{"meta":{"query_hash":"73e1d0dea5d3","filters":{"venue":"29th AIAA Applied Aerodynamics Conference"},"cohort_total":4,"direct_labels_cover":0,"predictions_cover":4,"exported":4,"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/73e1d0dea5d3","api":"https://metacan.xera.ac/api/v1/cohort?venue=29th+AIAA+Applied+Aerodynamics+Conference"},"results":[{"id":"W1993429204","doi":"10.2514/6.2011-3519","title":"Far-Field Drag Prediction and Decomposition Method for Unsteady Flows","year":2011,"lang":"en","type":"article","venue":"29th AIAA Applied Aerodynamics Conference","topic":"Fluid Dynamics and Turbulent Flows","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université du Québec; Polytechnique Montréal","funders":"","keywords":"Drag; Field (mathematics); Decomposition; Mechanics; Computer science; Aerospace engineering; Physics; Mathematics; Engineering","score_opus":0.01391029139042882,"score_gpt":0.22613892229307428,"score_spread":0.21222863090264546,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1993429204","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0064819427,0.00013964371,0.9916078,0.000037050275,0.000046370693,0.000018024448,0.000028119455,0.0003077327,0.0013333109],"genre_scores_gemma":[0.17556201,0.00049239,0.8147376,0.00006169746,0.000092614,0.00014950172,0.00024042574,0.00028603917,0.008377742],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99983644,0.0000439192,0.000007232829,0.000017537259,0.000080155805,0.000014634536],"domain_scores_gemma":[0.99979395,0.00006369334,0.00001940049,0.00002269402,0.00008187799,0.000018331737],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00033892435,0.00048840244,0.00039292607,0.00045302894,0.00030017187,0.00041309668,0.00049143605,0.0004300132,0.0023424646],"category_scores_gemma":[0.0008150758,0.00021025084,0.00040250496,0.0002483655,0.00026640447,0.00050620874,0.00044837606,0.00080651237,0.0008716509],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00015591187,0.00015069159,0.0015636135,0.00022526075,0.000039207363,0.0001943187,0.00020079876,0.495432,0.058067072,0.05769885,0.007118127,0.37915412],"study_design_scores_gemma":[0.000006619631,0.000010564469,0.00016561883,0.00000781105,0.0000022594595,0.000019739342,0.0000054053776,0.99368614,0.0022753626,0.0016493468,0.0021635415,0.0000075504527],"about_ca_topic_score_codex":0.0017766908,"about_ca_topic_score_gemma":0.0015077643,"teacher_disagreement_score":0.0023424646,"about_ca_system_score_codex":0.00020216106,"about_ca_system_score_gemma":0.0005678147,"threshold_uncertainty_score":0.007836342},"labels":[],"label_agreement":null},{"id":"W2116708442","doi":"10.2514/6.2011-3657","title":"Unsteady Flows Past Oscillating Airfoils at Low Reynolds Numbers","year":2011,"lang":"en","type":"article","venue":"29th AIAA Applied Aerodynamics Conference","topic":"Fluid Dynamics and Turbulent Flows","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"Natural Sciences and Engineering Research Council of Canada; Consejo Nacional de Ciencia y Tecnología","keywords":"Reynolds number; Airfoil; Mechanics; Physics; Aerodynamics; Computer science; Aerospace engineering; Turbulence; Engineering","score_opus":0.013450090439184699,"score_gpt":0.18036029994221717,"score_spread":0.16691020950303248,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2116708442","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9409706,0.0003292207,0.055669006,0.00007140402,0.000026012349,0.000019259009,0.000035805853,0.00010743575,0.0027712353],"genre_scores_gemma":[0.9884015,0.00020613808,0.009991671,0.000015097926,0.00001707572,0.000012134752,0.000079008256,0.000037011992,0.0012403378],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997867,0.000026340877,0.000013809498,0.00002722268,0.00009170244,0.000054280987],"domain_scores_gemma":[0.9994093,0.00028201475,0.00008696956,0.000043758493,0.00013073246,0.000047308255],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00022178909,0.00040371664,0.0004934472,0.0008926824,0.0006078323,0.0007533356,0.0003611522,0.0004553717,0.0005577211],"category_scores_gemma":[0.0014852597,0.0001978385,0.00043024754,0.00031326443,0.0011136709,0.0008054318,0.00045010485,0.00076599856,0.00013197577],"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":[0.0007840159,0.00018026469,0.0141563285,0.00032628427,0.000054742137,0.0016761569,0.001120863,0.37417287,0.5373779,0.018972075,0.00041104402,0.050767362],"study_design_scores_gemma":[0.00003720665,0.00027814548,0.017708141,0.000050560568,0.000032019707,0.0006167756,0.00047613337,0.7997111,0.17313136,0.005648751,0.0022308296,0.00007901672],"about_ca_topic_score_codex":0.0017458666,"about_ca_topic_score_gemma":0.0010706022,"teacher_disagreement_score":0.0017458666,"about_ca_system_score_codex":0.00037838568,"about_ca_system_score_gemma":0.00031699825,"threshold_uncertainty_score":0.003471434},"labels":[],"label_agreement":null},{"id":"W2149772012","doi":"10.2514/6.2011-3178","title":"Design of Low-Sweep Wings for Maximum Range","year":2011,"lang":"en","type":"article","venue":"29th AIAA Applied Aerodynamics Conference","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 Toronto","funders":"","keywords":"Range (aeronautics); Computer science; Engineering; Aerospace engineering","score_opus":0.024842597783543786,"score_gpt":0.1990422242569765,"score_spread":0.17419962647343273,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2149772012","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.30159152,0.00037475026,0.68751097,0.00008412207,0.000023877017,0.00009229403,0.00010127559,0.00036751002,0.009853662],"genre_scores_gemma":[0.8920135,0.00010399533,0.1057649,0.000019374347,0.000008321407,0.00008857741,0.00008464764,0.00005819973,0.0018585117],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998789,0.000019204097,0.000006151429,0.000016444363,0.00005819123,0.000021084454],"domain_scores_gemma":[0.99978787,0.00006778269,0.000044899873,0.000026586597,0.000046359135,0.000026528902],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00026088842,0.00038417798,0.00032240577,0.0003446077,0.00024137016,0.00047415163,0.00044092076,0.0003535692,0.0011678565],"category_scores_gemma":[0.0004688987,0.00017899452,0.00026435655,0.0001339512,0.00020527154,0.00030382528,0.00052315847,0.0003088865,0.00034458947],"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":[0.00035993708,0.00016201957,0.00391278,0.00039253413,0.00004566415,0.00035247457,0.00018060333,0.41650972,0.4202994,0.008350309,0.0010004372,0.14843406],"study_design_scores_gemma":[0.00006924636,0.0005525507,0.003026503,0.00004372001,0.000022256861,0.00023375751,0.000053488824,0.89421856,0.09474991,0.002250184,0.004748024,0.00003183721],"about_ca_topic_score_codex":0.00019301007,"about_ca_topic_score_gemma":0.0003640486,"teacher_disagreement_score":0.0011678565,"about_ca_system_score_codex":0.0001587644,"about_ca_system_score_gemma":0.00029850638,"threshold_uncertainty_score":0.0039069057},"labels":[],"label_agreement":null},{"id":"W2314296076","doi":"10.2514/6.2011-3027","title":"CFD and Parametric study on a 155 mm artillery shell equipped with a roll-decoupled course correction fuze","year":2011,"lang":"en","type":"article","venue":"29th AIAA Applied Aerodynamics Conference","topic":"Electromagnetic Launch and Propulsion Technology","field":"Engineering","cited_by":9,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Defence Research and Development Canada","funders":"","keywords":"Fuze; Artillery; Parametric statistics; Shell (structure); Course (navigation); Engineering; Computer science; Structural engineering; Aerospace engineering; Mechanical engineering; Materials science; Mathematics","score_opus":0.013111261881800293,"score_gpt":0.18974171376772533,"score_spread":0.17663045188592505,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2314296076","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9834396,0.000054064956,0.007327127,0.00015774253,0.000032923883,0.000030067526,0.00028145034,0.00027955984,0.008397448],"genre_scores_gemma":[0.9961105,0.000018027054,0.0019244121,0.000012242338,0.0000030972494,0.000008908011,0.00008610296,0.00002329386,0.0018135111],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998122,0.000024830912,0.000007537773,0.000037212463,0.00008013774,0.000038136695],"domain_scores_gemma":[0.9996532,0.00016421807,0.000034016994,0.000048354446,0.000054929842,0.00004527775],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002488946,0.00043986074,0.00073126185,0.0003196016,0.0007864041,0.0005742936,0.00074009853,0.0011810777,0.0024778906],"category_scores_gemma":[0.00067668007,0.00027216654,0.0005188924,0.00025109484,0.00085757626,0.0005990392,0.0005901215,0.0004655158,0.0003093598],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0007947302,0.00028350062,0.0097990045,0.00015176865,0.000037904654,0.0029129523,0.00050331344,0.8536948,0.11567676,0.001800484,0.0012522192,0.013092563],"study_design_scores_gemma":[0.00009505535,0.00043737137,0.014562031,0.000014714074,0.000022845985,0.00027757703,0.00026482923,0.9561771,0.02652148,0.0002319632,0.0013342364,0.000060758834],"about_ca_topic_score_codex":0.0065859556,"about_ca_topic_score_gemma":0.003713265,"teacher_disagreement_score":0.0065859556,"about_ca_system_score_codex":0.00037184136,"about_ca_system_score_gemma":0.0006597894,"threshold_uncertainty_score":0.01309526},"labels":[],"label_agreement":null}]}