{"meta":{"page":1,"per_page":50,"max_per_page":100,"total":10,"total_is_capped":false,"direct_labels_cover":0,"predictions_cover":10,"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":"ed44a8b3d732","filters":{"venue":"Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery"}},"results":[{"id":"W2010208956","doi":"10.1115/2000-gt-0482","title":"Aerodynamic Performance of a Transonic Turbine Cascade at Off-Design Conditions","year":2000,"lang":"en","type":"article","venue":"Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery","topic":"Turbomachinery Performance and Optimization","field":"Engineering","cited_by":33,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":true,"ca_venue":false,"about_ca":false},"ca_institutions":"Carleton University","funders":"Pratt and Whitney Canada","keywords":"Transonic; Mach number; Aerodynamics; Reynolds number; Aerospace engineering; Cascade; Turbine; Trailing edge; Airfoil; Mechanics; Computational fluid dynamics; Structural engineering; Engineering; Physics; Turbulence","authors":[{"name":"D. B. M. Jouini","is_ca":true},{"name":"S. A. Sjolander","is_ca":true},{"name":"S. H. Moustapha","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.005101006677268607,"gpt":0.1739529020822589,"spread":0.1688518954049903,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001673817,0.0003671822,0.0003577824,0.0002736202,0.0004252507,0.0002248499,0.0002033283,0.0002401304,0.001721057],"category_scores_gemma":[0.0004609599,0.0001682576,0.0001293055,0.0001384228,0.0002664266,0.0003128335,0.0003306936,0.0004191581,0.0003005292],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0003559936,"about_ca_system_score_gemma":0.0001651051,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.002443027,"about_ca_topic_score_gemma":0.003264829,"domain_scores_codex":[0.999731,0.00002292193,0.000007964421,0.00004070612,0.0001336927,0.00006365952],"domain_scores_gemma":[0.9997529,0.00005092465,0.00002813324,0.00001686433,0.00009743162,0.00005369121],"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":[0.001567476,0.0003060365,0.02685185,0.00005988164,0.00002573469,0.0008782194,0.0004907966,0.00622997,0.9466277,0.00015868,0.0005363849,0.01626731],"study_design_scores_gemma":[0.0001064684,0.006877571,0.5263583,0.00002232536,0.00004711607,0.001625894,0.0006966025,0.04084924,0.4207667,0.0001266939,0.002415059,0.0001079642],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.999158,0.00001143967,0.0001902874,0.000005427275,0.000001387595,0.000004100428,0.0000474602,0.00001050385,0.0005713807],"genre_scores_gemma":[0.9992518,0.00001189756,0.000168185,0.000005524244,9.087146e-7,0.000003543475,0.0001040869,0.000004540472,0.0004494619],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.002443027,"threshold_uncertainty_score":0.005757511,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2051296752","doi":"10.1115/2001-gt-0434","title":"A Parametric Analysis of Reduced Order Models of Potential Flows in Turbomachinery Using Proper Orthogonal Decomposition","year":2001,"lang":"en","type":"article","venue":"Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery","topic":"Turbomachinery Performance and Optimization","field":"Engineering","cited_by":23,"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":"Transonic; Inviscid flow; Airfoil; Aerodynamics; Mach number; Cascade; Mechanics; Shock (circulatory); Turbomachinery; Flow (mathematics); Physics; Mathematics; Engineering","authors":[{"name":"Bogdan I. Epureanu","is_ca":true},{"name":"Earl H. Dowell","is_ca":false},{"name":"Kenneth C. Hall","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.009925987245523522,"gpt":0.2129239999614926,"spread":0.202998012715969,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003669544,0.0005994736,0.0005683867,0.0003355011,0.0002775127,0.0006812366,0.0004494241,0.0005159982,0.0007106846],"category_scores_gemma":[0.001046496,0.000394531,0.0006773063,0.0001993387,0.0006607409,0.0006638691,0.0003100886,0.0005751616,0.0001631539],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0004688817,"about_ca_system_score_gemma":0.0006458576,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.004711786,"about_ca_topic_score_gemma":0.002744899,"domain_scores_codex":[0.9998752,0.00004500824,0.000004316942,0.00001113114,0.00004235381,0.0000221068],"domain_scores_gemma":[0.9997103,0.0001493962,0.00005037762,0.00002886866,0.00004381857,0.00001720486],"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":[0.00001722517,0.00001475453,0.0002025005,0.00002033599,0.0000050914,0.00002385933,0.00003052988,0.9854698,0.002228803,0.009552971,0.00005306373,0.00238104],"study_design_scores_gemma":[0.000001305414,0.00001124425,0.00004338567,0.000001146743,0.000001100364,0.000003009286,0.000002300633,0.9989613,0.0001990667,0.0006909634,0.00008346856,0.000001764029],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.426505,0.0004691236,0.5646111,0.000145183,0.00002342091,0.00007269758,0.0000815164,0.0001840095,0.007907848],"genre_scores_gemma":[0.9726768,0.0003554795,0.02387185,0.00001037359,0.00001032845,0.00008292811,0.00006852346,0.00003884768,0.002884878],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.004711786,"threshold_uncertainty_score":0.009368718,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2077813465","doi":"10.1115/2001-gt-0493","title":"Midspan Flow-Field Measurements for Two Transonic Linear Turbine Cascades at Off-Design Conditions","year":2001,"lang":"en","type":"article","venue":"Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery","topic":"Turbomachinery Performance and Optimization","field":"Engineering","cited_by":16,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":true,"ca_venue":false,"about_ca":false},"ca_institutions":"Carleton University","funders":"Pratt and Whitney Canada","keywords":"Transonic; Aerodynamics; Turbine; Mach number; Reynolds number; Turbine blade; Aerospace engineering; Structural engineering; Mechanics; Engineering; Physics; Turbulence","authors":[{"name":"D. B. M. Jouini","is_ca":true},{"name":"S. A. Sjolander","is_ca":true},{"name":"S. H. Moustapha","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.01906068880169057,"gpt":0.2291973886208812,"spread":0.2101366998191907,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002480853,0.0003688438,0.000377257,0.0004354823,0.0004233662,0.0002014451,0.0002822248,0.0004282536,0.001498987],"category_scores_gemma":[0.0003385775,0.0001785142,0.0001981836,0.0002162329,0.0003128925,0.0003488366,0.0003455479,0.0005123287,0.0003604443],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0002178128,"about_ca_system_score_gemma":0.0001537464,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.00122121,"about_ca_topic_score_gemma":0.003218552,"domain_scores_codex":[0.9997703,0.00001336924,0.000009010468,0.0000493647,0.0001157125,0.00004210938],"domain_scores_gemma":[0.9997409,0.00004558454,0.00002714768,0.00002233912,0.0001200151,0.0000439733],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","study_design_scores_codex":[0.001002426,0.0003854852,0.03060878,0.00008373459,0.00001664355,0.0005420612,0.0005056189,0.002495818,0.9489061,0.000123708,0.000353044,0.01497664],"study_design_scores_gemma":[0.0001534005,0.004759727,0.4685166,0.00004156852,0.00006175496,0.0007829287,0.001476589,0.02562089,0.4955214,0.0002081405,0.002769689,0.00008730331],"study_design_candidate":"observational","study_design_consensus":null,"genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.9981833,0.00002150763,0.0007472896,0.000009724409,0.000005367574,0.00002214379,0.0001837264,0.00003343724,0.0007934596],"genre_scores_gemma":[0.9978066,0.00003488056,0.001236957,0.00001081763,0.000002590214,0.00001875325,0.0002841594,0.00000969234,0.0005955464],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.001498987,"threshold_uncertainty_score":0.005014658,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W1970222692","doi":"10.1115/2001-gt-0548","title":"Development of Fault Diagnosis and Failure Prediction Techniques for Small Gas Turbine Engines","year":2001,"lang":"en","type":"article","venue":"Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery","topic":"Technical Engine Diagnostics and Monitoring","field":"Engineering","cited_by":6,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":true,"ca_venue":false,"about_ca":false},"ca_institutions":"Queen's University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Gas turbines; Fault (geology); Turbine; Operating point; Combined cycle; Automotive engineering; Reliability engineering; Power (physics); Gas engine; Engineering; Computer science; Mechanical engineering; Electrical engineering","authors":[{"name":"Craig R. Davison","is_ca":true},{"name":"A. M. Birk","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.009817451845324916,"gpt":0.2046588593724338,"spread":0.1948414075271089,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002489183,0.0004032385,0.0004171912,0.0003759378,0.0002111269,0.000239637,0.0005081703,0.0004041818,0.0009208078],"category_scores_gemma":[0.001876203,0.0002562286,0.0003229758,0.0002120885,0.0002368829,0.0004439153,0.0002014107,0.0005387677,0.0001832669],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0004327585,"about_ca_system_score_gemma":0.000578844,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.00626015,"about_ca_topic_score_gemma":0.003974149,"domain_scores_codex":[0.9999051,0.00001677622,0.00000626071,0.00002313232,0.00003879218,0.000009883796],"domain_scores_gemma":[0.9993538,0.0004074488,0.00005253647,0.00004496671,0.0001229132,0.00001828092],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","study_design_scores_codex":[0.00009068917,0.0000542289,0.001631382,0.00008503802,0.00002510087,0.0001360046,0.00009085071,0.7843295,0.02075483,0.00370441,0.0006409739,0.188457],"study_design_scores_gemma":[0.000004525388,0.00002734426,0.0002657083,0.000003009753,0.000003652071,0.00001967755,0.000003720701,0.995562,0.00314444,0.0006805906,0.0002821464,0.000003133055],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.05786383,0.0001849965,0.9397568,0.00007089671,0.00001728176,0.0000514495,0.0000489223,0.001392356,0.0006134882],"genre_scores_gemma":[0.6645475,0.0001824887,0.3339586,0.00001885441,0.00001548811,0.0001142505,0.00007770843,0.00004982207,0.001035272],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.00626015,"threshold_uncertainty_score":0.01244742,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W4256223997","doi":"10.1115/2001-gt-0324","title":"Numerical Investigation of Tandem-Impeller Designs for a Gas Turbine Compressor","year":2001,"lang":"en","type":"article","venue":"Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery","topic":"Turbomachinery Performance and Optimization","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":false,"ca_fund":true,"ca_venue":false,"about_ca":false},"ca_institutions":"","funders":"Pratt and Whitney Canada","keywords":"Impeller; Slip factor; Tandem; Gas compressor; Turbine; Aerodynamics; Centrifugal compressor; Mechanical engineering; Computational fluid dynamics; Mechanics; Materials science; Engineering; Physics; Aerospace engineering","authors":[{"name":"Douglas Roberts","is_ca":false},{"name":"S. C. Kacker","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.01458481135164126,"gpt":0.2028510142835818,"spread":0.1882662029319405,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004729371,0.0003459824,0.0004982155,0.0004166007,0.0004430884,0.000500281,0.0005677298,0.0009732076,0.001553203],"category_scores_gemma":[0.001162057,0.000218257,0.0004540425,0.0003444999,0.00050955,0.0003090765,0.0003958819,0.0003236919,0.0001295385],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0004263411,"about_ca_system_score_gemma":0.0006062311,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.003678776,"about_ca_topic_score_gemma":0.003415699,"domain_scores_codex":[0.9998517,0.00002843957,0.000009380342,0.00002159058,0.000051528,0.00003727911],"domain_scores_gemma":[0.9994465,0.00030199,0.00009584395,0.0000349194,0.00008176699,0.00003912097],"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":[0.0002379492,0.0001333752,0.004920522,0.0001057006,0.00001591144,0.0003381752,0.00005491474,0.9723365,0.0148149,0.001026502,0.0002338246,0.005781655],"study_design_scores_gemma":[0.00002486451,0.0001874338,0.001178302,0.000005087608,0.00000772951,0.00004198991,0.00003997522,0.9961479,0.002063854,0.00007325,0.0002234699,0.000006236262],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.9804078,0.000144075,0.01408493,0.00008049829,0.00002176709,0.00005785922,0.0001218964,0.00006713074,0.005014062],"genre_scores_gemma":[0.9914937,0.00005085949,0.007679532,0.000007921581,0.000004040225,0.00002750045,0.00004682345,0.000005936045,0.0006837512],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.003678776,"threshold_uncertainty_score":0.007314742,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2045950278","doi":"10.1115/2000-gt-0623","title":"Steady State Performance Simulation of Auxiliary Power Unit With Faults for Component Diagnosis","year":2000,"lang":"en","type":"article","venue":"Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery","topic":"Engineering Diagnostics and Reliability","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"Queen's University","funders":"","keywords":"Fault (geology); Steady state (chemistry); Power (physics); Component (thermodynamics); Turbine; Computer science; Baseline (sea); Automotive engineering; Control theory (sociology); Simulation; Engineering; Mechanical engineering","authors":[{"name":"Craig R. Davison","is_ca":true},{"name":"A. M. Birk","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.0060913737935562,"gpt":0.1886536072986204,"spread":0.1825622335050642,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002814938,0.0004783837,0.0005430788,0.0003362603,0.0002859026,0.0003913614,0.0006562921,0.0007325861,0.002607346],"category_scores_gemma":[0.001061237,0.0002136145,0.0003918811,0.0002550285,0.0003755863,0.0003721524,0.000244724,0.0005414991,0.0003210421],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0005062644,"about_ca_system_score_gemma":0.0004935215,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.008201381,"about_ca_topic_score_gemma":0.004817053,"domain_scores_codex":[0.999885,0.00003147118,0.000005238787,0.00001482074,0.0000377912,0.00002567358],"domain_scores_gemma":[0.9993256,0.0003822671,0.00004872218,0.00005719597,0.0001461024,0.00004012271],"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":[0.00009074578,0.00004790173,0.001272081,0.0000253613,0.000008648446,0.00006070848,0.00004071917,0.9928983,0.002841048,0.0006253032,0.0001958171,0.001893278],"study_design_scores_gemma":[0.000005661548,0.00003853151,0.0003477414,0.000001260195,0.000002800812,0.000004906914,0.000005873233,0.9983664,0.001044454,0.0001057433,0.00007456297,0.00000209836],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.9316722,0.0001152456,0.05891246,0.0001184986,0.00003062213,0.00007296254,0.0005198055,0.0007794205,0.00777882],"genre_scores_gemma":[0.9964448,0.00002996861,0.002356144,0.000005916158,0.000001874235,0.00003365094,0.0001244742,0.00001992526,0.0009833411],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.008201381,"threshold_uncertainty_score":0.01630729,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2050318067","doi":"10.1115/2000-gt-0483","title":"Design of Low-Speed Cascades for Investigating Viscous Effects in High-Speed Axial Turbines","year":2000,"lang":"en","type":"article","venue":"Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery","topic":"Turbomachinery Performance and Optimization","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"Carleton University","funders":"","keywords":"Cascade; Computational fluid dynamics; Reynolds number; Speedup; Mechanics; Turbulence; Pressure coefficient; Solver; Navier–Stokes equations; Computer science; Control theory (sociology); Flow (mathematics); Inverse problem; Freestream; Axial compressor; Turbine blade; Mathematical optimization; Turbine; Mathematics; Physics; Mechanical engineering; Mathematical analysis; Engineering; Compressibility","authors":[{"name":"K. Zavitz","is_ca":true},{"name":"S. A. Sjolander","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.00677404906486547,"gpt":0.1905155338761944,"spread":0.183741484811329,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004769542,0.0006342361,0.0004061935,0.0003141515,0.0004492386,0.0004462435,0.000658915,0.0003946345,0.001910103],"category_scores_gemma":[0.0007817604,0.0003606635,0.0003102515,0.0001299324,0.0004515929,0.0004902925,0.0006008243,0.0004902472,0.0003520009],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0004933373,"about_ca_system_score_gemma":0.0008277313,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.0008636079,"about_ca_topic_score_gemma":0.001461722,"domain_scores_codex":[0.9997519,0.00004742106,0.000007118361,0.00003637616,0.0001271052,0.00003001516],"domain_scores_gemma":[0.9997634,0.00007383683,0.00005673253,0.00002142202,0.0000507459,0.00003382586],"domain_codex":null,"domain_gemma":null,"domain_candidate":null,"domain_consensus":null,"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","study_design_scores_codex":[0.0003407995,0.0002414644,0.003232416,0.0003666511,0.00003229105,0.0003461895,0.0001717001,0.6692872,0.2785463,0.007541647,0.0005553071,0.03933804],"study_design_scores_gemma":[0.00008792093,0.001125359,0.002810071,0.00003881646,0.00003347905,0.0001008622,0.0000663326,0.9168167,0.07428961,0.002097878,0.002509574,0.0000233516],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"genre_codex":"methods","genre_gemma":"empirical","genre_scores_codex":[0.4353583,0.0003338483,0.5463246,0.0001191548,0.00003730196,0.0006235222,0.0001114545,0.0002893167,0.01680249],"genre_scores_gemma":[0.9170204,0.0001776346,0.08086133,0.00001710957,0.000006496835,0.000266854,0.00003766226,0.00002559372,0.001586958],"genre_candidate":"empirical","genre_consensus":null,"teacher_disagreement_score":0.001910103,"threshold_uncertainty_score":0.006389916,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2008804754","doi":"10.1115/2000-gt-0649","title":"Experimental and Computational Investigation of Losses in a Circular to Oblong Diffusing Gas Turbine Transition Duct With Offset","year":2000,"lang":"en","type":"article","venue":"Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery","topic":"Turbomachinery Performance and Optimization","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"Queen's University","funders":"","keywords":"Duct (anatomy); Computational fluid dynamics; Atmospheric duct; Nacelle; Aerodynamics; Turbulence; Turbofan; Turbine; Mechanics; Inlet; Mechanical engineering; Aerospace engineering; Engineering; Physics","authors":[{"name":"A. J. Stronach","is_ca":true},{"name":"A. M. Birk","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.004689030428118016,"gpt":0.1755702140727224,"spread":0.1708811836446044,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004846739,0.0002897705,0.0003808302,0.0003425551,0.0004292617,0.00031369,0.000439932,0.0003431972,0.0009930785],"category_scores_gemma":[0.001014012,0.0001915816,0.0001795694,0.0003315956,0.000624578,0.0004367068,0.0002593411,0.0003048178,0.0001840652],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0003529209,"about_ca_system_score_gemma":0.0001596493,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.0008392152,"about_ca_topic_score_gemma":0.0009425532,"domain_scores_codex":[0.9997513,0.00003635079,0.00001610566,0.00003340199,0.0001124832,0.00005039448],"domain_scores_gemma":[0.99915,0.0003426472,0.000121468,0.0001252462,0.0002186835,0.00004189504],"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":[0.001477264,0.001259403,0.0203584,0.0002819177,0.00002668132,0.000592854,0.000615249,0.1757357,0.7543537,0.001779662,0.001001411,0.04251766],"study_design_scores_gemma":[0.00005560726,0.00292056,0.02360706,0.00001845184,0.00002261282,0.000329401,0.0002439342,0.34118,0.6300023,0.0002204919,0.00136029,0.00003942397],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.9978973,0.00003199601,0.001411657,0.00001257288,0.000003568828,0.000005196157,0.00004547506,0.00003796559,0.0005543656],"genre_scores_gemma":[0.9982172,0.0000279677,0.001265729,0.00000366112,0.000001516823,0.000008105835,0.0000555735,0.00001098727,0.0004092574],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.0009930785,"threshold_uncertainty_score":0.003322184,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2016483440","doi":"10.1115/2000-gt-0647","title":"Effect of Swirl on the Performance of a Gas Turbine Reversing Exhaust Duct","year":2000,"lang":"en","type":"article","venue":"Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery","topic":"Combustion and flame dynamics","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"Carleton University; Queen's University","funders":"","keywords":"Duct (anatomy); Mach number; Turbine; Mechanics; Aerodynamics; Secondary air injection; Mechanical engineering; Materials science; Engineering; Automotive engineering; Physics","authors":[{"name":"Mark Cunningham","is_ca":true},{"name":"A. M. Birk","is_ca":true},{"name":"Jérôme Gauthier","is_ca":true},{"name":"W. Di Bartolomeo","is_ca":false}],"retraction":null,"screen_n_in":null,"score":{"opus":0.003583767163467654,"gpt":0.172925983441848,"spread":0.1693422162783803,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004810727,0.000680615,0.0004851251,0.0003881383,0.0005031521,0.000642409,0.0004181548,0.0005273334,0.002286359],"category_scores_gemma":[0.002098385,0.0003672641,0.0003144973,0.0003067419,0.0004752002,0.0006514147,0.000454281,0.0003825167,0.0006545522],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0003130725,"about_ca_system_score_gemma":0.000233991,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.0009231142,"about_ca_topic_score_gemma":0.001199878,"domain_scores_codex":[0.9995732,0.00006386337,0.00004229448,0.00006835035,0.0001401227,0.0001121325],"domain_scores_gemma":[0.9982228,0.0007677836,0.0003369347,0.000130784,0.0003663434,0.0001753575],"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":[0.003878478,0.0004702858,0.01335023,0.0002828203,0.00004633898,0.0007665116,0.0004768431,0.01737197,0.9428466,0.0001206712,0.0002546377,0.02013479],"study_design_scores_gemma":[0.00005498,0.004361586,0.02648171,0.00002449062,0.00004877066,0.000300597,0.0002689451,0.01074163,0.957108,0.00003152669,0.0005367936,0.00004100045],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.9992504,0.00007455472,0.0002713592,0.00001082891,0.000006075002,0.00000376365,0.00003270763,0.0000480749,0.0003021635],"genre_scores_gemma":[0.9991697,0.00004611694,0.0002641487,0.00001007009,0.000003092696,0.000002856893,0.00006071509,0.00002135665,0.0004219691],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.002286359,"threshold_uncertainty_score":0.007648587,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null},{"id":"W2016935047","doi":"10.1115/2000-gt-0328","title":"Water Mist Fire-Fighting System in the Marine LM2500 Gas Turbine Module","year":2000,"lang":"en","type":"article","venue":"Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery","topic":"Combustion and Detonation Processes","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"routes":{"ca_aff":true,"ca_fund":false,"ca_venue":false,"about_ca":false},"ca_institutions":"Royal Canadian Navy","funders":"","keywords":"Mist; Enclosure; Gas turbines; Turbine; Environmental science; Marine engineering; Aeronautics; Fire protection; Firefighting; Engineering; Computer science; Aerospace engineering; Mechanical engineering; Meteorology; Electrical engineering; Civil engineering; Physics; Geography","authors":[{"name":"Glenn McAndrews","is_ca":false},{"name":"Victor M. Gameiro","is_ca":false},{"name":"Tom Shirriff","is_ca":true}],"retraction":null,"screen_n_in":null,"score":{"opus":0.005374022433000245,"gpt":0.1770352331114279,"spread":0.1716612106784276,"validation_status":"score_only:v0-immature-baseline"},"prediction":{"model_version":"metacan-v3-hybrid-931329e0061c","candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001495133,0.0002066541,0.000296384,0.0001662137,0.0003029165,0.0001453702,0.0005009324,0.0002629581,0.003278025],"category_scores_gemma":[0.0001539161,0.0001043356,0.0001277611,0.00010999,0.0001294643,0.0002106208,0.0002278864,0.0001359235,0.0007054806],"about_ca_system_candidate":false,"about_ca_system_consensus":false,"about_ca_system_score_codex":0.0001737213,"about_ca_system_score_gemma":0.0001801135,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_topic_score_codex":0.001081319,"about_ca_topic_score_gemma":0.001248345,"domain_scores_codex":[0.9999429,0.000009329984,0.000003322301,0.00001281588,0.00001861272,0.00001302473],"domain_scores_gemma":[0.9999269,0.00001435406,0.000008574317,0.000009920199,0.00001842959,0.00002171777],"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":[0.002046394,0.0003156143,0.01282525,0.0002125412,0.00004476373,0.001814238,0.0003875037,0.02606007,0.8349755,0.001646559,0.00237773,0.1172938],"study_design_scores_gemma":[0.0002242938,0.005831804,0.04072317,0.00004783557,0.00009807566,0.001765323,0.0002008202,0.3089385,0.6290075,0.0005258436,0.01254262,0.00009425298],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","genre_codex":"empirical","genre_gemma":"empirical","genre_scores_codex":[0.9731626,0.00007287162,0.02236393,0.0000544778,0.00002335322,0.00005049548,0.0000769514,0.001275787,0.002919586],"genre_scores_gemma":[0.9871767,0.00002260966,0.008686217,0.00002583484,0.000004229767,0.00002008455,0.00006615906,0.00001978972,0.003978483],"genre_candidate":"empirical","genre_consensus":"empirical","teacher_disagreement_score":0.003278025,"threshold_uncertainty_score":0.01096606,"prediction_status":"machine_predicted_unvalidated"},"labels":[],"label_agreement":null}]}