{"meta":{"query_hash":"0b9248e7264f","filters":{"venue":"41st Aerospace Sciences Meeting and Exhibit"},"cohort_total":25,"direct_labels_cover":0,"predictions_cover":25,"exported":25,"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/0b9248e7264f","api":"https://metacan.xera.ac/api/v1/cohort?venue=41st+Aerospace+Sciences+Meeting+and+Exhibit"},"results":[{"id":"W1982499032","doi":"10.2514/6.2003-214","title":"An Iterative Inverse Design Method Based on Aerodynamic Streamline Equations","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Computational Fluid Dynamics and Aerodynamics","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":"Polytechnique Montréal","funders":"","keywords":"Aerodynamics; Computer science; Iterative method; Inverse; Applied mathematics; Mathematical optimization; Algorithm; Mathematics; Mechanics; Physics; Geometry","score_opus":0.024943207362417917,"score_gpt":0.2692730123914879,"score_spread":0.24432980502906995,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1982499032","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":[0.0015852441,0.00001727936,0.99727136,0.000014431016,0.000011511116,0.000025825699,0.000007192983,0.0001540761,0.00091301],"genre_scores_gemma":[0.0655446,0.00008571188,0.93003273,0.00003722396,0.000024932044,0.00030849816,0.000054743286,0.000103861326,0.0038076497],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99957746,0.00008004164,0.000019263707,0.000060434155,0.0002405846,0.000022144539],"domain_scores_gemma":[0.999635,0.00013007478,0.000039457733,0.00003619885,0.0001445902,0.00001474346],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006593196,0.00059034344,0.0007013592,0.0004539497,0.00037345066,0.0005993236,0.0008485702,0.0006784025,0.0032729823],"category_scores_gemma":[0.0012395491,0.00038851012,0.00066974544,0.000284214,0.00046058724,0.0006826606,0.00074739207,0.0008656824,0.0009384566],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0001082652,0.0000805139,0.00075334794,0.00032504954,0.000045675624,0.0001537547,0.0004054449,0.5907874,0.054157447,0.03736393,0.0022235382,0.31359553],"study_design_scores_gemma":[0.000022095901,0.000052611333,0.0000711963,0.000008822019,0.000007510908,0.00004715793,0.000008422101,0.98855907,0.004329391,0.0018635277,0.005019871,0.0000102521835],"about_ca_topic_score_codex":0.0019421328,"about_ca_topic_score_gemma":0.0019596256,"teacher_disagreement_score":0.0032729823,"about_ca_system_score_codex":0.00036429736,"about_ca_system_score_gemma":0.0011651265,"threshold_uncertainty_score":0.010949194},"labels":[],"label_agreement":null},{"id":"W2029081201","doi":"10.2514/6.2003-274","title":"A Newton-Krylov Algorithm for the Euler Equations Using Unstructured Grids","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Advanced Numerical Methods in Computational Mathematics","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 Toronto","funders":"","keywords":"Computer science; Euler's formula; Newton's method; Unstructured grid; Backward Euler method; Euler equations; Algorithm; Applied mathematics; Computational science; Mathematics; Grid; Physics; Mathematical analysis; Nonlinear system; Geometry","score_opus":0.06610549988179834,"score_gpt":0.3162599446095172,"score_spread":0.25015444472771886,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2029081201","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":[0.00044789995,0.00008368235,0.9971058,0.00004075141,0.000048447848,0.00005220353,0.000043873,0.000574384,0.0016030876],"genre_scores_gemma":[0.015335392,0.00024023639,0.9784266,0.00003767262,0.00004008758,0.0003434305,0.0002575633,0.000282277,0.005036748],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99942255,0.00008770526,0.0000331455,0.000050482322,0.00036657826,0.000039600345],"domain_scores_gemma":[0.99963343,0.00012233613,0.000034122244,0.000055979872,0.00012777824,0.000026382566],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005415745,0.0008990245,0.0010691544,0.0005908506,0.0009680884,0.0006770829,0.0013294487,0.00087157905,0.007979814],"category_scores_gemma":[0.0013850353,0.000473998,0.0007842694,0.0007468552,0.0005242327,0.0008331104,0.0017191122,0.0015851907,0.005001219],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00005636989,0.00009436128,0.0005055634,0.00042377203,0.000052337862,0.00027026146,0.00021218407,0.3703526,0.01380411,0.14535767,0.021003108,0.44786772],"study_design_scores_gemma":[0.000047748763,0.000054480013,0.00013036648,0.000037192163,0.000012200953,0.00017835118,0.000025320873,0.91271245,0.0043129353,0.026777254,0.05567739,0.00003429042],"about_ca_topic_score_codex":0.003069542,"about_ca_topic_score_gemma":0.003904152,"teacher_disagreement_score":0.007979814,"about_ca_system_score_codex":0.00045548193,"about_ca_system_score_gemma":0.0019159293,"threshold_uncertainty_score":0.026695132},"labels":[],"label_agreement":null},{"id":"W2120662324","doi":"10.2514/6.2003-1076","title":"Prediction of 2D Airfoil Ice Accretion by Bisection Method and by Rivulets and Beads Modeling","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Icing and De-icing Technologies","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":true,"ca_institutions":"Université du Québec à Rimouski; Université du Québec à Chicoutimi","funders":"","keywords":"Airfoil; Bisection method; Computer science; Geology; Mechanics; Algorithm; Physics","score_opus":0.023125540143809017,"score_gpt":0.23217671641352225,"score_spread":0.20905117626971323,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2120662324","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.73294085,0.0005692983,0.25643986,0.00026581515,0.00009597761,0.00008828171,0.00050764653,0.00092535693,0.008167002],"genre_scores_gemma":[0.96930736,0.0002070308,0.028565824,0.000029447676,0.000021095158,0.00007622856,0.00026648157,0.00009201245,0.0014344796],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99988186,0.000034615477,0.000006552867,0.000023360211,0.000030386733,0.000023233039],"domain_scores_gemma":[0.99964213,0.00016093686,0.000058420974,0.000026189095,0.000064416665,0.000047891946],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00026062987,0.00076724746,0.0005423661,0.00063123624,0.00041208018,0.0008378772,0.0006929867,0.0011920922,0.0007878938],"category_scores_gemma":[0.00091057696,0.00036789262,0.00074714347,0.00033832,0.00038899746,0.00052485365,0.00052616454,0.00051945564,0.00021344525],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000035016008,0.000017178763,0.0013038302,0.000013685187,0.000010875369,0.000036147732,0.000021227024,0.99419135,0.0013113891,0.00045481283,0.0001009338,0.0025036344],"study_design_scores_gemma":[0.0000016466415,0.0000031941775,0.00008187063,8.506649e-7,6.525646e-7,0.0000016505389,0.0000017139581,0.9996965,0.00013495583,0.000033062926,0.00004261329,0.0000012995656],"about_ca_topic_score_codex":0.022171257,"about_ca_topic_score_gemma":0.0067409365,"teacher_disagreement_score":0.022171257,"about_ca_system_score_codex":0.00065202714,"about_ca_system_score_gemma":0.00062308804,"threshold_uncertainty_score":0.04408443},"labels":[],"label_agreement":null},{"id":"W2126116164","doi":"10.2514/6.2003-163","title":"Fluid Flow and Heat Transfer From a Pin Fin: Analytical Approach","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Fluid Dynamics and Vibration Analysis","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 Waterloo","funders":"","keywords":"Fin; Heat transfer; Flow (mathematics); Mechanics; Fluid dynamics; Heat transfer fluid; Computer science; Materials science; Mechanical engineering; Physics; Engineering","score_opus":0.016502883062468693,"score_gpt":0.2104509164603527,"score_spread":0.193948033397884,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2126116164","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":[0.056117117,0.0073799496,0.9076784,0.00022624247,0.0002870501,0.00016434237,0.00011026924,0.00042199367,0.027614595],"genre_scores_gemma":[0.7836977,0.008778214,0.17807731,0.00016605663,0.00021473652,0.00030939106,0.000120822246,0.000094629926,0.028541094],"study_design_codex":"simulation_or_modeling","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.9998598,0.000025628317,0.000005042877,0.000028660257,0.00006178224,0.000019172036],"domain_scores_gemma":[0.99988127,0.000053094067,0.000014767162,0.0000120296845,0.000034228982,0.000004553439],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00027170012,0.00054409576,0.0005282626,0.00081958604,0.00050230534,0.0007395934,0.00086908374,0.0007478159,0.0025299909],"category_scores_gemma":[0.0008835942,0.00028498218,0.00045371216,0.00057212845,0.00081107335,0.0014615649,0.00045590458,0.00051883137,0.000496452],"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":[0.000110061424,0.00015812293,0.0009459009,0.0011298119,0.000037672537,0.0006440415,0.00046489766,0.61135393,0.12235896,0.1676088,0.0017599082,0.093427904],"study_design_scores_gemma":[0.0000126686145,0.00012398553,0.00043778348,0.000039965445,0.000012892095,0.00036981798,0.00012529973,0.9567577,0.013848284,0.020759376,0.007474972,0.00003720666],"about_ca_topic_score_codex":0.0019326564,"about_ca_topic_score_gemma":0.0011841417,"teacher_disagreement_score":0.0025299909,"about_ca_system_score_codex":0.0005107119,"about_ca_system_score_gemma":0.00072434073,"threshold_uncertainty_score":0.008463621},"labels":[],"label_agreement":null},{"id":"W2138396290","doi":"10.2514/6.2003-159","title":"Conduction Shape Factor Models for 3-D Enclosures","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Icing and De-icing Technologies","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":"Factor (programming language); Computer science; Programming language","score_opus":0.05498692074689601,"score_gpt":0.2478396116037393,"score_spread":0.19285269085684328,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2138396290","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":[0.022620402,0.00026399625,0.96726346,0.00008602944,0.00003987093,0.000041691394,0.00012945622,0.00059649674,0.008958624],"genre_scores_gemma":[0.8408931,0.0012487333,0.13031456,0.00012748112,0.000067338835,0.00036966772,0.00048067857,0.00056474184,0.025933806],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99959475,0.0000521903,0.000019990974,0.00006604277,0.00021544799,0.0000515298],"domain_scores_gemma":[0.9991818,0.000334256,0.0001215171,0.00009751461,0.00022705043,0.000037935868],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00048645682,0.000905324,0.00068047165,0.00068866677,0.00048287297,0.0011312988,0.0018060474,0.0014927996,0.0025609306],"category_scores_gemma":[0.0019141419,0.0005697563,0.0014721343,0.00041732116,0.0007216632,0.0011546352,0.00064117165,0.00074080063,0.0013539052],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000015147049,0.000007973565,0.0002268404,0.000019574203,0.0000047582103,0.000048291262,0.00004850954,0.9862191,0.0033895345,0.0055525205,0.00030879377,0.004158999],"study_design_scores_gemma":[0.0000027927806,0.000008026531,0.000089231486,0.0000054709462,0.0000029125333,0.00003422676,0.0000067891015,0.9962186,0.0010461065,0.0014024989,0.0011754582,0.000007952849],"about_ca_topic_score_codex":0.0044748923,"about_ca_topic_score_gemma":0.0028770443,"teacher_disagreement_score":0.0044748923,"about_ca_system_score_codex":0.0012526625,"about_ca_system_score_gemma":0.000755185,"threshold_uncertainty_score":0.009088755},"labels":[],"label_agreement":null},{"id":"W2313230181","doi":"10.2514/6.2003-1038","title":"Experimental Investigation of Performance Characteristics of Small Loop Heat Pipes","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Heat Transfer and Boiling Studies","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":"Carleton University","funders":"Goddard Space Flight Center","keywords":"Loop (graph theory); Materials science; Computer science; Mathematics","score_opus":0.02781259421456956,"score_gpt":0.21869803503201035,"score_spread":0.1908854408174408,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2313230181","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9966102,0.000072411494,0.0026857182,0.000018980661,0.000010465076,0.000016325086,0.000084458276,0.00009197291,0.0004093617],"genre_scores_gemma":[0.9987086,0.000035178666,0.00058628124,0.000005197361,0.000008185118,0.000012206237,0.000084477484,0.000026559035,0.00053328765],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99950624,0.00010355306,0.000022510589,0.000105962354,0.00014303015,0.00011868952],"domain_scores_gemma":[0.99723285,0.0015119604,0.00029101456,0.00033464888,0.00048712207,0.00014240097],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00057615276,0.0005937011,0.00041435324,0.00032884657,0.0005455995,0.00034789377,0.00073829165,0.0008604103,0.0029057167],"category_scores_gemma":[0.0022439866,0.00031434893,0.0002834101,0.00033751465,0.00064773153,0.0008585799,0.0004068532,0.00049024576,0.00036443822],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0017295395,0.00033652995,0.0013916073,0.000092497605,0.000013565061,0.00005976903,0.00014937422,0.001835716,0.99091536,0.00011999293,0.000089727626,0.0032663206],"study_design_scores_gemma":[0.00008890443,0.005006477,0.007674366,0.0000072949715,0.000030605206,0.000084828425,0.00008680952,0.008987816,0.9774147,0.000067522196,0.00053324807,0.000017475144],"about_ca_topic_score_codex":0.00040950225,"about_ca_topic_score_gemma":0.00027912177,"teacher_disagreement_score":0.0029057167,"about_ca_system_score_codex":0.00027879438,"about_ca_system_score_gemma":0.00015689242,"threshold_uncertainty_score":0.0097206235},"labels":[],"label_agreement":null},{"id":"W2314415627","doi":"10.2514/6.2003-759","title":"RLV Power Generation Systems Trail from 1st to 2nd Generation","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Electric and Hybrid Vehicle Technologies","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":"Lockheed Martin (Canada)","funders":"","keywords":"Electricity generation; Computer science; Power (physics); Physics","score_opus":0.0341699772575486,"score_gpt":0.2200802395772298,"score_spread":0.18591026231968122,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2314415627","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":[0.25729904,0.0036719488,0.12248164,0.0051165014,0.00086314866,0.00038850808,0.002641254,0.0064663994,0.6010716],"genre_scores_gemma":[0.79338366,0.0014478844,0.028419377,0.00052577583,0.0001546216,0.000069883434,0.0028219442,0.00032347717,0.17285338],"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99970067,0.000055221288,0.000011639491,0.000049991097,0.00011997195,0.00006246843],"domain_scores_gemma":[0.99957925,0.000036318543,0.00003282985,0.000078013996,0.00022515701,0.000048273923],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003916154,0.00032134986,0.00021854525,0.00066621735,0.0007911835,0.0021232793,0.0006085934,0.00034953724,0.02479259],"category_scores_gemma":[0.00054504594,0.00018575457,0.00025253248,0.0004793301,0.00037828414,0.0011047861,0.0009329204,0.0012350783,0.006352039],"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":[0.0004760071,0.0002837217,0.011261442,0.00035945943,0.00006471136,0.0003694649,0.0006209688,0.031616602,0.025398485,0.07422214,0.058888108,0.79643893],"study_design_scores_gemma":[0.00016905715,0.0011154338,0.024383448,0.00030899534,0.000050009578,0.0005313112,0.0009797094,0.0659405,0.04160023,0.036344633,0.8285032,0.000073436655],"about_ca_topic_score_codex":0.005836742,"about_ca_topic_score_gemma":0.0152831655,"teacher_disagreement_score":0.02479259,"about_ca_system_score_codex":0.0011132451,"about_ca_system_score_gemma":0.0012435752,"threshold_uncertainty_score":0.082939446},"labels":[],"label_agreement":null},{"id":"W2315791200","doi":"10.2514/6.2003-733","title":"Optimization of a Hot-Air Anti-Icing System","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Icing and De-icing Technologies","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":"Polytechnique Montréal","funders":"","keywords":"Icing; Computer science; Environmental science; Meteorology; Geography","score_opus":0.013575508702038672,"score_gpt":0.20299027281382823,"score_spread":0.18941476411178956,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2315791200","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.5119065,0.0009415925,0.41631982,0.0009540942,0.00024132851,0.0004097163,0.00046753383,0.001144644,0.06761474],"genre_scores_gemma":[0.9813669,0.00009356116,0.012803745,0.00005621848,0.000022973829,0.000105894294,0.000066499175,0.000045117107,0.005439204],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99977666,0.000058131096,0.0000072589933,0.00004067294,0.00005140762,0.00006587079],"domain_scores_gemma":[0.9996816,0.00013917375,0.000046421806,0.000014206026,0.000086902466,0.000031696618],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00041214735,0.00097647123,0.0012648923,0.0005597683,0.0007430777,0.0013623922,0.0006158313,0.0016808009,0.0063146516],"category_scores_gemma":[0.0008517799,0.00073058094,0.00046293862,0.0003408184,0.0005841213,0.00054125785,0.00072898593,0.00060475897,0.00056661316],"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":[0.00010101239,0.000024878922,0.00017668847,0.000042512052,0.000018114495,0.000041371986,0.000014065723,0.9910987,0.003139601,0.0005114465,0.00031773883,0.004513725],"study_design_scores_gemma":[0.000037596932,0.00010651778,0.0002900096,0.0000042094343,0.00002151356,0.000009077795,0.000014536008,0.99771106,0.0012277637,0.00019957595,0.0003712498,0.000006793199],"about_ca_topic_score_codex":0.008583115,"about_ca_topic_score_gemma":0.00473598,"teacher_disagreement_score":0.008583115,"about_ca_system_score_codex":0.00092147227,"about_ca_system_score_gemma":0.0014070055,"threshold_uncertainty_score":0.021124661},"labels":[],"label_agreement":null},{"id":"W2317503549","doi":"10.2514/6.2003-1223","title":"FENSAP-ICE : Effect of Ice Shapes on 3D Eulerian Droplet Impingement","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Icing and De-icing Technologies","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":"McGill University","funders":"","keywords":"Eulerian path; Geology; Mechanics; Physics","score_opus":0.013447487183462026,"score_gpt":0.22769744667537278,"score_spread":0.21424995949191075,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2317503549","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9834765,0.00023218387,0.011403142,0.00009442372,0.0000836267,0.00002922782,0.0005010607,0.00087398273,0.0033058699],"genre_scores_gemma":[0.99253243,0.00012475492,0.006021939,0.0000233846,0.000008382868,0.000011253295,0.00034499425,0.00028050615,0.0006523003],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99985087,0.000027578724,0.00000799373,0.000028666835,0.000046640824,0.000038265574],"domain_scores_gemma":[0.99895334,0.00066882366,0.00007133758,0.00007310993,0.00012200064,0.00011142895],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00036301513,0.00056475465,0.00059322704,0.00028691645,0.00034335727,0.0007803533,0.00056686735,0.00056881004,0.0034882177],"category_scores_gemma":[0.00222317,0.0002889319,0.0002988854,0.00037126066,0.00039782815,0.0007565749,0.0007237331,0.00045023748,0.0002798831],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.002917985,0.0002355639,0.00701567,0.00027350712,0.000080980266,0.0005998578,0.00026292185,0.8475006,0.1006129,0.0008340787,0.0020989086,0.03756696],"study_design_scores_gemma":[0.00011994414,0.00032514945,0.0032252898,0.000014417579,0.000027409167,0.00008698206,0.00007901301,0.93354017,0.06159941,0.00019143784,0.0007571145,0.00003369354],"about_ca_topic_score_codex":0.0036982007,"about_ca_topic_score_gemma":0.0042704903,"teacher_disagreement_score":0.0036982007,"about_ca_system_score_codex":0.00028287803,"about_ca_system_score_gemma":0.0005227507,"threshold_uncertainty_score":0.011669219},"labels":[],"label_agreement":null},{"id":"W2318023244","doi":"10.2514/6.2003-1240","title":"CFD Investigation of Fin Aeroheating on a Hypersonic Projectile","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Gas Dynamics and Kinetic Theory","field":"Mathematics","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":"National Research Council Canada","funders":"","keywords":"Projectile; Hypersonic speed; Fin; Aerospace engineering; Computational fluid dynamics; Materials science; Engineering","score_opus":0.061649072629100354,"score_gpt":0.2855067903629673,"score_spread":0.22385771773386692,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2318023244","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9692134,0.00014688837,0.0042451564,0.00035830896,0.000092815106,0.000050614082,0.00036353385,0.0002610602,0.025268259],"genre_scores_gemma":[0.9943756,0.000044328648,0.00075251225,0.000020240299,0.000007714552,0.0000059023632,0.0001028556,0.000021946154,0.0046688495],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99989283,0.000011485136,0.00000380621,0.000017914728,0.00004200095,0.000031996486],"domain_scores_gemma":[0.99976677,0.00010058537,0.000014377435,0.000020736408,0.000057204954,0.00004030018],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012636524,0.00033621528,0.00067215937,0.00046154842,0.0011087313,0.000683504,0.0003800785,0.0008173831,0.0067064324],"category_scores_gemma":[0.00058626535,0.00017807781,0.00038961854,0.00029986267,0.0006082156,0.00039868543,0.00052139466,0.00045321768,0.0004132369],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.002157392,0.0003553683,0.028675992,0.0002852691,0.000069220274,0.011537191,0.0007009593,0.7736123,0.13572085,0.0033501708,0.0052023353,0.03833299],"study_design_scores_gemma":[0.000075021424,0.00057406526,0.03023791,0.00003174221,0.00002639182,0.00084474974,0.0006242388,0.9171155,0.0462059,0.000750517,0.0034482242,0.00006577483],"about_ca_topic_score_codex":0.009290374,"about_ca_topic_score_gemma":0.005536225,"teacher_disagreement_score":0.009290374,"about_ca_system_score_codex":0.0005466536,"about_ca_system_score_gemma":0.00055603666,"threshold_uncertainty_score":0.022435308},"labels":[],"label_agreement":null},{"id":"W2318049051","doi":"10.2514/6.2003-725","title":"Efficient Optimized Airfoil Parameterization","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Advanced Numerical Analysis Techniques","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":"Polytechnique Montréal","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Airfoil; Computer science; Aerospace engineering; Engineering","score_opus":0.01416601986680012,"score_gpt":0.23146010296262093,"score_spread":0.21729408309582082,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2318049051","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":[0.09684662,0.00016539094,0.8789798,0.00016384927,0.00009187238,0.000101788726,0.00029920824,0.0020147176,0.02133669],"genre_scores_gemma":[0.8426878,0.00008998123,0.14980963,0.00006757831,0.00002953866,0.00013336467,0.00035804455,0.00077042246,0.0060537364],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997595,0.000040888088,0.000007901611,0.00002795837,0.000120528566,0.00004332607],"domain_scores_gemma":[0.9998099,0.00003649151,0.000016969447,0.00006409983,0.00006115924,0.0000114915465],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023108392,0.000752834,0.0006712279,0.00060963404,0.00047272578,0.0008244146,0.0008145405,0.00061286904,0.0056299237],"category_scores_gemma":[0.00082334486,0.00030851978,0.00033117915,0.00044817524,0.00026834029,0.0009152501,0.00085356523,0.0005830384,0.0010629836],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00017984812,0.00008070745,0.00056949613,0.00007417773,0.000029202742,0.000058245263,0.00005902318,0.8430672,0.039361045,0.017082289,0.0032006267,0.09623814],"study_design_scores_gemma":[0.000017924895,0.000028201539,0.00023039134,0.0000045056754,0.0000068799654,0.000017272068,0.000019529976,0.9814435,0.011468754,0.003598859,0.0031533842,0.000010748512],"about_ca_topic_score_codex":0.0017940559,"about_ca_topic_score_gemma":0.0028095974,"teacher_disagreement_score":0.0056299237,"about_ca_system_score_codex":0.0005698753,"about_ca_system_score_gemma":0.00076704717,"threshold_uncertainty_score":0.018833995},"labels":[],"label_agreement":null},{"id":"W2318616356","doi":"10.2514/6.2003-1333","title":"Cost Modelling as a Holistic Tool in the Multi-disciplinary Systems Architecture of Aircraft Design: The Next Frontier","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Manufacturing Process and Optimization","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":"Queen's University","funders":"Government of the United Kingdom","keywords":"Frontier; Architecture; Systems engineering; Computer science; Discipline; Systems design; Computer architecture; Software engineering; Engineering; Architectural engineering; Sociology; Geography","score_opus":0.10172996623939046,"score_gpt":0.27233711544365635,"score_spread":0.1706071492042659,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2318616356","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":[0.017912256,0.0012266302,0.9739116,0.0012894401,0.00007313909,0.00002274054,0.00005225196,0.00006113127,0.005450838],"genre_scores_gemma":[0.77085674,0.002319627,0.22218703,0.00021334695,0.00017521999,0.00016236262,0.0000952205,0.00019095774,0.0037995107],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99869484,0.0007262676,0.00003848233,0.00008231727,0.00038793308,0.00007022875],"domain_scores_gemma":[0.9987451,0.00072502554,0.00011390197,0.00013776227,0.00019886106,0.00007930374],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0022695237,0.0011280735,0.0015253068,0.0007844514,0.000555655,0.0023279907,0.0015798007,0.0011596909,0.002329956],"category_scores_gemma":[0.005124184,0.0008244963,0.0010062308,0.0013241362,0.0012294023,0.0042676367,0.0016551504,0.0016126604,0.0002828214],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000017744638,0.000012800794,0.00023012715,0.000051164567,0.000036391273,0.000018827779,0.00002870269,0.8988265,0.00035260027,0.082476504,0.00045253773,0.017496157],"study_design_scores_gemma":[0.0000069153216,0.000019903813,0.00014078595,0.000020322528,0.000019830431,0.00001584998,0.000029707178,0.90966684,0.00013003212,0.08841876,0.0015197714,0.000011276154],"about_ca_topic_score_codex":0.0038301887,"about_ca_topic_score_gemma":0.005288305,"teacher_disagreement_score":0.0038301887,"about_ca_system_score_codex":0.0013855657,"about_ca_system_score_gemma":0.0019350575,"threshold_uncertainty_score":0.012002528},"labels":[],"label_agreement":null},{"id":"W2320514444","doi":"10.2514/6.2003-227","title":"Unsteady Aerodynamic Solutions for Oscillating Airfoils","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Biomimetic flight and propulsion mechanisms","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":"McGill University","funders":"","keywords":"Airfoil; Aerodynamics; Aerospace engineering; Mechanics; Computer science; Physics; Acoustics; Engineering","score_opus":0.03595958307323533,"score_gpt":0.23213398340958155,"score_spread":0.19617440033634623,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2320514444","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7487258,0.0013955791,0.1961377,0.0010873306,0.00051471184,0.0000916924,0.00018521224,0.00019210616,0.051669955],"genre_scores_gemma":[0.94971484,0.0004903642,0.018868236,0.00015066826,0.0001379446,0.000070631206,0.00020182243,0.0001002433,0.030265374],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998734,0.000025932251,0.0000069218613,0.00001662766,0.000044508746,0.000032676064],"domain_scores_gemma":[0.99969614,0.0001147638,0.000041936695,0.00002050436,0.00007997842,0.000046740108],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002478926,0.0005535012,0.00041413683,0.0007433018,0.000592947,0.0011172321,0.0008354421,0.0014391292,0.00336402],"category_scores_gemma":[0.0025354465,0.00040981642,0.00046343575,0.00034110865,0.0011132074,0.0009332075,0.0012289837,0.0009072328,0.00031669374],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00029059712,0.00012964121,0.0014522348,0.00018193775,0.000054215325,0.0007379914,0.00047013853,0.8222506,0.023308808,0.12360192,0.0024280518,0.025093833],"study_design_scores_gemma":[0.000030627227,0.000029134513,0.000597897,0.000013204238,0.000004779322,0.00005637428,0.00013006949,0.9854709,0.0010995718,0.011679635,0.0008715209,0.000016332526],"about_ca_topic_score_codex":0.003787681,"about_ca_topic_score_gemma":0.0026606596,"teacher_disagreement_score":0.003787681,"about_ca_system_score_codex":0.00033793558,"about_ca_system_score_gemma":0.00047203546,"threshold_uncertainty_score":0.011253774},"labels":[],"label_agreement":null},{"id":"W2320516950","doi":"10.2514/6.2003-160","title":"Comparisons Between Plastic Contact Hardness Models and Experiments","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Adhesion, Friction, and Surface Interactions","field":"Engineering","cited_by":4,"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":"Materials science; Hardness; Indentation hardness; Composite material; Microstructure","score_opus":0.06257376769022605,"score_gpt":0.2718022809349413,"score_spread":0.20922851324471525,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2320516950","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.83653647,0.0014509371,0.12522957,0.00033172837,0.0002703645,0.0003697152,0.004850717,0.0017813774,0.02917915],"genre_scores_gemma":[0.99100715,0.0003732357,0.004584656,0.000041479805,0.000019545261,0.00015946545,0.000948078,0.00021316501,0.0026532726],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99839705,0.00020855501,0.00011567709,0.00030726462,0.0008065891,0.00016480699],"domain_scores_gemma":[0.99465007,0.003022873,0.0003458781,0.0011081385,0.0007799807,0.000093116505],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0013674079,0.0010754414,0.00090625265,0.0017110532,0.00080160296,0.0013423369,0.0024831034,0.0014338011,0.017554238],"category_scores_gemma":[0.006280982,0.00070024084,0.00096569234,0.0017863486,0.00082291826,0.002472228,0.0008173235,0.00092082814,0.0020648835],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.005586145,0.001428153,0.02831335,0.0021401478,0.00035585414,0.00072740426,0.0014113039,0.55608237,0.20736939,0.012406667,0.009230101,0.17494911],"study_design_scores_gemma":[0.00023919487,0.0018879431,0.035968702,0.00010486497,0.00017989753,0.0004400967,0.0006516451,0.7735992,0.17173402,0.0037059223,0.0112478975,0.0002405615],"about_ca_topic_score_codex":0.0038173434,"about_ca_topic_score_gemma":0.004547698,"teacher_disagreement_score":0.017554238,"about_ca_system_score_codex":0.0010682488,"about_ca_system_score_gemma":0.0005356197,"threshold_uncertainty_score":0.05872482},"labels":[],"label_agreement":null},{"id":"W2321190310","doi":"10.2514/6.2003-221","title":"Moving Surface Boundary-layer Control for Aircraft Operation at High Angles of Attack","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Guidance and Control Systems","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":"University of British Columbia","funders":"","keywords":"Boundary layer; Surface (topology); Layer (electronics); Aerospace engineering; Boundary (topology); Angle of attack; Boundary layer control; Computer science; Aeronautics; Aerodynamics; Materials science; Engineering; Geometry; Flow separation; Mathematics; Composite material","score_opus":0.020309683138803717,"score_gpt":0.23395887010620586,"score_spread":0.21364918696740215,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2321190310","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":[0.4039258,0.0009922441,0.58486503,0.00036455432,0.00051211484,0.000043494485,0.00003452316,0.000571021,0.0086913025],"genre_scores_gemma":[0.98948586,0.00007574952,0.009224199,0.000026879661,0.000021628179,0.000013987152,0.000013474899,0.00001587466,0.001122403],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999341,0.000015134858,0.0000038350868,0.000009975674,0.000020901107,0.000016089383],"domain_scores_gemma":[0.99986327,0.000046481546,0.000025318257,0.000009650015,0.000038578237,0.000016744962],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024389631,0.00037610758,0.00037973572,0.00019493113,0.00045146185,0.00068295054,0.0004981955,0.00047190522,0.0013347262],"category_scores_gemma":[0.0005537468,0.00017186906,0.00018709412,0.000107101725,0.00038063945,0.00055033196,0.0007001374,0.00053645583,0.00014419688],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0011977862,0.00018145858,0.0010843343,0.00016394215,0.000055829816,0.00016585378,0.00026693937,0.7286556,0.1445512,0.0131725455,0.0025428948,0.10796167],"study_design_scores_gemma":[0.000025576952,0.00007162064,0.00017416096,0.0000038841754,0.0000043141517,0.0000038013848,0.000013660659,0.9957398,0.0030944517,0.00061348284,0.0002505171,0.000004694397],"about_ca_topic_score_codex":0.0032796895,"about_ca_topic_score_gemma":0.0030011768,"teacher_disagreement_score":0.0032796895,"about_ca_system_score_codex":0.00024167847,"about_ca_system_score_gemma":0.00025811122,"threshold_uncertainty_score":0.0065211654},"labels":[],"label_agreement":null},{"id":"W2322912868","doi":"10.2514/6.2003-71","title":"A Newton-Krylov Algorithm for Turbulent Aerodynamic Flows","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Computational Fluid Dynamics and Aerodynamics","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":"University of Toronto","funders":"","keywords":"Aerodynamics; Turbulence; Computer science; Computational fluid dynamics; Mechanics; Physics","score_opus":0.01213327392738127,"score_gpt":0.2205977382769048,"score_spread":0.2084644643495235,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2322912868","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":[0.0074144914,0.00013578197,0.98944926,0.00007910023,0.00011881691,0.000042091906,0.00005010622,0.00062238984,0.0020879982],"genre_scores_gemma":[0.096769914,0.00021489324,0.89415777,0.00006821042,0.00009184215,0.00013257482,0.00023913156,0.0005303843,0.007795356],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99969244,0.000071167335,0.000020053156,0.000033444263,0.00015285352,0.000030081083],"domain_scores_gemma":[0.99961495,0.000099992176,0.000028300978,0.00006545064,0.00014702398,0.000044243563],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005253074,0.0005098724,0.00078415126,0.00042272545,0.0006375727,0.000763949,0.001212932,0.000984156,0.003253739],"category_scores_gemma":[0.0014115355,0.00046134324,0.0004910422,0.0005040423,0.0005027911,0.000998831,0.0012943748,0.0011771495,0.0017025954],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00030002615,0.00015611944,0.0006406515,0.0001486648,0.000059200564,0.00009580358,0.00013739074,0.5678049,0.014810032,0.06804942,0.007548122,0.34024975],"study_design_scores_gemma":[0.000020510826,0.000021545731,0.000075218624,0.000004965211,0.000003639516,0.000013534557,0.0000043861014,0.9913902,0.001209431,0.0043939627,0.0028520573,0.000010520507],"about_ca_topic_score_codex":0.0039979327,"about_ca_topic_score_gemma":0.0044229534,"teacher_disagreement_score":0.0039979327,"about_ca_system_score_codex":0.0003982142,"about_ca_system_score_gemma":0.0013397213,"threshold_uncertainty_score":0.010884821},"labels":[],"label_agreement":null},{"id":"W2324811470","doi":"10.2514/6.2003-1098","title":"Aerodynamic Solutions for Finite-span Wings of Arbitrary Shapes","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Wind and Air Flow Studies","field":"Environmental Science","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":"Aerodynamics; Span (engineering); Finite element method; Computer science; Structural engineering; Aerospace engineering; Engineering","score_opus":0.026722626137208882,"score_gpt":0.23339057110498682,"score_spread":0.20666794496777793,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2324811470","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":[0.033514928,0.00018840253,0.9599271,0.000069261056,0.000035752368,0.000018973944,0.000022920647,0.000080658676,0.0061420905],"genre_scores_gemma":[0.5718869,0.00077778194,0.41332865,0.00008171418,0.00009153151,0.00018417857,0.00014361281,0.00013225879,0.013373356],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99989414,0.000022286598,0.0000047902813,0.000011419207,0.00005694492,0.000010422085],"domain_scores_gemma":[0.99977475,0.000099228375,0.00002811559,0.000028336615,0.00005933034,0.00001020448],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00028996533,0.00032542838,0.0002685028,0.00033505325,0.00026793612,0.00032515085,0.0005352946,0.0007330907,0.0013541701],"category_scores_gemma":[0.001176548,0.00018381455,0.0005289052,0.00016183966,0.0005435619,0.00056766754,0.00045614087,0.0005914907,0.00043089644],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00003743301,0.000029955145,0.0007866217,0.00014565603,0.000016799995,0.00037223383,0.00030982913,0.74980676,0.03710353,0.15223336,0.0010631802,0.058094632],"study_design_scores_gemma":[0.000007175341,0.000015424053,0.00016130491,0.000012363873,0.0000020946395,0.00011620462,0.00003117611,0.9821669,0.0023869246,0.012619036,0.0024747762,0.000006584312],"about_ca_topic_score_codex":0.00039842687,"about_ca_topic_score_gemma":0.0004812773,"teacher_disagreement_score":0.0013541701,"about_ca_system_score_codex":0.00017699777,"about_ca_system_score_gemma":0.0002222582,"threshold_uncertainty_score":0.004530132},"labels":[],"label_agreement":null},{"id":"W2325131514","doi":"10.2514/6.2003-1093","title":"Force and Moment Corrections for a Three-Dimensional Model in a Low Speed Wind Tunnel","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Fluid Dynamics Simulations and Interactions","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":"Lockheed Martin (Canada)","funders":"","keywords":"Moment (physics); Physics; Wind tunnel; Wind speed; Environmental science; Mechanics; Meteorology; Classical mechanics","score_opus":0.019992513527788917,"score_gpt":0.23811881696065784,"score_spread":0.21812630343286893,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2325131514","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.88381594,0.00038444623,0.0897457,0.001311692,0.00041811835,0.00015766571,0.001003674,0.002283368,0.020879433],"genre_scores_gemma":[0.98636985,0.00011278045,0.008242705,0.000083317056,0.000044001667,0.000038933158,0.00023823083,0.00024210566,0.004628165],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998611,0.000032327767,0.0000106821,0.000021370568,0.00004636598,0.000028115337],"domain_scores_gemma":[0.99917763,0.00028401686,0.00010264801,0.00008946632,0.00021762728,0.00012851317],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00037844013,0.00062819786,0.00072240666,0.00047184766,0.0010994158,0.00078424736,0.0012071099,0.00196147,0.004068528],"category_scores_gemma":[0.0020212345,0.0005190003,0.0005705661,0.00059705024,0.00080587587,0.0007143537,0.00056799524,0.0011036962,0.00038484528],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000079620855,0.00006344032,0.00092945754,0.000022424752,0.000009973231,0.00018822448,0.000040620074,0.9923523,0.0020038295,0.0017043785,0.00065219303,0.0019535457],"study_design_scores_gemma":[0.00002083897,0.000015407984,0.0004011094,0.0000025107092,0.0000031050404,0.000013401865,0.00001436482,0.9988543,0.0002960913,0.00021025892,0.0001597148,0.000008908285],"about_ca_topic_score_codex":0.06166858,"about_ca_topic_score_gemma":0.031817846,"teacher_disagreement_score":0.06166858,"about_ca_system_score_codex":0.00086164917,"about_ca_system_score_gemma":0.0013984465,"threshold_uncertainty_score":0.12261927},"labels":[],"label_agreement":null},{"id":"W2325548490","doi":"10.2514/6.2003-856","title":"Improvement of Velocity Role in Coupling of Mass and Momentum Equations","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Computational Fluid Dynamics and Aerodynamics","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 Waterloo","funders":"Sharif University of Technology","keywords":"Momentum (technical analysis); Physics; Coupling (piping); Mechanics; Quantum electrodynamics; Classical mechanics; Mechanical engineering; Engineering; Business","score_opus":0.009450597983066349,"score_gpt":0.20937288447412536,"score_spread":0.199922286491059,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2325548490","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":[0.23017256,0.0008318155,0.74411243,0.0006346752,0.00075972883,0.00011063138,0.00007387223,0.000787679,0.022516645],"genre_scores_gemma":[0.88297296,0.00042007974,0.107419826,0.00011195553,0.00020845831,0.00007248134,0.00011212638,0.00026881436,0.008413358],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995933,0.00014656232,0.000026954121,0.00007760511,0.00010142176,0.000054181335],"domain_scores_gemma":[0.9993625,0.00019755847,0.00006143836,0.00012887327,0.00017330404,0.00007626451],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00055325276,0.0006563087,0.00054031017,0.000540422,0.0006175437,0.0010657625,0.00092515873,0.00066690246,0.0038051323],"category_scores_gemma":[0.0023760272,0.00022525736,0.00048909266,0.00024220698,0.00039655025,0.0012654617,0.0013126883,0.00081562286,0.00069622765],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0010320432,0.0008071201,0.0103486655,0.00055788807,0.00012927444,0.00073001237,0.00075261074,0.2825881,0.2512612,0.18892902,0.0035460421,0.259318],"study_design_scores_gemma":[0.00003395713,0.00015851532,0.0013691989,0.000020645972,0.000027258144,0.000092983864,0.000067958674,0.9716259,0.017401405,0.0050998474,0.004085387,0.00001697443],"about_ca_topic_score_codex":0.0024898895,"about_ca_topic_score_gemma":0.0018136684,"teacher_disagreement_score":0.0038051323,"about_ca_system_score_codex":0.00026785414,"about_ca_system_score_gemma":0.0006389673,"threshold_uncertainty_score":0.012729406},"labels":[],"label_agreement":null},{"id":"W2326500577","doi":"10.2514/6.2003-1222","title":"FENSAP-ICE: Roughness Effects on Ice Accretion Prediction","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Icing and De-icing Technologies","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":"McGill University","funders":"","keywords":"Geology; Surface roughness; Accretion (finance); Surface finish; Sea ice; Sea ice growth processes; Sea ice thickness; Materials science; Arctic ice pack; Climatology; Physics; Astrophysics; Composite material","score_opus":0.014422404524733385,"score_gpt":0.22310293136031115,"score_spread":0.20868052683557775,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2326500577","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9257918,0.00018555862,0.061438184,0.00018309063,0.000086044594,0.00007516238,0.0016267723,0.0034343102,0.0071789776],"genre_scores_gemma":[0.973154,0.000064586704,0.025111698,0.000028194167,0.000012224086,0.000032952703,0.00065996224,0.00024050302,0.0006959863],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99986935,0.000033786237,0.000005581903,0.000024001802,0.000043040312,0.000024183617],"domain_scores_gemma":[0.9995491,0.00020961047,0.00002932168,0.000051572333,0.00012027634,0.00004012254],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00047974518,0.00046914307,0.0005875533,0.00023240679,0.000351478,0.00049425353,0.0006316346,0.00044905467,0.0013662212],"category_scores_gemma":[0.0012792192,0.00030115797,0.00039097868,0.00026989338,0.00024337784,0.000548034,0.00038417228,0.00051036297,0.00019775101],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00015892499,0.000043615477,0.0066531673,0.00003228529,0.000027106296,0.00005479049,0.00003728915,0.9711557,0.0057510897,0.0002882517,0.0013366111,0.014461194],"study_design_scores_gemma":[0.000017659027,0.00001780646,0.00095967087,0.0000015900478,0.0000029723885,0.0000065800714,0.000003796862,0.99614716,0.002531646,0.000042445798,0.00026446077,0.0000042822317],"about_ca_topic_score_codex":0.028526142,"about_ca_topic_score_gemma":0.018844107,"teacher_disagreement_score":0.028526142,"about_ca_system_score_codex":0.00050917274,"about_ca_system_score_gemma":0.0006958923,"threshold_uncertainty_score":0.056720197},"labels":[],"label_agreement":null},{"id":"W2331988066","doi":"10.2514/6.2003-246","title":"Coupling of the Precursor Shock Wave and the Detonation in Channels Lined with Explosives","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Combustion and Detonation Processes","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":"McGill University","funders":"","keywords":"Explosive material; Detonation; Coupling (piping); Shock wave; Mechanics; Shock (circulatory); Materials science; Acoustics; Physics; Chemistry; Composite material","score_opus":0.01792052316050332,"score_gpt":0.20404018434787116,"score_spread":0.18611966118736784,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2331988066","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.988113,0.00007125415,0.0056840605,0.00005364003,0.00002983505,0.000020802,0.000031821182,0.000103353144,0.0058923145],"genre_scores_gemma":[0.99787617,0.00003379683,0.00038405176,0.0000075750054,0.0000053938747,0.0000041305343,0.000020147567,0.00001687055,0.0016519137],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99990606,0.000011766426,0.0000023522527,0.00001807758,0.00002415106,0.000037560534],"domain_scores_gemma":[0.99964607,0.00016085709,0.000034237873,0.000020499463,0.000052528994,0.00008582777],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00010892734,0.00025207663,0.00045785483,0.00047319778,0.00049968483,0.00084926665,0.00045920323,0.00046914103,0.0035590273],"category_scores_gemma":[0.00080507644,0.0004324239,0.00018522699,0.0002358957,0.0007190491,0.00057159865,0.00097158586,0.0008964857,0.00032050934],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.005743508,0.00090270466,0.017816553,0.0001488627,0.000097506985,0.004168916,0.0012729109,0.2160326,0.676753,0.03739373,0.0014512871,0.03821842],"study_design_scores_gemma":[0.00035776454,0.0008417784,0.06433603,0.00003979043,0.00006220672,0.0007423853,0.000853251,0.7842009,0.13685209,0.009149043,0.0024160855,0.0001487967],"about_ca_topic_score_codex":0.0036990687,"about_ca_topic_score_gemma":0.0020519705,"teacher_disagreement_score":0.0036990687,"about_ca_system_score_codex":0.00055347086,"about_ca_system_score_gemma":0.0004183115,"threshold_uncertainty_score":0.011906147},"labels":[],"label_agreement":null},{"id":"W2332177357","doi":"10.2514/6.2003-619","title":"Actuator Disk Implementation in FENSAP-ICE, a 3D Navier-Stokes In-Flight Simulation System","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Icing and De-icing Technologies","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":"Bell Helicopter Textron (Canada)","funders":"","keywords":"Actuator; Aerospace engineering; Computer science; Simulation; Engineering; Artificial intelligence","score_opus":0.01541145096280101,"score_gpt":0.2609386542228077,"score_spread":0.2455272032600067,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2332177357","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.46551725,0.00036195145,0.4370233,0.0006236438,0.00046555934,0.00038972276,0.0032147362,0.050177757,0.042226166],"genre_scores_gemma":[0.8626911,0.00017841837,0.12504178,0.00019153567,0.000026675749,0.00023864224,0.001763583,0.0030251115,0.0068432265],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998105,0.00005096431,0.000013251418,0.000026289932,0.00006936906,0.000029673374],"domain_scores_gemma":[0.99948406,0.00021229817,0.000027043296,0.000081342594,0.000145109,0.000050129685],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00040272743,0.0007446067,0.0006668386,0.00028192464,0.0005221922,0.0009496441,0.0014690568,0.0008456091,0.010733168],"category_scores_gemma":[0.0013967715,0.0004252943,0.0003952591,0.00021081831,0.00033010868,0.0006446433,0.0005742126,0.0007337707,0.0012231639],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0009344706,0.00029320782,0.0032692559,0.0003290565,0.0001337222,0.000332428,0.0003851172,0.9041905,0.020118738,0.004583931,0.008031647,0.057397954],"study_design_scores_gemma":[0.000088856395,0.000056496614,0.00022504036,0.0000073819356,0.000010200846,0.000017888246,0.000026588037,0.9895383,0.0064844457,0.00029669688,0.0032364384,0.00001156847],"about_ca_topic_score_codex":0.010283166,"about_ca_topic_score_gemma":0.008705996,"teacher_disagreement_score":0.010733168,"about_ca_system_score_codex":0.00040195647,"about_ca_system_score_gemma":0.0008381755,"threshold_uncertainty_score":0.035906017},"labels":[],"label_agreement":null},{"id":"W2335763547","doi":"10.2514/6.2003-604","title":"Low-Speed Characteristics of a High Subsonic Mach Number OHS Aircraft Configuration","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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 Calgary","funders":"","keywords":"Mach number; Aerospace engineering; Computer science; Aeronautics; Physics; Engineering","score_opus":0.013750082505702211,"score_gpt":0.23109759464216528,"score_spread":0.21734751213646308,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2335763547","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9932696,0.000050482253,0.001550213,0.000024950448,0.000006230341,0.000005368084,0.00007531136,0.00007639214,0.0049413536],"genre_scores_gemma":[0.9992268,0.000008560342,0.00014169945,0.000005283444,0.0000024606477,0.0000010001523,0.000043097112,0.000007670734,0.0005634448],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998995,0.000021354885,0.0000029532946,0.000014552993,0.00003193533,0.000029594707],"domain_scores_gemma":[0.99955493,0.00022454449,0.000055078814,0.000024918165,0.00009555771,0.000045021763],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012244681,0.00020216704,0.00020628494,0.00040445605,0.00026461727,0.00030109452,0.0002260463,0.00032680135,0.0036355774],"category_scores_gemma":[0.00033269753,0.00009720527,0.00010544897,0.00028540063,0.0001976443,0.00021789962,0.000106650135,0.00018183494,0.00053291844],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.007876866,0.0002910975,0.05357456,0.00018578483,0.000059536505,0.0016215742,0.0008259636,0.068307295,0.8256562,0.0033804472,0.002291363,0.03592941],"study_design_scores_gemma":[0.00047379537,0.008240833,0.29263678,0.0000758142,0.00017238471,0.0020387745,0.0010837783,0.50773495,0.17917214,0.001415331,0.0068114297,0.00014401667],"about_ca_topic_score_codex":0.0017910968,"about_ca_topic_score_gemma":0.002374948,"teacher_disagreement_score":0.0036355774,"about_ca_system_score_codex":0.00022158155,"about_ca_system_score_gemma":0.00011025819,"threshold_uncertainty_score":0.012162268},"labels":[],"label_agreement":null},{"id":"W2997242994","doi":"10.2514/6.2003-634","title":"Optimization of Controlled Jets in Crossflow","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Fluid Dynamics and Turbulent Flows","field":"Engineering","cited_by":19,"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":"McGill University; National Aeronautics and Space Administration; National Science Foundation","keywords":"Computer science; Aerospace engineering; Mechanics; Physics; Engineering","score_opus":0.010740535280789023,"score_gpt":0.20947452684582585,"score_spread":0.19873399156503682,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2997242994","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.5554902,0.0016548947,0.41765863,0.0010407645,0.00040750552,0.00028955334,0.0002124154,0.0005096781,0.0227364],"genre_scores_gemma":[0.9715091,0.00029421112,0.022879094,0.00013443248,0.00008393449,0.00013512296,0.00012092872,0.00018385574,0.004659371],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99961275,0.00016285788,0.00001571657,0.00005959017,0.0000723964,0.00007670423],"domain_scores_gemma":[0.9986853,0.00074925745,0.00018354657,0.00004313542,0.000177522,0.00016126408],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0012902686,0.0016966027,0.0017046202,0.00092803774,0.00054316747,0.0021828339,0.0009181975,0.0020235819,0.0032829924],"category_scores_gemma":[0.0035239342,0.0011572428,0.00058946776,0.0005513613,0.0013458104,0.0012057463,0.0017669853,0.0011490308,0.00028788918],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00026292473,0.00012455994,0.00028835217,0.00004926514,0.000034709294,0.000068053945,0.000028953802,0.98659164,0.0034937297,0.0039800783,0.00039770064,0.00467994],"study_design_scores_gemma":[0.000044489734,0.00011881468,0.00009646934,0.00000419648,0.00000555683,0.000005007606,0.000007104169,0.9981889,0.0006533689,0.00074326945,0.00012629532,0.000006551637],"about_ca_topic_score_codex":0.0044269757,"about_ca_topic_score_gemma":0.0023050145,"teacher_disagreement_score":0.0044269757,"about_ca_system_score_codex":0.0012393816,"about_ca_system_score_gemma":0.0010510124,"threshold_uncertainty_score":0.010982692},"labels":[],"label_agreement":null},{"id":"W4237750401","doi":"10.2514/6.2003-1185","title":"Numerical Investigations of Nacelle Anemometry for Horizontal Axis Wind Turbines","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Wind Energy Research and Development","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":"École de Technologie Supérieure","funders":"","keywords":"Nacelle; Marine engineering; Horizontal axis; Wind power; Aerospace engineering; Vertical axis; Computational fluid dynamics; Environmental science; Mechanics; Engineering; Computer science; Geology; Turbine; Mechanical engineering; Acoustics; Physics; Electrical engineering; Engineering drawing; Structural engineering","score_opus":0.024942525387742952,"score_gpt":0.23773274188862237,"score_spread":0.21279021650087943,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4237750401","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9768708,0.0003310404,0.012149684,0.0002501473,0.0000415248,0.00003512015,0.0000783261,0.00010148155,0.0101418225],"genre_scores_gemma":[0.99605054,0.00007495872,0.003064748,0.000014474565,0.0000064903143,0.0000072627927,0.000027232214,0.000012658481,0.00074167014],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99976844,0.000070278176,0.000012464472,0.000024951789,0.00009286554,0.000030975803],"domain_scores_gemma":[0.9983333,0.00095901004,0.0001928265,0.00012460114,0.0003253291,0.000064947904],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00044822675,0.0003167786,0.00036289144,0.00053100864,0.00066570006,0.0006344229,0.00039479384,0.0008622081,0.0010210956],"category_scores_gemma":[0.0037836453,0.00023263824,0.00024335927,0.0005861575,0.0006306081,0.0007190165,0.0005494501,0.00044972808,0.00010563003],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00020913572,0.00014756244,0.013654007,0.00008475552,0.000024452762,0.00035237626,0.00022548145,0.9486713,0.017289344,0.003905484,0.0005655624,0.014870596],"study_design_scores_gemma":[0.000012436568,0.0000514667,0.0038881388,0.000007249034,0.000004145813,0.000042777483,0.00007375667,0.9942015,0.0011812311,0.00029561168,0.00023176245,0.000009912224],"about_ca_topic_score_codex":0.005871091,"about_ca_topic_score_gemma":0.005048949,"teacher_disagreement_score":0.005871091,"about_ca_system_score_codex":0.00038345277,"about_ca_system_score_gemma":0.0004388422,"threshold_uncertainty_score":0.011673808},"labels":[],"label_agreement":null}]}