{"meta":{"query_hash":"0b9248e7264f","filters":{"venue":"41st Aerospace Sciences Meeting and Exhibit"},"cohort_total":25,"direct_labels_cover":0,"predictions_cover":25,"exported":25,"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/0b9248e7264f","api":"https://metacan.xera.ac/api/v1/cohort?venue=41st+Aerospace+Sciences+Meeting+and+Exhibit"},"results":[{"id":"W1982499032","doi":"10.2514/6.2003-214","title":"An Iterative Inverse Design Method Based on Aerodynamic Streamline Equations","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Computational Fluid Dynamics and Aerodynamics","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Polytechnique Montréal","funders":"","keywords":"Aerodynamics; Computer science; Iterative method; Inverse; Applied mathematics; Mathematical optimization; Algorithm; Mathematics; Mechanics; Physics; Geometry","score_opus":0.024943207362417917,"score_gpt":0.2692730123914879,"score_spread":0.24432980502906995,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1982499032","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":[0.2812789,0.000058576883,0.7146116,0.00019363876,0.00023365342,0.00017460604,0.000016425189,0.00019549274,0.0032371285],"genre_scores_gemma":[0.8154946,0.000011033894,0.18425716,0.00011052327,0.000025775791,0.000010402258,0.000015047691,0.00001881749,0.00005667092],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9985863,0.00019036309,0.00020747121,0.00039570907,0.0002997284,0.00032043998],"domain_scores_gemma":[0.9989445,0.0006242292,0.000045942525,0.00017412427,0.00006680237,0.00014438211],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0012536555,0.0002164239,0.00017576104,0.00015695205,0.00043007208,0.00022154463,0.00014357545,0.00006232409,0.000015723106],"category_scores_gemma":[0.00020193312,0.00020191119,0.00004206207,0.0005346301,0.00012252635,0.00021160847,0.000012562939,0.0001506055,0.000009523549],"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":[0.0000032577257,0.000027893499,0.00037881482,0.000008360404,0.0000051562806,0.0000016395309,0.00022000025,0.98533225,0.004397337,0.008929929,0.00003939361,0.0006559444],"study_design_scores_gemma":[0.00025008465,0.00017649647,0.0002917378,0.00005414793,0.000010879368,0.0000025117633,0.00025982704,0.99737585,0.00044315093,0.00084546313,0.000044483953,0.0002453695],"about_ca_topic_score_codex":0.000029468127,"about_ca_topic_score_gemma":0.00016995207,"teacher_disagreement_score":0.5342156,"about_ca_system_score_codex":0.00006748073,"about_ca_system_score_gemma":0.00008458152,"threshold_uncertainty_score":0.8233699},"labels":[],"label_agreement":null},{"id":"W2029081201","doi":"10.2514/6.2003-274","title":"A Newton-Krylov Algorithm for the Euler Equations Using Unstructured Grids","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Advanced Numerical Methods in Computational Mathematics","field":"Engineering","cited_by":11,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto","funders":"","keywords":"Computer science; Euler's formula; Newton's method; Unstructured grid; Backward Euler method; Euler equations; Algorithm; Applied mathematics; Computational science; Mathematics; Grid; Physics; Mathematical analysis; Nonlinear system; Geometry","score_opus":0.06610549988179834,"score_gpt":0.3162599446095172,"score_spread":0.25015444472771886,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2029081201","genre_codex":"methods","genre_gemma":"methods","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.00901189,0.0006598824,0.9884109,0.00015642907,0.0006852195,0.00019804553,0.0000054123043,0.00010497253,0.00076728076],"genre_scores_gemma":[0.08447953,0.000022868882,0.91527444,0.000043338223,0.000102215,0.000017761364,5.6525647e-7,0.000019143205,0.000040124727],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99904454,0.000036264384,0.00018986642,0.00021411045,0.00022567382,0.0002895299],"domain_scores_gemma":[0.9975368,0.0021598842,0.00005999029,0.000121130906,0.000058922345,0.00006327212],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0007143972,0.00014236728,0.00014706085,0.00004429319,0.0006107764,0.0001152787,0.00014447524,0.00004425499,0.0000066866564],"category_scores_gemma":[0.0009488212,0.00010256493,0.000044846278,0.00045274192,0.00025960684,0.00012658874,0.00002559088,0.00010797631,0.0000017838781],"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":[0.0000011956174,0.0000113803535,0.00014352372,0.000048699763,0.000025822861,4.3574573e-7,0.0007432404,0.9216775,0.0035404393,0.027471136,0.00017676926,0.04615988],"study_design_scores_gemma":[0.00014514096,0.000025213842,0.000031431227,0.000043518558,0.00002078344,0.000011291218,0.0004788821,0.9706733,0.0016238592,0.025386391,0.0013933425,0.00016679954],"about_ca_topic_score_codex":0.000006073384,"about_ca_topic_score_gemma":0.0000018614552,"teacher_disagreement_score":0.075467646,"about_ca_system_score_codex":0.000032926615,"about_ca_system_score_gemma":0.000034621684,"threshold_uncertainty_score":0.46976602},"labels":[],"label_agreement":null},{"id":"W2120662324","doi":"10.2514/6.2003-1076","title":"Prediction of 2D Airfoil Ice Accretion by Bisection Method and by Rivulets and Beads Modeling","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Icing and De-icing Technologies","field":"Engineering","cited_by":26,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"Université du Québec à Rimouski; Université du Québec à Chicoutimi","funders":"","keywords":"Airfoil; Bisection method; Computer science; Geology; Mechanics; Algorithm; Physics","score_opus":0.023125540143809017,"score_gpt":0.23217671641352225,"score_spread":0.20905117626971323,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2120662324","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":[0.91239613,0.0018357771,0.08318537,0.00012993875,0.00015282544,0.00007095735,0.000007782448,0.00033075898,0.0018904305],"genre_scores_gemma":[0.99065423,0.00084660295,0.008412097,0.000013084926,0.0000126074865,0.0000049033974,0.0000023676985,0.000011522802,0.000042603635],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9990646,0.00004639388,0.00018261078,0.00029716504,0.00017844836,0.00023077395],"domain_scores_gemma":[0.9996834,0.00008239635,0.00005475913,0.00009622117,0.00003239097,0.00005084576],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0010723758,0.00014131359,0.00017453745,0.0001041092,0.0003064091,0.000082882296,0.00005746848,0.00012419243,8.315269e-7],"category_scores_gemma":[0.00017536116,0.00013064328,0.000016062131,0.00029755078,0.00018059071,0.00021191576,0.000030984662,0.00013711081,3.2549065e-7],"study_design_candidate":"bench_or_experimental","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":[0.000021841039,0.00004402776,0.045579657,0.00044870234,0.00004783316,9.694323e-7,0.0034786784,0.10578415,0.7884832,0.0013103049,0.005261624,0.049538985],"study_design_scores_gemma":[0.00043663132,0.00024104344,0.00032791344,0.00033774154,0.000042146887,0.000033421522,0.00296995,0.63380206,0.36029702,0.00066473224,0.00053247536,0.0003148374],"about_ca_topic_score_codex":0.0002593383,"about_ca_topic_score_gemma":0.000014479375,"teacher_disagreement_score":0.52801794,"about_ca_system_score_codex":0.000024518893,"about_ca_system_score_gemma":0.0000092331,"threshold_uncertainty_score":0.5327478},"labels":[],"label_agreement":null},{"id":"W2126116164","doi":"10.2514/6.2003-163","title":"Fluid Flow and Heat Transfer From a Pin Fin: Analytical Approach","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Fluid Dynamics and Vibration Analysis","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Waterloo","funders":"","keywords":"Fin; Heat transfer; Flow (mathematics); Mechanics; Fluid dynamics; Heat transfer fluid; Computer science; Materials science; Mechanical engineering; Physics; Engineering","score_opus":0.016502883062468693,"score_gpt":0.2104509164603527,"score_spread":0.193948033397884,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2126116164","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":[0.9520847,0.0015817848,0.030948125,0.00029846563,0.00009386555,0.00007206534,0.000010016994,0.00010557137,0.01480536],"genre_scores_gemma":[0.9909403,0.00028232663,0.0085222395,0.00008151674,0.00003429913,0.0000044272642,0.000006088112,0.000012056942,0.00011679226],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99899685,0.000040383315,0.00017494077,0.00030906286,0.00020253604,0.00027621863],"domain_scores_gemma":[0.999646,0.000061484076,0.000004807878,0.0001219492,0.000018401377,0.00014734524],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00044922417,0.00015872675,0.00021295865,0.0000827323,0.0002555317,0.00024410158,0.00008216408,0.00007148653,0.000039061044],"category_scores_gemma":[0.000047079222,0.00013671284,0.00005047612,0.00041294406,0.00020040791,0.00014570604,0.000015007466,0.000105183135,0.0000056716635],"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":[0.00003223484,0.00016341584,0.046989422,0.00022363644,0.00028424503,0.000011361031,0.010089186,0.80831087,0.09443974,0.031561933,0.0036931285,0.004200857],"study_design_scores_gemma":[0.00020860405,0.000026282582,0.00045512244,0.000023789054,0.000030997264,0.000003972701,0.0007158395,0.99623543,0.0014716061,0.00008218008,0.0005485094,0.00019769401],"about_ca_topic_score_codex":0.00011636193,"about_ca_topic_score_gemma":0.000084298124,"teacher_disagreement_score":0.18792456,"about_ca_system_score_codex":0.000014576299,"about_ca_system_score_gemma":0.0000203076,"threshold_uncertainty_score":0.5574988},"labels":[],"label_agreement":null},{"id":"W2138396290","doi":"10.2514/6.2003-159","title":"Conduction Shape Factor Models for 3-D Enclosures","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Icing and De-icing Technologies","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":"University of Waterloo","funders":"","keywords":"Factor (programming language); Computer science; Programming language","score_opus":0.05498692074689601,"score_gpt":0.2478396116037393,"score_spread":0.19285269085684328,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2138396290","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":[0.9750517,0.00069831434,0.011176553,0.00019517668,0.00055912643,0.00016410493,0.000005731782,0.0009286399,0.01122065],"genre_scores_gemma":[0.9895502,0.000114382274,0.010064941,0.000026013928,0.000037970392,0.000015802247,7.340223e-7,0.000014985248,0.00017501874],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99906445,0.000015710542,0.00014115471,0.0002680927,0.00015464975,0.00035595393],"domain_scores_gemma":[0.99964184,0.00011444629,0.000034928053,0.00012417356,0.0000358099,0.00004882751],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00045097197,0.00014883142,0.00016059566,0.00009247681,0.00039512335,0.00012664737,0.000119902186,0.00009628101,0.0000053362596],"category_scores_gemma":[0.00021745016,0.00012718668,0.000039169703,0.00023708062,0.00021124433,0.00021928921,0.000019560463,0.000102800346,0.0000039819674],"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":[0.000033665157,0.00009324238,0.022101339,0.00083192845,0.000120690434,0.0000059899016,0.010166272,0.58212364,0.17998911,0.10258395,0.020413183,0.08153697],"study_design_scores_gemma":[0.00075047975,0.00037294693,0.00040975912,0.00031853083,0.000034627083,0.00003731308,0.0062294826,0.3509885,0.61344844,0.019315196,0.007124958,0.0009697828],"about_ca_topic_score_codex":0.00003493165,"about_ca_topic_score_gemma":0.000019854095,"teacher_disagreement_score":0.4334593,"about_ca_system_score_codex":0.000021450107,"about_ca_system_score_gemma":0.000021028034,"threshold_uncertainty_score":0.51865226},"labels":[],"label_agreement":null},{"id":"W2313230181","doi":"10.2514/6.2003-1038","title":"Experimental Investigation of Performance Characteristics of Small Loop Heat Pipes","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Heat Transfer and Boiling Studies","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Carleton University","funders":"Goddard Space Flight Center","keywords":"Loop (graph theory); Materials science; Computer science; Mathematics","score_opus":0.02781259421456956,"score_gpt":0.21869803503201035,"score_spread":0.1908854408174408,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2313230181","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":[0.99479693,0.0010744487,0.00013528067,0.000022767244,0.00014713466,0.000053917873,0.0000027682288,0.000040149538,0.0037265718],"genre_scores_gemma":[0.99837697,0.00022403596,0.0013392476,0.000008588512,0.000016247011,0.0000031345344,7.2529826e-7,0.0000065198915,0.000024548288],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9993335,0.000019128973,0.00020290862,0.00013236096,0.00013698143,0.00017510905],"domain_scores_gemma":[0.999798,0.000043999273,0.000017528393,0.0000654187,0.000031237334,0.000043803026],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00037675773,0.000102278595,0.00018183548,0.00004595882,0.00012652068,0.00001741518,0.000062719504,0.000032866355,0.0000033327913],"category_scores_gemma":[0.00003091548,0.00008929745,0.000023893146,0.0001882665,0.00033792658,0.000082362516,0.000010574464,0.000054300537,9.4057674e-7],"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":[0.0000046007044,0.000018048097,0.21420987,0.00036697424,0.000013953527,3.8772504e-7,0.0050077187,0.0017729551,0.77755076,0.00040578676,0.000022031682,0.0006269383],"study_design_scores_gemma":[0.0001434796,0.00012633506,0.01283612,0.0002280391,0.000008858356,0.000002604918,0.0011338675,0.0028781255,0.98245496,0.000009290405,0.000054195145,0.00012410454],"about_ca_topic_score_codex":0.000025403053,"about_ca_topic_score_gemma":0.00000643754,"teacher_disagreement_score":0.20490424,"about_ca_system_score_codex":0.000009624436,"about_ca_system_score_gemma":0.000021039132,"threshold_uncertainty_score":0.3641444},"labels":[],"label_agreement":null},{"id":"W2314415627","doi":"10.2514/6.2003-759","title":"RLV Power Generation Systems Trail from 1st to 2nd Generation","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Electric and Hybrid Vehicle Technologies","field":"Engineering","cited_by":6,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lockheed Martin (Canada)","funders":"","keywords":"Electricity generation; Computer science; Power (physics); Physics","score_opus":0.0341699772575486,"score_gpt":0.2200802395772298,"score_spread":0.18591026231968122,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2314415627","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":[0.98587286,0.0030932361,0.0040838295,0.00023264559,0.0005591645,0.00014959346,0.000004489169,0.0004042467,0.005599927],"genre_scores_gemma":[0.9960345,0.00014972802,0.0033402687,0.000053208347,0.0001480154,0.000018508475,0.0000036773638,0.000014431696,0.00023764337],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9988817,0.000034492892,0.00018370769,0.0003381685,0.00023086999,0.00033103835],"domain_scores_gemma":[0.9996675,0.000036928574,0.000034993824,0.00014702338,0.000031707783,0.00008183911],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00049029256,0.00015556277,0.00015985103,0.000096808806,0.00035266264,0.00030233746,0.00012440742,0.000084333275,0.000012738978],"category_scores_gemma":[0.0001078219,0.00014115142,0.000023574581,0.0004160946,0.00008339844,0.00018779466,0.000018264525,0.00010992955,0.000023546594],"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":[0.0000021889332,0.000019312592,0.008590865,0.000016863078,0.000022605353,0.0000048608194,0.0011318002,0.08052718,0.8827482,0.007224383,0.016346414,0.003365313],"study_design_scores_gemma":[0.0006616335,0.0004279636,0.002611035,0.00016304544,0.00004303166,0.000035322206,0.0029923874,0.39793816,0.56904644,0.00022605997,0.024555428,0.0012994726],"about_ca_topic_score_codex":0.00020744654,"about_ca_topic_score_gemma":0.00016838804,"teacher_disagreement_score":0.31741098,"about_ca_system_score_codex":0.000043900927,"about_ca_system_score_gemma":0.000021837079,"threshold_uncertainty_score":0.57559884},"labels":[],"label_agreement":null},{"id":"W2315791200","doi":"10.2514/6.2003-733","title":"Optimization of a Hot-Air Anti-Icing System","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Icing and De-icing Technologies","field":"Engineering","cited_by":15,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Polytechnique Montréal","funders":"","keywords":"Icing; Computer science; Environmental science; Meteorology; Geography","score_opus":0.013575508702038672,"score_gpt":0.20299027281382823,"score_spread":0.18941476411178956,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2315791200","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":[0.94685644,0.00049522903,0.025214965,0.000057543857,0.00035171854,0.00009586239,0.0000013964399,0.00094163674,0.02598523],"genre_scores_gemma":[0.9808745,0.000077756216,0.018967096,0.000008327474,0.000016364715,0.000003030206,4.177216e-7,0.000013441763,0.000039111408],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99904907,0.000029474759,0.00020668394,0.00022230977,0.00019788914,0.00029455838],"domain_scores_gemma":[0.9996188,0.0000747435,0.00007018372,0.00015723427,0.00003905788,0.000039975337],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0007398317,0.00013756577,0.00022342379,0.00014157553,0.00025013916,0.0000513617,0.00012950499,0.00008359694,0.0000016825277],"category_scores_gemma":[0.00017352692,0.0001205371,0.0000314367,0.0005464964,0.00020921469,0.00012317458,0.000028857687,0.00009887016,0.0000029380276],"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":[0.0000013242109,0.000006059121,0.00880332,0.00021542468,0.000008390848,0.0000018381489,0.00058855093,0.9803204,0.0061526895,0.0030862999,0.00017083663,0.0006448694],"study_design_scores_gemma":[0.0005003754,0.00017836019,0.0012945964,0.0017738503,0.000041198175,0.0000695934,0.0140967835,0.4097512,0.5713319,0.000088486115,0.0002559422,0.0006176704],"about_ca_topic_score_codex":0.00006990394,"about_ca_topic_score_gemma":0.0000074772006,"teacher_disagreement_score":0.5705692,"about_ca_system_score_codex":0.00002800007,"about_ca_system_score_gemma":0.000021426873,"threshold_uncertainty_score":0.49153605},"labels":[],"label_agreement":null},{"id":"W2317503549","doi":"10.2514/6.2003-1223","title":"FENSAP-ICE : Effect of Ice Shapes on 3D Eulerian Droplet Impingement","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Icing and De-icing Technologies","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"","keywords":"Eulerian path; Geology; Mechanics; Physics","score_opus":0.013447487183462026,"score_gpt":0.22769744667537278,"score_spread":0.21424995949191075,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2317503549","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":[0.9689528,0.0003781304,0.0003701819,0.00016362261,0.0003361559,0.00014081664,0.0000022149527,0.00053534773,0.029120753],"genre_scores_gemma":[0.9974437,0.00010655321,0.0022397346,0.000037140326,0.00003065215,0.000009113442,4.99921e-7,0.000018209985,0.00011439664],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99862295,0.000067940324,0.00021637657,0.00034301076,0.00030342853,0.00044631909],"domain_scores_gemma":[0.99929297,0.00034766944,0.000074008734,0.00019719185,0.000026102403,0.000062034254],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0013647276,0.0002307037,0.0003022037,0.00015055318,0.00030648825,0.00009473487,0.00021024574,0.000095305964,0.000009643813],"category_scores_gemma":[0.00053441204,0.00018387454,0.000048947037,0.00047653035,0.00027726815,0.00009396039,0.000053017244,0.0001732806,0.000016818689],"study_design_candidate":"bench_or_experimental","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":[0.00018906625,0.00022878799,0.11240488,0.003180511,0.0003019103,0.00005849523,0.01084369,0.35716847,0.34673095,0.01535822,0.013352219,0.1401828],"study_design_scores_gemma":[0.00096000446,0.0017043875,0.0023018324,0.0012549866,0.00006370122,0.000019669043,0.0019010678,0.020098235,0.96602595,0.00019127628,0.004670918,0.00080800056],"about_ca_topic_score_codex":0.000092558206,"about_ca_topic_score_gemma":0.000032643053,"teacher_disagreement_score":0.61929494,"about_ca_system_score_codex":0.000032933895,"about_ca_system_score_gemma":0.000016855329,"threshold_uncertainty_score":0.7498186},"labels":[],"label_agreement":null},{"id":"W2318023244","doi":"10.2514/6.2003-1240","title":"CFD Investigation of Fin Aeroheating on a Hypersonic Projectile","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Gas Dynamics and Kinetic Theory","field":"Mathematics","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"National Research Council Canada","funders":"","keywords":"Projectile; Hypersonic speed; Fin; Aerospace engineering; Computational fluid dynamics; Materials science; Engineering","score_opus":0.061649072629100354,"score_gpt":0.2855067903629673,"score_spread":0.22385771773386692,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2318023244","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":[0.977606,0.00009763625,0.000076594,0.00023188537,0.000100789475,0.00015492576,0.0000012288699,0.000037997484,0.02169293],"genre_scores_gemma":[0.9798526,0.00001227379,0.019635674,0.00005186217,0.000021612008,0.000007678631,3.6642442e-7,0.0000109424345,0.000406998],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.9988139,0.00012313684,0.00022251252,0.00029632504,0.00028334255,0.00026078493],"domain_scores_gemma":[0.99911237,0.0004330619,0.00018898997,0.00015220586,0.000047020625,0.00006636604],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0017556243,0.00012958582,0.0001907229,0.00008324286,0.00029958814,0.00005570326,0.00010846309,0.000055801018,0.000011935077],"category_scores_gemma":[0.0010874015,0.00010551169,0.000040394938,0.00034862568,0.00035429088,0.00006499828,0.000028467366,0.00011055447,0.0000029804169],"study_design_candidate":"theoretical_or_conceptual","study_design_consensus":"theoretical_or_conceptual","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000031827843,0.00015791468,0.057903618,0.00047153013,0.000031650194,0.000003989047,0.02006471,0.0006956076,0.100276306,0.8176135,0.00073297997,0.0020163641],"study_design_scores_gemma":[0.0033959514,0.0035167662,0.007609848,0.0047570043,0.00020007507,0.00013501424,0.047668684,0.023773056,0.2937244,0.6123157,0.00082608167,0.0020774219],"about_ca_topic_score_codex":0.00006515244,"about_ca_topic_score_gemma":0.000039824354,"teacher_disagreement_score":0.20529781,"about_ca_system_score_codex":0.000019833305,"about_ca_system_score_gemma":0.000088207686,"threshold_uncertainty_score":0.43026417},"labels":[],"label_agreement":null},{"id":"W2318049051","doi":"10.2514/6.2003-725","title":"Efficient Optimized Airfoil Parameterization","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Advanced Numerical Analysis Techniques","field":"Engineering","cited_by":6,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Polytechnique Montréal","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Airfoil; Computer science; Aerospace engineering; Engineering","score_opus":0.01416601986680012,"score_gpt":0.23146010296262093,"score_spread":0.21729408309582082,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2318049051","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":[0.8565924,0.0008437773,0.11869547,0.00012547857,0.00015470157,0.00013002231,0.000001249796,0.0007717059,0.022685185],"genre_scores_gemma":[0.8971047,0.0001064057,0.10262211,0.00003751939,0.000013886006,0.000011436517,7.8087214e-7,0.000012471893,0.00009072662],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989907,0.000042239553,0.00017396225,0.00027768666,0.00021672127,0.00029865286],"domain_scores_gemma":[0.99964076,0.000075835735,0.00004347784,0.00012516945,0.000026285055,0.00008846499],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00046952465,0.0001431415,0.00018490262,0.00007879858,0.00023554437,0.0000876142,0.0001014028,0.000046956317,0.000016821856],"category_scores_gemma":[0.00018176198,0.00012201767,0.00004294458,0.0006305722,0.00020093466,0.00007015014,0.000023342376,0.000088966786,0.000010296381],"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":[0.0000023821822,0.00001605378,0.0008846062,0.000021555168,0.000008500416,0.0000013116813,0.00020685917,0.9666877,0.028947057,0.0010488131,0.00012533196,0.0020498703],"study_design_scores_gemma":[0.00037238817,0.00011218897,0.00022215337,0.00012928848,0.000034632187,0.00001296836,0.00056814525,0.8769517,0.117204815,0.0007999485,0.0029804003,0.0006113854],"about_ca_topic_score_codex":0.000010861913,"about_ca_topic_score_gemma":0.0000022374606,"teacher_disagreement_score":0.08973597,"about_ca_system_score_codex":0.000027553766,"about_ca_system_score_gemma":0.000010384225,"threshold_uncertainty_score":0.4975736},"labels":[],"label_agreement":null},{"id":"W2318616356","doi":"10.2514/6.2003-1333","title":"Cost Modelling as a Holistic Tool in the Multi-disciplinary Systems Architecture of Aircraft Design: The Next Frontier","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Manufacturing Process and Optimization","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Queen's University","funders":"Government of the United Kingdom","keywords":"Frontier; Architecture; Systems engineering; Computer science; Discipline; Systems design; Computer architecture; Software engineering; Engineering; Architectural engineering; Sociology; Geography","score_opus":0.10172996623939046,"score_gpt":0.27233711544365635,"score_spread":0.1706071492042659,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2318616356","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":[0.47126573,0.004075755,0.5218509,0.00018649903,0.0002986474,0.0005185225,0.0000021836158,0.0000622255,0.0017395361],"genre_scores_gemma":[0.9863699,0.00015937617,0.013290021,0.000023255468,0.00002803793,0.000033253997,7.0449533e-7,0.000011662717,0.00008380046],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.998942,0.00011364957,0.00020573165,0.00021554992,0.0002498199,0.00027323465],"domain_scores_gemma":[0.99952143,0.00020309228,0.000061293475,0.00016425291,0.000023662746,0.000026293137],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0013672714,0.00014530386,0.00015675886,0.00006439449,0.00033051823,0.00021789096,0.00024001302,0.00005587671,0.0000030655774],"category_scores_gemma":[0.00008830453,0.000083850224,0.000028035176,0.00031803237,0.00017454008,0.00012937149,0.00002558696,0.00018146305,0.0000015686725],"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":[0.000003315228,0.000008856336,0.0004073925,0.00007886952,0.0000030640836,0.0000011329038,0.0044504465,0.99447423,0.00008265093,0.0002607548,0.000035312733,0.00019396345],"study_design_scores_gemma":[0.00018670344,0.000035069013,0.00014322867,0.0002211169,0.000012136559,0.000015291524,0.004469264,0.9933891,0.00081376673,0.0002974367,0.00026486145,0.00015201257],"about_ca_topic_score_codex":0.00014409423,"about_ca_topic_score_gemma":0.000023385266,"teacher_disagreement_score":0.5151042,"about_ca_system_score_codex":0.000015908498,"about_ca_system_score_gemma":0.000031685526,"threshold_uncertainty_score":0.34193128},"labels":[],"label_agreement":null},{"id":"W2320514444","doi":"10.2514/6.2003-227","title":"Unsteady Aerodynamic Solutions for Oscillating Airfoils","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Biomimetic flight and propulsion mechanisms","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":"McGill University","funders":"","keywords":"Airfoil; Aerodynamics; Aerospace engineering; Mechanics; Computer science; Physics; Acoustics; Engineering","score_opus":0.03595958307323533,"score_gpt":0.23213398340958155,"score_spread":0.19617440033634623,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2320514444","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":[0.909874,0.003076206,0.02317631,0.0008075772,0.0021362875,0.0005733704,0.000018637236,0.00066082855,0.05967679],"genre_scores_gemma":[0.9712998,0.00007447508,0.027958864,0.000044921868,0.00005745069,0.000020932672,0.0000020281245,0.0000198743,0.0005216305],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99863404,0.00003897419,0.00020794202,0.00031747718,0.00019501126,0.0006065717],"domain_scores_gemma":[0.9995226,0.00014412802,0.000045304994,0.000133753,0.00003745084,0.000116758136],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.001358137,0.00017394661,0.00017843251,0.00008584165,0.000900674,0.00014431545,0.00012610134,0.000091886985,0.00002386667],"category_scores_gemma":[0.00015779065,0.00015185015,0.00005712107,0.00035956176,0.00016318764,0.00013370499,0.00003143844,0.00010218604,0.000017119548],"study_design_candidate":"bench_or_experimental","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":[0.000016877193,0.00006665526,0.003984269,0.00056329055,0.0000730954,0.000003980388,0.0031743809,0.04421432,0.7775528,0.13762358,0.009066143,0.023660647],"study_design_scores_gemma":[0.0036624507,0.0011792389,0.0010400082,0.0011615955,0.00020939823,0.00013845295,0.010780422,0.6346114,0.2563741,0.026818207,0.060364164,0.003660535],"about_ca_topic_score_codex":0.000025055126,"about_ca_topic_score_gemma":0.0000662069,"teacher_disagreement_score":0.5903971,"about_ca_system_score_codex":0.000028265542,"about_ca_system_score_gemma":0.000032798027,"threshold_uncertainty_score":0.6927347},"labels":[],"label_agreement":null},{"id":"W2320516950","doi":"10.2514/6.2003-160","title":"Comparisons Between Plastic Contact Hardness Models and Experiments","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Adhesion, Friction, and Surface Interactions","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Materials science; Hardness; Indentation hardness; Composite material; Microstructure","score_opus":0.06257376769022605,"score_gpt":0.2718022809349413,"score_spread":0.20922851324471525,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2320516950","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":[0.97810465,0.0010896857,0.0063471426,0.000045944533,0.00066879374,0.000083810606,0.0000056927565,0.0001646649,0.013489626],"genre_scores_gemma":[0.9977126,0.00014955031,0.0018141046,0.000009894094,0.00003961909,0.00000778939,0.0000013640328,0.0000136835815,0.00025140122],"study_design_codex":"observational","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9990079,0.000040525447,0.00018294764,0.0002726335,0.00018837993,0.00030762784],"domain_scores_gemma":[0.99948615,0.00020268768,0.000038631722,0.000095017014,0.000028688592,0.00014881826],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00029350733,0.0001637883,0.00020356126,0.0000719989,0.0006143609,0.00017136968,0.00007773377,0.000058924896,0.000016718794],"category_scores_gemma":[0.0000630674,0.00014943168,0.000027862958,0.00019886167,0.00013412541,0.00038151158,0.00002094012,0.00012691208,0.000010311271],"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":[0.000015828828,0.00009910702,0.79693437,0.00015788653,0.00013610198,0.0000065349677,0.012727781,0.13261475,0.037104953,0.0074472525,0.01213824,0.0006171794],"study_design_scores_gemma":[0.0038099114,0.0009093409,0.118006095,0.0016741927,0.00032290933,0.00014577928,0.06257828,0.63481647,0.12060331,0.0023422863,0.05080412,0.00398732],"about_ca_topic_score_codex":0.00010702329,"about_ca_topic_score_gemma":0.000044659686,"teacher_disagreement_score":0.6789283,"about_ca_system_score_codex":0.000029337254,"about_ca_system_score_gemma":0.000023074768,"threshold_uncertainty_score":0.6093647},"labels":[],"label_agreement":null},{"id":"W2321190310","doi":"10.2514/6.2003-221","title":"Moving Surface Boundary-layer Control for Aircraft Operation at High Angles of Attack","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Guidance and Control Systems","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of British Columbia","funders":"","keywords":"Boundary layer; Surface (topology); Layer (electronics); Aerospace engineering; Boundary (topology); Angle of attack; Boundary layer control; Computer science; Aeronautics; Aerodynamics; Materials science; Engineering; Geometry; Flow separation; Mathematics; Composite material","score_opus":0.020309683138803717,"score_gpt":0.23395887010620586,"score_spread":0.21364918696740215,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2321190310","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":[0.9897785,0.0030333623,0.003297867,0.00018701011,0.0004252833,0.00029881342,0.000012271854,0.00009253167,0.002874344],"genre_scores_gemma":[0.9971088,0.00004268529,0.0022590854,0.00004203423,0.00006576544,0.000018391314,0.0000016864603,0.000017175762,0.00044433938],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9988205,0.00004845898,0.00027102046,0.0002730813,0.0002263349,0.00036059806],"domain_scores_gemma":[0.99949855,0.0001526155,0.000075627315,0.00013408317,0.00006788567,0.00007124443],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0009920596,0.00016092547,0.00028049806,0.00003731232,0.00041398068,0.00013404425,0.00011430674,0.0000706756,0.0000109301845],"category_scores_gemma":[0.000104616825,0.00014170977,0.0000569498,0.00016155117,0.0001525577,0.00022734639,0.0000149869975,0.000055404093,0.000007077521],"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":[0.000025319476,0.000020437808,0.043885756,0.00024441432,0.00004366714,0.0000011740477,0.0011694117,0.40680358,0.54345924,0.0018629206,0.0020333147,0.00045077672],"study_design_scores_gemma":[0.009057709,0.0010383591,0.011856523,0.0011975411,0.00019856363,0.000052629737,0.0059492085,0.55013883,0.37583002,0.00049679,0.042026337,0.0021574595],"about_ca_topic_score_codex":0.000111775815,"about_ca_topic_score_gemma":0.00023302989,"teacher_disagreement_score":0.16762918,"about_ca_system_score_codex":0.000042997508,"about_ca_system_score_gemma":0.00004037517,"threshold_uncertainty_score":0.5778757},"labels":[],"label_agreement":null},{"id":"W2322912868","doi":"10.2514/6.2003-71","title":"A Newton-Krylov Algorithm for Turbulent Aerodynamic Flows","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Computational Fluid Dynamics and Aerodynamics","field":"Engineering","cited_by":13,"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; Turbulence; Computer science; Computational fluid dynamics; Mechanics; Physics","score_opus":0.01213327392738127,"score_gpt":0.2205977382769048,"score_spread":0.2084644643495235,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2322912868","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":[0.7990278,0.0011763348,0.19351578,0.00036819326,0.0008451413,0.00035316191,0.000025751804,0.00028979927,0.0043980107],"genre_scores_gemma":[0.8836481,0.00019193768,0.11540111,0.00007905314,0.00011733807,0.00003853937,0.000017460126,0.000044313005,0.00046211755],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9985827,0.000020460833,0.00023966351,0.00040873492,0.0002640894,0.00048432112],"domain_scores_gemma":[0.9994516,0.0001686733,0.00004101723,0.00013639002,0.000066349436,0.00013596793],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006395648,0.00022924953,0.00021137905,0.00009485146,0.0004072474,0.00020537828,0.00016197372,0.00007437749,0.0000073964316],"category_scores_gemma":[0.00005384985,0.00021844594,0.0000813809,0.00035720546,0.000119982185,0.0001437442,0.000029436611,0.00011854706,0.000009097534],"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":[0.000006392308,0.00009327464,0.0019170617,0.0001628645,0.00006816859,0.000010936014,0.0007135015,0.89388645,0.015722798,0.034737304,0.0014849901,0.051196247],"study_design_scores_gemma":[0.0002627794,0.00005557868,0.00034376525,0.00005347321,0.000012490977,0.0000306494,0.00014418321,0.99501574,0.000116904266,0.0013159034,0.0023508635,0.00029769234],"about_ca_topic_score_codex":0.000027102158,"about_ca_topic_score_gemma":0.00008275836,"teacher_disagreement_score":0.101129256,"about_ca_system_score_codex":0.000062376304,"about_ca_system_score_gemma":0.00005318714,"threshold_uncertainty_score":0.8907967},"labels":[],"label_agreement":null},{"id":"W2324811470","doi":"10.2514/6.2003-1098","title":"Aerodynamic Solutions for Finite-span Wings of Arbitrary Shapes","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Wind and Air Flow Studies","field":"Environmental Science","cited_by":6,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"","keywords":"Aerodynamics; Span (engineering); Finite element method; Computer science; Structural engineering; Aerospace engineering; Engineering","score_opus":0.026722626137208882,"score_gpt":0.23339057110498682,"score_spread":0.20666794496777793,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2324811470","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":[0.9612395,0.0005006303,0.00059148093,0.00095601444,0.00013479764,0.00018910796,0.000010948426,0.000043879994,0.03633363],"genre_scores_gemma":[0.9922203,0.00006671564,0.00675341,0.00013364507,0.0000275112,0.000015106336,9.189792e-7,0.000007881511,0.00077453646],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.9986006,0.000039404556,0.00019767485,0.00040471827,0.00025838678,0.000499204],"domain_scores_gemma":[0.99944746,0.00025590442,0.000106434076,0.000094858966,0.000012274429,0.0000830757],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0010141786,0.0001471331,0.0001925268,0.000037808848,0.0009956339,0.00004928699,0.00017089261,0.000045646295,0.000072496616],"category_scores_gemma":[0.00034098292,0.00012087111,0.00007195932,0.00036005102,0.0009972419,0.00021910052,0.00012981365,0.00007258077,0.000016592952],"study_design_candidate":"observational","study_design_consensus":"observational","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00005740117,0.00054040755,0.66416156,0.00028750152,0.000084992374,0.0000055082387,0.01223007,0.047679756,0.22498265,0.02510663,0.015638493,0.009225003],"study_design_scores_gemma":[0.008435984,0.005360593,0.48904893,0.0025592546,0.0005905826,0.00010926687,0.062049538,0.13894267,0.08603201,0.050459713,0.1491866,0.007224868],"about_ca_topic_score_codex":0.00019174066,"about_ca_topic_score_gemma":0.0002567159,"teacher_disagreement_score":0.17511268,"about_ca_system_score_codex":0.000022521368,"about_ca_system_score_gemma":0.000023430834,"threshold_uncertainty_score":0.76577115},"labels":[],"label_agreement":null},{"id":"W2325131514","doi":"10.2514/6.2003-1093","title":"Force and Moment Corrections for a Three-Dimensional Model in a Low Speed Wind Tunnel","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Fluid Dynamics Simulations and Interactions","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lockheed Martin (Canada)","funders":"","keywords":"Moment (physics); Physics; Wind tunnel; Wind speed; Environmental science; Mechanics; Meteorology; Classical mechanics","score_opus":0.019992513527788917,"score_gpt":0.23811881696065784,"score_spread":0.21812630343286893,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2325131514","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":[0.9842947,0.00022802567,0.011079066,0.00012615637,0.0002543988,0.00020134951,0.000008957755,0.00005226044,0.0037550873],"genre_scores_gemma":[0.99335706,0.000017380311,0.005805991,0.00002356769,0.000015486174,0.000010810165,0.0000019277393,0.000010682685,0.00075707806],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992748,0.000008557135,0.00015162947,0.00022115956,0.00010477833,0.00023910672],"domain_scores_gemma":[0.99970186,0.000105586565,0.000022318629,0.00007153698,0.00003259304,0.00006611061],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00030211481,0.00010993975,0.00011386859,0.000116482595,0.0003701427,0.000089016954,0.000040637224,0.000041767675,0.000005332573],"category_scores_gemma":[0.00005668133,0.00010492271,0.000027171367,0.00019950466,0.000106996995,0.00019173721,0.000016268676,0.00008554577,0.0000014956107],"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":[0.0000026508294,0.00001415156,0.0031967154,0.000013819747,0.0000034995346,1.6860128e-7,0.00025203652,0.98940504,0.0053375643,0.0015988381,0.00007446739,0.00010103223],"study_design_scores_gemma":[0.0002860365,0.000037888796,0.0008410937,0.00008959881,0.000005573297,0.0000053663157,0.00023087153,0.9969555,0.00022803062,0.0011332257,0.000058103727,0.00012869437],"about_ca_topic_score_codex":0.00005781956,"about_ca_topic_score_gemma":0.00096301193,"teacher_disagreement_score":0.009062379,"about_ca_system_score_codex":0.00004264108,"about_ca_system_score_gemma":0.000030389827,"threshold_uncertainty_score":0.42786238},"labels":[],"label_agreement":null},{"id":"W2325548490","doi":"10.2514/6.2003-856","title":"Improvement of Velocity Role in Coupling of Mass and Momentum Equations","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Computational Fluid Dynamics and Aerodynamics","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":"University of Waterloo","funders":"Sharif University of Technology","keywords":"Momentum (technical analysis); Physics; Coupling (piping); Mechanics; Quantum electrodynamics; Classical mechanics; Mechanical engineering; Engineering; Business","score_opus":0.009450597983066349,"score_gpt":0.20937288447412536,"score_spread":0.199922286491059,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2325548490","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":[0.9940834,0.00045456065,0.0043457025,0.00003589926,0.00006307235,0.00006450125,0.000004541514,0.000012495822,0.00093582174],"genre_scores_gemma":[0.99642444,0.00009043788,0.003455476,0.0000029513865,0.0000041620574,0.0000025402137,0.0000010787421,0.000004457558,0.000014454444],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994025,0.0000044657327,0.00018614296,0.00012783552,0.00014506021,0.00013398506],"domain_scores_gemma":[0.999754,0.00009518685,0.000042357027,0.000047715464,0.00002920437,0.000031505864],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00052076514,0.0000689129,0.00011722741,0.000069665,0.00006342368,0.000021446473,0.000046784637,0.000023372868,0.0000015989954],"category_scores_gemma":[0.000055338725,0.000068616784,0.000014069542,0.00024115582,0.0000998865,0.00006199524,0.000019868252,0.000048171896,1.5154966e-7],"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":[0.0000012134497,0.000015295645,0.020813843,0.000067527566,0.0000058312976,2.048489e-7,0.00047931162,0.7876585,0.17667335,0.013701501,0.000002074067,0.00058131595],"study_design_scores_gemma":[0.0001533482,0.000039175055,0.0029914672,0.00006441462,0.000003525822,3.4988753e-7,0.0007664905,0.98848385,0.0058609024,0.0015529554,0.0000059502854,0.000077576806],"about_ca_topic_score_codex":0.00007587501,"about_ca_topic_score_gemma":0.000082661,"teacher_disagreement_score":0.20082532,"about_ca_system_score_codex":0.000020100082,"about_ca_system_score_gemma":0.00002391598,"threshold_uncertainty_score":0.27981114},"labels":[],"label_agreement":null},{"id":"W2326500577","doi":"10.2514/6.2003-1222","title":"FENSAP-ICE: Roughness Effects on Ice Accretion Prediction","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Icing and De-icing Technologies","field":"Engineering","cited_by":12,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"","keywords":"Geology; Surface roughness; Accretion (finance); Surface finish; Sea ice; Sea ice growth processes; Sea ice thickness; Materials science; Arctic ice pack; Climatology; Physics; Astrophysics; Composite material","score_opus":0.014422404524733385,"score_gpt":0.22310293136031115,"score_spread":0.20868052683557775,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2326500577","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":[0.9672508,0.00032719842,0.001824889,0.00023576194,0.0009820432,0.00013889592,0.0000017329852,0.001361705,0.027876968],"genre_scores_gemma":[0.99789834,0.0001345096,0.0016046963,0.00005472905,0.000081019825,0.000013929266,0.0000014211914,0.000018000703,0.00019338151],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99875027,0.00005272499,0.00015453115,0.0003522911,0.00028667616,0.000403511],"domain_scores_gemma":[0.99946284,0.00020432817,0.00004598723,0.00019593407,0.000029066987,0.00006186798],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0008199514,0.0001948001,0.00017908527,0.00013319896,0.0004971276,0.00015819081,0.00013969639,0.00014017105,0.000002659121],"category_scores_gemma":[0.00041627936,0.00016964713,0.000034121946,0.0005279362,0.00016845735,0.00018851602,0.000028023846,0.00022209137,0.000026474969],"study_design_candidate":"bench_or_experimental","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":[0.000106239866,0.0002248163,0.16798346,0.0022252363,0.00016171376,0.00006712963,0.010782051,0.3607683,0.20379512,0.0389437,0.031655192,0.18328707],"study_design_scores_gemma":[0.00088178634,0.00070883427,0.01150765,0.001406036,0.000052841096,0.000055952198,0.0026884733,0.027486553,0.94769377,0.0014497685,0.0052222507,0.00084608246],"about_ca_topic_score_codex":0.00004007661,"about_ca_topic_score_gemma":0.000013779149,"teacher_disagreement_score":0.74389863,"about_ca_system_score_codex":0.000049225386,"about_ca_system_score_gemma":0.000017586326,"threshold_uncertainty_score":0.6918009},"labels":[],"label_agreement":null},{"id":"W2331988066","doi":"10.2514/6.2003-246","title":"Coupling of the Precursor Shock Wave and the Detonation in Channels Lined with Explosives","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Combustion and Detonation Processes","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":"McGill University","funders":"","keywords":"Explosive material; Detonation; Coupling (piping); Shock wave; Mechanics; Shock (circulatory); Materials science; Acoustics; Physics; Chemistry; Composite material","score_opus":0.01792052316050332,"score_gpt":0.20404018434787116,"score_spread":0.18611966118736784,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2331988066","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":[0.99494475,0.0012485294,0.00038043046,0.00057633576,0.00011221077,0.00015317227,5.31643e-7,0.00003198272,0.002552051],"genre_scores_gemma":[0.9992809,0.00018162739,0.00036820868,0.000026927139,0.000010955562,0.000012499541,1.6346779e-7,0.0000052770197,0.00011339269],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994134,0.000020924208,0.00012655921,0.0001325901,0.00018409996,0.00012243818],"domain_scores_gemma":[0.9996233,0.00018703312,0.00005187032,0.00006615094,0.000048082144,0.000023556522],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006470016,0.00007981918,0.0001018139,0.000049172308,0.00018277764,0.00007052681,0.00006870727,0.000025409672,0.000003554253],"category_scores_gemma":[0.0002314997,0.00004318571,0.000012970675,0.00042075626,0.0003188384,0.00012977014,0.000019995596,0.000074991694,3.0613194e-7],"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":[0.00008294073,0.000052537882,0.049108554,0.0003596412,0.000028796814,0.0000011260985,0.025717847,0.8807964,0.009389296,0.032466438,0.00014471335,0.0018517497],"study_design_scores_gemma":[0.0032686817,0.00013644794,0.007937341,0.0010507258,0.000038918166,0.000032616685,0.018403638,0.7905532,0.1748075,0.0025391318,0.00073014933,0.00050165417],"about_ca_topic_score_codex":0.000011790254,"about_ca_topic_score_gemma":0.00009876444,"teacher_disagreement_score":0.16541821,"about_ca_system_score_codex":0.000009075126,"about_ca_system_score_gemma":0.000027254562,"threshold_uncertainty_score":0.17610623},"labels":[],"label_agreement":null},{"id":"W2332177357","doi":"10.2514/6.2003-619","title":"Actuator Disk Implementation in FENSAP-ICE, a 3D Navier-Stokes In-Flight Simulation System","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Icing and De-icing Technologies","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":"Bell Helicopter Textron (Canada)","funders":"","keywords":"Actuator; Aerospace engineering; Computer science; Simulation; Engineering; Artificial intelligence","score_opus":0.01541145096280101,"score_gpt":0.2609386542228077,"score_spread":0.2455272032600067,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2332177357","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":[0.99326205,0.00031220805,0.00090713723,0.00007261113,0.00024269077,0.0001645468,0.0000018529307,0.00038591863,0.004650955],"genre_scores_gemma":[0.9970753,0.000045360466,0.0027954602,0.000012020796,0.000018431529,0.000014888543,0.0000015256949,0.000012944039,0.0000240407],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9987747,0.00005138518,0.0002772635,0.0002880026,0.000215444,0.00039318713],"domain_scores_gemma":[0.99960405,0.00014313219,0.000060668517,0.00013237857,0.000020068526,0.000039721795],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0009675676,0.00016233829,0.0002014047,0.00024932873,0.00019389039,0.000116805226,0.00011130383,0.00008755308,0.000003110213],"category_scores_gemma":[0.00013402935,0.00014674607,0.00002210047,0.0007358031,0.00009597551,0.00023512713,0.00002669227,0.00014573398,0.000008210229],"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":[0.0000126876,0.000035054818,0.34402892,0.00042623427,0.000013563356,0.000019208814,0.008207671,0.610086,0.008482936,0.0035663599,0.00021138656,0.02490993],"study_design_scores_gemma":[0.003211104,0.00038540747,0.06423211,0.0030988255,0.000053220232,0.000046419147,0.08081776,0.69170296,0.15086369,0.0007081516,0.002897047,0.0019833327],"about_ca_topic_score_codex":0.0002720766,"about_ca_topic_score_gemma":0.00063458394,"teacher_disagreement_score":0.2797968,"about_ca_system_score_codex":0.00011727693,"about_ca_system_score_gemma":0.000025174913,"threshold_uncertainty_score":0.5984131},"labels":[],"label_agreement":null},{"id":"W2335763547","doi":"10.2514/6.2003-604","title":"Low-Speed Characteristics of a High Subsonic Mach Number OHS Aircraft Configuration","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"University of Calgary","funders":"","keywords":"Mach number; Aerospace engineering; Computer science; Aeronautics; Physics; Engineering","score_opus":0.013750082505702211,"score_gpt":0.23109759464216528,"score_spread":0.21734751213646308,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2335763547","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":[0.9802063,0.000055064804,0.0009833679,0.0003175472,0.00013683064,0.00014988221,0.000004430781,0.0001065239,0.018040014],"genre_scores_gemma":[0.9937803,0.000095878546,0.0052750274,0.00007143937,0.000013407116,0.000005307283,0.0000021156504,0.000009842735,0.00074666913],"study_design_codex":"observational","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99845594,0.00006191984,0.00026643724,0.0004514298,0.00037504573,0.00038921268],"domain_scores_gemma":[0.99939483,0.00010062426,0.00020076991,0.00020531131,0.00001963062,0.00007885735],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00062841445,0.0001770442,0.00023794592,0.000035105735,0.00033971076,0.00006445758,0.00021925652,0.000097292366,0.00036885682],"category_scores_gemma":[0.00030788057,0.0001506657,0.000039579198,0.000495987,0.0011054181,0.000278058,0.00008403993,0.00013284471,0.00011290724],"study_design_candidate":"bench_or_experimental","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":[0.00003440016,0.00020208376,0.53036565,0.00007340308,0.000016307304,0.000015899375,0.0011422982,0.000985056,0.43352145,0.01661482,0.0009229373,0.01610568],"study_design_scores_gemma":[0.0014758401,0.00057900004,0.12958634,0.00036248605,0.000056993493,0.0000953822,0.0039345073,0.002375605,0.84386194,0.011895328,0.0044283736,0.0013481955],"about_ca_topic_score_codex":0.00020122943,"about_ca_topic_score_gemma":0.00004415843,"teacher_disagreement_score":0.41034052,"about_ca_system_score_codex":0.000046737274,"about_ca_system_score_gemma":0.000026029162,"threshold_uncertainty_score":0.61439687},"labels":[],"label_agreement":null},{"id":"W2997242994","doi":"10.2514/6.2003-634","title":"Optimization of Controlled Jets in Crossflow","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Fluid Dynamics and Turbulent Flows","field":"Engineering","cited_by":19,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"McGill University; National Aeronautics and Space Administration; National Science Foundation","keywords":"Computer science; Aerospace engineering; Mechanics; Physics; Engineering","score_opus":0.010740535280789023,"score_gpt":0.20947452684582585,"score_spread":0.19873399156503682,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2997242994","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":[0.96777225,0.0012747836,0.0017445185,0.00008371816,0.00023206418,0.00015113286,0.0000017562951,0.000054667504,0.028685134],"genre_scores_gemma":[0.9933782,0.00023200484,0.0062354538,0.000012085818,0.0000137153875,0.0000060347193,7.300868e-7,0.00000829434,0.00011343833],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992261,0.00002755147,0.0002052668,0.00016365778,0.00015537627,0.00022205853],"domain_scores_gemma":[0.999748,0.00006782118,0.000036795565,0.00007888291,0.000024586872,0.00004391036],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006977068,0.000099984674,0.0002076089,0.00012021806,0.000084620886,0.000061226005,0.00007475018,0.00004733599,0.000011188517],"category_scores_gemma":[0.00018092076,0.00008739779,0.00003123607,0.0004193896,0.00012295558,0.000104855426,0.000012772685,0.00006315117,0.0000014042245],"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":[0.0000049595014,0.000009252608,0.007640342,0.00001883063,0.0000030644248,7.281357e-7,0.00019677596,0.9881161,0.0020003146,0.0018851021,0.00002221471,0.00010234709],"study_design_scores_gemma":[0.0011607928,0.000032736414,0.00040873798,0.00007466416,0.0000037271798,0.0000021374992,0.00010782616,0.99669623,0.0012021895,0.00010925829,0.00008513023,0.00011655774],"about_ca_topic_score_codex":0.0000450855,"about_ca_topic_score_gemma":0.000051993567,"teacher_disagreement_score":0.028571695,"about_ca_system_score_codex":0.000019187068,"about_ca_system_score_gemma":0.00003296739,"threshold_uncertainty_score":0.35639787},"labels":[],"label_agreement":null},{"id":"W4237750401","doi":"10.2514/6.2003-1185","title":"Numerical Investigations of Nacelle Anemometry for Horizontal Axis Wind Turbines","year":2003,"lang":"en","type":"article","venue":"41st Aerospace Sciences Meeting and Exhibit","topic":"Wind Energy Research and Development","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure","funders":"","keywords":"Nacelle; Marine engineering; Horizontal axis; Wind power; Aerospace engineering; Vertical axis; Computational fluid dynamics; Environmental science; Mechanics; Engineering; Computer science; Geology; Turbine; Mechanical engineering; Acoustics; Physics; Electrical engineering; Engineering drawing; Structural engineering","score_opus":0.024942525387742952,"score_gpt":0.23773274188862237,"score_spread":0.21279021650087943,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4237750401","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":[0.98384905,0.0011127985,0.0006927185,0.00020825713,0.00020818239,0.000108819244,0.0000046170576,0.00006926616,0.013746312],"genre_scores_gemma":[0.98016554,0.00006385755,0.01942564,0.000017121218,0.00003923009,0.0000101032665,0.0000024600736,0.000010331703,0.0002657295],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99903196,0.000021461748,0.0001637669,0.000203762,0.00023909559,0.00033994627],"domain_scores_gemma":[0.9995204,0.0001317504,0.000028319659,0.0000839698,0.00004400657,0.00019152083],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005168692,0.000113125556,0.00015498488,0.00010328684,0.00025686427,0.000055613455,0.0001040569,0.00004901616,0.00001795659],"category_scores_gemma":[0.00038545966,0.00009741444,0.000036909507,0.00053609896,0.00024041376,0.00011381411,0.00001947236,0.00007266262,0.0000033421347],"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":[0.00006860399,0.0003038537,0.29409385,0.0015950138,0.00024565568,0.000014171358,0.0093078585,0.24559061,0.37132302,0.020742565,0.045701273,0.011013517],"study_design_scores_gemma":[0.002254236,0.0012561505,0.010823182,0.0006632088,0.00003971874,0.000055881548,0.0073717814,0.04720336,0.874743,0.003325159,0.05063781,0.0016265126],"about_ca_topic_score_codex":0.000045085886,"about_ca_topic_score_gemma":0.000016879223,"teacher_disagreement_score":0.50342,"about_ca_system_score_codex":0.000020410342,"about_ca_system_score_gemma":0.00009259659,"threshold_uncertainty_score":0.39724457},"labels":[],"label_agreement":null}]}