{"meta":{"query_hash":"06716983be19","filters":{"venue":"42nd AIAA Aerospace Sciences Meeting and Exhibit"},"cohort_total":24,"direct_labels_cover":0,"predictions_cover":24,"exported":24,"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/06716983be19","api":"https://metacan.xera.ac/api/v1/cohort?venue=42nd+AIAA+Aerospace+Sciences+Meeting+and+Exhibit"},"results":[{"id":"W2014081442","doi":"10.2514/6.2004-667","title":"Toward Blade-Tip Vortex Simulation with an Actuator-Lifting Surface Model","year":2004,"lang":"en","type":"article","venue":"42nd AIAA Aerospace Sciences Meeting and Exhibit","topic":"Fluid Dynamics and Turbulent 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":"École de Technologie Supérieure","funders":"Natural Sciences and Engineering Research Council of Canada; Canada Research Chairs","keywords":"Blade (archaeology); Vortex; Actuator; Surface (topology); Aerospace engineering; Mechanical engineering; Mechanics; Materials science; Engineering; Acoustics; Computer science; Physics; Electrical engineering; Geometry; Mathematics","score_opus":0.01968293534591951,"score_gpt":0.23314027108417884,"score_spread":0.21345733573825934,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2014081442","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9844514,0.00025021646,0.012024956,0.00020836938,0.00012485548,0.00013752276,0.000004697574,0.00031152027,0.0024864785],"genre_scores_gemma":[0.97604793,0.000050071645,0.02367602,0.000050263516,0.0000675203,0.0000023369505,0.000004385249,0.00003186344,0.00006961303],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99848026,0.000015934622,0.00020513349,0.00043600338,0.000380161,0.00048251418],"domain_scores_gemma":[0.9994788,0.000057510664,0.00005448467,0.00018217925,0.000047118185,0.00017986611],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00048886955,0.00024536927,0.00020759109,0.000060976006,0.00039204862,0.0002784543,0.00018602819,0.000086822576,0.0000039235374],"category_scores_gemma":[0.00003423584,0.00020373716,0.000035618115,0.00035409085,0.00017045703,0.00051486574,0.000043563494,0.00017105776,0.000007500261],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000006055838,0.000014713647,0.001177477,0.000021564229,0.0000072560756,0.0000027382196,0.0012214609,0.99274164,0.003885098,0.00056966295,0.000005507124,0.00034685127],"study_design_scores_gemma":[0.00044534024,0.0001256868,0.00048075203,0.00012947264,0.00001459293,0.000005720119,0.00026212208,0.9968018,0.0010217582,0.00036319665,0.000032596436,0.00031698067],"about_ca_topic_score_codex":0.00011525898,"about_ca_topic_score_gemma":0.000096348114,"teacher_disagreement_score":0.011651064,"about_ca_system_score_codex":0.000054356944,"about_ca_system_score_gemma":0.000060926388,"threshold_uncertainty_score":0.83081603},"labels":[],"label_agreement":null},{"id":"W2096546219","doi":"10.2514/6.2004-1053","title":"Aerodynamic Analysis of Airfoils at Very Low Reynolds Numbers","year":2004,"lang":"en","type":"article","venue":"42nd AIAA Aerospace Sciences Meeting and Exhibit","topic":"Fluid Dynamics and Turbulent 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":"McGill University","funders":"","keywords":"Airfoil; Aerodynamics; Reynolds number; Computer science; Aerospace engineering; Mechanics; Physics; Engineering; Turbulence","score_opus":0.00525019644660367,"score_gpt":0.20142144802246284,"score_spread":0.19617125157585916,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2096546219","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99112517,0.00085869123,0.0001820333,0.00017440984,0.00029747532,0.00007978004,0.000016540362,0.00013787721,0.0071280547],"genre_scores_gemma":[0.99786973,0.00038364044,0.0013479351,0.000034464192,0.000029725843,0.000004248966,0.000009836813,0.000017715227,0.0003027098],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99846655,0.0000186971,0.00030386535,0.00039530304,0.0003720817,0.00044351284],"domain_scores_gemma":[0.9994419,0.00006622327,0.00007740383,0.00024860355,0.000037318438,0.00012853017],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00053251704,0.00021739812,0.00038031512,0.00028049594,0.00027170722,0.00007782151,0.00022579936,0.00009598735,0.000021390324],"category_scores_gemma":[0.00003958041,0.00019870455,0.00015850621,0.0014576643,0.00031607383,0.00016916351,0.000092855196,0.00011729781,0.000013190938],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000005093492,0.000019924237,0.015648285,0.00006060646,0.00013991831,0.000004452828,0.00060359004,0.96249783,0.019884314,0.0007434365,0.00009833514,0.00029424045],"study_design_scores_gemma":[0.0009892181,0.00017483924,0.028401125,0.0004309948,0.00053595775,0.000014755402,0.0004913064,0.95836556,0.009024422,0.000327984,0.00035245222,0.00089135766],"about_ca_topic_score_codex":0.00045197862,"about_ca_topic_score_gemma":0.0014233413,"teacher_disagreement_score":0.01275284,"about_ca_system_score_codex":0.00013581458,"about_ca_system_score_gemma":0.000033363194,"threshold_uncertainty_score":0.8102937},"labels":[],"label_agreement":null},{"id":"W2168793094","doi":"10.2514/6.2004-821","title":"Thermal Resistances of Gaseous Gap for Conforming Rough Contacts","year":2004,"lang":"en","type":"article","venue":"42nd AIAA Aerospace Sciences Meeting and Exhibit","topic":"Adhesion, Friction, and Surface Interactions","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":"University of Waterloo","funders":"","keywords":"Materials science; Thermal; Thermal resistance; Engineering physics; Optoelectronics; Composite material; Thermodynamics; Engineering; Physics","score_opus":0.021103174461347046,"score_gpt":0.2496671600357967,"score_spread":0.22856398557444965,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2168793094","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9811305,0.001061099,0.0013492972,0.00022994893,0.00046990244,0.00015201766,0.000010042794,0.00012503927,0.01547217],"genre_scores_gemma":[0.9951058,0.00017866844,0.0042544063,0.000024399997,0.000079378944,0.000010613733,0.0000016619553,0.000012506621,0.00033256566],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9990499,0.000011620691,0.00023944944,0.00020518116,0.00018535746,0.00030851885],"domain_scores_gemma":[0.99949443,0.00017976799,0.00008166003,0.00009888971,0.000069961425,0.00007529045],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003861847,0.00013877623,0.00019138491,0.000062930536,0.00045800928,0.00007678971,0.0001132669,0.000055621305,0.000009130448],"category_scores_gemma":[0.00009674955,0.00011935972,0.00006124763,0.00019924079,0.00018078116,0.00033744425,0.000015041634,0.00008119794,0.0000033600152],"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":[0.0001007874,0.00009010994,0.010714781,0.0004788793,0.00008419891,0.000006742389,0.013421784,0.61658335,0.3441972,0.009719998,0.0012486833,0.0033534975],"study_design_scores_gemma":[0.0040022274,0.0013941715,0.007457234,0.0026991426,0.00016484981,0.00007150413,0.033754837,0.037141282,0.87562114,0.004408875,0.03137574,0.0019089845],"about_ca_topic_score_codex":0.00022128088,"about_ca_topic_score_gemma":0.00028620166,"teacher_disagreement_score":0.579442,"about_ca_system_score_codex":0.000035772726,"about_ca_system_score_gemma":0.000052257048,"threshold_uncertainty_score":0.4867348},"labels":[],"label_agreement":null},{"id":"W2312927329","doi":"10.2514/6.2004-59","title":"The Effects of Leading-Edge Ice Roughness on Downstream Frost Formation","year":2004,"lang":"en","type":"article","venue":"42nd AIAA 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":"National Aeronautics and Space Administration","keywords":"Frost (temperature); Enhanced Data Rates for GSM Evolution; Surface roughness; Geology; Frost heaving; Downstream (manufacturing); Ice formation; Leading edge; Surface finish; Meteorology; Materials science; Geotechnical engineering; Atmospheric sciences; Geomorphology; Computer science; Engineering; Physics; Composite material; Telecommunications","score_opus":0.006813824679530313,"score_gpt":0.21396966160471934,"score_spread":0.20715583692518902,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2312927329","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98951465,0.00051767495,0.0011831479,0.0004307167,0.00046477187,0.00012316815,0.0000013662391,0.00040793914,0.007356562],"genre_scores_gemma":[0.99900734,0.00028110718,0.00054454827,0.000026668878,0.00003915381,0.00000817353,7.3701545e-7,0.000009965706,0.00008228429],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.999054,0.00001804668,0.00017528451,0.00018512517,0.00023660209,0.00033093127],"domain_scores_gemma":[0.9993349,0.00033907694,0.000071360475,0.000189624,0.000028555743,0.000036514568],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00048821868,0.00015014966,0.00017282883,0.00008030446,0.00057367916,0.00012724136,0.00022411691,0.000078126344,2.715564e-7],"category_scores_gemma":[0.0003534391,0.00010056651,0.000036681573,0.0003905035,0.00036236964,0.00018744732,0.00004913305,0.00014952141,0.000012389192],"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":[0.00008196549,0.0001790846,0.011004167,0.0025246097,0.00009919037,0.000023394608,0.019960415,0.35755023,0.3206052,0.044735514,0.006167401,0.23706885],"study_design_scores_gemma":[0.00045908787,0.0003438587,0.00087401463,0.001102824,0.000015459242,0.0000109477205,0.001873822,0.0024472668,0.99084705,0.0013548502,0.00042976218,0.0002410841],"about_ca_topic_score_codex":0.000085216576,"about_ca_topic_score_gemma":0.000059328497,"teacher_disagreement_score":0.67024183,"about_ca_system_score_codex":0.000039133858,"about_ca_system_score_gemma":0.00001611385,"threshold_uncertainty_score":0.44123346},"labels":[],"label_agreement":null},{"id":"W2313294797","doi":"10.2514/6.2004-282","title":"Integration of Aerodynamic, Structural, Cost and Manufacturing Cosiderations During the Conceptual Design of a Thrust Reverser Cascade","year":2004,"lang":"en","type":"article","venue":"42nd AIAA Aerospace Sciences Meeting and Exhibit","topic":"Rocket and propulsion systems research","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":"Queen's University","funders":"","keywords":"Aerodynamics; Cascade; Conceptual design; Computer science; Aerospace engineering; Engineering; Mechanical engineering","score_opus":0.028936110929447766,"score_gpt":0.26538957823448167,"score_spread":0.23645346730503392,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2313294797","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99730116,0.00064210984,0.001029409,0.00015940351,0.000088131295,0.00029992693,0.0000065389013,0.000031140687,0.00044217272],"genre_scores_gemma":[0.9979485,0.00023001834,0.0016952733,0.0000056497674,0.000031364154,0.000010545676,0.0000010285374,0.000008580679,0.000068985006],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.998982,0.00006686328,0.00025280818,0.0001898227,0.0002839952,0.00022447912],"domain_scores_gemma":[0.9995572,0.0001431132,0.000080454185,0.00011461516,0.000046087538,0.00005850693],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00059173047,0.000124088,0.00018277242,0.00007475717,0.0004567819,0.00009081363,0.00012313551,0.00005664455,0.00001178786],"category_scores_gemma":[0.00007020878,0.0000824156,0.000025840434,0.0001703106,0.00048143684,0.00022724345,0.00005267072,0.00015249033,9.441095e-7],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000022762875,0.0000062810964,0.0016975815,0.00019180134,0.000024851835,0.0000022927065,0.009688538,0.12575066,0.85779136,0.00023671518,0.00007269381,0.004514458],"study_design_scores_gemma":[0.0005980322,0.00010452948,0.010824144,0.00049044803,0.0000143115085,0.00004676103,0.011411693,0.0101221,0.9659527,0.00018094234,0.000037855254,0.00021647717],"about_ca_topic_score_codex":0.00030088768,"about_ca_topic_score_gemma":0.00017958123,"teacher_disagreement_score":0.11562856,"about_ca_system_score_codex":0.00003193805,"about_ca_system_score_gemma":0.000031569572,"threshold_uncertainty_score":0.35132435},"labels":[],"label_agreement":null},{"id":"W2315819667","doi":"10.2514/6.2004-644","title":"Influence of the Fuel Nozzle Material on Soot Formation and Temperature Field in Coflow Laminar Diffusion Flames","year":2004,"lang":"en","type":"article","venue":"42nd AIAA Aerospace Sciences Meeting and Exhibit","topic":"Combustion and flame dynamics","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 Toronto","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Laminar flow; Soot; Nozzle; Diffusion flame; Materials science; Diffusion; Combustion; Mechanics; Field (mathematics); Nuclear engineering; Thermodynamics; Environmental science; Combustor; Chemistry; Engineering; Physics","score_opus":0.0035516938528534344,"score_gpt":0.18887357917990166,"score_spread":0.18532188532704824,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2315819667","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9985476,0.00008972657,0.000012938865,0.0005814846,0.00014335212,0.000089908746,0.0000034863804,0.00003229129,0.00049918966],"genre_scores_gemma":[0.9995192,0.00016890824,0.00017574357,0.00007455946,0.00002069431,0.0000025972308,9.223167e-7,0.000004342952,0.0000329949],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9994351,0.000015935952,0.00013259357,0.00012600912,0.00014711684,0.00014323411],"domain_scores_gemma":[0.9997957,0.000039085662,0.000036116395,0.0000852625,0.000015663687,0.000028177834],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002089293,0.00009212322,0.000099946716,0.000052558407,0.00013597251,0.00006989082,0.000092245195,0.00006328463,0.0000017114097],"category_scores_gemma":[0.000060040293,0.00006526007,0.000015806318,0.00021397913,0.00011532908,0.00016028131,0.000048063353,0.00011271484,7.5294184e-7],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000038155566,0.00004025995,0.01831155,0.0003304294,0.0000038439293,0.0000025573834,0.0065975306,0.44492632,0.52548385,0.0019108655,0.00010324956,0.0022513655],"study_design_scores_gemma":[0.0035024164,0.0009308957,0.3662034,0.004896982,0.00003281521,0.000066214525,0.006896234,0.11764475,0.4952202,0.0027311938,0.00066828635,0.0012065959],"about_ca_topic_score_codex":0.000063758496,"about_ca_topic_score_gemma":0.0002413486,"teacher_disagreement_score":0.34789184,"about_ca_system_score_codex":0.000019024827,"about_ca_system_score_gemma":0.0000117581985,"threshold_uncertainty_score":0.26612288},"labels":[],"label_agreement":null},{"id":"W2316725492","doi":"10.2514/6.2004-494","title":"Numerical and Experimental PIV/PLIF Studies of Entropy Production in Natural Convection","year":2004,"lang":"en","type":"article","venue":"42nd AIAA Aerospace Sciences Meeting and Exhibit","topic":"Geothermal Energy Systems and Applications","field":"Energy","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 Manitoba","funders":"","keywords":"Entropy production; Natural convection; Convection; Mechanics; Entropy (arrow of time); Computer science; Materials science; Thermodynamics; Physics","score_opus":0.01900950030151238,"score_gpt":0.27920568343973606,"score_spread":0.2601961831382237,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2316725492","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99491477,0.0028682256,0.00000873152,0.0009485537,0.00022306315,0.000094174924,3.2014088e-7,0.000029680608,0.0009124545],"genre_scores_gemma":[0.9989277,0.000082376515,0.0006699691,0.000027350423,0.000085252665,0.000023122197,6.5274907e-7,0.000005704593,0.00017786291],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9991006,0.000035128185,0.00019320201,0.00032368724,0.00016354262,0.00018383017],"domain_scores_gemma":[0.99971676,0.000028582486,0.000101868114,0.000078757424,0.000034223292,0.000039810446],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00030545608,0.00010613574,0.00017747743,0.000060216495,0.00023626108,0.000031621716,0.0000543562,0.000033792352,0.0000032355301],"category_scores_gemma":[0.00006314648,0.000084486586,0.000021567199,0.00029541302,0.00038690947,0.00014388197,0.00003526912,0.00006797929,0.0000019463419],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000048511418,0.00020353931,0.017182117,0.000101175865,0.000034613728,0.0000023433058,0.010861416,0.13504316,0.79972386,0.034039665,0.00005081123,0.0027087973],"study_design_scores_gemma":[0.0017075269,0.00047907082,0.01524746,0.00061175146,0.000020693402,0.00007955033,0.037440345,0.0034925318,0.93756527,0.0016860183,0.0011269819,0.0005427751],"about_ca_topic_score_codex":0.004551912,"about_ca_topic_score_gemma":0.00028700475,"teacher_disagreement_score":0.13784145,"about_ca_system_score_codex":0.00003651502,"about_ca_system_score_gemma":0.000020473326,"threshold_uncertainty_score":0.688116},"labels":[],"label_agreement":null},{"id":"W2316737403","doi":"10.2514/6.2004-1239","title":"The Effect of the Porous Diverter Fairing on the Aerodynamic Performance of Natural Blockage Thrust Reverser","year":2004,"lang":"en","type":"article","venue":"42nd AIAA Aerospace Sciences Meeting and Exhibit","topic":"Rocket and propulsion systems research","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":"Bombardier (Canada)","funders":"","keywords":"Aerodynamics; Porosity; Natural (archaeology); Aerospace engineering; Computer science; Geology; Engineering; Geotechnical engineering","score_opus":0.005988222590292087,"score_gpt":0.2080429914235022,"score_spread":0.2020547688332101,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2316737403","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.994087,0.0007547525,0.000001828996,0.000584148,0.0003858851,0.00024764639,0.0000016353516,0.000026574453,0.0039105336],"genre_scores_gemma":[0.999432,0.00013098957,0.000017841072,0.000013330955,0.00004109562,0.000008585866,1.61812e-7,0.000009335666,0.0003466392],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9986392,0.00011414232,0.00020229418,0.00018086538,0.00054275617,0.00032068676],"domain_scores_gemma":[0.9991987,0.00037246916,0.00008228502,0.0002779462,0.000035037647,0.000033598048],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0017117643,0.00014345418,0.00017276515,0.000034922276,0.00084476074,0.00007959249,0.0004886345,0.000044606866,0.000004526288],"category_scores_gemma":[0.00012745835,0.000057779245,0.00006939301,0.00039304126,0.0004554393,0.00009796241,0.00014450282,0.000278822,0.0000058452006],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0003354665,0.00004813955,0.26456112,0.0017197131,0.00021004572,0.000007735293,0.012696899,0.103920616,0.49650237,0.0004824807,0.00271732,0.1167981],"study_design_scores_gemma":[0.001235897,0.0010293717,0.054143284,0.0025363152,0.000039431987,0.000035106263,0.0030599278,0.020021778,0.9167719,0.0000659507,0.00056025886,0.00050078076],"about_ca_topic_score_codex":0.0001079399,"about_ca_topic_score_gemma":0.00006546688,"teacher_disagreement_score":0.42026955,"about_ca_system_score_codex":0.000028416947,"about_ca_system_score_gemma":0.000019861973,"threshold_uncertainty_score":0.6497302},"labels":[],"label_agreement":null},{"id":"W2318415033","doi":"10.2514/6.2004-995","title":"Distributed Mass Weighting of Non-Inverted Convection Upwind Variables for Three-Dimensional Flow SImulations","year":2004,"lang":"en","type":"article","venue":"42nd AIAA Aerospace Sciences Meeting and Exhibit","topic":"Fluid Dynamics and Heat Transfer","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 Manitoba","funders":"","keywords":"Weighting; Upwind scheme; Flow (mathematics); Mechanics; Convection; Computer science; Geology; Physics; Mathematics; Mathematical analysis; Acoustics","score_opus":0.010229404600786262,"score_gpt":0.2177217435569654,"score_spread":0.20749233895617916,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2318415033","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7785653,0.00011847105,0.22018449,0.00018949353,0.0002724632,0.00019847103,0.0000985273,0.000083226594,0.000289554],"genre_scores_gemma":[0.97767544,0.000010349043,0.022172473,0.000013565836,0.000057643825,0.00000774706,0.000035226694,0.000014812814,0.00001272398],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99899244,0.000007816515,0.00024282337,0.0002526042,0.00019840323,0.0003059227],"domain_scores_gemma":[0.9995773,0.00013937657,0.000029822519,0.00009237556,0.000084404914,0.00007673203],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00035355403,0.00015016836,0.00020166425,0.000077302924,0.00041526722,0.000063166815,0.00008665005,0.00008653741,0.000009397847],"category_scores_gemma":[0.00004110322,0.0001368448,0.000054619522,0.00035049886,0.00015647213,0.00016119574,0.000014962435,0.00008997575,0.0000013788328],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000059398653,0.000011909547,0.0020159502,0.00006795805,0.00001433499,3.7234787e-7,0.00012219333,0.8848291,0.11188385,0.0008605014,0.000030919527,0.0001569795],"study_design_scores_gemma":[0.0006634979,0.00007696429,0.0010113029,0.0001776748,0.000024681849,0.0000025066472,0.00005193228,0.9800306,0.016395962,0.0013489103,0.00004319436,0.00017278126],"about_ca_topic_score_codex":0.00012712849,"about_ca_topic_score_gemma":0.00025261022,"teacher_disagreement_score":0.19911015,"about_ca_system_score_codex":0.00003845306,"about_ca_system_score_gemma":0.000054146556,"threshold_uncertainty_score":0.55803686},"labels":[],"label_agreement":null},{"id":"W2318517974","doi":"10.2514/6.2004-520","title":"3D Computation of Noise Propagation from Ducted Fans Using a Spectral Element Method","year":2004,"lang":"en","type":"article","venue":"42nd AIAA Aerospace Sciences Meeting and Exhibit","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Computation; Noise (video); Acoustics; Computer science; Element (criminal law); Physics; Algorithm; Computer vision","score_opus":0.013898756462983648,"score_gpt":0.25955543102040163,"score_spread":0.245656674557418,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2318517974","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7005823,0.00014515838,0.2983539,0.00006270877,0.00019744298,0.000103305414,0.00000980117,0.00006403999,0.00048127727],"genre_scores_gemma":[0.7557177,0.000027550448,0.24415076,0.000009666753,0.000071488364,0.0000018322313,0.0000055270966,0.00001080677,0.000004684753],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989167,0.000026950202,0.0002581841,0.00026649318,0.0002766252,0.00025504036],"domain_scores_gemma":[0.99965656,0.00004735751,0.00009545948,0.00008701988,0.00005277595,0.000060833],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004946713,0.00014449864,0.00018493197,0.00007222699,0.00020303331,0.00008120129,0.000100738755,0.000052035477,0.0000044082494],"category_scores_gemma":[0.000044114637,0.00013428059,0.000032980064,0.00033302497,0.00012954649,0.00014280439,0.000036498466,0.00010720387,0.0000013414117],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000020554028,0.0000117787295,0.0005589549,0.000027724209,0.000008167068,9.776415e-7,0.00069585966,0.766895,0.23053609,0.00024427145,0.000004135085,0.0010150177],"study_design_scores_gemma":[0.0003208147,0.000059928192,0.0012008344,0.00021650826,0.00003001481,0.0000037068482,0.00063838466,0.96340775,0.032649618,0.0012783856,0.0000071359614,0.00018692929],"about_ca_topic_score_codex":0.00044015513,"about_ca_topic_score_gemma":0.00010106212,"teacher_disagreement_score":0.19788647,"about_ca_system_score_codex":0.00007055861,"about_ca_system_score_gemma":0.000044955214,"threshold_uncertainty_score":0.54758036},"labels":[],"label_agreement":null},{"id":"W2319494462","doi":"10.2514/6.2004-1290","title":"Aplication of a Sensitivity Equation Method to Turbulent Flows with Heat Transfer","year":2004,"lang":"en","type":"article","venue":"42nd AIAA Aerospace Sciences Meeting and Exhibit","topic":"Radiative Heat Transfer Studies","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":"Polytechnique Montréal","funders":"","keywords":"Sensitivity (control systems); Turbulence; Heat transfer; Computer science; Mechanics; Physics; Engineering; Electronic engineering","score_opus":0.018144955941425817,"score_gpt":0.24640414711744307,"score_spread":0.22825919117601726,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2319494462","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7165262,0.00022908028,0.2809758,0.0012003935,0.000032718504,0.00020373042,0.0000035339604,0.00008221732,0.0007463687],"genre_scores_gemma":[0.9584201,0.00006118147,0.04139801,0.00005187172,0.000029654122,0.00002073724,9.462843e-7,0.000012099891,0.0000053749845],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.998945,0.000052918676,0.0001653989,0.00029958086,0.00028015042,0.00025694416],"domain_scores_gemma":[0.99963224,0.00010894862,0.000006059626,0.000108551,0.000057846708,0.00008635499],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0008249942,0.00015640123,0.00022147065,0.00008865449,0.00019199231,0.00003851426,0.000057925234,0.0000380476,0.0000013740602],"category_scores_gemma":[0.000022240434,0.00012565075,0.000030703337,0.000502179,0.00011429687,0.00015674585,0.0000095038395,0.00007906561,0.0000033345098],"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":[0.000015276952,0.000021168353,0.0011151987,0.00008353575,0.00002172225,0.0000017094426,0.0074253646,0.7608251,0.22762008,0.0008340875,0.000011573811,0.0020251728],"study_design_scores_gemma":[0.0012234674,0.0007378582,0.017885713,0.0007028275,0.00007840455,0.000039146344,0.0025860944,0.082979225,0.8925927,0.00026904407,0.00023158433,0.0006738978],"about_ca_topic_score_codex":0.0003080544,"about_ca_topic_score_gemma":0.00039249528,"teacher_disagreement_score":0.6778459,"about_ca_system_score_codex":0.000052971078,"about_ca_system_score_gemma":0.000030433612,"threshold_uncertainty_score":0.51238894},"labels":[],"label_agreement":null},{"id":"W2321240445","doi":"10.2514/6.2004-832","title":"Nacelle Thermal Analysis of Wind Turbines Operating in Nordic Climate","year":2004,"lang":"en","type":"article","venue":"42nd AIAA Aerospace Sciences Meeting and Exhibit","topic":"Wind and Air Flow Studies","field":"Environmental Science","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":"École de Technologie Supérieure","funders":"Natural Sciences and Engineering Research Council of Canada; Canadian Natural Resources Limited","keywords":"Nacelle; Wind power; Environmental science; Meteorology; Marine engineering; Aerospace engineering; Turbine; Engineering; Electrical engineering; Geography","score_opus":0.009278776739823982,"score_gpt":0.23074712694497995,"score_spread":0.22146835020515598,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2321240445","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98256785,0.00032524572,0.0000068450195,0.0005084263,0.000057091118,0.000078620345,0.0000036171866,0.0000195507,0.01643277],"genre_scores_gemma":[0.99823195,0.000088802364,0.0014589189,0.00008981124,0.000026207583,0.0000026520186,0.0000010639266,0.0000055122305,0.00009508634],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.99847126,0.00004299779,0.00026745294,0.00044041174,0.0003473569,0.00043050307],"domain_scores_gemma":[0.9996225,0.000067099485,0.00011065467,0.00012362903,0.000008491377,0.0000676211],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00094935903,0.00015712003,0.00030950335,0.00011432347,0.00049893465,0.000066896144,0.00019796283,0.00004260853,0.00008528085],"category_scores_gemma":[0.00006873422,0.00011871697,0.00007594281,0.0015160383,0.00067363743,0.00023450686,0.00028085898,0.00009465006,0.000015388507],"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":[0.0000025509742,0.000040664152,0.78255796,0.0000109185985,0.000019586749,0.0000032004502,0.003175913,0.16933349,0.044274576,0.000056391553,0.000014596765,0.000510159],"study_design_scores_gemma":[0.00077460235,0.00018300762,0.9682216,0.00019634132,0.00014245651,0.0000030958424,0.006586854,0.006690464,0.016513927,0.000101550846,0.00013244241,0.00045365802],"about_ca_topic_score_codex":0.0014866635,"about_ca_topic_score_gemma":0.0008874231,"teacher_disagreement_score":0.18566366,"about_ca_system_score_codex":0.000035067253,"about_ca_system_score_gemma":0.000014728695,"threshold_uncertainty_score":0.48411375},"labels":[],"label_agreement":null},{"id":"W2322363821","doi":"10.2514/6.2004-1095","title":"Airfoil Shape Optimization Using NURBS Representation Under Thickness Constraint","year":2004,"lang":"en","type":"article","venue":"42nd AIAA Aerospace Sciences Meeting and Exhibit","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Natural Sciences and Engineering Research Council of Canada; Fonds Québécois de la Recherche sur la Nature et les Technologies","keywords":"Airfoil; Transonic; Solver; Mach number; Representation (politics); Computer science; Mathematical optimization; Shape optimization; Flow (mathematics); Computational fluid dynamics; Mathematics; Algorithm; Aerodynamics; Aerospace engineering; Engineering; Structural engineering; Geometry; Finite element method","score_opus":0.030515210026876783,"score_gpt":0.2753654010233061,"score_spread":0.2448501909964293,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2322363821","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8979651,0.00011169253,0.091458604,0.00208783,0.00015744727,0.0001889917,0.0000017642338,0.00024547055,0.007783143],"genre_scores_gemma":[0.8982331,0.00005867514,0.10139855,0.00019583688,0.000023249377,0.0000054589104,0.0000015302511,0.000009721389,0.00007387306],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9984006,0.00004207673,0.00020195772,0.0005792158,0.00039223762,0.00038387682],"domain_scores_gemma":[0.9995205,0.000066828165,0.00013891308,0.00017351823,0.000015946764,0.00008429691],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00050067075,0.0001735474,0.00015719849,0.000056173852,0.0007628983,0.00014568253,0.00021484266,0.00010040133,0.00013682626],"category_scores_gemma":[0.00015172784,0.00014934894,0.000036422258,0.00049659825,0.0015270995,0.00056131295,0.00018158377,0.00014135867,0.000022994403],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000005300093,0.000025243618,0.008827603,0.000004791177,0.0000030167218,0.0000042417437,0.00035861763,0.9510119,0.033136737,0.0023414677,0.000019289193,0.0042618117],"study_design_scores_gemma":[0.0038502484,0.00079414144,0.019624487,0.00094535237,0.0001197133,0.00050978904,0.04156944,0.7084737,0.15538873,0.065548666,0.00040206796,0.0027736654],"about_ca_topic_score_codex":0.00038438587,"about_ca_topic_score_gemma":0.000056996527,"teacher_disagreement_score":0.24253817,"about_ca_system_score_codex":0.00012542671,"about_ca_system_score_gemma":0.000036350106,"threshold_uncertainty_score":0.6090273},"labels":[],"label_agreement":null},{"id":"W2325177980","doi":"10.2514/6.2004-454","title":"Comparison of Optimization Algorithms Applied to Aerodynamic Design","year":2004,"lang":"en","type":"article","venue":"42nd AIAA Aerospace Sciences Meeting and Exhibit","topic":"Advanced Aircraft Design and Technologies","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":"University of Toronto","funders":"","keywords":"Aerodynamics; Computer science; Optimization algorithm; Algorithm design; Algorithm; Mathematical optimization; Engineering; Aerospace engineering; Mathematics","score_opus":0.02608644645479334,"score_gpt":0.2845203022060978,"score_spread":0.25843385575130445,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2325177980","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.42668033,0.00010381574,0.56545913,0.0008056857,0.000085769396,0.00038381285,0.0000013950284,0.00019221581,0.006287872],"genre_scores_gemma":[0.68781394,0.000017026532,0.3120398,0.000054709395,0.0000075035705,0.00001088418,6.126116e-7,0.0000065809363,0.000048967107],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9985472,0.00002372395,0.0002349349,0.00047809514,0.00036587944,0.00035017348],"domain_scores_gemma":[0.9995202,0.000069524525,0.00013263142,0.00017251812,0.000010354501,0.00009481632],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005373877,0.00016136661,0.00023238864,0.00006882357,0.000360603,0.000050252012,0.0002967372,0.00007255187,0.000028162081],"category_scores_gemma":[0.00010186594,0.00013737362,0.000025706788,0.000743207,0.0006714893,0.00017412174,0.00020031918,0.00009715594,0.000032833235],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000008300244,0.00003780897,0.0047915815,0.0000045489633,0.0000018071444,5.522341e-7,0.00055133255,0.9383533,0.050623097,0.0003341767,0.000062780906,0.0052307383],"study_design_scores_gemma":[0.0027326504,0.002806558,0.015951946,0.0005151645,0.00007431535,0.000028467963,0.014077954,0.21503767,0.7317615,0.014108491,0.0006468117,0.0022584656],"about_ca_topic_score_codex":0.00011587921,"about_ca_topic_score_gemma":0.00003704798,"teacher_disagreement_score":0.7233156,"about_ca_system_score_codex":0.00007079265,"about_ca_system_score_gemma":0.000018921519,"threshold_uncertainty_score":0.56019336},"labels":[],"label_agreement":null},{"id":"W2325316534","doi":"10.2514/6.2004-63","title":"Surface Heat Transfer Study for Ice Accretion and Anti-icing Prediction in Three Dimension","year":2004,"lang":"en","type":"article","venue":"42nd AIAA Aerospace Sciences Meeting and Exhibit","topic":"Icing and De-icing Technologies","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":"Polytechnique Montréal","funders":"","keywords":"Icing; Dimension (graph theory); Heat transfer; Surface (topology); Accretion (finance); Environmental science; Meteorology; Geology; Physics; Mechanics; Geometry; Mathematics; Astrophysics","score_opus":0.017717393079870553,"score_gpt":0.2370620999022159,"score_spread":0.21934470682234536,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2325316534","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.991105,0.00034657787,0.0069413856,0.00031824622,0.00021542434,0.00038579266,0.0000029437015,0.00046401654,0.00022059603],"genre_scores_gemma":[0.99807036,0.00010320493,0.0017479961,0.00001395729,0.000028990746,0.000010194012,0.0000012335964,0.000015406966,0.0000086595555],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99886525,0.000017453074,0.00020644956,0.0003747176,0.00019024033,0.00034588654],"domain_scores_gemma":[0.9997041,0.000095350864,0.000011680183,0.00012027045,0.00002490252,0.000043667744],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0009252465,0.00017290724,0.00022098275,0.000121565674,0.00038004195,0.00011328907,0.0000896208,0.000096519,4.8932156e-7],"category_scores_gemma":[0.0000697823,0.00015126562,0.000022824841,0.00038011308,0.00015109709,0.00024606608,0.00003545333,0.00015410715,0.0000010254792],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000027495105,0.000074704396,0.23162892,0.00016754621,0.000015811947,0.000004531853,0.006182139,0.60103345,0.15715139,0.00034856773,0.000041251526,0.0033241708],"study_design_scores_gemma":[0.006830383,0.0025167975,0.21603352,0.0027642054,0.00013295388,0.000059146845,0.029826513,0.2196406,0.5183277,0.0023438924,0.0000825873,0.0014416685],"about_ca_topic_score_codex":0.00048395808,"about_ca_topic_score_gemma":0.00059866766,"teacher_disagreement_score":0.38139287,"about_ca_system_score_codex":0.00004410511,"about_ca_system_score_gemma":0.000015593072,"threshold_uncertainty_score":0.6168433},"labels":[],"label_agreement":null},{"id":"W2327536934","doi":"10.2514/6.2004-435","title":"A Modified Upwind-Biased Strategy to Calculate Flow on Structured-Unstructured Grid Topologies","year":2004,"lang":"en","type":"article","venue":"42nd AIAA Aerospace Sciences Meeting and Exhibit","topic":"Computational Fluid Dynamics and Aerodynamics","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 Waterloo","funders":"","keywords":"Grid; Network topology; Flow (mathematics); Computer science; Unstructured grid; Upwind scheme; Topology (electrical circuits); Mechanics; Mathematics; Geometry; Physics; Computer network; Mathematical analysis","score_opus":0.012304330258236957,"score_gpt":0.23405011123025327,"score_spread":0.2217457809720163,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2327536934","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9926499,0.00014854454,0.0035340004,0.0005985277,0.0007490789,0.00018680426,0.00006441231,0.00025851803,0.0018102257],"genre_scores_gemma":[0.9894762,0.000032282485,0.010085714,0.0001603557,0.00014832462,0.0000067734345,0.000014191676,0.000022257746,0.000053916905],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99837846,0.000020898815,0.00024761315,0.00047869023,0.00037231558,0.0005020204],"domain_scores_gemma":[0.99947107,0.00007780392,0.000040539944,0.00017818678,0.00004737618,0.0001850523],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00026098668,0.00028843695,0.00025466265,0.00014075672,0.00040375133,0.00027792715,0.0002478119,0.000103165345,0.0000068290005],"category_scores_gemma":[0.00006877412,0.00024777607,0.00006500751,0.00047513563,0.00018193055,0.00012640473,0.000069107526,0.00020418517,0.0000089615905],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000009063283,0.00000639763,0.00011545728,0.000018077797,0.000010300313,0.000006431303,0.00034471933,0.98399645,0.007083439,0.0055597317,0.00006904776,0.002780904],"study_design_scores_gemma":[0.0008427649,0.00041248713,0.007042702,0.00021300979,0.000017579436,0.00002929598,0.0006123252,0.9766523,0.003572091,0.009765524,0.0001262638,0.0007136315],"about_ca_topic_score_codex":0.00012975166,"about_ca_topic_score_gemma":0.0004571062,"teacher_disagreement_score":0.0073441057,"about_ca_system_score_codex":0.00009089784,"about_ca_system_score_gemma":0.00006555995,"threshold_uncertainty_score":0.99999744},"labels":[],"label_agreement":null},{"id":"W2328755083","doi":"10.2514/6.2004-433","title":"A Runge-Kutta-Newton-Krylov Algorithm for Fourth-Order Implicit Time Marching Applied to Unsteady Flows","year":2004,"lang":"en","type":"article","venue":"42nd AIAA Aerospace Sciences Meeting and Exhibit","topic":"Computational Fluid Dynamics and Aerodynamics","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":"University of Toronto","funders":"","keywords":"Runge–Kutta methods; Computer science; Applied mathematics; Newton's method; Unsteady flow; Algorithm; Mathematics; Mathematical analysis; Numerical analysis; Mechanics; Physics; Nonlinear system","score_opus":0.005877613530241315,"score_gpt":0.21981985527282366,"score_spread":0.21394224174258233,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2328755083","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.65232414,0.00012920673,0.34332088,0.0008312731,0.00030241298,0.00047211963,0.000046144516,0.00026047428,0.0023133522],"genre_scores_gemma":[0.57083833,0.000038402042,0.42805365,0.00023864707,0.00033509126,0.00007931037,0.00003710649,0.00007965177,0.00029982484],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9980984,0.000010219953,0.00030540687,0.0005632631,0.00035373858,0.00066901284],"domain_scores_gemma":[0.99928033,0.00018053775,0.0000486336,0.00017676466,0.00007965395,0.00023406216],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00064741075,0.00030189095,0.000311194,0.00016362498,0.0005488801,0.00030856064,0.00027744126,0.000085024214,0.0000055365913],"category_scores_gemma":[0.00004303397,0.00029156738,0.00007711594,0.0006082403,0.00009099876,0.00014569516,0.00012765512,0.00016566561,0.00003749141],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000005431228,0.000020217045,0.0000842842,0.000033682787,0.000021402378,0.0000018970082,0.0005862599,0.9460227,0.028753027,0.0021415057,0.00016503484,0.02216456],"study_design_scores_gemma":[0.0006394441,0.00012297086,0.0004832649,0.000119022225,0.000019453955,0.000015949608,0.00016320412,0.9943008,0.00046669476,0.0026273597,0.0005642424,0.0004776349],"about_ca_topic_score_codex":0.000069216294,"about_ca_topic_score_gemma":0.00010256261,"teacher_disagreement_score":0.08473277,"about_ca_system_score_codex":0.00010333836,"about_ca_system_score_gemma":0.00007963988,"threshold_uncertainty_score":0.9999536},"labels":[],"label_agreement":null},{"id":"W2329225652","doi":"10.2514/6.2004-84","title":"Efficient Anisotropic Mesh Adaptation on Weak and Multiple Shocks","year":2004,"lang":"en","type":"article","venue":"42nd AIAA 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":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Adaptation (eye); Anisotropy; Computer science; Physics; Optics","score_opus":0.024734789148747265,"score_gpt":0.26679846518916533,"score_spread":0.24206367604041806,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2329225652","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7942446,0.00031159222,0.20248117,0.00023355726,0.0001981226,0.000115557,0.0000019358577,0.00016643788,0.0022470597],"genre_scores_gemma":[0.7177055,0.000032106138,0.28215683,0.00003592249,0.000038026927,0.0000036872025,4.017526e-7,0.000010611218,0.000016933318],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9990178,0.000025689034,0.00016792648,0.00027362595,0.00027197986,0.00024299342],"domain_scores_gemma":[0.99929976,0.00044752692,0.000047743615,0.000086828,0.000026219237,0.000091908594],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00031635334,0.00014812914,0.0001552119,0.00006309946,0.00027352027,0.00007578421,0.000083360515,0.0000428172,0.0000020647446],"category_scores_gemma":[0.00032981456,0.00012863088,0.00002172747,0.00026365995,0.00020144653,0.00006087798,0.000039441744,0.00011582237,0.000007046568],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000027981337,0.00001399981,0.00023506314,0.000032984928,0.0000031610282,8.163899e-7,0.00067901297,0.98705286,0.0023825644,0.0052450486,0.000007336839,0.0043443637],"study_design_scores_gemma":[0.00047120513,0.00018558162,0.0008107643,0.00024235749,0.000008900131,0.000011477286,0.0014806652,0.9803244,0.004365075,0.011717592,0.000118526565,0.00026348076],"about_ca_topic_score_codex":0.00001095103,"about_ca_topic_score_gemma":0.0000043663445,"teacher_disagreement_score":0.07967566,"about_ca_system_score_codex":0.00004459699,"about_ca_system_score_gemma":0.000015314918,"threshold_uncertainty_score":0.5245415},"labels":[],"label_agreement":null},{"id":"W2330479303","doi":"10.2514/6.2004-496","title":"Analytical Modeling of Natural Convection in Concentric Spherical Enclosures","year":2004,"lang":"en","type":"article","venue":"42nd AIAA Aerospace Sciences Meeting and Exhibit","topic":"Nanofluid Flow and Heat Transfer","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 Waterloo","funders":"","keywords":"Concentric; Natural convection; Natural (archaeology); Mechanics; Convection; Computer science; Materials science; Environmental science; Physics; Geology; Geometry; Mathematics","score_opus":0.011926597947243527,"score_gpt":0.22604547440327946,"score_spread":0.21411887645603594,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2330479303","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99237645,0.0020009056,0.0027614224,0.00016862765,0.00023326484,0.000077247365,0.0000010137738,0.00006951246,0.0023115394],"genre_scores_gemma":[0.99807847,0.0002464618,0.0015759044,0.000022260398,0.000050063365,0.0000023094806,6.111447e-7,0.000008084773,0.00001581571],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99896526,0.000017371545,0.00023851873,0.00022407733,0.00023643515,0.00031832882],"domain_scores_gemma":[0.9997761,0.000043941865,0.000012014315,0.00006653166,0.000028067932,0.00007331502],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003492029,0.00012402923,0.00021386711,0.00006961982,0.000094187635,0.000041540065,0.00009160279,0.00006969151,0.000007663195],"category_scores_gemma":[0.000037506477,0.00010720243,0.000043964188,0.0005684222,0.00019195362,0.00015227405,0.00001582667,0.0001705957,0.0000029081612],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000020541569,0.00004109751,0.033839036,0.00011043265,0.000013314122,0.000008959954,0.0014896446,0.9121168,0.048174087,0.0032666146,0.00003377651,0.0008856462],"study_design_scores_gemma":[0.0011348875,0.0001366505,0.0023256578,0.00032663994,0.000020546446,0.000016715265,0.0009541724,0.96141005,0.032803327,0.00046983312,0.00006791737,0.00033358726],"about_ca_topic_score_codex":0.00026739365,"about_ca_topic_score_gemma":0.00009981926,"teacher_disagreement_score":0.04929322,"about_ca_system_score_codex":0.000045328834,"about_ca_system_score_gemma":0.00004120488,"threshold_uncertainty_score":0.43715882},"labels":[],"label_agreement":null},{"id":"W2333325203","doi":"10.2514/6.2004-121","title":"The Canadian Space Agency Microgravity Science Program Overview","year":2004,"lang":"en","type":"article","venue":"42nd AIAA Aerospace Sciences Meeting and Exhibit","topic":"Planetary Science and Exploration","field":"Physics and Astronomy","cited_by":4,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"Canadian Space Agency","funders":"","keywords":"Agency (philosophy); Space (punctuation); Weightlessness; Computer science; Aerospace engineering; Aeronautics; Engineering; Physics; Sociology; Social science","score_opus":0.021436307233028275,"score_gpt":0.2740815843724477,"score_spread":0.2526452771394194,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2333325203","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9736565,0.0008600198,0.000038107337,0.0065894076,0.0003534976,0.00034272615,0.000009995784,0.00005746121,0.018092282],"genre_scores_gemma":[0.99719167,0.00007644327,0.002258614,0.00011848885,0.000120315795,0.000017147115,0.000008982698,0.000004901701,0.00020344925],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.9979382,0.000033077868,0.00016884903,0.0005153197,0.0004988433,0.0008456801],"domain_scores_gemma":[0.9991808,0.00004305032,0.00010428591,0.00022726004,0.000083295046,0.00036130106],"candidate_categories":["sts","scholarly_communication"],"consensus_categories":[],"category_scores_codex":[0.0018663245,0.00016986005,0.0001281502,0.000093623246,0.0055301907,0.0013362275,0.0005374937,0.00002927906,0.000009015649],"category_scores_gemma":[0.00003947198,0.000115959076,0.000046433157,0.0012498205,0.0019614864,0.00073877175,0.000083631276,0.0001607902,0.00009121644],"study_design_candidate":"observational","study_design_consensus":"observational","about_ca_topic_candidate":true,"about_ca_topic_consensus":true,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000018872426,0.00029147093,0.41626692,0.00005245758,0.000044103388,0.000018268162,0.01103353,0.0061467635,0.034990095,0.28673062,0.002617677,0.24178922],"study_design_scores_gemma":[0.0038463017,0.002902952,0.36272067,0.0017084477,0.00021348051,0.00013817703,0.03256704,0.010225653,0.069576725,0.19611481,0.31419197,0.0057938006],"about_ca_topic_score_codex":0.094692506,"about_ca_topic_score_gemma":0.07885225,"teacher_disagreement_score":0.31157428,"about_ca_system_score_codex":0.00006328085,"about_ca_system_score_gemma":0.0010954983,"threshold_uncertainty_score":0.9997005},"labels":[],"label_agreement":null},{"id":"W2335025007","doi":"10.2514/6.2004-493","title":"Fluid Flow and Heat Transfer from a Cylinder Between Parallel Planes: Analytical Approach","year":2004,"lang":"en","type":"article","venue":"42nd AIAA Aerospace Sciences Meeting and Exhibit","topic":"Fluid Dynamics and Vibration Analysis","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 Waterloo","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Heat transfer; Mechanics; Fluid dynamics; Cylinder; Flow (mathematics); Materials science; Mechanical engineering; Physics; Engineering","score_opus":0.015885924702176854,"score_gpt":0.22017827843386595,"score_spread":0.20429235373168908,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2335025007","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9344005,0.00077819754,0.060748722,0.0005997026,0.000054281983,0.00008810298,0.000025513471,0.00012728285,0.0031776936],"genre_scores_gemma":[0.9876758,0.0002170587,0.011826851,0.00008352638,0.000110515706,0.000004882678,0.000029770723,0.000015257488,0.00003633972],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9986904,0.000023883795,0.00023463748,0.00042745733,0.0002836216,0.00033996327],"domain_scores_gemma":[0.999571,0.00007202186,0.0000075532184,0.00013423518,0.000018352088,0.00019679213],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00035123716,0.00020650311,0.0002984364,0.00010025751,0.00029819127,0.0002700474,0.00012643724,0.00010862526,0.000013916754],"category_scores_gemma":[0.000019392723,0.00017352469,0.000061424966,0.00035398704,0.00025189482,0.00018960702,0.000028633334,0.00014973602,0.000007008361],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000012767894,0.00003648762,0.027784506,0.00006222326,0.00012477263,0.0000052202013,0.0026834845,0.96185064,0.0043238313,0.0020299437,0.00014660362,0.00093953393],"study_design_scores_gemma":[0.0006147644,0.000053486354,0.0050239908,0.000059507853,0.00007762329,0.000004845186,0.0008162741,0.99202293,0.00056613394,0.00031488435,0.00011653363,0.00032903848],"about_ca_topic_score_codex":0.00038276537,"about_ca_topic_score_gemma":0.0001318088,"teacher_disagreement_score":0.0532753,"about_ca_system_score_codex":0.000023041423,"about_ca_system_score_gemma":0.00002658271,"threshold_uncertainty_score":0.70761317},"labels":[],"label_agreement":null},{"id":"W2335506059","doi":"10.2514/6.2004-742","title":"Second Order Sensitivity and Uncertainty Analysis of Laminar Airfoil Flows","year":2004,"lang":"en","type":"article","venue":"42nd AIAA Aerospace Sciences Meeting and Exhibit","topic":"Probabilistic and Robust Engineering Design","field":"Decision Sciences","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":"Polytechnique Montréal","funders":"","keywords":"Airfoil; Laminar flow; Sensitivity (control systems); Computer science; Order (exchange); Mechanics; Physics; Engineering; Electronic engineering; Economics","score_opus":0.03967307090387425,"score_gpt":0.3002776642155421,"score_spread":0.26060459331166785,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2335506059","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98334783,0.0004509678,0.012880817,0.00070742035,0.00015135875,0.000101925136,0.00002165505,0.00004355876,0.00229448],"genre_scores_gemma":[0.9871445,0.000039333117,0.012265098,0.00007686374,0.000034924306,0.0000025989318,0.0000015772238,0.0000063602765,0.00042876226],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99724495,0.00016481343,0.00047510347,0.00078932475,0.00092472293,0.00040108108],"domain_scores_gemma":[0.9977123,0.0012601234,0.00022998503,0.00034741513,0.00026681263,0.00018333056],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0066293217,0.00021348022,0.0005758484,0.00042707703,0.00046475945,0.00024755986,0.00026418394,0.000099027406,0.000047174937],"category_scores_gemma":[0.0025425276,0.00014925518,0.000106878004,0.0032108852,0.00084765925,0.00026125854,0.00018014712,0.00014118744,0.0000068241593],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000026223086,0.00007538774,0.029997714,0.000040942126,0.00013894618,0.000018513812,0.0031848117,0.9405844,0.015991878,0.0049288473,0.00026308632,0.004749208],"study_design_scores_gemma":[0.0028182932,0.0011521289,0.16477379,0.0005891757,0.0012073166,0.00012425866,0.015072912,0.7752219,0.012882825,0.020287719,0.0036343823,0.0022352831],"about_ca_topic_score_codex":0.00032385148,"about_ca_topic_score_gemma":0.0015248025,"teacher_disagreement_score":0.16536254,"about_ca_system_score_codex":0.000029121096,"about_ca_system_score_gemma":0.00014342158,"threshold_uncertainty_score":0.60864496},"labels":[],"label_agreement":null},{"id":"W2995714829","doi":"10.2514/6.2004-1283","title":"Turbulence Models for Flows with Free Surfaces and Interfaces","year":2004,"lang":"en","type":"article","venue":"42nd AIAA Aerospace Sciences Meeting and Exhibit","topic":"Fluid Dynamics and Heat Transfer","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 Toronto","funders":"","keywords":"Turbulence; Computer science; K-epsilon turbulence model; Mechanics; Physics","score_opus":0.011399567285548673,"score_gpt":0.1989467456201669,"score_spread":0.18754717833461823,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2995714829","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98100746,0.0024902974,0.013438523,0.0006675849,0.000117586744,0.00018657488,0.000017115306,0.00013645153,0.0019384224],"genre_scores_gemma":[0.97737545,0.00056521234,0.021905784,0.00003508309,0.000031801283,0.000013991035,9.925919e-7,0.000017904247,0.000053804823],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989855,0.00000653088,0.0001353182,0.00033665317,0.0001766077,0.00035938167],"domain_scores_gemma":[0.9996575,0.00006595756,0.000013333176,0.00012892738,0.000032303302,0.00010198348],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00033660867,0.00018273159,0.00018625463,0.000052529853,0.0003150992,0.00021052345,0.00017252081,0.000056723606,0.0000016907061],"category_scores_gemma":[0.000014713437,0.00013824193,0.00002098279,0.00016272064,0.00025905593,0.0003283511,0.000036898935,0.00009427657,9.211342e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000013617025,0.000009722909,0.0005587271,0.00013761033,0.000013108137,0.0000013481035,0.0017016242,0.98098457,0.012083517,0.0038683908,0.00006827134,0.0005594881],"study_design_scores_gemma":[0.0011350348,0.00041049777,0.0003631222,0.00056390685,0.000027618544,0.000019900828,0.0010901658,0.9789471,0.010239374,0.006554385,0.00015797451,0.0004909147],"about_ca_topic_score_codex":0.00016215593,"about_ca_topic_score_gemma":0.0007774025,"teacher_disagreement_score":0.008467261,"about_ca_system_score_codex":0.00001830069,"about_ca_system_score_gemma":0.00002848529,"threshold_uncertainty_score":0.56373423},"labels":[],"label_agreement":null},{"id":"W4230473712","doi":"10.2514/6.2004-822","title":"Thermal Resistances of Gaseous Gap for Non-Conforming Rough Contacts","year":2004,"lang":"en","type":"article","venue":"42nd AIAA 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":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Waterloo","funders":"","keywords":"Materials science; Thermal; Thermal resistance; Engineering physics; Electrical engineering; Optoelectronics; Engineering; Physics; Thermodynamics","score_opus":0.017288321647742955,"score_gpt":0.24677456902306033,"score_spread":0.22948624737531736,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4230473712","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9804165,0.0006157374,0.0016540587,0.00020389057,0.0004968674,0.00016626721,0.000008761496,0.0001051658,0.016332759],"genre_scores_gemma":[0.9944435,0.00015718357,0.004900237,0.000023450193,0.000091814305,0.000012518166,0.0000016400368,0.000013793108,0.00035589273],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99899757,0.000009635027,0.00025019562,0.00022074961,0.00019076401,0.00033111603],"domain_scores_gemma":[0.99949026,0.0001664229,0.00008555312,0.00010851251,0.0000697426,0.00007951885],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00039763478,0.00014943056,0.00020422577,0.00007048685,0.00047956358,0.00008091422,0.00012500295,0.00005971932,0.000008196517],"category_scores_gemma":[0.00008367312,0.00012869645,0.00006749553,0.00022272415,0.00016632365,0.00037185635,0.000016705459,0.000087773886,0.0000039663823],"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":[0.000099286786,0.00009459041,0.011414218,0.0005233416,0.00008414744,0.000007348821,0.0152998855,0.54732233,0.4168863,0.0035496284,0.0012873098,0.003431595],"study_design_scores_gemma":[0.0034304655,0.0012014046,0.009111005,0.002607137,0.00013966867,0.000055390647,0.027168382,0.04712555,0.88942236,0.002592074,0.0154704815,0.001676073],"about_ca_topic_score_codex":0.000244254,"about_ca_topic_score_gemma":0.00030434068,"teacher_disagreement_score":0.50019675,"about_ca_system_score_codex":0.000038243892,"about_ca_system_score_gemma":0.000056461333,"threshold_uncertainty_score":0.52480894},"labels":[],"label_agreement":null}]}