{"meta":{"query_hash":"c0049a6bd2a1","filters":{"venue":"19th AIAA Applied Aerodynamics Conference"},"cohort_total":9,"direct_labels_cover":0,"predictions_cover":9,"exported":9,"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/c0049a6bd2a1","api":"https://metacan.xera.ac/api/v1/cohort?venue=19th+AIAA+Applied+Aerodynamics+Conference"},"results":[{"id":"W2140981804","doi":"10.2514/6.2001-1328","title":"Refined design curves for compressive buckling of curved panels using nonlinear finite element analysis","year":2001,"lang":"en","type":"article","venue":"19th AIAA Applied Aerodynamics Conference","topic":"Composite Structure Analysis and Optimization","field":"Engineering","cited_by":15,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Bombardier (Canada)","funders":"","keywords":"Buckling; Finite element method; Structural engineering; Nonlinear system; RADIUS; Stress (linguistics); Compression (physics); Dependency (UML); Work (physics); Materials science; Engineering; Computer science; Composite material; Mechanical engineering; Physics","score_opus":0.029989456629779976,"score_gpt":0.24750702743697262,"score_spread":0.21751757080719264,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2140981804","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.038100526,0.00018372867,0.9605274,0.000018747467,0.000059854887,0.00047937938,0.000090834714,0.00009492904,0.00044456727],"genre_scores_gemma":[0.9019363,0.00055601,0.0967955,0.000038304162,0.00004211849,0.000035622044,0.00054390274,0.0000329775,0.000019293035],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9984417,0.00003368115,0.0006239266,0.0003412417,0.0002345026,0.00032495768],"domain_scores_gemma":[0.9987849,0.00021180832,0.00023969889,0.00039503764,0.00028750807,0.000081036116],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00023622459,0.00028883584,0.0006441058,0.00028526993,0.00010093216,0.00005209473,0.00027158242,0.000099575176,0.00009183279],"category_scores_gemma":[0.000025173598,0.00029381193,0.00019584046,0.0009279366,0.000042390173,0.00007535942,0.000046443685,0.00013639485,0.0000013525456],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00004550353,0.000022878454,0.00023077954,0.00011294402,0.00062262523,9.0818946e-7,0.00010212343,0.9742891,0.021982087,0.0005880419,0.000007823753,0.0019951616],"study_design_scores_gemma":[0.00043289893,0.000024732066,0.0004238362,0.00008213333,0.0010357753,7.0444764e-7,0.00004203152,0.99483943,0.0025081811,0.00022721551,0.000079828,0.00030321477],"about_ca_topic_score_codex":0.00003434748,"about_ca_topic_score_gemma":0.00009551207,"teacher_disagreement_score":0.86383575,"about_ca_system_score_codex":0.00007324021,"about_ca_system_score_gemma":0.000040573097,"threshold_uncertainty_score":0.9999514},"labels":[],"label_agreement":null},{"id":"W2312663217","doi":"10.2514/6.2001-1361","title":"Design and testing of an adaptive RPV aeroelastic demonstrator","year":2001,"lang":"en","type":"article","venue":"19th AIAA Applied Aerodynamics Conference","topic":"Aeroelasticity and Vibration Control","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 Victoria","funders":"","keywords":"Aeroelasticity; Computer science; Aerospace engineering; Engineering; Aerodynamics","score_opus":0.024947201235374483,"score_gpt":0.2032510557310564,"score_spread":0.17830385449568192,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2312663217","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":[0.30378518,0.00002355213,0.69276774,0.000007449404,0.00005748887,0.00026984056,0.00000997149,0.00018562593,0.0028931508],"genre_scores_gemma":[0.94807136,0.000020040916,0.05174659,0.000023668457,0.000041215448,0.000041598192,0.000010285515,0.00003203805,0.000013187346],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99884623,0.000035734676,0.000347389,0.00028292564,0.00016821046,0.00031953104],"domain_scores_gemma":[0.9990429,0.00037977053,0.00008750343,0.00021242451,0.00010777897,0.00016958683],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00016540516,0.00025139347,0.00030848422,0.00007886316,0.00009677125,0.0000576548,0.00018528473,0.00012916067,0.000036008827],"category_scores_gemma":[0.000056886744,0.00026698894,0.000020486046,0.00024053559,0.00014386773,0.00019176262,0.00003219109,0.00023403026,0.00001423597],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00031887466,0.00013610107,0.00066896656,0.00012308462,0.00013258404,0.000023608012,0.00061940384,0.56741077,0.28500468,0.06694061,0.00001914294,0.07860217],"study_design_scores_gemma":[0.00045267213,0.00017213599,0.0014520515,0.000034814704,0.000038766688,0.000016066313,0.0001537851,0.99361897,0.002402886,0.0013736687,0.000012188083,0.00027199308],"about_ca_topic_score_codex":0.000008944969,"about_ca_topic_score_gemma":0.00005339481,"teacher_disagreement_score":0.6442862,"about_ca_system_score_codex":0.000030331306,"about_ca_system_score_gemma":0.00007469103,"threshold_uncertainty_score":0.99997824},"labels":[],"label_agreement":null},{"id":"W2314374010","doi":"10.2514/6.2001-1551","title":"Optimum design of structures with multiple frequency constraints using the finite element force method","year":2001,"lang":"en","type":"article","venue":"19th AIAA Applied Aerodynamics Conference","topic":"Composite Structure Analysis and Optimization","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Victoria","funders":"","keywords":"Finite element method; Computer science; Structural engineering; Engineering","score_opus":0.01563926891493526,"score_gpt":0.23130786427347222,"score_spread":0.21566859535853697,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2314374010","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.027118407,0.000040456773,0.9703366,0.000013597601,0.00005387309,0.00043656025,0.000023462006,0.000074695796,0.0019023312],"genre_scores_gemma":[0.72568244,0.00004179295,0.27415425,0.00002113781,0.000020783022,0.000013996213,0.000033777298,0.00002427344,0.000007541521],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99876213,0.000046949117,0.00037578275,0.00026721868,0.0002476675,0.0003002571],"domain_scores_gemma":[0.99905646,0.00019820797,0.00014720057,0.00039654897,0.00013809155,0.000063467516],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018793785,0.0002760615,0.00032731664,0.00009610283,0.0001239157,0.000066814784,0.0003085235,0.00008594955,0.00014536775],"category_scores_gemma":[0.00001258442,0.00019816439,0.00005414095,0.0003639991,0.00013096821,0.00006972279,0.000038371607,0.0002064866,0.0000010509459],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000028476477,0.000006421771,0.00046345097,0.000020666845,0.00012156198,0.0000020776065,0.00022111669,0.95160764,0.03292597,0.010044416,0.0000023268665,0.004555862],"study_design_scores_gemma":[0.0004174578,0.000029205934,0.0006210179,0.000019150984,0.00010357757,0.000011833436,0.0001559944,0.9941736,0.0021472578,0.0020636658,0.000011796929,0.00024546665],"about_ca_topic_score_codex":0.00003411059,"about_ca_topic_score_gemma":0.00010328488,"teacher_disagreement_score":0.69856405,"about_ca_system_score_codex":0.00006730521,"about_ca_system_score_gemma":0.00005820006,"threshold_uncertainty_score":0.8080909},"labels":[],"label_agreement":null},{"id":"W2317622366","doi":"10.2514/6.2001-1489","title":"Finite element design and analysis of a bolted patch repair for composites","year":2001,"lang":"en","type":"article","venue":"19th AIAA Applied Aerodynamics Conference","topic":"Mechanical Behavior of Composites","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"National Research Council Canada","funders":"","keywords":"Fastener; Finite element method; Materials science; Structural engineering; Bolted joint; Composite material; Composite number; Stress (linguistics); Composite laminates; Fibre-reinforced plastic; Engineering","score_opus":0.0212073339177554,"score_gpt":0.23583224388506652,"score_spread":0.21462490996731112,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2317622366","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":[0.3274889,0.000051236708,0.67122304,0.000017201875,0.00003266978,0.00054258684,0.000059971055,0.00024528656,0.00033912394],"genre_scores_gemma":[0.9186463,0.000110287794,0.080815285,0.00002567453,0.00000963931,0.00016235812,0.00017524106,0.00003077745,0.000024429903],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99858165,0.000025671448,0.00049870176,0.00034748417,0.00020712768,0.0003393444],"domain_scores_gemma":[0.99875695,0.00048452883,0.00009803626,0.00040750086,0.00011999529,0.0001330204],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0002696607,0.0002627797,0.0005634006,0.00023333426,0.000061245555,0.000041817435,0.00023697024,0.00011401064,0.00006936555],"category_scores_gemma":[0.000020311563,0.00027409778,0.00013906747,0.0005716507,0.000055352564,0.000048298214,0.00006260629,0.00013414673,0.0000038920634],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0003881244,0.00025744716,0.009876416,0.00027988886,0.0021708189,0.0000091320435,0.00047916858,0.4169373,0.4918481,0.060789157,0.00013818759,0.01682625],"study_design_scores_gemma":[0.00048058358,0.000090705726,0.00483501,0.000019664223,0.00079834205,9.3692586e-7,0.000024488694,0.98598474,0.00657378,0.00074241153,0.0001574865,0.00029182134],"about_ca_topic_score_codex":0.000015033664,"about_ca_topic_score_gemma":0.000052519656,"teacher_disagreement_score":0.59115744,"about_ca_system_score_codex":0.0000426199,"about_ca_system_score_gemma":0.000019592535,"threshold_uncertainty_score":0.9999711},"labels":[],"label_agreement":null},{"id":"W2321209703","doi":"10.2514/6.2001-2413","title":"Investigation of propeller effects on the Aurora aircraft","year":2001,"lang":"en","type":"article","venue":"19th AIAA Applied Aerodynamics Conference","topic":"Rocket and propulsion systems research","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":"National Research Council Canada","funders":"","keywords":"Propeller; Aeronautics; Marine engineering; Environmental science; Aerospace engineering; Computer science; Engineering","score_opus":0.02745828041632807,"score_gpt":0.22050277156046694,"score_spread":0.19304449114413885,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2321209703","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9570252,0.00003297414,0.002770483,0.00021428465,0.00014653384,0.0007414739,0.00000463244,0.00014230306,0.038922172],"genre_scores_gemma":[0.99903363,0.000067990935,0.00018270577,0.000055912427,0.0000628981,0.00012861761,0.000016139627,0.000033113465,0.00041899557],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9987628,0.00006601021,0.0002800713,0.00021485209,0.0003842933,0.00029197778],"domain_scores_gemma":[0.99909836,0.0002227065,0.00005704662,0.0004317718,0.00009341823,0.000096690725],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00033592826,0.00019364241,0.00022421023,0.000094095565,0.00008754591,0.000048060134,0.00035501903,0.00010905578,0.000091542184],"category_scores_gemma":[0.000033460234,0.00013422333,0.00004136923,0.0003547338,0.000081062724,0.000049366252,0.000053707947,0.00032647653,0.00025654407],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00018292628,0.000056487646,0.0058048153,0.0011581315,0.00016969962,0.000022353554,0.0025786199,0.0037565327,0.5977605,0.034998573,0.0036891012,0.34982225],"study_design_scores_gemma":[0.0027927046,0.00048785025,0.033840068,0.00095813506,0.00006426058,0.0000244969,0.00070647756,0.27609348,0.6523262,0.016422134,0.014509599,0.0017745404],"about_ca_topic_score_codex":0.000015882275,"about_ca_topic_score_gemma":0.000024065568,"teacher_disagreement_score":0.3480477,"about_ca_system_score_codex":0.000041970794,"about_ca_system_score_gemma":0.000046388366,"threshold_uncertainty_score":0.5473469},"labels":[],"label_agreement":null},{"id":"W2326373890","doi":"10.2514/6.2001-1590","title":"Modal damping identification for a structurally nonlinear airfoil using sweep excitation","year":2001,"lang":"en","type":"article","venue":"19th AIAA Applied Aerodynamics Conference","topic":"Structural Health Monitoring Techniques","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":"McGill University","funders":"","keywords":"Airfoil; Nonlinear system; Acoustics; Modal; Excitation; Identification (biology); Structural engineering; Modal analysis; Physics; Materials science; Computer science; Engineering; Vibration; Electrical engineering; Composite material","score_opus":0.032971276505424314,"score_gpt":0.2900921508113382,"score_spread":0.2571208743059139,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2326373890","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7366516,0.000026629414,0.2610475,0.000026350017,0.00055465946,0.0006772561,0.0000349651,0.0007095846,0.0002714445],"genre_scores_gemma":[0.9084275,0.00005489936,0.090810016,0.00002337738,0.0002745436,0.00014089575,0.00017620146,0.00006950483,0.000023110677],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99830616,0.000015220088,0.0005386059,0.00040279597,0.00024496374,0.0004922445],"domain_scores_gemma":[0.99901825,0.00008664545,0.00014659985,0.0003992884,0.00023095561,0.000118240554],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00017770182,0.0003042886,0.00027746323,0.00016195515,0.00020496485,0.00013303033,0.00033874004,0.00019387442,0.000013595229],"category_scores_gemma":[0.000038831593,0.00034322572,0.000058885125,0.00027979407,0.000055280343,0.00023184849,0.000042570777,0.00025691622,0.000007946076],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0002681838,0.000040244504,0.0011671149,0.0016523168,0.00013229589,0.000007454543,0.00209691,0.14534442,0.40647176,0.07837213,0.00006165198,0.36438552],"study_design_scores_gemma":[0.0003779314,0.000024264007,0.016516069,0.00007391966,0.000027748161,0.000013801294,0.00012839265,0.9644443,0.0025321022,0.015271682,0.000148117,0.0004416676],"about_ca_topic_score_codex":0.0000817395,"about_ca_topic_score_gemma":0.00007162495,"teacher_disagreement_score":0.8190999,"about_ca_system_score_codex":0.00037539683,"about_ca_system_score_gemma":0.00006655698,"threshold_uncertainty_score":0.99990195},"labels":[],"label_agreement":null},{"id":"W2330873571","doi":"10.2514/6.2001-2456","title":"Aerodynamics of a building with momentum injection","year":2001,"lang":"en","type":"article","venue":"19th AIAA Applied Aerodynamics Conference","topic":"Wind and Air Flow Studies","field":"Environmental Science","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 British Columbia","funders":"","keywords":"Aerodynamics; Aerospace engineering; Momentum (technical analysis); Computer science; Architectural engineering; Physics; Engineering","score_opus":0.007449521089100442,"score_gpt":0.19884685499302454,"score_spread":0.1913973339039241,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2330873571","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.91693175,0.000010063601,0.036551435,0.00013440422,0.00010070064,0.0003267989,0.000012025966,0.00009231535,0.045840498],"genre_scores_gemma":[0.9952704,0.000066126646,0.0038023759,0.00007148548,0.000035477322,0.00004941392,0.000016537399,0.000028108607,0.0006600778],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.99820656,0.00002220761,0.00033707055,0.00052542123,0.0004428336,0.0004659279],"domain_scores_gemma":[0.9992215,0.00004519135,0.0002099938,0.0003779379,0.00003166663,0.000113720795],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00019177231,0.00029783818,0.00033791727,0.00006681431,0.00020219121,0.000038996375,0.00034685928,0.000093202696,0.0003559142],"category_scores_gemma":[0.000012425499,0.00025330286,0.00005299158,0.0005377089,0.00038202942,0.00016013173,0.000260312,0.00022471992,0.00006750764],"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":[0.0010705044,0.0013791732,0.3194065,0.0002045207,0.0003768627,0.00007140367,0.0039633047,0.122608185,0.2988644,0.12754275,0.00087835104,0.12363403],"study_design_scores_gemma":[0.008538492,0.0025321136,0.49459544,0.00054668175,0.0004963697,0.00030716235,0.006119533,0.43209186,0.009051689,0.028007133,0.012294277,0.005419248],"about_ca_topic_score_codex":0.00023178119,"about_ca_topic_score_gemma":0.0008273697,"teacher_disagreement_score":0.30948368,"about_ca_system_score_codex":0.00016042207,"about_ca_system_score_gemma":0.000028229953,"threshold_uncertainty_score":0.9999919},"labels":[],"label_agreement":null},{"id":"W2333840830","doi":"10.2514/6.2001-1432","title":"Aircraft loads methodology for MDO","year":2001,"lang":"en","type":"article","venue":"19th AIAA Applied Aerodynamics Conference","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Bombardier (Canada)","funders":"","keywords":"Computer science; Aerospace engineering; Aeronautics; Engineering","score_opus":0.04653456285609414,"score_gpt":0.276203338691874,"score_spread":0.22966877583577988,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2333840830","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.079008296,0.000025093426,0.88041836,0.0006467698,0.00018322363,0.0007793789,0.00002099565,0.0005321292,0.03838578],"genre_scores_gemma":[0.8310394,0.000100059835,0.16646887,0.0004143091,0.00003379048,0.00028335757,0.000032685344,0.000034690205,0.0015928004],"study_design_codex":"design_other","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.99790895,0.000042200667,0.00034429113,0.0007573042,0.00023405715,0.00071319105],"domain_scores_gemma":[0.99874645,0.00033129612,0.00014870864,0.0006179366,0.000025215422,0.00013040037],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00040009167,0.00033263737,0.00038701115,0.000068839116,0.00022040286,0.000041479343,0.0007456336,0.00026491028,0.00085276685],"category_scores_gemma":[0.00013924802,0.0003162006,0.000091509966,0.0003553793,0.00054014433,0.00014552512,0.00032073117,0.00028631414,0.00049163157],"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":[0.00033946737,0.0002251363,0.0065289605,0.000034318247,0.00005347261,0.00002821634,0.00031728362,0.004172601,0.20083636,0.32637465,0.001919838,0.4591697],"study_design_scores_gemma":[0.0033250928,0.00056840986,0.01417312,0.000033563734,0.000118162476,0.000111792986,0.0010011088,0.052357282,0.01861785,0.7477459,0.15953487,0.002412869],"about_ca_topic_score_codex":0.00004392378,"about_ca_topic_score_gemma":0.0002705544,"teacher_disagreement_score":0.75203115,"about_ca_system_score_codex":0.0001526945,"about_ca_system_score_gemma":0.000028357219,"threshold_uncertainty_score":0.999929},"labels":[],"label_agreement":null},{"id":"W4247408143","doi":"10.2514/6.2001-1657","title":"Analysis of nonlinear aeroelastic signals","year":2001,"lang":"en","type":"article","venue":"19th AIAA Applied Aerodynamics Conference","topic":"Structural Health Monitoring Techniques","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":"National Research Council Canada; Toronto Metropolitan University","funders":"","keywords":"Aeroelasticity; Nonlinear system; Computer science; Aerodynamics; Engineering; Aerospace engineering; Physics","score_opus":0.01708536188487078,"score_gpt":0.2588129540500582,"score_spread":0.24172759216518744,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4247408143","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.94861466,0.00004734789,0.04366072,0.000015761534,0.00021231714,0.00026175895,0.000051517556,0.0006893499,0.0064465785],"genre_scores_gemma":[0.9899495,0.00020056617,0.009575629,0.00001966949,0.00006532315,0.00004366069,0.00007033711,0.000038089496,0.000037190748],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9984743,0.000015891128,0.0005157512,0.000294711,0.00028071387,0.00041861137],"domain_scores_gemma":[0.9989909,0.00014240188,0.00010894467,0.00049537554,0.00012090512,0.00014149274],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00014797304,0.00026772378,0.0005478837,0.00039119727,0.00005145996,0.000027409485,0.00039895947,0.00015826985,0.0001545752],"category_scores_gemma":[0.000021689533,0.00027555227,0.00010649572,0.0012216083,0.00008415887,0.000061266684,0.00005840916,0.00027064374,0.000020495465],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00024829776,0.00018287652,0.03075457,0.0009092479,0.0031281046,0.00004655063,0.0015252666,0.5284058,0.10480838,0.045629032,0.00025266685,0.2841092],"study_design_scores_gemma":[0.00024292083,0.000049529724,0.06005467,0.00004704149,0.00044413074,0.000003883258,0.00006380682,0.9334705,0.0035069915,0.0012697405,0.00036703778,0.00047974376],"about_ca_topic_score_codex":0.000050883777,"about_ca_topic_score_gemma":0.00009766983,"teacher_disagreement_score":0.4050647,"about_ca_system_score_codex":0.000105361825,"about_ca_system_score_gemma":0.000039596074,"threshold_uncertainty_score":0.99996966},"labels":[],"label_agreement":null}]}