,0.000025503807],"about_ca_topic_score_codex":0.006101381,"about_ca_topic_score_gemma":0.002394774,"teacher_disagreement_score":0.006101381,"about_ca_system_score_codex":0.00035783727,"about_ca_system_score_gemma":0.0005581348,"threshold_uncertainty_score":0.012131691},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9311693,0.00014707158,0.06487415,0.00009718456,0.00015612837,0.000026819433,0.00015107953,0.00043368744,0.00294448],"genre_scores_gemma":[0.99757993,0.000022113483,0.0018264464,0.000005676884,0.000011443009,0.0000044837284,0.000046863297,0.000013427864,0.0004895435],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998375,0.000047812857,0.0000063753578,0.000044341454,0.00003699878,0.000027026661],"domain_scores_gemma":[0.998995,0.0006771218,0.000048047623,0.000031627787,0.0001776824,0.00007061109],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000383096,0.00073843385,0.0004037501,0.00037781417,0.00029114596,0.00051016477,0.0004445882,0.0006710386,0.0009216501],"category_scores_gemma":[0.001826289,0.00032467349,0.00031719985,0.0001501104,0.00029972976,0.00038816084,0.00035929622,0.00045646034,0.00018857149],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00014851279,0.000068321584,0.0040130536,0.000018789422,0.000013682964,0.00005492873,0.000013924111,0.9850928,0.0037655223,0.00028309654,0.00016005895,0.0063672457],"study_design_scores_gemma":[0.000002006103,0.000010875901,0.0004403474,4.2306718e-7,9.388429e-7,0.0000019558006,0.00000142257,0.99923706,0.0002725572,0.000020612946,0.000010675381,0.0000011834801],"about_ca_topic_score_codex":0.008742933,"about_ca_topic_score_gemma":0.0046775513,"teacher_disagreement_score":0.008742933,"about_ca_system_score_codex":0.00038519566,"about_ca_system_score_gemma":0.00035038064,"threshold_uncertainty_score":0.017384052},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.93929636,0.0016603329,0.054510254,0.00013412366,0.00011437182,0.000048843478,0.00011066009,0.0013110287,0.002814071],"genre_scores_gemma":[0.9688311,0.00075419643,0.026793072,0.0000837809,0.00007145155,0.00002187453,0.00016101457,0.00014918222,0.00313415],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9996886,0.000055875113,0.00002154005,0.000053454427,0.00011588319,0.000064671665],"domain_scores_gemma":[0.9995602,0.00018596965,0.00006894658,0.000029952073,0.00012121743,0.000033676213],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005705215,0.00039032058,0.00046177924,0.0004383474,0.00020456269,0.00072669424,0.0004841757,0.00027580425,0.0013328514],"category_scores_gemma":[0.0005922757,0.00025834856,0.00029137562,0.00029626937,0.0002783779,0.00069682574,0.000636573,0.00041749104,0.0004233725],"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":[0.00024076908,0.000052283627,0.0007507727,0.00013822143,0.000009263845,0.00007017479,0.000052187188,0.00049902353,0.95890146,0.00021619706,0.00024229531,0.03882735],"study_design_scores_gemma":[0.000022375034,0.00074574735,0.0037119621,0.000008986521,0.000031259966,0.00020720805,0.000015010716,0.0040162127,0.9882145,0.000052391,0.002959225,0.000015080107],"about_ca_topic_score_codex":0.00018170652,"about_ca_topic_score_gemma":0.00015475953,"teacher_disagreement_score":0.0013328514,"about_ca_system_score_codex":0.00019486944,"about_ca_system_score_gemma":0.00024340197,"threshold_uncertainty_score":0.0044588447},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97869146,0.0000824279,0.016285634,0.00010139173,0.000027652839,0.00004327742,0.00020728895,0.00022578688,0.0043350873],"genre_scores_gemma":[0.9952159,0.00003925483,0.0035469995,0.000012857613,0.0000057129905,0.000027691915,0.000102129525,0.000026665972,0.0010229626],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999156,0.000017108232,0.0000055304126,0.000010210727,0.00002612219,0.000025522011],"domain_scores_gemma":[0.99961543,0.00021230239,0.00004174287,0.000017498603,0.000058614238,0.00005435664],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002733876,0.00039328058,0.0005251041,0.0002673462,0.00037611168,0.00060807477,0.0005267491,0.0007000363,0.001275893],"category_scores_gemma":[0.00075132423,0.00024050959,0.0003615899,0.0002651044,0.00039166803,0.000364811,0.00034168916,0.00047207574,0.00012163719],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00013561899,0.00009105879,0.002568789,0.00002713971,0.000015025138,0.00012505024,0.0000464511,0.9865242,0.007901245,0.0007511538,0.00014066845,0.0016735678],"study_design_scores_gemma":[0.000017962278,0.000022184917,0.00054777286,0.0000014459017,0.0000021657252,0.0000047636213,0.000009458823,0.9982658,0.0009974709,0.000067958004,0.000059088787,0.0000038816816],"about_ca_topic_score_codex":0.011363557,"about_ca_topic_score_gemma":0.005304677,"teacher_disagreement_score":0.011363557,"about_ca_system_score_codex":0.0005190038,"about_ca_system_score_gemma":0.0006953076,"threshold_uncertainty_score":0.02259487},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9267338,0.000085036496,0.07168246,0.0000687548,0.000048929363,0.000019102392,0.000084811836,0.000404753,0.00087229145],"genre_scores_gemma":[0.9843829,0.00003855185,0.014930068,0.000010980918,0.0000129364,0.0000064508495,0.00009509017,0.000019399678,0.00050365337],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998128,0.000029063838,0.000010328449,0.0000366102,0.00006646824,0.000044746248],"domain_scores_gemma":[0.9993905,0.00025424975,0.000044815264,0.000040025756,0.00020428334,0.000066150096],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003604694,0.0004054619,0.0005769924,0.0007610092,0.0004043801,0.00080860197,0.0004139886,0.0007317718,0.000502364],"category_scores_gemma":[0.001297584,0.0002998418,0.00025447598,0.00043807022,0.00036943183,0.00068930665,0.00049629936,0.00055106345,0.00017243867],"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":[0.002543744,0.0007244625,0.030615658,0.00016800419,0.00006004822,0.0009719095,0.00044409506,0.196896,0.55866957,0.0013786417,0.0012909386,0.20623697],"study_design_scores_gemma":[0.000027826298,0.00018314495,0.013105148,0.0000063935636,0.000012573145,0.000079573474,0.00006237721,0.94916016,0.03702325,0.00014799698,0.0001667533,0.000024815445],"about_ca_topic_score_codex":0.0038305214,"about_ca_topic_score_gemma":0.0028605098,"teacher_disagreement_score":0.0038305214,"about_ca_system_score_codex":0.00020624936,"about_ca_system_score_gemma":0.000661671,"threshold_uncertainty_score":0.0076164603},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98470944,0.00014178272,0.013572824,0.0001377927,0.000036040037,0.000015522375,0.00008828325,0.00009734932,0.0012009986],"genre_scores_gemma":[0.99897087,0.00003830441,0.0007003361,0.00001025238,0.0000037336656,0.000005615634,0.000030465024,0.00001398808,0.00022654382],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996892,0.00013285106,0.000021545036,0.00005335286,0.000046978195,0.000056058863],"domain_scores_gemma":[0.99730885,0.0020502934,0.00014511903,0.00011903029,0.0002929688,0.00008372351],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0008979526,0.0005473822,0.0004565067,0.0002891821,0.00044024648,0.0010329954,0.000563305,0.0013531148,0.0008910549],"category_scores_gemma":[0.004043808,0.000354531,0.00053781486,0.00022157627,0.00047345093,0.00074409845,0.00041536608,0.0006698824,0.00017165123],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00017453896,0.00009162538,0.0070854956,0.000025509657,0.000018163093,0.00006621359,0.00001841493,0.98587924,0.003974582,0.000270876,0.00007304831,0.0023223176],"study_design_scores_gemma":[0.000017325348,0.00006436785,0.0022896992,0.000006360111,0.000013259263,0.000008289763,0.000015152984,0.994981,0.0024975128,0.000070971895,0.000028648557,0.00000734197],"about_ca_topic_score_codex":0.010890656,"about_ca_topic_score_gemma":0.004875103,"teacher_disagreement_score":0.010890656,"about_ca_system_score_codex":0.00048686343,"about_ca_system_score_gemma":0.0006203892,"threshold_uncertainty_score":0.021654546},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6865925,0.00032959547,0.29389197,0.00022577126,0.00033153535,0.00008820731,0.0003656743,0.0022030827,0.015971579],"genre_scores_gemma":[0.9757583,0.000058027174,0.021498995,0.000022480974,0.00003234856,0.000023956603,0.00016122227,0.000109335604,0.0023353563],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997898,0.000055294455,0.000011512858,0.000036706333,0.00007646384,0.00003017153],"domain_scores_gemma":[0.9991654,0.00037755995,0.000055882203,0.000066671004,0.0002797131,0.000054879798],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005768913,0.00088891375,0.0009422133,0.0006302005,0.0006831657,0.0007497854,0.00076855073,0.0011970361,0.0017216376],"category_scores_gemma":[0.0020184335,0.0005480186,0.0005679936,0.00039685884,0.00045364015,0.0008756254,0.00044305835,0.00069483503,0.0005084787],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000629872,0.000036992195,0.0009206242,0.000011802326,0.000008180434,0.000059004484,0.000013513045,0.9908694,0.0013935461,0.00055745384,0.0002501775,0.005816346],"study_design_scores_gemma":[0.0000023401212,0.0000029162884,0.000044561297,4.8298637e-7,6.21946e-7,0.0000011060625,0.0000010144748,0.99971443,0.00017532466,0.00004008037,0.000016017226,0.0000010293269],"about_ca_topic_score_codex":0.025885481,"about_ca_topic_score_gemma":0.015078958,"teacher_disagreement_score":0.025885481,"about_ca_system_score_codex":0.0005663467,"about_ca_system_score_gemma":0.0010008829,"threshold_uncertainty_score":0.051469624},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9952355,0.000081166174,0.0032239768,0.000028500837,0.000036676334,0.000014577545,0.00004470178,0.00005815651,0.0012767861],"genre_scores_gemma":[0.9986833,0.000031316926,0.00071877654,0.0000052079567,0.0000074990576,0.0000057040133,0.00003108676,0.000008079853,0.0005089275],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99949837,0.00010299675,0.000029426894,0.000076346994,0.00021103513,0.00008178059],"domain_scores_gemma":[0.998536,0.0007311992,0.0001267302,0.0001636992,0.00034571273,0.00009660712],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005267225,0.00036242954,0.000454853,0.00035609677,0.00069210026,0.00031041718,0.0006112206,0.00069930014,0.0015661444],"category_scores_gemma":[0.0017259102,0.00022319451,0.00031509876,0.00022746937,0.0010386038,0.00040795445,0.00039138924,0.00033915852,0.0001682549],"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":[0.0019247405,0.00058204273,0.0049569462,0.00019342871,0.000023313125,0.000798164,0.0004148382,0.021957196,0.9613692,0.0007839835,0.00020930813,0.0067868335],"study_design_scores_gemma":[0.00022058249,0.0036962938,0.03158615,0.00003094227,0.00008391223,0.00061155274,0.00047574076,0.18225181,0.7791583,0.00041512778,0.0013757143,0.00009397706],"about_ca_topic_score_codex":0.0010024474,"about_ca_topic_score_gemma":0.00062908704,"teacher_disagreement_score":0.0015661444,"about_ca_system_score_codex":0.0002611841,"about_ca_system_score_gemma":0.00018691938,"threshold_uncertainty_score":0.0052392483},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.978571,0.0000687992,0.01384727,0.000077972196,0.000038830793,0.00004418949,0.00027384458,0.00020643,0.0068716123],"genre_scores_gemma":[0.99428284,0.000031435553,0.004441899,0.000017122145,0.000004572016,0.000030772197,0.00012797535,0.000017539121,0.0010459174],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998989,0.000017789567,0.0000042736146,0.000013396331,0.000032642012,0.000032913274],"domain_scores_gemma":[0.99964523,0.00015602646,0.000048374448,0.000026680915,0.00006565274,0.000057963152],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001714319,0.00041163125,0.0004921669,0.00031302977,0.00035354137,0.0005065324,0.00071864005,0.0009410179,0.0020443557],"category_scores_gemma":[0.0007061559,0.00017489736,0.00041616886,0.00025580343,0.0005909134,0.00022211013,0.0003637147,0.00046620454,0.00015056999],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00012804272,0.00009892044,0.002287625,0.00004921365,0.000017229597,0.00018700081,0.00006639008,0.98584634,0.00851348,0.00077734055,0.00015886407,0.0018696061],"study_design_scores_gemma":[0.000017760396,0.000049417977,0.00055058143,0.000003365133,0.0000034837349,0.000012392703,0.000018183515,0.9979576,0.0012000189,0.00007278812,0.000109678935,0.000004710518],"about_ca_topic_score_codex":0.011269022,"about_ca_topic_score_gemma":0.0050223484,"teacher_disagreement_score":0.011269022,"about_ca_system_score_codex":0.000416728,"about_ca_system_score_gemma":0.0005761667,"threshold_uncertainty_score":0.022406876},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9316659,0.00019413322,0.054812446,0.0001512446,0.000068963884,0.000050593822,0.00016916363,0.0003054147,0.012582082],"genre_scores_gemma":[0.9959804,0.000042254578,0.002528116,0.000014723457,0.0000036701877,0.00002901457,0.000057731868,0.000013463581,0.001330663],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998919,0.00002442468,0.0000059834706,0.000014719063,0.000036507277,0.000026559052],"domain_scores_gemma":[0.9996271,0.00021894995,0.00003686752,0.0000149778325,0.00007135977,0.00003076078],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021938077,0.0004574075,0.00043448035,0.00031170814,0.00033265344,0.00056627084,0.00057200494,0.00081169227,0.0019115966],"category_scores_gemma":[0.0005437492,0.00013516175,0.00041097822,0.00018090059,0.0005554069,0.00022265632,0.0003937328,0.0004327507,0.00012193484],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000074812546,0.0000536011,0.0011307378,0.000036359088,0.000009943501,0.000101399826,0.00005991406,0.9914042,0.0039423485,0.0009126899,0.00011960291,0.0021544176],"study_design_scores_gemma":[0.0000042480574,0.000025690704,0.00020819168,0.0000023935102,0.0000020792163,0.0000044551452,0.000014878525,0.9987224,0.0008158375,0.00010787027,0.000089711706,0.0000022923264],"about_ca_topic_score_codex":0.00832519,"about_ca_topic_score_gemma":0.0036203521,"teacher_disagreement_score":0.00832519,"about_ca_system_score_codex":0.00033796765,"about_ca_system_score_gemma":0.0003447896,"threshold_uncertainty_score":0.016553462},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.1617271,0.0006738858,0.8235331,0.0003174465,0.00008902136,0.000086976775,0.00016394707,0.0007910098,0.012617472],"genre_scores_gemma":[0.9216292,0.00021843363,0.07469543,0.000047181322,0.000027268932,0.0001214721,0.00016212821,0.0002680131,0.0028308728],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996106,0.00009831203,0.00001560555,0.000045308556,0.0001812745,0.000048986403],"domain_scores_gemma":[0.99963224,0.00015262046,0.00005880301,0.000039465973,0.00010130642,0.000015573165],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00059141516,0.0009411766,0.000548674,0.0005625002,0.000357274,0.00077546714,0.00060371717,0.00094651914,0.0016831197],"category_scores_gemma":[0.0015710621,0.00034483528,0.0006240892,0.00041468596,0.00033251487,0.0006900589,0.0004969027,0.00041254674,0.0005534458],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00016568082,0.0000903732,0.00070179935,0.00012064218,0.0000443049,0.00005571901,0.00004344933,0.92689806,0.044418562,0.0042052683,0.0005436282,0.022712467],"study_design_scores_gemma":[0.000013712413,0.0000532309,0.00026611995,0.0000099082845,0.0000147254905,0.000023831544,0.00001336478,0.99030495,0.007741188,0.0006896291,0.00085835875,0.000010991713],"about_ca_topic_score_codex":0.0010970429,"about_ca_topic_score_gemma":0.0018491554,"teacher_disagreement_score":0.0016831197,"about_ca_system_score_codex":0.0006342675,"about_ca_system_score_gemma":0.00046426812,"threshold_uncertainty_score":0.0056306124},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99232364,0.000050961513,0.007007266,0.000019853189,0.0000073156743,0.000017799084,0.00008067202,0.0001270893,0.0003654506],"genre_scores_gemma":[0.9963096,0.00003385546,0.0032974929,0.000005765039,0.0000045059196,0.00001358055,0.00017602323,0.000019340216,0.00013979244],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998165,0.000050421662,0.000019206269,0.000030594856,0.000060623013,0.000022682176],"domain_scores_gemma":[0.99922,0.0004955409,0.00007802695,0.00006437374,0.00010535622,0.000036715446],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005081267,0.00059152255,0.0004886439,0.0005472985,0.00035516036,0.0005332105,0.0004046489,0.0004624087,0.00038864385],"category_scores_gemma":[0.0013425319,0.00026483586,0.00046275483,0.0003821815,0.00037515935,0.000522025,0.0003007442,0.0002990858,0.00005651997],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0010820971,0.00045715802,0.05247377,0.00019722735,0.00011527308,0.0006952334,0.00039489073,0.82055634,0.10366551,0.0012234165,0.0002502124,0.018888904],"study_design_scores_gemma":[0.000043050757,0.00011316194,0.013206797,0.0000052006017,0.00001573924,0.000026005042,0.000032349017,0.9684695,0.01782968,0.00011891365,0.00012017879,0.000019465046],"about_ca_topic_score_codex":0.005342536,"about_ca_topic_score_gemma":0.004326773,"teacher_disagreement_score":0.005342536,"about_ca_system_score_codex":0.00033656592,"about_ca_system_score_gemma":0.00025990827,"threshold_uncertainty_score":0.010622919},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9746549,0.000079863385,0.016896458,0.000055102664,0.000028745364,0.00003326358,0.0003124492,0.0001489582,0.007790243],"genre_scores_gemma":[0.9971718,0.000033933462,0.0015054682,0.0000085075335,0.0000030324566,0.000019095713,0.000118516255,0.000010702961,0.0011287803],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998635,0.000023868995,0.000006974285,0.000020963591,0.000046406658,0.00003823957],"domain_scores_gemma":[0.9996605,0.00015887273,0.00003603197,0.000045443543,0.00006173617,0.00003743075],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002217244,0.00039903977,0.0005027774,0.0003226247,0.0003089233,0.0005697993,0.0005853162,0.00079854764,0.0022028605],"category_scores_gemma":[0.0006203147,0.0001910757,0.00055942556,0.00031914,0.00035223033,0.00028483305,0.0003750081,0.00041510104,0.00027763998],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00009396361,0.00006766247,0.0015438303,0.000048547954,0.000009990719,0.00020425518,0.000038585913,0.98421776,0.011634177,0.0003719471,0.00009075048,0.0016785207],"study_design_scores_gemma":[0.00002377096,0.000115508905,0.0018720368,0.000004965496,0.0000073130764,0.000033604687,0.00002868419,0.9951815,0.0024488627,0.000094224655,0.000181931,0.0000076276965],"about_ca_topic_score_codex":0.005184664,"about_ca_topic_score_gemma":0.00240655,"teacher_disagreement_score":0.005184664,"about_ca_system_score_codex":0.00030137738,"about_ca_system_score_gemma":0.00039460065,"threshold_uncertainty_score":0.010308921},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.03858897,0.00004224287,0.95871997,0.00004004352,0.000024154479,0.000019404617,0.00003697308,0.00038711168,0.002141079],"genre_scores_gemma":[0.5017101,0.00019990905,0.49284792,0.000056352637,0.000030022366,0.00013164028,0.00017189182,0.00020070026,0.0046514547],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998567,0.000037740072,0.000007174019,0.000014696777,0.000073653326,0.000009966706],"domain_scores_gemma":[0.99955493,0.00023696254,0.000031512554,0.000028155313,0.0001233371,0.000025137324],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003277277,0.0005219579,0.00048753194,0.00047148886,0.00032616637,0.0005344867,0.00043933588,0.0007337889,0.0017353897],"category_scores_gemma":[0.0011717567,0.0003431336,0.00042468132,0.00025826483,0.0004913356,0.000531002,0.00061629567,0.0004643456,0.00047214935],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000055309836,0.000045317396,0.00082730805,0.000057052173,0.000021537415,0.000100231715,0.00012420195,0.9475805,0.016562084,0.011019756,0.00029573095,0.02331093],"study_design_scores_gemma":[0.0000031802474,0.0000065207905,0.000036251,0.0000025912495,0.0000011509736,0.000009743276,0.0000053321123,0.9979638,0.0011287285,0.0005459047,0.00029403198,0.0000029169732],"about_ca_topic_score_codex":0.0020137038,"about_ca_topic_score_gemma":0.0022211506,"teacher_disagreement_score":0.0020137038,"about_ca_system_score_codex":0.00029105355,"about_ca_system_score_gemma":0.00068883057,"threshold_uncertainty_score":0.005805433},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9977404,0.00015710465,0.00141471,0.0000078403455,0.0000076230326,0.000010268963,0.00004304425,0.000050221708,0.00056890934],"genre_scores_gemma":[0.9979005,0.000089767826,0.0016589827,0.000014972951,0.0000045586294,0.000007296642,0.000057141424,0.000030114341,0.00023678137],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99975127,0.000045464534,0.000023524057,0.000045496196,0.000059690632,0.0000745222],"domain_scores_gemma":[0.9988525,0.00043670327,0.00031374057,0.00011957444,0.00013437272,0.00014318108],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002832896,0.0003401591,0.00035361183,0.00019885275,0.0001583225,0.00071377965,0.00019959795,0.00025692314,0.001240959],"category_scores_gemma":[0.0012991725,0.00027051553,0.00024504217,0.00016452615,0.00033610853,0.0003145051,0.00034002602,0.00028660859,0.00021017608],"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":[0.00094565545,0.00008670298,0.0033175247,0.00008211418,0.000021196418,0.0001472703,0.00008434718,0.0041762413,0.98403406,0.00018380264,0.000055298562,0.0068658455],"study_design_scores_gemma":[0.00008335326,0.0023589374,0.029142208,0.000016379503,0.00007472244,0.0003378564,0.000094675626,0.009944747,0.9566996,0.00010892267,0.0011043176,0.000034263125],"about_ca_topic_score_codex":0.0003286748,"about_ca_topic_score_gemma":0.0002837735,"teacher_disagreement_score":0.001240959,"about_ca_system_score_codex":0.00013273579,"about_ca_system_score_gemma":0.00013706053,"threshold_uncertainty_score":0.0041514635},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9940117,0.00012256074,0.0025899732,0.000051890383,0.00004098632,0.000006785046,0.0000752535,0.00012996563,0.0029709598],"genre_scores_gemma":[0.99932945,0.000040367002,0.0002530019,0.000009328049,0.0000069347616,0.0000011801843,0.000029906916,0.000033874887,0.00029604434],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9996178,0.000093460454,0.000016610415,0.00006910678,0.00007137441,0.00013161122],"domain_scores_gemma":[0.9965113,0.0023875588,0.00023483462,0.00019660257,0.0003698948,0.00029982402],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003337554,0.0006100418,0.000640985,0.0005817772,0.00048227474,0.0009414115,0.00032249675,0.0007701497,0.0038278277],"category_scores_gemma":[0.0035530003,0.00036165953,0.00028510258,0.00030612253,0.0005850861,0.00046081035,0.00046262518,0.0003592724,0.00063861354],"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":[0.007997285,0.00062938256,0.017715532,0.00017293106,0.000106735206,0.003246344,0.00028148963,0.15555443,0.7854004,0.0014883718,0.00084298797,0.026564151],"study_design_scores_gemma":[0.0005516801,0.0030718509,0.13630244,0.00008401393,0.00063768943,0.002139298,0.00089949986,0.32479292,0.5284231,0.0014723567,0.0013643409,0.00026085455],"about_ca_topic_score_codex":0.0015766653,"about_ca_topic_score_gemma":0.0013157718,"teacher_disagreement_score":0.0038278277,"about_ca_system_score_codex":0.00033693804,"about_ca_system_score_gemma":0.0003349415,"threshold_uncertainty_score":0.012805402},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98544437,0.00009612743,0.010853691,0.000051280716,0.0000121230605,0.000014126939,0.000020830592,0.000076710254,0.003430765],"genre_scores_gemma":[0.99764144,0.000025323383,0.0008235432,0.0000019729348,0.000002767478,0.0000034337493,0.000007793522,0.000006290469,0.0014875802],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99993753,0.0000132183,0.0000023341502,0.000007796432,0.00002071524,0.000018356344],"domain_scores_gemma":[0.9997738,0.000073849704,0.00004904919,0.000017336271,0.0000536826,0.000032262826],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000110027446,0.00027339175,0.00022056345,0.0002437336,0.0002881006,0.00034989996,0.00027113754,0.00023274806,0.001290552],"category_scores_gemma":[0.00040924433,0.00021162227,0.00012899494,0.00019738046,0.0004424531,0.00028786968,0.00022517703,0.00016822344,0.00016499164],"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":[0.0022234486,0.00026014078,0.011889415,0.0001827992,0.000036890568,0.0012139269,0.0009226074,0.13345826,0.7845679,0.020633886,0.0009893402,0.043621458],"study_design_scores_gemma":[0.00005803403,0.0004205379,0.0075863297,0.000009020693,0.000017400664,0.00021843864,0.00021348883,0.8691477,0.11996058,0.0014683751,0.0008672147,0.00003279789],"about_ca_topic_score_codex":0.0011310417,"about_ca_topic_score_gemma":0.000892858,"teacher_disagreement_score":0.001290552,"about_ca_system_score_codex":0.00029490594,"about_ca_system_score_gemma":0.0002493283,"threshold_uncertainty_score":0.0043173432},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9657813,0.00016384819,0.020919645,0.00020760686,0.00009450441,0.000077959405,0.0022780125,0.00050621846,0.009971004],"genre_scores_gemma":[0.9750861,0.000087977656,0.018790713,0.000040870982,0.000024252879,0.00009064847,0.0022101807,0.00011754032,0.0035517116],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999806,0.000038654318,0.000013201042,0.000033295426,0.00006965579,0.000039261766],"domain_scores_gemma":[0.99956864,0.00019341249,0.00004478296,0.000044757726,0.00009990623,0.000048485745],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003812821,0.0005926574,0.0006310579,0.00038867697,0.00034028885,0.00096027687,0.00080133154,0.0008966347,0.0017501703],"category_scores_gemma":[0.0009109904,0.0001789503,0.00036259647,0.00046593026,0.0004396254,0.00045778457,0.0004606937,0.000769781,0.00021058909],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00049228064,0.0004262313,0.0061595202,0.0001343279,0.000035926092,0.0005633142,0.00018495382,0.95636517,0.021702124,0.0035394013,0.001805401,0.008591305],"study_design_scores_gemma":[0.000046015342,0.00006277202,0.0022382427,0.000007731718,0.0000032633857,0.000025960118,0.00005753043,0.99320674,0.0033956182,0.00031162257,0.00063299196,0.000011600885],"about_ca_topic_score_codex":0.0037268677,"about_ca_topic_score_gemma":0.0019464635,"teacher_disagreement_score":0.0037268677,"about_ca_system_score_codex":0.00040414848,"about_ca_system_score_gemma":0.00049467303,"threshold_uncertainty_score":0.0074103475},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7872983,0.00037701614,0.18075205,0.00041580803,0.00019264512,0.0003752137,0.0032561678,0.0018897806,0.025442872],"genre_scores_gemma":[0.94792306,0.00017447244,0.04636992,0.000061145205,0.000027009795,0.0003056223,0.0018262328,0.00020114356,0.0031114279],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995202,0.00010328318,0.000037793056,0.00004952822,0.00020564832,0.000083601386],"domain_scores_gemma":[0.99911875,0.00039188573,0.00011052423,0.00009612351,0.00022145727,0.000061289145],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005539392,0.00072867546,0.0012174868,0.0006274586,0.00052861666,0.0010171923,0.001311295,0.0014127069,0.002541446],"category_scores_gemma":[0.001770958,0.0003531838,0.00078242784,0.0008148146,0.00053569605,0.00066836976,0.00060422317,0.0007634639,0.0003126021],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00007310467,0.00006829562,0.0008764875,0.000057386806,0.000017871283,0.00011904904,0.00004883587,0.9906668,0.004138199,0.0018960895,0.0003464713,0.0016914351],"study_design_scores_gemma":[0.000028925644,0.0000217943,0.00028089527,0.000003824192,0.0000030928463,0.000013548258,0.000011853966,0.9978811,0.0011976267,0.00025241994,0.00029731842,0.000007654912],"about_ca_topic_score_codex":0.0073565603,"about_ca_topic_score_gemma":0.002643264,"teacher_disagreement_score":0.0073565603,"about_ca_system_score_codex":0.0007323676,"about_ca_system_score_gemma":0.0010283533,"threshold_uncertainty_score":0.014627457},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8900646,0.00019846759,0.0992515,0.00020306835,0.000044068274,0.00011091449,0.00016625041,0.00055687473,0.009404326],"genre_scores_gemma":[0.9883817,0.000059709866,0.010198816,0.000011676881,0.000007644356,0.000044032837,0.00006655466,0.00003373305,0.0011961664],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99990034,0.00003360216,0.0000059300423,0.000015600219,0.000031369178,0.0000131671695],"domain_scores_gemma":[0.9996382,0.00020777615,0.00003382891,0.000030318313,0.00006348337,0.000026342064],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003648006,0.0005365213,0.00043801803,0.0003576405,0.0003446235,0.00040627594,0.00050448737,0.00083473587,0.00096740475],"category_scores_gemma":[0.0008731771,0.00022925215,0.0004429857,0.00026548505,0.0003309674,0.00044793988,0.00033086925,0.00040300586,0.00014064793],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000079933656,0.00006936139,0.001206515,0.00003082778,0.000010157637,0.00006960205,0.000035534304,0.9880455,0.0062557557,0.00093745766,0.00014450916,0.0031147772],"study_design_scores_gemma":[0.0000033654587,0.00001111668,0.00013350903,5.6198223e-7,8.6980356e-7,0.0000015281216,0.000002320702,0.99944,0.0003543396,0.000028304015,0.000022499782,0.0000015016952],"about_ca_topic_score_codex":0.014150264,"about_ca_topic_score_gemma":0.008185955,"teacher_disagreement_score":0.014150264,"about_ca_system_score_codex":0.00046927636,"about_ca_system_score_gemma":0.0005589587,"threshold_uncertainty_score":0.028135777},"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":"methods","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0071440996,0.00004596461,0.98608893,0.000034692068,0.00002804318,0.000046906865,0.000034739314,0.00065482577,0.005921782],"genre_scores_gemma":[0.18627867,0.0001456204,0.80361897,0.00005418951,0.00002100375,0.00020357136,0.00014422189,0.00043855346,0.009095241],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99977523,0.0000410573,0.00000918985,0.000015087193,0.00014218708,0.00001724279],"domain_scores_gemma":[0.99948114,0.00019271839,0.00002858306,0.0000797187,0.0001862293,0.000031640524],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005388716,0.000522677,0.0006024807,0.00053219026,0.00057737174,0.0006396924,0.0010848411,0.00054866204,0.0065207873],"category_scores_gemma":[0.0015720879,0.0003135519,0.0004188334,0.00041426517,0.00044176806,0.000754075,0.00070114096,0.0007672873,0.0023696823],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00015121607,0.0001977548,0.0014221362,0.00022705772,0.000044495868,0.00022747484,0.00027487773,0.63277894,0.04520681,0.13227563,0.004697337,0.18249628],"study_design_scores_gemma":[0.00001100716,0.000013060274,0.00006812178,0.00000848202,0.0000032576286,0.000040971318,0.000014501682,0.98639953,0.0047193826,0.0050954754,0.0036193046,0.000006972743],"about_ca_topic_score_codex":0.0025084908,"about_ca_topic_score_gemma":0.003164142,"teacher_disagreement_score":0.0065207873,"about_ca_system_score_codex":0.00046741494,"about_ca_system_score_gemma":0.00119093,"threshold_uncertainty_score":0.021814167},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.95545244,0.00022198327,0.03364157,0.00027533472,0.00008485658,0.0002811961,0.00092639663,0.0013461545,0.007770035],"genre_scores_gemma":[0.9647029,0.000146994,0.032114565,0.000037695525,0.000014915944,0.00007857771,0.00044344255,0.00008600856,0.002374888],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99976355,0.000058595924,0.000016082531,0.000046184763,0.00008927571,0.000026377445],"domain_scores_gemma":[0.9986052,0.0006455178,0.00002583049,0.00010674814,0.0005411031,0.00007564403],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00085184595,0.0006309316,0.00056435645,0.00056802126,0.00096568686,0.0006699596,0.0008878477,0.0010549492,0.0022251776],"category_scores_gemma":[0.002336734,0.0003569628,0.00044211227,0.00055259716,0.0004087622,0.0005901356,0.00052283896,0.0005397075,0.00046083555],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0022847184,0.0014621898,0.046172105,0.00031283125,0.00012037553,0.0006971793,0.000558035,0.67710674,0.12358642,0.0015856002,0.0033341325,0.14277963],"study_design_scores_gemma":[0.00007961568,0.00031944766,0.010517461,0.000014647398,0.00002568248,0.000038059254,0.00009775559,0.9627851,0.02447913,0.00020887109,0.0014109256,0.000023236198],"about_ca_topic_score_codex":0.03022072,"about_ca_topic_score_gemma":0.031904474,"teacher_disagreement_score":0.03022072,"about_ca_system_score_codex":0.0007595512,"about_ca_system_score_gemma":0.00097488635,"threshold_uncertainty_score":0.060089648},"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":"methods","genre_gemma":"methods","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.28743,0.00026266693,0.70552135,0.00010067588,0.00011163899,0.0018265854,0.00032150294,0.0006610995,0.0037644343],"genre_scores_gemma":[0.4985872,0.00052804995,0.49535275,0.000059331167,0.000046776724,0.003380711,0.00022810703,0.00009961956,0.0017174578],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9991621,0.00012012673,0.000064237785,0.00018664647,0.00037133423,0.00009557137],"domain_scores_gemma":[0.99848586,0.00040572134,0.00024077887,0.00040611485,0.00037439552,0.0000872208],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0013086251,0.0008974676,0.000533238,0.00073573476,0.000989149,0.00044323344,0.0006720866,0.0004970083,0.003580037],"category_scores_gemma":[0.0015866735,0.0004288263,0.00022492211,0.00061485596,0.0011847453,0.00046231458,0.00084974355,0.0008835025,0.00053426187],"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":[0.00009816607,0.00017294742,0.00037565443,0.00012986016,0.0000040314117,0.000086200154,0.00015718385,0.0017156188,0.9856036,0.0023880133,0.000112357804,0.009156396],"study_design_scores_gemma":[0.000079569,0.0012907456,0.002051772,0.000027098646,0.000014479679,0.00030156074,0.00007151407,0.01104315,0.9792749,0.0011189104,0.0046727923,0.00005351326],"about_ca_topic_score_codex":0.0005755789,"about_ca_topic_score_gemma":0.00058254064,"teacher_disagreement_score":0.003580037,"about_ca_system_score_codex":0.00041998987,"about_ca_system_score_gemma":0.00088394154,"threshold_uncertainty_score":0.011976421},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9699064,0.00006505783,0.02440961,0.00010342849,0.00008000189,0.000028580256,0.00087584084,0.000635294,0.0038957307],"genre_scores_gemma":[0.9934314,0.00003762471,0.004571523,0.000020938787,0.000007454401,0.000013632409,0.00057359046,0.00003460678,0.0013091875],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99987507,0.000015228941,0.0000043292025,0.000034850847,0.00005160421,0.000018904795],"domain_scores_gemma":[0.9999188,0.000020172547,0.0000059195067,0.0000123999225,0.000029667564,0.000012902933],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00009589105,0.00035265606,0.0003865908,0.00024551083,0.0002714821,0.00020962872,0.00026843985,0.0005886194,0.0016863028],"category_scores_gemma":[0.00018456498,0.0001582297,0.0002531185,0.00014619384,0.00012026485,0.00020669702,0.00019454304,0.00033024087,0.00047862015],"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":[0.00076755293,0.00015813993,0.008255356,0.00008888384,0.000045277568,0.00033611926,0.00032488987,0.03441321,0.92483574,0.00042499328,0.0016180514,0.028731773],"study_design_scores_gemma":[0.00016602983,0.001424352,0.2041428,0.000021730571,0.00016979457,0.0006488235,0.00033589522,0.4257823,0.3582868,0.00045157634,0.008433115,0.00013667275],"about_ca_topic_score_codex":0.0031665508,"about_ca_topic_score_gemma":0.004149407,"teacher_disagreement_score":0.0031665508,"about_ca_system_score_codex":0.00016136828,"about_ca_system_score_gemma":0.00021495251,"threshold_uncertainty_score":0.006296277},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9788294,0.00016465786,0.017696775,0.0000600852,0.000019223075,0.000021138889,0.00022781998,0.00014835675,0.0028324537],"genre_scores_gemma":[0.98872477,0.00013474983,0.009225292,0.000019850826,0.000037736765,0.000012274093,0.00020870347,0.00002387997,0.0016127669],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999552,0.00000267684,0.0000014130446,0.0000090060075,0.000024821296,0.0000069004454],"domain_scores_gemma":[0.9999043,0.000027764665,0.00001919012,0.0000048651027,0.000024038194,0.000019869323],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00007965888,0.00022044255,0.00015312142,0.0005534677,0.00016733682,0.00021860214,0.00011686605,0.00017791538,0.0012065632],"category_scores_gemma":[0.00022565416,0.00015978725,0.0001224363,0.0002748561,0.00018247271,0.00019552959,0.0001284534,0.0002709732,0.00015206145],"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":[0.00056708575,0.000093521114,0.008549284,0.00008678397,0.000018217992,0.00080565206,0.00023258776,0.008568466,0.93346393,0.00094232184,0.00040816353,0.04626398],"study_design_scores_gemma":[0.00006970024,0.0006942404,0.64495283,0.000043027205,0.000053745905,0.0015328148,0.0003493899,0.21303017,0.1354386,0.0011122166,0.0026362648,0.00008699545],"about_ca_topic_score_codex":0.0008700104,"about_ca_topic_score_gemma":0.0010522793,"teacher_disagreement_score":0.0012065632,"about_ca_system_score_codex":0.000111930894,"about_ca_system_score_gemma":0.00011073856,"threshold_uncertainty_score":0.0040364265},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8307187,0.00024934762,0.16311005,0.00015778992,0.00017070567,0.000016225722,0.000105217354,0.00062367145,0.004848296],"genre_scores_gemma":[0.99479383,0.00003829763,0.004574519,0.000014613952,0.000014406331,0.0000036930096,0.000053160653,0.000043045427,0.0004645159],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99979025,0.0000757213,0.000008451813,0.00004344876,0.00004464248,0.000037399208],"domain_scores_gemma":[0.99938154,0.0003598358,0.000039734186,0.000039778464,0.00014035404,0.00003871404],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005249462,0.0006408151,0.00033449472,0.00027490171,0.00029839197,0.00034996032,0.00031874623,0.0009091356,0.00082195667],"category_scores_gemma":[0.0022516395,0.00023312985,0.00037616518,0.00012014747,0.00025928725,0.0004973533,0.00031273116,0.0004084321,0.00030049885],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0002196051,0.00006149888,0.0056995437,0.000031207965,0.000022547238,0.00013015566,0.000031310723,0.95399904,0.024123136,0.000941881,0.00031962656,0.014420445],"study_design_scores_gemma":[0.000003060308,0.000014002556,0.00068049564,0.0000025876298,0.0000036132908,0.0000056146087,0.000002703382,0.99596065,0.0032296104,0.00005369515,0.000041589297,0.0000024287376],"about_ca_topic_score_codex":0.0047162645,"about_ca_topic_score_gemma":0.0033958117,"teacher_disagreement_score":0.0047162645,"about_ca_system_score_codex":0.00020035685,"about_ca_system_score_gemma":0.0003511769,"threshold_uncertainty_score":0.009377658},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.017408246,0.0032383732,0.9315804,0.00072269415,0.0003767963,0.00009319775,0.000053637144,0.0002200178,0.04630658],"genre_scores_gemma":[0.7531339,0.010514525,0.18865092,0.0008917712,0.0010280603,0.00041401703,0.00012307691,0.00024595964,0.044997778],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997075,0.00004923062,0.000011302996,0.000035832778,0.00016358378,0.000032484855],"domain_scores_gemma":[0.99978524,0.000077990866,0.000031105126,0.000013404955,0.00007587873,0.0000162905],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004626221,0.00052888633,0.00060456933,0.001092434,0.0010024069,0.0015442556,0.0010170605,0.0010859852,0.0025311317],"category_scores_gemma":[0.0011040432,0.00041384285,0.0007083133,0.00043836137,0.0018320044,0.0016776761,0.0007376893,0.0008823528,0.0007267718],"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":[0.000025178408,0.00006378383,0.000422268,0.00017653218,0.000014779687,0.0003561764,0.00034337415,0.18899599,0.010735842,0.7712283,0.0023054953,0.02533228],"study_design_scores_gemma":[0.00001609374,0.000075908254,0.00016683983,0.000065050735,0.000011783687,0.00021925391,0.00008710322,0.88173026,0.0017667562,0.10418483,0.011644444,0.000031622298],"about_ca_topic_score_codex":0.0015651203,"about_ca_topic_score_gemma":0.00070435094,"teacher_disagreement_score":0.0025311317,"about_ca_system_score_codex":0.0010823079,"about_ca_system_score_gemma":0.001262193,"threshold_uncertainty_score":0.008467495},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.94306356,0.00016316537,0.026080135,0.0003331632,0.00015447893,0.000058412123,0.00040220047,0.00048787124,0.02925704],"genre_scores_gemma":[0.9951598,0.00003580081,0.0017190973,0.000020575211,0.000007677698,0.000008622122,0.00008451724,0.000025970343,0.0029379688],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99987817,0.000018747989,0.0000055165738,0.000016517453,0.000045002493,0.000036005804],"domain_scores_gemma":[0.9996648,0.00016135715,0.000027750153,0.000019823632,0.00007798943,0.000048370915],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016790359,0.00041713737,0.000587232,0.00039558348,0.0005100114,0.00068352645,0.00057909294,0.0014357715,0.0032355755],"category_scores_gemma":[0.00080347166,0.00031618934,0.00056248764,0.00027868222,0.00058225176,0.00033448453,0.00043088122,0.00044329706,0.00031952118],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00019801335,0.00004791489,0.0020239155,0.000027969147,0.000016037038,0.00044351388,0.00007875052,0.9873067,0.0057615805,0.0013123367,0.00036712547,0.0024160794],"study_design_scores_gemma":[0.000015529158,0.000029432931,0.00073914864,0.0000029681134,0.0000043067184,0.00003321165,0.00002436281,0.9978042,0.0010476796,0.0000941675,0.00019734562,0.000007584622],"about_ca_topic_score_codex":0.019806853,"about_ca_topic_score_gemma":0.006864272,"teacher_disagreement_score":0.019806853,"about_ca_system_score_codex":0.0006071786,"about_ca_system_score_gemma":0.00075237785,"threshold_uncertainty_score":0.039383173},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.71400654,0.0005992578,0.2650997,0.0011806801,0.00024311445,0.00015396923,0.0008736934,0.0019088305,0.015934248],"genre_scores_gemma":[0.99228996,0.000058540685,0.0048423824,0.00020301889,0.00002291918,0.000065019005,0.00023392793,0.00016782356,0.0021163155],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9977877,0.0005507974,0.000108506894,0.0005242669,0.0007935548,0.0002350955],"domain_scores_gemma":[0.990185,0.006041754,0.00065541506,0.0015133814,0.0014213533,0.00018301273],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0016055377,0.00045066664,0.0003898654,0.00048470928,0.00088111317,0.0013738353,0.0007715362,0.0011011248,0.0036769223],"category_scores_gemma":[0.012037833,0.00067487254,0.00025628388,0.00040011242,0.0017668398,0.0016767469,0.0011768299,0.0021207046,0.0015879468],"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":[0.0011641775,0.00015169517,0.011672664,0.00019621005,0.000050079365,0.00014821818,0.0006632901,0.00795164,0.9500813,0.0045464826,0.00071620813,0.022658035],"study_design_scores_gemma":[0.00006002506,0.0010044108,0.04086407,0.00004678119,0.00004658068,0.00038816035,0.00029401065,0.041725405,0.9107367,0.0027657056,0.0019642897,0.0001038803],"about_ca_topic_score_codex":0.0011822793,"about_ca_topic_score_gemma":0.0008692088,"teacher_disagreement_score":0.0036769223,"about_ca_system_score_codex":0.0005867665,"about_ca_system_score_gemma":0.00049163564,"threshold_uncertainty_score":0.012300551},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99792576,0.00020259987,0.0012076229,0.0000148608315,0.000007530708,0.000003206025,0.00006675507,0.000030735177,0.0005410258],"genre_scores_gemma":[0.99841285,0.00011464501,0.0005039659,0.000011988923,0.0000059494946,0.000003203576,0.00017790144,0.000016553504,0.00075289357],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997657,0.000019982232,0.000013267894,0.000031800777,0.00013454714,0.000034758225],"domain_scores_gemma":[0.9993144,0.00026783493,0.00011550159,0.000032280954,0.00020668491,0.000063257066],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025470147,0.00016677933,0.00021795924,0.00017643296,0.00014973,0.0003032309,0.00017020901,0.00023763232,0.00091509655],"category_scores_gemma":[0.0007130648,0.00011470565,0.00014803963,0.00015830182,0.00019125032,0.00031095775,0.00022175233,0.00022513692,0.00009986792],"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":[0.0002880321,0.000020319922,0.0047132038,0.00007622861,0.000009040331,0.00022302271,0.00020320824,0.0010521042,0.9872989,0.00008565301,0.000097819655,0.0059323995],"study_design_scores_gemma":[0.000043746935,0.0014153523,0.10248485,0.000023566821,0.000049816837,0.0008363706,0.00032574715,0.013245129,0.8786855,0.0001257267,0.0027072693,0.000056892237],"about_ca_topic_score_codex":0.00043541697,"about_ca_topic_score_gemma":0.00039007232,"teacher_disagreement_score":0.00091509655,"about_ca_system_score_codex":0.00018103622,"about_ca_system_score_gemma":0.00008724338,"threshold_uncertainty_score":0.0030613542},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.83016354,0.00018400984,0.16144615,0.00022639167,0.000061314364,0.00007820754,0.00017999393,0.00034520112,0.0073152543],"genre_scores_gemma":[0.9807974,0.00006165409,0.017559597,0.000022885251,0.000006434774,0.000046627934,0.00007018993,0.000027555328,0.0014076564],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998591,0.000028335386,0.0000072985704,0.000017459422,0.00004938834,0.00003845726],"domain_scores_gemma":[0.99943227,0.0003060859,0.0000759364,0.000023155098,0.0001121435,0.000050507806],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005305437,0.00040450462,0.000557971,0.0003144068,0.0005133998,0.0007050652,0.0006206015,0.00082158117,0.0011149304],"category_scores_gemma":[0.0012445137,0.00027181386,0.0005688133,0.0002810007,0.0006605211,0.00038571964,0.00043218836,0.0005783091,0.00018874633],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000042749372,0.000029737732,0.0019480862,0.000028677316,0.0000070147553,0.00005918658,0.000032327996,0.9882478,0.006332075,0.0015325887,0.00006708964,0.0016727595],"study_design_scores_gemma":[0.0000051456755,0.000009297775,0.00013235294,0.00000134695,9.439958e-7,0.0000028603695,0.0000041722647,0.9990497,0.0006646045,0.0001040359,0.000023180388,0.0000021873543],"about_ca_topic_score_codex":0.010304424,"about_ca_topic_score_gemma":0.003363077,"teacher_disagreement_score":0.010304424,"about_ca_system_score_codex":0.0008876278,"about_ca_system_score_gemma":0.0012645911,"threshold_uncertainty_score":0.020488858},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9821415,0.00008344353,0.014958382,0.0000668542,0.000012567164,0.000029195075,0.000073268995,0.00009142532,0.0025434156],"genre_scores_gemma":[0.99324507,0.00005688352,0.0061140363,0.000015298681,0.0000067511146,0.000020437019,0.00006429773,0.000020770045,0.00045638965],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999843,0.000044066503,0.000008816831,0.000021034894,0.00004107238,0.000041934138],"domain_scores_gemma":[0.9983353,0.0012529776,0.00011827877,0.000056723722,0.00018306625,0.000053640237],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006646652,0.00046471955,0.00067379547,0.0006215613,0.00070656213,0.0006530835,0.0005239467,0.0010938898,0.0009966961],"category_scores_gemma":[0.0025883683,0.00031651114,0.0005956134,0.00063940225,0.0005519797,0.0006265061,0.00026244068,0.0004109255,0.000115022835],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00020423095,0.00015249393,0.008491116,0.000057828634,0.000046134737,0.00023406105,0.00012190383,0.9741313,0.009480206,0.0013300992,0.00013894691,0.005611672],"study_design_scores_gemma":[0.0000128707425,0.000040180796,0.0017952861,0.000003751702,0.000008884976,0.00001028777,0.000018371862,0.99713504,0.0008410004,0.00008584796,0.000043056552,0.00000542641],"about_ca_topic_score_codex":0.024311274,"about_ca_topic_score_gemma":0.012211905,"teacher_disagreement_score":0.024311274,"about_ca_system_score_codex":0.00059601426,"about_ca_system_score_gemma":0.00049558224,"threshold_uncertainty_score":0.048339546},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8583913,0.0002641062,0.11920497,0.00043465127,0.00015599678,0.00028202578,0.002498983,0.0011181345,0.01764985],"genre_scores_gemma":[0.94533706,0.00013043247,0.04827779,0.0000830502,0.000034441888,0.0003528249,0.0017507867,0.00019509366,0.0038385682],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996338,0.00007264586,0.000028487435,0.000041398052,0.00014484342,0.00007893392],"domain_scores_gemma":[0.9989704,0.00049986347,0.0001246898,0.000082623155,0.00022212615,0.00010037153],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00052741583,0.00081358675,0.0010979406,0.000715645,0.0004669985,0.0011459138,0.001463282,0.001805651,0.0026299674],"category_scores_gemma":[0.0020880308,0.00037703666,0.0009681313,0.0007306468,0.00068625517,0.0005757243,0.0008759541,0.0011278157,0.0003233258],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000094195944,0.000100446785,0.0012586929,0.000048097554,0.000022991784,0.00010830271,0.00006324421,0.9916888,0.0033423386,0.0015204696,0.00028904804,0.0014633993],"study_design_scores_gemma":[0.000022141148,0.000023038352,0.00026090656,0.0000038367016,0.0000027208885,0.000009120143,0.000016349637,0.9984394,0.0008235553,0.00018416985,0.00020820396,0.000006506532],"about_ca_topic_score_codex":0.00827551,"about_ca_topic_score_gemma":0.0029340854,"teacher_disagreement_score":0.00827551,"about_ca_system_score_codex":0.0006701947,"about_ca_system_score_gemma":0.001053214,"threshold_uncertainty_score":0.016454697},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.007045223,0.000034197667,0.99146104,0.00003327572,0.000016877086,0.000013118878,0.000004387164,0.00008104942,0.0013108456],"genre_scores_gemma":[0.4357036,0.00012942686,0.56132907,0.00006913933,0.000024791108,0.00011297772,0.000035773734,0.000095725525,0.0024994938],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998073,0.000060473652,0.0000069528282,0.000017509707,0.00009503567,0.000012893696],"domain_scores_gemma":[0.9997981,0.00009138561,0.000019024132,0.000023442499,0.000055479955,0.0000126054],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004816984,0.00037122561,0.00042967088,0.00030187372,0.0002512953,0.0005077365,0.00032883591,0.0005169119,0.0009270236],"category_scores_gemma":[0.00070784404,0.00025165663,0.00033744625,0.0002387977,0.000618737,0.00032219038,0.00053665246,0.000629674,0.00016976279],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00003885567,0.000048712274,0.00024374055,0.000059749134,0.000014443799,0.000044908604,0.00005222766,0.90195036,0.0196336,0.031177165,0.00025659052,0.046479646],"study_design_scores_gemma":[0.0000046269815,0.000015047684,0.000024993435,0.0000020635794,0.0000013747424,0.000008798986,0.0000028941383,0.99585426,0.0014841706,0.0020949962,0.0005046784,0.0000021199346],"about_ca_topic_score_codex":0.0008842398,"about_ca_topic_score_gemma":0.0010835021,"teacher_disagreement_score":0.0009270236,"about_ca_system_score_codex":0.00027592893,"about_ca_system_score_gemma":0.0005241068,"threshold_uncertainty_score":0.0031012297},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.011810983,0.00043851728,0.9541117,0.00025129915,0.00032035878,0.00009311593,0.00017341948,0.00051358045,0.032287043],"genre_scores_gemma":[0.57957965,0.0019041869,0.37263104,0.0005692105,0.0005884172,0.00050613354,0.00048747554,0.0009520953,0.04278179],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997403,0.000039925522,0.000011216377,0.000028020266,0.00014696729,0.000033637723],"domain_scores_gemma":[0.9997569,0.00005923148,0.000023527422,0.000024517994,0.00011206347,0.000023812885],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002404617,0.00075202127,0.00068109547,0.0010359653,0.0008138919,0.0019391848,0.0016131848,0.0016954546,0.0058378656],"category_scores_gemma":[0.00085618533,0.00067214103,0.0011511511,0.0005561082,0.00079307513,0.0008784621,0.00141489,0.0010170465,0.001794108],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00003964893,0.00012820943,0.00072101684,0.000106700165,0.000042355012,0.0004909993,0.00022219654,0.86600745,0.013526585,0.08085947,0.0032441563,0.03461119],"study_design_scores_gemma":[0.0000024401234,0.0000051572893,0.000058917896,0.0000059435147,0.000002555869,0.000040491243,0.000018306686,0.9944754,0.00028906882,0.0029578495,0.0021352614,0.000008697338],"about_ca_topic_score_codex":0.00547837,"about_ca_topic_score_gemma":0.005366184,"teacher_disagreement_score":0.0058378656,"about_ca_system_score_codex":0.0006889642,"about_ca_system_score_gemma":0.0010562938,"threshold_uncertainty_score":0.019529581},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9717049,0.00010761844,0.022140915,0.00015961989,0.000053675423,0.00004207399,0.00010341287,0.0003213181,0.005366588],"genre_scores_gemma":[0.9967969,0.00004362122,0.0020161478,0.000011552061,0.000006968714,0.0000108531285,0.000042247902,0.000019134426,0.001052417],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99987173,0.000032696767,0.0000049964924,0.000015511789,0.000041994936,0.00003312171],"domain_scores_gemma":[0.99949336,0.00030262466,0.00004809654,0.000017537528,0.00008092629,0.000057408542],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002874172,0.00067453465,0.00056161656,0.00031699974,0.00045077386,0.0004985637,0.00047904556,0.00088782364,0.0012516648],"category_scores_gemma":[0.001039726,0.00021561056,0.00040403559,0.00019710176,0.0007715255,0.00031235188,0.00039258352,0.0004484028,0.00013374227],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00019805171,0.00007207628,0.002306928,0.000041097403,0.000009478653,0.00040377857,0.00006300727,0.98178023,0.011898435,0.00056370633,0.00016701088,0.0024962388],"study_design_scores_gemma":[0.000010709553,0.000039444465,0.00046192767,0.0000013162055,0.0000017719944,0.0000115876965,0.000009576069,0.9982741,0.0011147797,0.000036839952,0.000034785327,0.0000031881914],"about_ca_topic_score_codex":0.015084,"about_ca_topic_score_gemma":0.005857164,"teacher_disagreement_score":0.015084,"about_ca_system_score_codex":0.00050227926,"about_ca_system_score_gemma":0.00044834826,"threshold_uncertainty_score":0.029992402},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.53399104,0.00019701247,0.45064688,0.00026722907,0.00027590437,0.00023222335,0.00072277157,0.0027654318,0.0109015],"genre_scores_gemma":[0.9596035,0.00011334809,0.036853302,0.000039235016,0.000017467126,0.00009363466,0.00033416844,0.00012169176,0.0028237372],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99932885,0.0001266249,0.00003544494,0.000114160975,0.00034037416,0.0000545501],"domain_scores_gemma":[0.9988739,0.00040599456,0.000067469584,0.00022568046,0.0003852994,0.00004152029],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0008330525,0.0008454504,0.0005538556,0.0003560019,0.00051612395,0.00079899945,0.0011390254,0.0013881437,0.0019492093],"category_scores_gemma":[0.0017434285,0.0002770693,0.0004476381,0.00032786644,0.00052119844,0.0008628988,0.0005708065,0.00046778578,0.0008692398],"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":[0.0006600354,0.0010333186,0.0029235384,0.00033092615,0.000052524814,0.00025394632,0.0002782819,0.66097254,0.28668413,0.003731787,0.0020846587,0.04099432],"study_design_scores_gemma":[0.00002929496,0.00020805228,0.0005559779,0.000009564784,0.000014114981,0.000040594525,0.000019462463,0.9647294,0.033331756,0.00024466225,0.00079785136,0.000019352301],"about_ca_topic_score_codex":0.0032835605,"about_ca_topic_score_gemma":0.0022972494,"teacher_disagreement_score":0.0032835605,"about_ca_system_score_codex":0.00046537587,"about_ca_system_score_gemma":0.0007125862,"threshold_uncertainty_score":0.006528914},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.5976995,0.0007656881,0.34572983,0.0006484233,0.00045689024,0.00015054073,0.0007353192,0.0011132543,0.052700456],"genre_scores_gemma":[0.9404008,0.00047842864,0.0506451,0.000108647124,0.00007242279,0.00004473094,0.00022274243,0.00022841984,0.007798772],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997559,0.00003921377,0.000008163672,0.00005329961,0.00010326508,0.000040257793],"domain_scores_gemma":[0.9996414,0.00013859941,0.00004847845,0.000060161416,0.00008850901,0.00002279362],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00037536075,0.0009824632,0.00043279276,0.0006659844,0.0005783725,0.0018147454,0.0008673221,0.0009356928,0.0029416042],"category_scores_gemma":[0.0009835014,0.00058074226,0.0006819668,0.00046573754,0.0011397385,0.0018726893,0.00082785316,0.0008092595,0.00057402544],"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":[0.0007489006,0.00029545673,0.0037397386,0.00036966984,0.000091472175,0.0012514334,0.00069791364,0.19549948,0.5112422,0.24409825,0.0045106383,0.037454836],"study_design_scores_gemma":[0.00018553446,0.00019408051,0.00500408,0.00007803805,0.00008605194,0.0008793643,0.00017389568,0.81319743,0.15575862,0.018090399,0.006167128,0.00018548315],"about_ca_topic_score_codex":0.0016870856,"about_ca_topic_score_gemma":0.001517971,"teacher_disagreement_score":0.0029416042,"about_ca_system_score_codex":0.0010117731,"about_ca_system_score_gemma":0.0005749327,"threshold_uncertainty_score":0.009840667},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.89978063,0.00040640085,0.09125393,0.000110306704,0.00006498811,0.000069394104,0.00013963704,0.00023000069,0.00794483],"genre_scores_gemma":[0.98472875,0.00010905285,0.014014487,0.000011036153,0.000005592568,0.000022221218,0.00004994832,0.000012432398,0.0010463728],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99980015,0.0000319923,0.000012234551,0.000027146723,0.000089885034,0.00003862723],"domain_scores_gemma":[0.99963284,0.00015080204,0.00007346645,0.00003254413,0.00007369057,0.000036652098],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00046908445,0.00032825486,0.0005634368,0.00026990444,0.00040449656,0.00074488274,0.00049582886,0.00046932267,0.0010179742],"category_scores_gemma":[0.00069242815,0.00020295019,0.00045051737,0.00027296666,0.00054765254,0.00029197626,0.00047463027,0.00032465305,0.00012894096],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00021498936,0.00015704571,0.006491952,0.00017015477,0.000031803513,0.00048812735,0.00019689681,0.78210884,0.19185333,0.008333738,0.00020843325,0.009744659],"study_design_scores_gemma":[0.000033272114,0.00011636668,0.0009267573,0.000006413022,0.0000061782043,0.000054197753,0.00002132606,0.9799059,0.018299619,0.00027319964,0.00034485856,0.000011951854],"about_ca_topic_score_codex":0.0025194557,"about_ca_topic_score_gemma":0.001128122,"teacher_disagreement_score":0.0025194557,"about_ca_system_score_codex":0.00046805118,"about_ca_system_score_gemma":0.0006339236,"threshold_uncertainty_score":0.005009532},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9964485,0.00008438491,0.0031254848,0.000017680988,0.000009637321,0.000008800013,0.000013459174,0.000037386417,0.0002546384],"genre_scores_gemma":[0.99514174,0.00006366409,0.0042520757,0.0000075272083,0.000010404194,0.000009324853,0.000016345663,0.000009649489,0.00048918603],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999746,0.00005572804,0.000015746467,0.000059033177,0.000080197344,0.000043317923],"domain_scores_gemma":[0.99948454,0.00017401601,0.0002048711,0.000048767408,0.000045589586,0.000042207652],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00042369915,0.0005067808,0.0004573778,0.00019591383,0.00019354155,0.00030929313,0.0004916419,0.0003907206,0.00070659176],"category_scores_gemma":[0.00057705323,0.00036803784,0.00027705825,0.0001534371,0.0006080206,0.00037385212,0.00042732028,0.00025886513,0.000224272],"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":[0.00016291185,0.000019066669,0.00030633982,0.000029516277,0.000005382624,0.00008240489,0.00005253853,0.0021130545,0.9958584,0.00017218295,0.000023644614,0.00117466],"study_design_scores_gemma":[0.000093587485,0.00065788144,0.002493492,0.0000060895254,0.000021506447,0.000108197186,0.00004011712,0.039144747,0.95697564,0.00009538684,0.00034757913,0.000015730493],"about_ca_topic_score_codex":0.00057205564,"about_ca_topic_score_gemma":0.00080455764,"teacher_disagreement_score":0.00070659176,"about_ca_system_score_codex":0.00031743132,"about_ca_system_score_gemma":0.00021831656,"threshold_uncertainty_score":0.0023637414},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9797238,0.00010499659,0.0101165995,0.00030956068,0.0002996785,0.00005460831,0.00019097982,0.0007490866,0.008450669],"genre_scores_gemma":[0.9923901,0.000048452937,0.0010879305,0.00007199239,0.000088598026,0.000011880552,0.00014308837,0.000104788276,0.0060531558],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991529,0.00018312044,0.000030685347,0.00016809399,0.00031190412,0.0001532251],"domain_scores_gemma":[0.9983205,0.00057340716,0.00006678352,0.000116284056,0.0005269156,0.00039602522],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00071628974,0.000991035,0.0011642533,0.0011288594,0.0018985566,0.0008920416,0.0008822957,0.0025604737,0.006696745],"category_scores_gemma":[0.0014838475,0.00046656135,0.0006512549,0.00038362882,0.0008257558,0.0005204456,0.0010727257,0.0010110254,0.00096624787],"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":[0.01936088,0.0013975105,0.059536755,0.0008864191,0.00031147664,0.03149283,0.005273617,0.07592983,0.70261574,0.0017541462,0.012501098,0.088939644],"study_design_scores_gemma":[0.0005306868,0.012998118,0.43368354,0.00044551716,0.0008855609,0.011072262,0.0061384724,0.22716859,0.2881375,0.0016421333,0.01671149,0.0005860805],"about_ca_topic_score_codex":0.0022824523,"about_ca_topic_score_gemma":0.0024459788,"teacher_disagreement_score":0.006696745,"about_ca_system_score_codex":0.0005806778,"about_ca_system_score_gemma":0.0003917789,"threshold_uncertainty_score":0.022402823},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9976299,0.00008358481,0.001830218,0.000010283986,0.000009002529,0.000005632376,0.000006998611,0.000026960995,0.00039746333],"genre_scores_gemma":[0.9995147,0.000026561442,0.00034218913,0.000005760751,0.0000024295325,0.0000025664356,0.0000052615055,0.0000026168893,0.000097995784],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998441,0.000034564884,0.000008560045,0.000024063718,0.000035682093,0.00005304705],"domain_scores_gemma":[0.99936026,0.00037190304,0.000094372204,0.00005519211,0.000060578997,0.000057783993],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00022199283,0.00016912169,0.00021796259,0.00011163798,0.00017973607,0.00029138368,0.00014725783,0.0002035005,0.0009064189],"category_scores_gemma":[0.000986697,0.00012900676,0.00015969768,0.000037095608,0.00045461764,0.0001694256,0.00034781633,0.00021412363,0.00011024894],"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":[0.00029216407,0.000023256536,0.0011054616,0.000048215097,0.0000061963956,0.00019606178,0.000058344165,0.0018891769,0.9919721,0.0000911852,0.000024783954,0.004293119],"study_design_scores_gemma":[0.00006682066,0.00091973844,0.019837454,0.00001722146,0.000031940475,0.00024580694,0.00018662306,0.035752244,0.9419775,0.00012977523,0.0008097049,0.000025269168],"about_ca_topic_score_codex":0.0004063079,"about_ca_topic_score_gemma":0.00030571537,"teacher_disagreement_score":0.0009064189,"about_ca_system_score_codex":0.0001379266,"about_ca_system_score_gemma":0.00013554741,"threshold_uncertainty_score":0.0030322075},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.88962924,0.00028877414,0.10587758,0.00013979342,0.00007521695,0.00006814222,0.00012874752,0.00075928547,0.0030332184],"genre_scores_gemma":[0.99373513,0.00007772085,0.005645503,0.000014064512,0.000008544863,0.000020422724,0.000052838357,0.00003567647,0.00041015694],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999757,0.0000693375,0.000017225611,0.000032176857,0.000076199925,0.00004802012],"domain_scores_gemma":[0.9993667,0.00035388037,0.00007377403,0.00005912964,0.00010815007,0.00003837408],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005050903,0.0007332737,0.00047628838,0.0004750963,0.00038982547,0.00058396463,0.0005337379,0.00076766283,0.0005708658],"category_scores_gemma":[0.0018659612,0.0002870735,0.0006245366,0.00021806255,0.00044066698,0.0005405706,0.00055784953,0.00047066173,0.0001463883],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00013144949,0.000052789892,0.0021490816,0.00004394721,0.000010828843,0.00017208916,0.00003986789,0.9759587,0.015737208,0.0006762762,0.00007236265,0.0049553644],"study_design_scores_gemma":[0.00000911999,0.00010834053,0.0011500149,0.0000053130625,0.0000064634346,0.000022930539,0.000010166751,0.9942675,0.0042247497,0.00011201323,0.000074014686,0.000009327793],"about_ca_topic_score_codex":0.005892024,"about_ca_topic_score_gemma":0.003902719,"teacher_disagreement_score":0.005892024,"about_ca_system_score_codex":0.00042846487,"about_ca_system_score_gemma":0.00053856254,"threshold_uncertainty_score":0.011715472},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9902193,0.000093405615,0.007357021,0.00004293928,0.00003557979,0.000013757883,0.00004470164,0.00014556276,0.0020477665],"genre_scores_gemma":[0.9981165,0.000036572004,0.0011278467,0.0000129393875,0.0000071642858,0.000007443259,0.000025382866,0.000007923082,0.00065837527],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99957174,0.00007606689,0.00002351638,0.00008620906,0.0001664178,0.000076040924],"domain_scores_gemma":[0.99861157,0.0008057367,0.00011252107,0.00008873029,0.0002697169,0.00011170198],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00045275842,0.00033072606,0.00037789575,0.00024316652,0.00028686284,0.00033089324,0.00046987814,0.00062495045,0.0021566143],"category_scores_gemma":[0.0009883736,0.00021076486,0.00024875512,0.00018359612,0.0005505337,0.0003367463,0.00062047614,0.00030950317,0.00040410645],"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":[0.0010234389,0.00016642013,0.0067326985,0.00013720062,0.000023890918,0.0013117476,0.00040114808,0.014723486,0.96333414,0.0003343347,0.00020091355,0.011610577],"study_design_scores_gemma":[0.000111556736,0.0045388467,0.039041203,0.000056007655,0.00005590205,0.0020179,0.00074047904,0.19989204,0.749702,0.00055728387,0.0031895072,0.00009723111],"about_ca_topic_score_codex":0.0005359884,"about_ca_topic_score_gemma":0.00037810495,"teacher_disagreement_score":0.0021566143,"about_ca_system_score_codex":0.00019878225,"about_ca_system_score_gemma":0.00014959913,"threshold_uncertainty_score":0.007214606},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97004414,0.0001866429,0.013947142,0.00031110516,0.00016373777,0.00004248005,0.00017467969,0.00025065083,0.014879384],"genre_scores_gemma":[0.99335116,0.000056508605,0.0034438372,0.000036236,0.000013421202,0.000020870393,0.00007565597,0.000027628907,0.0029747419],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998266,0.000027349692,0.000009870153,0.00001872008,0.00006761828,0.000049879],"domain_scores_gemma":[0.9993699,0.00032815762,0.00007077406,0.000041466537,0.00009611908,0.00009355025],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024070621,0.00043672722,0.00059952383,0.00047711306,0.00089207524,0.001064525,0.00069644937,0.0012273156,0.002749627],"category_scores_gemma":[0.0011849502,0.00042359572,0.0005377613,0.0003901292,0.0008842908,0.000536929,0.0005694222,0.0007045648,0.00019575961],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0001675715,0.00012063635,0.0015983429,0.000027135584,0.000021647973,0.00026972484,0.00008498129,0.9888136,0.0052719293,0.0013118865,0.00023882651,0.0020737431],"study_design_scores_gemma":[0.000011024451,0.0000414655,0.00042498307,0.0000019434628,0.0000034813463,0.000009748158,0.000023781724,0.9985619,0.00074855535,0.00007166264,0.00009552025,0.0000059606114],"about_ca_topic_score_codex":0.01744009,"about_ca_topic_score_gemma":0.009399008,"teacher_disagreement_score":0.01744009,"about_ca_system_score_codex":0.00066558755,"about_ca_system_score_gemma":0.00096385635,"threshold_uncertainty_score":0.034677148},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9991621,0.000055250046,0.00037839552,0.000012957821,0.000013674224,0.0000028864981,0.000014724011,0.000015914608,0.00034420445],"genre_scores_gemma":[0.99956363,0.000024775307,0.00018413526,0.0000057445955,0.0000048834536,0.0000015732825,0.000015637741,0.000009274204,0.00019028605],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997538,0.000043966196,0.00001696835,0.000040409566,0.000047601578,0.000097351454],"domain_scores_gemma":[0.9979786,0.0012620437,0.00018620401,0.00010574543,0.00021626528,0.00025111486],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00040066647,0.0003951975,0.0005157499,0.00037178397,0.00044371685,0.0008123616,0.00042566442,0.00058763736,0.0017975826],"category_scores_gemma":[0.002327676,0.00026741577,0.0003370349,0.00017143924,0.00065413624,0.0005324774,0.00055432535,0.0006489497,0.0001690551],"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":[0.0087101795,0.00030545803,0.007028611,0.000096112235,0.000045468758,0.0012892154,0.00018843471,0.01679562,0.9564137,0.00041276636,0.000106804466,0.008607574],"study_design_scores_gemma":[0.00023805411,0.0043242793,0.047424894,0.000020221903,0.00012401934,0.0004771808,0.00040239442,0.08675023,0.8596471,0.00014815536,0.0003592642,0.00008430882],"about_ca_topic_score_codex":0.0010955798,"about_ca_topic_score_gemma":0.0007352042,"teacher_disagreement_score":0.0017975826,"about_ca_system_score_codex":0.00027076298,"about_ca_system_score_gemma":0.00028069923,"threshold_uncertainty_score":0.0060135126},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9946885,0.00007939344,0.004251068,0.000026017326,0.000016553398,0.000035636363,0.00012089706,0.000057847217,0.0007239842],"genre_scores_gemma":[0.99555653,0.00006376027,0.0035430216,0.0000086857945,0.0000052509954,0.000027787382,0.00008909712,0.000010233761,0.00069572194],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99964404,0.000048428858,0.000015499561,0.00008848418,0.00011819079,0.00008527955],"domain_scores_gemma":[0.9992847,0.00029701178,0.00008895062,0.00008045036,0.0001538049,0.000095111536],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004016962,0.00048811088,0.00044689223,0.00026523613,0.00041214598,0.00033166038,0.0004284663,0.00046910552,0.0011558987],"category_scores_gemma":[0.00083728787,0.0001438316,0.00015080966,0.00021873286,0.00066219014,0.00034693247,0.00056168565,0.00035241258,0.00016986219],"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":[0.00056801224,0.0001965403,0.0019042747,0.00011383465,0.000008938703,0.0003280125,0.000231542,0.004366744,0.9858797,0.0001870487,0.00009109829,0.0061242334],"study_design_scores_gemma":[0.00016699036,0.004078844,0.023377225,0.000023677314,0.000028148304,0.0005685596,0.00038003875,0.016641414,0.9521007,0.00013106686,0.0024338965,0.000069374735],"about_ca_topic_score_codex":0.0012706878,"about_ca_topic_score_gemma":0.0012971967,"teacher_disagreement_score":0.0012706878,"about_ca_system_score_codex":0.00032044886,"about_ca_system_score_gemma":0.00025270254,"threshold_uncertainty_score":0.003866911},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9986364,0.000033343327,0.0006609984,0.000009712008,0.0000067508076,0.0000028735456,0.000021309246,0.000027174148,0.00060142274],"genre_scores_gemma":[0.99963355,0.000009488048,0.000098863944,0.0000025828613,0.0000057896923,0.0000013579979,0.000030133777,0.000007604704,0.00021049821],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99992716,0.000012205221,0.0000030180033,0.0000147194705,0.000017985516,0.00002489162],"domain_scores_gemma":[0.9994704,0.00023304737,0.0000678996,0.000026649499,0.000090563335,0.00011141264],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001300436,0.00016315452,0.00028951478,0.00076246285,0.0003008122,0.0003448514,0.00021741565,0.00038833846,0.0010692048],"category_scores_gemma":[0.0009462012,0.0001932187,0.00015380095,0.00017222963,0.00036488893,0.00043714434,0.00024956898,0.00020360084,0.00017439511],"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":[0.0070585385,0.0011536118,0.21928571,0.00017048081,0.000105610525,0.002740297,0.0014168383,0.071917936,0.639202,0.0025712529,0.001828069,0.05254961],"study_design_scores_gemma":[0.00011731229,0.00081522245,0.7458709,0.00002010628,0.00005247716,0.0011634226,0.0006439154,0.21156311,0.037820652,0.0011885468,0.0006625383,0.000081823164],"about_ca_topic_score_codex":0.00084514875,"about_ca_topic_score_gemma":0.00073653174,"teacher_disagreement_score":0.0010692048,"about_ca_system_score_codex":0.00015605034,"about_ca_system_score_gemma":0.00008205888,"threshold_uncertainty_score":0.0035768747},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9549554,0.00018838601,0.023778645,0.00014501046,0.00008321748,0.00004638642,0.00012973092,0.00020920373,0.02046401],"genre_scores_gemma":[0.9967301,0.000036965837,0.0010655598,0.000009177303,0.000010682469,0.000008440775,0.000035289504,0.000017374352,0.0020863255],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998565,0.00002653143,0.0000043383466,0.000025925208,0.000058442474,0.0000282981],"domain_scores_gemma":[0.999263,0.00045151846,0.000032014534,0.000028920513,0.00016795882,0.000056552813],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00026416304,0.0005882375,0.00046586563,0.0003872213,0.0005119335,0.0009420172,0.00059079455,0.0008593668,0.00217873],"category_scores_gemma":[0.0014232777,0.00033773447,0.0004150504,0.00019286197,0.00088458066,0.0005316391,0.00056406093,0.0006538941,0.00034375966],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00016418991,0.000079087054,0.0029413821,0.00003189801,0.000007001959,0.00015344577,0.00004904468,0.9851364,0.0056582214,0.0014431326,0.00026409107,0.0040720645],"study_design_scores_gemma":[0.000021009451,0.00004413333,0.00077740906,0.0000017765134,0.0000030563688,0.000012599006,0.000014317777,0.99735826,0.0014551976,0.0002052364,0.00010228087,0.000004711435],"about_ca_topic_score_codex":0.015816677,"about_ca_topic_score_gemma":0.008554375,"teacher_disagreement_score":0.015816677,"about_ca_system_score_codex":0.0007229714,"about_ca_system_score_gemma":0.00065522187,"threshold_uncertainty_score":0.03144926},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9967313,0.000072971794,0.0023886643,0.000014881398,0.00001005146,0.0000058933706,0.000023476183,0.000037429778,0.0007153126],"genre_scores_gemma":[0.9992981,0.00002978532,0.0003567593,0.000004319135,0.000003398447,0.000003395188,0.000031873325,0.000008777521,0.00026362616],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998017,0.000052457468,0.000011277831,0.000029285293,0.000057937566,0.00004729272],"domain_scores_gemma":[0.99742585,0.0016182245,0.0001225297,0.00009331335,0.0005423437,0.00019764119],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00053055806,0.00033349523,0.0003594718,0.00030830927,0.00031472917,0.00037296786,0.0002811323,0.00033236304,0.0014005837],"category_scores_gemma":[0.0019605174,0.00016765323,0.00021419449,0.00017089413,0.0006299846,0.0004497808,0.0003365494,0.00024547993,0.000261918],"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":[0.0048203003,0.00026316027,0.010993869,0.00011467395,0.000025746174,0.00029204067,0.00036264324,0.019415995,0.94531405,0.00065581687,0.00023612966,0.017505562],"study_design_scores_gemma":[0.00020042004,0.0022417582,0.02431436,0.000025975525,0.00004540476,0.00054637936,0.0002906563,0.13264479,0.83831173,0.00046708505,0.00085221214,0.000059264334],"about_ca_topic_score_codex":0.0006906007,"about_ca_topic_score_gemma":0.0005015133,"teacher_disagreement_score":0.0014005837,"about_ca_system_score_codex":0.0002007992,"about_ca_system_score_gemma":0.00017303308,"threshold_uncertainty_score":0.0046854615},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99768066,0.000023275554,0.0019573765,0.000008215962,0.000005276647,0.000004739,0.000030345409,0.000028321443,0.0002617439],"genre_scores_gemma":[0.9984366,0.000018893988,0.0013015039,0.0000026960533,0.0000028009772,0.000006130635,0.000038515296,0.000004145154,0.00018865174],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99975723,0.000038413284,0.0000157363,0.000041965784,0.000101254176,0.000045372195],"domain_scores_gemma":[0.99938715,0.00029913278,0.0000848999,0.000067268906,0.00010512542,0.000056450986],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003458221,0.00032215382,0.00033118358,0.0002294052,0.00031338123,0.00024463437,0.00036221297,0.000385421,0.0007421135],"category_scores_gemma":[0.0007602518,0.00011172445,0.0002227077,0.00015792582,0.00057261396,0.00022233218,0.000347823,0.00027973263,0.00007178623],"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":[0.0005557531,0.00043538067,0.011748392,0.00015876106,0.000021946445,0.00054297387,0.0004495305,0.049248062,0.9271666,0.00048279972,0.00014125065,0.009048478],"study_design_scores_gemma":[0.000090927264,0.003615354,0.049141057,0.000026402862,0.0000514243,0.0002681293,0.0003940007,0.3176654,0.62746316,0.00026019168,0.0009352962,0.000088657944],"about_ca_topic_score_codex":0.0007918341,"about_ca_topic_score_gemma":0.0005702926,"teacher_disagreement_score":0.0007918341,"about_ca_system_score_codex":0.00016548054,"about_ca_system_score_gemma":0.00013322932,"threshold_uncertainty_score":0.002482593},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97178215,0.0003472942,0.02467105,0.000075977434,0.000052020798,0.000066210894,0.000051092335,0.00012630985,0.0028279335],"genre_scores_gemma":[0.9970029,0.000077940436,0.00269523,0.0000039206484,0.000005268066,0.0000165199,0.000009277266,0.000004029183,0.00018490854],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9995295,0.00010040616,0.00002212271,0.000050949013,0.000224949,0.00007206174],"domain_scores_gemma":[0.9993986,0.0002787432,0.00010689023,0.00005727973,0.00011656138,0.000041962256],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00076969294,0.00046949784,0.0004481438,0.00032555,0.0003900593,0.00037562422,0.00035333366,0.00035288322,0.00090780185],"category_scores_gemma":[0.0010162876,0.0001681601,0.00025132045,0.00023098457,0.00096479803,0.00031988078,0.00040178082,0.00023562595,0.00007066022],"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":[0.0010696114,0.0005455793,0.0020265745,0.0004376601,0.000020852074,0.00017623688,0.00023406003,0.07701166,0.9022013,0.0018144894,0.00024161473,0.014220307],"study_design_scores_gemma":[0.00019729268,0.0021657133,0.0073641627,0.000024768746,0.000040818846,0.0000889294,0.00013300971,0.44849452,0.53884387,0.0004992659,0.002063959,0.000083778],"about_ca_topic_score_codex":0.001150779,"about_ca_topic_score_gemma":0.0008749745,"teacher_disagreement_score":0.001150779,"about_ca_system_score_codex":0.0004376347,"about_ca_system_score_gemma":0.00026511223,"threshold_uncertainty_score":0.00407058},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9845808,0.000037721835,0.013953826,0.000016647566,0.000008386375,0.00002423288,0.00006165439,0.00011665821,0.0012000276],"genre_scores_gemma":[0.9979043,0.000021856542,0.0017234338,0.000003952064,0.0000026068788,0.000008099632,0.0000758211,0.000009695563,0.00025018232],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99980086,0.000035653444,0.000007866658,0.000023067698,0.00010834264,0.000024229628],"domain_scores_gemma":[0.99948275,0.00028049952,0.000028302227,0.000030045992,0.00014032742,0.000037903315],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00027421667,0.0005336842,0.00031876934,0.00040463553,0.00024019863,0.00030678135,0.00030756445,0.0005931287,0.0006510833],"category_scores_gemma":[0.00072773686,0.00021513886,0.000328635,0.00022478128,0.00043423395,0.00029098307,0.00030014757,0.0002692968,0.00018344737],"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":[0.0014917607,0.00041416837,0.052869357,0.00024438396,0.00007055256,0.0025874258,0.0008272568,0.4834993,0.40777367,0.0011468282,0.00061734125,0.048457984],"study_design_scores_gemma":[0.00005969043,0.0008660957,0.07566587,0.000016284876,0.000024239738,0.00033919077,0.0002988945,0.8712051,0.05071749,0.0003768326,0.0003874009,0.00004293563],"about_ca_topic_score_codex":0.0021972677,"about_ca_topic_score_gemma":0.0018596709,"teacher_disagreement_score":0.0021972677,"about_ca_system_score_codex":0.00021638349,"about_ca_system_score_gemma":0.00020418367,"threshold_uncertainty_score":0.004368961},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.50766873,0.0005934673,0.48450702,0.00010228133,0.000027685352,0.00009437688,0.000038849168,0.00029273645,0.0066748173],"genre_scores_gemma":[0.84345764,0.00024261235,0.15480888,0.000031370346,0.000007102566,0.000056702385,0.00003018134,0.00010976384,0.0012557374],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99973375,0.00008479483,0.000013069478,0.00004588004,0.000084923355,0.000037538703],"domain_scores_gemma":[0.9992563,0.00049313845,0.00009599695,0.000054064552,0.00007822462,0.000022218219],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00080097455,0.00096331286,0.0006417689,0.0003664893,0.00025728226,0.000553594,0.00041531675,0.00045018335,0.0006531127],"category_scores_gemma":[0.00195737,0.00040928178,0.0004928314,0.00028782332,0.00040422071,0.00043852103,0.0002783779,0.000379976,0.00013477051],"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":[0.0001351726,0.000081848826,0.00054397614,0.00009909708,0.000025764775,0.000054836888,0.000043918822,0.94221365,0.03364859,0.0022878763,0.000113918504,0.020751385],"study_design_scores_gemma":[0.00002069778,0.0005103768,0.00042078653,0.000011381407,0.000020390342,0.0000354214,0.000019742653,0.9822947,0.01580979,0.0003767497,0.0004657856,0.0000143022735],"about_ca_topic_score_codex":0.0014963042,"about_ca_topic_score_gemma":0.0016909327,"teacher_disagreement_score":0.0014963042,"about_ca_system_score_codex":0.00040863382,"about_ca_system_score_gemma":0.00075825915,"threshold_uncertainty_score":0.004235983},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9876281,0.00007494206,0.010579657,0.00006852604,0.00007460298,0.000018690487,0.000054720276,0.00016371613,0.0013369916],"genre_scores_gemma":[0.9963266,0.00003660138,0.0029751947,0.000018584977,0.000009686015,0.0000069131856,0.00004150986,0.00006515314,0.0005197528],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9995777,0.0001114566,0.0000327549,0.00008327779,0.00010039147,0.00009432975],"domain_scores_gemma":[0.99484336,0.0036407658,0.00030218431,0.00033820537,0.00058690907,0.000288488],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005737831,0.0005258993,0.0003387536,0.00032170664,0.00035613988,0.00087602716,0.0003906098,0.0005724167,0.0017435298],"category_scores_gemma":[0.00596305,0.00027788308,0.00014954207,0.00026039415,0.0005542392,0.0006765508,0.000310266,0.00045865576,0.00022981656],"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":[0.012892994,0.0014626663,0.0063255974,0.00021240496,0.00007891761,0.00042049531,0.00028177636,0.17218076,0.7617939,0.0027349524,0.00055259204,0.041062944],"study_design_scores_gemma":[0.0003564582,0.0027675463,0.009035045,0.000024121042,0.0001024231,0.00022202863,0.00015430292,0.50684077,0.47902834,0.0005622311,0.00078841305,0.00011832236],"about_ca_topic_score_codex":0.0007770094,"about_ca_topic_score_gemma":0.00042595642,"teacher_disagreement_score":0.0017435298,"about_ca_system_score_codex":0.00022807789,"about_ca_system_score_gemma":0.0004152724,"threshold_uncertainty_score":0.005832672},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.96015596,0.00009349551,0.0358678,0.0000569684,0.000046726207,0.00003540951,0.00005168165,0.00017202755,0.0035199318],"genre_scores_gemma":[0.992706,0.000027134822,0.006709071,0.000008456809,0.000006902846,0.000013923256,0.000040186093,0.000014340849,0.00047399648],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99983025,0.000042763808,0.000009218331,0.000026261183,0.00006207754,0.000029411913],"domain_scores_gemma":[0.9993042,0.00036751945,0.00007521362,0.000052133844,0.00012696325,0.000074013304],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00036334907,0.0004934133,0.0005060317,0.0003957102,0.00034990313,0.0005896925,0.0005949036,0.0007454977,0.0007830458],"category_scores_gemma":[0.001328071,0.00016482828,0.00039542152,0.0002925882,0.00060231076,0.0003594704,0.00045736475,0.00036950174,0.00010062012],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00048644806,0.00019103139,0.007033348,0.00009307144,0.000039149516,0.0005901839,0.00026926567,0.93557703,0.039544243,0.0018092406,0.00020912575,0.014157864],"study_design_scores_gemma":[0.000014559044,0.00009251877,0.0013789196,0.0000038194526,0.0000066590583,0.000029114684,0.000035000856,0.9956117,0.002598273,0.00009822328,0.00012048268,0.000010810554],"about_ca_topic_score_codex":0.0048375595,"about_ca_topic_score_gemma":0.002692028,"teacher_disagreement_score":0.0048375595,"about_ca_system_score_codex":0.00028687352,"about_ca_system_score_gemma":0.00039972682,"threshold_uncertainty_score":0.009618819},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99719465,0.00009115538,0.0023697307,0.000005212209,0.000004031595,0.000006146639,0.000009719948,0.00004239329,0.0002770199],"genre_scores_gemma":[0.99802834,0.000046445868,0.0018060309,0.000004491921,0.0000019050108,0.0000031748043,0.000008418065,0.000008304731,0.00009277377],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99973243,0.000058638878,0.000017777125,0.000057581638,0.00006284479,0.00007082419],"domain_scores_gemma":[0.9986939,0.0006810314,0.00027598257,0.00012554074,0.00015175258,0.00007177272],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00034667342,0.00038025517,0.0003100451,0.00021417264,0.00016142662,0.0002848469,0.00029203834,0.00027950443,0.00053070096],"category_scores_gemma":[0.0010572266,0.00024626078,0.00018967364,0.0000980792,0.0003886607,0.00027982815,0.0003599004,0.0002183886,0.0001344577],"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":[0.0003032154,0.000027983117,0.0022691328,0.00008614649,0.0000061745604,0.00016847612,0.00007092579,0.003657525,0.9872291,0.00007554376,0.000021535432,0.006084378],"study_design_scores_gemma":[0.000020523696,0.0018532556,0.020221684,0.000013019082,0.000048714614,0.00020683848,0.000111339905,0.011151807,0.9659571,0.000044464854,0.00034790783,0.00002346662],"about_ca_topic_score_codex":0.0002222296,"about_ca_topic_score_gemma":0.00037058012,"teacher_disagreement_score":0.00053070096,"about_ca_system_score_codex":0.00010933674,"about_ca_system_score_gemma":0.0001012973,"threshold_uncertainty_score":0.0018334389},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8014511,0.002803822,0.078985885,0.0055226567,0.0010790302,0.0027874056,0.0057185423,0.0072436137,0.094408005],"genre_scores_gemma":[0.86009413,0.0009739526,0.08432483,0.00096541847,0.00022554683,0.0007913811,0.008409158,0.00033676898,0.043878853],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9986356,0.00019142692,0.000015632446,0.00012905763,0.00066215126,0.0003662173],"domain_scores_gemma":[0.9988795,0.000091661444,0.000052398234,0.00008806206,0.00039979603,0.000488692],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0037106834,0.0009658636,0.00043202462,0.0007065426,0.0015990934,0.0008884451,0.0018513183,0.0013946587,0.0063033733],"category_scores_gemma":[0.0010378363,0.0001635757,0.00040894345,0.000305445,0.0011950572,0.0012278225,0.0014726038,0.0011449127,0.001199136],"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":[0.0072519686,0.0053412216,0.021229997,0.0013925452,0.00022755515,0.0016623907,0.0011619825,0.010797959,0.4669626,0.009523079,0.056250222,0.4181985],"study_design_scores_gemma":[0.0030489962,0.056000914,0.08955233,0.00034271253,0.00026287435,0.0019649111,0.0017001645,0.041546024,0.45850286,0.0028841118,0.34398392,0.00021021867],"about_ca_topic_score_codex":0.011737463,"about_ca_topic_score_gemma":0.018530047,"teacher_disagreement_score":0.011737463,"about_ca_system_score_codex":0.0013248861,"about_ca_system_score_gemma":0.0036142252,"threshold_uncertainty_score":0.023338318},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.02422037,0.000110735724,0.9664256,0.00014079924,0.00009405254,0.000069578746,0.000050928204,0.00029958072,0.008588339],"genre_scores_gemma":[0.4046569,0.00033894143,0.58111614,0.00010405684,0.00008182274,0.00026862283,0.00014212835,0.00015251289,0.013138855],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99985373,0.000023485582,0.000006959467,0.000020540632,0.00008004986,0.000015224579],"domain_scores_gemma":[0.99980515,0.00006147442,0.00002787873,0.000020837138,0.00007170233,0.00001287331],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00029115708,0.0004945377,0.00034318038,0.00030387627,0.00045712086,0.0006568293,0.00077252276,0.0008901636,0.0018457605],"category_scores_gemma":[0.00066887285,0.00025791838,0.0005822176,0.00022473415,0.00044209204,0.00055068143,0.00057851616,0.0008001522,0.00046262163],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000040209936,0.00006511187,0.0009907439,0.00007703814,0.00001692029,0.00013018903,0.0001233834,0.9246783,0.020672115,0.026055729,0.00082927226,0.02632102],"study_design_scores_gemma":[0.000002858401,0.000009120751,0.000030508456,0.0000023713142,0.0000010760351,0.000008767877,0.0000030807394,0.998585,0.00050443196,0.00038316648,0.00046748618,0.0000021125265],"about_ca_topic_score_codex":0.0032919468,"about_ca_topic_score_gemma":0.0037284312,"teacher_disagreement_score":0.0032919468,"about_ca_system_score_codex":0.00042583566,"about_ca_system_score_gemma":0.0012437606,"threshold_uncertainty_score":0.0065455437},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97140324,0.00066137663,0.013177642,0.00011701634,0.0001959666,0.000028649518,0.00022278917,0.00017888984,0.0140145095],"genre_scores_gemma":[0.99840754,0.0001407188,0.00039695972,0.000011360452,0.000023539851,0.000003295676,0.00008851558,0.00006329629,0.0008648311],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9992681,0.00015944867,0.000033384888,0.00012616195,0.0002347139,0.00017821777],"domain_scores_gemma":[0.99331564,0.0045580915,0.00020190467,0.00031459096,0.0012876475,0.00032213822],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004726255,0.0005194702,0.0006365063,0.0005480168,0.0005811927,0.0009207267,0.00036972828,0.0005140334,0.0060314606],"category_scores_gemma":[0.008855864,0.00025664576,0.000335742,0.00043369184,0.0005911238,0.00054299977,0.0004421641,0.00042777823,0.000929582],"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":[0.0153526515,0.00048030482,0.037606683,0.000668343,0.00017341043,0.0030636564,0.0011173047,0.14271417,0.69514745,0.0031824692,0.001438263,0.09905528],"study_design_scores_gemma":[0.00025516417,0.0018852687,0.20342803,0.00012449776,0.0004589787,0.0036201593,0.0009919486,0.37849188,0.40302426,0.0015786253,0.005901148,0.00024007095],"about_ca_topic_score_codex":0.0038810095,"about_ca_topic_score_gemma":0.0019174024,"teacher_disagreement_score":0.0060314606,"about_ca_system_score_codex":0.0005648852,"about_ca_system_score_gemma":0.00039476,"threshold_uncertainty_score":0.020177245},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.698924,0.0005586863,0.27991933,0.00025032053,0.0002684597,0.00006254248,0.00005232227,0.00020630487,0.019757979],"genre_scores_gemma":[0.994412,0.000047608857,0.0026973798,0.0000113516835,0.000013393089,0.000008553628,0.000009247336,0.000014043871,0.0027865202],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.999835,0.00003724807,0.000006319783,0.000044806387,0.000054277192,0.00002238347],"domain_scores_gemma":[0.99972945,0.00010376888,0.00003176577,0.000018998115,0.000088197616,0.000027720049],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024904963,0.00054969895,0.0002697614,0.00022577275,0.0003444154,0.00052936893,0.00041665396,0.00038541164,0.0012304989],"category_scores_gemma":[0.0008678413,0.000105600724,0.0002356664,0.00008733352,0.00050156715,0.00033682177,0.0003588132,0.0003063929,0.00007481112],"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":[0.0015789323,0.00031628975,0.0020532054,0.00027349193,0.00007203007,0.00028937787,0.0002451222,0.4293666,0.4488216,0.0600661,0.0012241767,0.055692997],"study_design_scores_gemma":[0.000019476936,0.000094804265,0.00040473047,0.0000038267744,0.0000069890575,0.000014018546,0.000013931171,0.97849244,0.01929539,0.0012577504,0.0003844239,0.000012193726],"about_ca_topic_score_codex":0.0023723939,"about_ca_topic_score_gemma":0.001350502,"teacher_disagreement_score":0.0023723939,"about_ca_system_score_codex":0.0004503259,"about_ca_system_score_gemma":0.00027414685,"threshold_uncertainty_score":0.004717171},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.995271,0.00005403649,0.0036452275,0.000007794381,0.000011538161,0.000008185231,0.000087773726,0.00009593761,0.00081854424],"genre_scores_gemma":[0.9953577,0.00005381783,0.003693079,0.000010040844,0.0000055681853,0.000015758127,0.00018925691,0.000022814911,0.00065195485],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.9998815,0.000008992926,0.000007909195,0.000025673051,0.000048963335,0.000026912006],"domain_scores_gemma":[0.9998018,0.00003245277,0.000038444166,0.000017977534,0.00007098138,0.000038245566],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00013766055,0.0002064465,0.00021614511,0.00032930492,0.00029396807,0.0003016102,0.00016264923,0.00019280921,0.00086047256],"category_scores_gemma":[0.00027423288,0.00009942768,0.00014003395,0.00025248577,0.000222315,0.00018523776,0.00029241113,0.0003133606,0.0001752775],"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":[0.00010360111,0.000033901615,0.003927997,0.000014261948,0.000003843995,0.000104286286,0.00008848004,0.00037043818,0.99171054,0.00016976724,0.00008543047,0.0033874454],"study_design_scores_gemma":[0.00007249083,0.0012423797,0.142758,0.000018040608,0.000027206159,0.00025539802,0.00027224183,0.011745498,0.8420978,0.00022466539,0.001235909,0.000050373365],"about_ca_topic_score_codex":0.0008851835,"about_ca_topic_score_gemma":0.0006823123,"teacher_disagreement_score":0.0008851835,"about_ca_system_score_codex":0.00013445488,"about_ca_system_score_gemma":0.00011926364,"threshold_uncertainty_score":0.0028786063},"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":"review","genre_gemma":"review","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"review","genre_consensus":"review","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.00076955,0.9958467,0.00029567984,0.00064502517,0.0008623887,0.0000050816966,0.00003522744,0.0000068702593,0.0015334849],"genre_scores_gemma":[0.004996273,0.99008816,0.0005144296,0.0005422103,0.0013475723,0.000008709804,0.00009871897,0.000007676566,0.0023961912],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.99938226,0.00007309823,0.0000996029,0.0001594722,0.00023676846,0.00004888431],"domain_scores_gemma":[0.9980963,0.00059293275,0.00022354063,0.0000419612,0.0009340105,0.00011119794],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0015443101,0.00075228,0.0011538903,0.004520346,0.00041370717,0.0015484985,0.000955476,0.0012755364,0.0045713596],"category_scores_gemma":[0.00212097,0.00036580945,0.00041014922,0.003939039,0.0006354664,0.0014733361,0.0007990946,0.0009428095,0.0021436685],"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":[0.0001698986,0.000037959715,0.0010791912,0.013344808,0.00006238013,0.00020961878,0.00017211997,0.00030847394,0.0032515086,0.0016097379,0.022322807,0.9574314],"study_design_scores_gemma":[0.000016095113,0.00024241637,0.010965965,0.008371321,0.00016000037,0.00088222214,0.00039558762,0.000112548136,0.0017932698,0.00067849905,0.97634625,0.00003578179],"about_ca_topic_score_codex":0.005600946,"about_ca_topic_score_gemma":0.008528854,"teacher_disagreement_score":0.005600946,"about_ca_system_score_codex":0.0012963902,"about_ca_system_score_gemma":0.0030127359,"threshold_uncertainty_score":0.015292704},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7340829,0.00060694,0.23874503,0.0006342856,0.00033226662,0.00011031779,0.00041100883,0.0006682679,0.024409035],"genre_scores_gemma":[0.9926178,0.00006861518,0.0033906766,0.00003035037,0.00002632192,0.000025318905,0.00008515267,0.000027785376,0.0037280428],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997569,0.00005717788,0.000007625862,0.00005051236,0.0000766149,0.000051178897],"domain_scores_gemma":[0.9995796,0.00022967173,0.00003077666,0.000036635538,0.000085732805,0.000037695012],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00030862246,0.00066121586,0.0010260639,0.00033897103,0.00065583445,0.0008021635,0.000802363,0.0021382428,0.0014264698],"category_scores_gemma":[0.0008487675,0.0003628041,0.00091367256,0.00022063749,0.000787008,0.00052703894,0.000546056,0.0006905862,0.00042577457],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000099683195,0.00005171604,0.0007997248,0.00003686316,0.000017117312,0.00013517628,0.000032145108,0.99113125,0.0045689573,0.0010491543,0.0002547231,0.0018235785],"study_design_scores_gemma":[0.000005071876,0.000013892998,0.00021335187,0.0000010242916,0.000002634466,0.00000486211,0.0000028141988,0.99945503,0.00020898497,0.0000557378,0.000033331828,0.0000032501077],"about_ca_topic_score_codex":0.014247377,"about_ca_topic_score_gemma":0.005633165,"teacher_disagreement_score":0.014247377,"about_ca_system_score_codex":0.000614462,"about_ca_system_score_gemma":0.0007500012,"threshold_uncertainty_score":0.028328896},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.39962375,0.00078319357,0.5491646,0.0006850179,0.00044760737,0.00015322628,0.0010940272,0.0027372641,0.045311302],"genre_scores_gemma":[0.95195925,0.00045178464,0.038925346,0.00011654139,0.00010434695,0.000112527974,0.00045750634,0.00031041066,0.007562319],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998561,0.00003327465,0.00000848737,0.000024019437,0.000052834122,0.000025353424],"domain_scores_gemma":[0.99959,0.00013413085,0.000045002053,0.000041629897,0.00015493899,0.00003437368],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00027088486,0.00092827866,0.00080357766,0.00056862197,0.0005071135,0.0009761792,0.0011683701,0.0022175247,0.0032489363],"category_scores_gemma":[0.0010709413,0.0005564332,0.0010413423,0.0003595294,0.00054440135,0.00068269344,0.00069053983,0.00089212885,0.0013709351],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000025616388,0.00001564649,0.00037329842,0.000023128887,0.0000074461686,0.000069113354,0.000022082602,0.99461854,0.0013355925,0.001017214,0.00022676875,0.0022655334],"study_design_scores_gemma":[0.0000053769513,0.0000068327718,0.00013719579,0.000004618666,0.0000019690472,0.0000049006658,0.0000067728774,0.99921227,0.0003237561,0.00013010773,0.00016208453,0.000004038793],"about_ca_topic_score_codex":0.014149526,"about_ca_topic_score_gemma":0.009036264,"teacher_disagreement_score":0.014149526,"about_ca_system_score_codex":0.00046013042,"about_ca_system_score_gemma":0.00083209533,"threshold_uncertainty_score":0.028134286},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9960373,0.0001705512,0.0014188717,0.000085492145,0.000019529105,0.000009015586,0.00004117361,0.000064429914,0.002153801],"genre_scores_gemma":[0.99903345,0.000036728798,0.00017209542,0.000011807686,0.0000049475047,0.0000037205841,0.000021057145,0.000011432707,0.0007046427],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99993145,0.000007940517,0.000002692522,0.00001073805,0.000015825646,0.000031273164],"domain_scores_gemma":[0.99939585,0.0003777857,0.00004629533,0.000023450571,0.00004917788,0.00010732436],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012913105,0.000097556665,0.00016505632,0.00018789289,0.00041701517,0.0005847009,0.00025094382,0.00026254077,0.0038991708],"category_scores_gemma":[0.00081094506,0.00018014769,0.00013265203,0.00010656668,0.00048405342,0.00038433712,0.00036361537,0.0005714096,0.0002983075],"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":[0.0024463704,0.00011630631,0.0017687319,0.000063380205,0.000013529655,0.00043705222,0.0003311725,0.0034744528,0.9828136,0.0015463595,0.00034994396,0.006639108],"study_design_scores_gemma":[0.000094578216,0.00082495774,0.021124225,0.000021220992,0.000027981996,0.00015372128,0.00043485986,0.039803848,0.9353933,0.00048113902,0.001589226,0.000051012412],"about_ca_topic_score_codex":0.0012328933,"about_ca_topic_score_gemma":0.0009193838,"teacher_disagreement_score":0.0038991708,"about_ca_system_score_codex":0.0002874065,"about_ca_system_score_gemma":0.00022724998,"threshold_uncertainty_score":0.013044},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.48628205,0.00079617597,0.5053687,0.000108477696,0.00016488192,0.00008365329,0.0005160918,0.0018579589,0.004822004],"genre_scores_gemma":[0.97909456,0.00030265324,0.018669227,0.0000250252,0.00002974209,0.00004005195,0.00024961383,0.00007987158,0.0015093071],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998982,0.000013623098,0.0000108734275,0.000015878937,0.00004238533,0.000019065124],"domain_scores_gemma":[0.9996995,0.0001228792,0.000044246928,0.00001256079,0.00009542235,0.000025402354],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00034867553,0.00060660735,0.0004693372,0.0008213843,0.00027005145,0.0006791445,0.00050240854,0.0005563749,0.000881484],"category_scores_gemma":[0.00095039624,0.00022762643,0.00041941772,0.0006012818,0.00028569196,0.0006457182,0.0003665239,0.0004370627,0.0002437982],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0001982382,0.00009886425,0.011795058,0.00007179711,0.000027046986,0.00027587503,0.000036006135,0.94463074,0.018947456,0.0022811356,0.000513953,0.021123888],"study_design_scores_gemma":[0.000005688095,0.000025384485,0.0012569786,0.0000026094378,0.0000051765014,0.000010211686,0.000004563779,0.99696046,0.0015067977,0.00013630433,0.00008018918,0.0000057189245],"about_ca_topic_score_codex":0.0051023737,"about_ca_topic_score_gemma":0.0025264123,"teacher_disagreement_score":0.0051023737,"about_ca_system_score_codex":0.0003372012,"about_ca_system_score_gemma":0.00059508224,"threshold_uncertainty_score":0.010145307},"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":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.17072302,0.0065745,0.12940174,0.021233477,0.004898656,0.0018268273,0.017901989,0.010412027,0.63702774],"genre_scores_gemma":[0.38879588,0.003147177,0.09633099,0.0012383219,0.00033634473,0.00045718218,0.0070568183,0.001384579,0.50125265],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9945754,0.00037622463,0.00010520588,0.00063238794,0.0038237826,0.00048699806],"domain_scores_gemma":[0.99461055,0.00045064493,0.00013784626,0.00021823565,0.004188772,0.00039390533],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.002402117,0.000535813,0.00061762054,0.0014791158,0.00338125,0.0028294215,0.0013293353,0.0009150765,0.02778173],"category_scores_gemma":[0.0034298631,0.00031975427,0.00026493333,0.00094180804,0.001551508,0.00091070664,0.0013173172,0.0009350507,0.0054003573],"study_design_candidate":"not_applicable","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":[0.0021324316,0.00065453217,0.034000736,0.0009816644,0.00013217644,0.0015213119,0.0050864853,0.007402628,0.1651244,0.040012676,0.25242835,0.4905225],"study_design_scores_gemma":[0.00019265474,0.00050876936,0.032881357,0.00024231424,0.00007141086,0.0005015167,0.0024773884,0.020452617,0.07605561,0.002494057,0.8639851,0.00013726053],"about_ca_topic_score_codex":0.6162055,"about_ca_topic_score_gemma":0.7013407,"teacher_disagreement_score":0.9722183,"about_ca_system_score_codex":0.01148014,"about_ca_system_score_gemma":0.029276555,"threshold_uncertainty_score":0.77210945},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9945233,0.00007433377,0.0044185915,0.00002446615,0.000019201247,0.000007684592,0.000022564998,0.000118214884,0.00079169514],"genre_scores_gemma":[0.99908376,0.000016287999,0.000718405,0.00000660666,0.000002302122,0.0000022714703,0.000017565299,0.000007718387,0.00014518044],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999828,0.00003051394,0.000010740164,0.000022854538,0.000059026697,0.000048946615],"domain_scores_gemma":[0.9994648,0.00022988487,0.00009116976,0.00007219912,0.00008251203,0.000059443548],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002495659,0.00043349862,0.0003503499,0.00029266241,0.00034801487,0.0007141587,0.00030018302,0.00055335695,0.00083954073],"category_scores_gemma":[0.0010632459,0.00018495643,0.00046725987,0.00012724745,0.00052536494,0.00032570245,0.00043039542,0.000349188,0.00016113765],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0012637096,0.0002600022,0.051105443,0.00022399938,0.000089275934,0.0021423209,0.000225854,0.707997,0.20424521,0.00079561974,0.0004507651,0.031200847],"study_design_scores_gemma":[0.00004289835,0.0010570182,0.04453981,0.00004257332,0.000050230603,0.000489336,0.00028973885,0.86861765,0.08391286,0.00024904247,0.0006581838,0.00005074081],"about_ca_topic_score_codex":0.002452763,"about_ca_topic_score_gemma":0.0022793382,"teacher_disagreement_score":0.002452763,"about_ca_system_score_codex":0.00022485243,"about_ca_system_score_gemma":0.0002762087,"threshold_uncertainty_score":0.004877031},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97938603,0.0001589215,0.008901942,0.0001390791,0.000047510013,0.000025878013,0.000112714035,0.00013553434,0.011092319],"genre_scores_gemma":[0.9980831,0.00003756915,0.0011990258,0.000011386334,0.0000056905533,0.0000054471266,0.000021716645,0.000009120967,0.000626918],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99986255,0.000032224696,0.00000776014,0.000019962225,0.0000442333,0.000033296703],"domain_scores_gemma":[0.9986046,0.0009878677,0.00010580065,0.000084355495,0.000142153,0.00007523383],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002944146,0.00032803745,0.00046870657,0.00039190447,0.0005220469,0.000538658,0.0004878471,0.00094429153,0.002813742],"category_scores_gemma":[0.001995607,0.00031236676,0.0003969188,0.00040282012,0.0008447828,0.0004220224,0.00038218807,0.00046061448,0.00017521484],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0004366084,0.00017967123,0.0036136282,0.00009201658,0.000027012633,0.00052179146,0.00007758356,0.95506173,0.03315489,0.0012173615,0.00023566511,0.00538198],"study_design_scores_gemma":[0.00005210623,0.00012329669,0.0023532833,0.000005748954,0.00001079258,0.000051888932,0.000038674454,0.9929047,0.004187121,0.00010812952,0.00015137358,0.000012779755],"about_ca_topic_score_codex":0.0068106954,"about_ca_topic_score_gemma":0.0031832657,"teacher_disagreement_score":0.0068106954,"about_ca_system_score_codex":0.0003791582,"about_ca_system_score_gemma":0.000433417,"threshold_uncertainty_score":0.013542116},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99711716,0.00007113213,0.002280996,0.000027164317,0.000014307778,0.000007721611,0.000029142,0.00003522653,0.00041721482],"genre_scores_gemma":[0.9992151,0.000031531326,0.00048637463,0.00000818887,0.00000483236,0.0000050786193,0.00002891604,0.000005364306,0.00021450585],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.99981743,0.000029389555,0.0000063019293,0.00003682088,0.00007826847,0.000031796542],"domain_scores_gemma":[0.9995085,0.00027341497,0.000043541862,0.0000234326,0.00008427097,0.00006693967],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020498365,0.00031874742,0.0003409789,0.00025811346,0.00022344172,0.000288577,0.00030480677,0.00040505393,0.0006412969],"category_scores_gemma":[0.0008661935,0.00009746387,0.00014459078,0.00012165309,0.0005796747,0.00031926326,0.0003341406,0.00026523916,0.00007506967],"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":[0.0011410818,0.00008433451,0.0026679046,0.00010098304,0.000009589368,0.0003562446,0.00020915492,0.0025238718,0.9852195,0.00014533129,0.00008664268,0.007455335],"study_design_scores_gemma":[0.0002110533,0.004219341,0.16519094,0.00006514102,0.00010223269,0.0015967117,0.0006860149,0.11566524,0.7095581,0.00049079926,0.0020594683,0.00015487621],"about_ca_topic_score_codex":0.00074789755,"about_ca_topic_score_gemma":0.000565938,"teacher_disagreement_score":0.00074789755,"about_ca_system_score_codex":0.00020070578,"about_ca_system_score_gemma":0.00009082457,"threshold_uncertainty_score":0.0021452904},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.012720528,0.0000755884,0.98366976,0.00002573768,0.00004523104,0.000023781478,0.000023908688,0.00016524219,0.003250219],"genre_scores_gemma":[0.74610215,0.0004792882,0.23446949,0.00008134414,0.00011340993,0.00013026292,0.00017919746,0.00023532093,0.01820954],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998671,0.000026672818,0.0000073120746,0.000022781684,0.000059704777,0.000016448514],"domain_scores_gemma":[0.99985075,0.000052028365,0.000019886593,0.000019421695,0.000045749697,0.000012058446],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00029304408,0.0007307115,0.0004553975,0.00042479977,0.00034692948,0.00044922723,0.0012940796,0.0010596315,0.0019436715],"category_scores_gemma":[0.0005784108,0.0003058057,0.0008665745,0.00033340493,0.00029146508,0.0012230951,0.0005768022,0.000642937,0.0006570541],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00012252247,0.000114129136,0.00079023506,0.00008182775,0.000046588848,0.0002771581,0.00011983579,0.8816123,0.03356562,0.039179437,0.0011313099,0.042959187],"study_design_scores_gemma":[0.0000015654488,0.0000065724453,0.00004525642,0.0000017409284,0.0000025074962,0.000011987733,0.0000020593218,0.9978206,0.0011322174,0.0007699393,0.00020275963,0.000002768722],"about_ca_topic_score_codex":0.0017347364,"about_ca_topic_score_gemma":0.0019357116,"teacher_disagreement_score":0.0019436715,"about_ca_system_score_codex":0.00028346063,"about_ca_system_score_gemma":0.00039928258,"threshold_uncertainty_score":0.0065022707},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.96447873,0.00013572976,0.029507801,0.000050367602,0.000036775084,0.00055689673,0.0017851298,0.00072933274,0.0027191958],"genre_scores_gemma":[0.9584094,0.0001637675,0.036613837,0.000021706315,0.000011186995,0.0005705684,0.0026055707,0.00009005509,0.0015138127],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99928504,0.00010855847,0.000062745836,0.00013799958,0.0003086153,0.00009704465],"domain_scores_gemma":[0.99851364,0.00053809566,0.00009478579,0.00031502565,0.00040903006,0.00012953705],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0011578663,0.00084438245,0.0006970865,0.001020616,0.00092849624,0.00039189812,0.0011218159,0.00070543814,0.0034643884],"category_scores_gemma":[0.0020595882,0.00027122986,0.0004079451,0.0008011074,0.00065743306,0.0005044403,0.0006845542,0.0005702393,0.0006753661],"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":[0.002335066,0.008051942,0.04938588,0.0010925407,0.00009170323,0.0013836893,0.00086473866,0.41130105,0.43088713,0.0039645447,0.002994925,0.087646805],"study_design_scores_gemma":[0.00066204363,0.006342673,0.04035422,0.00010081889,0.000081597136,0.0005755189,0.00047840903,0.51339686,0.42978686,0.0012030058,0.006863456,0.00015447027],"about_ca_topic_score_codex":0.0026945397,"about_ca_topic_score_gemma":0.00328883,"teacher_disagreement_score":0.0034643884,"about_ca_system_score_codex":0.00045664987,"about_ca_system_score_gemma":0.00054491113,"threshold_uncertainty_score":0.011589587},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99035865,0.000038565093,0.0067372415,0.000054139124,0.000012179264,0.000028893783,0.00013448209,0.0000944159,0.0025414787],"genre_scores_gemma":[0.99494827,0.000034898127,0.0038602413,0.00001701735,0.0000029964735,0.00003387843,0.00017687154,0.000013875427,0.0009120162],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99994075,0.000011849999,0.0000036269003,0.000008994402,0.000014021532,0.000020794125],"domain_scores_gemma":[0.99972624,0.00013364639,0.000033477845,0.000015750707,0.000041028205,0.00004985079],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00022480334,0.00023662647,0.00038696616,0.00027050366,0.00032968188,0.00062056957,0.00040213545,0.00066596916,0.00089551794],"category_scores_gemma":[0.00058711926,0.00018372116,0.00034003673,0.00028907406,0.00043965786,0.00032514744,0.0002725306,0.00040473972,0.00007800935],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0001474438,0.00013971099,0.0046253195,0.000028506733,0.000018998744,0.0002558015,0.0000957921,0.9829804,0.008455272,0.0012230616,0.00016913077,0.0018606037],"study_design_scores_gemma":[0.000014511048,0.000053102194,0.001278907,0.0000019171114,0.000002466651,0.000008027469,0.000024883562,0.9977043,0.0007138846,0.00011500711,0.00007873686,0.000004223189],"about_ca_topic_score_codex":0.008275029,"about_ca_topic_score_gemma":0.0040675467,"teacher_disagreement_score":0.008275029,"about_ca_system_score_codex":0.000379995,"about_ca_system_score_gemma":0.0006254713,"threshold_uncertainty_score":0.016453743},"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":"other","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.20673946,0.004310402,0.1259708,0.011462859,0.0034541488,0.003623421,0.020939995,0.0105526885,0.61294615],"genre_scores_gemma":[0.24625178,0.0019136912,0.13688277,0.0014062016,0.00045725255,0.0012549575,0.032846212,0.0009352554,0.5780518],"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9989705,0.00017630108,0.000017741704,0.00012349102,0.000532037,0.00017989802],"domain_scores_gemma":[0.99830097,0.00006387675,0.000054955708,0.00013089669,0.0010990183,0.0003502905],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0025263424,0.0010930856,0.00037891683,0.0021276483,0.0012454635,0.00061824534,0.0006853,0.0006023748,0.02719657],"category_scores_gemma":[0.0009560598,0.00017387873,0.0002528599,0.0008026899,0.00032348244,0.00048502054,0.0010283123,0.00082884013,0.008500378],"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":[0.0014561143,0.002084957,0.010346589,0.00020340057,0.000079133846,0.00019713545,0.00042692793,0.00788391,0.05212966,0.027298851,0.27755073,0.62034273],"study_design_scores_gemma":[0.00040034755,0.002770866,0.026342012,0.00008724066,0.00006367402,0.0002348347,0.000185504,0.011966723,0.032455835,0.0028622372,0.92259353,0.000037081623],"about_ca_topic_score_codex":0.0157983,"about_ca_topic_score_gemma":0.020669334,"teacher_disagreement_score":0.02719657,"about_ca_system_score_codex":0.0013647804,"about_ca_system_score_gemma":0.005850842,"threshold_uncertainty_score":0.09098154},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8640654,0.0002163044,0.11890557,0.0001544128,0.00007596127,0.00010913624,0.0004404789,0.0005093558,0.015523426],"genre_scores_gemma":[0.988634,0.000058700996,0.009315351,0.000017286326,0.0000050085064,0.00006267793,0.00009877554,0.000019383691,0.0017888636],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998093,0.000040009243,0.000008848138,0.000030455894,0.00008400662,0.000027441547],"domain_scores_gemma":[0.999668,0.0001687748,0.000029799614,0.000040407333,0.00007127943,0.000021776554],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003308705,0.00038448995,0.0004654098,0.0003193071,0.00032807374,0.0005728468,0.0006696105,0.000763956,0.0014824776],"category_scores_gemma":[0.000692887,0.00013948223,0.00038706654,0.00024730808,0.00048492855,0.00027630277,0.00039129783,0.00034544314,0.0002496411],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0001775015,0.00010261464,0.0017965105,0.000114469665,0.000015628393,0.00022135928,0.00010896314,0.97126746,0.017765477,0.0029518933,0.00031490915,0.0051632514],"study_design_scores_gemma":[0.000009331209,0.00005985741,0.0002509924,0.0000036519905,0.0000023964046,0.0000141260725,0.000013635025,0.99709725,0.0022880933,0.00009750616,0.00015843876,0.0000047044737],"about_ca_topic_score_codex":0.0039116936,"about_ca_topic_score_gemma":0.0015932308,"teacher_disagreement_score":0.0039116936,"about_ca_system_score_codex":0.00042265732,"about_ca_system_score_gemma":0.00052286586,"threshold_uncertainty_score":0.0077778697},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.96733886,0.00014041942,0.011685922,0.0002632289,0.00006188276,0.000038934835,0.000091394526,0.0001735179,0.020205798],"genre_scores_gemma":[0.99756074,0.000021355976,0.00075943256,0.000017760109,0.000005467731,0.000008150137,0.000016775659,0.000016744396,0.0015936466],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999062,0.000018235638,0.000002816702,0.000012392401,0.000029895082,0.000030348692],"domain_scores_gemma":[0.999637,0.00019418812,0.000030288571,0.000021878835,0.000068358815,0.000048199247],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00019220148,0.0002744612,0.00052725244,0.00031192275,0.00070555956,0.0004963604,0.0006049581,0.0006030253,0.0031981373],"category_scores_gemma":[0.00071811565,0.00022404095,0.00039111733,0.00028345143,0.0009238115,0.00041354314,0.00041277942,0.00062349613,0.0002322721],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00027767874,0.00012596515,0.0020377885,0.000043861015,0.000020285413,0.0003381365,0.00010203654,0.9664922,0.022385124,0.0049044634,0.00044458907,0.002827886],"study_design_scores_gemma":[0.0000345197,0.000042857504,0.0006936106,0.0000020084942,0.000003896473,0.00001658869,0.000021523856,0.9955694,0.003132998,0.00030867147,0.00016693202,0.0000070059627],"about_ca_topic_score_codex":0.013424529,"about_ca_topic_score_gemma":0.004457789,"teacher_disagreement_score":0.013424529,"about_ca_system_score_codex":0.0006470951,"about_ca_system_score_gemma":0.00071703625,"threshold_uncertainty_score":0.026692748},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99854565,0.000054787623,0.001179867,0.0000030439323,0.0000046680057,0.00000328992,0.000013836875,0.000015886915,0.00017899032],"genre_scores_gemma":[0.99914587,0.000021008043,0.0006159522,0.000002962661,0.000002811869,0.000002615392,0.000041065512,0.000005765098,0.00016182956],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997254,0.000021577893,0.00001506473,0.000056142802,0.00014050065,0.000041282263],"domain_scores_gemma":[0.99919397,0.00024145936,0.00018434068,0.00006352322,0.00019152062,0.00012508637],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024555414,0.0002148273,0.0004147346,0.00040943554,0.00023352004,0.00058648805,0.00022603145,0.00028822367,0.0007001274],"category_scores_gemma":[0.0009919769,0.00017674817,0.00022771976,0.00030654893,0.0004152667,0.00047973922,0.00033215908,0.0003524846,0.000072826],"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":[0.00058008335,0.000056993274,0.008672476,0.00003782797,0.000010898082,0.0004891372,0.00014743156,0.0017868166,0.9842074,0.00023779561,0.000029362312,0.0037437894],"study_design_scores_gemma":[0.00008452317,0.002517903,0.17848058,0.000018268578,0.00007693178,0.0012043351,0.00056303066,0.057107132,0.7585329,0.00043034874,0.0008960064,0.00008809453],"about_ca_topic_score_codex":0.00026959684,"about_ca_topic_score_gemma":0.00022764747,"teacher_disagreement_score":0.0007001274,"about_ca_system_score_codex":0.00016738137,"about_ca_system_score_gemma":0.000119808145,"threshold_uncertainty_score":0.002342105},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9965264,0.00042300433,0.0017294048,0.000018894692,0.000020495836,0.0000074793084,0.000035846246,0.000035114223,0.001203238],"genre_scores_gemma":[0.99890566,0.00014372432,0.0005956378,0.000009987486,0.000007316722,0.000002979588,0.000037920392,0.000014020221,0.00028278588],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99963427,0.00006379295,0.000031167507,0.00006483884,0.00011965171,0.00008621954],"domain_scores_gemma":[0.9985954,0.0008017253,0.00018457301,0.00010071839,0.00024020938,0.000077440585],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00032283913,0.0003067179,0.000377981,0.00031910013,0.00017627337,0.00044641236,0.00016000436,0.00023454851,0.0006724557],"category_scores_gemma":[0.0015909289,0.00015251478,0.00018249342,0.00019160972,0.0002533522,0.00037063242,0.00016352955,0.00027103443,0.00014216074],"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":[0.0010372866,0.00009521409,0.013222761,0.00012810623,0.000014827847,0.00048656276,0.00014503469,0.0038757573,0.9672569,0.0002465839,0.00009879411,0.013392139],"study_design_scores_gemma":[0.00004302599,0.0018097376,0.09118418,0.00003316905,0.00007090418,0.0005415793,0.000164788,0.015682511,0.88867825,0.00025531434,0.0014663839,0.0000702079],"about_ca_topic_score_codex":0.00018881689,"about_ca_topic_score_gemma":0.00019209356,"teacher_disagreement_score":0.0006724557,"about_ca_system_score_codex":0.00013774681,"about_ca_system_score_gemma":0.00009037893,"threshold_uncertainty_score":0.0022495985},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9945556,0.00025323918,0.0044498234,0.000013847905,0.000037867943,0.000010094993,0.000015931213,0.00004109778,0.0006224929],"genre_scores_gemma":[0.998035,0.00008662976,0.0014757301,0.000007889058,0.000008544239,0.0000060949064,0.000030181372,0.000017828845,0.0003321023],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9995291,0.000056526616,0.00003892472,0.000084523665,0.00020182221,0.00008901294],"domain_scores_gemma":[0.9983937,0.000676762,0.00033673068,0.0001285258,0.00030364766,0.00016065847],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00048050674,0.00037081903,0.0004601223,0.00042325386,0.0002597061,0.00082662574,0.00025481783,0.00028507132,0.00075818616],"category_scores_gemma":[0.0020899363,0.00027303904,0.0003040707,0.00024262209,0.0004570357,0.00059176475,0.00037350564,0.00047304106,0.00011112148],"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":[0.0003297613,0.00003539376,0.0022367574,0.000037199217,0.000006879858,0.00018406249,0.00009138593,0.001227774,0.99200684,0.00022451872,0.000025928359,0.0035934525],"study_design_scores_gemma":[0.000023594243,0.00085115235,0.026370766,0.000010414354,0.000041179122,0.00029591168,0.00011358247,0.02599444,0.9454464,0.00018054924,0.0006209527,0.00005109004],"about_ca_topic_score_codex":0.00021515446,"about_ca_topic_score_gemma":0.00017825652,"teacher_disagreement_score":0.00082662574,"about_ca_system_score_codex":0.0001990269,"about_ca_system_score_gemma":0.00014445698,"threshold_uncertainty_score":0.0025411844},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9981996,0.000026675052,0.0014563473,0.000009429779,0.000009862223,0.000014508356,0.00003640686,0.000026238338,0.00022079467],"genre_scores_gemma":[0.99727076,0.000037835016,0.0021924903,0.000007732329,0.0000039971324,0.000019600038,0.000036512207,0.000005480977,0.00042564477],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998363,0.0000120313925,0.000008229476,0.00003869732,0.00006830167,0.000036362304],"domain_scores_gemma":[0.9997501,0.00006365557,0.000049225815,0.000031656735,0.00006235344,0.000043109816],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002443602,0.00028887624,0.00025312766,0.00015115547,0.00022542407,0.0001731453,0.0004181084,0.0003624147,0.000977579],"category_scores_gemma":[0.00033701237,0.00014618073,0.00020800921,0.00011485023,0.00034640665,0.00023472591,0.00027248668,0.00029755846,0.00010041145],"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":[0.00012942766,0.000066423745,0.0008216369,0.000065949826,0.0000056546933,0.00015263532,0.000073603165,0.00089103205,0.9948723,0.00009392779,0.00004329759,0.0027840224],"study_design_scores_gemma":[0.00011244887,0.004972915,0.024904486,0.000019634721,0.000037795446,0.00026439514,0.00019369462,0.026730433,0.94145525,0.000104311286,0.0011514423,0.000053150783],"about_ca_topic_score_codex":0.00037511517,"about_ca_topic_score_gemma":0.00045775992,"teacher_disagreement_score":0.000977579,"about_ca_system_score_codex":0.00010175385,"about_ca_system_score_gemma":0.00016991372,"threshold_uncertainty_score":0.003270328},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.627405,0.0032903475,0.33490658,0.00081328076,0.00038083363,0.00022352181,0.0011072981,0.0016849696,0.030188171],"genre_scores_gemma":[0.96737057,0.0009929092,0.019308912,0.00006766943,0.000035977093,0.00007143916,0.00062186184,0.00012308879,0.011407555],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99938965,0.00007112529,0.00004296849,0.00011890701,0.00028551556,0.000091734146],"domain_scores_gemma":[0.99945253,0.00019787044,0.00006791296,0.000050604587,0.00020733578,0.000023806862],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0008964365,0.000980238,0.00087415404,0.0010831485,0.0006162945,0.002752339,0.00068132783,0.0010962934,0.007118914],"category_scores_gemma":[0.001544527,0.00041258964,0.0009014077,0.00074701395,0.00053440576,0.0020590855,0.0009280187,0.0009896089,0.001856489],"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":[0.00135296,0.00046372655,0.043424923,0.0017207413,0.0003509609,0.0011158547,0.0015982105,0.36634132,0.17113832,0.013583147,0.006243382,0.3926665],"study_design_scores_gemma":[0.000038697028,0.0005382215,0.050467268,0.00021021451,0.00023822059,0.0006392946,0.002689109,0.8075807,0.10789687,0.0073704636,0.022077724,0.000253187],"about_ca_topic_score_codex":0.0074272337,"about_ca_topic_score_gemma":0.005915259,"teacher_disagreement_score":0.0074272337,"about_ca_system_score_codex":0.0007540527,"about_ca_system_score_gemma":0.0011593916,"threshold_uncertainty_score":0.023815155},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9961429,0.00015595458,0.0029925636,0.000010232292,0.00001844328,0.000012223347,0.00007158325,0.000062288105,0.00053392415],"genre_scores_gemma":[0.99801624,0.0001378822,0.0014003357,0.000012403104,0.000004703177,0.000008873283,0.00010512087,0.000018289127,0.00029613276],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.999691,0.000028840339,0.000024323688,0.000060959697,0.00013761451,0.000057237292],"domain_scores_gemma":[0.99926895,0.00027658112,0.00017398164,0.00006056711,0.00016089258,0.000058905993],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003421905,0.00032203653,0.0003049521,0.00023301785,0.00017217002,0.0008368463,0.00019231696,0.0003503646,0.00091285765],"category_scores_gemma":[0.0011062725,0.00023881684,0.00031290264,0.00026901992,0.00031249126,0.00031302948,0.00020649256,0.00038612285,0.00015041516],"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":[0.00015050266,0.000027213073,0.0036465754,0.000054723565,0.0000062083977,0.00021714608,0.00008779144,0.0030520929,0.98863924,0.00008643852,0.000047695343,0.003984316],"study_design_scores_gemma":[0.000035043406,0.0011962366,0.10770216,0.000022150722,0.000053953794,0.00039804075,0.00023581044,0.032803655,0.85622966,0.00012541833,0.0011133819,0.000084459556],"about_ca_topic_score_codex":0.00052819337,"about_ca_topic_score_gemma":0.00040661535,"teacher_disagreement_score":0.00091285765,"about_ca_system_score_codex":0.00018612972,"about_ca_system_score_gemma":0.00015401699,"threshold_uncertainty_score":0.0030537844},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9989292,0.00014016627,0.0007152977,0.0000050733956,0.0000050580957,0.0000072948496,0.000011590758,0.0000092385335,0.00017704135],"genre_scores_gemma":[0.99859744,0.0000939594,0.0010128077,0.0000085721,0.0000065260765,0.0000061886485,0.000029294126,0.000010716179,0.00023445372],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9994856,0.00009495717,0.000041923748,0.00011545772,0.00016575961,0.000096299955],"domain_scores_gemma":[0.998422,0.00076433155,0.00042720302,0.00010177605,0.00017959258,0.00010509474],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005299286,0.0002944233,0.00037104837,0.00026948584,0.00027030695,0.0007485218,0.0002395829,0.00028347742,0.00080823724],"category_scores_gemma":[0.0016820959,0.0001895818,0.00019702189,0.00016635605,0.00050840556,0.0005033775,0.00034730328,0.000360828,0.000114034265],"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":[0.0007947645,0.00008464929,0.0032974558,0.00005149106,0.0000056994945,0.00016859038,0.0000845665,0.00062853,0.99149656,0.00008171569,0.000012997084,0.0032930623],"study_design_scores_gemma":[0.000052761217,0.0025282514,0.04590091,0.00000904513,0.00003232853,0.00021971852,0.00010297194,0.0044367923,0.9460835,0.000091526286,0.00051162485,0.000030496094],"about_ca_topic_score_codex":0.00026733978,"about_ca_topic_score_gemma":0.00026547493,"teacher_disagreement_score":0.00080823724,"about_ca_system_score_codex":0.00022126085,"about_ca_system_score_gemma":0.000109577944,"threshold_uncertainty_score":0.0028025508},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0062983604,0.000031719956,0.9922671,0.000046102865,0.000045883724,0.0000113783,0.000010923198,0.00010273504,0.0011857903],"genre_scores_gemma":[0.43644357,0.00009987192,0.5549844,0.00015061196,0.00010586552,0.0001197419,0.0000925682,0.00016818523,0.007835252],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999777,0.00007065019,0.000008732787,0.000027893582,0.00009228241,0.000023543203],"domain_scores_gemma":[0.9996438,0.00020421804,0.00002019789,0.000025075364,0.0000772971,0.000029462655],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00052083243,0.00044247528,0.00057897926,0.00029937734,0.0003113781,0.00071445585,0.00085036195,0.00093161425,0.0031617517],"category_scores_gemma":[0.00095412513,0.00034512617,0.00046674104,0.00024584416,0.0006282745,0.0006147109,0.0010187683,0.0012495855,0.00037081903],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00018267745,0.0002480637,0.00025783034,0.00010097109,0.000042764776,0.000086133936,0.00009228959,0.8478733,0.021002099,0.03808244,0.0013063902,0.09072507],"study_design_scores_gemma":[0.0000043207597,0.000010039927,0.000011388844,0.000001176949,0.0000012219499,0.0000031081013,0.000002480231,0.99826115,0.0002904439,0.0012520079,0.00016107068,0.0000016515411],"about_ca_topic_score_codex":0.0013988174,"about_ca_topic_score_gemma":0.0017259142,"teacher_disagreement_score":0.0031617517,"about_ca_system_score_codex":0.00021137203,"about_ca_system_score_gemma":0.00049815135,"threshold_uncertainty_score":0.010577142},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99829215,0.00006296641,0.0014787543,0.0000028707066,0.0000033557478,0.0000029789085,0.000017375794,0.000018186558,0.00012139119],"genre_scores_gemma":[0.9989459,0.000043442673,0.0007877905,0.0000049134064,0.0000025356965,0.0000036293438,0.0000493358,0.000012068255,0.00015037811],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997588,0.000024401223,0.000011512062,0.00005096576,0.0001124567,0.000041817395],"domain_scores_gemma":[0.9991671,0.00041254234,0.00015942873,0.00006318974,0.00013825807,0.000059438935],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003352494,0.00022196322,0.000345204,0.0001820216,0.00015588912,0.00046150907,0.00019245144,0.00016317598,0.00055201445],"category_scores_gemma":[0.001147107,0.0001682156,0.00020802785,0.0002076151,0.0003349239,0.00026792104,0.00022719127,0.00029872102,0.000085418724],"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":[0.00023120952,0.000022858658,0.0018576428,0.000027658898,0.000006483776,0.00014815526,0.000058532172,0.0019904904,0.992157,0.000059766586,0.000012980933,0.003427148],"study_design_scores_gemma":[0.000039841907,0.002188252,0.06471464,0.000010278931,0.00005419176,0.00028550366,0.00018622211,0.040942416,0.8908779,0.00014753047,0.00051088573,0.000042432082],"about_ca_topic_score_codex":0.00042747147,"about_ca_topic_score_gemma":0.00030659424,"teacher_disagreement_score":0.00055201445,"about_ca_system_score_codex":0.00020848495,"about_ca_system_score_gemma":0.00014158958,"threshold_uncertainty_score":0.0018467307},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.85294366,0.0003452722,0.14289829,0.00010571269,0.000038532537,0.0000668952,0.00011455694,0.00044370626,0.0030433512],"genre_scores_gemma":[0.90316087,0.0004322283,0.09438968,0.000058893107,0.00002704492,0.00004271041,0.0001848724,0.000061001905,0.0016426757],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99986243,0.000022096756,0.000004335965,0.000031081287,0.000052320902,0.000027768587],"domain_scores_gemma":[0.9997023,0.00011442081,0.00003847327,0.000030577245,0.000086160064,0.000028024171],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002949068,0.0005417224,0.00028855115,0.0007504026,0.00022934396,0.00037679283,0.00023539513,0.00034488493,0.0010057756],"category_scores_gemma":[0.0007511467,0.00016237758,0.00022044424,0.00028880793,0.0004228425,0.0005495918,0.0006431843,0.0002368524,0.0002404092],"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":[0.00045923234,0.00010012178,0.003771533,0.00013765944,0.000033502423,0.00055077695,0.00047178837,0.011607287,0.8937978,0.0007244347,0.0003022498,0.08804365],"study_design_scores_gemma":[0.000043897347,0.0013232321,0.041461818,0.00005936887,0.00008849783,0.0016755072,0.00059687154,0.11392558,0.83469385,0.001208741,0.004845359,0.0000773972],"about_ca_topic_score_codex":0.0012082297,"about_ca_topic_score_gemma":0.002586045,"teacher_disagreement_score":0.0012082297,"about_ca_system_score_codex":0.00016494823,"about_ca_system_score_gemma":0.00033334806,"threshold_uncertainty_score":0.0033646226},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9354825,0.00033000874,0.0626636,0.000077155695,0.000028422568,0.000032936245,0.000061732324,0.00025146044,0.0010722898],"genre_scores_gemma":[0.9731627,0.00008845632,0.026484735,0.0000133955855,0.000019024174,0.00001222956,0.000040256433,0.000011515065,0.00016762703],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9996587,0.000076138975,0.000011908652,0.000062870124,0.00016092694,0.000029512279],"domain_scores_gemma":[0.9994306,0.00023927007,0.00009580122,0.000063318985,0.00014697375,0.000024027584],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00064818206,0.00031377914,0.00022497425,0.0005043165,0.00018552535,0.00024027031,0.00035422895,0.00025695915,0.00018752526],"category_scores_gemma":[0.0011208972,0.00013400729,0.00012843135,0.0002957805,0.00030081073,0.00033399032,0.0001970775,0.00022802112,0.000059151993],"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":[0.000159541,0.00004147252,0.007941678,0.00003394962,0.000008888779,0.00008498846,0.00010226714,0.0011327819,0.9706683,0.00053140515,0.00009158463,0.019203095],"study_design_scores_gemma":[0.000036453675,0.0004890625,0.03893595,0.000007486406,0.00003656056,0.00044841977,0.000069176465,0.07269895,0.8857828,0.00041593213,0.0010137622,0.000065527194],"about_ca_topic_score_codex":0.00054306496,"about_ca_topic_score_gemma":0.00061134587,"teacher_disagreement_score":0.00064818206,"about_ca_system_score_codex":0.00029308657,"about_ca_system_score_gemma":0.00016953438,"threshold_uncertainty_score":0.0034279823},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.021265276,0.000120569195,0.97565836,0.0001021859,0.00006410261,0.000052877418,0.000048414608,0.0003736308,0.00231468],"genre_scores_gemma":[0.24566981,0.00055227976,0.7436357,0.00012127258,0.000052247895,0.00015880649,0.00016240387,0.00027964445,0.009367787],"study_design_codex":"bench_or_experimental","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.9997758,0.00005423186,0.0000146691245,0.000018245646,0.000121424324,0.000015624139],"domain_scores_gemma":[0.99945945,0.00026270965,0.000076888,0.000093805924,0.00009041753,0.00001672422],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00046647686,0.0007566718,0.00036891305,0.00037278692,0.00022422902,0.00064414064,0.00039693317,0.00059839926,0.0026748066],"category_scores_gemma":[0.0011162896,0.00022692197,0.00044545488,0.0003871728,0.0006792189,0.0012423345,0.00052215665,0.000745296,0.000645648],"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":[0.0003893259,0.0003139772,0.0013406967,0.00067916315,0.000055829638,0.0006827821,0.0004966616,0.14985926,0.4664568,0.13757634,0.0032759602,0.23887321],"study_design_scores_gemma":[0.000035142883,0.00013062781,0.00060700235,0.000039035338,0.000020880985,0.00047047855,0.000102442296,0.8048285,0.17942265,0.0076440023,0.0066479957,0.00005117098],"about_ca_topic_score_codex":0.00051335327,"about_ca_topic_score_gemma":0.0008267353,"teacher_disagreement_score":0.0026748066,"about_ca_system_score_codex":0.00039837105,"about_ca_system_score_gemma":0.00073946477,"threshold_uncertainty_score":0.008948147},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.926997,0.00038911696,0.062299907,0.0001586751,0.00005723187,0.00004789597,0.00016950372,0.0002165058,0.009664116],"genre_scores_gemma":[0.9947253,0.0001303479,0.0037104553,0.000013151055,0.000008225789,0.000025207788,0.00005922353,0.000012005914,0.001316081],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998839,0.00002010146,0.000008987204,0.00001585246,0.00003801071,0.000033209664],"domain_scores_gemma":[0.99975795,0.0000846082,0.000063397856,0.000014453221,0.00005160294,0.000028008924],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023717465,0.0004899421,0.00039881314,0.00044374733,0.00045058652,0.00072709046,0.00048543944,0.0006304687,0.0008380229],"category_scores_gemma":[0.0007147684,0.00018591547,0.00040543522,0.00038885025,0.00058644084,0.00030954776,0.00060415,0.00023831462,0.0001239336],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00011306831,0.0000523774,0.0029972966,0.00006264648,0.000015243985,0.00038332862,0.0000904054,0.95211995,0.037233252,0.0021178676,0.00012698471,0.0046876734],"study_design_scores_gemma":[0.00000551693,0.000030880175,0.00059482985,0.0000035088378,0.0000030383553,0.000016705348,0.000017313423,0.9979431,0.0011519376,0.00011703955,0.00011124165,0.000004802219],"about_ca_topic_score_codex":0.010950122,"about_ca_topic_score_gemma":0.0040634726,"teacher_disagreement_score":0.010950122,"about_ca_system_score_codex":0.00059169036,"about_ca_system_score_gemma":0.00060884486,"threshold_uncertainty_score":0.021772742},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0031746803,0.00007243176,0.9956844,0.00004557731,0.000012882597,0.000020439593,0.000017559405,0.00016069398,0.000811405],"genre_scores_gemma":[0.30265576,0.000401159,0.6934988,0.00007542962,0.000056913483,0.00034249065,0.00018399076,0.00017818868,0.0026072268],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997904,0.000074419426,0.000009458996,0.00002738994,0.00008296175,0.000015499952],"domain_scores_gemma":[0.9992956,0.00047042084,0.000048326914,0.000036894115,0.00012431356,0.000024380057],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00048726387,0.0008360676,0.00044891174,0.00045435037,0.00034462017,0.00043976682,0.00044590223,0.0004913262,0.002225961],"category_scores_gemma":[0.0020644425,0.00034035862,0.00032976453,0.00029567396,0.00056362647,0.00062073075,0.000675053,0.0006508348,0.00072681095],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00009908781,0.000037679856,0.0004995802,0.00013383139,0.000028027953,0.00008512335,0.00009195149,0.8336094,0.030052302,0.016124284,0.0009818547,0.11825694],"study_design_scores_gemma":[0.0000051520187,0.00001552452,0.00008750755,0.00000727832,0.0000022931556,0.000012948691,0.000011106911,0.99416804,0.002031297,0.002962024,0.0006911339,0.0000057128022],"about_ca_topic_score_codex":0.002626655,"about_ca_topic_score_gemma":0.0027117713,"teacher_disagreement_score":0.002626655,"about_ca_system_score_codex":0.0002912337,"about_ca_system_score_gemma":0.0006965486,"threshold_uncertainty_score":0.007446587},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.87642527,0.00034201777,0.11917218,0.00007301871,0.00008911602,0.000039629682,0.000049396753,0.00022606847,0.0035832508],"genre_scores_gemma":[0.9937723,0.000074124015,0.0052759666,0.000012992337,0.000012932531,0.000015282194,0.000016384134,0.0000102898875,0.00080966693],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999012,0.000012308114,0.000004780603,0.000025932204,0.000029760326,0.000025949843],"domain_scores_gemma":[0.99980265,0.000059181504,0.000050362956,0.000022916422,0.00003898713,0.00002583903],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00014393067,0.00045524622,0.00030379224,0.00013280808,0.00017250229,0.00038064364,0.00027902465,0.00020961631,0.00058308005],"category_scores_gemma":[0.00029292147,0.000105435,0.00017049782,0.000052395073,0.00033846276,0.00024480958,0.000430857,0.00022086818,0.00011596411],"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":[0.0001534047,0.00005030309,0.0006813733,0.00007515594,0.0000086690325,0.00009193154,0.00004359547,0.015171649,0.9684116,0.0008547265,0.00010602347,0.0143516185],"study_design_scores_gemma":[0.00007890857,0.0014466255,0.007303643,0.000020637188,0.000043686967,0.00014370475,0.00007265849,0.5093113,0.47586873,0.00091793475,0.004741722,0.000050449347],"about_ca_topic_score_codex":0.0005990275,"about_ca_topic_score_gemma":0.0006611014,"teacher_disagreement_score":0.0005990275,"about_ca_system_score_codex":0.00014507512,"about_ca_system_score_gemma":0.00026152897,"threshold_uncertainty_score":0.0019506216},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9981698,0.000054910768,0.0014558296,0.000016177117,0.000007412431,0.000010890799,0.00001735932,0.00003268921,0.0002349022],"genre_scores_gemma":[0.9978891,0.00005241612,0.0015259846,0.000018925508,0.000007064235,0.000020662043,0.000049460738,0.000011139705,0.0004253175],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997341,0.000035739537,0.000010215633,0.000047395715,0.000098148994,0.000074331896],"domain_scores_gemma":[0.9995946,0.00017740122,0.000074115065,0.000022619257,0.00006856517,0.00006278623],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021337446,0.00034989414,0.0004633556,0.00017514967,0.0003235916,0.0003233736,0.00034916005,0.00036439288,0.0010000484],"category_scores_gemma":[0.0005442088,0.00014656511,0.00017144546,0.000081724495,0.00045605956,0.00028578512,0.0005817597,0.0003933003,0.00013155738],"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":[0.00022980582,0.00004764383,0.00068240456,0.000040946634,0.0000032742767,0.0001974441,0.00007877916,0.0004988464,0.9963637,0.000056360932,0.000028968743,0.0017718441],"study_design_scores_gemma":[0.000035260287,0.0014398425,0.013083119,0.000011391101,0.000013664017,0.00020259511,0.00012651614,0.016090041,0.9684775,0.000042769767,0.00045593642,0.000021534805],"about_ca_topic_score_codex":0.000886705,"about_ca_topic_score_gemma":0.00073877274,"teacher_disagreement_score":0.0010000484,"about_ca_system_score_codex":0.00030097595,"about_ca_system_score_gemma":0.00014161943,"threshold_uncertainty_score":0.0033454895},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99857664,0.00003538919,0.0010300319,0.000006063107,0.0000012223978,0.0000016497705,0.00003760426,0.00002394534,0.00028752926],"genre_scores_gemma":[0.999353,0.000029964061,0.00044171375,0.0000018857994,0.0000016387374,0.000003898671,0.00004995208,0.000005058254,0.00011280066],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99990606,0.000009357834,0.0000066785515,0.000030921507,0.000026659107,0.000020271453],"domain_scores_gemma":[0.9997557,0.00008972799,0.000066852095,0.00002245004,0.000026167352,0.000039096027],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001523475,0.00031054122,0.00027140163,0.0003222933,0.00020534162,0.00046484047,0.0002193318,0.00015483526,0.0004630366],"category_scores_gemma":[0.00035484595,0.00018152884,0.00016124923,0.00017414852,0.00049402134,0.0003456652,0.00027380337,0.000188549,0.000076999626],"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":[0.00065128325,0.00006859155,0.010247385,0.000041140232,0.000035863515,0.00026846127,0.00014630714,0.040584933,0.9409205,0.0013756901,0.00006422874,0.0055955867],"study_design_scores_gemma":[0.00008768418,0.0012092451,0.19380929,0.000017574841,0.00011303098,0.00037535193,0.00020985532,0.38865486,0.41389152,0.0010866784,0.0004282424,0.00011662867],"about_ca_topic_score_codex":0.001085362,"about_ca_topic_score_gemma":0.0006120542,"teacher_disagreement_score":0.001085362,"about_ca_system_score_codex":0.00025172575,"about_ca_system_score_gemma":0.00016700098,"threshold_uncertainty_score":0.0021580458},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99899167,0.000037934653,0.0007417003,0.00000719018,0.000001626124,0.0000014190829,0.00001982756,0.000014757795,0.00018371583],"genre_scores_gemma":[0.9996557,0.000009176841,0.00011771487,0.0000014761316,8.2872054e-7,0.0000011862296,0.00002779795,0.0000075574158,0.00017857346],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999032,0.000010880993,0.0000060352086,0.00002417551,0.000021223039,0.000034481192],"domain_scores_gemma":[0.99824286,0.0008959431,0.0003026807,0.00013553732,0.00024283185,0.00018006003],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00037768995,0.00012535592,0.00026851895,0.0004986915,0.00030269392,0.0007817899,0.00035860343,0.00031872772,0.0010936904],"category_scores_gemma":[0.0039716945,0.00020608482,0.00017101572,0.00028023636,0.0005935721,0.0005917013,0.00042008198,0.00036237718,0.00014061118],"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":[0.015351677,0.0006409135,0.2680851,0.00012369287,0.00010020957,0.0011631156,0.0020313195,0.10139948,0.54016244,0.0070205578,0.000875776,0.06304577],"study_design_scores_gemma":[0.000082930506,0.00049153564,0.38239855,0.00001437912,0.00003286752,0.0004104573,0.0006090396,0.5374431,0.07680727,0.001273682,0.00035012612,0.0000860371],"about_ca_topic_score_codex":0.006468391,"about_ca_topic_score_gemma":0.0030391393,"teacher_disagreement_score":0.006468391,"about_ca_system_score_codex":0.000569881,"about_ca_system_score_gemma":0.00027920614,"threshold_uncertainty_score":0.01286149},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97949743,0.00038580463,0.013896777,0.00037149256,0.00024582277,0.000045301233,0.0004055132,0.00046789175,0.0046839626],"genre_scores_gemma":[0.9927953,0.0001179881,0.005463835,0.00007098896,0.000077039855,0.00002246002,0.0001253311,0.000043266493,0.0012837534],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99976605,0.00001859933,0.000005443671,0.000043252003,0.00012038725,0.000046206555],"domain_scores_gemma":[0.999684,0.00009031114,0.00004635432,0.000037731897,0.000080701095,0.000060971826],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015875803,0.0004091267,0.00036481902,0.00048242853,0.0005519631,0.00050908956,0.0006649791,0.0009877426,0.002132282],"category_scores_gemma":[0.00052405783,0.00024558854,0.00015026449,0.00025539694,0.00048169887,0.00091172504,0.00055776286,0.0009736389,0.00034086793],"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":[0.00029393483,0.00007845886,0.0014842489,0.00004346443,0.000007797419,0.00030301698,0.00012989207,0.0002385454,0.99128175,0.00017476022,0.0005010009,0.005463119],"study_design_scores_gemma":[0.000104780884,0.0008288297,0.040866267,0.000020923744,0.000025388263,0.00095167954,0.00033685984,0.018266855,0.9346482,0.0003040944,0.0035789842,0.00006713181],"about_ca_topic_score_codex":0.00045825238,"about_ca_topic_score_gemma":0.0006999796,"teacher_disagreement_score":0.002132282,"about_ca_system_score_codex":0.00017002587,"about_ca_system_score_gemma":0.00015569765,"threshold_uncertainty_score":0.0071332455},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9946813,0.0000813395,0.003606381,0.00004401655,0.000023776329,0.000028328004,0.00028098965,0.00011643504,0.0011374162],"genre_scores_gemma":[0.99530894,0.00006578344,0.0038482002,0.000014749273,0.000012325406,0.000030399351,0.0002898936,0.000019449759,0.00041024803],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997003,0.00003305173,0.000024927542,0.000073181065,0.000099312056,0.000069355716],"domain_scores_gemma":[0.9994211,0.00023989614,0.000055470136,0.000102032114,0.00011143127,0.000070056594],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004551202,0.0003642951,0.0004609138,0.00046563923,0.00075377256,0.000470802,0.00044864326,0.00059274666,0.0016807193],"category_scores_gemma":[0.0006201497,0.00015257705,0.00026207487,0.00051971193,0.0007215999,0.0004537682,0.0005474315,0.00079628173,0.00015481503],"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":[0.0007258504,0.0013181978,0.012247892,0.00018491162,0.000033040902,0.0010360259,0.00048793422,0.04240976,0.92630357,0.001808387,0.0007738082,0.012670724],"study_design_scores_gemma":[0.0003301355,0.0039110705,0.10133002,0.000046690202,0.000060263705,0.0006990749,0.00055022637,0.32563144,0.5629284,0.0010336722,0.0032889347,0.00019007683],"about_ca_topic_score_codex":0.001213296,"about_ca_topic_score_gemma":0.000923852,"teacher_disagreement_score":0.0016807193,"about_ca_system_score_codex":0.00023436005,"about_ca_system_score_gemma":0.0003044388,"threshold_uncertainty_score":0.0056226254},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9952767,0.00015349512,0.0041313856,0.000011175812,0.0000069753337,0.000013336299,0.00007148186,0.000028488239,0.00030697076],"genre_scores_gemma":[0.9987909,0.00005918497,0.00091461313,0.0000062266913,0.0000042940515,0.000007684473,0.000074666124,0.000011564863,0.00013084857],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994887,0.00004940895,0.00003869379,0.00012024808,0.0002176554,0.00008520825],"domain_scores_gemma":[0.9977417,0.0010893835,0.0004777299,0.00012191635,0.00041880965,0.00015039163],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0007015253,0.00017650431,0.0003102163,0.0004456311,0.00022598232,0.000652796,0.0001975533,0.00020582521,0.00051107735],"category_scores_gemma":[0.0026809166,0.00015120563,0.00019335783,0.00030181618,0.00048703913,0.00036139434,0.00023417934,0.0003867152,0.00009210476],"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":[0.0003032556,0.00005246359,0.010806767,0.000057486934,0.000010289094,0.00017616435,0.00014480774,0.0034057659,0.9775344,0.00028483552,0.000055235476,0.0071685193],"study_design_scores_gemma":[0.000026440102,0.0011751864,0.17947781,0.0000147131595,0.00004012892,0.00031093968,0.00022389225,0.04166243,0.7758932,0.00040082008,0.0006951659,0.00007924346],"about_ca_topic_score_codex":0.0004682303,"about_ca_topic_score_gemma":0.00037392214,"teacher_disagreement_score":0.0007015253,"about_ca_system_score_codex":0.0002693903,"about_ca_system_score_gemma":0.0001580537,"threshold_uncertainty_score":0.003710091},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97311664,0.00010194342,0.014839083,0.00009297026,0.0000419556,0.00005774681,0.00028213268,0.00017611487,0.011291438],"genre_scores_gemma":[0.9951656,0.000027728302,0.0036129123,0.000017146174,0.000004040025,0.000043022108,0.000111789836,0.000011919631,0.0010058322],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998627,0.000023493049,0.0000066448583,0.000018371766,0.000047193866,0.000041624542],"domain_scores_gemma":[0.99956113,0.0001750472,0.000047601396,0.000044005454,0.000111924164,0.00006032463],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00019742092,0.00037351032,0.0005518613,0.00041888992,0.00042402578,0.0005873554,0.0008372982,0.0008245984,0.0017447303],"category_scores_gemma":[0.0010876921,0.00014133385,0.00035674797,0.00033253452,0.000617932,0.0002543695,0.0005644877,0.0005126433,0.00012402331],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00019685259,0.00015628114,0.0038983675,0.00008230451,0.000018592173,0.00033717713,0.00013346976,0.9809754,0.007824362,0.0029817633,0.00027957273,0.003115806],"study_design_scores_gemma":[0.000020554126,0.000045061068,0.0006697082,0.0000044928584,0.0000026479286,0.00001908588,0.000026155214,0.99754757,0.00131522,0.00017679327,0.00016815297,0.0000045584866],"about_ca_topic_score_codex":0.010779023,"about_ca_topic_score_gemma":0.0037835247,"teacher_disagreement_score":0.010779023,"about_ca_system_score_codex":0.000633209,"about_ca_system_score_gemma":0.0005916001,"threshold_uncertainty_score":0.021432579},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9857529,0.00013113626,0.012571086,0.000021259235,0.00003213844,0.000046828944,0.00012027464,0.00014250042,0.0011818934],"genre_scores_gemma":[0.99656385,0.00007347688,0.0021810464,0.000013661589,0.000009069087,0.000028899665,0.00008855408,0.000027795822,0.0010137378],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9993554,0.000085437816,0.000034607878,0.00016287403,0.00025063765,0.00011112776],"domain_scores_gemma":[0.9988649,0.00045384842,0.000095071664,0.00019421939,0.0002790522,0.00011295026],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00057395815,0.0004037343,0.00052249094,0.00035736937,0.00035222684,0.00045225074,0.00055245525,0.00078562327,0.00238535],"category_scores_gemma":[0.0014756669,0.00016017364,0.00029597347,0.00021484963,0.00051457906,0.0004823437,0.0006055705,0.00055305054,0.00036602994],"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":[0.0006457644,0.00023298943,0.0020396628,0.00016017132,0.000017512713,0.00030309378,0.00030950358,0.0030887774,0.9850072,0.00027863652,0.00008130693,0.007835267],"study_design_scores_gemma":[0.00007632213,0.008150409,0.016370073,0.00004335474,0.000048929527,0.00046420342,0.0003911,0.018767772,0.95320755,0.0002838479,0.0021397758,0.000056504596],"about_ca_topic_score_codex":0.00021658516,"about_ca_topic_score_gemma":0.00017064191,"teacher_disagreement_score":0.00238535,"about_ca_system_score_codex":0.00015839197,"about_ca_system_score_gemma":0.000115438634,"threshold_uncertainty_score":0.00797981},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9793722,0.000112878006,0.01663676,0.00006446984,0.00003619915,0.000086040935,0.00011060324,0.00010024939,0.003480573],"genre_scores_gemma":[0.9923653,0.00005273694,0.0053792507,0.000009369159,0.0000072549306,0.000021736321,0.000040339335,0.000013641463,0.002110332],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999485,0.00008231941,0.000027029913,0.00006244401,0.0002868838,0.000056252287],"domain_scores_gemma":[0.99857116,0.00077638397,0.0001176097,0.00018349549,0.00024989512,0.00010141453],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00061497756,0.00031051575,0.0005689169,0.0003188976,0.0006573037,0.0006244208,0.0007070795,0.0007836683,0.002904645],"category_scores_gemma":[0.0017666313,0.00030243373,0.0003353976,0.00038682026,0.0011624593,0.000617798,0.0006103139,0.0005439143,0.00041869152],"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":[0.0011291527,0.00027911254,0.0031603582,0.00017030044,0.000010341806,0.00024948842,0.00033984534,0.009892785,0.9754514,0.0011088554,0.00015540213,0.008053021],"study_design_scores_gemma":[0.00023911538,0.0032901783,0.023612034,0.00002645823,0.000035715024,0.000440992,0.00027614424,0.11009507,0.85910314,0.0006215121,0.002184307,0.00007519179],"about_ca_topic_score_codex":0.0010060938,"about_ca_topic_score_gemma":0.0010617272,"teacher_disagreement_score":0.002904645,"about_ca_system_score_codex":0.0004469674,"about_ca_system_score_gemma":0.00041856695,"threshold_uncertainty_score":0.009717047},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.40982598,0.007216189,0.5710701,0.00037759228,0.00074805925,0.00022973375,0.0012380539,0.0048859296,0.0044083293],"genre_scores_gemma":[0.82340515,0.0018266505,0.1688196,0.00013956868,0.00027079583,0.00021296137,0.0022856086,0.00044622677,0.0025934186],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9988551,0.00027862084,0.00012131528,0.00020453973,0.00043911074,0.00010122515],"domain_scores_gemma":[0.9946008,0.0031206235,0.00026874352,0.0003422649,0.001508635,0.00015888004],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0026747442,0.0017967547,0.0012621364,0.002074934,0.0008689231,0.0011964571,0.001789113,0.0018384018,0.0014932296],"category_scores_gemma":[0.0051549627,0.00037284291,0.0011767453,0.0012440082,0.00040589576,0.0011153808,0.000993228,0.0010016479,0.00057048694],"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":[0.0024816354,0.0011510383,0.016918274,0.00085246447,0.0010502341,0.00014593589,0.00021556226,0.47396657,0.014352144,0.0018247626,0.0025830201,0.4844584],"study_design_scores_gemma":[0.000056822526,0.00020572504,0.00315605,0.00001722937,0.000059644524,0.000024413648,0.000033029584,0.9926191,0.0032285189,0.00019855872,0.00037863784,0.000022323607],"about_ca_topic_score_codex":0.013786864,"about_ca_topic_score_gemma":0.010385123,"teacher_disagreement_score":0.013786864,"about_ca_system_score_codex":0.00050330703,"about_ca_system_score_gemma":0.0010590955,"threshold_uncertainty_score":0.02741319},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9972893,0.000039949908,0.0012600917,0.000009019293,0.000013280243,0.000010565097,0.00025076675,0.000047285583,0.0010796773],"genre_scores_gemma":[0.998686,0.000033323082,0.00071670726,0.000007931874,0.0000035755718,0.000006365483,0.00022226038,0.0000082498345,0.00031559126],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99977714,0.000012186805,0.000010612584,0.0000490888,0.000075216,0.000075752665],"domain_scores_gemma":[0.9995567,0.000111639674,0.00006570573,0.000031027663,0.00013261738,0.000102302416],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016586663,0.00030819964,0.00038813215,0.0006647805,0.0005652326,0.000588503,0.00023995507,0.0004888838,0.0009927455],"category_scores_gemma":[0.0005411493,0.00021269257,0.00024967585,0.0004264338,0.00050115946,0.00030860567,0.00044184134,0.00039633503,0.00018786333],"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":[0.0025108238,0.0002158579,0.036263578,0.00008553697,0.000053839765,0.00053090084,0.00063026097,0.0030532079,0.94337964,0.000366013,0.00033028857,0.012580085],"study_design_scores_gemma":[0.00009244243,0.001355893,0.61954236,0.00002392337,0.00009211577,0.0006160311,0.0009001401,0.010768254,0.36514786,0.00023471471,0.001123293,0.00010305139],"about_ca_topic_score_codex":0.002017385,"about_ca_topic_score_gemma":0.002943192,"teacher_disagreement_score":0.002017385,"about_ca_system_score_codex":0.0001900723,"about_ca_system_score_gemma":0.00025516888,"threshold_uncertainty_score":0.0040112734},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.5755181,0.00007326173,0.41700935,0.00021199934,0.000050605362,0.000030286044,0.00012683844,0.00046136839,0.006518237],"genre_scores_gemma":[0.98925936,0.000010494272,0.010102436,0.000013875101,0.00000836287,0.0000056222266,0.00007423736,0.000022885426,0.0005027086],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991872,0.00017078065,0.00002981899,0.00016737732,0.00033473794,0.00011023115],"domain_scores_gemma":[0.99651176,0.0015799013,0.00037393442,0.00034209952,0.0010161335,0.00017607743],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0012554342,0.0004757418,0.00045448568,0.00063858525,0.0004999228,0.001049687,0.00079763547,0.0010267411,0.0014866451],"category_scores_gemma":[0.007884017,0.00028606507,0.000286631,0.00025896015,0.0006205997,0.0011359985,0.000801312,0.0005828856,0.0004984668],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00021816003,0.00013825104,0.018962702,0.000037998452,0.000019811281,0.00017487956,0.00006435595,0.9181243,0.013610604,0.0037921234,0.000778736,0.044078104],"study_design_scores_gemma":[0.0000023577577,0.00002054149,0.0023951954,0.0000035040177,0.0000017848502,0.000012983458,0.000009212226,0.9956488,0.0013532796,0.00049521076,0.000052351937,0.0000046884693],"about_ca_topic_score_codex":0.005318382,"about_ca_topic_score_gemma":0.0045825914,"teacher_disagreement_score":0.005318382,"about_ca_system_score_codex":0.00034795664,"about_ca_system_score_gemma":0.0008109385,"threshold_uncertainty_score":0.010574818},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9036071,0.00013902273,0.08195306,0.00020349739,0.00007342125,0.00008958997,0.00047536474,0.0005381107,0.012920861],"genre_scores_gemma":[0.9843211,0.00004680157,0.013468315,0.000029329629,0.000006830671,0.000080213606,0.00018947931,0.000040549374,0.0018173568],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999019,0.000019172589,0.0000037008801,0.000012015464,0.00003762785,0.000025601446],"domain_scores_gemma":[0.99965847,0.00016486892,0.000036782527,0.000024815874,0.000063145984,0.000051892064],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020001002,0.0003871571,0.0005237467,0.00026176646,0.00034464613,0.000507268,0.0007254788,0.00083367026,0.0018932329],"category_scores_gemma":[0.00061143003,0.00019125197,0.00036804433,0.00023504505,0.00047308055,0.0002523777,0.00038244828,0.00053735886,0.00017226905],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00007711858,0.00006206784,0.0012064883,0.00003818874,0.000013613446,0.00008306038,0.000039296356,0.98777676,0.0075659878,0.0015025819,0.00014019092,0.0014946935],"study_design_scores_gemma":[0.000011907147,0.000016115655,0.00013963274,0.000001593192,0.0000013484006,0.000005031073,0.000005662023,0.998895,0.00074303907,0.00009632266,0.00008189515,0.0000026055725],"about_ca_topic_score_codex":0.0130152395,"about_ca_topic_score_gemma":0.0045238407,"teacher_disagreement_score":0.0130152395,"about_ca_system_score_codex":0.00049106305,"about_ca_system_score_gemma":0.00077665073,"threshold_uncertainty_score":0.025878966},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.018729702,0.00009892988,0.95952654,0.00014279025,0.000118896685,0.00007948777,0.00023824204,0.0014650809,0.019600255],"genre_scores_gemma":[0.34411737,0.0002409583,0.61043096,0.00011071029,0.00013585118,0.00017093137,0.0006338835,0.0007346858,0.043424625],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998005,0.000024605972,0.000010659807,0.00002583858,0.000120653225,0.000017830465],"domain_scores_gemma":[0.9994754,0.00023860014,0.000029819288,0.00007449332,0.00015761319,0.000024061499],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00039146608,0.0004619494,0.00032655345,0.00052710896,0.0005285275,0.0011201366,0.0008778479,0.0009607573,0.023074895],"category_scores_gemma":[0.0012241167,0.0003187216,0.00038032787,0.00028303883,0.00046708956,0.0007348862,0.0009993188,0.00085919205,0.004207703],"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":[0.00025236097,0.0003014965,0.00315574,0.00077059394,0.000077632416,0.0009669788,0.00038113983,0.2849993,0.23371524,0.023752501,0.012901319,0.43872574],"study_design_scores_gemma":[0.000026739828,0.000054578282,0.0011859043,0.000022301601,0.000008825801,0.00026000474,0.00007428432,0.94220674,0.032559197,0.0025868744,0.02098957,0.00002502792],"about_ca_topic_score_codex":0.0015551939,"about_ca_topic_score_gemma":0.0026097316,"teacher_disagreement_score":0.023074895,"about_ca_system_score_codex":0.0002363951,"about_ca_system_score_gemma":0.0005259028,"threshold_uncertainty_score":0.0771932},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97812736,0.00032466007,0.019583879,0.00012730663,0.0001007505,0.000015711003,0.00002317418,0.00023313136,0.0014640837],"genre_scores_gemma":[0.995083,0.00011866341,0.002928835,0.000042879277,0.000036558486,0.000009578962,0.000027650638,0.000028936363,0.0017239964],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997168,0.00005000526,0.000016970911,0.000073590854,0.000087830456,0.00005486381],"domain_scores_gemma":[0.9995498,0.00017856288,0.00007846094,0.000043939704,0.00009956499,0.000049679315],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003501816,0.00030732495,0.00055071845,0.00025510878,0.0004914503,0.00039998695,0.0005565929,0.00070144807,0.0011809646],"category_scores_gemma":[0.00050592655,0.00024582937,0.00033593588,0.00016808091,0.0003201444,0.000447107,0.00045666142,0.00027444813,0.00029277406],"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":[0.0009664185,0.000096772994,0.0013653826,0.000074938434,0.000017960301,0.00048634098,0.00015641512,0.00090184156,0.98514694,0.00023069019,0.00022934374,0.010326953],"study_design_scores_gemma":[0.00012055325,0.002280565,0.014676817,0.000018235132,0.00014643688,0.00044929626,0.00017390274,0.032930873,0.94615686,0.00012482362,0.0028660137,0.000055619505],"about_ca_topic_score_codex":0.0004163738,"about_ca_topic_score_gemma":0.00046052516,"teacher_disagreement_score":0.0011809646,"about_ca_system_score_codex":0.00025808613,"about_ca_system_score_gemma":0.00017656406,"threshold_uncertainty_score":0.0039507747},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99613875,0.000052294294,0.0029069793,0.000046175657,0.000017686418,0.000013370132,0.000070482434,0.00007174301,0.00068247144],"genre_scores_gemma":[0.99822134,0.000037222584,0.00080494385,0.00002664629,0.000016589804,0.000007904667,0.0001359209,0.000029875177,0.00071956933],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9994149,0.00010058988,0.000021977607,0.00016440236,0.00018221822,0.00011601432],"domain_scores_gemma":[0.99901617,0.00051293743,0.000064937434,0.000073159375,0.0001803995,0.00015233741],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00074725744,0.00045481295,0.00066729187,0.00038377658,0.0008038867,0.0005267958,0.00077262364,0.00096434227,0.0013194015],"category_scores_gemma":[0.0010464096,0.00028082557,0.00047483027,0.00028251632,0.0005598865,0.00077279663,0.00065246574,0.00057068816,0.00022046297],"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":[0.0022364329,0.00021230432,0.010460973,0.000058006575,0.000058943817,0.0005954177,0.000573052,0.0016093226,0.9801807,0.00023166412,0.00013160997,0.0036516234],"study_design_scores_gemma":[0.00059259904,0.0069646067,0.13464922,0.000028835382,0.00032916927,0.0009698028,0.0005986545,0.041249275,0.81194174,0.0003888072,0.002115718,0.00017163053],"about_ca_topic_score_codex":0.0013121769,"about_ca_topic_score_gemma":0.0008643508,"teacher_disagreement_score":0.0013194015,"about_ca_system_score_codex":0.00039902265,"about_ca_system_score_gemma":0.0002567985,"threshold_uncertainty_score":0.004413843},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.93676096,0.000277016,0.04394548,0.00016667585,0.00006329048,0.000069838636,0.0012505794,0.0020137578,0.015452288],"genre_scores_gemma":[0.99694353,0.00006155002,0.0017718037,0.000023435588,0.0000035129938,0.000019355182,0.0005571045,0.00011998065,0.0004996253],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9979716,0.000515691,0.000083693456,0.0003933323,0.0008130115,0.00022268484],"domain_scores_gemma":[0.99562496,0.0027486004,0.00032242772,0.00039060702,0.0008463843,0.000067010056],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0018914739,0.0006343963,0.00030229308,0.0007299407,0.00050524704,0.0009948105,0.0004859,0.0008044342,0.0011748318],"category_scores_gemma":[0.0050349883,0.00032895693,0.00071447657,0.0009426142,0.00045717316,0.000896276,0.0005907687,0.000837092,0.00044223238],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.001184267,0.000241021,0.06605799,0.0001964046,0.000110239744,0.00041424853,0.00024843763,0.83329123,0.057799626,0.002976818,0.0021916004,0.035288077],"study_design_scores_gemma":[0.00008939894,0.0006276914,0.09927518,0.00007891784,0.00015211638,0.00020180187,0.0001967635,0.78831357,0.10718325,0.0008683062,0.002892479,0.00012047819],"about_ca_topic_score_codex":0.019234398,"about_ca_topic_score_gemma":0.013555345,"teacher_disagreement_score":0.019234398,"about_ca_system_score_codex":0.0012395367,"about_ca_system_score_gemma":0.00064774853,"threshold_uncertainty_score":0.038244843},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7295195,0.0005935655,0.2591795,0.00013685874,0.00010851494,0.000065920285,0.00007248078,0.00061802566,0.009705604],"genre_scores_gemma":[0.97230273,0.00009181578,0.025917271,0.000025098478,0.000012580507,0.000032903536,0.00003893212,0.00006631627,0.0015122691],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997912,0.00006234578,0.000008722215,0.000022111812,0.00008945425,0.000026091007],"domain_scores_gemma":[0.9993585,0.00034602423,0.00006782133,0.000078205914,0.000100431884,0.000049052247],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00051603833,0.00062448665,0.00042310578,0.00030121196,0.0002975454,0.0007893287,0.00070019515,0.0007089603,0.0018748662],"category_scores_gemma":[0.001242747,0.00024887515,0.00039052026,0.00022676731,0.00058302365,0.00051441375,0.0006394245,0.0004570063,0.0003149387],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0006709636,0.00020773693,0.005462418,0.00022924838,0.000071987895,0.00037167294,0.00041492583,0.8816292,0.04220554,0.0069038887,0.0005451814,0.06128715],"study_design_scores_gemma":[0.000014316314,0.00009785815,0.00050690176,0.000009546213,0.000007685424,0.0000329342,0.000027675116,0.99430686,0.0043977704,0.0002732702,0.00031444183,0.000010756079],"about_ca_topic_score_codex":0.002138083,"about_ca_topic_score_gemma":0.0018983082,"teacher_disagreement_score":0.002138083,"about_ca_system_score_codex":0.00038662396,"about_ca_system_score_gemma":0.00038868494,"threshold_uncertainty_score":0.006272018},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9694194,0.00014178251,0.025602007,0.00006704234,0.00002611449,0.000023243903,0.000074365744,0.0002401201,0.00440588],"genre_scores_gemma":[0.9979929,0.000037423193,0.0010717841,0.00000632187,0.0000050101526,0.0000049564173,0.00003405916,0.000011484584,0.0008361794],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999391,0.000012572755,0.0000023652112,0.000012532424,0.000023565015,0.0000097803695],"domain_scores_gemma":[0.9998597,0.000074397125,0.000013365971,0.0000075047556,0.000032938486,0.000012102969],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00010560898,0.00029519034,0.00020134867,0.00028886797,0.00018777898,0.00020257899,0.00024461755,0.00032614399,0.0011721792],"category_scores_gemma":[0.00038578289,0.00007162697,0.0002745798,0.00015507033,0.000306686,0.0001659416,0.00015169331,0.00023325323,0.000115365554],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00049327244,0.00018000627,0.011403903,0.00019205143,0.000050068236,0.002423475,0.00034271387,0.6253513,0.32409692,0.0037797634,0.0006142388,0.03107233],"study_design_scores_gemma":[0.0000143371,0.000117646254,0.014440141,0.000005886516,0.000009613749,0.00014485318,0.0000791146,0.97350425,0.010934148,0.00037565822,0.00035455133,0.00001987008],"about_ca_topic_score_codex":0.0033542342,"about_ca_topic_score_gemma":0.0012098552,"teacher_disagreement_score":0.0033542342,"about_ca_system_score_codex":0.00016891991,"about_ca_system_score_gemma":0.0001441353,"threshold_uncertainty_score":0.006669402},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9949662,0.000052435127,0.0044654203,0.000013084725,0.000007642296,0.000011577818,0.000067588386,0.000047412315,0.0003685943],"genre_scores_gemma":[0.9956709,0.000044725602,0.0039034914,0.000009544797,0.0000046101773,0.0000061069104,0.00012776804,0.0000068958852,0.0002259305],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99992085,0.0000060301945,0.000003852668,0.000020459038,0.000029425297,0.000019462144],"domain_scores_gemma":[0.9998895,0.000018785715,0.000025150463,0.000010173448,0.000032614505,0.000023767578],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017331856,0.00023510108,0.00018361013,0.0007818495,0.00024313107,0.00034927306,0.000116758136,0.00023658788,0.00025583807],"category_scores_gemma":[0.00020253149,0.00010637581,0.00018207349,0.00030539755,0.00035926627,0.00017643835,0.00020015711,0.00037647615,0.000046964207],"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":[0.00017441617,0.00022748961,0.025589777,0.00004640635,0.000019098401,0.0005838465,0.00033138233,0.017580222,0.9368935,0.0011509146,0.0003056607,0.017097173],"study_design_scores_gemma":[0.000052587842,0.0011932706,0.3445673,0.000019682788,0.00003857924,0.0003809905,0.0004486443,0.36035547,0.29071233,0.0006245017,0.001520063,0.00008668368],"about_ca_topic_score_codex":0.0023924718,"about_ca_topic_score_gemma":0.0014880076,"teacher_disagreement_score":0.0023924718,"about_ca_system_score_codex":0.00014840568,"about_ca_system_score_gemma":0.00027369766,"threshold_uncertainty_score":0.0047571063},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.71283156,0.00029639553,0.28493693,0.00007275316,0.000030091955,0.000045118868,0.000030781015,0.00054179033,0.0012145467],"genre_scores_gemma":[0.99373925,0.000054113534,0.005953795,0.000003869605,0.0000050891495,0.000011831893,0.000009575218,0.000013801904,0.00020863094],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997664,0.00004161787,0.00001101927,0.000056318695,0.00009704716,0.000027719065],"domain_scores_gemma":[0.9987966,0.0007472076,0.00018252277,0.00007282854,0.00015777917,0.00004312694],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00051334716,0.00043326127,0.0005236509,0.00056553434,0.00016903285,0.00030231525,0.00047981722,0.0006955208,0.00041943934],"category_scores_gemma":[0.002147965,0.0004018134,0.0004471681,0.00020117807,0.0005897178,0.0006727605,0.00042415498,0.00056603213,0.00009524156],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00016745596,0.0001521356,0.009910053,0.00016070438,0.000035489855,0.0007492513,0.00019849812,0.6779547,0.27726144,0.0031410188,0.00016846783,0.030100798],"study_design_scores_gemma":[0.0000045046727,0.000029416964,0.0010106361,0.0000024786561,0.0000031540853,0.000037721336,0.000005546277,0.9919294,0.006756182,0.0001703099,0.000045444373,0.0000051598477],"about_ca_topic_score_codex":0.001255714,"about_ca_topic_score_gemma":0.00073538534,"teacher_disagreement_score":0.001255714,"about_ca_system_score_codex":0.00027619713,"about_ca_system_score_gemma":0.00031884926,"threshold_uncertainty_score":0.0027148724},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9965305,0.00019621712,0.002972546,0.0000057559764,0.00001317011,0.000014944511,0.000032124168,0.000017606839,0.00021711242],"genre_scores_gemma":[0.99679935,0.00014111694,0.002662063,0.000014926093,0.000007459414,0.00001150569,0.00011462392,0.00001229378,0.00023672906],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9996124,0.000044613258,0.000042218566,0.00008545767,0.00015508171,0.000060371978],"domain_scores_gemma":[0.99930525,0.00022636692,0.00017292265,0.000051762436,0.00016604437,0.00007757638],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00050472957,0.00034934568,0.00042249437,0.00037909695,0.0002633636,0.00081508356,0.00027286314,0.0003489356,0.00056667667],"category_scores_gemma":[0.0009465642,0.00016892813,0.00032114403,0.0003179856,0.0004947119,0.00046463203,0.000297771,0.0003273227,0.00006254411],"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":[0.00045801303,0.00004026932,0.002205062,0.000059590522,0.000012350452,0.00018119854,0.000082101076,0.0010222244,0.9928901,0.0001336077,0.0000137383795,0.0029016272],"study_design_scores_gemma":[0.00008271497,0.003099242,0.067077816,0.000021308131,0.00009127065,0.00036483706,0.00023091026,0.013627298,0.9143795,0.00019222857,0.00076841505,0.00006449384],"about_ca_topic_score_codex":0.00027129296,"about_ca_topic_score_gemma":0.00024189286,"teacher_disagreement_score":0.00081508356,"about_ca_system_score_codex":0.0002562228,"about_ca_system_score_gemma":0.00013348542,"threshold_uncertainty_score":0.0026693344},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99058574,0.00017007158,0.006598405,0.00002252095,0.000022551318,0.000047582875,0.00023060244,0.00010958468,0.0022129393],"genre_scores_gemma":[0.9914806,0.00014693949,0.0070601655,0.00000978738,0.00000969294,0.00004579435,0.00021422164,0.000019206433,0.0010136303],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99960655,0.000029838677,0.000032021566,0.00007702438,0.00019345745,0.00006111946],"domain_scores_gemma":[0.9996244,0.00009368613,0.000074106174,0.000057976482,0.00011358997,0.00003624596],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004781605,0.0003511471,0.00041152904,0.00046949222,0.0006157547,0.00049277034,0.00046470689,0.00031325937,0.0023038348],"category_scores_gemma":[0.0007139127,0.00011212445,0.0002754096,0.00057609286,0.00047200304,0.00030159758,0.0003873696,0.00033874248,0.00015917154],"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":[0.0004937581,0.00059120875,0.006152399,0.0001915276,0.000015574029,0.00042966375,0.00029932556,0.023010481,0.9566638,0.0013514073,0.00014954414,0.0106512355],"study_design_scores_gemma":[0.000068005604,0.0014939768,0.032516684,0.000025577508,0.00003671301,0.00021344505,0.0002032467,0.17643914,0.7866192,0.000516658,0.0018036299,0.00006365037],"about_ca_topic_score_codex":0.000970656,"about_ca_topic_score_gemma":0.00057116896,"teacher_disagreement_score":0.0023038348,"about_ca_system_score_codex":0.00031190494,"about_ca_system_score_gemma":0.00022715294,"threshold_uncertainty_score":0.007707119},"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":"review","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.06421001,0.47303817,0.09614978,0.006390465,0.0052597146,0.00009792299,0.00031970628,0.0002787783,0.3542554],"genre_scores_gemma":[0.5708773,0.2771958,0.018024158,0.0017930347,0.005692984,0.00010935767,0.00041986819,0.00010821295,0.1257793],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"not_applicable","domain_scores_codex":[0.9993511,0.00012723515,0.000034147008,0.0001145319,0.0002997614,0.00007320435],"domain_scores_gemma":[0.9993962,0.00030804914,0.00010101106,0.000028696022,0.00013390879,0.000032143536],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025060694,0.0006000332,0.00044197365,0.0010841376,0.00067773985,0.0015261321,0.00048413323,0.0016076756,0.0059896],"category_scores_gemma":[0.0011124266,0.00018240817,0.00027005732,0.001493704,0.0017781758,0.0010840312,0.0010405008,0.0012239726,0.0013564257],"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":[0.00014326074,0.00018140518,0.0051730536,0.0015530487,0.00003615924,0.0021219905,0.0016517335,0.032884922,0.020113038,0.6205774,0.01664161,0.29892242],"study_design_scores_gemma":[0.000022488535,0.000409583,0.024525832,0.0015057669,0.00004222838,0.004722909,0.0019758136,0.019462354,0.00540671,0.44306603,0.49870932,0.00015093316],"about_ca_topic_score_codex":0.003604199,"about_ca_topic_score_gemma":0.0028658311,"teacher_disagreement_score":0.0059896,"about_ca_system_score_codex":0.0006965847,"about_ca_system_score_gemma":0.000534325,"threshold_uncertainty_score":0.020037234},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.03422926,0.00009984441,0.96158004,0.000102526414,0.000041728254,0.000042562307,0.000023570596,0.00016518046,0.0037151966],"genre_scores_gemma":[0.4679074,0.00021722142,0.5282281,0.000041068426,0.000037480448,0.00011003633,0.00007043305,0.000074449905,0.0033137808],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998388,0.000040118208,0.000009169756,0.000031103264,0.000060811344,0.000020002111],"domain_scores_gemma":[0.9996425,0.0001600553,0.000050011844,0.000046281544,0.00007844315,0.00002275633],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005535698,0.0005118774,0.00043742845,0.00086692465,0.0005932277,0.0012731198,0.00052213843,0.0007346908,0.0019622012],"category_scores_gemma":[0.0022723046,0.00033485368,0.00047183302,0.00036174004,0.00090456917,0.0006373771,0.0007347713,0.00061656366,0.00029504095],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00028764777,0.00013065345,0.0043014055,0.0003415153,0.00005657459,0.00036833403,0.000489143,0.70351446,0.10157997,0.08872394,0.00075940066,0.099446855],"study_design_scores_gemma":[0.000009673305,0.00004015512,0.00058464566,0.000016172693,0.000008245974,0.00006711608,0.000060174687,0.98239017,0.0064887973,0.00887829,0.0014428435,0.000013711639],"about_ca_topic_score_codex":0.0007212352,"about_ca_topic_score_gemma":0.0007608286,"teacher_disagreement_score":0.0019622012,"about_ca_system_score_codex":0.00029401545,"about_ca_system_score_gemma":0.0006058184,"threshold_uncertainty_score":0.0065642595},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6057575,0.0003205263,0.35899797,0.00033679447,0.00017408757,0.0002598395,0.0007955706,0.0017467304,0.03161107],"genre_scores_gemma":[0.93647826,0.0001268992,0.06004292,0.000034058245,0.00002179056,0.0001235365,0.00029621786,0.00013861277,0.0027376239],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99976784,0.000047937545,0.000012805655,0.000027814222,0.00011134817,0.000032313714],"domain_scores_gemma":[0.9990281,0.0005144043,0.000059202524,0.00008214841,0.0002698304,0.00004636722],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004037882,0.000522814,0.0004886928,0.0005252145,0.0004412918,0.00065088447,0.00088317005,0.0006971576,0.0017589714],"category_scores_gemma":[0.0019463467,0.00024893117,0.0004548437,0.0004732898,0.0005833699,0.0004143736,0.00067557074,0.00055551727,0.000289644],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000041031974,0.000031724565,0.0012529414,0.000024747746,0.000004916519,0.00004948424,0.00002401653,0.9896477,0.002235003,0.001018847,0.00018031872,0.0054892926],"study_design_scores_gemma":[0.000008655278,0.000009221187,0.00019048824,0.00000127995,7.040017e-7,0.000003890999,0.000003995214,0.99896085,0.00062223757,0.00010093047,0.00009511,0.0000025463924],"about_ca_topic_score_codex":0.019828275,"about_ca_topic_score_gemma":0.008863149,"teacher_disagreement_score":0.019828275,"about_ca_system_score_codex":0.000603458,"about_ca_system_score_gemma":0.0012468921,"threshold_uncertainty_score":0.03942567},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.4527936,0.0006023309,0.5382061,0.0002478566,0.00029098458,0.00028264205,0.0003773376,0.0047056274,0.0024935747],"genre_scores_gemma":[0.82647705,0.00011212132,0.17050913,0.00015399297,0.00009332667,0.00015920948,0.0006195808,0.00010262977,0.0017729573],"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99853635,0.00040691328,0.000089535686,0.0003042337,0.00054759637,0.0001154471],"domain_scores_gemma":[0.99659616,0.0015582605,0.00014179379,0.0003584076,0.0012083718,0.00013696362],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0023726241,0.00080179167,0.00071604573,0.00058950734,0.0006285851,0.00114404,0.0012884487,0.0010005555,0.0022427272],"category_scores_gemma":[0.0057063513,0.0003733291,0.00026763257,0.00069651933,0.0003404563,0.0011405315,0.0010341441,0.00052701304,0.0007764542],"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":[0.00897153,0.0013530762,0.03055496,0.0002801163,0.00040012767,0.00023379897,0.00028026782,0.087705836,0.15883224,0.002746553,0.005025522,0.70361596],"study_design_scores_gemma":[0.00021688717,0.00070200046,0.006900954,0.000008894799,0.000057733112,0.00012875974,0.000028669612,0.9606962,0.029549383,0.00029364962,0.0013785223,0.00003836286],"about_ca_topic_score_codex":0.007970855,"about_ca_topic_score_gemma":0.008384556,"teacher_disagreement_score":0.007970855,"about_ca_system_score_codex":0.00080119935,"about_ca_system_score_gemma":0.0012637314,"threshold_uncertainty_score":0.015848935},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99781764,0.000039659335,0.0017424149,0.000025349556,0.000006596576,0.0000022544586,0.0000160879,0.000047342633,0.0003027648],"genre_scores_gemma":[0.99911195,0.000018501318,0.00060318655,0.000007926462,0.000003051284,0.0000014217652,0.000009612355,0.000015726771,0.00022858077],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997392,0.00006502045,0.000018690725,0.000045074747,0.000059752223,0.000072222385],"domain_scores_gemma":[0.9938305,0.004816894,0.0003922549,0.0004162733,0.00030522983,0.00023894537],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005906758,0.00022578437,0.0003501886,0.0002498642,0.00035032103,0.0006755138,0.00040772703,0.00046668478,0.0009530177],"category_scores_gemma":[0.0030432034,0.00036408,0.0001348335,0.00026383935,0.0010827096,0.00080185506,0.00042327525,0.0003810924,0.00010069172],"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":[0.008092864,0.0005732363,0.004918458,0.000111958514,0.00005455855,0.0009495786,0.0005883236,0.049266826,0.924114,0.0025465959,0.00027413064,0.008509484],"study_design_scores_gemma":[0.00016000406,0.0013992544,0.011998531,0.000015203246,0.000056696485,0.00020364138,0.0002465958,0.13489132,0.85025275,0.0004854164,0.00022527765,0.000065357584],"about_ca_topic_score_codex":0.001043632,"about_ca_topic_score_gemma":0.0008120877,"teacher_disagreement_score":0.001043632,"about_ca_system_score_codex":0.00037381987,"about_ca_system_score_gemma":0.00022602562,"threshold_uncertainty_score":0.0031881928},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9965294,0.00013906806,0.0001652654,0.000052550018,0.000011258364,0.0000116360325,0.0015104703,0.000053836906,0.0015265113],"genre_scores_gemma":[0.9975884,0.00008635753,0.0003062061,0.000022811544,0.000005221463,0.000009336759,0.0012595655,0.0000051049556,0.0007171444],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.9998398,0.000009295434,0.000012413081,0.00007885401,0.00003188392,0.000027739],"domain_scores_gemma":[0.99965715,0.000047963054,0.000032980282,0.00001863978,0.00019068901,0.000052603616],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002185738,0.0002586083,0.00033031328,0.0006596677,0.00065328984,0.00068304036,0.00049674354,0.00035576968,0.00081606436],"category_scores_gemma":[0.00031980916,0.00016300895,0.00018534128,0.00065543054,0.0002563391,0.00030633537,0.0002653803,0.00018670171,0.00016399802],"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":[0.0029513994,0.0006035088,0.8841315,0.00016628495,0.0007091066,0.0010911804,0.0012742551,0.009101286,0.036487307,0.0006357876,0.0063029625,0.05654543],"study_design_scores_gemma":[0.000045531353,0.000020514566,0.99562573,0.000006553299,0.000040249815,0.000021244396,0.00024616084,0.0023326932,0.00063940545,0.000027938444,0.0009840304,0.00000992615],"about_ca_topic_score_codex":0.4243675,"about_ca_topic_score_gemma":0.6454436,"teacher_disagreement_score":0.4243675,"about_ca_system_score_codex":0.0018527614,"about_ca_system_score_gemma":0.0012549679,"threshold_uncertainty_score":0.8437948},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9554519,0.00034777576,0.008612004,0.00064474327,0.0002283396,0.00010498869,0.0029907227,0.0005260154,0.031093456],"genre_scores_gemma":[0.9922983,0.00011226146,0.003428086,0.000087591216,0.000030456036,0.000050911927,0.0010044471,0.00007199974,0.0029160522],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99968636,0.000052320273,0.000028989332,0.00004701759,0.000087338485,0.000098015415],"domain_scores_gemma":[0.9979956,0.0011884198,0.00015124927,0.00009805291,0.00035198368,0.00021468851],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004961383,0.00066930515,0.0010371967,0.000964344,0.0010900176,0.0015711443,0.0015261619,0.0025271946,0.006049801],"category_scores_gemma":[0.0027066115,0.00041686886,0.0009813224,0.0012035908,0.0010899683,0.0006262309,0.0007586552,0.0013431618,0.00048911734],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00020357379,0.00022350998,0.004513855,0.00006350806,0.000034694433,0.00021939815,0.00008700364,0.987727,0.00231436,0.0015713908,0.00081395585,0.002227783],"study_design_scores_gemma":[0.00007010722,0.0000665548,0.0020060155,0.000013364205,0.00001056469,0.000022235079,0.0000939897,0.99615675,0.00086979923,0.00029995525,0.00037250374,0.000018087114],"about_ca_topic_score_codex":0.030876404,"about_ca_topic_score_gemma":0.014111318,"teacher_disagreement_score":0.030876404,"about_ca_system_score_codex":0.0012046512,"about_ca_system_score_gemma":0.0015927607,"threshold_uncertainty_score":0.06139338},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.45347422,0.00064238557,0.5258101,0.00016534612,0.00022823967,0.00027812482,0.00072379847,0.0014941625,0.017183611],"genre_scores_gemma":[0.9722911,0.00024565074,0.02523218,0.000024198265,0.00001699412,0.00015191422,0.00035875375,0.00006837125,0.0016107688],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9992398,0.00016483947,0.000052356983,0.00013802478,0.00035942195,0.000045583725],"domain_scores_gemma":[0.99886155,0.0005577618,0.00008612012,0.00016504648,0.000308818,0.000020713325],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0011491242,0.0009976688,0.00048771972,0.0007444389,0.00036114684,0.0007535083,0.0008148685,0.0010295415,0.0018233922],"category_scores_gemma":[0.0032788725,0.0002644014,0.0005531921,0.00045130507,0.0005258033,0.00086266856,0.00044907627,0.00048483425,0.0005124515],"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":[0.00020766177,0.00021281067,0.0033373188,0.0003288641,0.000024710387,0.00017293697,0.00014782409,0.9204538,0.04413425,0.0030442625,0.00039774802,0.027537739],"study_design_scores_gemma":[0.000013328967,0.00012282234,0.00085994776,0.000022644012,0.000010608329,0.000047219382,0.00003421368,0.9817847,0.01571083,0.00051005685,0.0008655505,0.000018131974],"about_ca_topic_score_codex":0.003390953,"about_ca_topic_score_gemma":0.0021063867,"teacher_disagreement_score":0.003390953,"about_ca_system_score_codex":0.0004560387,"about_ca_system_score_gemma":0.00055560435,"threshold_uncertainty_score":0.0067424774},"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":"methods","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0032333587,0.00005704273,0.9961637,0.00003901107,0.000011609276,0.000012191889,0.000011089033,0.000079317004,0.00039275194],"genre_scores_gemma":[0.11610596,0.00032445378,0.8804657,0.00013451191,0.00003931835,0.00006733249,0.00009809608,0.00008176935,0.0026828672],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99965334,0.00010171932,0.00002120398,0.000040642957,0.00016010283,0.000022869797],"domain_scores_gemma":[0.9993292,0.00031182353,0.000093428665,0.00010006565,0.00013767571,0.000027822389],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0010212642,0.00055227487,0.0005067929,0.00046943585,0.00020090298,0.0007138899,0.0007766222,0.00083872554,0.0013618324],"category_scores_gemma":[0.0018082304,0.0002874676,0.00062229246,0.00037202856,0.0007611053,0.0014053241,0.0010488804,0.0009241545,0.0004507564],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00019641056,0.00013503677,0.0013043025,0.00036677878,0.00007543567,0.00021593543,0.0002662507,0.5577859,0.07739529,0.0876943,0.001484778,0.2730795],"study_design_scores_gemma":[0.000005872499,0.000026869255,0.00013772199,0.000010398811,0.000006392643,0.0000858601,0.000013065142,0.98427,0.0103084305,0.00346088,0.0016595257,0.000014951484],"about_ca_topic_score_codex":0.0016892981,"about_ca_topic_score_gemma":0.0018078078,"teacher_disagreement_score":0.0016892981,"about_ca_system_score_codex":0.00046333706,"about_ca_system_score_gemma":0.0010383872,"threshold_uncertainty_score":0.0054010153},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.91824,0.0003861621,0.077546924,0.00007548713,0.000052218733,0.000023949924,0.00017773657,0.00012983633,0.0033677628],"genre_scores_gemma":[0.9854752,0.00022022885,0.012090465,0.0000185098,0.000035802128,0.000013208982,0.00022603184,0.000022158421,0.0018984735],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.99992836,0.0000116218625,0.000003579463,0.000013887122,0.000028845261,0.000013648778],"domain_scores_gemma":[0.99960274,0.00012973808,0.000082543884,0.000026542713,0.000109650406,0.000048785176],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023451922,0.00021311625,0.00013343553,0.0010161743,0.00014669388,0.0003165069,0.00017071319,0.00028464763,0.0007787944],"category_scores_gemma":[0.00083678693,0.00013551561,0.000119216,0.00042646393,0.00017919927,0.00033023866,0.0003535262,0.00025131134,0.00022450111],"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":[0.0008779203,0.00019042772,0.045516033,0.00012175059,0.00005806942,0.0006165094,0.00019024439,0.010613784,0.8111918,0.003088226,0.00050064723,0.12703454],"study_design_scores_gemma":[0.00005834735,0.0006152429,0.405112,0.000068991096,0.00015200632,0.0022266107,0.0004595984,0.3988859,0.18536352,0.0028202052,0.004153221,0.00008434212],"about_ca_topic_score_codex":0.00041554132,"about_ca_topic_score_gemma":0.00088978495,"teacher_disagreement_score":0.0010161743,"about_ca_system_score_codex":0.00009130322,"about_ca_system_score_gemma":0.0001720947,"threshold_uncertainty_score":0.002605319},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.96161973,0.00006841265,0.037192184,0.000025002897,0.000010263165,0.000041337684,0.00010709507,0.00020831844,0.00072763074],"genre_scores_gemma":[0.9869571,0.000040661296,0.012646446,0.000008504624,0.0000033143308,0.000027337679,0.000037215887,0.0000143166735,0.00026515787],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9996414,0.000038898477,0.0000130747285,0.00007517015,0.00019867314,0.000032795404],"domain_scores_gemma":[0.999171,0.00033432347,0.00014507836,0.000077003744,0.00021653113,0.000056105626],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00047244152,0.0004561363,0.00029514672,0.00033043677,0.00021771374,0.00020737926,0.00041481366,0.0004095019,0.00062804285],"category_scores_gemma":[0.001066862,0.00026001732,0.00018456709,0.00019075951,0.00039996716,0.0002893081,0.0005305151,0.00038469434,0.00020927741],"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":[0.00004131518,0.000016533915,0.0011416286,0.00003101671,0.0000029826924,0.000041093284,0.00006082456,0.00039686865,0.9953121,0.00007644797,0.00001694794,0.0028622642],"study_design_scores_gemma":[0.000024498691,0.00053762883,0.011263468,0.000008650842,0.00001576204,0.00017073649,0.000055680997,0.013514576,0.9739051,0.00006196417,0.00042183496,0.000020165628],"about_ca_topic_score_codex":0.0004103262,"about_ca_topic_score_gemma":0.0004793235,"teacher_disagreement_score":0.00062804285,"about_ca_system_score_codex":0.00025297928,"about_ca_system_score_gemma":0.0003627401,"threshold_uncertainty_score":0.002498567},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9885421,0.00010608156,0.010383782,0.000018584871,0.000009926054,0.000025857938,0.00010031548,0.00013789593,0.0006755973],"genre_scores_gemma":[0.9964246,0.00006594819,0.0032503663,0.0000051714446,0.000003578437,0.000009984233,0.000039906892,0.0000059278527,0.00019449393],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997212,0.000028879165,0.000009581321,0.000038876882,0.00015608282,0.000045336827],"domain_scores_gemma":[0.9996006,0.00014627421,0.00005196106,0.000024695028,0.00012119435,0.00005530224],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00022605815,0.00031816482,0.00041188186,0.00052835676,0.00027542008,0.00021945628,0.00032496304,0.00034182597,0.00038941856],"category_scores_gemma":[0.00063379103,0.00023635566,0.00018478792,0.00028058016,0.00045020162,0.00027008515,0.00041815123,0.00031323757,0.00010419942],"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":[0.00030519036,0.00004905154,0.0056445957,0.0000764399,0.00000870474,0.00033611016,0.00023196898,0.0020004911,0.98200697,0.00011095148,0.00007425913,0.009155274],"study_design_scores_gemma":[0.000087524255,0.0022836032,0.11343417,0.00003367963,0.000047137466,0.00089316303,0.0004980656,0.04198497,0.83952576,0.0002786443,0.00084183173,0.00009134743],"about_ca_topic_score_codex":0.0011077963,"about_ca_topic_score_gemma":0.0012567502,"teacher_disagreement_score":0.0011077963,"about_ca_system_score_codex":0.00019918787,"about_ca_system_score_gemma":0.0002478673,"threshold_uncertainty_score":0.0022027493},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9988405,0.0000672867,0.0006032018,0.000009333414,0.000017396584,0.0000020737607,0.000021155482,0.000022636426,0.00041644234],"genre_scores_gemma":[0.9996057,0.000028659915,0.00014202029,0.000004890678,0.0000038105063,7.300844e-7,0.000021027294,0.000009271269,0.00018392749],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998147,0.000021560256,0.000012400311,0.000028916647,0.00005493264,0.00006756779],"domain_scores_gemma":[0.9983689,0.00096174894,0.00018374652,0.00009571423,0.00019484872,0.00019499483],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00022911602,0.0003357332,0.0003153578,0.00025734262,0.00037289338,0.00072824646,0.00021544495,0.00038442324,0.0028127038],"category_scores_gemma":[0.0014827105,0.00026483586,0.0002220411,0.0003188459,0.00047946034,0.00040430453,0.00033138035,0.00046353828,0.00022979529],"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":[0.0061020115,0.00027162745,0.010202509,0.0001169372,0.000028914992,0.0008776039,0.00018611262,0.021616325,0.9459855,0.00045767266,0.00014108453,0.0140136955],"study_design_scores_gemma":[0.00018933127,0.005054671,0.09399404,0.000029966734,0.00020646879,0.0003675572,0.000617367,0.06521319,0.83308685,0.00021972327,0.0009011823,0.000119630764],"about_ca_topic_score_codex":0.000704501,"about_ca_topic_score_gemma":0.0006667722,"teacher_disagreement_score":0.0028127038,"about_ca_system_score_codex":0.00024847232,"about_ca_system_score_gemma":0.00025644712,"threshold_uncertainty_score":0.009409487},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9895984,0.0003657244,0.008671966,0.000033658755,0.000026024582,0.0000121694275,0.000019907322,0.00010677478,0.0011653224],"genre_scores_gemma":[0.99673814,0.00010601926,0.0028750424,0.000010639964,0.000005289409,0.0000060275565,0.000017758026,0.000015284888,0.00022571177],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99935275,0.0000737832,0.00004448349,0.00014073534,0.0002587729,0.00012951293],"domain_scores_gemma":[0.996608,0.0018871629,0.0005524307,0.00021463611,0.0004884613,0.00024936386],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00052161736,0.0006805281,0.0005665794,0.0004168985,0.00032700828,0.00057283125,0.0003795381,0.00046656025,0.0015446763],"category_scores_gemma":[0.0021762063,0.00036980232,0.0003157152,0.00023781638,0.00054877496,0.0005697007,0.0009150268,0.00062485697,0.0002787093],"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":[0.00043570518,0.00007542571,0.0019676941,0.00011681361,0.000016569305,0.00033123238,0.000082152124,0.0065897712,0.9792478,0.00018871605,0.000045734832,0.010902394],"study_design_scores_gemma":[0.000043939435,0.0013883045,0.009039662,0.000021683063,0.000057091213,0.00035915888,0.00014255207,0.023258764,0.9647177,0.00014658384,0.00078770507,0.000036951344],"about_ca_topic_score_codex":0.00026402605,"about_ca_topic_score_gemma":0.00033794026,"teacher_disagreement_score":0.0015446763,"about_ca_system_score_codex":0.00022391453,"about_ca_system_score_gemma":0.00032855483,"threshold_uncertainty_score":0.0051674843},"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":"methods","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.3801428,0.0005128724,0.60357684,0.00019945965,0.00009105509,0.00011907554,0.00028209516,0.0015663615,0.013509373],"genre_scores_gemma":[0.9522773,0.0003067762,0.04287412,0.000026259271,0.000030121224,0.00008519289,0.00019546186,0.00016239939,0.0040423158],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99985266,0.000039553586,0.000005515823,0.00002295933,0.000059689,0.000019584515],"domain_scores_gemma":[0.99966764,0.00017203887,0.00003952515,0.000021989978,0.000084716085,0.0000140196935],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003879627,0.00089387095,0.0005771597,0.0004529167,0.00047734604,0.0005142336,0.00071885955,0.0007802678,0.0013062037],"category_scores_gemma":[0.0011163407,0.0002619582,0.00057179155,0.00025808957,0.00043820366,0.00049691804,0.00028653236,0.00044138986,0.00041404983],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000039154245,0.00003479357,0.001001145,0.000051427498,0.000008657698,0.00014454994,0.000054550936,0.97455263,0.016083477,0.002227928,0.00017920404,0.0056224954],"study_design_scores_gemma":[0.0000018877998,0.000008113494,0.00010448364,0.000001994283,0.0000012339591,0.000009917708,0.0000028597312,0.9990288,0.0006066753,0.00013464261,0.00009725757,0.0000022209422],"about_ca_topic_score_codex":0.0070037823,"about_ca_topic_score_gemma":0.004497818,"teacher_disagreement_score":0.0070037823,"about_ca_system_score_codex":0.0005647205,"about_ca_system_score_gemma":0.00074285676,"threshold_uncertainty_score":0.013926029},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.057780623,0.0010229913,0.89393276,0.00068060466,0.0007896338,0.00026948564,0.00031148808,0.0006236702,0.044588663],"genre_scores_gemma":[0.62587154,0.00094764726,0.34026462,0.00068230403,0.00047764508,0.00056723674,0.00049662584,0.0006976213,0.029994838],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991597,0.00013473991,0.000065154214,0.00012984667,0.00040953993,0.00010103657],"domain_scores_gemma":[0.9992656,0.0002496043,0.0001116736,0.000086811226,0.00023697168,0.00004938577],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00082591793,0.0009045381,0.0006231332,0.00084839965,0.0008775878,0.0012748186,0.0013693294,0.0016601755,0.006872072],"category_scores_gemma":[0.003942844,0.0004168738,0.00043079336,0.0003239231,0.001339942,0.0025011946,0.001338843,0.0012443418,0.0019790235],"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":[0.0005392772,0.000070157475,0.0011670197,0.00055929535,0.000022081314,0.0012450045,0.00048702586,0.04879644,0.21496806,0.6398985,0.009518027,0.08272908],"study_design_scores_gemma":[0.0002574461,0.0005369958,0.0027093457,0.00029544588,0.000049996524,0.0019023953,0.0003581936,0.5581465,0.14672647,0.15927182,0.12941572,0.000329583],"about_ca_topic_score_codex":0.0018905461,"about_ca_topic_score_gemma":0.0013983573,"teacher_disagreement_score":0.006872072,"about_ca_system_score_codex":0.0006376809,"about_ca_system_score_gemma":0.00097328087,"threshold_uncertainty_score":0.022989333},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.20804515,0.0017394816,0.75777435,0.0005366229,0.00041299648,0.00010588748,0.00014130473,0.0003355531,0.030908786],"genre_scores_gemma":[0.9188222,0.0010309566,0.06434456,0.00014456589,0.00029914296,0.00011793161,0.00020602955,0.00015221135,0.014882341],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994166,0.0001365298,0.000037921847,0.00008108199,0.00025569324,0.00007221086],"domain_scores_gemma":[0.9991375,0.00038483916,0.00012313308,0.000049446593,0.00023794969,0.00006698583],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0008099152,0.0007458296,0.00068638864,0.0007340481,0.0007395021,0.0012298188,0.00081619155,0.0014369895,0.0025004358],"category_scores_gemma":[0.0030296491,0.00029418312,0.00037509677,0.00035453352,0.0016400394,0.0014223685,0.0012910843,0.0010637692,0.000735902],"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":[0.0005604959,0.000118008145,0.0017411798,0.0005273126,0.0000210314,0.0026106492,0.0009919832,0.121976055,0.25820097,0.5596011,0.0034854815,0.050165713],"study_design_scores_gemma":[0.00011808896,0.000254092,0.0023225914,0.000089986715,0.000018378598,0.00093994464,0.00038189426,0.8342199,0.033119228,0.117074855,0.011321997,0.00013913299],"about_ca_topic_score_codex":0.0016821809,"about_ca_topic_score_gemma":0.00075503497,"teacher_disagreement_score":0.0025004358,"about_ca_system_score_codex":0.00043178935,"about_ca_system_score_gemma":0.0006710636,"threshold_uncertainty_score":0.008364797},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.12157605,0.00038017725,0.8546472,0.0004783278,0.0004159376,0.00022902862,0.00029907195,0.004014188,0.017960042],"genre_scores_gemma":[0.74988675,0.00021400678,0.23821175,0.00025781264,0.0000931546,0.00022767458,0.0004628506,0.0021186268,0.00852739],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99969983,0.00010042452,0.00002453217,0.000034343968,0.0001020775,0.000038714406],"domain_scores_gemma":[0.99867094,0.00053310074,0.00006710368,0.00021108094,0.0004344219,0.00008337207],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005916779,0.00092437014,0.0008442819,0.00034992181,0.00079865765,0.0011118513,0.0011910638,0.0012793757,0.0061495374],"category_scores_gemma":[0.0036205638,0.00039873747,0.0006268056,0.00033331817,0.0004167618,0.0013588422,0.0008760865,0.0016691326,0.0012613612],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0003706029,0.00056502974,0.0024339492,0.00024162969,0.00008427349,0.00022791284,0.00024367443,0.8713441,0.05054669,0.011766734,0.0033318975,0.05884352],"study_design_scores_gemma":[0.000016771279,0.000026718662,0.00014717031,0.000006280533,0.00000586053,0.000010371729,0.000012174655,0.99436104,0.0040716785,0.0005080498,0.0008267124,0.0000071249665],"about_ca_topic_score_codex":0.005704779,"about_ca_topic_score_gemma":0.0050915773,"teacher_disagreement_score":0.0061495374,"about_ca_system_score_codex":0.000332281,"about_ca_system_score_gemma":0.001130282,"threshold_uncertainty_score":0.020572245},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.022932028,0.00006293814,0.9757706,0.00008205182,0.000015344105,0.0000241306,0.000062669096,0.00017310391,0.00087713706],"genre_scores_gemma":[0.28646368,0.00031598037,0.7099482,0.000068320885,0.000026417005,0.00012219223,0.0004827264,0.000092517264,0.0024799008],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998109,0.000050116338,0.000010438644,0.000019016992,0.00009422775,0.000015254621],"domain_scores_gemma":[0.9994868,0.00027082898,0.00006615225,0.00006482728,0.0000915976,0.000019789768],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00067398464,0.000488412,0.00035804475,0.00056372426,0.00019454566,0.00054604927,0.00040454412,0.00062769843,0.00086293166],"category_scores_gemma":[0.0016503548,0.0002136939,0.00042440894,0.0005370155,0.0005413701,0.0006826226,0.00057312177,0.00068853784,0.00026722054],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00021341396,0.00015799976,0.0013900925,0.00026466695,0.000051414077,0.00018519492,0.00021112744,0.67142487,0.11956988,0.036650144,0.0018585976,0.16802256],"study_design_scores_gemma":[0.0000045368006,0.000018994378,0.00019029743,0.0000046308455,0.0000024516185,0.000026188054,0.000013332313,0.9888616,0.008501843,0.0019209685,0.00044690078,0.0000081931075],"about_ca_topic_score_codex":0.002005219,"about_ca_topic_score_gemma":0.0023062078,"teacher_disagreement_score":0.002005219,"about_ca_system_score_codex":0.00035401626,"about_ca_system_score_gemma":0.00094724895,"threshold_uncertainty_score":0.003987074},"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":"editorial","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"other","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0019450578,0.002813207,0.027429964,0.027848745,0.90637624,0.00009732216,0.005164006,0.0037020985,0.024623293],"genre_scores_gemma":[0.029880377,0.008256439,0.066957474,0.023693016,0.052490942,0.00030171737,0.018956997,0.011288282,0.78817475],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.9980374,0.00017118287,0.0003526686,0.00019922642,0.0011630204,0.00007658174],"domain_scores_gemma":[0.9884725,0.0017800572,0.0003986932,0.00068062224,0.008446733,0.00022132105],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0018480275,0.0026788432,0.0012560431,0.0028305561,0.0033373418,0.0020490307,0.0030624936,0.003668254,0.071830295],"category_scores_gemma":[0.023693638,0.0010283745,0.0011206068,0.0018857248,0.0014682477,0.0034315602,0.0017602327,0.0038699792,0.055470966],"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":[0.000066268956,0.000020471667,0.00013234487,0.00010570306,0.000009198695,0.0002560847,0.000040035506,0.00043552686,0.0004609245,0.0025855731,0.9789838,0.01690408],"study_design_scores_gemma":[0.00004312836,0.000047083497,0.0006806799,0.00035109316,0.00003647568,0.00079521025,0.000113269634,0.0053543053,0.0030844677,0.0030961502,0.98631185,0.00008626357],"about_ca_topic_score_codex":0.014933808,"about_ca_topic_score_gemma":0.018424831,"teacher_disagreement_score":0.071830295,"about_ca_system_score_codex":0.002399414,"about_ca_system_score_gemma":0.0028904702,"threshold_uncertainty_score":0.2402963},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.2753925,0.0016657223,0.67849183,0.0011930242,0.00076600723,0.00019466561,0.0004233732,0.001556114,0.04031681],"genre_scores_gemma":[0.90353656,0.0009640957,0.079784244,0.00022584868,0.0004066164,0.00013988667,0.0003129047,0.0005945342,0.014035405],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997017,0.00011860693,0.000019638223,0.000036254365,0.00008645418,0.000037387264],"domain_scores_gemma":[0.99923444,0.00031380547,0.00007401441,0.0000692634,0.00025472042,0.000053859527],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00064982177,0.0012480066,0.0010133557,0.0007952118,0.0007180872,0.0017445924,0.0010949763,0.0018005961,0.0019540351],"category_scores_gemma":[0.0022474355,0.0005096928,0.0010194815,0.0005924453,0.0009343477,0.0017812669,0.0010078859,0.0013235152,0.00043610192],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00012426339,0.00020133828,0.0018463052,0.00012098171,0.000060209164,0.00041036398,0.00010435624,0.9584492,0.012944851,0.014639894,0.0007570273,0.01034121],"study_design_scores_gemma":[0.000007072452,0.0000055086457,0.00008885596,0.000004268813,0.000002850482,0.000007273403,0.000006637171,0.9989736,0.00044274738,0.00032188202,0.0001341566,0.000005137223],"about_ca_topic_score_codex":0.009845365,"about_ca_topic_score_gemma":0.005367719,"teacher_disagreement_score":0.009845365,"about_ca_system_score_codex":0.00065498904,"about_ca_system_score_gemma":0.0009820225,"threshold_uncertainty_score":0.019576132},"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":"commentary","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"other","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.003390919,0.28260648,0.0038911074,0.39564833,0.13305421,0.00004097477,0.00020146977,0.0003750677,0.18079153],"genre_scores_gemma":[0.04833714,0.25481534,0.00493031,0.12265324,0.112652965,0.00010504336,0.00024783838,0.0009601489,0.45529807],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.9981469,0.00047249603,0.00010072597,0.00027435596,0.0007848913,0.00022062052],"domain_scores_gemma":[0.9969798,0.00085865916,0.00020945365,0.00012768053,0.00063056254,0.0011938731],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0023406749,0.0005312463,0.00039069826,0.0013294035,0.0029555075,0.0065924167,0.00068976235,0.002065482,0.016893035],"category_scores_gemma":[0.007877408,0.00041267223,0.00019029662,0.0016360031,0.002582773,0.0051237,0.003188907,0.0053731464,0.011117043],"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":[0.000019685733,0.000021070882,0.00026074,0.00016391804,0.0000021564751,0.0003270785,0.0023466647,0.000035183017,0.00019974764,0.013963037,0.9194831,0.063177586],"study_design_scores_gemma":[9.4786776e-7,0.0000068767376,0.00012083498,0.00012969464,7.580266e-7,0.0004292587,0.00052392954,0.000009496281,0.000039629616,0.0017620489,0.99697113,0.0000053228373],"about_ca_topic_score_codex":0.0020405613,"about_ca_topic_score_gemma":0.003123803,"teacher_disagreement_score":0.016893035,"about_ca_system_score_codex":0.0014633713,"about_ca_system_score_gemma":0.0027147247,"threshold_uncertainty_score":0.056512833},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8500899,0.00038463413,0.13727453,0.00015986878,0.00006427459,0.0001391791,0.0006335939,0.0012508107,0.010003285],"genre_scores_gemma":[0.9881765,0.00014341807,0.010738093,0.000010714217,0.0000064665637,0.00007919604,0.0003379903,0.000031224146,0.00047622106],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995565,0.0000786252,0.00003768954,0.00007373809,0.00022189495,0.000031625746],"domain_scores_gemma":[0.9987888,0.00064943434,0.00009975767,0.00012022278,0.000316792,0.000025016408],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00072594977,0.00071895175,0.000414888,0.00059698906,0.00040982134,0.0008740591,0.00091618806,0.0007371995,0.00083946466],"category_scores_gemma":[0.0024528785,0.00032795867,0.000536929,0.00053032296,0.0005222059,0.0008514898,0.0003642397,0.00065894204,0.0002790752],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000520797,0.00011181319,0.003562197,0.00006194558,0.000009661967,0.00003655912,0.000037909645,0.9786902,0.0047268416,0.00051224924,0.00021706105,0.011981605],"study_design_scores_gemma":[0.0000066725047,0.000024611012,0.0010602407,0.000004700683,0.000002351468,0.0000056203985,0.000011335061,0.996329,0.0023620836,0.000083736944,0.00010409789,0.0000055254],"about_ca_topic_score_codex":0.019201305,"about_ca_topic_score_gemma":0.01391595,"teacher_disagreement_score":0.019201305,"about_ca_system_score_codex":0.00089791924,"about_ca_system_score_gemma":0.00083752203,"threshold_uncertainty_score":0.0381791},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.01704454,0.00089503784,0.9588223,0.00032519604,0.00023630261,0.000043377462,0.0002309064,0.0007489113,0.021653501],"genre_scores_gemma":[0.6871231,0.0036957394,0.22745438,0.00034957635,0.000567043,0.0003261743,0.0013702571,0.0005275708,0.07858609],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99978834,0.000039191378,0.000009202116,0.00003487905,0.000110719455,0.000017679213],"domain_scores_gemma":[0.99985445,0.00002831656,0.000018333772,0.000024834566,0.00006356902,0.0000105257095],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00028150645,0.0005966298,0.00048462683,0.00032303834,0.00030461737,0.0007610273,0.00088593195,0.00082529016,0.0030711154],"category_scores_gemma":[0.0005356508,0.00020141088,0.0005474472,0.00031381505,0.00032231756,0.0010481677,0.00069158897,0.00070771377,0.0014502269],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00003731772,0.000033211843,0.0005667484,0.00008425236,0.00001800584,0.00013625128,0.00008672213,0.8756217,0.012937947,0.06237579,0.0034566252,0.044645507],"study_design_scores_gemma":[0.0000030311023,0.00001953254,0.00016969912,0.000010548416,0.0000032846594,0.00002819897,0.000011265563,0.98083866,0.0006832764,0.00921452,0.009010462,0.0000075785047],"about_ca_topic_score_codex":0.0028919147,"about_ca_topic_score_gemma":0.0013162775,"teacher_disagreement_score":0.0030711154,"about_ca_system_score_codex":0.0004880292,"about_ca_system_score_gemma":0.00048783713,"threshold_uncertainty_score":0.010273933},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.021187117,0.17795193,0.729893,0.034426965,0.004512409,0.00010133026,0.0021166469,0.0009883821,0.028822256],"genre_scores_gemma":[0.2979283,0.09454702,0.57399553,0.0058482774,0.01232233,0.00036498767,0.0022777817,0.00054881326,0.012166932],"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9970413,0.0010682992,0.00016485495,0.00060769165,0.0009882537,0.00012955615],"domain_scores_gemma":[0.98519635,0.009175081,0.00041449894,0.002046888,0.0027100365,0.00045724277],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.010029542,0.0016834203,0.0022088815,0.0026338578,0.0005298523,0.005275035,0.0028846338,0.004031637,0.006592726],"category_scores_gemma":[0.014271203,0.0012624508,0.0010263133,0.0037414175,0.004052611,0.014579865,0.0033825259,0.0051436354,0.0018941965],"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":[0.00054331106,0.0003084027,0.013830273,0.0021288767,0.00056215294,0.00030220384,0.00054969394,0.02317109,0.02654763,0.36525413,0.030794285,0.536008],"study_design_scores_gemma":[0.0001833386,0.00047781918,0.014923561,0.0012232151,0.0002844355,0.0009823067,0.0007654277,0.18136305,0.01195328,0.5390341,0.24813917,0.0006701701],"about_ca_topic_score_codex":0.0023975335,"about_ca_topic_score_gemma":0.0028180734,"teacher_disagreement_score":0.010029542,"about_ca_system_score_codex":0.0013681314,"about_ca_system_score_gemma":0.0008988185,"threshold_uncertainty_score":0.053041935},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99691135,0.000101330574,0.00220297,0.00001936508,0.000016541728,0.00001716741,0.000036046345,0.00002221037,0.0006731085],"genre_scores_gemma":[0.99854726,0.00006386119,0.00072402623,0.000007497664,0.000011434099,0.000008911274,0.00002810269,0.00000848917,0.000600463],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.999524,0.00012387848,0.000030729756,0.000087292654,0.0001491839,0.000084967905],"domain_scores_gemma":[0.99825734,0.0011505698,0.00013590403,0.0001459753,0.0002269254,0.00008327644],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00066101423,0.00047363958,0.00057648675,0.0003091428,0.0006478371,0.00026928243,0.0006159842,0.0007512577,0.0021518911],"category_scores_gemma":[0.0013902388,0.00031898578,0.00048136723,0.0001837257,0.0010664058,0.0005209116,0.0005405312,0.00048370633,0.00019189421],"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":[0.0022030547,0.00053071877,0.0029583126,0.00023254908,0.000037706304,0.0005447722,0.0004977881,0.0029985611,0.9842093,0.0003234344,0.000087124936,0.0053766132],"study_design_scores_gemma":[0.0003600853,0.0111887725,0.028361369,0.000038205755,0.00014727982,0.0009828478,0.00074407406,0.017622579,0.93890184,0.00022800444,0.0013563286,0.00006867683],"about_ca_topic_score_codex":0.00033635262,"about_ca_topic_score_gemma":0.00024284217,"teacher_disagreement_score":0.0021518911,"about_ca_system_score_codex":0.00020831208,"about_ca_system_score_gemma":0.00017962935,"threshold_uncertainty_score":0.007198751},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9971475,0.000058123052,0.002363818,0.000020679714,0.000004634515,0.000006483436,0.00001390432,0.000033746037,0.00035112607],"genre_scores_gemma":[0.99905723,0.000025680476,0.0006811243,0.0000071582,0.0000015526483,0.0000050499325,0.000016060734,0.000004708357,0.0002014207],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998951,0.000009700537,0.0000039141864,0.000020627012,0.00003816806,0.000032514938],"domain_scores_gemma":[0.99971396,0.00012285565,0.000057861253,0.000010707472,0.00003979432,0.000054727054],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012277652,0.00016100206,0.00020564669,0.00016765801,0.00027702653,0.00028249022,0.00018111321,0.00030612777,0.0007727956],"category_scores_gemma":[0.0004908024,0.0001232979,0.00011952675,0.0000942678,0.00049754156,0.000316126,0.00041426084,0.00036057012,0.000066825276],"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":[0.00033710027,0.000042079682,0.0023300124,0.00004182056,0.0000070449746,0.00041336,0.00022710778,0.0037000084,0.98818797,0.000578543,0.000067788635,0.0040670703],"study_design_scores_gemma":[0.000055640772,0.0011946217,0.04196021,0.000017618207,0.000022537835,0.00037683363,0.000535097,0.16874953,0.78536755,0.0006279803,0.001033989,0.000058353973],"about_ca_topic_score_codex":0.001103774,"about_ca_topic_score_gemma":0.000917476,"teacher_disagreement_score":0.001103774,"about_ca_system_score_codex":0.00025007848,"about_ca_system_score_gemma":0.00015942124,"threshold_uncertainty_score":0.0025852919},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9975866,0.00014236839,0.0017287148,0.000010728767,0.0000122043675,0.000006696402,0.000064994834,0.000065123895,0.00038260437],"genre_scores_gemma":[0.99706346,0.00008745519,0.0019526737,0.000008590711,0.000005829937,0.0000106303105,0.000079049576,0.000026159007,0.00076607504],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99951804,0.000050857943,0.00003448863,0.00015484261,0.00018059101,0.00006114436],"domain_scores_gemma":[0.99822634,0.00046174525,0.00070979074,0.00019015366,0.00031777428,0.00009426693],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005981948,0.00045055585,0.00032164194,0.0003502629,0.00011577784,0.00055523426,0.0003905955,0.0004842385,0.001233665],"category_scores_gemma":[0.001861473,0.00044491867,0.00026827047,0.00032761678,0.0005333658,0.00049861457,0.0004028113,0.00027149994,0.00048381815],"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":[0.00034406694,0.00003581258,0.0023015528,0.000081840524,0.000021940155,0.00012013439,0.00025477362,0.0030934457,0.9896852,0.00018822412,0.00011691873,0.0037561199],"study_design_scores_gemma":[0.00010619202,0.0033967143,0.02987545,0.00003422901,0.000116068564,0.0006181076,0.00060745206,0.034796845,0.92597973,0.00013739936,0.0042245607,0.00010720837],"about_ca_topic_score_codex":0.00034058126,"about_ca_topic_score_gemma":0.0002605747,"teacher_disagreement_score":0.001233665,"about_ca_system_score_codex":0.00019388602,"about_ca_system_score_gemma":0.00008260564,"threshold_uncertainty_score":0.0041270256},"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":"other","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.1537865,0.012692246,0.19519693,0.006568255,0.0022352925,0.00012833063,0.00025445552,0.00020465505,0.62893337],"genre_scores_gemma":[0.92458487,0.005076821,0.021370124,0.0011476866,0.0016945645,0.00012675983,0.00014219338,0.000053260923,0.045803692],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.99977344,0.000067322064,0.000010696801,0.000031872434,0.00008956048,0.00002713911],"domain_scores_gemma":[0.9996332,0.0001667558,0.000052585707,0.0000326325,0.00008774927,0.000027105276],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002750745,0.00024754208,0.00018759591,0.0011926577,0.0004026637,0.0012407446,0.00044235148,0.0007871752,0.007846982],"category_scores_gemma":[0.0014821923,0.00011638808,0.00020137824,0.00075467775,0.0017119234,0.0016917808,0.0008714354,0.0008514199,0.00045724094],"study_design_candidate":"theoretical_or_conceptual","study_design_consensus":"theoretical_or_conceptual","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000028863815,0.000022229013,0.00045029467,0.000078092555,0.0000056703952,0.00023442596,0.00029508694,0.001831702,0.0022229014,0.9759645,0.0022103752,0.016655894],"study_design_scores_gemma":[0.00003618076,0.00006643094,0.0028734305,0.00012979348,0.0000074034647,0.0006628864,0.0004484369,0.016449519,0.0011689728,0.89984685,0.078292035,0.000018038618],"about_ca_topic_score_codex":0.00044070353,"about_ca_topic_score_gemma":0.00020453772,"teacher_disagreement_score":0.007846982,"about_ca_system_score_codex":0.0003809195,"about_ca_system_score_gemma":0.00021835903,"threshold_uncertainty_score":0.02625078},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.16821872,0.00045068967,0.81380063,0.0003546655,0.0002693222,0.00010804984,0.00007016275,0.00036517548,0.016362589],"genre_scores_gemma":[0.9842487,0.00007734898,0.013469496,0.000038835653,0.000040481096,0.000040725663,0.000020947347,0.00004415462,0.0020193195],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99962604,0.00010508228,0.00001472846,0.000078212455,0.0000710518,0.00010485444],"domain_scores_gemma":[0.99941814,0.00030634616,0.000068531495,0.000024277288,0.00012861744,0.00005413558],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005741836,0.0012440473,0.0012652038,0.0004279493,0.00040022098,0.0010773117,0.00049443234,0.0010187785,0.002467942],"category_scores_gemma":[0.0021722142,0.00045152838,0.00043600012,0.00027158565,0.0008069033,0.000556459,0.0010019295,0.0004859783,0.00021064331],"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":[0.00042255368,0.00010823612,0.00028914458,0.00012072401,0.000039015533,0.00008006689,0.000044053155,0.96484494,0.012749477,0.004061246,0.00053331145,0.016707215],"study_design_scores_gemma":[0.000017657196,0.000072832154,0.00011569304,0.0000032424207,0.000008912266,0.0000063707557,0.0000064262535,0.9985233,0.0007096063,0.00038536938,0.00014514009,0.000005474062],"about_ca_topic_score_codex":0.0030464313,"about_ca_topic_score_gemma":0.0016538736,"teacher_disagreement_score":0.0030464313,"about_ca_system_score_codex":0.00045574966,"about_ca_system_score_gemma":0.0008227861,"threshold_uncertainty_score":0.008256078},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99651706,0.00029854436,0.0022852304,0.000021661426,0.000038418122,0.00002085087,0.00007303095,0.00005530553,0.0006898147],"genre_scores_gemma":[0.99784374,0.00016525219,0.0015870081,0.000023562057,0.00000823535,0.000010550797,0.000046189187,0.00002535046,0.000290132],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9995926,0.00005491478,0.00003953206,0.00007356543,0.00014063116,0.000098814184],"domain_scores_gemma":[0.9976654,0.0013277734,0.00037114095,0.00017708584,0.0003100922,0.00014847655],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00070253754,0.0005764312,0.0004450003,0.00038041038,0.0003044028,0.0011293079,0.0002846102,0.00049000495,0.0014626349],"category_scores_gemma":[0.002684803,0.0004439637,0.00028970145,0.00023270037,0.0005350314,0.00056199514,0.0004914377,0.00058414525,0.00019510853],"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":[0.0010601627,0.00008266932,0.0026158362,0.00011504434,0.000019081861,0.00028077228,0.00006272432,0.003921703,0.9871057,0.00010323626,0.000043119828,0.0045900512],"study_design_scores_gemma":[0.00009929111,0.002209256,0.024560478,0.00004704726,0.000096895346,0.0001875385,0.00017209073,0.009497679,0.96246266,0.000080570506,0.00053526746,0.000051192488],"about_ca_topic_score_codex":0.000455312,"about_ca_topic_score_gemma":0.0004022472,"teacher_disagreement_score":0.0014626349,"about_ca_system_score_codex":0.00024869677,"about_ca_system_score_gemma":0.00026699388,"threshold_uncertainty_score":0.004893005},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98264503,0.0002127068,0.016465215,0.000028277129,0.000016082195,0.000014617723,0.000011353112,0.00013209872,0.00047449427],"genre_scores_gemma":[0.99160707,0.00008238525,0.00795978,0.00000939926,0.000009658805,0.00001267382,0.000009599922,0.0000152069,0.0002942549],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998311,0.00004482023,0.000009673633,0.00003012499,0.000045361703,0.000038860282],"domain_scores_gemma":[0.9992611,0.00031279348,0.00023674879,0.000052828316,0.00009082578,0.000045825996],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004426183,0.00031471867,0.00033826326,0.00024378239,0.00013487735,0.00016778131,0.00029488487,0.00023492273,0.0004983102],"category_scores_gemma":[0.0006750125,0.00018460829,0.00016302327,0.00012609562,0.00043109077,0.00025153477,0.0003994617,0.0001959682,0.00013088882],"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":[0.00012210904,0.000019069723,0.0004421659,0.0000463976,0.0000036203733,0.00008982965,0.00007584041,0.0008794832,0.99292046,0.00014931137,0.000028504886,0.0052231564],"study_design_scores_gemma":[0.00003784321,0.000966823,0.0023546848,0.0000102756385,0.000012224754,0.00010898298,0.000046525267,0.01562289,0.9801107,0.000078282785,0.0006375666,0.000013205536],"about_ca_topic_score_codex":0.00011641117,"about_ca_topic_score_gemma":0.00017938443,"teacher_disagreement_score":0.0004983102,"about_ca_system_score_codex":0.00010930014,"about_ca_system_score_gemma":0.00014561924,"threshold_uncertainty_score":0.0023408532},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98649675,0.00019781562,0.0112744905,0.000020830594,0.00002282983,0.000013147154,0.000025556836,0.000059410773,0.0018892259],"genre_scores_gemma":[0.99685246,0.00007873239,0.0018220103,0.00000926107,0.0000055783185,0.000006475068,0.000026277827,0.000011523402,0.0011876853],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99985373,0.000010998603,0.0000058828905,0.000029132214,0.00006765761,0.0000326033],"domain_scores_gemma":[0.99980026,0.00006101545,0.000050427192,0.000023092822,0.00004214961,0.000022980317],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00010742257,0.00022392305,0.00023242542,0.00018434513,0.00014216537,0.00025352085,0.00026052553,0.00019399828,0.0014401528],"category_scores_gemma":[0.0003528876,0.00012230911,0.00014123092,0.00012052707,0.00033889737,0.00022614417,0.000290087,0.00019601232,0.00015402434],"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":[0.000117403775,0.000017863233,0.00056035316,0.0000417358,0.0000045365973,0.000077971774,0.000047634425,0.0013536928,0.9883535,0.00017131776,0.00003493768,0.009218993],"study_design_scores_gemma":[0.000029319495,0.0004861446,0.013969201,0.0000126211435,0.000013100565,0.00017283177,0.0001564847,0.026239386,0.9571706,0.0002125119,0.0015203186,0.000017385548],"about_ca_topic_score_codex":0.00033623385,"about_ca_topic_score_gemma":0.00043630594,"teacher_disagreement_score":0.0014401528,"about_ca_system_score_codex":0.00014130621,"about_ca_system_score_gemma":0.00010602986,"threshold_uncertainty_score":0.0048178434},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.65086704,0.00015824311,0.33998296,0.000114572176,0.00015206703,0.0029341714,0.00043510945,0.0012316755,0.0041241385],"genre_scores_gemma":[0.8901683,0.00010730639,0.10636436,0.000032848046,0.000011674582,0.0012127733,0.00030424286,0.000062859486,0.0017356841],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99902344,0.00018654246,0.00007605722,0.00010925137,0.00046263248,0.00014202505],"domain_scores_gemma":[0.99803835,0.00027994142,0.00019146467,0.00020688964,0.0008493394,0.00043409606],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0023030152,0.00074399175,0.00046944144,0.00061646634,0.00056414405,0.00078234094,0.0012822803,0.00078805414,0.0013976817],"category_scores_gemma":[0.0017682473,0.0004188278,0.00028669686,0.00019775535,0.000507268,0.0005930544,0.0006443089,0.00045080046,0.00032302696],"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":[0.00235981,0.002088144,0.026489867,0.0011685862,0.000083820894,0.0008483035,0.0004127442,0.16173956,0.71701294,0.0025620896,0.0011180331,0.08411613],"study_design_scores_gemma":[0.0013349729,0.034160376,0.06898794,0.00022475791,0.00024707767,0.0011061342,0.00062042027,0.47563112,0.39939487,0.00077551464,0.017276315,0.00024049619],"about_ca_topic_score_codex":0.00092703773,"about_ca_topic_score_gemma":0.0012003977,"teacher_disagreement_score":0.0023030152,"about_ca_system_score_codex":0.0004182788,"about_ca_system_score_gemma":0.0020327023,"threshold_uncertainty_score":0.012179673},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9984164,0.00008872496,0.001275557,0.0000030034248,0.000008213942,0.0000038020037,0.000015409589,0.00001097,0.00017785392],"genre_scores_gemma":[0.99899584,0.00006398268,0.0008033795,0.000004695759,0.0000017013384,0.0000028980896,0.000023710085,0.0000064710316,0.00009745128],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99978834,0.000018650724,0.000017722225,0.00004839679,0.000075207376,0.000051643943],"domain_scores_gemma":[0.9995111,0.0001276939,0.00015951163,0.000035310095,0.000102752994,0.000063567444],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00031062737,0.00025832,0.00039163054,0.00012645515,0.00017184463,0.00058023824,0.00016598529,0.00019431522,0.00047220988],"category_scores_gemma":[0.00069027895,0.0002562008,0.00019324927,0.00018256163,0.0002754088,0.00032481528,0.0003259326,0.00032429607,0.000059310772],"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":[0.00014059487,0.000016264159,0.0017147141,0.000022458202,0.0000033638873,0.00008885153,0.000036635636,0.0010196501,0.99551255,0.00007398619,0.000010113508,0.0013607637],"study_design_scores_gemma":[0.000038734383,0.000611906,0.046368595,0.000010401791,0.00003972751,0.00016699114,0.00015609809,0.01779939,0.9342581,0.000084278894,0.0004308638,0.000034904442],"about_ca_topic_score_codex":0.00041680786,"about_ca_topic_score_gemma":0.00043484746,"teacher_disagreement_score":0.00058023824,"about_ca_system_score_codex":0.00027685758,"about_ca_system_score_gemma":0.0002161179,"threshold_uncertainty_score":0.0020087957},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98688114,0.00071948837,0.011339211,0.000018893961,0.000040461284,0.000028502787,0.00007095206,0.00009742455,0.00080392277],"genre_scores_gemma":[0.9900423,0.00030504403,0.009068759,0.000005846791,0.00001106565,0.00001496052,0.00008491141,0.00003468878,0.00043226028],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9994099,0.000059984344,0.000056242912,0.000110133195,0.00027452296,0.0000893022],"domain_scores_gemma":[0.99877924,0.00043708223,0.00023593451,0.000099606616,0.00033179385,0.00011622271],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0009859909,0.00044892202,0.0006461593,0.00073380256,0.000358063,0.0011789331,0.00033208434,0.00035192256,0.0008049387],"category_scores_gemma":[0.0018437866,0.00022804004,0.00032162416,0.00069528015,0.00039247723,0.0006596898,0.00044040888,0.00034517207,0.0001022583],"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":[0.0008820512,0.00015921674,0.006481275,0.0002014161,0.00004295772,0.00033635876,0.00017828622,0.011252546,0.9519007,0.00058473943,0.00014156075,0.027838796],"study_design_scores_gemma":[0.000038368675,0.0011466312,0.015737997,0.000015594576,0.00007899997,0.000213888,0.00018396179,0.093077414,0.88838845,0.00016550254,0.00090005615,0.00005317938],"about_ca_topic_score_codex":0.00061428046,"about_ca_topic_score_gemma":0.00064504065,"teacher_disagreement_score":0.0011789331,"about_ca_system_score_codex":0.00026782783,"about_ca_system_score_gemma":0.00023889837,"threshold_uncertainty_score":0.0052145123},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9968733,0.00005350859,0.0020478938,0.00002233256,0.000009510175,0.000013809381,0.00006742827,0.000027260143,0.00088500645],"genre_scores_gemma":[0.9988181,0.00003312397,0.0007281855,0.000006377318,0.000006088205,0.000010305547,0.000046205772,0.000007635838,0.0003440118],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9996468,0.00007849863,0.000018472427,0.00006386302,0.00010325952,0.00008901085],"domain_scores_gemma":[0.9981944,0.0010871508,0.00015246154,0.00013130729,0.00032066528,0.00011404803],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00060474884,0.000364105,0.00030668455,0.000339482,0.00067267107,0.0004019672,0.00047316373,0.00052607455,0.0047819167],"category_scores_gemma":[0.001755311,0.00025718904,0.0001451843,0.00021032842,0.0013523638,0.00061057427,0.00065440784,0.00041955113,0.00029740192],"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":[0.001924662,0.0005421068,0.0041673845,0.00009526114,0.000008631217,0.00020500389,0.00029275025,0.0019337941,0.9841583,0.0006847917,0.00011977814,0.005867465],"study_design_scores_gemma":[0.00051387737,0.0052397177,0.044043873,0.000047780177,0.000047242527,0.0006202787,0.00084833853,0.033960525,0.9123014,0.0007720057,0.0015337713,0.0000711985],"about_ca_topic_score_codex":0.000563089,"about_ca_topic_score_gemma":0.0005869038,"teacher_disagreement_score":0.0047819167,"about_ca_system_score_codex":0.00022000539,"about_ca_system_score_gemma":0.0002842392,"threshold_uncertainty_score":0.015997171},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8982115,0.0011202962,0.06923014,0.0007398112,0.0001794047,0.00025874714,0.0014274991,0.00074781914,0.028084796],"genre_scores_gemma":[0.97426075,0.000307635,0.02323736,0.00006922398,0.000029008908,0.00013698939,0.0004941931,0.00009702605,0.0013677374],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99957305,0.00011479038,0.000024841502,0.00003509065,0.00020468401,0.00004751198],"domain_scores_gemma":[0.9981323,0.0012230641,0.00014771454,0.00010695412,0.00030851338,0.00008149035],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00063951133,0.00080932735,0.0006186904,0.0006581945,0.0006308528,0.0009822181,0.00081506255,0.001088623,0.0024501465],"category_scores_gemma":[0.0029443635,0.00032803338,0.00057452655,0.00049405335,0.0006130408,0.0005480732,0.00059506635,0.0007348915,0.0002998261],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00012717849,0.00012946123,0.0036141353,0.00010485229,0.00002187552,0.00013986205,0.00007978393,0.9847371,0.0049193082,0.0010915559,0.00035328168,0.0046816035],"study_design_scores_gemma":[0.000009499228,0.00004184207,0.0007441556,0.000010509894,0.0000031288641,0.00001635978,0.000025441357,0.9977258,0.000965879,0.00016362284,0.00028629173,0.000007487903],"about_ca_topic_score_codex":0.00722293,"about_ca_topic_score_gemma":0.0052274778,"teacher_disagreement_score":0.00722293,"about_ca_system_score_codex":0.0006087425,"about_ca_system_score_gemma":0.00063998083,"threshold_uncertainty_score":0.014361739},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99699116,0.00013444311,0.0026009355,0.0000047952963,0.000011711264,0.000011734542,0.000045081568,0.00002314145,0.00017700887],"genre_scores_gemma":[0.9966444,0.000107623455,0.002931006,0.0000057038233,0.000007084936,0.000011433552,0.00007787482,0.000018469289,0.00019638315],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99918026,0.00010495351,0.000078800804,0.00020026232,0.00034072818,0.00009484934],"domain_scores_gemma":[0.99762136,0.0010628832,0.0005651461,0.00025214686,0.00034273628,0.00015576954],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0007512831,0.00036322165,0.00044942554,0.00028816736,0.00024641393,0.00049441843,0.00043466076,0.00034589414,0.0011121639],"category_scores_gemma":[0.0027218382,0.0003142815,0.0002370754,0.00038007525,0.00047348294,0.0004580801,0.00043288953,0.00031533136,0.00010282554],"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":[0.0007603541,0.00006565708,0.0028638288,0.000082530976,0.00001109216,0.00016863795,0.00010916012,0.0023616967,0.9895845,0.00009981393,0.000022145692,0.0038707084],"study_design_scores_gemma":[0.0000448457,0.0022468169,0.01913398,0.000007795437,0.000035078818,0.0002584327,0.00008551336,0.009935734,0.96775603,0.000069815,0.00038714998,0.000038781454],"about_ca_topic_score_codex":0.00022370071,"about_ca_topic_score_gemma":0.00024428288,"teacher_disagreement_score":0.0011121639,"about_ca_system_score_codex":0.00024364576,"about_ca_system_score_gemma":0.00019267267,"threshold_uncertainty_score":0.0039732456},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.96634096,0.0004005669,0.02268058,0.0002706564,0.0000759629,0.000070638336,0.000251185,0.00016803898,0.009741428],"genre_scores_gemma":[0.9909402,0.00014566667,0.006769341,0.00002692592,0.0000168758,0.000028804245,0.00009784056,0.000020658566,0.001953566],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99975985,0.000053328953,0.000016234611,0.000035306082,0.000082810766,0.000052464628],"domain_scores_gemma":[0.99892896,0.0007286151,0.00013569153,0.000048445145,0.00011278893,0.000045526198],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00048125893,0.0005199832,0.00054681645,0.00080132997,0.00066003815,0.0005615173,0.00050522893,0.0010911672,0.0011379513],"category_scores_gemma":[0.0018334395,0.00020361131,0.0005877292,0.00053917017,0.0009865331,0.00040232946,0.00043580274,0.00048356366,0.00012253066],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00017372785,0.0001418764,0.006401243,0.00012616774,0.000032199277,0.0004933476,0.00018552675,0.96438384,0.02057008,0.0021968745,0.00026612,0.005028909],"study_design_scores_gemma":[0.000012429101,0.000091760274,0.0022186409,0.00001272874,0.0000082441975,0.00007065465,0.00006689537,0.99415624,0.0028206948,0.00028723542,0.00024027795,0.000014229623],"about_ca_topic_score_codex":0.009657607,"about_ca_topic_score_gemma":0.005046951,"teacher_disagreement_score":0.009657607,"about_ca_system_score_codex":0.0005423093,"about_ca_system_score_gemma":0.00045967384,"threshold_uncertainty_score":0.019202828},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9931543,0.00015196162,0.0056296582,0.000029546945,0.00001776763,0.0000104241435,0.00010956759,0.0000522546,0.0008445401],"genre_scores_gemma":[0.9967913,0.00007594897,0.0024724188,0.00001549172,0.000011110611,0.000010479383,0.00007505204,0.000025093557,0.00052300544],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9996475,0.000056909317,0.000014511273,0.00008078007,0.00015125291,0.000049098497],"domain_scores_gemma":[0.9993018,0.00026446566,0.00013659525,0.000082448954,0.00012458827,0.00009001261],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00041856102,0.0004027708,0.0002993762,0.0004410498,0.00047006633,0.0005265398,0.0003481954,0.0005306845,0.0007320522],"category_scores_gemma":[0.00095236633,0.00033616013,0.0001511719,0.00043847464,0.00069069973,0.00057880045,0.00043098105,0.00061509246,0.00020217436],"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":[0.00051675213,0.000048999515,0.0025339662,0.000016005615,0.0000060513044,0.000028915945,0.000069219175,0.00025701246,0.99351066,0.00023456418,0.000046609905,0.0027313202],"study_design_scores_gemma":[0.000051678246,0.00025498128,0.020561915,0.000003495733,0.000016467893,0.00015335287,0.0000556886,0.007278376,0.9710349,0.00019402042,0.00037568895,0.000019551071],"about_ca_topic_score_codex":0.00088376045,"about_ca_topic_score_gemma":0.0005351515,"teacher_disagreement_score":0.00088376045,"about_ca_system_score_codex":0.0002928081,"about_ca_system_score_gemma":0.00020613453,"threshold_uncertainty_score":0.002448976},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97415924,0.000067146786,0.022024553,0.00007388246,0.000029480625,0.00001891139,0.00005800627,0.00010136725,0.0034674096],"genre_scores_gemma":[0.99834895,0.000020296113,0.0009381257,0.000005741545,0.000004526425,0.000005784469,0.00002669574,0.000008381398,0.0006414302],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999182,0.000021147713,0.000003214458,0.000014223096,0.000023977444,0.00001924016],"domain_scores_gemma":[0.999785,0.00010585482,0.000021868182,0.000011627957,0.000046833684,0.000028836781],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002324511,0.00056455657,0.0003920704,0.00030324995,0.0004134495,0.0004506542,0.00042460262,0.00083616684,0.0005749566],"category_scores_gemma":[0.0005335743,0.0002232954,0.0005666774,0.00014238215,0.00052793237,0.00029252685,0.00031675686,0.0003918389,0.000107125205],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0001076542,0.000054360127,0.003771731,0.000025221723,0.000010334345,0.00024404422,0.00006747044,0.98264664,0.009387063,0.0008377968,0.00016000446,0.0026877206],"study_design_scores_gemma":[0.0000031519533,0.000018735294,0.00077932293,8.5531815e-7,0.0000018890854,0.000009935721,0.000008273059,0.9984676,0.0006240829,0.000053350715,0.00002985139,0.000002984622],"about_ca_topic_score_codex":0.012495041,"about_ca_topic_score_gemma":0.0048108324,"teacher_disagreement_score":0.012495041,"about_ca_system_score_codex":0.00042595807,"about_ca_system_score_gemma":0.0004267742,"threshold_uncertainty_score":0.024844646},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9868536,0.000029565452,0.010341671,0.000051940377,0.0000067530186,0.000013158659,0.00006137753,0.00010684237,0.0025351045],"genre_scores_gemma":[0.99847466,0.000008356297,0.0011795653,0.0000052524883,0.000001355238,0.0000057331627,0.00003332334,0.000008314065,0.00028351726],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99995387,0.000008793841,0.0000017259417,0.0000066572884,0.000018091794,0.000010948643],"domain_scores_gemma":[0.99976665,0.00012461841,0.000026168886,0.000011025506,0.000042489097,0.000028918566],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00014990657,0.00021115267,0.00016873736,0.00036581472,0.00032014563,0.0002708084,0.00022614871,0.00034770448,0.0013064619],"category_scores_gemma":[0.00059317,0.00009673756,0.00023440787,0.00012060639,0.00033521204,0.00020261356,0.00016697122,0.00022880688,0.00008131405],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00018591837,0.00012558325,0.009964451,0.00007377113,0.000034585693,0.00029179215,0.00019452086,0.91928035,0.059000243,0.0020242245,0.0003563374,0.008468172],"study_design_scores_gemma":[0.000005236092,0.000030004425,0.0024912255,0.0000015438261,0.0000031660854,0.000020265506,0.000024006677,0.9955884,0.0016456278,0.00011898529,0.00006692814,0.0000045972133],"about_ca_topic_score_codex":0.0051019965,"about_ca_topic_score_gemma":0.0032507665,"teacher_disagreement_score":0.0051019965,"about_ca_system_score_codex":0.00038022947,"about_ca_system_score_gemma":0.00024872122,"threshold_uncertainty_score":0.010144651},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6725217,0.00012764578,0.31989902,0.000082930965,0.00009984389,0.002550909,0.0007318245,0.0008340595,0.0031520783],"genre_scores_gemma":[0.89319927,0.00010696374,0.10275837,0.000035079735,0.00001170559,0.001227355,0.0004711667,0.00005528488,0.002134729],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99923575,0.000096893484,0.000061322986,0.000081661936,0.00041839285,0.00010601382],"domain_scores_gemma":[0.99835134,0.00025535547,0.00021021038,0.00019066197,0.0006700538,0.00032249765],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0014555778,0.0006712218,0.00045107192,0.00057975505,0.0005325475,0.0006851302,0.0009854101,0.0006786983,0.0012334002],"category_scores_gemma":[0.0011731711,0.00037659353,0.0002676305,0.00020646479,0.0005374413,0.0003928802,0.00046557194,0.00045150772,0.00030768558],"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":[0.0007425924,0.00059203355,0.0153635135,0.0005494243,0.000027600705,0.00053538574,0.00032272466,0.044742655,0.9035041,0.0013202309,0.0006485672,0.031651177],"study_design_scores_gemma":[0.0004611639,0.0148196835,0.07743369,0.00015277155,0.00011756836,0.0009996813,0.0004492433,0.19042963,0.69822836,0.00053928274,0.016206132,0.00016280665],"about_ca_topic_score_codex":0.0009369971,"about_ca_topic_score_gemma":0.0014782703,"teacher_disagreement_score":0.0014555778,"about_ca_system_score_codex":0.000361379,"about_ca_system_score_gemma":0.0016231579,"threshold_uncertainty_score":0.0076978803},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.314907,0.003972879,0.6431203,0.00030605475,0.0004366778,0.00024678648,0.00014334843,0.0007600986,0.036106836],"genre_scores_gemma":[0.86351824,0.0013099988,0.12775758,0.000060339065,0.00003290442,0.0001572581,0.00014108467,0.000054335804,0.0069682146],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99989855,0.000013769065,0.0000040826576,0.000017071286,0.000043282325,0.000023218276],"domain_scores_gemma":[0.99991846,0.000008984908,0.000021559965,0.0000057923476,0.000031272968,0.0000140082275],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021120258,0.0004920278,0.00034423714,0.00043891082,0.00031548322,0.00066369766,0.0005082512,0.00052775576,0.0014697354],"category_scores_gemma":[0.00013938079,0.0002044917,0.0005394318,0.00013557299,0.00018163255,0.00039401161,0.00027783038,0.00026658026,0.00047580758],"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":[0.00031005117,0.00021739247,0.0039901766,0.0008824385,0.00013608731,0.00078221335,0.00013302287,0.27911288,0.5656202,0.017690899,0.0023118467,0.1288128],"study_design_scores_gemma":[0.000086908774,0.0027031165,0.009969407,0.0001463278,0.00026993,0.0011181439,0.00033666004,0.8334488,0.09236989,0.006111928,0.05332643,0.00011234279],"about_ca_topic_score_codex":0.0007467993,"about_ca_topic_score_gemma":0.0014374015,"teacher_disagreement_score":0.0014697354,"about_ca_system_score_codex":0.00026315651,"about_ca_system_score_gemma":0.0005139477,"threshold_uncertainty_score":0.0049167275},"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":"review","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.05011225,0.514349,0.36690545,0.012643082,0.002458518,0.000090677255,0.0012051931,0.0027572892,0.049478535],"genre_scores_gemma":[0.44953611,0.41075018,0.11444503,0.0017372868,0.0031073056,0.0002169374,0.0029618281,0.0008165988,0.016428798],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994892,0.0001076415,0.00002807806,0.00008558593,0.00024600266,0.000043430708],"domain_scores_gemma":[0.9984119,0.00051069143,0.000114380404,0.00012891692,0.0007052026,0.00012890229],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.002768724,0.0013421157,0.0009191866,0.0007770398,0.00023334399,0.0019940927,0.0020453425,0.0014233291,0.0049189525],"category_scores_gemma":[0.0024710733,0.0005033272,0.0006704965,0.0005811944,0.0007729186,0.002915459,0.0010539,0.0015732679,0.0029845994],"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":[0.00040188665,0.0002598304,0.005783425,0.0030531662,0.00014231924,0.00020509496,0.00027314233,0.29115722,0.009003788,0.05645978,0.022721043,0.6105393],"study_design_scores_gemma":[0.000059452897,0.00035599197,0.0036467542,0.0033416152,0.00012608549,0.00014595379,0.0003922184,0.6010785,0.00815905,0.11196434,0.27053496,0.00019507656],"about_ca_topic_score_codex":0.0018681048,"about_ca_topic_score_gemma":0.0014225208,"teacher_disagreement_score":0.0049189525,"about_ca_system_score_codex":0.000691356,"about_ca_system_score_gemma":0.0010978145,"threshold_uncertainty_score":0.01645559},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9231308,0.00006211026,0.06613605,0.00012567238,0.000048037855,0.00015880933,0.0011946261,0.0016637067,0.007480044],"genre_scores_gemma":[0.97690195,0.000037006874,0.020104038,0.000017598648,0.0000042345173,0.00007667461,0.0009699491,0.00008488295,0.0018037481],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995944,0.00007984568,0.000025093068,0.0000883871,0.00017020786,0.000042034884],"domain_scores_gemma":[0.9988869,0.00036914373,0.000064475134,0.00014825923,0.00049301726,0.000038378963],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0014054825,0.0007766315,0.00045271163,0.00042975828,0.00055650773,0.000591504,0.0011115464,0.0006339454,0.0015949954],"category_scores_gemma":[0.002178927,0.00024309306,0.00039535956,0.0003941318,0.0003003611,0.00055554375,0.00052905746,0.000849856,0.00044410894],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00033027804,0.00029725092,0.010913211,0.0000821724,0.00003797402,0.00011876579,0.00016715661,0.92590404,0.023132784,0.0009808701,0.0009523039,0.03708323],"study_design_scores_gemma":[0.00004907972,0.00012790428,0.0034904967,0.0000066142093,0.000008895623,0.000016519156,0.000049032005,0.9885875,0.006786483,0.00011233947,0.0007496179,0.000015474092],"about_ca_topic_score_codex":0.0930546,"about_ca_topic_score_gemma":0.06756653,"teacher_disagreement_score":0.0930546,"about_ca_system_score_codex":0.0008757059,"about_ca_system_score_gemma":0.0017246538,"threshold_uncertainty_score":0.18502593},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9987827,0.000032821335,0.0007882194,0.000007916568,0.000003674415,0.0000029670887,0.000033431326,0.000034134682,0.00031412698],"genre_scores_gemma":[0.998782,0.000026676034,0.0007126045,0.0000039541974,0.000001939116,0.000003510984,0.00005717766,0.000009672842,0.00040250868],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99994016,0.0000052143323,0.0000025049437,0.000013367939,0.000015043629,0.000023719487],"domain_scores_gemma":[0.99985135,0.000022019056,0.00006161232,0.000014993169,0.000020095822,0.00002981964],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000094452706,0.00018499648,0.00015748161,0.0001427123,0.00013969654,0.00025839882,0.00017032589,0.00013483697,0.0008252858],"category_scores_gemma":[0.00017108407,0.0001268906,0.0000984116,0.00011580587,0.0002770712,0.0001221492,0.0002047258,0.00026872227,0.00014642264],"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":[0.00015515578,0.000031482177,0.0021017736,0.000018837774,0.0000035742585,0.00023762038,0.000094479925,0.0015602425,0.99326986,0.0002760201,0.00006874799,0.002182235],"study_design_scores_gemma":[0.000026636242,0.0006958698,0.07280353,0.000007386339,0.000010105524,0.00031870182,0.0002361791,0.05466681,0.86962056,0.00013489473,0.0014463516,0.00003296202],"about_ca_topic_score_codex":0.00028375184,"about_ca_topic_score_gemma":0.0003429083,"teacher_disagreement_score":0.0008252858,"about_ca_system_score_codex":0.00016502295,"about_ca_system_score_gemma":0.00010365654,"threshold_uncertainty_score":0.0027608275},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9986504,0.00003999081,0.0010590515,0.000005799834,0.000005820929,0.00000761117,0.000054145505,0.00001901228,0.00015817184],"genre_scores_gemma":[0.9987612,0.00005236191,0.0008813896,0.0000046019254,0.0000025873223,0.000009083988,0.00006241212,0.0000058444325,0.00022050421],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99971706,0.000029776278,0.00002426848,0.00004289342,0.00013386559,0.000052082614],"domain_scores_gemma":[0.9994505,0.00022640587,0.00007591013,0.000057484478,0.00014744767,0.00004220335],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004162004,0.00026725265,0.0004748414,0.00022972935,0.00040919048,0.00032976017,0.00029075623,0.00025775537,0.0007978916],"category_scores_gemma":[0.00081556453,0.00011864601,0.00025395997,0.00034310287,0.00044196224,0.00035318686,0.00029014976,0.00036992837,0.000089471854],"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":[0.0006231667,0.0001822483,0.007378168,0.00013747565,0.000013391929,0.00026195543,0.00026584222,0.0057752235,0.97600013,0.0001401585,0.000080105434,0.009142185],"study_design_scores_gemma":[0.000075275835,0.0028901799,0.026533028,0.000011830241,0.000032418742,0.000119674376,0.00034431825,0.04693335,0.9223729,0.00010368616,0.000548369,0.000034829955],"about_ca_topic_score_codex":0.0008607087,"about_ca_topic_score_gemma":0.000907018,"teacher_disagreement_score":0.0008607087,"about_ca_system_score_codex":0.00025282157,"about_ca_system_score_gemma":0.00016312138,"threshold_uncertainty_score":0.0026692152},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.949247,0.0001337314,0.046586063,0.0000544114,0.000030456287,0.0000155297,0.000075916425,0.000116471536,0.0037405007],"genre_scores_gemma":[0.9957606,0.000057910787,0.0027994013,0.000011197893,0.000011166881,0.0000041812596,0.00004370131,0.000017331633,0.0012945313],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999218,0.000015914668,0.0000030110357,0.000013680628,0.00003321764,0.000012388412],"domain_scores_gemma":[0.9998037,0.00006971198,0.000031689124,0.00001411334,0.000055461005,0.00002533247],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001547529,0.00030257995,0.00019446312,0.00038787082,0.00020600407,0.00024900402,0.000260274,0.00026775303,0.0011198343],"category_scores_gemma":[0.00031175063,0.00011210735,0.00021161683,0.00022103968,0.0002740507,0.00024839275,0.00024881086,0.00023290057,0.00013704353],"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":[0.0018035171,0.00030359122,0.020855526,0.0001544785,0.0000821118,0.0025716063,0.00044202773,0.15116541,0.7567872,0.006275014,0.00068880426,0.058870777],"study_design_scores_gemma":[0.000016224947,0.00019645193,0.04791949,0.000011432213,0.000026095451,0.00040236078,0.00016643587,0.9273559,0.022583673,0.00065257546,0.00063526473,0.000034110828],"about_ca_topic_score_codex":0.0009696522,"about_ca_topic_score_gemma":0.0008886483,"teacher_disagreement_score":0.0011198343,"about_ca_system_score_codex":0.00011986986,"about_ca_system_score_gemma":0.00012984176,"threshold_uncertainty_score":0.003746152},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.95013696,0.00006511221,0.0470838,0.000049093764,0.000024114528,0.000020049116,0.000028279394,0.00010227922,0.002490389],"genre_scores_gemma":[0.9962501,0.000041715924,0.0031894867,0.0000068776253,0.0000025079107,0.000008248571,0.000017515446,0.00000500282,0.00047853548],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999349,0.000014030478,0.0000028639906,0.000013275887,0.000022745084,0.000012158195],"domain_scores_gemma":[0.9999114,0.000020256894,0.00002226918,0.000011183666,0.000019799083,0.000015089549],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00011099472,0.0006349201,0.00032053777,0.00019218956,0.00021090216,0.00024973942,0.0002821777,0.0003217775,0.00049111363],"category_scores_gemma":[0.00023737329,0.00013274516,0.0003805876,0.00008944745,0.0004025328,0.00026474902,0.00023568889,0.00015876499,0.0000687588],"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":[0.0001730956,0.000100152734,0.0032865682,0.000063577405,0.00003073482,0.00029147152,0.00007833672,0.8033965,0.18366542,0.0017984794,0.0001652432,0.0069503137],"study_design_scores_gemma":[0.000016914582,0.00020354477,0.0010942993,0.0000029664827,0.000013278811,0.000020353767,0.000022849681,0.98784524,0.010368603,0.00020836215,0.0001923174,0.0000111175505],"about_ca_topic_score_codex":0.002812129,"about_ca_topic_score_gemma":0.001553778,"teacher_disagreement_score":0.002812129,"about_ca_system_score_codex":0.00019606185,"about_ca_system_score_gemma":0.00029345482,"threshold_uncertainty_score":0.0055915713},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.3026999,0.00054967974,0.6869596,0.00022384294,0.0001303512,0.00014953219,0.00023275136,0.0029029944,0.0061513474],"genre_scores_gemma":[0.7633927,0.0002614294,0.23358232,0.000041600873,0.000038172737,0.00015416012,0.00025023066,0.0002462288,0.0020331573],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9990576,0.00022749491,0.000056033063,0.000110030756,0.00049150526,0.00005742616],"domain_scores_gemma":[0.9955641,0.0029478155,0.0002768564,0.00026774255,0.0008488202,0.00009469635],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0015450675,0.0012019995,0.00058302283,0.0008666472,0.00046162173,0.0009743126,0.0013280318,0.0009590993,0.0017055512],"category_scores_gemma":[0.0057519507,0.0003560652,0.00047109782,0.00045982504,0.00042828702,0.0006605501,0.0006679765,0.0008181425,0.00045148315],"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":[0.00027231977,0.00017401642,0.0035695606,0.00016281113,0.00005542858,0.000091040325,0.00011926931,0.8896541,0.015243084,0.0014548327,0.0004389098,0.0887647],"study_design_scores_gemma":[0.000015986752,0.000050198567,0.00027550323,0.0000078540015,0.0000051549373,0.000011999004,0.000016231632,0.9958171,0.0034176765,0.000121701385,0.00025178018,0.000008805432],"about_ca_topic_score_codex":0.008262098,"about_ca_topic_score_gemma":0.0064392095,"teacher_disagreement_score":0.008262098,"about_ca_system_score_codex":0.00054857804,"about_ca_system_score_gemma":0.0011762505,"threshold_uncertainty_score":0.016427994},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.94801193,0.00015782975,0.02742963,0.00013146058,0.000044783465,0.00006249349,0.00033637413,0.00024297653,0.023582565],"genre_scores_gemma":[0.9953441,0.0000396432,0.0025014463,0.000012588765,0.000006004661,0.00002777544,0.00012142081,0.000030208179,0.0019166856],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998024,0.00003889988,0.0000072794646,0.000024336423,0.00008189804,0.00004524919],"domain_scores_gemma":[0.9991297,0.00049331115,0.00009797999,0.00004556784,0.00017560572,0.000057834113],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00037976488,0.00041511157,0.0003866319,0.00039817626,0.00036385746,0.0005159943,0.0006370091,0.0008029255,0.001962315],"category_scores_gemma":[0.0019048813,0.00019848054,0.00042954943,0.00020386075,0.00059897214,0.00028491073,0.0004290655,0.00035604977,0.0003095262],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00014099128,0.000053798616,0.0019648392,0.000055990975,0.0000069362213,0.00015023138,0.00007233929,0.98120683,0.012798373,0.000876238,0.00023098117,0.0024423723],"study_design_scores_gemma":[0.000014571837,0.000040300452,0.0010880199,0.0000040595683,0.0000021688722,0.000012820771,0.000017988943,0.99628615,0.0023067908,0.00011948775,0.000101532765,0.00000618708],"about_ca_topic_score_codex":0.0050792806,"about_ca_topic_score_gemma":0.0026400618,"teacher_disagreement_score":0.0050792806,"about_ca_system_score_codex":0.00045610522,"about_ca_system_score_gemma":0.00042269903,"threshold_uncertainty_score":0.010099411},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99861264,0.00011590228,0.0006358039,0.000009025192,0.000015804713,0.0000018329654,0.000009059038,0.000018426235,0.0005814146],"genre_scores_gemma":[0.99964356,0.000025461033,0.0002066089,0.000003672444,0.0000040177697,7.1933243e-7,0.000008171609,0.0000079823685,0.00009982048],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99971133,0.000058489524,0.000022344851,0.000053115727,0.00007390138,0.00008086031],"domain_scores_gemma":[0.9979955,0.0012215496,0.00029577749,0.00007287409,0.00018718034,0.00022718805],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000395964,0.00026621885,0.00044574522,0.00038823445,0.00036912062,0.0008634495,0.0002728543,0.00026780536,0.001950901],"category_scores_gemma":[0.0016732439,0.00025537697,0.0002068654,0.0002856143,0.00033728755,0.00037180274,0.0004048225,0.00028313816,0.00017240875],"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":[0.004443738,0.00030589447,0.0076571917,0.00011971461,0.00003884708,0.0008191623,0.00016709906,0.026240917,0.9501952,0.0005958464,0.00013885471,0.009277572],"study_design_scores_gemma":[0.0002048183,0.0023150055,0.036778275,0.000022857883,0.00015318414,0.0004909219,0.0004369063,0.119255096,0.8393728,0.00024976677,0.0006435746,0.00007666343],"about_ca_topic_score_codex":0.00038450994,"about_ca_topic_score_gemma":0.000433467,"teacher_disagreement_score":0.001950901,"about_ca_system_score_codex":0.0002728769,"about_ca_system_score_gemma":0.00028574205,"threshold_uncertainty_score":0.006526351},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.009432161,0.00004625844,0.98989236,0.00001611476,0.000015229094,0.000030926312,0.00006617488,0.00021291304,0.00028788595],"genre_scores_gemma":[0.087811925,0.00016886185,0.9093791,0.00002997584,0.000028223978,0.00015621651,0.00049341744,0.000113521884,0.0018186823],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997327,0.000073427,0.00001999686,0.000043275104,0.000103163366,0.000027421604],"domain_scores_gemma":[0.9993285,0.0002710998,0.000048935693,0.000083405714,0.00022981953,0.00003831326],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000849888,0.0004924191,0.00045166636,0.0010754177,0.00036062356,0.0005482236,0.00058090617,0.00067589694,0.0030617148],"category_scores_gemma":[0.0020810212,0.00023723232,0.0006081174,0.0007206735,0.00032079426,0.0004946964,0.0007656563,0.0009894817,0.0016484979],"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":[0.0004525558,0.00024839348,0.00093571364,0.00021815207,0.00010342195,0.0001964675,0.00011993863,0.027709404,0.35176396,0.01286278,0.001741121,0.6036481],"study_design_scores_gemma":[0.00003915098,0.00019547991,0.0032490795,0.000022333375,0.000070885486,0.0003005982,0.000048338967,0.91974604,0.06927195,0.0034756442,0.003532892,0.000047656165],"about_ca_topic_score_codex":0.000670927,"about_ca_topic_score_gemma":0.000999796,"teacher_disagreement_score":0.0030617148,"about_ca_system_score_codex":0.00015458476,"about_ca_system_score_gemma":0.0008425584,"threshold_uncertainty_score":0.010242462},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.95008284,0.00041666758,0.03566288,0.00030585274,0.00012359288,0.00007425307,0.00010703603,0.0003072053,0.012919806],"genre_scores_gemma":[0.9956655,0.00005088776,0.0028239733,0.000022630546,0.000017767035,0.000015573769,0.000028946402,0.000023901002,0.001350866],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99973816,0.0000807207,0.000014322258,0.000038994433,0.0000760686,0.000051818304],"domain_scores_gemma":[0.99869114,0.00071587414,0.00013776009,0.00006108177,0.0002643366,0.00012986649],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005031305,0.0006737101,0.0010148769,0.00087563164,0.00085686636,0.00094788725,0.0007137318,0.0018951223,0.001398507],"category_scores_gemma":[0.002851288,0.00043817694,0.00062996784,0.000502956,0.001240207,0.0008802137,0.00064574,0.00058339996,0.00017306789],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0006912209,0.00036740064,0.0051082596,0.00017472086,0.000064234664,0.0011550036,0.0002555582,0.94907176,0.02915178,0.005615346,0.00055257557,0.0077921227],"study_design_scores_gemma":[0.00002415947,0.00005719918,0.00085383543,0.000006150347,0.000009954677,0.000045954697,0.000034585035,0.9973157,0.0013505535,0.00020186676,0.00008871323,0.000011219436],"about_ca_topic_score_codex":0.004981232,"about_ca_topic_score_gemma":0.0022151014,"teacher_disagreement_score":0.004981232,"about_ca_system_score_codex":0.0006039666,"about_ca_system_score_gemma":0.0006406924,"threshold_uncertainty_score":0.009904444},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.040228754,0.000120341065,0.9572055,0.00014011891,0.000051020088,0.00003606742,0.000040318817,0.00028245852,0.0018955015],"genre_scores_gemma":[0.6838754,0.00021020752,0.3109207,0.000093116454,0.00004031014,0.00015743289,0.00017406003,0.00025337806,0.004275525],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99981457,0.00006757532,0.000014114568,0.000022197246,0.000058973357,0.000022576256],"domain_scores_gemma":[0.9988821,0.0007040238,0.00008299396,0.00008938136,0.00018220117,0.000059309714],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005900023,0.00044382538,0.00062242063,0.00028615643,0.00047620962,0.0007752732,0.0008115349,0.0013102756,0.0010215694],"category_scores_gemma":[0.002977939,0.00049209414,0.0005064998,0.0003530577,0.0006962758,0.0009377005,0.00090929546,0.0011876215,0.00023342011],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000043078297,0.00003984604,0.00031936337,0.000024146306,0.000012320582,0.000033371445,0.000037525075,0.98232067,0.0025559682,0.0072172685,0.0002126143,0.0071837883],"study_design_scores_gemma":[0.0000020364037,0.0000021650237,0.000011202625,7.450976e-7,4.3731492e-7,0.0000012655961,0.000001379538,0.9994473,0.00018149707,0.00030126225,0.000049575166,0.0000011132648],"about_ca_topic_score_codex":0.010830783,"about_ca_topic_score_gemma":0.006957171,"teacher_disagreement_score":0.010830783,"about_ca_system_score_codex":0.00061536045,"about_ca_system_score_gemma":0.0011225668,"threshold_uncertainty_score":0.021535516},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97148246,0.00011667263,0.022780726,0.0001093964,0.00003848196,0.00004100961,0.00023340591,0.00030740726,0.0048903734],"genre_scores_gemma":[0.9936394,0.00004234702,0.0048260647,0.000010244999,0.0000059614085,0.00003229842,0.0001659394,0.000028488663,0.001249301],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998896,0.000028494453,0.0000063999228,0.000014591622,0.000041952775,0.000018948409],"domain_scores_gemma":[0.99967825,0.00018435968,0.000024311064,0.000018331835,0.00006731443,0.0000274289],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00030297082,0.0006356715,0.00049952575,0.00030072933,0.00041850854,0.00061153114,0.00043910477,0.0008492104,0.0008740212],"category_scores_gemma":[0.0007906088,0.00020358375,0.00048520273,0.00023497311,0.00044386683,0.00033816893,0.0003216999,0.0005343079,0.00013122761],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00010010563,0.00007497014,0.0033376452,0.000031939675,0.000010770655,0.000105753286,0.000056060846,0.98262817,0.0085739205,0.00055398396,0.0002025648,0.004324155],"study_design_scores_gemma":[0.00000668954,0.00002061571,0.0004680371,0.0000018518606,0.0000012522944,0.000004137424,0.000010955103,0.99827933,0.0010989526,0.0000309123,0.00007445017,0.0000027411745],"about_ca_topic_score_codex":0.029702686,"about_ca_topic_score_gemma":0.013203405,"teacher_disagreement_score":0.029702686,"about_ca_system_score_codex":0.0006524035,"about_ca_system_score_gemma":0.0008529685,"threshold_uncertainty_score":0.05905962},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.95371443,0.00045179712,0.039368227,0.00013265392,0.00008677259,0.000036563033,0.000053296506,0.00015724584,0.0059990427],"genre_scores_gemma":[0.99128246,0.00010126532,0.0054138904,0.000016816535,0.000016786042,0.000015896541,0.000024812822,0.000031724223,0.0030964],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998913,0.000016079108,0.000002939196,0.00002553013,0.000047547554,0.000016534344],"domain_scores_gemma":[0.99979895,0.0000851645,0.000027906062,0.000024551973,0.00005184286,0.000011559391],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00019148242,0.00029158962,0.0002697465,0.00013601767,0.00031972685,0.00033512898,0.00040769338,0.00032881615,0.0020953454],"category_scores_gemma":[0.00048173053,0.00013255895,0.00015368867,0.00008236644,0.0005396995,0.00045548825,0.00026276766,0.00028053977,0.00014477664],"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":[0.0005445716,0.00017435725,0.0005038545,0.00018631098,0.000009268211,0.00005654422,0.00014335262,0.015811615,0.9637743,0.0035696533,0.00033848162,0.014887681],"study_design_scores_gemma":[0.00014440285,0.0008577006,0.002946016,0.000016340116,0.000032341835,0.000102944105,0.00012161864,0.2546532,0.73520625,0.0006146508,0.005268441,0.000036015983],"about_ca_topic_score_codex":0.00059586915,"about_ca_topic_score_gemma":0.0006866761,"teacher_disagreement_score":0.0020953454,"about_ca_system_score_codex":0.00024849342,"about_ca_system_score_gemma":0.00015321882,"threshold_uncertainty_score":0.0070096254},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.43199223,0.00068288756,0.50735444,0.0008098949,0.0006046196,0.00006451311,0.0002718717,0.0011333072,0.057086244],"genre_scores_gemma":[0.96045035,0.00013330067,0.027428763,0.00009326569,0.00008738029,0.000021423162,0.00013375732,0.00025209782,0.01139969],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99988985,0.00003065578,0.0000037961213,0.000022241044,0.000027911368,0.000025497391],"domain_scores_gemma":[0.99962103,0.00017377657,0.0000234992,0.000024109338,0.000111802314,0.00004576388],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025178673,0.00057237555,0.00054923544,0.00059949275,0.00051827653,0.0007617072,0.00054702966,0.0010272763,0.004417212],"category_scores_gemma":[0.001467699,0.00024018397,0.00040633325,0.000296918,0.0004974332,0.0008104406,0.0005723188,0.00059859717,0.00040723098],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00021301763,0.00008576718,0.0026249685,0.000081036254,0.000040942236,0.00036578136,0.000108587614,0.93552434,0.011496576,0.028829575,0.0018372423,0.018792298],"study_design_scores_gemma":[0.0000031471739,0.000006380614,0.00016548704,0.0000030547149,0.0000024659942,0.0000098680885,0.000009689929,0.9983637,0.0005711882,0.0006479469,0.00021471117,0.0000024089015],"about_ca_topic_score_codex":0.00893888,"about_ca_topic_score_gemma":0.009200016,"teacher_disagreement_score":0.00893888,"about_ca_system_score_codex":0.00047316033,"about_ca_system_score_gemma":0.00048144197,"threshold_uncertainty_score":0.017773688},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.055829305,0.019182943,0.6903414,0.0030638238,0.0057539525,0.0010713972,0.0038274175,0.029882807,0.19104698],"genre_scores_gemma":[0.40450966,0.010440213,0.35713226,0.0033496537,0.0021698256,0.0011192256,0.0025093541,0.0013556062,0.21741429],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9991229,0.00019314067,0.00004548634,0.00021936398,0.00033802915,0.0000810104],"domain_scores_gemma":[0.9992711,0.00022217246,0.000061029936,0.00008425625,0.0002922575,0.00006932661],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005964931,0.0012778115,0.00071675435,0.0007793037,0.00047033344,0.0010863945,0.0018642932,0.0017152824,0.043255553],"category_scores_gemma":[0.0015922702,0.00046180762,0.000517163,0.0005439936,0.0002160007,0.0010379268,0.0010813932,0.00050921086,0.022089535],"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":[0.0009876975,0.00020000243,0.0051039765,0.0015683939,0.000098013865,0.0022406166,0.00055461476,0.0033838395,0.25841126,0.0051949015,0.061216652,0.66104],"study_design_scores_gemma":[0.00024268944,0.0014206835,0.015792947,0.0007274291,0.00035502762,0.00945405,0.0006304999,0.03312995,0.15606523,0.0042334935,0.77766573,0.00028224068],"about_ca_topic_score_codex":0.0016706152,"about_ca_topic_score_gemma":0.0020705252,"teacher_disagreement_score":0.043255553,"about_ca_system_score_codex":0.000329062,"about_ca_system_score_gemma":0.0004311623,"threshold_uncertainty_score":0.14470416},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.03914778,0.0002824446,0.95237255,0.00012166702,0.000056611934,0.000096340475,0.00003608216,0.0005881239,0.0072983713],"genre_scores_gemma":[0.54904133,0.00045089566,0.4419118,0.000074326796,0.000019515526,0.00031032975,0.00008616807,0.00023033748,0.007875284],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997764,0.000045560388,0.000009377864,0.000025810918,0.0001117131,0.000031165604],"domain_scores_gemma":[0.9997372,0.00009448634,0.000028021195,0.000024433646,0.0000831246,0.00003283216],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003933676,0.0005477554,0.00061285007,0.00039350317,0.000373156,0.0009438683,0.0010065755,0.00073097623,0.0036184038],"category_scores_gemma":[0.00096958654,0.0005725441,0.0006323345,0.00020183073,0.00044938037,0.0004558277,0.00068187714,0.00063238153,0.0014515816],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00005610685,0.000041468476,0.0008008225,0.000092904345,0.000023792574,0.00005951948,0.00005651536,0.9510281,0.015683636,0.00332867,0.00026761644,0.028560821],"study_design_scores_gemma":[0.000013114533,0.000025641823,0.000086111984,0.000008962273,0.0000045499005,0.000011998715,0.00001507372,0.996307,0.0017081341,0.00079490215,0.0010193875,0.0000050364156],"about_ca_topic_score_codex":0.0048386175,"about_ca_topic_score_gemma":0.004734012,"teacher_disagreement_score":0.0048386175,"about_ca_system_score_codex":0.00056219095,"about_ca_system_score_gemma":0.0014599576,"threshold_uncertainty_score":0.01210469},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9689169,0.00015134315,0.022258222,0.00014276816,0.00004904306,0.000031305797,0.000183047,0.00019453853,0.008072839],"genre_scores_gemma":[0.9970374,0.000048893955,0.0013605476,0.0000096008525,0.000008020956,0.0000131100505,0.000086244916,0.000021691616,0.001414513],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998908,0.000029413526,0.0000065722647,0.000021053322,0.00002234541,0.00002981382],"domain_scores_gemma":[0.9998591,0.000049428396,0.000020668054,0.000010800279,0.000040918374,0.000019146079],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00029043207,0.0006716128,0.0005100936,0.00043440086,0.00045603458,0.00082634814,0.00049264,0.00092835876,0.000716459],"category_scores_gemma":[0.0004825281,0.00017908397,0.00063679536,0.00023763663,0.0005757427,0.00035143358,0.00032037095,0.0003768586,0.00013965019],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00014298121,0.000057587837,0.0050173877,0.00003219516,0.0000108366885,0.00019175123,0.000060658684,0.9837947,0.005963784,0.0014538562,0.00027628668,0.002997927],"study_design_scores_gemma":[0.000014136543,0.000025025893,0.0010947256,0.0000029215196,0.0000023456716,0.00000939456,0.000013373351,0.9982065,0.0004481738,0.00007601416,0.00010140283,0.0000060036195],"about_ca_topic_score_codex":0.03525694,"about_ca_topic_score_gemma":0.009255513,"teacher_disagreement_score":0.03525694,"about_ca_system_score_codex":0.00072052353,"about_ca_system_score_gemma":0.0005326079,"threshold_uncertainty_score":0.07010347},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9987727,0.00010024664,0.00058568595,0.0000069252883,0.0000066426423,0.0000028041816,0.000026444324,0.000018908984,0.00047965086],"genre_scores_gemma":[0.99965835,0.000035205103,0.00013137951,0.0000045338666,0.000002218513,8.4816173e-7,0.000022171902,0.0000133246185,0.00013192944],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997843,0.00005571614,0.000015357062,0.000042586842,0.00005373413,0.000048266054],"domain_scores_gemma":[0.9983442,0.0010625117,0.00025465857,0.00010024884,0.00012440384,0.000114004244],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00028189455,0.00032179867,0.00034677208,0.0003151174,0.00023813493,0.0008628606,0.0002586776,0.00034680185,0.0017921592],"category_scores_gemma":[0.0018857421,0.0002794762,0.00022441852,0.0002919401,0.00045226756,0.0003202067,0.0002972338,0.00025250527,0.00025973385],"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":[0.0019098007,0.00016189028,0.016909178,0.00009324501,0.00003773757,0.0008030864,0.00015005753,0.035204425,0.93506664,0.00039194358,0.00012647611,0.009145541],"study_design_scores_gemma":[0.0001332198,0.0025186162,0.23781155,0.000024353552,0.00018979078,0.0007449671,0.0003829317,0.07747272,0.67949235,0.00035016498,0.00078209786,0.00009723424],"about_ca_topic_score_codex":0.00076388026,"about_ca_topic_score_gemma":0.00078968756,"teacher_disagreement_score":0.0017921592,"about_ca_system_score_codex":0.00031902775,"about_ca_system_score_gemma":0.0001542192,"threshold_uncertainty_score":0.005995393},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9954841,0.00011518118,0.003932916,0.000009620293,0.000009757543,0.000008927448,0.000044982702,0.00006270163,0.0003319549],"genre_scores_gemma":[0.9984774,0.000052554467,0.0011216031,0.000008557023,0.0000021085355,0.00000590539,0.00004702056,0.000009545211,0.00027532107],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999318,0.0000049183254,0.000004164352,0.000018536995,0.00001979862,0.000020751504],"domain_scores_gemma":[0.9998739,0.000022223685,0.000049814047,0.00001870867,0.00001626349,0.000019179291],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00009182974,0.00016337496,0.00014796625,0.00013730435,0.0001360645,0.00031728065,0.00014710653,0.00013116018,0.0010482166],"category_scores_gemma":[0.00023831484,0.00013305437,0.00017041671,0.000083342995,0.00025228653,0.00019765807,0.00020167511,0.000230183,0.00010478511],"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":[0.00027095503,0.00005852475,0.0042341575,0.000054156906,0.000017626175,0.0004891118,0.00008074583,0.017636554,0.9702141,0.00025221944,0.00008226171,0.0066095586],"study_design_scores_gemma":[0.000033972996,0.0010658165,0.08023765,0.000014473663,0.000029672836,0.00060560444,0.00028520075,0.19297732,0.7224435,0.00038064196,0.0018862478,0.000039934643],"about_ca_topic_score_codex":0.0005229765,"about_ca_topic_score_gemma":0.0004253754,"teacher_disagreement_score":0.0010482166,"about_ca_system_score_codex":0.00018710554,"about_ca_system_score_gemma":0.00012065103,"threshold_uncertainty_score":0.0035066009},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.118330985,0.00036361816,0.87595814,0.00021586791,0.00004997059,0.00006760743,0.000107103144,0.00023665352,0.0046700696],"genre_scores_gemma":[0.9179765,0.00035489578,0.07760125,0.00007510168,0.000019894915,0.00024642464,0.00016546517,0.000058777267,0.0035016956],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998858,0.000035761528,0.000005674454,0.000025144109,0.00003115579,0.000016435211],"domain_scores_gemma":[0.9996419,0.00022892852,0.00004379711,0.0000115007315,0.00006056597,0.000013222612],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00039311268,0.0008224294,0.0005832896,0.0005192041,0.0003256863,0.000630827,0.00089019706,0.0010661102,0.0007587261],"category_scores_gemma":[0.001097972,0.0003814986,0.0007060098,0.00048193656,0.00054047734,0.0004912232,0.00052334723,0.0007766571,0.00014740505],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00000365086,0.0000049649943,0.00019233435,0.000005606841,0.0000033102708,0.000011723311,0.000007837866,0.99748373,0.00028116765,0.00043781401,0.000025953057,0.0015418455],"study_design_scores_gemma":[5.999641e-7,0.0000029330897,0.000025357027,8.4923863e-7,8.133687e-7,0.0000014128144,0.0000012367925,0.9997427,0.00007294586,0.00012147346,0.000028771803,9.778369e-7],"about_ca_topic_score_codex":0.009266836,"about_ca_topic_score_gemma":0.004952942,"teacher_disagreement_score":0.009266836,"about_ca_system_score_codex":0.0006273513,"about_ca_system_score_gemma":0.00079818815,"threshold_uncertainty_score":0.018425763},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.96857834,0.0011003715,0.023259774,0.00012165365,0.00015934346,0.00012368306,0.00050382066,0.0005120237,0.0056411275],"genre_scores_gemma":[0.9910432,0.00032777313,0.0053240573,0.000076278644,0.000034662575,0.000051693452,0.0007581826,0.000066196364,0.0023179753],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995529,0.000033037843,0.000047052625,0.000054285687,0.0002517142,0.00006108477],"domain_scores_gemma":[0.9974032,0.0012335954,0.00035205245,0.000119819466,0.0005974507,0.00029379872],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006343978,0.0004135297,0.00048105716,0.0010444546,0.00041753103,0.0021841656,0.0003269369,0.00071706186,0.0023163545],"category_scores_gemma":[0.0027601493,0.00023980504,0.00036467507,0.0007961615,0.0004758189,0.0005031178,0.00048768692,0.0006508221,0.00042671623],"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":[0.0021745667,0.000489242,0.03668042,0.00026705087,0.000049989278,0.0018032718,0.00082668604,0.020887023,0.87892383,0.0028555163,0.0013737564,0.053668715],"study_design_scores_gemma":[0.00029732243,0.0026113687,0.15129536,0.00013451566,0.00011473914,0.0025290854,0.0007397406,0.2545935,0.57522404,0.001759372,0.010218974,0.0004819645],"about_ca_topic_score_codex":0.0010794839,"about_ca_topic_score_gemma":0.0005219917,"teacher_disagreement_score":0.0023163545,"about_ca_system_score_codex":0.00040123175,"about_ca_system_score_gemma":0.00047060678,"threshold_uncertainty_score":0.0077489614},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99111664,0.0000763364,0.0076210895,0.00002986174,0.000012553171,0.0000142974895,0.000055705605,0.000058007034,0.0010155261],"genre_scores_gemma":[0.9969535,0.000025317726,0.0027581025,0.000005616707,0.0000032887583,0.000005849548,0.00006147231,0.00000651619,0.00018030056],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998386,0.000025453131,0.000013551668,0.000029770725,0.00005774603,0.00003485965],"domain_scores_gemma":[0.999671,0.00011763486,0.00006120978,0.000019394514,0.00006827449,0.00006247588],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025532657,0.00055385294,0.0005121705,0.0006584931,0.0004246704,0.00074285426,0.00042659385,0.00064970565,0.0003013274],"category_scores_gemma":[0.00067212444,0.00023823192,0.00046623457,0.00043242678,0.00060000434,0.000538714,0.00038012725,0.00037779997,0.00005169045],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0008767164,0.00045306925,0.044616103,0.00014777233,0.00014829948,0.0025262788,0.00038345164,0.7209766,0.21565183,0.0044856686,0.00036756284,0.009366629],"study_design_scores_gemma":[0.000028587927,0.00009428148,0.0068171434,0.000004543128,0.00001431472,0.00007363631,0.00005329119,0.9827361,0.009818624,0.00021661125,0.00012097038,0.000021932401],"about_ca_topic_score_codex":0.0044885552,"about_ca_topic_score_gemma":0.0019762462,"teacher_disagreement_score":0.0044885552,"about_ca_system_score_codex":0.0006214855,"about_ca_system_score_gemma":0.00039693675,"threshold_uncertainty_score":0.008924842},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9957889,0.00008156119,0.0018037063,0.00007450271,0.000040156297,0.000031218868,0.00024692965,0.00014405369,0.0017889931],"genre_scores_gemma":[0.99836284,0.00002764493,0.0010835129,0.000010387504,0.0000061055894,0.000016290582,0.00015184932,0.00002582991,0.00031565587],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999833,0.00003686597,0.000015095591,0.000025973799,0.000044571894,0.000044405915],"domain_scores_gemma":[0.9988745,0.0006364979,0.000050919418,0.00010129394,0.00020729868,0.00012948232],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005330469,0.00063977495,0.00070373865,0.00029553924,0.0010779775,0.0010005764,0.0007982852,0.0010140917,0.001997783],"category_scores_gemma":[0.0014427237,0.0004283836,0.0006171374,0.00038712408,0.000806296,0.0008542162,0.00038309817,0.0009983715,0.00018827846],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0016500546,0.002203404,0.014024414,0.00018319214,0.00010219552,0.00036759945,0.00034561421,0.8997111,0.06877093,0.0015519117,0.0018443879,0.009245205],"study_design_scores_gemma":[0.00018979561,0.00042709,0.0066065085,0.000007153186,0.000015832426,0.000018567458,0.00008189722,0.97733283,0.014860343,0.00017616582,0.00025300108,0.00003078741],"about_ca_topic_score_codex":0.010250179,"about_ca_topic_score_gemma":0.008842526,"teacher_disagreement_score":0.010250179,"about_ca_system_score_codex":0.0008031015,"about_ca_system_score_gemma":0.00084236293,"threshold_uncertainty_score":0.020381033},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.90367234,0.00030659826,0.08758703,0.000265106,0.000088474786,0.00007909981,0.00021594524,0.00022521922,0.007560202],"genre_scores_gemma":[0.990175,0.00013390664,0.007915258,0.000019511592,0.000011929188,0.000035923884,0.000076896926,0.000012129521,0.0016194533],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998191,0.00003918791,0.000017683702,0.000034827935,0.000048476897,0.000040783547],"domain_scores_gemma":[0.99962914,0.00014150892,0.00009376855,0.000030264599,0.00006261283,0.000042730382],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00029585697,0.00061312615,0.0006763374,0.00045038853,0.0005897665,0.00094598846,0.0007434088,0.0013055296,0.0009149554],"category_scores_gemma":[0.0007770579,0.0002454584,0.00081373757,0.00047842972,0.00082865614,0.0005071744,0.0006727076,0.00057486945,0.00011713517],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000034013043,0.000039507482,0.0020221514,0.00001936152,0.000009090916,0.00014231289,0.000034925564,0.9901738,0.0048493696,0.0007752519,0.000056325436,0.0018438651],"study_design_scores_gemma":[0.000006133276,0.000016125807,0.00036337262,0.0000018911115,0.0000025612103,0.000010441575,0.000015643851,0.99890673,0.0005049622,0.00009537052,0.00007229705,0.0000043821174],"about_ca_topic_score_codex":0.015203734,"about_ca_topic_score_gemma":0.0052915667,"teacher_disagreement_score":0.015203734,"about_ca_system_score_codex":0.000646744,"about_ca_system_score_gemma":0.0009281969,"threshold_uncertainty_score":0.030230522},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.4220482,0.00021656715,0.57302237,0.00009403978,0.000056399742,0.000046739733,0.00008103938,0.0006208716,0.0038138146],"genre_scores_gemma":[0.962792,0.00011062311,0.035737652,0.000032374566,0.00001513596,0.00005320947,0.000091345704,0.000055506778,0.0011121606],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99988663,0.000020077568,0.0000072265384,0.00002001694,0.000052293337,0.000013677904],"domain_scores_gemma":[0.99972373,0.00013795723,0.000038092,0.000021513646,0.00005321653,0.00002535558],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020541273,0.0006371147,0.00047087984,0.00064830063,0.00025693417,0.0004780773,0.00047444456,0.0007501642,0.0004874808],"category_scores_gemma":[0.0007513848,0.0003007637,0.00047631696,0.00020651323,0.00034764994,0.0005656716,0.00042766222,0.00030875637,0.00015651797],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00001669143,0.000017408078,0.0015360106,0.000011304342,0.000008259777,0.000052254498,0.000017151828,0.99030274,0.0039937976,0.00028537976,0.000039689185,0.0037194176],"study_design_scores_gemma":[0.0000010736401,0.0000048155634,0.00016387553,9.1843026e-7,9.987756e-7,0.000004037934,0.0000023822859,0.99928755,0.00044073325,0.000060652917,0.000031092342,0.0000019457302],"about_ca_topic_score_codex":0.0033606167,"about_ca_topic_score_gemma":0.0022729156,"teacher_disagreement_score":0.0033606167,"about_ca_system_score_codex":0.0003311962,"about_ca_system_score_gemma":0.0005113846,"threshold_uncertainty_score":0.0066821575},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.979227,0.00011964807,0.015604737,0.00016617114,0.000041274096,0.00004256162,0.00023714235,0.00013182932,0.0044296524],"genre_scores_gemma":[0.99059814,0.00010526121,0.0077518146,0.000027165404,0.0000063549082,0.000048943777,0.00019437239,0.000015414565,0.001252512],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99984276,0.000035145942,0.00001434994,0.000024171144,0.000043242246,0.000040276154],"domain_scores_gemma":[0.9995074,0.0002393921,0.00006397493,0.000034938817,0.000098161836,0.00005612773],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00033786232,0.0005621291,0.00063716026,0.00039616125,0.0006567867,0.0007221241,0.00072636013,0.0012822504,0.0010873005],"category_scores_gemma":[0.00081452227,0.00024992044,0.00086855225,0.00048628115,0.0005981848,0.0004330055,0.00051680574,0.0006736455,0.00012458776],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000076422744,0.00008524784,0.0029935956,0.000034585108,0.000019703462,0.00016532472,0.00007435229,0.98833907,0.005617019,0.000637026,0.000109560555,0.0018480915],"study_design_scores_gemma":[0.0000104892015,0.000029725767,0.0007396627,0.0000026044977,0.000004127421,0.000009658361,0.000031012867,0.9979755,0.0010345745,0.00006930054,0.000086596185,0.000006695589],"about_ca_topic_score_codex":0.017686417,"about_ca_topic_score_gemma":0.008456483,"teacher_disagreement_score":0.017686417,"about_ca_system_score_codex":0.000653293,"about_ca_system_score_gemma":0.00078049576,"threshold_uncertainty_score":0.03516698},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.44377017,0.0013626121,0.52824825,0.00046101608,0.00021474528,0.000101332516,0.00037869439,0.0007506986,0.024712486],"genre_scores_gemma":[0.954312,0.0005009625,0.03908672,0.00008172741,0.00009063757,0.000064518164,0.00017570032,0.00017977983,0.00550794],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998468,0.000020705264,0.000009900577,0.000047404676,0.00005226862,0.000022891747],"domain_scores_gemma":[0.9996723,0.00007955379,0.00011799163,0.000040808172,0.00006849664,0.000020842954],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00031097792,0.00046030086,0.00019303933,0.00046270085,0.00023727665,0.00087038317,0.0005386028,0.0004140279,0.002408346],"category_scores_gemma":[0.0011495891,0.00019263098,0.00032085393,0.00029227373,0.0007856101,0.00087313476,0.0004641223,0.0007882257,0.0005311253],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00023470259,0.00009595744,0.020583225,0.0003125784,0.00004507697,0.00096684264,0.0010988818,0.3039503,0.2950281,0.28685078,0.0037623427,0.08707116],"study_design_scores_gemma":[0.000028768669,0.00025830616,0.033503894,0.000070270326,0.000032525142,0.0011934881,0.00020018057,0.87945133,0.04961333,0.023554005,0.0119760875,0.00011785102],"about_ca_topic_score_codex":0.0007153313,"about_ca_topic_score_gemma":0.00062277727,"teacher_disagreement_score":0.002408346,"about_ca_system_score_codex":0.00058138027,"about_ca_system_score_gemma":0.00039774604,"threshold_uncertainty_score":0.00805676},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9973387,0.00015062925,0.0022235725,0.0000035158077,0.00000784157,0.000009533871,0.000017767336,0.0000143460475,0.00023406174],"genre_scores_gemma":[0.9987206,0.000074412084,0.0010461416,0.000004634382,0.000002187347,0.0000034274467,0.000028726412,0.000010877953,0.00010899703],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994703,0.0000999676,0.00004889435,0.00010939138,0.00019243971,0.00007906791],"domain_scores_gemma":[0.9985991,0.00051899423,0.00045471924,0.00009890755,0.00022220417,0.00010597741],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0007822772,0.00032487104,0.00033885214,0.00024910423,0.00018133405,0.0008175069,0.00018628081,0.00020166319,0.0006627107],"category_scores_gemma":[0.0023132546,0.0002758374,0.00017812978,0.00023802802,0.00028885584,0.00036865377,0.00030312856,0.00026390023,0.00008266639],"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":[0.00072394375,0.000044439035,0.004604402,0.00004073015,0.0000105598665,0.00009292742,0.000058193767,0.0012955983,0.98957914,0.000091011825,0.000011855817,0.0034470744],"study_design_scores_gemma":[0.000048904378,0.0010384602,0.049517862,0.000012539647,0.000057682544,0.00017548408,0.00011162672,0.010446909,0.93804014,0.000061057704,0.0004489184,0.00004045459],"about_ca_topic_score_codex":0.00036613064,"about_ca_topic_score_gemma":0.00030942739,"teacher_disagreement_score":0.0008175069,"about_ca_system_score_codex":0.00023012461,"about_ca_system_score_gemma":0.00015149688,"threshold_uncertainty_score":0.0041371584},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99858475,0.000048352907,0.0011218814,0.000002662539,0.000004571545,0.000011626864,0.000028670669,0.000011615549,0.00018599807],"genre_scores_gemma":[0.99835193,0.00005889674,0.0013543558,0.000005969961,0.0000025853597,0.000008966453,0.000042438158,0.000009440938,0.00016533745],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99956733,0.00006500574,0.000039372437,0.00008422523,0.0001657803,0.000078319375],"domain_scores_gemma":[0.9990711,0.00031861305,0.00025253184,0.00008719755,0.0002050279,0.00006553254],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006562371,0.00032051574,0.00033891594,0.00022634307,0.00029527704,0.0004971237,0.00022183353,0.0002852366,0.0007882047],"category_scores_gemma":[0.001151631,0.0001867838,0.00019184571,0.00033711555,0.00034067756,0.00033750836,0.00028958463,0.00026420737,0.00008519818],"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":[0.00076809706,0.00012756477,0.002668612,0.000051485902,0.0000096511085,0.00012441713,0.000093084025,0.0018677252,0.9910182,0.0001007041,0.000021672251,0.0031488254],"study_design_scores_gemma":[0.000041841286,0.00197481,0.017463965,0.000009024079,0.000029703662,0.0001030285,0.00009480511,0.00462328,0.97526747,0.00004437324,0.00031424957,0.00003347105],"about_ca_topic_score_codex":0.00036240913,"about_ca_topic_score_gemma":0.000306834,"teacher_disagreement_score":0.0007882047,"about_ca_system_score_codex":0.00021918882,"about_ca_system_score_gemma":0.00014869124,"threshold_uncertainty_score":0.00347054},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8910261,0.00021008648,0.086264975,0.00025049134,0.0000957538,0.00009108902,0.00011752302,0.00036282747,0.02158121],"genre_scores_gemma":[0.9955723,0.000041882326,0.0022532055,0.000010226568,0.00000817591,0.000018663712,0.000032732347,0.000018790191,0.0020439487],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99987054,0.00003720321,0.0000028303448,0.000014465013,0.000052472984,0.000022412956],"domain_scores_gemma":[0.99975127,0.00013720605,0.000011745299,0.0000062905365,0.00007457417,0.000018852856],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00027255734,0.0004960258,0.00033563143,0.00032663037,0.0003265986,0.00037633535,0.0003198238,0.00056383386,0.0014531561],"category_scores_gemma":[0.0009813602,0.00017352164,0.00032638226,0.00016879191,0.0004776808,0.00017965057,0.00029502125,0.00034027913,0.00019748401],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000057718004,0.000030584044,0.0011298762,0.00002430998,0.0000049818823,0.00020069684,0.000046870067,0.9864238,0.007720069,0.001146334,0.00019573796,0.0030190852],"study_design_scores_gemma":[0.000009570789,0.000022212955,0.0004252857,0.0000014233702,0.0000011979636,0.0000089784235,0.000008184839,0.9986785,0.0006446362,0.00010624531,0.00009143941,0.0000023683629],"about_ca_topic_score_codex":0.024022905,"about_ca_topic_score_gemma":0.008965396,"teacher_disagreement_score":0.024022905,"about_ca_system_score_codex":0.00053259416,"about_ca_system_score_gemma":0.0005274053,"threshold_uncertainty_score":0.04776615},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.14802101,0.00051157695,0.79068345,0.0007663167,0.00016764902,0.0002025555,0.00013391153,0.0012427544,0.058270846],"genre_scores_gemma":[0.91222394,0.00022724083,0.07813129,0.0002968084,0.00006583654,0.00014138395,0.00014479917,0.00023803576,0.008530784],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.997267,0.0007453497,0.00008823994,0.00030739343,0.0011656435,0.00042638194],"domain_scores_gemma":[0.99785775,0.0008437521,0.0001954137,0.00022538572,0.0007867924,0.00009088213],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0024226047,0.0010195213,0.0006327565,0.0007041761,0.00066449796,0.0019294114,0.001360779,0.0012597877,0.0037192309],"category_scores_gemma":[0.007345291,0.0003470532,0.00042162894,0.00027826964,0.0006493271,0.0011960913,0.0012853636,0.000779765,0.0012865989],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0007740039,0.0004532929,0.0054890937,0.0007004523,0.000087549895,0.00031683518,0.0006714614,0.5105573,0.227623,0.060725432,0.005180721,0.1874209],"study_design_scores_gemma":[0.00014193599,0.002170838,0.0077115553,0.00024335648,0.00014220737,0.0006035936,0.00086074986,0.7935653,0.13196371,0.027571438,0.034912724,0.00011255775],"about_ca_topic_score_codex":0.0017876609,"about_ca_topic_score_gemma":0.0026584435,"teacher_disagreement_score":0.0037192309,"about_ca_system_score_codex":0.00062721554,"about_ca_system_score_gemma":0.0015601766,"threshold_uncertainty_score":0.012812078},"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":"review","genre_gemma":"review","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"review","genre_consensus":"review","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0906156,0.41766435,0.38621926,0.0021813856,0.0019396982,0.00035981036,0.0007863884,0.0010098487,0.09922365],"genre_scores_gemma":[0.5051965,0.30016166,0.1499617,0.0008106371,0.0021241955,0.0003305652,0.0017462119,0.00049565075,0.03917285],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9974275,0.0003851075,0.00015276691,0.00035592515,0.0015615071,0.000117064345],"domain_scores_gemma":[0.9958931,0.0013794526,0.00017402422,0.00031782317,0.00208252,0.0001531032],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0048910975,0.00055040093,0.0007864644,0.0016851376,0.00043370758,0.003158255,0.0017115519,0.0013197938,0.0039593917],"category_scores_gemma":[0.004323282,0.00078094285,0.00049251906,0.0014597741,0.0015650578,0.0027475345,0.0012763712,0.0012383048,0.0014035099],"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":[0.00042397744,0.00023157569,0.0039652674,0.0034275563,0.000051758816,0.00014001374,0.0007513973,0.011955933,0.049116418,0.014250356,0.003666846,0.91201895],"study_design_scores_gemma":[0.000089444206,0.0017541687,0.029504538,0.006445971,0.00017408487,0.0024177555,0.001950825,0.0660988,0.08257579,0.019440655,0.7889647,0.00058318465],"about_ca_topic_score_codex":0.001859192,"about_ca_topic_score_gemma":0.0013548958,"teacher_disagreement_score":0.0048910975,"about_ca_system_score_codex":0.0007246476,"about_ca_system_score_gemma":0.00096873567,"threshold_uncertainty_score":0.025866926},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.31421137,0.0002815353,0.6369453,0.000567011,0.00032063175,0.00042194585,0.0027571486,0.0052801385,0.03921491],"genre_scores_gemma":[0.8374049,0.0001092592,0.1509848,0.00011267136,0.00005585116,0.00033669054,0.0021982794,0.00053167366,0.008265882],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997383,0.000046905694,0.000014974641,0.000032265398,0.00013080517,0.00003664799],"domain_scores_gemma":[0.999199,0.00034045862,0.000073283874,0.000070119015,0.0002489895,0.000068285546],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00041811974,0.0006732181,0.00096078345,0.00044890982,0.00057180243,0.0009225431,0.0010670375,0.0011233579,0.003525939],"category_scores_gemma":[0.0017056178,0.00036988856,0.00060426863,0.00047299484,0.00041691595,0.00049530715,0.0006139735,0.00067033165,0.0006019314],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000047843765,0.000038598497,0.0007107582,0.000029638386,0.00001499756,0.00007839492,0.000026291358,0.98942775,0.003003557,0.0014865622,0.0009523988,0.0041832197],"study_design_scores_gemma":[0.000009893497,0.000004378597,0.000102328675,0.0000010107653,9.317434e-7,0.0000028151971,0.0000019751756,0.99934715,0.0002319785,0.00014136826,0.00015383623,0.0000023564196],"about_ca_topic_score_codex":0.01686598,"about_ca_topic_score_gemma":0.009068808,"teacher_disagreement_score":0.01686598,"about_ca_system_score_codex":0.00060117664,"about_ca_system_score_gemma":0.0018158159,"threshold_uncertainty_score":0.0335356},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.13721709,0.00066224276,0.858433,0.00011891151,0.000066263856,0.000042226617,0.00009821784,0.00075139117,0.0026105852],"genre_scores_gemma":[0.651639,0.0005144709,0.34400466,0.000101197955,0.00007081755,0.00006686767,0.00019831008,0.000060941453,0.003343738],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9995976,0.00012779426,0.0000133158055,0.00009693846,0.00013651115,0.000027813014],"domain_scores_gemma":[0.9995061,0.00022111318,0.00005739132,0.000041059793,0.00015562256,0.000018628753],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00046782836,0.0004412136,0.00036246688,0.0005358533,0.00013273275,0.00031854908,0.00033161708,0.00054628926,0.00078014034],"category_scores_gemma":[0.001430807,0.00028255352,0.00020359579,0.00037159474,0.00027216706,0.0005733384,0.00047919448,0.00020475333,0.00062836317],"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":[0.0009886608,0.000093234215,0.0034666276,0.0002631903,0.000070808885,0.0003385566,0.0004476145,0.048198037,0.64704823,0.0027249954,0.0011904413,0.2951696],"study_design_scores_gemma":[0.000100992555,0.0004734263,0.012453041,0.00004907552,0.00006500929,0.0011255896,0.00019215402,0.69071764,0.28647822,0.0021887932,0.0060452963,0.000110749395],"about_ca_topic_score_codex":0.0006498924,"about_ca_topic_score_gemma":0.00089797226,"teacher_disagreement_score":0.00078014034,"about_ca_system_score_codex":0.00015845495,"about_ca_system_score_gemma":0.00020662864,"threshold_uncertainty_score":0.0026097894},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8284329,0.00039547612,0.16354409,0.00040767557,0.00008622598,0.00005244749,0.00030575393,0.0013297934,0.0054456154],"genre_scores_gemma":[0.98941994,0.00007282017,0.009985465,0.000018400291,0.00001836672,0.000018883838,0.0001334519,0.000035472425,0.0002972045],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99869126,0.00041934737,0.000088256464,0.00018272783,0.00049922033,0.000119253615],"domain_scores_gemma":[0.9935836,0.0041679568,0.000537326,0.000600506,0.00094680226,0.00016366181],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0032934803,0.00086684705,0.0005929213,0.0010110687,0.000506684,0.0010803316,0.00076306576,0.0009248195,0.0005580327],"category_scores_gemma":[0.008876228,0.0003475752,0.00067987206,0.0005184727,0.0004950895,0.0012214525,0.00073679385,0.0006187786,0.00013332005],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00010606154,0.000058958154,0.0032063248,0.000026132451,0.000032058877,0.00002788728,0.000029248205,0.98293465,0.0012222759,0.0018292416,0.00010787087,0.010419336],"study_design_scores_gemma":[0.0000040359732,0.00003945021,0.00050502864,0.0000035177318,0.000004647504,0.0000057195484,0.0000042652446,0.9987099,0.00042177775,0.00025043875,0.000043932523,0.0000072838648],"about_ca_topic_score_codex":0.014195768,"about_ca_topic_score_gemma":0.005988919,"teacher_disagreement_score":0.014195768,"about_ca_system_score_codex":0.000764201,"about_ca_system_score_gemma":0.0010326195,"threshold_uncertainty_score":0.028226256},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.93257725,0.00012990653,0.05367097,0.000071545386,0.000035995803,0.00003686805,0.00008681125,0.00031541847,0.01307511],"genre_scores_gemma":[0.9977081,0.000035826997,0.001508022,0.000010787316,0.000007249254,0.000006010898,0.000044068292,0.000012706091,0.0006672721],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.999767,0.000029505289,0.0000047142235,0.000038120466,0.00011366806,0.00004692176],"domain_scores_gemma":[0.9994404,0.00018966549,0.00012665233,0.000048119226,0.00013143959,0.00006382371],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00026844317,0.0002612765,0.00025111064,0.00059348356,0.00019444717,0.00061373855,0.00031453688,0.00022942905,0.0033687283],"category_scores_gemma":[0.0009732943,0.00021016505,0.0001825848,0.0003803607,0.0005925902,0.00032633432,0.00052736606,0.0002715955,0.00035186653],"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":[0.00089736783,0.0001050789,0.009446555,0.00015246736,0.000039961727,0.0011218265,0.0004039908,0.062123775,0.84068584,0.034090206,0.0008510721,0.050081816],"study_design_scores_gemma":[0.00022904297,0.002109231,0.09598157,0.000035038356,0.00008595578,0.0023014597,0.0007891293,0.4585747,0.4119294,0.02126966,0.0065021515,0.00019265439],"about_ca_topic_score_codex":0.000276609,"about_ca_topic_score_gemma":0.00017471834,"teacher_disagreement_score":0.0033687283,"about_ca_system_score_codex":0.00036114908,"about_ca_system_score_gemma":0.00019043566,"threshold_uncertainty_score":0.011269569},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9990977,0.000054230957,0.0006779507,0.0000021333722,0.0000035750913,0.0000043036202,0.00003219347,0.0000109403845,0.00011691109],"genre_scores_gemma":[0.9990841,0.000051212886,0.000651661,0.000005620359,0.0000018381274,0.0000050463664,0.00006334141,0.000009394098,0.00012785464],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99969816,0.00003872047,0.000030173196,0.0000584955,0.00011289312,0.000061690065],"domain_scores_gemma":[0.9994623,0.00014706969,0.00016637419,0.00004203346,0.000121191,0.0000610649],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004371198,0.00031426293,0.00034415018,0.00023478635,0.0001713064,0.00065101223,0.00018512845,0.00021448961,0.00056720997],"category_scores_gemma":[0.0008014003,0.00015647634,0.00018778024,0.00031861922,0.00029151453,0.00029370893,0.00022842629,0.00021105948,0.00007230217],"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":[0.00060283253,0.000049260652,0.0030065693,0.000035147434,0.000014772912,0.00012356357,0.00005497572,0.0020742123,0.9915045,0.000091814654,0.000022705966,0.0024196415],"study_design_scores_gemma":[0.00005185901,0.0015749343,0.04655776,0.0000152097045,0.00005499213,0.00012536597,0.00014953573,0.010804678,0.9401674,0.00007318707,0.00038017303,0.000044808425],"about_ca_topic_score_codex":0.00037065786,"about_ca_topic_score_gemma":0.00023776492,"teacher_disagreement_score":0.00065101223,"about_ca_system_score_codex":0.00025684404,"about_ca_system_score_gemma":0.00010301417,"threshold_uncertainty_score":0.0023117661},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7038124,0.0001915793,0.28661835,0.00015403506,0.00024046584,0.002813185,0.0005468725,0.0020367191,0.0035864625],"genre_scores_gemma":[0.8032517,0.0002300131,0.18339661,0.00016031504,0.000039806782,0.0017598982,0.0010672229,0.0002148768,0.009879541],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99825746,0.00022332335,0.00011231664,0.00017063932,0.0010700385,0.00016612848],"domain_scores_gemma":[0.9955987,0.0007324373,0.0002360789,0.0004381283,0.0024514764,0.00054322777],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0027132586,0.0008054589,0.00050443714,0.00061478297,0.00046249092,0.00044145092,0.0012381143,0.0007391228,0.0021636093],"category_scores_gemma":[0.0027545518,0.00044512804,0.0003692093,0.00025724425,0.00044874958,0.0006285108,0.00064371654,0.0005734024,0.00056280935],"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":[0.0006136131,0.0007346702,0.00928406,0.00025253918,0.000042014824,0.00049936736,0.00029034112,0.010629656,0.94447684,0.00058440585,0.0008019917,0.031790502],"study_design_scores_gemma":[0.00049026293,0.017177667,0.035074588,0.00008537125,0.00010071199,0.0011868912,0.00030423078,0.0361384,0.8919434,0.00015843542,0.017227406,0.00011269661],"about_ca_topic_score_codex":0.0017035845,"about_ca_topic_score_gemma":0.0030480204,"teacher_disagreement_score":0.0027132586,"about_ca_system_score_codex":0.00043464935,"about_ca_system_score_gemma":0.001047187,"threshold_uncertainty_score":0.014349282},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9955029,0.000031326585,0.0028930446,0.000012404546,0.000012885311,0.000015691363,0.000042425912,0.00003014223,0.0014591317],"genre_scores_gemma":[0.9977664,0.00005022335,0.001047086,0.0000070721285,0.0000030283325,0.000009958948,0.000046428588,0.0000081023445,0.0010617408],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998621,0.000016655307,0.000005623722,0.000022741997,0.000061266925,0.00003161367],"domain_scores_gemma":[0.999584,0.00020894757,0.00003712047,0.00002827043,0.00009399736,0.00004761992],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001934421,0.0003690573,0.00031333673,0.00027283322,0.00023838368,0.00026374654,0.00025474542,0.00027398067,0.0012612062],"category_scores_gemma":[0.0005415311,0.00017376221,0.00024119437,0.00016283155,0.0005023944,0.00022105315,0.00023012045,0.00022640525,0.00024102128],"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":[0.0006550961,0.00016450082,0.00562427,0.00009011494,0.000010560486,0.0006524914,0.00014991574,0.014824274,0.969163,0.00031640756,0.00009148666,0.008258029],"study_design_scores_gemma":[0.00014045466,0.0049122428,0.107550055,0.00004072398,0.000048216967,0.00084967137,0.00084592745,0.122386314,0.76039195,0.0004963932,0.0022787335,0.00005942411],"about_ca_topic_score_codex":0.0022482376,"about_ca_topic_score_gemma":0.0022576335,"teacher_disagreement_score":0.0022482376,"about_ca_system_score_codex":0.00018142622,"about_ca_system_score_gemma":0.00021396956,"threshold_uncertainty_score":0.0044702888},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.28492522,0.00022600428,0.6306296,0.000732138,0.00044117603,0.002661825,0.0021925915,0.0107243005,0.067467116],"genre_scores_gemma":[0.7026186,0.00013864337,0.27595204,0.00012721539,0.000043564,0.0009934041,0.001273412,0.00022329892,0.018629864],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99933124,0.00006966973,0.000026481479,0.00011430004,0.00031506838,0.00014325653],"domain_scores_gemma":[0.9993167,0.00004663458,0.000070371076,0.00014892114,0.00021489663,0.00020246168],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006064325,0.0006089804,0.00053360715,0.0008745856,0.0013086231,0.001046467,0.0017937144,0.0010207527,0.013930477],"category_scores_gemma":[0.00065444084,0.0004155942,0.00050508283,0.00060176454,0.0005222472,0.00081922376,0.0012910591,0.00076791417,0.0045795846],"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":[0.001278438,0.0011324805,0.011951419,0.0010243864,0.000083021325,0.0013908064,0.00059346616,0.11442681,0.49438336,0.018815937,0.022821428,0.33209848],"study_design_scores_gemma":[0.0015851387,0.0133938,0.047600362,0.0003149469,0.00023817818,0.0017749816,0.0016505241,0.38171494,0.24931432,0.005665891,0.29636392,0.00038301156],"about_ca_topic_score_codex":0.002625466,"about_ca_topic_score_gemma":0.0037497217,"teacher_disagreement_score":0.013930477,"about_ca_system_score_codex":0.0010050983,"about_ca_system_score_gemma":0.0031371359,"threshold_uncertainty_score":0.04660207},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9907102,0.00007027772,0.008279804,0.00002155472,0.000009690176,0.000010548984,0.00003250534,0.00008972753,0.0007755306],"genre_scores_gemma":[0.9979633,0.00003331485,0.0016851489,0.0000056693366,0.0000024600217,0.0000062457034,0.000023445245,0.000009738004,0.00027068632],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998154,0.000037171932,0.00000948809,0.000039378607,0.00005401639,0.000044557342],"domain_scores_gemma":[0.99924684,0.0003399576,0.00011217916,0.000060929473,0.00018392863,0.00005612883],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00038806908,0.00033257098,0.00047123077,0.0002898943,0.00024862753,0.00031766412,0.00031780254,0.0004912489,0.0006096076],"category_scores_gemma":[0.0009325613,0.00022030556,0.000423871,0.00021924566,0.0006355418,0.00044632432,0.00030614968,0.00027639812,0.00012868817],"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":[0.00042052945,0.00027760223,0.029706113,0.00027873914,0.000075816926,0.0011072651,0.000501099,0.4390431,0.51042056,0.00094085897,0.00029298334,0.01693528],"study_design_scores_gemma":[0.000051796647,0.0009839941,0.022828933,0.000028439963,0.000059979706,0.0002674531,0.00029087186,0.87220556,0.10223603,0.0002308569,0.0007472633,0.00006891912],"about_ca_topic_score_codex":0.0012477778,"about_ca_topic_score_gemma":0.00088400097,"teacher_disagreement_score":0.0012477778,"about_ca_system_score_codex":0.00017863288,"about_ca_system_score_gemma":0.0002866433,"threshold_uncertainty_score":0.0024809837},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98463583,0.00002366445,0.0145859225,0.000030023504,0.0000052625874,0.000012439573,0.000101248195,0.0001443315,0.00046126262],"genre_scores_gemma":[0.9949597,0.000023997052,0.0047217933,0.000005118104,0.000003160172,0.000007458539,0.00009769033,0.000010072038,0.00017087157],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998171,0.000035836198,0.0000110303745,0.000048598722,0.00005944896,0.000027926695],"domain_scores_gemma":[0.99930465,0.00040173388,0.00008152531,0.000079414334,0.000098644974,0.00003401986],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00036955476,0.00057479576,0.00030542054,0.00041050444,0.00016103475,0.00045108914,0.00030548256,0.000451458,0.0004162744],"category_scores_gemma":[0.0014192605,0.00022544494,0.00022904851,0.00041605302,0.00032040762,0.00041033264,0.00047918208,0.00045462546,0.00015142927],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00133508,0.00078266335,0.14171067,0.0002505508,0.00008295793,0.0012712529,0.0006630969,0.48975682,0.16199948,0.0005658273,0.0007707472,0.20081075],"study_design_scores_gemma":[0.000016149412,0.00019572246,0.0379202,0.000009661564,0.0000131096485,0.000074502335,0.00013356905,0.93860596,0.022684215,0.00016408322,0.00016513625,0.000017648432],"about_ca_topic_score_codex":0.0043391543,"about_ca_topic_score_gemma":0.004644715,"teacher_disagreement_score":0.0043391543,"about_ca_system_score_codex":0.00013852329,"about_ca_system_score_gemma":0.0003044037,"threshold_uncertainty_score":0.008627832},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99601364,0.00003258763,0.003341317,0.000011252988,0.000006131391,0.0000049329637,0.00007591708,0.00006685802,0.00044723146],"genre_scores_gemma":[0.9980399,0.000034007146,0.0015887482,0.000011041978,0.000005402709,0.000010291902,0.00008499699,0.000013777906,0.00021192632],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998185,0.000015952653,0.0000101923215,0.000028760242,0.000093660004,0.000032832042],"domain_scores_gemma":[0.99949276,0.00020560934,0.00007392815,0.000034600947,0.00012064325,0.00007246542],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020829719,0.00020184787,0.00026915612,0.00036671938,0.0002231726,0.0005927707,0.00018829586,0.0002579909,0.0006567173],"category_scores_gemma":[0.00079112884,0.00016630816,0.00013821994,0.00028411593,0.00052774925,0.0003481267,0.0002564606,0.0005798026,0.00011889382],"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":[0.00023116164,0.000058917918,0.0066876756,0.000028717697,0.000011709815,0.000228858,0.00022197232,0.0029012992,0.9813163,0.0003192779,0.000076601704,0.007917495],"study_design_scores_gemma":[0.00004675131,0.0010577617,0.26448628,0.000020888445,0.00003151833,0.00038654578,0.0003630569,0.06787808,0.6642858,0.00041102857,0.00091114076,0.00012121972],"about_ca_topic_score_codex":0.0006160752,"about_ca_topic_score_gemma":0.00042847448,"teacher_disagreement_score":0.0006567173,"about_ca_system_score_codex":0.00017212883,"about_ca_system_score_gemma":0.00018461375,"threshold_uncertainty_score":0.0021969676},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9695749,0.00013199591,0.021240715,0.00011117575,0.000041909163,0.00002920167,0.00012975321,0.00033219354,0.0084080165],"genre_scores_gemma":[0.9970438,0.00003466372,0.000996089,0.000011784035,0.000009568739,0.000004584423,0.000040821844,0.000018858582,0.0018398163],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998679,0.000020306086,0.0000036410454,0.00002296012,0.00006884171,0.000016161688],"domain_scores_gemma":[0.9996779,0.00018019132,0.00001579272,0.000016819666,0.0000841935,0.000025072179],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012896185,0.00025236976,0.0002716895,0.00043903154,0.00034631402,0.00022153633,0.00025965463,0.0003796465,0.0026010913],"category_scores_gemma":[0.00049411814,0.000083778774,0.00022052077,0.000258032,0.00032564628,0.00019297088,0.00014681465,0.00023449864,0.00021285833],"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":[0.0018854074,0.00022349053,0.012037242,0.00018710768,0.00006482278,0.003151561,0.0004438595,0.08186557,0.84011424,0.0015635012,0.0009989564,0.057464324],"study_design_scores_gemma":[0.000076908735,0.00077191385,0.14815867,0.000020764439,0.00007144754,0.0016703466,0.0005464931,0.7413148,0.10228598,0.001118343,0.0038691547,0.00009519431],"about_ca_topic_score_codex":0.0037441985,"about_ca_topic_score_gemma":0.0033163542,"teacher_disagreement_score":0.0037441985,"about_ca_system_score_codex":0.00020940835,"about_ca_system_score_gemma":0.00016278359,"threshold_uncertainty_score":0.008701503},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6928756,0.00033635556,0.30270407,0.00013299144,0.000030126532,0.000031801814,0.00012462569,0.00033250713,0.0034318003],"genre_scores_gemma":[0.9835775,0.00015166248,0.015408621,0.000016056458,0.000018144396,0.000012389378,0.000088795605,0.00006538536,0.0006613733],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99993455,0.0000137383695,0.0000027026126,0.00001266035,0.00002353351,0.000012849449],"domain_scores_gemma":[0.99977225,0.00010180374,0.000041326977,0.000026015206,0.000039333892,0.000019282368],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00019536522,0.00029232638,0.00018766461,0.00032858114,0.00020763806,0.00042866118,0.00025353392,0.0002441525,0.0006733609],"category_scores_gemma":[0.00060754415,0.00016110708,0.00028057693,0.00034938895,0.00031969146,0.0005741133,0.0002054705,0.0003029997,0.000101142374],"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":[0.0005267062,0.00023674614,0.0074957954,0.000143397,0.00012036424,0.0006124217,0.0002750628,0.29577196,0.60200644,0.02832566,0.0011818007,0.06330371],"study_design_scores_gemma":[0.000005359452,0.000035039662,0.0027005866,0.0000015825793,0.00000858529,0.000019051387,0.000011474942,0.9906356,0.0059211394,0.00047640418,0.00017477693,0.00001050821],"about_ca_topic_score_codex":0.0017396078,"about_ca_topic_score_gemma":0.0017147607,"teacher_disagreement_score":0.0017396078,"about_ca_system_score_codex":0.00018696449,"about_ca_system_score_gemma":0.0002856941,"threshold_uncertainty_score":0.0034589767},"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":"review","genre_gemma":"review","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"review","genre_consensus":"review","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.00370204,0.60141796,0.004849583,0.0058859587,0.0072164536,0.000016517995,0.00008433103,0.00005224551,0.3767749],"genre_scores_gemma":[0.09148813,0.64741474,0.0017171567,0.003952043,0.015504037,0.00004657184,0.000137212,0.00014208886,0.23959804],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"not_applicable","domain_scores_codex":[0.99971133,0.00006429689,0.000019173505,0.000077354154,0.00008806507,0.000039759125],"domain_scores_gemma":[0.9996879,0.00018758523,0.000026167201,0.000017674016,0.000050496357,0.000030126996],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006753712,0.00073012616,0.00036500653,0.002485585,0.0015423725,0.0055968976,0.0008671362,0.002273414,0.009092342],"category_scores_gemma":[0.0010827432,0.000388377,0.00019411059,0.0031659114,0.0048431936,0.0043219314,0.0019749103,0.0034260792,0.0023826906],"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":[0.000052223033,0.000056528952,0.00022615226,0.0008098114,0.000008420167,0.00034824453,0.0019712253,0.0014880811,0.00055989716,0.7646837,0.038277533,0.19151817],"study_design_scores_gemma":[0.0000026875255,0.00003884648,0.0004892325,0.00072977226,0.000005364325,0.0003480458,0.00052203634,0.00035181112,0.00035425034,0.030426526,0.9667116,0.000019852501],"about_ca_topic_score_codex":0.0030852405,"about_ca_topic_score_gemma":0.0043581882,"teacher_disagreement_score":0.009092342,"about_ca_system_score_codex":0.0024514578,"about_ca_system_score_gemma":0.0012850526,"threshold_uncertainty_score":0.030416906},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"review","genre_consensus":"review","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.008994718,0.8113062,0.15211743,0.0019256283,0.0013000086,0.00013597889,0.00076703366,0.00057049666,0.022882562],"genre_scores_gemma":[0.042797748,0.90476954,0.04461976,0.00047103546,0.0013525381,0.00013322198,0.0010139804,0.00019872237,0.0046434547],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9991579,0.00016114589,0.00014721866,0.00016380833,0.000324706,0.000045191355],"domain_scores_gemma":[0.9988452,0.0006163705,0.00008590069,0.00007066004,0.00034203086,0.00003986567],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0012316381,0.0014736251,0.0017470979,0.0023020853,0.0006545871,0.0025987136,0.0017015395,0.0015693189,0.003437547],"category_scores_gemma":[0.0025652947,0.0008336723,0.0018276499,0.0033123314,0.0008817923,0.0021388237,0.0011319881,0.0015452978,0.0017355302],"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":[0.00010106017,0.00015945034,0.004114685,0.010709008,0.00016777222,0.00044515653,0.00036771112,0.15782931,0.00412191,0.032502435,0.017920878,0.77156067],"study_design_scores_gemma":[0.000038167946,0.00024383483,0.003378993,0.006199466,0.00033205427,0.0012688637,0.00045603633,0.28847227,0.007793077,0.021274678,0.67024547,0.00029699682],"about_ca_topic_score_codex":0.0063687977,"about_ca_topic_score_gemma":0.0028212415,"teacher_disagreement_score":0.0063687977,"about_ca_system_score_codex":0.0010278133,"about_ca_system_score_gemma":0.0018806609,"threshold_uncertainty_score":0.012663424},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9978235,0.000090959125,0.0015655444,0.000012592148,0.00001075331,0.000013929705,0.00006817027,0.000019869336,0.00039478077],"genre_scores_gemma":[0.9970475,0.00012432736,0.0023073351,0.00000757218,0.0000066476887,0.000019705807,0.00005144807,0.00000829857,0.00042713003],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99979705,0.000017894556,0.000014096968,0.000054493794,0.00007649416,0.000040042534],"domain_scores_gemma":[0.99962544,0.00015934907,0.000073938594,0.00004126507,0.000060770773,0.000039236187],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002602604,0.00031002532,0.000289106,0.00030837688,0.00026177295,0.00043102296,0.0002895711,0.0004535403,0.0017735005],"category_scores_gemma":[0.0004801576,0.00017908482,0.00018810818,0.0003184528,0.00063725014,0.00042437192,0.00030840363,0.00043523975,0.00013008316],"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":[0.00028843715,0.00023133846,0.0017075757,0.00006701854,0.000007740659,0.0002448511,0.00016284411,0.0023316615,0.9905815,0.00019724727,0.00004931238,0.0041303695],"study_design_scores_gemma":[0.00009181617,0.003354274,0.042449806,0.000024504903,0.000039973882,0.0003630157,0.0005829699,0.039767288,0.9119868,0.0002059795,0.0010697318,0.000063815016],"about_ca_topic_score_codex":0.00050186383,"about_ca_topic_score_gemma":0.00047441045,"teacher_disagreement_score":0.0017735005,"about_ca_system_score_codex":0.00014878655,"about_ca_system_score_gemma":0.00016466694,"threshold_uncertainty_score":0.0059329867},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.76560366,0.00020894328,0.23102453,0.0001112562,0.000059527196,0.000042333857,0.00007142991,0.00039069896,0.0024876222],"genre_scores_gemma":[0.99140316,0.00009057681,0.007936206,0.000011203399,0.000013600438,0.000015478025,0.000052843265,0.00001337576,0.0004636091],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99986863,0.00002834625,0.0000062845284,0.000032537715,0.000039674807,0.000024429097],"domain_scores_gemma":[0.9996245,0.00017581052,0.00005486136,0.000015228086,0.00009355552,0.000036129386],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00050441356,0.000844477,0.000429634,0.00037596366,0.00025832318,0.00037219978,0.00050362427,0.0008514646,0.00030446987],"category_scores_gemma":[0.001060203,0.00025250504,0.00036912345,0.00015533403,0.00051629246,0.00038668938,0.00028962106,0.00046380964,0.0000909518],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00006592491,0.00003731826,0.003555216,0.000027004206,0.000007636604,0.00009931683,0.000021454143,0.98152095,0.007965413,0.00078427175,0.000144773,0.005770701],"study_design_scores_gemma":[0.000001633581,0.000008125639,0.00024865274,4.4966555e-7,6.8149757e-7,0.0000020784237,0.0000014918872,0.99939144,0.00029945088,0.000035781708,0.000009018244,0.0000011947477],"about_ca_topic_score_codex":0.0071274326,"about_ca_topic_score_gemma":0.002765403,"teacher_disagreement_score":0.0071274326,"about_ca_system_score_codex":0.00028775417,"about_ca_system_score_gemma":0.00054646004,"threshold_uncertainty_score":0.014171898},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.87399995,0.00044799835,0.12263952,0.000046663623,0.000038068272,0.000020496105,0.000040651663,0.00016680697,0.0025999518],"genre_scores_gemma":[0.99356824,0.00011060462,0.005278028,0.000010543922,0.000022370881,0.000008445239,0.000055384993,0.000031569125,0.000914696],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.99954873,0.00011252962,0.000011619744,0.00008506698,0.0001978006,0.000044158183],"domain_scores_gemma":[0.99786747,0.0012590487,0.00011831267,0.000120380006,0.0005421146,0.00009258525],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005774942,0.0003839398,0.00040437336,0.00065311894,0.00032573598,0.0003003634,0.0004162135,0.00047542065,0.00070510316],"category_scores_gemma":[0.0014665667,0.00017493589,0.0004061278,0.00052426016,0.00040039327,0.00056125614,0.00029772674,0.0002851705,0.00013824868],"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":[0.001725984,0.00060957624,0.02406027,0.0003842709,0.00024769874,0.0021967539,0.0009491619,0.15241192,0.72393507,0.0088730855,0.00088379317,0.083722375],"study_design_scores_gemma":[0.000026134896,0.0006830405,0.02910505,0.00001984474,0.00014308038,0.0009631533,0.00016927315,0.88400584,0.082697704,0.0008993956,0.0012085155,0.00007903556],"about_ca_topic_score_codex":0.0012560873,"about_ca_topic_score_gemma":0.0006495654,"teacher_disagreement_score":0.0012560873,"about_ca_system_score_codex":0.00013604891,"about_ca_system_score_gemma":0.00029410093,"threshold_uncertainty_score":0.003054142},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9904722,0.00009898657,0.008462896,0.00001393283,0.000007910656,0.000015058605,0.000053535343,0.000064902684,0.0008105172],"genre_scores_gemma":[0.9968696,0.00004830283,0.002685814,0.0000038673766,0.000004822272,0.000009076551,0.00003993858,0.000012765527,0.0003257742],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9996327,0.000056722896,0.000016908049,0.000061009763,0.00016636575,0.00006620817],"domain_scores_gemma":[0.99907434,0.00044743807,0.00010182459,0.00008852538,0.0002191459,0.00006872911],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004258817,0.00042852882,0.000344575,0.0004548667,0.00037001056,0.00020525824,0.00034361775,0.0003694297,0.0009826027],"category_scores_gemma":[0.0011271997,0.00012359607,0.00017340934,0.00029629195,0.0007029256,0.00029933968,0.00027556665,0.00023365211,0.00012238143],"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":[0.000351018,0.00014421546,0.0026629863,0.00010301759,0.0000083742125,0.00019728295,0.00020043558,0.0048836055,0.9834379,0.00028875913,0.000052567088,0.007669978],"study_design_scores_gemma":[0.000056921483,0.0026619108,0.029402591,0.00001620317,0.000025126088,0.0005392835,0.00020680805,0.04733774,0.91800386,0.00027871906,0.0014008522,0.00007001549],"about_ca_topic_score_codex":0.00071085186,"about_ca_topic_score_gemma":0.0007084895,"teacher_disagreement_score":0.0009826027,"about_ca_system_score_codex":0.0002553753,"about_ca_system_score_gemma":0.00011934043,"threshold_uncertainty_score":0.0032871366},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9152069,0.0028435346,0.07500307,0.00026954323,0.00026203378,0.00012209048,0.00008437039,0.0005119805,0.0056964383],"genre_scores_gemma":[0.95176864,0.0010593344,0.040607803,0.00026716565,0.00007400789,0.0000751019,0.000092276634,0.00007827362,0.005977487],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99985254,0.000019106663,0.000005063742,0.000040542727,0.000055360244,0.000027422539],"domain_scores_gemma":[0.99990654,0.00002122588,0.000019975369,0.000014228519,0.000020683803,0.000017204824],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015755235,0.00030764804,0.00020332537,0.00026359066,0.00014007563,0.00018057985,0.00026262138,0.00024483923,0.0019456272],"category_scores_gemma":[0.00015462398,0.00013588309,0.00030770726,0.00012431863,0.00023027585,0.00026683585,0.00028278554,0.0003152953,0.0004120423],"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":[0.000056875928,0.000031099764,0.00009931587,0.00007890313,0.0000062274544,0.000050522325,0.00002422195,0.000088776986,0.9863825,0.00007972594,0.00014942899,0.012952416],"study_design_scores_gemma":[0.000049801383,0.0014093339,0.0064447043,0.000016406848,0.000036688965,0.0006006417,0.00009425907,0.0028163032,0.97643185,0.00010644791,0.011967576,0.000026045713],"about_ca_topic_score_codex":0.00014928222,"about_ca_topic_score_gemma":0.00028719148,"teacher_disagreement_score":0.0019456272,"about_ca_system_score_codex":0.000072980474,"about_ca_system_score_gemma":0.00008091909,"threshold_uncertainty_score":0.006508708},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9599529,0.00018911326,0.034038067,0.00019888065,0.00016116892,0.000032820357,0.0001230858,0.00028913488,0.005014952],"genre_scores_gemma":[0.9975223,0.000026292024,0.0014285657,0.000018507872,0.000014721493,0.00000695408,0.000049330465,0.000016192329,0.0009171699],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99985695,0.000028930583,0.0000053231765,0.00003276071,0.000026576443,0.000049378534],"domain_scores_gemma":[0.99948007,0.00020507135,0.00004332565,0.000027094999,0.00012770382,0.000116700685],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00029730354,0.0008892954,0.0007171746,0.00040152372,0.00074061536,0.00071963965,0.00083993195,0.002127117,0.0011937745],"category_scores_gemma":[0.0011614624,0.0003707655,0.00065427524,0.00021539051,0.0007258657,0.00066210784,0.0005379151,0.0006716506,0.0001978038],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00014927497,0.00010323816,0.003168494,0.000023910547,0.000017161441,0.0002670238,0.000026814678,0.990343,0.0029879208,0.0005451459,0.00024815762,0.0021198809],"study_design_scores_gemma":[0.000004107263,0.000011326855,0.00028893744,0.0000011799004,0.0000017991385,0.0000034609059,0.00000422776,0.9994759,0.00016737382,0.000024264571,0.000015204681,0.0000022769088],"about_ca_topic_score_codex":0.03053326,"about_ca_topic_score_gemma":0.009236957,"teacher_disagreement_score":0.03053326,"about_ca_system_score_codex":0.0005798325,"about_ca_system_score_gemma":0.00084227585,"threshold_uncertainty_score":0.060711086},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9901125,0.000085188825,0.008848561,0.000019929901,0.000010954355,0.000012585116,0.000027988483,0.00007228634,0.0008100849],"genre_scores_gemma":[0.99819547,0.000037020753,0.0014410034,0.000005592193,0.0000026269888,0.0000061884466,0.000020724303,0.0000069319876,0.00028453377],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998447,0.0000270267,0.000008504977,0.000033971082,0.000050602575,0.000035160625],"domain_scores_gemma":[0.99943703,0.00025265396,0.00008886632,0.000038182785,0.00013979676,0.000043471082],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00032863158,0.000295641,0.0004413575,0.00027965932,0.00022979989,0.00027188333,0.0002664545,0.00036744712,0.0005926597],"category_scores_gemma":[0.00079405215,0.00018035495,0.00035436204,0.00018648287,0.0005740572,0.000384191,0.00028944827,0.00024199969,0.00010876533],"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":[0.00048475736,0.000298249,0.026710777,0.0003329978,0.00007356778,0.0010291721,0.00047506427,0.33798197,0.6112272,0.0010943576,0.0002864522,0.02000537],"study_design_scores_gemma":[0.0000502441,0.0009345456,0.023268193,0.00002957924,0.000055766464,0.00024929616,0.00023855003,0.8645654,0.10962996,0.00022008157,0.00069973205,0.000058597452],"about_ca_topic_score_codex":0.001197583,"about_ca_topic_score_gemma":0.00091047504,"teacher_disagreement_score":0.001197583,"about_ca_system_score_codex":0.00016128784,"about_ca_system_score_gemma":0.00027790508,"threshold_uncertainty_score":0.0023812056},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6760123,0.0005706255,0.3065013,0.0002850969,0.00013129506,0.00014326238,0.00028925753,0.00038951763,0.015677407],"genre_scores_gemma":[0.9847835,0.0002445588,0.012499726,0.00003830011,0.000021933663,0.00006261311,0.00010454579,0.000023388222,0.0022215175],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99979824,0.000049864226,0.000017007598,0.00003661504,0.000051811192,0.0000463647],"domain_scores_gemma":[0.99969923,0.000096019896,0.00008336595,0.00002417768,0.00006230254,0.000034790664],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023664045,0.00060303736,0.00053840934,0.00050572667,0.00056454906,0.0010203453,0.0007460538,0.0011658459,0.00072597887],"category_scores_gemma":[0.0007720264,0.00025567834,0.0006563312,0.0006054395,0.0008785944,0.00052301463,0.0006867664,0.0004778295,0.00016309385],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000026152753,0.00002603696,0.0017421657,0.00001542427,0.00001047907,0.00014353827,0.000037817168,0.990428,0.0041561676,0.0016190262,0.00007130301,0.0017239334],"study_design_scores_gemma":[0.0000036692413,0.000008394164,0.00022579428,0.0000016116687,0.000002177182,0.000007552367,0.000009822077,0.99927956,0.00024591965,0.00013678864,0.0000752241,0.0000035525202],"about_ca_topic_score_codex":0.01582523,"about_ca_topic_score_gemma":0.004115241,"teacher_disagreement_score":0.01582523,"about_ca_system_score_codex":0.00065742026,"about_ca_system_score_gemma":0.00090605405,"threshold_uncertainty_score":0.031466246},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9851715,0.00039640244,0.012222317,0.000037517475,0.000044099732,0.00003644317,0.000113789,0.000101690166,0.0018762202],"genre_scores_gemma":[0.99320626,0.000109479,0.0047492534,0.00001377297,0.0000058538635,0.000013265119,0.00006637957,0.000012725106,0.0018231376],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99987507,0.000010547492,0.000003033503,0.000024904524,0.000068404705,0.00001801065],"domain_scores_gemma":[0.99988115,0.00002776246,0.000028979804,0.000015387666,0.000034853354,0.000011963396],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015428435,0.00025169214,0.0001834458,0.0001921564,0.00020957155,0.00018399024,0.0002076832,0.00027241601,0.001182945],"category_scores_gemma":[0.00022157755,0.00010081076,0.00017604177,0.00010571327,0.0003307674,0.00012694205,0.00014230383,0.00027643185,0.00017914802],"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":[0.000089666995,0.000032251468,0.00035565507,0.00007199018,0.0000045230613,0.000084880354,0.00003451989,0.0024755194,0.9926918,0.0001360435,0.00008492334,0.0039381622],"study_design_scores_gemma":[0.000015138153,0.0007456904,0.01114489,0.000010329399,0.000024198822,0.0001527742,0.00008234636,0.017580537,0.9678949,0.000052577572,0.002279343,0.000017129089],"about_ca_topic_score_codex":0.0012786875,"about_ca_topic_score_gemma":0.0017254805,"teacher_disagreement_score":0.0012786875,"about_ca_system_score_codex":0.00020210362,"about_ca_system_score_gemma":0.0002265903,"threshold_uncertainty_score":0.003957331},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98208964,0.0000734365,0.010925418,0.00014273777,0.00003314256,0.00006652619,0.00032072782,0.00016023542,0.0061881333],"genre_scores_gemma":[0.995271,0.000028731178,0.0033881299,0.000023057259,0.000005418425,0.00004310503,0.0001893215,0.000021376056,0.0010298578],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99986696,0.000029133073,0.000007428589,0.000019150537,0.000031592874,0.00004580999],"domain_scores_gemma":[0.99940884,0.0002864887,0.00006081795,0.000037207097,0.00010215033,0.00010458461],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00032430072,0.00042346693,0.000748423,0.0003547066,0.00056043186,0.0007119315,0.00079284015,0.0013957216,0.0020668358],"category_scores_gemma":[0.0011332062,0.0002408878,0.00059404864,0.00033042542,0.0006155616,0.00044941675,0.00041454763,0.0006105752,0.00017060206],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00014834818,0.000119469805,0.0022324307,0.000035495814,0.00002067497,0.00020123717,0.000055047298,0.9906957,0.0043949103,0.00063461706,0.0001928659,0.0012691101],"study_design_scores_gemma":[0.000027302971,0.000048817943,0.00095553097,0.000004145854,0.000004839724,0.000012892498,0.000025514391,0.99800354,0.00073220354,0.00008052334,0.00009893731,0.0000057591988],"about_ca_topic_score_codex":0.015317994,"about_ca_topic_score_gemma":0.0061828704,"teacher_disagreement_score":0.015317994,"about_ca_system_score_codex":0.0006614944,"about_ca_system_score_gemma":0.0009663298,"threshold_uncertainty_score":0.030457675},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98632413,0.00006498446,0.008235746,0.00012733717,0.000029450559,0.000029263818,0.0001871539,0.0001434153,0.00485856],"genre_scores_gemma":[0.9964965,0.000021605441,0.0021941115,0.000016980053,0.0000041958338,0.000016647915,0.00012932888,0.00001615023,0.0011045198],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999076,0.000019949897,0.0000053900308,0.000014718987,0.000020552516,0.00003186793],"domain_scores_gemma":[0.9996039,0.00021958307,0.000040594274,0.000021275,0.000052836866,0.0000617563],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023108964,0.0003222515,0.00041290873,0.00025422015,0.00041652942,0.0006583077,0.00046656156,0.0009997627,0.0013647284],"category_scores_gemma":[0.0008591032,0.00016383047,0.0003332127,0.00021050197,0.0005431269,0.0003325754,0.00042133644,0.00040666436,0.00009641441],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00024298465,0.00013529537,0.0046009943,0.000038189042,0.000021055386,0.0002826324,0.000070236645,0.9829826,0.008292349,0.0010757158,0.0003278999,0.0019299511],"study_design_scores_gemma":[0.000023805582,0.00005072667,0.0014716109,0.000003200266,0.000003471521,0.000010870806,0.000037094876,0.99725,0.0008809327,0.000106168736,0.00015699687,0.00000516941],"about_ca_topic_score_codex":0.011876948,"about_ca_topic_score_gemma":0.0050889645,"teacher_disagreement_score":0.011876948,"about_ca_system_score_codex":0.00047767555,"about_ca_system_score_gemma":0.0006347827,"threshold_uncertainty_score":0.023615599},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8703517,0.00036156937,0.1121992,0.0002401081,0.00005582843,0.000069396425,0.00017749041,0.00021523889,0.016329544],"genre_scores_gemma":[0.9841649,0.00004964166,0.014546511,0.000019602816,0.0000048558145,0.00003615074,0.000069671485,0.000021306312,0.0010874523],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99984705,0.000046800247,0.0000050585054,0.000016014843,0.000049681246,0.00003539554],"domain_scores_gemma":[0.9996358,0.00018077651,0.000059452927,0.000022093938,0.00007106503,0.000030758645],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00054347125,0.0005520833,0.0007203326,0.0003472309,0.000333983,0.00055146276,0.00031784558,0.00076126447,0.0009841585],"category_scores_gemma":[0.0011358465,0.00019245711,0.0005203186,0.0002126873,0.00043624226,0.0002661577,0.00031897755,0.00028287212,0.000112772315],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00007818397,0.00003249172,0.00058149436,0.00003701983,0.000009517711,0.000079434205,0.000020850579,0.99086094,0.0052429135,0.00091227976,0.00015774617,0.0019870647],"study_design_scores_gemma":[0.000007879596,0.00004039387,0.00022173427,0.00000335391,0.0000028171335,0.000007563792,0.000009845541,0.99843365,0.0010740807,0.000100378275,0.00009490835,0.0000033920699],"about_ca_topic_score_codex":0.003401987,"about_ca_topic_score_gemma":0.002162255,"teacher_disagreement_score":0.003401987,"about_ca_system_score_codex":0.0003766564,"about_ca_system_score_gemma":0.0005927111,"threshold_uncertainty_score":0.006764412},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98432356,0.00009953793,0.012187737,0.00009893452,0.000021488315,0.00002532372,0.00009037863,0.0002004174,0.0029526392],"genre_scores_gemma":[0.9960742,0.000032405304,0.0029073288,0.000014386502,0.0000037090433,0.00001068046,0.000056524965,0.000013615737,0.0008871745],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99992204,0.000022061075,0.0000027648196,0.00001214309,0.00002453023,0.000016474223],"domain_scores_gemma":[0.9997614,0.00011450999,0.000029338791,0.000012859115,0.000052358442,0.000029625462],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023623354,0.0004590595,0.00038821928,0.00038752725,0.00041217054,0.00045777802,0.00035041873,0.0010595865,0.0010620473],"category_scores_gemma":[0.0006419111,0.00015543243,0.00039094768,0.00018382893,0.00039779366,0.00029377223,0.0002929815,0.00028912805,0.00015893525],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00048242632,0.00017799866,0.011435656,0.000093577655,0.00003056382,0.0016228267,0.0003061468,0.8719371,0.09543037,0.0030870233,0.000792034,0.014604279],"study_design_scores_gemma":[0.000013654496,0.00014385613,0.0021524704,0.0000058684145,0.000005439812,0.00006190557,0.000029721434,0.99298006,0.004311704,0.00012985106,0.00015472593,0.000010853223],"about_ca_topic_score_codex":0.0045645298,"about_ca_topic_score_gemma":0.0022941008,"teacher_disagreement_score":0.0045645298,"about_ca_system_score_codex":0.00047884881,"about_ca_system_score_gemma":0.00040290307,"threshold_uncertainty_score":0.00907594},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9994467,0.00003853797,0.00040963278,0.000003722581,0.0000025635504,0.000002260279,0.000016216636,0.00000588974,0.00007451172],"genre_scores_gemma":[0.9985896,0.000049383903,0.0011003965,0.0000055120395,0.0000017148448,0.0000032704313,0.00006740787,0.000003473046,0.00017921855],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99993575,0.0000043931586,0.000004048673,0.000014486899,0.000024062207,0.000017178649],"domain_scores_gemma":[0.99985564,0.00003975383,0.000045846267,0.000009443876,0.000022035578,0.000027146027],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00013969294,0.00018948456,0.00030245795,0.00020536296,0.00014416306,0.00028652936,0.00020319647,0.00021059992,0.00039290043],"category_scores_gemma":[0.00024461336,0.00009217794,0.00019277741,0.00020857084,0.00026043836,0.00023262581,0.00026546128,0.00031418237,0.00004172017],"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":[0.00022096763,0.00002557686,0.005231571,0.00003255082,0.000006395752,0.00031757433,0.000072455565,0.0017754952,0.98888284,0.00010682057,0.00002201667,0.003305865],"study_design_scores_gemma":[0.00010435011,0.003044398,0.20105895,0.000025746864,0.00004981967,0.0004897482,0.0006165944,0.0647366,0.7287384,0.00022547708,0.0008487549,0.000061187566],"about_ca_topic_score_codex":0.00045930545,"about_ca_topic_score_gemma":0.00050036184,"teacher_disagreement_score":0.00045930545,"about_ca_system_score_codex":0.00019515763,"about_ca_system_score_gemma":0.00019644338,"threshold_uncertainty_score":0.0014159679},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9817607,0.00051425514,0.015607545,0.00004094972,0.000012286298,0.000008814215,0.00002124409,0.00007288912,0.0019614173],"genre_scores_gemma":[0.9987991,0.00012305945,0.0009473805,0.000002837341,0.0000020819575,0.0000013404708,0.0000041303897,0.0000052975815,0.000114841496],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998567,0.000023543284,0.00000616125,0.00001851419,0.00005044428,0.000044556844],"domain_scores_gemma":[0.9995766,0.00018122497,0.0000938845,0.000047789625,0.000061693456,0.000038716425],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00019028717,0.00027362723,0.00020790212,0.00023117715,0.0001621452,0.000355039,0.00022621751,0.0002205008,0.00060015987],"category_scores_gemma":[0.000652406,0.00009276018,0.0002045149,0.00012300584,0.00047474884,0.0003322832,0.0003460678,0.00016174217,0.00010315011],"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":[0.0006355361,0.00009112228,0.0036680314,0.00022311244,0.00003332325,0.00040308925,0.00009651546,0.04016953,0.9309604,0.0021504408,0.00005146156,0.021517426],"study_design_scores_gemma":[0.000038327555,0.0014288415,0.033127833,0.000075837845,0.00013571023,0.00043255155,0.00027957553,0.17464049,0.78721243,0.0010141478,0.0015647785,0.00004948011],"about_ca_topic_score_codex":0.00054791756,"about_ca_topic_score_gemma":0.00049220276,"teacher_disagreement_score":0.00060015987,"about_ca_system_score_codex":0.00011529836,"about_ca_system_score_gemma":0.00015435308,"threshold_uncertainty_score":0.0020077229},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9949968,0.00014209347,0.004543991,0.0000062796835,0.000012911214,0.000019620878,0.000058115897,0.00002846103,0.000191748],"genre_scores_gemma":[0.9926846,0.00013623817,0.0067805136,0.000010072025,0.000004119521,0.00002663724,0.000092798946,0.000021702937,0.0002433417],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99940956,0.00005702854,0.00005403485,0.000168984,0.00023098849,0.00007935574],"domain_scores_gemma":[0.999116,0.0002449874,0.00022670922,0.00009993178,0.00021355387,0.000098915916],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0007707891,0.00047320657,0.000739826,0.00018536851,0.00024819365,0.0006052243,0.00043559217,0.00040741073,0.0006928645],"category_scores_gemma":[0.001424452,0.00029118927,0.0003340734,0.00038523236,0.00035318566,0.0006110199,0.00055337354,0.00044743164,0.000094250274],"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":[0.00012132061,0.00002134636,0.000972302,0.000054723292,0.0000040833365,0.00009942485,0.00004607328,0.0007547566,0.996603,0.00004687177,0.000011717316,0.0012645365],"study_design_scores_gemma":[0.000024977204,0.0012850648,0.012393307,0.000009722484,0.000033262957,0.00018168053,0.00009860341,0.011175021,0.9743069,0.000072662755,0.0003904637,0.000028430515],"about_ca_topic_score_codex":0.0002769983,"about_ca_topic_score_gemma":0.00032675182,"teacher_disagreement_score":0.0007707891,"about_ca_system_score_codex":0.0002576232,"about_ca_system_score_gemma":0.00021739617,"threshold_uncertainty_score":0.0040763617},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.71943784,0.0006839721,0.21410243,0.0014403088,0.0010322713,0.00010747832,0.00061544543,0.001305581,0.06127474],"genre_scores_gemma":[0.9810372,0.00017552103,0.004466162,0.000061199054,0.000041099014,0.000013785759,0.00015177595,0.00010608793,0.013947205],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997725,0.000042616975,0.0000046065593,0.000031903666,0.00010795291,0.00004032909],"domain_scores_gemma":[0.99941194,0.00036746063,0.00003026567,0.000025479032,0.00012655575,0.000038291626],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00030471175,0.00062337256,0.00032779016,0.0004464017,0.00034251524,0.00047811994,0.000479629,0.0006990843,0.0065741516],"category_scores_gemma":[0.0014572152,0.00013037598,0.0003349175,0.00023567246,0.0006058649,0.00060725294,0.00039398344,0.00045896386,0.00059115706],"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":[0.0046383683,0.00037994643,0.004497972,0.00039397675,0.00011517344,0.0017710414,0.0005405404,0.6441543,0.20860875,0.048403606,0.011385618,0.075110726],"study_design_scores_gemma":[0.000040803454,0.00011031295,0.001582613,0.000021362637,0.00001363858,0.00007273135,0.000057247944,0.9812805,0.01379496,0.0017273128,0.0012753429,0.000023260951],"about_ca_topic_score_codex":0.009113228,"about_ca_topic_score_gemma":0.0047289575,"teacher_disagreement_score":0.009113228,"about_ca_system_score_codex":0.00053583394,"about_ca_system_score_gemma":0.00032617262,"threshold_uncertainty_score":0.021992743},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.85875875,0.00028029544,0.13422036,0.000053388445,0.000041289673,0.00004951988,0.00015854069,0.00036448005,0.006073361],"genre_scores_gemma":[0.9957426,0.000082033315,0.0033533762,0.0000052375317,0.0000052799546,0.000011931116,0.00005836254,0.00002442705,0.00071669044],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999074,0.00002682778,0.000003254622,0.000017175902,0.00003252914,0.000012821729],"domain_scores_gemma":[0.99978703,0.000119666234,0.000021430209,0.00001239661,0.00004436891,0.000015172689],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00022864768,0.0006588783,0.00031509245,0.00040391777,0.00018172471,0.00037260627,0.00032272958,0.0004968584,0.00065018726],"category_scores_gemma":[0.0005297094,0.00011976223,0.0003569824,0.00017008245,0.00020628455,0.00036732666,0.0002654089,0.00022728032,0.00018882121],"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":[0.0001932778,0.00008731333,0.0055285445,0.000100388796,0.000023317898,0.0002988935,0.000102968406,0.950736,0.02472671,0.00085141236,0.00019041219,0.017160805],"study_design_scores_gemma":[0.0000030235194,0.000052442025,0.0016167961,0.0000039987453,0.000004645505,0.000025309053,0.000024519733,0.9958747,0.002116639,0.00011256618,0.00016024656,0.0000051311818],"about_ca_topic_score_codex":0.0033858775,"about_ca_topic_score_gemma":0.0019847825,"teacher_disagreement_score":0.0033858775,"about_ca_system_score_codex":0.00023501345,"about_ca_system_score_gemma":0.00015515655,"threshold_uncertainty_score":0.0067323446},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97585243,0.00006262231,0.020147458,0.00011623663,0.000014064706,0.000046402005,0.000248406,0.00024240933,0.0032699131],"genre_scores_gemma":[0.9955231,0.000025570458,0.003785226,0.000014249487,0.0000029865187,0.000023457298,0.00013313934,0.00002021486,0.00047210374],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99988186,0.000037706195,0.0000072330063,0.000016101621,0.000032342126,0.000024790523],"domain_scores_gemma":[0.9995096,0.0002832393,0.00004701058,0.00003290975,0.00008709267,0.000040055274],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004141019,0.0004664546,0.000572279,0.00047761886,0.0004761608,0.0006096459,0.0005870868,0.0011187929,0.0010152395],"category_scores_gemma":[0.0010993613,0.00024533953,0.00043004315,0.00034600004,0.00051852956,0.0004558247,0.00032771425,0.0004270611,0.00011881833],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00007259867,0.000057444628,0.0026024668,0.000017980847,0.000011685753,0.00010568969,0.000035118544,0.99246347,0.0029591753,0.00051662955,0.000101084086,0.0010566157],"study_design_scores_gemma":[0.000011668592,0.0000237963,0.00059025484,0.000002012885,0.0000024488386,0.0000075571816,0.000012213778,0.99862623,0.00059235346,0.00008088262,0.00004601074,0.000004493532],"about_ca_topic_score_codex":0.013518356,"about_ca_topic_score_gemma":0.005357708,"teacher_disagreement_score":0.013518356,"about_ca_system_score_codex":0.00050523283,"about_ca_system_score_gemma":0.00066368125,"threshold_uncertainty_score":0.02687937},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.91822976,0.00016987232,0.077656105,0.00009461007,0.00004562948,0.00004665501,0.000094308285,0.00031966987,0.003343444],"genre_scores_gemma":[0.9940823,0.00003386648,0.0051251305,0.0000063628254,0.000004787867,0.000016964395,0.000046610887,0.000019435201,0.00066459575],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998957,0.00003073676,0.00000575021,0.00001519825,0.00003918131,0.000013432774],"domain_scores_gemma":[0.99912745,0.0006181847,0.00006001957,0.000028707214,0.00012340234,0.000042267075],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00028649412,0.0004157832,0.0004265379,0.00035318028,0.00030527645,0.00048550116,0.00040022423,0.00049909524,0.0010262751],"category_scores_gemma":[0.0014386778,0.00018374654,0.00031689217,0.00021294135,0.0004603783,0.00028739418,0.00029020954,0.0004247866,0.00011872126],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000058762223,0.000042193824,0.0016441908,0.000021433523,0.000005504489,0.00007132002,0.000019425406,0.9899248,0.005024654,0.00026674182,0.00007294528,0.0028480235],"study_design_scores_gemma":[0.0000023128162,0.000013240709,0.00022702402,8.4987255e-7,5.364395e-7,0.000002246615,0.0000028656077,0.999196,0.0004963564,0.000034019988,0.000023441096,0.0000010903769],"about_ca_topic_score_codex":0.01610867,"about_ca_topic_score_gemma":0.0064733964,"teacher_disagreement_score":0.01610867,"about_ca_system_score_codex":0.0004196491,"about_ca_system_score_gemma":0.0005108149,"threshold_uncertainty_score":0.032029808},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.985914,0.00008750962,0.006205291,0.00008088248,0.000026561132,0.000080697406,0.00022901155,0.00013559406,0.0072403993],"genre_scores_gemma":[0.9947296,0.000045773588,0.0036281117,0.000011115687,0.000003966729,0.000030840503,0.00008250836,0.000010950838,0.0014572629],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99984443,0.000022746692,0.000007814636,0.00003164324,0.000060859085,0.000032389067],"domain_scores_gemma":[0.9997193,0.000108551394,0.000038141843,0.0000299669,0.00005479247,0.000049197646],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025207567,0.00051791256,0.0005449672,0.0004096194,0.00048570093,0.0005395951,0.000575811,0.0007176952,0.0028368293],"category_scores_gemma":[0.0005552097,0.00020025163,0.0003911354,0.00029969861,0.00064804027,0.0002917175,0.0005140983,0.00049484894,0.00017823545],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00050243584,0.00038095386,0.0061137513,0.0001459366,0.00003680668,0.0010264724,0.00017201436,0.89030445,0.09076059,0.0025315806,0.00046271263,0.007562222],"study_design_scores_gemma":[0.000042502776,0.00035615164,0.0029367793,0.0000070861606,0.00000870194,0.00006604842,0.00006461127,0.9884022,0.007543284,0.00017616156,0.0003824927,0.000014025823],"about_ca_topic_score_codex":0.009409851,"about_ca_topic_score_gemma":0.004252878,"teacher_disagreement_score":0.009409851,"about_ca_system_score_codex":0.00052450184,"about_ca_system_score_gemma":0.0005451106,"threshold_uncertainty_score":0.018710136},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.082502134,0.00028792638,0.9138131,0.00013619252,0.000046830115,0.00006387636,0.000034188335,0.00014748804,0.0029681313],"genre_scores_gemma":[0.9311721,0.00062080735,0.064274885,0.00006797076,0.000079235215,0.00017437109,0.000094064715,0.00013336742,0.0033831487],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99949217,0.0002018627,0.000019874758,0.00006413559,0.0001667946,0.00005510446],"domain_scores_gemma":[0.99833065,0.0010182252,0.000275727,0.00011653758,0.00019613639,0.000062695],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0012897336,0.0011578122,0.00069598656,0.0009453172,0.000563635,0.001069079,0.001188973,0.0011669374,0.00032253243],"category_scores_gemma":[0.003433167,0.00043219826,0.0007698276,0.0007680653,0.0012012714,0.0012447229,0.0008979637,0.0012743396,0.00018118264],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000026867694,0.000053078897,0.0012184848,0.00002631365,0.000013954258,0.00013957951,0.00007110067,0.96728843,0.0030776483,0.02377975,0.00012466103,0.004180118],"study_design_scores_gemma":[3.8052724e-7,0.000003664809,0.000045716824,8.3103856e-7,5.1630826e-7,0.0000032331554,0.0000011952777,0.99939346,0.00008440225,0.0004393545,0.000024398772,0.0000027027297],"about_ca_topic_score_codex":0.007229207,"about_ca_topic_score_gemma":0.0050724195,"teacher_disagreement_score":0.007229207,"about_ca_system_score_codex":0.0007729336,"about_ca_system_score_gemma":0.0010288483,"threshold_uncertainty_score":0.014374256},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.994235,0.00008683373,0.005431546,0.000004502514,0.000011362311,0.0000101516725,0.000035021887,0.00002002409,0.00016560477],"genre_scores_gemma":[0.9935169,0.00008071258,0.006085668,0.0000058790397,0.0000033825647,0.000009403445,0.00007384872,0.000011218893,0.00021298949],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99971694,0.00003336111,0.000027496983,0.00005884165,0.00012153465,0.000041770287],"domain_scores_gemma":[0.9993098,0.00021521839,0.00018017566,0.00004099031,0.00017727881,0.00007663272],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000655771,0.00025935302,0.00032723782,0.00040202355,0.0002460057,0.00060007384,0.00018725601,0.0002186209,0.00036669214],"category_scores_gemma":[0.0011123853,0.00020400563,0.00021439185,0.00036151166,0.00039270983,0.0003025716,0.0002490152,0.0003223861,0.000057224966],"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":[0.00027199328,0.000036494264,0.0038047472,0.000017469409,0.000007453998,0.000048594906,0.0000682226,0.00075389905,0.9926825,0.00012888918,0.000018191367,0.0021615953],"study_design_scores_gemma":[0.000037911006,0.0008165601,0.029498931,0.0000070792003,0.000036738405,0.000115975155,0.000093681236,0.01609861,0.952912,0.000057230212,0.00029807576,0.000027175236],"about_ca_topic_score_codex":0.0005632578,"about_ca_topic_score_gemma":0.00041402827,"teacher_disagreement_score":0.000655771,"about_ca_system_score_codex":0.000270383,"about_ca_system_score_gemma":0.000189008,"threshold_uncertainty_score":0.0034680963},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99782854,0.00007118145,0.001814826,0.000003550665,0.0000027023423,0.000004016285,0.000017504859,0.000028219678,0.00022943431],"genre_scores_gemma":[0.99897504,0.000029243112,0.00069547107,0.000004287996,0.0000019144231,0.0000047674653,0.000035763456,0.000008397323,0.0002451634],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99991107,0.0000073443216,0.0000052045075,0.000017973909,0.000038349346,0.000019972334],"domain_scores_gemma":[0.9994685,0.00015254438,0.00015883647,0.00003641669,0.000120787445,0.00006291052],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001627448,0.00010870549,0.00018976066,0.00027282827,0.00013293097,0.0002930223,0.0001874039,0.00017264942,0.00048255685],"category_scores_gemma":[0.0005352265,0.00009056174,0.00014036402,0.0001712455,0.0002469137,0.00023165416,0.00023813017,0.00015138826,0.000075250435],"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":[0.000108626904,0.000032372238,0.008266016,0.00004179972,0.000011062311,0.00038332294,0.00016337511,0.002017956,0.98210686,0.00015358214,0.00005857954,0.0066563883],"study_design_scores_gemma":[0.000051914227,0.0015073254,0.2355996,0.000027605221,0.00005175155,0.0014845957,0.0005269878,0.08457623,0.6736332,0.0003749213,0.0020572902,0.00010870969],"about_ca_topic_score_codex":0.00030332137,"about_ca_topic_score_gemma":0.00023449105,"teacher_disagreement_score":0.00048255685,"about_ca_system_score_codex":0.000118566386,"about_ca_system_score_gemma":0.0000974187,"threshold_uncertainty_score":0.0016143322},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99646133,0.000021286187,0.0028124389,0.0000158168,0.000003586078,0.0000063708007,0.00002171726,0.00002903005,0.0006284704],"genre_scores_gemma":[0.99907327,0.000011444597,0.00066790695,0.0000030475744,6.1425783e-7,0.0000060381294,0.000015797279,0.00000564046,0.00021615013],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999424,0.000009662852,0.0000031958168,0.000011693513,0.000014643876,0.000018373421],"domain_scores_gemma":[0.99986386,0.000036285743,0.00003342264,0.00001428939,0.00002327098,0.000028892515],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020229294,0.00021838631,0.00021657978,0.000244439,0.00026167888,0.00037284236,0.0002642817,0.00033204886,0.0007220966],"category_scores_gemma":[0.00040583656,0.00018031918,0.00020560651,0.000111138754,0.0005066627,0.0003092218,0.00034519576,0.00026657444,0.000083332656],"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":[0.00032949357,0.0002208065,0.017768946,0.00010727952,0.00004677907,0.0009132531,0.00065938977,0.6383378,0.32747513,0.004596792,0.00035879473,0.009185635],"study_design_scores_gemma":[0.00002606267,0.00010955091,0.0049373712,0.000005086364,0.000005566511,0.000044351345,0.00007626218,0.9832161,0.011109138,0.00029383317,0.00016066156,0.000016007052],"about_ca_topic_score_codex":0.002111429,"about_ca_topic_score_gemma":0.0009007226,"teacher_disagreement_score":0.002111429,"about_ca_system_score_codex":0.00028808962,"about_ca_system_score_gemma":0.00037233141,"threshold_uncertainty_score":0.0041983128},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9961516,0.00015616967,0.0020696719,0.000051514617,0.000038081555,0.000005354601,0.0000674283,0.000073234696,0.0013867511],"genre_scores_gemma":[0.9994049,0.00004208074,0.00020361195,0.000006403547,0.000007185482,0.0000014932255,0.000030346671,0.000020472677,0.00028350012],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99992883,0.00001596936,0.000004622895,0.000018414552,0.000012890443,0.000019297735],"domain_scores_gemma":[0.99969435,0.00013512335,0.00003124059,0.000017246854,0.00004570242,0.00007644328],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017752088,0.0003016597,0.0002825457,0.00029644734,0.0003629864,0.0010779733,0.00018066581,0.0003288011,0.0009923725],"category_scores_gemma":[0.0008655611,0.00023017818,0.00025738016,0.00014605979,0.0005131104,0.0005218228,0.0003981666,0.00040429604,0.00016402226],"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":[0.0044204453,0.00051892456,0.025863338,0.00014894614,0.00012761855,0.001471722,0.00040612824,0.081720084,0.8626939,0.0046015405,0.00084767264,0.01717964],"study_design_scores_gemma":[0.00030691503,0.0010050024,0.09622976,0.00002389053,0.0001420527,0.00038515063,0.00027950542,0.61035955,0.28812855,0.001536818,0.0014321612,0.0001705751],"about_ca_topic_score_codex":0.0014206487,"about_ca_topic_score_gemma":0.00067029847,"teacher_disagreement_score":0.0014206487,"about_ca_system_score_codex":0.00024083475,"about_ca_system_score_gemma":0.00015772626,"threshold_uncertainty_score":0.0033197403},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8951771,0.00010745484,0.101346076,0.00007740848,0.000045612287,0.000042755095,0.0005342362,0.00038387554,0.0022856235],"genre_scores_gemma":[0.96926224,0.000112442685,0.029491343,0.000023664606,0.000028995146,0.00004118684,0.00040814988,0.000038600458,0.00059341383],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99985707,0.000015969174,0.000005658425,0.000024508623,0.00008219431,0.0000145527365],"domain_scores_gemma":[0.99973613,0.0000800968,0.000020149655,0.000018328894,0.00012942357,0.00001587576],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017052203,0.0002253044,0.00018520842,0.0007908628,0.00018222268,0.00017165336,0.00016470745,0.00017343777,0.0008621846],"category_scores_gemma":[0.0005285484,0.00009809379,0.00012757487,0.00058603624,0.00012323794,0.00025939877,0.00015474403,0.00017529972,0.00019668949],"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":[0.00028137138,0.000107809916,0.012349929,0.00008742578,0.000033941044,0.00017093676,0.00022380806,0.005320934,0.91495186,0.0008304371,0.0006988265,0.06494264],"study_design_scores_gemma":[0.00003925369,0.0004408424,0.24048772,0.00003215442,0.000051133564,0.000530215,0.00031387995,0.2861693,0.46700796,0.0009019411,0.0039271475,0.00009851431],"about_ca_topic_score_codex":0.00073733024,"about_ca_topic_score_gemma":0.00083723874,"teacher_disagreement_score":0.0008621846,"about_ca_system_score_codex":0.00013303,"about_ca_system_score_gemma":0.00013413053,"threshold_uncertainty_score":0.0028842688},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.5931989,0.00044777014,0.4022575,0.00014175918,0.00006722464,0.00005473712,0.00009766195,0.00039134116,0.0033429558],"genre_scores_gemma":[0.98837495,0.00013327575,0.010974498,0.0000123701575,0.000015815005,0.000015256746,0.000031958465,0.000037600217,0.00040429697],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99977654,0.00008231366,0.000010283033,0.000035384674,0.00007002632,0.00002547982],"domain_scores_gemma":[0.9982938,0.0012390874,0.00016198977,0.00009979776,0.00015789915,0.000047414444],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00080156635,0.0005810019,0.0003898762,0.00036008903,0.00020843526,0.00051621324,0.00048937154,0.0005798023,0.00059818],"category_scores_gemma":[0.0027330418,0.00016275239,0.0005269796,0.00014308254,0.0007301602,0.0004145749,0.0003975256,0.0006267208,0.0001366307],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00009280093,0.00004226602,0.0025732047,0.00006788374,0.000014187889,0.00018762005,0.000060797167,0.9594814,0.028143343,0.0019885919,0.000076636265,0.007271224],"study_design_scores_gemma":[0.0000021324768,0.000017880588,0.00032003692,0.0000031568668,0.000001639383,0.00000803536,0.0000040836917,0.99681914,0.002605101,0.00017653617,0.000038668728,0.0000034686877],"about_ca_topic_score_codex":0.0025123595,"about_ca_topic_score_gemma":0.0010191164,"teacher_disagreement_score":0.0025123595,"about_ca_system_score_codex":0.00025980046,"about_ca_system_score_gemma":0.00036857382,"threshold_uncertainty_score":0.0049954057},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9358814,0.001025735,0.061382737,0.00017009345,0.00024277643,0.00013837904,0.00014275467,0.00043829603,0.000577792],"genre_scores_gemma":[0.9476488,0.0003286561,0.05101174,0.00016677781,0.00007347309,0.00017945898,0.00016522573,0.00012624999,0.00029954317],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99504787,0.0022929395,0.00042696754,0.000654598,0.0013603835,0.0002172093],"domain_scores_gemma":[0.9496077,0.042879812,0.0018992776,0.0027894566,0.0024022583,0.00042148182],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0062315776,0.0008346619,0.0010574496,0.0006423781,0.0004930045,0.0008424195,0.0006522733,0.00090116035,0.00049297395],"category_scores_gemma":[0.026277766,0.0006805115,0.00031532714,0.00056376774,0.0008559794,0.0006983981,0.000870161,0.0005249392,0.00014443493],"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":[0.003859742,0.0005122535,0.024549372,0.00032120725,0.00015742963,0.00025434582,0.00040768532,0.018954597,0.90411747,0.00040948164,0.0002301637,0.046226196],"study_design_scores_gemma":[0.00013925477,0.0050838063,0.04902821,0.00004927346,0.00021332827,0.00030923024,0.00018077674,0.055896513,0.8874615,0.00039638678,0.0011083782,0.00013347082],"about_ca_topic_score_codex":0.0010946931,"about_ca_topic_score_gemma":0.0010400238,"teacher_disagreement_score":0.0062315776,"about_ca_system_score_codex":0.0003097978,"about_ca_system_score_gemma":0.00041001692,"threshold_uncertainty_score":0.032956123},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6846739,0.0004229208,0.29956433,0.00005736332,0.000051599985,0.000086002394,0.000059796494,0.0002916858,0.014792456],"genre_scores_gemma":[0.91826624,0.0001855626,0.07921507,0.000016873742,0.0000051845254,0.000034318724,0.000043398617,0.000040750452,0.0021927566],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999866,0.000020575508,0.0000074268255,0.000022423179,0.00006192419,0.00002155937],"domain_scores_gemma":[0.99973196,0.0000873284,0.0000687333,0.000023480794,0.000068049245,0.000020390355],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000297339,0.0006229761,0.0002834074,0.00032013128,0.00013595348,0.00049444014,0.00030147136,0.00032805715,0.00091323827],"category_scores_gemma":[0.0005920536,0.00020705228,0.00037613805,0.00021872995,0.00027675307,0.00025672236,0.00024229383,0.00024871124,0.0002238522],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00030239392,0.00018421107,0.0014611651,0.00024547835,0.000024064715,0.00029718012,0.000084856816,0.649156,0.29825142,0.0027642902,0.0003116929,0.0469173],"study_design_scores_gemma":[0.00005326354,0.0010575319,0.001896836,0.000025615687,0.000033094893,0.00014905384,0.00006570975,0.8937959,0.09975599,0.0007032099,0.0024373517,0.000026459078],"about_ca_topic_score_codex":0.0003916996,"about_ca_topic_score_gemma":0.0010762637,"teacher_disagreement_score":0.00091323827,"about_ca_system_score_codex":0.00023688018,"about_ca_system_score_gemma":0.0004119319,"threshold_uncertainty_score":0.0030550957},"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":"review","genre_gemma":"review","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"review","genre_consensus":"review","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.00044024186,0.998161,0.0005223257,0.00009381423,0.00017619485,0.0000055344676,0.000015570664,0.000009473718,0.000575798],"genre_scores_gemma":[0.0022557066,0.9965834,0.0004714305,0.000082854545,0.00024478274,0.000007262452,0.00003472264,0.0000033580325,0.00031650666],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.99956983,0.000058595357,0.00008203242,0.00009867661,0.00014726586,0.000043673877],"domain_scores_gemma":[0.9989619,0.00053030637,0.00017918316,0.000031005,0.00024009253,0.000057430792],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0012547815,0.0012306495,0.0018243012,0.0028678458,0.00040627594,0.001885619,0.0011419224,0.0013423216,0.0028348393],"category_scores_gemma":[0.0012181881,0.0006785997,0.0010702019,0.003762576,0.0007457095,0.0023113263,0.00095935696,0.0013902142,0.0011408151],"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":[0.00016793724,0.0002237832,0.00086054206,0.053702887,0.00019686557,0.00044860673,0.00025415485,0.0030605893,0.01017128,0.009719647,0.012553478,0.90864027],"study_design_scores_gemma":[0.00002344177,0.0005258284,0.0022064075,0.006737093,0.0004226823,0.0014274284,0.00022839801,0.0016568506,0.006665621,0.0033658827,0.97662795,0.000112392656],"about_ca_topic_score_codex":0.0012993898,"about_ca_topic_score_gemma":0.0010886203,"teacher_disagreement_score":0.0028678458,"about_ca_system_score_codex":0.00046933026,"about_ca_system_score_gemma":0.0012120098,"threshold_uncertainty_score":0.009483457},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.95497465,0.0002022838,0.034985002,0.0001642739,0.00014456875,0.000047303976,0.00031275698,0.0007690876,0.008400082],"genre_scores_gemma":[0.99609935,0.000038931394,0.0028798054,0.000011861373,0.000009485796,0.000008898995,0.00010042602,0.000028262508,0.00082292955],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999064,0.000014269271,0.000005681166,0.000020242733,0.00003056559,0.000022806884],"domain_scores_gemma":[0.9996165,0.00018055335,0.000029985658,0.000023732531,0.00010096166,0.000048186994],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020814709,0.00057405856,0.0006033168,0.0004936968,0.00055445824,0.00081807113,0.00059028383,0.0010396339,0.0012119844],"category_scores_gemma":[0.0008412195,0.00032309562,0.00047973168,0.00034952787,0.0005739467,0.00053178763,0.00045603697,0.00048801288,0.0002848735],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0002883901,0.00016311531,0.0052826186,0.000067894,0.000023435563,0.00030993338,0.00005518954,0.9650486,0.018893663,0.00087300554,0.00054099347,0.008453192],"study_design_scores_gemma":[0.00000807426,0.00001133576,0.0007497691,0.000001538559,0.0000022210145,0.0000064526107,0.0000046543255,0.99772364,0.0014128269,0.000041892086,0.000033834356,0.000003753283],"about_ca_topic_score_codex":0.014250511,"about_ca_topic_score_gemma":0.0050577135,"teacher_disagreement_score":0.014250511,"about_ca_system_score_codex":0.00052060286,"about_ca_system_score_gemma":0.00078262016,"threshold_uncertainty_score":0.028335154},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.58900815,0.0002711929,0.39579666,0.00016838605,0.00024947067,0.0034632967,0.0007563907,0.0014058767,0.008880534],"genre_scores_gemma":[0.5777001,0.00025946874,0.41551107,0.00003564548,0.00003027276,0.0014443306,0.00049269,0.00009304085,0.0044334256],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.999236,0.000071931696,0.00003887918,0.00006885438,0.00047225525,0.00011208213],"domain_scores_gemma":[0.9987717,0.00016834134,0.00014155389,0.00021868333,0.00054776017,0.00015182087],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0020454805,0.0004242795,0.0003462462,0.0005775174,0.0009489938,0.00064662995,0.0007146744,0.000558456,0.00095167477],"category_scores_gemma":[0.0011368775,0.00033974735,0.00025075465,0.00031639315,0.00063070736,0.00042004333,0.00048456536,0.00073148106,0.00025440246],"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":[0.00015668261,0.00031854748,0.0038968131,0.00025445464,0.000009217851,0.00029136057,0.00037646774,0.010549197,0.9398157,0.0027316657,0.000865937,0.04073391],"study_design_scores_gemma":[0.00020761462,0.0053909947,0.034658354,0.00006644754,0.000033425054,0.0009570586,0.00036990189,0.03548383,0.89140123,0.00050260784,0.03083676,0.00009178956],"about_ca_topic_score_codex":0.0009856655,"about_ca_topic_score_gemma":0.0026775328,"teacher_disagreement_score":0.0020454805,"about_ca_system_score_codex":0.00041194545,"about_ca_system_score_gemma":0.0024693592,"threshold_uncertainty_score":0.010817647},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.91212,0.00033227686,0.07390532,0.0001180042,0.00015492865,0.000026858937,0.00004311796,0.0002806423,0.01301884],"genre_scores_gemma":[0.9963282,0.00005028021,0.0014637135,0.00000776321,0.0000056842055,0.0000036730064,0.000009453554,0.000007364753,0.002123835],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99997914,0.0000032239072,0.0000010221601,0.0000036441186,0.000005714684,0.000007215073],"domain_scores_gemma":[0.99993587,0.000025106025,0.0000066201815,0.000007026116,0.000018140829,0.000007254294],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00008089617,0.00016611797,0.00016270707,0.00010302665,0.00018154044,0.00019883076,0.00014463686,0.00010659869,0.0022429107],"category_scores_gemma":[0.00020556769,0.00006062983,0.00007031815,0.000035155565,0.00015064338,0.00013668659,0.00016915798,0.00013063918,0.00015944101],"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":[0.001291772,0.0001951043,0.0023632108,0.0001702384,0.000032560456,0.00049011555,0.00028372108,0.27165523,0.45711645,0.0060371654,0.0038905672,0.25647384],"study_design_scores_gemma":[0.00003940249,0.00040479648,0.0015324174,0.000008848612,0.0000067655997,0.00003714032,0.00004793026,0.9681553,0.027409822,0.0007306872,0.00161901,0.000007862984],"about_ca_topic_score_codex":0.0010833483,"about_ca_topic_score_gemma":0.0016246949,"teacher_disagreement_score":0.0022429107,"about_ca_system_score_codex":0.00011719795,"about_ca_system_score_gemma":0.000110968474,"threshold_uncertainty_score":0.0075033307},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.012345433,0.00010027695,0.98360795,0.000064764296,0.000019542345,0.00002738746,0.000056009656,0.00042326056,0.0033553436],"genre_scores_gemma":[0.5792296,0.00040672292,0.41411632,0.00008246552,0.00006804331,0.00026254656,0.00038390484,0.00028991594,0.0051604994],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99978393,0.00004894334,0.000007922132,0.000028100354,0.000110804314,0.000020326448],"domain_scores_gemma":[0.9997458,0.000062370775,0.000037396545,0.000031934836,0.000105213105,0.000017291912],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000491738,0.000831363,0.0005510203,0.0007107384,0.0003999151,0.00071133644,0.0010865527,0.00071595015,0.0020682584],"category_scores_gemma":[0.00091513497,0.00037017127,0.00059286534,0.00028753423,0.00032521287,0.0008995282,0.0006346218,0.00057716493,0.00061709125],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000014277266,0.00003809625,0.00064682576,0.00003400055,0.000010896599,0.00004781467,0.000027148426,0.9608484,0.0052224277,0.0073841014,0.00056184514,0.02516418],"study_design_scores_gemma":[8.539412e-7,0.0000046601044,0.00004437157,0.0000021762398,0.0000010525556,0.000003867399,0.0000029433209,0.9988053,0.00029234393,0.0005345614,0.00030586525,0.0000019928386],"about_ca_topic_score_codex":0.00521133,"about_ca_topic_score_gemma":0.004290564,"teacher_disagreement_score":0.00521133,"about_ca_system_score_codex":0.00055167597,"about_ca_system_score_gemma":0.0012933877,"threshold_uncertainty_score":0.0103619695},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.31454766,0.005828606,0.5476326,0.0007434527,0.0005454847,0.00033192677,0.0006064638,0.0010097774,0.12875403],"genre_scores_gemma":[0.9170971,0.0024847523,0.038822092,0.00013772836,0.0002904683,0.00018381453,0.0003329692,0.00018864198,0.04046255],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999798,0.00004777209,0.000014830214,0.000032681888,0.00007517146,0.00003153038],"domain_scores_gemma":[0.99970347,0.00014099634,0.00004814552,0.000022904384,0.0000436075,0.000040811],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00030374766,0.00078074605,0.0010085631,0.0006952596,0.0008343466,0.0022837687,0.0013036832,0.0025895257,0.004177088],"category_scores_gemma":[0.0011215957,0.0007768132,0.0008468541,0.0009650619,0.0008969834,0.0013631191,0.0015139537,0.00097421365,0.0006267614],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00003974332,0.000082164,0.0005983481,0.00004170629,0.000013668779,0.0001271009,0.00005412266,0.97676736,0.0036605233,0.009215284,0.00045672772,0.008943292],"study_design_scores_gemma":[0.000007606751,0.000013305637,0.00014935761,0.0000050276835,0.000003001832,0.000019969157,0.000010752731,0.9976804,0.0002647933,0.0013676493,0.00047284577,0.000005184095],"about_ca_topic_score_codex":0.0064863516,"about_ca_topic_score_gemma":0.0035341578,"teacher_disagreement_score":0.0064863516,"about_ca_system_score_codex":0.0007597296,"about_ca_system_score_gemma":0.00062925374,"threshold_uncertainty_score":0.0139737725},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9871136,0.00006270736,0.00991424,0.000056729445,0.000024408037,0.000018314977,0.000051341533,0.000078913734,0.002679712],"genre_scores_gemma":[0.99836224,0.000024194926,0.0011697303,0.0000068409713,0.000002291185,0.000006833942,0.000018454846,0.000005064306,0.00040432217],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999323,0.000018826191,0.0000034032803,0.000009304516,0.00001778626,0.00001839359],"domain_scores_gemma":[0.99974674,0.00015334104,0.0000313157,0.000013847812,0.000030475749,0.000024270174],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00019367559,0.00027659847,0.0002663557,0.00022528505,0.0002619722,0.0003390334,0.00031851872,0.0006655517,0.000790547],"category_scores_gemma":[0.0005141363,0.00012630766,0.00035935154,0.0001245873,0.0004047499,0.00023817694,0.00022852629,0.0002919593,0.000058094207],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00017096191,0.000113998954,0.0036073788,0.00005103184,0.000014796161,0.000346631,0.00008734536,0.9758077,0.01514838,0.00076129875,0.00014372141,0.003746715],"study_design_scores_gemma":[0.000008754859,0.00006695432,0.0009787857,0.0000024683359,0.000004167902,0.000011413578,0.0000186228,0.9974227,0.001365549,0.00006233228,0.000054680986,0.0000036011477],"about_ca_topic_score_codex":0.0057555544,"about_ca_topic_score_gemma":0.0026058708,"teacher_disagreement_score":0.0057555544,"about_ca_system_score_codex":0.00018247966,"about_ca_system_score_gemma":0.00021789692,"threshold_uncertainty_score":0.011444092},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9919938,0.000488609,0.002347124,0.00011326588,0.00006426807,0.000031237243,0.000040743067,0.0000949863,0.00482594],"genre_scores_gemma":[0.9991159,0.00009158447,0.0001668142,0.000010048888,0.000014175854,0.0000039815804,0.000017452701,0.000017551047,0.00056258467],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995091,0.00008435456,0.000014326175,0.00006926472,0.00007737127,0.00024569905],"domain_scores_gemma":[0.99792105,0.0013554125,0.00020636916,0.00007489294,0.00019772499,0.0002445712],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00052912754,0.0005166415,0.00065978843,0.00053182896,0.00095493183,0.0013439449,0.0004813339,0.0004998322,0.003324437],"category_scores_gemma":[0.0028074647,0.00039005,0.00049214275,0.0002311509,0.0016391457,0.0009984851,0.0011974137,0.0007097756,0.00028189347],"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":[0.006227289,0.00047177888,0.008431341,0.00042729624,0.00014563292,0.0020521116,0.00090524205,0.22712302,0.7204062,0.011418215,0.001016653,0.021375254],"study_design_scores_gemma":[0.00061884755,0.0022576666,0.026496587,0.00005250075,0.0001333036,0.00023688881,0.0007242876,0.6105169,0.35363087,0.0034460332,0.0017294115,0.00015663443],"about_ca_topic_score_codex":0.010030952,"about_ca_topic_score_gemma":0.004094213,"teacher_disagreement_score":0.010030952,"about_ca_system_score_codex":0.00125144,"about_ca_system_score_gemma":0.0012418773,"threshold_uncertainty_score":0.019945145},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98064846,0.0002536457,0.0154594425,0.000033533113,0.00002816166,0.000056884746,0.000074081334,0.00010167075,0.0033441077],"genre_scores_gemma":[0.98980486,0.000103417915,0.009593763,0.0000074465297,0.0000019437127,0.000017109394,0.00003874331,0.000016388296,0.00041643172],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997533,0.000047238595,0.000012508485,0.000042540876,0.00010118321,0.00004317883],"domain_scores_gemma":[0.9994727,0.00015827749,0.00014144441,0.00005110612,0.0001280773,0.000048436075],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00050121895,0.00093257736,0.0003748151,0.00049835106,0.0002029018,0.000504291,0.00044403126,0.00043895136,0.00074541714],"category_scores_gemma":[0.0012177513,0.00023084984,0.00035989203,0.0001952157,0.00033515837,0.00029169332,0.00022756286,0.00020382072,0.00018329648],"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":[0.0006037597,0.00040045232,0.006639812,0.0004702404,0.000048035465,0.00055178395,0.000093773924,0.7145644,0.24441908,0.0008165052,0.0003822506,0.031009847],"study_design_scores_gemma":[0.000103958846,0.0042048423,0.01792555,0.00006087082,0.00013954708,0.00023274055,0.00032199483,0.737581,0.23715001,0.00021099192,0.0019828638,0.000085530766],"about_ca_topic_score_codex":0.0014444586,"about_ca_topic_score_gemma":0.0021506106,"teacher_disagreement_score":0.0014444586,"about_ca_system_score_codex":0.0003333131,"about_ca_system_score_gemma":0.00039454835,"threshold_uncertainty_score":0.0028721094},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.972508,0.00038294957,0.02565612,0.00005572188,0.000019832074,0.000057898895,0.00011608311,0.00013772305,0.0010656328],"genre_scores_gemma":[0.9645087,0.00044062358,0.03437021,0.000034465735,0.000009810908,0.000032675627,0.000077483215,0.000021833668,0.00050430803],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9996406,0.00003575058,0.000019389412,0.00008709768,0.00014967988,0.00006743186],"domain_scores_gemma":[0.99947494,0.00020714219,0.00014813502,0.000055546447,0.000086073705,0.000028217893],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00044713233,0.00035919243,0.00024318394,0.00040274314,0.00019458479,0.00033676653,0.00027490142,0.0003035285,0.0007362457],"category_scores_gemma":[0.0007960371,0.0002259,0.00018274206,0.00029510536,0.0005777166,0.0005951143,0.00047535787,0.0003520345,0.000086205175],"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":[0.000067224726,0.000012955538,0.0009931319,0.00004307752,0.0000026712123,0.00005918315,0.000069450994,0.00047321466,0.99438643,0.00015174701,0.000029607114,0.003711256],"study_design_scores_gemma":[0.000017936345,0.00032059554,0.01079435,0.000008545261,0.000007827033,0.00020119858,0.000088481924,0.008651488,0.9792788,0.000072542716,0.0005272587,0.000030886626],"about_ca_topic_score_codex":0.0010002576,"about_ca_topic_score_gemma":0.0011086948,"teacher_disagreement_score":0.0010002576,"about_ca_system_score_codex":0.00040362176,"about_ca_system_score_gemma":0.00035017525,"threshold_uncertainty_score":0.002928555},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.91784614,0.00023943455,0.08071543,0.000040364448,0.000043314976,0.000042886917,0.000016783886,0.0002389236,0.0008167295],"genre_scores_gemma":[0.98768926,0.00005246838,0.011962396,0.000006202805,0.000007247838,0.000018384122,0.000007578232,0.000010007579,0.0002464521],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99989855,0.000019226885,0.000008100848,0.000022540073,0.000032006676,0.000019514531],"domain_scores_gemma":[0.99960726,0.00009994373,0.00016317444,0.000035930407,0.00006024238,0.00003351462],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00029301504,0.00027452924,0.00018304482,0.00016101063,0.000118131786,0.00021239367,0.00036032425,0.00012467393,0.00030929878],"category_scores_gemma":[0.0004036643,0.0001113558,0.00012183569,0.000061411556,0.00027521324,0.00020032113,0.00026089663,0.00017743272,0.00006412069],"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":[0.0000997914,0.000037065456,0.00035456457,0.00004859045,0.0000042840966,0.00004366625,0.000034760054,0.0027584527,0.98734224,0.00044436642,0.00004910076,0.008783052],"study_design_scores_gemma":[0.000084018444,0.001138532,0.0020637945,0.000011415838,0.000018712984,0.000063329426,0.000027234764,0.12307638,0.8718834,0.00016108596,0.0014536252,0.000018553641],"about_ca_topic_score_codex":0.00017705787,"about_ca_topic_score_gemma":0.00029476735,"teacher_disagreement_score":0.00036032425,"about_ca_system_score_codex":0.000114630195,"about_ca_system_score_gemma":0.00020795486,"threshold_uncertainty_score":0.0015496612},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9984219,0.000010323411,0.0011354486,0.000011057335,0.000005265843,0.000009669013,0.00002981389,0.000032789805,0.00034379665],"genre_scores_gemma":[0.99952114,0.000008755784,0.00028184004,0.0000049337973,8.8233907e-7,0.0000098859755,0.000023997927,0.000004394345,0.00014416386],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99983037,0.000032373602,0.000006917617,0.00002059912,0.000050036553,0.000059611444],"domain_scores_gemma":[0.99962556,0.000203065,0.000050242754,0.000024667093,0.000057288147,0.000039083443],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021044498,0.0003244541,0.00026623585,0.00018183026,0.0002442116,0.00028953602,0.00027520012,0.00033203748,0.0009589316],"category_scores_gemma":[0.00091372617,0.000106980966,0.00018913871,0.00007524734,0.00039814532,0.00018631652,0.00035376794,0.00036451567,0.000074539166],"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":[0.0021309843,0.00048710266,0.0134767,0.00023346825,0.000048165482,0.00077399233,0.00039410772,0.2385826,0.73289955,0.00070262887,0.00036248728,0.009908198],"study_design_scores_gemma":[0.00012977535,0.0015883071,0.028935248,0.000020781647,0.000029794182,0.00012619399,0.00025099565,0.705027,0.2631212,0.0002308691,0.00049023575,0.000049562088],"about_ca_topic_score_codex":0.0025506867,"about_ca_topic_score_gemma":0.0016096921,"teacher_disagreement_score":0.0025506867,"about_ca_system_score_codex":0.00028664086,"about_ca_system_score_gemma":0.00020656483,"threshold_uncertainty_score":0.00507164},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9654598,0.00086583407,0.03077629,0.00006768104,0.00003332211,0.000039212642,0.000083877865,0.00015974492,0.0025141414],"genre_scores_gemma":[0.99252146,0.00029203668,0.0064949077,0.00002891924,0.000020374528,0.000019535963,0.000059310987,0.000023805771,0.0005395897],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99989164,0.000011817694,0.00000860191,0.000030189685,0.000032677377,0.000025156729],"domain_scores_gemma":[0.9995534,0.000091661714,0.00021200576,0.000031602915,0.000045607336,0.000065696615],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015065889,0.00055108103,0.00037911627,0.0007939984,0.000408083,0.0013150809,0.00029985065,0.0003360124,0.0005978568],"category_scores_gemma":[0.0006421941,0.00023572237,0.00026064055,0.0003279824,0.0010323062,0.00057800685,0.00071693095,0.0005432752,0.00012102966],"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":[0.00081509375,0.00029116048,0.022406032,0.00019259368,0.00003940504,0.0014213339,0.0007796493,0.022568004,0.9044247,0.01653527,0.00038486993,0.030141879],"study_design_scores_gemma":[0.00019435752,0.0016135878,0.123002335,0.000121507226,0.00011165379,0.0023594764,0.00058579276,0.4545615,0.38998866,0.023486814,0.003726216,0.00024810532],"about_ca_topic_score_codex":0.0004901395,"about_ca_topic_score_gemma":0.0004228873,"teacher_disagreement_score":0.0013150809,"about_ca_system_score_codex":0.00022663156,"about_ca_system_score_gemma":0.00018061827,"threshold_uncertainty_score":0.0020000339},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98232496,0.000065431064,0.01593794,0.000024443743,0.000028853507,0.000013959446,0.000012553746,0.00010725471,0.0014846162],"genre_scores_gemma":[0.99736327,0.000012384591,0.00236125,0.0000060838374,0.000002695627,0.0000066521025,0.000007558054,0.0000088505385,0.00023118593],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997907,0.000031328185,0.00001417115,0.00005225771,0.000059638533,0.0000519111],"domain_scores_gemma":[0.9995932,0.00011348627,0.00012567872,0.000063590254,0.00005374051,0.00005022819],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00029795477,0.0002948891,0.0003132053,0.00021857588,0.0002875049,0.0003365584,0.00026616888,0.0002742909,0.0010449552],"category_scores_gemma":[0.00066518196,0.00022086692,0.00025663743,0.000084895844,0.00052211236,0.00037318072,0.00077212864,0.00031339677,0.0001439548],"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":[0.00020964227,0.000042148316,0.0032826,0.0000761708,0.000015611378,0.0005239316,0.0002004194,0.018791176,0.9674788,0.0024312902,0.0001346122,0.0068136677],"study_design_scores_gemma":[0.00008282977,0.0004515666,0.009346038,0.000020176276,0.000040764935,0.00046859938,0.00017773753,0.44381362,0.5429189,0.0010450952,0.0015861284,0.000048455655],"about_ca_topic_score_codex":0.0003755041,"about_ca_topic_score_gemma":0.00027744178,"teacher_disagreement_score":0.0010449552,"about_ca_system_score_codex":0.0001686415,"about_ca_system_score_gemma":0.0003057142,"threshold_uncertainty_score":0.0034957528},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97304326,0.00032234023,0.02406097,0.000032506316,0.000014495928,0.00003271038,0.00017042425,0.00018536694,0.0021379518],"genre_scores_gemma":[0.99538213,0.00013607256,0.0038110686,0.000009915631,0.000005319384,0.000023414443,0.00012531993,0.000022422668,0.00048424653],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997626,0.000023481021,0.000012016974,0.000045894583,0.00012861723,0.000027435031],"domain_scores_gemma":[0.9981969,0.0009143847,0.00019449882,0.00012969815,0.00050073554,0.00006374972],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00046071742,0.0002868437,0.00019327526,0.00035247556,0.00016849668,0.0002828039,0.00027088536,0.00026266446,0.0015594319],"category_scores_gemma":[0.0013910963,0.00014041785,0.00020360666,0.0002644372,0.00044557318,0.00040819097,0.00018281944,0.00032860434,0.00021323616],"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":[0.00022671415,0.000045328903,0.0015222777,0.00008230328,0.000004893953,0.000081415514,0.00009674299,0.002123969,0.98808426,0.00020637459,0.00004182387,0.0074838726],"study_design_scores_gemma":[0.00003157652,0.00066535437,0.020657687,0.0000144832375,0.000020909314,0.00020651658,0.00008556238,0.02779563,0.94967794,0.0002592102,0.00055623887,0.00002876109],"about_ca_topic_score_codex":0.00030358956,"about_ca_topic_score_gemma":0.00025294672,"teacher_disagreement_score":0.0015594319,"about_ca_system_score_codex":0.00025258065,"about_ca_system_score_gemma":0.00014044128,"threshold_uncertainty_score":0.005216837},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8804912,0.00022872594,0.113626696,0.00010646203,0.000026880722,0.00003613562,0.0000736061,0.00017309323,0.005237182],"genre_scores_gemma":[0.99574345,0.00007058695,0.0032315555,0.0000053942067,0.000006049008,0.000007864986,0.000017867067,0.000013953556,0.00090314815],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99994814,0.000016784179,0.000001945335,0.0000106407515,0.000015364267,0.000007194731],"domain_scores_gemma":[0.99988604,0.0000562762,0.000016441785,0.000010970591,0.00002196619,0.000008283398],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018085142,0.0003112612,0.000235335,0.00026850664,0.00019322736,0.0003070163,0.0003419751,0.00048760488,0.0007456597],"category_scores_gemma":[0.00048855285,0.0001540236,0.00023818424,0.00015613176,0.000368616,0.0003106404,0.00017488285,0.0001925063,0.00015925564],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00010077659,0.000047402486,0.0035910753,0.000056472993,0.000017846134,0.00076138426,0.00020356209,0.924511,0.053533483,0.0043629818,0.00023085445,0.012583237],"study_design_scores_gemma":[0.0000022147447,0.000021467486,0.0009060665,0.0000029064997,0.0000025505901,0.000032354896,0.000018459594,0.99767095,0.00097418245,0.00019375668,0.00017124049,0.00000379931],"about_ca_topic_score_codex":0.002936049,"about_ca_topic_score_gemma":0.0017096569,"teacher_disagreement_score":0.002936049,"about_ca_system_score_codex":0.0002128423,"about_ca_system_score_gemma":0.00017697313,"threshold_uncertainty_score":0.0058379173},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7685387,0.0003533292,0.22446099,0.00007368913,0.000071903705,0.00004407924,0.000120421326,0.00042091782,0.0059159715],"genre_scores_gemma":[0.99333984,0.000074219686,0.0059897793,0.0000069859348,0.000006806505,0.000011896265,0.000059448044,0.00003120434,0.0004797756],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998276,0.0000447194,0.0000075845223,0.000023778668,0.00007551485,0.000020664427],"domain_scores_gemma":[0.9991585,0.00060057675,0.000069893125,0.000039207163,0.000107979045,0.000023794366],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000465416,0.00042334443,0.0003212218,0.00034408687,0.00016092346,0.00035716128,0.00036803467,0.0005520807,0.0011047513],"category_scores_gemma":[0.001533991,0.000113616064,0.0004835694,0.00017689638,0.00036321543,0.0002961321,0.0002677382,0.0005017051,0.00018284036],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00008888017,0.00006605473,0.0030971016,0.000092290495,0.000013778436,0.00012798244,0.000059277416,0.9680711,0.016306229,0.0012208807,0.0001132161,0.010743186],"study_design_scores_gemma":[0.0000023078514,0.000037948335,0.0005209168,0.0000061036408,0.0000022586594,0.000008399849,0.000005542629,0.9955858,0.003622917,0.00010965456,0.000094962386,0.0000033054216],"about_ca_topic_score_codex":0.0015669902,"about_ca_topic_score_gemma":0.00086680904,"teacher_disagreement_score":0.0015669902,"about_ca_system_score_codex":0.00019740079,"about_ca_system_score_gemma":0.00021202481,"threshold_uncertainty_score":0.0036957264},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9776573,0.00005478817,0.01957551,0.000091879,0.000013410909,0.000041744923,0.00020889509,0.00026035175,0.0020961342],"genre_scores_gemma":[0.9959357,0.000017325294,0.0035245009,0.000010176557,0.000002590896,0.000020280213,0.00012742389,0.000016600254,0.000345339],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998908,0.00003734252,0.0000069469334,0.000015959879,0.000029905686,0.00001906051],"domain_scores_gemma":[0.99946123,0.00033528634,0.0000441603,0.00003212157,0.00008858755,0.000038478087],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00039547207,0.00050917856,0.000511437,0.00049672084,0.00041732693,0.00061290443,0.00054336374,0.001083774,0.00089058775],"category_scores_gemma":[0.0010771295,0.00023334667,0.00037233956,0.0002585112,0.00041429835,0.00038376325,0.00028443986,0.000340956,0.00011159561],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000078913814,0.00006556713,0.0025964065,0.000017218052,0.000012306666,0.00010068984,0.000027567792,0.9921355,0.003235903,0.000344735,0.000096044474,0.0012891766],"study_design_scores_gemma":[0.000008474024,0.000017918255,0.0004595991,0.0000013515784,0.0000015718376,0.000004343602,0.0000070866427,0.99891245,0.00050673005,0.00004543107,0.000031985575,0.0000031514544],"about_ca_topic_score_codex":0.01082048,"about_ca_topic_score_gemma":0.0046546613,"teacher_disagreement_score":0.01082048,"about_ca_system_score_codex":0.00044928674,"about_ca_system_score_gemma":0.0005852367,"threshold_uncertainty_score":0.021515012},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9912429,0.00010448005,0.0016890978,0.0003779649,0.00006137533,0.000015000505,0.00006461948,0.000099740915,0.0063448423],"genre_scores_gemma":[0.99815565,0.000033343556,0.0002819453,0.000028078866,0.000021566973,0.0000059158747,0.000027848107,0.000027084914,0.0014185243],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99983764,0.00002316661,0.000004979911,0.000038219263,0.000027394997,0.00006854051],"domain_scores_gemma":[0.9987923,0.00053368753,0.00009140806,0.000052666586,0.00014956514,0.00038031852],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00031171346,0.0004124156,0.00086806,0.0010594497,0.0019462077,0.0029514115,0.00075392774,0.0013096081,0.0051427525],"category_scores_gemma":[0.0024274024,0.00046724675,0.00038033712,0.0004221035,0.0029468029,0.0028131881,0.0015139724,0.0016963369,0.00032613808],"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":[0.015811533,0.0037512528,0.043266732,0.0004126872,0.00020950321,0.009172482,0.005766611,0.33157808,0.361912,0.18588206,0.009330188,0.032906808],"study_design_scores_gemma":[0.0005662939,0.0013142615,0.053012434,0.00006876289,0.00009797441,0.0004975546,0.0031492382,0.88473696,0.022510787,0.031744346,0.0020275258,0.00027374938],"about_ca_topic_score_codex":0.005744309,"about_ca_topic_score_gemma":0.0026213499,"teacher_disagreement_score":0.005744309,"about_ca_system_score_codex":0.0009518865,"about_ca_system_score_gemma":0.0008626181,"threshold_uncertainty_score":0.017204225},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97668207,0.00015071705,0.00877699,0.00028991466,0.00014360278,0.00005750724,0.00046687762,0.0006235441,0.012808848],"genre_scores_gemma":[0.9950636,0.000028379623,0.0029352189,0.000040485993,0.000013623355,0.000014010185,0.00021544099,0.00008525656,0.0016040484],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998572,0.000035040317,0.000007065596,0.000022514714,0.000033526005,0.00004474597],"domain_scores_gemma":[0.998771,0.00062241574,0.0000906992,0.00006974752,0.00018026236,0.00026585977],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00039317712,0.00049698417,0.0007176398,0.00046125992,0.000644518,0.0010079512,0.0009186828,0.0012119532,0.004455276],"category_scores_gemma":[0.0017434402,0.00059040904,0.0005068828,0.00045554925,0.00064436166,0.0008211292,0.00048818186,0.0007517411,0.00035548335],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0003566947,0.00022723223,0.0028482478,0.00003491462,0.000036719477,0.00014979338,0.00005102567,0.98916143,0.0027775823,0.0010696235,0.0010182837,0.0022685062],"study_design_scores_gemma":[0.000044990895,0.000044077708,0.0004983932,0.0000020550074,0.0000033181973,0.0000053573394,0.0000138947025,0.9987753,0.0003941103,0.00010896736,0.00010428732,0.0000053099684],"about_ca_topic_score_codex":0.016828125,"about_ca_topic_score_gemma":0.010661913,"teacher_disagreement_score":0.016828125,"about_ca_system_score_codex":0.0008419068,"about_ca_system_score_gemma":0.0010060314,"threshold_uncertainty_score":0.03346032},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9974782,0.000095931464,0.0020593568,0.000007199623,0.0000083284995,0.000006553606,0.000023208131,0.000046346133,0.00027489685],"genre_scores_gemma":[0.99848676,0.000056352328,0.0010998781,0.000009666009,0.0000020845898,0.0000041104518,0.000024462432,0.000016417975,0.0003002405],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99977654,0.000037346515,0.000011644737,0.000051358467,0.00007227911,0.00005084253],"domain_scores_gemma":[0.9993494,0.0002538006,0.00014822719,0.00007446213,0.00011298738,0.000061214494],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017519579,0.00056384003,0.00032317388,0.00023993633,0.00016508621,0.00039757317,0.0003754776,0.00037660627,0.0010580417],"category_scores_gemma":[0.0007016082,0.00019108628,0.00022759821,0.00014582655,0.00043223143,0.00016560586,0.00029995415,0.00021408587,0.0002208488],"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":[0.0005245814,0.000038352413,0.00095269666,0.000061828476,0.000018377381,0.00014835136,0.000045157703,0.003860356,0.9917568,0.000028849077,0.00002072099,0.0025440557],"study_design_scores_gemma":[0.000031547872,0.0013580897,0.008102945,0.000009881528,0.000060590715,0.00009023386,0.00008188821,0.008141725,0.9817941,0.000011914488,0.00029976264,0.000017182014],"about_ca_topic_score_codex":0.0008782315,"about_ca_topic_score_gemma":0.0011973908,"teacher_disagreement_score":0.0010580417,"about_ca_system_score_codex":0.00019666097,"about_ca_system_score_gemma":0.000114944014,"threshold_uncertainty_score":0.0035395026},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8745142,0.00028537997,0.042249598,0.00051997416,0.00021589964,0.00013440562,0.0015227357,0.00080356636,0.07975415],"genre_scores_gemma":[0.9924481,0.00007164345,0.0023206535,0.000038222483,0.000017307648,0.000040288796,0.00025202625,0.000066352186,0.004745497],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996505,0.000066960805,0.000014207821,0.000041887895,0.000112040754,0.0001144629],"domain_scores_gemma":[0.99896705,0.00056633545,0.0000827893,0.00010467096,0.00019403484,0.000085180596],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00028467912,0.00070091983,0.0010790552,0.00053648703,0.00087030896,0.0010102296,0.0013172902,0.002065011,0.0063652378],"category_scores_gemma":[0.001564207,0.0005621564,0.0009552817,0.0007796873,0.00091386324,0.00077007955,0.0006301425,0.0010409947,0.00082646514],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000055016288,0.00004022568,0.0004847879,0.000026233927,0.00000795504,0.00012226844,0.000032359345,0.9962374,0.0012078815,0.00061341346,0.00027681544,0.0008957597],"study_design_scores_gemma":[0.000031800962,0.000036650432,0.00061383634,0.0000036831143,0.000006418897,0.000020199948,0.000027690246,0.99832135,0.00051943085,0.00014406182,0.000265018,0.000009899623],"about_ca_topic_score_codex":0.02721954,"about_ca_topic_score_gemma":0.013709548,"teacher_disagreement_score":0.02721954,"about_ca_system_score_codex":0.0009407045,"about_ca_system_score_gemma":0.0011142386,"threshold_uncertainty_score":0.05412221},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9910194,0.00014640295,0.0080282055,0.000011079488,0.000011770367,0.000010425154,0.000050793096,0.0000686808,0.00065311376],"genre_scores_gemma":[0.9982134,0.000049283455,0.0013253696,0.000004084322,0.0000025217403,0.0000061896912,0.000082597246,0.000011038001,0.00030557267],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996718,0.000037117148,0.000030582087,0.000054684886,0.00014306803,0.00006267907],"domain_scores_gemma":[0.999131,0.00040657475,0.0001235356,0.00007236468,0.0001916518,0.0000748897],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00048784318,0.0003626974,0.0004913524,0.00053976744,0.00033405365,0.00094414665,0.0004919347,0.00051029876,0.0008222927],"category_scores_gemma":[0.001362341,0.0002686398,0.0005587206,0.00037815075,0.0005246656,0.0006047526,0.00031499274,0.0002095176,0.00008101591],"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":[0.0017412619,0.00022730452,0.022131506,0.00028211967,0.00013437406,0.0010579543,0.00048831705,0.23576726,0.70657104,0.0028653578,0.0003558026,0.028377717],"study_design_scores_gemma":[0.00013729134,0.0016296123,0.05051061,0.000025929614,0.00011664994,0.0003836893,0.00021452099,0.73663306,0.20839468,0.0006997876,0.0011077755,0.00014633678],"about_ca_topic_score_codex":0.0010799711,"about_ca_topic_score_gemma":0.0006029647,"teacher_disagreement_score":0.0010799711,"about_ca_system_score_codex":0.00047167632,"about_ca_system_score_gemma":0.0002851314,"threshold_uncertainty_score":0.00342232},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99504083,0.000058943915,0.0034708576,0.000021702523,0.000010362027,0.0000108207505,0.000081325925,0.000056819386,0.0012484338],"genre_scores_gemma":[0.99857366,0.000025818814,0.00092650234,0.0000030498409,0.000002132164,0.000004053149,0.0000339766,0.000006026092,0.00042474535],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99984,0.000012040689,0.0000057983702,0.000021402097,0.000077764445,0.00004299007],"domain_scores_gemma":[0.99969053,0.00009303008,0.000057522688,0.000037572143,0.00007936276,0.00004199998],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018348725,0.00023957537,0.00016071567,0.00026654216,0.00031162758,0.00031009893,0.00028342928,0.0003161984,0.002039802],"category_scores_gemma":[0.00038144388,0.000110399276,0.00016172613,0.00019483933,0.0005367722,0.00024113139,0.00030474894,0.00033497214,0.0001562156],"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":[0.0002274519,0.00013710768,0.0019482973,0.00005354589,0.000005717638,0.0003626287,0.00012109824,0.0040289676,0.9879925,0.00045955332,0.00012443787,0.004538556],"study_design_scores_gemma":[0.00003307879,0.0014744012,0.03325335,0.000023769317,0.000018292598,0.00052367005,0.00043593213,0.059683748,0.9030697,0.00024038483,0.0011959103,0.000047845893],"about_ca_topic_score_codex":0.0008229041,"about_ca_topic_score_gemma":0.00074670854,"teacher_disagreement_score":0.002039802,"about_ca_system_score_codex":0.00021937532,"about_ca_system_score_gemma":0.00012010613,"threshold_uncertainty_score":0.006823778},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9962913,0.000036377067,0.003381741,0.000011165674,0.0000029472264,0.0000073255756,0.000037790425,0.000045399487,0.000185939],"genre_scores_gemma":[0.99680686,0.00003884852,0.0028206222,0.000004326302,0.0000017529221,0.000007169448,0.00006425111,0.000006174389,0.00024987216],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998927,0.000008367758,0.0000047328854,0.0000208458,0.000056249803,0.00001701818],"domain_scores_gemma":[0.99979013,0.000064243235,0.000041448417,0.00001164392,0.0000629178,0.000029597],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016626598,0.00023992146,0.0003356836,0.00045971,0.0002113166,0.00017094026,0.0002195605,0.0002643868,0.0003185427],"category_scores_gemma":[0.00030353805,0.00017907422,0.00022673812,0.00021738974,0.0002902065,0.00020033946,0.00032211666,0.00031722133,0.000056878125],"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":[0.00015754979,0.000033403507,0.0043897405,0.000021809246,0.0000058325923,0.000117444506,0.00013570092,0.0020228894,0.9886332,0.000092461654,0.000055031644,0.0043349857],"study_design_scores_gemma":[0.00007337024,0.0013193986,0.13847493,0.000014782427,0.00005103297,0.00027295,0.00028449413,0.082787715,0.7757726,0.00019920092,0.00069089135,0.000058681304],"about_ca_topic_score_codex":0.0017350966,"about_ca_topic_score_gemma":0.0016714663,"teacher_disagreement_score":0.0017350966,"about_ca_system_score_codex":0.0002802575,"about_ca_system_score_gemma":0.00023106695,"threshold_uncertainty_score":0.0034499764},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8559666,0.00017758226,0.13700424,0.00011167197,0.000047306854,0.00008558668,0.0002204662,0.00067675853,0.0057097287],"genre_scores_gemma":[0.9874018,0.000061188475,0.011329045,0.0000105227155,0.000006763346,0.000041796535,0.0001558969,0.000035478148,0.00095754827],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998828,0.000027888182,0.0000057191382,0.000023034305,0.000041699757,0.000018764425],"domain_scores_gemma":[0.99964213,0.00017715993,0.000042737254,0.000022457594,0.00008751988,0.00002793566],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00044318108,0.00081974384,0.00045456892,0.0005063605,0.0003192879,0.000635468,0.00051813456,0.0008189525,0.00057949655],"category_scores_gemma":[0.0008415077,0.0002401423,0.000572528,0.0002379241,0.00036229932,0.0004228036,0.00029200214,0.0004035652,0.00017576819],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00004760529,0.000045684475,0.0022984538,0.000028884093,0.000009629653,0.000050300343,0.000024499494,0.9891583,0.0049488833,0.00044557068,0.000092129885,0.0028500035],"study_design_scores_gemma":[0.0000025533789,0.000010376363,0.00023706644,0.0000012761192,0.0000011840118,0.0000016759623,0.0000030962076,0.99923813,0.0004365489,0.000033019824,0.000032952375,0.0000021755684],"about_ca_topic_score_codex":0.01670472,"about_ca_topic_score_gemma":0.008622299,"teacher_disagreement_score":0.01670472,"about_ca_system_score_codex":0.00053130375,"about_ca_system_score_gemma":0.0007880308,"threshold_uncertainty_score":0.033214927},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.5588717,0.001904877,0.38406464,0.00039615532,0.00021046835,0.00018243192,0.0006005165,0.0017110548,0.052058198],"genre_scores_gemma":[0.9897306,0.00022273225,0.007970994,0.000016103448,0.000022156353,0.00004730585,0.00012479142,0.000076810975,0.0017884967],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99955195,0.0001353361,0.000020000913,0.000060308368,0.00018257686,0.00004980613],"domain_scores_gemma":[0.99855965,0.0008791745,0.00008296859,0.00020696968,0.00024322301,0.000028092372],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00066844426,0.00075562485,0.00057563186,0.00046976394,0.00043590556,0.0008435707,0.001187703,0.00078721764,0.002895061],"category_scores_gemma":[0.0031738486,0.00030726637,0.00063385384,0.00033912653,0.00039016324,0.0008077206,0.0006592702,0.00065646606,0.00061537186],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0001479157,0.00014144642,0.0013479495,0.0001656917,0.00004049761,0.00015753295,0.0001288689,0.9489032,0.01637096,0.0047812276,0.00092886365,0.026885854],"study_design_scores_gemma":[0.0000030204367,0.00003901762,0.0002333748,0.000009410826,0.0000097640095,0.000019452767,0.000013655403,0.99626166,0.0025200117,0.0003241516,0.0005593842,0.000007077927],"about_ca_topic_score_codex":0.0023412493,"about_ca_topic_score_gemma":0.0016961076,"teacher_disagreement_score":0.002895061,"about_ca_system_score_codex":0.0002681081,"about_ca_system_score_gemma":0.00040021504,"threshold_uncertainty_score":0.00968492},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9705719,0.00006221826,0.028214578,0.000021919059,0.000011095439,0.000008920624,0.000015683665,0.0002453055,0.00084840413],"genre_scores_gemma":[0.99743575,0.000028206012,0.0020868322,0.000006750161,0.0000025805518,0.0000055050614,0.000011147755,0.000024076946,0.00039917819],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997948,0.00005025835,0.000009675459,0.000041058804,0.000059712645,0.000044496715],"domain_scores_gemma":[0.99938774,0.00027551348,0.00015423913,0.00006370268,0.0000618347,0.000056955225],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005444171,0.00050473656,0.0004641252,0.000378185,0.00033902563,0.0007083437,0.00051388546,0.00043426233,0.0010670038],"category_scores_gemma":[0.0010723814,0.00027427185,0.00045537797,0.00018815087,0.0009358293,0.00054669427,0.00067107443,0.00039964603,0.0002095374],"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":[0.0012290704,0.00020215737,0.005323233,0.000119679855,0.00004356705,0.0009756371,0.00055909023,0.3122056,0.65351534,0.003672113,0.00015481167,0.021999754],"study_design_scores_gemma":[0.00004105975,0.0007683765,0.003062375,0.000011194236,0.00003659973,0.00016011906,0.000106853695,0.7874092,0.20743181,0.0006227647,0.0003098067,0.000039878378],"about_ca_topic_score_codex":0.000716808,"about_ca_topic_score_gemma":0.00037183057,"teacher_disagreement_score":0.0010670038,"about_ca_system_score_codex":0.00031961652,"about_ca_system_score_gemma":0.00020583444,"threshold_uncertainty_score":0.0035694838},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99248827,0.00016073254,0.006742887,0.000031140742,0.000032129283,0.000008014691,0.0000377701,0.0000581759,0.00044079756],"genre_scores_gemma":[0.99723816,0.00006240145,0.0023337586,0.000013876944,0.0000074718273,0.000010072717,0.00003187963,0.00001276535,0.00028964086],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99968755,0.000038301343,0.000018628722,0.000070334645,0.00012876577,0.000056376808],"domain_scores_gemma":[0.9988361,0.0006110148,0.00020391181,0.000061057035,0.0002157401,0.000072140356],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00037718494,0.00029020177,0.00025753674,0.0002379191,0.00015802086,0.00025405633,0.00025791812,0.0003925676,0.00097295997],"category_scores_gemma":[0.0009918767,0.00016073498,0.00015741886,0.00013401073,0.0003464679,0.0002612683,0.00029822503,0.00028139484,0.00013758705],"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":[0.0002050365,0.000024446352,0.0006670716,0.000048267102,0.0000069473176,0.000065019274,0.00008660572,0.0015456657,0.9926803,0.00008045104,0.000047607788,0.0045425263],"study_design_scores_gemma":[0.000026177391,0.0009679551,0.012502645,0.000016412541,0.000013102252,0.00013366477,0.00014175677,0.023509528,0.96157044,0.00008356738,0.001006183,0.000028605044],"about_ca_topic_score_codex":0.00014295761,"about_ca_topic_score_gemma":0.0001375439,"teacher_disagreement_score":0.00097295997,"about_ca_system_score_codex":0.00018367193,"about_ca_system_score_gemma":0.000112618756,"threshold_uncertainty_score":0.0032548904},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.954929,0.00027729425,0.034482677,0.000051966923,0.000085516935,0.000038101338,0.00015503069,0.0005710698,0.009409385],"genre_scores_gemma":[0.9889098,0.00013817684,0.005131286,0.000038830472,0.000013901635,0.000018542787,0.00027803166,0.000050947296,0.0054204985],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997669,0.000022642345,0.000014550397,0.00003096672,0.000108068605,0.000056851448],"domain_scores_gemma":[0.99967444,0.0000591099,0.000029153196,0.000027178821,0.00017920037,0.000030796906],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00027406454,0.0003995272,0.00025963457,0.00024682705,0.00022877459,0.00032006507,0.00029244737,0.00027833888,0.0045134183],"category_scores_gemma":[0.0003737231,0.000112801354,0.00018389431,0.00016246662,0.00020839869,0.00025995955,0.000519727,0.00025798724,0.0005844914],"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":[0.0012051323,0.00011719848,0.006373779,0.00035977247,0.000020759486,0.00042965807,0.00035973202,0.0143125085,0.8964932,0.0014144197,0.0008945195,0.07801922],"study_design_scores_gemma":[0.00008973391,0.0035470913,0.073157206,0.000085166765,0.00013963014,0.0008805493,0.0005684348,0.08915116,0.8077044,0.0007543594,0.023839302,0.000082966246],"about_ca_topic_score_codex":0.0020571786,"about_ca_topic_score_gemma":0.0039278143,"teacher_disagreement_score":0.0045134183,"about_ca_system_score_codex":0.00021203591,"about_ca_system_score_gemma":0.00027668526,"threshold_uncertainty_score":0.01509887},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9288596,0.0001612441,0.06910106,0.00005210747,0.000017072927,0.000021532493,0.0000716626,0.0004107934,0.0013048963],"genre_scores_gemma":[0.9953845,0.000023551871,0.0037737803,0.0000105236095,0.0000036049519,0.0000064132423,0.000032059786,0.000014450603,0.00075116276],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99991107,0.000011573142,0.0000023607508,0.000023282626,0.000038514278,0.000013189983],"domain_scores_gemma":[0.9998443,0.000059972655,0.000018365876,0.000010189086,0.00005622734,0.000010849784],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017546628,0.0002103579,0.0002921857,0.00036616204,0.00020411788,0.00022272981,0.00037354216,0.00030189878,0.0011427021],"category_scores_gemma":[0.00020466608,0.00013771922,0.00021820294,0.0001689618,0.00018741141,0.00022971314,0.00017383811,0.00013897232,0.00018012364],"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":[0.0005674063,0.000077251374,0.0045025754,0.00008153101,0.000024774921,0.00013693205,0.00011093073,0.014871669,0.94720817,0.00031801316,0.0002493498,0.031851444],"study_design_scores_gemma":[0.00004971981,0.00085554976,0.06531599,0.000023688743,0.00011247463,0.000207808,0.00016360015,0.3662504,0.564741,0.0002201231,0.0020149741,0.00004450068],"about_ca_topic_score_codex":0.0010826322,"about_ca_topic_score_gemma":0.00087599637,"teacher_disagreement_score":0.0011427021,"about_ca_system_score_codex":0.00020874273,"about_ca_system_score_gemma":0.00021574834,"threshold_uncertainty_score":0.003822744},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9878753,0.00021171501,0.009008359,0.00004104455,0.000017354132,0.000017230695,0.000065302025,0.00009077917,0.0026730103],"genre_scores_gemma":[0.99755585,0.00008113071,0.0015255223,0.000011193534,0.0000042084175,0.0000058378746,0.00003990331,0.000014582076,0.0007617296],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99991035,0.000018168745,0.000003687362,0.000015120505,0.000030282697,0.000022339222],"domain_scores_gemma":[0.99967575,0.00018515122,0.00001882933,0.000025148203,0.00005870118,0.000036375506],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015691979,0.0002912662,0.00035040083,0.00038288257,0.00052301935,0.00040188825,0.00024897626,0.0004999571,0.0019360661],"category_scores_gemma":[0.00046939263,0.00014586256,0.0003250374,0.00030254447,0.0005148339,0.00027693226,0.00021033123,0.0002939011,0.00012184023],"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":[0.0020169213,0.00049732934,0.013140582,0.00025694046,0.000058562753,0.0030002326,0.00083276344,0.09229529,0.8529158,0.0017557808,0.0005547099,0.032674983],"study_design_scores_gemma":[0.000090369664,0.0010655395,0.14864692,0.000046996236,0.00010090332,0.0012002403,0.00094485254,0.6177222,0.2268607,0.0007456753,0.0024350528,0.00014058076],"about_ca_topic_score_codex":0.0022372217,"about_ca_topic_score_gemma":0.0015629162,"teacher_disagreement_score":0.0022372217,"about_ca_system_score_codex":0.00012733981,"about_ca_system_score_gemma":0.00016665834,"threshold_uncertainty_score":0.0064768195},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98813695,0.00043759134,0.0073600984,0.0002008802,0.000034728768,0.000008751772,0.00087974884,0.00024668896,0.0026944648],"genre_scores_gemma":[0.9961415,0.00015283207,0.0019657507,0.00002455209,0.000011590222,0.0000064775495,0.0005536502,0.000040167604,0.0011033979],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999436,0.0000059140452,0.000001183434,0.000015275891,0.000018823637,0.000015225613],"domain_scores_gemma":[0.99991214,0.000027672071,0.000014917517,0.0000070421293,0.000023254492,0.000015023252],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00011107328,0.0002815129,0.00008502466,0.0009578317,0.00037153135,0.00013131235,0.0003249463,0.0002512268,0.0026420525],"category_scores_gemma":[0.00020187213,0.00009713735,0.00013105104,0.00045521805,0.00016805943,0.00024170913,0.00023112776,0.00028205317,0.00021539256],"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":[0.0005656192,0.000065294436,0.0076661734,0.000086425294,0.000029247216,0.00018466274,0.00026647968,0.0006266111,0.9725274,0.00046437778,0.0011739244,0.016343893],"study_design_scores_gemma":[0.000037142516,0.0002199766,0.2959251,0.00003416701,0.000065010885,0.00044391982,0.0004660473,0.020844733,0.67147726,0.0006908517,0.0097386,0.00005726668],"about_ca_topic_score_codex":0.004695062,"about_ca_topic_score_gemma":0.006728389,"teacher_disagreement_score":0.004695062,"about_ca_system_score_codex":0.00019526726,"about_ca_system_score_gemma":0.00014220712,"threshold_uncertainty_score":0.009335458},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99794894,0.000050414095,0.0015750258,0.000015085766,0.0000056383215,0.000010972563,0.00004063329,0.000019937002,0.0003334223],"genre_scores_gemma":[0.99776244,0.000054938635,0.0016202695,0.0000123516065,0.0000061484975,0.000021313004,0.00006616401,0.000012818187,0.00044336403],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9996259,0.000046524077,0.000017163551,0.00008154227,0.00015237616,0.00007641348],"domain_scores_gemma":[0.99924135,0.00034065495,0.00012052552,0.000055342814,0.00016140282,0.000080685364],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00028836084,0.00042067346,0.00037703593,0.00023970653,0.00040919555,0.00025303595,0.0003060204,0.0004153952,0.0011528768],"category_scores_gemma":[0.00075856014,0.00011564654,0.00015745757,0.00018626466,0.0006354471,0.00030831777,0.00038551967,0.0003977415,0.00012781742],"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":[0.00033395117,0.00006880348,0.0010981188,0.000046093417,0.0000037617028,0.000106892454,0.000109999244,0.00033098756,0.9962638,0.000047155176,0.00001997975,0.0015703717],"study_design_scores_gemma":[0.000058997583,0.002499645,0.02726229,0.000014744177,0.00001889249,0.00028210186,0.0002510296,0.006286612,0.9623514,0.00007513635,0.0008671178,0.000032063217],"about_ca_topic_score_codex":0.0005700021,"about_ca_topic_score_gemma":0.0007104821,"teacher_disagreement_score":0.0011528768,"about_ca_system_score_codex":0.00026973468,"about_ca_system_score_gemma":0.00011928787,"threshold_uncertainty_score":0.0038567185},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99652463,0.000044790217,0.0028150675,0.000015932823,0.000014336238,0.000024230118,0.000044294324,0.000038397684,0.00047823228],"genre_scores_gemma":[0.9961443,0.000054215587,0.0029566076,0.000013658234,0.000007363309,0.000047444017,0.0000520098,0.000013121737,0.00071122166],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9993262,0.00009944147,0.00004037665,0.00011697263,0.00030857182,0.000108425134],"domain_scores_gemma":[0.99884653,0.0004102773,0.00013514493,0.00011298352,0.00039511485,0.00009994848],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00051719823,0.0006021426,0.00047504876,0.00036147304,0.00048399525,0.00027262804,0.00044210654,0.0005205148,0.0012572885],"category_scores_gemma":[0.0013147271,0.00021158898,0.00027525157,0.00023233413,0.0006048264,0.00036803362,0.00044932702,0.00034133377,0.00014994173],"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":[0.0007182095,0.00032260318,0.0020454712,0.00014242956,0.000012239843,0.00021251471,0.00026388373,0.0039408607,0.98549485,0.00013445114,0.000090588495,0.0066219163],"study_design_scores_gemma":[0.00009869682,0.006833792,0.024327662,0.000029723175,0.000043227294,0.00027180807,0.00036637145,0.030072795,0.93641806,0.00011913923,0.001343947,0.00007486201],"about_ca_topic_score_codex":0.0008207287,"about_ca_topic_score_gemma":0.0010381315,"teacher_disagreement_score":0.0012572885,"about_ca_system_score_codex":0.00022922941,"about_ca_system_score_gemma":0.00020302567,"threshold_uncertainty_score":0.0042060614},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9974323,0.00011126236,0.0007207178,0.000046785986,0.00003384277,0.000019899144,0.00067027577,0.000069587164,0.0008952216],"genre_scores_gemma":[0.99463636,0.00015276947,0.0015038804,0.00005431062,0.0000121665,0.00004357344,0.000895937,0.000048626007,0.002652281],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9994161,0.00006679689,0.00006381139,0.00008470503,0.00027005107,0.00009848959],"domain_scores_gemma":[0.99930894,0.00024770235,0.000101380145,0.000029797324,0.00023873657,0.000073504314],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00044840574,0.0003515936,0.00036261894,0.00038056273,0.0005890137,0.00076298177,0.00032043146,0.00041869926,0.0021746329],"category_scores_gemma":[0.0014395041,0.0001814347,0.00040615434,0.00040911773,0.00042587038,0.000588838,0.00032024577,0.00044712998,0.00047728437],"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":[0.0017989307,0.00013789612,0.0052330187,0.000068218236,0.000016660759,0.00015886934,0.00040462625,0.00095623574,0.9834751,0.000201349,0.0005452818,0.0070038377],"study_design_scores_gemma":[0.000021584212,0.0012997953,0.02466525,0.000009544636,0.000029777777,0.00009098462,0.0006229672,0.0046464307,0.96711427,0.000064556596,0.0013819035,0.000052951193],"about_ca_topic_score_codex":0.0051529654,"about_ca_topic_score_gemma":0.0033172355,"teacher_disagreement_score":0.0051529654,"about_ca_system_score_codex":0.0005003402,"about_ca_system_score_gemma":0.0006019361,"threshold_uncertainty_score":0.010245979},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9186213,0.0006080485,0.06272531,0.00006924078,0.000059788814,0.00008819553,0.0005626879,0.0002436267,0.01702179],"genre_scores_gemma":[0.98554647,0.00037145385,0.010071159,0.000015317175,0.000011621208,0.000047665173,0.00043802868,0.000054453252,0.0034438286],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998472,0.00001559075,0.000008650772,0.000019366065,0.00008627164,0.000022843276],"domain_scores_gemma":[0.9997825,0.00008925493,0.000031749583,0.000015737027,0.00007100445,0.000009840526],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018396042,0.0004316262,0.00032341582,0.0005224267,0.00039106587,0.0005111597,0.00027143708,0.00038134897,0.0020073394],"category_scores_gemma":[0.00042741603,0.00017818889,0.0004674443,0.0003782791,0.0002614011,0.00032905984,0.0002122657,0.0002547559,0.00041601554],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00012500524,0.000085070664,0.0076968553,0.00018373091,0.000035727167,0.00038513998,0.00012017143,0.8124859,0.14516935,0.0031905745,0.00062374474,0.029898848],"study_design_scores_gemma":[0.000019850891,0.0002433826,0.020882431,0.000021115351,0.000013246819,0.00015589014,0.00011469214,0.9490332,0.025473475,0.0010411172,0.0029713763,0.000030105477],"about_ca_topic_score_codex":0.0018956835,"about_ca_topic_score_gemma":0.0015224381,"teacher_disagreement_score":0.0020073394,"about_ca_system_score_codex":0.0001987629,"about_ca_system_score_gemma":0.0003471584,"threshold_uncertainty_score":0.0067151785},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9833904,0.00014174396,0.01288624,0.000036198577,0.00004362661,0.000039292285,0.00014872247,0.0001250965,0.0031887742],"genre_scores_gemma":[0.9906623,0.00006347061,0.00822749,0.000007779589,0.0000030074389,0.000029798788,0.00006905924,0.000013385945,0.0009239161],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998635,0.000019589379,0.000006470873,0.000020939215,0.000064563355,0.000024923434],"domain_scores_gemma":[0.9995049,0.00017341155,0.000069724985,0.0000696489,0.00014490572,0.00003737427],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00038713973,0.0003607525,0.000266438,0.0002459813,0.0002523859,0.00027655918,0.0003194453,0.0003483898,0.0011154987],"category_scores_gemma":[0.000774655,0.00010908024,0.00016289864,0.0001501923,0.00034668946,0.00025861422,0.00020062945,0.000261615,0.00015401142],"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":[0.00059597264,0.0006820828,0.0041661817,0.00038470348,0.000019315978,0.00018497652,0.000197517,0.1744787,0.78205705,0.0015402287,0.00079807726,0.034895156],"study_design_scores_gemma":[0.000049339218,0.0018928823,0.0077584814,0.000032916752,0.000022951848,0.00009173212,0.00016955036,0.4926153,0.49493617,0.00033673647,0.0020569284,0.000036976035],"about_ca_topic_score_codex":0.00049040234,"about_ca_topic_score_gemma":0.0007741078,"teacher_disagreement_score":0.0011154987,"about_ca_system_score_codex":0.00017984254,"about_ca_system_score_gemma":0.00016171101,"threshold_uncertainty_score":0.0037317276},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9811462,0.00023488664,0.016599227,0.00003646483,0.0000325757,0.00005137884,0.00014700484,0.00010951937,0.0016426622],"genre_scores_gemma":[0.9818564,0.0002021237,0.0166748,0.00001537363,0.000006421763,0.000056840978,0.00017873709,0.000024546265,0.000984654],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994137,0.00014829061,0.000044446766,0.000057682635,0.00026477716,0.000071087605],"domain_scores_gemma":[0.9988367,0.00047831802,0.00016525453,0.00014251375,0.0003296596,0.000047489026],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.001131059,0.00085610006,0.00046273414,0.00036052044,0.00032226194,0.0003146089,0.00051302725,0.00054302334,0.0014103303],"category_scores_gemma":[0.00148806,0.00019995378,0.00041059227,0.0002993825,0.00036459925,0.0003200013,0.00029278663,0.00032081996,0.0001632099],"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":[0.00102117,0.0013940467,0.0072438535,0.0009372709,0.000052546635,0.00039929536,0.0002885562,0.19944057,0.7497808,0.0008054423,0.00071125943,0.037925202],"study_design_scores_gemma":[0.00013943549,0.011247841,0.016798155,0.00009607392,0.0000829249,0.00030307975,0.00044905904,0.3072957,0.6605666,0.00030000188,0.0026262642,0.000094866096],"about_ca_topic_score_codex":0.00061502215,"about_ca_topic_score_gemma":0.0015183135,"teacher_disagreement_score":0.0014103303,"about_ca_system_score_codex":0.0001677087,"about_ca_system_score_gemma":0.00019802629,"threshold_uncertainty_score":0.0059816837},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99167496,0.000086217784,0.006394313,0.000037141515,0.000015263446,0.000006924917,0.000106682564,0.00011265228,0.0015659167],"genre_scores_gemma":[0.99794227,0.000062084,0.0014890317,0.0000073679093,0.000008109053,0.0000042834326,0.000100379126,0.000018324767,0.00036815982],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99994683,0.000006187704,0.0000037185273,0.000012450299,0.000016204063,0.000014612288],"domain_scores_gemma":[0.9997868,0.00004824786,0.000059683585,0.000015822738,0.00003610446,0.000053286058],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000119112025,0.00021325627,0.00021103934,0.00032395555,0.00018966172,0.00056736,0.00018785939,0.00011651533,0.0005371059],"category_scores_gemma":[0.00035595082,0.00011586839,0.00022773433,0.000236037,0.00044171335,0.00034735014,0.00028892775,0.00023798332,0.000057981906],"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":[0.0009883781,0.00022372829,0.023344884,0.000092426744,0.00006401749,0.001324785,0.000541143,0.20839469,0.7328886,0.012709971,0.001103257,0.01832418],"study_design_scores_gemma":[0.00006397428,0.00048839074,0.1332124,0.0000134509655,0.0000269458,0.00030414393,0.00019288165,0.8199942,0.04123009,0.0031314576,0.0012515914,0.0000904551],"about_ca_topic_score_codex":0.0024926034,"about_ca_topic_score_gemma":0.0012009529,"teacher_disagreement_score":0.0024926034,"about_ca_system_score_codex":0.00035114758,"about_ca_system_score_gemma":0.00020444706,"threshold_uncertainty_score":0.004956186},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9878682,0.00006273501,0.010086479,0.000015865147,0.00001955077,0.00001868922,0.00003056317,0.00008292638,0.0018151064],"genre_scores_gemma":[0.9966354,0.00003205306,0.002629484,0.0000074161067,0.0000025456304,0.000004955523,0.000025531492,0.000005770467,0.00065703626],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99981946,0.000018477307,0.0000068913355,0.000023765688,0.00010381653,0.000027624157],"domain_scores_gemma":[0.9992086,0.00032342103,0.00008465902,0.00007510681,0.000241276,0.00006679883],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024685223,0.00032736576,0.0002443544,0.00028407777,0.00021300165,0.00022855046,0.00024911016,0.00035219744,0.00074909366],"category_scores_gemma":[0.0007628207,0.00014406907,0.00018535471,0.00014365232,0.00045127966,0.00024171652,0.0002479271,0.00023628377,0.0001415607],"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":[0.00040028238,0.000108307526,0.0057530664,0.000086495515,0.000008974236,0.00081427925,0.00014658229,0.022074848,0.956741,0.00041505255,0.00008292197,0.01336808],"study_design_scores_gemma":[0.00006604446,0.0036630253,0.044445276,0.00003065515,0.000020000201,0.0011027626,0.0002739167,0.20168275,0.74646735,0.00060957833,0.0015794357,0.00005925367],"about_ca_topic_score_codex":0.00087517785,"about_ca_topic_score_gemma":0.00075223227,"teacher_disagreement_score":0.00087517785,"about_ca_system_score_codex":0.00013885641,"about_ca_system_score_gemma":0.00016589793,"threshold_uncertainty_score":0.0025058985},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99594575,0.00004397611,0.0015721275,0.00008155786,0.00002800735,0.0000096562535,0.000117228694,0.00014807553,0.0020536268],"genre_scores_gemma":[0.9994072,0.0000106565385,0.00019122363,0.00000946386,0.000005522938,0.000001978458,0.000039529215,0.00001257483,0.000321964],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997894,0.000032222768,0.0000055500977,0.000040090414,0.000076311924,0.000056406912],"domain_scores_gemma":[0.99867344,0.00070337375,0.000051614104,0.0000648236,0.00033502333,0.00017172229],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002208764,0.00030184755,0.00047117932,0.0006665473,0.0005262947,0.00041527578,0.0004793843,0.00069200434,0.0042126165],"category_scores_gemma":[0.00096029206,0.0001699082,0.00024042616,0.00034066293,0.0006532435,0.00038244628,0.00034223046,0.00062761316,0.00024226494],"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":[0.008543852,0.0009381477,0.033709295,0.0003236912,0.00009273245,0.0050758296,0.0014492978,0.051265087,0.8247246,0.0015588471,0.0039501227,0.06836847],"study_design_scores_gemma":[0.00019257657,0.002630028,0.33766025,0.00007253711,0.00008442866,0.0013667508,0.0014864618,0.44834688,0.20536731,0.0007550327,0.0018725325,0.00016516904],"about_ca_topic_score_codex":0.002539852,"about_ca_topic_score_gemma":0.001454572,"teacher_disagreement_score":0.0042126165,"about_ca_system_score_codex":0.00033858026,"about_ca_system_score_gemma":0.00022896752,"threshold_uncertainty_score":0.014092624},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9985033,0.00010987977,0.0011502113,0.000003276299,0.000005733623,0.0000047091316,0.000011615509,0.00001446012,0.00019680762],"genre_scores_gemma":[0.9988821,0.000059956496,0.0007836318,0.000005457334,0.000006489972,0.0000060195207,0.000052712327,0.000005998226,0.00019755957],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99979514,0.000025971698,0.000010700909,0.000053712116,0.000067768975,0.000046682457],"domain_scores_gemma":[0.9996093,0.00011048468,0.00012885175,0.000016659515,0.00004442588,0.0000903678],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003078804,0.00029043428,0.00036779745,0.00046252864,0.00032188394,0.0006168322,0.00018311988,0.0001984423,0.00038274153],"category_scores_gemma":[0.0006230774,0.00011807379,0.00014987883,0.00029440536,0.0006326797,0.00035066335,0.0004237262,0.00026921672,0.00005707144],"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":[0.0007210989,0.00010849554,0.009756585,0.000034163866,0.000014079123,0.00030351957,0.00023715802,0.0015372069,0.9810688,0.00037912314,0.000051019342,0.005788717],"study_design_scores_gemma":[0.00009300182,0.0021557303,0.22552057,0.000021136191,0.000064785585,0.0005043777,0.00045949582,0.049598623,0.71950877,0.00048444368,0.0015231286,0.00006596012],"about_ca_topic_score_codex":0.00052934827,"about_ca_topic_score_gemma":0.0003463312,"teacher_disagreement_score":0.0006168322,"about_ca_system_score_codex":0.00025838995,"about_ca_system_score_gemma":0.00014108178,"threshold_uncertainty_score":0.0018747449},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9987025,0.000043871067,0.00097360305,0.00000635795,0.0000020285736,0.0000052268456,0.00003350611,0.000019718518,0.00021318554],"genre_scores_gemma":[0.99943584,0.000017781449,0.00042152937,0.0000034585635,0.0000015697813,0.0000049071646,0.000035828136,0.0000022903046,0.00007668539],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99994063,0.000006125792,0.00000273444,0.000018049368,0.000011801267,0.000020598014],"domain_scores_gemma":[0.9997851,0.000065910936,0.000059400252,0.000019136263,0.000027080507,0.000043454962],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012668218,0.00015506396,0.00022261089,0.000363316,0.00020980646,0.00022412321,0.00012429716,0.0001860912,0.00051014754],"category_scores_gemma":[0.00040276005,0.00009553601,0.00011284611,0.00014081998,0.00046981836,0.00015917684,0.00030061865,0.00020533655,0.000046678582],"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":[0.00030117398,0.000045683493,0.016354803,0.000045357818,0.000008055376,0.00032979925,0.00033925028,0.0033153556,0.97130877,0.0003209679,0.00014514777,0.007485622],"study_design_scores_gemma":[0.00007983459,0.0010845184,0.63635314,0.000040133287,0.000040938467,0.0008567236,0.0009521225,0.11675678,0.24195296,0.0005958907,0.0011711871,0.00011585705],"about_ca_topic_score_codex":0.00095603656,"about_ca_topic_score_gemma":0.0005509148,"teacher_disagreement_score":0.00095603656,"about_ca_system_score_codex":0.00013910556,"about_ca_system_score_gemma":0.00015998453,"threshold_uncertainty_score":0.0019009709},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.5759231,0.0005305887,0.41439724,0.00031477463,0.000064751584,0.00003978178,0.0002074281,0.0003991064,0.008123168],"genre_scores_gemma":[0.98884577,0.00012929944,0.009947752,0.000018276249,0.000012368075,0.00002473951,0.000070350805,0.000018871764,0.00093255413],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99985814,0.000044686014,0.000009125414,0.00003081658,0.000036346388,0.00002076922],"domain_scores_gemma":[0.99955744,0.00023662914,0.00007200254,0.000028412167,0.0000893504,0.000016213302],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00045182588,0.0006256579,0.00034972705,0.00039597493,0.00022770457,0.0006179431,0.00061741687,0.000692131,0.00047695872],"category_scores_gemma":[0.0014533238,0.00026221207,0.00034221678,0.00034462954,0.00043569016,0.00073534995,0.00031594405,0.00063433737,0.000118649186],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000010709334,0.000010227545,0.00058813463,0.000007004843,0.000006410515,0.000012990291,0.00000765355,0.99515873,0.0008899458,0.0005286747,0.000038877868,0.0027406402],"study_design_scores_gemma":[3.1530547e-7,0.0000017459522,0.000104107836,8.458863e-7,4.8786586e-7,0.0000010390727,7.757272e-7,0.9996308,0.00012555705,0.0001217253,0.000011903664,7.621298e-7],"about_ca_topic_score_codex":0.003999205,"about_ca_topic_score_gemma":0.0023911132,"teacher_disagreement_score":0.003999205,"about_ca_system_score_codex":0.00039110947,"about_ca_system_score_gemma":0.00032140315,"threshold_uncertainty_score":0.007951856},"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":"review","genre_gemma":"review","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"review","genre_consensus":"review","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0028983874,0.85914487,0.019007958,0.03696836,0.03149903,0.000021693637,0.00016512962,0.0003220925,0.049972538],"genre_scores_gemma":[0.050970692,0.83356816,0.017613042,0.018909838,0.042610805,0.000107813496,0.0004030151,0.00048659515,0.035330053],"study_design_codex":"design_other","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.99704534,0.00068440905,0.00026256568,0.0004441419,0.0012866253,0.00027692452],"domain_scores_gemma":[0.99550927,0.00215096,0.00022471401,0.00049554405,0.0012236666,0.00039585304],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0036698806,0.00080326764,0.0015268836,0.0017564335,0.0010489378,0.0054658805,0.0016992043,0.003499326,0.009076374],"category_scores_gemma":[0.0075169886,0.00037708518,0.0006777689,0.0015173886,0.0036254385,0.008354845,0.0031965675,0.0051683737,0.0042777066],"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":[0.00015064838,0.00007105173,0.0007119298,0.0030331411,0.0000510575,0.00035146956,0.00063354603,0.0017880113,0.0027852375,0.36082646,0.13822055,0.49137694],"study_design_scores_gemma":[0.0000051698557,0.000045817087,0.0001637484,0.0007176214,0.0000068711506,0.00025139799,0.00013373067,0.00031036075,0.00038168143,0.031158121,0.96680796,0.00001758885],"about_ca_topic_score_codex":0.0008907885,"about_ca_topic_score_gemma":0.0005460139,"teacher_disagreement_score":0.009076374,"about_ca_system_score_codex":0.0012673796,"about_ca_system_score_gemma":0.0025465086,"threshold_uncertainty_score":0.03036356},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9808257,0.00020431732,0.012849801,0.0001664626,0.000049956736,0.000039831564,0.00012975476,0.00009849236,0.0056357523],"genre_scores_gemma":[0.9955012,0.000076579614,0.003718743,0.000018955165,0.00000581638,0.000012386747,0.000056121233,0.000007221378,0.0006030316],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998097,0.000041584164,0.000015605727,0.00003014337,0.00005323684,0.00004970996],"domain_scores_gemma":[0.99936944,0.0002978255,0.00012959515,0.00003918269,0.0000975627,0.00006642033],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003398076,0.00055620016,0.00060471107,0.00046526606,0.0006707567,0.00084167015,0.000478844,0.0009164504,0.0011422145],"category_scores_gemma":[0.0011405782,0.00020513321,0.0005741535,0.0004746936,0.0006955731,0.00045366935,0.0006005968,0.0005206833,0.00009141926],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00017259267,0.00015143695,0.012587972,0.00007101146,0.000034542605,0.00056355254,0.000091339105,0.9674864,0.012403366,0.0013771697,0.00021934988,0.004841241],"study_design_scores_gemma":[0.000020845493,0.0000786034,0.0016955958,0.0000056534514,0.000010996993,0.00003074082,0.000060418843,0.99639314,0.0014112901,0.00013650961,0.00014585312,0.000010414644],"about_ca_topic_score_codex":0.012883508,"about_ca_topic_score_gemma":0.0059260363,"teacher_disagreement_score":0.012883508,"about_ca_system_score_codex":0.0004801091,"about_ca_system_score_gemma":0.0006599897,"threshold_uncertainty_score":0.025617063},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6726515,0.0005998434,0.31409281,0.00017526797,0.00009364721,0.00015141645,0.0003677247,0.00073151774,0.0111362925],"genre_scores_gemma":[0.98501796,0.00029541022,0.012078518,0.000010980825,0.000010444864,0.00007670565,0.00013627135,0.00004104736,0.00233262],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998956,0.000024715346,0.000007901405,0.000017906597,0.000037541053,0.000016404398],"domain_scores_gemma":[0.9998228,0.000089184934,0.0000270489,0.000017444723,0.000032892887,0.000010702879],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00028059914,0.00052587176,0.00040755156,0.00028604787,0.00031409372,0.00076944986,0.000561646,0.00063808676,0.00045175225],"category_scores_gemma":[0.00070705754,0.0003289723,0.00037361414,0.0002585435,0.00043740467,0.00062050304,0.00032301986,0.0005325368,0.00014307597],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000023908478,0.000026130321,0.0007788968,0.000034003748,0.00000796749,0.000050352723,0.000034925008,0.9837249,0.008583796,0.0021880928,0.0001222669,0.004424744],"study_design_scores_gemma":[0.0000024838605,0.000007999188,0.00035005691,0.0000018169659,0.0000014137636,0.0000044249628,0.000002611398,0.99830806,0.0009726307,0.00023741521,0.00010838689,0.0000027521846],"about_ca_topic_score_codex":0.0037026273,"about_ca_topic_score_gemma":0.0015248336,"teacher_disagreement_score":0.0037026273,"about_ca_system_score_codex":0.00038952197,"about_ca_system_score_gemma":0.00051295,"threshold_uncertainty_score":0.007362187},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.20358713,0.0007379187,0.7913366,0.00015398867,0.000053206455,0.000055325698,0.00014910357,0.0007602784,0.003166395],"genre_scores_gemma":[0.9388782,0.0011669964,0.05855716,0.000030458064,0.00006964704,0.00006448957,0.00020813358,0.00016052103,0.000864446],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993845,0.00017050222,0.000043355234,0.00011073786,0.00024633537,0.00004448338],"domain_scores_gemma":[0.99532664,0.0030228805,0.00045618738,0.0004652279,0.0006545042,0.00007454707],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0020504948,0.0009967834,0.00084285426,0.0007131396,0.0003726871,0.0010814797,0.0011540937,0.0008288461,0.00044387425],"category_scores_gemma":[0.007950034,0.0006388491,0.00069688255,0.0005354977,0.00095294364,0.0017808997,0.00049655064,0.0010776714,0.00026383155],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00004105924,0.00008841831,0.0031259991,0.00011721747,0.000027404378,0.000051267987,0.000072112154,0.9511148,0.0131337335,0.010452328,0.00012859158,0.021647086],"study_design_scores_gemma":[0.0000021418134,0.000011368184,0.00033348854,0.0000033347194,0.0000020685752,0.000007905218,0.000002552579,0.99641895,0.0023731333,0.00072013465,0.00011762446,0.0000071837517],"about_ca_topic_score_codex":0.003176727,"about_ca_topic_score_gemma":0.00131532,"teacher_disagreement_score":0.003176727,"about_ca_system_score_codex":0.0006034775,"about_ca_system_score_gemma":0.0011725711,"threshold_uncertainty_score":0.010844171},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99912566,0.00004612757,0.0005459367,0.000009488763,0.000004894151,0.0000034678526,0.000015380938,0.000027799086,0.00022126839],"genre_scores_gemma":[0.9995683,0.00001460996,0.00020503039,0.0000040589666,0.0000017342866,0.0000027258723,0.000024957217,0.0000056577346,0.00017285027],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99966574,0.00005392529,0.000023920235,0.000053529573,0.000102891856,0.00009997914],"domain_scores_gemma":[0.99872655,0.00054197246,0.00016272049,0.00013299998,0.0002207699,0.00021497057],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00046334762,0.0005825032,0.00061348034,0.00042307656,0.00040295225,0.0004807791,0.00029853568,0.0006234522,0.0012860683],"category_scores_gemma":[0.0019213979,0.00014162308,0.00022234957,0.00013153303,0.0006507009,0.0004691406,0.00054333033,0.0003367643,0.0002385499],"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":[0.0023256056,0.00022606438,0.007988253,0.00022514869,0.000029298812,0.00043449193,0.00027489284,0.017547721,0.9589723,0.00012960445,0.00010456346,0.011742089],"study_design_scores_gemma":[0.00015561887,0.005811125,0.057196993,0.000045698314,0.000054113567,0.00045908536,0.0002985612,0.052184153,0.88311416,0.00012834927,0.0004980008,0.000054081836],"about_ca_topic_score_codex":0.00070829986,"about_ca_topic_score_gemma":0.0006252513,"teacher_disagreement_score":0.0012860683,"about_ca_system_score_codex":0.00017975888,"about_ca_system_score_gemma":0.0001354753,"threshold_uncertainty_score":0.004302323},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99912566,0.00004612757,0.0005459367,0.000009488763,0.000004894151,0.0000034678526,0.000015380938,0.000027799086,0.00022126839],"genre_scores_gemma":[0.9995683,0.00001460996,0.00020503039,0.0000040589666,0.0000017342866,0.0000027258723,0.000024957217,0.0000056577346,0.00017285027],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99966574,0.00005392529,0.000023920235,0.000053529573,0.000102891856,0.00009997914],"domain_scores_gemma":[0.99872655,0.00054197246,0.00016272049,0.00013299998,0.0002207699,0.00021497057],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00046334762,0.0005825032,0.00061348034,0.00042307656,0.00040295225,0.0004807791,0.00029853568,0.0006234522,0.0012860683],"category_scores_gemma":[0.0019213979,0.00014162308,0.00022234957,0.00013153303,0.0006507009,0.0004691406,0.00054333033,0.0003367643,0.0002385499],"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":[0.0023256056,0.00022606438,0.007988253,0.00022514869,0.000029298812,0.00043449193,0.00027489284,0.017547721,0.9589723,0.00012960445,0.00010456346,0.011742089],"study_design_scores_gemma":[0.00015561887,0.005811125,0.057196993,0.000045698314,0.000054113567,0.00045908536,0.0002985612,0.052184153,0.88311416,0.00012834927,0.0004980008,0.000054081836],"about_ca_topic_score_codex":0.00070829986,"about_ca_topic_score_gemma":0.0006252513,"teacher_disagreement_score":0.0012860683,"about_ca_system_score_codex":0.00017975888,"about_ca_system_score_gemma":0.0001354753,"threshold_uncertainty_score":0.004302323},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"dataset","genre_consensus":"dataset","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.00020776747,0.00010267214,0.00026486276,0.000075000724,0.000060007333,0.000028355811,0.99254334,0.0032278737,0.0034900322],"genre_scores_gemma":[0.0005032683,0.00009724227,0.00039338024,0.000043182943,0.000009040853,0.000063757834,0.9971042,0.00019660234,0.0015893059],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.9992011,0.00009869272,0.00007484639,0.00021885498,0.00022970675,0.0001769403],"domain_scores_gemma":[0.99935967,0.000096679985,0.00003213249,0.00028452164,0.0001435715,0.00008345551],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0007767044,0.0032522117,0.0017621666,0.0027021102,0.0010261235,0.0028296881,0.0033295788,0.0030905146,0.26543266],"category_scores_gemma":[0.0022291976,0.00077504263,0.0013489126,0.0052368836,0.0005090519,0.0015192688,0.0025548246,0.0021658877,0.53594124],"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":[0.000059381964,0.000040371357,0.0009477033,0.0005993975,0.000029422568,0.000041641764,0.000020802234,0.0007944128,0.0002054764,0.0006016385,0.98542804,0.011231734],"study_design_scores_gemma":[0.00014867523,0.000018235563,0.0020840908,0.00023737579,0.000012895778,0.000045286208,0.000056323974,0.0015317695,0.0005163078,0.0013787188,0.99394566,0.000024770863],"about_ca_topic_score_codex":0.014590686,"about_ca_topic_score_gemma":0.013779271,"teacher_disagreement_score":0.73456734,"about_ca_system_score_codex":0.0010036989,"about_ca_system_score_gemma":0.0012653057,"threshold_uncertainty_score":0.8879607},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9228025,0.00012862365,0.07427599,0.00008088978,0.000022243694,0.000019865776,0.00007444138,0.00032630962,0.0022692494],"genre_scores_gemma":[0.99705493,0.000032559412,0.0022906598,0.00000608064,0.0000033386114,0.000007811808,0.000036267204,0.000015455731,0.0005529735],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999237,0.000018866524,0.0000025385077,0.000015824317,0.000023395345,0.000015680193],"domain_scores_gemma":[0.9997979,0.000103776976,0.000031669362,0.0000072521448,0.000034501933,0.000025003405],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00019527397,0.00062684057,0.00036740632,0.00030028092,0.00036282587,0.0005274133,0.0002946859,0.0005825812,0.00044275922],"category_scores_gemma":[0.0006330859,0.0002776712,0.00027696235,0.00011243109,0.00039104163,0.00029200412,0.0002845494,0.0003646608,0.0001312151],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00006445898,0.00003758597,0.0029308966,0.000021279335,0.0000062774843,0.00008606968,0.00003746326,0.98106074,0.012639137,0.000269737,0.00007629847,0.002770052],"study_design_scores_gemma":[0.0000024235474,0.000011459917,0.0006202974,0.0000010518553,0.00000114403,0.0000034456393,0.00000486302,0.9986092,0.00069283595,0.000028976963,0.000022501865,0.0000016879119],"about_ca_topic_score_codex":0.01664358,"about_ca_topic_score_gemma":0.00816781,"teacher_disagreement_score":0.01664358,"about_ca_system_score_codex":0.00043249564,"about_ca_system_score_gemma":0.0004781694,"threshold_uncertainty_score":0.033093393},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.954929,0.00027729425,0.034482677,0.000051966923,0.000085516935,0.000038101338,0.00015503069,0.0005710698,0.009409385],"genre_scores_gemma":[0.9889098,0.00013817684,0.005131286,0.000038830472,0.000013901635,0.000018542787,0.00027803166,0.000050947296,0.0054204985],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997669,0.000022642345,0.000014550397,0.00003096672,0.000108068605,0.000056851448],"domain_scores_gemma":[0.99967444,0.0000591099,0.000029153196,0.000027178821,0.00017920037,0.000030796906],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00027406454,0.0003995272,0.00025963457,0.00024682705,0.00022877459,0.00032006507,0.00029244737,0.00027833888,0.0045134183],"category_scores_gemma":[0.0003737231,0.000112801354,0.00018389431,0.00016246662,0.00020839869,0.00025995955,0.000519727,0.00025798724,0.0005844914],"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":[0.0012051323,0.00011719848,0.006373779,0.00035977247,0.000020759486,0.00042965807,0.00035973202,0.0143125085,0.8964932,0.0014144197,0.0008945195,0.07801922],"study_design_scores_gemma":[0.00008973391,0.0035470913,0.073157206,0.000085166765,0.00013963014,0.0008805493,0.0005684348,0.08915116,0.8077044,0.0007543594,0.023839302,0.000082966246],"about_ca_topic_score_codex":0.0020571786,"about_ca_topic_score_gemma":0.0039278143,"teacher_disagreement_score":0.0045134183,"about_ca_system_score_codex":0.00021203591,"about_ca_system_score_gemma":0.00027668526,"threshold_uncertainty_score":0.01509887},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9818185,0.000083443374,0.017069656,0.000048136473,0.000026571015,0.000029466039,0.000024247767,0.000112568596,0.000787441],"genre_scores_gemma":[0.9942648,0.00003144182,0.0053981864,0.000010090935,0.0000047748913,0.000011963413,0.000022644705,0.000012047748,0.00024407748],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99978644,0.00007969972,0.00001582673,0.000027859443,0.000050336213,0.000039845356],"domain_scores_gemma":[0.99897015,0.0006395304,0.0001071771,0.00004617871,0.00012415912,0.00011275616],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0008277218,0.00048290362,0.00041716007,0.00040964203,0.0004106297,0.0006068685,0.000543379,0.0010079474,0.00041037917],"category_scores_gemma":[0.0019175994,0.00029822133,0.00052097166,0.00020464891,0.00061293977,0.0005096712,0.0004781391,0.000653444,0.00007483067],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0001496415,0.00007151968,0.003021278,0.000027007993,0.000012637368,0.000108091954,0.000036982397,0.9863084,0.0068093087,0.0001947571,0.00004148956,0.0032189307],"study_design_scores_gemma":[0.000006497286,0.00006581373,0.0003461243,0.000002168731,0.0000028739541,0.0000063508573,0.000010827308,0.9981766,0.0013428993,0.000020999656,0.000015623264,0.0000033610056],"about_ca_topic_score_codex":0.015059806,"about_ca_topic_score_gemma":0.007900946,"teacher_disagreement_score":0.015059806,"about_ca_system_score_codex":0.00046082612,"about_ca_system_score_gemma":0.00084734894,"threshold_uncertainty_score":0.0299443},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"dataset","genre_consensus":"dataset","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.00019635173,0.00009881343,0.00021576909,0.00006046084,0.00005086125,0.00002516319,0.9941935,0.0025349958,0.002624151],"genre_scores_gemma":[0.00047383556,0.00009606616,0.00034831482,0.000038150793,0.000007760811,0.00006228068,0.9974936,0.00017005389,0.001309925],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.99922216,0.00009612815,0.00007313107,0.00020398984,0.0002248035,0.00017985652],"domain_scores_gemma":[0.99938905,0.00010015929,0.000034277153,0.00025265626,0.00014203339,0.00008174981],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00077570695,0.003269195,0.0016704099,0.0025931837,0.00094991375,0.0025737835,0.0032906341,0.003105589,0.23687693],"category_scores_gemma":[0.0022798423,0.00079642364,0.001292623,0.004919564,0.0005084773,0.0014355116,0.002473097,0.002079376,0.5039857],"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":[0.00006338841,0.000041254356,0.0010084066,0.00072850555,0.00003095034,0.00004346765,0.000023571503,0.0008387711,0.00021555563,0.00059989624,0.98643225,0.009974147],"study_design_scores_gemma":[0.00018415884,0.000021665042,0.0023994094,0.0002962612,0.000014798982,0.00004682381,0.000066589986,0.0015959742,0.00060906686,0.0014636184,0.99327314,0.000028497612],"about_ca_topic_score_codex":0.01500354,"about_ca_topic_score_gemma":0.015744112,"teacher_disagreement_score":0.76312304,"about_ca_system_score_codex":0.0009916693,"about_ca_system_score_gemma":0.0013454598,"threshold_uncertainty_score":0.7924323},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"dataset","genre_consensus":"dataset","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.00033478093,0.00012695792,0.00040295266,0.000087353474,0.000067599256,0.00003927156,0.9926373,0.0033579648,0.0029457968],"genre_scores_gemma":[0.00039739732,0.000078550576,0.00039740567,0.00002081657,0.000007387315,0.00006745,0.9973201,0.00013958235,0.001571264],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.99885345,0.00015062498,0.00011023091,0.00023698759,0.00041064693,0.00023798617],"domain_scores_gemma":[0.99927264,0.00009243531,0.00005118241,0.0003389893,0.00016290823,0.000081700855],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0008940524,0.0037152732,0.0019522876,0.0051225624,0.00084163446,0.0030405817,0.0030862102,0.002613361,0.21185651],"category_scores_gemma":[0.0027207937,0.0006801355,0.0011856614,0.007681899,0.00048638682,0.0012612417,0.0025348943,0.0019447966,0.48804787],"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":[0.00006625496,0.00006202201,0.0008726205,0.00062879897,0.00003032077,0.000052530377,0.000026097665,0.0007105229,0.00036534842,0.00048434397,0.97329354,0.023407582],"study_design_scores_gemma":[0.00011283626,0.000023763547,0.0029290216,0.00015614483,0.000013288559,0.00006884288,0.000054639608,0.0016145562,0.00073816,0.0011631664,0.9931023,0.000023162842],"about_ca_topic_score_codex":0.0140607385,"about_ca_topic_score_gemma":0.013562673,"teacher_disagreement_score":0.7881435,"about_ca_system_score_codex":0.00093719317,"about_ca_system_score_gemma":0.0014420609,"threshold_uncertainty_score":0.70873064},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.4740798,0.0007396239,0.5150709,0.000100164,0.00012403462,0.000080900674,0.00004275955,0.0013288463,0.00843299],"genre_scores_gemma":[0.99140376,0.00009958221,0.007407029,0.000012325203,0.000021815309,0.00001233401,0.00001594583,0.000023792594,0.0010034028],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9996458,0.00006811285,0.00001749835,0.00007791769,0.00013708578,0.00005355475],"domain_scores_gemma":[0.9996333,0.00014300823,0.000082551924,0.000026079326,0.000082323066,0.00003268218],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003172888,0.00052258535,0.00036683827,0.00040764656,0.00033791302,0.00032390552,0.00038342318,0.0002466685,0.00090809073],"category_scores_gemma":[0.00059242104,0.00011853599,0.00021537654,0.00017073484,0.0005588564,0.00026515292,0.00054491137,0.00019176745,0.00012399399],"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":[0.0013432449,0.0002286721,0.003024637,0.00040368122,0.000036771704,0.00026563904,0.00032142038,0.09874271,0.7771094,0.007867271,0.000581624,0.11007492],"study_design_scores_gemma":[0.0002133261,0.002361565,0.008644945,0.0000601294,0.00013094909,0.00022980003,0.000099809586,0.63448656,0.33768702,0.0034321414,0.012547587,0.00010630402],"about_ca_topic_score_codex":0.0008287351,"about_ca_topic_score_gemma":0.0007648982,"teacher_disagreement_score":0.00090809073,"about_ca_system_score_codex":0.00027090783,"about_ca_system_score_gemma":0.00024910376,"threshold_uncertainty_score":0.0030378103},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.997033,0.00007922399,0.0024163185,0.000010864689,0.0000062145054,0.0000061985356,0.00001762711,0.000021305854,0.00040934124],"genre_scores_gemma":[0.99936026,0.000042817148,0.00045763334,0.000007244741,0.0000016917915,0.0000019961815,0.0000109855355,0.0000047446424,0.00011261564],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998196,0.000030304245,0.000013215343,0.000028852302,0.00005579574,0.000052270087],"domain_scores_gemma":[0.9990338,0.000612353,0.00012049289,0.0000584413,0.00009787169,0.00007697937],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004217548,0.0003347164,0.000301832,0.00021082294,0.0002226557,0.0005279175,0.00018142934,0.00028046864,0.0008429367],"category_scores_gemma":[0.0012090863,0.00016969514,0.00031446855,0.0001496565,0.00051619456,0.00029545696,0.00051831163,0.00031457408,0.0001061715],"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":[0.0025991066,0.00016789288,0.019515676,0.00016688304,0.00004536929,0.0007073909,0.0002838198,0.15300149,0.8071262,0.00048614183,0.000085871514,0.015814167],"study_design_scores_gemma":[0.00016642259,0.0034652282,0.063871264,0.000044005003,0.00013673604,0.00027892593,0.00044892915,0.20531681,0.72504133,0.00035025144,0.00077812973,0.00010192553],"about_ca_topic_score_codex":0.00085222267,"about_ca_topic_score_gemma":0.00090355397,"teacher_disagreement_score":0.00085222267,"about_ca_system_score_codex":0.0003759943,"about_ca_system_score_gemma":0.00017707559,"threshold_uncertainty_score":0.0028198957},"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":"other","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"other","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.00020299209,0.00010187292,0.00024301946,0.00007022569,0.000053706714,0.000025831876,0.99346936,0.002785824,0.0030471864],"genre_scores_gemma":[0.00045678578,0.0000935016,0.00035515934,0.0000366653,0.000008079239,0.000060178332,0.9975061,0.00016658085,0.0013169257],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.99915266,0.00010997954,0.000078350815,0.00022295563,0.0002496732,0.00018642769],"domain_scores_gemma":[0.99932337,0.00010804085,0.00003642783,0.00029519195,0.00015268261,0.0000842282],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0007976225,0.00324715,0.0017123333,0.0027926816,0.0009897269,0.0027056232,0.0032794399,0.0031120987,0.237798],"category_scores_gemma":[0.0024546948,0.00072103005,0.0012593475,0.005262672,0.00048016032,0.0015504992,0.0024118952,0.0021449132,0.50313187],"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":[0.000056279503,0.000039283506,0.0008752714,0.0006317018,0.00002728136,0.0000377708,0.000020628902,0.00082525687,0.00019341295,0.00060064625,0.9857451,0.010947333],"study_design_scores_gemma":[0.00015148502,0.000020081683,0.0021709495,0.00025209933,0.000013281692,0.000042920215,0.00005787997,0.0016447849,0.00054702774,0.0015848469,0.9934888,0.000025807733],"about_ca_topic_score_codex":0.013958368,"about_ca_topic_score_gemma":0.014044328,"teacher_disagreement_score":0.762202,"about_ca_system_score_codex":0.0010045561,"about_ca_system_score_gemma":0.001314744,"threshold_uncertainty_score":0.7955136},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.72005403,0.00032110143,0.27069435,0.000236998,0.00007916606,0.00013488617,0.00016248453,0.00057887455,0.00773815],"genre_scores_gemma":[0.9785452,0.000093198156,0.0198229,0.000012969668,0.0000078695175,0.0000757731,0.00006627831,0.00003373621,0.0013420971],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998704,0.000041234343,0.0000065868385,0.000020413805,0.00004174703,0.000019644873],"domain_scores_gemma":[0.9994803,0.0003237482,0.000040443854,0.000028348783,0.000092095215,0.000035119065],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004905316,0.0007683571,0.0005812312,0.0005083888,0.0004736405,0.00063212455,0.00055111304,0.0014807138,0.0010090326],"category_scores_gemma":[0.0013380158,0.00030461242,0.0007414628,0.0002525816,0.0006837903,0.00031533706,0.00047591943,0.00063862547,0.000173955],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000041380776,0.000055215765,0.001128006,0.000035337584,0.00001043627,0.00007552731,0.00004558284,0.9887307,0.0053870003,0.00063420576,0.00007911254,0.0037774893],"study_design_scores_gemma":[0.000004857561,0.000018557665,0.000158642,0.0000026097364,0.0000018219242,0.000005844799,0.000006297354,0.9989581,0.00072646525,0.00005273786,0.00006099523,0.0000029690164],"about_ca_topic_score_codex":0.0067865048,"about_ca_topic_score_gemma":0.0027256045,"teacher_disagreement_score":0.0067865048,"about_ca_system_score_codex":0.0005152092,"about_ca_system_score_gemma":0.0007084507,"threshold_uncertainty_score":0.013494015},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"dataset","genre_consensus":"dataset","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.00020633268,0.00010041631,0.0002281611,0.00006834586,0.00005529899,0.000026603588,0.99377716,0.0026810006,0.0028566825],"genre_scores_gemma":[0.00048138673,0.00009372252,0.00035753177,0.000038952167,0.0000082763045,0.000059905236,0.9974705,0.00016335213,0.0013263599],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.9991959,0.0001017563,0.000075994496,0.00021196833,0.00023381783,0.0001806501],"domain_scores_gemma":[0.99935395,0.00010371418,0.000034779645,0.0002739461,0.0001492923,0.000084382256],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0007993322,0.0032875093,0.0016678482,0.002652411,0.0010101858,0.0026766541,0.0032488864,0.0031587954,0.23055702],"category_scores_gemma":[0.00227485,0.0007634749,0.00130509,0.004852593,0.0005109658,0.0014688428,0.0024463162,0.0021403478,0.4962493],"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":[0.00006361642,0.00004221797,0.0010150669,0.00067965145,0.000030438378,0.000042591837,0.000022399629,0.0008213668,0.00022120865,0.0006082197,0.98589516,0.010558102],"study_design_scores_gemma":[0.00017359394,0.00002051505,0.0023726348,0.0002722022,0.00001425983,0.000045091536,0.00006363299,0.0015768922,0.0005916768,0.0014275772,0.99341464,0.000027240356],"about_ca_topic_score_codex":0.014757635,"about_ca_topic_score_gemma":0.014870381,"teacher_disagreement_score":0.769443,"about_ca_system_score_codex":0.00097442203,"about_ca_system_score_gemma":0.0013162938,"threshold_uncertainty_score":0.77129006},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0014221485,0.013676892,0.0234667,0.0011369868,0.003492743,0.000036610316,0.00014631018,0.0003297467,0.9562919],"genre_scores_gemma":[0.010114773,0.007659182,0.002803725,0.00045692705,0.00078167877,0.000024951487,0.00018216716,0.00010847014,0.9778682],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9998,0.000019363084,0.0000056150234,0.000035201396,0.0001228906,0.000016897548],"domain_scores_gemma":[0.99991906,0.000015651462,0.0000042840575,0.00001080918,0.000041264597,0.000008980836],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00013332856,0.0009637759,0.00035002508,0.00085630605,0.0007301272,0.00134759,0.0005131782,0.00092236773,0.050234154],"category_scores_gemma":[0.00033297326,0.00019750999,0.00028540008,0.00047332843,0.000563908,0.00085689785,0.00096200855,0.0010508127,0.02977677],"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":[0.00003572629,0.000041974396,0.00020335069,0.00031853584,0.000011921087,0.00016088664,0.00037431068,0.002380487,0.006831334,0.14519942,0.28137398,0.5630681],"study_design_scores_gemma":[0.0000021834114,0.000019684747,0.00028618437,0.00012726305,0.0000055574023,0.00020077637,0.00007907438,0.0007122059,0.0009916533,0.014219546,0.9833482,0.000007680025],"about_ca_topic_score_codex":0.0015976622,"about_ca_topic_score_gemma":0.0032638204,"teacher_disagreement_score":0.050234154,"about_ca_system_score_codex":0.0006201634,"about_ca_system_score_gemma":0.000493323,"threshold_uncertainty_score":0.16804999},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99361414,0.000042337866,0.0031489388,0.00010579467,0.000017027822,0.000024055114,0.00021224222,0.00009251322,0.0027429159],"genre_scores_gemma":[0.9967405,0.000021734724,0.002264646,0.000017263032,0.0000033789365,0.000011419485,0.00011921276,0.000014756196,0.00080697524],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99991226,0.000015096673,0.000005343012,0.000013999045,0.000023163657,0.000030185845],"domain_scores_gemma":[0.9995272,0.00026476005,0.000040590494,0.000022688484,0.00005993797,0.000084751046],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002496818,0.0003533862,0.00045721393,0.00034954987,0.0005654271,0.0006935083,0.00041942994,0.0008710004,0.0014127742],"category_scores_gemma":[0.0009550046,0.00022990356,0.00033350443,0.00031395062,0.0006800373,0.00037174037,0.00039949673,0.0005305401,0.000092845046],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00039823807,0.00019159402,0.012298756,0.00005232916,0.00002680114,0.00064172747,0.00020851032,0.96353877,0.01582359,0.0016307529,0.0005499929,0.0046389643],"study_design_scores_gemma":[0.000024557978,0.000058222908,0.002350176,0.0000036195563,0.0000033845743,0.000021324176,0.000037942125,0.99596137,0.0012574638,0.0001310404,0.00014280505,0.000008018146],"about_ca_topic_score_codex":0.015566532,"about_ca_topic_score_gemma":0.008165651,"teacher_disagreement_score":0.015566532,"about_ca_system_score_codex":0.00080594345,"about_ca_system_score_gemma":0.0008008433,"threshold_uncertainty_score":0.030951858},"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":"editorial","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"editorial","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0010517058,0.004003558,0.00015854581,0.9227423,0.054510668,0.00001741764,0.00004534086,0.000049175003,0.017421268],"genre_scores_gemma":[0.019413251,0.0036437074,0.00025571685,0.8626664,0.07210292,0.00005424215,0.000032686086,0.000060817776,0.041770335],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.99880147,0.0003100763,0.00007211488,0.00021646073,0.00032809362,0.0002716427],"domain_scores_gemma":[0.99752885,0.0011490795,0.00014594961,0.00010323363,0.00056203984,0.0005109748],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.001234712,0.0005753033,0.00092079863,0.00066507835,0.0035490235,0.0030694152,0.0011505883,0.025301447,0.012012369],"category_scores_gemma":[0.018474344,0.0004154799,0.0005960268,0.00034151264,0.0017078058,0.002272723,0.001186571,0.018467342,0.0060484684],"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":[0.000029639474,0.000015429492,0.00026374328,0.000028466922,0.0000056432086,0.0056669684,0.00010926805,0.00003680687,0.00006841049,0.0025694652,0.98557824,0.0056279325],"study_design_scores_gemma":[0.000049463648,0.000029055644,0.00051521073,0.00017533092,0.000016589418,0.0074475217,0.00046180023,0.00027502025,0.00019605445,0.00820268,0.9825988,0.00003260464],"about_ca_topic_score_codex":0.0023832528,"about_ca_topic_score_gemma":0.00363986,"teacher_disagreement_score":0.025301447,"about_ca_system_score_codex":0.0018453054,"about_ca_system_score_gemma":0.002528902,"threshold_uncertainty_score":0.040185332},"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":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0015047921,0.008749214,0.006214847,0.026838535,0.21727847,0.0005547775,0.013438565,0.0014868821,0.723934],"genre_scores_gemma":[0.004473297,0.002989747,0.0016828614,0.0043690186,0.017188545,0.00020401829,0.006532425,0.00055627956,0.9620037],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.99936014,0.00008031913,0.00003978494,0.000107654596,0.00034777008,0.0000643533],"domain_scores_gemma":[0.9949799,0.00058334216,0.00016017741,0.00041288772,0.0031817404,0.0006819372],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0011797841,0.0008323642,0.00055897253,0.0030545173,0.0022891946,0.0026399738,0.0010767002,0.00083674904,0.47972855],"category_scores_gemma":[0.0101782195,0.00023214435,0.00045130934,0.0017001873,0.00043065232,0.0019021854,0.0017996724,0.0020351384,0.32108814],"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":[0.00001968263,0.000014194494,0.000090665984,0.000049488684,0.000001206732,0.000025433032,0.000034576555,0.00003847917,0.00007883653,0.0029685777,0.96657336,0.0301055],"study_design_scores_gemma":[0.000003230513,0.0000087732,0.0002772406,0.00007015592,0.0000013814355,0.000025428208,0.000053204763,0.000023438633,0.0000708302,0.0020685443,0.99739456,0.0000031848447],"about_ca_topic_score_codex":0.0049824165,"about_ca_topic_score_gemma":0.0070117954,"teacher_disagreement_score":0.47972855,"about_ca_system_score_codex":0.0016864337,"about_ca_system_score_gemma":0.002124771,"threshold_uncertainty_score":0},"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":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0025501146,0.0051114117,0.07836358,0.0006473435,0.0040604216,0.000094979405,0.00021148038,0.0005250854,0.9084356],"genre_scores_gemma":[0.072108984,0.009623498,0.021358054,0.0012974301,0.0014703387,0.000095509204,0.000515745,0.00057751476,0.89295286],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99961567,0.000038060793,0.000023017195,0.00010442854,0.00018458036,0.000034251854],"domain_scores_gemma":[0.9998807,0.000022771676,0.000007077375,0.000034806406,0.000046150235,0.000008631118],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00033573847,0.00062163034,0.00061308494,0.00056891656,0.00070537365,0.0019286787,0.0010817925,0.0010186445,0.04156183],"category_scores_gemma":[0.00059400074,0.00035693063,0.00068922294,0.0008197403,0.0009508776,0.003797301,0.0010966006,0.0025247124,0.020314297],"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":[0.00007527483,0.0000705817,0.00006834629,0.00046619965,0.000015806685,0.00020385702,0.00022790767,0.0010483842,0.016139012,0.69075423,0.074922286,0.21600804],"study_design_scores_gemma":[0.000024900997,0.00009505376,0.00016100975,0.00011966507,0.000016627077,0.00078436034,0.00006931094,0.0026270428,0.011210912,0.13609767,0.8487687,0.000024749335],"about_ca_topic_score_codex":0.00018375268,"about_ca_topic_score_gemma":0.00028512947,"teacher_disagreement_score":0.04156183,"about_ca_system_score_codex":0.00053469464,"about_ca_system_score_gemma":0.00051279186,"threshold_uncertainty_score":0.1390382},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.86730343,0.0006659666,0.07577431,0.00050116685,0.00043436396,0.000036774047,0.000064203436,0.00023353494,0.05498633],"genre_scores_gemma":[0.98399574,0.00012691306,0.003660107,0.00006822272,0.00006723212,0.000015230822,0.000039759285,0.00004330565,0.011983439],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998461,0.000023933177,0.0000044559833,0.00002796631,0.00006214357,0.000035486024],"domain_scores_gemma":[0.9998617,0.000045296176,0.00002229725,0.0000166449,0.000018947609,0.0000350696],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001587618,0.00036108214,0.0004898695,0.00029739397,0.0003036246,0.0010446133,0.0007753777,0.00090831355,0.0032760128],"category_scores_gemma":[0.0006278768,0.00034173718,0.00033822664,0.00021614326,0.0011102749,0.000650601,0.0012561686,0.00072984264,0.00040020572],"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":[0.0016413025,0.00037436667,0.0024891126,0.00042909212,0.00020051823,0.003478674,0.0020558618,0.16612619,0.45560578,0.27806252,0.004468638,0.08506798],"study_design_scores_gemma":[0.00026030277,0.000389576,0.0065091737,0.00005111923,0.00006119519,0.0011904527,0.0006601015,0.89676434,0.022460686,0.06417473,0.007335654,0.00014269917],"about_ca_topic_score_codex":0.00019219783,"about_ca_topic_score_gemma":0.00012368543,"teacher_disagreement_score":0.0032760128,"about_ca_system_score_codex":0.00025296237,"about_ca_system_score_gemma":0.00013939236,"threshold_uncertainty_score":0.010959387},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"dataset","genre_consensus":"dataset","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.00020295985,0.000099603574,0.0002453799,0.00006929803,0.00005646784,0.000027835042,0.99313545,0.002991392,0.0031715655],"genre_scores_gemma":[0.00047301716,0.00009442942,0.00037155312,0.00003962683,0.000008574064,0.0000620797,0.99729186,0.00018350733,0.0014754126],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.99920446,0.00009957018,0.00007435235,0.00021073097,0.00023317206,0.00017765207],"domain_scores_gemma":[0.9993622,0.00009868735,0.000033294233,0.00027463576,0.00014900506,0.000082272876],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00077312184,0.0032087334,0.0016987232,0.00268779,0.0009923801,0.002682877,0.0032768224,0.0030431182,0.24988312],"category_scores_gemma":[0.0022740944,0.00073533173,0.0012819683,0.0050249323,0.00049070345,0.0014453022,0.0024090093,0.0020802182,0.5227319],"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":[0.00005920459,0.00003916388,0.00090129673,0.0006284986,0.000028180826,0.000039363604,0.00002074067,0.0007706101,0.0002018934,0.0005812158,0.98602515,0.010704767],"study_design_scores_gemma":[0.0001625473,0.000018875184,0.0021383804,0.0002558928,0.000013218876,0.000043548,0.00005859448,0.0014889516,0.0005486971,0.0014082162,0.99383754,0.000025481366],"about_ca_topic_score_codex":0.01432636,"about_ca_topic_score_gemma":0.014049908,"teacher_disagreement_score":0.7501169,"about_ca_system_score_codex":0.00096659584,"about_ca_system_score_gemma":0.0012714233,"threshold_uncertainty_score":0.83594227},"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":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.002685632,0.012526787,0.074581206,0.00083412975,0.0024818394,0.00005243927,0.00020544535,0.0010155139,0.9056169],"genre_scores_gemma":[0.021956453,0.008029485,0.010989757,0.00041412696,0.00058731245,0.000049000962,0.0003130768,0.0002644658,0.9573963],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.9998741,0.000009439241,0.0000046950354,0.000024631025,0.00007569285,0.000011415668],"domain_scores_gemma":[0.99994564,0.000008760872,0.0000036124952,0.000013681763,0.000020656384,0.0000076728265],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012358687,0.0008129106,0.0004671274,0.00078952924,0.00076995924,0.0021673536,0.00061098003,0.0007876802,0.033852067],"category_scores_gemma":[0.0002580315,0.0003295257,0.00034827107,0.0007000313,0.0007285067,0.0013419554,0.0010582771,0.0011620302,0.019667746],"study_design_candidate":"theoretical_or_conceptual","study_design_consensus":"theoretical_or_conceptual","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00004244542,0.00006115353,0.00017264986,0.00030869883,0.0000137542775,0.00017711941,0.0003816712,0.0024372,0.012702635,0.42283177,0.14454302,0.41632786],"study_design_scores_gemma":[0.000007832524,0.00003268791,0.00035752068,0.00010555409,0.000009843523,0.0003388158,0.0000665277,0.002660315,0.0048212917,0.063549966,0.9280341,0.000015557147],"about_ca_topic_score_codex":0.0004841473,"about_ca_topic_score_gemma":0.0007282985,"teacher_disagreement_score":0.033852067,"about_ca_system_score_codex":0.0004239862,"about_ca_system_score_gemma":0.00041643178,"threshold_uncertainty_score":0.11324644},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.36039722,0.00056704704,0.62751704,0.00045210874,0.00047983186,0.001121099,0.00016731278,0.0012267036,0.008071648],"genre_scores_gemma":[0.8614776,0.0001475788,0.13277557,0.000084916384,0.00005056286,0.00022603224,0.00008624384,0.000043444405,0.0051080636],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995209,0.00006739581,0.00002770042,0.00012312231,0.00021878183,0.00004221369],"domain_scores_gemma":[0.9986255,0.00023481812,0.0001491953,0.00017019456,0.000684476,0.00013577768],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00065935566,0.00049177645,0.00039126258,0.00036159004,0.0006247489,0.00084893574,0.0012632573,0.0013613061,0.0027741008],"category_scores_gemma":[0.0010640854,0.00034372346,0.0004060486,0.000098204415,0.0003440129,0.00073923863,0.00044413516,0.00043606473,0.0008896378],"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":[0.0007331811,0.00041102146,0.002756225,0.0004729806,0.000036159334,0.00054328877,0.00036012696,0.010368926,0.8797927,0.0023841083,0.0011551224,0.10098612],"study_design_scores_gemma":[0.0007677726,0.022500856,0.012214527,0.00013479905,0.00016984904,0.0018557768,0.00049850333,0.31549388,0.60625005,0.001203375,0.038764693,0.00014591748],"about_ca_topic_score_codex":0.0004679956,"about_ca_topic_score_gemma":0.0005639494,"teacher_disagreement_score":0.0027741008,"about_ca_system_score_codex":0.00025971181,"about_ca_system_score_gemma":0.00081439264,"threshold_uncertainty_score":0.009280264},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.5514262,0.00061954197,0.43331957,0.00025078628,0.00015109932,0.00019447513,0.00017729402,0.0020897004,0.011771323],"genre_scores_gemma":[0.86897135,0.00018803442,0.1279663,0.00004054227,0.000032094984,0.00011979582,0.00014862695,0.00019316806,0.002340056],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992304,0.00020951647,0.00003719517,0.00008072049,0.00038726148,0.000054991193],"domain_scores_gemma":[0.9969078,0.0020615705,0.0001905067,0.00015583336,0.0005922295,0.00009212786],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0013249271,0.0010787864,0.0007806531,0.00083140505,0.00049111666,0.0009885258,0.0012128482,0.0010416469,0.0014506537],"category_scores_gemma":[0.0042240876,0.0003634388,0.0004989678,0.00043649998,0.0005245251,0.00055265747,0.0007771331,0.00074238545,0.00037490515],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00014137705,0.00012382527,0.0024544194,0.00010782851,0.00004532337,0.00007375522,0.00009114253,0.9580294,0.0077508143,0.0015239844,0.00022006856,0.029438088],"study_design_scores_gemma":[0.000006977523,0.00003473881,0.000172345,0.0000041344438,0.000003557393,0.0000047249664,0.000010361538,0.998353,0.00122523,0.00007983943,0.00010103427,0.0000041357725],"about_ca_topic_score_codex":0.009476282,"about_ca_topic_score_gemma":0.00682722,"teacher_disagreement_score":0.009476282,"about_ca_system_score_codex":0.00057359017,"about_ca_system_score_gemma":0.0014010152,"threshold_uncertainty_score":0.01884222},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"dataset","genre_consensus":"dataset","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.00030969703,0.0000959102,0.00029963694,0.000076831406,0.00006772425,0.0000367101,0.99262965,0.002878411,0.003605442],"genre_scores_gemma":[0.0006100941,0.00008947902,0.00048087517,0.000035013334,0.000008712465,0.000064418535,0.9969313,0.0001486076,0.0016315231],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.99923754,0.00011171115,0.00006697063,0.00017279077,0.00022994395,0.00018114413],"domain_scores_gemma":[0.9994562,0.000077309196,0.000031527776,0.00023550121,0.00013076489,0.00006858549],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00078557606,0.0027483422,0.001285071,0.0025675127,0.0008488565,0.0021768278,0.0026714862,0.0024966078,0.20720188],"category_scores_gemma":[0.0018011522,0.00058139744,0.0011046692,0.0043850024,0.0004070328,0.0011494987,0.0020834378,0.001730869,0.44040117],"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":[0.000073739306,0.00005350404,0.0012696228,0.0007136335,0.00002902048,0.00004761444,0.000031947686,0.0009806545,0.00029901753,0.00066854514,0.9784248,0.017407924],"study_design_scores_gemma":[0.00013623618,0.000024449317,0.0032458715,0.00026377605,0.000011304068,0.000044710418,0.0000783463,0.0019572682,0.0005150591,0.0011579468,0.99254227,0.000022751505],"about_ca_topic_score_codex":0.018409556,"about_ca_topic_score_gemma":0.016731974,"teacher_disagreement_score":0.7927981,"about_ca_system_score_codex":0.00085887196,"about_ca_system_score_gemma":0.0010913513,"threshold_uncertainty_score":0.69315934},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.051908374,0.00036817676,0.94392824,0.0001725868,0.00009046865,0.0000882616,0.00009154048,0.00045575458,0.0028966416],"genre_scores_gemma":[0.80083346,0.00040206205,0.19543591,0.000078532874,0.000095421456,0.00036039183,0.00016933621,0.00018336081,0.0024414686],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995838,0.00013687674,0.000023746765,0.000051464605,0.00016462737,0.00003946052],"domain_scores_gemma":[0.99899095,0.00055821426,0.00014115448,0.00006771517,0.00019937969,0.00004258943],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0012348954,0.0009151013,0.00094841665,0.00066094147,0.0005695373,0.0011168953,0.0013167158,0.0016552293,0.0010120638],"category_scores_gemma":[0.0036557193,0.0005339887,0.00096425397,0.00034050384,0.0012220604,0.00066089706,0.0010635611,0.0011939621,0.0002899338],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000020292993,0.000013627488,0.00021022686,0.00001838328,0.000013766997,0.00003047449,0.000010908198,0.9921225,0.0023435822,0.0026361658,0.000050986277,0.0025291243],"study_design_scores_gemma":[0.0000013137117,0.0000037980353,0.000014244976,7.340882e-7,6.907297e-7,0.0000010546421,6.159263e-7,0.9996959,0.00010924237,0.00014675864,0.000024691426,0.0000010862259],"about_ca_topic_score_codex":0.0090797115,"about_ca_topic_score_gemma":0.0030546058,"teacher_disagreement_score":0.0090797115,"about_ca_system_score_codex":0.0007712767,"about_ca_system_score_gemma":0.0016409172,"threshold_uncertainty_score":0.01805377},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0046895314,0.0005959169,0.988279,0.00008765222,0.000055560686,0.00003513689,0.00019365584,0.00049498037,0.0055685053],"genre_scores_gemma":[0.39412457,0.0019290338,0.5825823,0.00019757128,0.00024603403,0.00042152256,0.0016905011,0.00046658318,0.018341828],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99974805,0.000051343093,0.00000854477,0.000041834493,0.00012313468,0.000027118424],"domain_scores_gemma":[0.9997582,0.0000979363,0.000020343301,0.000014541988,0.00009460753,0.000014359608],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005934063,0.0011836378,0.0008235478,0.00050936814,0.00037531622,0.0010270982,0.0016889297,0.0008035646,0.007126343],"category_scores_gemma":[0.0010442855,0.00041034908,0.00066091906,0.0003558577,0.00027093806,0.0008602914,0.00083093497,0.0009404743,0.0020563928],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000019214967,0.000026233158,0.00034311108,0.000054869848,0.000013716743,0.000043019438,0.000015716561,0.946191,0.0011001051,0.0060880077,0.0020767006,0.044028312],"study_design_scores_gemma":[0.0000010170145,0.0000079739,0.000036997993,0.0000069429707,0.0000024801056,0.0000056745994,0.0000030184399,0.997537,0.000114677896,0.0016020895,0.0006803664,0.0000017813398],"about_ca_topic_score_codex":0.0074298843,"about_ca_topic_score_gemma":0.0075379102,"teacher_disagreement_score":0.0074298843,"about_ca_system_score_codex":0.00054481765,"about_ca_system_score_gemma":0.000800915,"threshold_uncertainty_score":0.02383995},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"dataset","genre_consensus":"dataset","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.00030932497,0.000102695616,0.0003322119,0.000081518614,0.00007329665,0.000038360056,0.992015,0.0032151765,0.0038324718],"genre_scores_gemma":[0.000614155,0.000091072965,0.0004966375,0.000035426954,0.000008950617,0.00006422503,0.9969289,0.00015299898,0.0016076821],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.9992048,0.000114380986,0.00007083543,0.00017720847,0.00024593456,0.0001867408],"domain_scores_gemma":[0.99943787,0.000074401214,0.000031025804,0.00025094583,0.00013731253,0.00006843462],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0007872548,0.002807892,0.0014045767,0.0027071482,0.00089661294,0.0022968987,0.0027867416,0.0025066482,0.2155286],"category_scores_gemma":[0.0018590788,0.0005810205,0.0011478552,0.004759347,0.00041537994,0.001169888,0.0021506832,0.0017731527,0.443552],"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":[0.00007182797,0.000051606537,0.0011770172,0.0007203256,0.000030541793,0.00004813085,0.00003080057,0.0011133492,0.00028363086,0.0006839596,0.9776284,0.018160459],"study_design_scores_gemma":[0.00013224449,0.000024738883,0.003135363,0.00026320157,0.000011879631,0.000047520654,0.00007532154,0.0021600102,0.00053841743,0.0013597249,0.9922271,0.000024559899],"about_ca_topic_score_codex":0.019676805,"about_ca_topic_score_gemma":0.017415674,"teacher_disagreement_score":0.7844714,"about_ca_system_score_codex":0.0009321163,"about_ca_system_score_gemma":0.0011111584,"threshold_uncertainty_score":0.721015},"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":"other","genre_gemma":"dataset","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"dataset","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.007862426,0.004493052,0.02600038,0.0022179375,0.003150227,0.00066890917,0.014563564,0.014236385,0.9268071],"genre_scores_gemma":[0.0885345,0.0031343168,0.024874141,0.0019940664,0.00077437196,0.001646483,0.04092143,0.0046675694,0.8334531],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.99927455,0.000088981615,0.000029026927,0.00015881972,0.00032091158,0.00012765589],"domain_scores_gemma":[0.9996327,0.000053009742,0.000029028884,0.00010725207,0.00009225396,0.00008574734],"candidate_categories":["insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.00069687655,0.0015844399,0.0019309784,0.0019144736,0.0016571207,0.003981786,0.0035364425,0.0048853084,0.8051016],"category_scores_gemma":[0.00080889673,0.0007452811,0.0010980677,0.0031045305,0.0013919703,0.0020718717,0.0035221933,0.0033436506,0.74266714],"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":[0.000618639,0.0007011276,0.0028036572,0.0024992668,0.00021583162,0.0011443993,0.00032936328,0.0058766077,0.033284094,0.050709188,0.5532021,0.3486157],"study_design_scores_gemma":[0.00011561289,0.000063983854,0.0007955432,0.00022542903,0.000025287034,0.00044481037,0.00010320264,0.016812308,0.004873567,0.0068481425,0.9696213,0.000070729715],"about_ca_topic_score_codex":0.0017679083,"about_ca_topic_score_gemma":0.0016999624,"teacher_disagreement_score":0.19489843,"about_ca_system_score_codex":0.0023031805,"about_ca_system_score_gemma":0.00069105334,"threshold_uncertainty_score":0.27799898},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9869653,0.00012700855,0.0028917491,0.00015253008,0.000046301375,0.00002947257,0.0003376164,0.00010646265,0.009343511],"genre_scores_gemma":[0.9967886,0.000058319525,0.0011915254,0.000027356446,0.000009078766,0.000013255158,0.00016294881,0.000018877074,0.0017300561],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998394,0.00002036357,0.000010653993,0.000023715038,0.00003756398,0.000068349844],"domain_scores_gemma":[0.9993722,0.00030721852,0.00006191197,0.000032028784,0.00008523611,0.0001414762],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002030609,0.0004950072,0.0008405637,0.0005804194,0.00097205717,0.0010775472,0.0008042185,0.0013198924,0.0031113045],"category_scores_gemma":[0.000982182,0.00041282037,0.00057449756,0.00082940306,0.0010595461,0.0004911785,0.0007690921,0.0007157329,0.0002160351],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00016085008,0.00019016626,0.0047759283,0.00003510624,0.000025004596,0.00025242794,0.00010325671,0.98829216,0.0025612854,0.0008148139,0.00039271312,0.0023963742],"study_design_scores_gemma":[0.000041997235,0.00010438343,0.0027659964,0.000007904529,0.000008129401,0.00002227359,0.00012494944,0.9958401,0.00063535216,0.00025733514,0.00018000441,0.000011511566],"about_ca_topic_score_codex":0.026879521,"about_ca_topic_score_gemma":0.017097559,"teacher_disagreement_score":0.026879521,"about_ca_system_score_codex":0.0010156682,"about_ca_system_score_gemma":0.0008783679,"threshold_uncertainty_score":0.053446114},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9764667,0.00009243624,0.013645156,0.00015347141,0.00003776995,0.000059292433,0.0003218361,0.00034231285,0.008881062],"genre_scores_gemma":[0.99401736,0.000021510747,0.00467384,0.000016171854,0.0000045295155,0.000026760754,0.00019385963,0.000034116234,0.0010118226],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99987066,0.000028197639,0.0000056002423,0.000015355256,0.00004804473,0.00003209804],"domain_scores_gemma":[0.9996606,0.00012868633,0.0000391148,0.00003193833,0.00009590875,0.000043713848],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023287126,0.0005016319,0.0004949942,0.00033640635,0.00035074644,0.00047510694,0.00060413213,0.0006860194,0.002103473],"category_scores_gemma":[0.00071297475,0.000139829,0.00033378977,0.00020062008,0.00044074722,0.00025959843,0.00037603086,0.00047522126,0.00014873804],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00030006884,0.00018665774,0.0046614646,0.00010655914,0.000026902859,0.00027233706,0.00011395174,0.959312,0.026339248,0.0013247286,0.0006099051,0.00674614],"study_design_scores_gemma":[0.000025413126,0.000065006185,0.0012795804,0.0000053887984,0.0000041976937,0.000015023102,0.000033639706,0.9960343,0.0021956963,0.00006777946,0.0002670329,0.0000069240546],"about_ca_topic_score_codex":0.012411698,"about_ca_topic_score_gemma":0.008003301,"teacher_disagreement_score":0.012411698,"about_ca_system_score_codex":0.0005064761,"about_ca_system_score_gemma":0.00063104945,"threshold_uncertainty_score":0.024678886},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9913565,0.00006629949,0.0065611415,0.000087583634,0.000011464449,0.000013553289,0.000023161298,0.000079971775,0.0018002482],"genre_scores_gemma":[0.99897027,0.00002730209,0.00060152746,0.000008866736,0.000004696879,0.0000039494093,0.00001363553,0.00000638264,0.0003634011],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99986684,0.000022132203,0.0000031176821,0.00001554693,0.00004260848,0.000049847244],"domain_scores_gemma":[0.999673,0.00014738293,0.000056691817,0.000016159785,0.00005299747,0.000053735683],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015571293,0.00046285012,0.0004902532,0.00038768968,0.00047479654,0.00047531165,0.00040340866,0.0006422921,0.00077689276],"category_scores_gemma":[0.00055103214,0.00015668476,0.0003559084,0.0001564541,0.0008374087,0.00037865486,0.00054334797,0.0004753214,0.00007676407],"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":[0.0013359587,0.0006131109,0.008934585,0.0002579493,0.00012744986,0.0058819703,0.0007492731,0.4253965,0.5327621,0.0070428755,0.0010395575,0.015858583],"study_design_scores_gemma":[0.000042736818,0.0002973159,0.008183115,0.000008372375,0.00001622088,0.00015824233,0.00016748712,0.9656497,0.024669588,0.00058233144,0.00019210608,0.000032695378],"about_ca_topic_score_codex":0.0028681937,"about_ca_topic_score_gemma":0.0011859535,"teacher_disagreement_score":0.0028681937,"about_ca_system_score_codex":0.00033349523,"about_ca_system_score_gemma":0.00021233778,"threshold_uncertainty_score":0.0057029724},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99804866,0.000020846564,0.0016797532,0.000008081374,0.000003737793,0.000010000334,0.00003356134,0.000022379649,0.00017311069],"genre_scores_gemma":[0.99821174,0.000018096636,0.0013627673,0.0000062499576,0.0000023572377,0.000012133239,0.00005733001,0.0000043203518,0.00032495832],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998223,0.00002413711,0.0000080620985,0.000052910185,0.000059422007,0.000033115335],"domain_scores_gemma":[0.99962735,0.000112696776,0.00005744839,0.000026166264,0.00011118546,0.00006514245],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025410624,0.00036074306,0.00028572898,0.0003557154,0.0003045834,0.0002619532,0.00033158986,0.0003018107,0.00061374943],"category_scores_gemma":[0.000549376,0.0000917583,0.00011246026,0.000118483425,0.0005261605,0.0002608633,0.00032507273,0.00022428653,0.000077442564],"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":[0.00041680218,0.00011572037,0.0025847596,0.000035884106,0.000002407474,0.00007760182,0.00008500173,0.0014048378,0.9927377,0.000067144254,0.000024043915,0.0024481048],"study_design_scores_gemma":[0.00012229776,0.0031456987,0.055792194,0.000016515694,0.000018256083,0.00024716256,0.00024527512,0.032447655,0.90718776,0.000067815934,0.00066820154,0.00004113644],"about_ca_topic_score_codex":0.002485994,"about_ca_topic_score_gemma":0.0017720467,"teacher_disagreement_score":0.002485994,"about_ca_system_score_codex":0.00024723972,"about_ca_system_score_gemma":0.00022800307,"threshold_uncertainty_score":0.004943013},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99563783,0.000036291614,0.0034246154,0.000009858608,0.0000031789289,0.000008271646,0.000028713657,0.000037645073,0.00081347994],"genre_scores_gemma":[0.9985203,0.000024191719,0.0008676282,0.0000020663294,0.0000012871789,0.0000031213858,0.000021821781,0.0000028687623,0.000556706],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99991655,0.000022159658,0.0000025512022,0.000014855769,0.000030684532,0.000013261053],"domain_scores_gemma":[0.9998259,0.0000706294,0.00001543863,0.000012371013,0.000055243006,0.000020514493],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016372037,0.00022280499,0.000191987,0.00028399247,0.00023155987,0.00016364249,0.0001630542,0.0002193634,0.0008124007],"category_scores_gemma":[0.00028010787,0.00007065045,0.00010154401,0.00016199035,0.00039996716,0.00012051648,0.0001796069,0.0001299406,0.00013336645],"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":[0.00080096256,0.00020608169,0.024129193,0.0001295248,0.000019679206,0.0023744947,0.0005213434,0.055980258,0.8971897,0.000997221,0.0001787616,0.017472755],"study_design_scores_gemma":[0.00009909071,0.002945596,0.11224731,0.000030623127,0.00003472687,0.0017584814,0.0011685425,0.39136657,0.4848748,0.00071790384,0.0046894485,0.000066793546],"about_ca_topic_score_codex":0.0018281536,"about_ca_topic_score_gemma":0.0022705183,"teacher_disagreement_score":0.0018281536,"about_ca_system_score_codex":0.00015946868,"about_ca_system_score_gemma":0.00012556216,"threshold_uncertainty_score":0.0036349893},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99312496,0.000044057288,0.0018291628,0.00007856249,0.000015653835,0.000027848528,0.00022794679,0.00009251027,0.004559301],"genre_scores_gemma":[0.9971208,0.000025674297,0.0013039453,0.000015724121,0.000005504635,0.000015995352,0.00019349015,0.000020885798,0.0012978397],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998361,0.000026371108,0.000008397662,0.000026434538,0.000056466324,0.000046272457],"domain_scores_gemma":[0.9997211,0.00011997818,0.000029377477,0.000019397487,0.00005319229,0.00005690754],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023573675,0.0008094377,0.000743242,0.00034920132,0.0005940098,0.00068385294,0.00072380144,0.00096119085,0.002501537],"category_scores_gemma":[0.0005850811,0.00019746911,0.00038741517,0.00037076476,0.0007448867,0.00048173396,0.00048700665,0.0007408282,0.00016926188],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0012400305,0.00062174274,0.01044297,0.00015408758,0.000071526156,0.0021166648,0.00035817694,0.9009512,0.07246885,0.0028642735,0.0013490965,0.0073614],"study_design_scores_gemma":[0.00004859848,0.00020295903,0.0042048153,0.00000856133,0.000008002794,0.000048836682,0.00010440423,0.987852,0.0071616042,0.0001173554,0.00022695068,0.000015985368],"about_ca_topic_score_codex":0.009805751,"about_ca_topic_score_gemma":0.0046539125,"teacher_disagreement_score":0.009805751,"about_ca_system_score_codex":0.00062534463,"about_ca_system_score_gemma":0.0005527138,"threshold_uncertainty_score":0.019497335},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.76905894,0.0005011401,0.2078433,0.0003141372,0.00009298639,0.00012218833,0.0002594606,0.00030618554,0.02150164],"genre_scores_gemma":[0.9785029,0.00014169498,0.018639201,0.0000312533,0.000013043481,0.00005607869,0.00008303384,0.00003826379,0.00249453],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99985445,0.00004040809,0.0000039804822,0.000012454446,0.000057037225,0.00003168124],"domain_scores_gemma":[0.9996356,0.00019209764,0.000034796678,0.00002431341,0.000083485866,0.000029691932],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00036067495,0.0003313655,0.00049521367,0.00028743088,0.00037899436,0.0005125292,0.0006804554,0.0005484696,0.0015058266],"category_scores_gemma":[0.0009360928,0.0002581447,0.00042239734,0.00028527604,0.0006493875,0.00038437836,0.00044544705,0.00043412286,0.0002666774],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000495585,0.000049109236,0.0013380763,0.000041606905,0.00001174225,0.00007077188,0.000036831072,0.9827467,0.009362233,0.0040338356,0.00009912178,0.0021603708],"study_design_scores_gemma":[0.000007542419,0.000013629749,0.00020699405,0.0000025250474,0.0000013432312,0.000008938958,0.000008056943,0.99825925,0.001030835,0.0003470282,0.00011029453,0.000003494319],"about_ca_topic_score_codex":0.0077831578,"about_ca_topic_score_gemma":0.0030091687,"teacher_disagreement_score":0.0077831578,"about_ca_system_score_codex":0.0004335435,"about_ca_system_score_gemma":0.0008927976,"threshold_uncertainty_score":0.01547569},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9169915,0.0005348036,0.07496014,0.00025603911,0.00012827174,0.000109230736,0.00036965447,0.0009281598,0.0057221656],"genre_scores_gemma":[0.9705713,0.00009054347,0.02845758,0.000038976963,0.000008497077,0.000042861662,0.00017688844,0.00015410662,0.00045924797],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995277,0.00017384355,0.000047740094,0.00005702892,0.000112741436,0.00008093232],"domain_scores_gemma":[0.9953336,0.0034054865,0.00024488993,0.00043746416,0.0004493785,0.00012920184],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0011565649,0.0007587044,0.0007296497,0.00047384144,0.0004005977,0.0008275731,0.00086984754,0.0007172187,0.001584661],"category_scores_gemma":[0.008052194,0.00025775094,0.0005118145,0.00038547095,0.0006057032,0.00052374,0.0008486556,0.0006171459,0.00026044156],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0006600678,0.00019504395,0.00750849,0.00020196148,0.000061402636,0.00021497476,0.00031098223,0.93737835,0.018463943,0.0022938757,0.00041832088,0.03229255],"study_design_scores_gemma":[0.000029561339,0.00016563293,0.0009951547,0.000026557003,0.000019923727,0.000019898378,0.00007841873,0.98789704,0.010141472,0.00023566837,0.00037743856,0.000013292254],"about_ca_topic_score_codex":0.00986034,"about_ca_topic_score_gemma":0.007324096,"teacher_disagreement_score":0.00986034,"about_ca_system_score_codex":0.00048234093,"about_ca_system_score_gemma":0.0006989451,"threshold_uncertainty_score":0.019605875},"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":"review","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"review","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.009709621,0.4189274,0.5560839,0.0011567068,0.0008423945,0.00007980025,0.0001798973,0.0008205429,0.012199696],"genre_scores_gemma":[0.13378465,0.54135823,0.30774525,0.0013643048,0.003399946,0.00023187496,0.00074651686,0.0003505524,0.011018597],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9986142,0.00026347133,0.00010120517,0.0003902507,0.00057929906,0.00005160371],"domain_scores_gemma":[0.99448353,0.003458164,0.00045037433,0.00025570238,0.0012775685,0.00007465069],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0019629865,0.0012341524,0.0011409231,0.002755554,0.00026569146,0.0015772058,0.0012161481,0.0010246704,0.003275611],"category_scores_gemma":[0.0045227585,0.0006579226,0.00069193245,0.0023960844,0.0009972032,0.0026753407,0.0010664668,0.0012059973,0.0018866174],"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":[0.00013112031,0.00007629807,0.0014628156,0.0054038567,0.00009293664,0.00012271253,0.0002027375,0.0054065324,0.028159346,0.009039807,0.0031200394,0.9467817],"study_design_scores_gemma":[0.00008174662,0.0013412301,0.011420576,0.0043770503,0.0007939269,0.003834697,0.000825973,0.09237179,0.10605781,0.031431064,0.74699885,0.00046534953],"about_ca_topic_score_codex":0.00079575984,"about_ca_topic_score_gemma":0.0006343304,"teacher_disagreement_score":0.003275611,"about_ca_system_score_codex":0.0004179179,"about_ca_system_score_gemma":0.00085909094,"threshold_uncertainty_score":0.010957956},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.60309154,0.0051980605,0.37828353,0.00038222258,0.0006121548,0.00018443864,0.000240941,0.0013150931,0.010691851],"genre_scores_gemma":[0.9109131,0.0010311818,0.08437586,0.00019079911,0.00005466309,0.00008074676,0.00016795943,0.000069767826,0.0031159907],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998084,0.000012057406,0.000013633858,0.000041929525,0.00009242764,0.00003175062],"domain_scores_gemma":[0.999764,0.000026148937,0.0001024534,0.00001708376,0.00006299307,0.000027185766],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002229344,0.0003802155,0.00028460828,0.0002914006,0.00015117205,0.00042291466,0.00061580807,0.0006186279,0.0009396529],"category_scores_gemma":[0.00030295635,0.00016347281,0.00035776224,0.00016905075,0.00018108213,0.0004494007,0.00034990913,0.00038203908,0.00025742973],"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":[0.000067206456,0.000057624802,0.0010066198,0.00020913806,0.000014119357,0.00024127882,0.00003699986,0.0049418407,0.96210635,0.000935223,0.0004184335,0.029965118],"study_design_scores_gemma":[0.00009117643,0.002100842,0.010130222,0.000057216188,0.000111992864,0.0014990786,0.00008459424,0.09688965,0.86540914,0.00057886686,0.022939028,0.00010816384],"about_ca_topic_score_codex":0.00023956965,"about_ca_topic_score_gemma":0.00037308343,"teacher_disagreement_score":0.0009396529,"about_ca_system_score_codex":0.00022611527,"about_ca_system_score_gemma":0.00023925443,"threshold_uncertainty_score":0.0031434894},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.1720058,0.00036212974,0.8176781,0.00016161053,0.000053814692,0.00010851311,0.00019457696,0.00057799474,0.0088574365],"genre_scores_gemma":[0.9469028,0.00037481845,0.0471235,0.000042163298,0.000027268245,0.00016310735,0.0002142101,0.00011509717,0.0050369417],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99982435,0.0000380364,0.000011245448,0.00003191208,0.000072038536,0.000022546032],"domain_scores_gemma":[0.9993888,0.0002950033,0.00009060448,0.000067126755,0.00012985723,0.000028517416],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00042866304,0.00061363535,0.00045652842,0.0003951011,0.000343846,0.0007426642,0.0012976268,0.00088527286,0.0012214908],"category_scores_gemma":[0.0013169302,0.00039603512,0.0005974606,0.00029737214,0.000591866,0.0012166776,0.000556992,0.0007511474,0.0004852754],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000020334603,0.00005255736,0.00064095965,0.000026257721,0.000007551046,0.000060751,0.0000475509,0.9834313,0.0037334329,0.004812455,0.00024080268,0.006926069],"study_design_scores_gemma":[9.4306284e-7,0.0000028504821,0.00006333894,0.0000011926799,5.477604e-7,0.000004541403,0.0000019533543,0.99925953,0.0002239124,0.00035794303,0.0000813282,0.0000019632525],"about_ca_topic_score_codex":0.0039275554,"about_ca_topic_score_gemma":0.00237816,"teacher_disagreement_score":0.0039275554,"about_ca_system_score_codex":0.0003564641,"about_ca_system_score_gemma":0.0005678599,"threshold_uncertainty_score":0.0078094006},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.85075045,0.0007147531,0.09586179,0.0003064432,0.00025636223,0.00010196228,0.00043805924,0.0007634467,0.05080679],"genre_scores_gemma":[0.97947925,0.0001379861,0.014534269,0.000039460112,0.000025379974,0.000041416835,0.00019338887,0.000058606125,0.005490349],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998553,0.00002873054,0.000007898586,0.000014664945,0.00006483833,0.000028553428],"domain_scores_gemma":[0.9995925,0.00021013878,0.000031501357,0.000033758333,0.000080431404,0.00005173615],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021812953,0.00045482008,0.0007698767,0.00043135678,0.0005192195,0.0008454714,0.00083358295,0.0008184626,0.0028670782],"category_scores_gemma":[0.0009901059,0.00034380963,0.00025387885,0.0006156581,0.00065645884,0.0005220894,0.00088661676,0.0005967055,0.00027017167],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00010293058,0.00008146245,0.00070871547,0.00003706727,0.000009919758,0.00008003691,0.000037882117,0.9857524,0.0038901782,0.003484231,0.0002911096,0.005524066],"study_design_scores_gemma":[0.000016922559,0.000025698639,0.00026030606,0.0000027345245,0.000001720472,0.000009663992,0.000010111766,0.99854124,0.0005004079,0.00043188754,0.0001959545,0.0000034280474],"about_ca_topic_score_codex":0.007189342,"about_ca_topic_score_gemma":0.0048575625,"teacher_disagreement_score":0.007189342,"about_ca_system_score_codex":0.000662783,"about_ca_system_score_gemma":0.00066985685,"threshold_uncertainty_score":0.014294982},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99669844,0.00016544721,0.001792692,0.00002133725,0.000016121969,0.000015961154,0.00008567251,0.00004547356,0.0011588334],"genre_scores_gemma":[0.99760014,0.00010363737,0.0009744287,0.000008062135,0.0000095016285,0.000010760709,0.00007459226,0.000018422514,0.0012003809],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9996024,0.00005837365,0.000019455647,0.00007547063,0.00015885911,0.000085580454],"domain_scores_gemma":[0.99870193,0.00062466116,0.00021909681,0.00013055347,0.00025490267,0.000068886795],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00038092985,0.00037295025,0.00036831494,0.0002819943,0.0005775286,0.000487968,0.0004320483,0.0004560161,0.0028094102],"category_scores_gemma":[0.0010278897,0.0001911721,0.00021992905,0.0005122842,0.0006703525,0.00057011924,0.00036981344,0.0003831356,0.00038361858],"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":[0.00097303145,0.00032112026,0.001257681,0.0000779059,0.000008112284,0.00014986239,0.00016793974,0.0006923338,0.99275064,0.00020650875,0.00009742743,0.003297278],"study_design_scores_gemma":[0.000086851964,0.0019832398,0.012254615,0.000007785073,0.000027113583,0.00014407682,0.00025126175,0.0071590613,0.9772446,0.000085636915,0.0007330626,0.00002267541],"about_ca_topic_score_codex":0.0012012058,"about_ca_topic_score_gemma":0.0006712525,"teacher_disagreement_score":0.0028094102,"about_ca_system_score_codex":0.00031196736,"about_ca_system_score_gemma":0.00018978887,"threshold_uncertainty_score":0.009398401},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9585735,0.000108164924,0.038008027,0.00006003223,0.000017785325,0.000038926373,0.0002726235,0.00013026068,0.00279068],"genre_scores_gemma":[0.99435,0.00008790099,0.0043474617,0.000013316908,0.0000035374842,0.000024171643,0.000120252786,0.000009070107,0.0010442997],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99991107,0.000012627677,0.000008490339,0.000017663988,0.000021098367,0.000029054254],"domain_scores_gemma":[0.9998313,0.00006515475,0.00003971425,0.000012198744,0.000028983197,0.000022691123],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000119448254,0.0004343793,0.00028494332,0.00030077403,0.0002679448,0.00058289664,0.00036323082,0.00078664394,0.0008556573],"category_scores_gemma":[0.00044562537,0.0001906166,0.00043003474,0.0003042337,0.0003068501,0.0004146178,0.0005410941,0.0003679912,0.000114791204],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00004099626,0.000040577805,0.0051884693,0.000040875788,0.000008899585,0.00015436293,0.000057758058,0.9709052,0.018231813,0.0007149678,0.00011124306,0.0045048823],"study_design_scores_gemma":[0.000010461583,0.000094042975,0.0026777221,0.0000075662606,0.0000050373474,0.00003053967,0.000059671067,0.9932712,0.0028965452,0.00046410336,0.00047357075,0.000009610586],"about_ca_topic_score_codex":0.010150323,"about_ca_topic_score_gemma":0.0060680443,"teacher_disagreement_score":0.010150323,"about_ca_system_score_codex":0.00057065365,"about_ca_system_score_gemma":0.00068320346,"threshold_uncertainty_score":0.02018249},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6835813,0.00042144587,0.3001854,0.00054951996,0.00015724728,0.00009034853,0.0002903251,0.0012775455,0.01344685],"genre_scores_gemma":[0.9801717,0.000054736116,0.018061489,0.000054270648,0.000023469707,0.00004189094,0.000102043676,0.00009364768,0.0013968175],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99976116,0.000086804765,0.00001159707,0.000032424072,0.00006397737,0.0000440036],"domain_scores_gemma":[0.9968485,0.0022725798,0.00017925876,0.00012391128,0.00036317747,0.00021260863],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00096550374,0.0005546226,0.00089108467,0.0005880063,0.000970459,0.0010515046,0.0011288793,0.0019398688,0.0022285935],"category_scores_gemma":[0.0043998184,0.00072024576,0.00043368316,0.000540157,0.0011221938,0.0007793586,0.000719737,0.0009712059,0.0002916591],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000075757656,0.00003501734,0.00058479316,0.000015375374,0.000010129603,0.000034966182,0.000019368848,0.9956657,0.0006529308,0.0015229543,0.00011178928,0.0012711319],"study_design_scores_gemma":[0.0000036623505,0.0000030997244,0.0000506756,9.1825905e-7,7.928369e-7,0.0000011249576,0.0000015782849,0.9996712,0.00011464499,0.00013965252,0.000011392645,0.0000013337853],"about_ca_topic_score_codex":0.021577584,"about_ca_topic_score_gemma":0.013599308,"teacher_disagreement_score":0.021577584,"about_ca_system_score_codex":0.00094812346,"about_ca_system_score_gemma":0.0015129289,"threshold_uncertainty_score":0.04290402},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6460034,0.0017590822,0.34648588,0.00024723238,0.0005100012,0.000318122,0.0010107972,0.0011805358,0.0024850534],"genre_scores_gemma":[0.72530925,0.0009001126,0.26985744,0.00017418104,0.00020044806,0.00097237236,0.00056985865,0.00012866217,0.0018876672],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99924076,0.00008164217,0.000042890282,0.00021826751,0.00031641134,0.00010013153],"domain_scores_gemma":[0.99931383,0.0002693509,0.000097802724,0.0001258081,0.00010807084,0.000085217966],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005308669,0.00064547604,0.0005988597,0.0006378192,0.00042496258,0.00045409077,0.00094060675,0.00083280605,0.00282991],"category_scores_gemma":[0.00056323846,0.00042406056,0.00036587086,0.00036054655,0.00051735603,0.00078093394,0.0011430314,0.0013648701,0.0004270473],"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":[0.000030649266,0.000017970719,0.00009501724,0.000033860415,0.0000032697287,0.000033605662,0.000018595552,0.00009022196,0.99798465,0.00011815482,0.000043414406,0.0015306193],"study_design_scores_gemma":[0.00006994303,0.00083195686,0.0054547302,0.00001822347,0.00002756973,0.00048897753,0.00010206149,0.009150962,0.9783012,0.00031210063,0.005178646,0.00006363838],"about_ca_topic_score_codex":0.00029794,"about_ca_topic_score_gemma":0.0004096727,"teacher_disagreement_score":0.00282991,"about_ca_system_score_codex":0.00036247377,"about_ca_system_score_gemma":0.00030406142,"threshold_uncertainty_score":0.009467006},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9403093,0.00042362706,0.04245255,0.00024230764,0.00012789606,0.00003353959,0.00007800776,0.0001635873,0.016169263],"genre_scores_gemma":[0.9953082,0.00007169133,0.0029999202,0.000016997114,0.000005511639,0.000014833433,0.000021456919,0.000009963826,0.0015514425],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999354,0.000015862093,0.0000025386635,0.000010759619,0.0000198429,0.00001572431],"domain_scores_gemma":[0.9998124,0.00008769255,0.00002259441,0.000009880052,0.00003807939,0.000029393725],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00019555123,0.0003561718,0.0004976497,0.00038770464,0.000600232,0.0004872685,0.0005574001,0.0008745094,0.0011602775],"category_scores_gemma":[0.0004742321,0.00016430323,0.00038123867,0.00026705113,0.00059276645,0.0002726478,0.00044226737,0.00028298754,0.000103643295],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000068024965,0.000046657155,0.0012778429,0.00003177814,0.000016332375,0.0001459481,0.000044459895,0.9878414,0.006371399,0.0016868234,0.00014626911,0.0023230484],"study_design_scores_gemma":[0.000004690822,0.00002014188,0.0002441857,0.0000019502447,0.000002979849,0.000009986591,0.000009714958,0.9991351,0.00038360798,0.00008808207,0.000096097596,0.0000035444436],"about_ca_topic_score_codex":0.009585294,"about_ca_topic_score_gemma":0.0045557306,"teacher_disagreement_score":0.009585294,"about_ca_system_score_codex":0.00044885502,"about_ca_system_score_gemma":0.0005206547,"threshold_uncertainty_score":0.019059002},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.019251702,0.004600376,0.9572599,0.00087861647,0.00032982448,0.000051396983,0.0002341841,0.00079118705,0.016602824],"genre_scores_gemma":[0.82982665,0.011635992,0.13450618,0.0006614342,0.0010898506,0.00032482733,0.00048595463,0.0004330649,0.021036068],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99897027,0.00033950649,0.000055212055,0.0001213096,0.00041929015,0.0000944108],"domain_scores_gemma":[0.99822134,0.00096259953,0.00013727206,0.00023086289,0.00038212482,0.00006571414],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0010672534,0.0013177376,0.0011016311,0.0012994324,0.00052423094,0.0016137057,0.00349257,0.0017540967,0.0018780302],"category_scores_gemma":[0.0043433965,0.00053959276,0.0012623583,0.0006882482,0.0010927015,0.0025346894,0.0012228965,0.001478968,0.0013071327],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000042885895,0.00006498262,0.0007119939,0.00022362811,0.000053568783,0.0001484464,0.00011462345,0.8871237,0.0017307377,0.07377474,0.0018426707,0.034168016],"study_design_scores_gemma":[0.000004386198,0.000029203125,0.00007401977,0.000048188056,0.000011328384,0.000051479106,0.000021458578,0.9726777,0.0003450948,0.023143347,0.0035791614,0.000014525237],"about_ca_topic_score_codex":0.004107013,"about_ca_topic_score_gemma":0.0017030686,"teacher_disagreement_score":0.004107013,"about_ca_system_score_codex":0.00066971197,"about_ca_system_score_gemma":0.0008416116,"threshold_uncertainty_score":0.008166194},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.72573143,0.0017530326,0.26426587,0.00007179518,0.00022543907,0.00014677871,0.00030200448,0.00040147413,0.007102065],"genre_scores_gemma":[0.9754152,0.00060001976,0.021884782,0.000044522312,0.000072319104,0.000037760128,0.0004380916,0.00006925441,0.0014380034],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992054,0.00007504742,0.00006532033,0.00019390225,0.00035095765,0.00010952375],"domain_scores_gemma":[0.9980338,0.00044876986,0.0006682616,0.00028337265,0.00042028722,0.0001454474],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006176137,0.00053767266,0.0009161622,0.0012575723,0.00045884313,0.0021248176,0.0005008135,0.00056131795,0.0008495605],"category_scores_gemma":[0.0025643348,0.00022193106,0.0006838676,0.0007972691,0.0007566711,0.0014029258,0.0010045302,0.00097243785,0.00028069015],"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":[0.0014934811,0.00056794536,0.05789477,0.0007875858,0.0002725494,0.0029558635,0.0009503578,0.21026127,0.50090545,0.08005235,0.0020799455,0.14177845],"study_design_scores_gemma":[0.000054798875,0.0010425746,0.05429757,0.00006248895,0.00008802056,0.0021125197,0.00036439524,0.8198695,0.08936995,0.025395034,0.0071503087,0.00019281755],"about_ca_topic_score_codex":0.000461068,"about_ca_topic_score_gemma":0.00020122585,"teacher_disagreement_score":0.0021248176,"about_ca_system_score_codex":0.00038403628,"about_ca_system_score_gemma":0.00040406582,"threshold_uncertainty_score":0.003266275},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.88949466,0.00059922814,0.033160303,0.001064618,0.00025043386,0.00011867818,0.00048905704,0.00045183438,0.07437107],"genre_scores_gemma":[0.9940264,0.00008260627,0.0022677665,0.00006081897,0.000030947587,0.000025506266,0.00008484682,0.0000540685,0.0033669255],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99980646,0.000053612624,0.000006746083,0.00002536358,0.000051223527,0.000056598088],"domain_scores_gemma":[0.99898344,0.00056843023,0.00007862015,0.00006302563,0.0001612467,0.00014526154],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00038187322,0.0005144439,0.0008338741,0.00065829896,0.0009062328,0.0009957682,0.000980869,0.0010991838,0.0046424917],"category_scores_gemma":[0.0016288558,0.00032441202,0.0006177983,0.0005582213,0.0014767002,0.00074526516,0.00073550345,0.0010424852,0.00034192554],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00014040234,0.0000892701,0.0013070966,0.000043597527,0.000021218255,0.0003279402,0.00007601187,0.98007214,0.004241468,0.011691837,0.00060404674,0.0013850125],"study_design_scores_gemma":[0.00002716957,0.000014243502,0.00025595128,0.0000025923616,0.00000259689,0.000016634103,0.000019295732,0.9981693,0.00038658545,0.00097077846,0.00012798827,0.0000068325307],"about_ca_topic_score_codex":0.015778732,"about_ca_topic_score_gemma":0.005386095,"teacher_disagreement_score":0.015778732,"about_ca_system_score_codex":0.00079063483,"about_ca_system_score_gemma":0.0008906107,"threshold_uncertainty_score":0.03137374},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.16966109,0.00046502388,0.8084266,0.0004427681,0.00021591122,0.0001012419,0.00008152473,0.00039016188,0.020215606],"genre_scores_gemma":[0.9816,0.00010179095,0.015224462,0.000048935923,0.000054091965,0.00004821364,0.00002698666,0.000059132275,0.002836481],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996302,0.00011555672,0.000011997808,0.000076669,0.00006955095,0.00009587291],"domain_scores_gemma":[0.99926513,0.00043247466,0.00007553803,0.000026962236,0.00013614909,0.00006374696],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005681964,0.0012736582,0.0011971907,0.00041840304,0.00037417997,0.00117739,0.0004585712,0.0011078286,0.0029571352],"category_scores_gemma":[0.0023741561,0.00040100788,0.00044259426,0.00029657062,0.0008924663,0.0005533501,0.0009875948,0.00054243,0.00026191372],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0003834405,0.000084271436,0.00026454907,0.00012009262,0.00003140572,0.0000635623,0.0000413878,0.9682413,0.010250235,0.0031972958,0.00056452147,0.01675805],"study_design_scores_gemma":[0.00001576188,0.00007307157,0.00012884369,0.000003588934,0.000007917766,0.0000067104297,0.0000069953594,0.99839586,0.0007196968,0.00048101242,0.00015540418,0.0000051357506],"about_ca_topic_score_codex":0.0029270116,"about_ca_topic_score_gemma":0.0015449984,"teacher_disagreement_score":0.0029571352,"about_ca_system_score_codex":0.0004987512,"about_ca_system_score_gemma":0.0007600116,"threshold_uncertainty_score":0.009892583},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.71504784,0.00023449602,0.26355225,0.0003565626,0.00025169918,0.000070283626,0.00017342823,0.0008350118,0.019478342],"genre_scores_gemma":[0.9748286,0.00004120038,0.01819849,0.00003153269,0.000033456276,0.000015345397,0.00007686695,0.00012806228,0.0066464273],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999038,0.00003145304,0.0000038006804,0.000014080952,0.000028993258,0.000017912758],"domain_scores_gemma":[0.9994566,0.00025298732,0.000030314426,0.000033874738,0.000154697,0.00007163094],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00033256656,0.0005178721,0.000581592,0.0003797808,0.00059279357,0.00069441367,0.00060277624,0.0009692979,0.0020079834],"category_scores_gemma":[0.001492003,0.0002909093,0.00040858943,0.00027534552,0.00046592846,0.0005288276,0.00042424677,0.00054209685,0.00028033016],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0003118023,0.000076796896,0.0027887754,0.000055873697,0.000021828953,0.00037061193,0.000107344276,0.96084344,0.014613852,0.0063893655,0.00087842427,0.013541963],"study_design_scores_gemma":[0.0000052696632,0.0000112933,0.00026171675,0.0000017424336,0.0000013201551,0.000010066574,0.0000073338065,0.9986595,0.00069809105,0.00024209713,0.00009949537,0.0000020245784],"about_ca_topic_score_codex":0.008642863,"about_ca_topic_score_gemma":0.0072547714,"teacher_disagreement_score":0.008642863,"about_ca_system_score_codex":0.0005412449,"about_ca_system_score_gemma":0.00074379286,"threshold_uncertainty_score":0.017185092},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9951841,0.00007129148,0.0041826786,0.000019480582,0.0000029814785,0.000007746321,0.00001035684,0.000031077914,0.0004903234],"genre_scores_gemma":[0.9973943,0.000025885427,0.0020625414,0.000010364173,0.000002876375,0.0000066850307,0.000030466528,0.000006916866,0.0004599965],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999279,0.0000065237177,0.0000019889483,0.000012141911,0.000029827354,0.000021610851],"domain_scores_gemma":[0.9998338,0.000033240318,0.000040804218,0.000009003713,0.000028806084,0.0000542616],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00008654527,0.000086314256,0.00015689677,0.00026012294,0.00024742295,0.00031237895,0.00013373028,0.00021807627,0.0006140308],"category_scores_gemma":[0.00026562787,0.00016701309,0.00008436989,0.00008924587,0.0002809769,0.00032147332,0.00043701622,0.00023602665,0.00009567832],"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":[0.00013855871,0.000038667502,0.0038477576,0.00002282573,0.0000072647013,0.0005828749,0.00026930586,0.0025691427,0.98576665,0.0010570249,0.00009596684,0.00560393],"study_design_scores_gemma":[0.0000867436,0.0016315064,0.097507305,0.000031900694,0.000040464205,0.0020974465,0.0010521548,0.12484979,0.76555943,0.0015193018,0.0055460795,0.00007799397],"about_ca_topic_score_codex":0.0006559701,"about_ca_topic_score_gemma":0.0005247861,"teacher_disagreement_score":0.0006559701,"about_ca_system_score_codex":0.0002111291,"about_ca_system_score_gemma":0.00017987049,"threshold_uncertainty_score":0.0020540953},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.89520663,0.00011189878,0.09920242,0.0002004006,0.00012193665,0.000036780883,0.00006564133,0.0005372135,0.00451698],"genre_scores_gemma":[0.99766695,0.000011663344,0.0013893719,0.000006830355,0.000006227127,0.000008127958,0.000010984057,0.00000797271,0.00089184684],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997923,0.00005271057,0.000005932615,0.000062541585,0.00005098696,0.00003556919],"domain_scores_gemma":[0.99919707,0.00048397924,0.000060312377,0.000028860362,0.00016648493,0.00006335656],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00047046592,0.0009959441,0.00081774074,0.0003046897,0.00068285,0.0005526432,0.00048444347,0.0008964766,0.0010043771],"category_scores_gemma":[0.0008556458,0.00033789052,0.00032978374,0.00011614008,0.0006165081,0.00028348388,0.00043488145,0.00053442334,0.00015969723],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000919352,0.00020544764,0.0025459386,0.00008583292,0.00002269497,0.00029177364,0.000094326846,0.93425786,0.043512918,0.00035985626,0.00050149916,0.017202448],"study_design_scores_gemma":[0.0000075840467,0.00008642066,0.00082075986,0.0000013370027,0.000004202877,0.000006103794,0.0000072429066,0.9968003,0.0021895687,0.000035979996,0.000035862566,0.0000046668606],"about_ca_topic_score_codex":0.015031484,"about_ca_topic_score_gemma":0.010874207,"teacher_disagreement_score":0.015031484,"about_ca_system_score_codex":0.0006261342,"about_ca_system_score_gemma":0.0005981723,"threshold_uncertainty_score":0.029887974},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9683257,0.00014131791,0.027558252,0.00007747527,0.000028055669,0.000041179585,0.00048320653,0.00055033056,0.0027945123],"genre_scores_gemma":[0.9968485,0.000034968147,0.0025813878,0.000006210725,0.0000042191605,0.000017628001,0.00018660522,0.000039140774,0.00028124894],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996934,0.000060927294,0.000028694018,0.00003973745,0.00011292715,0.00006427268],"domain_scores_gemma":[0.99818414,0.0010247575,0.00020505639,0.0001557644,0.00035096525,0.000079400976],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00083037815,0.0005167629,0.0006792111,0.000673921,0.00045023533,0.0007784371,0.0006221994,0.00075966073,0.0008947022],"category_scores_gemma":[0.0023292247,0.00019455548,0.00056521664,0.00040346175,0.0004508959,0.0004257596,0.00029079034,0.00047356487,0.0001482846],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0002412879,0.000106763335,0.009966582,0.00006494021,0.00001992348,0.00031891858,0.0001314438,0.9613501,0.020417,0.0022414322,0.00032362013,0.004818012],"study_design_scores_gemma":[0.0000045556158,0.000018248567,0.00091844745,0.0000023316388,0.0000013961144,0.000009931013,0.000010551826,0.9972398,0.0016748494,0.00004226091,0.00007312275,0.000004480593],"about_ca_topic_score_codex":0.021179141,"about_ca_topic_score_gemma":0.006161191,"teacher_disagreement_score":0.021179141,"about_ca_system_score_codex":0.0009184172,"about_ca_system_score_gemma":0.0007099731,"threshold_uncertainty_score":0.042111754},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98207617,0.00008638346,0.015284932,0.00008290819,0.00004258405,0.000008803536,0.00007353572,0.0001398783,0.0022046866],"genre_scores_gemma":[0.99876946,0.000021089922,0.00047715416,0.000004659511,0.0000068577824,0.0000021751453,0.00003503837,0.000008579172,0.0006748991],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99988985,0.000021746477,0.000003926856,0.000025318664,0.00003261875,0.000026445312],"domain_scores_gemma":[0.9995252,0.00026505408,0.000026968277,0.000021914791,0.00011257065,0.000048299265],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021660044,0.00060539646,0.00046493043,0.00038757198,0.0004886099,0.00045407497,0.00039997074,0.00095341954,0.00083582907],"category_scores_gemma":[0.00052472786,0.00024954116,0.00059337297,0.00023438732,0.00046348016,0.00034602394,0.00028866174,0.0004237268,0.00019968762],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00072453753,0.00013306887,0.008779376,0.00006705419,0.00002831201,0.0005245195,0.0000949706,0.9577977,0.021770306,0.0004811201,0.00046851762,0.009130469],"study_design_scores_gemma":[0.000005407055,0.000053731364,0.003536859,0.0000014109424,0.0000047912076,0.000023032806,0.000016935677,0.9946849,0.0015621367,0.000049595666,0.000052368432,0.0000087456865],"about_ca_topic_score_codex":0.015262168,"about_ca_topic_score_gemma":0.008802163,"teacher_disagreement_score":0.015262168,"about_ca_system_score_codex":0.0003390368,"about_ca_system_score_gemma":0.00037253788,"threshold_uncertainty_score":0.030346632},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9540506,0.0000845624,0.042630065,0.000042672535,0.000016977507,0.000016902612,0.00008833871,0.0001719121,0.0028980402],"genre_scores_gemma":[0.9932288,0.000058977752,0.00585682,0.0000075898083,0.0000054954467,0.0000070004658,0.00010245303,0.000016491003,0.00071630714],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.9999536,0.0000053587364,0.0000021510848,0.0000071719583,0.00001970015,0.00001198946],"domain_scores_gemma":[0.99981695,0.00006159439,0.000021206844,0.000022743205,0.00003901302,0.000038502352],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015355171,0.0002266333,0.00027937468,0.0004437541,0.0002357808,0.0005229972,0.00013581768,0.00020033946,0.00088668737],"category_scores_gemma":[0.00036118354,0.0001216858,0.00024187464,0.00020606261,0.00037813865,0.00028604435,0.0002242816,0.00041709963,0.00007947966],"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":[0.0005457206,0.0003405146,0.0122516425,0.00013515392,0.000053390653,0.0014095213,0.00036620765,0.12559836,0.80446154,0.009009876,0.0007506794,0.0450773],"study_design_scores_gemma":[0.00006575129,0.00037392497,0.076645404,0.000016031352,0.000021257176,0.000644674,0.0001966456,0.8586045,0.059539147,0.002532442,0.00130186,0.000058382277],"about_ca_topic_score_codex":0.00064379605,"about_ca_topic_score_gemma":0.00037757817,"teacher_disagreement_score":0.00088668737,"about_ca_system_score_codex":0.00016313334,"about_ca_system_score_gemma":0.0002522115,"threshold_uncertainty_score":0.0029662251},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7082119,0.00008912886,0.28874305,0.00006293394,0.000017087119,0.000031286876,0.000040702158,0.00032257484,0.0024812834],"genre_scores_gemma":[0.9761633,0.000052164112,0.02295602,0.000007779501,0.0000061458277,0.000014127917,0.000029717425,0.000020819818,0.0007499003],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998678,0.0000495973,0.000005093018,0.00001398076,0.0000465368,0.000016975157],"domain_scores_gemma":[0.99948066,0.0003482774,0.000033415752,0.000028079266,0.00009267285,0.00001690372],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005329001,0.0003342282,0.000248762,0.00036851992,0.00022026166,0.00031373758,0.000327235,0.00027913455,0.0006922421],"category_scores_gemma":[0.0010988902,0.0001012187,0.00021138934,0.00021928895,0.00056445814,0.00046690216,0.00022168549,0.00027597576,0.00008020004],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00020257359,0.00012933726,0.0028585934,0.00007934023,0.000025811978,0.0003092672,0.00029449363,0.80004096,0.14046046,0.015738586,0.00031840045,0.0395422],"study_design_scores_gemma":[0.000003478032,0.000027212765,0.00068290235,0.0000015100184,0.000001985976,0.000013127345,0.000013104455,0.99110794,0.007372129,0.00058666867,0.00018325006,0.0000066778566],"about_ca_topic_score_codex":0.0017662168,"about_ca_topic_score_gemma":0.0009113668,"teacher_disagreement_score":0.0017662168,"about_ca_system_score_codex":0.00029665316,"about_ca_system_score_gemma":0.00034341114,"threshold_uncertainty_score":0.003511846},"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":"empirical","genre_gemma":"methods","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.57458746,0.00014385364,0.42133003,0.000053063966,0.000029908693,0.000043902306,0.00006423766,0.0005435326,0.0032040058],"genre_scores_gemma":[0.9772035,0.000052135303,0.021361662,0.0000046284717,0.000004758211,0.000021767577,0.000065055436,0.00004057917,0.0012460138],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997881,0.000060981318,0.000009966933,0.000017126717,0.000099298806,0.000024504898],"domain_scores_gemma":[0.9994892,0.00027126982,0.000029388228,0.000028436467,0.00015554944,0.000026037942],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004831057,0.0005257219,0.0005341455,0.00062849163,0.0004071675,0.0006228351,0.0004370281,0.00065157085,0.0009405679],"category_scores_gemma":[0.0014263116,0.00035770325,0.0004575656,0.00028938206,0.00040296165,0.0006056224,0.00034962653,0.0004858014,0.00020292755],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00027378913,0.000092995666,0.0024102305,0.000044276207,0.000016048845,0.00011695257,0.00009578639,0.9402049,0.02792248,0.0020408072,0.00019103121,0.026590712],"study_design_scores_gemma":[0.000004656919,0.000015017629,0.00017109298,0.0000010039054,0.0000013276103,0.0000059547506,0.0000066193716,0.9966833,0.0029572498,0.00010046467,0.000050288585,0.0000030861686],"about_ca_topic_score_codex":0.010897326,"about_ca_topic_score_gemma":0.00834359,"teacher_disagreement_score":0.010897326,"about_ca_system_score_codex":0.0003845387,"about_ca_system_score_gemma":0.00062651775,"threshold_uncertainty_score":0.021667838},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8235767,0.00025269933,0.1713881,0.0001081932,0.000030151028,0.00004772281,0.00010319153,0.00035764195,0.004135532],"genre_scores_gemma":[0.9791701,0.00006444602,0.02030356,0.000010831298,0.000005133855,0.000023918137,0.0000330482,0.000037139976,0.00035177777],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99970526,0.00012239662,0.000014197465,0.000021917818,0.0001009608,0.00003533454],"domain_scores_gemma":[0.9980866,0.0014374794,0.000121142315,0.0001006423,0.0001902647,0.00006396555],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0007972148,0.000410836,0.0005632736,0.0003272459,0.00037555097,0.0004799613,0.00045478085,0.00042548365,0.00090283493],"category_scores_gemma":[0.0028467784,0.00019595101,0.00032725342,0.0003275543,0.00064184295,0.00036935208,0.00042740506,0.00037802043,0.00011703402],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00026765728,0.000064094,0.0029417772,0.00006453986,0.00002769241,0.00012500811,0.00006282931,0.95867264,0.02605952,0.002485322,0.00007003023,0.009158851],"study_design_scores_gemma":[0.000011089363,0.00004412464,0.00029601532,0.0000036656866,0.0000042034358,0.000013663467,0.0000075211988,0.9947627,0.0045346185,0.00024554768,0.000069885304,0.000007065216],"about_ca_topic_score_codex":0.0023691978,"about_ca_topic_score_gemma":0.001871295,"teacher_disagreement_score":0.0023691978,"about_ca_system_score_codex":0.0003258857,"about_ca_system_score_gemma":0.00042156302,"threshold_uncertainty_score":0.004710853},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98623616,0.000012699069,0.010211199,0.000016515423,0.000026034095,0.00010739797,0.00044634932,0.00019620922,0.0027474996],"genre_scores_gemma":[0.9909774,0.000020839314,0.006975964,0.000028637203,0.0000065748645,0.00009473788,0.00033805633,0.00003742019,0.0015202549],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99947494,0.00006565576,0.000025258487,0.000066526496,0.00029234865,0.00007524441],"domain_scores_gemma":[0.9992618,0.0002341057,0.00006410833,0.00004456691,0.00032605464,0.00006940786],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005385048,0.00039229673,0.00021769901,0.0006097613,0.00038928588,0.0002622711,0.00034617836,0.0004381999,0.0019572405],"category_scores_gemma":[0.00089577347,0.00015767272,0.00016772229,0.00037844322,0.00041776692,0.0002668351,0.00035370808,0.00049170636,0.00026193747],"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":[0.0012529334,0.00055171014,0.03171904,0.00013930819,0.00002491323,0.00069413485,0.0005805133,0.0060249134,0.9312864,0.00036585066,0.00074240786,0.026617866],"study_design_scores_gemma":[0.00021526191,0.008435684,0.2720869,0.000050449285,0.000081682076,0.0016535149,0.0013982446,0.040193863,0.6713663,0.000507384,0.003900442,0.000110242465],"about_ca_topic_score_codex":0.0011882891,"about_ca_topic_score_gemma":0.0025509938,"teacher_disagreement_score":0.0019572405,"about_ca_system_score_codex":0.00012601496,"about_ca_system_score_gemma":0.00024291211,"threshold_uncertainty_score":0.00654763},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.578391,0.0005523434,0.4128049,0.000094773044,0.00010503534,0.00008841354,0.00005733083,0.0009658124,0.0069403667],"genre_scores_gemma":[0.88472885,0.00022411949,0.1097217,0.00006702489,0.00005931828,0.000058594112,0.000057333153,0.00006803469,0.0050150836],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9995554,0.0000788901,0.000026159938,0.00009253803,0.00020239111,0.000044434717],"domain_scores_gemma":[0.99933916,0.00022854272,0.0001630027,0.00009242224,0.00012843593,0.000048400052],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00043820552,0.0007198025,0.0005617113,0.0002546364,0.00015142813,0.0003398264,0.0007041849,0.00031625232,0.0019999775],"category_scores_gemma":[0.0006565674,0.0002713954,0.0003209102,0.00016115487,0.0003388956,0.00042637816,0.00058326096,0.000396727,0.00046038796],"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":[0.0004075714,0.00011487487,0.0007505402,0.00017984446,0.000037621445,0.000074283744,0.00009257051,0.0051367334,0.9435753,0.00061899435,0.00018011358,0.048831634],"study_design_scores_gemma":[0.0000829565,0.002130416,0.0032929648,0.000018996692,0.000062546686,0.00026426552,0.00004500917,0.033400346,0.9554968,0.00016163704,0.005010096,0.000034101882],"about_ca_topic_score_codex":0.00017389563,"about_ca_topic_score_gemma":0.0003770938,"teacher_disagreement_score":0.0019999775,"about_ca_system_score_codex":0.00017321747,"about_ca_system_score_gemma":0.00019305259,"threshold_uncertainty_score":0.006690562},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.993972,0.00024472407,0.005182212,0.000015718222,0.000013274714,0.0000060530692,0.000033631964,0.0000375123,0.0004948312],"genre_scores_gemma":[0.9971041,0.00013887635,0.0020619463,0.000007977336,0.000011445614,0.0000045154943,0.00006450231,0.0000135106875,0.0005931022],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99986625,0.000009473554,0.000004253917,0.000027715752,0.00007355597,0.0000187041],"domain_scores_gemma":[0.99964714,0.00013862108,0.00007676666,0.000017159775,0.000086083535,0.000034232035],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001901934,0.00019508693,0.00033192354,0.00050035137,0.0002110482,0.00034709836,0.00023659195,0.0002904285,0.0009031172],"category_scores_gemma":[0.00045380043,0.00012016076,0.00021576996,0.0002726101,0.00034936098,0.00044608975,0.00028782277,0.00027068038,0.00008591582],"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":[0.00031513936,0.000059937604,0.010220725,0.00015543518,0.000028592243,0.0007716116,0.00046614837,0.0047778906,0.9617068,0.0002702428,0.00009887357,0.021128643],"study_design_scores_gemma":[0.00004893902,0.0023525276,0.1770276,0.00004617682,0.00013456351,0.001951606,0.0012014109,0.10339468,0.70951194,0.0005699922,0.0036698228,0.00009072518],"about_ca_topic_score_codex":0.000309302,"about_ca_topic_score_gemma":0.00034028836,"teacher_disagreement_score":0.0009031172,"about_ca_system_score_codex":0.00013835945,"about_ca_system_score_gemma":0.00010174009,"threshold_uncertainty_score":0.0030212402},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9899659,0.00007525891,0.007721443,0.000041109804,0.000013716703,0.000028145008,0.00014144758,0.00017476341,0.0018383444],"genre_scores_gemma":[0.99783033,0.00002492485,0.0017285385,0.0000052170244,0.000002609414,0.00001563591,0.00006081143,0.000015493837,0.00031637662],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99991167,0.000019533889,0.0000070745173,0.000015605056,0.000021614167,0.000024580419],"domain_scores_gemma":[0.99962187,0.00020915107,0.000048788526,0.000031537937,0.000050249564,0.00003833555],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00026961588,0.00043929525,0.000440597,0.00031892527,0.00029606972,0.0005495795,0.00048147436,0.00062806136,0.0010898266],"category_scores_gemma":[0.0005854434,0.00015255566,0.00045131322,0.0002307519,0.00038574444,0.00032281608,0.00032131062,0.00039171058,0.00012611221],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00021914602,0.00031376106,0.00711035,0.00009828785,0.00003198507,0.00025724844,0.000083941704,0.9515527,0.034817666,0.0007184288,0.00022459959,0.0045719384],"study_design_scores_gemma":[0.000011068336,0.00005858819,0.0021013871,0.0000032187509,0.0000055270502,0.00000684549,0.000021611784,0.9940911,0.0035732589,0.000048307542,0.0000720105,0.000007062089],"about_ca_topic_score_codex":0.0056441324,"about_ca_topic_score_gemma":0.0022996366,"teacher_disagreement_score":0.0056441324,"about_ca_system_score_codex":0.00032074132,"about_ca_system_score_gemma":0.0003127136,"threshold_uncertainty_score":0.011222601},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9988042,0.000048554164,0.00039509774,0.000019731775,0.000017641107,0.0000021867145,0.0000331695,0.00002144654,0.00065790996],"genre_scores_gemma":[0.9989467,0.000026139522,0.00008552562,0.000010013524,0.0000035354883,0.0000015487856,0.000028464165,0.000020083959,0.00087796495],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99979657,0.00002374027,0.00000970904,0.000038107053,0.000048872735,0.00008311201],"domain_scores_gemma":[0.99916875,0.00035574014,0.00010237181,0.00005196968,0.00015213287,0.000169109],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00027123812,0.00021446383,0.00046700405,0.00018807178,0.00047508313,0.0006099514,0.00018889576,0.0004214823,0.004975778],"category_scores_gemma":[0.0015165659,0.00018569913,0.00031193733,0.00012774968,0.0005815119,0.0004134692,0.0005919027,0.00039019913,0.00065440184],"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":[0.009327498,0.00015279176,0.017525123,0.00013139116,0.00003074901,0.0010508894,0.0007756846,0.004773443,0.9530068,0.00034784232,0.0004742095,0.012403577],"study_design_scores_gemma":[0.00019156918,0.00642201,0.30504185,0.000051378727,0.00018498377,0.0011159632,0.002430401,0.029276777,0.6502485,0.00040204744,0.0045537744,0.00008076775],"about_ca_topic_score_codex":0.0018666507,"about_ca_topic_score_gemma":0.0010632914,"teacher_disagreement_score":0.004975778,"about_ca_system_score_codex":0.00031722803,"about_ca_system_score_gemma":0.00034405192,"threshold_uncertainty_score":0.01664561},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99954695,0.00001900559,0.00027362586,0.0000051426423,0.0000011880318,0.0000012142373,0.000018336947,0.0000130752005,0.000121443896],"genre_scores_gemma":[0.9997471,0.000012389851,0.00013882839,0.0000013993042,7.3815903e-7,0.0000013431539,0.000028191249,0.000003772577,0.00006626698],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998777,0.000015290045,0.00000680899,0.000026401449,0.00003693959,0.00003689593],"domain_scores_gemma":[0.999569,0.00022011255,0.00007696568,0.000021872676,0.000052830434,0.000059230173],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00010944731,0.00029747168,0.00026693635,0.00026763562,0.00018708146,0.00036094827,0.00023542679,0.00021341149,0.00061085337],"category_scores_gemma":[0.0005032636,0.00013981768,0.00018587754,0.000162071,0.00049279805,0.00021636944,0.00030517197,0.00024715724,0.00008385759],"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":[0.0021605461,0.00021561886,0.022693696,0.000106848864,0.000032039286,0.0007003759,0.00027787374,0.056142,0.9071175,0.00037152367,0.00015561667,0.010026378],"study_design_scores_gemma":[0.00012658912,0.0017520208,0.22955558,0.000026204083,0.00005370507,0.00020707826,0.00030096422,0.2630567,0.50420856,0.00018558817,0.0004284121,0.00009850086],"about_ca_topic_score_codex":0.0026318266,"about_ca_topic_score_gemma":0.0016339686,"teacher_disagreement_score":0.0026318266,"about_ca_system_score_codex":0.0002671296,"about_ca_system_score_gemma":0.000131558,"threshold_uncertainty_score":0.0052330494},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.10327806,0.0011214971,0.858658,0.00072278903,0.0002824795,0.00005801653,0.00013593203,0.00041898215,0.035324186],"genre_scores_gemma":[0.9133424,0.001190391,0.06500469,0.00019136416,0.00035348698,0.00005471205,0.00012136847,0.00030768587,0.019433916],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998037,0.0000631992,0.000008798779,0.000025436471,0.000072269075,0.000026639658],"domain_scores_gemma":[0.9997446,0.00008630895,0.00005467281,0.00003495854,0.000050081195,0.000029361612],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003613459,0.0008999055,0.0008056582,0.0008021619,0.00052221835,0.0017777323,0.0009992889,0.0013632177,0.0022053407],"category_scores_gemma":[0.0015471588,0.00037958985,0.0005161758,0.0005181155,0.0011759027,0.001930565,0.0012915209,0.0009315587,0.00044932484],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000045426186,0.00012407126,0.0010718193,0.000064722,0.000018423598,0.0002090629,0.00015914666,0.7523216,0.012227856,0.21507363,0.0010980418,0.017586218],"study_design_scores_gemma":[0.0000048499483,0.0000069971056,0.00018228966,0.0000053212643,0.0000026437453,0.00002413365,0.00001617712,0.9842949,0.00044978122,0.013897842,0.00110749,0.0000075706766],"about_ca_topic_score_codex":0.0030969235,"about_ca_topic_score_gemma":0.0024820182,"teacher_disagreement_score":0.0030969235,"about_ca_system_score_codex":0.00051600736,"about_ca_system_score_gemma":0.00039007008,"threshold_uncertainty_score":0.0073776245},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9976955,0.0001531971,0.001724302,0.000008244216,0.000014154377,0.000012422375,0.00001441264,0.000042120006,0.0003356331],"genre_scores_gemma":[0.9983034,0.000075253905,0.0010900337,0.000011169205,0.000003036063,0.0000053064123,0.000017113583,0.000011255132,0.0004833908],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99951255,0.00008444799,0.00003141205,0.00010514814,0.0001466092,0.00011983984],"domain_scores_gemma":[0.9987362,0.00046566816,0.00033084268,0.00013089906,0.00021320717,0.00012315418],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00033699875,0.0006037257,0.0003795696,0.00022062425,0.0002055426,0.0004714475,0.00039904812,0.00049266865,0.0017832759],"category_scores_gemma":[0.0012390587,0.0002486079,0.00018293278,0.00016144555,0.00040544022,0.0002779586,0.00036373013,0.00029102218,0.0001852752],"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":[0.0011051885,0.00012065008,0.0014804633,0.00009445427,0.00001563622,0.00019475714,0.00007995455,0.0012557092,0.9887677,0.00009317481,0.00003559573,0.0067567416],"study_design_scores_gemma":[0.0000357567,0.0040705423,0.010832705,0.000014296114,0.000045137727,0.00017176941,0.000102107726,0.0021504813,0.9817762,0.000022774211,0.0007553717,0.000022698474],"about_ca_topic_score_codex":0.00073891884,"about_ca_topic_score_gemma":0.0010079122,"teacher_disagreement_score":0.0017832759,"about_ca_system_score_codex":0.0001723259,"about_ca_system_score_gemma":0.00016059267,"threshold_uncertainty_score":0.00596565},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.02387119,0.00017737228,0.97189045,0.000054622808,0.000033803834,0.00005643611,0.000050970462,0.00026255983,0.0036026158],"genre_scores_gemma":[0.5550237,0.00023359033,0.43926647,0.00006629776,0.000029663712,0.00037371158,0.00022885896,0.00022505976,0.0045526307],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996716,0.00010074187,0.00001290373,0.00003491581,0.00014379065,0.000036105354],"domain_scores_gemma":[0.99937266,0.00041235224,0.000045479403,0.000029961535,0.00011776631,0.000021715008],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0009592999,0.0009571575,0.00078109844,0.0006203788,0.00033441948,0.00086123496,0.0005507859,0.0008041376,0.0018892662],"category_scores_gemma":[0.001633918,0.00044781654,0.00075495616,0.0003625823,0.000417276,0.0004298993,0.00072806084,0.00078112376,0.00038799862],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000019765102,0.000015909418,0.0001412751,0.00005116772,0.000010983021,0.00001949322,0.000015363365,0.9830966,0.0016584232,0.0017212719,0.00015038426,0.013099404],"study_design_scores_gemma":[0.0000040412606,0.000022242286,0.00006258132,0.000003921574,0.0000018068622,0.0000046547643,0.000005050911,0.9982917,0.00060030504,0.0006638108,0.0003371616,0.000002692553],"about_ca_topic_score_codex":0.0023390807,"about_ca_topic_score_gemma":0.002222269,"teacher_disagreement_score":0.0023390807,"about_ca_system_score_codex":0.00042385544,"about_ca_system_score_gemma":0.00085983204,"threshold_uncertainty_score":0.0063201785},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.14925691,0.0009396706,0.8346179,0.00021056898,0.00027735636,0.00009129248,0.000057469704,0.00060151506,0.013947259],"genre_scores_gemma":[0.96557724,0.000211347,0.030939188,0.000048213766,0.000037068377,0.000049560233,0.000037153673,0.000020195248,0.003079963],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99984014,0.000018498176,0.0000067505835,0.0000266543,0.000093237286,0.0000146959455],"domain_scores_gemma":[0.99981564,0.00007670706,0.000031550517,0.000008024871,0.000058596182,0.000009435377],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020722035,0.0003296643,0.00018765834,0.00015195535,0.00020294166,0.0002822054,0.00045833213,0.00025082016,0.0019212434],"category_scores_gemma":[0.00036463665,0.000097236516,0.00018540917,0.000094457035,0.00021009851,0.00025171062,0.00024250761,0.00024576235,0.00026277694],"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":[0.0005089376,0.00012146217,0.0003890231,0.000408653,0.000028750203,0.00015988512,0.00019579711,0.04801717,0.79196614,0.006221677,0.001249235,0.15073325],"study_design_scores_gemma":[0.000039474835,0.00065579783,0.00076818746,0.000031816075,0.000025141864,0.000070281225,0.000038129954,0.8392373,0.15299901,0.00086959294,0.0052443966,0.000020835905],"about_ca_topic_score_codex":0.0003994076,"about_ca_topic_score_gemma":0.0006548467,"teacher_disagreement_score":0.0019212434,"about_ca_system_score_codex":0.00020299664,"about_ca_system_score_gemma":0.00018708789,"threshold_uncertainty_score":0.006427169},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9959234,0.00005705307,0.0026565413,0.00003333635,0.000011473871,0.000025872358,0.0002288155,0.000115366274,0.00094810186],"genre_scores_gemma":[0.99749136,0.000021056789,0.0013478594,0.000010469116,0.000002364909,0.00001325823,0.00017616329,0.000008774043,0.00092865893],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99992394,0.0000067787746,0.0000031827522,0.00001958539,0.000026843298,0.000019682006],"domain_scores_gemma":[0.99980575,0.000059348644,0.000023011738,0.000015030122,0.00005685453,0.00003999655],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018332253,0.00023773318,0.00023561878,0.00044561797,0.00034569684,0.00025933867,0.0003405527,0.000359189,0.0024524867],"category_scores_gemma":[0.00028771823,0.00006960343,0.00011710768,0.00013091764,0.00041444646,0.00018517241,0.00022902734,0.00022769807,0.00015345072],"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":[0.0012003046,0.00029515452,0.006351055,0.0001038252,0.0000057287793,0.00053268677,0.0002539763,0.007440635,0.9696181,0.00032470562,0.00045455998,0.013419263],"study_design_scores_gemma":[0.00016936484,0.004566957,0.11980326,0.00008095266,0.000029131594,0.0006105109,0.00083994906,0.17901081,0.69091773,0.0003297831,0.0035193374,0.0001222062],"about_ca_topic_score_codex":0.0023357691,"about_ca_topic_score_gemma":0.0017328786,"teacher_disagreement_score":0.0024524867,"about_ca_system_score_codex":0.00028293146,"about_ca_system_score_gemma":0.00019214248,"threshold_uncertainty_score":0.008204401},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9399099,0.00026614234,0.039073337,0.00022712402,0.00006607102,0.00012088687,0.0005465882,0.00032201473,0.019467972],"genre_scores_gemma":[0.98783815,0.000059544913,0.009573149,0.000020676964,0.0000066181524,0.00003711925,0.00014781959,0.000022882992,0.0022941018],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99990106,0.000021385573,0.0000056559975,0.000012444031,0.000037458394,0.000022121521],"domain_scores_gemma":[0.9995407,0.00022797249,0.00007960297,0.00002511583,0.000079604026,0.000047092093],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00026267898,0.0003564242,0.00038307332,0.0004364715,0.00047881115,0.00054788566,0.00045879395,0.0007989567,0.0030330387],"category_scores_gemma":[0.0007995535,0.00020384754,0.00031935214,0.0003265718,0.000457465,0.0002465354,0.00034974556,0.00031273774,0.00027396344],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00009573804,0.000069185306,0.0054122494,0.00005586087,0.000012406466,0.0003129976,0.00008318912,0.9785003,0.008377693,0.0019225208,0.00042967766,0.0047281273],"study_design_scores_gemma":[0.0000114391505,0.000044648936,0.0012481889,0.0000072062753,0.0000021207152,0.00002993674,0.000035143847,0.99723035,0.0008911917,0.00020145449,0.0002927444,0.0000055656737],"about_ca_topic_score_codex":0.0065564928,"about_ca_topic_score_gemma":0.004716916,"teacher_disagreement_score":0.0065564928,"about_ca_system_score_codex":0.00040817537,"about_ca_system_score_gemma":0.0005315613,"threshold_uncertainty_score":0.013036609},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9682929,0.0005338078,0.008022826,0.000088339446,0.000086907945,0.0000641584,0.0012110836,0.00012220841,0.021577867],"genre_scores_gemma":[0.99031293,0.00029023335,0.0022403991,0.000034647735,0.000014822376,0.000019858267,0.0007623171,0.00002778777,0.0062969215],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998779,0.000013943244,0.0000059295476,0.000029956165,0.000053155796,0.000018982952],"domain_scores_gemma":[0.99977857,0.00006819847,0.000016938262,0.00001618546,0.00009077347,0.000029375691],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00009624731,0.00022988296,0.0001460797,0.00076075434,0.00020566299,0.00037286762,0.000111983085,0.00027905818,0.00525216],"category_scores_gemma":[0.0004540631,0.000089458204,0.00013235246,0.0002897075,0.00011572198,0.0001757129,0.0002822603,0.00022824081,0.00092307595],"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":[0.0013569377,0.00016703318,0.07413262,0.00033653525,0.00008762139,0.0036141963,0.0012697746,0.011579865,0.67545146,0.0011054743,0.003954395,0.22694407],"study_design_scores_gemma":[0.000088623325,0.0014055518,0.814988,0.00016197121,0.0000890161,0.008123593,0.0031373242,0.038560458,0.107782334,0.0010578493,0.024503892,0.00010143905],"about_ca_topic_score_codex":0.0027613055,"about_ca_topic_score_gemma":0.0038997263,"teacher_disagreement_score":0.00525216,"about_ca_system_score_codex":0.00013831843,"about_ca_system_score_gemma":0.00008870955,"threshold_uncertainty_score":0.017570198},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9868716,0.00004529193,0.009758747,0.00003231147,0.000018561324,0.000024807992,0.00039937717,0.00017602569,0.0026732793],"genre_scores_gemma":[0.9945857,0.000027984739,0.004197133,0.000009160641,0.0000036037184,0.00002724221,0.00028300128,0.00004084898,0.0008253692],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997862,0.000015365575,0.000008358701,0.000046687026,0.00010948044,0.000033843346],"domain_scores_gemma":[0.9995303,0.00014469176,0.000041553718,0.00008219386,0.00015651922,0.000044653774],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002810144,0.00033358426,0.00027698613,0.0002901,0.00039707017,0.00028511614,0.0004579993,0.00045838783,0.0030365256],"category_scores_gemma":[0.0006930276,0.00013810243,0.00018989749,0.0001933112,0.00048093701,0.0002892946,0.0004309517,0.00036067324,0.00036119248],"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":[0.00073570356,0.00036196678,0.009205148,0.00013061168,0.000017977829,0.00041558017,0.00029792514,0.038884364,0.92976874,0.0012241309,0.0008439099,0.01811392],"study_design_scores_gemma":[0.0000405821,0.00094783393,0.022006352,0.000023412871,0.000015158482,0.00017488026,0.00021084349,0.31767893,0.65683955,0.00037498304,0.0016419991,0.000045482833],"about_ca_topic_score_codex":0.0014100859,"about_ca_topic_score_gemma":0.0017199289,"teacher_disagreement_score":0.0030365256,"about_ca_system_score_codex":0.00017830546,"about_ca_system_score_gemma":0.00019465567,"threshold_uncertainty_score":0.010158181},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.28561577,0.0025821086,0.7007921,0.00019796882,0.00029509704,0.00010170347,0.000063189065,0.00066111557,0.009691009],"genre_scores_gemma":[0.97009426,0.00031849713,0.027949704,0.000038976235,0.00005018628,0.000031968593,0.00002688377,0.000017692488,0.001471754],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997851,0.000019344689,0.000008339064,0.000030286299,0.00014068361,0.000016228567],"domain_scores_gemma":[0.999764,0.000100150915,0.000055518547,0.000009430941,0.00005848413,0.000012338861],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018803697,0.00040585283,0.00018817525,0.00020083673,0.00014828332,0.00025941312,0.0005013174,0.00024586523,0.0011676336],"category_scores_gemma":[0.00037428038,0.00009987954,0.00015567597,0.00009426843,0.00024526796,0.00023473622,0.00026395003,0.00024054077,0.00019719724],"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":[0.00022599498,0.00006814198,0.00022064426,0.00025186306,0.00001255909,0.000092600036,0.00006889303,0.011995294,0.925944,0.0013106407,0.00027112986,0.059538376],"study_design_scores_gemma":[0.00004806694,0.0013491183,0.0017470863,0.000037821555,0.000046499525,0.00017824443,0.000037668207,0.39465126,0.59472734,0.0008539283,0.00628976,0.00003319763],"about_ca_topic_score_codex":0.00018745376,"about_ca_topic_score_gemma":0.00036239083,"teacher_disagreement_score":0.0011676336,"about_ca_system_score_codex":0.00019283165,"about_ca_system_score_gemma":0.00010222701,"threshold_uncertainty_score":0.0039060712},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.94204307,0.00024329723,0.028330464,0.00044712247,0.0001501632,0.00008474469,0.0007339556,0.0007677809,0.027199423],"genre_scores_gemma":[0.9937256,0.00002869554,0.0032690382,0.000031242547,0.000011611905,0.000027917584,0.00018110871,0.000072128605,0.002652608],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998807,0.000030987496,0.0000052069017,0.000020263187,0.000029931802,0.0000329329],"domain_scores_gemma":[0.9992483,0.00045975516,0.000043439293,0.00003423241,0.00013182241,0.00008228045],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00032139305,0.0006761183,0.00082832936,0.000387201,0.0008804481,0.0008708121,0.0009618331,0.0019932988,0.004879502],"category_scores_gemma":[0.0014542138,0.000494165,0.00065645727,0.0003698286,0.00056266243,0.0005582952,0.00045234925,0.00088395586,0.00042035876],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00009875985,0.00007553479,0.0014751728,0.00002828748,0.000013685118,0.00006961816,0.000022142072,0.99460536,0.0011763033,0.00055714237,0.00038269913,0.001495273],"study_design_scores_gemma":[0.000010074903,0.0000136109875,0.00026486017,0.0000014529467,0.0000015665381,0.000002087237,0.000006032281,0.999461,0.00014596271,0.00003680768,0.00005392674,0.0000025797985],"about_ca_topic_score_codex":0.058826525,"about_ca_topic_score_gemma":0.029622793,"teacher_disagreement_score":0.058826525,"about_ca_system_score_codex":0.0009698786,"about_ca_system_score_gemma":0.0014391292,"threshold_uncertainty_score":0.116968274},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.19923602,0.0015199876,0.78139144,0.00044679648,0.00014297834,0.00015141339,0.0001704006,0.00020962988,0.016731448],"genre_scores_gemma":[0.9193612,0.0005105491,0.07324378,0.00013473773,0.00007955268,0.00020576228,0.00016150375,0.00014201802,0.0061609796],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997682,0.00010767525,0.000007794028,0.00002491609,0.000062281586,0.000029186394],"domain_scores_gemma":[0.9993899,0.00043645533,0.000039144576,0.000018322948,0.00008738122,0.000028767026],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0010975635,0.0012345844,0.0013274406,0.00056977593,0.0005734215,0.0010765484,0.0005555554,0.0012587268,0.001924462],"category_scores_gemma":[0.0017771983,0.00049893046,0.0009277027,0.00040519255,0.00048684276,0.0006722955,0.00073309103,0.000685543,0.00017382766],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000021020407,0.00002644023,0.000120727374,0.00004180136,0.000016660271,0.000031878048,0.000007869989,0.99606043,0.0006643227,0.0005757793,0.00010998066,0.0023231718],"study_design_scores_gemma":[0.0000030094056,0.000019173794,0.00007959619,0.0000030512801,0.0000058001447,0.0000034652846,0.000006220381,0.9995272,0.00014345828,0.0001316898,0.00007568579,0.0000017677858],"about_ca_topic_score_codex":0.0062772124,"about_ca_topic_score_gemma":0.0054666786,"teacher_disagreement_score":0.0062772124,"about_ca_system_score_codex":0.00034121663,"about_ca_system_score_gemma":0.00095435244,"threshold_uncertainty_score":0.012481332},"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":"editorial","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0009599351,0.0008249513,0.0031692889,0.012169884,0.9722649,0.000037953312,0.0049240245,0.0024025384,0.0032464876],"genre_scores_gemma":[0.14553264,0.0071815085,0.04723711,0.036260776,0.23303878,0.00064998365,0.029874325,0.016752964,0.4834719],"study_design_codex":"not_applicable","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9965636,0.0002981267,0.00043633708,0.00046049256,0.001913108,0.00032827823],"domain_scores_gemma":[0.96986043,0.00265781,0.0011109458,0.0021544262,0.023262275,0.00095407624],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0015052117,0.0027323582,0.0020976488,0.0050612255,0.00225479,0.0031665585,0.0037968338,0.004705401,0.117552444],"category_scores_gemma":[0.044673666,0.0012350802,0.0018159186,0.003637172,0.0013630133,0.0025562102,0.0025346978,0.005768995,0.039354544],"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":[0.00007413691,0.000007303943,0.0001508469,0.00022811396,0.000020880487,0.00017668752,0.00003417638,0.0005722784,0.00026804008,0.0008310514,0.98689806,0.010738462],"study_design_scores_gemma":[0.00019399486,0.00004495985,0.0033375989,0.00044021048,0.00007626885,0.00075686764,0.00022021736,0.006456692,0.0027121746,0.0025843717,0.9830546,0.00012216273],"about_ca_topic_score_codex":0.04208303,"about_ca_topic_score_gemma":0.03921445,"teacher_disagreement_score":0.117552444,"about_ca_system_score_codex":0.0032592288,"about_ca_system_score_gemma":0.0046320697,"threshold_uncertainty_score":0.39325207},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9575062,0.000341199,0.03995219,0.00019158605,0.000028236853,0.000060191236,0.0004469104,0.00018764657,0.0012859395],"genre_scores_gemma":[0.9974625,0.000054123408,0.0020941172,0.000021355501,0.0000037129805,0.000019537514,0.00022548692,0.000013517502,0.000105647916],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9984143,0.00090368337,0.00008456267,0.0002571426,0.00017993868,0.00016040627],"domain_scores_gemma":[0.9781185,0.01960573,0.00077530165,0.0008078512,0.00058945734,0.000103319835],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0035401932,0.0010755801,0.0005727392,0.0007727377,0.00043117913,0.0008353175,0.0005162632,0.0012555479,0.00060647004],"category_scores_gemma":[0.014062008,0.00039953765,0.0010981471,0.0004367422,0.00065458403,0.00078037824,0.0009207706,0.0011416,0.000086924665],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0001306308,0.00005647832,0.0057802238,0.000053331427,0.00009579291,0.000062067236,0.000025910957,0.9894378,0.0015912232,0.00027860093,0.000080439175,0.0024074654],"study_design_scores_gemma":[0.000010739618,0.00013861308,0.0059036706,0.000019895711,0.00005321886,0.00003347629,0.000054303095,0.99010557,0.0031266266,0.00041820435,0.00011438747,0.000021313881],"about_ca_topic_score_codex":0.011246343,"about_ca_topic_score_gemma":0.004411097,"teacher_disagreement_score":0.011246343,"about_ca_system_score_codex":0.00070143974,"about_ca_system_score_gemma":0.0004646245,"threshold_uncertainty_score":0.022361755},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9982603,0.000049073635,0.0010089158,0.000007793993,0.0000035859118,0.000005457563,0.000024075833,0.000015039512,0.0006257921],"genre_scores_gemma":[0.99966574,0.000016348486,0.0000982615,0.0000026966861,0.0000020604225,0.0000025278046,0.000017884,0.000004019453,0.0001904119],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.99989736,0.000019099958,0.0000050415665,0.000019196797,0.00003326409,0.00002611992],"domain_scores_gemma":[0.99855834,0.0009906451,0.000120580815,0.000054910306,0.00017922116,0.00009620519],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025630512,0.00016109725,0.00033590608,0.00030234552,0.00018603125,0.00030542666,0.00021226471,0.00032128027,0.0017876244],"category_scores_gemma":[0.0012776855,0.00014878115,0.0001831293,0.00018958017,0.00051072944,0.00033092953,0.00028998443,0.00023059861,0.00018116209],"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":[0.0016257513,0.00012321031,0.01112202,0.00006542758,0.000018861876,0.0008386998,0.00040045858,0.011251025,0.96854454,0.0005377391,0.00012675027,0.005345549],"study_design_scores_gemma":[0.0002825705,0.002716186,0.29789123,0.00004048116,0.00009599567,0.0021377725,0.0012145553,0.2535538,0.4395338,0.0013176759,0.0010637072,0.00015224128],"about_ca_topic_score_codex":0.0010935221,"about_ca_topic_score_gemma":0.00060893426,"teacher_disagreement_score":0.0017876244,"about_ca_system_score_codex":0.00012981477,"about_ca_system_score_gemma":0.00013363647,"threshold_uncertainty_score":0.005980253},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.52355075,0.00052640715,0.46829718,0.00015211068,0.00010533607,0.000059152448,0.00003707145,0.00017579054,0.0070961593],"genre_scores_gemma":[0.97656304,0.00027053864,0.021071065,0.00003081384,0.000039691677,0.000020821253,0.000015283837,0.00002572281,0.0019631593],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99990106,0.00002800703,0.0000048460183,0.000019963869,0.000030960924,0.000015028043],"domain_scores_gemma":[0.99960655,0.00015247542,0.00012869654,0.000027642254,0.00005083728,0.000033832683],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00040465448,0.00056608923,0.00033650885,0.0006514104,0.00022040117,0.00060278026,0.0004235271,0.0004438461,0.0007554103],"category_scores_gemma":[0.0011005632,0.00016344164,0.00028725227,0.00025036905,0.0011072541,0.0010156953,0.00064170925,0.0005002028,0.00009500209],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00019905066,0.00009411204,0.0029101784,0.00017070839,0.00003371048,0.00074832566,0.00035737563,0.40822732,0.22135043,0.33992413,0.0004334644,0.02555124],"study_design_scores_gemma":[0.000006592742,0.00007624874,0.0005712902,0.000007375653,0.000006929558,0.00006668347,0.000025151623,0.97607285,0.006864206,0.015674638,0.00061086606,0.000017181368],"about_ca_topic_score_codex":0.0006316346,"about_ca_topic_score_gemma":0.00032870178,"teacher_disagreement_score":0.0007554103,"about_ca_system_score_codex":0.00027530012,"about_ca_system_score_gemma":0.00020906002,"threshold_uncertainty_score":0.0025270581},"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":"review","genre_gemma":"review","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"review","genre_consensus":"review","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.028640492,0.529621,0.4106743,0.0015609527,0.0010155211,0.00006755594,0.00012891131,0.0008127571,0.027478535],"genre_scores_gemma":[0.25137377,0.52118945,0.21095014,0.00080746674,0.0016805572,0.00012271808,0.0004080266,0.0003940168,0.0130738225],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.99951434,0.000059423593,0.00003557507,0.00012250624,0.00023597016,0.000032126038],"domain_scores_gemma":[0.9989304,0.00052116904,0.00010307339,0.000082159095,0.0003213623,0.000041782503],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0009778016,0.00084595085,0.00083089457,0.0010211646,0.00030313348,0.0011173051,0.0008500869,0.000812177,0.0029574698],"category_scores_gemma":[0.001442497,0.00049112533,0.0008517121,0.0009378282,0.0005361226,0.0013900687,0.0008308412,0.0011266678,0.0010951307],"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":[0.00015186214,0.00015994624,0.0010224232,0.007438362,0.00009263725,0.00011727188,0.00021899199,0.03863819,0.055479407,0.018995142,0.0042263316,0.8734594],"study_design_scores_gemma":[0.000050640785,0.0012173039,0.004343984,0.0018041176,0.0005133596,0.000938945,0.00037059715,0.23765111,0.12264857,0.020325517,0.6098999,0.00023600234],"about_ca_topic_score_codex":0.0007533801,"about_ca_topic_score_gemma":0.0006802603,"teacher_disagreement_score":0.0029574698,"about_ca_system_score_codex":0.00035538204,"about_ca_system_score_gemma":0.00058319984,"threshold_uncertainty_score":0.009893715},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9942233,0.0001232696,0.004344736,0.000025582412,0.0000115853045,0.000010859581,0.0000292055,0.000048445694,0.0011830496],"genre_scores_gemma":[0.9984004,0.000047516744,0.0010534695,0.00000900808,0.000004004936,0.000004674989,0.000031556225,0.0000042007728,0.00044522167],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997509,0.000021307509,0.0000072996945,0.00004633002,0.00012942142,0.000044799115],"domain_scores_gemma":[0.9997286,0.00010471609,0.00003535414,0.000018612156,0.00007755952,0.000035088215],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00013730252,0.00025493884,0.00041368703,0.00037846414,0.00032223522,0.00021172178,0.000248804,0.00034718905,0.00081582105],"category_scores_gemma":[0.00047055786,0.00008689051,0.00017539001,0.00013313127,0.0005117018,0.00028584505,0.00033665146,0.00029160405,0.00010263265],"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":[0.00023785893,0.000062258085,0.0040222947,0.00007005308,0.000008153068,0.0010321873,0.00026707182,0.004430849,0.9806024,0.00023291643,0.00007288106,0.0089610545],"study_design_scores_gemma":[0.00005080538,0.0020532059,0.12501644,0.000026765943,0.0000346137,0.0018822068,0.0010379882,0.07787296,0.7881526,0.00050325115,0.0032714948,0.00009775703],"about_ca_topic_score_codex":0.0012587431,"about_ca_topic_score_gemma":0.0012757484,"teacher_disagreement_score":0.0012587431,"about_ca_system_score_codex":0.00022950585,"about_ca_system_score_gemma":0.00014273137,"threshold_uncertainty_score":0.0027291775},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.024206912,0.054474797,0.8064748,0.0013213046,0.0021147488,0.00027282958,0.00046909472,0.0020494524,0.10861606],"genre_scores_gemma":[0.2736612,0.04974859,0.62629586,0.0010266646,0.0009947715,0.00045993447,0.0009914584,0.001089665,0.045731876],"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99914384,0.00009927912,0.000061164734,0.00018749225,0.00043829367,0.00006978846],"domain_scores_gemma":[0.99903536,0.00025461236,0.00013420149,0.00020672356,0.0002973854,0.000071770766],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000871408,0.0008815776,0.0008422129,0.0012698247,0.00046150666,0.0021789125,0.0016797299,0.0016027556,0.010211271],"category_scores_gemma":[0.0016478538,0.0006480625,0.001227298,0.0009919438,0.0007388266,0.0018143808,0.0011009644,0.0018348047,0.0073994305],"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":[0.00022117529,0.00020514507,0.0014235313,0.0030669412,0.00008475527,0.00063849473,0.0003502251,0.04774969,0.13168518,0.15049641,0.011500118,0.65257835],"study_design_scores_gemma":[0.000056761473,0.001258753,0.0016122573,0.0006194047,0.00014264636,0.002329672,0.00015744536,0.10716865,0.08866939,0.03874825,0.75904137,0.00019539382],"about_ca_topic_score_codex":0.00047431458,"about_ca_topic_score_gemma":0.000496593,"teacher_disagreement_score":0.010211271,"about_ca_system_score_codex":0.0007256662,"about_ca_system_score_gemma":0.0006700768,"threshold_uncertainty_score":0.034160078},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.5131784,0.0002442529,0.4720674,0.00021593295,0.0000475106,0.000051196992,0.00007148105,0.00056273345,0.013561058],"genre_scores_gemma":[0.9277794,0.000072463365,0.07044241,0.000042397784,0.000009525253,0.00004807227,0.00006925484,0.00007091475,0.0014657216],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998549,0.000024862327,0.000004315594,0.000018896431,0.00007155534,0.000025491518],"domain_scores_gemma":[0.99972194,0.00012368649,0.00003824966,0.000031487776,0.000065227076,0.000019462503],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00035498894,0.000501789,0.00041112848,0.00025177543,0.00022713105,0.00051121233,0.0004251514,0.00044083022,0.0008320247],"category_scores_gemma":[0.00085481134,0.00019157246,0.00034506826,0.00012654829,0.00045740657,0.00042621762,0.0004423802,0.00037057928,0.00020654414],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00014630595,0.000119485485,0.0013949518,0.00007168325,0.00001688027,0.0001355872,0.00006517455,0.904854,0.0622979,0.0045786197,0.00032573074,0.025993655],"study_design_scores_gemma":[0.000014185796,0.00007317801,0.00030972678,0.0000032957544,0.0000026168539,0.000025011486,0.000013832599,0.988308,0.010128668,0.0007321577,0.00038296962,0.0000064053183],"about_ca_topic_score_codex":0.0010524357,"about_ca_topic_score_gemma":0.0009828943,"teacher_disagreement_score":0.0010524357,"about_ca_system_score_codex":0.00024317998,"about_ca_system_score_gemma":0.00042399365,"threshold_uncertainty_score":0.0027834177},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.08772609,0.0001811305,0.90981877,0.00007983173,0.000043947053,0.000031522835,0.000027370332,0.00023100713,0.0018604],"genre_scores_gemma":[0.90982,0.00033122778,0.08747072,0.00004357319,0.00004503299,0.00008229946,0.000069033755,0.00004816705,0.0020898494],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998385,0.000034710236,0.000009742578,0.00003766776,0.00006301272,0.000016277343],"domain_scores_gemma":[0.9998047,0.00008626336,0.000033096378,0.000015730355,0.000047581852,0.000012619339],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003526255,0.0005532314,0.00049229333,0.0008166221,0.00030762778,0.00048531237,0.00069649576,0.00085405214,0.0005280292],"category_scores_gemma":[0.0008333002,0.00022496696,0.0006516348,0.0004749378,0.00042962315,0.00085973827,0.00046295515,0.00047653585,0.00011677761],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000276208,0.000046659312,0.0016649566,0.000039965587,0.000013803349,0.00010678284,0.000037226524,0.9556631,0.013583137,0.005953754,0.00021369821,0.022649243],"study_design_scores_gemma":[7.287741e-7,0.0000038788803,0.00008133018,5.5790787e-7,0.0000011066084,0.0000058119263,0.0000012210235,0.9993963,0.00026390993,0.00020407366,0.00003889335,0.0000021625115],"about_ca_topic_score_codex":0.0035937359,"about_ca_topic_score_gemma":0.0019051324,"teacher_disagreement_score":0.0035937359,"about_ca_system_score_codex":0.00038011928,"about_ca_system_score_gemma":0.00063283974,"threshold_uncertainty_score":0.0071456432},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9629056,0.00031928567,0.03198533,0.00008086035,0.00004656586,0.00004978755,0.00016211656,0.0002636438,0.0041868067],"genre_scores_gemma":[0.9863272,0.00012204465,0.012394015,0.000010478025,0.000004372066,0.000024345507,0.000107071006,0.000016857899,0.0009936661],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99981576,0.000019521214,0.000017186487,0.000031494816,0.000070754075,0.00004527086],"domain_scores_gemma":[0.9994615,0.00020061099,0.00011470775,0.000046207457,0.0001324551,0.00004446644],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00040439205,0.00046981388,0.000536622,0.000670787,0.0004922642,0.0006819996,0.0005583817,0.00072116614,0.0010201631],"category_scores_gemma":[0.00096055644,0.00019297843,0.00040988988,0.00087604683,0.0006309971,0.0004408884,0.00027824365,0.000295976,0.00012392922],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00037874098,0.0003323494,0.015167537,0.00029300275,0.00004587274,0.000805099,0.00040477747,0.8360046,0.1217102,0.0032237147,0.0005784166,0.021055698],"study_design_scores_gemma":[0.000016533006,0.00009049259,0.0031061536,0.0000070204987,0.0000073000588,0.00005880681,0.000056336965,0.98855245,0.007678154,0.00020260208,0.00020437346,0.000019879457],"about_ca_topic_score_codex":0.0052286554,"about_ca_topic_score_gemma":0.0031728833,"teacher_disagreement_score":0.0052286554,"about_ca_system_score_codex":0.00042270892,"about_ca_system_score_gemma":0.0006096282,"threshold_uncertainty_score":0.010396481},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.743392,0.00045031693,0.23693691,0.0003299324,0.00014277718,0.00010676133,0.00033988283,0.0009936717,0.017307797],"genre_scores_gemma":[0.97057915,0.00012603588,0.02680505,0.000028260627,0.000017051963,0.00006785006,0.00016168536,0.000047792866,0.0021671008],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998548,0.000031064603,0.0000065319505,0.000016945854,0.0000542866,0.000036436744],"domain_scores_gemma":[0.99977404,0.00009213344,0.000029754412,0.0000149845055,0.000062076244,0.000026982452],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023012265,0.0004833945,0.0005534416,0.00042989454,0.0005332616,0.0004945537,0.00050382107,0.00091303734,0.0014142535],"category_scores_gemma":[0.0005151046,0.0002333313,0.0005630302,0.00031563966,0.00038568524,0.00040646148,0.00041965127,0.00037464828,0.00015870354],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000046267083,0.000038138995,0.0014352975,0.000042404416,0.000014160597,0.00014750334,0.000053864424,0.985719,0.008057577,0.0009974499,0.00014836066,0.0032999124],"study_design_scores_gemma":[0.000007314814,0.00001181233,0.00028046445,0.0000020415998,0.0000017461078,0.000011230299,0.000009658704,0.99881846,0.00061858876,0.00009322742,0.00014204317,0.0000034633265],"about_ca_topic_score_codex":0.011639651,"about_ca_topic_score_gemma":0.0048154234,"teacher_disagreement_score":0.011639651,"about_ca_system_score_codex":0.0004301975,"about_ca_system_score_gemma":0.0006772298,"threshold_uncertainty_score":0.023143828},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8490038,0.0044707553,0.14150308,0.00015399882,0.00019938033,0.000071171635,0.00009550321,0.0007694425,0.0037328599],"genre_scores_gemma":[0.95911777,0.00086452236,0.038420822,0.0000855164,0.000018541425,0.000040998322,0.0000637312,0.00003266702,0.0013555912],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998012,0.000018228648,0.000016017408,0.000044126224,0.0000914226,0.000029033226],"domain_scores_gemma":[0.99971324,0.000051077586,0.00012176356,0.000024170273,0.00006987886,0.000019833516],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002858731,0.0003256593,0.00028747227,0.00022006202,0.00012779415,0.0003288638,0.0003885675,0.00046318467,0.00053751096],"category_scores_gemma":[0.00048020683,0.00012910002,0.0002793265,0.00011790324,0.00022742643,0.00048877735,0.00033376558,0.00022350927,0.0001496288],"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":[0.00006251956,0.000023371993,0.0010501846,0.00022177055,0.000009031283,0.00022354744,0.000052428244,0.003424937,0.97685814,0.00038413645,0.0001354072,0.017554458],"study_design_scores_gemma":[0.000028234394,0.00081413717,0.005165873,0.000042001775,0.000032228854,0.0005149781,0.000091614675,0.037504725,0.94931275,0.0001769007,0.0062793205,0.000037234513],"about_ca_topic_score_codex":0.00014216604,"about_ca_topic_score_gemma":0.00021136798,"teacher_disagreement_score":0.00053751096,"about_ca_system_score_codex":0.00016871437,"about_ca_system_score_gemma":0.00015428317,"threshold_uncertainty_score":0.0017981529},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"review","genre_consensus":"review","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.00038734154,0.99501085,0.0020580757,0.00021080533,0.00036590733,0.000007194235,0.000046291978,0.00003303149,0.001880473],"genre_scores_gemma":[0.0019334605,0.9953054,0.0012936452,0.00012721166,0.00029402864,0.000008661513,0.00008126513,0.000011758442,0.0009445706],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.99976844,0.00003123924,0.000032509455,0.000058376947,0.0000904957,0.000018935509],"domain_scores_gemma":[0.9993445,0.00040112127,0.000054878226,0.000025837364,0.00014644062,0.000027153326],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006091096,0.0011563363,0.0013590669,0.002318446,0.00028267017,0.0014329951,0.0009928684,0.0011631027,0.003914067],"category_scores_gemma":[0.0012182519,0.0005304317,0.000907471,0.003009917,0.00044881523,0.0017727889,0.0006856615,0.0014951164,0.0028289133],"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":[0.000064175816,0.00010713697,0.00033455394,0.025931904,0.00010149254,0.00021422746,0.00013184987,0.0041402476,0.0034906084,0.01153859,0.022515364,0.93142974],"study_design_scores_gemma":[0.000009947934,0.00016008032,0.00092445756,0.0074680736,0.00018799718,0.001025677,0.00013654865,0.0019152154,0.002396419,0.0054322355,0.98027956,0.00006388485],"about_ca_topic_score_codex":0.0011925153,"about_ca_topic_score_gemma":0.0010345944,"teacher_disagreement_score":0.003914067,"about_ca_system_score_codex":0.0004216858,"about_ca_system_score_gemma":0.0010004201,"threshold_uncertainty_score":0.013093829},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9683192,0.00035043096,0.02795573,0.00009423332,0.00014118751,0.00025867386,0.00025638784,0.00022348751,0.0024007806],"genre_scores_gemma":[0.9765413,0.000288519,0.019724304,0.00004950328,0.00004647951,0.00017586442,0.00016630386,0.000082788225,0.002924848],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9992625,0.00008837166,0.00003872139,0.00016106732,0.00033993294,0.000109359666],"domain_scores_gemma":[0.9989405,0.0004129333,0.0001640062,0.000113984475,0.0002608006,0.00010779716],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00083336333,0.0006219456,0.0003275949,0.00030364515,0.0002828454,0.00032418664,0.0004995748,0.0006124758,0.0023739573],"category_scores_gemma":[0.0011740542,0.00026326996,0.000276771,0.00032400034,0.00069899834,0.00048606098,0.00062275346,0.0005800834,0.00037242708],"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":[0.00024108544,0.00018981755,0.00039257418,0.0001868977,0.000008652401,0.00007101831,0.00017798341,0.0004909365,0.989881,0.00020433511,0.00013815699,0.008017527],"study_design_scores_gemma":[0.000038894355,0.0018281001,0.0027461608,0.000008717514,0.000013155198,0.00007533383,0.0000477672,0.0017299193,0.9916454,0.00005009818,0.001801953,0.000014535657],"about_ca_topic_score_codex":0.00042723806,"about_ca_topic_score_gemma":0.00041901533,"teacher_disagreement_score":0.0023739573,"about_ca_system_score_codex":0.00022471012,"about_ca_system_score_gemma":0.00029491325,"threshold_uncertainty_score":0.007941723},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.83773553,0.00010590281,0.16040744,0.00006569662,0.000029175313,0.000030580944,0.00008137408,0.00075171894,0.0007925391],"genre_scores_gemma":[0.9615194,0.000029976492,0.037902787,0.000010858983,0.0000069204234,0.00001545343,0.00009612514,0.00003646085,0.0003820478],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997156,0.000086208885,0.000017453254,0.000051700303,0.00010398202,0.000025023388],"domain_scores_gemma":[0.99840826,0.00093708385,0.00016498244,0.00012422237,0.00032038396,0.000045094228],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0011110059,0.00046384038,0.0004484109,0.00043449755,0.00017133384,0.00043463506,0.0005082488,0.0005407687,0.00061037793],"category_scores_gemma":[0.0031656718,0.00020403381,0.00028780274,0.00026869922,0.00029499482,0.0008076287,0.00049631903,0.00039819998,0.00015058435],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0019260808,0.0006116523,0.030336753,0.00042256142,0.0002031734,0.00017557321,0.00034563366,0.5614126,0.18364522,0.001159782,0.000524787,0.21923618],"study_design_scores_gemma":[0.000017240638,0.00020580483,0.004612912,0.000006122304,0.000012325371,0.000026244144,0.000025112817,0.96597165,0.028899599,0.00008030485,0.00012558384,0.000016987533],"about_ca_topic_score_codex":0.0024854986,"about_ca_topic_score_gemma":0.0023874706,"teacher_disagreement_score":0.0024854986,"about_ca_system_score_codex":0.00017140884,"about_ca_system_score_gemma":0.0004715257,"threshold_uncertainty_score":0.0058755875},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9956939,0.00031716435,0.0032505314,0.000028034683,0.000034868506,0.00002290067,0.000070465205,0.000053755975,0.0005283492],"genre_scores_gemma":[0.99725074,0.00016626208,0.001919817,0.00002066086,0.00001955437,0.000018171677,0.000063637744,0.000025532983,0.0005156693],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.999483,0.0000637186,0.0000394515,0.00010241552,0.0002199033,0.000091409536],"domain_scores_gemma":[0.99856323,0.0005452653,0.00036920508,0.00013335692,0.00029750212,0.000091429036],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00052693894,0.0005628512,0.00031600217,0.0004176672,0.00036656423,0.0005388634,0.0003960253,0.00052302884,0.0018242352],"category_scores_gemma":[0.0012473761,0.0001978704,0.00020286255,0.00028099082,0.0006617028,0.0005457758,0.00051670475,0.0005909103,0.00020828248],"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":[0.00015386309,0.0001281178,0.00070423604,0.000047080957,0.0000041799794,0.00009023123,0.0000800858,0.00024893598,0.9965102,0.000091616246,0.000027897258,0.0019136387],"study_design_scores_gemma":[0.000023251327,0.0011593909,0.0045716576,0.000009111352,0.000013392106,0.00009555479,0.0000635169,0.004225837,0.98933524,0.000043143344,0.0004444978,0.000015376076],"about_ca_topic_score_codex":0.00044094914,"about_ca_topic_score_gemma":0.00028590419,"teacher_disagreement_score":0.0018242352,"about_ca_system_score_codex":0.00026888476,"about_ca_system_score_gemma":0.00016038271,"threshold_uncertainty_score":0.006102681},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7134924,0.0003175109,0.27920496,0.00014654019,0.000046472967,0.0000517303,0.000105932435,0.00034988477,0.006284552],"genre_scores_gemma":[0.9598257,0.000106661566,0.038503576,0.000011783822,0.000005074446,0.00002594203,0.00005131494,0.000023116841,0.0014468841],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999188,0.00001994314,0.0000034281768,0.00000933745,0.00003779223,0.000010650043],"domain_scores_gemma":[0.999853,0.00006205368,0.000018166696,0.000017177917,0.000037412185,0.000012242972],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016449919,0.00022036713,0.00031717055,0.00015779246,0.00025337006,0.000263744,0.00033052845,0.00032180786,0.0009858599],"category_scores_gemma":[0.00038103975,0.00013991249,0.00019203825,0.0001319569,0.00034428507,0.00025138084,0.00030269218,0.00026006467,0.00026540257],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0001786739,0.00017224063,0.005687119,0.00016722736,0.00002039194,0.00046207494,0.00022384677,0.61472315,0.34360293,0.011488507,0.0003167386,0.022957088],"study_design_scores_gemma":[0.000006805972,0.00003953109,0.00047905388,0.0000028750142,0.0000010115924,0.00003595545,0.00001665746,0.9906171,0.008246265,0.0003025907,0.00024669047,0.000005336956],"about_ca_topic_score_codex":0.0017675867,"about_ca_topic_score_gemma":0.0010978434,"teacher_disagreement_score":0.0017675867,"about_ca_system_score_codex":0.00015784346,"about_ca_system_score_gemma":0.0003858456,"threshold_uncertainty_score":0.0035145879},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99293435,0.000031963522,0.0039854604,0.00005053765,0.000015527703,0.000017548371,0.00010091209,0.00009715715,0.0027666453],"genre_scores_gemma":[0.9979381,0.0000112763,0.0012576006,0.000010968855,0.0000023461103,0.000011190201,0.00011251824,0.000020591373,0.0006354211],"study_design_codex":"simulation_or_modeling","study_design_gemma":"observational","domain_scores_codex":[0.9998838,0.00002228473,0.0000042119395,0.000017251965,0.000039583796,0.000032977943],"domain_scores_gemma":[0.9997483,0.000108432556,0.00002367162,0.000018702198,0.000066153465,0.00003469572],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021237605,0.00044509643,0.00041509533,0.000288038,0.00028732952,0.0005036727,0.00038999645,0.00070124655,0.0017733318],"category_scores_gemma":[0.0007723984,0.00013787112,0.00028625032,0.00019246407,0.00038601743,0.00033120223,0.0002976819,0.0004570932,0.00015794509],"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":[0.0006523002,0.00026612877,0.008320342,0.00012244031,0.000051630846,0.00049897033,0.00018768678,0.9083717,0.07176136,0.0012929549,0.00056979986,0.007904758],"study_design_scores_gemma":[0.000054101438,0.0002381176,0.005094404,0.000006274323,0.000010873695,0.000047429894,0.000080475176,0.98371094,0.010346194,0.000074530646,0.00032455166,0.0000119697825],"about_ca_topic_score_codex":0.011108878,"about_ca_topic_score_gemma":0.005669978,"teacher_disagreement_score":0.011108878,"about_ca_system_score_codex":0.00038721986,"about_ca_system_score_gemma":0.0004281511,"threshold_uncertainty_score":0.022088408},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.96536547,0.00017300925,0.01779721,0.00039194117,0.00011971459,0.000080960766,0.0008495179,0.00019692925,0.015025279],"genre_scores_gemma":[0.99260265,0.00005734539,0.004281268,0.000051900657,0.000010335335,0.0000455394,0.00051856507,0.00002615774,0.0024063145],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99984884,0.000029547635,0.000006134747,0.000024636276,0.000051338673,0.000039455106],"domain_scores_gemma":[0.9995459,0.00024061327,0.000034025445,0.00002634531,0.00009727627,0.000055864257],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000310274,0.00054329593,0.00053485675,0.00039359418,0.0006471302,0.0010498806,0.00074720505,0.0014806759,0.0027803618],"category_scores_gemma":[0.0010393575,0.0002425254,0.00084935693,0.00027479112,0.0006699644,0.0004346334,0.0006490237,0.0008094569,0.00033802824],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00009118951,0.00006410931,0.0030409624,0.000032318927,0.000011770356,0.0001464679,0.000029587287,0.9930488,0.0014310698,0.00036052737,0.0003292242,0.001414048],"study_design_scores_gemma":[0.000012235214,0.00004140778,0.0009631928,0.0000049368914,0.0000027216408,0.000013525581,0.000038410457,0.9982223,0.00039272354,0.000084662766,0.00021891411,0.000004981537],"about_ca_topic_score_codex":0.029320331,"about_ca_topic_score_gemma":0.01461026,"teacher_disagreement_score":0.029320331,"about_ca_system_score_codex":0.0006082452,"about_ca_system_score_gemma":0.0009506493,"threshold_uncertainty_score":0.058299303},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9960531,0.00002045196,0.0019479102,0.000024068393,0.000011832883,0.000009747816,0.000053673404,0.000045934525,0.0018331516],"genre_scores_gemma":[0.998917,0.000009196622,0.00066946936,0.000005433542,0.0000014764581,0.000006114527,0.000029672909,0.000005617913,0.00035619971],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99989545,0.000015350102,0.000004081687,0.000015461645,0.000034092343,0.000035588768],"domain_scores_gemma":[0.99964845,0.0001517728,0.000048842663,0.000026520953,0.000064888125,0.000059436155],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016956493,0.00031476098,0.00037048143,0.0002818123,0.0003788141,0.0004717123,0.00048852933,0.00057021383,0.0015812486],"category_scores_gemma":[0.00077391317,0.00017295407,0.0002451976,0.00016303135,0.00066355563,0.00024804912,0.00041825746,0.0003901136,0.00011962048],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0004014092,0.00026868656,0.0075213434,0.00006829109,0.000022071212,0.0003186481,0.00013687524,0.9618382,0.024817262,0.0011337724,0.00021348184,0.0032599345],"study_design_scores_gemma":[0.00005921964,0.00015679025,0.0020484421,0.000004561301,0.000005804569,0.000021665952,0.000035556954,0.99181163,0.005625689,0.00008244863,0.00013869787,0.000009365646],"about_ca_topic_score_codex":0.008349483,"about_ca_topic_score_gemma":0.0037566433,"teacher_disagreement_score":0.008349483,"about_ca_system_score_codex":0.0005485216,"about_ca_system_score_gemma":0.00043187663,"threshold_uncertainty_score":0.016601741},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98499876,0.00006960973,0.009679463,0.00008894173,0.00003627909,0.00002011079,0.000037350193,0.00007819658,0.0049912324],"genre_scores_gemma":[0.9985808,0.000010415128,0.0005972011,0.000007730489,0.0000035962119,0.000005855454,0.000020648165,0.000006152648,0.0007677196],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999132,0.000014648212,0.0000027849255,0.000016108115,0.000033227934,0.000020007683],"domain_scores_gemma":[0.99960965,0.000148301,0.000035920002,0.00001630346,0.0001063396,0.000083564075],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024870672,0.00040316358,0.00027130407,0.00027980306,0.0003933494,0.00053372944,0.00038021803,0.0007346069,0.0012849481],"category_scores_gemma":[0.00091677613,0.00015192869,0.00023400906,0.000093822004,0.0007770405,0.00041850697,0.0003228804,0.00043594258,0.00016590253],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0003668307,0.00015949199,0.0030157208,0.00006488979,0.000020737825,0.00028521297,0.00012379409,0.96103793,0.029548127,0.002495605,0.00032021673,0.0025614733],"study_design_scores_gemma":[0.000030324536,0.0000755878,0.0005362974,0.0000025170043,0.0000031294167,0.00001207616,0.0000139901795,0.9965268,0.00257858,0.00011883808,0.00009665384,0.000005243957],"about_ca_topic_score_codex":0.007164247,"about_ca_topic_score_gemma":0.0018461515,"teacher_disagreement_score":0.007164247,"about_ca_system_score_codex":0.0006188104,"about_ca_system_score_gemma":0.0004234653,"threshold_uncertainty_score":0.014245093},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8501437,0.00019839175,0.13450272,0.0002463364,0.000037869508,0.00004651024,0.00017178318,0.00036704823,0.014285712],"genre_scores_gemma":[0.970159,0.000056852943,0.02688714,0.000032330558,0.000008447776,0.000044594606,0.00015676058,0.00008454914,0.002570209],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999918,0.00001649519,0.00000254666,0.000009319614,0.000034504534,0.000019193223],"domain_scores_gemma":[0.9998005,0.00007364356,0.000027163693,0.00001582223,0.00006221034,0.000020634132],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00032666366,0.00039610665,0.00043832295,0.00036176693,0.00028676083,0.00052145857,0.00035528597,0.0006255753,0.0015231523],"category_scores_gemma":[0.00062279776,0.0001654979,0.00026125257,0.00018032882,0.00041718752,0.00038541752,0.00040498172,0.00028951038,0.00026611204],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00030854452,0.00016694177,0.002048489,0.0001162737,0.000021639986,0.00021149757,0.00008719443,0.9150466,0.059284057,0.003542102,0.00066736725,0.018499365],"study_design_scores_gemma":[0.000026386797,0.00006226589,0.00087530527,0.000004736435,0.0000034224431,0.00003972374,0.000025732343,0.98972076,0.008337169,0.00051376934,0.00038318528,0.0000075303983],"about_ca_topic_score_codex":0.0015414174,"about_ca_topic_score_gemma":0.0010345194,"teacher_disagreement_score":0.0015414174,"about_ca_system_score_codex":0.00030637975,"about_ca_system_score_gemma":0.00044483767,"threshold_uncertainty_score":0.005095482},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9766816,0.0001052439,0.013647281,0.0002369045,0.00006301468,0.00006109759,0.00037254352,0.00033659363,0.008495725],"genre_scores_gemma":[0.9957761,0.000015912687,0.0028398943,0.000023905824,0.0000044062367,0.000034606182,0.00013507016,0.000033867294,0.0011362497],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999021,0.00002364611,0.000005215168,0.0000151302465,0.00002662173,0.000027301616],"domain_scores_gemma":[0.9994062,0.000314524,0.000054435204,0.00003748509,0.000115105766,0.00007222573],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00035484342,0.0004220009,0.00044488898,0.00031532894,0.0005350484,0.000658688,0.00067498477,0.0013344504,0.0029334314],"category_scores_gemma":[0.0011482527,0.00027459784,0.00041420455,0.000272062,0.0005182405,0.00042431024,0.0004075292,0.00060778594,0.000215567],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00016267766,0.00015041867,0.0050240816,0.000048685502,0.00004250744,0.0002319574,0.00006978234,0.9869912,0.003861248,0.0009252693,0.00050102035,0.0019911735],"study_design_scores_gemma":[0.000015453032,0.000023190405,0.0007031284,0.0000027270344,0.000002702558,0.0000050569456,0.000019037396,0.9985726,0.00041130857,0.00008849299,0.00015210315,0.0000042262764],"about_ca_topic_score_codex":0.013642717,"about_ca_topic_score_gemma":0.009199599,"teacher_disagreement_score":0.013642717,"about_ca_system_score_codex":0.00062910235,"about_ca_system_score_gemma":0.00067439454,"threshold_uncertainty_score":0.02712661},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9913668,0.000016672418,0.005601366,0.0000275976,0.000009864648,0.00002391254,0.00008813026,0.00009493649,0.002770785],"genre_scores_gemma":[0.99774086,0.0000061510273,0.0017639551,0.000006559747,0.0000015929122,0.000011756387,0.000065743676,0.000012869329,0.0003906413],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999907,0.000015493382,0.000003821293,0.000009559881,0.000031735224,0.000032405867],"domain_scores_gemma":[0.999658,0.00015201356,0.00004160233,0.000024786626,0.000070588045,0.000053044107],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023135045,0.00034900897,0.0003895706,0.00027661378,0.0004293748,0.00047444913,0.00056712324,0.0006691827,0.0014632834],"category_scores_gemma":[0.00070568564,0.00016959112,0.0003137313,0.00015154194,0.0004645324,0.0002889798,0.0002970967,0.00037334513,0.00011217578],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0002165004,0.00014616048,0.004473753,0.000040097693,0.00002485585,0.00021622288,0.00007415506,0.9782405,0.012838692,0.0007329312,0.00021022135,0.0027858305],"study_design_scores_gemma":[0.000016566479,0.000038746417,0.0008710556,0.000002273408,0.000002402863,0.000007031499,0.000016713664,0.99658585,0.0023268235,0.00004593311,0.00008275454,0.0000038051153],"about_ca_topic_score_codex":0.012750313,"about_ca_topic_score_gemma":0.007052173,"teacher_disagreement_score":0.012750313,"about_ca_system_score_codex":0.0005603945,"about_ca_system_score_gemma":0.0007502836,"threshold_uncertainty_score":0.02535224},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9947507,0.000115581184,0.0046063964,0.000012993178,0.000021762942,0.000016114756,0.000023699136,0.000045211724,0.00040754772],"genre_scores_gemma":[0.99532926,0.00013483418,0.0035847363,0.000021169679,0.000007875889,0.000017178425,0.00005986061,0.00001808271,0.0008270578],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99943024,0.000060725248,0.00004080218,0.00012917166,0.00024066713,0.00009837401],"domain_scores_gemma":[0.9993388,0.00018886235,0.00021721842,0.00004959527,0.00013585406,0.00006968594],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004934119,0.00044397768,0.00036243524,0.00026313143,0.00017968072,0.0005385551,0.00044242278,0.0004125414,0.0009338106],"category_scores_gemma":[0.0010537128,0.00017020787,0.00019958332,0.0001937718,0.0004701418,0.00047450702,0.0008984392,0.0002962431,0.00014535441],"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":[0.0004516024,0.00008392801,0.0018991018,0.00009232319,0.0000058262026,0.00015931204,0.000085913474,0.0009978396,0.99135196,0.00011503149,0.000037494643,0.004719736],"study_design_scores_gemma":[0.000023197854,0.0024702586,0.010996389,0.000014642903,0.000023177421,0.00017493758,0.00011993361,0.004858289,0.9802664,0.000035962035,0.0009940906,0.000022702874],"about_ca_topic_score_codex":0.00042567842,"about_ca_topic_score_gemma":0.00054470886,"teacher_disagreement_score":0.0009338106,"about_ca_system_score_codex":0.0003065112,"about_ca_system_score_gemma":0.00023518133,"threshold_uncertainty_score":0.0031238794},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.4769257,0.00060254603,0.5125898,0.00017436445,0.000104861494,0.00008407452,0.000091756585,0.00013565064,0.009291224],"genre_scores_gemma":[0.9761411,0.00025011378,0.019349935,0.000023735747,0.000023942062,0.000031154883,0.000048655053,0.00001609586,0.0041152663],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99993837,0.000015985359,0.0000034511206,0.000013166704,0.000021729267,0.0000073777273],"domain_scores_gemma":[0.99992824,0.000024923003,0.00001394626,0.000007614247,0.000019506846,0.0000057833295],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015974672,0.0005880323,0.0002910541,0.00022916144,0.0002581612,0.00047330605,0.00034899462,0.0005527863,0.0005912568],"category_scores_gemma":[0.0003278074,0.000103827675,0.0004050991,0.00014981354,0.00032038684,0.0003748435,0.00044801185,0.000337036,0.00009619043],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000049826933,0.000048140242,0.0038393599,0.00007133595,0.000026259402,0.00037266244,0.00009519305,0.9331493,0.03946536,0.00998189,0.00018792565,0.012712673],"study_design_scores_gemma":[0.0000013695175,0.000018255741,0.00047694694,0.0000022958911,0.000003428203,0.000022730712,0.000007962013,0.997142,0.0016187393,0.00044219656,0.00026106922,0.0000029924026],"about_ca_topic_score_codex":0.0047416426,"about_ca_topic_score_gemma":0.0036122047,"teacher_disagreement_score":0.0047416426,"about_ca_system_score_codex":0.00026546128,"about_ca_system_score_gemma":0.00034334927,"threshold_uncertainty_score":0.009428084},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9601871,0.00012266182,0.037070625,0.00004483936,0.000022715616,0.000028091,0.000072080016,0.00028222887,0.002169746],"genre_scores_gemma":[0.99808717,0.000013302433,0.0015391968,0.000005078042,0.000002631179,0.000012035089,0.000041423144,0.000025007179,0.0002741669],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995566,0.00010769466,0.0000141265455,0.000068736575,0.00017802611,0.00007470228],"domain_scores_gemma":[0.9986223,0.0007244416,0.00011459986,0.00009795442,0.00031777908,0.00012289893],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003502616,0.0006777014,0.0005788289,0.0007660876,0.00047578922,0.00059715775,0.0005892113,0.0008766568,0.001665698],"category_scores_gemma":[0.0013988734,0.0002662978,0.0003205769,0.0003003299,0.0005712332,0.0005035966,0.0005514128,0.00036334596,0.00028681743],"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":[0.007416655,0.00073076575,0.024941515,0.000539186,0.00010057219,0.0020477287,0.0011858965,0.18708438,0.7218112,0.0026484446,0.00070454145,0.050789166],"study_design_scores_gemma":[0.00015683695,0.0014599398,0.047998864,0.000074468895,0.000074938594,0.0011445197,0.0005164814,0.7007171,0.24556838,0.0013764959,0.0008092986,0.00010266049],"about_ca_topic_score_codex":0.00045018186,"about_ca_topic_score_gemma":0.00040172914,"teacher_disagreement_score":0.001665698,"about_ca_system_score_codex":0.0002363658,"about_ca_system_score_gemma":0.00019229863,"threshold_uncertainty_score":0.0055723786},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9925816,0.00019793508,0.0055358205,0.000027910828,0.0000103309185,0.000008466111,0.000016832504,0.00007513893,0.0015460398],"genre_scores_gemma":[0.9983341,0.00006090663,0.00074295513,0.000006847632,0.0000030668375,0.000004183878,0.000008996066,0.000009970356,0.0008290477],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998586,0.000023260787,0.0000043242535,0.00003142853,0.00004483604,0.00003756208],"domain_scores_gemma":[0.9992786,0.00032622338,0.00022027535,0.000054544285,0.00007855538,0.000041873995],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023318522,0.00032396265,0.00025365286,0.00038197552,0.0002276987,0.00040749542,0.00030213286,0.00040955676,0.0013358078],"category_scores_gemma":[0.0011491687,0.00020848891,0.00016508937,0.00014749434,0.00081077934,0.00056834373,0.00042219527,0.0002388314,0.00025000886],"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":[0.0004507202,0.000047461814,0.0016900767,0.000119031334,0.000019963742,0.00049941806,0.0003897838,0.013880916,0.97281104,0.0043302146,0.00012845587,0.005632972],"study_design_scores_gemma":[0.000089514986,0.0012450994,0.013661453,0.000051728504,0.000046685505,0.0011167174,0.00030373855,0.3258803,0.65104735,0.004097779,0.002386331,0.00007334385],"about_ca_topic_score_codex":0.00032518865,"about_ca_topic_score_gemma":0.00016587453,"teacher_disagreement_score":0.0013358078,"about_ca_system_score_codex":0.000205241,"about_ca_system_score_gemma":0.000093209106,"threshold_uncertainty_score":0.0044686794},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.020573853,0.00027789446,0.9781677,0.00009544991,0.000039309012,0.000025821553,0.00005218665,0.00029518752,0.00047248817],"genre_scores_gemma":[0.3124511,0.00039137976,0.6838892,0.00011709858,0.00008360897,0.00008732238,0.00045483012,0.00014717838,0.0023783376],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995127,0.00019510431,0.000021151556,0.00010251608,0.00012571654,0.000042737385],"domain_scores_gemma":[0.9985649,0.0010124246,0.000116341806,0.000074068164,0.00020331902,0.000029009605],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.001194883,0.0012286222,0.00068588444,0.0008111274,0.00045752234,0.0005658385,0.0005368147,0.0009818167,0.0014117131],"category_scores_gemma":[0.0036057576,0.00031485013,0.0011624658,0.00042296323,0.00052430766,0.0009446537,0.00056040596,0.001062445,0.00063872983],"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":[0.0007809107,0.00021340982,0.001609427,0.00036593797,0.00022192973,0.0003888226,0.00035651762,0.396324,0.09633559,0.0077523207,0.0030992,0.4925519],"study_design_scores_gemma":[0.000020543439,0.000055488505,0.0009222376,0.00001690257,0.000018636747,0.00011148273,0.000038502276,0.98368925,0.010181051,0.0034403852,0.0014799312,0.000025694953],"about_ca_topic_score_codex":0.0040556667,"about_ca_topic_score_gemma":0.006141982,"teacher_disagreement_score":0.0040556667,"about_ca_system_score_codex":0.00034316324,"about_ca_system_score_gemma":0.00076738745,"threshold_uncertainty_score":0.008064151},"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":"methods","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.038654886,0.00036365443,0.94059443,0.00017887837,0.00009955075,0.00007545248,0.00009629714,0.00031632697,0.01962037],"genre_scores_gemma":[0.8138298,0.0006529418,0.15874851,0.00020306496,0.00008040414,0.00014158344,0.00022880208,0.00018370498,0.025931198],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998412,0.000030615403,0.000005777909,0.000023157947,0.000083837374,0.000015446449],"domain_scores_gemma":[0.9997749,0.00007729949,0.000053930664,0.000029995728,0.000050856655,0.000012934116],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024381727,0.0004217431,0.0002786166,0.00021096409,0.00020827177,0.0006442923,0.0009055643,0.00072031544,0.001562336],"category_scores_gemma":[0.0006966661,0.00026801098,0.00050295336,0.00013807557,0.00058442034,0.0007444396,0.0004440315,0.0007914282,0.00051963486],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00006973774,0.00008121095,0.00092296925,0.00014668202,0.00002201875,0.00068864564,0.00029412433,0.83562493,0.063405715,0.081416756,0.0019894133,0.015337719],"study_design_scores_gemma":[0.000007016275,0.00002340972,0.00013467202,0.0000054203456,0.000003030964,0.0001476946,0.00001698636,0.9928778,0.0019004128,0.002814629,0.0020624439,0.0000064496007],"about_ca_topic_score_codex":0.0010921395,"about_ca_topic_score_gemma":0.000777914,"teacher_disagreement_score":0.001562336,"about_ca_system_score_codex":0.0004123014,"about_ca_system_score_gemma":0.0005210983,"threshold_uncertainty_score":0.005226493},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.88364154,0.00042633005,0.11124715,0.00010284867,0.00007642452,0.000055806195,0.00019120997,0.000527334,0.003731346],"genre_scores_gemma":[0.97782487,0.00008799269,0.021324655,0.000019709049,0.0000071335576,0.00001942102,0.00014101288,0.00003962058,0.00053561263],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995721,0.00008627925,0.000029953344,0.00005283473,0.00019783805,0.0000611153],"domain_scores_gemma":[0.9979291,0.0010926098,0.00031681676,0.00024189561,0.0003032529,0.00011638555],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0009917794,0.0004884632,0.00040880838,0.00039686507,0.0004326016,0.00081577396,0.00061523786,0.0007424566,0.0013112812],"category_scores_gemma":[0.0031633887,0.00030721366,0.00050186843,0.00024633546,0.0005178657,0.0008582011,0.0007406383,0.0007096271,0.00023822012],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00042935341,0.00027309707,0.025840996,0.00025632765,0.000057638892,0.00061885436,0.00027268144,0.8612252,0.05238612,0.0014180903,0.00054975034,0.0566719],"study_design_scores_gemma":[0.000020085237,0.00022026934,0.005356258,0.000025840942,0.0000119712295,0.000113233764,0.00005979339,0.98129225,0.012175478,0.00013135222,0.00057117344,0.000022348142],"about_ca_topic_score_codex":0.0042626164,"about_ca_topic_score_gemma":0.0046668546,"teacher_disagreement_score":0.0042626164,"about_ca_system_score_codex":0.00031242543,"about_ca_system_score_gemma":0.0004978803,"threshold_uncertainty_score":0.008475602},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0018699511,0.000059557897,0.9962076,0.00007896071,0.00002062931,0.00002319982,0.000047517853,0.000116900424,0.0015757451],"genre_scores_gemma":[0.59996593,0.0008026994,0.38635582,0.00019131498,0.0002433535,0.0006044411,0.0008031451,0.0002453128,0.010787959],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99870324,0.00040667012,0.000057847265,0.00023488568,0.0004501767,0.00014717819],"domain_scores_gemma":[0.99862003,0.0006042687,0.00016622606,0.00007719452,0.00046213073,0.00007021935],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.002265391,0.0010723369,0.00080335943,0.0010490977,0.0006173589,0.0014452608,0.0021007534,0.00109004,0.0032929403],"category_scores_gemma":[0.005295763,0.00049891026,0.0012256993,0.0007876479,0.00076592807,0.0016661873,0.002111607,0.0014839104,0.0006779714],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000020611657,0.000027204454,0.0007759276,0.00004426931,0.000023275086,0.00006978801,0.00006562601,0.9348409,0.00079162844,0.045849945,0.0009050903,0.016585762],"study_design_scores_gemma":[0.000001934584,0.000010892227,0.00009925467,0.000006750334,0.000005712447,0.000011698912,0.000015953288,0.99174833,0.0001594998,0.007149888,0.0007831335,0.0000069484645],"about_ca_topic_score_codex":0.024376953,"about_ca_topic_score_gemma":0.013924047,"teacher_disagreement_score":0.024376953,"about_ca_system_score_codex":0.0015262621,"about_ca_system_score_gemma":0.0022725856,"threshold_uncertainty_score":0.04847014},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9969823,0.00006858492,0.0025263997,0.000012340843,0.000010356158,0.000007057876,0.000025876412,0.00003545481,0.0003315603],"genre_scores_gemma":[0.9975712,0.00003868761,0.0020345054,0.0000029532537,0.0000048446223,0.000007699003,0.000019390132,0.000005137815,0.0003155828],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9996517,0.0000610908,0.000017051178,0.000060632967,0.00013458607,0.00007505488],"domain_scores_gemma":[0.99873275,0.0006372332,0.00022787554,0.00013903806,0.00014649915,0.00011666204],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005212218,0.00032083463,0.00034705584,0.0002955167,0.00025662643,0.00020651007,0.00045734993,0.00054862304,0.0011380126],"category_scores_gemma":[0.0010362451,0.00021543691,0.000257806,0.0002505527,0.000830405,0.0002962188,0.0005968007,0.00044232258,0.000105986794],"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":[0.00055193674,0.00031071308,0.0032154864,0.00014891013,0.000018453533,0.00052122417,0.0002728217,0.012540304,0.9775122,0.0003939411,0.00007112372,0.0044428906],"study_design_scores_gemma":[0.00010049085,0.0043303855,0.026003968,0.000027068756,0.00005687092,0.0004770057,0.0003303246,0.079753734,0.8876589,0.00021356119,0.0009957062,0.000051977488],"about_ca_topic_score_codex":0.00039043408,"about_ca_topic_score_gemma":0.00037832526,"teacher_disagreement_score":0.0011380126,"about_ca_system_score_codex":0.00017598688,"about_ca_system_score_gemma":0.00014168359,"threshold_uncertainty_score":0.0038070083},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.80020076,0.0002409454,0.18756418,0.00030971892,0.00014752749,0.000049010625,0.00004481054,0.00039703367,0.011045944],"genre_scores_gemma":[0.99345326,0.00008467208,0.0051929974,0.00003165356,0.000020208281,0.0000149742,0.000013088985,0.000019095083,0.0011699483],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999052,0.000026014028,0.000004187434,0.000017819988,0.00003070649,0.00001606016],"domain_scores_gemma":[0.99982125,0.00006163949,0.000050193674,0.000020973224,0.000026272419,0.000019803],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017026206,0.00040785765,0.000259265,0.00022316046,0.00023671468,0.0006092974,0.00049042574,0.0004215757,0.00058840995],"category_scores_gemma":[0.0009594264,0.00022608187,0.0002040955,0.00013678269,0.00097587844,0.0007910357,0.0005670081,0.00047828446,0.00007832936],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00023035347,0.0001308197,0.002700096,0.00010104577,0.000034055545,0.0006417732,0.00021861946,0.68680245,0.20819771,0.08358157,0.0005916218,0.01676986],"study_design_scores_gemma":[0.000010527407,0.000021055848,0.00044830254,0.0000018249665,0.0000025413428,0.000016446533,0.000007934849,0.9934776,0.004227263,0.0016360455,0.0001443929,0.0000059722047],"about_ca_topic_score_codex":0.001749061,"about_ca_topic_score_gemma":0.0007300413,"teacher_disagreement_score":0.001749061,"about_ca_system_score_codex":0.00045859392,"about_ca_system_score_gemma":0.00048921665,"threshold_uncertainty_score":0.0034776926},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9909601,0.00043830622,0.007678284,0.000033259068,0.000014983217,0.00001281717,0.000052987154,0.00006185823,0.00074738014],"genre_scores_gemma":[0.995452,0.00021414194,0.0037897686,0.000020318073,0.000007915008,0.00001195207,0.00008074556,0.0000124578055,0.00041071652],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99991715,0.000005961187,0.000003482934,0.000016901362,0.000042989323,0.000013511101],"domain_scores_gemma":[0.9998647,0.000036258098,0.000031468913,0.000009272751,0.00003895922,0.000019300176],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012078408,0.00017319235,0.00018574641,0.00022202142,0.00015713167,0.00029487698,0.00016684516,0.00019618995,0.00032413102],"category_scores_gemma":[0.00024864628,0.000106480846,0.000153593,0.00018695378,0.00027739658,0.00024384564,0.0001822253,0.00020148695,0.00006427135],"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":[0.00008025215,0.000021269409,0.002435167,0.00004947583,0.0000062579134,0.00020479994,0.00007942755,0.00034831217,0.9916646,0.0002310518,0.00006298259,0.004816351],"study_design_scores_gemma":[0.00004241556,0.00045326224,0.045895368,0.000014881042,0.000027136122,0.0007144999,0.00021975617,0.027588496,0.9226032,0.0003310497,0.0020820636,0.000027883283],"about_ca_topic_score_codex":0.0003444333,"about_ca_topic_score_gemma":0.00020767529,"teacher_disagreement_score":0.0003444333,"about_ca_system_score_codex":0.00017918629,"about_ca_system_score_gemma":0.00012681984,"threshold_uncertainty_score":0.0013000965},"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":"review","genre_gemma":"review","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"review","genre_consensus":"review","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0008641317,0.98584807,0.0052218665,0.0007562273,0.0024349806,0.000012032659,0.00011658233,0.00006424732,0.004681922],"genre_scores_gemma":[0.00707828,0.9811451,0.0018430799,0.0007354546,0.0039014353,0.000026542892,0.00034200412,0.000054443834,0.0048737326],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.99938655,0.00010343585,0.000079742036,0.00012796372,0.00026114608,0.00004122217],"domain_scores_gemma":[0.9977817,0.0010613421,0.00013969997,0.00007311072,0.00086401496,0.00008019326],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0011144786,0.0010624906,0.001216037,0.0024991422,0.00037817235,0.001266693,0.0012019342,0.0012503094,0.0061518284],"category_scores_gemma":[0.0026179051,0.00045168982,0.00068364537,0.0020965692,0.00043616784,0.0018440271,0.00085373485,0.0013705428,0.0048357276],"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":[0.00011798074,0.00009569874,0.00057067134,0.017583396,0.00012429596,0.00024765002,0.000112992544,0.005064716,0.002995177,0.010848904,0.063855805,0.8983827],"study_design_scores_gemma":[0.0000078591975,0.00022979686,0.0017845,0.004965781,0.00014083672,0.0011280028,0.000084101615,0.002000807,0.0025131812,0.005148725,0.9819218,0.000074608804],"about_ca_topic_score_codex":0.001026502,"about_ca_topic_score_gemma":0.0007990086,"teacher_disagreement_score":0.0061518284,"about_ca_system_score_codex":0.0005484818,"about_ca_system_score_gemma":0.0013460348,"threshold_uncertainty_score":0.020579934},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99767536,0.00009981148,0.001923692,0.000010168961,0.000015782141,0.000007239358,0.0000120336335,0.000023485447,0.00023237248],"genre_scores_gemma":[0.99905187,0.00005084499,0.00074045936,0.0000049839523,0.000004089694,0.000005103053,0.00002633696,0.000008728001,0.00010764069],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995671,0.00005390557,0.000033909128,0.00008140989,0.00015098696,0.000112655274],"domain_scores_gemma":[0.99889696,0.00040140035,0.00027492084,0.00008675537,0.000090152396,0.0002497817],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004853364,0.0004996798,0.0005953333,0.00039661545,0.0005491417,0.0009623239,0.00020746273,0.00022228238,0.00074954034],"category_scores_gemma":[0.0015083137,0.00026521005,0.000322669,0.00021872202,0.0009369004,0.000760911,0.0011635515,0.0005370851,0.000058013986],"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":[0.0013706794,0.00009605103,0.0054608188,0.00006726386,0.000025303674,0.00037867238,0.00017064586,0.007900637,0.9783775,0.000824388,0.000035812904,0.005292219],"study_design_scores_gemma":[0.00008974736,0.0012678872,0.030122185,0.000015071314,0.000059932023,0.0003146797,0.00014342353,0.0640397,0.90263426,0.00051082677,0.00074973964,0.00005255396],"about_ca_topic_score_codex":0.0003458043,"about_ca_topic_score_gemma":0.00025841928,"teacher_disagreement_score":0.0009623239,"about_ca_system_score_codex":0.00037524538,"about_ca_system_score_gemma":0.0003654738,"threshold_uncertainty_score":0.0027225614},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.09307828,0.002312222,0.86953866,0.00036310536,0.0003142301,0.00016571386,0.00024318714,0.0005546941,0.033429954],"genre_scores_gemma":[0.83181864,0.0025378335,0.14565668,0.00015024298,0.00010776559,0.00017932717,0.0002717533,0.00010969433,0.01916806],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99976045,0.0000380158,0.000014022519,0.000052610158,0.000101862744,0.000032992717],"domain_scores_gemma":[0.99978536,0.00009099146,0.000025589237,0.00001668656,0.00007103181,0.000010269286],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00031912114,0.0005499473,0.000622582,0.00068182126,0.00046203745,0.0012159587,0.00072652387,0.0015583305,0.0026454434],"category_scores_gemma":[0.0007039295,0.00028960366,0.00087009545,0.00042930586,0.00051273784,0.0006035353,0.0004988173,0.0004756616,0.00064699113],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00008472196,0.000100927726,0.0025170262,0.0002445706,0.000029194114,0.00071341795,0.00017722762,0.8403638,0.08531754,0.018943446,0.0013427738,0.0501653],"study_design_scores_gemma":[0.000006151015,0.000043384392,0.0006192874,0.000014518805,0.0000056963595,0.00012014614,0.00003346503,0.9913633,0.0038470768,0.0011665733,0.0027610732,0.000019313367],"about_ca_topic_score_codex":0.0028832546,"about_ca_topic_score_gemma":0.0013181085,"teacher_disagreement_score":0.0028832546,"about_ca_system_score_codex":0.00052287383,"about_ca_system_score_gemma":0.00081146375,"threshold_uncertainty_score":0.008849859},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9767237,0.0002587671,0.017977118,0.000044188757,0.000041978798,0.00001395959,0.00022501723,0.00046968987,0.004245573],"genre_scores_gemma":[0.9982632,0.000043053456,0.0012313261,0.000005548611,0.0000045017573,0.000006451429,0.0000581212,0.000041746476,0.00034622234],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999498,0.00014774593,0.000019990166,0.0000849486,0.00015253143,0.00009681239],"domain_scores_gemma":[0.99590474,0.0029917168,0.00020644184,0.00033417897,0.00047336062,0.00008958189],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00059295516,0.0006497125,0.0007312594,0.0006723929,0.00037189986,0.0005079873,0.00051615835,0.00108006,0.0021959643],"category_scores_gemma":[0.004111942,0.00045881447,0.0004812394,0.0005398268,0.0006208618,0.00048251456,0.0005485213,0.0004906544,0.00043437307],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0013832821,0.000199728,0.0070168516,0.00031353044,0.000041925312,0.0003043865,0.00012323253,0.9289377,0.045473635,0.0006383946,0.0005159071,0.015051429],"study_design_scores_gemma":[0.000057984456,0.0004980301,0.020573711,0.00003531576,0.000106126005,0.00011322736,0.000059895017,0.9352861,0.04252704,0.00018088677,0.0005034739,0.00005819619],"about_ca_topic_score_codex":0.002650565,"about_ca_topic_score_gemma":0.0015877192,"teacher_disagreement_score":0.002650565,"about_ca_system_score_codex":0.00040512357,"about_ca_system_score_gemma":0.0001969768,"threshold_uncertainty_score":0.007346213},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.91257304,0.00022643656,0.07111895,0.0001641574,0.000069819405,0.00006419724,0.0004085636,0.0004886652,0.014886202],"genre_scores_gemma":[0.98859745,0.000118014985,0.008893326,0.000016106917,0.000007733344,0.000047387657,0.0002394799,0.000027891609,0.0020525963],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998919,0.000024369561,0.0000065719582,0.0000150391315,0.00003614488,0.00002597897],"domain_scores_gemma":[0.9996125,0.00021252339,0.000042761512,0.000028383427,0.00006460799,0.000039212562],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00019695803,0.0003320682,0.0004831522,0.0003653416,0.00035138903,0.000615796,0.00069343526,0.00072004506,0.0018468642],"category_scores_gemma":[0.0007646923,0.0001922299,0.0004094127,0.00044209394,0.00051197817,0.00038020388,0.0003809582,0.00049390853,0.00012712326],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000081832055,0.00004868804,0.0014705776,0.000035227364,0.000013797076,0.00015494438,0.000059898568,0.988715,0.004590579,0.0019767764,0.00018847678,0.002664227],"study_design_scores_gemma":[0.0000074966642,0.000024878598,0.00045963013,0.0000018900582,0.0000026245139,0.000012433812,0.000009862199,0.99822754,0.0008931794,0.00017916024,0.00017806276,0.0000031883467],"about_ca_topic_score_codex":0.007313927,"about_ca_topic_score_gemma":0.003260662,"teacher_disagreement_score":0.007313927,"about_ca_system_score_codex":0.00044514838,"about_ca_system_score_gemma":0.0006206654,"threshold_uncertainty_score":0.014542758},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98818064,0.0001347853,0.009642598,0.00004143991,0.000027470996,0.000013156728,0.000051550185,0.000053745654,0.001854701],"genre_scores_gemma":[0.99518895,0.0001056294,0.0037704401,0.000014397588,0.0000033664712,0.000008434341,0.000034503413,0.0000069136663,0.0008674903],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99992466,0.000007540412,0.0000035749604,0.000013111502,0.000041668623,0.000009399483],"domain_scores_gemma":[0.99984133,0.000053052972,0.000026670248,0.00001636535,0.000047841044,0.0000147532555],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001312803,0.00018000242,0.00015212134,0.00014916711,0.00011848626,0.0001594135,0.00013031185,0.00027742673,0.00064614386],"category_scores_gemma":[0.00019790717,0.00008299506,0.00013738136,0.00010648409,0.00029185633,0.0001534933,0.00013266201,0.00020695281,0.00013708575],"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":[0.00009143458,0.000045406072,0.0010712274,0.00005371288,0.000004376221,0.0005865214,0.00008105416,0.0054312977,0.9868145,0.00032358925,0.00010439728,0.00539254],"study_design_scores_gemma":[0.000033839355,0.0019805043,0.022984384,0.000026530359,0.00002195213,0.0010570599,0.00035571968,0.113626696,0.85521334,0.00049723487,0.004158775,0.000043950447],"about_ca_topic_score_codex":0.00022095624,"about_ca_topic_score_gemma":0.00032881176,"teacher_disagreement_score":0.00064614386,"about_ca_system_score_codex":0.0000768774,"about_ca_system_score_gemma":0.00008424471,"threshold_uncertainty_score":0.0021615624},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.47799176,0.00026962944,0.5089326,0.00019173438,0.000045309014,0.000054333443,0.00004379747,0.0004812476,0.011989572],"genre_scores_gemma":[0.9326228,0.00008027995,0.06603765,0.000029512987,0.000009642845,0.00003900912,0.00003693661,0.000051726016,0.0010923796],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998375,0.000029071518,0.000004477606,0.00001990443,0.00008352487,0.000025421617],"domain_scores_gemma":[0.9996729,0.00016124969,0.000050988216,0.000028021585,0.00006659662,0.000020220315],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003801276,0.00052347075,0.000408232,0.00024623802,0.00021803596,0.00050441164,0.00037305107,0.00044149696,0.00062324275],"category_scores_gemma":[0.0008914558,0.00016716667,0.00032853478,0.00012356248,0.0004850481,0.0003966525,0.00039729528,0.0003513468,0.0001577911],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00016809787,0.00014868521,0.0013151993,0.0000983475,0.000017580513,0.0001550371,0.00007458644,0.86060464,0.10149725,0.0057586846,0.0003099933,0.029851904],"study_design_scores_gemma":[0.000017875389,0.000119661076,0.0003275377,0.0000044666917,0.0000037011355,0.00003205381,0.000014202632,0.98256934,0.015712766,0.00077301264,0.00041740693,0.000007957918],"about_ca_topic_score_codex":0.0007699802,"about_ca_topic_score_gemma":0.0007280153,"teacher_disagreement_score":0.0007699802,"about_ca_system_score_codex":0.00024317767,"about_ca_system_score_gemma":0.00042438877,"threshold_uncertainty_score":0.0020849705},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9928469,0.000017822606,0.0048640333,0.00004379515,0.000010273033,0.000018607328,0.000050843686,0.00007221674,0.0020755106],"genre_scores_gemma":[0.9983303,0.000007868718,0.0012761697,0.0000067618553,0.0000021680848,0.000009966248,0.00004140902,0.000011380044,0.00031407844],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998925,0.0000209132,0.000005019943,0.000012958541,0.00003620686,0.00003243566],"domain_scores_gemma":[0.9994081,0.00031753667,0.000055846067,0.000035052355,0.00011283357,0.00007061321],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00026836334,0.00040357118,0.0004848738,0.00035912413,0.00050745124,0.00048748057,0.0005167565,0.0007741414,0.0009120257],"category_scores_gemma":[0.0009879265,0.0002193634,0.0004445011,0.00018513764,0.00056052406,0.0003462432,0.00033228763,0.0004497103,0.000082018676],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0001390409,0.00009927881,0.005299594,0.000028812592,0.000019511775,0.00019306512,0.00005996716,0.98108727,0.010206373,0.00057788304,0.00011133639,0.002177944],"study_design_scores_gemma":[0.000009886523,0.000022167422,0.0007457698,9.753329e-7,0.0000016280521,0.0000050227322,0.000009244987,0.998237,0.00090100954,0.000037705642,0.000027181288,0.0000025268096],"about_ca_topic_score_codex":0.019175634,"about_ca_topic_score_gemma":0.009507956,"teacher_disagreement_score":0.019175634,"about_ca_system_score_codex":0.0005652474,"about_ca_system_score_gemma":0.0007351026,"threshold_uncertainty_score":0.038128078},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9968066,0.000067346125,0.0025491707,0.000009884999,0.000011323138,0.0000042267675,0.000019042227,0.000021301465,0.00051110616],"genre_scores_gemma":[0.999255,0.000041474024,0.00044577746,0.0000042692664,0.0000025157678,0.0000016438185,0.000014960524,0.0000058465694,0.00022850734],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998462,0.000038159713,0.0000110719475,0.00003333362,0.000040704293,0.000030393705],"domain_scores_gemma":[0.99905044,0.00062520365,0.00007952152,0.000053057334,0.00014747807,0.0000443049],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025071017,0.00030285615,0.00023140009,0.00013117206,0.00017205697,0.00029614763,0.00010293433,0.000207057,0.00096146745],"category_scores_gemma":[0.0010130965,0.0001319891,0.00010252974,0.000060182418,0.00027773317,0.00018359383,0.00018047246,0.00016180988,0.00024109874],"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":[0.0015701229,0.00007489423,0.0075590448,0.00010125798,0.000017919278,0.0005915337,0.00018081597,0.011577239,0.9637305,0.00009190833,0.0000621632,0.01444261],"study_design_scores_gemma":[0.00005886557,0.0034247362,0.053456575,0.000032192493,0.00007441675,0.0005398932,0.00035690345,0.022724174,0.91829014,0.00010478802,0.0008939976,0.00004327109],"about_ca_topic_score_codex":0.0002444928,"about_ca_topic_score_gemma":0.0003906709,"teacher_disagreement_score":0.00096146745,"about_ca_system_score_codex":0.00008061487,"about_ca_system_score_gemma":0.00008190027,"threshold_uncertainty_score":0.0032163858},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6549099,0.000871579,0.32829347,0.0012140063,0.00016870262,0.0002472351,0.00087915786,0.00065130816,0.012764679],"genre_scores_gemma":[0.9929,0.00008858802,0.0056285765,0.000043099728,0.000010945416,0.00004992442,0.00016193201,0.000027965405,0.0010889532],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995784,0.00017326215,0.000019722,0.00007840827,0.00009958635,0.0000505006],"domain_scores_gemma":[0.99708015,0.0022112108,0.00015510438,0.00017536654,0.00032728523,0.000050789375],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0012932424,0.0009525569,0.0006154364,0.00052135123,0.00028040927,0.0006757691,0.00067229324,0.0013968693,0.001667449],"category_scores_gemma":[0.0057420004,0.00033892048,0.0006834457,0.00025463398,0.0006044691,0.0006826323,0.0009838641,0.0014969996,0.00017734375],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000093076655,0.00005049831,0.0009291356,0.00007831251,0.00002092948,0.00008388303,0.000030436067,0.98915803,0.004766486,0.0017603728,0.00026588177,0.0027629277],"study_design_scores_gemma":[0.0000020841333,0.000017149017,0.00015588895,0.000002723199,0.0000020335742,0.0000067343476,0.0000037557033,0.9987232,0.0008416241,0.0001897835,0.00005139652,0.0000035742628],"about_ca_topic_score_codex":0.0062564434,"about_ca_topic_score_gemma":0.0020321936,"teacher_disagreement_score":0.0062564434,"about_ca_system_score_codex":0.00051961927,"about_ca_system_score_gemma":0.00050611416,"threshold_uncertainty_score":0.012440026},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9969644,0.000019926014,0.0025736627,0.000010054885,0.000005515878,0.000019094015,0.000060163267,0.000025992586,0.00032119604],"genre_scores_gemma":[0.99698955,0.000029642271,0.002153997,0.000012999157,0.0000035747817,0.000052260206,0.00010770571,0.0000119628385,0.0006383583],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997534,0.000052916934,0.000014965217,0.00004645685,0.000085492145,0.000046700367],"domain_scores_gemma":[0.999423,0.0001655082,0.000079984406,0.000034120916,0.00020706408,0.00009037587],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006216443,0.00028083468,0.00022056134,0.0002538573,0.00042149192,0.00029450053,0.0002987891,0.0003322376,0.0009084619],"category_scores_gemma":[0.00064711046,0.00010903595,0.0001277062,0.00017100954,0.0004372219,0.00032639282,0.00052833965,0.00038494344,0.00012354163],"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":[0.0006233822,0.0004525181,0.0067830286,0.00006676607,0.000012293358,0.00045525964,0.00070224836,0.0040700794,0.980409,0.00032769958,0.00017266184,0.005925105],"study_design_scores_gemma":[0.00022922133,0.008214186,0.09290473,0.0000549828,0.000054582244,0.00064943533,0.002692633,0.04901258,0.8433975,0.00047281504,0.0022086455,0.00010863425],"about_ca_topic_score_codex":0.0014536821,"about_ca_topic_score_gemma":0.0019808572,"teacher_disagreement_score":0.0014536821,"about_ca_system_score_codex":0.00018163915,"about_ca_system_score_gemma":0.00027691777,"threshold_uncertainty_score":0.0032876134},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9980476,0.000008592189,0.0015991861,0.000009179282,0.0000042564,0.0000049917785,0.000045971494,0.000023462795,0.00025666525],"genre_scores_gemma":[0.99886084,0.000008919311,0.00079891214,0.0000059322506,0.000001716844,0.000009256218,0.00008978851,0.00000663124,0.00021815083],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9996505,0.00008581586,0.000021447091,0.00006421233,0.00012748598,0.00005052741],"domain_scores_gemma":[0.9994293,0.00020551943,0.000049524562,0.00003819243,0.00018694867,0.000090429974],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00082105014,0.00032634553,0.00033645623,0.00035507116,0.0002937154,0.00047403167,0.00038661514,0.0004186061,0.00037089543],"category_scores_gemma":[0.0009982107,0.00011729332,0.00016669554,0.00024175938,0.00047540548,0.00045948985,0.0004637798,0.00028851815,0.0000819337],"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":[0.002844357,0.0008467671,0.06420172,0.00014880711,0.00006551514,0.0013132915,0.0016249777,0.14391102,0.7617356,0.0011413993,0.00047584545,0.021690795],"study_design_scores_gemma":[0.00021293641,0.0034103894,0.1846767,0.00006685291,0.00006740353,0.00047917097,0.0012836432,0.6141507,0.1938001,0.0005261489,0.0011765703,0.0001493651],"about_ca_topic_score_codex":0.004657738,"about_ca_topic_score_gemma":0.0044830376,"teacher_disagreement_score":0.004657738,"about_ca_system_score_codex":0.00025031058,"about_ca_system_score_gemma":0.00024971872,"threshold_uncertainty_score":0.0092612505},"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":"methods","genre_gemma":"methods","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.024022197,0.00018628912,0.974068,0.00019084767,0.000026684087,0.00002795831,0.000088358436,0.0002977065,0.0010920106],"genre_scores_gemma":[0.769765,0.0007860419,0.22282256,0.00016666022,0.00007984671,0.00030262032,0.00051514845,0.00016479146,0.0053973407],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996784,0.00009088416,0.000025332822,0.000081761165,0.000090470465,0.000033117514],"domain_scores_gemma":[0.9989141,0.0007014514,0.000105357525,0.00006855032,0.00019578107,0.000014701459],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0011175367,0.0006218031,0.00050819165,0.0005579386,0.00029552658,0.00075544737,0.0009852645,0.0010041182,0.0008070344],"category_scores_gemma":[0.0038889807,0.00050283084,0.00062103523,0.00052023976,0.00040779097,0.0010107278,0.00044640453,0.0012902176,0.0004914126],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000010504401,0.000029848326,0.0014786397,0.000028576971,0.000016061813,0.000034772183,0.000030172934,0.975493,0.0017383739,0.0030106166,0.00034649324,0.01778286],"study_design_scores_gemma":[5.508693e-7,0.0000035274484,0.0001665143,0.0000023539726,0.0000012214834,0.0000050928793,0.0000018479556,0.99911135,0.00021249706,0.00038922275,0.00010345855,0.0000024001763],"about_ca_topic_score_codex":0.013704435,"about_ca_topic_score_gemma":0.007921317,"teacher_disagreement_score":0.013704435,"about_ca_system_score_codex":0.00062948046,"about_ca_system_score_gemma":0.0008824087,"threshold_uncertainty_score":0.027249336},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.87573093,0.00061852025,0.113460645,0.0011295152,0.00007416455,0.00010754008,0.00013476421,0.00035073757,0.008393289],"genre_scores_gemma":[0.99291974,0.00009397654,0.0061097257,0.000025602334,0.000016610578,0.000016941001,0.000027259988,0.00003673484,0.0007533712],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997507,0.00007915038,0.000010975269,0.000028254171,0.00008422951,0.00004665114],"domain_scores_gemma":[0.99953556,0.00023882622,0.0000650755,0.0000524286,0.00007173155,0.00003642893],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00054822076,0.00027091868,0.00044383254,0.00044805562,0.000471599,0.0011349558,0.00037723905,0.0005179511,0.0006222246],"category_scores_gemma":[0.0020145692,0.00020855293,0.00024253906,0.0002927746,0.0012605025,0.0007411064,0.0007185442,0.00071756257,0.00009764666],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00029554387,0.00026493886,0.01508319,0.00014659372,0.000029794563,0.0013063676,0.0007830364,0.813815,0.10693322,0.034891047,0.0007264297,0.025724847],"study_design_scores_gemma":[0.0000046001805,0.000021644268,0.0010710674,0.000008377451,0.0000012917696,0.000051773117,0.00006033451,0.99381506,0.0036048295,0.0010049329,0.0003472359,0.000008878893],"about_ca_topic_score_codex":0.0028694635,"about_ca_topic_score_gemma":0.0012149799,"teacher_disagreement_score":0.0028694635,"about_ca_system_score_codex":0.00044401325,"about_ca_system_score_gemma":0.0003838077,"threshold_uncertainty_score":0.005705595},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99404705,0.00006844968,0.0046194666,0.000055484077,0.000012287787,0.000016047798,0.000031806117,0.00007208571,0.0010773125],"genre_scores_gemma":[0.99904424,0.000019831987,0.00066043803,0.000006218923,0.0000017956538,0.0000055819746,0.000020601778,0.000005997449,0.00023536284],"study_design_codex":"simulation_or_modeling","study_design_gemma":"observational","domain_scores_codex":[0.9998888,0.000021381453,0.000005786776,0.000017429164,0.000031615084,0.000034980694],"domain_scores_gemma":[0.9995171,0.00025834743,0.00005552887,0.000021555383,0.000090462076,0.00005710554],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003171382,0.0005053222,0.00047921017,0.0005380423,0.00046174647,0.00048790383,0.00045115125,0.0006412862,0.00076028355],"category_scores_gemma":[0.0010563793,0.0002010866,0.0002953311,0.00016728738,0.00075518683,0.000425791,0.00033750822,0.0003846815,0.00008585341],"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":[0.0007658665,0.00021860076,0.011186719,0.00012549858,0.00003436396,0.000789242,0.00025458742,0.8646518,0.11378885,0.0024016807,0.0002006843,0.005582193],"study_design_scores_gemma":[0.000034907844,0.00015147378,0.0044837357,0.000006192185,0.000009357709,0.000035656678,0.00004736455,0.9829742,0.011984266,0.00016220633,0.00009439223,0.000016297192],"about_ca_topic_score_codex":0.009422278,"about_ca_topic_score_gemma":0.004043038,"teacher_disagreement_score":0.009422278,"about_ca_system_score_codex":0.00057540997,"about_ca_system_score_gemma":0.00047798597,"threshold_uncertainty_score":0.018734872},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9908406,0.00003616221,0.0051449714,0.00009974962,0.000017821601,0.000030977968,0.00014212177,0.00009335136,0.003594291],"genre_scores_gemma":[0.9971656,0.000015065172,0.0020011696,0.000017687893,0.0000035416192,0.000017122664,0.000098003984,0.0000121611865,0.0006695651],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999312,0.000016737446,0.0000034189597,0.000008702356,0.000018148654,0.000021791058],"domain_scores_gemma":[0.99967754,0.00017616156,0.00003103881,0.000016406295,0.000052456304,0.000046453766],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023549414,0.0003534423,0.00037796603,0.000298388,0.00040252035,0.0004408018,0.00034180857,0.00097504794,0.0010103923],"category_scores_gemma":[0.0007661307,0.00017302878,0.0003352162,0.00015821627,0.00049572234,0.00026543142,0.00025768756,0.00039231507,0.000108077584],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00016759968,0.00012982274,0.0048216926,0.000028794153,0.000017021945,0.00025793258,0.000089290814,0.9840772,0.007439302,0.00068358076,0.0002716471,0.0020161374],"study_design_scores_gemma":[0.000016264752,0.000040166342,0.0015026531,0.000002723061,0.0000026538721,0.000009692355,0.000029258861,0.9975836,0.00067444984,0.00006576963,0.000068688234,0.000004091215],"about_ca_topic_score_codex":0.013446328,"about_ca_topic_score_gemma":0.0067409473,"teacher_disagreement_score":0.013446328,"about_ca_system_score_codex":0.00037136703,"about_ca_system_score_gemma":0.0005012899,"threshold_uncertainty_score":0.02673614},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9866854,0.000020260268,0.012256815,0.000026380938,0.000010210566,0.000010303295,0.00005557058,0.00009161393,0.0008433427],"genre_scores_gemma":[0.9973954,0.000010251921,0.002134009,0.0000067431383,0.0000011812042,0.0000061002024,0.000046094967,0.000007367834,0.00039289903],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.9998739,0.000016183918,0.0000031645002,0.00002322098,0.000062718354,0.000020817852],"domain_scores_gemma":[0.9998228,0.00005971614,0.00001634555,0.000020438196,0.000049277212,0.000031561],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017689097,0.00037861423,0.00029259687,0.00020181303,0.00018674781,0.00022063077,0.00022854263,0.0003142258,0.00075205206],"category_scores_gemma":[0.00032064476,0.0001163641,0.00020791007,0.0001006157,0.00028335824,0.0001956512,0.00027296538,0.00019792267,0.00011898092],"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":[0.0004855086,0.00010978047,0.007914947,0.00006822721,0.000014590192,0.0006635812,0.00021972276,0.027773926,0.9464465,0.00023315895,0.00018040132,0.0158897],"study_design_scores_gemma":[0.0000654357,0.0017484486,0.10666277,0.000027217658,0.000032720833,0.0009013887,0.00040974107,0.33895767,0.549586,0.0002912439,0.0012423177,0.00007505317],"about_ca_topic_score_codex":0.0010603055,"about_ca_topic_score_gemma":0.0012908943,"teacher_disagreement_score":0.0010603055,"about_ca_system_score_codex":0.00015743506,"about_ca_system_score_gemma":0.0001867448,"threshold_uncertainty_score":0.002515912},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6540601,0.0002569435,0.33936387,0.00014794321,0.000032827098,0.00007415472,0.00016124966,0.00055832864,0.005344543],"genre_scores_gemma":[0.9473191,0.00021170113,0.050939135,0.000016216363,0.000010527964,0.000036912195,0.00012134919,0.000043978438,0.0013010364],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.9999025,0.000024663435,0.0000031408983,0.000013509357,0.000041479296,0.000014691775],"domain_scores_gemma":[0.99979025,0.00010996516,0.000021635797,0.000014189263,0.000042835894,0.000021128315],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021425352,0.0006680265,0.00030383136,0.00039312075,0.00012690392,0.00036489675,0.0003004227,0.00041325207,0.0011105145],"category_scores_gemma":[0.0005418468,0.00018616488,0.00033962703,0.00034829383,0.00029158933,0.00041332733,0.0003801555,0.00028309875,0.0001722019],"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":[0.00061652664,0.00009877582,0.002129475,0.00021917507,0.00003812849,0.00069733884,0.00035497884,0.22611342,0.6935169,0.003680831,0.0004165373,0.07211793],"study_design_scores_gemma":[0.00003980543,0.00017635502,0.0064478866,0.00003271655,0.000021639466,0.00022683146,0.0000933863,0.87895477,0.11202507,0.0011583776,0.00076720834,0.000055982502],"about_ca_topic_score_codex":0.0015682456,"about_ca_topic_score_gemma":0.0014165619,"teacher_disagreement_score":0.0015682456,"about_ca_system_score_codex":0.00021346439,"about_ca_system_score_gemma":0.00027132864,"threshold_uncertainty_score":0.003715098},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98148084,0.00047239245,0.015731502,0.000032027547,0.00012295226,0.00003713412,0.00005877166,0.00022491762,0.0018393253],"genre_scores_gemma":[0.99411666,0.00016742016,0.0050759544,0.000020459578,0.000013683846,0.0000074583195,0.000029960927,0.000036010963,0.00053241575],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9992505,0.00013576084,0.000070285656,0.00014031943,0.0002885567,0.00011462493],"domain_scores_gemma":[0.9960633,0.001926337,0.00089524785,0.000495164,0.00052218797,0.00009768124],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0007441428,0.00078899524,0.00034630264,0.0006073777,0.00027058905,0.0004890642,0.00039422707,0.00037974783,0.0010870394],"category_scores_gemma":[0.0029235291,0.00036956178,0.0004570821,0.00026962103,0.00048465643,0.00043883195,0.00038175329,0.00035468952,0.00020463896],"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":[0.0011413296,0.00017431311,0.009824129,0.0005446207,0.00004447666,0.001148073,0.00025965046,0.034095265,0.9063537,0.0003481508,0.0001962964,0.04586993],"study_design_scores_gemma":[0.00005502488,0.0049667154,0.06508448,0.000046784826,0.00024031247,0.0008438871,0.00026623058,0.026713816,0.8982444,0.00015682908,0.0032930565,0.000088446075],"about_ca_topic_score_codex":0.0005232884,"about_ca_topic_score_gemma":0.0006406185,"teacher_disagreement_score":0.0010870394,"about_ca_system_score_codex":0.00025694273,"about_ca_system_score_gemma":0.0001626134,"threshold_uncertainty_score":0.0039354563},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99286956,0.000029994026,0.00561639,0.000025276418,0.000017942015,0.000017847642,0.000047538546,0.00007401678,0.0013013544],"genre_scores_gemma":[0.99680954,0.000017242097,0.00237264,0.000008788187,0.0000019586219,0.0000072085604,0.00003321692,0.00001074722,0.00073875196],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.999757,0.000029194194,0.0000061040364,0.000031244126,0.0001230759,0.000053331805],"domain_scores_gemma":[0.9995142,0.00017328224,0.00003518972,0.00005358668,0.00014961616,0.00007416446],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000319825,0.00047643913,0.00043382996,0.00020255522,0.0002737569,0.0002922938,0.00029740986,0.000431848,0.0013526395],"category_scores_gemma":[0.000717999,0.00019036393,0.0002793803,0.000087594504,0.00039351816,0.00029854506,0.00039583282,0.0003311915,0.0002514391],"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":[0.0010227469,0.00015745328,0.0067942506,0.00008181814,0.000012443404,0.0007218547,0.00024927972,0.053465363,0.91861415,0.00025028334,0.00023872886,0.018391546],"study_design_scores_gemma":[0.00016794699,0.004104981,0.06297895,0.00003869923,0.0000413237,0.00096813974,0.00042863784,0.33147773,0.59754425,0.00025951432,0.0019021097,0.00008782132],"about_ca_topic_score_codex":0.0028040346,"about_ca_topic_score_gemma":0.0038546585,"teacher_disagreement_score":0.0028040346,"about_ca_system_score_codex":0.00026026237,"about_ca_system_score_gemma":0.00034665375,"threshold_uncertainty_score":0.0055754185},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8992668,0.00014160582,0.093170516,0.00017757218,0.00006308935,0.00008668062,0.00020640009,0.00057308044,0.006314177],"genre_scores_gemma":[0.9864595,0.000035252408,0.012507084,0.000022596572,0.000006232409,0.000043802094,0.00011517445,0.000031348278,0.0007789122],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996784,0.00009796473,0.000020130705,0.000047034388,0.000117609816,0.000038913684],"domain_scores_gemma":[0.9989748,0.00056333875,0.00008456377,0.000068451336,0.0002461595,0.00006269036],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0009677219,0.0007219865,0.00052205735,0.0003718687,0.0004110127,0.00088916876,0.00084880635,0.00077705126,0.0008694735],"category_scores_gemma":[0.0018279074,0.00022640651,0.00060842116,0.00019293776,0.00032776516,0.00043862913,0.00054143614,0.0007096762,0.00019602745],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000099566576,0.0000616053,0.002222149,0.000019488529,0.00001435727,0.000031592095,0.000029097062,0.99137104,0.002271493,0.000360956,0.00008171501,0.0034369526],"study_design_scores_gemma":[0.000004152654,0.00003209775,0.00019458127,0.0000018761925,0.0000017204075,0.0000024207784,0.0000051041993,0.99908864,0.00060474203,0.000024985931,0.00003704992,0.0000024860442],"about_ca_topic_score_codex":0.015148425,"about_ca_topic_score_gemma":0.00743935,"teacher_disagreement_score":0.015148425,"about_ca_system_score_codex":0.0006818635,"about_ca_system_score_gemma":0.00077734893,"threshold_uncertainty_score":0.030120492},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9464003,0.00020722834,0.046691008,0.000075288204,0.000045925328,0.00006598015,0.0004274395,0.0004986786,0.0055881827],"genre_scores_gemma":[0.99050224,0.00009609792,0.0071715442,0.000011934144,0.0000022852364,0.000051231793,0.00021097042,0.000033099663,0.001920674],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999826,0.00003483921,0.000007986186,0.000031847256,0.00006850332,0.00003078202],"domain_scores_gemma":[0.9998306,0.00004358074,0.000024336181,0.000035395908,0.00004212718,0.00002402006],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00040609294,0.00068961387,0.00042398032,0.00030259753,0.00022990225,0.0007183757,0.0009016439,0.0009063209,0.0013689213],"category_scores_gemma":[0.00050075236,0.00019388973,0.0004903455,0.0001399688,0.0005382926,0.00032515114,0.0004505163,0.0003758637,0.00051996636],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00080694136,0.0002306651,0.007862519,0.0003186854,0.00003938635,0.000345285,0.000231195,0.8575086,0.10629786,0.001435588,0.00065002334,0.024273168],"study_design_scores_gemma":[0.00008764309,0.0018543528,0.0055254255,0.00006638046,0.000040395582,0.000106510626,0.00018734908,0.91458654,0.07251784,0.00040914616,0.004564388,0.000053960233],"about_ca_topic_score_codex":0.0025837547,"about_ca_topic_score_gemma":0.0017845121,"teacher_disagreement_score":0.0025837547,"about_ca_system_score_codex":0.0003691551,"about_ca_system_score_gemma":0.0004899416,"threshold_uncertainty_score":0.005137384},"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":"methods","genre_gemma":"methods","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.13439772,0.0009229418,0.8332367,0.00023998869,0.00016856675,0.00015824799,0.00011928223,0.0002479832,0.030508533],"genre_scores_gemma":[0.90678775,0.00088328787,0.08361255,0.00006191708,0.00007486482,0.00022348463,0.00009593838,0.00008130763,0.008178927],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99986196,0.000040716546,0.000005812743,0.000017200331,0.000055496144,0.000018688917],"domain_scores_gemma":[0.99971086,0.0001271269,0.000045345005,0.000023678747,0.00007271752,0.000020322464],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00033783945,0.0006286102,0.00054058194,0.000542201,0.0005352747,0.0007342492,0.00078223733,0.0009491475,0.0016837094],"category_scores_gemma":[0.0010736192,0.00023086436,0.0006075134,0.00030127252,0.00085434155,0.00057286595,0.00056852825,0.0005653678,0.0003088594],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000023970351,0.000042264597,0.0005849094,0.00007527053,0.000010007721,0.00015529657,0.000080763115,0.9695995,0.007867496,0.016929757,0.00014186566,0.004488905],"study_design_scores_gemma":[0.0000025008158,0.00001087277,0.00006816596,0.0000046322716,0.0000017141906,0.00001721181,0.000013674497,0.9981743,0.00050723477,0.00096646155,0.00022933244,0.0000039096344],"about_ca_topic_score_codex":0.0032391732,"about_ca_topic_score_gemma":0.0022196854,"teacher_disagreement_score":0.0032391732,"about_ca_system_score_codex":0.00042761271,"about_ca_system_score_gemma":0.0006727169,"threshold_uncertainty_score":0.0064406395},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.014048349,0.00006597063,0.9833487,0.00006396788,0.00003466922,0.000040956664,0.00016915011,0.0014611483,0.000767107],"genre_scores_gemma":[0.67830986,0.0001089096,0.3153429,0.00014045283,0.000049236343,0.00039047658,0.0013455987,0.00034033734,0.003972177],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99980503,0.000031153922,0.000009181854,0.000054571825,0.000080392674,0.000019645238],"domain_scores_gemma":[0.99954045,0.00021663906,0.000034773097,0.00004017729,0.00014873009,0.00001923865],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005713219,0.0006378134,0.0005095646,0.0004505509,0.00025714713,0.00051524607,0.0011421938,0.00069151056,0.0019171459],"category_scores_gemma":[0.0017473648,0.00048387604,0.0005210931,0.00027452613,0.000327763,0.00060836546,0.00062816794,0.001114924,0.0006888401],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00006232127,0.000047773534,0.00079751527,0.00004033984,0.000026289219,0.000042274503,0.000017675737,0.93859535,0.0047967955,0.0023101598,0.0008894525,0.052373935],"study_design_scores_gemma":[0.0000019340011,0.0000056814843,0.00005115253,0.000001346505,0.0000010204328,0.0000025795377,0.0000010529703,0.9988759,0.000533197,0.00035105558,0.00017299033,0.0000019395866],"about_ca_topic_score_codex":0.0052153068,"about_ca_topic_score_gemma":0.0049169855,"teacher_disagreement_score":0.0052153068,"about_ca_system_score_codex":0.0004879036,"about_ca_system_score_gemma":0.00088924926,"threshold_uncertainty_score":0.010369897},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0724245,0.02528448,0.8376549,0.0013576304,0.0013042061,0.00009779111,0.00017750308,0.00032829022,0.061370604],"genre_scores_gemma":[0.9226997,0.014120312,0.04904119,0.00043347158,0.0013527714,0.00017017701,0.00018844353,0.00025141131,0.011742483],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.99932504,0.00019518938,0.000028538285,0.00017655936,0.00020661537,0.000068070476],"domain_scores_gemma":[0.9989512,0.000616692,0.00014821181,0.000051707397,0.00018948028,0.00004266876],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00067260215,0.0009046152,0.00050421146,0.0009002168,0.0007053384,0.001241053,0.0007715862,0.0010194922,0.0029260486],"category_scores_gemma":[0.004111899,0.00034395733,0.00046621947,0.00095373025,0.0018116168,0.0021764454,0.0008867266,0.0016311187,0.00062941416],"study_design_candidate":"theoretical_or_conceptual","study_design_consensus":"theoretical_or_conceptual","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0001881895,0.000058365644,0.0008851033,0.00028063188,0.000020066998,0.00029750072,0.00040256683,0.08546748,0.013228877,0.8646178,0.002218141,0.0323353],"study_design_scores_gemma":[0.00003615591,0.00019465358,0.00067728263,0.00010016038,0.000023527367,0.00031729921,0.00010420695,0.415087,0.0046143257,0.56671804,0.012056569,0.00007075406],"about_ca_topic_score_codex":0.0014318915,"about_ca_topic_score_gemma":0.00049693254,"teacher_disagreement_score":0.0029260486,"about_ca_system_score_codex":0.00090379466,"about_ca_system_score_gemma":0.00032488312,"threshold_uncertainty_score":0.009788632},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99271554,0.000026877633,0.004918787,0.000036772355,0.00001103524,0.000014041319,0.00011527149,0.000079831305,0.0020818072],"genre_scores_gemma":[0.99761117,0.000015197155,0.001769589,0.000007820931,0.0000023312973,0.000009592736,0.00009498467,0.000012399795,0.0004768904],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999368,0.000011616443,0.0000039520696,0.000008325017,0.0000223422,0.000016983162],"domain_scores_gemma":[0.99973506,0.00015630871,0.000025133197,0.000017757993,0.00004259734,0.000023147717],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001831892,0.00029060937,0.000300151,0.00022524125,0.00025216173,0.00037130824,0.00026655028,0.0004925198,0.0008388394],"category_scores_gemma":[0.00062637625,0.00010430281,0.00026074098,0.0001430727,0.00028244444,0.0002751516,0.00022390088,0.00031259854,0.00008162978],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00020541667,0.00013606624,0.008089342,0.000044497316,0.000024001707,0.00024252267,0.000100958496,0.96513134,0.020255756,0.0007172519,0.00022663685,0.0048261643],"study_design_scores_gemma":[0.000008476008,0.000043247124,0.0019932075,0.0000026245805,0.0000025868737,0.000010166428,0.000035362806,0.9954313,0.002309748,0.00006239813,0.000096646254,0.000004265953],"about_ca_topic_score_codex":0.005059991,"about_ca_topic_score_gemma":0.0039947815,"teacher_disagreement_score":0.005059991,"about_ca_system_score_codex":0.00019612297,"about_ca_system_score_gemma":0.00028204214,"threshold_uncertainty_score":0.010061085},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9398231,0.00012698714,0.053726707,0.00014725345,0.000051438357,0.000059021688,0.00012645396,0.00031109052,0.0056279427],"genre_scores_gemma":[0.99038917,0.000037740716,0.008535977,0.000015191265,0.0000073600545,0.000033046777,0.00007497081,0.00003336227,0.0008731396],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998368,0.000037062287,0.000008146677,0.000019671528,0.00006591031,0.00003245731],"domain_scores_gemma":[0.9990688,0.00055677304,0.00007520178,0.000043778724,0.00020483961,0.00005072293],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00038393945,0.00044294054,0.0004950343,0.00039542472,0.00038896035,0.0006666566,0.00061517983,0.00061748276,0.0009196225],"category_scores_gemma":[0.0021901273,0.00018953823,0.0004043433,0.00022223045,0.00060811243,0.00032772895,0.00035347935,0.00063851406,0.00012741865],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00006885905,0.000039754283,0.0022049707,0.000026913565,0.0000059002414,0.000082878905,0.0000396612,0.9880788,0.0060232845,0.0008457515,0.00010931152,0.002473958],"study_design_scores_gemma":[0.0000037833963,0.000010415195,0.00029465964,0.0000011194987,5.965281e-7,0.0000030607391,0.0000044675276,0.9989845,0.00060915225,0.000051628904,0.000034691868,0.0000019113638],"about_ca_topic_score_codex":0.018030012,"about_ca_topic_score_gemma":0.0072433823,"teacher_disagreement_score":0.018030012,"about_ca_system_score_codex":0.0006772259,"about_ca_system_score_gemma":0.00065846555,"threshold_uncertainty_score":0.035850167},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.714201,0.0006360026,0.245291,0.00043514793,0.00023945568,0.00014343813,0.0018543714,0.006759964,0.030439653],"genre_scores_gemma":[0.92812294,0.00017626688,0.06463515,0.00007184032,0.000021713757,0.0001329581,0.0012333839,0.00029286105,0.0053130137],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99981254,0.000040650593,0.000014507248,0.000022027527,0.00008730071,0.000023048462],"domain_scores_gemma":[0.99947566,0.00020776596,0.00006190262,0.00009390958,0.00013174492,0.000028919358],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00044504934,0.00038760967,0.00048550623,0.00046438456,0.00026006022,0.0005760139,0.00053176633,0.0005652905,0.0034664862],"category_scores_gemma":[0.0012822963,0.00014658748,0.0003360672,0.0003299869,0.0002481617,0.000332525,0.00048794574,0.00052366685,0.0007088205],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0006959544,0.00046504123,0.021186538,0.0007604466,0.00006369779,0.0003513671,0.00031715416,0.6887159,0.10879077,0.006769228,0.004705587,0.16717829],"study_design_scores_gemma":[0.00002465438,0.0001404706,0.0042741764,0.00002475621,0.000007280832,0.00007876426,0.00008043839,0.9774349,0.013706574,0.0003595375,0.0038504587,0.000017960869],"about_ca_topic_score_codex":0.0024680148,"about_ca_topic_score_gemma":0.0032900607,"teacher_disagreement_score":0.0034664862,"about_ca_system_score_codex":0.0002409636,"about_ca_system_score_gemma":0.00042683363,"threshold_uncertainty_score":0.0115965605},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8249131,0.00046559845,0.17031564,0.000083655475,0.000048952,0.000257509,0.00047612507,0.0010222131,0.0024172524],"genre_scores_gemma":[0.9358247,0.00027365694,0.060821727,0.000039591156,0.000019039644,0.00027854327,0.00034903522,0.00011270471,0.002280979],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.99940217,0.00008608664,0.000018591834,0.000089984314,0.00036878334,0.000034389253],"domain_scores_gemma":[0.9991805,0.0002903232,0.0000882667,0.00009139782,0.0003092898,0.000040130086],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00089489185,0.00063507445,0.0004049514,0.0009236073,0.0003501554,0.00034073894,0.00065930065,0.0005256051,0.0013673727],"category_scores_gemma":[0.0007943291,0.00019086285,0.00024340359,0.0005757805,0.00037575728,0.00035762752,0.00047208992,0.00033319174,0.00036482335],"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":[0.00041430732,0.00028558576,0.0053178663,0.00022733756,0.000030756262,0.00015431018,0.0002999328,0.0025733956,0.95128167,0.00028414835,0.00024828812,0.03888254],"study_design_scores_gemma":[0.00009791308,0.004325355,0.040015534,0.000025884427,0.000113856615,0.00043101996,0.00021394099,0.0336409,0.91692525,0.00021775671,0.003932295,0.00006023575],"about_ca_topic_score_codex":0.0013756545,"about_ca_topic_score_gemma":0.0039417637,"teacher_disagreement_score":0.0013756545,"about_ca_system_score_codex":0.00029418792,"about_ca_system_score_gemma":0.00035832849,"threshold_uncertainty_score":0.0047326684},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.94674313,0.00037066377,0.0365924,0.0004757207,0.00007208941,0.00008125306,0.00032072095,0.00024951872,0.015094552],"genre_scores_gemma":[0.9864639,0.0001289757,0.01100801,0.00005065846,0.000014554003,0.0000377698,0.00012412453,0.0000419541,0.0021298362],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99984527,0.000032284734,0.000008303861,0.000023171695,0.00005442802,0.000036493464],"domain_scores_gemma":[0.9988481,0.0007706212,0.00012978895,0.000048864986,0.00014330915,0.000059277267],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00035316276,0.0004291283,0.00059599493,0.0005742895,0.00050644256,0.0006996312,0.00052035553,0.0012155077,0.0025544623],"category_scores_gemma":[0.002526245,0.0001504589,0.00041132353,0.0004649661,0.0012419814,0.0004018647,0.00047501954,0.0006592815,0.00019417278],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00024946933,0.0001620426,0.0063439766,0.0001907203,0.000032320957,0.0006978671,0.0002868254,0.9557736,0.024186404,0.004008718,0.00040315388,0.0076648667],"study_design_scores_gemma":[0.0000140359325,0.000051913023,0.001574903,0.000015214574,0.0000058346536,0.00003889378,0.00006595272,0.99590504,0.0017565778,0.00027201645,0.00028970584,0.000009892724],"about_ca_topic_score_codex":0.010188207,"about_ca_topic_score_gemma":0.0055575254,"teacher_disagreement_score":0.010188207,"about_ca_system_score_codex":0.0004079249,"about_ca_system_score_gemma":0.00049050024,"threshold_uncertainty_score":0.02025783},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9708209,0.00005661316,0.026128758,0.000058806145,0.000031969572,0.00002757248,0.00003830952,0.00015304852,0.002683988],"genre_scores_gemma":[0.9976361,0.000013697448,0.0020518876,0.0000049351884,0.0000026177759,0.00000844103,0.000016799884,0.000007282253,0.00025824344],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99988663,0.00003497208,0.0000060978864,0.000014729715,0.000041606007,0.000015924386],"domain_scores_gemma":[0.99943477,0.0003490697,0.000057834008,0.0000307056,0.00009202272,0.00003564824],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002640253,0.00031929428,0.00028311356,0.00024345072,0.00024178842,0.0003690847,0.00032019996,0.0004068189,0.0005818548],"category_scores_gemma":[0.0012341905,0.00013620169,0.00023073607,0.00014154639,0.00056285923,0.00023475321,0.00025340004,0.00031057556,0.00007180115],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00012762353,0.00008509298,0.0049553066,0.000044675613,0.000011825312,0.00018519718,0.000052477135,0.954144,0.034880776,0.0006755764,0.00013174833,0.0047056694],"study_design_scores_gemma":[0.000005242781,0.000028525352,0.00073536846,0.0000012011029,0.0000011657331,0.000004761712,0.0000062510094,0.9972045,0.0019296856,0.00004557912,0.00003499979,0.0000027352764],"about_ca_topic_score_codex":0.0056861253,"about_ca_topic_score_gemma":0.002586878,"teacher_disagreement_score":0.0056861253,"about_ca_system_score_codex":0.00035709247,"about_ca_system_score_gemma":0.0002807541,"threshold_uncertainty_score":0.011306047},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.03178312,0.00021224935,0.9588587,0.000155139,0.0001221706,0.00011613204,0.0003475058,0.005229918,0.003175117],"genre_scores_gemma":[0.459198,0.00026007235,0.5251298,0.00018809536,0.00012507115,0.00030201278,0.002506145,0.0007722816,0.011518472],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99982613,0.000033221557,0.000011742013,0.000043770608,0.00006542296,0.000019662784],"domain_scores_gemma":[0.9997197,0.00007927067,0.000028789447,0.00002888901,0.0001233672,0.000019910362],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004933884,0.0009046971,0.0006493092,0.00036594432,0.0003524853,0.0008079004,0.0013130509,0.0012183482,0.005478163],"category_scores_gemma":[0.0012042945,0.00057845993,0.00062377285,0.00026005178,0.00022070293,0.0006090292,0.0006638982,0.0012083403,0.0025559878],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00022900922,0.0001455524,0.0018343782,0.00012233933,0.00008566464,0.00017254899,0.00007662922,0.8065813,0.009021998,0.0025369702,0.0060092187,0.17318441],"study_design_scores_gemma":[0.0000044371495,0.0000095319765,0.0000647491,0.0000022495924,0.0000016498726,0.0000037382013,0.0000036611602,0.9992901,0.00027779024,0.00008803325,0.00025120133,0.000002852726],"about_ca_topic_score_codex":0.015072303,"about_ca_topic_score_gemma":0.008054213,"teacher_disagreement_score":0.015072303,"about_ca_system_score_codex":0.0002800283,"about_ca_system_score_gemma":0.001012424,"threshold_uncertainty_score":0.029969156},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"review","genre_consensus":"review","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.00021383684,0.9971052,0.0003073919,0.00018617416,0.00032405407,0.000006710497,0.000054665143,0.000014366933,0.0017876647],"genre_scores_gemma":[0.0007290837,0.997948,0.00027031818,0.00014826219,0.00018055375,0.000006746411,0.00007063429,0.0000032420612,0.00064312055],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9997601,0.000028146485,0.000040749917,0.000057498444,0.000093582494,0.00001995093],"domain_scores_gemma":[0.9994925,0.00025367815,0.00008519575,0.00001569353,0.000120064964,0.000032737276],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004755981,0.0010849434,0.0013818725,0.0036769432,0.00039547545,0.0012655829,0.00087327574,0.001026434,0.007298254],"category_scores_gemma":[0.0011469414,0.0004353514,0.0008888381,0.0035496592,0.00032676145,0.0018766454,0.0006921257,0.0011836856,0.0030393505],"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":[0.00008455531,0.000102788596,0.00033133104,0.06873163,0.00015213845,0.00033911684,0.00012787564,0.0009261426,0.004238516,0.0066952547,0.04955963,0.8687111],"study_design_scores_gemma":[0.000005998402,0.00008321688,0.0006420646,0.006598274,0.00013794508,0.00070503145,0.0000533085,0.00011012635,0.0007488488,0.0014861756,0.9894058,0.000023154997],"about_ca_topic_score_codex":0.0009906212,"about_ca_topic_score_gemma":0.0012671497,"teacher_disagreement_score":0.007298254,"about_ca_system_score_codex":0.00038356392,"about_ca_system_score_gemma":0.0013038595,"threshold_uncertainty_score":0.024415135},"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":"other","genre_gemma":"commentary","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"commentary","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.23721795,0.001812478,0.37172538,0.004582242,0.0017597387,0.0004948286,0.0012377099,0.0036170634,0.37755263],"genre_scores_gemma":[0.8799022,0.0011345176,0.08249243,0.0011178659,0.00009669512,0.00020471643,0.0006127444,0.0008000509,0.033638857],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9992085,0.0001898779,0.000036064004,0.00014096836,0.00036382975,0.00006085606],"domain_scores_gemma":[0.9987583,0.00032336902,0.00009725341,0.00022553602,0.000502399,0.00009309663],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0010951963,0.0007937998,0.0002590298,0.0005188517,0.0011427576,0.0028091243,0.0007189024,0.0007270391,0.008180339],"category_scores_gemma":[0.0031069324,0.00029624449,0.00030600114,0.0004712678,0.0010947525,0.002167206,0.001661809,0.00090843474,0.0023950315],"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":[0.0012403451,0.0005414686,0.026632398,0.0013784674,0.00016147955,0.00046923885,0.005807645,0.057526596,0.123902544,0.11214586,0.05415319,0.61604077],"study_design_scores_gemma":[0.0001428902,0.0018618961,0.055961777,0.0015704418,0.00031287724,0.0010213442,0.011217192,0.04222461,0.09552005,0.06884183,0.72084934,0.000475672],"about_ca_topic_score_codex":0.005540866,"about_ca_topic_score_gemma":0.00887549,"teacher_disagreement_score":0.008180339,"about_ca_system_score_codex":0.0008093085,"about_ca_system_score_gemma":0.0009361294,"threshold_uncertainty_score":0.027365983},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9404554,0.00007950058,0.056948315,0.000042653952,0.000030228504,0.00035903073,0.00023430743,0.0004199813,0.0014304968],"genre_scores_gemma":[0.97900337,0.000033951554,0.019374145,0.000013068484,0.000004620364,0.00013765677,0.0002347734,0.000032577547,0.0011658344],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9994697,0.00010249193,0.000030221934,0.00006643396,0.00025372198,0.000077330005],"domain_scores_gemma":[0.9987552,0.0002507051,0.0001212074,0.00011481203,0.0005378482,0.0002202629],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0015164497,0.00058615865,0.00047522402,0.0004716325,0.00051447086,0.0006381031,0.0007891922,0.00055885105,0.0012223556],"category_scores_gemma":[0.0013544591,0.0002818013,0.00026998835,0.00021697849,0.0003719541,0.0003978894,0.00045604393,0.00032127573,0.0002224609],"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":[0.0019344757,0.00076308625,0.010553498,0.00022273888,0.000024495212,0.00022780991,0.00024302147,0.03919854,0.9169695,0.00026099815,0.0003463627,0.029255532],"study_design_scores_gemma":[0.00051144476,0.018307978,0.084871724,0.00006639548,0.00017315232,0.00049394486,0.00064078014,0.3169984,0.57167155,0.00028330504,0.005805023,0.00017631473],"about_ca_topic_score_codex":0.001837834,"about_ca_topic_score_gemma":0.0033602382,"teacher_disagreement_score":0.001837834,"about_ca_system_score_codex":0.00035687076,"about_ca_system_score_gemma":0.00075587194,"threshold_uncertainty_score":0.008019805},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6156307,0.0006432925,0.3714187,0.00013946144,0.000054873144,0.00010105516,0.00006898734,0.00030409728,0.011638864],"genre_scores_gemma":[0.9256022,0.00013107905,0.073075645,0.00002783214,0.0000068265326,0.000051351224,0.000040090432,0.000043509455,0.0010214008],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99985397,0.000047819347,0.0000066155376,0.00001727486,0.000045712426,0.000028412036],"domain_scores_gemma":[0.9996797,0.00015896671,0.000060322174,0.000020024445,0.00006250813,0.00001848454],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00044663454,0.0005061629,0.0003927018,0.0004649114,0.00024191709,0.00047583296,0.00032345345,0.00040091883,0.00081617053],"category_scores_gemma":[0.001047437,0.00023735904,0.00029669786,0.00018998262,0.00026070667,0.0003806879,0.00034108217,0.00025264928,0.00011882037],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000062537445,0.000064213826,0.0011187104,0.000058067984,0.000014979586,0.00004553351,0.000026089458,0.9691092,0.0080659175,0.0010832701,0.00019151154,0.0201599],"study_design_scores_gemma":[0.000010672721,0.000103819075,0.00028714916,0.000005899025,0.000007750506,0.000010455449,0.000016116388,0.9963953,0.0024904714,0.0002893908,0.0003797895,0.0000032669445],"about_ca_topic_score_codex":0.0009339832,"about_ca_topic_score_gemma":0.0017147984,"teacher_disagreement_score":0.0009339832,"about_ca_system_score_codex":0.0002702196,"about_ca_system_score_gemma":0.00056927325,"threshold_uncertainty_score":0.0027303696},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.18173835,0.0005382611,0.812207,0.00017616917,0.000046534307,0.000048973066,0.000098360666,0.0016298014,0.0035165471],"genre_scores_gemma":[0.78951424,0.0006729417,0.20687066,0.000037106405,0.000035309622,0.00006679344,0.0002533089,0.0001179455,0.0024317505],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99957436,0.000076076954,0.000020724667,0.00011710036,0.00018561367,0.00002607326],"domain_scores_gemma":[0.99960333,0.00014329854,0.000041211653,0.000044903707,0.00014445676,0.000022815631],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0007760367,0.0006743364,0.00045942655,0.0006161538,0.00021979971,0.0008103576,0.00078342535,0.000637618,0.00066448597],"category_scores_gemma":[0.0013380477,0.0003088176,0.0005165455,0.00032154168,0.00024540926,0.0008296932,0.0006533748,0.0006118162,0.00042847855],"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":[0.00024054271,0.00018782805,0.011972885,0.00014986644,0.00009412397,0.00015211997,0.00014719795,0.5977125,0.090418324,0.0031821043,0.00048673473,0.2952558],"study_design_scores_gemma":[0.000003155174,0.000056847784,0.0009755718,0.000007803726,0.000011729537,0.00001774204,0.000012039456,0.9855945,0.012444368,0.00031476244,0.0005519372,0.0000094432835],"about_ca_topic_score_codex":0.0025706873,"about_ca_topic_score_gemma":0.001287189,"teacher_disagreement_score":0.0025706873,"about_ca_system_score_codex":0.0003068934,"about_ca_system_score_gemma":0.0004604593,"threshold_uncertainty_score":0.005111456},"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":"editorial","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"other","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.002545427,0.00215218,0.0022760837,0.035416637,0.9358636,0.00006448475,0.003523553,0.00075321796,0.017404836],"genre_scores_gemma":[0.05127466,0.011168483,0.017618053,0.05885939,0.09768402,0.00041512647,0.017273668,0.0034529518,0.7422536],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.99810106,0.00012035526,0.000358362,0.00022494394,0.0010759755,0.00011937231],"domain_scores_gemma":[0.9910823,0.0018788602,0.00048830477,0.0006376212,0.005507601,0.0004053114],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0015379793,0.0022038743,0.0011777972,0.0031370763,0.0050267917,0.0018040292,0.0030202558,0.004969641,0.060375147],"category_scores_gemma":[0.018699346,0.0010342967,0.0008532961,0.0019870894,0.0018889739,0.002598003,0.0016635727,0.0036445565,0.03458795],"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":[0.00013096978,0.000038945072,0.00019652813,0.00016190355,0.000009324133,0.00050125737,0.00004656419,0.000113322094,0.00091665104,0.0012972992,0.9834579,0.013129469],"study_design_scores_gemma":[0.00007800618,0.0001309581,0.003120237,0.00041217892,0.00007866396,0.0011059769,0.00028605922,0.00091005984,0.0066523324,0.0023582284,0.98473465,0.0001327221],"about_ca_topic_score_codex":0.013269953,"about_ca_topic_score_gemma":0.021074245,"teacher_disagreement_score":0.060375147,"about_ca_system_score_codex":0.0020836112,"about_ca_system_score_gemma":0.0028964323,"threshold_uncertainty_score":0.20197499},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.667255,0.017925171,0.17134261,0.002043026,0.0013938061,0.000078799436,0.00076154765,0.0019726113,0.13722737],"genre_scores_gemma":[0.97849965,0.003068889,0.006838341,0.000088589026,0.00063357234,0.000029971234,0.00017246202,0.00022657277,0.010441917],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998466,0.00002759689,0.0000073862084,0.000036020396,0.000060642127,0.000021728101],"domain_scores_gemma":[0.9993808,0.00023303936,0.000111713845,0.00008936,0.000087807544,0.000097245],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000271523,0.00050381053,0.00045418623,0.0008994023,0.0004274187,0.0016029021,0.0004929669,0.00037161438,0.0034353193],"category_scores_gemma":[0.00194842,0.00031614985,0.0002622748,0.0005023645,0.00083681126,0.001172866,0.0005589294,0.0008674766,0.00041747317],"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":[0.00039061657,0.0001770561,0.002204328,0.00031289193,0.00006300812,0.00058047345,0.00048561048,0.11173958,0.0892726,0.6973313,0.010024767,0.08741783],"study_design_scores_gemma":[0.00003505027,0.00011922429,0.016931798,0.000054324006,0.000017056744,0.00054093305,0.0001440435,0.559931,0.0104168905,0.4038254,0.007875062,0.00010921632],"about_ca_topic_score_codex":0.0004019191,"about_ca_topic_score_gemma":0.00031407096,"teacher_disagreement_score":0.0034353193,"about_ca_system_score_codex":0.00044725405,"about_ca_system_score_gemma":0.00016226103,"threshold_uncertainty_score":0.011492252},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9980799,0.000092835566,0.0012778349,0.000007568658,0.000006182575,0.0000066765087,0.000026839494,0.00008647097,0.00041569764],"genre_scores_gemma":[0.998324,0.000040035084,0.0011089424,0.00001116933,0.000002895097,0.000003993744,0.000043763444,0.000017386792,0.0004478514],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99960107,0.000059878636,0.00003588183,0.00008343491,0.00011510559,0.00010460453],"domain_scores_gemma":[0.9989241,0.0002806833,0.00026490248,0.00013469708,0.00025556676,0.00014006627],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0010208879,0.00045924375,0.0004275489,0.00053043646,0.00032117157,0.00062114233,0.0004398727,0.00044669694,0.0018220249],"category_scores_gemma":[0.0012959581,0.00021810518,0.00034049572,0.0002502717,0.00039520787,0.0004339892,0.0005025934,0.0003066489,0.00053934514],"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":[0.0027622194,0.000473162,0.0324737,0.00019870915,0.0000435745,0.00037802858,0.00024307451,0.034159772,0.8897044,0.0003637773,0.00026636798,0.03893313],"study_design_scores_gemma":[0.00004935881,0.004832829,0.067240275,0.0000319256,0.000052922867,0.0002760872,0.00026640578,0.029770846,0.8959284,0.00006783174,0.0014345997,0.000048470178],"about_ca_topic_score_codex":0.00067599746,"about_ca_topic_score_gemma":0.001048303,"teacher_disagreement_score":0.0018220249,"about_ca_system_score_codex":0.0002781219,"about_ca_system_score_gemma":0.00022081535,"threshold_uncertainty_score":0.00609529},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97212845,0.00021459401,0.011339662,0.00080145156,0.00069136894,0.00015455051,0.00095495064,0.0009022992,0.0128126815],"genre_scores_gemma":[0.97757715,0.00014239569,0.006316896,0.00017275914,0.0001275852,0.00007513104,0.00065500475,0.00021150002,0.014721581],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9992317,0.00008899817,0.000036394213,0.00021130181,0.0003175569,0.00011393812],"domain_scores_gemma":[0.9983884,0.00035326838,0.0000923286,0.00043260297,0.00049755484,0.00023578347],"candidate_categories":["research_integrity"],"consensus_categories":[],"category_scores_codex":[0.0010701602,0.00043468893,0.00067849434,0.00052539876,0.0015804553,0.0014841189,0.0014724082,0.0017682264,0.013079966],"category_scores_gemma":[0.002052913,0.00027292556,0.00039024602,0.00045533,0.0010636998,0.0011420578,0.0015354757,0.0015244482,0.0023655286],"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":[0.0030703847,0.0014058487,0.011478548,0.00035396442,0.00007790802,0.0032372747,0.0025110191,0.0055497233,0.91198623,0.0028361126,0.009176692,0.04831628],"study_design_scores_gemma":[0.0007404824,0.0073943906,0.086899064,0.00008815836,0.00018029005,0.0016692257,0.004057066,0.046393573,0.8196641,0.0027882983,0.02994386,0.0001815309],"about_ca_topic_score_codex":0.0043041715,"about_ca_topic_score_gemma":0.0025061222,"teacher_disagreement_score":0.99823177,"about_ca_system_score_codex":0.0004057474,"about_ca_system_score_gemma":0.00058482157,"threshold_uncertainty_score":0.043756843},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.044351693,0.00033819926,0.9534011,0.00006977798,0.00003333081,0.000031147596,0.000017306249,0.00018764171,0.0015698595],"genre_scores_gemma":[0.63632905,0.00024429357,0.36179668,0.00007211747,0.00003368134,0.00009993613,0.000048585287,0.0000496193,0.0013260318],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998061,0.000031563726,0.000012859959,0.000052582764,0.00007879325,0.000018069826],"domain_scores_gemma":[0.9997712,0.00011027686,0.000051026065,0.00002620949,0.000029077657,0.00001225788],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005135777,0.00048807435,0.0004705904,0.00026382325,0.00022615993,0.0005436329,0.0004805333,0.00058251235,0.0005256044],"category_scores_gemma":[0.0007142686,0.00028212846,0.0004292263,0.0002819287,0.0004738593,0.00051850657,0.0005310175,0.0005107528,0.00010721453],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00010760194,0.00008603329,0.00073946995,0.00014298482,0.000038805436,0.000084539926,0.00003537861,0.8443697,0.07433777,0.00825435,0.00030574854,0.07149755],"study_design_scores_gemma":[0.000010131649,0.000051879015,0.0001103423,0.0000025119048,0.0000032934115,0.000011650808,0.0000021727988,0.99399203,0.004929576,0.0006000518,0.00028154816,0.0000048261304],"about_ca_topic_score_codex":0.00052458036,"about_ca_topic_score_gemma":0.000569978,"teacher_disagreement_score":0.00058251235,"about_ca_system_score_codex":0.00030923597,"about_ca_system_score_gemma":0.00042867282,"threshold_uncertainty_score":0.002716124},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.85672987,0.0010297718,0.13360173,0.00011604604,0.00018561726,0.00015233582,0.000099309334,0.00053361116,0.0075517315],"genre_scores_gemma":[0.980664,0.00042160312,0.01696203,0.000035366505,0.00003944497,0.000020717407,0.00005674992,0.00001687511,0.0017832462],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998636,0.000009775733,0.000009128241,0.000028700108,0.00006822821,0.000020479572],"domain_scores_gemma":[0.99973387,0.000057270867,0.00008516033,0.000025716108,0.00006270617,0.000035265122],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016760112,0.00063673925,0.00035790534,0.00039924507,0.0002395571,0.000543277,0.00035471254,0.00019854981,0.0010681516],"category_scores_gemma":[0.00026000766,0.00018449494,0.00019877161,0.0003040443,0.00048604363,0.00042723236,0.00046769972,0.00036992185,0.00023538839],"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":[0.00022485702,0.00006472418,0.0010468477,0.00015615905,0.0000072009984,0.00017242803,0.00009558465,0.011518862,0.9602542,0.0017451938,0.0002241774,0.02448983],"study_design_scores_gemma":[0.000105833526,0.0021713465,0.0046042013,0.00002835053,0.000024983561,0.00019658497,0.00008396885,0.13109925,0.85682184,0.00070960796,0.0041161245,0.00003792074],"about_ca_topic_score_codex":0.00045689524,"about_ca_topic_score_gemma":0.0004461661,"teacher_disagreement_score":0.0010681516,"about_ca_system_score_codex":0.00026929114,"about_ca_system_score_gemma":0.0002818838,"threshold_uncertainty_score":0.0035732985},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.978744,0.00006634959,0.018048977,0.000020374458,0.0000114905215,0.000027473261,0.00016346664,0.00018980664,0.002728113],"genre_scores_gemma":[0.9976023,0.000030682317,0.0018802128,0.0000033230197,0.0000017348152,0.000015758578,0.000109085966,0.0000142280005,0.00034262106],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997787,0.000033505024,0.000015268102,0.000033625514,0.000108060594,0.000030789106],"domain_scores_gemma":[0.9992925,0.00040130812,0.00006132939,0.000061701685,0.00015204726,0.000031120115],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00035096318,0.0003084783,0.0003627301,0.00035545556,0.0003266123,0.00039044453,0.0003125908,0.00036420187,0.0007784876],"category_scores_gemma":[0.0009995593,0.00012941431,0.0003806001,0.00025576318,0.0003813699,0.00020196068,0.00015452597,0.00028486783,0.000101323756],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00048260257,0.00015822804,0.011644834,0.00015247235,0.00004599274,0.00044234435,0.0002750888,0.7915173,0.18339723,0.0011973982,0.00024784132,0.010438636],"study_design_scores_gemma":[0.000053745476,0.0004458315,0.017557578,0.000008911593,0.00002946849,0.00009339683,0.00006419474,0.9283686,0.052626297,0.000195713,0.00052088697,0.00003536651],"about_ca_topic_score_codex":0.0029813389,"about_ca_topic_score_gemma":0.0015962496,"teacher_disagreement_score":0.0029813389,"about_ca_system_score_codex":0.000383811,"about_ca_system_score_gemma":0.00035801504,"threshold_uncertainty_score":0.00592798},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9973923,0.000077771634,0.0019486654,0.000006371549,0.0000025161407,0.000003431193,0.000018366336,0.000027966642,0.00052254274],"genre_scores_gemma":[0.99956864,0.000031315674,0.0003270636,0.0000019375882,9.965787e-7,0.00000262801,0.000010306566,0.0000046082473,0.000052492273],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999374,0.000013927887,0.0000034584582,0.000008820641,0.000015963804,0.000020410247],"domain_scores_gemma":[0.9995408,0.00024100843,0.000101483,0.00002415198,0.00003905785,0.000053409585],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016470336,0.00024494267,0.0001960555,0.00021094902,0.00028091314,0.00041602209,0.00014896016,0.00012872044,0.00042904072],"category_scores_gemma":[0.00058419094,0.0001312554,0.00015284147,0.00014905763,0.0003661877,0.00023008842,0.0003799068,0.00012580882,0.00003577396],"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":[0.00092000066,0.00025020042,0.019433925,0.0001768718,0.00008428636,0.0010077973,0.00031428164,0.52849394,0.4352905,0.0017595575,0.00018534885,0.012083322],"study_design_scores_gemma":[0.00004691618,0.0006151159,0.028957602,0.000016655444,0.0000362948,0.00013258233,0.00015774179,0.892501,0.076663576,0.00038445424,0.00045294382,0.000035154684],"about_ca_topic_score_codex":0.0021743453,"about_ca_topic_score_gemma":0.0017830016,"teacher_disagreement_score":0.0021743453,"about_ca_system_score_codex":0.00018561682,"about_ca_system_score_gemma":0.00020975247,"threshold_uncertainty_score":0.0043233037},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8289161,0.0016653413,0.13254088,0.00033499298,0.00024283538,0.000064032894,0.00013067095,0.0003102402,0.035794947],"genre_scores_gemma":[0.9680233,0.00042681946,0.011029655,0.000035377303,0.00007674889,0.000020063728,0.000109191446,0.000047662834,0.02023127],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999218,0.00001862701,0.0000023765297,0.000018185488,0.000023943116,0.000015063021],"domain_scores_gemma":[0.99986315,0.000055284698,0.000020325308,0.000013201004,0.000027886412,0.000020097881],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012855792,0.00036634415,0.00048257294,0.00029071243,0.0003057728,0.0008249156,0.00043667122,0.0005681767,0.0027918639],"category_scores_gemma":[0.00045929695,0.00023900521,0.00013740167,0.00021446342,0.00058424135,0.0006642957,0.0004862607,0.0002798244,0.00058049825],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0013640834,0.00022133849,0.0020268254,0.00025560084,0.000033181765,0.00047470618,0.00029922428,0.5146032,0.34129518,0.07734423,0.0028980856,0.059184317],"study_design_scores_gemma":[0.00009225278,0.00027552468,0.0015219249,0.000011189269,0.0000064283863,0.00008257538,0.0000748071,0.9769984,0.012144164,0.006975423,0.0018050619,0.000012297554],"about_ca_topic_score_codex":0.0007688492,"about_ca_topic_score_gemma":0.00049989374,"teacher_disagreement_score":0.0027918639,"about_ca_system_score_codex":0.00028403036,"about_ca_system_score_gemma":0.00021099388,"threshold_uncertainty_score":0.00933969},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.1598711,0.0003170478,0.83503383,0.00016850457,0.00006910944,0.00009569053,0.00032132393,0.0005902295,0.00353319],"genre_scores_gemma":[0.9538583,0.00025578108,0.042541604,0.00008044901,0.000039558327,0.00018680819,0.00044933503,0.00013364274,0.002454476],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996815,0.00009061045,0.000020259595,0.00007783536,0.000089415014,0.00004048634],"domain_scores_gemma":[0.9994248,0.00023867795,0.00011002334,0.00007590137,0.00011301045,0.00003763365],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00078744674,0.0008589702,0.0007242109,0.00071912305,0.0003133881,0.00095546653,0.0021028705,0.0012687196,0.00065781316],"category_scores_gemma":[0.001910564,0.00037213042,0.0008265824,0.0006061838,0.0007093455,0.0013568798,0.0007328298,0.0007382544,0.0002865638],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00001727555,0.000023542745,0.0006707936,0.00002534157,0.000013426986,0.00005046386,0.000027471155,0.9896708,0.0019706902,0.004362667,0.00013121424,0.0030363144],"study_design_scores_gemma":[9.688257e-7,0.0000023658051,0.000066008724,8.7899446e-7,9.1908623e-7,0.0000031573488,0.0000017027844,0.99932826,0.00007588058,0.00047447847,0.000043824268,0.0000016622009],"about_ca_topic_score_codex":0.0052593127,"about_ca_topic_score_gemma":0.0026914366,"teacher_disagreement_score":0.0052593127,"about_ca_system_score_codex":0.0005487459,"about_ca_system_score_gemma":0.0008904749,"threshold_uncertainty_score":0.0104573965},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.1789557,0.00054449757,0.81313604,0.00014582512,0.000058789916,0.00012224205,0.00006510902,0.00043541982,0.006536361],"genre_scores_gemma":[0.8873569,0.0002807442,0.110654406,0.00003382824,0.000016165082,0.00005354118,0.00005962615,0.000084807936,0.0014598799],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99971765,0.00005549448,0.000011824633,0.000027427415,0.00016456952,0.000023065955],"domain_scores_gemma":[0.9995061,0.00016261874,0.000100570374,0.000070413415,0.00013154605,0.000028798398],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005409332,0.000676398,0.0004112304,0.0003652488,0.0002438584,0.0006970446,0.0006427213,0.00058044813,0.0009004926],"category_scores_gemma":[0.0014938307,0.00030518422,0.0006581393,0.00016690245,0.00041290218,0.0003675342,0.000373659,0.00045784828,0.00034864098],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00018932347,0.000084824016,0.0030423673,0.0003114794,0.000027778302,0.0005551866,0.00019461774,0.7681674,0.13782252,0.005271351,0.00044214312,0.083891064],"study_design_scores_gemma":[0.000018972152,0.00034507853,0.0016124961,0.000027762962,0.000024489189,0.0002836985,0.000067253335,0.9739257,0.019986859,0.0010536587,0.0026282966,0.00002575792],"about_ca_topic_score_codex":0.0006691024,"about_ca_topic_score_gemma":0.0013686834,"teacher_disagreement_score":0.0009004926,"about_ca_system_score_codex":0.00021237078,"about_ca_system_score_gemma":0.0005467927,"threshold_uncertainty_score":0.0030124784},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9650949,0.00008130525,0.032732144,0.00003545445,0.000017923765,0.00001978561,0.00004077005,0.00020580972,0.0017718454],"genre_scores_gemma":[0.99817514,0.0000090811,0.0015381988,0.0000049239356,0.0000018689827,0.000009985495,0.000024798435,0.000016680922,0.00021931669],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99959594,0.00008862314,0.000012627322,0.000062174964,0.00017262145,0.000067964036],"domain_scores_gemma":[0.9989685,0.0004845661,0.00009751044,0.00007094462,0.00028754663,0.00009088859],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003075105,0.00055323273,0.0004712613,0.00062327634,0.00045459293,0.00044753763,0.00050350087,0.00067700486,0.001146356],"category_scores_gemma":[0.0011482451,0.00025106923,0.000262537,0.0002237963,0.0005090786,0.00044995602,0.00043982427,0.00025871166,0.0002028993],"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":[0.0031566976,0.00041071195,0.016269514,0.00025226595,0.000053752185,0.0011187218,0.0008065901,0.100318,0.84429824,0.001468444,0.0004058769,0.031441092],"study_design_scores_gemma":[0.00009689018,0.0011184344,0.04221972,0.000049366135,0.00006061556,0.00090924994,0.000515686,0.6069957,0.34629342,0.0008432352,0.00080679747,0.00009083659],"about_ca_topic_score_codex":0.00042849997,"about_ca_topic_score_gemma":0.00048561156,"teacher_disagreement_score":0.001146356,"about_ca_system_score_codex":0.00022931969,"about_ca_system_score_gemma":0.00020595477,"threshold_uncertainty_score":0.0038349032},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.953794,0.00012716372,0.04029927,0.00004315298,0.000025152196,0.000042991676,0.00015310576,0.00027312673,0.0052420385],"genre_scores_gemma":[0.9968491,0.000037567675,0.0025492234,0.0000046824916,0.000002620455,0.000020436724,0.000069085545,0.000014454678,0.0004528414],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99978167,0.000036742953,0.00001089221,0.000027290725,0.000110794026,0.000032652883],"domain_scores_gemma":[0.99941564,0.00031516832,0.000060218485,0.000042392683,0.00014046341,0.000026189653],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00035436236,0.00028746243,0.0004114237,0.0003281751,0.00032602646,0.0005193091,0.00033148463,0.00045140056,0.0007711914],"category_scores_gemma":[0.001072649,0.00013027793,0.0003616266,0.00022800003,0.00042712587,0.00026615872,0.00020157859,0.00029642927,0.000099009114],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00017918611,0.000088587905,0.0045567746,0.000092847746,0.00002547799,0.0002670642,0.00015293137,0.9103882,0.07777842,0.0011529177,0.00015747595,0.005160211],"study_design_scores_gemma":[0.000020298936,0.00013915027,0.0038067189,0.0000060216794,0.000010418648,0.000028677978,0.00003334044,0.9815089,0.014030466,0.00013679019,0.00026422855,0.00001503594],"about_ca_topic_score_codex":0.003992172,"about_ca_topic_score_gemma":0.0018528487,"teacher_disagreement_score":0.003992172,"about_ca_system_score_codex":0.0004042429,"about_ca_system_score_gemma":0.0004365451,"threshold_uncertainty_score":0.007937849},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9908048,0.00013476753,0.00808088,0.000020393749,0.00003206668,0.000007978284,0.000026111778,0.000058339458,0.00083465787],"genre_scores_gemma":[0.99871767,0.000035297475,0.0010405828,0.000004555789,0.0000028589118,0.0000022502795,0.000012098556,0.000003353978,0.00018135282],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99988437,0.000012067342,0.000007733896,0.00002142968,0.00005076463,0.000023562938],"domain_scores_gemma":[0.9997812,0.00007332783,0.000042341668,0.000021616008,0.00006280669,0.000018780062],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018590252,0.00029098446,0.00015882617,0.00017228138,0.00019018326,0.00025029507,0.00012612292,0.00017195576,0.000721678],"category_scores_gemma":[0.00033080744,0.00009210344,0.00019211756,0.00013020329,0.00030603644,0.00017936595,0.00017726023,0.0002133592,0.00009448433],"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":[0.00046971827,0.00008744485,0.00290139,0.00012289447,0.00000804088,0.00033173172,0.00013094682,0.025197871,0.9463218,0.00033686284,0.00015416846,0.023937088],"study_design_scores_gemma":[0.00006297289,0.0032214704,0.025744958,0.000022277027,0.00002463299,0.00032372912,0.00022303696,0.17884326,0.7895032,0.00033487467,0.0016541871,0.000041425727],"about_ca_topic_score_codex":0.0005482119,"about_ca_topic_score_gemma":0.00064805476,"teacher_disagreement_score":0.000721678,"about_ca_system_score_codex":0.00011523999,"about_ca_system_score_gemma":0.00011561566,"threshold_uncertainty_score":0.0024142265},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9877694,0.00030070567,0.0087944055,0.000087141736,0.000052548956,0.000012257076,0.00014515406,0.00019793335,0.0026404797],"genre_scores_gemma":[0.9989311,0.00007484937,0.00048969727,0.00001170429,0.00000708345,0.0000036001882,0.00007866823,0.00003292576,0.00037032826],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998287,0.000019200075,0.000007157274,0.000032834883,0.000041411615,0.000070773276],"domain_scores_gemma":[0.99962926,0.000072929375,0.000052195086,0.000022794082,0.000069594345,0.0001532242],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020663948,0.0005043254,0.00041754995,0.0005087594,0.00052828394,0.001605699,0.00026860062,0.000262678,0.0013111633],"category_scores_gemma":[0.00074816414,0.00023582959,0.0003484551,0.00024060823,0.000503457,0.00066595356,0.0006439092,0.0005647619,0.00022290868],"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":[0.002942869,0.00065074046,0.0471972,0.0001570233,0.00016229415,0.001863082,0.0002823429,0.16037823,0.7425212,0.01281977,0.002140501,0.028884677],"study_design_scores_gemma":[0.00016708375,0.0006774757,0.15348123,0.000034125394,0.00008675137,0.0002492049,0.00026912743,0.71482897,0.12570132,0.0028250252,0.0015512424,0.00012843173],"about_ca_topic_score_codex":0.0049352422,"about_ca_topic_score_gemma":0.0018980769,"teacher_disagreement_score":0.0049352422,"about_ca_system_score_codex":0.00061531144,"about_ca_system_score_gemma":0.00036761828,"threshold_uncertainty_score":0.009813011},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0005179617,0.00038633822,0.00068501185,0.00033917013,0.00034090976,0.00009644345,0.00065314403,0.0007032579,0.99627787],"genre_scores_gemma":[0.00080314657,0.00022189094,0.00032737394,0.00020424345,0.000084627376,0.000047207417,0.00035151397,0.00014931275,0.9978108],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.99941015,0.000041672014,0.00005033071,0.00021770243,0.0001432598,0.00013700248],"domain_scores_gemma":[0.99804085,0.0004755849,0.00011377044,0.00022224245,0.0004906755,0.0006569446],"candidate_categories":["insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.00092792854,0.002591079,0.0016118154,0.002590048,0.0026357898,0.0036736452,0.0030750688,0.0051255133,0.98734856],"category_scores_gemma":[0.0013725712,0.0010220878,0.0013250192,0.0023273185,0.002092002,0.0048261755,0.0028436626,0.0025108554,0.9914408],"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":[0.00039675244,0.00024512608,0.0011830232,0.00073185633,0.000048277583,0.00036101128,0.00017353785,0.0006044559,0.003194621,0.006435992,0.4141649,0.5724605],"study_design_scores_gemma":[0.000049971233,0.0001426206,0.0008637372,0.00034270572,0.000016571952,0.00042371408,0.00016375782,0.00020683957,0.00042522766,0.0007620793,0.99657863,0.000024235385],"about_ca_topic_score_codex":0.0045542563,"about_ca_topic_score_gemma":0.0034494414,"teacher_disagreement_score":0.0126514435,"about_ca_system_score_codex":0.0009703781,"about_ca_system_score_gemma":0.00091840664,"threshold_uncertainty_score":0.018045664},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0005554069,0.0003760199,0.0006589761,0.00036837478,0.00033903826,0.00010576452,0.00061177264,0.00075437356,0.9962302],"genre_scores_gemma":[0.000750422,0.00022435641,0.00034542513,0.00022777761,0.00007781232,0.000051454153,0.0003207927,0.00014582633,0.9978561],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9993963,0.000039234754,0.00005379894,0.00021990835,0.00014543028,0.00014519788],"domain_scores_gemma":[0.997759,0.0005290647,0.00013269219,0.00024973924,0.00055783783,0.0007716412],"candidate_categories":["insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.001029111,0.0028729131,0.0017356756,0.0025915636,0.0028858276,0.0037576142,0.00321434,0.0054310523,0.988521],"category_scores_gemma":[0.0015151087,0.0011422314,0.0013324249,0.0023484498,0.0024462556,0.0055148625,0.0029203892,0.0027333603,0.9922895],"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":[0.00044736124,0.00029019295,0.0012821944,0.0007664533,0.000052557407,0.0003853168,0.00018718262,0.000575877,0.0032451088,0.0066201636,0.41295907,0.5731885],"study_design_scores_gemma":[0.000055925208,0.00015234236,0.0009866195,0.00036200345,0.000017991544,0.00045498254,0.00018312388,0.00021961142,0.0004529011,0.00080746476,0.99627906,0.00002793226],"about_ca_topic_score_codex":0.0044837,"about_ca_topic_score_gemma":0.003731357,"teacher_disagreement_score":0.01147902,"about_ca_system_score_codex":0.001037601,"about_ca_system_score_gemma":0.0009504071,"threshold_uncertainty_score":0.016373336},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98622537,0.00017099667,0.0103967,0.000027007136,0.000024212664,0.000028715573,0.00022429145,0.00022669998,0.0026759428],"genre_scores_gemma":[0.99685246,0.000052093998,0.00270214,0.000007489251,0.0000032470004,0.000018416662,0.00010566731,0.000026527074,0.00023194912],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99963784,0.000073016294,0.000021286902,0.000055203498,0.00013601295,0.00007665014],"domain_scores_gemma":[0.99803835,0.0011175328,0.00017556218,0.00019131992,0.00037228985,0.000104907784],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005499694,0.00071284024,0.0006125056,0.0006957833,0.00039034142,0.0005404238,0.0006463326,0.00069280504,0.001336175],"category_scores_gemma":[0.0028613843,0.00032519517,0.00048484004,0.00044533875,0.00045738282,0.00040401673,0.0005900243,0.0005036528,0.00015235505],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00024852983,0.00014299675,0.007228008,0.00013111574,0.00002581827,0.00013827308,0.00006326331,0.9684684,0.01832028,0.00048792336,0.00018524948,0.004560081],"study_design_scores_gemma":[0.000028419667,0.00016071169,0.0044957446,0.000014283683,0.000019299707,0.00002907581,0.000023816097,0.9770982,0.017785344,0.00008103333,0.00024053865,0.000023533827],"about_ca_topic_score_codex":0.0050549572,"about_ca_topic_score_gemma":0.0026130753,"teacher_disagreement_score":0.0050549572,"about_ca_system_score_codex":0.00078800344,"about_ca_system_score_gemma":0.00032277667,"threshold_uncertainty_score":0.010051072},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9969995,0.00016142588,0.002003864,0.000021993344,0.000019204208,0.00001201968,0.000022963393,0.000024825844,0.00073424046],"genre_scores_gemma":[0.9984773,0.00015745657,0.0011277972,0.000016177752,0.000005053807,0.000010255909,0.000021383243,0.000008655544,0.00017593041],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998405,0.00002260069,0.00001565846,0.00002195005,0.000055554578,0.00004374169],"domain_scores_gemma":[0.9994929,0.00025623175,0.00010891895,0.000030745447,0.000049312657,0.000061860956],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002703374,0.00033944432,0.00024383797,0.00017180777,0.00024830678,0.00033882548,0.00017627171,0.00018318396,0.00068384246],"category_scores_gemma":[0.00074777845,0.00014090244,0.0001470876,0.00009872195,0.00036001246,0.00016427739,0.00038736846,0.00024120428,0.000072293624],"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":[0.00015814246,0.000031300995,0.00072865543,0.00005606677,0.0000036260392,0.00013378235,0.00006396489,0.0018060997,0.9939871,0.00009025315,0.000026312648,0.00291469],"study_design_scores_gemma":[0.00002265647,0.00056907185,0.015676366,0.000014502823,0.000008841065,0.000104715604,0.000067286,0.014530603,0.9682073,0.000058223904,0.00072062114,0.000019914756],"about_ca_topic_score_codex":0.00040609954,"about_ca_topic_score_gemma":0.000529846,"teacher_disagreement_score":0.00068384246,"about_ca_system_score_codex":0.00019987106,"about_ca_system_score_gemma":0.00025294503,"threshold_uncertainty_score":0.0022876859},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.022158895,0.00006533773,0.97051126,0.00009819708,0.000033341184,0.00006097306,0.000064044536,0.0010916198,0.0059162984],"genre_scores_gemma":[0.4739846,0.00009645274,0.5207257,0.00008931623,0.00003277586,0.00024115945,0.0002286659,0.00050962076,0.0040916177],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997787,0.000035846064,0.0000066054513,0.00001918149,0.00013835865,0.000021416832],"domain_scores_gemma":[0.9995433,0.00019037948,0.000057999703,0.00006018972,0.00010938602,0.000038704504],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00048484516,0.00057343213,0.00055372255,0.00030865072,0.00038252302,0.00065629056,0.00093113724,0.0007109579,0.002206474],"category_scores_gemma":[0.0012730476,0.00034716836,0.0004320942,0.00023233167,0.00052606827,0.00047443237,0.00071908196,0.0007596047,0.00040631776],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000037193797,0.000047617756,0.0003882593,0.000029008357,0.000012864122,0.000036809553,0.000018657376,0.97771674,0.0064940797,0.003432761,0.0005508903,0.011235096],"study_design_scores_gemma":[0.000007861935,0.000006894416,0.000034421657,0.0000013105025,8.2804235e-7,0.0000046050654,0.0000014307356,0.99846613,0.000830965,0.00029169896,0.00035141426,0.0000025210031],"about_ca_topic_score_codex":0.004825566,"about_ca_topic_score_gemma":0.005218019,"teacher_disagreement_score":0.004825566,"about_ca_system_score_codex":0.00048287577,"about_ca_system_score_gemma":0.0014687596,"threshold_uncertainty_score":0.009594977},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.005507871,0.0528448,0.01988289,0.006011736,0.0037398553,0.00016509547,0.004023422,0.0014458118,0.90637845],"genre_scores_gemma":[0.029610012,0.030615317,0.021456864,0.0025053197,0.00073228066,0.00035726547,0.0070771636,0.0007401326,0.90690565],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9991961,0.00015420631,0.000036824327,0.00016821962,0.000360221,0.000084513566],"domain_scores_gemma":[0.99947935,0.0001028005,0.00006074607,0.00007674082,0.0001686519,0.00011176973],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0015382298,0.0008953247,0.00047338093,0.0011384906,0.00059060066,0.0022810986,0.00095544825,0.0018545425,0.052622948],"category_scores_gemma":[0.0009780499,0.0001693849,0.0003029295,0.0014624719,0.00045945655,0.001629495,0.0024452726,0.0011739603,0.02925377],"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":[0.00029332045,0.00010587548,0.0006682484,0.00075391185,0.000018992278,0.00027040637,0.00020804117,0.0014048492,0.005259789,0.13658859,0.27729225,0.5771358],"study_design_scores_gemma":[0.000010358489,0.000034655404,0.00040666142,0.00009540025,0.0000037351638,0.000110177716,0.000024456176,0.00016736051,0.0007940187,0.0030095447,0.9953388,0.000004785021],"about_ca_topic_score_codex":0.0025473295,"about_ca_topic_score_gemma":0.0017843685,"teacher_disagreement_score":0.052622948,"about_ca_system_score_codex":0.0011291046,"about_ca_system_score_gemma":0.0029249904,"threshold_uncertainty_score":0.1760413},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99100894,0.0001589354,0.007825041,0.000024485013,0.000009428135,0.000007686388,0.00010439434,0.000106186664,0.0007548975],"genre_scores_gemma":[0.99562776,0.00010714223,0.003740598,0.000025445039,0.000004585415,0.000011537256,0.00012435319,0.0000106096195,0.00034782678],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99985623,0.000013777033,0.000005253655,0.000042194602,0.00004948476,0.000033117376],"domain_scores_gemma":[0.9998648,0.000045944475,0.00002724894,0.000006344005,0.000040207313,0.000015398453],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00022410312,0.0002676305,0.00017259855,0.00030325286,0.00035735592,0.0004974126,0.0001610739,0.0003080234,0.00043887921],"category_scores_gemma":[0.0003121429,0.00010903969,0.00013878956,0.00021303557,0.00034212234,0.0003973097,0.00028547057,0.00029042212,0.00009255042],"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":[0.00009509748,0.00002629358,0.0046002525,0.000022801638,0.0000040870955,0.00006789321,0.00011129289,0.00054462417,0.9912445,0.000099942656,0.00006515324,0.003117939],"study_design_scores_gemma":[0.000021418533,0.0005792708,0.026831744,0.000013888213,0.000022416332,0.00012609988,0.0004260726,0.0147201335,0.95586544,0.00014277056,0.0012177732,0.000032970936],"about_ca_topic_score_codex":0.0016320336,"about_ca_topic_score_gemma":0.001611794,"teacher_disagreement_score":0.0016320336,"about_ca_system_score_codex":0.0003472751,"about_ca_system_score_gemma":0.0001945924,"threshold_uncertainty_score":0.0032450557},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.54340917,0.00079624896,0.44486725,0.00053417723,0.00009904358,0.00009202026,0.00016157038,0.0008419174,0.009198591],"genre_scores_gemma":[0.96312654,0.00041970934,0.034710705,0.000042644344,0.00004490741,0.000030807445,0.000056836376,0.00016261013,0.0014052577],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998355,0.00007898433,0.0000093069175,0.00002290212,0.00003945345,0.000013881199],"domain_scores_gemma":[0.99891555,0.0007157721,0.00009766404,0.00012667397,0.000110022775,0.000034336015],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000565363,0.00068186445,0.00045610112,0.00039321464,0.00029437474,0.00080623495,0.00066388206,0.0011411981,0.0008470224],"category_scores_gemma":[0.003517338,0.00027195903,0.0004803872,0.0002963626,0.00069024536,0.0008843476,0.00054621714,0.00096145057,0.00023415747],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000114766604,0.00006487448,0.00077646674,0.0000616035,0.000015239632,0.00012187087,0.00006061506,0.9609122,0.024872279,0.004419285,0.00016812967,0.008412655],"study_design_scores_gemma":[0.0000030599638,0.000012184128,0.00015631002,0.0000028926981,0.0000026096393,0.0000052939295,0.0000028782513,0.9980202,0.0013102889,0.0004139906,0.000067728375,0.000002590378],"about_ca_topic_score_codex":0.0032937434,"about_ca_topic_score_gemma":0.0017990439,"teacher_disagreement_score":0.0032937434,"about_ca_system_score_codex":0.00020560395,"about_ca_system_score_gemma":0.00025467062,"threshold_uncertainty_score":0.0065491796},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.18421645,0.00020211503,0.8140403,0.00012537943,0.00005356516,0.00004078942,0.000014833258,0.0002511273,0.0010553729],"genre_scores_gemma":[0.9591216,0.00009540464,0.039672356,0.000026947175,0.000026528687,0.00003777779,0.000018949944,0.000035096706,0.0009653952],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99981135,0.00007282852,0.000009555648,0.000031430583,0.000053606753,0.000021270042],"domain_scores_gemma":[0.99940145,0.0003786001,0.00007897383,0.000026608834,0.00007924166,0.000035121586],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00072225794,0.00073985214,0.00047294344,0.00030298898,0.00036591673,0.0006144482,0.00065776083,0.0009580613,0.0002346872],"category_scores_gemma":[0.0017712312,0.000270391,0.0005371138,0.00010633361,0.00074267277,0.0006690842,0.0006543707,0.0005257427,0.000043849675],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00009007036,0.000052373995,0.001899285,0.000054279735,0.0000271806,0.00014051447,0.00012597739,0.9665003,0.015764138,0.0047405916,0.00009186226,0.010513395],"study_design_scores_gemma":[0.0000017643929,0.000026812964,0.00011501179,0.0000014701367,0.00000262276,0.000007202819,0.000005643398,0.9986369,0.0009209639,0.0002117092,0.000067467074,0.000002473288],"about_ca_topic_score_codex":0.0035998847,"about_ca_topic_score_gemma":0.0021185232,"teacher_disagreement_score":0.0035998847,"about_ca_system_score_codex":0.00032621023,"about_ca_system_score_gemma":0.00055167696,"threshold_uncertainty_score":0.007157862},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7569105,0.00068070245,0.14852686,0.0016150131,0.00024318713,0.0003554627,0.00013688215,0.0008047704,0.09072666],"genre_scores_gemma":[0.90605277,0.0003234184,0.048430834,0.0001986521,0.00007036668,0.00012690233,0.00009836683,0.00031151605,0.04438723],"study_design_codex":"design_other","study_design_gemma":"case_report","domain_scores_codex":[0.9987997,0.000466213,0.00004501667,0.00014661155,0.00039041642,0.00015208566],"domain_scores_gemma":[0.99868256,0.00084331323,0.000045858473,0.00014279812,0.00011057927,0.0001749262],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.001515738,0.0006159352,0.0003610286,0.0006050631,0.0033909418,0.0027011402,0.0012914268,0.0018754443,0.0083873905],"category_scores_gemma":[0.0029119705,0.00027009365,0.00046497228,0.0005389852,0.0021071646,0.0018763989,0.0032007848,0.0015659797,0.0013344772],"study_design_candidate":"case_report","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":[0.0020111839,0.0018739789,0.011466497,0.001633608,0.00011049934,0.03838572,0.23167267,0.028822284,0.1611281,0.115066886,0.01622769,0.39160094],"study_design_scores_gemma":[0.0002763969,0.0019930692,0.013400647,0.0005349302,0.00014305695,0.02327823,0.19700281,0.097644344,0.16034433,0.045976315,0.45913094,0.00027495302],"about_ca_topic_score_codex":0.0018373198,"about_ca_topic_score_gemma":0.0043549677,"teacher_disagreement_score":0.0083873905,"about_ca_system_score_codex":0.0008367813,"about_ca_system_score_gemma":0.0005525129,"threshold_uncertainty_score":0.028058589},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9875072,0.000074602955,0.009844126,0.00005542842,0.0000147769715,0.0000279847,0.00019287082,0.0001606598,0.0021222844],"genre_scores_gemma":[0.99619305,0.000029642664,0.0032268602,0.000013351113,0.0000030039555,0.0000141841965,0.00015511988,0.000016662603,0.0003480744],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999138,0.000013488487,0.0000062212735,0.00001564389,0.000029046467,0.000021769594],"domain_scores_gemma":[0.99973184,0.00010089399,0.000047586826,0.000020990516,0.000050717204,0.00004792896],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00026220232,0.0004967237,0.0004929543,0.00035741949,0.00048624747,0.0008761562,0.0006177771,0.00073994556,0.0008800409],"category_scores_gemma":[0.0005449239,0.00018323689,0.00056190195,0.00038112784,0.00044395425,0.00041684718,0.0003739767,0.00043173437,0.000101566766],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00017999491,0.0001371993,0.008487768,0.00003274776,0.000022472032,0.00020788814,0.000058187823,0.97654676,0.011183457,0.00040478737,0.0001551048,0.0025836064],"study_design_scores_gemma":[0.000015060428,0.00004139922,0.0019390373,0.000003003953,0.000003984307,0.0000080761165,0.000023974475,0.9970066,0.0008465612,0.00005400969,0.000050926472,0.000007307368],"about_ca_topic_score_codex":0.014898145,"about_ca_topic_score_gemma":0.008663683,"teacher_disagreement_score":0.014898145,"about_ca_system_score_codex":0.0006150836,"about_ca_system_score_gemma":0.00090018247,"threshold_uncertainty_score":0.029622853},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99401134,0.00021159834,0.004798699,0.000015373604,0.000013347688,0.000026041478,0.0001290856,0.000044133463,0.00075025356],"genre_scores_gemma":[0.99337703,0.00018735362,0.005620552,0.00001292793,0.0000063188018,0.000024068257,0.00013934985,0.000013196318,0.0006192161],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997137,0.000021126214,0.000019328612,0.00008100576,0.00011823285,0.00004659317],"domain_scores_gemma":[0.9995976,0.00009907408,0.0001250088,0.00005670376,0.000080984144,0.00004064844],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003860612,0.00023064809,0.00022218765,0.00020852352,0.0002539723,0.00032163088,0.00029971177,0.00037193781,0.0009392214],"category_scores_gemma":[0.0005094104,0.00011344502,0.00017663023,0.00032727214,0.00044625966,0.00028044696,0.00030999043,0.00030529712,0.000108744374],"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":[0.00012162647,0.000046837325,0.00053674914,0.0000401794,0.000002738893,0.000075261116,0.00005012678,0.00074201333,0.9964226,0.00016422807,0.000028743032,0.0017688845],"study_design_scores_gemma":[0.000021047532,0.0005895365,0.007280155,0.0000037073944,0.0000070698215,0.00013042171,0.00004666247,0.0077556954,0.9833002,0.000059523558,0.0007919675,0.000013998982],"about_ca_topic_score_codex":0.00056821265,"about_ca_topic_score_gemma":0.00042049825,"teacher_disagreement_score":0.0009392214,"about_ca_system_score_codex":0.00024739228,"about_ca_system_score_gemma":0.00023091324,"threshold_uncertainty_score":0.0031419992},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9513102,0.00043562808,0.047327545,0.00010790966,0.000031704,0.000054581436,0.00012010121,0.00023727461,0.00037505847],"genre_scores_gemma":[0.961616,0.00020118509,0.037679628,0.000036762918,0.0000111154495,0.00004296545,0.000034081528,0.00001298554,0.00036526137],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997868,0.00002377001,0.00001450693,0.000049567134,0.00009660249,0.000028628117],"domain_scores_gemma":[0.9995334,0.00020086837,0.00010505572,0.00003467034,0.00008816493,0.00003784066],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00032307004,0.0002777104,0.00030764277,0.00030927666,0.00015220825,0.00024546307,0.0003338502,0.00044339892,0.00040958682],"category_scores_gemma":[0.0007681703,0.00017096911,0.00010208604,0.0001433439,0.0005275619,0.0005671197,0.00035844365,0.00029165662,0.00008439467],"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":[0.000020535685,0.00001034379,0.00054451026,0.000019313948,0.0000012454825,0.000035748562,0.000039169663,0.00019264805,0.997592,0.00006325224,0.000014927992,0.0014662943],"study_design_scores_gemma":[0.000012930293,0.0003825371,0.009149124,0.000007538505,0.000010640775,0.00028973617,0.0001354164,0.017766774,0.9712244,0.00016957815,0.000826847,0.00002441712],"about_ca_topic_score_codex":0.00039921005,"about_ca_topic_score_gemma":0.00059325364,"teacher_disagreement_score":0.00044339892,"about_ca_system_score_codex":0.00018042857,"about_ca_system_score_gemma":0.00017356566,"threshold_uncertainty_score":0.0017085671},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9390106,0.0010237846,0.05041383,0.00018610928,0.00011552228,0.000090123765,0.0005657889,0.0020612173,0.006533091],"genre_scores_gemma":[0.9836025,0.00022372587,0.014744091,0.000024807512,0.000017255112,0.00003445276,0.00044596815,0.00008744461,0.00081976515],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993648,0.00013110804,0.00005682143,0.000106870924,0.0002749208,0.00006542477],"domain_scores_gemma":[0.99845004,0.0006590542,0.00015155415,0.00013604763,0.0005399739,0.000063301035],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0012615944,0.0009768956,0.0009022747,0.0011791661,0.0004833784,0.0009500735,0.00086369214,0.00077988126,0.0015149695],"category_scores_gemma":[0.002270499,0.00020467817,0.00061306887,0.0007845161,0.0006788724,0.0012821559,0.00039465554,0.0005024277,0.00035887858],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0030908785,0.0011270498,0.06887575,0.0009970778,0.000121715115,0.0019252317,0.0010850389,0.5924764,0.09082359,0.00584698,0.004252525,0.22937776],"study_design_scores_gemma":[0.000023781016,0.00038084135,0.010184108,0.000024181005,0.000016706588,0.00011831463,0.00020893225,0.9731203,0.0148700625,0.00017374316,0.0008349754,0.000044001055],"about_ca_topic_score_codex":0.00514449,"about_ca_topic_score_gemma":0.0035860247,"teacher_disagreement_score":0.00514449,"about_ca_system_score_codex":0.00047348568,"about_ca_system_score_gemma":0.0005015007,"threshold_uncertainty_score":0.010229051},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.13675672,0.00022020545,0.85799026,0.00024819758,0.000098822165,0.00005538591,0.000101531885,0.0019970424,0.002531782],"genre_scores_gemma":[0.78411317,0.00013426015,0.21329181,0.00009924697,0.00002493431,0.00007871759,0.00025693458,0.00016553512,0.0018353172],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99987805,0.000029344339,0.000007945456,0.00002731661,0.00003760647,0.000019633186],"domain_scores_gemma":[0.9996947,0.00014804357,0.000025319372,0.000030292687,0.00008118395,0.000020545673],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00060843246,0.00069797755,0.0004198998,0.00028500854,0.00025422522,0.00047426642,0.000576465,0.0006293896,0.0008725368],"category_scores_gemma":[0.0013402617,0.00030088905,0.0005946661,0.00018067098,0.0004066099,0.0004692882,0.00055380963,0.0009732841,0.0002057687],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00006063109,0.00004551117,0.0010151507,0.000036834845,0.000034809073,0.00007051738,0.000038321396,0.94991404,0.0073927566,0.0018531078,0.0004124005,0.03912593],"study_design_scores_gemma":[9.053929e-7,0.0000068554505,0.00004850982,9.7315e-7,0.0000010587761,0.0000024797703,0.0000015879868,0.9990508,0.0006773018,0.00013762215,0.000070686525,0.0000011705932],"about_ca_topic_score_codex":0.009479326,"about_ca_topic_score_gemma":0.006945229,"teacher_disagreement_score":0.009479326,"about_ca_system_score_codex":0.00041084504,"about_ca_system_score_gemma":0.0008524266,"threshold_uncertainty_score":0.0188483},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98400116,0.00024204265,0.013988595,0.00007210235,0.000025241512,0.00002356111,0.00021224908,0.00005357119,0.0013814407],"genre_scores_gemma":[0.99259263,0.00010992509,0.0062112627,0.000017842409,0.0000048032953,0.000022671002,0.00018293099,0.000009780572,0.0008480172],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998586,0.0000123036,0.000009121722,0.000021178967,0.00008533374,0.000013306434],"domain_scores_gemma":[0.99975127,0.00007556729,0.00003896056,0.000014411326,0.00010165704,0.00001817008],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024307382,0.00015431599,0.00012868179,0.00023951779,0.00018274572,0.00015412761,0.00017905119,0.00021015843,0.0013056739],"category_scores_gemma":[0.0003593817,0.00006738669,0.00012773956,0.000136203,0.00020796598,0.00015420406,0.00011347748,0.00018005737,0.0001727805],"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":[0.000057946996,0.000025516565,0.0008076728,0.000045242505,0.0000019964382,0.000027772534,0.000043094762,0.0020905603,0.99299204,0.000103134946,0.00007197316,0.0037330212],"study_design_scores_gemma":[0.000022572956,0.0011791677,0.0320649,0.000020791871,0.000012408351,0.00013200857,0.0002077876,0.079294614,0.88438606,0.00016558595,0.0024869654,0.000027134425],"about_ca_topic_score_codex":0.0005957843,"about_ca_topic_score_gemma":0.00074073434,"teacher_disagreement_score":0.0013056739,"about_ca_system_score_codex":0.00014963165,"about_ca_system_score_gemma":0.0001440545,"threshold_uncertainty_score":0.004367888},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.57201374,0.00041977302,0.41328055,0.00029670878,0.000100028745,0.00017024454,0.00034347683,0.00073009887,0.012645286],"genre_scores_gemma":[0.8218821,0.00017070782,0.17517738,0.000037247297,0.000008518419,0.00018039714,0.0001995297,0.00012959943,0.002214499],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99978906,0.00003192267,0.00001279383,0.000029643748,0.000112355054,0.000024188153],"domain_scores_gemma":[0.9995931,0.00016017778,0.00008337817,0.00005891173,0.00008456907,0.000019842484],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00053805334,0.00047227467,0.0003662792,0.00033855703,0.00026578442,0.0006431739,0.00037295843,0.00051806495,0.0011210936],"category_scores_gemma":[0.0008745052,0.00027249628,0.00046077013,0.00021707657,0.00033355594,0.00027146967,0.00036584123,0.00030775307,0.000244068],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000091070346,0.00011347169,0.0010866963,0.00023067786,0.000025077807,0.00014777074,0.0000972784,0.80193377,0.17173095,0.0021984866,0.00070128334,0.021643482],"study_design_scores_gemma":[0.000026208996,0.00028571175,0.0010352711,0.000016149283,0.000015318483,0.000079698526,0.000044271932,0.91448927,0.08049165,0.0004488957,0.0030452851,0.000022213355],"about_ca_topic_score_codex":0.00040449304,"about_ca_topic_score_gemma":0.00082512276,"teacher_disagreement_score":0.0011210936,"about_ca_system_score_codex":0.00034959454,"about_ca_system_score_gemma":0.0005939665,"threshold_uncertainty_score":0.0037504435},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9948309,0.00019601759,0.0019960967,0.00009449774,0.000044205168,0.000011703645,0.0000685332,0.000049502625,0.0027085315],"genre_scores_gemma":[0.99941456,0.00004238241,0.0001879271,0.000008053724,0.000006690801,0.000002396773,0.000021836557,0.000009267923,0.00030695274],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998567,0.000034038523,0.000008064913,0.000029012526,0.000035149682,0.000036977584],"domain_scores_gemma":[0.99913967,0.0005128653,0.00006435678,0.000046241767,0.00013652802,0.000100433645],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025216918,0.00041837234,0.0004956264,0.00049185054,0.00055698876,0.0005794521,0.000369729,0.0007749024,0.0010977717],"category_scores_gemma":[0.001366721,0.00020627846,0.00041647963,0.00016389483,0.0009323353,0.0006058687,0.00033800455,0.00042284472,0.000116079056],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0032601506,0.0008266994,0.018823905,0.00030613272,0.00013579532,0.003213279,0.00031622866,0.5536773,0.40262687,0.00315029,0.0010432586,0.012620085],"study_design_scores_gemma":[0.0000870133,0.00039178456,0.017008351,0.0000128628535,0.00004615498,0.00015643153,0.00013299147,0.94398665,0.037544373,0.00025343226,0.00032848376,0.000051420167],"about_ca_topic_score_codex":0.006274946,"about_ca_topic_score_gemma":0.0022559187,"teacher_disagreement_score":0.006274946,"about_ca_system_score_codex":0.00048031207,"about_ca_system_score_gemma":0.00027109543,"threshold_uncertainty_score":0.012476802},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9941398,0.000058250924,0.004608533,0.000018216231,0.000013079556,0.000015589403,0.00009688181,0.0000392513,0.0010104472],"genre_scores_gemma":[0.9984211,0.000032358323,0.0009999693,0.000006497508,0.000004392482,0.0000100819625,0.000058882626,0.00001097519,0.00045586118],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.999648,0.00008230363,0.000016584449,0.00008278113,0.00009790048,0.00007246388],"domain_scores_gemma":[0.9987452,0.0007960534,0.000085687796,0.00011731763,0.00018536084,0.00007026634],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00040782185,0.00044660966,0.00026279545,0.00024340478,0.000469027,0.00033071724,0.00047292543,0.0007831006,0.004593484],"category_scores_gemma":[0.0011325949,0.0002481991,0.00029174058,0.00020625563,0.00078719243,0.00046410732,0.00044850665,0.00053683564,0.00043789693],"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":[0.0016293462,0.00027772825,0.0022895546,0.00008203887,0.000017705132,0.00009391623,0.000095677635,0.0015036495,0.98989314,0.00013917562,0.00006494427,0.00391321],"study_design_scores_gemma":[0.00015054221,0.003182719,0.026569514,0.000013212268,0.000060558254,0.00016404974,0.00017701117,0.011826505,0.95736575,0.000073326235,0.0003940877,0.000022640686],"about_ca_topic_score_codex":0.00038567864,"about_ca_topic_score_gemma":0.00030585035,"teacher_disagreement_score":0.004593484,"about_ca_system_score_codex":0.0001585553,"about_ca_system_score_gemma":0.00014104896,"threshold_uncertainty_score":0.015366733},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.96740115,0.00024891502,0.022175433,0.000105800784,0.000060906128,0.000037363843,0.0004915592,0.00037549488,0.009103366],"genre_scores_gemma":[0.9947448,0.00007117829,0.0032911177,0.000010567124,0.0000116302235,0.000022515438,0.00023917134,0.00002495145,0.0015840579],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998907,0.000021626252,0.000007504616,0.000017188593,0.000042998847,0.00001996271],"domain_scores_gemma":[0.9997404,0.00013050601,0.000033395572,0.000018084796,0.00005667131,0.000020934522],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020441996,0.0004844257,0.00043201578,0.0005126076,0.00031034765,0.0007253589,0.00030369117,0.0005572633,0.0015595811],"category_scores_gemma":[0.00044112743,0.00014196814,0.00034365922,0.00037811196,0.00041326488,0.0004183418,0.00031963998,0.00039299933,0.00019257037],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0004991031,0.00042056077,0.016540535,0.00026786598,0.00009994501,0.0010343855,0.0003506139,0.8118735,0.1407017,0.0042156726,0.00160669,0.022389462],"study_design_scores_gemma":[0.000007517635,0.00004227426,0.0034293314,0.0000074595446,0.0000053854055,0.000022705774,0.000060922615,0.9882223,0.0075633316,0.00018714124,0.00043891274,0.000012701051],"about_ca_topic_score_codex":0.002762305,"about_ca_topic_score_gemma":0.0013869578,"teacher_disagreement_score":0.002762305,"about_ca_system_score_codex":0.00022610923,"about_ca_system_score_gemma":0.00021527224,"threshold_uncertainty_score":0.005492449},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9822733,0.00014740632,0.016084578,0.000027162469,0.0000064057194,0.000010864381,0.000022789349,0.00007092606,0.0013565733],"genre_scores_gemma":[0.99870753,0.0000516169,0.0010027157,0.000003280189,0.0000070609726,0.0000049792657,0.00001530951,0.000008881395,0.00019859147],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999058,0.00001591842,0.0000067941137,0.00001726706,0.00003598716,0.00001816213],"domain_scores_gemma":[0.99952614,0.00010092173,0.0001905079,0.000071203554,0.00006164834,0.000049602393],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002189816,0.00028670672,0.00018736477,0.00053522777,0.00024483644,0.00059911085,0.00022042554,0.00013213934,0.0003589121],"category_scores_gemma":[0.00085232296,0.00015460866,0.00019582364,0.00016197504,0.00058686995,0.0005554929,0.0003924095,0.0002890046,0.000053370575],"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":[0.00044471698,0.00022577042,0.032019187,0.00011060372,0.00008076214,0.0014671624,0.0007342094,0.22004521,0.6455854,0.062229767,0.00044765475,0.036609527],"study_design_scores_gemma":[0.000019382753,0.00016867311,0.057401266,0.0000061498563,0.000012688011,0.00023202664,0.00006164898,0.8764194,0.054781105,0.010364378,0.0004847422,0.000048622165],"about_ca_topic_score_codex":0.00064029044,"about_ca_topic_score_gemma":0.00028576877,"teacher_disagreement_score":0.00064029044,"about_ca_system_score_codex":0.00030375662,"about_ca_system_score_gemma":0.00012968016,"threshold_uncertainty_score":0.0022039413},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.06275515,0.0003005852,0.93091136,0.00017645047,0.00012070345,0.00002634841,0.00023210883,0.00037330957,0.0051038824],"genre_scores_gemma":[0.96062994,0.00019714433,0.0329509,0.00006667491,0.00004665476,0.00007583931,0.00048547218,0.00008367677,0.005463639],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998153,0.00005784196,0.000007787075,0.000034670687,0.0000598897,0.00002466561],"domain_scores_gemma":[0.9995981,0.00016931935,0.00004012083,0.00003567369,0.00013393648,0.000022871542],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00035599968,0.00046574464,0.0006772585,0.00031311216,0.00028734514,0.0006859413,0.0006555014,0.0010693077,0.0013659338],"category_scores_gemma":[0.0014938086,0.00034141153,0.0005604882,0.00034159143,0.0003314505,0.00074497575,0.0004892836,0.0008012212,0.0005405255],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000019605073,0.000011512717,0.00021263628,0.000010710317,0.000007739635,0.000019466388,0.00000597897,0.9941744,0.0008307714,0.0010742777,0.0002160252,0.0034168714],"study_design_scores_gemma":[4.8729265e-7,0.0000020463713,0.000024053916,5.7040796e-7,3.28841e-7,0.0000017583095,5.1037404e-7,0.9997675,0.000052320276,0.00011425565,0.000035559962,6.7668407e-7],"about_ca_topic_score_codex":0.00442034,"about_ca_topic_score_gemma":0.003228968,"teacher_disagreement_score":0.00442034,"about_ca_system_score_codex":0.0003178983,"about_ca_system_score_gemma":0.0005742312,"threshold_uncertainty_score":0.008789241},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9716257,0.0014831898,0.023990363,0.00008431442,0.00007522338,0.000071784256,0.00035220967,0.00018132353,0.0021359886],"genre_scores_gemma":[0.9814563,0.0008435129,0.014962564,0.00010143728,0.000034003584,0.000057333604,0.00029079916,0.000025801253,0.0022282475],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997689,0.000022785487,0.000015350675,0.0000483552,0.00012868812,0.000015848611],"domain_scores_gemma":[0.9995302,0.00019566955,0.00007386523,0.000020539745,0.00016168876,0.000018071682],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003039226,0.00020065719,0.00016679538,0.00069288135,0.00013830735,0.00030007144,0.00027940187,0.00040312187,0.0008465262],"category_scores_gemma":[0.00085191376,0.00012608671,0.00020528935,0.0003393393,0.00015451034,0.00040666398,0.00020753336,0.00042042029,0.00025798427],"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":[0.0002474883,0.00015685143,0.020643646,0.00015575523,0.00001794782,0.00016303794,0.00027880736,0.00079570955,0.93343735,0.00029531537,0.0003557975,0.04345243],"study_design_scores_gemma":[0.000025191659,0.0014210591,0.13061447,0.00005328346,0.000081997416,0.00091873005,0.00044981277,0.033178348,0.8277298,0.00041956417,0.0050179646,0.000089812456],"about_ca_topic_score_codex":0.00049372826,"about_ca_topic_score_gemma":0.0004648735,"teacher_disagreement_score":0.0008465262,"about_ca_system_score_codex":0.00011761487,"about_ca_system_score_gemma":0.000123444,"threshold_uncertainty_score":0.0028319359},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98804444,0.0001659853,0.009055453,0.0000290485,0.000034873196,0.000011513843,0.000047708123,0.00007887471,0.0025321806],"genre_scores_gemma":[0.9993094,0.00003767667,0.00048559182,0.0000043345008,0.0000021888932,0.0000027489666,0.00001923868,0.000008347737,0.00013045188],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997379,0.000033742002,0.000012272164,0.000044009543,0.000099802586,0.000072289404],"domain_scores_gemma":[0.9994375,0.0003136155,0.00006742639,0.00003984475,0.000091658614,0.000049926966],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025476608,0.00042526715,0.00032084718,0.00038139804,0.00029668372,0.0006273576,0.00020959332,0.00038373013,0.0007555237],"category_scores_gemma":[0.0014760765,0.00012867381,0.0002712521,0.00016298548,0.00042230112,0.00041709188,0.00035083355,0.0003274644,0.00015378278],"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":[0.0011036546,0.0001841074,0.032560267,0.00017009542,0.00004375821,0.0011212626,0.00027391588,0.66256815,0.27059186,0.0015198499,0.00029095472,0.02957216],"study_design_scores_gemma":[0.00003524727,0.0005993834,0.025652047,0.000044624976,0.000032034903,0.00026161456,0.00026820862,0.8608002,0.1108414,0.00035482223,0.0010574801,0.000052982858],"about_ca_topic_score_codex":0.0021111378,"about_ca_topic_score_gemma":0.0012595076,"teacher_disagreement_score":0.0021111378,"about_ca_system_score_codex":0.00022979027,"about_ca_system_score_gemma":0.00028023022,"threshold_uncertainty_score":0.0041977167},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.09045182,0.000112740796,0.9005539,0.00013630933,0.0000311245,0.000066711145,0.000091582995,0.00091977173,0.007636081],"genre_scores_gemma":[0.7357667,0.00007620702,0.26113987,0.00004885046,0.00001892649,0.00014333583,0.0001815167,0.00022168447,0.0024029198],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998305,0.00003800556,0.000005953279,0.000018207671,0.00009243127,0.00001481646],"domain_scores_gemma":[0.99973565,0.000104544306,0.00003153316,0.000045836397,0.00006258321,0.000019856978],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00038068992,0.00048442036,0.0004433425,0.000272581,0.00028134332,0.0005373893,0.0005541452,0.00049861404,0.0010718625],"category_scores_gemma":[0.0007777039,0.00025611676,0.0004071964,0.00017453085,0.0003622216,0.00041929563,0.0005588953,0.00043595626,0.00020547441],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00003250576,0.00003343535,0.00053838757,0.000024879333,0.000012195962,0.00003379291,0.000020988939,0.97742575,0.008962512,0.002432602,0.00022203065,0.010260999],"study_design_scores_gemma":[0.00000477016,0.0000070200654,0.00007184421,0.0000013266902,8.340522e-7,0.000004570767,0.000002318675,0.9983804,0.0010318897,0.00026751362,0.0002256548,0.0000019036265],"about_ca_topic_score_codex":0.0027266496,"about_ca_topic_score_gemma":0.0025106093,"teacher_disagreement_score":0.0027266496,"about_ca_system_score_codex":0.00036864972,"about_ca_system_score_gemma":0.0007983164,"threshold_uncertainty_score":0.005421579},"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":"methods","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.078673355,0.00015986137,0.9142063,0.00007750927,0.00013119861,0.00008155176,0.00045443818,0.004581276,0.001634517],"genre_scores_gemma":[0.3180734,0.00014703983,0.6771084,0.000063903324,0.000029790986,0.00010789575,0.0011515166,0.0015694976,0.0017486068],"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9991536,0.00013269014,0.00006628609,0.00020939171,0.00036751368,0.00007044298],"domain_scores_gemma":[0.9978746,0.00050938304,0.0005383354,0.00055094017,0.00047531616,0.00005133664],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0012994498,0.0010928784,0.000453351,0.0015299625,0.00072119257,0.0012601953,0.0010544669,0.0005562487,0.0019234171],"category_scores_gemma":[0.005207977,0.0005115219,0.00082128606,0.0010887998,0.00038227605,0.0007383628,0.000984428,0.0011934753,0.0007386481],"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":[0.000971427,0.00024975318,0.06459832,0.0003076194,0.00058688864,0.0003854971,0.0007079464,0.24755287,0.19671254,0.016083183,0.004192373,0.46765155],"study_design_scores_gemma":[0.000071221206,0.00018076425,0.02630999,0.00004924774,0.0001434313,0.00041371118,0.00014504483,0.7385917,0.20699635,0.0040798136,0.022822516,0.00019626923],"about_ca_topic_score_codex":0.0057866536,"about_ca_topic_score_gemma":0.006404234,"teacher_disagreement_score":0.0057866536,"about_ca_system_score_codex":0.0006125757,"about_ca_system_score_gemma":0.001326525,"threshold_uncertainty_score":0.011505961},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.026735887,0.00017844979,0.96895456,0.000095495976,0.000067908666,0.000022686025,0.000058261176,0.002274293,0.0016125409],"genre_scores_gemma":[0.67015684,0.00022804033,0.32730836,0.000120496785,0.000061386876,0.000071860646,0.00028230407,0.00023964139,0.0015310596],"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99957377,0.000101982216,0.000022181954,0.00006461195,0.00014324268,0.000094241084],"domain_scores_gemma":[0.9991868,0.00027023305,0.000055780907,0.0002529164,0.00016290668,0.000071337454],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00036916212,0.00049241347,0.00060281303,0.00037323462,0.00027833306,0.0009409021,0.00093595014,0.0004842085,0.002714091],"category_scores_gemma":[0.0017463388,0.00024530446,0.00036893538,0.0004038217,0.0004579629,0.0013747193,0.0022660247,0.0009830714,0.0010582196],"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":[0.0011174302,0.00034946264,0.0021316628,0.00018754616,0.0001065311,0.00039302945,0.00026014252,0.102294944,0.4182293,0.028769085,0.0070220004,0.43913886],"study_design_scores_gemma":[0.000023721335,0.00008290739,0.00033193588,0.00000895791,0.0000135239,0.00016919883,0.000047811503,0.93538475,0.053038236,0.008030926,0.0028457935,0.000022260043],"about_ca_topic_score_codex":0.0010071382,"about_ca_topic_score_gemma":0.0012312768,"teacher_disagreement_score":0.002714091,"about_ca_system_score_codex":0.00025392557,"about_ca_system_score_gemma":0.00073487987,"threshold_uncertainty_score":0.009079576},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.013317021,0.00010615148,0.9849857,0.0001290571,0.000021357784,0.000029786721,0.00007583324,0.00080644846,0.0005285891],"genre_scores_gemma":[0.52525866,0.0003999439,0.46766618,0.00033623393,0.00009249458,0.000259625,0.0009421086,0.0003104717,0.004734228],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997757,0.00005297507,0.000011375336,0.00006233672,0.00007528845,0.000022336555],"domain_scores_gemma":[0.9995065,0.00021749845,0.000055884757,0.00010583523,0.00008144518,0.000032794982],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0010104048,0.0007551756,0.0005925676,0.0004972751,0.00024809784,0.0006068277,0.001631931,0.001084918,0.0016131888],"category_scores_gemma":[0.0025327634,0.00040952003,0.0006172445,0.00044509387,0.00097290624,0.0015441754,0.0015430769,0.0016083469,0.000638686],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00014155533,0.00013764742,0.0011184312,0.00017036575,0.000079019315,0.00012978578,0.00012312281,0.7603289,0.03220815,0.013811707,0.0021435549,0.1896079],"study_design_scores_gemma":[0.000005811799,0.000020283758,0.000094430536,0.0000031590037,0.0000026738237,0.000017126356,0.0000064060027,0.99259067,0.0033160076,0.0035819442,0.00035519313,0.0000062541894],"about_ca_topic_score_codex":0.002461804,"about_ca_topic_score_gemma":0.0026920943,"teacher_disagreement_score":0.002461804,"about_ca_system_score_codex":0.0005291114,"about_ca_system_score_gemma":0.000993778,"threshold_uncertainty_score":0.005396664},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.44079912,0.00031101753,0.5352193,0.00035838241,0.0003005839,0.000097589116,0.00006589616,0.0009956543,0.021852463],"genre_scores_gemma":[0.9335045,0.00013461088,0.040810063,0.000099471144,0.000071296716,0.00006508867,0.000030644278,0.00009056112,0.02519371],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99979395,0.00003452586,0.000005225347,0.00006206049,0.00008144218,0.000022852475],"domain_scores_gemma":[0.99972683,0.00013490049,0.000029635457,0.000026154248,0.00005844103,0.000024017338],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002534996,0.0005735742,0.00022583648,0.00021294135,0.00027406166,0.0005950227,0.00023238841,0.00044611568,0.0043497314],"category_scores_gemma":[0.00044209685,0.00013849964,0.00020118614,0.00010234776,0.00040959226,0.00038749995,0.00033456233,0.00033462868,0.0005626002],"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":[0.0003972609,0.000092824375,0.00055204687,0.0000785389,0.00003133138,0.00022004187,0.0003028815,0.012434607,0.9017524,0.003968442,0.0006038472,0.07956583],"study_design_scores_gemma":[0.00012342985,0.0010074037,0.007172818,0.000034455417,0.00007188705,0.0004600023,0.0002040189,0.28431353,0.68666065,0.0017906608,0.018090453,0.00007066545],"about_ca_topic_score_codex":0.0009708548,"about_ca_topic_score_gemma":0.0011246284,"teacher_disagreement_score":0.0043497314,"about_ca_system_score_codex":0.00026018644,"about_ca_system_score_gemma":0.00017073093,"threshold_uncertainty_score":0.0145513415},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97343045,0.00025591863,0.020030415,0.00008034764,0.00013123144,0.00003809442,0.00016173885,0.00033272823,0.005539181],"genre_scores_gemma":[0.99494755,0.00011584874,0.0023521024,0.000018139046,0.000026365593,0.000016919934,0.00011596337,0.000061242405,0.002345794],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99953365,0.00015456058,0.00002091632,0.00007499508,0.00011080373,0.0001050304],"domain_scores_gemma":[0.9988813,0.00062672864,0.00006408581,0.00008922356,0.00019123332,0.00014744086],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00074393005,0.0006101883,0.00076713046,0.0005102954,0.00040372182,0.00049186085,0.00044758033,0.0007536494,0.0061349776],"category_scores_gemma":[0.0012242799,0.0003226336,0.00047197472,0.00035391198,0.00070007605,0.00042964297,0.0007262055,0.00036782352,0.0006105632],"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":[0.0069696363,0.00026093933,0.0037226148,0.0003216141,0.000057703157,0.0012385229,0.00038552933,0.026218424,0.9365667,0.002152527,0.00087678066,0.021229014],"study_design_scores_gemma":[0.00044104602,0.0025005972,0.038435616,0.00013605451,0.0001992003,0.0015704819,0.00034817136,0.21841738,0.7330184,0.001991267,0.0027849714,0.00015687432],"about_ca_topic_score_codex":0.00021545212,"about_ca_topic_score_gemma":0.00022251012,"teacher_disagreement_score":0.0061349776,"about_ca_system_score_codex":0.00026655613,"about_ca_system_score_gemma":0.00018322328,"threshold_uncertainty_score":0.020523548},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.13371745,0.00094139075,0.85701907,0.0010858326,0.0001809445,0.000036985984,0.00010893752,0.0011202889,0.0057891416],"genre_scores_gemma":[0.7548496,0.0009937683,0.22976466,0.00032266998,0.00028390327,0.000052399708,0.0001858438,0.00036663876,0.013180568],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9995442,0.00012855396,0.000021292015,0.00016461458,0.0000882076,0.0000531108],"domain_scores_gemma":[0.9991339,0.00034521942,0.00010443754,0.0002029301,0.00015571763,0.000057835125],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00075993594,0.00094181165,0.0008380932,0.00030339396,0.0003147847,0.0012818408,0.00046350557,0.001706525,0.0048878076],"category_scores_gemma":[0.0018937222,0.00062747323,0.00046764847,0.00034468886,0.0007400837,0.0021473854,0.00040255085,0.0006676367,0.0024483174],"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":[0.00055678585,0.00009076823,0.0025659627,0.00023507097,0.00012480274,0.00041388886,0.0002622441,0.020757468,0.8020865,0.0087891435,0.0017199717,0.16239744],"study_design_scores_gemma":[0.00019197605,0.00080241926,0.015141453,0.000100009034,0.00023160555,0.0043448266,0.00060971826,0.3735977,0.5566757,0.018819757,0.02930706,0.00017787237],"about_ca_topic_score_codex":0.0007395215,"about_ca_topic_score_gemma":0.0012961401,"teacher_disagreement_score":0.0048878076,"about_ca_system_score_codex":0.00020085645,"about_ca_system_score_gemma":0.00028452039,"threshold_uncertainty_score":0.016351402},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.989286,0.000078979094,0.009983684,0.000022541757,0.000014477637,0.000008049754,0.00001460827,0.00008490839,0.0005067281],"genre_scores_gemma":[0.9945326,0.00003229485,0.005078238,0.000009678472,0.0000064494293,0.000010455197,0.000017000071,0.000010189305,0.00030309852],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99976546,0.000043351327,0.0000151573795,0.00004894841,0.000085986154,0.000041144114],"domain_scores_gemma":[0.99922144,0.000257904,0.00025594753,0.00007528583,0.00010686303,0.00008256908],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024327388,0.00025175692,0.00027079112,0.00025182945,0.00024003013,0.00029551474,0.00026800996,0.00025003724,0.0007282683],"category_scores_gemma":[0.0008697349,0.00018445626,0.00011025431,0.00014728999,0.0003687009,0.00045244026,0.00032617355,0.00020136904,0.00013617806],"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":[0.00015627684,0.000050165625,0.0013018912,0.000045685254,0.0000063391135,0.00012284162,0.000087986,0.0055940244,0.9877658,0.00031194134,0.0000576424,0.004499454],"study_design_scores_gemma":[0.000029468827,0.0014054683,0.009251483,0.000012332962,0.000027216547,0.00020456748,0.0001298258,0.11152896,0.87557507,0.00030051067,0.0015113271,0.000023794068],"about_ca_topic_score_codex":0.00011568071,"about_ca_topic_score_gemma":0.0002290922,"teacher_disagreement_score":0.0007282683,"about_ca_system_score_codex":0.00019493965,"about_ca_system_score_gemma":0.00011683252,"threshold_uncertainty_score":0.0024363399},"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":"methods","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.016188808,0.0004632793,0.9760416,0.00013862533,0.00032011038,0.00014909961,0.00037903024,0.004099336,0.0022200705],"genre_scores_gemma":[0.12842962,0.00041309212,0.84412247,0.00022901375,0.000109070774,0.0009323728,0.0006209882,0.0007614095,0.024381975],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99940205,0.00015947597,0.000023102917,0.00014840657,0.00022796587,0.000039071947],"domain_scores_gemma":[0.9973578,0.0018176088,0.00008488618,0.0001358664,0.0005430537,0.000060688333],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0014249797,0.0011618503,0.0010507756,0.0006737406,0.00044343757,0.00085237174,0.001037259,0.0020365492,0.009983443],"category_scores_gemma":[0.0037596622,0.00081035105,0.00059101457,0.00038338278,0.0003912508,0.00071676227,0.0006852853,0.0017378771,0.0037916268],"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":[0.0009095994,0.00030926216,0.0027973047,0.0008079115,0.00033701604,0.0003468798,0.0003361061,0.40196574,0.07584973,0.0077264565,0.012464736,0.4961492],"study_design_scores_gemma":[0.0001040085,0.000059298603,0.0011099133,0.000029384964,0.000019897107,0.00009354656,0.000027265512,0.9805879,0.010859418,0.000622762,0.0064521683,0.00003440365],"about_ca_topic_score_codex":0.01178174,"about_ca_topic_score_gemma":0.009798092,"teacher_disagreement_score":0.01178174,"about_ca_system_score_codex":0.0004629267,"about_ca_system_score_gemma":0.0013956605,"threshold_uncertainty_score":0.033397973},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.752913,0.0010468068,0.2248583,0.00042744758,0.00023782058,0.00006249568,0.001344435,0.0049673677,0.014142339],"genre_scores_gemma":[0.9702985,0.00027498615,0.024325442,0.00005484199,0.000037930484,0.000056703913,0.00036488037,0.00042642446,0.0041603995],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99923825,0.00012627096,0.000028843668,0.00017739649,0.00034494052,0.00008430106],"domain_scores_gemma":[0.9969393,0.0023207774,0.00020650103,0.00014222974,0.0003210691,0.00007002472],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0008068844,0.0013074023,0.00041065784,0.0011854814,0.00028424815,0.0013074826,0.0005467688,0.0011536254,0.007551089],"category_scores_gemma":[0.0028607408,0.00038518241,0.00034705983,0.000801849,0.0005723736,0.0016251504,0.0004861189,0.0008882648,0.0013410961],"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":[0.003663153,0.00018194247,0.0074267294,0.00034607993,0.00008820822,0.00083532627,0.0015974205,0.027766619,0.7390972,0.0021318663,0.0021223016,0.21474318],"study_design_scores_gemma":[0.00015346518,0.0009367741,0.08850033,0.00006122473,0.00012945106,0.0013325149,0.0006898419,0.14979984,0.7448646,0.0022008368,0.011083502,0.00024774083],"about_ca_topic_score_codex":0.0015805892,"about_ca_topic_score_gemma":0.001275667,"teacher_disagreement_score":0.007551089,"about_ca_system_score_codex":0.0004390372,"about_ca_system_score_gemma":0.00020501412,"threshold_uncertainty_score":0.025260985},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99893636,0.000017184997,0.00066063285,0.000010287834,0.000004353269,0.000007838357,0.00003181958,0.000015367792,0.00031604327],"genre_scores_gemma":[0.99913234,0.00002350046,0.000624939,0.000006751584,0.0000017809366,0.0000051510556,0.00004799158,0.0000037960174,0.0001538077],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998932,0.000016537262,0.0000086850705,0.000017904813,0.000025915408,0.000037837457],"domain_scores_gemma":[0.999742,0.00009791473,0.00003998206,0.000020942538,0.000039751965,0.000059457143],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021807669,0.0004842401,0.00063645624,0.00033852377,0.0005382095,0.0008610057,0.00038839527,0.0006621251,0.00060040393],"category_scores_gemma":[0.0005558319,0.00019643533,0.0006023739,0.00025865616,0.0004352219,0.0003954144,0.0004715181,0.00044965802,0.00008009182],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0005023182,0.0004716523,0.04765767,0.000081555474,0.000087582244,0.0015533092,0.00018066286,0.8900442,0.0535796,0.00047939352,0.00015391991,0.0052081165],"study_design_scores_gemma":[0.00006118109,0.00039721094,0.013884778,0.000007783653,0.000031937212,0.000051817216,0.0002029502,0.9793426,0.005775019,0.00007489811,0.0001469713,0.000022810678],"about_ca_topic_score_codex":0.011344641,"about_ca_topic_score_gemma":0.006099519,"teacher_disagreement_score":0.011344641,"about_ca_system_score_codex":0.00039690558,"about_ca_system_score_gemma":0.00053503877,"threshold_uncertainty_score":0.022557199},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99207497,0.0000497097,0.0050799726,0.00004452924,0.000016510172,0.000010986205,0.00007509112,0.00011854459,0.0025296544],"genre_scores_gemma":[0.99923325,0.000016457867,0.00048502744,0.0000060867287,0.0000017210587,0.0000036302354,0.000025188352,0.000009894407,0.0002188664],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998417,0.000034234614,0.000005323187,0.000023793385,0.000044372013,0.000050505325],"domain_scores_gemma":[0.9995407,0.00029982795,0.000040903666,0.00002734573,0.000047041907,0.000044200046],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00029008256,0.0003768742,0.00045695686,0.00024112863,0.00035340423,0.00062826194,0.00045630633,0.0008153267,0.0015585774],"category_scores_gemma":[0.00097546383,0.00023631848,0.0003920263,0.00020495841,0.00066097133,0.0003800095,0.00047745,0.00043687838,0.0001504919],"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":[0.0002594954,0.00010956785,0.0067966473,0.000048986734,0.000020427662,0.00031093336,0.00006026672,0.96849835,0.020597178,0.00047288983,0.00011989777,0.0027052877],"study_design_scores_gemma":[0.000067909445,0.00029988925,0.006147037,0.000012312436,0.000021377315,0.000062199106,0.000082911385,0.97998834,0.0128842015,0.00016488411,0.00024714062,0.000021772436],"about_ca_topic_score_codex":0.006428264,"about_ca_topic_score_gemma":0.003394137,"teacher_disagreement_score":0.006428264,"about_ca_system_score_codex":0.0004127991,"about_ca_system_score_gemma":0.00052153465,"threshold_uncertainty_score":0.012781739},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9911157,0.000076434095,0.007793159,0.000015649068,0.000010018612,0.000008116166,0.00005130847,0.000098290846,0.0008313507],"genre_scores_gemma":[0.9982231,0.00004160204,0.0013961245,0.0000063428492,0.00000412173,0.0000076249903,0.000049349026,0.000022110444,0.00024953802],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998087,0.000032757005,0.0000063243433,0.000031448253,0.00008016482,0.00004053175],"domain_scores_gemma":[0.9996973,0.00013076002,0.000044265613,0.000032337117,0.00007824623,0.000017113896],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00033894114,0.00028344415,0.00026316504,0.000293325,0.00021529729,0.00030052607,0.00024055982,0.00026050542,0.0011179029],"category_scores_gemma":[0.00076810224,0.00017973591,0.00020943672,0.00017856748,0.00040272533,0.00033925864,0.000294322,0.00019304689,0.0002201777],"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":[0.0003886074,0.00010184487,0.028937286,0.00022448252,0.000023428605,0.00038263772,0.00033308228,0.06641892,0.86105454,0.0006482259,0.00033437685,0.04115256],"study_design_scores_gemma":[0.000031208,0.0011535273,0.18457474,0.00004390528,0.000074881085,0.00051782344,0.00052259205,0.17066796,0.63775533,0.00034442625,0.0042432314,0.00007036521],"about_ca_topic_score_codex":0.0005544027,"about_ca_topic_score_gemma":0.0005628735,"teacher_disagreement_score":0.0011179029,"about_ca_system_score_codex":0.00017534618,"about_ca_system_score_gemma":0.0001808485,"threshold_uncertainty_score":0.0037397742},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.00053670915,0.0003978464,0.0008070617,0.00037935103,0.00037838038,0.00013027048,0.0006299213,0.0008095604,0.99593085],"genre_scores_gemma":[0.0007428054,0.00025042382,0.0003912402,0.0002487218,0.00008785783,0.00006563864,0.0003562252,0.00016901948,0.99768794],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9992975,0.000044295655,0.00006404371,0.0002670685,0.00015570482,0.00017138723],"domain_scores_gemma":[0.99767333,0.0005424371,0.00012664971,0.00026034884,0.00058457215,0.0008126212],"candidate_categories":["insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.001241675,0.003236557,0.0020825455,0.0028458824,0.0030877553,0.0041208146,0.0035349089,0.006264429,0.9890912],"category_scores_gemma":[0.001630049,0.001340902,0.0015526577,0.0026377838,0.0028240306,0.005984907,0.0033749796,0.0030705843,0.9934187],"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":[0.0005018849,0.00031785088,0.0012780515,0.00079510023,0.00005675964,0.00039783874,0.00017335021,0.0006175006,0.0032518313,0.0062605864,0.42670617,0.5596431],"study_design_scores_gemma":[0.000076484015,0.00018270001,0.000949335,0.00040878684,0.000020071975,0.00050845486,0.0001874728,0.00027567468,0.00045658517,0.0008267824,0.9960758,0.00003184772],"about_ca_topic_score_codex":0.004414749,"about_ca_topic_score_gemma":0.0035520312,"teacher_disagreement_score":0.0109087825,"about_ca_system_score_codex":0.0011822917,"about_ca_system_score_gemma":0.0010197699,"threshold_uncertainty_score":0.015560031},"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":"other","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.27137527,0.0126360515,0.32018557,0.000795937,0.010246137,0.00030255746,0.0011561945,0.008413685,0.37488872],"genre_scores_gemma":[0.4950497,0.002694398,0.034617603,0.00025100325,0.00078105857,0.00008502931,0.0014600921,0.0010002323,0.46406096],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99976987,0.000019396062,0.000009121633,0.00007117529,0.00008564305,0.00004471434],"domain_scores_gemma":[0.9998374,0.000017546776,0.000015577489,0.00005575349,0.00004146904,0.000032138134],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020730887,0.00083402515,0.000756833,0.0006314234,0.00072323706,0.0020585319,0.0009720085,0.0009838458,0.032157987],"category_scores_gemma":[0.00035242332,0.0004382609,0.00046685516,0.00037418923,0.00059852586,0.0012752309,0.001435008,0.0014577231,0.012984674],"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":[0.0013270439,0.00036848092,0.0014051073,0.0004698398,0.000067230205,0.002334862,0.0005877979,0.023709971,0.4613871,0.13760008,0.033777997,0.33696452],"study_design_scores_gemma":[0.0003010568,0.0010462118,0.00919768,0.00021383008,0.00008032244,0.0019385659,0.00039028443,0.19787101,0.42334226,0.047204114,0.31817216,0.00024248105],"about_ca_topic_score_codex":0.000337944,"about_ca_topic_score_gemma":0.00044594624,"teacher_disagreement_score":0.032157987,"about_ca_system_score_codex":0.00027043093,"about_ca_system_score_gemma":0.00033514205,"threshold_uncertainty_score":0.10757917},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99957305,0.000028402806,0.000049587317,0.0000057186426,5.9747293e-7,0.0000050257054,0.000080804406,0.0000035838264,0.00025315967],"genre_scores_gemma":[0.99906975,0.000056263463,0.00021047141,0.000020899499,5.570441e-7,0.000007887165,0.00016997257,0.000002791097,0.00046143492],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.99985313,0.0000059168833,0.0000058093447,0.00004874693,0.00004578123,0.000040608997],"domain_scores_gemma":[0.9997533,0.000021499001,0.000050295293,0.000010445252,0.00011855865,0.000045824574],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001234745,0.00019784512,0.00024714024,0.0003284142,0.0007759616,0.0006003312,0.00030560346,0.00020925068,0.0004609441],"category_scores_gemma":[0.00022888523,0.00021490085,0.00021206525,0.00050361943,0.0005500577,0.0002724446,0.0002863876,0.0002951909,0.00008787552],"study_design_candidate":"observational","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":[0.00042401973,0.00008198961,0.37492326,0.000101307014,0.00007081656,0.00021282432,0.0014114904,0.0004293538,0.61279273,0.00006499658,0.00023867961,0.009248579],"study_design_scores_gemma":[0.0000036637089,0.00005585336,0.9865943,0.0000022139318,0.000014204184,0.000037918555,0.0005510292,0.00032036423,0.012070299,0.000009938575,0.00033339162,0.000006792713],"about_ca_topic_score_codex":0.4988862,"about_ca_topic_score_gemma":0.67327666,"teacher_disagreement_score":0.5011138,"about_ca_system_score_codex":0.0033853932,"about_ca_system_score_gemma":0.0014946304,"threshold_uncertainty_score":0.9919647},"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":"review","genre_gemma":"review","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"review","genre_consensus":"review","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0005331146,0.9683413,0.024416799,0.0005308524,0.0010638348,0.00004414841,0.00015959688,0.0001454258,0.0047649695],"genre_scores_gemma":[0.0027748104,0.96856,0.022600625,0.0006294469,0.0015351464,0.000071185656,0.0002457926,0.00006693526,0.003516025],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9988158,0.00015668293,0.0001718018,0.0002503323,0.0005650656,0.000040301184],"domain_scores_gemma":[0.99785644,0.0012130686,0.0001575558,0.00008294686,0.0006369325,0.000052985488],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0014727988,0.0011606219,0.0012387614,0.0036579117,0.00037116138,0.0014178089,0.0013735299,0.0015815714,0.00619826],"category_scores_gemma":[0.0024598062,0.0008774386,0.00084499543,0.0035495884,0.0006830661,0.002372007,0.000721196,0.0014902998,0.0063331304],"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":[0.00007479819,0.00006035954,0.00028682756,0.015300529,0.00008232621,0.00016804205,0.0000807938,0.0008985543,0.010617872,0.0030227962,0.021297447,0.94810957],"study_design_scores_gemma":[0.000014116469,0.00019324235,0.0018903532,0.004442991,0.00016639367,0.0029797782,0.0001002485,0.001861226,0.0077975327,0.0035744077,0.976845,0.00013464101],"about_ca_topic_score_codex":0.000993352,"about_ca_topic_score_gemma":0.0010475348,"teacher_disagreement_score":0.00619826,"about_ca_system_score_codex":0.00045421722,"about_ca_system_score_gemma":0.0010117192,"threshold_uncertainty_score":0.020735264},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.009359803,0.00005023797,0.00046062082,0.00033973428,0.00009733722,0.0018165774,0.98399943,0.00021425761,0.0036619783],"genre_scores_gemma":[0.14112388,0.0003554706,0.010826302,0.0018539184,0.0003058344,0.056461953,0.7285258,0.00066231535,0.059884556],"study_design_codex":"not_applicable","study_design_gemma":"observational","domain_scores_codex":[0.999086,0.00023165815,0.00018107505,0.00014967006,0.00021005694,0.0001415713],"domain_scores_gemma":[0.96666425,0.023226958,0.0029244518,0.0018628042,0.0041541145,0.0011673997],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0023396784,0.00082064106,0.0014972714,0.0014493142,0.0016465567,0.0010963886,0.0018980858,0.001358931,0.7276889],"category_scores_gemma":[0.036530174,0.0005904186,0.0012264217,0.0020231255,0.000307074,0.0017964501,0.000990332,0.0014387914,0.08394535],"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":[0.0040470003,0.004727765,0.026463015,0.0032014882,0.00021464012,0.00013597659,0.00041349418,0.0006386824,0.00009699596,0.00096386124,0.9100943,0.049002815],"study_design_scores_gemma":[0.049815938,0.008432219,0.67021906,0.0057180505,0.0010290567,0.0007975485,0.0037864428,0.00576034,0.0018077525,0.010079397,0.24204825,0.00050588365],"about_ca_topic_score_codex":0.014741725,"about_ca_topic_score_gemma":0.021177532,"teacher_disagreement_score":0.7276889,"about_ca_system_score_codex":0.0013994417,"about_ca_system_score_gemma":0.002696525,"threshold_uncertainty_score":0.38841867},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.021101857,0.00013552551,0.9685703,0.000052472253,0.000042780677,0.0000683501,0.00008180201,0.0005917852,0.0093551725],"genre_scores_gemma":[0.46322608,0.00040380048,0.52659744,0.00006410214,0.000047988266,0.00023670918,0.000348258,0.0004278763,0.008647755],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99975294,0.000060926275,0.000019172692,0.000045279154,0.00009187958,0.000029808401],"domain_scores_gemma":[0.9995029,0.00016274978,0.000041051637,0.000077815224,0.00018668255,0.000028763176],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00049164385,0.0006752875,0.0006276488,0.0008072535,0.0003795381,0.00092448207,0.001380705,0.00076466496,0.0028165837],"category_scores_gemma":[0.0014237846,0.0003050978,0.0006227045,0.0005277417,0.0004539724,0.00091533375,0.0009285693,0.00079239864,0.00058914814],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00011267775,0.000106914595,0.0017330509,0.00015155335,0.0000409582,0.00019873722,0.00019034575,0.8031396,0.029003205,0.08145705,0.0010933706,0.0827725],"study_design_scores_gemma":[0.0000065964005,0.00001681057,0.00012221272,0.0000035334256,0.0000018392075,0.000024001185,0.000009725854,0.9942517,0.0026087328,0.0014989009,0.001449448,0.000006378012],"about_ca_topic_score_codex":0.003958638,"about_ca_topic_score_gemma":0.0021557636,"teacher_disagreement_score":0.003958638,"about_ca_system_score_codex":0.0008680414,"about_ca_system_score_gemma":0.0008670374,"threshold_uncertainty_score":0.009422421},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9831238,0.000037601298,0.012796817,0.00003448785,0.00003179249,0.00014805446,0.0005544304,0.00017253746,0.0031005032],"genre_scores_gemma":[0.9878878,0.000035033525,0.0077674305,0.000032155225,0.000008030415,0.00009628465,0.00079503853,0.000035906964,0.0033422804],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99966323,0.000041545096,0.000016917258,0.00004672707,0.00019540242,0.0000361675],"domain_scores_gemma":[0.99905664,0.000159123,0.000054168824,0.00007677248,0.00051185774,0.00014138501],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005921571,0.0002628972,0.00022543162,0.00046052664,0.00044871066,0.00033609284,0.00057578576,0.00041130662,0.002669571],"category_scores_gemma":[0.00072539167,0.00013689412,0.00018897936,0.00026346731,0.0003372271,0.00028823302,0.00028206123,0.00035895608,0.00037702225],"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":[0.0011063665,0.0004823287,0.014085243,0.0001335548,0.000015527587,0.0005042325,0.00069680635,0.009039292,0.949203,0.00026767945,0.0008817754,0.023584235],"study_design_scores_gemma":[0.0004141649,0.011356946,0.32539198,0.00011608793,0.00008826704,0.0011567589,0.0025095434,0.09823345,0.549341,0.00047116808,0.0107341055,0.00018655542],"about_ca_topic_score_codex":0.002232044,"about_ca_topic_score_gemma":0.0033331173,"teacher_disagreement_score":0.002669571,"about_ca_system_score_codex":0.00015303952,"about_ca_system_score_gemma":0.00040898166,"threshold_uncertainty_score":0.0089306235},"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":"commentary","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"other","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0091396505,0.0031202147,0.00029123874,0.5721101,0.015137607,0.00041847778,0.004498994,0.00018798468,0.39509577],"genre_scores_gemma":[0.019205794,0.0013848293,0.00013617826,0.3791898,0.0017916614,0.00074230117,0.00072496576,0.00008739812,0.5967372],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.9990306,0.00023066299,0.000035696205,0.000120010045,0.00020137653,0.00038161018],"domain_scores_gemma":[0.9976502,0.00055095204,0.00010466934,0.000055239096,0.0009376395,0.0007013413],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.001222925,0.00037939864,0.00043947579,0.0006671911,0.0071320296,0.001991032,0.0008378964,0.0064219385,0.27279514],"category_scores_gemma":[0.0072028213,0.00039486142,0.0002296109,0.00093040784,0.00059404696,0.0026040124,0.001669239,0.005648606,0.0802249],"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":[0.000008198385,0.0000077910445,0.00036135875,0.000020455338,3.6879385e-7,0.00007231329,0.0006257009,0.0000027649783,0.000026022431,0.0005082528,0.9952538,0.0031128768],"study_design_scores_gemma":[0.000006057636,0.0000094291,0.0016497532,0.00010896743,8.4326695e-7,0.00010646859,0.0066993725,0.000017028298,0.000025581108,0.00028413834,0.9910857,0.0000066099115],"about_ca_topic_score_codex":0.024625208,"about_ca_topic_score_gemma":0.045849178,"teacher_disagreement_score":0.72720486,"about_ca_system_score_codex":0.0024454028,"about_ca_system_score_gemma":0.0039448803,"threshold_uncertainty_score":0.9125907},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0023264973,0.008820792,0.0005386268,0.0024406945,0.001965776,0.000011832889,0.0001117743,0.00007899227,0.9837051],"genre_scores_gemma":[0.01486569,0.010929618,0.00055872614,0.0012541915,0.00048016856,0.000016510643,0.00018743594,0.00007184177,0.9716357],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.9998559,0.000019932946,0.000006396497,0.00002330282,0.00006848453,0.00002588295],"domain_scores_gemma":[0.99989736,0.000027710907,0.0000058967694,0.000012825429,0.000028083903,0.000028129578],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00017666814,0.00031536954,0.00022971336,0.00076919876,0.0015008765,0.002889919,0.00034648986,0.0005324731,0.073685005],"category_scores_gemma":[0.00044973218,0.000097567085,0.00017833438,0.0011824972,0.00094966445,0.0015636218,0.00089673337,0.0007327058,0.031277556],"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":[0.00004099398,0.000052813502,0.0011575739,0.00041531769,0.0000042649503,0.00030908533,0.0061937803,0.00020707418,0.0013835832,0.21903487,0.4361882,0.33501253],"study_design_scores_gemma":[5.4896486e-7,0.000003992728,0.00044223852,0.000065444096,5.9926265e-7,0.000092382725,0.00082165137,0.000015984308,0.000077194025,0.0019729198,0.9965055,0.0000015489811],"about_ca_topic_score_codex":0.002840606,"about_ca_topic_score_gemma":0.009374386,"teacher_disagreement_score":0.926315,"about_ca_system_score_codex":0.00069711206,"about_ca_system_score_gemma":0.0008828596,"threshold_uncertainty_score":0},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.95264274,0.00024741597,0.044355705,0.00006274726,0.000081598766,0.000032689488,0.00012343969,0.00026988256,0.0021836944],"genre_scores_gemma":[0.99718434,0.00008278134,0.0021681744,0.000013854587,0.000005887251,0.000006566569,0.00013347616,0.000021962185,0.00038293915],"study_design_codex":"simulation_or_modeling","study_design_gemma":"observational","domain_scores_codex":[0.99948835,0.000052047268,0.000030608917,0.000110379486,0.00026619408,0.000052347885],"domain_scores_gemma":[0.99941635,0.00024871636,0.00008194187,0.00006473549,0.00016053801,0.00002782256],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000377549,0.0005582641,0.0003569426,0.0004463109,0.00024708017,0.0004735448,0.00030925957,0.00043037796,0.00046819574],"category_scores_gemma":[0.0014444442,0.0002267779,0.000733948,0.000376885,0.0004255159,0.00047857343,0.00033512898,0.00035105585,0.00021272706],"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":[0.0013756308,0.0002669142,0.06558958,0.00046281377,0.00010864305,0.0025906,0.0007726712,0.45636633,0.38922456,0.0018350703,0.0010540249,0.080353156],"study_design_scores_gemma":[0.000040756964,0.0007750602,0.0922257,0.000041737658,0.000085098305,0.0008093576,0.00018065359,0.80075926,0.10355686,0.0005249258,0.00090584636,0.00009472728],"about_ca_topic_score_codex":0.003609249,"about_ca_topic_score_gemma":0.0026765282,"teacher_disagreement_score":0.003609249,"about_ca_system_score_codex":0.0003786857,"about_ca_system_score_gemma":0.00024233425,"threshold_uncertainty_score":0.007176459},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9833068,0.00042507457,0.013442997,0.00007880156,0.00011296374,0.00015302633,0.00014621718,0.00013779194,0.002196232],"genre_scores_gemma":[0.98546416,0.00023124892,0.010665095,0.000052518943,0.000015804608,0.000036795805,0.00010862519,0.00003225084,0.0033934144],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.999361,0.000099432036,0.000045035184,0.00012421954,0.00029791816,0.00007244225],"domain_scores_gemma":[0.9989374,0.00039165272,0.0000616088,0.00011711036,0.00041435054,0.000077864934],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0009828144,0.00026730105,0.0006150077,0.00025519443,0.0007202571,0.0006095152,0.00074203213,0.0008038967,0.003021692],"category_scores_gemma":[0.0014356285,0.00020230933,0.00038094656,0.00030212078,0.0005283235,0.00062752113,0.0004879834,0.0003797156,0.0005056688],"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":[0.0012092063,0.0007895256,0.0025635886,0.0002924533,0.000021483698,0.0003938175,0.0005173768,0.002844147,0.9700207,0.0003582577,0.00042784822,0.020561537],"study_design_scores_gemma":[0.00029818554,0.01524635,0.020967692,0.00006735469,0.00016341697,0.00056874193,0.0008482134,0.025802618,0.92980874,0.00023707676,0.0059019374,0.00008968364],"about_ca_topic_score_codex":0.0011144711,"about_ca_topic_score_gemma":0.0014650611,"teacher_disagreement_score":0.003021692,"about_ca_system_score_codex":0.00024159855,"about_ca_system_score_gemma":0.00041332596,"threshold_uncertainty_score":0.0101085305},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.96610093,0.00033261522,0.030572506,0.00006829037,0.00006925223,0.000032410477,0.00021553549,0.00016620557,0.00244223],"genre_scores_gemma":[0.9865992,0.0003850385,0.011489565,0.000044622095,0.00002332829,0.000041785748,0.000098515105,0.000018360839,0.0012995533],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.9996568,0.000032593707,0.000013946159,0.00009961202,0.0001512621,0.00004586986],"domain_scores_gemma":[0.9997094,0.000104084356,0.000073237585,0.000024686035,0.00006660445,0.000021831149],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021189445,0.00036961463,0.00032050142,0.00028584423,0.00023683252,0.00037353238,0.0003974091,0.0005797731,0.0009851641],"category_scores_gemma":[0.00043735732,0.00019282373,0.00015722518,0.00025150503,0.00046076707,0.00044874678,0.00043277402,0.0005289869,0.00020213964],"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":[0.000040087016,0.000020621454,0.00068855094,0.000041701478,0.0000027838087,0.000054062046,0.00007727564,0.00012731283,0.9971814,0.00004124222,0.000023524579,0.0017015353],"study_design_scores_gemma":[0.000009332669,0.00025637055,0.009896293,0.000007362437,0.000019031057,0.00017239305,0.00022154777,0.004409822,0.9841706,0.000105310224,0.0007160457,0.000015854373],"about_ca_topic_score_codex":0.00043903972,"about_ca_topic_score_gemma":0.00081896805,"teacher_disagreement_score":0.0009851641,"about_ca_system_score_codex":0.00016435102,"about_ca_system_score_gemma":0.00011173243,"threshold_uncertainty_score":0.0032957196},"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":"methods","genre_gemma":"methods","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.44955295,0.0044885334,0.49066702,0.0013881867,0.0005791267,0.00017350867,0.00088683696,0.001208671,0.05105518],"genre_scores_gemma":[0.9046102,0.0009788582,0.087190315,0.00016766757,0.00009993106,0.00008965027,0.0002907124,0.00017620326,0.0063963654],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99971575,0.000043410197,0.000009753858,0.000064907355,0.00011410818,0.000052066513],"domain_scores_gemma":[0.99963164,0.00013543935,0.000043867767,0.000052489024,0.00008881516,0.000047728943],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003639261,0.00034891898,0.00066274137,0.00034696603,0.0004611087,0.0008362405,0.0004967859,0.00079001277,0.0017939566],"category_scores_gemma":[0.0011573166,0.00022573747,0.00068058,0.0003817762,0.0007701232,0.00083874195,0.0011079663,0.0009090205,0.00026913176],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00009103783,0.000069735725,0.0047998508,0.00018493985,0.00004343029,0.000759789,0.0002856714,0.78035325,0.06390848,0.11976791,0.0029526248,0.026783282],"study_design_scores_gemma":[0.000040065806,0.000052859585,0.0035247323,0.000032530927,0.000008745924,0.0002622419,0.000053933305,0.961161,0.009675836,0.013812353,0.011336611,0.000039053906],"about_ca_topic_score_codex":0.002036996,"about_ca_topic_score_gemma":0.0010343026,"teacher_disagreement_score":0.002036996,"about_ca_system_score_codex":0.0006683529,"about_ca_system_score_gemma":0.00087572547,"threshold_uncertainty_score":0.0060013533},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9926005,0.000096346055,0.006720678,0.0000092313,0.000019034838,0.00004550475,0.000095726005,0.000048929607,0.00036403918],"genre_scores_gemma":[0.9811023,0.00024946698,0.017234314,0.000030282949,0.00001795537,0.00013427556,0.0003636282,0.00003600616,0.00083173387],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9994797,0.00004391568,0.000053283056,0.00012982596,0.00020829908,0.00008503328],"domain_scores_gemma":[0.99939895,0.00011958762,0.00014197115,0.000091387556,0.00011985101,0.00012819898],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005356312,0.00047431595,0.0005294159,0.00035986645,0.00048443308,0.00074249937,0.00045113944,0.00050446816,0.001106819],"category_scores_gemma":[0.00063017826,0.00028425088,0.0003200065,0.00050885737,0.00055423816,0.00045258173,0.0006670248,0.00064308563,0.00015310623],"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":[0.00049140165,0.00036511183,0.0030763568,0.000096120566,0.000011385804,0.00033780577,0.00017322224,0.0029301073,0.9874737,0.00045078498,0.000058550188,0.0045353766],"study_design_scores_gemma":[0.00014778538,0.00616313,0.02916169,0.00003356517,0.000057340745,0.00047149492,0.00033059338,0.030692898,0.93075186,0.00032722644,0.0017442201,0.00011818186],"about_ca_topic_score_codex":0.00028656598,"about_ca_topic_score_gemma":0.0002635482,"teacher_disagreement_score":0.001106819,"about_ca_system_score_codex":0.00021281712,"about_ca_system_score_gemma":0.0002923317,"threshold_uncertainty_score":0.0037027001},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.69828856,0.00034950767,0.285064,0.00014771253,0.00004709282,0.000051084407,0.00013887865,0.00019124849,0.015721923],"genre_scores_gemma":[0.98818856,0.00006590951,0.00938911,0.000020735095,0.000008509943,0.000029802894,0.000054748725,0.000044951743,0.0021977392],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998907,0.000042749063,0.0000027949893,0.00001809883,0.000026129015,0.000019558942],"domain_scores_gemma":[0.9997569,0.00015475883,0.000016382315,0.000019252911,0.00004383119,0.0000089121695],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025530587,0.0006218378,0.0006932809,0.00019161466,0.0002975094,0.000518321,0.00030547965,0.00062585884,0.002183959],"category_scores_gemma":[0.00055464957,0.00022768245,0.000668523,0.00019485771,0.0002749536,0.0003291803,0.0003163838,0.00033968856,0.00021307824],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000099325975,0.000056427165,0.00039568346,0.000052817468,0.000024933317,0.0001292386,0.00003112135,0.9707898,0.022344887,0.00058105955,0.00017895922,0.005315799],"study_design_scores_gemma":[0.000005213265,0.000056541903,0.00048442825,0.0000021973683,0.0000102420245,0.000014636812,0.000019925568,0.99626726,0.002885673,0.00012327566,0.00012431954,0.000006299664],"about_ca_topic_score_codex":0.0020444053,"about_ca_topic_score_gemma":0.0015128743,"teacher_disagreement_score":0.002183959,"about_ca_system_score_codex":0.0001795968,"about_ca_system_score_gemma":0.00025336933,"threshold_uncertainty_score":0.0073060393},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98721784,0.00020293341,0.01013654,0.000030619405,0.00003486277,0.0000354057,0.00020340677,0.00029057363,0.0018478725],"genre_scores_gemma":[0.99450976,0.00009867618,0.0022360561,0.000028383174,0.000009060852,0.000012988965,0.00030404027,0.00007974984,0.0027212997],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9979882,0.00024787162,0.000111169364,0.00019509828,0.0011595383,0.00029809255],"domain_scores_gemma":[0.9939154,0.0021797637,0.00062002335,0.00047635616,0.0025433882,0.0002651596],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00069046486,0.0008978829,0.00065812643,0.0010836553,0.0003917569,0.00062991853,0.00062580424,0.0009155479,0.0044151535],"category_scores_gemma":[0.0034979708,0.0003790245,0.00058635254,0.00063324283,0.0005313754,0.0007709038,0.000578995,0.0006188001,0.0012900033],"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":[0.0019602405,0.0003334426,0.0089975,0.00019953183,0.00003391777,0.00081996014,0.00042703937,0.0061443197,0.9615212,0.00014247892,0.00030188088,0.01911852],"study_design_scores_gemma":[0.000039942715,0.0052034054,0.026593091,0.000024534906,0.000079123165,0.000776693,0.00029671373,0.008804838,0.95668966,0.00007799073,0.0013680577,0.000045962825],"about_ca_topic_score_codex":0.0009976584,"about_ca_topic_score_gemma":0.0011413628,"teacher_disagreement_score":0.0044151535,"about_ca_system_score_codex":0.00037992402,"about_ca_system_score_gemma":0.00016192086,"threshold_uncertainty_score":0.01477015},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.36549056,0.002787133,0.26204136,0.003929217,0.0025050454,0.0017712294,0.051388506,0.110050134,0.20003672],"genre_scores_gemma":[0.77858686,0.00063274417,0.13641125,0.0012018832,0.00038202744,0.0009816765,0.035366673,0.0055727735,0.040864095],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99864346,0.00023463118,0.000085469816,0.00032642452,0.0005294905,0.00018044814],"domain_scores_gemma":[0.99908626,0.00026698707,0.000085435175,0.00019883018,0.00021089,0.00015160313],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0037176814,0.0009510272,0.00095358666,0.0012282149,0.0011984252,0.0027850233,0.0012681874,0.0015826139,0.02607878],"category_scores_gemma":[0.0019411811,0.0008588527,0.00051288697,0.0015718266,0.0003614062,0.0015545882,0.0021604237,0.001136772,0.007615168],"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":[0.029062849,0.0012730934,0.04352247,0.0015043447,0.0008060987,0.0034104658,0.0019246313,0.032925084,0.4213905,0.032714903,0.15044338,0.28102222],"study_design_scores_gemma":[0.0062462883,0.0032498348,0.05316456,0.00032142282,0.0005320204,0.0012839857,0.0009855321,0.27314517,0.28418285,0.016966652,0.3591791,0.0007425769],"about_ca_topic_score_codex":0.0027414216,"about_ca_topic_score_gemma":0.0036427889,"teacher_disagreement_score":0.02607878,"about_ca_system_score_codex":0.0011098174,"about_ca_system_score_gemma":0.0015688901,"threshold_uncertainty_score":0.087242246},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.46729192,0.0003132183,0.50426507,0.0003388351,0.00010304512,0.0001913902,0.000111395064,0.00070858153,0.026676584],"genre_scores_gemma":[0.98929954,0.00007528834,0.0064956173,0.000020818838,0.000008666531,0.00008664743,0.000024859444,0.000013090016,0.0039755125],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998381,0.000027583053,0.000006447634,0.0000326287,0.000071123075,0.000024080975],"domain_scores_gemma":[0.9996923,0.00012358108,0.000058725393,0.000018612758,0.00007600703,0.00003069404],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00030292285,0.00040805072,0.00037106837,0.00024592597,0.00031563547,0.0006727707,0.0005109729,0.0005454313,0.0025938535],"category_scores_gemma":[0.00053360587,0.00019300473,0.00028874294,0.00009617209,0.0007317913,0.0003356159,0.0007126531,0.00039097882,0.00029373975],"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":[0.00064561743,0.00027240257,0.0030312233,0.00043157002,0.00010801163,0.00081338733,0.000906309,0.5758984,0.34070644,0.031114575,0.0012397373,0.044832215],"study_design_scores_gemma":[0.00003087367,0.0003757537,0.0009791387,0.00001405444,0.00001504786,0.00006749226,0.00006969397,0.985028,0.01067018,0.0014727565,0.0012574877,0.000019578702],"about_ca_topic_score_codex":0.0018364736,"about_ca_topic_score_gemma":0.00085240544,"teacher_disagreement_score":0.0025938535,"about_ca_system_score_codex":0.00028686557,"about_ca_system_score_gemma":0.0004196937,"threshold_uncertainty_score":0.008677304},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9966698,0.0000760258,0.0016173017,0.000036228168,0.000017545131,0.0000050160907,0.0000521713,0.00007660367,0.0014492257],"genre_scores_gemma":[0.9992816,0.000027628997,0.00032235731,0.000008667003,0.000003986987,0.0000019361564,0.000027497594,0.000015004273,0.00031140097],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99970144,0.000055052384,0.000015003164,0.000046771922,0.000075028984,0.00010665437],"domain_scores_gemma":[0.996141,0.0030143308,0.00019047296,0.00016129058,0.000286277,0.00020654949],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005699682,0.0002464158,0.00029884322,0.00028375996,0.00034521768,0.0004967173,0.00032186616,0.00051763473,0.0037783147],"category_scores_gemma":[0.0024696882,0.00030149522,0.00026494949,0.00018211083,0.00061505113,0.000487469,0.00048610268,0.0004142079,0.000399388],"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":[0.0049479925,0.0003119846,0.0061474643,0.0001927295,0.000027747052,0.0005537798,0.00033949583,0.041935008,0.92842984,0.00058616337,0.0004501655,0.016077604],"study_design_scores_gemma":[0.00009371403,0.0024666858,0.04374162,0.00003463173,0.00008895202,0.00027600117,0.00049203285,0.075062536,0.87670237,0.0001728539,0.0007734144,0.00009521904],"about_ca_topic_score_codex":0.00073960045,"about_ca_topic_score_gemma":0.0007505961,"teacher_disagreement_score":0.0037783147,"about_ca_system_score_codex":0.00021669504,"about_ca_system_score_gemma":0.00025747318,"threshold_uncertainty_score":0.012639701},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9979202,0.000038194707,0.0013776261,0.000014456665,0.00001103398,0.0000075237886,0.000033842927,0.000022730255,0.00057440053],"genre_scores_gemma":[0.9987264,0.000035917885,0.00064974226,0.000008095961,0.0000049164414,0.000005864546,0.000029608398,0.0000069151874,0.0005325778],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997663,0.000032852407,0.0000071952063,0.000045574874,0.000106062624,0.000042008935],"domain_scores_gemma":[0.99939215,0.00028612246,0.00009374622,0.000061573686,0.00010902665,0.000057350095],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020468209,0.00028519472,0.0002984483,0.0003054427,0.00029117038,0.00036502045,0.00038992582,0.0004636408,0.0012886751],"category_scores_gemma":[0.00075837364,0.00021151034,0.00021369981,0.00021394771,0.0007246189,0.00023206625,0.00038340065,0.0005629127,0.00017170819],"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":[0.00034045405,0.000018888551,0.0012092121,0.000018276953,0.0000077144105,0.00012879676,0.00012487649,0.00048127558,0.99607533,0.000047464986,0.00002198151,0.0015257953],"study_design_scores_gemma":[0.00004262824,0.0019001851,0.0717387,0.000013413365,0.000046967863,0.0002909996,0.00051511696,0.011156373,0.91348356,0.000105731626,0.0006709066,0.0000354894],"about_ca_topic_score_codex":0.0010069477,"about_ca_topic_score_gemma":0.00053862465,"teacher_disagreement_score":0.0012886751,"about_ca_system_score_codex":0.00019355041,"about_ca_system_score_gemma":0.00019445959,"threshold_uncertainty_score":0.0043110847},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.02115779,0.00029088825,0.9697687,0.000097305725,0.00004959805,0.000049899416,0.000095051546,0.00038399044,0.008106785],"genre_scores_gemma":[0.7947329,0.0011726837,0.17348512,0.00015634693,0.000080142054,0.00035157974,0.00031646763,0.00028445633,0.029420221],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99982136,0.000035554516,0.000009424047,0.000031166557,0.0000775756,0.0000249859],"domain_scores_gemma":[0.99971753,0.00011236865,0.00005203389,0.00002413656,0.00007685294,0.000017016755],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00032126805,0.00058961613,0.00058722304,0.00031636664,0.00038798526,0.0011116766,0.0015778029,0.00095636,0.0017109816],"category_scores_gemma":[0.00064801646,0.0005676941,0.00085635914,0.00026863595,0.0006703106,0.00078414456,0.0006575515,0.0010230708,0.000543807],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000027612878,0.000022321192,0.00035979602,0.000076215576,0.0000096975255,0.0001967789,0.00011055531,0.9655065,0.012929049,0.012902221,0.0004569384,0.0074023707],"study_design_scores_gemma":[0.0000033727868,0.000014543416,0.00006823586,0.000004049243,0.0000023820512,0.00003444559,0.000007823984,0.9976047,0.0006624727,0.00077882316,0.0008141994,0.0000048556917],"about_ca_topic_score_codex":0.003063769,"about_ca_topic_score_gemma":0.0016688172,"teacher_disagreement_score":0.003063769,"about_ca_system_score_codex":0.00061129837,"about_ca_system_score_gemma":0.00084790465,"threshold_uncertainty_score":0.0060918927},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.76572406,0.0005519478,0.1628374,0.00156999,0.0004859895,0.00010947525,0.0007510091,0.00093059556,0.06703957],"genre_scores_gemma":[0.97996587,0.0001122127,0.010375396,0.000103908715,0.000043232976,0.00006844291,0.00018987404,0.0000834532,0.009057645],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996965,0.00009101844,0.000010337437,0.000043503398,0.00008302306,0.000075547876],"domain_scores_gemma":[0.99678874,0.0025279708,0.00014593551,0.00009033912,0.00035154578,0.000095577234],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000587096,0.000697761,0.0008976202,0.00070704275,0.00076590583,0.001128747,0.0009504895,0.0035472347,0.005806343],"category_scores_gemma":[0.0029778343,0.00059765426,0.00089725904,0.00060724514,0.0013908097,0.000804453,0.0005215776,0.0013400026,0.00037885582],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000083867824,0.00003486346,0.0005909069,0.000033854172,0.0000145940985,0.000089271816,0.00003853436,0.99487215,0.0009885839,0.0018240834,0.00024792782,0.0011812635],"study_design_scores_gemma":[0.000017461352,0.000009694269,0.0001709051,0.0000032820708,0.0000023010298,0.0000086087375,0.000009898507,0.99921656,0.00029444884,0.00014725229,0.00011560147,0.0000039717715],"about_ca_topic_score_codex":0.042196568,"about_ca_topic_score_gemma":0.012721792,"teacher_disagreement_score":0.042196568,"about_ca_system_score_codex":0.0014658679,"about_ca_system_score_gemma":0.0011308343,"threshold_uncertainty_score":0.08390194},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9921748,0.0005380213,0.0027107724,0.000028106251,0.000038277645,0.000017348568,0.00022845525,0.00016163915,0.0041025174],"genre_scores_gemma":[0.99704736,0.00026555944,0.000688929,0.0000071506015,0.00000675124,0.0000065369086,0.00030894697,0.000025373169,0.0016432855],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997794,0.000017285207,0.000013635751,0.00004021461,0.00011858142,0.00003090674],"domain_scores_gemma":[0.9996761,0.00008412618,0.000030413354,0.000025529796,0.0001508546,0.000032948778],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002729745,0.00029610106,0.00033205363,0.0007836168,0.00027584028,0.0006004854,0.0005530419,0.00035337624,0.0034814305],"category_scores_gemma":[0.000545391,0.000090326976,0.00033668964,0.0005547305,0.00023866068,0.00047597202,0.0002264251,0.00024320524,0.00081419514],"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":[0.017926283,0.0008851109,0.022331353,0.001726364,0.0001720662,0.00080623664,0.00050845003,0.05920543,0.61066663,0.0015694915,0.0037752828,0.28042722],"study_design_scores_gemma":[0.000479097,0.018767102,0.12626687,0.00012212721,0.00033210128,0.0010797483,0.0008224949,0.10009149,0.7407272,0.00042284036,0.010700918,0.00018800818],"about_ca_topic_score_codex":0.0023872126,"about_ca_topic_score_gemma":0.0016460787,"teacher_disagreement_score":0.0034814305,"about_ca_system_score_codex":0.00032158184,"about_ca_system_score_gemma":0.00023859403,"threshold_uncertainty_score":0.011646509},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9956785,0.00080796634,0.0023773,0.00002065555,0.00002421899,0.000051532887,0.00012116901,0.000047622598,0.00087098946],"genre_scores_gemma":[0.9970035,0.00036493636,0.0021445055,0.0000216423,0.000006358797,0.000016446735,0.00012484418,0.000032218348,0.00028545465],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9989692,0.00018463047,0.000095399315,0.00020337496,0.00043984308,0.00010762686],"domain_scores_gemma":[0.99795985,0.001096059,0.00042196852,0.00012756747,0.0002954303,0.00009911042],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0008529473,0.00042100783,0.0005480045,0.0003161984,0.00022680084,0.0011790476,0.00036371264,0.0004163377,0.00071283686],"category_scores_gemma":[0.0034572936,0.00042024037,0.00030196813,0.00029226395,0.0003143061,0.0006270981,0.0003160606,0.00032740756,0.00016978172],"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":[0.0007846691,0.00007332899,0.0036132317,0.00015965817,0.000027477454,0.00028576076,0.000097103635,0.003488005,0.9858072,0.00012520066,0.000041335097,0.0054971008],"study_design_scores_gemma":[0.000078778445,0.002259627,0.055594955,0.00002394756,0.000091286594,0.00038859123,0.00011355612,0.008013435,0.93239635,0.0000904356,0.00088211143,0.00006694325],"about_ca_topic_score_codex":0.00055529864,"about_ca_topic_score_gemma":0.0005970135,"teacher_disagreement_score":0.0011790476,"about_ca_system_score_codex":0.00045543985,"about_ca_system_score_gemma":0.00025078023,"threshold_uncertainty_score":0.00451082},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9524173,0.0000684669,0.04527979,0.000026242977,0.000026028474,0.000020867905,0.000041102965,0.00015587965,0.0019643428],"genre_scores_gemma":[0.9977476,0.00001833437,0.0018790042,0.0000038865437,0.000002292698,0.000005008076,0.000020931062,0.000012217342,0.00031068551],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999362,0.000013246007,0.000002829095,0.00001092219,0.000020689607,0.000016048747],"domain_scores_gemma":[0.999739,0.000119521115,0.000038475973,0.000018823377,0.00005532678,0.000028869765],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002183074,0.00043037345,0.0002654208,0.00031649394,0.00020014816,0.0004713608,0.00039996658,0.00048341317,0.0006467902],"category_scores_gemma":[0.0006974579,0.00018424129,0.00035290155,0.000079565725,0.00033968483,0.0003800104,0.00021772287,0.0003046833,0.00010161336],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00009201212,0.00004165453,0.0026944366,0.000026302318,0.000008706427,0.00009338928,0.00003227567,0.98291034,0.010551142,0.00033938806,0.00007114771,0.0031391752],"study_design_scores_gemma":[0.0000026865748,0.000015030913,0.0004449075,8.605715e-7,8.943733e-7,0.000003897661,0.000004743858,0.9984434,0.0010265189,0.00003591603,0.000019387702,0.0000017632034],"about_ca_topic_score_codex":0.0039368747,"about_ca_topic_score_gemma":0.0027143634,"teacher_disagreement_score":0.0039368747,"about_ca_system_score_codex":0.00029776193,"about_ca_system_score_gemma":0.0003315374,"threshold_uncertainty_score":0.007827938},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9980059,0.00013270263,0.001231351,0.000016421844,0.000009159329,0.00004718037,0.00005059215,0.00003405678,0.0004726623],"genre_scores_gemma":[0.9959378,0.00016718215,0.001985787,0.000026823453,0.0000042268553,0.000030324223,0.00012030957,0.000012222451,0.001715373],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.9994728,0.00007342948,0.000019521145,0.00005072452,0.00029740614,0.00008618087],"domain_scores_gemma":[0.99947387,0.00007309238,0.000054944823,0.000023029781,0.0003234782,0.00005164651],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00048006905,0.0004495976,0.00028709267,0.0004716381,0.00040766614,0.00039612444,0.00043274264,0.000377834,0.0010680442],"category_scores_gemma":[0.0007550112,0.00011639961,0.0002354059,0.000222403,0.00022416146,0.00029561704,0.00030419856,0.00015248165,0.00020561689],"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":[0.0015327411,0.00045865166,0.012214759,0.00038219697,0.00002935506,0.0004132688,0.00048066076,0.0029712948,0.9457767,0.0000826391,0.0003962083,0.03526148],"study_design_scores_gemma":[0.000106379404,0.021010796,0.12858178,0.000057043293,0.00020904769,0.0006273716,0.0017858006,0.011820639,0.83068955,0.00006341321,0.0049927304,0.000055522916],"about_ca_topic_score_codex":0.007756116,"about_ca_topic_score_gemma":0.01338196,"teacher_disagreement_score":0.007756116,"about_ca_system_score_codex":0.00054747873,"about_ca_system_score_gemma":0.00045644748,"threshold_uncertainty_score":0.015421927},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.5503094,0.0006006,0.39869252,0.0007654287,0.00041266074,0.00047656993,0.0014484919,0.0016039523,0.045690432],"genre_scores_gemma":[0.9558948,0.00014019247,0.03977905,0.000045938785,0.000027672275,0.0001892334,0.00024181356,0.000051094452,0.0036302211],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997911,0.00003625778,0.000011570904,0.000039383955,0.000094913754,0.000026889253],"domain_scores_gemma":[0.99970055,0.00014006357,0.000023678504,0.000045506124,0.00007703354,0.0000132192135],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004212445,0.00042267086,0.00041019477,0.00038879408,0.0005524773,0.00087705784,0.0008591576,0.0006601775,0.0055384412],"category_scores_gemma":[0.00084929424,0.00021212186,0.0003609441,0.00028928192,0.0005149119,0.00057292706,0.0005151434,0.0005634215,0.0003975529],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0008290213,0.0014351803,0.0038032643,0.0005824196,0.00005625499,0.00025822618,0.00018892858,0.6907115,0.23688231,0.015600489,0.0024917382,0.047160722],"study_design_scores_gemma":[0.000054639808,0.00027293342,0.0009655727,0.000010044438,0.000014394388,0.000024289107,0.000060467602,0.9677555,0.028717682,0.0009594891,0.0011473717,0.000017661214],"about_ca_topic_score_codex":0.0025505023,"about_ca_topic_score_gemma":0.0019132292,"teacher_disagreement_score":0.0055384412,"about_ca_system_score_codex":0.00032632222,"about_ca_system_score_gemma":0.0006441511,"threshold_uncertainty_score":0.018527925},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9814897,0.00006325283,0.013805029,0.000037020065,0.000030867213,0.00006054623,0.0005970971,0.00023641212,0.0036800753],"genre_scores_gemma":[0.9862017,0.00007394554,0.0088805,0.000025586987,0.0000032321161,0.000058440368,0.0006526848,0.00004536767,0.0040585645],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996531,0.000021055183,0.000013971493,0.000063393636,0.00020937354,0.00003914585],"domain_scores_gemma":[0.99944097,0.00014553514,0.00004293813,0.00010039583,0.00023463498,0.000035573816],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00051369617,0.00035537477,0.00021069394,0.0004574585,0.0003498921,0.0003069967,0.00048768744,0.00043823165,0.0055942917],"category_scores_gemma":[0.00079906604,0.00018391044,0.0002687059,0.0002659725,0.00036981693,0.00033455246,0.00035065698,0.00039932804,0.0009628072],"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":[0.00030018308,0.00017904301,0.0050482573,0.00021204092,0.000012664288,0.00024974853,0.0005391575,0.012915684,0.9486785,0.00076820486,0.0010859533,0.03001052],"study_design_scores_gemma":[0.000032765915,0.0045192307,0.07344633,0.00008566068,0.00006648929,0.00041007303,0.0014999326,0.0552928,0.85064065,0.00039879346,0.013526671,0.00008063755],"about_ca_topic_score_codex":0.0012993767,"about_ca_topic_score_gemma":0.0034060096,"teacher_disagreement_score":0.0055942917,"about_ca_system_score_codex":0.00029495318,"about_ca_system_score_gemma":0.00025758293,"threshold_uncertainty_score":0.018714726},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.92394626,0.00020679577,0.06751679,0.00014175965,0.00015965194,0.0000935194,0.0013378015,0.0011820409,0.0054153535],"genre_scores_gemma":[0.96907693,0.00016923886,0.026239766,0.000085251275,0.000020302707,0.00005683851,0.0014189412,0.00009450171,0.0028381867],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99964714,0.000037903545,0.00001622964,0.000083730185,0.00018541062,0.000029617895],"domain_scores_gemma":[0.99968493,0.000060003884,0.000019654084,0.000044951677,0.00016333627,0.00002706855],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00035201284,0.0006215924,0.00047897524,0.0005092451,0.00023174497,0.0004179127,0.00039893045,0.0006412037,0.0019594326],"category_scores_gemma":[0.0007260522,0.00022244286,0.000352741,0.00036382896,0.00016643522,0.00038938312,0.00040197984,0.00044148054,0.0007716844],"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":[0.0004982789,0.00015198081,0.009851044,0.00015598502,0.0000483987,0.00038941664,0.00051134377,0.031094043,0.90361553,0.00045983956,0.0017371186,0.05148713],"study_design_scores_gemma":[0.0001642446,0.0029614174,0.14173849,0.00007663605,0.00021960841,0.0011224853,0.0006073606,0.35242626,0.4877282,0.000670804,0.0120245805,0.0002599291],"about_ca_topic_score_codex":0.0017240724,"about_ca_topic_score_gemma":0.002559501,"teacher_disagreement_score":0.0019594326,"about_ca_system_score_codex":0.0001822086,"about_ca_system_score_gemma":0.00024616971,"threshold_uncertainty_score":0.006554961},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8918874,0.0014473867,0.076244,0.00050046685,0.00025800132,0.00015074665,0.0012717049,0.0038511623,0.024389058],"genre_scores_gemma":[0.98443294,0.000228379,0.012559258,0.00003689131,0.000034086785,0.00009407616,0.00062542764,0.00031101424,0.0016780944],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99804485,0.00035478943,0.0001668394,0.00026567988,0.000987047,0.00018089134],"domain_scores_gemma":[0.9850594,0.008732703,0.00081653334,0.0020313119,0.0032325303,0.00012756878],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0023321174,0.00074961863,0.0006296815,0.0015618361,0.0007973823,0.0008316483,0.0013718911,0.0013557863,0.008024578],"category_scores_gemma":[0.016715076,0.00025572223,0.0005656082,0.0015708527,0.0011431,0.0010838045,0.0007026289,0.0009543788,0.00091446686],"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":[0.002390935,0.0023382325,0.014170476,0.0025905282,0.00019582578,0.00089925353,0.0019644632,0.18027437,0.61772186,0.018466035,0.005421874,0.15356608],"study_design_scores_gemma":[0.00013472445,0.0009833865,0.01997547,0.00017889039,0.000077558994,0.00039024264,0.00068660965,0.5469139,0.42093712,0.0033705072,0.0062143076,0.00013716459],"about_ca_topic_score_codex":0.00091090833,"about_ca_topic_score_gemma":0.00043656197,"teacher_disagreement_score":0.008024578,"about_ca_system_score_codex":0.00048715682,"about_ca_system_score_gemma":0.00031738594,"threshold_uncertainty_score":0.02684486},"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":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0006225703,0.0030066266,0.003589216,0.005082749,0.0143082235,0.0004985835,0.011017047,0.0025089358,0.959366],"genre_scores_gemma":[0.003277162,0.0027024716,0.0021963376,0.002682084,0.0032067206,0.00021587899,0.0092899995,0.00090532296,0.9755239],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.9988971,0.0001249649,0.00007085442,0.00025457324,0.0005447193,0.000107895736],"domain_scores_gemma":[0.9975936,0.00030585512,0.00011159013,0.0002966675,0.0012440799,0.00044831357],"candidate_categories":["insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.000806874,0.0009567937,0.0010384149,0.0022840623,0.00211222,0.0061735776,0.0021255387,0.0020239295,0.8181796],"category_scores_gemma":[0.0053919298,0.0004025898,0.0007529853,0.0019310116,0.0005692472,0.0033241366,0.003107655,0.0021149586,0.74654824],"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":[0.000026560681,0.00003805756,0.00022370848,0.0002629969,0.0000049072755,0.00007688315,0.000057533747,0.00011508203,0.00028783092,0.004817129,0.90647894,0.087610446],"study_design_scores_gemma":[0.0000030274891,0.000012288679,0.00016971231,0.00009697852,0.0000024665055,0.00007098721,0.00004318101,0.000042355547,0.00010146014,0.00090516586,0.99854785,0.000004393819],"about_ca_topic_score_codex":0.002603257,"about_ca_topic_score_gemma":0.0030035474,"teacher_disagreement_score":0.1818204,"about_ca_system_score_codex":0.0022552942,"about_ca_system_score_gemma":0.0032266714,"threshold_uncertainty_score":0.25934464},"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":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.13607268,0.022403847,0.10785061,0.05202566,0.044771392,0.0017021799,0.01654912,0.005660265,0.61296433],"genre_scores_gemma":[0.04294846,0.0024257943,0.008296802,0.0005698562,0.00063265563,0.0000923965,0.0031864606,0.00039889888,0.9414487],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.99927205,0.00006279423,0.000014503914,0.00010678348,0.0003163033,0.00022760103],"domain_scores_gemma":[0.9984037,0.00008294772,0.000021776284,0.00004376093,0.0011530453,0.00029476397],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0016166014,0.001292905,0.0010658554,0.00096591143,0.00374486,0.002634058,0.0014146988,0.0011780114,0.18896407],"category_scores_gemma":[0.0012230129,0.00042019293,0.0004231798,0.00067933416,0.0010075552,0.0005955909,0.0010528744,0.0011175899,0.05391226],"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":[0.0007250305,0.00030894,0.006369969,0.00018236747,0.000047818707,0.00046567473,0.00048440162,0.0020757648,0.014811645,0.002142488,0.83066165,0.14172432],"study_design_scores_gemma":[0.00007677712,0.00018496838,0.00905735,0.00010593645,0.000050849572,0.0002005587,0.00080479996,0.008719038,0.007730226,0.0008278986,0.97217137,0.000070377755],"about_ca_topic_score_codex":0.4790774,"about_ca_topic_score_gemma":0.82156014,"teacher_disagreement_score":0.4790774,"about_ca_system_score_codex":0.00795902,"about_ca_system_score_gemma":0.010779904,"threshold_uncertainty_score":0.9525777},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9972313,0.000037148948,0.0021525384,0.000005005351,0.0000040804744,0.00001039105,0.00007073802,0.0000454366,0.0004433624],"genre_scores_gemma":[0.9992698,0.000012821132,0.00047265488,0.0000019746592,0.0000020407192,0.000004482444,0.00008043727,0.000005214416,0.00015052229],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.9998871,0.000016980277,0.0000056613367,0.000019999989,0.000041331412,0.000028947383],"domain_scores_gemma":[0.99955815,0.000075493626,0.00009190496,0.00004282885,0.000117894815,0.00011381123],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024945292,0.00020397158,0.00022911796,0.00096486375,0.0002655,0.0003683174,0.000257128,0.00022275974,0.00070528255],"category_scores_gemma":[0.00046899708,0.00014406398,0.00014377483,0.0004695173,0.00039454157,0.00023460711,0.00025700373,0.00022285257,0.000106444],"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":[0.0034421633,0.0009787149,0.3602153,0.00028770146,0.00014162419,0.0051226323,0.0014827204,0.048402887,0.52363443,0.001882968,0.0011123873,0.0532965],"study_design_scores_gemma":[0.00006904695,0.00078230415,0.89699715,0.000030400208,0.000044585508,0.0011845188,0.00069599313,0.07147272,0.027646545,0.00030847845,0.0007144217,0.000053835294],"about_ca_topic_score_codex":0.0012556022,"about_ca_topic_score_gemma":0.0012922968,"teacher_disagreement_score":0.0012556022,"about_ca_system_score_codex":0.00014644818,"about_ca_system_score_gemma":0.00012754349,"threshold_uncertainty_score":0.0024966598},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99658126,0.000039193095,0.0027380313,0.0000056972376,0.0000048795,0.000011649895,0.00007656093,0.000053147083,0.0004895499],"genre_scores_gemma":[0.99921775,0.000013158206,0.00052244304,0.0000020687885,0.0000022367724,0.000004707438,0.00008185257,0.0000057151597,0.00015010178],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99987054,0.0000198689,0.000006677054,0.000022339205,0.000047307887,0.000033228414],"domain_scores_gemma":[0.9995009,0.000087255685,0.000099923476,0.00004954696,0.00013465692,0.00012767712],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002688476,0.00022464113,0.0002582481,0.0009674725,0.00027982253,0.00040693526,0.00027553565,0.00023855921,0.0007441722],"category_scores_gemma":[0.0005282563,0.00014449762,0.00015435631,0.0005289334,0.00043459883,0.00026113505,0.00027430765,0.00024065022,0.00010636343],"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":[0.0037633353,0.0010556966,0.36120838,0.00032812392,0.00014851922,0.0059345937,0.0015714883,0.06984774,0.49292225,0.0022035446,0.0012655468,0.059750747],"study_design_scores_gemma":[0.00008300095,0.0008705969,0.8612318,0.000034447967,0.000051732648,0.001263073,0.00084083487,0.10457668,0.029768052,0.00040807851,0.0008064162,0.0000652671],"about_ca_topic_score_codex":0.0013171597,"about_ca_topic_score_gemma":0.0012918832,"teacher_disagreement_score":0.0013171597,"about_ca_system_score_codex":0.00015683722,"about_ca_system_score_gemma":0.00014209503,"threshold_uncertainty_score":0.0026189685},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.96318907,0.00039322342,0.0238892,0.000174895,0.000057252335,0.00006925637,0.00009584095,0.00011985331,0.012011357],"genre_scores_gemma":[0.9953738,0.00009242401,0.0020112018,0.000011590262,0.000012425669,0.000009120443,0.000028600729,0.000012838443,0.002447868],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999833,0.000050015362,0.0000060202997,0.000025103798,0.00005115488,0.000034626],"domain_scores_gemma":[0.99938667,0.00032392473,0.00005681471,0.000031060154,0.00013424802,0.00006723129],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00041067763,0.0004473069,0.0005761401,0.00052826834,0.00067765353,0.000808404,0.0008592149,0.0008790972,0.0018265035],"category_scores_gemma":[0.0014791737,0.00025994718,0.0003921511,0.00035412493,0.0015911374,0.0008264388,0.00047063685,0.0005952984,0.000105700354],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0017077646,0.0009655862,0.0055586766,0.00036411226,0.00006234536,0.0019522004,0.00047069255,0.7768381,0.16859615,0.028531978,0.001017241,0.013935125],"study_design_scores_gemma":[0.000032157946,0.00020509989,0.0015935645,0.000010167178,0.0000062034646,0.00011070283,0.0000775554,0.99342006,0.0033726045,0.00091681484,0.0002393013,0.00001582422],"about_ca_topic_score_codex":0.0043845135,"about_ca_topic_score_gemma":0.0023866906,"teacher_disagreement_score":0.0043845135,"about_ca_system_score_codex":0.00040810206,"about_ca_system_score_gemma":0.000948436,"threshold_uncertainty_score":0.008718014},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9885451,0.00006573947,0.0077501526,0.0000387614,0.000036974117,0.00003303597,0.00019641947,0.00017730305,0.0031564685],"genre_scores_gemma":[0.9958995,0.000028061604,0.003229486,0.000010757332,0.000003837972,0.000023440803,0.00010568304,0.000021377682,0.0006779009],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997259,0.00004360345,0.000011592658,0.000039548457,0.00010571944,0.0000737181],"domain_scores_gemma":[0.999019,0.00048251014,0.00010681265,0.00008756198,0.00022554884,0.00007846744],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00035494828,0.0005560934,0.0005610393,0.0004516207,0.00038562954,0.00058024627,0.00062611274,0.0007436688,0.0017991712],"category_scores_gemma":[0.0017962586,0.00024018648,0.00047804066,0.00038002798,0.0005778229,0.00031335434,0.0005939507,0.0005494433,0.0001321314],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00020680667,0.00013542551,0.004494717,0.0000829291,0.000018691613,0.00016013521,0.00007440405,0.97757167,0.01299454,0.00053124805,0.00022899467,0.0035004609],"study_design_scores_gemma":[0.000041766023,0.00017136172,0.0022694285,0.0000069111416,0.000010682749,0.000028438093,0.000034808007,0.9901309,0.0069616186,0.000093749586,0.00023722481,0.000013081541],"about_ca_topic_score_codex":0.00928421,"about_ca_topic_score_gemma":0.004385844,"teacher_disagreement_score":0.00928421,"about_ca_system_score_codex":0.0006728153,"about_ca_system_score_gemma":0.0004949317,"threshold_uncertainty_score":0.018460333},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.92108047,0.00046386014,0.07358805,0.000088189496,0.00003522868,0.00006116105,0.00010142382,0.00038322096,0.0041983635],"genre_scores_gemma":[0.9351885,0.00021497323,0.060809586,0.000014571035,0.0000047002986,0.00003604276,0.00012456145,0.00007932784,0.0035277822],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99942553,0.00006943975,0.000021279318,0.00009661078,0.00032722863,0.000059889477],"domain_scores_gemma":[0.9992617,0.00031410024,0.00014486602,0.000091974754,0.00014854674,0.000038878028],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00096437806,0.0008260305,0.00043810363,0.00063174777,0.00030813206,0.0010441139,0.0004230336,0.0009000483,0.0016717678],"category_scores_gemma":[0.0015037855,0.00039640945,0.0005712555,0.00027981348,0.00044187251,0.00039722843,0.00027853958,0.00044893718,0.0004530056],"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":[0.00044284723,0.00025204007,0.009431714,0.0003009551,0.00005956794,0.0001798622,0.00018343808,0.40512666,0.50569904,0.0011101738,0.00041635742,0.076797396],"study_design_scores_gemma":[0.000053740077,0.0020205416,0.03589745,0.000049525577,0.00007498907,0.00028227048,0.00027177887,0.60350776,0.3525774,0.00025720807,0.004927779,0.00007963597],"about_ca_topic_score_codex":0.0042421934,"about_ca_topic_score_gemma":0.0047872043,"teacher_disagreement_score":0.0042421934,"about_ca_system_score_codex":0.0004915054,"about_ca_system_score_gemma":0.00071906997,"threshold_uncertainty_score":0.008434951},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9892819,0.000015637117,0.010178271,0.000009770454,0.0000057019583,0.000015054369,0.000052778545,0.00006935201,0.0003715732],"genre_scores_gemma":[0.9931657,0.000016015065,0.0064987885,0.000007243194,0.0000019168665,0.000019445373,0.0000514248,0.000007940358,0.00023162832],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9995505,0.00010813128,0.00003300552,0.00006412961,0.000195567,0.000048613947],"domain_scores_gemma":[0.9992562,0.0001900455,0.0000947683,0.00008662433,0.00028669668,0.00008555849],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006935744,0.00026792256,0.00019538552,0.0003922154,0.00027629329,0.00030999075,0.00035388465,0.0003883096,0.0003130038],"category_scores_gemma":[0.0011064153,0.00010648765,0.00011553002,0.00022903213,0.00032724717,0.0002585262,0.0004498027,0.00020020083,0.000070783506],"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":[0.00028104082,0.00012813511,0.010386961,0.00004545278,0.000012474138,0.0002245014,0.0004224656,0.007533849,0.96967334,0.00022600859,0.000065989254,0.010999837],"study_design_scores_gemma":[0.00007254662,0.0038751557,0.0779785,0.000033596712,0.000040792107,0.00065984845,0.0007997255,0.122765705,0.7923346,0.00017750844,0.0011602197,0.00010173456],"about_ca_topic_score_codex":0.0015155496,"about_ca_topic_score_gemma":0.0020255242,"teacher_disagreement_score":0.0015155496,"about_ca_system_score_codex":0.00014891173,"about_ca_system_score_gemma":0.00017935825,"threshold_uncertainty_score":0.0036680102},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9616566,0.00006661332,0.01585893,0.0001494562,0.000046536115,0.000091950664,0.000400969,0.00030702562,0.021422036],"genre_scores_gemma":[0.9904246,0.00003979398,0.0066945395,0.00002369355,0.000005600844,0.000050050014,0.0002801722,0.00003670604,0.0024448333],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997588,0.000041115793,0.000010874254,0.000029129447,0.00009290592,0.000067113826],"domain_scores_gemma":[0.9995079,0.0001620691,0.00005939477,0.000039274884,0.00017992698,0.0000515238],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004246097,0.00053693977,0.0004982494,0.00042481677,0.00068534276,0.0009914893,0.00077719823,0.0009165058,0.0020612825],"category_scores_gemma":[0.0013484881,0.00025971775,0.00061747956,0.00030735604,0.0005374426,0.00042777107,0.00053005514,0.00057284464,0.00036966804],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000073161165,0.000065054446,0.0027258864,0.000019221348,0.0000062945956,0.00011688323,0.000047766367,0.99102974,0.0025270204,0.0008209396,0.0002528415,0.0023151976],"study_design_scores_gemma":[0.000009699414,0.000032881704,0.0007145828,0.0000032853695,0.0000015827668,0.000008379362,0.000025382637,0.9984987,0.00054189085,0.000045556044,0.000113187656,0.0000049156206],"about_ca_topic_score_codex":0.048186827,"about_ca_topic_score_gemma":0.025503166,"teacher_disagreement_score":0.048186827,"about_ca_system_score_codex":0.0010052894,"about_ca_system_score_gemma":0.0014427099,"threshold_uncertainty_score":0.09581274},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97472316,0.00054776244,0.01842603,0.00010022526,0.000057349444,0.000063271465,0.0001700779,0.00012990576,0.005782168],"genre_scores_gemma":[0.99437594,0.0001893326,0.0021225058,0.000020434449,0.000013447445,0.000027760758,0.00012178025,0.000013248395,0.003115506],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9996829,0.000039833518,0.000011952917,0.000056908077,0.00017087531,0.000037620364],"domain_scores_gemma":[0.9997334,0.00010164243,0.000022168619,0.000012433831,0.0001172758,0.000013083516],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00039274112,0.0002903518,0.00033593492,0.00041436093,0.00034000285,0.0004040466,0.00034384962,0.00042020134,0.0022619534],"category_scores_gemma":[0.0005312807,0.00014827894,0.000268659,0.00021673946,0.0002378792,0.00025267215,0.00022603918,0.00021816239,0.00033462356],"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":[0.000617976,0.00023356613,0.032371633,0.0005403072,0.00008400918,0.0005248114,0.000893537,0.0534785,0.8101585,0.0011470191,0.0012267051,0.098723404],"study_design_scores_gemma":[0.000076656695,0.0021760832,0.25765187,0.00012949093,0.000118109005,0.0005956821,0.0014477153,0.42598355,0.2895747,0.0005937507,0.021534141,0.00011820039],"about_ca_topic_score_codex":0.003059115,"about_ca_topic_score_gemma":0.002903873,"teacher_disagreement_score":0.003059115,"about_ca_system_score_codex":0.00033345993,"about_ca_system_score_gemma":0.00035660143,"threshold_uncertainty_score":0.007567048},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.18923698,0.0008384251,0.78436667,0.00028829143,0.00017097357,0.00014039956,0.00026616565,0.00070699846,0.023985043],"genre_scores_gemma":[0.9342354,0.00069846946,0.052966118,0.00008766473,0.00006594111,0.0001772708,0.00040097488,0.00019438777,0.011173827],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99963,0.000074017946,0.000015858912,0.00007665121,0.00017318038,0.000030328418],"domain_scores_gemma":[0.999689,0.00011687836,0.000029485405,0.000022312583,0.00013007213,0.000012412416],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003170463,0.000704917,0.00046603085,0.00041460196,0.0005738203,0.0006005713,0.0007126334,0.0006247611,0.001478499],"category_scores_gemma":[0.0008258759,0.00023694366,0.0008364939,0.00032321733,0.00023744776,0.0008235227,0.00034544466,0.00038344256,0.0004304627],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00005883968,0.00006350345,0.0038929621,0.000121369354,0.000023382187,0.0002831638,0.00016317196,0.95454353,0.011486928,0.00598751,0.0010920733,0.022283511],"study_design_scores_gemma":[0.000003607872,0.000018045883,0.000382088,0.0000073062024,0.0000068324625,0.000036285117,0.00001570649,0.99735343,0.0010339222,0.0004153509,0.0007218174,0.0000056367685],"about_ca_topic_score_codex":0.018872393,"about_ca_topic_score_gemma":0.008706317,"teacher_disagreement_score":0.018872393,"about_ca_system_score_codex":0.00056185375,"about_ca_system_score_gemma":0.0008467016,"threshold_uncertainty_score":0.037525058},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.40062267,0.005914937,0.5435544,0.0012353325,0.0006148,0.00015650087,0.0006657446,0.0009903185,0.046245318],"genre_scores_gemma":[0.8833513,0.0016808306,0.10646981,0.00015141159,0.00013195425,0.00010381713,0.00028322174,0.0001781888,0.0076493947],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99972814,0.000048680955,0.000009648361,0.00006054215,0.00010544338,0.000047541922],"domain_scores_gemma":[0.99962735,0.00015600967,0.00004240736,0.000048333186,0.000080416874,0.00004544061],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00039471613,0.00036065,0.0007205843,0.00037639524,0.00041372588,0.00090135913,0.00048089505,0.0007789421,0.0017731055],"category_scores_gemma":[0.0011336802,0.0002288717,0.00072749594,0.00042137664,0.00082160934,0.000872139,0.0011067105,0.00090702757,0.00028954126],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00010047529,0.00007992291,0.0030342028,0.00025071093,0.000047780526,0.00058540836,0.00026370236,0.7767745,0.06633619,0.12067618,0.0023140393,0.029536892],"study_design_scores_gemma":[0.000045017718,0.000061500476,0.002237005,0.000035873803,0.000009963771,0.00026096866,0.000049227976,0.9563193,0.011191059,0.017890353,0.011862586,0.00003703459],"about_ca_topic_score_codex":0.001107608,"about_ca_topic_score_gemma":0.0005819516,"teacher_disagreement_score":0.0017731055,"about_ca_system_score_codex":0.0005334093,"about_ca_system_score_gemma":0.00076732785,"threshold_uncertainty_score":0.0059316754},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.25434184,0.003565038,0.66064143,0.0005144302,0.00052382407,0.00024537445,0.00022044512,0.0040330044,0.07591462],"genre_scores_gemma":[0.83602685,0.0007725117,0.095938735,0.00027876993,0.00015164092,0.00015400483,0.0003846654,0.001171249,0.06512156],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99937135,0.00009977218,0.000013475848,0.00006142496,0.00039927545,0.000054742013],"domain_scores_gemma":[0.999483,0.00023233551,0.000035962956,0.00006583424,0.00013891234,0.000043886936],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004990877,0.0008260801,0.00044875042,0.00043882485,0.00044547825,0.0007659635,0.0012968484,0.00078180246,0.008324103],"category_scores_gemma":[0.0006118235,0.0003735883,0.00036181882,0.00027615658,0.0004977427,0.00075606385,0.0010196402,0.0007733514,0.00262362],"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":[0.00044080854,0.00014380965,0.0006792332,0.00016157932,0.000020641106,0.0003585305,0.00031704316,0.0030282636,0.8880227,0.003843873,0.0028091818,0.10017433],"study_design_scores_gemma":[0.000076029326,0.0015514857,0.004738,0.00007990664,0.00006612154,0.0018515688,0.00018582166,0.050054714,0.90978986,0.0033506497,0.028176574,0.000079266894],"about_ca_topic_score_codex":0.00021221211,"about_ca_topic_score_gemma":0.0006900274,"teacher_disagreement_score":0.008324103,"about_ca_system_score_codex":0.00031016662,"about_ca_system_score_gemma":0.00020802942,"threshold_uncertainty_score":0.027846932},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9497388,0.0005475923,0.046738505,0.00014216993,0.00009323946,0.00040964,0.00016033069,0.00045633255,0.0017133569],"genre_scores_gemma":[0.9785534,0.000081421844,0.020344494,0.000034880577,0.0000065928643,0.00006959341,0.00006643182,0.00004073129,0.00080231146],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99750936,0.0004513771,0.00024846607,0.00034317022,0.0012347508,0.00021287888],"domain_scores_gemma":[0.99377304,0.0017739112,0.0012883055,0.0007092133,0.0019985207,0.00045697638],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0032134494,0.0005762019,0.00076914375,0.00065235974,0.00066706777,0.0009091699,0.0020989268,0.0014132902,0.0014351412],"category_scores_gemma":[0.006114105,0.0005256753,0.00041798205,0.00027804793,0.00081304385,0.0010438081,0.00095750054,0.00040727406,0.00027842197],"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":[0.0012037441,0.0007460398,0.021032317,0.00084524485,0.00006448224,0.0006280302,0.00069977593,0.040725566,0.8855249,0.0014162856,0.00055457203,0.04655906],"study_design_scores_gemma":[0.00067390694,0.0127462195,0.030454496,0.00013674208,0.00011893622,0.00077092834,0.00029052622,0.14703481,0.80239177,0.0005607345,0.0046843057,0.0001367512],"about_ca_topic_score_codex":0.0006465301,"about_ca_topic_score_gemma":0.00078356493,"teacher_disagreement_score":0.0032134494,"about_ca_system_score_codex":0.0010110514,"about_ca_system_score_gemma":0.0009542156,"threshold_uncertainty_score":0.016994536},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.059348054,0.0009420284,0.8970578,0.00021155846,0.000105788866,0.00008060259,0.00009897576,0.00037019636,0.04178493],"genre_scores_gemma":[0.7615796,0.0015227335,0.14656816,0.00011417353,0.00017588279,0.00010381669,0.00026462274,0.0004504665,0.08922064],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999238,0.00001216119,0.0000029204289,0.000012604292,0.000039529852,0.000008825511],"domain_scores_gemma":[0.999913,0.00003728584,0.000007238648,0.000010588932,0.000026580288,0.0000053461404],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015615975,0.00061605,0.0005323739,0.0003920332,0.00028436663,0.00085646764,0.0008272432,0.00078054634,0.0054098857],"category_scores_gemma":[0.00046027298,0.00022312556,0.0008063859,0.00021749755,0.00043431905,0.0006234968,0.00052387954,0.00054043205,0.0010136976],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00019736344,0.00010800338,0.0010370811,0.0005038007,0.00009249973,0.0013121472,0.0005273523,0.41250262,0.16900398,0.28221977,0.005640699,0.12685472],"study_design_scores_gemma":[0.000006625115,0.00003616826,0.00040269922,0.000015682266,0.000018877427,0.00032242015,0.000084518644,0.96851236,0.008817786,0.01748989,0.004279469,0.000013431995],"about_ca_topic_score_codex":0.00077790656,"about_ca_topic_score_gemma":0.0007513705,"teacher_disagreement_score":0.0054098857,"about_ca_system_score_codex":0.00032025247,"about_ca_system_score_gemma":0.0003042679,"threshold_uncertainty_score":0.018097878},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.08435283,0.00029757066,0.9083248,0.00008030964,0.00009647585,0.00008998698,0.000016010132,0.0002859281,0.0064561577],"genre_scores_gemma":[0.9532248,0.000086756576,0.045198362,0.000033866323,0.000025272057,0.000076779215,0.0000131489105,0.000020002293,0.0013210921],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998337,0.00003307153,0.000009959996,0.000034067423,0.00006191812,0.000027221495],"domain_scores_gemma":[0.9997912,0.000055150922,0.00004346613,0.000013878744,0.0000783594,0.000017990309],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025626406,0.0004867797,0.00041744925,0.0002778783,0.00038203705,0.00039565854,0.0005518726,0.00040652388,0.0010868147],"category_scores_gemma":[0.000376846,0.00018682833,0.00027524948,0.00011696852,0.00024049998,0.00029074072,0.0004408203,0.0002508319,0.0001578254],"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":[0.00058223493,0.00032813725,0.0012687584,0.00047005867,0.00010794073,0.0002277345,0.000233653,0.13380766,0.6907779,0.021023443,0.0009000815,0.15027238],"study_design_scores_gemma":[0.000058652768,0.00069482444,0.0010194774,0.000022181106,0.000058169033,0.000105026375,0.00002814875,0.94534355,0.046833668,0.001246856,0.004565146,0.00002422851],"about_ca_topic_score_codex":0.00038255547,"about_ca_topic_score_gemma":0.0007141396,"teacher_disagreement_score":0.0010868147,"about_ca_system_score_codex":0.00019428426,"about_ca_system_score_gemma":0.00022166267,"threshold_uncertainty_score":0.0036357045},"labels":[],"label_agreement":null}]}