{"meta":{"page":1,"per_page":50,"max_per_page":100,"total":20,"total_is_capped":false,"direct_labels_cover":0,"predictions_cover":20,"direct_label_status":"direct model label, unvalidated","prediction_status":"machine_predicted_unvalidated (Codex and Gemma teacher distillation)","score_status":"score_only:v0-immature-baseline (scores rank; they never assert a category)","snapshot":{"source":"OpenAlex, pinned release, all 482 partitions","release":"2026-06-24","frame_built":"2026-07-12","author_layer_release":"2026-06-26"},"query_hash":"adcd7169a118","filters":{"venue":"55th AIAA Aerospace Sciences Meeting"}},"results":[{"id":"W2570987851","doi":"10.2514/6.2017-0583","title":"CFD Simulation of a Quad-Rotor UAV with Rotors in Motion Explicitly Modeled Using an LBM Approach with Adaptive Refinement","year":2017,"lang":"en","type":"article","venue":"55th AIAA Aerospace Sciences Meeting","topic":"Lattice Boltzmann Simulation Studies","field":"Engineering","cited_by":25,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"Extendicare (Canada)","funders":"","keywords":"Computational fluid dynamics; Computer science; Rotor (electric); Motion (physics); Control engineering; Aerospace engineering; Mechanical engineering; Artificial intelligence; Engineering","authors":[{"name":"Scott Thibault","is_ca":true},{"name":"David Holman","is_ca":false},{"name":"Santiago Garcia","is_ca":false},{"name":"Giuseppe Di Trapani","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.0857185591049446,"gpt":0.3088843665845809,"spread":0.2231658074796363,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002334092,0.0004193556,0.0007338309,0.0003948138,0.001023587,0.0008607141,0.0008442534,0.001911077,0.002400351],"category_scores_gemma":[0.001127444,0.0004735412,0.0005840784,0.0004574439,0.001018929,0.000552721,0.0007228422,0.000828149,0.0002742206],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0007379636,"about_ca_system_score_gemma":0.001497497,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.03807387,"about_ca_topic_score_gemma":0.015959,"domain_scores_codex":[0.9998426,0.00003422152,0.000009331664,0.00002231354,0.00004590955,0.00004563411],"domain_scores_gemma":[0.9995434,0.0002032614,0.00005225066,0.00003779443,0.00008349839,0.00007967214],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.00006660452,0.00004681031,0.001306963,0.00001868525,0.00001214129,0.0001660071,0.00004485496,0.9938594,0.001136412,0.001821355,0.0002901731,0.001230649],"study_design_scores_gemma":[0.00001376126,0.0000128791,0.0002757235,0.000003047659,0.000002045678,0.000009599516,0.00001926885,0.9991983,0.0001794106,0.0001408137,0.0001412166,0.000004004319],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.875388,0.0004639182,0.07433493,0.001323987,0.0003802522,0.0001343816,0.0008198035,0.000520116,0.04663462],"genre_scores_gemma":[0.984985,0.00007362688,0.01148964,0.00008338493,0.00002135659,0.0000449415,0.000188131,0.00004063682,0.003073206],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.03807387,"threshold_uncertainty_score":0.07570451,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2569681108","doi":"10.2514/6.2017-1182","title":"Development of Parametric Power Generation and Distribution Subsystem Models at the Conceptual Aircraft Design Stage","year":2017,"lang":"en","type":"article","venue":"55th AIAA Aerospace Sciences Meeting","topic":"Advanced Battery Technologies Research","field":"Engineering","cited_by":14,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"Safran Electronics (Canada)","funders":"","keywords":"Conceptual design; Parametric statistics; Stage (stratigraphy); Computer science; Power (physics); Systems engineering; Engineering; Geology; Mathematics; Physics","authors":[{"name":"Gökçin Çınar","is_ca":false},{"name":"Dimitri N. Mavris","is_ca":false},{"name":"Mathias Emeneth","is_ca":false},{"name":"Alexander Schneegans","is_ca":false},{"name":"Yann Fefermann","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.09544276669891524,"gpt":0.300953246614785,"spread":0.2055104799158697,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002656,0.0005836786,0.0004904884,0.0003607608,0.0003064014,0.0006424708,0.0009918044,0.0006844286,0.002828232],"category_scores_gemma":[0.0007867279,0.0004367561,0.0007641565,0.0002692991,0.0003067784,0.0007353531,0.0003298211,0.001045825,0.0005792329],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0006231643,"about_ca_system_score_gemma":0.0009962986,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.005629123,"about_ca_topic_score_gemma":0.005512632,"domain_scores_codex":[0.9998548,0.00003283521,0.000006849056,0.00001796709,0.00006953547,0.00001811474],"domain_scores_gemma":[0.9997246,0.0001160258,0.00002589392,0.00004945381,0.00007571488,0.000008397061],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.00001681573,0.00001382881,0.000376737,0.00006754884,0.00001026204,0.00003430712,0.00004876174,0.9846312,0.005318034,0.002413458,0.0002082124,0.006860712],"study_design_scores_gemma":[0.000005294919,0.00004774653,0.0002787043,0.00000982156,0.00001050792,0.00002197764,0.00001701819,0.9912532,0.004516625,0.000730931,0.00310053,0.000007628691],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.1720645,0.0003743371,0.7938821,0.0002357225,0.00006593053,0.0003892631,0.001277843,0.001589634,0.0301208],"genre_scores_gemma":[0.869991,0.0007169844,0.1145496,0.00004321183,0.0000179721,0.0008054526,0.0009321994,0.0002836035,0.01266001],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.005629123,"threshold_uncertainty_score":0.01119274,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2568866629","doi":"10.2514/6.2017-1425","title":"Numerical and Experimental Testing of a Morphing Upper Surface Wing Equipped with Conventional and Morphing Ailerons","year":2017,"lang":"en","type":"article","venue":"55th AIAA Aerospace Sciences Meeting","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":10,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"National Research Council Canada; Université du Québec","funders":"","keywords":"Morphing; Aileron; Computer science; Wing; Structural engineering; Computer graphics (images); Engineering","authors":[{"name":"Ruxandra Mihaela Botez","is_ca":true},{"name":"Andreea Koreanschi","is_ca":true},{"name":"Yussef Mebarki","is_ca":true},{"name":"Mahmoud Mamou","is_ca":true},{"name":"Yvan Tondji","is_ca":true},{"name":"Francesco Amoroso","is_ca":false},{"name":"Rosario Pecora","is_ca":false},{"name":"Leonardo Lecce","is_ca":false},{"name":"Gianluca Amendola","is_ca":false},{"name":"Ignazio Dimino","is_ca":false},{"name":"Antonio Concilio","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.0259881109624222,"gpt":0.2564862911149097,"spread":0.2304981801524875,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.001950141,0.0008270615,0.0004682089,0.001045555,0.0004871197,0.001171791,0.001435719,0.001462627,0.01401133],"category_scores_gemma":[0.01109577,0.0003617489,0.0009556103,0.0004589507,0.001588174,0.001039866,0.00152175,0.0009295236,0.001767713],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.000424101,"about_ca_system_score_gemma":0.0006131559,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.001534672,"about_ca_topic_score_gemma":0.001186434,"domain_scores_codex":[0.9983523,0.0003204063,0.0001672761,0.0003204323,0.0005930616,0.0002465103],"domain_scores_gemma":[0.9956226,0.002393,0.0003030022,0.0006324766,0.0007010294,0.0003478442],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.01969107,0.01004697,0.03027725,0.002446342,0.0002260471,0.002081048,0.005781304,0.08718602,0.5044852,0.01619275,0.004680949,0.3169049],"study_design_scores_gemma":[0.001388957,0.1156698,0.1065469,0.001443237,0.0008539545,0.001488722,0.009015562,0.462723,0.2379981,0.01664297,0.04566378,0.0005651275],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.9515207,0.0002264816,0.03575085,0.0002212769,0.0004908794,0.0006931681,0.0004461484,0.0002992387,0.01035122],"genre_scores_gemma":[0.9668501,0.0001923238,0.02706518,0.0001027968,0.00002991639,0.0005955065,0.0002450841,0.00007422143,0.0048449],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.01401133,"threshold_uncertainty_score":0.04687256,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2571361457","doi":"10.2514/6.2017-0048","title":"Design and Testing of Conventional Riblets and 3-D Riblets with Streamwise Variable Height","year":2017,"lang":"en","type":"article","venue":"55th AIAA Aerospace Sciences Meeting","topic":"Rheology and Fluid Dynamics Studies","field":"Chemical Engineering","cited_by":8,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"Lockheed Martin (Canada)","funders":"Air Force Research Laboratory; Langley Research Center","keywords":"Variable (mathematics); Materials science; Computer science; Mathematics; Mathematical analysis","authors":[{"name":"Paul D. McClure","is_ca":true},{"name":"Brian Smith","is_ca":true},{"name":"Wendell Baker","is_ca":true},{"name":"Pat Yagle","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.02626463300560243,"gpt":0.2471997227424631,"spread":0.2209350897368607,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.001627539,0.0006499531,0.00055675,0.0007019941,0.0003677227,0.0007900079,0.002262237,0.0013241,0.002678897],"category_scores_gemma":[0.002460738,0.00067352,0.0005813927,0.0003676891,0.0006560223,0.0008787911,0.0008702771,0.000525013,0.001267834],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0006699746,"about_ca_system_score_gemma":0.0009404701,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.0003986392,"about_ca_topic_score_gemma":0.0005979756,"domain_scores_codex":[0.9986367,0.0001743571,0.00009076938,0.0002481275,0.0006887845,0.0001613604],"domain_scores_gemma":[0.9959357,0.0006075159,0.0008516669,0.0008971942,0.001191769,0.0005162149],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","study_design_scores_codex":[0.001290267,0.0008038512,0.007450822,0.0006045102,0.00009991631,0.0006384517,0.0002919625,0.1010074,0.81392,0.004446717,0.002354467,0.06709162],"study_design_scores_gemma":[0.0002630776,0.008811986,0.01495137,0.00007656504,0.0001171944,0.0005429702,0.0001453068,0.2513314,0.7078599,0.0008143046,0.01493443,0.0001515364],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.7043846,0.000514804,0.2823185,0.0003707016,0.0004024408,0.0006435937,0.0006461656,0.002560642,0.008158564],"genre_scores_gemma":[0.8401634,0.0001854784,0.1540194,0.0001379913,0.00002919509,0.0002606745,0.0004309045,0.0001952041,0.004577892],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.002678897,"threshold_uncertainty_score":0.008961797,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2568424546","doi":"10.2514/6.2017-0085","title":"Finite-Element Formulation of a Jacobian-free Solver for Supersonic Viscous Flows on Hybrid Grids","year":2017,"lang":"en","type":"article","venue":"55th AIAA Aerospace Sciences Meeting","topic":"Computational Fluid Dynamics and Aerodynamics","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"McGill University","funders":"","keywords":"Jacobian matrix and determinant; Inviscid flow; Mach number; Solver; Roe solver; Discretization; Polygon mesh; Finite element method; Mathematics; Mesh generation; Applied mathematics; Computer science; Mathematical analysis; Geometry; Mathematical optimization; Physics; Classical mechanics; Mechanics","authors":[{"name":"Song Gao","is_ca":true},{"name":"Wagdi G. Habashi","is_ca":true},{"name":"Marco Fossati","is_ca":true},{"name":"Dario Isola","is_ca":false},{"name":"Guido S. Baruzzi","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.01785418759972015,"gpt":0.2596866441245497,"spread":0.2418324565248295,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002765402,0.0004148441,0.0004326383,0.0002806446,0.000370118,0.0005075567,0.001217965,0.000709064,0.003211429],"category_scores_gemma":[0.0005500619,0.0002695411,0.0004199268,0.0002498821,0.000390627,0.0004167977,0.0008774959,0.000717973,0.000830354],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0002665226,"about_ca_system_score_gemma":0.0008063514,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.00169164,"about_ca_topic_score_gemma":0.001752608,"domain_scores_codex":[0.9998241,0.00002777608,0.00000903927,0.00001597351,0.0001094124,0.00001373827],"domain_scores_gemma":[0.999757,0.00007684271,0.00002140393,0.00003878625,0.00008539556,0.00002047028],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.00005914709,0.00008927903,0.001054519,0.0001559799,0.00004229164,0.0002534456,0.0001387875,0.8048079,0.04756124,0.06434809,0.004001197,0.07748808],"study_design_scores_gemma":[0.000009540642,0.00002007244,0.00007702877,0.00000353285,0.000003329121,0.00003842555,0.000007593808,0.9918416,0.003001261,0.001754881,0.003237044,0.000005710619],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"methods","genre_scores_codex":[0.009519906,0.00005230236,0.98531,0.00007106767,0.00004485227,0.00004158368,0.00008817641,0.0004106006,0.0044615],"genre_scores_gemma":[0.2663242,0.0001486981,0.7217522,0.00009166021,0.00005718308,0.0003250089,0.0004762034,0.0002565228,0.01056836],"genre_candidate":"methods","genre_consensus":"methods","teacher_disagreement_score":0.003211429,"threshold_uncertainty_score":0.01074332,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2569828073","doi":"10.2514/6.2017-0582","title":"Stitching and Deformation of Non-overlapping Meshes for Unsteady Rotorcraft Aerodynamics","year":2017,"lang":"en","type":"article","venue":"55th AIAA Aerospace Sciences Meeting","topic":"Icing and De-icing Technologies","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":true,"ca_venue":false,"about_ca":false},"ca_institutions":"McGill University","funders":"Natural Sciences and Engineering Research Council of Canada; Compute Canada","keywords":"Aerodynamics; Image stitching; Polygon mesh; Deformation (meteorology); Computer science; Aerospace engineering; Mechanical engineering; Computer graphics (images); Engineering; Geology; Artificial intelligence","authors":[{"name":"Munir Nathoo","is_ca":true},{"name":"Wagdi G. Habashi","is_ca":true},{"name":"Marco Fossati","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.01565630077705181,"gpt":0.2641981948351256,"spread":0.2485418940580738,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005389079,0.0004622535,0.000468508,0.0004651592,0.0003987042,0.0006469603,0.0007443651,0.001157275,0.002650976],"category_scores_gemma":[0.003935181,0.0003939429,0.0005021744,0.0004131211,0.0006974403,0.0008549967,0.0008122865,0.0009661065,0.0003023348],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0002827098,"about_ca_system_score_gemma":0.000428634,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.001962624,"about_ca_topic_score_gemma":0.002718689,"domain_scores_codex":[0.9996574,0.00008984195,0.00002323932,0.00004876449,0.0001418958,0.00003878601],"domain_scores_gemma":[0.9985657,0.0007450947,0.000110722,0.0003131779,0.0001872632,0.00007806761],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.0003793367,0.0001825027,0.002581901,0.0001411144,0.00004590576,0.0001969321,0.0003226032,0.8245524,0.0391186,0.009145973,0.001344012,0.1219888],"study_design_scores_gemma":[0.000004565788,0.00002432762,0.0002133946,0.00000354349,0.000001398387,0.00001847593,0.00001441009,0.9968916,0.001991544,0.0005585349,0.0002743132,0.000003919601],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.2922625,0.0003296081,0.7013187,0.0002160809,0.0002201858,0.00008224988,0.0001390007,0.0008105556,0.004621027],"genre_scores_gemma":[0.8542716,0.0001304172,0.1425522,0.00004437214,0.00004210206,0.00004256675,0.000196125,0.000262101,0.002458648],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.002650976,"threshold_uncertainty_score":0.008868396,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2568092284","doi":"10.2514/6.2017-0302","title":"Effect of Freestream Turbulence on Laminar Separation Bubbles and Flow Transition on an SD7003 Airfoil at Low Reynolds Numbers","year":2017,"lang":"en","type":"article","venue":"55th AIAA Aerospace Sciences Meeting","topic":"Fluid Dynamics and Turbulent Flows","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":true,"ca_venue":false,"about_ca":false},"ca_institutions":"University of Toronto","funders":"Natural Sciences and Engineering Research Council of Canada; Kenneth M. Molson Foundation","keywords":"Airfoil; Freestream; Laminar flow; Reynolds number; Turbulence; Mechanics; Flow separation; Separation (statistics); Materials science; Physics; Mathematics","authors":[{"name":"Jacob Zilli","is_ca":true},{"name":"David Sutton","is_ca":true},{"name":"Philippe Lavoie","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.00615829171272323,"gpt":0.2516035620872877,"spread":0.2454452703745645,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002394569,0.000276016,0.0004693895,0.0003369372,0.0008040828,0.0007224118,0.0002757972,0.0004045686,0.002053302],"category_scores_gemma":[0.0008901038,0.0001651955,0.0002906742,0.0001975155,0.0006676004,0.0005050792,0.0004219555,0.000591833,0.0001550402],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0005943167,"about_ca_system_score_gemma":0.0003781194,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.003366144,"about_ca_topic_score_gemma":0.002362836,"domain_scores_codex":[0.9998149,0.00002345043,0.00001036454,0.00003200324,0.00004123072,0.00007799637],"domain_scores_gemma":[0.9989753,0.0005343583,0.00008066403,0.0000528325,0.0001469071,0.0002099245],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.007314538,0.0006244329,0.01050345,0.0001780794,0.00005545908,0.0009256076,0.0005226859,0.02486439,0.9377917,0.0009122056,0.0009370361,0.01537047],"study_design_scores_gemma":[0.0002097468,0.002078322,0.03329731,0.00002430344,0.00008939326,0.0001177235,0.0003330205,0.1242277,0.8386405,0.0002330645,0.0006727482,0.0000761569],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.9990036,0.0000751199,0.0004422684,0.00003251651,0.00001307314,0.000002856822,0.00002790674,0.00004236805,0.0003602543],"genre_scores_gemma":[0.9996997,0.00001902143,0.0001125932,0.000008910343,0.000002938625,0.000001279422,0.00002131278,0.000008565439,0.000125614],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.003366144,"threshold_uncertainty_score":0.006868958,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2568679852","doi":"10.2514/6.2017-0150","title":"Investigation of Engine Performance at Altitude Using Selected Alternative Fuels for the National Jet Fuels Combustion Program","year":2017,"lang":"en","type":"article","venue":"55th AIAA Aerospace Sciences Meeting","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":6,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":true,"ca_venue":false,"about_ca":true},"ca_institutions":"National Research Council Canada","funders":"Air Force Research Laboratory; Ministère de la Défense Nationale","keywords":"Combustion; Jet fuel; Jet engine; Alternative fuels; Jet (fluid); Altitude (triangle); Aerospace engineering; Environmental science; Automotive engineering; Aeronautics; Nuclear engineering; Engineering; Chemistry","authors":[{"name":"Pervez Canteenwalla","is_ca":true},{"name":"Wajid A. Chishty","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.06407679783589447,"gpt":0.3120203385345566,"spread":0.2479435406986621,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003493746,0.0002389549,0.0002297304,0.0004507265,0.0003996856,0.0002912931,0.0003720444,0.0003288375,0.0008211503],"category_scores_gemma":[0.0004608839,0.000105906,0.0002288859,0.0003774401,0.0001209828,0.000265088,0.0001863178,0.0002435057,0.0001887015],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0003851624,"about_ca_system_score_gemma":0.0002401684,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.007613993,"about_ca_topic_score_gemma":0.01481854,"domain_scores_codex":[0.9996749,0.00003276492,0.00002389145,0.00003942579,0.0001865612,0.00004251394],"domain_scores_gemma":[0.9996712,0.00007024769,0.00004025945,0.00001990435,0.0001654829,0.00003286329],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","study_design_scores_codex":[0.003149067,0.000849158,0.04742556,0.000317666,0.00008559017,0.0003660753,0.000253568,0.006443217,0.917481,0.0001057255,0.0001854382,0.02333786],"study_design_scores_gemma":[0.00004934498,0.00871668,0.1745398,0.00001542916,0.00008613399,0.0002462666,0.0002758249,0.008245239,0.8067778,0.00003191243,0.0009847496,0.00003080603],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.9991731,0.00009005184,0.0002129892,0.000004557457,0.000002673869,0.00001138692,0.0000991733,0.000005221415,0.0004008221],"genre_scores_gemma":[0.9986023,0.0001174903,0.0005803721,0.000005697832,0.000001248998,0.000007770934,0.0002673055,0.000004020066,0.0004137591],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.007613993,"threshold_uncertainty_score":0.01513934,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2568339193","doi":"10.2514/6.2017-0082","title":"An hp-Adaptive Unstructured Finite Volume Solver for Compressible Aerodynamic Flows","year":2017,"lang":"en","type":"article","venue":"55th AIAA Aerospace Sciences Meeting","topic":"Computational Fluid Dynamics and Aerodynamics","field":"Engineering","cited_by":6,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"University of British Columbia","funders":"","keywords":"Aerodynamics; Finite volume method; Solver; Compressibility; Computer science; Compressible flow; Volume (thermodynamics); Aerospace engineering; Mechanics; Physics; Engineering","authors":[{"name":"Alireza Jalali","is_ca":true},{"name":"Carl Ollivier‐Gooch","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.01760143425219322,"gpt":0.2687216349073301,"spread":0.2511202006551369,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001869283,0.0003453689,0.0004204053,0.0001877367,0.0003109032,0.0004285039,0.001340877,0.0005831025,0.006081983],"category_scores_gemma":[0.0009710348,0.0002477877,0.0002967035,0.0002517843,0.0003336272,0.0005108085,0.001058438,0.0008015163,0.001106932],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0001633444,"about_ca_system_score_gemma":0.0006557688,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.00281014,"about_ca_topic_score_gemma":0.003303653,"domain_scores_codex":[0.9998729,0.00002703396,0.00000596264,0.00001557201,0.00006299927,0.00001542961],"domain_scores_gemma":[0.9997472,0.00008060927,0.00001315874,0.00003983156,0.00009356059,0.00002571709],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.0002824021,0.0002193791,0.001627991,0.0002090497,0.00005785926,0.0002814622,0.0001576098,0.6861314,0.03136202,0.0171976,0.0113172,0.2511561],"study_design_scores_gemma":[0.0000277735,0.00002050051,0.0001141299,0.000003885395,0.000002931907,0.00002259493,0.000006456723,0.9945327,0.001810992,0.000887241,0.00256671,0.00000404317],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"methods","genre_scores_codex":[0.04964172,0.0001844763,0.9224514,0.0002024779,0.0002478593,0.0001357056,0.0002774016,0.00357823,0.02328066],"genre_scores_gemma":[0.3045702,0.0001442215,0.6802116,0.0002139435,0.00009511355,0.000238011,0.0005660839,0.000895603,0.01306527],"genre_candidate":"methods","genre_consensus":"methods","teacher_disagreement_score":0.006081983,"threshold_uncertainty_score":0.02034622,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2569931528","doi":"10.2514/6.2017-1007","title":"Linearized Fluid Film Forces for Squeeze Film Dampers Executing Small Amplitude Circular-Centered Orbits in Aero-Engines","year":2017,"lang":"en","type":"article","venue":"55th AIAA Aerospace Sciences Meeting","topic":"Tribology and Lubrication Engineering","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"University of Toronto","funders":"","keywords":"Damper; Amplitude; Structural engineering; Mechanics; Engineering; Materials science; Physics; Optics","authors":[{"name":"Sina Hamzelouia","is_ca":true},{"name":"Kamran Behdinan","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.03309901311235415,"gpt":0.2677597233744827,"spread":0.2346607102621285,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001419249,0.0003417915,0.0002793324,0.0003311687,0.0004142981,0.0006889189,0.0003445068,0.0006085809,0.003647096],"category_scores_gemma":[0.001114175,0.0002093926,0.0002131851,0.0001537898,0.0005642333,0.0005128686,0.0004739309,0.0004639259,0.0002698813],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0004276092,"about_ca_system_score_gemma":0.0003926484,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.005426985,"about_ca_topic_score_gemma":0.00387448,"domain_scores_codex":[0.9999347,0.00001557155,0.000003005365,0.000007937727,0.00002143996,0.00001739336],"domain_scores_gemma":[0.99978,0.0001043656,0.00002678494,0.00001573642,0.0000433594,0.00002970126],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.001227825,0.0002688056,0.0053154,0.000142335,0.00005361949,0.0007035108,0.0006649456,0.8786016,0.07418458,0.01126307,0.001270722,0.02630368],"study_design_scores_gemma":[0.00001577253,0.00007777441,0.001876693,0.000004981667,0.000004715532,0.00002018233,0.00009290932,0.9918372,0.005413664,0.0004502305,0.0001944465,0.00001145368],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.971215,0.0001032074,0.02131502,0.0001719208,0.00003969932,0.00002456925,0.0000754388,0.00025399,0.006801215],"genre_scores_gemma":[0.9974186,0.00002140658,0.0009821361,0.000007835934,0.000002831964,0.000005047096,0.0000237074,0.00002763235,0.001510775],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.005426985,"threshold_uncertainty_score":0.01220071,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2570207712","doi":"10.2514/6.2017-0267","title":"Effects of Speed on Coupled Sweep and Camber in Morphing Wings","year":2017,"lang":"en","type":"article","venue":"55th AIAA Aerospace Sciences Meeting","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":false,"ca_fund":true,"ca_venue":false,"about_ca":false},"ca_institutions":"","funders":"Air Force Office of Scientific Research; Natural Sciences and Engineering Research Council of Canada; U.S. Air Force","keywords":"Morphing; Camber (aerodynamics); Computer science; Aerospace engineering; Engineering; Computer graphics (images)","authors":[{"name":"Lawren L. Gamble","is_ca":false},{"name":"Amin Moosavian","is_ca":false},{"name":"Daniel J. Inman","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.00983558498725836,"gpt":0.2351978842209249,"spread":0.2253622992336665,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003935446,0.0001859016,0.000307327,0.0004564815,0.0004640228,0.0007035462,0.000238253,0.0005021955,0.006069316],"category_scores_gemma":[0.004220535,0.0002203094,0.0001697822,0.0001631206,0.0002763175,0.0004801594,0.0004948586,0.0002144784,0.0008077271],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0001370318,"about_ca_system_score_gemma":0.0002284949,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.0005266783,"about_ca_topic_score_gemma":0.0009892521,"domain_scores_codex":[0.9997037,0.00006382123,0.00001286185,0.00004408449,0.0001169459,0.00005861706],"domain_scores_gemma":[0.9966061,0.001835277,0.0002465617,0.0001655226,0.0008763005,0.0002703182],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","study_design_scores_codex":[0.004328676,0.0003013336,0.04430624,0.0002699002,0.0001138213,0.001295659,0.0005984641,0.04376556,0.7912172,0.0009720815,0.001173038,0.1116582],"study_design_scores_gemma":[0.0001497212,0.002245912,0.3463657,0.00005972642,0.0001635283,0.001023894,0.001281629,0.2783479,0.3650509,0.0008148191,0.004372175,0.000124066],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.997,0.00006828026,0.001201005,0.00002758122,0.00002717994,0.000007351503,0.00001833374,0.00002975593,0.001620454],"genre_scores_gemma":[0.9986017,0.00003004081,0.0003494173,0.000005093997,0.000005086104,0.000001908417,0.00001543575,0.00002946342,0.0009617476],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.006069316,"threshold_uncertainty_score":0.02030385,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2568480339","doi":"10.2514/6.2017-0734","title":"Reconstruction Map Stability Analysis for Cell Centered Finite Volume Methods on Unstructured Meshes","year":2017,"lang":"en","type":"article","venue":"55th AIAA Aerospace Sciences Meeting","topic":"Advanced Numerical Methods in Computational Mathematics","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"University of British Columbia","funders":"","keywords":"Polygon mesh; Computer science; Stability (learning theory); Finite volume method; Volume (thermodynamics); Computer graphics (images); Machine learning; Physics; Mechanics","authors":[{"name":"Reza Zangeneh","is_ca":true},{"name":"Carl Ollivier‐Gooch","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.07822902749620762,"gpt":0.3718660360156537,"spread":0.293637008519446,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.001608994,0.0006435482,0.0005828842,0.001065673,0.0006251974,0.001526549,0.001224296,0.001304507,0.002866047],"category_scores_gemma":[0.01092049,0.0004028417,0.0005821541,0.0004003567,0.001427205,0.001381863,0.002147127,0.001180756,0.0004722],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0007082563,"about_ca_system_score_gemma":0.0008972578,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.002212651,"about_ca_topic_score_gemma":0.0008504486,"domain_scores_codex":[0.9993597,0.0002076012,0.00002201213,0.0000783861,0.0002866052,0.00004562364],"domain_scores_gemma":[0.9946334,0.003201668,0.0003633623,0.0002661705,0.001395861,0.0001394498],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.0004946903,0.00009841604,0.002084101,0.0002722132,0.00006605394,0.000190071,0.0004455408,0.7743973,0.02422308,0.1490633,0.002371001,0.04629425],"study_design_scores_gemma":[0.000002187056,0.00001043233,0.00007279914,0.000005400516,0.00000215801,0.00001274476,0.00001454587,0.9938117,0.001394135,0.004457628,0.0002119371,0.000004181489],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"methods","genre_scores_codex":[0.0517639,0.0002475868,0.9418385,0.0003022079,0.00005202019,0.00006504348,0.00006407588,0.0002123727,0.005454216],"genre_scores_gemma":[0.8472059,0.0003788174,0.1412514,0.0001669808,0.00008828384,0.0001867027,0.0003402845,0.0004987647,0.009882919],"genre_candidate":"methods","genre_consensus":"methods","teacher_disagreement_score":0.002866047,"threshold_uncertainty_score":0.009587944,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W4244411680","doi":"10.2514/6.2017-0116","title":"Reducing Edney Type-IV Cowl Shock-On-Lip Heating Via Leading Edge Geometry Optimization","year":2017,"lang":"en","type":"article","venue":"55th AIAA Aerospace Sciences Meeting","topic":"Combustion and flame dynamics","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"Lockheed Martin (Canada)","funders":"","keywords":"Geometry; Enhanced Data Rates for GSM Evolution; Shock (circulatory); Materials science; Computer science; Mathematics; Artificial intelligence","authors":[{"name":"Patrick E. Rodi","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.02090871430058553,"gpt":0.2692686321397785,"spread":0.248359917839193,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002442913,0.00076048,0.0007859572,0.000370088,0.0004816406,0.0008809982,0.0008523538,0.0008220283,0.01121457],"category_scores_gemma":[0.0009975595,0.0004029288,0.0005211309,0.0002590271,0.0005051832,0.0006796842,0.00165818,0.001099435,0.001202225],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0006470985,"about_ca_system_score_gemma":0.0007857349,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.001829328,"about_ca_topic_score_gemma":0.0033024,"domain_scores_codex":[0.999842,0.00002061033,0.00000370979,0.00002068748,0.00005721177,0.00005571909],"domain_scores_gemma":[0.9998049,0.00006763133,0.00001834292,0.00003268888,0.00004666146,0.00002975743],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.000304753,0.0001309663,0.0009141067,0.0001133318,0.0000315527,0.0001486637,0.0000566205,0.9327803,0.01542593,0.01282404,0.003831157,0.03343857],"study_design_scores_gemma":[0.0000134003,0.0000340095,0.0001391211,0.000004517266,0.000004714284,0.00001288807,0.00002454928,0.9944634,0.002677066,0.00185647,0.0007652121,0.0000047761],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.1939029,0.0004753004,0.7171271,0.0005986129,0.0004041608,0.0001470992,0.0003079489,0.002314526,0.08472236],"genre_scores_gemma":[0.9376113,0.0001004367,0.04853716,0.0001796998,0.00004343505,0.00007492489,0.0001879818,0.0005404425,0.01272456],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.01121457,"threshold_uncertainty_score":0.03751642,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2568224995","doi":"10.2514/6.2017-0530","title":"Tensor-Product Summation-by-Parts Operators","year":2017,"lang":"en","type":"article","venue":"55th AIAA Aerospace Sciences Meeting","topic":"Advanced Numerical Methods in Computational Mathematics","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"University of Toronto","funders":"","keywords":"Tensor product; Cartesian tensor; Tensor (intrinsic definition); Product (mathematics); Computer science; Mathematics; Pure mathematics; Tensor density; Mathematical analysis; Tensor field; Geometry; Exact solutions in general relativity","authors":[{"name":"David C. Del Rey Fernández","is_ca":true},{"name":"Pieter D. Boom","is_ca":true},{"name":"Mehrdad Shademan","is_ca":true},{"name":"David W. Zingg","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.03587034181245085,"gpt":0.325183425601016,"spread":0.2893130837885651,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.002508576,0.0006220085,0.0005608254,0.000472003,0.0005219598,0.001453755,0.001205543,0.0005714772,0.004815302],"category_scores_gemma":[0.00504856,0.0002366969,0.0006175984,0.0007251498,0.001003198,0.002168085,0.001210382,0.001005004,0.001508436],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0004118799,"about_ca_system_score_gemma":0.0008591,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.0006701784,"about_ca_topic_score_gemma":0.000908539,"domain_scores_codex":[0.9990268,0.0002500058,0.00006611991,0.00007084321,0.0005271114,0.00005921306],"domain_scores_gemma":[0.9973673,0.001222239,0.0001677034,0.000587765,0.0005620204,0.00009294108],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.000193976,0.0001044853,0.0008958129,0.0003409553,0.00004957321,0.0002202652,0.0004491598,0.1646918,0.03308019,0.6753915,0.003472439,0.1211098],"study_design_scores_gemma":[0.00001921919,0.0000891605,0.0001964953,0.0000344624,0.00001704136,0.0002099141,0.00007176618,0.8893955,0.01215122,0.0879599,0.009834462,0.00002090219],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"genre_codex":"methods","genre_gemma":"methods","genre_scores_codex":[0.01579379,0.0002360752,0.970462,0.0001067991,0.00009570667,0.0000521101,0.00004421485,0.000286968,0.01292239],"genre_scores_gemma":[0.3274975,0.0005663044,0.6588204,0.0001847679,0.00005973132,0.0001748021,0.0001109264,0.0004538327,0.01213179],"genre_candidate":"methods","genre_consensus":"methods","teacher_disagreement_score":0.004815302,"threshold_uncertainty_score":0.01610881,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2570782496","doi":"10.2514/6.2017-1793","title":"Application of Detached Eddy Simulation to a Bluff Body Flame Stabilizer in Duct Flow","year":2017,"lang":"en","type":"article","venue":"55th AIAA Aerospace Sciences Meeting","topic":"Combustion and flame dynamics","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"University of Toronto","funders":"","keywords":"Bluff; Duct (anatomy); Large eddy simulation; Stabilizer (aeronautics); Mechanics; Flow (mathematics); Geology; Turbulence; Physics; Engineering; Aerospace engineering; Medicine","authors":[{"name":"Jonathan P. West","is_ca":true},{"name":"C. P. T. Groth","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.01477522170027587,"gpt":0.2876668936708552,"spread":0.2728916719705793,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005067181,0.0005719526,0.0008969359,0.0004280273,0.001046405,0.0009849182,0.0009785882,0.001403375,0.001981385],"category_scores_gemma":[0.001701084,0.0004130703,0.0005144792,0.0003312647,0.000695195,0.0005674977,0.0007088928,0.0007092208,0.0002490534],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0008062188,"about_ca_system_score_gemma":0.001032317,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.02080592,"about_ca_topic_score_gemma":0.009948688,"domain_scores_codex":[0.9998605,0.00004737839,0.000009120399,0.0000239186,0.00003395818,0.00002496689],"domain_scores_gemma":[0.9992354,0.0004074642,0.00004566371,0.00008114054,0.0001543015,0.00007608641],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.0003203716,0.0002774204,0.00417263,0.00005093555,0.00003799277,0.0001842507,0.0001115918,0.9778335,0.008429993,0.001527774,0.0004171745,0.006636374],"study_design_scores_gemma":[0.00002182923,0.00001945847,0.0002758493,0.000001238714,0.000002148343,0.000003274939,0.000008489913,0.998885,0.0006470157,0.00006736456,0.00006526141,0.000003099473],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.9427913,0.0001362703,0.04439468,0.0002591597,0.00009732288,0.0001200139,0.0002687253,0.001067686,0.01086487],"genre_scores_gemma":[0.987849,0.00002976028,0.01041616,0.00002677175,0.00001058376,0.0000240473,0.0001040226,0.00009173161,0.001448022],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.02080592,"threshold_uncertainty_score":0.04136962,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2570070774","doi":"10.2514/6.2017-0735","title":"A Posteriori Stability Analysis and Improvement for Finite Volume Methods on Unstructured Meshes","year":2017,"lang":"en","type":"article","venue":"55th AIAA Aerospace Sciences Meeting","topic":"Fluid Dynamics Simulations and Interactions","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"University of British Columbia","funders":"","keywords":"Polygon mesh; Stability (learning theory); Computer science; Finite volume method; A priori and a posteriori; Volume (thermodynamics); Finite element method; Computer graphics (images); Engineering; Machine learning; Mechanics; Physics; Structural engineering; Thermodynamics","authors":[{"name":"Reza Zangeneh","is_ca":true},{"name":"Carl Ollivier‐Gooch","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.02610597822029247,"gpt":0.3303593725549182,"spread":0.3042533943346257,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.004342427,0.0009467779,0.0008618918,0.00144292,0.0008580846,0.001152575,0.001334173,0.001288834,0.003062451],"category_scores_gemma":[0.01976565,0.0006569433,0.001239831,0.0005608227,0.001721737,0.001930364,0.002368252,0.002165172,0.0005468128],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0007757376,"about_ca_system_score_gemma":0.001318913,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.00273795,"about_ca_topic_score_gemma":0.002003887,"domain_scores_codex":[0.9984756,0.000708174,0.00008108758,0.0001570493,0.000501633,0.00007653101],"domain_scores_gemma":[0.9851296,0.01003622,0.000621076,0.0009195486,0.003069047,0.0002244409],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.000901568,0.0001919002,0.002514601,0.0004303015,0.0001112331,0.0001333932,0.0004922169,0.7423503,0.0364139,0.09886061,0.003506993,0.114093],"study_design_scores_gemma":[0.000004250433,0.00002175893,0.0001252268,0.000006187682,0.000003615892,0.000008918185,0.000007595752,0.9928451,0.00177321,0.004902753,0.0002963796,0.000004981881],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"methods","genre_scores_codex":[0.02092113,0.000221911,0.9757679,0.0002000473,0.00008054649,0.00005047859,0.00004759727,0.0002669202,0.002443526],"genre_scores_gemma":[0.5108071,0.000443899,0.4768472,0.0001593831,0.0002507171,0.0003741614,0.000436615,0.001069187,0.009611757],"genre_candidate":"methods","genre_consensus":"methods","teacher_disagreement_score":0.004342427,"threshold_uncertainty_score":0.02296519,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2569418430","doi":"10.2514/6.2017-0736","title":"Output Error Correction and Mesh Adaptation for Unstructured Mesh Finite Volume Method","year":2017,"lang":"en","type":"article","venue":"55th AIAA Aerospace Sciences Meeting","topic":"Computational Fluid Dynamics and Aerodynamics","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"University of British Columbia","funders":"","keywords":"Finite volume method; Computer science; Volume (thermodynamics); Adaptation (eye); Mesh generation; Algorithm; Finite element method; Mechanics; Physics; Structural engineering; Optics; Engineering; Thermodynamics","authors":[{"name":"Mahkame Sharbatdar","is_ca":true},{"name":"Carl Ollivier‐Gooch","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.02366608299878295,"gpt":0.282979853697714,"spread":0.2593137706989311,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0007319911,0.0004605824,0.0005448966,0.0003025508,0.0003535674,0.0006617043,0.001299613,0.0008706017,0.002402331],"category_scores_gemma":[0.004931132,0.0002902574,0.0003844374,0.0003177614,0.0005216984,0.0007432523,0.001250492,0.001242972,0.0006838774],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0002252988,"about_ca_system_score_gemma":0.000538054,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.001697592,"about_ca_topic_score_gemma":0.001294104,"domain_scores_codex":[0.9994412,0.0001599968,0.00003123218,0.00006717107,0.0002619311,0.0000385083],"domain_scores_gemma":[0.9985566,0.00046611,0.00008653182,0.000288962,0.0005635184,0.00003827257],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.000302133,0.0001230832,0.001426859,0.0001710868,0.0000425415,0.0001737535,0.0001847318,0.6977549,0.03544189,0.01907589,0.002869917,0.2424332],"study_design_scores_gemma":[0.00000445356,0.000009976173,0.00006228178,0.000002142529,0.000001869478,0.00000903788,0.000004257121,0.9956419,0.002905222,0.0008290335,0.0005261947,0.000003585549],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"methods","genre_scores_codex":[0.006874819,0.00002963429,0.9915227,0.00005294493,0.00007578075,0.00001895847,0.00001809484,0.0004196003,0.0009875185],"genre_scores_gemma":[0.443015,0.0000866179,0.5495058,0.0001042078,0.00008388236,0.0001268027,0.0002283644,0.0006015502,0.006247725],"genre_candidate":"methods","genre_consensus":"methods","teacher_disagreement_score":0.002402331,"threshold_uncertainty_score":0.008036613,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2569335350","doi":"10.2514/6.2017-1947","title":"A Truncation Error Based Anisotropic Mesh Adaptation Metric for CFD","year":2017,"lang":"en","type":"article","venue":"55th AIAA Aerospace Sciences Meeting","topic":"Computer Graphics and Visualization Techniques","field":"Computer Science","cited_by":0,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"University of British Columbia","funders":"","keywords":"Truncation error; Truncation (statistics); Computational fluid dynamics; Metric (unit); Computer science; Algorithm; Mesh generation; Adaptation (eye); Mathematical optimization; Applied mathematics; Mathematics; Finite element method; Physics; Mechanics; Engineering; Optics; Machine learning; Structural engineering","authors":[{"name":"Tyrone Phillips","is_ca":true},{"name":"Carl Ollivier‐Gooch","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.06892399952700047,"gpt":0.3492177227852002,"spread":0.2802937232581997,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00138024,0.0007196698,0.0007238204,0.0008642174,0.000386511,0.0009428693,0.001208263,0.0009462237,0.001373065],"category_scores_gemma":[0.00538692,0.0003249104,0.0005966622,0.0007285574,0.0007004514,0.001068077,0.001517861,0.00182074,0.0005491737],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0006052096,"about_ca_system_score_gemma":0.0008569142,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.001912251,"about_ca_topic_score_gemma":0.001823798,"domain_scores_codex":[0.9988187,0.0003470966,0.00008126751,0.00009512867,0.0006096901,0.00004798567],"domain_scores_gemma":[0.9980314,0.0005226653,0.0001760277,0.0003523313,0.0007917837,0.0001257234],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.0003723035,0.0001449657,0.001232635,0.0002242824,0.00005592289,0.0001367648,0.0001215885,0.4969438,0.07266328,0.08854295,0.007477677,0.3320839],"study_design_scores_gemma":[0.000004360237,0.00003413056,0.0001282674,0.000006475035,0.00000415923,0.00003689978,0.00000599141,0.9898712,0.004044131,0.00373934,0.00211297,0.00001208739],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"methods","genre_scores_codex":[0.006022872,0.0001836828,0.9920621,0.00008340092,0.0001059926,0.00002853026,0.00004291331,0.0001712843,0.0012992],"genre_scores_gemma":[0.2242529,0.0006011854,0.7694507,0.0001457926,0.0001635602,0.0001324855,0.0003080877,0.0004497478,0.004495512],"genre_candidate":"methods","genre_consensus":"methods","teacher_disagreement_score":0.001912251,"threshold_uncertainty_score":0.007299483,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2569786082","doi":"10.2514/6.2017-1530","title":"Modernization of the real time control and data acquisition systems at the National Research Council of Canada’s 1.5m Tri-Sonic Wind Tunnel","year":2017,"lang":"en","type":"article","venue":"55th AIAA Aerospace Sciences Meeting","topic":"Icing and De-icing Technologies","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":true},"ca_institutions":"National Research Council Canada","funders":"","keywords":"Modernization theory; Research council; Wind tunnel; Data acquisition; Computer science; Control (management); Meteorology; Remote sensing; Telecommunications; Environmental science; Real-time computing; Engineering; Geology; Geography; Aerospace engineering; Artificial intelligence; Political science","authors":[{"name":"Greg Burns","is_ca":true},{"name":"Mazen Sabbagh","is_ca":true},{"name":"Stuart Rutherford","is_ca":true},{"name":"Yves Cronier","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.1090838153916898,"gpt":0.3040252347260747,"spread":0.1949414193343849,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.002817526,0.0008310732,0.0004685777,0.001372822,0.000749795,0.001664585,0.001792739,0.000622034,0.006314036],"category_scores_gemma":[0.003277573,0.0006544084,0.0004366823,0.0007304912,0.0007997642,0.001318146,0.0008749923,0.002419372,0.00152499],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.002939127,"about_ca_system_score_gemma":0.008082888,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.07664875,"about_ca_topic_score_gemma":0.1300764,"domain_scores_codex":[0.9973391,0.0001340286,0.00006582911,0.0002260435,0.002015424,0.0002194808],"domain_scores_gemma":[0.994911,0.0003043736,0.0002161826,0.0003972736,0.003909204,0.0002618572],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"design_other","study_design_gemma":"not_applicable","study_design_scores_codex":[0.0004354028,0.0004171166,0.006409719,0.0005809984,0.0000908804,0.000327808,0.0009365869,0.01203008,0.4079131,0.01040047,0.02037984,0.5400779],"study_design_scores_gemma":[0.0002375218,0.00188307,0.0433272,0.0002677681,0.0002151954,0.001741452,0.0004337365,0.1109145,0.3401586,0.001758051,0.4986641,0.0003988063],"study_design_candidate":"not_applicable","study_design_consensus":null,"genre_codex":"methods","genre_gemma":"methods","genre_scores_codex":[0.09431063,0.001623787,0.8596544,0.001267695,0.0008379832,0.001067516,0.0009972348,0.009106216,0.03113453],"genre_scores_gemma":[0.2864331,0.001785551,0.6680594,0.0008373573,0.0002011396,0.0004647238,0.002266471,0.0008058068,0.03914649],"genre_candidate":"methods","genre_consensus":"methods","teacher_disagreement_score":0.07664875,"threshold_uncertainty_score":0.1524052,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2570127739","doi":"10.2514/6.2017-0666","title":"Uniform Design Correlations for Glaze Ice Accretion and Convective Heat Transfer from an Airfoil","year":2017,"lang":"en","type":"article","venue":"55th AIAA Aerospace Sciences Meeting","topic":"Icing and De-icing Technologies","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"routes":{"ca_aff":true,"ca_fund":true,"ca_venue":false,"about_ca":false},"ca_institutions":"Memorial University of Newfoundland","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Glaze; Airfoil; Convection; Convective heat transfer; Heat transfer; Atmospheric sciences; Geology; Materials science; Meteorology; Mechanics; Environmental science; Physics; Composite material","authors":[{"name":"Brian Peach","is_ca":true},{"name":"Kevin Pope","is_ca":true},{"name":"G.F. Naterer","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.03794728674929333,"gpt":0.2783911038345065,"spread":0.2404438170852132,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.003337472,0.0007392087,0.000662413,0.0007464045,0.0004670532,0.0007672678,0.0005858467,0.0005816125,0.002381713],"category_scores_gemma":[0.01007686,0.0003397535,0.0006079737,0.0004822573,0.00038368,0.0008363011,0.0006789824,0.0006231273,0.0003424699],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.001092284,"about_ca_system_score_gemma":0.001306267,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.001479136,"about_ca_topic_score_gemma":0.002951973,"domain_scores_codex":[0.9984277,0.0006870025,0.00007858286,0.000207358,0.0003965432,0.0002027294],"domain_scores_gemma":[0.9943679,0.002725014,0.0007270371,0.0006287618,0.001456,0.00009531311],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","study_design_scores_codex":[0.0004212173,0.0001193267,0.003978034,0.0001634797,0.00004151338,0.00004929423,0.00003720388,0.9500589,0.01643037,0.004289506,0.001036466,0.02337471],"study_design_scores_gemma":[0.0000224962,0.0002819542,0.001571389,0.00001284426,0.00002066065,0.00001365772,0.00001272303,0.9844548,0.01258019,0.0006407957,0.0003766203,0.00001193894],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.4284069,0.0008058092,0.5577004,0.0002040337,0.0001143119,0.0001614124,0.0004492127,0.001137166,0.01102074],"genre_scores_gemma":[0.9767435,0.00006011701,0.02182866,0.00003932994,0.00001383378,0.0001026199,0.0001794406,0.000121246,0.0009112631],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.003337472,"threshold_uncertainty_score":0.01765043,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null}]}