{"meta":{"query_hash":"8d5076654214","filters":{"venue":"35th AIAA Applied Aerodynamics Conference"},"cohort_total":12,"direct_labels_cover":0,"predictions_cover":12,"exported":12,"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/8d5076654214","api":"https://metacan.xera.ac/api/v1/cohort?venue=35th+AIAA+Applied+Aerodynamics+Conference"},"results":[{"id":"W2637749702","doi":"10.2514/6.2017-3052","title":"Investigating the impact of using CFD generated unsteady Mach number dynamic stall data for numerical rotor analysis of helicopter forward flight","year":2017,"lang":"en","type":"article","venue":"35th AIAA Applied Aerodynamics Conference","topic":"Aerospace and Aviation Technology","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Carleton University","funders":"Natural Sciences and Engineering Research Council of Canada; National Aeronautics and Space Administration","keywords":"Stall (fluid mechanics); Mach number; Computational fluid dynamics; Aerospace engineering; Computer science; Aerodynamics; Aeronautics; Rotor (electric); Mechanics; Engineering; Physics; Mechanical engineering","score_opus":0.04157824078128461,"score_gpt":0.3241883315404269,"score_spread":0.28261009075914234,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2637749702","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":[0.73877966,0.000012898009,0.25944757,0.00004006239,0.000053229152,0.00045533225,0.00078119955,0.00008096354,0.00034909218],"genre_scores_gemma":[0.98971224,0.000027553491,0.009529032,0.0000147138,0.000021483433,0.000047304045,0.00058385445,0.00004464452,0.000019152616],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99845546,0.0000229514,0.0005434769,0.00040170428,0.00020031533,0.00037605886],"domain_scores_gemma":[0.9974144,0.000103564795,0.00050031644,0.001748664,0.00015246152,0.00008057836],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024405579,0.00029306786,0.0006573623,0.00012758914,0.00021116422,0.00009371306,0.0012909964,0.00021502301,0.000049560676],"category_scores_gemma":[0.00011071164,0.00023111395,0.00016289919,0.0003802514,0.0002524849,0.00017904132,0.00032036693,0.0002445127,0.0000040034784],"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":[0.000043932192,0.00008737569,0.019002775,0.00018042047,0.0024318804,0.0000011886383,0.00040130666,0.3415726,0.61768854,0.012322581,0.00009885888,0.0061685136],"study_design_scores_gemma":[0.00037184413,0.000020367153,0.0071657314,0.0000211918,0.0003890514,0.0000012153462,0.000075101794,0.98597157,0.0052552316,0.0004764608,0.000011679302,0.00024053706],"about_ca_topic_score_codex":0.0002307359,"about_ca_topic_score_gemma":0.00022292718,"teacher_disagreement_score":0.644399,"about_ca_system_score_codex":0.000107740845,"about_ca_system_score_gemma":0.00011015062,"threshold_uncertainty_score":0.94245535},"labels":[],"label_agreement":null},{"id":"W2646146168","doi":"10.2514/6.2017-3573","title":"Propeller Analysis Using Low & High Fidelity Aero-acoustic Methods","year":2017,"lang":"en","type":"article","venue":"35th AIAA Applied Aerodynamics Conference","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Safran Electronics (Canada)","funders":"Horizon 2020 Framework Programme; Cleansky; European Commission","keywords":"Computer science; Propeller; Fidelity; Acoustics; Engineering; Marine engineering; Telecommunications; Physics","score_opus":0.031832889073524585,"score_gpt":0.30512202469065186,"score_spread":0.27328913561712725,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2646146168","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":[0.3476822,0.000028207134,0.6446399,0.000018839957,0.00066719594,0.0003477272,0.00011264043,0.00028495354,0.0062183463],"genre_scores_gemma":[0.82392955,0.00011023041,0.17518684,0.000043390937,0.00015485301,0.000048466205,0.00014581592,0.000104922474,0.00027594838],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99685025,0.00006843094,0.00080237485,0.0008836015,0.00046391244,0.00093141396],"domain_scores_gemma":[0.99639285,0.00014429544,0.00035918833,0.0025012873,0.00028280632,0.00031954827],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0008559489,0.0006900431,0.0010047156,0.00026324397,0.00079368375,0.00070830854,0.0014740246,0.00039287,0.00031157437],"category_scores_gemma":[0.00017511995,0.0007020595,0.00026013012,0.00044722296,0.0003710848,0.00023470056,0.00045811312,0.00078920927,0.00009700559],"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":[0.00002288486,0.00006471432,0.00041522516,0.00017369782,0.00067762745,0.000010520057,0.00014675308,0.8918114,0.08565996,0.010897168,0.000059730617,0.0100603225],"study_design_scores_gemma":[0.0003810694,0.000009238485,0.0063973283,0.000039077033,0.0007692241,0.0000036359525,0.00004463085,0.9878102,0.00026716825,0.0032368898,0.0001761188,0.0008654278],"about_ca_topic_score_codex":0.00019354661,"about_ca_topic_score_gemma":0.0011306772,"teacher_disagreement_score":0.47624734,"about_ca_system_score_codex":0.00027871653,"about_ca_system_score_gemma":0.00012580225,"threshold_uncertainty_score":0.9995431},"labels":[],"label_agreement":null},{"id":"W2670941913","doi":"10.2514/6.2017-3259","title":"Accuracy of Two Nonlinear Finite Wing Models in the Aerodynamic Prediction of Wing Sweep Effects","year":2017,"lang":"en","type":"article","venue":"35th AIAA Applied Aerodynamics Conference","topic":"Turbomachinery Performance and Optimization","field":"Engineering","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":"Université du Québec","funders":"Natural Sciences and Engineering Research Council of Canada; Canada Research Chairs","keywords":"Wing; Aerodynamics; Nonlinear system; Computer science; Swept wing; Wing configuration; Control theory (sociology); Aerospace engineering; Engineering; Physics; Artificial intelligence","score_opus":0.015114986370255117,"score_gpt":0.23462575231570237,"score_spread":0.21951076594544724,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2670941913","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":[0.90184885,0.000045035376,0.09198301,0.000018222263,0.00022029063,0.00046233286,0.000043975942,0.00007711335,0.0053011356],"genre_scores_gemma":[0.9959795,0.00024714225,0.003515916,0.000018519675,0.000057527264,0.000045727927,0.00009591182,0.000033216184,0.000006577831],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99869865,0.000028425708,0.00048330196,0.00023456033,0.00026719217,0.000287866],"domain_scores_gemma":[0.99864906,0.00020994709,0.00027653988,0.0007560914,0.000070609756,0.000037773334],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00036364386,0.00024227698,0.00034784543,0.00013801588,0.0001453808,0.00007785094,0.0006641915,0.000118270524,0.000004637825],"category_scores_gemma":[0.000063886706,0.0002095759,0.000061759914,0.00016475857,0.0001057661,0.0005263272,0.00008480121,0.0003554809,0.0000034627274],"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":[0.000022608885,0.000035587782,0.001757911,0.00025694672,0.000022849084,0.000001520894,0.00090529287,0.9623484,0.018690296,0.0054542255,0.0000024373016,0.010501924],"study_design_scores_gemma":[0.0008004858,0.000029650277,0.03263595,0.00016844254,0.00003046111,0.0000015117575,0.000066383924,0.96413106,0.00087686855,0.0010928644,0.000004208431,0.00016209164],"about_ca_topic_score_codex":0.000119446355,"about_ca_topic_score_gemma":0.0003553962,"teacher_disagreement_score":0.09413058,"about_ca_system_score_codex":0.00004544911,"about_ca_system_score_gemma":0.00004544286,"threshold_uncertainty_score":0.8546257},"labels":[],"label_agreement":null},{"id":"W2676139022","doi":"10.2514/6.2017-3752","title":"Investigation of Multimodality in Aerodynamic Shape Optimization Based on the Reynolds Averaged Navier-Stokes Equations","year":2017,"lang":"en","type":"article","venue":"35th AIAA Applied Aerodynamics Conference","topic":"Computational Fluid Dynamics and Aerodynamics","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":"University of Toronto","funders":"","keywords":"Aerodynamics; Reynolds-averaged Navier–Stokes equations; Multimodality; Navier–Stokes equations; Reynolds number; Mechanics; Computational fluid dynamics; Computer science; Physics; Aerospace engineering; Engineering; Turbulence; World Wide Web","score_opus":0.025560443401500547,"score_gpt":0.2257909522489539,"score_spread":0.20023050884745336,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2676139022","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":[0.7161039,0.000008109559,0.27873355,0.00042638244,0.0002525018,0.00067580916,0.00013101642,0.00013259072,0.0035361268],"genre_scores_gemma":[0.9926326,0.000035080546,0.0065802583,0.0000908584,0.00003074502,0.00012559559,0.0004285252,0.00005842664,0.000017897895],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99784976,0.00008676447,0.00072045473,0.0004647823,0.0004894982,0.0003887538],"domain_scores_gemma":[0.99772394,0.0005358771,0.00032424598,0.0010945951,0.0002169915,0.00010437858],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0007187967,0.0003917252,0.00040332938,0.00022052009,0.00042508633,0.00022652552,0.0008802006,0.00020918234,0.00007220707],"category_scores_gemma":[0.00024464712,0.00036757014,0.00010051102,0.00030358514,0.00029383466,0.0002162541,0.00010954879,0.0005188482,0.000013838709],"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":[0.000024546345,0.000033287553,0.0016847384,0.000054860062,0.000017885512,0.0000013837792,0.00014917138,0.922579,0.0034756693,0.070274934,0.0000043034765,0.0017001976],"study_design_scores_gemma":[0.0006381001,0.000025632833,0.06607173,0.00010902801,0.000017891949,4.3735483e-7,0.000040731604,0.92921764,0.00009144022,0.0034454209,0.0000020706202,0.00033990052],"about_ca_topic_score_codex":0.000098693614,"about_ca_topic_score_gemma":0.000895499,"teacher_disagreement_score":0.2765287,"about_ca_system_score_codex":0.0002527461,"about_ca_system_score_gemma":0.00016845457,"threshold_uncertainty_score":0.99987763},"labels":[],"label_agreement":null},{"id":"W2681425999","doi":"10.2514/6.2017-4076","title":"Measuring Atmospheric Gusts at Low Altitude","year":2017,"lang":"en","type":"article","venue":"35th AIAA Applied Aerodynamics Conference","topic":"Aerospace and Aviation Technology","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":"Toronto Metropolitan University","funders":"","keywords":"Altitude (triangle); Environmental science; Remote sensing; Computer science; Aerospace engineering; Meteorology; Atmospheric sciences; Geology; Engineering; Physics; Mathematics","score_opus":0.01591011669861537,"score_gpt":0.20338555549371706,"score_spread":0.1874754387951017,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2681425999","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":[0.93588316,0.00006363955,0.032282855,0.00016557715,0.0004629046,0.00030462162,0.000014174472,0.0009911401,0.029831897],"genre_scores_gemma":[0.9957498,0.0001737103,0.003038446,0.000048496888,0.000055365315,0.00007151399,0.000021307904,0.000058083122,0.00078328105],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99865127,0.0000063868483,0.00025586883,0.00036836974,0.00022132792,0.0004967844],"domain_scores_gemma":[0.99860036,0.000020270225,0.00013718702,0.0010585071,0.00006215634,0.00012151262],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00010697032,0.0002953905,0.00031079678,0.000019449399,0.0004533698,0.00016337926,0.00082218635,0.0002479808,0.00014413695],"category_scores_gemma":[0.000032375254,0.00032115311,0.00005734368,0.00007701114,0.00016065301,0.0001549511,0.00027890698,0.00032291483,0.0005377601],"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":[0.00010539779,0.00020609055,0.043694988,0.0006289963,0.00047012,0.00008739408,0.0013298459,0.07464773,0.44445965,0.29496092,0.0029591334,0.13644975],"study_design_scores_gemma":[0.0030852328,0.00008220974,0.22406758,0.00021526027,0.000108867855,0.000029536384,0.00027130582,0.72008246,0.035953853,0.0070337914,0.0062610917,0.002808798],"about_ca_topic_score_codex":0.00002566409,"about_ca_topic_score_gemma":0.00061942125,"teacher_disagreement_score":0.64543474,"about_ca_system_score_codex":0.00019560105,"about_ca_system_score_gemma":0.00003433167,"threshold_uncertainty_score":0.99992406},"labels":[],"label_agreement":null},{"id":"W2691305584","doi":"10.2514/6.2017-3054","title":"Trim Routine for Multirotor Vehicles in Straight and Level Flight","year":2017,"lang":"en","type":"article","venue":"35th AIAA Applied Aerodynamics Conference","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":3,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"University of Waterloo","keywords":"Multirotor; Trim; Aeronautics; Aerospace engineering; Automotive engineering; Computer science; Engineering; Operating system","score_opus":0.04115607820891681,"score_gpt":0.26833158955471653,"score_spread":0.22717551134579972,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2691305584","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":[0.92097133,0.000026050839,0.062734865,0.0007395779,0.00010188308,0.001560179,0.00011446209,0.00017931583,0.013572337],"genre_scores_gemma":[0.972213,0.00006160847,0.026389457,0.00006168764,0.000016789492,0.00023589372,0.0000140196,0.00002156066,0.0009859945],"study_design_codex":"design_other","study_design_gemma":"observational","domain_scores_codex":[0.9985427,0.000010460621,0.00026437186,0.0005763537,0.0001680989,0.00043799335],"domain_scores_gemma":[0.9990327,0.000083883184,0.00018089944,0.00060171506,0.000012047573,0.00008878315],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020833494,0.00025073093,0.00028757824,0.000046989007,0.0003602529,0.0001254511,0.00065450283,0.00017331853,0.00009812728],"category_scores_gemma":[0.00011006315,0.0002278325,0.000035543842,0.000069908834,0.0005826948,0.00023075327,0.00037152116,0.00021288964,0.000033463264],"study_design_candidate":"observational","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":[0.0003646021,0.0003025519,0.06983996,0.00009169481,0.000028340211,0.000022727954,0.0005965756,0.00047550583,0.25718063,0.18148434,0.00025678755,0.48935628],"study_design_scores_gemma":[0.0056393673,0.00020513787,0.8364734,0.00007853535,0.000029607849,0.000008208469,0.0004217299,0.07347433,0.019325754,0.059230886,0.0038402313,0.0012728244],"about_ca_topic_score_codex":0.00010727786,"about_ca_topic_score_gemma":0.0011988968,"teacher_disagreement_score":0.76663345,"about_ca_system_score_codex":0.000091844595,"about_ca_system_score_gemma":0.000019915871,"threshold_uncertainty_score":0.929074},"labels":[],"label_agreement":null},{"id":"W2700303014","doi":"10.2514/6.2017-3738","title":"Preliminary investigation on stall characteristics of a Regional BWB for low speed approach","year":2017,"lang":"en","type":"article","venue":"35th AIAA Applied Aerodynamics Conference","topic":"Computational Fluid Dynamics and Aerodynamics","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université du Québec","funders":"Consejo Nacional de Ciencia y Tecnología; Compute Canada","keywords":"Stall (fluid mechanics); Computer science; Automotive engineering; Aerospace engineering; Engineering","score_opus":0.0301527715707378,"score_gpt":0.2271296085213669,"score_spread":0.19697683695062912,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2700303014","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":[0.85106,0.000009328961,0.14272727,0.00009955933,0.0003117391,0.0007900971,0.00038690536,0.00014197918,0.0044731656],"genre_scores_gemma":[0.9885662,0.000043018063,0.009818006,0.0000621919,0.00011689454,0.00007693958,0.0011482254,0.00007114366,0.00009738319],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9983241,0.000012599265,0.00053161243,0.00043272803,0.00033992765,0.00035904543],"domain_scores_gemma":[0.99845207,0.00014937388,0.00030724244,0.00071044365,0.00023699006,0.00014386504],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00022600133,0.000353825,0.00044103048,0.00012376517,0.0002494395,0.00016067702,0.00063924334,0.00018638767,0.000006151904],"category_scores_gemma":[0.00006146808,0.00038814818,0.00011215716,0.00007882483,0.00022609184,0.00013193006,0.00010410505,0.00026418563,0.000008733846],"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":[0.00042644216,0.00024645793,0.00065526046,0.0009871421,0.00016700689,0.000003439127,0.0005018721,0.2151029,0.039190713,0.7256717,0.0002404507,0.016806584],"study_design_scores_gemma":[0.0006792937,0.00010888833,0.04156305,0.00008953613,0.000030150513,0.000002986445,0.000033254877,0.9486863,0.00015686548,0.008218722,0.000050008708,0.00038092784],"about_ca_topic_score_codex":0.000009789372,"about_ca_topic_score_gemma":0.000013990737,"teacher_disagreement_score":0.7335834,"about_ca_system_score_codex":0.000110251094,"about_ca_system_score_gemma":0.0001179104,"threshold_uncertainty_score":0.99985707},"labels":[],"label_agreement":null},{"id":"W2701988502","doi":"10.2514/6.2017-4072","title":"CFD-based Performance Analysis of Morphing Aileron for Vertical Axis Wind Turbines","year":2017,"lang":"en","type":"article","venue":"35th AIAA Applied Aerodynamics Conference","topic":"Wind Energy Research and Development","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Concordia University","funders":"Compute Canada; University of Michigan","keywords":"Aileron; Morphing; Marine engineering; Wind power; Vertical axis; Computational fluid dynamics; Horizontal axis; Geology; Aerospace engineering; Computer science; Wing; Engineering; Structural engineering; Electrical engineering; Engineering drawing; Computer graphics (images)","score_opus":0.023025253422220886,"score_gpt":0.24312553124510605,"score_spread":0.22010027782288516,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2701988502","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":[0.94092155,0.000016011474,0.054019533,0.000055050594,0.00012118569,0.00022454232,0.00004526502,0.00008829383,0.0045085754],"genre_scores_gemma":[0.99578744,0.000036376652,0.00382694,0.000020665577,0.000037914564,0.000071597984,0.00013502302,0.000028557553,0.000055507397],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9985496,0.0000074442028,0.0003379279,0.000304171,0.00031173567,0.0004891349],"domain_scores_gemma":[0.99887604,0.00008881434,0.00006343121,0.0006672241,0.00013872157,0.00016576781],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023786831,0.00023398716,0.00044723455,0.00023003411,0.00023849658,0.00012754611,0.00057800516,0.00012303582,0.000056939403],"category_scores_gemma":[0.00005896921,0.00022505323,0.00011775948,0.00020533401,0.00014613855,0.00012777827,0.00008320112,0.00017733943,0.000009953392],"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":[0.0003674777,0.00012712249,0.021627892,0.00066149596,0.0014771255,0.000005040464,0.00031513124,0.8731279,0.05292596,0.017123852,0.00018522613,0.032055784],"study_design_scores_gemma":[0.00053233706,0.0000375994,0.1183028,0.000031134463,0.00011997645,1.7100918e-7,0.000018705088,0.87309074,0.0073472904,0.00011528511,0.0001501234,0.0002538294],"about_ca_topic_score_codex":0.000030898984,"about_ca_topic_score_gemma":0.00014565975,"teacher_disagreement_score":0.09667491,"about_ca_system_score_codex":0.00007859334,"about_ca_system_score_gemma":0.0001141407,"threshold_uncertainty_score":0.9177404},"labels":[],"label_agreement":null},{"id":"W2716839344","doi":"10.2514/6.2017-3755","title":"Adjoint-Based Aerodynamic Optimization of Benchmark CRM Wing","year":2017,"lang":"en","type":"article","venue":"35th AIAA Applied Aerodynamics Conference","topic":"Computational Fluid Dynamics and Aerodynamics","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"McGill University","keywords":"Aerodynamics; Benchmark (surveying); Wing; Computer science; Aerospace engineering; Engineering; Geology","score_opus":0.010492571677269923,"score_gpt":0.21247271924226843,"score_spread":0.20198014756499852,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2716839344","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":[0.37441638,0.000038276696,0.60051495,0.00009910218,0.00066568993,0.00045390285,0.00015950379,0.00031215287,0.023340076],"genre_scores_gemma":[0.9710834,0.000075611824,0.028040867,0.000044220553,0.000073167896,0.00004918998,0.00048289783,0.00010199074,0.000048679733],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99757624,0.000024473193,0.0007656463,0.0005609264,0.00050163025,0.0005710844],"domain_scores_gemma":[0.9977822,0.00013538598,0.00036395714,0.0012287269,0.00029883554,0.00019091569],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00032887887,0.00050859485,0.00059896323,0.00022978029,0.00042960266,0.00030493014,0.0010773801,0.00024547827,0.00010683675],"category_scores_gemma":[0.00007864009,0.000580691,0.00016749564,0.00020149387,0.00027936723,0.00027885672,0.00019129808,0.00040485227,0.000021930706],"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":[0.00002562956,0.000051789568,0.0005276894,0.00013908102,0.000052918793,0.0000041153853,0.000048676447,0.91115874,0.007925547,0.07540544,0.000018602015,0.0046417597],"study_design_scores_gemma":[0.00080089155,0.00003593387,0.016229706,0.0001061331,0.000046157093,0.0000030051692,0.000032357188,0.9795147,0.00015881204,0.0024663045,0.000032206226,0.00057377986],"about_ca_topic_score_codex":0.000048951122,"about_ca_topic_score_gemma":0.00033763392,"teacher_disagreement_score":0.596667,"about_ca_system_score_codex":0.00019714393,"about_ca_system_score_gemma":0.00018567339,"threshold_uncertainty_score":0.9996644},"labels":[],"label_agreement":null},{"id":"W2718484116","doi":"10.2514/6.2017-3402","title":"Effect of Leading Edge Tubercles on Transonic Performance of Airfoils","year":2017,"lang":"en","type":"article","venue":"35th AIAA Applied Aerodynamics Conference","topic":"Biomimetic flight and propulsion mechanisms","field":"Engineering","cited_by":10,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Royal Military College of Canada","funders":"","keywords":"Transonic; Airfoil; Leading edge; Computer science; Aerospace engineering; Aerodynamics; Engineering","score_opus":0.009844364776344117,"score_gpt":0.22657332582910125,"score_spread":0.21672896105275713,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2718484116","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":[0.97840303,0.000044496057,0.0021403315,0.000019866393,0.00033147875,0.00030389676,0.000023059,0.000082252984,0.018651605],"genre_scores_gemma":[0.9991048,0.00016727504,0.0005403898,0.000005889965,0.000026794954,0.000028311604,0.00001047204,0.000034975958,0.00008111304],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9988814,0.000022711178,0.0003408607,0.00023632076,0.0002249096,0.00029378323],"domain_scores_gemma":[0.9989668,0.00009708949,0.00013887227,0.00068046094,0.00004129008,0.000075473225],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00036976745,0.00026035812,0.00050375867,0.0000944347,0.00013530147,0.000035427936,0.0005888676,0.00017289372,0.00006159386],"category_scores_gemma":[0.00001500286,0.00022817565,0.00008559268,0.00006718972,0.00014353417,0.00007848876,0.00004502094,0.0002505557,0.000049446968],"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":[0.00030456018,0.000038102095,0.0004133053,0.0015600811,0.00007176362,0.000001768024,0.00025919857,0.0018349647,0.710036,0.037477802,0.000029153722,0.2479733],"study_design_scores_gemma":[0.0008135688,0.0005095295,0.0013558511,0.0002430494,0.00004675042,0.0000015603679,0.000010064423,0.104302794,0.89201856,0.00035096632,0.00006605341,0.00028127432],"about_ca_topic_score_codex":0.000009295411,"about_ca_topic_score_gemma":0.000015593498,"teacher_disagreement_score":0.24769202,"about_ca_system_score_codex":0.000032562377,"about_ca_system_score_gemma":0.000023387256,"threshold_uncertainty_score":0.9304733},"labels":[],"label_agreement":null},{"id":"W2718857711","doi":"10.2514/6.2017-3037","title":"Experimental investigation of the turbulence intensity effect on a wingtip vortex in the near field","year":2017,"lang":"en","type":"article","venue":"35th AIAA Applied Aerodynamics Conference","topic":"Fluid Dynamics and Turbulent Flows","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":"Royal Military College of Canada; Université de Sherbrooke","funders":"","keywords":"Turbulence; Vortex; Wingtip vortices; Turbulence kinetic energy; Physics; Intensity (physics); Mechanics; Aerospace engineering; Horseshoe vortex; Optics; Vortex ring; Engineering","score_opus":0.010669962827426584,"score_gpt":0.21413440332474504,"score_spread":0.20346444049731846,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2718857711","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":[0.99279344,0.000021565043,0.00031673096,0.00024240407,0.000419901,0.0004971011,0.000008774205,0.000042608153,0.005657475],"genre_scores_gemma":[0.9995075,0.000008187162,0.00013295148,0.00022393097,0.00002985027,0.00005542582,0.000007724015,0.000018904046,0.000015560627],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99896,0.000038208942,0.0002311475,0.0002485876,0.00027463873,0.00024738052],"domain_scores_gemma":[0.9987039,0.00013567758,0.00010947019,0.00097617204,0.000031845077,0.000042937154],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003284826,0.00022750928,0.00024482206,0.000034201843,0.00024515143,0.00015985705,0.0009736966,0.00011908581,0.000009877545],"category_scores_gemma":[0.00006957989,0.00015027217,0.000072965544,0.000091971444,0.00022099864,0.00007966294,0.0001385275,0.00044729473,0.000011290798],"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":[0.0006537548,0.00032538938,0.08417618,0.00067306135,0.00021925782,0.000042152875,0.014258288,0.1775208,0.3679457,0.3341273,0.0008738382,0.01918426],"study_design_scores_gemma":[0.0005173721,0.00013157623,0.105053134,0.000136073,0.000014820294,0.0000033013987,0.00006610642,0.87404585,0.018531485,0.001224145,0.000030263967,0.00024587134],"about_ca_topic_score_codex":0.00010769204,"about_ca_topic_score_gemma":0.00013656043,"teacher_disagreement_score":0.69652504,"about_ca_system_score_codex":0.00005453406,"about_ca_system_score_gemma":0.00003255262,"threshold_uncertainty_score":0.61279213},"labels":[],"label_agreement":null},{"id":"W2723527028","doi":"10.2514/6.2017-3258","title":"Aerodynamic Shape Optimization of a Box-Wing Regional Aircraft Based on the Reynolds-Averaged Navier-Stokes Equations","year":2017,"lang":"en","type":"article","venue":"35th AIAA Applied Aerodynamics Conference","topic":"Computational Fluid Dynamics and Aerodynamics","field":"Engineering","cited_by":15,"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; Embraer; Compute Canada","keywords":"Aerodynamics; Wing; Navier–Stokes equations; Reynolds number; Reynolds-averaged Navier–Stokes equations; Aerospace engineering; Mechanics; Computational fluid dynamics; Computer science; Control theory (sociology); Physics; Engineering; Turbulence; Artificial intelligence; Control (management)","score_opus":0.02159514565247826,"score_gpt":0.22656135480691408,"score_spread":0.20496620915443584,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2723527028","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":[0.3413609,0.00002540663,0.6482718,0.00094518467,0.0004512517,0.0007817757,0.00018927392,0.0003004396,0.0076739583],"genre_scores_gemma":[0.9878261,0.00007312538,0.011080619,0.00018972513,0.000080001526,0.00012484835,0.0004546151,0.0001005068,0.000070421585],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99737126,0.00006367323,0.0007370285,0.00057802815,0.00071824464,0.0005317645],"domain_scores_gemma":[0.9971056,0.0006601614,0.00038164857,0.0013893091,0.0003164667,0.00014679322],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.000546266,0.0005238192,0.00049290503,0.00021638158,0.0009060934,0.00035327545,0.0012649392,0.00022912321,0.0001460369],"category_scores_gemma":[0.0001992984,0.00048050674,0.00019724821,0.00027352365,0.0003338295,0.00022971588,0.0001574667,0.0006051806,0.000029767987],"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":[0.000033632998,0.00006510903,0.00012013919,0.00005422733,0.00005126508,0.000002747405,0.00009953029,0.8604459,0.0030335058,0.13350122,0.00003878912,0.0025539391],"study_design_scores_gemma":[0.000664817,0.00004484154,0.00731107,0.00015168152,0.000046916048,0.0000023563312,0.000060055394,0.98859876,0.000045832418,0.0025348025,0.000041486233,0.0004973548],"about_ca_topic_score_codex":0.0000362512,"about_ca_topic_score_gemma":0.00023534836,"teacher_disagreement_score":0.64646524,"about_ca_system_score_codex":0.00022766447,"about_ca_system_score_gemma":0.00021605847,"threshold_uncertainty_score":0.9997647},"labels":[],"label_agreement":null}]}