{"meta":{"query_hash":"1a8225ba8946","filters":{"venue":"19th AIAA Computational Fluid Dynamics"},"cohort_total":6,"direct_labels_cover":0,"predictions_cover":6,"exported":6,"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/1a8225ba8946","api":"https://metacan.xera.ac/api/v1/cohort?venue=19th+AIAA+Computational+Fluid+Dynamics"},"results":[{"id":"W2089731814","doi":"10.2514/6.2009-3658","title":"Interface and Boundary Schemes for High-Order Methods","year":2009,"lang":"en","type":"article","venue":"19th AIAA Computational Fluid Dynamics","topic":"Computational Fluid Dynamics and Aerodynamics","field":"Engineering","cited_by":20,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Institute for Christian Studies; University of Toronto","funders":"","keywords":"Interface (matter); Computer science; Boundary (topology); Order (exchange); Operating system; Mathematics; Business","score_opus":0.006260099130506955,"score_gpt":0.2756167408820682,"score_spread":0.26935664175156127,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2089731814","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":[0.11734979,0.000712301,0.87968445,0.0006148293,0.00051350467,0.0003131225,0.00018008813,0.00031494873,0.00031697506],"genre_scores_gemma":[0.541837,0.000039611637,0.45704308,0.00022009239,0.000089494904,0.000016569036,0.0005933139,0.000043409258,0.0001174561],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.998534,0.00003451517,0.00045461592,0.00037289047,0.00023481628,0.00036914734],"domain_scores_gemma":[0.99885225,0.0004890602,0.000048604892,0.000168741,0.00029679033,0.00014453262],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00028676176,0.00032932244,0.0003258688,0.00018584424,0.00020503231,0.00017278771,0.0001982817,0.00012373994,0.000013010301],"category_scores_gemma":[0.00007620492,0.00036978122,0.00008525274,0.0003086227,0.00007509778,0.00021798273,0.000053089563,0.00019560146,0.000008559393],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000174134,0.00003512105,0.000037551963,0.000042495,0.0000618399,0.000001403849,0.000052913856,0.73268616,0.00043101443,0.18753818,0.00029433492,0.078801595],"study_design_scores_gemma":[0.000548977,0.00009861736,0.003321525,0.000022698006,0.000025371746,0.000019734716,0.000017754171,0.87870556,0.000027897324,0.11521877,0.0016343804,0.00035872706],"about_ca_topic_score_codex":0.0000037160507,"about_ca_topic_score_gemma":0.0000132348005,"teacher_disagreement_score":0.42448717,"about_ca_system_score_codex":0.00021117742,"about_ca_system_score_gemma":0.00007860555,"threshold_uncertainty_score":0.9998754},"labels":[],"label_agreement":null},{"id":"W2105928869","doi":"10.2514/6.2009-3805","title":"Continuous Eulerian and Lagrangian Sensitivities for the Design of Airfoils in Laminar Flow","year":2009,"lang":"en","type":"article","venue":"19th AIAA Computational Fluid Dynamics","topic":"Advanced Numerical Methods in Computational Mathematics","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Polytechnique Montréal","funders":"","keywords":"Airfoil; Laminar flow; Sensitivity (control systems); Eulerian path; Smoothness; Reynolds number; Mathematics; Representation (politics); Applied mathematics; Flow (mathematics); Computation; Mathematical analysis; Mathematical optimization; Computer science; Algorithm; Geometry; Mechanics; Lagrangian; Engineering; Physics; Turbulence","score_opus":0.01452490986696015,"score_gpt":0.25645674287327247,"score_spread":0.24193183300631232,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2105928869","genre_codex":"methods","genre_gemma":"methods","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.010558974,0.00030171144,0.9880718,0.00028672742,0.00013364371,0.00042491974,0.000060983442,0.00007669161,0.00008452348],"genre_scores_gemma":[0.41916773,0.000019621044,0.580643,0.00007312801,0.000031431926,0.000013170095,0.00002208028,0.000017055105,0.000012812652],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99908537,0.000059450922,0.00034684237,0.00014160656,0.00017652307,0.00019023572],"domain_scores_gemma":[0.9959078,0.0037873564,0.000054479613,0.00010024931,0.000110978675,0.00003917792],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003529707,0.00016081502,0.00026897909,0.000097083255,0.00006317123,0.000021313881,0.0001042021,0.000055245462,0.0000018257709],"category_scores_gemma":[0.00021948681,0.00014278425,0.000047075348,0.0001992725,0.000082501036,0.00008654819,0.0000157467,0.0001012969,0.0000010591713],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00002328485,0.000023300325,0.000017651753,0.00005523821,0.000019788695,0.000002338568,0.00026720774,0.9222086,0.00012300984,0.024569074,0.0000328978,0.052657608],"study_design_scores_gemma":[0.00032377365,0.00008275792,0.0016763766,0.000043985303,0.000012815643,0.00001568015,0.000119353754,0.8633235,0.000044249733,0.13420281,0.000025336569,0.00012938457],"about_ca_topic_score_codex":0.0000016608207,"about_ca_topic_score_gemma":0.0000030533145,"teacher_disagreement_score":0.40860873,"about_ca_system_score_codex":0.00007764999,"about_ca_system_score_gemma":0.000022078108,"threshold_uncertainty_score":0.5822573},"labels":[],"label_agreement":null},{"id":"W2316589612","doi":"10.2514/6.2009-3676","title":"A Fluid-Structure Interaction Solver for Nano-Air-Vehicle Flapping Wings","year":2009,"lang":"en","type":"article","venue":"19th AIAA Computational Fluid Dynamics","topic":"Biomimetic flight and propulsion mechanisms","field":"Engineering","cited_by":24,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université Laval","funders":"","keywords":"Flapping; Solver; Fluid–structure interaction; Aerospace engineering; Aerodynamics; Computational fluid dynamics; Computer science; Aeronautics; Engineering; Finite element method; Structural engineering; Wing","score_opus":0.006965759779194092,"score_gpt":0.2195679582991298,"score_spread":0.21260219851993573,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2316589612","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":[0.26614717,0.00011761926,0.7301667,0.0007686693,0.0013413426,0.00039117172,0.00011901133,0.00041135246,0.000536986],"genre_scores_gemma":[0.9474284,0.00000664577,0.051058177,0.00048143422,0.00022120586,0.0000122930305,0.00056586356,0.000039164825,0.00018682188],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9987934,0.000016955566,0.0003503522,0.00026868682,0.00025010336,0.00032045325],"domain_scores_gemma":[0.9994527,0.00010801464,0.000048177033,0.00014423806,0.00014181739,0.00010504945],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.000107739004,0.00024630065,0.00021860337,0.00015670752,0.00017194558,0.00006751002,0.0001681887,0.00016621624,0.00007841607],"category_scores_gemma":[0.00002319154,0.0002528378,0.00012376919,0.00022149313,0.000019635714,0.00023609618,0.000021301956,0.0001662265,0.000029892137],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000096637435,0.000045084456,0.000029338236,0.000101212296,0.00008287093,0.0000041333556,0.00037016306,0.78636897,0.12635112,0.03121997,0.005818539,0.049511988],"study_design_scores_gemma":[0.00057899783,0.00009844843,0.00039464224,0.000040629504,0.000023529281,0.000019294557,0.0000358851,0.9626398,0.0057504433,0.027779832,0.0023424895,0.00029599993],"about_ca_topic_score_codex":0.0000050180215,"about_ca_topic_score_gemma":0.000007925405,"teacher_disagreement_score":0.6812812,"about_ca_system_score_codex":0.00019738279,"about_ca_system_score_gemma":0.000030626663,"threshold_uncertainty_score":0.9999924},"labels":[],"label_agreement":null},{"id":"W2321644870","doi":"10.2514/6.2009-4146","title":"Shock/Boundary Layer Interaction Effects on Transverse Jets in Crossflow on a Body of Revolution","year":2009,"lang":"en","type":"article","venue":"19th AIAA Computational Fluid Dynamics","topic":"Fluid Dynamics and Turbulent Flows","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lockheed Martin (Canada)","funders":"","keywords":"Boundary layer; Transverse plane; Mechanics; Shock (circulatory); Boundary (topology); Physics; Materials science; Engineering; Structural engineering; Medicine; Mathematics; Mathematical analysis","score_opus":0.005594139368102193,"score_gpt":0.22665959267809896,"score_spread":0.22106545330999677,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2321644870","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.95357984,0.00008363021,0.04266611,0.00025577555,0.00076597027,0.0003540978,0.00007221021,0.000157718,0.0020646711],"genre_scores_gemma":[0.99794376,0.000035363646,0.0013461583,0.00017457032,0.00010248398,0.0000117590735,0.00030780717,0.000033151446,0.00004492587],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9985964,0.00004501408,0.00042765966,0.00027312496,0.00037644058,0.0002814085],"domain_scores_gemma":[0.99939054,0.00022179176,0.000048112142,0.0001852383,0.00007650538,0.00007779001],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00014710585,0.00026085807,0.00027777432,0.00046868104,0.00006534079,0.00003830844,0.00013443599,0.00013377321,0.00001369114],"category_scores_gemma":[0.000042453725,0.00028796462,0.00012471857,0.00038544452,0.000028832023,0.00017777385,0.000009797277,0.00030964107,0.00004154894],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00016616491,0.00018561026,0.00020179697,0.000078630495,0.000026334268,0.000018958634,0.00010608499,0.9702548,0.001757762,0.018307794,0.00020323876,0.008692853],"study_design_scores_gemma":[0.0009942146,0.00038873247,0.026076876,0.0002194493,0.000010939786,0.0000065240074,0.0000054420093,0.96826667,0.00021764472,0.0034695116,0.00010894962,0.00023505131],"about_ca_topic_score_codex":0.000023554267,"about_ca_topic_score_gemma":0.000046540183,"teacher_disagreement_score":0.044363968,"about_ca_system_score_codex":0.00065796426,"about_ca_system_score_gemma":0.00006009386,"threshold_uncertainty_score":0.99995726},"labels":[],"label_agreement":null},{"id":"W2327465687","doi":"10.2514/6.2009-3803","title":"Single- and Multi-Point Aerodynamic Shape Optimization Using a Parallel Newton-Krylov Approach","year":2009,"lang":"en","type":"article","venue":"19th AIAA Computational Fluid Dynamics","topic":"Computational Fluid Dynamics and Aerodynamics","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto","funders":"Canada Research Chairs","keywords":"Aerodynamics; Computer science; Point (geometry); Newton's method; Mathematical optimization; Computational science; Mechanics; Mathematics; Physics; Geometry; Nonlinear system","score_opus":0.01417831871724563,"score_gpt":0.21840420689114437,"score_spread":0.20422588817389875,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2327465687","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":[0.26890716,0.00025171772,0.72926366,0.00014899744,0.0002476856,0.0003634339,0.000097951524,0.00039502347,0.00032433655],"genre_scores_gemma":[0.6071061,0.000042129603,0.39119405,0.00015590382,0.00008247372,0.000008834285,0.0012918428,0.00007467722,0.00004398488],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99753803,0.000058871712,0.00076264836,0.0005688233,0.00047763454,0.0005940077],"domain_scores_gemma":[0.9988994,0.00015949541,0.0001147072,0.0002759901,0.0002765652,0.00027382697],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00022048735,0.00057259866,0.0004788684,0.00037662848,0.0002842735,0.00026135746,0.00028807909,0.00022584062,0.000023418497],"category_scores_gemma":[0.000044116467,0.00066446455,0.00015308354,0.000587504,0.000105774336,0.00046401253,0.000089626286,0.00033988798,0.00001000712],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000023573637,0.00022892332,0.00031122673,0.000046140198,0.00006676326,0.0000075946455,0.00013325077,0.97337824,0.0002843738,0.01785228,0.0000372544,0.0076303687],"study_design_scores_gemma":[0.001137612,0.00009730056,0.0076215686,0.000041576575,0.00005031972,0.00013773619,0.000059017246,0.9873441,5.183957e-7,0.002806769,0.000008539576,0.00069496053],"about_ca_topic_score_codex":0.000017075141,"about_ca_topic_score_gemma":0.000022829141,"teacher_disagreement_score":0.33819893,"about_ca_system_score_codex":0.0006250317,"about_ca_system_score_gemma":0.00008827312,"threshold_uncertainty_score":0.9995807},"labels":[],"label_agreement":null},{"id":"W2329529855","doi":"10.2514/6.2009-4271","title":"A NLFD Method for the Simulation of Periodic Unsteady Flows for Overset Meshes","year":2009,"lang":"en","type":"article","venue":"19th AIAA Computational Fluid Dynamics","topic":"Fluid Dynamics and Turbulent Flows","field":"Engineering","cited_by":6,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"","keywords":"Polygon mesh; Computer science; Computational science; Parallel computing; Computer graphics (images)","score_opus":0.010917851473388957,"score_gpt":0.26411190281061075,"score_spread":0.2531940513372218,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2329529855","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":[0.020858625,0.00024525617,0.97621435,0.00031718434,0.00048942893,0.0008935415,0.0006871913,0.000120066026,0.00017434593],"genre_scores_gemma":[0.8370783,0.00001692307,0.16153994,0.0001594208,0.0001463444,0.000060099064,0.00087808387,0.000040531348,0.00008036481],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9988017,0.000021209127,0.00043830424,0.00021794726,0.00025219633,0.00026862742],"domain_scores_gemma":[0.9980514,0.0013822635,0.0000672272,0.00019921137,0.00024151386,0.000058405607],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000326357,0.00022124512,0.00027312455,0.000112483634,0.00016281228,0.000051957788,0.0002077604,0.000100029894,0.000012434528],"category_scores_gemma":[0.000090796304,0.00019243185,0.00022496744,0.0001868322,0.0000268759,0.00011579021,0.000015711397,0.00009236958,0.0000031648185],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00005443384,0.000032421045,0.000021247406,0.000063424406,0.000074865005,2.7119543e-7,0.00013359178,0.9444179,0.00013357784,0.041721404,0.00039259935,0.0129543],"study_design_scores_gemma":[0.0008592861,0.00012929807,0.000973566,0.00001843829,0.00006974982,0.0000027712874,0.000025344734,0.98492104,0.000009326101,0.011242472,0.001542992,0.00020572054],"about_ca_topic_score_codex":0.000007189388,"about_ca_topic_score_gemma":0.000020682382,"teacher_disagreement_score":0.8162197,"about_ca_system_score_codex":0.0001297149,"about_ca_system_score_gemma":0.000053799147,"threshold_uncertainty_score":0.78471434},"labels":[],"label_agreement":null}]}