{"meta":{"query_hash":"6df3b09383e3","filters":{"venue":"21st AIAA Applied Aerodynamics Conference"},"cohort_total":5,"direct_labels_cover":0,"predictions_cover":5,"exported":5,"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/6df3b09383e3","api":"https://metacan.xera.ac/api/v1/cohort?venue=21st+AIAA+Applied+Aerodynamics+Conference"},"results":[{"id":"W2324839237","doi":"10.2514/6.2003-4296","title":"Nonlinear Theoretical Solutions for Airfoil Aerodynamics","year":2003,"lang":"en","type":"article","venue":"21st AIAA Applied Aerodynamics Conference","topic":"Computational Fluid Dynamics and Aerodynamics","field":"Engineering","cited_by":11,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"","keywords":"Airfoil; Aerodynamics; Nonlinear system; Aerospace engineering; Computer science; Physics; Engineering","score_opus":0.011695991101039598,"score_gpt":0.21106684408871354,"score_spread":0.19937085298767393,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2324839237","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":[0.0361369,0.00465411,0.6588175,0.0054307473,0.0030575797,0.000179196,0.00041791864,0.000413149,0.29089284],"genre_scores_gemma":[0.5198206,0.00798338,0.12843756,0.0013484025,0.0035500422,0.0006089146,0.00085366116,0.0008727233,0.33652467],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997533,0.00007716951,0.000010205409,0.00002276554,0.00010926885,0.000027179307],"domain_scores_gemma":[0.9997178,0.00006636515,0.000024090366,0.000030031337,0.00013628742,0.000025458916],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00045327234,0.001173308,0.0006507585,0.0012471932,0.0011308101,0.001331916,0.001641826,0.0021890367,0.009758943],"category_scores_gemma":[0.0024096349,0.00037902652,0.0008607559,0.0006041615,0.0016417252,0.0018903149,0.001907941,0.0018476994,0.0021239857],"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":[0.00001830394,0.000029714925,0.000076547534,0.00012358701,0.00001170476,0.000052886575,0.00009022937,0.09949087,0.001127479,0.88379365,0.0062188394,0.008966221],"study_design_scores_gemma":[0.000016096126,0.000009273043,0.00011475786,0.000028064538,0.0000047989693,0.00003723806,0.000060544236,0.72053343,0.0003228567,0.26649532,0.012362962,0.000014691191],"about_ca_topic_score_codex":0.0064622923,"about_ca_topic_score_gemma":0.0044676824,"teacher_disagreement_score":0.009758943,"about_ca_system_score_codex":0.0011895167,"about_ca_system_score_gemma":0.0008301819,"threshold_uncertainty_score":0.032646954},"labels":[],"label_agreement":null},{"id":"W2330275279","doi":"10.2514/6.2003-3403","title":"Numerical Correlations for Heat Transfer from an Array of Hot-Air Jets Impinging on a 3D Concave Surface","year":2003,"lang":"en","type":"article","venue":"21st AIAA Applied Aerodynamics Conference","topic":"Icing and De-icing Technologies","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":"Polytechnique Montréal","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Heat transfer; Surface (topology); Mechanics; Materials science; Physics; Geometry; Mathematics","score_opus":0.015378605725031315,"score_gpt":0.22675535666399443,"score_spread":0.21137675093896313,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2330275279","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":[0.8169094,0.00021787341,0.17631195,0.00012734006,0.000037797014,0.00008639009,0.0005431779,0.0006780516,0.005088089],"genre_scores_gemma":[0.9726273,0.00006595273,0.02651906,0.0000113491415,0.000004375584,0.00004654999,0.00024299856,0.00003725665,0.0004450691],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996928,0.000048133672,0.000023806135,0.000045009212,0.00016341079,0.00002685427],"domain_scores_gemma":[0.99812466,0.0012732047,0.00015998978,0.00014557902,0.0002632001,0.000033306515],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00057513115,0.00039108077,0.0003756287,0.0006221872,0.00038034547,0.0005966725,0.00037706847,0.00055619597,0.001349451],"category_scores_gemma":[0.0034253595,0.00020711584,0.0004186987,0.00063016446,0.000503595,0.00049911643,0.00028976,0.0005114682,0.00023635048],"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":[0.000100695164,0.0000697855,0.0069652195,0.00007770056,0.000013906571,0.00009132986,0.00008693207,0.95466393,0.02643626,0.0013233108,0.00021832224,0.009952632],"study_design_scores_gemma":[0.000006515779,0.000045202858,0.0019846845,0.0000031922068,0.0000029058779,0.000036181915,0.000021878634,0.9829359,0.01459579,0.00020861623,0.00014532183,0.000013810859],"about_ca_topic_score_codex":0.0030229678,"about_ca_topic_score_gemma":0.0024483476,"teacher_disagreement_score":0.0030229678,"about_ca_system_score_codex":0.00051371625,"about_ca_system_score_gemma":0.0005329931,"threshold_uncertainty_score":0.006010771},"labels":[],"label_agreement":null},{"id":"W2334223050","doi":"10.2514/6.2003-3526","title":"X-38 Aerodynamics During Rapid Pitch up","year":2003,"lang":"en","type":"article","venue":"21st AIAA Applied Aerodynamics Conference","topic":"Quantum, superfluid, helium dynamics","field":"Physics and Astronomy","cited_by":1,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Johnson Space Center; University of Illinois at Urbana-Champaign; Ryerson University; National Aeronautics and Space Administration","keywords":"Aerodynamics; Computer science; Aerospace engineering; Acoustics; Aeronautics; Physics; Engineering","score_opus":0.009331112123286205,"score_gpt":0.2108355445684747,"score_spread":0.20150443244518848,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2334223050","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":[0.94473124,0.0002345611,0.0047193374,0.00028402827,0.00037024912,0.00006107314,0.00016474312,0.00039558057,0.04903903],"genre_scores_gemma":[0.9890049,0.000054579858,0.00062040583,0.0000300982,0.000016586699,0.000010403673,0.00009500531,0.000044274326,0.010123665],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998609,0.000012829989,0.0000025657628,0.000020478463,0.00003920641,0.00006397643],"domain_scores_gemma":[0.9999261,0.000018698925,0.0000061788246,0.000012832979,0.000013864093,0.00002240501],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001609804,0.00029187024,0.0003117717,0.0002310317,0.0012159455,0.00051357277,0.00013437362,0.00035291235,0.011413588],"category_scores_gemma":[0.0003831869,0.0001713229,0.00018750523,0.000108361586,0.00029321905,0.00041161707,0.0009870534,0.0005449454,0.0014875344],"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":[0.0045513767,0.0003174367,0.030577471,0.00020715993,0.00007888771,0.008381916,0.003978381,0.04369856,0.7250656,0.015532099,0.019998252,0.14761284],"study_design_scores_gemma":[0.00034258614,0.0066948733,0.36602342,0.00019249695,0.00009506826,0.0044884803,0.013705655,0.19350943,0.2594825,0.010999698,0.14426103,0.00020492486],"about_ca_topic_score_codex":0.0010086606,"about_ca_topic_score_gemma":0.0011881221,"teacher_disagreement_score":0.011413588,"about_ca_system_score_codex":0.00025190966,"about_ca_system_score_gemma":0.00019443179,"threshold_uncertainty_score":0.0381822},"labels":[],"label_agreement":null},{"id":"W2334988280","doi":"10.2514/6.2003-4084","title":"Investigations of Acceleration Effects on Misssile Aerodynamics Using CFD","year":2003,"lang":"en","type":"article","venue":"21st AIAA Applied Aerodynamics Conference","topic":"Fluid dynamics and aerodynamics studies","field":"Engineering","cited_by":11,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Canadian Society of Intestinal Research","funders":"","keywords":"Aerodynamics; Acceleration; Computational fluid dynamics; Aerospace engineering; Computer science; Mechanics; Marine engineering; Aeronautics; Environmental science; Engineering; Physics; Classical mechanics","score_opus":0.01754957938426419,"score_gpt":0.21176460991168633,"score_spread":0.19421503052742214,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2334988280","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":[0.9814275,0.0013467923,0.009807439,0.000071043956,0.000054353713,0.000029627197,0.0000934151,0.00011526868,0.0070546144],"genre_scores_gemma":[0.99633396,0.0006147444,0.0019113251,0.00000919685,0.000016106056,0.000005786623,0.000049714243,0.000010367323,0.0010487154],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998135,0.00002587408,0.000008464336,0.000019584872,0.00009346948,0.0000392185],"domain_scores_gemma":[0.9994393,0.00036187068,0.000048483995,0.000039449176,0.000091438764,0.000019457411],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023741696,0.00038867793,0.00034956922,0.00047648977,0.000336035,0.00026418973,0.00019554899,0.00025132502,0.0013518886],"category_scores_gemma":[0.0011835976,0.00017486734,0.00024044196,0.00029798003,0.00034353227,0.000320609,0.0002674647,0.0002485164,0.00022449512],"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":[0.0008782735,0.00017639896,0.01689149,0.0005132771,0.000036461915,0.0016932192,0.00068084203,0.1368996,0.752874,0.0075329836,0.0007177764,0.081105754],"study_design_scores_gemma":[0.00005950169,0.0014362545,0.08456402,0.00008556574,0.00005138836,0.0011096736,0.00032271148,0.36304536,0.536692,0.0022381698,0.010299762,0.000095538],"about_ca_topic_score_codex":0.0014156495,"about_ca_topic_score_gemma":0.0010449876,"teacher_disagreement_score":0.0014156495,"about_ca_system_score_codex":0.00023061466,"about_ca_system_score_gemma":0.00013973504,"threshold_uncertainty_score":0.004522562},"labels":[],"label_agreement":null},{"id":"W2335639091","doi":"10.2514/6.2003-3416","title":"Frequency Analysis of Surface Pressures on an Airfoil After Stall","year":2003,"lang":"en","type":"article","venue":"21st AIAA Applied Aerodynamics Conference","topic":"Fluid Dynamics and Vibration Analysis","field":"Engineering","cited_by":47,"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":"McMaster University","keywords":"Angle of attack; Airfoil; Strouhal number; Vortex shedding; Freestream; Stall (fluid mechanics); Wake; Reynolds number; Mechanics; Drag; Lift (data mining); Physics; Chord (peer-to-peer); Reduced frequency; Relative wind; Acoustics; Aerodynamics; Computer science; Turbulence","score_opus":0.007919019231062042,"score_gpt":0.20708313840720852,"score_spread":0.1991641191761465,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2335639091","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":[0.9952217,0.000043579254,0.0029597613,0.000023751161,0.0000107185115,0.000006324266,0.000042041458,0.00008078217,0.0016113365],"genre_scores_gemma":[0.99927086,0.000014435259,0.0003352164,0.0000034572504,0.0000055605187,0.0000025815323,0.000040758692,0.000008049433,0.00031912592],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998524,0.000015968506,0.000003268421,0.00001465523,0.00006677999,0.000047011366],"domain_scores_gemma":[0.9996176,0.00018990455,0.00003248757,0.000027231032,0.00010293402,0.000029783736],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00013689582,0.00022485458,0.00029109739,0.0008128452,0.00032373972,0.00030415884,0.00020399006,0.00031762596,0.0016021462],"category_scores_gemma":[0.0006701311,0.00013186898,0.00021833407,0.00025420438,0.0003900245,0.00024277063,0.00022786095,0.0003918953,0.00025593006],"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":[0.0019135838,0.00029686073,0.047574986,0.00024127448,0.000056095672,0.002608584,0.0018419551,0.0502724,0.7828848,0.003365599,0.0011972436,0.10774668],"study_design_scores_gemma":[0.00006638311,0.0020142756,0.33829144,0.00004462739,0.00005083652,0.0010831341,0.0013083171,0.36093494,0.291275,0.0016459422,0.00318266,0.00010243378],"about_ca_topic_score_codex":0.00096081366,"about_ca_topic_score_gemma":0.00047603785,"teacher_disagreement_score":0.0016021462,"about_ca_system_score_codex":0.00017514819,"about_ca_system_score_gemma":0.00008549442,"threshold_uncertainty_score":0.0053597093},"labels":[],"label_agreement":null}]}