{"meta":{"query_hash":"ace3caddad5b","filters":{"topic":"Advanced Aircraft Design and Technologies"},"cohort_total":460,"direct_labels_cover":0,"predictions_cover":460,"exported":460,"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/ace3caddad5b","api":"https://metacan.xera.ac/api/v1/cohort?topic=Advanced+Aircraft+Design+and+Technologies"},"results":[{"id":"W1168118192","doi":"10.1520/stp14486s","title":"The Effect of Recirculation on Aircraft Cabin Air Quality — In-flight Tests and Simulation Study","year":2000,"lang":"en","type":"book-chapter","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Honeywell (Canada)","funders":"","keywords":"Aeronautics; Aerospace engineering; Environmental science; Engineering; Automotive engineering","score_opus":0.015696540221723385,"score_gpt":0.28101806779497374,"score_spread":0.26532152757325034,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1168118192","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":[0.5551609,0.00014841069,0.00044896008,0.00018496186,0.00008711915,0.002961066,0.000008498464,0.00023903683,0.4407611],"genre_scores_gemma":[0.9773216,0.00004925934,0.000047780733,0.000017185475,0.0000083331515,0.000017641474,0.0000036178021,0.000018300485,0.022516284],"study_design_codex":"design_other","study_design_gemma":"observational","domain_scores_codex":[0.99866664,0.00008404694,0.0003736927,0.00039092766,0.00033994386,0.00014474572],"domain_scores_gemma":[0.9984468,0.00094051525,0.00016117525,0.0004221749,0.000004690843,0.000024596213],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00047381475,0.00024261636,0.00029735832,0.00006285933,0.00009992263,0.000009296692,0.0001603033,0.00020187235,0.00019877289],"category_scores_gemma":[0.00009550667,0.00015296653,0.000048833444,0.000058438225,0.00023385663,0.00008964581,0.00008210809,0.00023549476,0.000067541005],"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":[0.0005685466,0.00018054582,0.17033863,0.00004336843,0.000058006575,0.000022347156,0.0003000276,0.15583248,0.0006679955,0.0074534407,0.00009750035,0.6644371],"study_design_scores_gemma":[0.0024564606,0.003984508,0.88558275,0.00019299336,0.00007960689,0.0000031652,0.000078530844,0.0042746877,0.0019564906,0.08466013,0.015664693,0.0010660131],"about_ca_topic_score_codex":0.00010741917,"about_ca_topic_score_gemma":0.00043475552,"teacher_disagreement_score":0.7152441,"about_ca_system_score_codex":0.0001484522,"about_ca_system_score_gemma":0.0000034081818,"threshold_uncertainty_score":0.62377936},"labels":[],"label_agreement":null},{"id":"W1208033369","doi":"10.19053/uptc.01233769.1645","title":"A Brief Summary of the Special Report on Aviation and the Global Atmosphere","year":2011,"lang":"en","type":"article","venue":"Perspectiva geográfica","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Civil aviation; Montreal Protocol; Aviation; Atmosphere (unit); Aeronautics; Climate change; Meteorology; Environmental science; Political science; Ozone layer; Engineering; Geography; Ozone; Aerospace engineering; Geology","score_opus":0.009963958869280264,"score_gpt":0.21191848160688154,"score_spread":0.20195452273760128,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1208033369","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":[0.6031261,0.00013476264,0.00059552176,0.0020959454,0.00024986558,0.00050874834,0.000007669794,0.000118628406,0.39316273],"genre_scores_gemma":[0.9986736,0.000033393026,0.0006798386,0.00008513258,0.00007231768,0.00001087301,3.2498002e-7,0.000005029215,0.00043946222],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.9992096,0.00004009003,0.00013872614,0.00024622705,0.00022467584,0.00014072769],"domain_scores_gemma":[0.9994141,0.00003726985,0.00011710509,0.0004003892,0.000008651906,0.00002248779],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001457216,0.000097486765,0.00011204999,0.0000020343844,0.00015195264,0.000008690899,0.0002550961,0.00005431125,0.00047021903],"category_scores_gemma":[0.00018439506,0.000052028587,0.00006554429,0.00020502205,0.00091884,0.00007245864,0.00020976766,0.00011543767,0.000021509792],"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":[0.0005570039,0.0002906974,0.7805036,0.000006101006,0.000048035643,0.0000551307,0.0026667537,0.000070295515,0.00025662634,0.17368549,0.005330713,0.036529567],"study_design_scores_gemma":[0.0006299661,0.00007329873,0.8827042,0.000012730025,0.000020696094,0.00007428175,0.001136908,0.000063677806,0.0011366043,0.10784199,0.0061776335,0.00012803618],"about_ca_topic_score_codex":0.00069042406,"about_ca_topic_score_gemma":0.00014966678,"teacher_disagreement_score":0.3955475,"about_ca_system_score_codex":0.0001184472,"about_ca_system_score_gemma":0.000007808559,"threshold_uncertainty_score":0.5148569},"labels":[],"label_agreement":null},{"id":"W1255169372","doi":"","title":"Propulsion Technologies for Future Commercial Aircraft","year":2013,"lang":"en","type":"article","venue":"NASA STI Repository (National Aeronautics and Space Administration)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"China Academy of Engineering Physics; National Aeronautics and Space Administration","keywords":"Aerospace; Summit; Aeronautics; Aviation; Propulsion; Engineering; Subject (documents); Business; Computer science; Aerospace engineering; Library science; Geography","score_opus":0.010291683785859063,"score_gpt":0.24021826538854985,"score_spread":0.22992658160269078,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1255169372","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":[0.89922893,0.0003830508,0.030923508,0.052283302,0.0008234763,0.0026332056,0.000052715877,0.001193922,0.0124778645],"genre_scores_gemma":[0.96211827,0.000031121708,0.035762824,0.00013081485,0.000096415424,0.00022781774,0.000026855136,0.0000130457,0.0015928425],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"observational","domain_scores_codex":[0.99882776,0.000015826456,0.00023544647,0.00034451726,0.00035784752,0.00021862752],"domain_scores_gemma":[0.99949545,0.00008892995,0.00011673756,0.00016395557,0.000079449215,0.0000555051],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000090029906,0.00017801777,0.00013956735,0.000042726315,0.00046654846,0.000097063516,0.00017951654,0.00019950791,0.0000603321],"category_scores_gemma":[0.00010199338,0.00015332653,0.000044973793,0.00013439152,0.0003315935,0.00036892592,0.00010317315,0.00015642833,0.000035831556],"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":[0.00032434048,0.0012709438,0.19029127,0.0001863123,0.0001447148,0.00003575191,0.00045619966,0.0007088879,0.14286931,0.32668957,0.07132097,0.2657017],"study_design_scores_gemma":[0.0015198904,0.0016064765,0.60575026,0.00004437765,0.00005648011,0.00019650377,0.0016840644,0.0058696168,0.0422408,0.1464591,0.19339454,0.0011778875],"about_ca_topic_score_codex":0.00001151686,"about_ca_topic_score_gemma":0.00003043136,"teacher_disagreement_score":0.415459,"about_ca_system_score_codex":0.000114435505,"about_ca_system_score_gemma":0.00004537631,"threshold_uncertainty_score":0.6252474},"labels":[],"label_agreement":null},{"id":"W130246569","doi":"10.1017/cbo9780511844652","title":"Aircraft Design","year":2010,"lang":"en","type":"book","venue":"Cambridge University Press eBooks","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":100,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Queen's University","funders":"","keywords":"Avionics; Sizing; Engineering; Conceptual design; Systems engineering; Cockpit; Process (computing); Multidisciplinary approach; Design process; Aerodynamics; Aviation; Computer science; Aeronautics; Aerospace engineering; Mechanical engineering; Operations management; Work in process","score_opus":0.017777414463776176,"score_gpt":0.19180432512434206,"score_spread":0.1740269106605659,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W130246569","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.000033869306,0.000031451804,0.037440527,0.000017675828,0.00020390522,0.0005120516,0.00005387504,0.00062871526,0.9610779],"genre_scores_gemma":[0.0001709792,0.000047282607,0.0075819353,0.000075742144,0.00005734293,0.0000022670633,0.000019442496,0.000052144507,0.9919929],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.99835765,0.000052096148,0.00015272333,0.00068064715,0.00032546773,0.00043143626],"domain_scores_gemma":[0.99872744,0.00010397736,0.00017365652,0.0008185017,0.000017763214,0.00015865643],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.000110474364,0.00041476815,0.000351113,0.00009417853,0.00023848914,0.000029133906,0.0010945426,0.0007933712,0.00005697789],"category_scores_gemma":[0.00002580313,0.0004618326,0.00016207254,0.000023186603,0.0008954689,0.00014549328,0.0009115269,0.0010730085,0.0003169892],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00006866596,0.000025833515,0.00000988412,0.000026713833,0.000052070856,0.000623768,0.00002429339,0.000079324614,0.0021233312,0.08660237,0.8991496,0.011214156],"study_design_scores_gemma":[0.00029695334,0.000059722952,0.00001950793,0.000031064123,0.000074291056,0.000019403331,0.00001105661,0.000085914944,0.0031628292,0.000114156246,0.9955906,0.00053444394],"about_ca_topic_score_codex":0.00006392029,"about_ca_topic_score_gemma":0.0000035740525,"teacher_disagreement_score":0.09644106,"about_ca_system_score_codex":0.0004945855,"about_ca_system_score_gemma":0.00008188122,"threshold_uncertainty_score":0.99978334},"labels":[],"label_agreement":null},{"id":"W1608780481","doi":"10.4271/2008-01-2886","title":"Dynamic Thermal Management System Modeling of a More Electric Aircraft","year":2008,"lang":"en","type":"article","venue":"SAE technical papers on CD-ROM/SAE technical paper series","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":46,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lockheed Martin (Canada)","funders":"","keywords":"Thermal management of electronic devices and systems; Computer science; Aerospace engineering; Systems engineering; Engineering; Mechanical engineering","score_opus":0.009841379105862804,"score_gpt":0.22299806086892995,"score_spread":0.21315668176306715,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1608780481","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":[0.92156684,0.00052913924,0.00014649147,0.0012669794,0.00013203303,0.0016551312,0.000025383768,0.005116185,0.0695618],"genre_scores_gemma":[0.9799303,0.00072755746,0.017977266,0.00039715687,0.000020614283,0.00034157245,0.000012855931,0.00011249972,0.00048019973],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.99515533,0.00009784069,0.0011028809,0.0013147453,0.0012218907,0.0011072917],"domain_scores_gemma":[0.997667,0.00015338617,0.000269495,0.0016335654,0.0000328027,0.00024373012],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00038179458,0.00076900225,0.0009235368,0.00024710104,0.0004822169,0.000024624216,0.0015868141,0.00066925416,0.00029463257],"category_scores_gemma":[0.00014292038,0.0006474881,0.00044432914,0.0013661259,0.0014343252,0.0004817033,0.00090724067,0.0010004728,0.00022255338],"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":[0.00021347686,0.00033776468,0.00036563695,0.00008051234,0.000047458267,0.00022980994,0.000029301696,0.003718968,0.9826539,0.0042442954,0.0003430187,0.0077358177],"study_design_scores_gemma":[0.0009023552,0.0011055823,0.9900177,0.0002743095,0.000106801606,0.00034167376,0.00036130563,0.000060634826,0.00045602355,0.0017644526,0.003576992,0.0010321819],"about_ca_topic_score_codex":0.00005100723,"about_ca_topic_score_gemma":0.0035479006,"teacher_disagreement_score":0.98965204,"about_ca_system_score_codex":0.00078086555,"about_ca_system_score_gemma":0.00003016105,"threshold_uncertainty_score":0.9995976},"labels":[],"label_agreement":null},{"id":"W1874132801","doi":"10.1109/pes.2004.1373274","title":"Modeling and simulation of the electric part of a grid connected microturbine","year":2004,"lang":"en","type":"article","venue":"IEEE Power Engineering Society General Meeting, 2004.","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":57,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure","funders":"","keywords":"Grid; Voltage; Software; Turbine; Three-phase; Computer science; Engineering; Electrical engineering; Control engineering; Mechanical engineering","score_opus":0.006368554679088664,"score_gpt":0.20055214019393094,"score_spread":0.19418358551484227,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1874132801","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":[0.91883826,0.00036259028,0.08034361,0.000054675755,0.00013939614,0.00013981415,0.000003368978,0.00008291795,0.000035376994],"genre_scores_gemma":[0.98553604,0.000042234577,0.014314749,0.000033774086,0.000026553778,0.000005765971,7.646777e-7,0.000015385052,0.000024728019],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992403,0.000008874363,0.00021542716,0.0001772891,0.00015697436,0.00020115104],"domain_scores_gemma":[0.9996801,0.000027256434,0.00007855838,0.00017225814,0.000015708712,0.000026107344],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012287637,0.00012714764,0.00014489476,0.000016009773,0.000049807782,0.000005025677,0.00014172719,0.00008700199,0.000009206576],"category_scores_gemma":[0.00007371402,0.00010215457,0.0000903762,0.00030292536,0.00006609473,0.00006749105,0.000052282958,0.00012806339,0.0000011291924],"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":[0.0000015811199,0.000010695509,0.00025841023,0.000007922215,0.000008068837,1.2154767e-7,0.00012875632,0.64356464,0.35589546,0.00001609901,0.00003674285,0.00007152042],"study_design_scores_gemma":[0.00033815927,0.000040771618,0.00045267105,0.00005261957,0.0000134416605,0.0000025740705,0.000024432691,0.7142701,0.28424433,0.00024516968,0.00017142411,0.00014429206],"about_ca_topic_score_codex":0.000066919696,"about_ca_topic_score_gemma":0.0000029417113,"teacher_disagreement_score":0.07165113,"about_ca_system_score_codex":0.00007991062,"about_ca_system_score_gemma":0.0000084789435,"threshold_uncertainty_score":0.41657424},"labels":[],"label_agreement":null},{"id":"W1967108662","doi":"10.1289/ehp.114-a95a","title":"Policy: Cloud Banks: Airlines Save Halon","year":2006,"lang":"en","type":"article","venue":"Environmental Health Perspectives","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":2,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Montreal Protocol; Ozone layer; Business; Ozone depletion; Environmental science; Developing country; Meteorology; Ozone; Economic growth; Economics; Geography","score_opus":0.007505214802485141,"score_gpt":0.25631192127124863,"score_spread":0.2488067064687635,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1967108662","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":[0.92519397,0.0051523694,0.011763492,0.019428818,0.00040924817,0.0016531404,0.00014838991,0.0013392305,0.034911327],"genre_scores_gemma":[0.9898373,0.00053051935,0.0061031836,0.0004695511,0.00031424387,0.00004252592,0.000019199471,0.00003792436,0.0026455445],"study_design_codex":"design_other","study_design_gemma":"observational","domain_scores_codex":[0.99797505,0.000073779745,0.00030915855,0.000633012,0.0003581546,0.00065085734],"domain_scores_gemma":[0.9992948,0.000046723784,0.00013960965,0.00038767245,0.0000012968937,0.00012987199],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.0001436,0.00028481593,0.0002567985,0.000086509004,0.00039987412,0.00001960129,0.00027604363,0.00010689695,0.0010068819],"category_scores_gemma":[0.000020855285,0.0002688148,0.000094150135,0.00023322813,0.00080012047,0.00027030386,0.0002395745,0.0002497439,0.0009904546],"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":[0.00057033106,0.008881424,0.32451674,0.00014495378,0.00012896872,0.0002339201,0.017850913,0.014130673,0.07381877,0.08101741,0.079561114,0.3991448],"study_design_scores_gemma":[0.0022518523,0.0015442711,0.7567291,0.00006111282,0.00001887268,0.00013534397,0.019992191,0.0007697621,0.011650442,0.08238566,0.122699454,0.0017619162],"about_ca_topic_score_codex":0.0016461873,"about_ca_topic_score_gemma":0.0002020351,"teacher_disagreement_score":0.43221238,"about_ca_system_score_codex":0.0015574152,"about_ca_system_score_gemma":0.000021752625,"threshold_uncertainty_score":0.9999764},"labels":[],"label_agreement":null},{"id":"W1973023095","doi":"10.1115/gt2014-25594","title":"Aerodynamic Calibration and Thrust Correction Method With Inflow Separation in Indoor Sea Level Test Facility","year":2014,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Turbofan; Thrust; Aerodynamics; Thrust specific fuel consumption; Marine engineering; Inflow; Calibration; Jet engine; Nozzle; Separation (statistics); Momentum (technical analysis); Environmental science; Aerospace engineering; Engineering; Fuel efficiency; Mechanics; Computer science; Mathematics; Physics; Statistics","score_opus":0.013344389985156625,"score_gpt":0.25533496221413476,"score_spread":0.24199057222897813,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1973023095","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":[0.3735069,0.00000167615,0.6241576,0.0001230331,0.000023670773,0.00015806011,0.0000035944913,0.00010401436,0.0019214181],"genre_scores_gemma":[0.9694295,0.0000037462094,0.030111428,0.000066310604,0.0000034919385,0.000020974894,0.000011996067,0.000003596326,0.00034898196],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.999367,0.00004809725,0.00011367999,0.00024340858,0.00010890846,0.000118908196],"domain_scores_gemma":[0.9996842,0.00012007759,0.000038429836,0.00012833472,0.0000041107905,0.000024856457],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002097025,0.00009242122,0.00009130221,0.000032979795,0.000064641485,0.000020724121,0.000052906085,0.00007267913,0.00011299792],"category_scores_gemma":[0.00012281732,0.00007001744,0.0000074900245,0.00020024297,0.00009662381,0.00042318908,0.000041286752,0.000106726555,0.000018703337],"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":[0.000020661639,0.00004237069,0.8434782,0.0000036079123,0.000001351245,5.841307e-7,0.000085289605,0.006694753,0.015757026,0.00008128249,0.00013235191,0.13370255],"study_design_scores_gemma":[0.00031427504,0.00015203144,0.6599477,0.000004863428,0.000002994912,0.000007641249,0.00011074196,0.32764897,0.010447832,0.0010356568,0.0001888407,0.00013847671],"about_ca_topic_score_codex":0.0004992731,"about_ca_topic_score_gemma":0.0059506735,"teacher_disagreement_score":0.5959225,"about_ca_system_score_codex":0.000082958075,"about_ca_system_score_gemma":0.0000044269705,"threshold_uncertainty_score":0.33206156},"labels":[],"label_agreement":null},{"id":"W1981463230","doi":"10.1115/gt2011-45147","title":"Combustion Emission Measurements With Preheated Jet Fuel","year":2011,"lang":"en","type":"article","venue":"Volume 2: Combustion, Fuels and Emissions, Parts A and B","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"National Research Council Canada","funders":"Government of Canada","keywords":"Combustor; Combustion; NOx; Nuclear engineering; Environmental science; Fuel injection; Jet fuel; Automotive engineering; Materials science; Waste management; Engineering; Chemistry","score_opus":0.03726421303210073,"score_gpt":0.2270957369014316,"score_spread":0.18983152386933086,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1981463230","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":[0.9865499,0.00088975416,0.0066855154,0.0004527881,0.00011179306,0.0005026135,0.0000093078315,0.00037248808,0.0044257995],"genre_scores_gemma":[0.9936608,0.0005686224,0.0039759735,0.00009436186,0.00001502762,0.000028603026,0.000013514556,0.000018473738,0.0016245926],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.99863297,0.000054234002,0.00024408048,0.00046312693,0.00028190148,0.0003236755],"domain_scores_gemma":[0.99933213,0.000019827738,0.000105476,0.00025711977,0.00003145507,0.00025398322],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020482569,0.00025089775,0.0002206769,0.000055489418,0.000459135,0.000041295567,0.00012835996,0.00015003924,0.00074648875],"category_scores_gemma":[0.00004503178,0.00017300503,0.000026505097,0.00022014166,0.00034911121,0.0003455422,0.000145378,0.00016902019,0.00003018599],"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":[0.00022700061,0.00027890678,0.9384208,0.000071991424,0.000027796166,0.000017073968,0.0008311476,0.00004480073,0.014444748,0.00010746604,0.009720682,0.03580761],"study_design_scores_gemma":[0.004076305,0.001989836,0.87773573,0.00088196166,0.00026725407,0.0002611664,0.0018707259,0.0022113232,0.03481468,0.015800394,0.05820913,0.001881487],"about_ca_topic_score_codex":0.000126048,"about_ca_topic_score_gemma":0.000027293176,"teacher_disagreement_score":0.060685042,"about_ca_system_score_codex":0.00003961571,"about_ca_system_score_gemma":0.000012629288,"threshold_uncertainty_score":0.81735283},"labels":[],"label_agreement":null},{"id":"W1990802887","doi":"10.1021/es8013985","title":"Particle and Gaseous Emissions from Commercial Aircraft at Each Stage of the Landing and Takeoff Cycle","year":2008,"lang":"en","type":"article","venue":"Environmental Science & Technology","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":103,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"Queensland Airports Limited","keywords":"Range (aeronautics); Takeoff; Environmental science; Airframe; Particle number; Thrust; NOx; Particle (ecology); Propulsion; Aerospace engineering; Atmospheric sciences; Engineering; Physics; Combustion; Chemistry; Geology; Plasma","score_opus":0.010614009135074832,"score_gpt":0.21510298929005336,"score_spread":0.20448898015497854,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1990802887","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":[0.99802876,0.00020814381,0.00025073154,0.00081056665,0.000039136674,0.00017709791,0.00002697421,0.000096927506,0.0003616946],"genre_scores_gemma":[0.9979771,0.00018584875,0.0012488193,0.000076597586,0.00000446204,0.000012339384,8.7710697e-7,0.000008474118,0.00048548702],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.99868256,0.000019996143,0.00017667787,0.00044896977,0.00030116356,0.0003706629],"domain_scores_gemma":[0.99936306,0.000045057768,0.000093694194,0.0004087111,0.0000010917843,0.00008837319],"candidate_categories":["sts"],"consensus_categories":[],"category_scores_codex":[0.000119893026,0.00014196832,0.00015620382,0.000058073776,0.0008963267,0.000007547167,0.0004859526,0.00011050407,0.00035599896],"category_scores_gemma":[0.00006529376,0.0001041792,0.000024336454,0.0004608303,0.008429033,0.00020280399,0.0016910592,0.00018652345,0.000031593852],"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":[0.0000048964966,0.000038474616,0.56799877,5.9492834e-7,0.0000015177836,0.0000076260453,0.00016318426,0.00005400267,0.4266692,0.00007752312,0.000021307962,0.004962876],"study_design_scores_gemma":[0.00033779073,0.00009447321,0.64176494,0.000007866708,0.000007102107,0.000077944766,0.00059159665,0.00074208766,0.3513028,0.0016404851,0.0032578502,0.00017507275],"about_ca_topic_score_codex":0.00008145552,"about_ca_topic_score_gemma":0.000061009676,"teacher_disagreement_score":0.07536639,"about_ca_system_score_codex":0.00019072146,"about_ca_system_score_gemma":0.000007665596,"threshold_uncertainty_score":0.99426943},"labels":[],"label_agreement":null},{"id":"W2001711553","doi":"10.1109/tasc.2013.2239471","title":"Development of a 3D Sizing Model for All-Superconducting Machines for Turbo-Electric Aircraft Propulsion","year":2013,"lang":"en","type":"article","venue":"IEEE Transactions on Applied Superconductivity","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":42,"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":"Sizing; Propulsion; Electrically powered spacecraft propulsion; Computer science; Automotive engineering; Aerospace engineering; Electromagnetic coil; Electrical engineering; Engineering","score_opus":0.03775775070770925,"score_gpt":0.25974320984032023,"score_spread":0.22198545913261097,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2001711553","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":[0.45978603,0.000008207181,0.53828526,0.00010503248,0.00007435517,0.0014719092,0.000012961661,0.00016174921,0.00009449202],"genre_scores_gemma":[0.6804028,0.000005078116,0.31764686,0.000047841422,0.0000103382,0.0017289307,0.0000038571434,0.00003763971,0.0001166618],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99807787,0.000018551998,0.00044341446,0.0006637086,0.0002603228,0.0005361567],"domain_scores_gemma":[0.9992499,0.00017949013,0.000084049105,0.00036035472,0.00003605194,0.00009020109],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00025990326,0.00034332473,0.0003786295,0.00014732464,0.0004563494,0.000025981726,0.00029017078,0.00020510243,0.00014466279],"category_scores_gemma":[0.000020531685,0.00030612876,0.00013648886,0.00030811073,0.0001534878,0.0006820179,0.000008702271,0.00027989183,0.000038585033],"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":[0.000041833,0.00024246039,0.000006464323,0.000049659026,0.000027984861,8.2471466e-8,0.0006369185,0.013644833,0.74283224,0.0000610716,0.000026318019,0.2424301],"study_design_scores_gemma":[0.00075525104,0.000093445626,0.00003847214,0.000017830469,0.00004370768,0.0000036532977,0.0004679661,0.13380237,0.8580601,0.0061425325,0.0001405626,0.00043411128],"about_ca_topic_score_codex":0.00005917544,"about_ca_topic_score_gemma":0.00007612986,"teacher_disagreement_score":0.24199599,"about_ca_system_score_codex":0.00024552195,"about_ca_system_score_gemma":0.0000442812,"threshold_uncertainty_score":0.9999391},"labels":[],"label_agreement":null},{"id":"W2005871329","doi":"10.1109/pes.2011.6039111","title":"A micro-turbine model for system studies incorporating validated thermodynamic data","year":2011,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Turbine; Transient (computer programming); Computer science; Transfer function; Steam turbine; Controller (irrigation); Electric power system; Control engineering; Experimental data; Modelica; Power (physics); Engineering; Simulation; Mechanical engineering","score_opus":0.1375930991017182,"score_gpt":0.29354122902091045,"score_spread":0.15594812991919224,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2005871329","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.13057892,0.00015290413,0.8599066,0.00007864613,0.00007410954,0.00066392345,0.00006721612,0.0009392339,0.0075384076],"genre_scores_gemma":[0.76444656,0.000008079137,0.23484032,0.000039761966,0.0000047258222,0.000041102874,0.00001762355,0.000013200971,0.00058864424],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991221,0.000012074485,0.000188811,0.00038144007,0.00009158417,0.00020403304],"domain_scores_gemma":[0.9991898,0.00003268121,0.00009010211,0.00065095944,0.000010579344,0.000025872745],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017263302,0.00013562133,0.00016355004,0.00002238058,0.00012250019,0.000008768233,0.0006334971,0.00005500168,0.000027172286],"category_scores_gemma":[0.00005100377,0.00009723699,0.000023131573,0.00011928275,0.00017883358,0.00031032405,0.00073176826,0.000057899546,0.000054991902],"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":[0.00025440133,0.00042116642,0.008150923,0.0003855371,0.0003975277,0.000046727342,0.0036950307,0.011569795,0.8701051,0.046655986,0.009204967,0.04911285],"study_design_scores_gemma":[0.00028407775,0.000048455226,0.00010510899,0.00002362149,0.000023749182,0.000006620331,0.0016425652,0.9674286,0.012758688,0.017432626,0.000036009602,0.00020984873],"about_ca_topic_score_codex":0.000043145785,"about_ca_topic_score_gemma":0.00006754772,"teacher_disagreement_score":0.9558588,"about_ca_system_score_codex":0.00009607236,"about_ca_system_score_gemma":0.0000054699353,"threshold_uncertainty_score":0.39652094},"labels":[],"label_agreement":null},{"id":"W2013093995","doi":"10.2514/1.c033101","title":"Spatial Simulation of Contrail Formation in Near-Field of Commercial Aircraft","year":2015,"lang":"en","type":"article","venue":"Journal of Aircraft","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":36,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure","funders":"","keywords":"Relative humidity; Environmental science; Mechanics; Meteorology; Condensation; Plume; Atmospheric sciences; Particle (ecology); Water vapor; Computational fluid dynamics; RADIUS; Reynolds number; Wake; Physics; Turbulence; Geology","score_opus":0.023331493209722026,"score_gpt":0.2791155848704748,"score_spread":0.2557840916607528,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2013093995","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":[0.8394262,0.000063486244,0.15882365,0.0006350659,0.0001580828,0.00013562116,0.0000028494744,0.0000138677615,0.00074116455],"genre_scores_gemma":[0.99281216,0.000014893389,0.00704505,0.00007353193,0.000030660758,9.798923e-7,8.184608e-7,0.000006869754,0.000015015637],"study_design_codex":"simulation_or_modeling","study_design_gemma":"observational","domain_scores_codex":[0.99859214,0.000054798304,0.0007004568,0.00007899487,0.00042378026,0.00014984173],"domain_scores_gemma":[0.99899185,0.00016021768,0.00057403714,0.00013780291,0.000072826304,0.00006328529],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00042678465,0.00009885606,0.0003038374,0.00010426616,0.000022558417,0.000007409936,0.00023078866,0.00011324379,0.000088404326],"category_scores_gemma":[0.0004840288,0.00008521018,0.00008421386,0.00023055739,0.00015218006,0.00059819914,0.00006735267,0.00020789077,0.000009185225],"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":[0.0011798954,0.00057889614,0.15830153,0.00005466966,0.000033298158,0.000058318714,0.0030079212,0.523407,0.029038273,0.00012494213,0.0027805304,0.2814347],"study_design_scores_gemma":[0.017096622,0.008590971,0.3676844,0.0006528648,0.00015819375,0.00022615916,0.0033420227,0.20513104,0.34449974,0.030332733,0.021205164,0.0010800919],"about_ca_topic_score_codex":0.00017258033,"about_ca_topic_score_gemma":0.00021052605,"teacher_disagreement_score":0.318276,"about_ca_system_score_codex":0.00011623867,"about_ca_system_score_gemma":0.00003334519,"threshold_uncertainty_score":0.34747702},"labels":[],"label_agreement":null},{"id":"W2015572265","doi":"10.5194/acpd-9-22337-2009","title":"Parametric studies of contrail ice particle formation in jet regime using one-dimensional microphysical modeling","year":2009,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Transport Canada; National Aeronautics and Space Administration","keywords":"Relative humidity; Cloud condensation nuclei; Ice nucleus; Water vapor; Soot; Cirrus; Atmospheric sciences; Condensation; Particle (ecology); Plume; Environmental science; Ice crystals; Jet (fluid); Meteorology; Aerosol; Nucleation; Chemistry; Combustion; Mechanics; Physics; Thermodynamics; Geology","score_opus":0.0688426887521882,"score_gpt":0.29555426357258047,"score_spread":0.22671157482039228,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2015572265","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":[0.97214687,0.00012871937,0.027179845,0.00023521857,0.000009233197,0.00010378772,4.7352688e-7,0.000046687168,0.00014916937],"genre_scores_gemma":[0.9705449,0.000021735565,0.029306592,0.000104051665,0.0000035227185,0.0000019474855,3.848325e-7,0.000002675131,0.000014241494],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99930066,0.000017976949,0.00021255756,0.00013960227,0.00015847871,0.00017073998],"domain_scores_gemma":[0.9997508,0.000055779183,0.000051395582,0.00011204426,0.000010622515,0.000019371311],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000092368304,0.0000757227,0.00015624562,0.000041797906,0.000041017298,0.0000045214115,0.000079830854,0.000036056277,0.00001656164],"category_scores_gemma":[0.000089691195,0.00006177739,0.000026623295,0.00039497673,0.000097224554,0.0003264814,0.000050130096,0.000059283542,0.000013661935],"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":[0.000032728876,0.00018260494,0.00088427047,0.000004630751,0.0000058603046,0.0000043789105,0.00015577555,0.2526589,0.7331153,0.0011937977,0.000028348757,0.01173338],"study_design_scores_gemma":[0.00037731932,0.00009979337,0.0011549537,0.000023933057,0.000007634107,0.0000039877245,0.0003307033,0.75758684,0.21793666,0.02235865,0.000005276338,0.00011424051],"about_ca_topic_score_codex":0.000045583463,"about_ca_topic_score_gemma":0.000018052891,"teacher_disagreement_score":0.5151787,"about_ca_system_score_codex":0.00009783139,"about_ca_system_score_gemma":0.0000025490065,"threshold_uncertainty_score":0.25192088},"labels":[],"label_agreement":null},{"id":"W2027733713","doi":"10.4271/2013-01-2318","title":"Design of a Human-Powered Aircraft Applying Multidisciplinary Optimization Method","year":2013,"lang":"en","type":"article","venue":"SAE technical papers on CD-ROM/SAE technical paper series","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Bombardier (Canada)","funders":"Massachusetts Institute of Technology","keywords":"Multidisciplinary design optimization; Multidisciplinary approach; Computer science; Aeronautics; Aerospace engineering; Engineering","score_opus":0.020649442597937,"score_gpt":0.27901700563853443,"score_spread":0.25836756304059744,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2027733713","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":[0.54288816,0.0019855176,0.08251381,0.016917827,0.0013490544,0.040955845,0.00022146638,0.042729,0.27043933],"genre_scores_gemma":[0.69958574,0.00012826377,0.2984543,0.00028838788,0.000023539482,0.0010694276,0.000019105712,0.00009144432,0.00033974778],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.99511975,0.00027872706,0.0012225278,0.001402521,0.0009773673,0.0009991294],"domain_scores_gemma":[0.99699813,0.00064759114,0.00042813685,0.0015776855,0.000059227128,0.0002892429],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0007585069,0.0007963184,0.0009779881,0.00021294197,0.000553589,0.0000695642,0.0014855936,0.0008992046,0.0032483838],"category_scores_gemma":[0.000588499,0.00067744375,0.00033982666,0.0011116253,0.0018194423,0.0010043579,0.0011825741,0.0010195731,0.00032195388],"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":[0.00011150715,0.00042142282,0.00028594423,0.00002654644,0.000026186937,0.00001979804,0.000042581676,0.012408189,0.9735718,0.0015116853,0.0009227171,0.010651631],"study_design_scores_gemma":[0.001403888,0.0029496138,0.96214056,0.00025200468,0.00011115648,0.00009406501,0.0005302943,0.000038272323,0.005015935,0.023641406,0.0022566735,0.0015661466],"about_ca_topic_score_codex":0.000105496074,"about_ca_topic_score_gemma":0.0026706385,"teacher_disagreement_score":0.96855587,"about_ca_system_score_codex":0.0003953456,"about_ca_system_score_gemma":0.000032480617,"threshold_uncertainty_score":0.9995677},"labels":[],"label_agreement":null},{"id":"W2030069513","doi":"10.2514/6.2013-4372","title":"Aerostructural design optimization of a 100-passenger regional jet with surrogate-based mission analysis","year":2013,"lang":"en","type":"article","venue":"2013 Aviation Technology, Integration, and Operations Conference","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":24,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto","funders":"University of Toronto; Government of Ontario; Compute Canada","keywords":"Surrogate model; Aerospace engineering; Computer science; Jet (fluid); Systems engineering; Engineering","score_opus":0.018457472266544192,"score_gpt":0.23387145575608295,"score_spread":0.21541398348953877,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2030069513","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.13354129,0.000032306332,0.8621052,0.003511199,0.000017056067,0.000511383,0.000006921561,0.00018953162,0.00008511207],"genre_scores_gemma":[0.77787787,0.00006258724,0.22161527,0.00005825297,0.0000037838606,0.000103703445,0.00008628244,0.000008136074,0.00018410989],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9988048,0.000075877746,0.00034574335,0.00037977236,0.00021558032,0.00017823835],"domain_scores_gemma":[0.9991095,0.00006076067,0.00015846429,0.00032943688,0.00029015762,0.000051659998],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00013463618,0.00020873376,0.00024237821,0.00039197868,0.00027057162,0.00008325503,0.0002114008,0.00022653826,0.0012574621],"category_scores_gemma":[0.0001118468,0.00015010833,0.000038568636,0.0012966943,0.0005819021,0.0006727783,0.000040578383,0.0001654733,0.000028160483],"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":[0.000048567927,0.00019582803,0.107815124,0.000012687075,0.00015046258,0.0000012672471,0.00044718408,0.7693038,0.07874445,0.02102093,0.0014407941,0.020818904],"study_design_scores_gemma":[0.00056944037,0.00031430306,0.02578182,0.000035727116,0.00013071686,0.0000063899497,0.0008154913,0.9156055,0.051816702,0.0044771046,0.00009536681,0.00035142526],"about_ca_topic_score_codex":0.0005212488,"about_ca_topic_score_gemma":0.00065941777,"teacher_disagreement_score":0.6443366,"about_ca_system_score_codex":0.00006522323,"about_ca_system_score_gemma":0.000053983036,"threshold_uncertainty_score":0.99965554},"labels":[],"label_agreement":null},{"id":"W2032175094","doi":"10.1115/imece2013-64102","title":"Dynamic Performance Simulation of an Aeroderivative Gas Turbine Using the Matlab Simulink Environment","year":2013,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":44,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Concordia University","funders":"Qatar National Research Fund; Qatar Foundation","keywords":"Prime mover; Computer science; MATLAB; Turbine; Fault (geology); Automotive engineering; Simulation; Control engineering; Engineering; Mechanical engineering","score_opus":0.014096208212968147,"score_gpt":0.23743761003416972,"score_spread":0.22334140182120157,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2032175094","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":[0.90599525,0.000009509021,0.09296181,0.00013268228,0.000014591612,0.0003042351,8.9434826e-7,0.000063584324,0.0005174379],"genre_scores_gemma":[0.9747252,0.000020528469,0.024942527,0.0000685944,0.0000036238048,0.0000115540715,0.000002753864,0.000009857554,0.00021534793],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999234,0.000025092591,0.00017536248,0.00019761143,0.00019155217,0.00017637086],"domain_scores_gemma":[0.9994863,0.000058323574,0.0000914706,0.00033100514,0.0000052720557,0.000027583837],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00007861247,0.00011581494,0.0000999086,0.000018504521,0.00011140337,0.000011824974,0.00022887868,0.000050502375,0.001719049],"category_scores_gemma":[0.000015171421,0.00007243902,0.000022920549,0.00011300693,0.000313701,0.0005085253,0.00014757508,0.00008884449,0.00015994791],"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":[0.000004618563,0.000034595978,0.0022825873,0.000002551241,0.0000033160509,2.2854886e-7,0.00011074089,0.9094594,0.05523275,0.000015067343,0.000004219656,0.03284991],"study_design_scores_gemma":[0.00011708699,0.00009222063,0.019021058,0.0000043538016,0.0000046365294,0.0000011486123,0.00023872784,0.9622848,0.016489098,0.0015226358,0.000120367564,0.00010385279],"about_ca_topic_score_codex":0.00008297996,"about_ca_topic_score_gemma":0.000005596749,"teacher_disagreement_score":0.06872996,"about_ca_system_score_codex":0.00010577166,"about_ca_system_score_gemma":0.0000022522029,"threshold_uncertainty_score":0.9991935},"labels":[],"label_agreement":null},{"id":"W2032431806","doi":"10.1115/imece2014-36903","title":"Multi-Disciplinary Design Optimization of Transonic Fan Blade Design Using Analytical Target Cascading","year":2014,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Transonic; Aerodynamics; Multidisciplinary design optimization; Aeroelasticity; Rotor (electric); Computer science; Blade (archaeology); Design process; Aerospace engineering; Engineering design process; Engineering; Process (computing); Systems engineering; Multidisciplinary approach; Mechanical engineering; Work in process","score_opus":0.058554332083584563,"score_gpt":0.2865238360469726,"score_spread":0.22796950396338805,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2032431806","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":[0.0085303215,0.000020528692,0.9904188,0.000065269225,0.00002640495,0.0002549474,9.0313284e-7,0.00016293894,0.0005198658],"genre_scores_gemma":[0.47288463,0.000006133131,0.52698964,0.000016099477,0.000004577556,0.0000035864177,7.218635e-7,0.00001093146,0.00008368035],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99879533,0.0001180842,0.00026427556,0.00032395887,0.00019778896,0.00030056608],"domain_scores_gemma":[0.9994546,0.00015214153,0.00007670571,0.0002395836,0.000008094177,0.000068845366],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00039328245,0.00016043513,0.00021049754,0.000071886265,0.00012894634,0.000012878847,0.00024848853,0.00012301306,0.0005639534],"category_scores_gemma":[0.00009645924,0.00013575784,0.00005996386,0.00033494565,0.00028577697,0.000270088,0.00008719217,0.000112448164,0.000023264927],"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":[0.000018570643,0.000057344936,0.0007074435,0.0000044801463,0.000007199607,0.0000025668808,0.000085063584,0.95762944,0.03964194,0.00012157383,0.000028524968,0.001695853],"study_design_scores_gemma":[0.00028782923,0.00012740276,0.00038479725,0.000012363714,0.000019828592,0.000007660907,0.0000961691,0.9496687,0.04776858,0.0014324469,0.000019208393,0.00017499698],"about_ca_topic_score_codex":0.000029616336,"about_ca_topic_score_gemma":0.0000024742606,"teacher_disagreement_score":0.4643543,"about_ca_system_score_codex":0.000110248846,"about_ca_system_score_gemma":0.000010273719,"threshold_uncertainty_score":0.6174894},"labels":[],"label_agreement":null},{"id":"W2037594083","doi":"10.1016/j.fuel.2014.12.021","title":"Impact of alternative jet fuels on aircraft-induced aerosols","year":2014,"lang":"en","type":"article","venue":"Fuel","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":46,"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":"Jet fuel; Jet (fluid); Environmental science; Aerospace engineering; Alternative fuels; Mechanics; Physics; Chemistry; Combustion; Engineering; Organic chemistry","score_opus":0.020555260239693236,"score_gpt":0.27520225131454173,"score_spread":0.2546469910748485,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2037594083","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":[0.9687609,0.0000073430115,0.0034577006,0.000073022406,0.000076433105,0.00014402976,0.000008923371,0.00011632352,0.02735534],"genre_scores_gemma":[0.9982784,0.000010645329,0.0013977501,0.000082309474,0.000025879403,0.0000118265025,0.0000019266845,0.000012664833,0.0001786168],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.9991282,0.000032199987,0.00014507404,0.00024729926,0.00021310241,0.00023408141],"domain_scores_gemma":[0.9994026,0.00009066045,0.00009402506,0.00035105224,0.0000061387364,0.000055559613],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000099764744,0.00014552992,0.00017557379,0.00003481587,0.00003744346,0.000007806813,0.00029956672,0.00007094207,0.0005333516],"category_scores_gemma":[0.0001305104,0.00010590914,0.00009457901,0.0001535816,0.00013771774,0.00013015272,0.00011213141,0.00012723471,0.00053508324],"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":[0.00014921,0.0005322863,0.20463009,0.000025874271,0.0000834432,0.000016257156,0.0006849329,0.00327286,0.66557556,0.0037300305,0.0032937124,0.11800576],"study_design_scores_gemma":[0.0016913268,0.00397751,0.53809506,0.000072274706,0.000021131784,0.000009914406,0.000108922206,0.0014445019,0.34338716,0.1079076,0.0025110566,0.00077354966],"about_ca_topic_score_codex":0.0001476902,"about_ca_topic_score_gemma":0.000015871097,"teacher_disagreement_score":0.33346498,"about_ca_system_score_codex":0.000116060124,"about_ca_system_score_gemma":0.000005255412,"threshold_uncertainty_score":0.6877591},"labels":[],"label_agreement":null},{"id":"W2056040929","doi":"10.1115/detc2003/dac-48801","title":"Optimization of Helicopter Air Intake Scoop Design","year":2003,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Manitoba","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Finite element method; SCOOP; Icing; Shape optimization; Penalty method; Computational fluid dynamics; Computer science; Multidisciplinary design optimization; Mechanical engineering; Thermal conduction; Engineering; Structural engineering; Mathematical optimization; Aerospace engineering; Materials science; Mathematics; Multidisciplinary approach","score_opus":0.018469671109855125,"score_gpt":0.22301277190234423,"score_spread":0.2045431007924891,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2056040929","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0045947838,0.000013599013,0.9484626,0.000058946924,0.000024396732,0.0001172064,2.3659099e-7,0.00010296589,0.04662528],"genre_scores_gemma":[0.6267252,0.000015753223,0.3721148,0.00010350005,0.000001170201,0.000005993824,3.4212084e-7,0.0000047048147,0.001028536],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9995262,0.00002323594,0.00010808597,0.00013224075,0.00009630202,0.000113909184],"domain_scores_gemma":[0.9997571,0.0000252955,0.000035313893,0.00015700253,0.000004198693,0.000021090833],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00009075555,0.00006495929,0.000070623,0.00002189653,0.000029257035,0.0000027777469,0.000099026016,0.000045879657,0.0031164053],"category_scores_gemma":[0.0000641049,0.000052083335,0.000018331217,0.00017604628,0.000120888944,0.0001337564,0.00003165206,0.000037720507,0.00015301233],"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":[0.000011218196,0.00008355442,0.005411582,0.000003934295,0.0000058105575,0.0000025731902,0.00005333119,0.95163834,0.020725658,0.0060024397,0.0016703831,0.014391186],"study_design_scores_gemma":[0.0005108006,0.00023894037,0.0014930797,0.000012930101,0.000009800269,0.000009534493,0.00022412433,0.017314347,0.958661,0.013989632,0.0072022323,0.00033356284],"about_ca_topic_score_codex":0.00000897269,"about_ca_topic_score_gemma":0.00000204754,"teacher_disagreement_score":0.93793535,"about_ca_system_score_codex":0.000028668095,"about_ca_system_score_gemma":0.0000034971654,"threshold_uncertainty_score":0.99779487},"labels":[],"label_agreement":null},{"id":"W2056278127","doi":"10.1016/j.ast.2015.02.011","title":"Wing weight model for conceptual design of nonplanar configurations","year":2015,"lang":"en","type":"article","venue":"Aerospace Science and Technology","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":29,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Royal Military College of Canada","funders":"","keywords":"Wing; Conceptual design; Conceptual model; Structural engineering; Engineering; Aerospace engineering; Computer science; Mechanical engineering","score_opus":0.041001582996670616,"score_gpt":0.2626446532393725,"score_spread":0.2216430702427019,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2056278127","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":[0.11854235,0.00017623043,0.87529814,0.0037986676,0.000073052535,0.0005654706,0.000008746552,0.0002988854,0.0012384309],"genre_scores_gemma":[0.90174496,0.000025399351,0.0978892,0.0000687562,0.0000034326472,0.000047617967,5.5400017e-7,0.000005776166,0.00021433341],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989536,0.0000063138978,0.00013895657,0.00034060128,0.00024509183,0.00031544574],"domain_scores_gemma":[0.99944824,0.00005092783,0.000081748796,0.00025998906,0.00008620293,0.00007288003],"candidate_categories":["sts"],"consensus_categories":[],"category_scores_codex":[0.00036919236,0.00010502292,0.00015274178,0.00013386225,0.00020081853,0.000013138954,0.00041610817,0.00011897692,0.000008849487],"category_scores_gemma":[0.00050648424,0.000090176865,0.000012360449,0.00090352184,0.0049858345,0.00036507542,0.00017608948,0.0000892236,0.000011889982],"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":[0.000029462453,0.00006590826,0.0044726427,0.000004575197,0.000007404181,0.0000031097215,0.0010278058,0.012139417,0.816544,0.14367193,0.0039290455,0.018104685],"study_design_scores_gemma":[0.001252514,0.0008189345,0.00016107746,0.000019148965,0.00002343931,0.00003590855,0.0051213778,0.42795083,0.37532893,0.18511195,0.003718657,0.0004572087],"about_ca_topic_score_codex":0.000009149462,"about_ca_topic_score_gemma":0.000009545513,"teacher_disagreement_score":0.7832026,"about_ca_system_score_codex":0.000071740906,"about_ca_system_score_gemma":0.000101648155,"threshold_uncertainty_score":0.997722},"labels":[],"label_agreement":null},{"id":"W2056289206","doi":"10.2514/6.2008-4579","title":"A Modular Aero-Propulsion System Simulation of a Large Commercial Aircraft Engine","year":2008,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":107,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Impact","funders":"Glenn Research Center; National Aeronautics and Space Administration","keywords":"Propulsion; Modular design; Aerospace engineering; Computer science; Automotive engineering; Aeronautics; Aero engine; Engineering; Mechanical engineering; Operating system","score_opus":0.01534575206731906,"score_gpt":0.23942071518331315,"score_spread":0.2240749631159941,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2056289206","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":[0.7066651,0.000020331758,0.29033193,0.00006567713,0.0000463525,0.00019683475,0.0000042427764,0.0003077287,0.002361803],"genre_scores_gemma":[0.9874773,0.000007878908,0.012131493,0.000035822603,0.000012632366,0.000008689579,0.000004002971,0.00000994058,0.0003122098],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991704,0.000021602023,0.00019641928,0.0001885752,0.00022948335,0.00019350475],"domain_scores_gemma":[0.999616,0.00003191767,0.000061101055,0.00024686623,0.000008825085,0.0000352671],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000085047206,0.0001046584,0.00015673204,0.00003791432,0.00011547881,0.0000021470833,0.00015351073,0.000083285544,0.00024774513],"category_scores_gemma":[0.00003339947,0.0000853397,0.000048260838,0.00021677624,0.00010988629,0.00016220391,0.00012671234,0.000077125274,0.00014106982],"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":[0.0001225237,0.0005875022,0.10202427,0.00010271139,0.00002887298,0.00010215192,0.00065452454,0.68506116,0.16218059,0.0030024892,0.0012037553,0.044929434],"study_design_scores_gemma":[0.0016358788,0.00033387128,0.13433036,0.00005979441,0.000020529083,0.00004163167,0.00043049274,0.79243547,0.062324863,0.0008307706,0.0070319227,0.00052441703],"about_ca_topic_score_codex":0.000053155574,"about_ca_topic_score_gemma":0.000014121207,"teacher_disagreement_score":0.28081223,"about_ca_system_score_codex":0.000087060725,"about_ca_system_score_gemma":0.0000029521573,"threshold_uncertainty_score":0.3480052},"labels":[],"label_agreement":null},{"id":"W2058401863","doi":"10.1016/j.ijhydene.2009.11.047","title":"Partial substitution of hydrogen for conventional fuel in an aircraft by utilizing unused cargo compartment space","year":2009,"lang":"en","type":"article","venue":"International Journal of Hydrogen Energy","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":25,"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 Ontario Institute of Technology","funders":"","keywords":"Aircraft fuel system; Tonne; Environmental science; Hydrogen storage; Aviation; Range (aeronautics); Volume (thermodynamics); Aviation fuel; Propulsion; Fuel efficiency; Aerospace engineering; Automotive engineering; Hydrogen; Aeronautics; Waste management; Engineering; Chemistry; Physics; Combustion","score_opus":0.018898690095187763,"score_gpt":0.2734520449661658,"score_spread":0.2545533548709781,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2058401863","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":[0.97611666,0.00037082555,0.022172444,0.00065986277,0.00023405591,0.000091416216,0.00002959835,0.000021205726,0.00030392612],"genre_scores_gemma":[0.99721426,0.00007573952,0.0024226245,0.00012664786,0.00006443984,0.0000053354856,0.000031888878,0.000007865863,0.000051229716],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9985605,0.000039551964,0.0005210555,0.00017786585,0.0005096186,0.00019144741],"domain_scores_gemma":[0.9993418,0.000041935964,0.00037100274,0.00010577985,0.00006522325,0.00007428142],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002135926,0.00013170489,0.00021601545,0.00013215384,0.000029967103,0.000014326619,0.00044896506,0.000071196715,0.00009683346],"category_scores_gemma":[0.000037388287,0.00012440856,0.00013426636,0.00011497159,0.00013418621,0.00041303708,0.000041339885,0.00009065468,0.0000034159727],"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":[0.0009422229,0.001668419,0.02684729,0.0000075404123,0.00020524845,0.00014161167,0.00021538029,0.1338242,0.77121615,0.048218455,0.0013173026,0.015396192],"study_design_scores_gemma":[0.0037640096,0.0009875225,0.0035531428,0.00008004662,0.00004127895,0.0001518861,0.00015505712,0.019051805,0.88561165,0.03943813,0.046804372,0.00036107094],"about_ca_topic_score_codex":0.00004858115,"about_ca_topic_score_gemma":0.00007768634,"teacher_disagreement_score":0.11477239,"about_ca_system_score_codex":0.00026140423,"about_ca_system_score_gemma":0.000031392865,"threshold_uncertainty_score":0.5073234},"labels":[],"label_agreement":null},{"id":"W2058654740","doi":"10.1029/2011jd015806","title":"Large eddy simulations of contrail development: Sensitivity to initial and ambient conditions over first twenty minutes","year":2011,"lang":"en","type":"article","venue":"Journal of Geophysical Research Atmospheres","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":47,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"National Centre for Supercomputing Applications; National Aeronautics and Space Administration; Transport Canada; National Science Foundation","keywords":"Environmental science; Atmospheric sciences; Optical depth; Relative humidity; Humidity; Wind shear; Wind speed; Meteorology; Atmospheric instability; Aerosol; Geology; Physics","score_opus":0.04557043004536678,"score_gpt":0.32374212453646517,"score_spread":0.2781716944910984,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2058654740","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":[0.99487495,0.000025940299,0.0041893953,0.00015131987,0.00003183647,0.00017270978,0.000026234491,0.000012419411,0.0005151953],"genre_scores_gemma":[0.9907869,0.000011693513,0.008993576,0.00003685303,0.000032559976,0.000004569739,0.0000011613644,0.000008382568,0.00012427128],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.998433,0.00010417194,0.00031023208,0.00016682773,0.0006242283,0.00036155115],"domain_scores_gemma":[0.99881953,0.0005959145,0.00012081144,0.00014420022,0.00011719811,0.00020236663],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004298128,0.00010647598,0.00022876184,0.000025450681,0.0002403387,0.00001937188,0.0001699329,0.000057551995,0.00069005333],"category_scores_gemma":[0.00070471235,0.00008575457,0.000058495916,0.0003322985,0.0004850725,0.00030866903,0.0002980449,0.0003077787,0.000041731542],"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":[0.0026801415,0.010538274,0.3129001,0.00020351425,0.00075227534,0.0015004365,0.019440863,0.004648422,0.53763044,0.016428068,0.024067247,0.069210246],"study_design_scores_gemma":[0.0010731232,0.000870337,0.90953785,0.00010706637,0.000017523438,0.000019965162,0.00084744114,0.0011063208,0.06205805,0.017297259,0.0068497215,0.00021531158],"about_ca_topic_score_codex":0.00018355208,"about_ca_topic_score_gemma":0.00069343887,"teacher_disagreement_score":0.5966378,"about_ca_system_score_codex":0.00008948485,"about_ca_system_score_gemma":0.000046463938,"threshold_uncertainty_score":0.75556},"labels":[],"label_agreement":null},{"id":"W2061068909","doi":"10.2514/6.2009-7050","title":"Integrated Analysis and Design Environment for a Climate Compatible Air Transport System","year":2009,"lang":"en","type":"article","venue":"9th AIAA Aviation Technology, Integration, and Operations Conference (ATIO)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":15,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Partenariat Canadien Contre Le Cancer","keywords":"Radiative forcing; Environmental science; Cirrus; Propulsion; Meteorology; Greenhouse gas; Aviation; Air traffic control; Aerospace engineering; Engineering; Aerosol; Geography","score_opus":0.015618470415710841,"score_gpt":0.23355992686908844,"score_spread":0.2179414564533776,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2061068909","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0570799,0.000078581455,0.93884003,0.0021093055,0.000037831145,0.001085344,0.000072345836,0.0005113265,0.00018532194],"genre_scores_gemma":[0.8510864,0.00025713144,0.14775121,0.00010866617,0.000007788753,0.00031992147,0.00023913829,0.000010395916,0.00021939471],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99831724,0.000066453715,0.0005280813,0.00059739465,0.00018150582,0.0003092987],"domain_scores_gemma":[0.99927366,0.00005939606,0.00014405297,0.00034939282,0.00009847496,0.000075055],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00036138052,0.00029753428,0.00037683392,0.0004800011,0.00067190494,0.00008313577,0.00021979447,0.00028530575,0.00011678031],"category_scores_gemma":[0.00008271061,0.00025782431,0.00006173101,0.0009750438,0.00039070714,0.0005812395,0.000031802938,0.00020273028,0.000023153034],"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":[0.00015838828,0.0005564654,0.089230694,0.00006988452,0.0003634755,0.000006942119,0.0026984373,0.038061026,0.059158716,0.40864226,0.0005398379,0.4005139],"study_design_scores_gemma":[0.0025931718,0.0018024037,0.18320122,0.00015044304,0.0010539033,0.00003857921,0.00977445,0.7022272,0.06474019,0.028764728,0.0040134946,0.0016402357],"about_ca_topic_score_codex":0.0001098317,"about_ca_topic_score_gemma":0.0006007293,"teacher_disagreement_score":0.79400647,"about_ca_system_score_codex":0.00017694656,"about_ca_system_score_gemma":0.000034943176,"threshold_uncertainty_score":0.9999874},"labels":[],"label_agreement":null},{"id":"W2061299639","doi":"10.1115/imece2014-36676","title":"Conceptual Design of a 200 Passenger Blended Wing Body Aircraft","year":2014,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Polytechnique Montréal","funders":"Fondation J. Armand Bombardier; Pratt and Whitney Canada","keywords":"Aerodynamics; Conceptual design; Payload (computing); Wing; Aerospace engineering; Automotive engineering; Airplane; Engineering; Aeronautics; Range (aeronautics); Longitudinal static stability; Computer science; Systems engineering; Mechanical engineering","score_opus":0.017137145382098148,"score_gpt":0.22843194140468057,"score_spread":0.21129479602258242,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2061299639","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.04807193,0.000026303762,0.9292006,0.00033429047,0.000064876425,0.00023674223,0.0000011464964,0.00036828654,0.021695858],"genre_scores_gemma":[0.91843015,0.000010976637,0.07993088,0.00015023103,0.000012294225,0.000012296966,6.756192e-7,0.000011083822,0.0014414084],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9990285,0.000056739565,0.00018902277,0.0002533182,0.00020906724,0.00026336202],"domain_scores_gemma":[0.9994331,0.00015814633,0.00006257472,0.00029012858,0.000006434416,0.000049608945],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00020140506,0.0001274145,0.00017051752,0.00002922324,0.000057617606,0.0000065253917,0.00025497784,0.00008345031,0.0019487682],"category_scores_gemma":[0.00012360924,0.000102943566,0.00004088338,0.00016404735,0.00047157035,0.00017932244,0.00012822785,0.000099884644,0.00033214156],"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":[0.0000611643,0.00022811402,0.018192658,0.000009964683,0.00003641002,0.000012558923,0.00043170922,0.013678569,0.86321867,0.033149146,0.016826456,0.05415458],"study_design_scores_gemma":[0.0026922743,0.0014053248,0.02470476,0.00005917873,0.00006341703,0.000030619478,0.0024548904,0.031639475,0.77176887,0.052258555,0.11142767,0.0014949886],"about_ca_topic_score_codex":0.000030581403,"about_ca_topic_score_gemma":0.00000474473,"teacher_disagreement_score":0.8703582,"about_ca_system_score_codex":0.00003902335,"about_ca_system_score_gemma":0.0000068397276,"threshold_uncertainty_score":0.9989636},"labels":[],"label_agreement":null},{"id":"W2062796339","doi":"10.1115/gt2011-45133","title":"Emissions Assessment of Alternative Aviation Fuel at Simulated Altitudes","year":2011,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":14,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"Communications Security Establishment; Environment and Climate Change Canada; National Research Council Canada","funders":"","keywords":"Jet fuel; Aviation; Environmental science; Diesel fuel; Aviation fuel; Baseline (sea); Renewable energy; Automotive engineering; Engineering; Waste management; Aerospace engineering","score_opus":0.03443010817746492,"score_gpt":0.2900105895633975,"score_spread":0.2555804813859326,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2062796339","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":[0.5815089,0.000022406362,0.12134884,0.00008622764,0.00007515874,0.00029863685,0.000005139127,0.0002810468,0.29637364],"genre_scores_gemma":[0.9713111,0.000021683516,0.026712619,0.00003084529,0.0000020310342,0.0000037035777,0.0000019947345,0.000004506399,0.0019115029],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.9994686,0.000013151293,0.00012479741,0.00014723281,0.00014080858,0.000105357976],"domain_scores_gemma":[0.99970615,0.00002696349,0.00007067285,0.00015818224,0.0000066974876,0.000031335258],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.000051085215,0.00006807327,0.00007814788,0.000021682778,0.00004394458,0.0000017777965,0.00014266424,0.000040229035,0.00482739],"category_scores_gemma":[0.00002401895,0.00005093195,0.000024939955,0.00010430566,0.00011649749,0.00012512966,0.0001786061,0.0000472852,0.000075523676],"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":[0.000029418867,0.000488969,0.7073649,0.000013907373,0.00004764671,0.000013156736,0.0010351881,0.0046435287,0.2453114,0.026922125,0.0006409004,0.013488836],"study_design_scores_gemma":[0.0005088504,0.00022550656,0.661076,0.00001677216,0.000016321943,0.000002334849,0.0002468463,0.016103104,0.2504097,0.070153475,0.0009783447,0.0002627436],"about_ca_topic_score_codex":0.00019175127,"about_ca_topic_score_gemma":0.00004670564,"teacher_disagreement_score":0.38980222,"about_ca_system_score_codex":0.000106479194,"about_ca_system_score_gemma":0.0000031798781,"threshold_uncertainty_score":0.9960823},"labels":[],"label_agreement":null},{"id":"W2068690002","doi":"10.4271/2011-01-2597","title":"Gaseous and Particle Emissions from a Turbo-Jet Engine Operating on Alternative Fuels at Simulated Altitudes","year":2011,"lang":"en","type":"article","venue":"SAE technical papers on CD-ROM/SAE technical paper series","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":11,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"National Research Council Canada; Environment and Climate Change Canada","funders":"National Research Council Canada; U.S. Air Force; Ministère de la Défense Nationale","keywords":"Jet engine; Environmental science; Jet (fluid); Turbo; Aerospace engineering; Jet fuel; Particle (ecology); Nuclear engineering; Automotive engineering; Engineering; Geology","score_opus":0.020927499546410103,"score_gpt":0.2475898853052026,"score_spread":0.2266623857587925,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2068690002","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":[0.979489,0.00020963821,0.000004000881,0.0011435478,0.0000964357,0.00074704393,0.00006934331,0.0021931904,0.016047765],"genre_scores_gemma":[0.98883164,0.0002923999,0.008865717,0.0013633594,0.0000456359,0.0001321756,0.000022252487,0.000085085725,0.0003617507],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.9962843,0.00012395383,0.0007062971,0.001349598,0.00065851235,0.0008773245],"domain_scores_gemma":[0.9976781,0.000596126,0.00018008961,0.0010980926,0.000024100966,0.00042346216],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00027250056,0.0007093029,0.00067566504,0.00007367434,0.0005761821,0.000061084684,0.00084381626,0.0005390809,0.0024735597],"category_scores_gemma":[0.00094905274,0.00054311525,0.00019355839,0.00047880984,0.0013674466,0.0004711682,0.0010887951,0.00093256176,0.0003315543],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":true,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00026774235,0.0004189428,0.0029655418,0.000006820869,0.000036364032,0.00015234842,0.00012722217,0.00017491005,0.98715097,0.0013516028,0.00040002933,0.0069475304],"study_design_scores_gemma":[0.0008821866,0.0016276409,0.96560884,0.00016169388,0.00005575032,0.00003716831,0.00014776962,0.0000037654022,0.017331483,0.00880364,0.0045772432,0.0007628067],"about_ca_topic_score_codex":0.00023832709,"about_ca_topic_score_gemma":0.02079944,"teacher_disagreement_score":0.9698195,"about_ca_system_score_codex":0.0003797364,"about_ca_system_score_gemma":0.00001643103,"threshold_uncertainty_score":0.99970204},"labels":[],"label_agreement":null},{"id":"W2072553263","doi":"10.2495/sdp-v5-n2-150-162","title":"Regional airports' environmental management: key messages from the evaluation of ten European airports","year":2010,"lang":"en","type":"article","venue":"International Journal of Sustainable Development and Planning","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":20,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Business; Aviation; Civil aviation; Scale (ratio); Process (computing); Environmental planning; Environmental resource management; Economics; Engineering; Geography","score_opus":0.016279176741277938,"score_gpt":0.24441200962448537,"score_spread":0.22813283288320743,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2072553263","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":[0.99296767,0.00020870904,0.00079626235,0.0003483513,0.00018120933,0.000111717265,0.0000018736054,0.0000099061945,0.00537431],"genre_scores_gemma":[0.9926866,0.000052554067,0.0066552055,0.00008548614,0.00006487746,0.0000034131565,0.000014668021,0.000007758148,0.00042941523],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.9985436,0.000042370008,0.0003324629,0.00013068813,0.0008138843,0.00013700106],"domain_scores_gemma":[0.99938786,0.000065345135,0.00036567866,0.00008843162,0.000055661687,0.0000370403],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0011387324,0.00010197161,0.000096434145,0.00008343373,0.000118708514,0.000036604917,0.00032623607,0.00003377049,0.00028516745],"category_scores_gemma":[0.00006196351,0.00007365725,0.000032242373,0.000058457113,0.00014737422,0.00033345746,0.00023868436,0.00019642993,0.0000053824365],"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":[0.0001706831,0.00016570865,0.62880194,0.000010586409,0.00044671874,0.0028527973,0.0093407715,0.002797011,0.0030677472,0.0019204746,0.005008826,0.34541672],"study_design_scores_gemma":[0.0006599129,0.000020804482,0.9325908,0.00005764731,0.000043519263,0.00011575387,0.015479956,0.00011313194,0.0021605005,0.0060638064,0.042552866,0.0001413177],"about_ca_topic_score_codex":0.000011181521,"about_ca_topic_score_gemma":0.0000023732932,"teacher_disagreement_score":0.3452754,"about_ca_system_score_codex":0.00009694117,"about_ca_system_score_gemma":0.000024443778,"threshold_uncertainty_score":0.31223834},"labels":[],"label_agreement":null},{"id":"W2073755139","doi":"10.5539/mas.v3n8p82","title":"Virtual Power Extraction Method of Designing Starting Control Law of Turbofan Engine","year":2009,"lang":"en","type":"article","venue":"Modern Applied Science","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"Northwestern Polytechnical University; Northwestern University","keywords":"Turbofan; Extrapolation; Computer science; Flight envelope; Control (management); Envelope (radar); Law; Acceleration; Automotive engineering; Aerospace engineering; Engineering; Aerodynamics; Artificial intelligence; Mathematics; Physics","score_opus":0.009696533463900859,"score_gpt":0.25798122888896596,"score_spread":0.2482846954250651,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2073755139","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.068428315,0.00001161361,0.9219955,0.0000675772,0.000024170236,0.00017855832,0.0000016307464,0.00008664511,0.009205966],"genre_scores_gemma":[0.85708576,0.0000010835348,0.1427757,0.000105889674,0.0000036259794,0.000005162413,1.9372659e-7,0.000004979404,0.000017610166],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99854696,0.000016851465,0.0002743369,0.00035913123,0.00049055053,0.00031219955],"domain_scores_gemma":[0.99935436,0.00009537408,0.00019257242,0.00028368656,0.000016698972,0.000057335215],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0008254033,0.00012153403,0.0001987671,0.00006919087,0.0001472688,0.000013881805,0.00040913903,0.000054963784,0.000053339787],"category_scores_gemma":[0.00006749305,0.000107937056,0.000034059492,0.00046800514,0.0007023112,0.00034075842,0.00006750381,0.00013427706,0.0000088282495],"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":[0.000023356284,0.000039877777,0.00007138084,0.0000010282004,0.0000013527006,7.567268e-7,0.00025639517,0.018706603,0.88811636,0.0075268135,0.000003304721,0.08525279],"study_design_scores_gemma":[0.00029887902,0.0001516316,0.0013252246,0.000007644686,0.000006199286,0.0000023553084,0.00017811422,0.058695342,0.8909932,0.04817763,0.00002995881,0.00013383225],"about_ca_topic_score_codex":0.000018339313,"about_ca_topic_score_gemma":0.000003202264,"teacher_disagreement_score":0.7886574,"about_ca_system_score_codex":0.00007809098,"about_ca_system_score_gemma":0.000015153936,"threshold_uncertainty_score":0.44015452},"labels":[],"label_agreement":null},{"id":"W2073819788","doi":"10.2514/1.c032150","title":"Multipoint High-Fidelity Aerostructural Optimization of a Transport Aircraft Configuration","year":2014,"lang":"en","type":"article","venue":"Journal of Aircraft","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":376,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Government of Ontario; Compute Canada; University of Toronto; National Aeronautics and Space Administration","keywords":"Takeoff; Airfoil; Reduction (mathematics); Aerodynamics; Shape optimization; Finite element method; Engineering; Control theory (sociology); Simulation; Computer science; Mathematics; Structural engineering; Aerospace engineering; Geometry","score_opus":0.008211750830287088,"score_gpt":0.22034966157327027,"score_spread":0.2121379107429832,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2073819788","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":[0.4448176,0.000024045055,0.5538464,0.00054783805,0.00020600313,0.00014273918,0.000004348693,0.00004553112,0.00036548296],"genre_scores_gemma":[0.8885136,0.000033718432,0.11123103,0.000092416805,0.000050714814,0.000002188115,0.000004308141,0.000013110707,0.00005889468],"study_design_codex":"simulation_or_modeling","study_design_gemma":"observational","domain_scores_codex":[0.9983149,0.00006593347,0.00077328307,0.00018139888,0.00045759266,0.00020688541],"domain_scores_gemma":[0.99887013,0.00007593942,0.00063943764,0.00023765869,0.000088574336,0.00008822865],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00043457368,0.00016930138,0.00035821376,0.00008634436,0.000070692724,0.000010350684,0.00030580786,0.00012809662,0.00050575857],"category_scores_gemma":[0.0001968792,0.00013609066,0.00014390815,0.00021878844,0.00026558732,0.0005559071,0.000035040473,0.00024375778,0.0000147471455],"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":[0.00025625288,0.0001740405,0.026154151,0.000039627055,0.000050048136,0.000019626488,0.0003590213,0.77980644,0.15342095,0.00060077873,0.00066626817,0.038452797],"study_design_scores_gemma":[0.0071249935,0.0032107003,0.4626862,0.0003093457,0.00027441594,0.00037412648,0.000679576,0.059197877,0.43691194,0.019632475,0.008321889,0.0012764444],"about_ca_topic_score_codex":0.00006583269,"about_ca_topic_score_gemma":0.00002260014,"teacher_disagreement_score":0.72060853,"about_ca_system_score_codex":0.000107733584,"about_ca_system_score_gemma":0.000021101447,"threshold_uncertainty_score":0.5549616},"labels":[],"label_agreement":null},{"id":"W2079930066","doi":"10.2514/6.2005-2811","title":"Identification of aircraft noise at landing","year":2005,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Bombardier (Canada)","funders":"","keywords":"Identification (biology); Noise (video); Computer science; Aircraft noise; Aeronautics; Aerospace engineering; Acoustics; Engineering; Noise reduction; Artificial intelligence; Physics","score_opus":0.010510144656446318,"score_gpt":0.23516741636106236,"score_spread":0.22465727170461605,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2079930066","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":[0.9268974,0.000028841065,0.04916731,0.0006604074,0.000030774234,0.000101589125,0.0000017231647,0.00020202123,0.022909956],"genre_scores_gemma":[0.98759747,0.000015252226,0.0053419154,0.000042649524,0.000006953421,0.0000044659123,8.520543e-7,0.0000035910286,0.0069868467],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99956363,0.0000046125165,0.00012596331,0.00011492377,0.00010049941,0.00009038723],"domain_scores_gemma":[0.99976635,0.000014641647,0.000045679477,0.00015468046,0.0000020505393,0.000016577093],"candidate_categories":["insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.00006453035,0.000043624288,0.000050587478,0.000018139986,0.0000409723,0.0000030738618,0.00011284982,0.000029590474,0.0013664481],"category_scores_gemma":[0.000020974649,0.00003594148,0.00001967535,0.00009650099,0.00008699749,0.00014202771,0.0000962198,0.000026308911,0.0009304536],"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":[0.0000043648124,0.000028182449,0.04541144,0.0000020488728,0.0000018660259,4.953892e-7,0.000053442058,0.0011305572,0.91881126,0.00066091603,0.0018689111,0.03202653],"study_design_scores_gemma":[0.0001436033,0.000017001363,0.035610046,0.000002701769,0.0000037835562,0.0000033661138,0.00005458824,0.003113245,0.9427896,0.0018117173,0.016350437,0.00009990084],"about_ca_topic_score_codex":0.000009702648,"about_ca_topic_score_gemma":0.00003974759,"teacher_disagreement_score":0.060700092,"about_ca_system_score_codex":0.0000830208,"about_ca_system_score_gemma":7.865805e-7,"threshold_uncertainty_score":0.9998474},"labels":[],"label_agreement":null},{"id":"W2080528525","doi":"10.4018/ijstmi.2013070102","title":"Challenges in Climate Change and Environmental Crisis","year":2013,"lang":"en","type":"article","venue":"International Journal of Space Technology Management and Innovation","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Aviation; Montreal Protocol; Climate change; Air pollution; Environmental planning; Environmental science; Environmental resource management; Ozone layer; Environmental issue; Environmental crisis; Environmental protection; Global warming; Business; Geography; Meteorology; Engineering; Ecology; Ozone","score_opus":0.03105523902814494,"score_gpt":0.25261638533024733,"score_spread":0.22156114630210239,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2080528525","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":[0.9654266,0.0007782306,0.00052493217,0.030364787,0.00010171811,0.0001828768,8.9395985e-7,0.000036376063,0.0025835757],"genre_scores_gemma":[0.98298734,0.012805229,0.0039817295,0.00015489632,0.000015392168,0.000019629526,0.0000010883335,0.0000047586414,0.000029912722],"study_design_codex":"design_other","study_design_gemma":"observational","domain_scores_codex":[0.9993847,0.0000057769817,0.00021613816,0.00012974972,0.00015409426,0.000109528824],"domain_scores_gemma":[0.9997389,0.0000071678287,0.0001648404,0.000065914275,0.00001300613,0.000010197444],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00014090262,0.00007698536,0.000087768654,0.00076360523,0.00002258742,0.00001750855,0.00016648174,0.00006821298,0.00006518186],"category_scores_gemma":[0.000011431148,0.00006863768,0.000008565963,0.00027550344,0.00013033832,0.00054938835,0.00027347403,0.000120755096,0.000013480135],"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":[0.000015406467,0.00006783482,0.13971135,0.000007165713,0.000029739835,0.000036159323,0.00013282232,0.0000056609,0.0032264295,0.08567046,0.00034526738,0.7707517],"study_design_scores_gemma":[0.0018079226,0.0003552351,0.75711226,0.0001289148,0.000020111132,0.00019503535,0.01268165,0.0005099142,0.0035618828,0.2027361,0.020541823,0.00034913336],"about_ca_topic_score_codex":0.000004877319,"about_ca_topic_score_gemma":0.000003969596,"teacher_disagreement_score":0.77040255,"about_ca_system_score_codex":0.000063577536,"about_ca_system_score_gemma":4.561031e-7,"threshold_uncertainty_score":0.27989632},"labels":[],"label_agreement":null},{"id":"W2081718323","doi":"10.1115/gt2008-51001","title":"Derivation of Correlations for Small Turbojet Engines","year":2008,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Defence Research and Development Canada; Carleton University","funders":"","keywords":"Turbojet; Thrust; Propulsion; Process (computing); Variable (mathematics); Turbine; Computer science; Control theory (sociology); Aerospace engineering; Engineering; Mathematics; Artificial intelligence","score_opus":0.029571865774004245,"score_gpt":0.22163382215136573,"score_spread":0.19206195637736148,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2081718323","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":[0.30181757,0.000010226223,0.6910003,0.00012147756,0.000030411738,0.00015171332,0.0000021776334,0.00011277148,0.006753348],"genre_scores_gemma":[0.8951678,0.0000103437205,0.103454396,0.000027939639,0.000004068385,0.00001581018,0.000003167961,0.0000030048675,0.0013134251],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.99975044,0.0000019710296,0.00007410907,0.00007090767,0.00003896919,0.0000636081],"domain_scores_gemma":[0.9998331,0.000047686524,0.000025019861,0.00008017642,0.0000045736733,0.000009408337],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000019506222,0.000035530724,0.00004397822,0.000015012559,0.000046287594,7.90954e-7,0.000060383885,0.000028260592,0.00014273709],"category_scores_gemma":[0.000060024162,0.000029351975,0.00001925649,0.00008906869,0.00008555056,0.00006357714,0.000020983427,0.000018416766,0.000020599533],"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":[0.00005319371,0.0003381154,0.4951478,0.000030685726,0.000028527202,0.000004210849,0.0008380848,0.0346595,0.29320264,0.056253772,0.020396404,0.09904709],"study_design_scores_gemma":[0.0010347932,0.0003261822,0.50988543,0.00001191153,0.000017501221,0.00002571346,0.00021886625,0.026439501,0.35409507,0.060632356,0.046858102,0.00045454968],"about_ca_topic_score_codex":0.000011487813,"about_ca_topic_score_gemma":0.000012589927,"teacher_disagreement_score":0.5933503,"about_ca_system_score_codex":0.0000125710485,"about_ca_system_score_gemma":0.0000019513914,"threshold_uncertainty_score":0.1562871},"labels":[],"label_agreement":null},{"id":"W2085556920","doi":"10.2514/1.c033592","title":"Aerodynamic Optimization Trade Study of a Box-Wing Aircraft Configuration","year":2016,"lang":"en","type":"article","venue":"Journal of Aircraft","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":36,"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":"Wing; Aerodynamics; Aerospace engineering; Wing configuration; Angle of attack; Swept wing; Wingtip device; Aileron; Wing loading; Computer science; Aeronautics; Engineering","score_opus":0.011219448790419351,"score_gpt":0.2362619152419821,"score_spread":0.22504246645156273,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2085556920","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":[0.71369284,0.000038871727,0.28423223,0.0011690282,0.0001702508,0.00024728978,0.0000021776182,0.000052847492,0.00039443307],"genre_scores_gemma":[0.9856558,0.00006242551,0.014056083,0.000039688523,0.00003635271,0.000003892116,3.9100152e-7,0.000016531165,0.00012885779],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.9984012,0.00008054163,0.0006532081,0.00018411867,0.00047640118,0.00020453506],"domain_scores_gemma":[0.9989788,0.00011347481,0.00057411,0.00023344105,0.00003114995,0.00006901218],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003370891,0.00015448497,0.00029785497,0.00013172318,0.00007397563,0.000013587742,0.0003281551,0.00008875666,0.00034918188],"category_scores_gemma":[0.00018420546,0.00010085657,0.00009576357,0.00027135442,0.00015157457,0.0007156938,0.00006159626,0.00014802432,0.000017358125],"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":[0.00033977823,0.0018033334,0.062899366,0.00002427107,0.00016514737,0.00013737057,0.0018665589,0.21549499,0.59269536,0.00014081445,0.0015962761,0.12283677],"study_design_scores_gemma":[0.030386817,0.02322374,0.64967954,0.0013397612,0.0008436223,0.0010846697,0.01706632,0.017807737,0.23529185,0.009897025,0.010341032,0.003037853],"about_ca_topic_score_codex":0.000012631386,"about_ca_topic_score_gemma":0.000025620326,"teacher_disagreement_score":0.5867802,"about_ca_system_score_codex":0.00017705275,"about_ca_system_score_gemma":0.00002097343,"threshold_uncertainty_score":0.41128117},"labels":[],"label_agreement":null},{"id":"W2088609066","doi":"10.1144/1467-7873/05-094","title":"Numerical simulation of air concentration and deposition of particulate metals around a copper smelter in northern Quebec, Canada","year":2006,"lang":"en","type":"article","venue":"Geochemistry Exploration Environment Analysis","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":17,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Particulates; Copper; Smelting; Deposition (geology); Metallurgy; Environmental science; Environmental chemistry; Materials science; Chemistry; Geology; Geomorphology","score_opus":0.006947670283393104,"score_gpt":0.19921511729469735,"score_spread":0.19226744701130424,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2088609066","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":[0.9417488,0.000043717086,0.057830907,0.00015377863,0.0000034490902,0.00012481985,0.000005230767,0.000009557367,0.00007972426],"genre_scores_gemma":[0.9992772,0.000017743065,0.00046516766,0.000011950686,0.000005246358,0.000027070633,0.00013979794,0.000004391605,0.000051445237],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9989845,0.0000304917,0.00036417303,0.00022574261,0.00027634026,0.000118763324],"domain_scores_gemma":[0.99955356,0.00003556487,0.0002151394,0.00016519938,0.0000065171444,0.000024047788],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000067671026,0.00010876488,0.00020536061,0.000022786546,0.000030987332,0.0000059439694,0.00005552961,0.000057184683,0.00009921937],"category_scores_gemma":[0.000011889402,0.00010805663,0.000047597245,0.00030146798,0.0001178347,0.00024909448,0.000027584516,0.00004447654,0.0000019450756],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":true,"about_ca_topic_consensus":true,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000009760934,0.00004596612,0.22266078,0.0000052923397,0.000027227114,0.000001275943,0.000030547548,0.70768714,0.06917762,0.0000030212682,0.000006114696,0.00034525027],"study_design_scores_gemma":[0.00037887745,0.000020128316,0.21629854,0.000010721171,0.00024854884,4.093193e-7,0.00028984717,0.35097858,0.43088815,0.0005860553,0.00007565246,0.00022447162],"about_ca_topic_score_codex":0.07635551,"about_ca_topic_score_gemma":0.30053946,"teacher_disagreement_score":0.36171052,"about_ca_system_score_codex":0.00022048067,"about_ca_system_score_gemma":0.000010617734,"threshold_uncertainty_score":0.9297951},"labels":[],"label_agreement":null},{"id":"W2102720800","doi":"10.2514/6.2004-4537","title":"Evaluation of Multidisciplinary Optimization Approaches for Aircraft Conceptual Design","year":2004,"lang":"en","type":"article","venue":"10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":105,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"University of Toronto","keywords":"Multidisciplinary design optimization; Multidisciplinary approach; Conceptual design; Computer science; Systems engineering; Management science; Engineering; Human–computer interaction","score_opus":0.08261102980735363,"score_gpt":0.29540532444740286,"score_spread":0.21279429464004923,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2102720800","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.024036776,0.00017350886,0.97358567,0.00032869255,0.000048860238,0.0013052486,0.00004161101,0.00012868943,0.00035095745],"genre_scores_gemma":[0.5795965,0.00010733472,0.41988233,0.0000070464844,0.000011713702,0.00018350282,0.00014767612,0.000017487218,0.00004640046],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99708515,0.0002347809,0.00067308266,0.00086435693,0.00076513446,0.0003774828],"domain_scores_gemma":[0.9983855,0.00019421126,0.0004705109,0.00048245947,0.0003303897,0.00013693425],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.001445796,0.00037131552,0.000552397,0.00031238323,0.00048511516,0.000060059952,0.00034565543,0.00023768526,0.00047528394],"category_scores_gemma":[0.00035687748,0.00034084677,0.00019663993,0.0013073852,0.0007983884,0.00078132126,0.00030868792,0.00014195223,0.000005204332],"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":[0.000094163304,0.00024225359,0.003012393,0.000013492813,0.00020068002,9.4015405e-7,0.0011314786,0.9866624,0.0003658073,0.00076533394,0.0000065530244,0.0075045363],"study_design_scores_gemma":[0.001807289,0.0002960442,0.003808322,0.000028830471,0.0013816823,0.000002482424,0.0018019318,0.9837779,0.0025762238,0.004104726,0.0000042223464,0.00041037065],"about_ca_topic_score_codex":0.00004798942,"about_ca_topic_score_gemma":0.00006179737,"teacher_disagreement_score":0.55555975,"about_ca_system_score_codex":0.00020952833,"about_ca_system_score_gemma":0.00012166954,"threshold_uncertainty_score":0.99990433},"labels":[],"label_agreement":null},{"id":"W2106910961","doi":"10.1007/s13272-011-0024-6","title":"A distributed toolbox for multidisciplinary preliminary aircraft design","year":2011,"lang":"en","type":"article","venue":"CEAS Aeronautical Journal","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":89,"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":"Partenariat Canadien Contre Le Cancer; Deutsches Zentrum für Luft- und Raumfahrt","keywords":"Toolbox; Multidisciplinary approach; Component (thermodynamics); Process (computing); Systems engineering; Engineering; Aerospace; Successor cardinal; Interface (matter); Software engineering; Data exchange; Engineering management; Computer science; Process management; World Wide Web; Operating system; Mechanical engineering; Aerospace engineering","score_opus":0.05218618735246637,"score_gpt":0.26405637129819004,"score_spread":0.21187018394572366,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2106910961","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.02193979,0.0001267924,0.97534174,0.0007351863,0.0001961489,0.00045849386,0.000018979134,0.00019904265,0.0009838232],"genre_scores_gemma":[0.74961835,0.000021619568,0.24989505,0.00010598705,0.000057101897,0.000050827388,0.000005876978,0.00002598002,0.00021917987],"study_design_codex":"design_other","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.9983593,0.00006807791,0.00035405252,0.0003364885,0.00027358966,0.0006084948],"domain_scores_gemma":[0.99913394,0.00019413495,0.0001078335,0.00026599763,0.000022574348,0.00027553932],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0003744499,0.0002271641,0.00022322428,0.000039551236,0.0004039754,0.000032306714,0.0005049949,0.00016635505,0.0011600142],"category_scores_gemma":[0.00027616098,0.00017939885,0.00014877385,0.00016882527,0.0004921781,0.00035826745,0.00022635696,0.00038563707,0.0002133394],"study_design_candidate":"design_other","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":[0.013568304,0.0076538133,0.074066125,0.00014199672,0.00055228436,0.0031659973,0.0042890557,0.009528209,0.05709688,0.026095383,0.13911997,0.66472197],"study_design_scores_gemma":[0.0063433745,0.009613412,0.32152775,0.00018890116,0.00035163248,0.0029866612,0.001656199,0.03702043,0.040344168,0.5537077,0.023953361,0.0023063777],"about_ca_topic_score_codex":0.0000030326337,"about_ca_topic_score_gemma":0.0000012306486,"teacher_disagreement_score":0.7276786,"about_ca_system_score_codex":0.00019242245,"about_ca_system_score_gemma":0.000027637154,"threshold_uncertainty_score":0.99975306},"labels":[],"label_agreement":null},{"id":"W2110277674","doi":"10.1007/s13272-015-0153-4","title":"Collaborative understanding of disciplinary correlations using a low-fidelity physics-based aerospace toolkit","year":2015,"lang":"en","type":"article","venue":"CEAS Aeronautical Journal","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":20,"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":"Partenariat Canadien Contre Le Cancer; U.S. Department of Energy","keywords":"Toolbox; Workflow; Aerospace; Systems engineering; Fidelity; Modular design; Process (computing); Airframe; Avionics; Computer science; Engineering; Engineering design process; Software engineering; Aerospace engineering; Mechanical engineering","score_opus":0.07813560639609982,"score_gpt":0.31349197758979785,"score_spread":0.23535637119369804,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2110277674","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":[0.26094866,0.000060792154,0.73684025,0.00064614724,0.00014005751,0.00012784515,0.0000084833,0.00004615021,0.0011816295],"genre_scores_gemma":[0.96738213,0.0000048775382,0.032476954,0.00004757217,0.00004050948,0.0000018641972,0.0000019341728,0.000012163328,0.00003202049],"study_design_codex":"simulation_or_modeling","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.99868834,0.000079606056,0.0002992747,0.00019322743,0.0004455103,0.0002940222],"domain_scores_gemma":[0.99920225,0.00015226798,0.00018748152,0.0001829526,0.000049814276,0.0002252237],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003046541,0.00014660138,0.00021100207,0.000030581657,0.00026744127,0.00004834571,0.0002076765,0.000092812625,0.00013630098],"category_scores_gemma":[0.0002828071,0.00012266921,0.00007059234,0.00047739912,0.00075453805,0.00047163587,0.00016013591,0.00035373107,0.000026254995],"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":[0.0008713159,0.0016612792,0.16295564,0.00004838934,0.000146939,0.00026068522,0.0024365487,0.6784266,0.05790315,0.08293467,0.0034307884,0.008923998],"study_design_scores_gemma":[0.004192395,0.0009442742,0.02608904,0.00035756652,0.00018679054,0.00017517329,0.013461114,0.29998302,0.009049884,0.64403236,0.0004944326,0.0010339201],"about_ca_topic_score_codex":0.0000051056577,"about_ca_topic_score_gemma":0.000006216443,"teacher_disagreement_score":0.7064335,"about_ca_system_score_codex":0.00092575623,"about_ca_system_score_gemma":0.0001456447,"threshold_uncertainty_score":0.50023055},"labels":[],"label_agreement":null},{"id":"W2125491879","doi":"10.2514/6.2013-4288","title":"A Usage-Based Analysis Method for Predicting Fleet Fuel Savings Due to Aircraft Improvements","year":2013,"lang":"en","type":"article","venue":"2013 Aviation Technology, Integration, and Operations Conference","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lockheed Martin (Canada)","funders":"","keywords":"Computer science; Automotive engineering; Aeronautics; Engineering","score_opus":0.012650890161536024,"score_gpt":0.26719097666678887,"score_spread":0.25454008650525284,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2125491879","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.077691324,0.000022322973,0.9123433,0.00787908,0.000054289012,0.0013535246,0.000038356764,0.00041554027,0.00020225126],"genre_scores_gemma":[0.65174866,0.000014000562,0.34592342,0.00039358303,0.000010008015,0.0012656358,0.000065131935,0.000010717383,0.00056882564],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99841815,0.000051276314,0.00043764903,0.0006010768,0.00018322968,0.00030864152],"domain_scores_gemma":[0.9990203,0.00010004065,0.00011523117,0.00042265293,0.0002528552,0.000088934496],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00033520968,0.00024269124,0.0002871169,0.0005187476,0.0006640983,0.00016942208,0.00034026214,0.0002548127,0.00057693076],"category_scores_gemma":[0.00050589687,0.00021293099,0.00006732651,0.0013106111,0.00020122313,0.00068403484,0.0001525357,0.00018844643,0.00009810923],"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":[0.000030246994,0.0004012881,0.1170183,0.000045807235,0.00033160418,0.0000017859544,0.0028363983,0.02066056,0.30544186,0.05461722,0.0040501724,0.49456474],"study_design_scores_gemma":[0.00081097055,0.00048264535,0.03802748,0.000038198385,0.00023345005,0.000004562794,0.0017221686,0.87130445,0.047572985,0.036297318,0.0028446056,0.0006611351],"about_ca_topic_score_codex":0.0011188253,"about_ca_topic_score_gemma":0.004194845,"teacher_disagreement_score":0.85064393,"about_ca_system_score_codex":0.00012321642,"about_ca_system_score_gemma":0.00003841446,"threshold_uncertainty_score":0.8683074},"labels":[],"label_agreement":null},{"id":"W2128821997","doi":"10.5589/q12-008","title":"A multidisciplinary design optimization approach to preliminary wing design using multifidelity analysis","year":2012,"lang":"en","type":"article","venue":"Canadian aeronautics and space journal","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Multidisciplinary design optimization; Aerodynamics; Aerospace; Solver; Wing; Aeroelasticity; Engineering; Finite element method; Wing configuration; Genetic algorithm; Optimal design; Computer science; Aerospace engineering; Structural engineering; Multidisciplinary approach; Mathematical optimization; Mathematics","score_opus":0.04750186901573032,"score_gpt":0.25821302361290643,"score_spread":0.2107111545971761,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2128821997","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":[0.026797378,0.0001936743,0.97159433,0.00023678647,0.00004921761,0.00025207616,0.000002798412,0.000031168125,0.0008425844],"genre_scores_gemma":[0.49238762,0.000020511361,0.5073364,0.000045858626,0.00001997891,0.0000032533944,8.889808e-7,0.00001544539,0.0001700575],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9987644,0.00010072832,0.00018739524,0.00022170937,0.00017086756,0.0005548993],"domain_scores_gemma":[0.99884856,0.000045168435,0.00008788308,0.00018228644,0.000013671507,0.0008224349],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00060670514,0.0001675302,0.00018735681,0.00027836915,0.00048554692,0.000070718794,0.0001604376,0.00010792699,0.0001603631],"category_scores_gemma":[0.000093047885,0.00015558217,0.000052348496,0.00061135035,0.00011416569,0.000309635,0.00009447822,0.00020027229,0.000011052759],"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":[0.000015183682,0.000034439465,0.017748034,0.0000017676298,0.000047473102,0.000009253571,0.00050618214,0.97790104,0.00065542146,0.000041011124,0.00024101385,0.0027991596],"study_design_scores_gemma":[0.00016413283,0.00007745333,0.028673925,0.000010284672,0.00018050411,0.0001030915,0.00071355223,0.9693088,0.00014232009,0.00012207651,0.00023744728,0.00026641673],"about_ca_topic_score_codex":0.0015100735,"about_ca_topic_score_gemma":0.0006567105,"teacher_disagreement_score":0.46559024,"about_ca_system_score_codex":0.0005020355,"about_ca_system_score_gemma":0.00005296244,"threshold_uncertainty_score":0.63444567},"labels":[],"label_agreement":null},{"id":"W2139936354","doi":"10.2514/6.2001-4316","title":"Advanced business jet conceptual design and cost optimization using a genetic algorithm approach","year":2001,"lang":"en","type":"article","venue":"AIAA Atmospheric Flight Mechanics Conference and Exhibit","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Toronto Metropolitan University","funders":"","keywords":"Computer science; Conceptual design; Genetic algorithm; Jet (fluid); Algorithm design; Algorithm; Mathematical optimization; Engineering; Mathematics; Aerospace engineering; Machine learning; Human–computer interaction","score_opus":0.024015393742899748,"score_gpt":0.21862923114831576,"score_spread":0.19461383740541602,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2139936354","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":[0.029120617,0.00044505397,0.96910125,0.00007610432,0.000075400756,0.000624757,0.0000027243127,0.00016753846,0.00038657902],"genre_scores_gemma":[0.24264173,0.0019781387,0.7550122,0.00012799219,0.000016900734,0.00005693487,0.000007357995,0.000028299526,0.00013040588],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99832433,0.00006127021,0.0002671455,0.00065657013,0.00024252542,0.00044818074],"domain_scores_gemma":[0.99935055,0.0000506136,0.00013025472,0.0002835702,0.0000483992,0.00013660407],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00012795739,0.00032955053,0.0003154092,0.000009080308,0.00027314408,0.000085268366,0.00021617583,0.00018761629,0.00028205503],"category_scores_gemma":[0.000041166924,0.00029369717,0.000026378382,0.0005531036,0.00026918534,0.0004534477,0.00024362934,0.00015606951,0.000014407357],"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":[0.000081777456,0.00014000296,0.0010388745,0.000019807256,0.00003290907,0.00007391809,0.00057104696,0.532659,0.008698827,0.0024716936,0.00009692738,0.45411524],"study_design_scores_gemma":[0.0006833,0.00011133756,0.00020373028,0.000027955819,0.000034900593,0.00013893258,0.00068907865,0.99247426,0.00082235504,0.0031298609,0.0012487313,0.0004355298],"about_ca_topic_score_codex":0.00006885181,"about_ca_topic_score_gemma":0.0000029685295,"teacher_disagreement_score":0.45981532,"about_ca_system_score_codex":0.00008156797,"about_ca_system_score_gemma":0.000032187123,"threshold_uncertainty_score":0.99995154},"labels":[],"label_agreement":null},{"id":"W2156030189","doi":"10.2514/6.2010-9191","title":"Multi-Fidelity Multidisciplinary Design Optimization of Metallic and Composite Regional and Business Jets","year":2010,"lang":"en","type":"article","venue":"13th AIAA/ISSMO Multidisciplinary Analysis Optimization Conference","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":17,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Bombardier (Canada)","funders":"","keywords":"Multidisciplinary approach; Composite number; Multidisciplinary design optimization; Materials science; Fidelity; Aerospace engineering; Computer science; Composite material; Engineering; Telecommunications","score_opus":0.03344011086048298,"score_gpt":0.27704157105186605,"score_spread":0.24360146019138307,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2156030189","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.1849189,0.00011058092,0.8137686,0.00038832007,0.00005161898,0.0004826065,0.000024871866,0.00015664304,0.000097859614],"genre_scores_gemma":[0.5269962,0.00035552497,0.4723828,0.0000134560305,0.000008173396,0.00003315574,0.000105881445,0.00001841401,0.00008639094],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9971675,0.00019329738,0.00076036673,0.0010387058,0.00043934345,0.00040074496],"domain_scores_gemma":[0.998006,0.000282342,0.00055032084,0.0006665893,0.0002708821,0.0002238659],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00055412285,0.00046471495,0.0006956212,0.00039772876,0.00055666856,0.000099324374,0.00044549178,0.0003028055,0.00050035963],"category_scores_gemma":[0.00022471428,0.0004294566,0.00012640201,0.0018805249,0.0013190733,0.0010456775,0.0007905251,0.00036423857,0.0000068745685],"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":[0.00010187972,0.00026269816,0.055889674,0.000026144342,0.00015658107,0.000007232862,0.00041521562,0.91975456,0.021865409,0.00014637451,0.000006824089,0.0013674131],"study_design_scores_gemma":[0.00073815923,0.000066865716,0.11346416,0.000023126719,0.00043563472,0.000015110897,0.0002315029,0.8827471,0.001385831,0.0004400575,0.000009647493,0.00044281594],"about_ca_topic_score_codex":0.00016210631,"about_ca_topic_score_gemma":0.00017033925,"teacher_disagreement_score":0.34207729,"about_ca_system_score_codex":0.00004889166,"about_ca_system_score_gemma":0.000049071183,"threshold_uncertainty_score":0.9998157},"labels":[],"label_agreement":null},{"id":"W2157131977","doi":"10.2514/6.2012-2926","title":"Aviation Emissions Index Derivation Methodologies from Flight Data, including Black Carbon and Aerosols","year":2012,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"National Research Council Canada","funders":"","keywords":"Index (typography); Aviation; Environmental science; Carbon black; Aeronautics; Aerospace engineering; Computer science; Meteorology; Engineering; Physics; Chemistry","score_opus":0.11792973887014528,"score_gpt":0.33290271397573273,"score_spread":0.21497297510558744,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2157131977","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":[0.75466156,0.00011605901,0.2394525,0.00048237783,0.000076573786,0.0001473435,0.0000069614657,0.0002838533,0.0047727935],"genre_scores_gemma":[0.9173048,0.0000773567,0.08226402,0.000087086395,0.000030149522,0.000006673405,0.000028881183,0.0000073035008,0.00019373091],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.999186,0.00005521978,0.00014062373,0.00026058278,0.00014422536,0.00021339575],"domain_scores_gemma":[0.9992404,0.0002495739,0.00006754929,0.0003839578,0.0000031744726,0.000055340694],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00028165916,0.00010754973,0.00010952166,0.00002515666,0.00011124634,0.000019568939,0.00023267379,0.00010893484,0.00022546854],"category_scores_gemma":[0.00043771815,0.000084135085,0.000009527715,0.00014148514,0.00016349886,0.00072091667,0.00081307476,0.0001037749,0.00003174782],"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":[0.000010193058,0.000030771407,0.67525524,0.0000034497914,0.000011775719,7.054037e-7,0.00044495333,0.00012603919,0.27752867,0.0006778611,0.0008481432,0.0450622],"study_design_scores_gemma":[0.00037371228,0.000034993656,0.74399036,0.000021402335,0.0000337478,0.000003000776,0.0016440612,0.009497799,0.19706415,0.042154994,0.0047002207,0.00048156973],"about_ca_topic_score_codex":0.0002683258,"about_ca_topic_score_gemma":0.00004011585,"teacher_disagreement_score":0.16264327,"about_ca_system_score_codex":0.000059943002,"about_ca_system_score_gemma":0.0000026698344,"threshold_uncertainty_score":0.34309292},"labels":[],"label_agreement":null},{"id":"W2165534856","doi":"10.2514/6.2004-4370","title":"The Application of Multi-Disciplinary Optimization Technologies to the Design of a Business Jet","year":2004,"lang":"en","type":"article","venue":"10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":16,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Bombardier (Canada)","funders":"","keywords":"Jet (fluid); Discipline; Computer science; Manufacturing engineering; Systems engineering; Engineering; Aerospace engineering; Sociology","score_opus":0.02259137944025313,"score_gpt":0.266096171168579,"score_spread":0.24350479172832584,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2165534856","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0052691423,0.00018295225,0.99069357,0.0028475914,0.000026637576,0.0007815649,0.00001668692,0.00013328173,0.000048545902],"genre_scores_gemma":[0.684293,0.000643929,0.3148623,0.000008777813,0.0000039804063,0.000118341515,0.000022215127,0.000010511534,0.00003697849],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99828357,0.000085069536,0.00055520295,0.0004964963,0.0003181134,0.00026157673],"domain_scores_gemma":[0.9983986,0.00019904527,0.00043840025,0.0007207185,0.00019356968,0.00004964002],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00046350737,0.00025019195,0.0003651004,0.00020502308,0.00063711766,0.00005242947,0.00069733936,0.00014158279,0.00002851876],"category_scores_gemma":[0.000281024,0.0001501107,0.000088940906,0.0030532142,0.00079609384,0.00030886108,0.0006648655,0.00013617236,0.000005159729],"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":[0.000062113264,0.00011319704,0.0044649774,0.0000098029495,0.000069261725,6.9989426e-7,0.00044260547,0.98361856,0.0011439358,0.0006030857,0.0000060292573,0.009465728],"study_design_scores_gemma":[0.00034380864,0.00011057111,0.0092926845,0.000024750494,0.00019566137,0.0000021087428,0.0015243503,0.98409015,0.0030055726,0.0011834396,0.00002368739,0.0002032007],"about_ca_topic_score_codex":0.000111244626,"about_ca_topic_score_gemma":0.00019006229,"teacher_disagreement_score":0.6790238,"about_ca_system_score_codex":0.00006253615,"about_ca_system_score_gemma":0.00003857111,"threshold_uncertainty_score":0.6121337},"labels":[],"label_agreement":null},{"id":"W2168082332","doi":"10.2514/6.2011-6884","title":"Global Fuel Analysis of Intermediate Stop Operations on Long-Haul Routes","year":2011,"lang":"en","type":"article","venue":"11th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":8,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Computer science","score_opus":0.019975302045859532,"score_gpt":0.2564539812821043,"score_spread":0.23647867923624474,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2168082332","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":[0.42464823,0.00007511518,0.5706335,0.000765423,0.00010859871,0.0004918505,0.00012562932,0.0003650403,0.0027866366],"genre_scores_gemma":[0.9839926,0.0002211675,0.014788327,0.00015163093,0.000011457241,0.00018329633,0.00017687627,0.0000116318615,0.00046304238],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"observational","domain_scores_codex":[0.9981384,0.00008243838,0.0006479793,0.00058814505,0.0002716836,0.00027131455],"domain_scores_gemma":[0.99887097,0.00004763134,0.00015971465,0.0005885417,0.00025654104,0.0000766144],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00023068751,0.0003015193,0.0003861384,0.0006226159,0.00036660556,0.00008805677,0.00046421736,0.0003150449,0.0009608047],"category_scores_gemma":[0.00043783867,0.0002643931,0.00008885345,0.0024009328,0.000811424,0.0007546123,0.0001384206,0.00023873262,0.00007400326],"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":[0.00003846504,0.0005356248,0.2826645,0.000014168786,0.0003527729,0.0000046159294,0.0029240437,0.007935109,0.0058627035,0.64518195,0.00020704739,0.054278985],"study_design_scores_gemma":[0.0008893767,0.00080655917,0.81431353,0.000076961565,0.0005888367,0.000010026943,0.004286223,0.109413944,0.023722524,0.044794757,0.00025332722,0.0008439366],"about_ca_topic_score_codex":0.00065441796,"about_ca_topic_score_gemma":0.0125050135,"teacher_disagreement_score":0.6003872,"about_ca_system_score_codex":0.00017944057,"about_ca_system_score_gemma":0.00006999989,"threshold_uncertainty_score":0.9999808},"labels":[],"label_agreement":null},{"id":"W2173122211","doi":"10.5539/mer.v5n2p89","title":"Thermodynamic Analysis of Different Configurations of Combined Cycle Power Plants","year":2015,"lang":"en","type":"article","venue":"Mechanical Engineering Research","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Combined cycle; Thermal efficiency; Gas turbines; Turbine; Work output; Thermodynamic cycle; Work (physics); Thermal power station; Environmental science; Nuclear engineering; Materials science; Mechanical engineering; Thermodynamics; Engineering; Chemistry; Physics; Combustion","score_opus":0.034767979696675305,"score_gpt":0.296423316295579,"score_spread":0.2616553365989037,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2173122211","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":[0.9544495,0.000013801751,0.044440564,0.000062805426,0.000027139547,0.00012323067,0.000012541704,0.00005744308,0.00081300904],"genre_scores_gemma":[0.99922365,0.0000069783373,0.0006922572,0.0000018137476,0.0000015941806,0.000013475898,0.0000053850463,0.000007677095,0.00004717249],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989198,0.000034398014,0.000185033,0.0001566757,0.00048606787,0.00021806367],"domain_scores_gemma":[0.9993962,0.00018115525,0.000029237228,0.00028652727,0.000025571439,0.0000812793],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00035269163,0.00007278656,0.00021663676,0.00018711398,0.000020634061,0.0000047428903,0.00028169208,0.000067273526,0.0002352818],"category_scores_gemma":[0.00030644392,0.000058479993,0.000058199934,0.00071178505,0.00009564685,0.00004503471,0.00017464093,0.00017745135,0.000015251892],"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":[0.000051853287,0.00023072069,0.0008585087,0.000009736232,0.00017831098,0.000005791076,0.00015009621,0.05778931,0.91990316,0.019185849,0.000056646113,0.0015800397],"study_design_scores_gemma":[0.00048760325,0.00046367774,0.023362245,0.000020500698,0.000043174823,8.6501905e-7,0.0002330796,0.814529,0.15195586,0.008673629,0.00006873336,0.00016163287],"about_ca_topic_score_codex":0.000048964175,"about_ca_topic_score_gemma":0.00001351965,"teacher_disagreement_score":0.76794726,"about_ca_system_score_codex":0.0000857282,"about_ca_system_score_gemma":0.0000068767417,"threshold_uncertainty_score":0.2576171},"labels":[],"label_agreement":null},{"id":"W2186363797","doi":"10.32920/ryerson.14653626.v1","title":"Preliminary Sailplane Design Using MDO And Multi-Fidelity Analysis","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Aerodynamics; Airworthiness; Multidisciplinary design optimization; Solver; Finite element method; Aerospace; Engineering; Aerospace engineering; Aeroelasticity; Wing; Computer science; Multidisciplinary approach; Structural engineering","score_opus":0.05925819300300604,"score_gpt":0.2871872764832746,"score_spread":0.22792908348026852,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2186363797","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.15084854,0.00038090904,0.84778744,0.000050829713,0.00004957302,0.00024773352,0.000007381856,0.00023025316,0.00039733577],"genre_scores_gemma":[0.50321305,0.00016063225,0.49627507,0.000051654355,0.0000058369087,0.000012352707,0.000019696221,0.000010949356,0.0002507521],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9982036,0.00012704139,0.00028574734,0.000875658,0.00022788359,0.000280101],"domain_scores_gemma":[0.9989593,0.00011685744,0.00013657493,0.0006933391,0.00001098918,0.00008293671],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00029837975,0.00029645854,0.00044439881,0.00010691125,0.00011736832,0.00008244769,0.00031230744,0.00035015531,0.00079784845],"category_scores_gemma":[0.00012397775,0.00026771484,0.00013072985,0.0003967011,0.00027801708,0.00014295775,0.0021953406,0.0004158194,0.000015107825],"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":[0.000060124654,0.00031705783,0.106448755,0.00009491726,0.0007483294,0.00015944791,0.00037860204,0.78084975,0.018078439,0.000054371485,0.00023436526,0.09257586],"study_design_scores_gemma":[0.00021388223,0.000063252526,0.07706858,0.00003844288,0.0007808552,0.000016970322,0.00039955744,0.9121009,0.006165801,0.0023837266,0.00009136311,0.0006766587],"about_ca_topic_score_codex":0.0009897698,"about_ca_topic_score_gemma":0.0001261961,"teacher_disagreement_score":0.3523645,"about_ca_system_score_codex":0.00016140462,"about_ca_system_score_gemma":0.000016332491,"threshold_uncertainty_score":0.9999775},"labels":[],"label_agreement":null},{"id":"W2188171131","doi":"10.1017/s000192400000659x","title":"Aircraft conceptual design for optimal environmental performance","year":2012,"lang":"en","type":"article","venue":"The Aeronautical Journal","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":115,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Royal Military College of Canada; University of Toronto","funders":"","keywords":"Airframe; Airplane; Takeoff and landing; Takeoff; Cruise; Propulsion; Conceptual design; Aviation; Engineering; Multidisciplinary design optimization; Genetic algorithm; Propulsive efficiency; Automotive engineering; Aerospace engineering; Computer science; Aeronautics; Multidisciplinary approach; Mechanical engineering","score_opus":0.03186858817412897,"score_gpt":0.24468910867985394,"score_spread":0.21282052050572497,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2188171131","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":[0.5918268,0.0003503264,0.40559867,0.0010336295,0.000250369,0.0003587869,0.0000047360763,0.000081636856,0.00049504795],"genre_scores_gemma":[0.9484935,0.000098008575,0.050423034,0.0003635372,0.00019379113,0.000028698212,0.0000012168559,0.000018874605,0.00037934887],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9985401,0.00007349033,0.000229362,0.00014718526,0.0003202008,0.00068967254],"domain_scores_gemma":[0.999281,0.00024549148,0.00007747573,0.00020632187,0.0000028263323,0.00018686673],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0006615894,0.00017121984,0.00014331857,0.000015943642,0.00052124314,0.000028043289,0.00047385893,0.00008581967,0.0014261825],"category_scores_gemma":[0.00006535916,0.00010602404,0.00008847633,0.00006569582,0.0010784221,0.000470258,0.00018747787,0.00038653647,0.00058445963],"study_design_candidate":"design_other","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":[0.0017344077,0.0018108138,0.09703349,0.000017460265,0.00027218793,0.00003605271,0.005152974,0.051516987,0.1307986,0.013904196,0.048580866,0.64914197],"study_design_scores_gemma":[0.00841822,0.005774566,0.27843872,0.00008524631,0.0005178468,0.0058723493,0.0075809835,0.05982305,0.14035901,0.02339127,0.4664864,0.0032523454],"about_ca_topic_score_codex":4.5481312e-7,"about_ca_topic_score_gemma":9.180509e-8,"teacher_disagreement_score":0.64588964,"about_ca_system_score_codex":0.0001844688,"about_ca_system_score_gemma":0.000008793844,"threshold_uncertainty_score":0.9994866},"labels":[],"label_agreement":null},{"id":"W2206197924","doi":"10.4271/2001-01-2916","title":"Evaluation of Current Conductivity of Composite Wiring Integrated Assembly for use on Bell / Agusta 609 Tiltrotor Aircraft","year":2001,"lang":"en","type":"article","venue":"SAE technical papers on CD-ROM/SAE technical paper series","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Bell Helicopter Textron (Canada)","funders":"","keywords":"Composite number; Conductivity; Current (fluid); Materials science; Aerospace engineering; Computer science; Electrical engineering; Engineering; Composite material; Physics","score_opus":0.05350039771655043,"score_gpt":0.31156698640734554,"score_spread":0.25806658869079513,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2206197924","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":[0.9909675,0.00019051603,0.00010550383,0.0005545859,0.00018014575,0.0026139375,0.00011005635,0.0010469272,0.0042308],"genre_scores_gemma":[0.99120384,0.00021404926,0.007665915,0.00015881278,0.00003397057,0.00050484325,0.000042279837,0.000072383395,0.000103927705],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.9952582,0.00026183832,0.0010458152,0.0011060331,0.0016123322,0.0007157659],"domain_scores_gemma":[0.997037,0.00078750093,0.0004932532,0.0012907294,0.00020295948,0.0001885808],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0014769274,0.0006332833,0.000915059,0.0001988489,0.00023776562,0.000037204773,0.0009353425,0.0005519494,0.00032551188],"category_scores_gemma":[0.001956978,0.00053135,0.0003999521,0.00090232893,0.0016336746,0.00075409573,0.00043342038,0.00085743953,0.00003783574],"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":[0.00057130295,0.00085607404,0.002034455,0.00003461924,0.000035639743,0.0000046439973,0.000014975066,0.0004617779,0.94402593,0.0017190439,0.00078741665,0.049454134],"study_design_scores_gemma":[0.001554755,0.002646142,0.9512689,0.0003848596,0.00022629964,0.000021091144,0.00009380309,0.0000088210745,0.018790936,0.0063635283,0.017951244,0.00068957836],"about_ca_topic_score_codex":0.00007789478,"about_ca_topic_score_gemma":0.013012262,"teacher_disagreement_score":0.9492345,"about_ca_system_score_codex":0.00072936097,"about_ca_system_score_gemma":0.00007586001,"threshold_uncertainty_score":0.9997138},"labels":[],"label_agreement":null},{"id":"W220643838","doi":"10.4271/2004-01-1804","title":"More Electric Small Turbofan","year":2004,"lang":"en","type":"article","venue":"SAE technical papers on CD-ROM/SAE technical paper series","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Turbofan; Computer science; Automotive engineering; Engineering","score_opus":0.010805731941281047,"score_gpt":0.22971461284106906,"score_spread":0.21890888089978802,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W220643838","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":[0.8697088,0.00060569425,0.000025915964,0.012838129,0.00026048854,0.0018409552,0.000034142806,0.009828116,0.104857765],"genre_scores_gemma":[0.9797991,0.00056644605,0.014896243,0.003380876,0.00008489734,0.0003535842,0.000021492711,0.00014219688,0.00075518986],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.994636,0.000080693266,0.00094208814,0.0017321777,0.0010561206,0.0015529096],"domain_scores_gemma":[0.9971318,0.0002521518,0.0002448762,0.0018873014,0.000030304902,0.0004535143],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.0004173747,0.00097566046,0.0008815305,0.00021419598,0.00056232756,0.00009575028,0.0019785303,0.0010744268,0.0011546293],"category_scores_gemma":[0.0008089658,0.0008168733,0.00047944568,0.0017757666,0.0020438395,0.00059833593,0.00095488015,0.0017992689,0.0010911527],"study_design_candidate":"bench_or_experimental","study_design_consensus":null,"about_ca_topic_candidate":true,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00015097667,0.00043283668,0.00047922018,0.000013953342,0.000021102487,0.00014700985,0.000021972392,0.00019451683,0.9685025,0.011886844,0.0013252082,0.016823834],"study_design_scores_gemma":[0.0008740971,0.0014643205,0.9068231,0.000090297624,0.000051597875,0.00018633969,0.000084926476,4.2395275e-8,0.0025638004,0.032272097,0.05459497,0.0009944097],"about_ca_topic_score_codex":0.000129154,"about_ca_topic_score_gemma":0.04811596,"teacher_disagreement_score":0.96593875,"about_ca_system_score_codex":0.0010089766,"about_ca_system_score_gemma":0.00006524058,"threshold_uncertainty_score":0.9997584},"labels":[],"label_agreement":null},{"id":"W2234597696","doi":"10.2514/1.b35943","title":"Numerical Prediction of Gaseous Aerosol Precursors and Particles in an Aircraft Engine","year":2016,"lang":"en","type":"article","venue":"Journal of Propulsion and Power","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"École de Technologie Supérieure","funders":"","keywords":"Combustor; Environmental science; Jet engine; Particulates; Nozzle; Combustion; Takeoff; Soot; Aerospace engineering; Meteorology; Chemistry; Engineering; Physics","score_opus":0.010364634075415673,"score_gpt":0.23068605553935864,"score_spread":0.22032142146394296,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2234597696","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":[0.9972045,0.00015192355,0.0019432511,0.00054684357,0.00004557756,0.000059826376,0.0000019767374,0.000010063732,0.00003606326],"genre_scores_gemma":[0.9963177,0.00021715475,0.003399716,0.00001876034,0.000008011358,0.0000010975483,7.839594e-8,0.0000039825577,0.000033509037],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.9994463,0.000029899073,0.00021303339,0.00008720676,0.00012831394,0.000095272415],"domain_scores_gemma":[0.9997328,0.000028115464,0.000102100545,0.0000634281,0.000009522736,0.00006402351],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00014408186,0.000058819784,0.00011450883,0.000039896735,0.00001909955,0.0000048545817,0.000054961358,0.00004574892,0.00012455831],"category_scores_gemma":[0.000070097565,0.00003274893,0.000016400914,0.00006792444,0.00012649618,0.00028468852,0.000029505936,0.00007208651,0.0000023867656],"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":[0.00021749696,0.00021593082,0.25894886,0.000008672212,0.0000052482605,0.000029356059,0.0003852781,0.00007484191,0.4148344,0.000025130576,0.00026667136,0.3249881],"study_design_scores_gemma":[0.004313099,0.006796084,0.6293689,0.00046654363,0.00003382404,0.0004941447,0.0006612186,0.001400469,0.34165075,0.00970762,0.0047179176,0.00038940768],"about_ca_topic_score_codex":0.0000031388072,"about_ca_topic_score_gemma":0.0000025142401,"teacher_disagreement_score":0.37042007,"about_ca_system_score_codex":0.000020537384,"about_ca_system_score_gemma":0.000003342728,"threshold_uncertainty_score":0.13638262},"labels":[],"label_agreement":null},{"id":"W2269794755","doi":"10.4271/2009-01-3151","title":"Quantifying the Fuel Consumption Penalties for an Operational Contrail Avoidance System","year":2009,"lang":"en","type":"article","venue":"SAE technical papers on CD-ROM/SAE technical paper series","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Boeing (Canada)","funders":"","keywords":"Fuel efficiency; Consumption (sociology); Environmental science; Computer science; Automotive engineering; Engineering","score_opus":0.03467495366590119,"score_gpt":0.28115318416745383,"score_spread":0.24647823050155265,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2269794755","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":[0.90883774,0.0018603443,0.00037763707,0.024547217,0.0006813541,0.0071268394,0.00026072678,0.011850304,0.04445787],"genre_scores_gemma":[0.9856534,0.00025014783,0.010334699,0.0027136714,0.000101184174,0.000559477,0.00004117281,0.00005642893,0.00028980777],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.99618995,0.00015649508,0.0008421057,0.0011346685,0.00081355113,0.0008632552],"domain_scores_gemma":[0.99772257,0.00057829364,0.00024349721,0.0011938646,0.00005051373,0.00021129157],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0008516406,0.00061781664,0.0006317397,0.00007988824,0.0010170583,0.00017944846,0.0013227913,0.0005600253,0.00028276368],"category_scores_gemma":[0.0005784354,0.0004363657,0.00029588555,0.00039196343,0.0017816535,0.0009804103,0.00023068435,0.0008413704,0.00018925942],"study_design_candidate":"observational","study_design_consensus":null,"about_ca_topic_candidate":true,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00029507466,0.00019693465,0.00039765157,0.00003493277,0.0000137281195,0.000010161946,0.000033267126,0.00015098372,0.90468484,0.08430011,0.0016453454,0.008236972],"study_design_scores_gemma":[0.00076704205,0.0016238843,0.9613471,0.00014344526,0.000049696948,0.00011614955,0.0003495267,0.000002806129,0.00045879223,0.008221984,0.026280938,0.00063862884],"about_ca_topic_score_codex":0.000027384205,"about_ca_topic_score_gemma":0.030569803,"teacher_disagreement_score":0.9609495,"about_ca_system_score_codex":0.0004556002,"about_ca_system_score_gemma":0.00003743242,"threshold_uncertainty_score":0.9998088},"labels":[],"label_agreement":null},{"id":"W2300818414","doi":"","title":"Optimisation robuste des aéronefs et des groupes turboréacteurs","year":2012,"lang":"fr","type":"article","venue":"PolyPublie (École Polytechnique de Montréal)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Humanities; Political science; Philosophy","score_opus":0.020762606896265856,"score_gpt":0.24131132750453507,"score_spread":0.22054872060826922,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2300818414","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.27126837,0.021711757,0.6989862,0.003287439,0.00040007048,0.00079861534,0.00006373904,0.0012863454,0.0021974917],"genre_scores_gemma":[0.5896134,0.005411509,0.39859405,0.0009779849,0.0001462813,0.00028064978,0.000019899568,0.0001035529,0.004852715],"study_design_codex":"design_other","study_design_gemma":"observational","domain_scores_codex":[0.9955859,0.00036761753,0.0006599438,0.00069030945,0.00054392696,0.002152307],"domain_scores_gemma":[0.99769795,0.00024038457,0.00034758722,0.0009864309,0.00005814052,0.0006695003],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0013052735,0.0007305762,0.00051813846,0.0003136587,0.0007435018,0.0002648487,0.00083088264,0.0007559715,0.00083960156],"category_scores_gemma":[0.0005905449,0.00076478405,0.00026416336,0.0009860742,0.0016424275,0.003498754,0.0006191935,0.0008792536,0.0004992897],"study_design_candidate":"observational","study_design_consensus":null,"about_ca_topic_candidate":true,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000108239954,0.0012197379,0.23400405,0.00017888214,0.00010606627,0.000062017025,0.004721412,0.056589756,0.030657992,0.04978356,0.0036145044,0.61895376],"study_design_scores_gemma":[0.0013549601,0.00077448826,0.71683884,0.00060289825,0.00029084217,0.00085545797,0.0038867497,0.05524981,0.09337204,0.08014236,0.043783955,0.0028476052],"about_ca_topic_score_codex":0.012353752,"about_ca_topic_score_gemma":0.0065484126,"teacher_disagreement_score":0.61610615,"about_ca_system_score_codex":0.0022443242,"about_ca_system_score_gemma":0.00007093387,"threshold_uncertainty_score":0.9994803},"labels":[],"label_agreement":null},{"id":"W2312198328","doi":"10.2514/6.2008-5955","title":"pyACDT: An Object-Oriented Framework for Aircraft Design Modelling and Multidisciplinary Optimization","year":2008,"lang":"en","type":"article","venue":"12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":28,"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":"Multidisciplinary design optimization; Multidisciplinary approach; Computer science; Object-oriented programming; Systems engineering; Object (grammar); Engineering; Artificial intelligence; Programming language","score_opus":0.04029868223006588,"score_gpt":0.27801591088943106,"score_spread":0.23771722865936518,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2312198328","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":[0.04834377,0.00014174148,0.94993764,0.000245548,0.000060022747,0.00083343533,0.000035314624,0.00030587634,0.0000966698],"genre_scores_gemma":[0.46582508,0.0008302422,0.5329364,0.000021130305,0.000020574305,0.00010449759,0.00013765889,0.00002804736,0.00009635971],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9970763,0.00014131438,0.00062018965,0.0012497704,0.00036577016,0.0005467039],"domain_scores_gemma":[0.99827576,0.00035170565,0.0003321916,0.0005971565,0.0001435287,0.00029967277],"candidate_categories":["metaepi_narrow","sts"],"consensus_categories":[],"category_scores_codex":[0.0003931421,0.00049512304,0.0006183664,0.00035309265,0.0014699401,0.000107125896,0.00032373707,0.00034824607,0.00034075248],"category_scores_gemma":[0.00015586404,0.00046461815,0.00014727665,0.0013587332,0.0006798036,0.0012803576,0.000409163,0.00027730226,0.0000050534554],"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":[0.00017335279,0.00019153941,0.014197019,0.000015419779,0.00010714636,0.000010346708,0.0018783528,0.98177344,0.00012281082,0.000494501,0.000010229572,0.0010258463],"study_design_scores_gemma":[0.00066019205,0.0003549436,0.0021605273,0.000032331547,0.00034754662,0.000014654989,0.0010623276,0.9905263,0.00055972923,0.0036591594,0.00001524645,0.0006070257],"about_ca_topic_score_codex":0.00006945144,"about_ca_topic_score_gemma":0.000029809975,"teacher_disagreement_score":0.4174813,"about_ca_system_score_codex":0.00008422588,"about_ca_system_score_gemma":0.00004290053,"threshold_uncertainty_score":0.99983},"labels":[],"label_agreement":null},{"id":"W2312312081","doi":"10.2514/6.2015-3804","title":"Fan Response to Inlet Swirl Distortions Produced by Boundary Layer Ingesting Aircraft Configurations","year":2015,"lang":"en","type":"article","venue":"51st AIAA/SAE/ASEE Joint Propulsion Conference","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":17,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"Langley Research Center","keywords":"Boundary layer; Inlet; Mechanics; Aerodynamics; Materials science; Layer (electronics); Aerospace engineering; Mechanical engineering; Engineering; Physics; Composite material","score_opus":0.056282526052428984,"score_gpt":0.27534060700529234,"score_spread":0.21905808095286336,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2312312081","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":[0.9428185,0.00008908595,0.034031183,0.016253207,0.00047671443,0.0016357978,0.00012521158,0.0010711038,0.0034991847],"genre_scores_gemma":[0.98459125,0.0000124281505,0.011230953,0.0005645631,0.000053479846,0.00035031428,0.000058837733,0.00005035635,0.0030878375],"study_design_codex":"bench_or_experimental","study_design_gemma":"not_applicable","domain_scores_codex":[0.99639523,0.00028157723,0.000707279,0.0010854219,0.00078880216,0.0007416626],"domain_scores_gemma":[0.9978803,0.00012856282,0.00027306288,0.001012369,0.00016552064,0.0005401863],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0009054107,0.00046405537,0.0004259368,0.00018978011,0.00066014484,0.00021409417,0.00064149994,0.000220995,0.0006948829],"category_scores_gemma":[0.0029911706,0.00041842464,0.00008919527,0.00079350267,0.00057103793,0.0007821069,0.00060606515,0.00055447273,0.0015911896],"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":[0.00023756332,0.00021153444,0.0032784662,0.0000142961835,0.000011228608,0.000031276682,0.0010077289,0.00025266717,0.94009006,0.00039112088,0.03464492,0.019829124],"study_design_scores_gemma":[0.0025285205,0.0023137096,0.05691418,0.00046814143,0.00009152635,0.00012898202,0.003668293,0.0009796016,0.42898378,0.011474766,0.48989797,0.0025505524],"about_ca_topic_score_codex":0.00017613075,"about_ca_topic_score_gemma":0.00037877017,"teacher_disagreement_score":0.5111063,"about_ca_system_score_codex":0.0006031375,"about_ca_system_score_gemma":0.00023291506,"threshold_uncertainty_score":0.9998267},"labels":[],"label_agreement":null},{"id":"W2312387668","doi":"10.2514/6.2014-3005","title":"Projet Pégase: Increasing Interest in STEM Through Design and Flight of a Human Powered Aircraft","year":2014,"lang":"en","type":"article","venue":"14th AIAA Aviation Technology, Integration, and Operations Conference","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"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 de Sherbrooke","funders":"","keywords":"Aeronautics; Aerospace engineering; Computer science; Automotive engineering; Engineering","score_opus":0.034498780941634874,"score_gpt":0.2666189790267816,"score_spread":0.23212019808514672,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2312387668","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":[0.490454,0.000060107028,0.50712967,0.0013441519,0.000026586236,0.00045017694,0.000004679001,0.00016306854,0.00036754727],"genre_scores_gemma":[0.95129377,0.00012494391,0.048227817,0.000055409735,0.00000680172,0.00011311023,0.000017103383,0.00001118521,0.00014984241],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9986251,0.00017519497,0.00045638139,0.0004308505,0.00010904846,0.00020340468],"domain_scores_gemma":[0.9993618,0.000088404624,0.00012406478,0.0003093168,0.00008122333,0.000035172245],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00043017627,0.00020720996,0.00026323393,0.0002524562,0.00025345947,0.00006902216,0.0002303795,0.00025207756,0.00006127835],"category_scores_gemma":[0.00030728537,0.000181999,0.000018683048,0.0005349511,0.0006656314,0.00062972726,0.00012257775,0.0002566317,0.000009310886],"study_design_candidate":"theoretical_or_conceptual","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":[0.00004169275,0.00024680878,0.09393627,0.000034918055,0.00002039477,0.0000030309363,0.002691103,0.0004943185,0.279887,0.53406465,0.00020770157,0.088372104],"study_design_scores_gemma":[0.0030787843,0.001983156,0.06618754,0.0006592997,0.00007238406,0.00010028475,0.010250805,0.08278364,0.53169245,0.30012488,0.0016235601,0.0014431899],"about_ca_topic_score_codex":0.00037721114,"about_ca_topic_score_gemma":0.0024905265,"teacher_disagreement_score":0.4608398,"about_ca_system_score_codex":0.000072761795,"about_ca_system_score_gemma":0.000029296369,"threshold_uncertainty_score":0.7421704},"labels":[],"label_agreement":null},{"id":"W2312767146","doi":"10.2514/6.2012-5407","title":"Implementing a Capstone Aircraft Design Project as an Integrated Multi-Disciplinary Development Experience","year":2012,"lang":"en","type":"article","venue":"12th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference and 14th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference","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":"Royal Military College of Canada","funders":"","keywords":"Capstone; Systems engineering; Discipline; Computer science; Engineering; Engineering management; Sociology","score_opus":0.039108351545095246,"score_gpt":0.316947553662716,"score_spread":0.27783920211762075,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2312767146","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.20329365,0.0001674301,0.79431397,0.00060874084,0.00004951125,0.0010847495,0.000025935524,0.0003343308,0.000121661746],"genre_scores_gemma":[0.6884946,0.00049042696,0.30939823,0.000052990545,0.000018339782,0.0005886604,0.00045014397,0.000021387563,0.000485216],"study_design_codex":"observational","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9965881,0.00022295941,0.0009773872,0.0010973087,0.00038539924,0.0007288269],"domain_scores_gemma":[0.9983501,0.0000886526,0.00035022,0.00052089855,0.00042990732,0.00026022957],"candidate_categories":["metaepi_narrow","sts"],"consensus_categories":[],"category_scores_codex":[0.0008141876,0.00060610427,0.00058817107,0.00094748737,0.0023335079,0.00049120066,0.00040259844,0.00043020205,0.00069170725],"category_scores_gemma":[0.00029658564,0.00052673975,0.0000663593,0.0021575831,0.00087706256,0.0030659798,0.00052877597,0.00042030888,0.000019148534],"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":[0.00029586282,0.002595501,0.49669114,0.00011133228,0.00089216273,0.000017409273,0.08549971,0.08412365,0.029794324,0.034680568,0.00020803984,0.26509032],"study_design_scores_gemma":[0.0011036542,0.0004182747,0.035762124,0.00009915237,0.00035348948,0.00003707088,0.033336904,0.914704,0.011647595,0.00083484495,0.0005622243,0.0011406571],"about_ca_topic_score_codex":0.0004995871,"about_ca_topic_score_gemma":0.002158839,"teacher_disagreement_score":0.83058035,"about_ca_system_score_codex":0.00014359645,"about_ca_system_score_gemma":0.00019782643,"threshold_uncertainty_score":0.9997184},"labels":[],"label_agreement":null},{"id":"W2314299377","doi":"10.2514/6.2002-5853","title":"Rapid Cost Modelling at the Conceptual Stage of Aircraft Design","year":2002,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"","keywords":"Conceptual design; Computer science; Stage (stratigraphy); Systems engineering; Reliability engineering; Aerospace engineering; Engineering; Human–computer interaction; Geology","score_opus":0.06978424930874941,"score_gpt":0.23437919983249222,"score_spread":0.16459495052374282,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2314299377","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":[0.030687956,0.00038788898,0.9360959,0.0004351168,0.0000386144,0.00043136164,0.0000072016405,0.00019067645,0.031725287],"genre_scores_gemma":[0.93616515,0.00031256006,0.026897,0.00021810549,0.000006182114,0.000024863177,7.0753384e-7,0.000012019733,0.036363382],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991458,0.000039948216,0.0001642016,0.00020694274,0.0002132435,0.00022988368],"domain_scores_gemma":[0.99941367,0.00016115421,0.00006067438,0.0003254567,0.0000045533357,0.000034489745],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00013806048,0.00011005384,0.00011360919,0.000014277215,0.00013324662,0.000006388298,0.00030341174,0.000058818765,0.019452212],"category_scores_gemma":[0.000023234417,0.00006881901,0.00004354718,0.00015569894,0.00085758336,0.00013019418,0.00018461845,0.00009809194,0.00067554717],"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":[0.000033057368,0.00012952511,0.0017834087,0.000005419714,0.00002069562,0.000013064307,0.0009527689,0.854515,0.029866828,0.0039741467,0.024236541,0.0844695],"study_design_scores_gemma":[0.0007316597,0.00026605258,0.0001224615,0.000009925321,0.000014855231,0.000009911826,0.0018826233,0.5293545,0.27642652,0.002499937,0.18823865,0.00044291563],"about_ca_topic_score_codex":0.000035384055,"about_ca_topic_score_gemma":0.000011194702,"teacher_disagreement_score":0.9091989,"about_ca_system_score_codex":0.00007555843,"about_ca_system_score_gemma":0.000001579788,"threshold_uncertainty_score":0.9814441},"labels":[],"label_agreement":null},{"id":"W2314652585","doi":"10.2514/6.2012-5494","title":"Multidisciplinary Design Optimization of Airframe and Trajectory Considering Cost, Noise, and Fuel Burn","year":2012,"lang":"en","type":"article","venue":"12th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference and 14th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Royal Military College of Canada","funders":"","keywords":"Airframe; Trajectory; Multidisciplinary approach; Burn-in; Noise (video); Trajectory optimization; Computer science; Multidisciplinary design optimization; Automotive engineering; Engineering; Aeronautics; Aerospace engineering; Reliability engineering; Physics","score_opus":0.024347376862905737,"score_gpt":0.2669626482280362,"score_spread":0.2426152713651305,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2314652585","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.08210748,0.0007514946,0.9146174,0.0009336913,0.000038420516,0.0009790794,0.00003513684,0.00018977166,0.0003475024],"genre_scores_gemma":[0.7690215,0.0033055416,0.22701512,0.000026871894,0.000014761249,0.00018357529,0.00011459355,0.000023312714,0.00029472797],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99775624,0.00014922972,0.00072738976,0.0007620038,0.00023355993,0.00037159293],"domain_scores_gemma":[0.99865204,0.00017150164,0.00034226943,0.00035299503,0.00026924355,0.00021196494],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00045347438,0.00044885158,0.0005821114,0.0006567368,0.0008130084,0.00021582762,0.00016255611,0.00041502592,0.0004350136],"category_scores_gemma":[0.00029022514,0.00040693692,0.00004960349,0.0011231202,0.0012631096,0.0015827796,0.00030702265,0.00029374627,0.0000032015307],"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":[0.00011912337,0.00047139023,0.4024384,0.00012846265,0.00037222015,0.0000035981338,0.008036085,0.50987285,0.012014607,0.02385419,0.0000453515,0.042643756],"study_design_scores_gemma":[0.0008500148,0.0002348616,0.05461038,0.00009022637,0.00037844776,0.00002332895,0.0050102035,0.93368167,0.002943309,0.0015801693,0.000039906132,0.00055751327],"about_ca_topic_score_codex":0.00013993018,"about_ca_topic_score_gemma":0.00041910817,"teacher_disagreement_score":0.6876023,"about_ca_system_score_codex":0.00004369859,"about_ca_system_score_gemma":0.000058088914,"threshold_uncertainty_score":0.99983823},"labels":[],"label_agreement":null},{"id":"W2315702621","doi":"10.2514/6.2015-3292","title":"Optimization of the Aerodynamic Performance of Regional and Wide-Body-Class Blended Wing-Body Aircraft","year":2015,"lang":"en","type":"article","venue":"33rd AIAA Applied Aerodynamics Conference","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":11,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto","funders":"Natural Sciences and Engineering Research Council of Canada; National Aeronautics and Space Administration","keywords":"Aerodynamics; Wing; Aerospace engineering; Class (philosophy); Computer science; Aeronautics; Engineering; Artificial intelligence","score_opus":0.014158564488038905,"score_gpt":0.207205401493448,"score_spread":0.1930468370054091,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2315702621","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":[0.94588524,0.000024598565,0.045931667,0.00040786355,0.000101098514,0.0004926344,0.000015051466,0.00011154511,0.007030323],"genre_scores_gemma":[0.9894171,0.00010679514,0.010113771,0.000078026635,0.0000070547944,0.0000313706,0.000016137432,0.000023586565,0.00020615515],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99819815,0.000041753163,0.00044800344,0.00046606545,0.00051885954,0.00032715758],"domain_scores_gemma":[0.9987538,0.00009178505,0.00038102406,0.00061078544,0.00006798919,0.000094652845],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00027496362,0.0002737585,0.00034574734,0.000060923292,0.000116490126,0.000018944675,0.00067012047,0.00017269432,0.000045016695],"category_scores_gemma":[0.00008111413,0.0002178725,0.000054124,0.0004411302,0.0012058977,0.00022709853,0.00050167134,0.00026890615,0.000011088985],"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":[0.00042263372,0.00038271624,0.09119032,0.0001784888,0.00008635024,0.0000035239811,0.00082354294,0.6168998,0.19267504,0.08493495,0.0003905375,0.012012074],"study_design_scores_gemma":[0.0016217098,0.0003032678,0.08527688,0.00013035336,0.000070332244,0.000021238926,0.00058991136,0.88814676,0.012362848,0.010455558,0.00032171016,0.00069945294],"about_ca_topic_score_codex":0.000041163355,"about_ca_topic_score_gemma":0.00007092955,"teacher_disagreement_score":0.2712469,"about_ca_system_score_codex":0.00013416902,"about_ca_system_score_gemma":0.00009194875,"threshold_uncertainty_score":0.88845825},"labels":[],"label_agreement":null},{"id":"W2316018157","doi":"10.2514/6.2012-4636","title":"Generic New Modelling Technique for Turbofan Engines Thrust","year":2012,"lang":"en","type":"article","venue":"AIAA Modeling and Simulation Technologies Conference","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université du Québec","funders":"Canada Research Chairs","keywords":"Turbofan; Thrust; Computer science; Aerospace engineering; Jet engine; Automotive engineering; Engineering","score_opus":0.06797740908771849,"score_gpt":0.2714324616768915,"score_spread":0.203455052589173,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2316018157","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.04833812,0.00047730748,0.9486852,0.00032543752,0.00005280354,0.00046623757,0.0000032324042,0.0013679252,0.00028369523],"genre_scores_gemma":[0.8086082,0.00021081259,0.19092588,0.00002666134,0.000020479578,0.00009189981,0.000004801048,0.000016865182,0.000094421455],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9988408,0.000009635342,0.00024029132,0.00034729365,0.00013568951,0.00042629632],"domain_scores_gemma":[0.99941635,0.00009591097,0.000077453544,0.00032711914,0.000026131274,0.000057051428],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001660871,0.00021993148,0.00019857494,0.000095525145,0.00020762571,0.00003799967,0.0002695925,0.00027925454,0.000029898507],"category_scores_gemma":[0.00014908939,0.0001944728,0.000043522996,0.00021805926,0.00014943758,0.00048291872,0.00021158399,0.00018497933,0.000010921175],"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":[0.000009032932,0.000014776262,0.0007512464,0.000008020268,0.000004408193,1.666015e-7,0.00009052657,0.90264016,0.005419746,0.0028140373,0.00002502877,0.08822287],"study_design_scores_gemma":[0.00015388224,0.000042587693,0.000014029244,0.000017736264,0.000011172486,0.0000024600338,0.0002931304,0.92953557,0.01109443,0.0577484,0.00082960585,0.00025702102],"about_ca_topic_score_codex":0.000039351504,"about_ca_topic_score_gemma":0.0000021332194,"teacher_disagreement_score":0.76027006,"about_ca_system_score_codex":0.00005100633,"about_ca_system_score_gemma":0.0000115326875,"threshold_uncertainty_score":0.79303706},"labels":[],"label_agreement":null},{"id":"W2317855592","doi":"10.2514/6.2007-1772","title":"Wind Tunnel Testing of a Twisted Wing for Longitudinal Control in a Joined-Wing Aircraft","year":2007,"lang":"en","type":"article","venue":"48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Victoria","funders":"University of Victoria","keywords":"Wing; Wind tunnel; Aerospace engineering; Aeronautics; Aerodynamics; Wing configuration; Engineering; Wing twist; Structural engineering; Marine engineering; Angle of attack","score_opus":0.020638677436361396,"score_gpt":0.24994658061130617,"score_spread":0.2293079031749448,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2317855592","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":[0.9775202,0.00013475216,0.019257171,0.00013302708,0.00069658435,0.0012866637,0.00045406862,0.00024758792,0.00026992967],"genre_scores_gemma":[0.97286284,0.000028543694,0.026591582,0.0001292272,0.00012747677,0.00003010708,0.00009052485,0.00006672272,0.00007297366],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.99557817,0.000102018894,0.0013343318,0.0011956078,0.00050315016,0.0012866976],"domain_scores_gemma":[0.997886,0.00046073148,0.00068869576,0.0006058708,0.00012240419,0.00023630656],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00069258193,0.00078431494,0.0011953274,0.000284635,0.00036009445,0.00018704837,0.00073398295,0.00044577618,0.00025645972],"category_scores_gemma":[0.00073206896,0.00069786207,0.00013367114,0.0004439568,0.0009951896,0.00069758424,0.0003910259,0.00040667524,0.000003981392],"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":[0.0010551943,0.000042558946,0.07610396,0.0005271394,0.00012290935,0.00010209662,0.0007436483,0.0009894597,0.8270336,0.020929616,0.00003216257,0.072317675],"study_design_scores_gemma":[0.0038893363,0.00045312935,0.8642848,0.00031221157,0.000117043586,0.00022759239,0.0006682018,0.011134419,0.03206075,0.08546681,0.00007550686,0.0013101673],"about_ca_topic_score_codex":0.0011996253,"about_ca_topic_score_gemma":0.0023068998,"teacher_disagreement_score":0.79497284,"about_ca_system_score_codex":0.00032833384,"about_ca_system_score_gemma":0.00007235142,"threshold_uncertainty_score":0.99954724},"labels":[],"label_agreement":null},{"id":"W2317890969","doi":"10.2514/6.2012-1721","title":"Airworthiness Evaluation of a Scaled Joined-Wing Aircraft","year":2012,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":9,"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 Victoria","funders":"","keywords":"Airworthiness; Aeronautics; Wing; Aerospace engineering; Computer science; Engineering; Automotive engineering; Marine engineering; Certification; Political science","score_opus":0.03123176681103423,"score_gpt":0.27969287648872176,"score_spread":0.24846110967768753,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2317890969","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":[0.9314733,0.00011438039,0.028689628,0.00016841738,0.000109437555,0.00024439127,7.071271e-7,0.00019114088,0.03900859],"genre_scores_gemma":[0.9849725,0.0000046195187,0.014571096,0.00005210601,0.00001728713,0.000020499225,0.0000013041983,0.000006775286,0.00035385377],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.99904656,0.00003513193,0.0001546965,0.00012347725,0.0004295298,0.000210595],"domain_scores_gemma":[0.9996425,0.000030724626,0.000056011504,0.00021330177,0.000015029192,0.000042442487],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0006178091,0.00008214382,0.000102653445,0.000030464791,0.0000452928,0.000003432826,0.00012851601,0.000053913755,0.0025256444],"category_scores_gemma":[0.00013880305,0.0000637196,0.000036121317,0.00023070487,0.00012203765,0.00039618186,0.00010932326,0.00005759968,0.00021866844],"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":[0.000014878231,0.0002548768,0.51367515,0.000012043903,0.000016090236,6.214493e-7,0.0003881576,0.0034632124,0.098512456,0.0020965147,0.001176243,0.38038972],"study_design_scores_gemma":[0.0013174543,0.00008568932,0.7562175,0.000031741263,0.00010035621,0.000014503839,0.0006353993,0.013541777,0.20596702,0.016141772,0.005430593,0.00051620224],"about_ca_topic_score_codex":0.000035721816,"about_ca_topic_score_gemma":0.000017848814,"teacher_disagreement_score":0.37987354,"about_ca_system_score_codex":0.00007663263,"about_ca_system_score_gemma":0.0000050519448,"threshold_uncertainty_score":0.9983862},"labels":[],"label_agreement":null},{"id":"W2318401727","doi":"10.2514/6.2013-4290","title":"New method for aircraft fuel saving using Flight Management System and its validation on the L-1011 aircraft","year":2013,"lang":"en","type":"article","venue":"2013 Aviation Technology, Integration, and Operations Conference","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":39,"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","funders":"","keywords":"Aeronautics; Aircraft fuel system; Computer science; Aerospace engineering; Automotive engineering; Flight management system; Environmental science; Flight simulator; Engineering","score_opus":0.023908374070083487,"score_gpt":0.26963289307822935,"score_spread":0.24572451900814588,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2318401727","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.040216945,0.00011200486,0.94821537,0.008774391,0.0000991712,0.0016937716,0.000009952942,0.00035225335,0.00052611984],"genre_scores_gemma":[0.76265836,0.00017715765,0.23530933,0.00014270945,0.000021335985,0.00047981745,0.000018872279,0.000015044919,0.0011773704],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9986956,0.00007284434,0.00035058294,0.00047630022,0.00016949064,0.00023519475],"domain_scores_gemma":[0.9992654,0.00010559363,0.00011347097,0.00033055994,0.00012869148,0.000056336758],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003080054,0.0002353782,0.00018357906,0.00020339599,0.00066332635,0.00021980602,0.0002647256,0.00021471413,0.00022549863],"category_scores_gemma":[0.000136196,0.0001705976,0.00003072983,0.0003885092,0.00013822854,0.0006857356,0.000120592485,0.00018767877,0.00010022936],"study_design_candidate":"theoretical_or_conceptual","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":[0.0000070117726,0.000043897733,0.001052793,0.00004253566,0.000038519665,6.0115013e-7,0.0005312494,0.0016400879,0.05074299,0.8380041,0.002418075,0.10547815],"study_design_scores_gemma":[0.0012349559,0.00041091605,0.008500558,0.00032547812,0.00016392404,0.00005040502,0.010197447,0.75146085,0.09950965,0.12042908,0.0066803037,0.0010364479],"about_ca_topic_score_codex":0.0002639554,"about_ca_topic_score_gemma":0.0002895253,"teacher_disagreement_score":0.74982077,"about_ca_system_score_codex":0.00013785395,"about_ca_system_score_gemma":0.000023489421,"threshold_uncertainty_score":0.6956768},"labels":[],"label_agreement":null},{"id":"W2319228435","doi":"10.1115/gt2003-38785","title":"An Output-Based Approach to Emissions Standards for Gas Turbine Facilities","year":2003,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Environment and Climate Change Canada","funders":"","keywords":"NOx; Environmental science; Gas turbines; Combustion; Automotive engineering; Thermal efficiency; Reliability (semiconductor); Turbine; Process engineering; Power (physics); Engineering; Mechanical engineering; Chemistry","score_opus":0.024261558527777415,"score_gpt":0.26622348182620287,"score_spread":0.24196192329842545,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2319228435","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.012807097,0.000010115457,0.92344517,0.0002771759,0.000031069663,0.00042276923,0.00008981364,0.0003403162,0.06257648],"genre_scores_gemma":[0.7118507,0.0000015071856,0.27774638,0.0003081422,0.000004730696,0.00011678611,0.000008380965,0.000011133358,0.009952249],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9990507,0.000018660503,0.00011557322,0.0003067979,0.00022953779,0.0002787415],"domain_scores_gemma":[0.9994849,0.000036419868,0.000017111422,0.00032239174,0.000012637263,0.00012652166],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00019767263,0.00012444828,0.000115294366,0.000032819207,0.0001470508,0.000021411013,0.00019554276,0.000062031366,0.000616882],"category_scores_gemma":[0.0002207249,0.00008283844,0.000040698007,0.00014934163,0.000115552255,0.000121145706,0.000026790109,0.000057471083,0.00003128455],"study_design_candidate":"not_applicable","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":[0.00059097423,0.0026729286,0.015551197,0.00018000377,0.00005095161,0.000010382201,0.0020846303,0.1874134,0.12211936,0.10725152,0.25864705,0.3034276],"study_design_scores_gemma":[0.00060332107,0.00056207454,0.00020759946,0.000005705286,0.0000062082695,0.0000023476812,0.0020312308,0.0044112657,0.09081524,0.013200344,0.88776916,0.00038547072],"about_ca_topic_score_codex":0.000020670415,"about_ca_topic_score_gemma":0.000011648009,"teacher_disagreement_score":0.69904363,"about_ca_system_score_codex":0.00012775464,"about_ca_system_score_gemma":0.000023533714,"threshold_uncertainty_score":0.6754425},"labels":[],"label_agreement":null},{"id":"W2319973819","doi":"10.2514/6.2014-2732","title":"Design Optimization and Staging Assignment for Long-Range Aircraft Operations","year":2014,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Royal Military College of Canada","funders":"","keywords":"Range (aeronautics); Duration (music); Automotive engineering; Computer science; Operations research; Engineering; Simulation; Aerospace engineering","score_opus":0.01792425592851808,"score_gpt":0.23769171746151255,"score_spread":0.21976746153299448,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2319973819","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0021375222,0.000012585033,0.99556035,0.00067633204,0.000026293423,0.00041309278,9.62093e-7,0.00017613257,0.0009967478],"genre_scores_gemma":[0.515478,0.000017779683,0.48349288,0.00020862326,0.00000827447,0.00008414333,0.0000028698526,0.000008728058,0.00069868704],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999411,0.000023317221,0.00009991099,0.00021593811,0.00009122815,0.00015862308],"domain_scores_gemma":[0.9997269,0.00007859588,0.000016696777,0.00013393075,0.000005365755,0.000038532846],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017218699,0.0000871053,0.000075420656,0.00002228378,0.0001770609,0.000036175345,0.00008622436,0.000042242522,0.00024246766],"category_scores_gemma":[0.000054881162,0.000072580035,0.000013663197,0.000070316666,0.00008726462,0.00023626564,0.000061567065,0.00003559175,0.000019194993],"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":[0.000005534797,0.000026105175,0.0066470504,0.000003712582,0.0000037116758,3.2689982e-7,0.00005564524,0.9694923,0.002514348,0.0010865098,0.0004805095,0.019684218],"study_design_scores_gemma":[0.00044699415,0.00016322633,0.0021820127,0.0000057953102,0.000010977784,0.000002031084,0.00007212775,0.9861836,0.0073083863,0.0021833167,0.0012420238,0.00019952947],"about_ca_topic_score_codex":0.0000114493705,"about_ca_topic_score_gemma":0.000012932964,"teacher_disagreement_score":0.5133405,"about_ca_system_score_codex":0.00004920934,"about_ca_system_score_gemma":0.000002651823,"threshold_uncertainty_score":0.2959728},"labels":[],"label_agreement":null},{"id":"W2321244448","doi":"10.2514/6.2015-0696","title":"Performance Based MDO of a Joined-Wing Regional Transport Aircraft (For Challenges in the Design of Joined Wings SPECIAL SESSION)","year":2015,"lang":"en","type":"article","venue":"56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"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 Victoria","funders":"","keywords":"Session (web analytics); Wing; Aeronautics; Computer science; Aerospace engineering; Engineering; World Wide Web","score_opus":0.05508341357008678,"score_gpt":0.24611029212993724,"score_spread":0.19102687855985045,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2321244448","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":[0.98916996,0.00013651984,0.008005636,0.0006659413,0.00046914027,0.0010340732,0.00021762634,0.00007176809,0.00022932526],"genre_scores_gemma":[0.98073316,0.00027384787,0.018550942,0.00009534595,0.0001434324,0.000049661583,0.000091856826,0.000031221603,0.000030508112],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.9970206,0.0001908388,0.0009278224,0.000679887,0.00062766485,0.0005531661],"domain_scores_gemma":[0.99851173,0.00018080346,0.0005431994,0.0005440333,0.000100505036,0.00011975164],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0007303485,0.00050054264,0.00084916083,0.00014898,0.00016164496,0.000046198802,0.0008020532,0.00028198073,0.00022839608],"category_scores_gemma":[0.00015297315,0.0003467487,0.000101557685,0.00020660773,0.0010146946,0.00042649018,0.00012425163,0.00023202268,0.0000017818365],"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":[0.010249127,0.0003282974,0.053023964,0.0034446095,0.0003144232,0.00012887528,0.017112773,0.019173924,0.42957357,0.16607726,0.0011449927,0.2994282],"study_design_scores_gemma":[0.006214428,0.0015993793,0.7454815,0.0005126144,0.0001555492,0.00015755546,0.0027929477,0.03399289,0.06257658,0.14414203,0.00066516263,0.0017093731],"about_ca_topic_score_codex":0.00019859469,"about_ca_topic_score_gemma":0.00025835328,"teacher_disagreement_score":0.69245756,"about_ca_system_score_codex":0.00011989525,"about_ca_system_score_gemma":0.00011801145,"threshold_uncertainty_score":0.99989843},"labels":[],"label_agreement":null},{"id":"W2322363495","doi":"10.2514/6.2015-3291","title":"Parametric Study of Box-Wing Aerodynamics for Minimum Drag Under Stability and Maneuverability Constraints","year":2015,"lang":"en","type":"article","venue":"33rd AIAA Applied Aerodynamics Conference","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":10,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Royal Military College of Canada","funders":"","keywords":"Aerodynamics; Drag; Parametric statistics; Wing; Aerodynamic drag; Aerospace engineering; Stability (learning theory); Zero-lift drag coefficient; Longitudinal static stability; Computer science; Lift-induced drag; Wave drag; Control theory (sociology); Engineering; Mathematics; Artificial intelligence","score_opus":0.047347518162429436,"score_gpt":0.2605644694145098,"score_spread":0.21321695125208034,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2322363495","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":[0.9190476,0.000009885141,0.076552145,0.00007302673,0.000099290366,0.001774292,0.00005272305,0.00016662921,0.0022244153],"genre_scores_gemma":[0.9883106,0.000008475556,0.011398833,0.000041934894,0.000008205797,0.00015843128,0.000018708219,0.000027287071,0.000027576705],"study_design_codex":"observational","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.99733865,0.00007817045,0.0006280656,0.00096298027,0.0004693194,0.0005227858],"domain_scores_gemma":[0.9981498,0.0004721915,0.00028969618,0.00079522625,0.00008584739,0.00020720097],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0008282613,0.0003821821,0.0005776258,0.00009567207,0.00015543473,0.000055479075,0.00054084416,0.00021360024,0.00006777681],"category_scores_gemma":[0.00032424318,0.00036488246,0.000060123555,0.000514765,0.0014176592,0.00020053092,0.0004944257,0.0003114058,0.000010335996],"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":[0.0019154174,0.008922374,0.49953592,0.00057395635,0.0004073803,0.000028890701,0.008918114,0.025620267,0.13039759,0.1377052,0.00016430639,0.1858106],"study_design_scores_gemma":[0.014207366,0.003916285,0.28796974,0.00007332099,0.0003680545,0.00003405192,0.073904425,0.20211487,0.00830257,0.40550798,0.0001590206,0.0034423186],"about_ca_topic_score_codex":0.00009564724,"about_ca_topic_score_gemma":0.00061684335,"teacher_disagreement_score":0.26780277,"about_ca_system_score_codex":0.0003163885,"about_ca_system_score_gemma":0.000072951836,"threshold_uncertainty_score":0.9998803},"labels":[],"label_agreement":null},{"id":"W2322363821","doi":"10.2514/6.2004-1095","title":"Airfoil Shape Optimization Using NURBS Representation Under Thickness Constraint","year":2004,"lang":"en","type":"article","venue":"42nd AIAA Aerospace Sciences Meeting and Exhibit","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":16,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Natural Sciences and Engineering Research Council of Canada; Fonds Québécois de la Recherche sur la Nature et les Technologies","keywords":"Airfoil; Transonic; Solver; Mach number; Representation (politics); Computer science; Mathematical optimization; Shape optimization; Flow (mathematics); Computational fluid dynamics; Mathematics; Algorithm; Aerodynamics; Aerospace engineering; Engineering; Structural engineering; Geometry; Finite element method","score_opus":0.030515210026876783,"score_gpt":0.2753654010233061,"score_spread":0.2448501909964293,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2322363821","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":[0.8979651,0.00011169253,0.091458604,0.00208783,0.00015744727,0.0001889917,0.0000017642338,0.00024547055,0.007783143],"genre_scores_gemma":[0.8982331,0.00005867514,0.10139855,0.00019583688,0.000023249377,0.0000054589104,0.0000015302511,0.000009721389,0.00007387306],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9984006,0.00004207673,0.00020195772,0.0005792158,0.00039223762,0.00038387682],"domain_scores_gemma":[0.9995205,0.000066828165,0.00013891308,0.00017351823,0.000015946764,0.00008429691],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00050067075,0.0001735474,0.00015719849,0.000056173852,0.0007628983,0.00014568253,0.00021484266,0.00010040133,0.00013682626],"category_scores_gemma":[0.00015172784,0.00014934894,0.000036422258,0.00049659825,0.0015270995,0.00056131295,0.00018158377,0.00014135867,0.000022994403],"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":[0.000005300093,0.000025243618,0.008827603,0.000004791177,0.0000030167218,0.0000042417437,0.00035861763,0.9510119,0.033136737,0.0023414677,0.000019289193,0.0042618117],"study_design_scores_gemma":[0.0038502484,0.00079414144,0.019624487,0.00094535237,0.0001197133,0.00050978904,0.04156944,0.7084737,0.15538873,0.065548666,0.00040206796,0.0027736654],"about_ca_topic_score_codex":0.00038438587,"about_ca_topic_score_gemma":0.000056996527,"teacher_disagreement_score":0.24253817,"about_ca_system_score_codex":0.00012542671,"about_ca_system_score_gemma":0.000036350106,"threshold_uncertainty_score":0.6090273},"labels":[],"label_agreement":null},{"id":"W2323926580","doi":"10.2514/6.2013-1786","title":"Design and Evaluation of Aeroelastically Tuned Joined-Wing SensorCraft Flight Test Article","year":2013,"lang":"en","type":"article","venue":"54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":5,"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 Victoria","funders":"Air Force Research Laboratory","keywords":"Wing; Test (biology); Aeronautics; Computer science; Flight test; Aerospace engineering; Engineering; Simulation; Geology","score_opus":0.015604447908614792,"score_gpt":0.2341065021679391,"score_spread":0.2185020542593243,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2323926580","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":[0.9836744,0.00011953865,0.013487745,0.00034570156,0.00041860892,0.0013590464,0.00011568824,0.00022346455,0.0002558048],"genre_scores_gemma":[0.97124666,0.0001243021,0.028192857,0.000099115474,0.000061076906,0.00006732176,0.000051299936,0.000046728175,0.00011066384],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.9963292,0.0002834816,0.0008625385,0.00096541946,0.00077433867,0.0007850041],"domain_scores_gemma":[0.9981972,0.00032084106,0.00041627366,0.00059400115,0.00020468539,0.00026701414],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0004974691,0.00063285884,0.0007617465,0.00012628133,0.00034530656,0.00031355483,0.00046250384,0.00035165157,0.002315988],"category_scores_gemma":[0.0006228205,0.00051261915,0.00006282872,0.00022430028,0.0011672539,0.00076067756,0.0004496701,0.00027427313,0.000037804468],"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":[0.00011843766,0.000026434516,0.0040510087,0.00011964244,0.00006484154,0.000010598119,0.00046844984,0.00073016604,0.9130604,0.009985598,0.0001218712,0.07124255],"study_design_scores_gemma":[0.0024837875,0.0005173876,0.43259037,0.00012601784,0.0002625257,0.00018540146,0.0004942705,0.115487374,0.22419772,0.22231133,0.000034104483,0.0013097364],"about_ca_topic_score_codex":0.00044648425,"about_ca_topic_score_gemma":0.00015314098,"teacher_disagreement_score":0.6888627,"about_ca_system_score_codex":0.00018237905,"about_ca_system_score_gemma":0.00006334326,"threshold_uncertainty_score":0.99973255},"labels":[],"label_agreement":null},{"id":"W2325120349","doi":"10.2514/6.2015-1031","title":"Demonstration of a Conceptual Design Tool for Multiple Lifting Elements","year":2015,"lang":"en","type":"article","venue":"53rd AIAA Aerospace Sciences Meeting","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Toronto Metropolitan University","funders":"","keywords":"Conceptual design; Computer science; Systems engineering; Engineering drawing; Software engineering; Human–computer interaction; Engineering","score_opus":0.06855099224242103,"score_gpt":0.2854113509789116,"score_spread":0.2168603587364906,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2325120349","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":[0.6763554,0.000068553374,0.31908467,0.0002847841,0.00015319983,0.0006986821,0.0000049435303,0.00016939391,0.0031803735],"genre_scores_gemma":[0.6906907,0.0000034018035,0.30908883,0.000040191786,0.000017705413,0.000036166457,0.0000010180258,0.000006774898,0.00011525453],"study_design_codex":"observational","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99827695,0.000065414926,0.00033925654,0.00040652166,0.0004807111,0.00043115666],"domain_scores_gemma":[0.9990567,0.00037669687,0.00029657668,0.00016058347,0.000036534002,0.000072940216],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0018188363,0.0001489939,0.00017919164,0.00004142709,0.00025441646,0.000039957064,0.00041397574,0.00006995419,0.000018096538],"category_scores_gemma":[0.0017350889,0.00012945788,0.00004824956,0.00047145836,0.0013149242,0.00051748974,0.00016682757,0.000077542616,0.00002185977],"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":[0.00008227825,0.00011811416,0.45724368,0.000017880635,0.000013589579,0.000002371875,0.0032540252,0.08397411,0.41977185,0.0021977888,0.0025128536,0.030811444],"study_design_scores_gemma":[0.003078833,0.0020873006,0.0029343227,0.00020234859,0.000041156432,0.000011175378,0.03286829,0.18235056,0.761931,0.00994402,0.0034677861,0.001083206],"about_ca_topic_score_codex":0.000051265673,"about_ca_topic_score_gemma":0.00003538212,"teacher_disagreement_score":0.45430934,"about_ca_system_score_codex":0.00009324392,"about_ca_system_score_gemma":0.0000480923,"threshold_uncertainty_score":0.5279139},"labels":[],"label_agreement":null},{"id":"W2325177980","doi":"10.2514/6.2004-454","title":"Comparison of Optimization Algorithms Applied to Aerodynamic Design","year":2004,"lang":"en","type":"article","venue":"42nd AIAA Aerospace Sciences Meeting and Exhibit","topic":"Advanced Aircraft Design and Technologies","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":"University of Toronto","funders":"","keywords":"Aerodynamics; Computer science; Optimization algorithm; Algorithm design; Algorithm; Mathematical optimization; Engineering; Aerospace engineering; Mathematics","score_opus":0.02608644645479334,"score_gpt":0.2845203022060978,"score_spread":0.25843385575130445,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2325177980","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":[0.42668033,0.00010381574,0.56545913,0.0008056857,0.000085769396,0.00038381285,0.0000013950284,0.00019221581,0.006287872],"genre_scores_gemma":[0.68781394,0.000017026532,0.3120398,0.000054709395,0.0000075035705,0.00001088418,6.126116e-7,0.0000065809363,0.000048967107],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9985472,0.00002372395,0.0002349349,0.00047809514,0.00036587944,0.00035017348],"domain_scores_gemma":[0.9995202,0.000069524525,0.00013263142,0.00017251812,0.000010354501,0.00009481632],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005373877,0.00016136661,0.00023238864,0.00006882357,0.000360603,0.000050252012,0.0002967372,0.00007255187,0.000028162081],"category_scores_gemma":[0.00010186594,0.00013737362,0.000025706788,0.000743207,0.0006714893,0.00017412174,0.00020031918,0.00009715594,0.000032833235],"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":[0.000008300244,0.00003780897,0.0047915815,0.0000045489633,0.0000018071444,5.522341e-7,0.00055133255,0.9383533,0.050623097,0.0003341767,0.000062780906,0.0052307383],"study_design_scores_gemma":[0.0027326504,0.002806558,0.015951946,0.0005151645,0.00007431535,0.000028467963,0.014077954,0.21503767,0.7317615,0.014108491,0.0006468117,0.0022584656],"about_ca_topic_score_codex":0.00011587921,"about_ca_topic_score_gemma":0.00003704798,"teacher_disagreement_score":0.7233156,"about_ca_system_score_codex":0.00007079265,"about_ca_system_score_gemma":0.000018921519,"threshold_uncertainty_score":0.56019336},"labels":[],"label_agreement":null},{"id":"W2325937409","doi":"10.2514/6.2011-642","title":"Preliminary Aerodynamic Shape Optimization of a Blended-Wing-Body Aircraft Configuration","year":2011,"lang":"en","type":"article","venue":"49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":36,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto","funders":"University of Toronto","keywords":"Aerodynamics; Wing; Aerospace engineering; Wing configuration; Computer science; Wing twist; Acoustics; Structural engineering; Automotive engineering; Engineering; Angle of attack; Physics","score_opus":0.020505108331782235,"score_gpt":0.24420246662157105,"score_spread":0.22369735828978882,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2325937409","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":[0.83355355,0.00038952412,0.1506696,0.0057011405,0.00046508235,0.0010363775,0.0000095117675,0.0005276466,0.0076475423],"genre_scores_gemma":[0.9470399,0.0001891866,0.05226661,0.0000998859,0.000042213283,0.00003540808,0.000007981093,0.000027053125,0.00029177996],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99746317,0.00013604357,0.00043969232,0.00071772747,0.0005914256,0.0006519612],"domain_scores_gemma":[0.9987408,0.00018456615,0.00050425506,0.00039238465,0.00003809167,0.00013989507],"candidate_categories":["metaepi_narrow","sts"],"consensus_categories":[],"category_scores_codex":[0.0007911385,0.00035332795,0.00030856047,0.000121671525,0.0015178707,0.0001038369,0.00063813315,0.00017961064,0.00019142397],"category_scores_gemma":[0.00023712534,0.0002735158,0.000096106094,0.0009530859,0.00139394,0.0010642235,0.00053846353,0.0002653213,0.000025580652],"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":[0.0005606262,0.00047096814,0.06306927,0.00009157718,0.00008865066,0.00001576465,0.0089125065,0.14112654,0.7326225,0.013652573,0.005534407,0.033854596],"study_design_scores_gemma":[0.0030525983,0.009565179,0.032343905,0.0012932663,0.00036494894,0.00019916674,0.028468557,0.4634647,0.43476322,0.023211494,0.00063872605,0.00263422],"about_ca_topic_score_codex":0.00044379555,"about_ca_topic_score_gemma":0.00014723705,"teacher_disagreement_score":0.32233816,"about_ca_system_score_codex":0.00013302719,"about_ca_system_score_gemma":0.00006051848,"threshold_uncertainty_score":0.9999717},"labels":[],"label_agreement":null},{"id":"W2326268642","doi":"10.2514/6.2012-5495","title":"Coupled Optimization of Aircraft Family Design and Fleet Assignment for Minimum Cost and Fuel Burn","year":2012,"lang":"en","type":"article","venue":"12th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference and 14th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":14,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Royal Military College of Canada","funders":"","keywords":"Computer science; Automotive engineering; Aeronautics; Engineering; Environmental science; Aerospace engineering","score_opus":0.02411104330554752,"score_gpt":0.2730401446938177,"score_spread":0.24892910138827018,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2326268642","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.045301173,0.0006165653,0.95083696,0.0013918999,0.000045838216,0.0015357123,0.000063699896,0.0001279124,0.00008026983],"genre_scores_gemma":[0.75462925,0.0034668532,0.24096212,0.00005140101,0.000015625848,0.00041434175,0.00027582957,0.00001643733,0.00016811832],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99776465,0.00011753893,0.0007589943,0.000739949,0.0002436277,0.00037523732],"domain_scores_gemma":[0.99852663,0.00021168742,0.00034919352,0.0003226405,0.00039908694,0.00019076401],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0005817853,0.00042467646,0.0005804673,0.00059766555,0.0008530772,0.00024563624,0.00017131191,0.0003979431,0.00016196894],"category_scores_gemma":[0.0002932464,0.0003774821,0.000053481737,0.0009614937,0.00093552336,0.001456085,0.00021075679,0.00020916003,0.0000014438881],"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":[0.0002441825,0.0006285758,0.12066038,0.00016206989,0.0005077764,0.0000014981746,0.0059631476,0.760788,0.020119134,0.037906867,0.00011894398,0.052899394],"study_design_scores_gemma":[0.0010113314,0.00033030065,0.013493065,0.000058232563,0.0004219902,0.000007506695,0.0036951008,0.97642964,0.0020695748,0.0019694665,0.00006276855,0.00045100544],"about_ca_topic_score_codex":0.00010393927,"about_ca_topic_score_gemma":0.00020409226,"teacher_disagreement_score":0.7098748,"about_ca_system_score_codex":0.000059147787,"about_ca_system_score_gemma":0.00006475144,"threshold_uncertainty_score":0.99986774},"labels":[],"label_agreement":null},{"id":"W2326295965","doi":"10.2514/6.2005-7051","title":"Unmanned Aerial Vehicle Conceptual Design Using a Genetic Algorithm and Data Mining","year":2005,"lang":"en","type":"article","venue":"Infotech@Aerospace","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":14,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Computer science; Genetic algorithm; Algorithm design; Data mining; Conceptual design; Artificial intelligence; Algorithm; Machine learning; Human–computer interaction","score_opus":0.05150348107750149,"score_gpt":0.27662752309249417,"score_spread":0.22512404201499267,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2326295965","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":[0.40680203,0.00025720088,0.5917179,0.00035442962,0.000084355044,0.0002995779,0.000017092209,0.0003176838,0.00014975964],"genre_scores_gemma":[0.36608115,0.000046601326,0.6334544,0.00018007026,0.0000797504,0.000007571427,0.0000039310457,0.000021948832,0.00012458724],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99847203,0.000046858022,0.00022466735,0.0005498349,0.0002613326,0.00044529288],"domain_scores_gemma":[0.9989739,0.0000966638,0.00010613399,0.0007114743,0.000007470588,0.000104332896],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021146006,0.0002236231,0.00020267427,0.00003827834,0.00022017218,0.000066431625,0.0006062307,0.0001745337,0.0001723165],"category_scores_gemma":[0.00012802973,0.00022014593,0.000021197262,0.00025160384,0.00070285535,0.0006141331,0.0009377624,0.00018228297,0.000107596956],"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":[0.00007282008,0.0001029935,0.0027415648,0.000007614876,0.000039345992,0.000058426067,0.0014896137,0.041535553,0.15232188,0.00008765964,0.004376042,0.79716647],"study_design_scores_gemma":[0.003375668,0.00056605233,0.006022178,0.00008761418,0.00009506567,0.00016557543,0.0025720135,0.83602,0.102528974,0.0013249887,0.045521595,0.001720259],"about_ca_topic_score_codex":0.00009744456,"about_ca_topic_score_gemma":0.00001739237,"teacher_disagreement_score":0.7954462,"about_ca_system_score_codex":0.00012365308,"about_ca_system_score_gemma":0.000020617008,"threshold_uncertainty_score":0.89772904},"labels":[],"label_agreement":null},{"id":"W2327608046","doi":"10.2514/6.2012-5589","title":"Sizing of a Short Range Civil Transport Aircraft Considering Aero-Structural and Stability Effects","year":2012,"lang":"en","type":"article","venue":"12th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference and 14th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":3,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Royal Military College of Canada","funders":"","keywords":"Sizing; Range (aeronautics); Stability (learning theory); Structural stability; Aerospace engineering; Computer science; Structural engineering; Engineering; Materials science; Environmental science; Automotive engineering; Chemistry","score_opus":0.016070869073989733,"score_gpt":0.2553887835450558,"score_spread":0.23931791447106604,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2327608046","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":[0.51434344,0.00033964604,0.48395616,0.00050971046,0.000032788386,0.0005296479,0.000029375815,0.00011410996,0.00014513487],"genre_scores_gemma":[0.9411375,0.0010178644,0.057416517,0.00002845835,0.0000152108205,0.00015912404,0.00015339034,0.000014434438,0.00005753598],"study_design_codex":"observational","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9979034,0.00010670443,0.0007045488,0.00068429095,0.00024577312,0.00035529636],"domain_scores_gemma":[0.9988603,0.00015280902,0.00020084964,0.00035570766,0.00026276562,0.00016756271],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00040213525,0.00039666222,0.00059149036,0.00047346554,0.00082447275,0.00013059018,0.00016424665,0.00033885802,0.00031794954],"category_scores_gemma":[0.0002523955,0.0003475661,0.00006702087,0.0010586765,0.0011095409,0.0015934224,0.00017816383,0.00029564058,0.0000015494334],"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":[0.00004178083,0.00013080881,0.9381345,0.000089803034,0.00017687413,0.0000021549902,0.004566087,0.0075901644,0.015488601,0.012095638,0.0000048847864,0.021678703],"study_design_scores_gemma":[0.0010119395,0.00030608597,0.3706836,0.00013926743,0.0007205006,0.000033072727,0.0065053985,0.5943733,0.022039482,0.0033064985,0.0000327085,0.00084814586],"about_ca_topic_score_codex":0.00021725986,"about_ca_topic_score_gemma":0.0015413762,"teacher_disagreement_score":0.5867831,"about_ca_system_score_codex":0.00005132555,"about_ca_system_score_gemma":0.000049605052,"threshold_uncertainty_score":0.99989766},"labels":[],"label_agreement":null},{"id":"W2327897272","doi":"10.2514/6.2013-2414","title":"Aerodynamic Shape Optimization of a Blended-Wing-Body Regional Transport for a Short Range Mission","year":2013,"lang":"en","type":"article","venue":"31st AIAA Applied Aerodynamics Conference","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":30,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto","funders":"Natural Sciences and Engineering Research Council of Canada; Western Canada Research Grid; Compute Canada","keywords":"Aerodynamics; Wing; Aerospace engineering; Range (aeronautics); Computer science; Aeronautics; Environmental science; Marine engineering; Engineering","score_opus":0.018132455078577366,"score_gpt":0.22874446295949122,"score_spread":0.21061200788091386,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2327897272","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":[0.46400702,0.00001653879,0.52803946,0.00055241206,0.000079642334,0.0018730048,0.000042000283,0.00031994018,0.0050699892],"genre_scores_gemma":[0.94457924,0.00008084835,0.05451429,0.000092152564,0.000016303275,0.0003042282,0.00016060118,0.000043286076,0.00020902597],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9978687,0.000018031804,0.00052405667,0.00069242757,0.00040299707,0.0004937679],"domain_scores_gemma":[0.99902225,0.00009560986,0.0001894249,0.0004994682,0.000067570574,0.00012565167],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00017659526,0.00035599124,0.00041456378,0.00009293883,0.000161936,0.000027423424,0.0006058239,0.00026000402,0.001147948],"category_scores_gemma":[0.000027916038,0.00033252136,0.00012313605,0.00033449117,0.00045528592,0.00030190026,0.000114399874,0.00022018579,0.00005274788],"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":[0.00042974416,0.00075887825,0.011597104,0.00024907,0.00010948241,0.0000060309367,0.000610483,0.22448216,0.5840334,0.046264652,0.0008779157,0.13058107],"study_design_scores_gemma":[0.001034456,0.0001780114,0.031091683,0.00006722256,0.000059190752,0.0000066871867,0.0002984319,0.9503312,0.0019419807,0.01384897,0.00042645348,0.0007156919],"about_ca_topic_score_codex":0.000059275917,"about_ca_topic_score_gemma":0.00008481651,"teacher_disagreement_score":0.72584903,"about_ca_system_score_codex":0.0001464154,"about_ca_system_score_gemma":0.000055545886,"threshold_uncertainty_score":0.9999127},"labels":[],"label_agreement":null},{"id":"W2329066791","doi":"10.2514/6.2012-5649","title":"Conceptual Design Framework for Blended Wing Body Aircraft","year":2012,"lang":"en","type":"article","venue":"12th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference and 14th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":7,"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":"Wing; Computer science; Conceptual design; Aeronautics; Aerospace engineering; Human–computer interaction; Systems engineering; Engineering","score_opus":0.026624714203787845,"score_gpt":0.28525336008639035,"score_spread":0.2586286458826025,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2329066791","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.031488404,0.00029471677,0.96365947,0.0027273064,0.00008848477,0.0012119664,0.0000574387,0.00031484303,0.00015736038],"genre_scores_gemma":[0.67509323,0.0007970425,0.32298332,0.00008186776,0.000037321297,0.000445431,0.0002464038,0.000018266246,0.00029712886],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99746895,0.00013904969,0.00074006605,0.0008522167,0.00027202198,0.00052772154],"domain_scores_gemma":[0.99838555,0.0002841681,0.00029115516,0.00044493043,0.00037957574,0.00021460104],"candidate_categories":["metaepi_narrow","sts"],"consensus_categories":[],"category_scores_codex":[0.00054626586,0.00048434403,0.0005707135,0.0006147551,0.0015272327,0.00034100589,0.00028617846,0.00054788054,0.00062867487],"category_scores_gemma":[0.00062888523,0.00043435805,0.00009211464,0.001434016,0.001070963,0.0019359308,0.00022750068,0.00038235117,0.000012110786],"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":[0.00017532476,0.00066211034,0.13551603,0.000054009077,0.00062932144,0.0000025968636,0.009703523,0.13266213,0.012509496,0.6476741,0.00027812587,0.060133263],"study_design_scores_gemma":[0.0010424155,0.0004359747,0.018385539,0.000098222976,0.0006733993,0.000013233173,0.009858711,0.9339659,0.008982769,0.025234994,0.00035302434,0.0009558213],"about_ca_topic_score_codex":0.00008012955,"about_ca_topic_score_gemma":0.0002312877,"teacher_disagreement_score":0.80130374,"about_ca_system_score_codex":0.00008467948,"about_ca_system_score_gemma":0.00009051268,"threshold_uncertainty_score":0.9998108},"labels":[],"label_agreement":null},{"id":"W2329173197","doi":"10.2514/6.2008-5967","title":"Aero-Structural Optimization of Non-Planar Lifting Surface Configurations","year":2008,"lang":"en","type":"article","venue":"12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":10,"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":"Planar; Surface (topology); Computer science; Geometry; Mathematics; Computer graphics (images)","score_opus":0.017304800323849494,"score_gpt":0.2533015251227551,"score_spread":0.23599672479890563,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2329173197","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":[0.25288686,0.000039573413,0.7454556,0.00017819855,0.000030964522,0.0002066005,0.000025955313,0.000089263776,0.0010869992],"genre_scores_gemma":[0.7487332,0.0003161866,0.25053182,0.00001564399,0.0000083698005,0.000008872916,0.0001524319,0.000011736006,0.0002217275],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99827504,0.000059145113,0.0005356988,0.0005420577,0.00030651205,0.00028155142],"domain_scores_gemma":[0.99892044,0.000106384585,0.0003705305,0.00037234684,0.00011302227,0.00011728919],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00014405133,0.0002660631,0.00044108654,0.00017152655,0.000646497,0.000041388153,0.00026646696,0.00014757352,0.0014119822],"category_scores_gemma":[0.00009134698,0.00024172854,0.00011610412,0.0013489339,0.00054434274,0.0006453565,0.00016456046,0.00015704027,0.000009152035],"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":[0.000021223357,0.000034742126,0.08291019,0.0000073835317,0.00007714238,0.0000057145658,0.0005469399,0.9123178,0.0035178042,0.00008244144,0.000020507325,0.00045808856],"study_design_scores_gemma":[0.00033274203,0.00007457671,0.04410032,0.000013987258,0.00018126673,0.000009999606,0.0004022037,0.95194983,0.0025522902,0.000090817826,0.000009362335,0.0002826033],"about_ca_topic_score_codex":0.0001462477,"about_ca_topic_score_gemma":0.000054954795,"teacher_disagreement_score":0.49584636,"about_ca_system_score_codex":0.000045179382,"about_ca_system_score_gemma":0.00003167071,"threshold_uncertainty_score":0.9995009},"labels":[],"label_agreement":null},{"id":"W2330981005","doi":"10.2514/6.2015-2793","title":"Multidisciplinary Analysis of a Box-Wing Aircraft Designed for a Regional-Jet Mission","year":2015,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Royal Military College of Canada","funders":"","keywords":"Multidisciplinary approach; Wing; Aerospace engineering; Jet (fluid); Aeronautics; Wing configuration; Computer science; Systems engineering; Engineering; Political science","score_opus":0.05337556303075773,"score_gpt":0.30246151973240937,"score_spread":0.24908595670165162,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2330981005","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":[0.2607496,0.00007086663,0.72436416,0.0006700559,0.000024641888,0.00046285696,0.000005453167,0.00033215943,0.013320196],"genre_scores_gemma":[0.8022817,0.000004665455,0.19338107,0.000040076422,0.0000045769684,0.000018678027,0.0000059292242,0.000013818375,0.0042494847],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99917275,0.00001812826,0.00017833711,0.00026105912,0.00018995539,0.00017978689],"domain_scores_gemma":[0.99946874,0.000091445596,0.00008058459,0.0002593266,0.0000123459395,0.00008752889],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018387794,0.00010882894,0.00021435157,0.00013466268,0.000052712803,0.0000046740483,0.00019578976,0.00007080157,0.00031564015],"category_scores_gemma":[0.00008817316,0.00008052681,0.00012311552,0.00066132937,0.00014335221,0.000121850724,0.00013885449,0.000034389363,0.00003537541],"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":[0.0005245586,0.0007906906,0.24701995,0.000034314835,0.0006926672,0.000024184175,0.002214026,0.04941941,0.6176516,0.0033907846,0.035722915,0.04251491],"study_design_scores_gemma":[0.0061669005,0.0020289284,0.11711211,0.000113798684,0.0019687945,0.000018080244,0.010964081,0.35448802,0.38003328,0.07833238,0.046639834,0.002133813],"about_ca_topic_score_codex":0.00007854903,"about_ca_topic_score_gemma":0.00005988571,"teacher_disagreement_score":0.5415321,"about_ca_system_score_codex":0.00006796787,"about_ca_system_score_gemma":0.000009170828,"threshold_uncertainty_score":0.34560382},"labels":[],"label_agreement":null},{"id":"W2331618308","doi":"10.2514/6.2013-1317","title":"Hybrids...the Airship Messiah?","year":2013,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":18,"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":"Messiah; Computer science; Geography","score_opus":0.009667846640436701,"score_gpt":0.2024985980206877,"score_spread":0.192830751380251,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2331618308","genre_codex":"other","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":[0.34125963,0.000070062444,0.030745247,0.014886594,0.00013060347,0.000550807,5.68563e-7,0.00097574724,0.61138076],"genre_scores_gemma":[0.98231393,0.000007001059,0.004083566,0.0008274642,0.00000918116,0.00004447466,2.572492e-7,0.0000052551086,0.012708863],"study_design_codex":"design_other","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.99949646,0.000011154548,0.000068643494,0.00013397171,0.00011307172,0.00017671012],"domain_scores_gemma":[0.9996612,0.000038939583,0.000017173514,0.00025196746,0.0000019446902,0.000028750246],"candidate_categories":["insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.000051861007,0.00006526366,0.000046158846,0.0000072420703,0.0000938158,0.000021915557,0.00028632488,0.00002659753,0.012272186],"category_scores_gemma":[0.000028785327,0.000034907724,0.000022677059,0.0001118743,0.0002230488,0.00019088338,0.00013991921,0.00007949465,0.010644766],"study_design_candidate":"not_applicable","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":[0.0000034683508,0.000077600875,0.050941728,0.0000032352716,0.000011804534,0.000009720665,0.00015346156,0.00036870164,0.029528657,0.021144342,0.30751964,0.5902376],"study_design_scores_gemma":[0.00039945508,0.00011728929,0.24650486,0.00000771044,0.000010388405,0.000041461775,0.0011922158,0.003680666,0.068124466,0.36374488,0.31553704,0.00063957163],"about_ca_topic_score_codex":0.00014935137,"about_ca_topic_score_gemma":0.000016958804,"teacher_disagreement_score":0.64105433,"about_ca_system_score_codex":0.000026712873,"about_ca_system_score_gemma":0.0000012847678,"threshold_uncertainty_score":0.99012554},"labels":[],"label_agreement":null},{"id":"W2331692794","doi":"10.2514/6.2004-4435","title":"Flight Dynamics and Control Multidisciplinary Integration in Aircraft Conceptual Design Optimization","year":2004,"lang":"en","type":"article","venue":"10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University; University of Toronto","funders":"","keywords":"Multidisciplinary design optimization; Multidisciplinary approach; Conceptual design; Computer science; Systems engineering; Dynamics (music); Control (management); Flight dynamics; Control engineering; Aerospace engineering; Aerodynamics; Engineering; Human–computer interaction; Artificial intelligence; Physics","score_opus":0.014330914014408768,"score_gpt":0.2448772049214,"score_spread":0.23054629090699122,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2331692794","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.041480444,0.00012888949,0.9562941,0.0009694743,0.000045492838,0.0006488964,0.000029696717,0.00016549809,0.0002374713],"genre_scores_gemma":[0.7237395,0.0004743455,0.27539715,0.000035735033,0.0000102847935,0.00006970135,0.00014349089,0.000019878156,0.00010991439],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99746794,0.00017782846,0.0006495978,0.0009424451,0.0003263141,0.00043589078],"domain_scores_gemma":[0.9989002,0.00017548751,0.00028497697,0.00037897643,0.00008113802,0.00017922465],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00040976636,0.00043351654,0.0005755843,0.0004349185,0.00045934366,0.0001345648,0.000272028,0.00028069023,0.00031618972],"category_scores_gemma":[0.00014937563,0.00039342398,0.000097458884,0.0015065009,0.00080126064,0.0010964634,0.00031308553,0.00030132043,0.000009658326],"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":[0.000111341964,0.00015392998,0.029971637,0.0000060528578,0.000056715435,0.000017862763,0.0010525025,0.96327525,0.00039398778,0.0011855684,0.0000024643641,0.0037726827],"study_design_scores_gemma":[0.0018175509,0.00021410883,0.022348322,0.000048232432,0.00022780645,0.000008332019,0.001828995,0.971171,0.00051599095,0.0013404083,0.0000018079755,0.0004774087],"about_ca_topic_score_codex":0.00016167911,"about_ca_topic_score_gemma":0.00068943074,"teacher_disagreement_score":0.6822591,"about_ca_system_score_codex":0.00027881007,"about_ca_system_score_gemma":0.000043924025,"threshold_uncertainty_score":0.99985176},"labels":[],"label_agreement":null},{"id":"W2332806700","doi":"10.2514/6.2015-2558","title":"Aero structural modeling of a wing using CATIA V5 and XFLR5 software and experimental validation using the Price- Païdoussis wing tunnel","year":2015,"lang":"en","type":"article","venue":"AIAA Atmospheric Flight Mechanics Conference","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":32,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université du Québec","funders":"","keywords":"Wing; Software; Computer science; Simulation; Structural engineering; Aerospace engineering; Engineering; Aeronautics; Operating system","score_opus":0.048026585439434055,"score_gpt":0.2579645333508146,"score_spread":0.20993794791138054,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2332806700","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":[0.6193621,0.00026092937,0.38001075,0.000027266115,0.00007309221,0.000174715,0.0000014427502,0.000058116122,0.000031553336],"genre_scores_gemma":[0.8209419,0.000024953808,0.17895488,0.000029481307,0.000011880454,0.0000070182286,0.0000014583371,0.000019044934,0.000009322426],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9986113,0.000056789606,0.00029827174,0.00041483296,0.00031468834,0.00030411888],"domain_scores_gemma":[0.9993297,0.00005168072,0.00019088252,0.0002916486,0.000039797775,0.000096278236],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020507505,0.00024134589,0.00024996058,0.00000701317,0.00028486163,0.00007571972,0.0002592191,0.00010940017,0.000041491807],"category_scores_gemma":[0.000099291065,0.00018639288,0.00003181528,0.00025894877,0.0001467657,0.00054593326,0.00044869215,0.00015582381,0.0000012960651],"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":[0.00008093649,0.000059343864,0.0066762986,0.00005691732,0.00007114915,0.000016324786,0.009869059,0.2864504,0.6769318,0.0044657397,0.000010752152,0.015311276],"study_design_scores_gemma":[0.00030695906,0.000064443644,0.00008406263,0.000054674292,0.00003269251,0.000040558883,0.0037063381,0.95934904,0.026195899,0.0098993955,0.000011400856,0.00025453445],"about_ca_topic_score_codex":0.0003688624,"about_ca_topic_score_gemma":0.000010728255,"teacher_disagreement_score":0.67289865,"about_ca_system_score_codex":0.00016892336,"about_ca_system_score_gemma":0.000043435663,"threshold_uncertainty_score":0.7600881},"labels":[],"label_agreement":null},{"id":"W2333840830","doi":"10.2514/6.2001-1432","title":"Aircraft loads methodology for MDO","year":2001,"lang":"en","type":"article","venue":"19th AIAA Applied Aerodynamics Conference","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Bombardier (Canada)","funders":"","keywords":"Computer science; Aerospace engineering; Aeronautics; Engineering","score_opus":0.04653456285609414,"score_gpt":0.276203338691874,"score_spread":0.22966877583577988,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2333840830","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.079008296,0.000025093426,0.88041836,0.0006467698,0.00018322363,0.0007793789,0.00002099565,0.0005321292,0.03838578],"genre_scores_gemma":[0.8310394,0.000100059835,0.16646887,0.0004143091,0.00003379048,0.00028335757,0.000032685344,0.000034690205,0.0015928004],"study_design_codex":"design_other","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.99790895,0.000042200667,0.00034429113,0.0007573042,0.00023405715,0.00071319105],"domain_scores_gemma":[0.99874645,0.00033129612,0.00014870864,0.0006179366,0.000025215422,0.00013040037],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00040009167,0.00033263737,0.00038701115,0.000068839116,0.00022040286,0.000041479343,0.0007456336,0.00026491028,0.00085276685],"category_scores_gemma":[0.00013924802,0.0003162006,0.000091509966,0.0003553793,0.00054014433,0.00014552512,0.00032073117,0.00028631414,0.00049163157],"study_design_candidate":"theoretical_or_conceptual","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":[0.00033946737,0.0002251363,0.0065289605,0.000034318247,0.00005347261,0.00002821634,0.00031728362,0.004172601,0.20083636,0.32637465,0.001919838,0.4591697],"study_design_scores_gemma":[0.0033250928,0.00056840986,0.01417312,0.000033563734,0.000118162476,0.000111792986,0.0010011088,0.052357282,0.01861785,0.7477459,0.15953487,0.002412869],"about_ca_topic_score_codex":0.00004392378,"about_ca_topic_score_gemma":0.0002705544,"teacher_disagreement_score":0.75203115,"about_ca_system_score_codex":0.0001526945,"about_ca_system_score_gemma":0.000028357219,"threshold_uncertainty_score":0.999929},"labels":[],"label_agreement":null},{"id":"W2333889481","doi":"10.2514/6.2004-4540","title":"Optimization of Transonic Wing with Fuselage by Real-Coded Genetic Algorithm","year":2004,"lang":"en","type":"article","venue":"10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":9,"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":"Office National d'études et de Recherches Aérospatiales","keywords":"Fuselage; Transonic; Wing; Genetic algorithm; Computer science; Aerodynamics; Aerospace engineering; Engineering","score_opus":0.008486633144055282,"score_gpt":0.2271500545498619,"score_spread":0.2186634214058066,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2333889481","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.077996895,0.00009656698,0.92096007,0.00017458736,0.000012736454,0.00025928646,0.000032342537,0.000116350064,0.00035114176],"genre_scores_gemma":[0.5697146,0.0009851478,0.4290813,0.000010180366,0.0000040156215,0.000019832538,0.00008466423,0.000014875824,0.00008535616],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9982626,0.000054416585,0.00043518035,0.0006194337,0.00032885288,0.00029955374],"domain_scores_gemma":[0.9991521,0.000043287677,0.00025831495,0.00036854172,0.00006065707,0.0001170795],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012010605,0.00029093263,0.0004362852,0.00018620022,0.00028416584,0.00005386226,0.00025213865,0.00014109227,0.00042453743],"category_scores_gemma":[0.000016705297,0.00023915469,0.00009381063,0.0012873565,0.00042427992,0.0004904106,0.000117714146,0.0001347867,0.0000030540318],"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":[0.000033165747,0.0001246324,0.007887357,0.000009591853,0.00010583097,0.0000065703703,0.00042436924,0.98349166,0.0013249102,0.000048143153,0.0000029853134,0.006540761],"study_design_scores_gemma":[0.0009615368,0.00025564418,0.007827092,0.00003301075,0.0004222324,0.000005340428,0.00044527746,0.9848665,0.0045614764,0.00025318487,0.0000075634703,0.00036111788],"about_ca_topic_score_codex":0.00021344684,"about_ca_topic_score_gemma":0.00011309843,"teacher_disagreement_score":0.4918788,"about_ca_system_score_codex":0.000079542464,"about_ca_system_score_gemma":0.000026242917,"threshold_uncertainty_score":0.9752445},"labels":[],"label_agreement":null},{"id":"W2334235544","doi":"10.2514/6.2005-6959","title":"Sky Spirit: Integration of UAV Design into an Aerospace Design Course","year":2005,"lang":"en","type":"article","venue":"Infotech@Aerospace","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lockheed Martin (Canada)","funders":"","keywords":"Course (navigation); Aerospace; Sky; Computer science; Systems engineering; Engineering; Aerospace engineering; Astronomy; Physics","score_opus":0.02566214263532682,"score_gpt":0.27606404173460164,"score_spread":0.2504018990992748,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2334235544","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.07606536,0.00016157413,0.9192197,0.0022083702,0.00009791015,0.0007686902,0.000003942254,0.0006539643,0.0008205045],"genre_scores_gemma":[0.64571697,0.000072285366,0.35322985,0.00021477415,0.000036566642,0.000051035546,0.0000039681977,0.000035446763,0.00063908973],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99768627,0.00014019104,0.0004611397,0.0005962026,0.0005607062,0.0005555027],"domain_scores_gemma":[0.99836737,0.0001686804,0.00031344307,0.00092625426,0.000046151607,0.0001780721],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00069578487,0.00041075874,0.00038583903,0.00009505418,0.00021853589,0.00006370004,0.00078722084,0.00037833015,0.00040170577],"category_scores_gemma":[0.00026952726,0.00037706626,0.000096181786,0.00066269696,0.00071399775,0.001253498,0.00023187624,0.0004341354,0.0005242763],"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":[0.00016255569,0.00047999693,0.001988843,0.000016242966,0.000029970925,0.000014207505,0.0018613215,0.081347205,0.6949533,0.0021166573,0.010326557,0.20670313],"study_design_scores_gemma":[0.0010110282,0.0012137814,0.0040322193,0.00008817535,0.00005195901,0.000020285528,0.0010722401,0.016689297,0.9528022,0.009438007,0.012657897,0.0009229162],"about_ca_topic_score_codex":0.0002713957,"about_ca_topic_score_gemma":0.00024913892,"teacher_disagreement_score":0.5696516,"about_ca_system_score_codex":0.00035825305,"about_ca_system_score_gemma":0.000049950842,"threshold_uncertainty_score":0.99986815},"labels":[],"label_agreement":null},{"id":"W2335218179","doi":"10.2514/6.2010-9188","title":"Effect of Size and Mission Requirements on the Design Optimization of Non-Planar Aircraft Configurations","year":2010,"lang":"en","type":"article","venue":"13th AIAA/ISSMO Multidisciplinary Analysis Optimization Conference","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Royal Military College of Canada","funders":"","keywords":"Aerodynamics; Planar; Aerospace engineering; Multidisciplinary design optimization; Computer science; Engineering design process; Multidisciplinary approach; Process (computing); Design process; Coupling (piping); Mechanical engineering; Systems engineering; Engineering; Work in process","score_opus":0.01818075345495868,"score_gpt":0.28292685919401045,"score_spread":0.2647461057390518,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2335218179","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":[0.1416189,0.000008239043,0.85610634,0.0004947082,0.00005078837,0.00071413233,0.000020736428,0.000063414845,0.0009227667],"genre_scores_gemma":[0.8936027,0.00007270919,0.10605085,0.000016856486,0.000007111984,0.00003730951,0.00004903707,0.000014945299,0.00014847884],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9980156,0.00026768903,0.00055436644,0.0005050862,0.0004211406,0.00023615107],"domain_scores_gemma":[0.99755514,0.0011148481,0.0005021877,0.000629591,0.000104235434,0.00009401904],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.000765778,0.00028933317,0.00045403425,0.00018688873,0.0003583238,0.00003835428,0.00043182808,0.00017979786,0.0014701914],"category_scores_gemma":[0.0007465184,0.00019986191,0.00012252432,0.0011587166,0.00062205567,0.00037624888,0.00015437901,0.0002472218,0.000008320339],"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":[0.00014368146,0.000099988305,0.006684242,0.000016302747,0.00009783808,0.0000015497076,0.00022896698,0.92711264,0.064331695,0.00018014199,0.0000316566,0.0010712744],"study_design_scores_gemma":[0.00048170486,0.00050993875,0.0050185486,0.000035241595,0.00034855155,0.0000014507116,0.00012901037,0.920878,0.07220933,0.00017062742,0.000007640469,0.00020995965],"about_ca_topic_score_codex":0.00004376789,"about_ca_topic_score_gemma":0.000014629472,"teacher_disagreement_score":0.7519838,"about_ca_system_score_codex":0.000032154567,"about_ca_system_score_gemma":0.000030094385,"threshold_uncertainty_score":0.9994426},"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":"W2339683930","doi":"10.1504/ijsa.2016.076077","title":"A review on potential use of hydrogen in aviation applications","year":2016,"lang":"en","type":"review","venue":"International Journal of Sustainable Aviation","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":123,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Ontario Tech University","funders":"","keywords":"Hydrogen production; Jet fuel; Aviation; Environmental science; Natural gas; Hydrogen fuel; Waste management; Greenhouse gas; Hydrogen; Steam reforming; Production (economics); Fuel cells; Engineering; Chemistry; Aerospace engineering; Economics","score_opus":0.022265904152033174,"score_gpt":0.3090690567560499,"score_spread":0.28680315260401673,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2339683930","genre_codex":"review","genre_gemma":"review","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"review","genre_consensus":"review","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.000027989308,0.97599185,0.022265445,0.00032950024,0.000118700525,0.0010026644,0.000022889564,0.000017922875,0.00022306242],"genre_scores_gemma":[0.0009756291,0.99766815,0.00055859395,0.000088981775,0.00008387948,0.00008673776,0.000026451688,0.000020266916,0.00049133855],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9978326,0.00010751644,0.001073981,0.00020579786,0.0005976219,0.00018248668],"domain_scores_gemma":[0.99751765,0.00016497086,0.0018446629,0.00021221953,0.0002215788,0.000038947037],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004525845,0.0002023511,0.00062094844,0.00046702524,0.000028888438,0.000024219318,0.0005949119,0.00015946604,0.00018269899],"category_scores_gemma":[0.00041601137,0.00014896004,0.00028261292,0.00041269427,0.000072542156,0.00073062145,0.00013980766,0.00025740502,0.00006654642],"study_design_candidate":"design_other","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":[0.000018780533,0.0001393489,0.00007235831,0.001596259,0.000070407725,0.000072567134,0.000011941857,0.00017973887,0.000014114394,0.0030980706,0.0007914561,0.9939349],"study_design_scores_gemma":[0.00023228145,0.0000788002,0.00006832158,0.014377201,0.000107003114,0.000069815585,0.000021400883,0.000007478299,0.00002117359,0.0073473803,0.9775068,0.00016233389],"about_ca_topic_score_codex":0.000022163305,"about_ca_topic_score_gemma":0.0000018576342,"teacher_disagreement_score":0.9937726,"about_ca_system_score_codex":0.0012656669,"about_ca_system_score_gemma":0.000104696024,"threshold_uncertainty_score":0.6074414},"labels":[],"label_agreement":null},{"id":"W2343165319","doi":"10.1504/ijsa.2015.074741","title":"Analysis and assessment of an integrated hydrogen fuelled energy system for aircrafts","year":2015,"lang":"en","type":"article","venue":"International Journal of Sustainable Aviation","topic":"Advanced Aircraft Design and Technologies","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":"Ontario Tech University","funders":"","keywords":"Exergy; Refrigeration; Combustor; Environmental science; Hydrogen fuel; Waste management; Solid oxide fuel cell; Hydrogen; Nuclear engineering; Engineering; Automotive engineering; Fuel cells; Combustion; Mechanical engineering; Chemistry","score_opus":0.010655730155848208,"score_gpt":0.27267691051574006,"score_spread":0.26202118035989186,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2343165319","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":[0.473659,0.000048750997,0.5254455,0.0001919646,0.00007981061,0.00009572517,0.0000058972037,0.000019842175,0.00045350494],"genre_scores_gemma":[0.9839776,0.000016138174,0.01570983,0.000018709025,0.00002832739,0.000008726536,0.00001609392,0.0000060099596,0.0002185628],"study_design_codex":"observational","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99895865,0.000043281827,0.00035928583,0.00011420199,0.00041159478,0.00011301636],"domain_scores_gemma":[0.99887973,0.00004779468,0.00045665642,0.00008474082,0.0004628097,0.00006826029],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005075647,0.0000793778,0.00018657876,0.0002993267,0.000031534928,0.000029151852,0.00024727013,0.000053439362,0.000015888554],"category_scores_gemma":[0.00012878311,0.00006641314,0.00007215179,0.00031536174,0.000055614873,0.0006148259,0.00006972317,0.000060216116,3.3904362e-7],"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":[0.0015738123,0.0011857947,0.39273217,0.000121162164,0.0037991677,0.00054925634,0.0019125106,0.24319965,0.024029939,0.10754054,0.0006796626,0.22267634],"study_design_scores_gemma":[0.012713648,0.0045440486,0.1304691,0.00016553911,0.0019266165,0.00041568276,0.07701481,0.48496735,0.12096577,0.13002162,0.035615027,0.0011808006],"about_ca_topic_score_codex":0.00025431943,"about_ca_topic_score_gemma":0.000027292,"teacher_disagreement_score":0.5103186,"about_ca_system_score_codex":0.0006483652,"about_ca_system_score_gemma":0.000065198394,"threshold_uncertainty_score":0.2708249},"labels":[],"label_agreement":null},{"id":"W2402003641","doi":"10.2514/1.c033591","title":"Euler-Equation-Based Drag Minimization of Unconventional Aircraft Configurations","year":2016,"lang":"en","type":"article","venue":"Journal of Aircraft","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":32,"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":"Wing; Lift-induced drag; Inviscid flow; Drag; Wingtip device; Lift (data mining); Euler equations; Lift-to-drag ratio; Wing configuration; Transonic; Compressibility; Mechanics; Structural engineering; Aerodynamics; Aerospace engineering; Engineering; Physics; Mathematics; Computer science; Mathematical analysis","score_opus":0.017409170779498665,"score_gpt":0.24062442290181704,"score_spread":0.22321525212231838,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2402003641","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":[0.10509043,0.000079027035,0.88566494,0.006850031,0.00043167904,0.00019085672,0.000024184923,0.00006666186,0.0016021752],"genre_scores_gemma":[0.96843606,0.000031383002,0.030923529,0.000090817884,0.000052833126,0.000004820256,0.0000032181442,0.00001340511,0.00044392978],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9984382,0.000059591704,0.000655685,0.00015317333,0.00051596004,0.00017741096],"domain_scores_gemma":[0.9986098,0.00035414268,0.0006316318,0.0002017853,0.00012329679,0.000079366735],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00027325426,0.00013377737,0.0002286851,0.00014657296,0.000078620826,0.00001145512,0.00029052174,0.0000990664,0.0024607312],"category_scores_gemma":[0.0005167331,0.00009100065,0.00016298643,0.0002894026,0.00033011643,0.0005085254,0.00003535822,0.00010726579,0.00009930063],"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":[0.00041380714,0.0012418425,0.1285908,0.000060684717,0.00019668147,0.00007048374,0.00030154837,0.052635033,0.62533635,0.008675963,0.02839788,0.1540789],"study_design_scores_gemma":[0.010715534,0.0025498548,0.26088938,0.0008958325,0.0002845094,0.00019094125,0.00054976396,0.0068591484,0.52558994,0.07505642,0.115059875,0.0013588107],"about_ca_topic_score_codex":0.000006506436,"about_ca_topic_score_gemma":0.000006860873,"teacher_disagreement_score":0.8633456,"about_ca_system_score_codex":0.00015326981,"about_ca_system_score_gemma":0.0000908252,"threshold_uncertainty_score":0.9984512},"labels":[],"label_agreement":null},{"id":"W2407555270","doi":"10.2514/1.c033646","title":"Coupled Optimization of Aircraft Families and Fleet Allocation for Multiple Markets","year":2016,"lang":"en","type":"article","venue":"Journal of Aircraft","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":22,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Royal Military College of Canada","funders":"","keywords":"Flexibility (engineering); Aviation; Sustainability; Operations research; Computer science; Engineering; Automotive engineering; Aerospace engineering; Economics","score_opus":0.010362536596327241,"score_gpt":0.2286947167711413,"score_spread":0.21833218017481407,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2407555270","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":[0.26487663,0.00015573458,0.7330157,0.0014227498,0.000121672725,0.00024515018,0.000009518002,0.000035264922,0.00011755312],"genre_scores_gemma":[0.8778376,0.00062639156,0.12123349,0.000048542388,0.000028671357,0.0000078839,0.0000010687166,0.000014003478,0.00020236381],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99898833,0.000026806876,0.00042529835,0.0001515527,0.00023675873,0.00017123598],"domain_scores_gemma":[0.99901706,0.00031625855,0.000382365,0.00015175495,0.000071614006,0.000060935447],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003482216,0.00012333039,0.00023415168,0.00009608357,0.000062278465,0.000009488858,0.00019096861,0.00009150458,0.00010012207],"category_scores_gemma":[0.0005516292,0.00008203568,0.00007550361,0.00012763767,0.00024954308,0.00048116024,0.0000669674,0.00006342304,0.000004011199],"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":[0.0013066261,0.00043297283,0.11159463,0.000121947174,0.00015265902,0.000015930264,0.00050121173,0.055129167,0.55814517,0.0003116443,0.006331558,0.26595646],"study_design_scores_gemma":[0.02613468,0.0059040394,0.29960343,0.0013188554,0.00048152517,0.00047454386,0.0027878075,0.20217414,0.3699838,0.025157604,0.06371733,0.002262253],"about_ca_topic_score_codex":0.000007332686,"about_ca_topic_score_gemma":0.000011874545,"teacher_disagreement_score":0.61296093,"about_ca_system_score_codex":0.00008168188,"about_ca_system_score_gemma":0.00001804983,"threshold_uncertainty_score":0.33453178},"labels":[],"label_agreement":null},{"id":"W2412956132","doi":"10.2514/6.2016-3874","title":"Aerodynamic Design of Blended Wing-Body and Lifting-Fuselage Aircraft","year":2016,"lang":"en","type":"article","venue":"34th AIAA Applied Aerodynamics Conference","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":18,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Fuselage; Aerodynamics; Wing; Aerospace engineering; Marine engineering; Computer science; Engineering; Structural engineering; Aeronautics","score_opus":0.012116196416161644,"score_gpt":0.21004602784983178,"score_spread":0.19792983143367013,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2412956132","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":[0.45350233,0.000028261325,0.5404001,0.00038156728,0.0000806299,0.00064765086,0.000027509095,0.00040147276,0.004530504],"genre_scores_gemma":[0.9771017,0.00024044905,0.021991076,0.00007370964,0.000013235777,0.00007222656,0.0000059155504,0.00004515187,0.0004565635],"study_design_codex":"bench_or_experimental","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.99755645,0.00006104541,0.0005074899,0.0008363209,0.00040341305,0.00063528825],"domain_scores_gemma":[0.9984651,0.00033514376,0.0002970089,0.00071395433,0.00003137942,0.0001573761],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00038008115,0.00042014502,0.0004723185,0.00010327828,0.00016067285,0.0000331646,0.0006777282,0.00024436685,0.0003360045],"category_scores_gemma":[0.0001370599,0.00031888005,0.00005732841,0.0003460508,0.0011220517,0.0002666462,0.000521208,0.00023622147,0.00016714148],"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":[0.00010473087,0.00011219285,0.0059400187,0.000030612504,0.000032283806,0.000011717882,0.00016588229,0.00082304486,0.8968492,0.031658627,0.000082834784,0.06418883],"study_design_scores_gemma":[0.012851018,0.002170532,0.27206877,0.0009083279,0.0004135681,0.00016643644,0.0018587211,0.13474901,0.16507572,0.4002471,0.0022556067,0.0072351834],"about_ca_topic_score_codex":0.000031112453,"about_ca_topic_score_gemma":0.000073805735,"teacher_disagreement_score":0.7317735,"about_ca_system_score_codex":0.00014541636,"about_ca_system_score_gemma":0.000057607303,"threshold_uncertainty_score":0.9999263},"labels":[],"label_agreement":null},{"id":"W2470781504","doi":"10.1017/aer.2016.83","title":"Using an optimisation process for sailplane winglet design","year":2016,"lang":"en","type":"article","venue":"The Aeronautical Journal","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":7,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"Kenneth M. Molson Foundation","keywords":"Wingtip device; Flight envelope; Aerodynamics; Trim; Wing; Engineering; Drag; Simulation; Automotive engineering; Computer science; Structural engineering; Aerospace engineering","score_opus":0.11536500003093202,"score_gpt":0.32672218133252584,"score_spread":0.2113571813015938,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2470781504","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":[0.17947486,0.0000127127705,0.81857395,0.0015963758,0.000048935668,0.00015849486,0.000001448984,0.00005086782,0.00008233895],"genre_scores_gemma":[0.9326053,0.000009904187,0.06706323,0.00015824869,0.000072826464,0.000007029768,2.8124325e-7,0.0000110395795,0.00007211995],"study_design_codex":"bench_or_experimental","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.99920076,0.000057382505,0.00014696733,0.00013337618,0.00019639681,0.00026508837],"domain_scores_gemma":[0.99955195,0.0001598371,0.000056134264,0.00014271379,0.000011091842,0.00007825137],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004532675,0.00008935702,0.000083044615,0.000014463418,0.0002910233,0.000029880577,0.00031231786,0.000052969182,0.00035970422],"category_scores_gemma":[0.00015621402,0.00004210239,0.000029799234,0.00006348519,0.00027720927,0.00034950965,0.000039562594,0.00010803853,0.00004334554],"study_design_candidate":"theoretical_or_conceptual","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":[0.00052375335,0.0002730489,0.0016161432,0.00000715955,0.000036289057,0.000023339688,0.00039930214,0.06020524,0.56094563,0.0031558645,0.0008130949,0.3720011],"study_design_scores_gemma":[0.0030050003,0.0018168064,0.004280447,0.00012546557,0.00012710616,0.0015903891,0.0005773456,0.07675266,0.17093939,0.7360487,0.0039484473,0.0007882287],"about_ca_topic_score_codex":0.000001338834,"about_ca_topic_score_gemma":0.0000010967431,"teacher_disagreement_score":0.75313044,"about_ca_system_score_codex":0.000119760385,"about_ca_system_score_gemma":0.000014031829,"threshold_uncertainty_score":0.3938509},"labels":[],"label_agreement":null},{"id":"W2491827695","doi":"","title":"Challenges in aero engine performance modeling","year":2016,"lang":"en","type":"dissertation","venue":"Chalmers Publication Library (Chalmers University of Technology)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Försvarets materielverk; Mälardalens högskola; GKN Aerospace Services; Försvarsmakten; VINNOVA; McGill University","keywords":"Turbofan; Dimensioning; Component (thermodynamics); Original equipment manufacturer; Turbine; Systems engineering; Engineering; Conceptual design; Computer science; Automotive engineering; Industrial engineering; Mechanical engineering; Aerospace engineering","score_opus":0.018689671247156304,"score_gpt":0.1970945789118146,"score_spread":0.17840490766465827,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2491827695","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":[0.67364544,0.0037167417,0.0009306653,0.01873103,0.00035455878,0.00112821,0.000047951726,0.0022924126,0.299153],"genre_scores_gemma":[0.962834,0.02202135,0.0049513667,0.000024272676,0.000016368362,0.000011899597,0.00027446196,0.000066937515,0.009799371],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.99803007,0.000026657957,0.00034844782,0.0008444611,0.0002864903,0.0004638518],"domain_scores_gemma":[0.99864817,0.00002700585,0.00040430855,0.0008029802,0.000036148384,0.00008138016],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.000120582954,0.00037195734,0.000460395,0.001370497,0.00015020143,0.000010462408,0.0014090567,0.0009835723,0.0009977849],"category_scores_gemma":[0.0000540801,0.0004012469,0.00011494354,0.0012529907,0.00039838915,0.0018549778,0.00032915702,0.0005485237,0.00018934884],"study_design_candidate":"design_other","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":[0.00015922016,0.00020326106,0.0059409137,0.00021253455,0.00006509741,0.000025761876,0.0005475369,0.00028652768,0.0028638944,0.0034875483,0.001089052,0.9851186],"study_design_scores_gemma":[0.014622823,0.0027781234,0.07004862,0.006464307,0.0005692003,0.00015263107,0.12511328,0.043969166,0.1840861,0.07592433,0.46320677,0.013064652],"about_ca_topic_score_codex":0.000016321996,"about_ca_topic_score_gemma":0.000025579231,"teacher_disagreement_score":0.972054,"about_ca_system_score_codex":0.00017966716,"about_ca_system_score_gemma":0.000056601377,"threshold_uncertainty_score":0.9999154},"labels":[],"label_agreement":null},{"id":"W2495421001","doi":"10.4018/978-1-60960-887-3.ch001","title":"Aviation Industry and Environment Crisis","year":2011,"lang":"en","type":"book-chapter","venue":"IGI Global eBooks","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Aviation; Montreal Protocol; Aeronautics; Aviation accident; Focus (optics); Political science; Engineering; Natural (archaeology); Ozone layer; Business; Meteorology; History; Geography; Aerospace engineering; Ozone","score_opus":0.017957094461376374,"score_gpt":0.21387514476899527,"score_spread":0.19591805030761889,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2495421001","genre_codex":"other","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"other","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.00045351157,0.00015895572,0.0011565527,0.00008271387,0.00006705099,0.00023024436,0.00003765808,0.00016804216,0.99764526],"genre_scores_gemma":[0.795401,0.00014267227,0.0044441493,0.00079993426,0.00008355796,0.000041779844,0.0000050132994,0.0000718982,0.19901004],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.998847,0.0000064800556,0.00019743368,0.0004781419,0.00024268057,0.00022825137],"domain_scores_gemma":[0.99938124,0.000007941079,0.00013903603,0.00037235706,0.0000024017202,0.000097032476],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.0000469239,0.0003028364,0.00021926958,0.000021792943,0.00008243281,0.00001795862,0.0002119217,0.00082239084,0.0009534581],"category_scores_gemma":[0.00000502968,0.00028978992,0.000058680132,0.000007620722,0.00028664104,0.00006073518,0.0003832253,0.00041141926,0.0008443438],"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":[0.000015303613,0.000012107386,0.00067857286,0.000007990481,0.000032910837,0.000047922687,0.00004851727,0.0000062060303,0.00012111381,0.91155523,0.004842056,0.08263206],"study_design_scores_gemma":[0.00012883649,0.00007560462,0.0005982894,0.000022009697,0.000040640894,0.000021483735,0.000016616072,0.0000020978391,0.00030356404,0.93099195,0.06743785,0.00036108552],"about_ca_topic_score_codex":0.00006976299,"about_ca_topic_score_gemma":0.000015626125,"teacher_disagreement_score":0.79863524,"about_ca_system_score_codex":0.00030575696,"about_ca_system_score_gemma":0.0000070567494,"threshold_uncertainty_score":0.9999598},"labels":[],"label_agreement":null},{"id":"W2497278501","doi":"10.4018/978-1-60960-887-3.ch002","title":"Emission Assessment of Aviation","year":2011,"lang":"en","type":"book-chapter","venue":"IGI Global eBooks","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Ontario Tech University","funders":"","keywords":"Aviation; Engineering; Section (typography); Environmental science; Aeronautics; Aerospace engineering; Computer science","score_opus":0.019988214171991415,"score_gpt":0.2573854488362482,"score_spread":0.23739723466425677,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2497278501","genre_codex":"other","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"other","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.00019314472,0.000036980164,0.0058867102,0.000012622574,0.000097865355,0.00020544692,0.000025785328,0.00013519406,0.99340624],"genre_scores_gemma":[0.83793825,0.000016193366,0.008063047,0.000075405485,0.000026680707,0.000011398448,0.000004064526,0.000028368451,0.1538366],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.9989787,0.000006295264,0.00025032647,0.00030415924,0.00030176723,0.00015877555],"domain_scores_gemma":[0.99930567,0.000010054911,0.0002521422,0.00036814762,0.0000101906035,0.00005380294],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000058192538,0.00021791247,0.0002393445,0.000021835125,0.000042857,0.000005823519,0.00027284172,0.00031266667,0.0005884929],"category_scores_gemma":[0.000008287646,0.00019295908,0.000095464995,0.0000123153595,0.00019136316,0.000042351807,0.00024274382,0.00016342915,0.0001376459],"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":[0.0000069096914,0.0000105853715,0.0007184052,0.000010452002,0.000013730592,0.000010075531,0.000010970399,0.0000044384096,0.0012002935,0.94876045,0.0010945837,0.048159122],"study_design_scores_gemma":[0.00012492744,0.00011077166,0.0013345698,0.000080380625,0.000028223925,0.0000059462996,0.0000037626642,0.000014255584,0.0015482646,0.9780835,0.018421551,0.00024385352],"about_ca_topic_score_codex":0.000043180728,"about_ca_topic_score_gemma":0.000013140557,"teacher_disagreement_score":0.8395697,"about_ca_system_score_codex":0.00030680318,"about_ca_system_score_gemma":0.000023213375,"threshold_uncertainty_score":0.7868643},"labels":[],"label_agreement":null},{"id":"W2503151312","doi":"10.1007/978-94-007-1664-3","title":"ICAF 2011 Structural Integrity: Influence of Efficiency and Green Imperatives","year":2011,"lang":"en","type":"book","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":43,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"National Research Council Canada","funders":"","keywords":"Event (particle physics); Structural integrity; Engineering; Aeronautics; Forensic engineering; Architectural engineering; Political science; Structural engineering; Physics","score_opus":0.01295384815877151,"score_gpt":0.22797790525324413,"score_spread":0.21502405709447261,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2503151312","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.30665648,0.000769176,0.0017728744,0.000097731,0.000080670514,0.00072020164,0.000050854615,0.00037656736,0.6894755],"genre_scores_gemma":[0.43844336,0.00032069988,0.008000143,0.00009571764,0.000017905571,0.000012919446,0.000007754225,0.00003316095,0.55306834],"study_design_codex":"design_other","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.99888307,0.000016321426,0.00025877627,0.0004197995,0.00020572192,0.00021629992],"domain_scores_gemma":[0.99937606,0.000053828302,0.000157127,0.00034249178,0.000014024006,0.000056479654],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0000682386,0.0002739365,0.0003260574,0.00006230661,0.00006538434,0.000008199532,0.00043108757,0.00029595502,0.0019746684],"category_scores_gemma":[0.00003339387,0.00019666083,0.000050069815,0.000051235365,0.001702844,0.00023031255,0.0004956429,0.00041699724,0.00014440173],"study_design_candidate":"theoretical_or_conceptual","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":[0.00027133225,0.00025835124,0.08377889,0.00074537046,0.00036022725,0.00016252091,0.007209793,0.00052104495,0.07475588,0.23381683,0.023101343,0.5750184],"study_design_scores_gemma":[0.00081513403,0.0013005584,0.078301586,0.00025539292,0.00011218239,0.000093843126,0.00032974253,0.00039409968,0.0195642,0.87471503,0.0219119,0.0022063167],"about_ca_topic_score_codex":0.00044300337,"about_ca_topic_score_gemma":0.00009241054,"teacher_disagreement_score":0.6408982,"about_ca_system_score_codex":0.00007918443,"about_ca_system_score_gemma":0.000029501743,"threshold_uncertainty_score":0.99893767},"labels":[],"label_agreement":null},{"id":"W2509079960","doi":"","title":"Upgraded PC-12 powers ahead : Pilatus launched its turboprop single in 1991 with modest sales expectations, but a quarter of a century and a string of updates later it is still in high demand; now, with engine update and other subtle but potent enhancements, its NG is sharper than ever","year":2016,"lang":"en","type":"article","venue":"Flight international","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Turboprop; Launched; Aeronautics; Quarter (Canadian coin); Engineering; Advertising; Business; History; Electrical engineering","score_opus":0.010258632555707373,"score_gpt":0.21085838332116977,"score_spread":0.20059975076546238,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2509079960","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":[0.9969312,0.00019964816,0.00105863,0.0013028919,0.000026251066,0.00023152857,0.00013002954,0.000019731615,0.00010010226],"genre_scores_gemma":[0.9974532,0.00012855505,0.0019538645,0.000097913064,0.0000065500126,0.000029551882,0.000015704782,0.000015475836,0.00029915676],"study_design_codex":"observational","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99891114,0.00001711172,0.0002596762,0.00032932684,0.00028172263,0.00020099616],"domain_scores_gemma":[0.999654,0.00003555878,0.00012675059,0.000121084944,0.000025121279,0.00003747962],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000056498546,0.00017240329,0.00018654406,0.00014800306,0.000018207613,0.000014703445,0.00014642965,0.00006079787,0.00025245227],"category_scores_gemma":[0.000012542677,0.00011001974,0.000017547978,0.00011194775,0.0001292625,0.00038292722,0.00008507079,0.00007270462,0.0000113593815],"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":[0.0009985636,0.0005982079,0.5604335,0.000058625068,0.00018838841,0.00003528068,0.0047559235,0.00027441344,0.4291582,0.00089003594,0.0002611594,0.0023477224],"study_design_scores_gemma":[0.005621459,0.0005511167,0.16802655,0.0008682262,0.000033651377,0.000027420512,0.0012158923,0.0017587784,0.81806105,0.001437853,0.0017819687,0.0006160108],"about_ca_topic_score_codex":0.00007787626,"about_ca_topic_score_gemma":0.00032030427,"teacher_disagreement_score":0.3924069,"about_ca_system_score_codex":0.000097660166,"about_ca_system_score_gemma":0.00000753727,"threshold_uncertainty_score":0.44864747},"labels":[],"label_agreement":null},{"id":"W2515449754","doi":"10.3901/jme.2016.14.079","title":"Discuss on Approximate Optimization Strategies Using Design of Computer Experiments and Metamodels for Flight Vehicle Design","year":2016,"lang":"en","type":"article","venue":"Journal of Mechanical Engineering","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":24,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Ministry of Education and Child Care; Simon Fraser University","funders":"","keywords":"Computer science; Design of experiments; Computer experiment; Simulation; Mathematics; Statistics","score_opus":0.03737155520179079,"score_gpt":0.25081925295360363,"score_spread":0.21344769775181283,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2515449754","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":[0.012577831,0.000034925833,0.98709565,0.000048779373,0.00006565296,0.00015246395,9.939693e-7,0.000021458414,0.0000022259314],"genre_scores_gemma":[0.47494686,0.000019785108,0.52500176,0.0000051107677,0.000012808486,0.0000028699824,3.8722856e-8,0.000008935092,0.0000017983361],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993069,0.000021952583,0.00026146177,0.00011145859,0.0001571385,0.0001410962],"domain_scores_gemma":[0.9995615,0.0001565655,0.00014030737,0.00008065193,0.000014344518,0.000046623798],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00027901752,0.0001043718,0.00019454642,0.00004941048,0.000027497937,0.000014443146,0.00012484634,0.000057413057,0.000013152667],"category_scores_gemma":[0.00003969464,0.0000625759,0.00004307201,0.00006293226,0.000028661856,0.00036394154,0.000047220856,0.00005584071,3.177201e-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":[0.00003760271,0.000021121738,9.620428e-7,0.0000046423856,0.00001140956,0.0000014033567,0.000012166893,0.6297969,0.36774445,0.00059283944,0.0000035925248,0.0017728952],"study_design_scores_gemma":[0.00040576255,0.00031569574,0.0000032826722,0.00006607011,0.000012334644,0.000008393753,0.000019785764,0.726484,0.27086276,0.0017466835,0.0000055637875,0.00006965661],"about_ca_topic_score_codex":3.8261604e-7,"about_ca_topic_score_gemma":1.7011104e-8,"teacher_disagreement_score":0.46236902,"about_ca_system_score_codex":0.00006225097,"about_ca_system_score_gemma":0.0000064893256,"threshold_uncertainty_score":0.2551771},"labels":[],"label_agreement":null},{"id":"W2533648150","doi":"10.1017/s0001924000010162","title":"Horizontal flight trajectories optimisation for commercial aircraft through a flight management system","year":2014,"lang":"en","type":"article","venue":"The Aeronautical Journal","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":30,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure","funders":"","keywords":"Cruise; Reduction (mathematics); Fuel efficiency; Environmental science; Atmosphere (unit); Aeronautics; Automotive engineering; Trajectory; Flight simulator; Computer science; Aerospace engineering; Meteorology; Simulation; Engineering; Mathematics","score_opus":0.015091352782351526,"score_gpt":0.24279179198730147,"score_spread":0.22770043920494995,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2533648150","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.04454191,0.00007643292,0.9357056,0.006539409,0.0007194565,0.0006364428,0.000005920798,0.00027464522,0.011500202],"genre_scores_gemma":[0.94038224,0.000031330615,0.05864585,0.00027243324,0.00028247063,0.000051634426,0.00000284942,0.000021672244,0.00030951938],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"not_applicable","domain_scores_codex":[0.9984973,0.00010234057,0.00032150475,0.00023531768,0.00040333057,0.0004401776],"domain_scores_gemma":[0.9993531,0.0001537505,0.000109169196,0.000285221,0.000013476292,0.00008529649],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005279714,0.00019670399,0.00021567012,0.000022137343,0.00069137267,0.00008243465,0.00055273826,0.00009526967,0.00012883065],"category_scores_gemma":[0.000051158135,0.00012163452,0.0001286135,0.00013811102,0.00036786374,0.00027832796,0.00017304996,0.00029160312,0.00014188251],"study_design_candidate":"theoretical_or_conceptual","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":[0.0007035155,0.00037665435,0.0016070594,0.000108942244,0.000246316,0.000058255282,0.0016181904,0.0026029756,0.0053334893,0.61625993,0.02748913,0.34359556],"study_design_scores_gemma":[0.0058038314,0.002497265,0.022015493,0.00024498452,0.00057867187,0.0012234724,0.004304188,0.01573778,0.01726856,0.20414472,0.7246292,0.0015518322],"about_ca_topic_score_codex":0.0000060570133,"about_ca_topic_score_gemma":0.000010589769,"teacher_disagreement_score":0.89584035,"about_ca_system_score_codex":0.00030300455,"about_ca_system_score_gemma":0.0000062891486,"threshold_uncertainty_score":0.531755},"labels":[],"label_agreement":null},{"id":"W2544607565","doi":"10.2514/1.c033798","title":"High-Fidelity Aerodynamic Shape Optimization of a Lifting-Fuselage Concept for Regional Aircraft","year":2016,"lang":"en","type":"article","venue":"Journal of Aircraft","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":50,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto","funders":"Natural Sciences and Engineering Research Council of Canada; Massachusetts Institute of Technology; National Aeronautics and Space Administration","keywords":"Fuselage; Wing; Aerodynamics; Drag; Wing twist; Aerospace engineering; Structural engineering; Lift-induced drag; Engineering; Lift-to-drag ratio; Computer science; Angle of attack; Control theory (sociology)","score_opus":0.01366575788057347,"score_gpt":0.24126499722871778,"score_spread":0.2275992393481443,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2544607565","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":[0.31323832,0.000150563,0.68252444,0.00327444,0.00027359262,0.00030630565,0.0000315586,0.00007993087,0.000120852594],"genre_scores_gemma":[0.8325792,0.00012425479,0.16671571,0.00023310706,0.00008951928,0.000007739149,0.0000024920046,0.00002448324,0.00022350124],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99814457,0.000054096126,0.00078766746,0.00025278085,0.0004532362,0.00030765837],"domain_scores_gemma":[0.9983219,0.00034225947,0.0008284271,0.0002766062,0.00012668796,0.000104107596],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00047569364,0.00019637392,0.00040233356,0.00010695248,0.000091775524,0.000012232434,0.0004890053,0.00015761366,0.00069674983],"category_scores_gemma":[0.0005262974,0.0001329548,0.0002207923,0.00023157502,0.00045528426,0.0005913496,0.00011320446,0.00015663379,0.000016208209],"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":[0.0015091293,0.0012400371,0.021691564,0.00012581785,0.00035512607,0.00009420089,0.0007650434,0.28993696,0.3935513,0.0050470466,0.045051493,0.2406323],"study_design_scores_gemma":[0.05652614,0.020975212,0.16992389,0.004368686,0.001356786,0.0018404763,0.0029974326,0.11205319,0.2615845,0.21480498,0.14647754,0.0070911692],"about_ca_topic_score_codex":0.000014149275,"about_ca_topic_score_gemma":0.000011825592,"teacher_disagreement_score":0.5193409,"about_ca_system_score_codex":0.00021381683,"about_ca_system_score_gemma":0.000047021447,"threshold_uncertainty_score":0.7628922},"labels":[],"label_agreement":null},{"id":"W2568679852","doi":"10.2514/6.2017-0150","title":"Investigation of Engine Performance at Altitude Using Selected Alternative Fuels for the National Jet Fuels Combustion Program","year":2017,"lang":"en","type":"article","venue":"55th AIAA Aerospace Sciences Meeting","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":6,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"National Research Council Canada","funders":"Air Force Research Laboratory; Ministère de la Défense Nationale","keywords":"Combustion; Jet fuel; Jet engine; Alternative fuels; Jet (fluid); Altitude (triangle); Aerospace engineering; Environmental science; Automotive engineering; Aeronautics; Nuclear engineering; Engineering; Chemistry","score_opus":0.06407679783589447,"score_gpt":0.31202033853455663,"score_spread":0.24794354069866215,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2568679852","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":[0.99344605,0.000053948996,0.004390179,0.00058323727,0.00014698002,0.00068139116,0.000006597484,0.00009850517,0.00059312757],"genre_scores_gemma":[0.9386805,0.000037843543,0.06104531,0.00004099438,0.000042996875,0.00006565603,0.0000025884078,0.000008128004,0.00007596863],"study_design_codex":"observational","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9984746,0.000030827436,0.00021366167,0.00035162413,0.0005910584,0.0003382176],"domain_scores_gemma":[0.9989563,0.000210077,0.00050824217,0.00019568525,0.0000857844,0.000043868855],"candidate_categories":["sts"],"consensus_categories":[],"category_scores_codex":[0.0010438005,0.00014818842,0.00014153111,0.000043235843,0.0020045314,0.000106830084,0.000723275,0.00005799388,0.000019136787],"category_scores_gemma":[0.0008704346,0.000104244034,0.00004005748,0.000350375,0.0017163929,0.0007649612,0.0002937219,0.000106578365,0.000006010324],"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":[0.00003082011,0.000033197586,0.51365787,0.000043444972,0.000019141402,3.5060583e-7,0.0006358356,0.07000065,0.3947087,0.00028867304,0.00018338156,0.02039792],"study_design_scores_gemma":[0.00043326008,0.00028272084,0.122185096,0.00011355426,0.000019873622,0.0000055836017,0.0001995661,0.28164378,0.5929074,0.0017162542,0.00024817782,0.0002447359],"about_ca_topic_score_codex":0.000118987395,"about_ca_topic_score_gemma":0.00010582281,"teacher_disagreement_score":0.3914728,"about_ca_system_score_codex":0.00019773016,"about_ca_system_score_gemma":0.00003815934,"threshold_uncertainty_score":0.9992947},"labels":[],"label_agreement":null},{"id":"W2570478055","doi":"10.1115/1.4035648","title":"System-Level Performance of Microturbines With an Inside-Out Ceramic Turbine","year":2017,"lang":"en","type":"article","venue":"Journal of Engineering for Gas Turbines and Power","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":7,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke; Institut interdisciplinaire d'innovation technologique","funders":"Natural Sciences and Engineering Research Council of Canada; Deutsches Zentrum für Luft- und Raumfahrt","keywords":"Turbine; Ceramic; Mechanical engineering; Engineering; Automotive engineering; Materials science; Composite material","score_opus":0.012792888119884167,"score_gpt":0.2206351534957407,"score_spread":0.20784226537585654,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2570478055","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":[0.9950159,0.00020144018,0.004156694,0.00009667922,0.00023786385,0.00012012211,0.000008256293,0.000025458154,0.00013758677],"genre_scores_gemma":[0.9806281,0.00006851616,0.019089112,0.000009472166,0.00005159491,0.0000035545463,6.655109e-7,0.000019317618,0.00012967194],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.99929166,0.0000035424418,0.00026637604,0.00012155599,0.00013861501,0.00017824143],"domain_scores_gemma":[0.9992731,0.000028691224,0.00032963898,0.00025453782,0.000047356127,0.000066631546],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00014884234,0.00015563633,0.0002747234,0.00006144984,0.00010814023,0.00003863211,0.00028962654,0.00006422452,0.000009715622],"category_scores_gemma":[0.00005645486,0.00010389426,0.000053435437,0.00003577632,0.0001196037,0.0005175449,0.000060117807,0.00012352376,9.4543583e-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":[0.0023879367,0.0003940399,0.20715776,0.0016512135,0.0004116532,0.00014941092,0.0013418613,0.07578582,0.6723295,0.0019311312,0.0012629202,0.035196744],"study_design_scores_gemma":[0.008176672,0.012551578,0.6585508,0.002546605,0.00030983656,0.0025183945,0.00063360063,0.048548162,0.23855205,0.0006292622,0.02511018,0.0018728382],"about_ca_topic_score_codex":0.000009894603,"about_ca_topic_score_gemma":0.0000060807142,"teacher_disagreement_score":0.45139307,"about_ca_system_score_codex":0.000033802055,"about_ca_system_score_gemma":0.000007974556,"threshold_uncertainty_score":0.42366847},"labels":[],"label_agreement":null},{"id":"W2581832142","doi":"10.1016/b978-0-08-097089-9.00019-x","title":"Exergy Analysis of Aircraft Flight Systems","year":2012,"lang":"en","type":"book-chapter","venue":"Elsevier eBooks","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":4,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Ontario Tech University","funders":"","keywords":"Aeronautics; Aerospace engineering; Environmental science; Computer science; Engineering","score_opus":0.013112685634246208,"score_gpt":0.2201361083005003,"score_spread":0.2070234226662541,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2581832142","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.00010127672,0.0028543654,0.00026054424,0.000013714417,0.00020819025,0.00034776094,0.000049150935,0.00017419155,0.9959908],"genre_scores_gemma":[0.029186161,0.0002902644,0.0007227545,0.000040339506,0.000058452,0.00003758649,0.000024785944,0.00006077761,0.96957886],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9980356,0.000021038468,0.0005627916,0.0004943853,0.0005025197,0.00038365976],"domain_scores_gemma":[0.99841464,0.00006239332,0.000443366,0.0009458183,0.000017838061,0.00011594342],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00019133833,0.00042802584,0.00093945087,0.00031300812,0.00007348763,0.000014670065,0.00054731674,0.00046706252,0.0018525372],"category_scores_gemma":[0.000012430111,0.0003688244,0.0004312596,0.00009354545,0.00047917737,0.00008041477,0.0003510698,0.00031179492,0.00056014245],"study_design_candidate":"not_applicable","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":[0.000007090443,0.000014192256,0.0003222438,0.000038961276,0.0007351503,0.000015104334,0.00009192754,0.00021272826,0.0005144975,0.007571743,0.0001819095,0.99029446],"study_design_scores_gemma":[0.00008528468,0.000037272574,0.00019921987,0.00008460623,0.0013183306,0.0000046846426,0.000014040321,0.00006959471,0.00034723716,0.00325892,0.99412525,0.000455555],"about_ca_topic_score_codex":0.0000055563123,"about_ca_topic_score_gemma":0.000037203095,"teacher_disagreement_score":0.99394333,"about_ca_system_score_codex":0.00018780938,"about_ca_system_score_gemma":0.000011694641,"threshold_uncertainty_score":0.9998764},"labels":[],"label_agreement":null},{"id":"W2587630481","doi":"10.1108/aeat-04-2015-0098","title":"Aerodynamic wing shape optimization based on the computational design framework CEASIOM","year":2017,"lang":"en","type":"article","venue":"Aircraft Engineering and Aerospace Technology","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Partenariat Canadien Contre Le Cancer","keywords":"Multidisciplinary design optimization; Aerodynamics; Transonic; Wing; Computer science; Engineering design process; Shape optimization; Design process; Wing configuration; MATLAB; Engineering; Aerospace engineering; Mechanical engineering; Finite element method; Multidisciplinary approach; Structural engineering; Work in process","score_opus":0.010559918276200531,"score_gpt":0.21718720487462767,"score_spread":0.20662728659842713,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2587630481","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.070923254,0.000040158375,0.91808873,0.009741186,0.00008605015,0.00023072318,0.0000020480356,0.0007627536,0.0001250956],"genre_scores_gemma":[0.7722757,0.000018403847,0.22747937,0.00012910887,0.000009676768,0.000039831033,0.0000013215558,0.000021518925,0.000025086887],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9990276,0.00001454969,0.00012631284,0.0003567334,0.0001679208,0.00030687428],"domain_scores_gemma":[0.9989965,0.0002624978,0.00009087599,0.00060055923,0.000009619886,0.000039942603],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017192864,0.00020718611,0.00015737176,0.00008626054,0.00059704774,0.00008164218,0.0005262088,0.00024116323,0.00009646113],"category_scores_gemma":[0.00064025767,0.00016403,0.000031565,0.00019983127,0.00043373264,0.00014300882,0.0002113613,0.0003846031,0.000034828183],"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":[0.000005617437,0.000016796199,0.0022532865,0.0000033768354,0.0000060668685,0.000006906222,0.000012788403,0.9885457,0.0010864884,0.003696773,0.00008295363,0.0042832545],"study_design_scores_gemma":[0.00016795626,0.00009478927,0.0039495756,0.00006303018,0.0000071171658,0.0000071862532,0.000033277345,0.98936355,0.0005718476,0.0053437143,0.0001960575,0.00020192223],"about_ca_topic_score_codex":0.000006645346,"about_ca_topic_score_gemma":0.0000015248703,"teacher_disagreement_score":0.7013524,"about_ca_system_score_codex":0.00006837726,"about_ca_system_score_gemma":0.0000072956313,"threshold_uncertainty_score":0.66889495},"labels":[],"label_agreement":null},{"id":"W2597201551","doi":"10.1038/nature21420","title":"Biofuel blending reduces particle emissions from aircraft engines at cruise conditions","year":2017,"lang":"en","type":"article","venue":"Nature","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":420,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"National Research Council Canada","funders":"National Research Council Canada; Transport Canada; Deutsche Forschungsgemeinschaft; National Aeronautics and Space Administration","keywords":"Environmental science; Aerosol; Biofuel; Cruise; Aviation; Meteorology; Atmospheric sciences; Aerospace engineering; Waste management; Engineering; Geography; Geology","score_opus":0.014801581208257997,"score_gpt":0.28192190732712263,"score_spread":0.26712032611886466,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2597201551","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":[0.9906692,0.00040886653,0.00010924691,0.003933205,0.00027743215,0.00011298458,0.0000785463,0.00027549957,0.0041350075],"genre_scores_gemma":[0.9937754,0.00007647419,0.003198488,0.00018903354,0.00005834867,0.000019951973,0.000015862803,0.00001251139,0.0026538877],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9991488,0.000011499697,0.00010363569,0.00030861289,0.00017380019,0.00025367978],"domain_scores_gemma":[0.99920034,0.00006352738,0.00008402851,0.0005534058,0.000006348245,0.00009232221],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00004346493,0.00012970559,0.00011260701,0.000017646467,0.0009663166,0.000057611047,0.00050163805,0.00050013623,0.0017889384],"category_scores_gemma":[0.00032421385,0.00010594694,0.000052233227,0.000073891206,0.00032169867,0.0003682254,0.0003762163,0.0006555291,0.00045861866],"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":[0.000012515095,0.00007041497,0.105671585,0.0000027658741,0.000018350402,0.00005622666,0.00018285935,0.000100297984,0.86498505,0.0007053344,0.018458271,0.00973633],"study_design_scores_gemma":[0.00040451135,0.000027796446,0.33689952,0.00004619334,0.000026107871,0.0000077935,0.0002098561,0.00040399545,0.5784702,0.030520953,0.052634846,0.00034826365],"about_ca_topic_score_codex":0.00003591245,"about_ca_topic_score_gemma":0.00007376161,"teacher_disagreement_score":0.28651488,"about_ca_system_score_codex":0.00008469104,"about_ca_system_score_gemma":0.0000052435566,"threshold_uncertainty_score":0.9991236},"labels":[],"label_agreement":null},{"id":"W2607799141","doi":"10.1016/b978-0-12-803581-8.09941-0","title":"3.10 Composite Aerostructures For Unmanned Aircraft","year":2017,"lang":"en","type":"book-chapter","venue":"Elsevier eBooks","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"University of Victoria","funders":"","keywords":"Airframe; Payload (computing); Engineering; Aeronautics; Process (computing); Manufacturing engineering; Systems engineering; Aerospace engineering; Automotive engineering; Computer science; Computer security; Operating system","score_opus":0.015126407275489542,"score_gpt":0.24109327914272782,"score_spread":0.2259668718672383,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2607799141","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.000038530055,0.00030189648,0.0001396512,0.00011660059,0.00021842345,0.0009842555,0.000091285845,0.00031187007,0.9977975],"genre_scores_gemma":[0.0014310902,0.000036635745,0.006408581,0.00019630897,0.00012859059,0.00009118516,0.000036344358,0.00010773365,0.99156356],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9981739,0.000008625064,0.00033388633,0.00072759425,0.00031114562,0.00044486043],"domain_scores_gemma":[0.9982908,0.00006884158,0.00037368253,0.0011370503,0.000019654168,0.00011002124],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.00011059745,0.000548502,0.00055384525,0.00006347338,0.000485112,0.000078541016,0.0009936915,0.000534664,0.0025644146],"category_scores_gemma":[0.0000380789,0.00048648237,0.0002966615,0.000004802634,0.0006599969,0.00009696595,0.0004912411,0.00038507418,0.0016275822],"study_design_candidate":"design_other","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":[0.000049973194,0.000004339533,0.000011311055,0.000030018211,0.000042717416,0.000018938399,0.000022746617,0.000008412397,0.0010428027,0.0014890278,0.002222373,0.99505734],"study_design_scores_gemma":[0.00031220922,0.00013474554,0.00004662476,0.00010249311,0.00006228565,0.000012776065,0.000001595346,0.000009968271,0.0012558495,0.12194053,0.87559295,0.0005279956],"about_ca_topic_score_codex":7.4221344e-7,"about_ca_topic_score_gemma":0.00003551611,"teacher_disagreement_score":0.99452937,"about_ca_system_score_codex":0.00015441226,"about_ca_system_score_gemma":0.000017807773,"threshold_uncertainty_score":0.99975866},"labels":[],"label_agreement":null},{"id":"W2612786765","doi":"10.1177/0954410017704215","title":"Analytic study of the conditions required for longitudinal stability of dual-wing aircraft","year":2017,"lang":"en","type":"article","venue":"Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":11,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Royal Military College of Canada","funders":"Los Alamos National Laboratory; National Nuclear Security Administration; Ministère de la Défense Nationale; U.S. Department of Energy","keywords":"Downwash; Wing; Longitudinal static stability; Lift-to-drag ratio; Center of gravity; Trim; Wing twist; Wing loading; Drag; Wing configuration; Lift (data mining); Washout; Lift-induced drag; Aerodynamics; Aerospace engineering; Aerodynamic center; Angle of attack; Airplane; Control theory (sociology); Engineering; Structural engineering; Pitching moment; Physics; Computer science; Meteorology","score_opus":0.027760706191885445,"score_gpt":0.2575777322340105,"score_spread":0.22981702604212503,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2612786765","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":[0.9827428,0.000025739126,0.01610756,0.00027388817,0.00037126508,0.00041283315,0.0000116402925,0.000016081201,0.000038224545],"genre_scores_gemma":[0.9957376,0.000012943066,0.0041906144,0.0000017640847,0.000029096278,0.000008253173,1.16505696e-7,0.000010609139,0.000008962687],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9984411,0.0000061525907,0.00071000104,0.00015533251,0.0005003775,0.00018702545],"domain_scores_gemma":[0.9982276,0.0000948083,0.001135293,0.00030190087,0.00018665066,0.00005373164],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0007660871,0.00015938055,0.00044872612,0.00006454675,0.00015909175,0.000011874427,0.0008021286,0.00008770458,0.0000090274025],"category_scores_gemma":[0.0023200635,0.00010721197,0.00026331798,0.00024310927,0.00034306044,0.00047283946,0.00027764728,0.00025653545,1.5209497e-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":[0.00010011806,0.00040084968,0.014836429,0.00026843967,0.00018376902,7.70896e-7,0.00039659426,0.17701241,0.7993221,0.0072834184,0.00009171516,0.00010335237],"study_design_scores_gemma":[0.0015686519,0.0007565186,0.023546245,0.0006797136,0.000267292,0.000020724114,0.0012172441,0.014776156,0.9558589,0.0010313129,0.00007659208,0.00020065725],"about_ca_topic_score_codex":0.000013378992,"about_ca_topic_score_gemma":0.000004913691,"teacher_disagreement_score":0.16223626,"about_ca_system_score_codex":0.000119144766,"about_ca_system_score_gemma":0.000028044635,"threshold_uncertainty_score":0.43719772},"labels":[],"label_agreement":null},{"id":"W2616941502","doi":"10.5430/rwe.v8n1p45","title":"Benefits of Aviation Weather Services: A Review of International Literature","year":2017,"lang":"en","type":"review","venue":"Research in World Economy","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":14,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"University of Ghana","keywords":"Aviation; SAFER; Work (physics); Business; Aeronautics; Transport engineering; Computer science; Engineering; Computer security","score_opus":0.12340242852289343,"score_gpt":0.4115516919485723,"score_spread":0.2881492634256788,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2616941502","genre_codex":"review","genre_gemma":"review","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"review","genre_consensus":"review","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0000015807695,0.9395443,0.0000043032956,0.00015833731,0.000042941392,0.00066042965,0.000040435458,0.000010462778,0.059537206],"genre_scores_gemma":[0.000043499094,0.99734855,0.0005043168,0.000018368748,0.00003131534,0.00015892377,0.000060630984,0.000016163329,0.0018182447],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9984624,0.00011622715,0.0005782748,0.00034659848,0.000259372,0.00023717339],"domain_scores_gemma":[0.99862444,0.00016401777,0.00046557616,0.0006694926,0.00004038848,0.000036091325],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0011366723,0.00016741022,0.00080539787,0.00042089802,0.000037034406,0.000028362194,0.0012755711,0.00013272928,0.00085403986],"category_scores_gemma":[0.000079167876,0.00013682098,0.00016607363,0.00054378295,0.00021154486,0.00032335572,0.00053484284,0.0005101143,0.00015006428],"study_design_candidate":"design_other","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":[0.0000016597509,0.00003552939,0.00037216488,0.042892795,0.00002024984,0.0000026391642,0.000017259788,0.0000032069345,1.4999216e-7,0.0012050133,0.000342783,0.95510656],"study_design_scores_gemma":[0.00005133513,0.000011448607,0.00006500468,0.14280243,0.000008888584,0.000002229197,0.000003036767,0.000004323313,0.0000033716676,0.0020700255,0.8548871,0.00009075287],"about_ca_topic_score_codex":0.00004189744,"about_ca_topic_score_gemma":0.00010559449,"teacher_disagreement_score":0.9550158,"about_ca_system_score_codex":0.00027680295,"about_ca_system_score_gemma":0.000039848743,"threshold_uncertainty_score":0.9351138},"labels":[],"label_agreement":null},{"id":"W2622862289","doi":"10.2514/6.2017-4090","title":"A Sailplane Split-Winglet Design Study","year":2017,"lang":"en","type":"article","venue":"17th AIAA Aviation Technology, Integration, and Operations Conference","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":"Toronto Metropolitan University","funders":"","keywords":"Wingtip device; Computer science; Aerodynamics; Aerospace engineering; Engineering","score_opus":0.032118223112472304,"score_gpt":0.27803210367118225,"score_spread":0.24591388055870994,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2622862289","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":[0.29670036,0.000043567758,0.69498545,0.0043544737,0.00013817142,0.0011461289,0.0000132235355,0.0005836448,0.002034975],"genre_scores_gemma":[0.9610264,0.000087856584,0.037166163,0.00008142124,0.00001890325,0.00026708536,0.00001762847,0.000013154025,0.0013214425],"study_design_codex":"design_other","study_design_gemma":"observational","domain_scores_codex":[0.9985687,0.0000735919,0.00034334674,0.0005462746,0.00020842676,0.0002596623],"domain_scores_gemma":[0.99877197,0.000042660107,0.00015184269,0.00087403913,0.00009925486,0.00006024817],"candidate_categories":["sts"],"consensus_categories":[],"category_scores_codex":[0.00037165833,0.00024326202,0.00022637188,0.0001772724,0.0017019863,0.00040052406,0.0006426695,0.00022737062,0.00048004373],"category_scores_gemma":[0.00073168543,0.00020848971,0.000025187603,0.0002288413,0.0007299496,0.000918779,0.00023131135,0.00030343985,0.00014301462],"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":[0.00005181067,0.0008542646,0.290675,0.000009708826,0.00007536111,0.000029484518,0.0028681285,0.0011393499,0.036024403,0.22573283,0.0025652598,0.43997437],"study_design_scores_gemma":[0.0045966073,0.0032537158,0.5687989,0.00017302627,0.00021790211,0.00012232072,0.01877685,0.09114513,0.07709018,0.22409052,0.009146117,0.0025887284],"about_ca_topic_score_codex":0.00032384312,"about_ca_topic_score_gemma":0.001959916,"teacher_disagreement_score":0.66432595,"about_ca_system_score_codex":0.00008869991,"about_ca_system_score_gemma":0.000041349616,"threshold_uncertainty_score":0.99959767},"labels":[],"label_agreement":null},{"id":"W2626427922","doi":"10.1109/aero.2017.7943699","title":"Datamining turbofan engine performance to improve fuel efficiency","year":2017,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Safran Electronics (Canada)","funders":"","keywords":"Turbofan; Fuel efficiency; Computer science; Reliability (semiconductor); Automotive engineering; Engineering","score_opus":0.012739596242858073,"score_gpt":0.23936502783657698,"score_spread":0.2266254315937189,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2626427922","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":[0.87822014,0.000011672439,0.024827443,0.0006909645,0.0002023322,0.00021302294,0.0000038265975,0.00031113075,0.09551945],"genre_scores_gemma":[0.9751584,0.000018340546,0.020720474,0.00015038707,0.000019618576,0.000015015929,9.588813e-7,0.000008494637,0.0039082877],"study_design_codex":"design_other","study_design_gemma":"observational","domain_scores_codex":[0.9991528,0.0000029134976,0.00010039848,0.0003055124,0.0001514653,0.00028694034],"domain_scores_gemma":[0.99903774,0.000013853388,0.000048194503,0.0008273784,0.0000031825305,0.000069633774],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00010924478,0.00011002563,0.00009071902,0.000022592347,0.00032205752,0.00006052346,0.00079873216,0.00004229106,0.0004758409],"category_scores_gemma":[0.00013424657,0.00008632285,0.000017868539,0.00006212696,0.0001621254,0.00045913548,0.00066764915,0.0000954736,0.0011129179],"study_design_candidate":"design_other","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":[0.000009181647,0.0000393341,0.032981135,0.000008297526,0.0000029428509,0.000007793914,0.00011993554,0.00044640494,0.05229406,0.0002208632,0.0009189267,0.9129511],"study_design_scores_gemma":[0.0009820723,0.0008570601,0.51784927,0.00004431055,0.000014654503,0.000017138334,0.00033558687,0.02071397,0.37400138,0.0022495063,0.08173006,0.0012050008],"about_ca_topic_score_codex":0.000041617433,"about_ca_topic_score_gemma":0.000018251714,"teacher_disagreement_score":0.91174614,"about_ca_system_score_codex":0.000045375953,"about_ca_system_score_gemma":0.000003102716,"threshold_uncertainty_score":0.99966484},"labels":[],"label_agreement":null},{"id":"W2626528125","doi":"","title":"Multidisciplinary Design Optimization of a Morphing Wingtip Concept with Multiple Morphing Stages at Cruise","year":2013,"lang":"en","type":"dissertation","venue":"TSpace (University of Toronto)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Morphing; Cruise; Multidisciplinary design optimization; Multidisciplinary approach; Computer science; Aeronautics; Engineering; Aerospace engineering; Artificial intelligence; Sociology","score_opus":0.014332872460083513,"score_gpt":0.22551347851764342,"score_spread":0.2111806060575599,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2626528125","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":[0.67887014,0.0007789451,0.28171486,0.00009392849,0.0001209187,0.0016880519,0.00003293086,0.00041857146,0.03628165],"genre_scores_gemma":[0.79372,0.00019559813,0.17775144,0.0000017184748,0.0000052526384,0.0000020622465,0.00006554437,0.000044141103,0.028214237],"study_design_codex":"simulation_or_modeling","study_design_gemma":"observational","domain_scores_codex":[0.9988704,0.000049210565,0.0001294254,0.00040573278,0.0003119476,0.00023333881],"domain_scores_gemma":[0.9989431,0.0000872182,0.00052313594,0.00034249708,0.000034977365,0.000069065834],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00007096441,0.0002577676,0.000372859,0.000049910945,0.0002159029,0.0000072010116,0.00040111164,0.0002363366,0.01581895],"category_scores_gemma":[0.000033728207,0.00027596767,0.00007892657,0.00009406186,0.0003085115,0.00065728504,0.00020582175,0.00012758946,0.000026572861],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":true,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0012644734,0.00033027824,0.015480213,0.00027293304,0.00024793638,0.0000903219,0.04500908,0.7873445,0.116250955,0.0000793673,0.0013452685,0.03228466],"study_design_scores_gemma":[0.0066422513,0.002072029,0.4607646,0.0017238918,0.0007003917,0.000016553842,0.2270146,0.23698556,0.06060805,0.00013168453,0.00030020575,0.0030401642],"about_ca_topic_score_codex":0.028830007,"about_ca_topic_score_gemma":0.013054208,"teacher_disagreement_score":0.55035895,"about_ca_system_score_codex":0.00045017444,"about_ca_system_score_gemma":0.000021495769,"threshold_uncertainty_score":0.99996924},"labels":[],"label_agreement":null},{"id":"W2642148458","doi":"","title":"Scaling of Hybrid Wing-Body-Type Aircraft: Exploration Through High-Fidelity Aerodynamic Shape Optimization","year":2016,"lang":"en","type":"dissertation","venue":"TSpace (University of Toronto)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"University of Toronto; Government of Ontario","keywords":"Wing; Aerodynamics; Aerospace engineering; Scaling; High fidelity; Engineering; Fidelity; Aeronautics; Computer science; Mathematics; Geometry","score_opus":0.012963434281633865,"score_gpt":0.23643215965687225,"score_spread":0.22346872537523838,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2642148458","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":[0.8457988,0.00038052088,0.12924255,0.00029898985,0.0005242977,0.00058519526,0.000048958085,0.0003110818,0.022809628],"genre_scores_gemma":[0.9676487,0.0015915536,0.02773498,0.000006883582,0.00001657371,7.5101883e-7,0.00027323226,0.000026570162,0.0027007526],"study_design_codex":"design_other","study_design_gemma":"observational","domain_scores_codex":[0.99862874,0.000052490803,0.00021546465,0.00047491604,0.0003884922,0.00023990747],"domain_scores_gemma":[0.99881804,0.00005362898,0.00056846446,0.00042722662,0.00008600295,0.00004666114],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00012211308,0.00025750362,0.00041247925,0.000038866907,0.0001953518,0.00000743325,0.00047665052,0.00023042117,0.013220826],"category_scores_gemma":[0.00007229669,0.00028678033,0.00011893381,0.00012623785,0.00023378903,0.0016030844,0.00013474766,0.00013825552,0.00004628375],"study_design_candidate":"design_other","study_design_consensus":null,"about_ca_topic_candidate":true,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.002874684,0.00088848703,0.0025480017,0.0009922798,0.00057647174,0.00009607197,0.021977982,0.15705884,0.31392828,0.0030721587,0.0023443159,0.49364245],"study_design_scores_gemma":[0.010113963,0.0035426116,0.46866632,0.00434994,0.0021491416,0.000023106362,0.13027906,0.23552679,0.11487104,0.019998994,0.002645215,0.007833813],"about_ca_topic_score_codex":0.023299847,"about_ca_topic_score_gemma":0.009863046,"teacher_disagreement_score":0.48580864,"about_ca_system_score_codex":0.00056972867,"about_ca_system_score_gemma":0.00003862217,"threshold_uncertainty_score":0.99995846},"labels":[],"label_agreement":null},{"id":"W268558142","doi":"","title":"Cessna Citation Mustang -- $2.7 mil, Mach .63, FL410, 1150 nm, 5 passengers","year":2007,"lang":"en","type":"article","venue":"Professional pilot","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Aerospace engineering; Mach number; Aeronautics; Environmental science; Engineering; Meteorology; Physics","score_opus":0.025437866472063756,"score_gpt":0.2871042976392479,"score_spread":0.26166643116718413,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W268558142","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":[0.9307308,0.0002514212,0.03446505,0.0025814055,0.0011388279,0.00064663705,0.000011846414,0.0006789802,0.029495025],"genre_scores_gemma":[0.9843025,0.00001896676,0.011205537,0.0004428624,0.00006253187,0.000028937533,0.000016466223,0.000022124234,0.0039000765],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.99836564,0.000045173132,0.00026045722,0.00037087165,0.0005046186,0.00045321684],"domain_scores_gemma":[0.999315,0.00022223167,0.00010786432,0.00023407208,0.000016504431,0.000104292965],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0005013396,0.00017837941,0.0001375229,0.000081490594,0.00027477206,0.000014490004,0.00030103166,0.000105929816,0.0010749452],"category_scores_gemma":[0.00013853866,0.00014728238,0.000042182506,0.0004041674,0.00022848102,0.00033896175,0.00020883285,0.00030564974,0.00062965724],"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":[0.0007098945,0.0011280082,0.12219203,0.00008319555,0.000045725796,0.00018526625,0.0009673573,0.00047520135,0.5694172,0.010732038,0.048069943,0.24599417],"study_design_scores_gemma":[0.0024135665,0.00081636565,0.73167795,0.00019184557,0.000039477352,0.000033121745,0.0046298406,0.0010191095,0.083407946,0.10297574,0.071311325,0.0014837194],"about_ca_topic_score_codex":0.000038248585,"about_ca_topic_score_gemma":0.00007234509,"teacher_disagreement_score":0.6094859,"about_ca_system_score_codex":0.00018723919,"about_ca_system_score_gemma":0.000014876079,"threshold_uncertainty_score":0.99983823},"labels":[],"label_agreement":null},{"id":"W2691305584","doi":"10.2514/6.2017-3054","title":"Trim Routine for Multirotor Vehicles in Straight and Level Flight","year":2017,"lang":"en","type":"article","venue":"35th AIAA Applied Aerodynamics Conference","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":3,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"University of Waterloo","keywords":"Multirotor; Trim; Aeronautics; Aerospace engineering; Automotive engineering; Computer science; Engineering; Operating system","score_opus":0.04115607820891681,"score_gpt":0.26833158955471653,"score_spread":0.22717551134579972,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2691305584","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.92097133,0.000026050839,0.062734865,0.0007395779,0.00010188308,0.001560179,0.00011446209,0.00017931583,0.013572337],"genre_scores_gemma":[0.972213,0.00006160847,0.026389457,0.00006168764,0.000016789492,0.00023589372,0.0000140196,0.00002156066,0.0009859945],"study_design_codex":"design_other","study_design_gemma":"observational","domain_scores_codex":[0.9985427,0.000010460621,0.00026437186,0.0005763537,0.0001680989,0.00043799335],"domain_scores_gemma":[0.9990327,0.000083883184,0.00018089944,0.00060171506,0.000012047573,0.00008878315],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020833494,0.00025073093,0.00028757824,0.000046989007,0.0003602529,0.0001254511,0.00065450283,0.00017331853,0.00009812728],"category_scores_gemma":[0.00011006315,0.0002278325,0.000035543842,0.000069908834,0.0005826948,0.00023075327,0.00037152116,0.00021288964,0.000033463264],"study_design_candidate":"observational","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0003646021,0.0003025519,0.06983996,0.00009169481,0.000028340211,0.000022727954,0.0005965756,0.00047550583,0.25718063,0.18148434,0.00025678755,0.48935628],"study_design_scores_gemma":[0.0056393673,0.00020513787,0.8364734,0.00007853535,0.000029607849,0.000008208469,0.0004217299,0.07347433,0.019325754,0.059230886,0.0038402313,0.0012728244],"about_ca_topic_score_codex":0.00010727786,"about_ca_topic_score_gemma":0.0011988968,"teacher_disagreement_score":0.76663345,"about_ca_system_score_codex":0.000091844595,"about_ca_system_score_gemma":0.000019915871,"threshold_uncertainty_score":0.929074},"labels":[],"label_agreement":null},{"id":"W2746350987","doi":"10.1115/gt2017-63131","title":"Characterization of Fuel Composition and Altitude Impact on Gaseous and Particle Emissions From a Turbojet Engine","year":2017,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":10,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"National Research Council Canada; Environment and Climate Change Canada","funders":"Air Force Research Laboratory; National Research Council Canada; Clean Air Regulatory Agenda; Environment and Climate Change Canada","keywords":"Cetane number; Combustion; Environmental science; Altitude (triangle); NOx; Jet fuel; Waste management; Chemistry; Engineering; Biodiesel","score_opus":0.011119690386950359,"score_gpt":0.250382492522539,"score_spread":0.23926280213558868,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2746350987","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":[0.997194,0.000010258071,0.00207626,0.00029067547,0.000012607129,0.00007457132,0.0000190475,0.0000375677,0.0002850291],"genre_scores_gemma":[0.99853253,0.00007293826,0.0013012767,0.000032942928,0.000005029106,0.0000027311369,0.000008448186,0.0000032884489,0.000040824867],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.9996779,0.0000064962137,0.00006373492,0.00011866253,0.00005850073,0.0000747267],"domain_scores_gemma":[0.9997126,0.000020529518,0.000052063875,0.00017147903,0.0000020758946,0.000041249543],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000025375512,0.000058867656,0.00007261939,0.000007822823,0.00009898662,0.000021546699,0.000061501334,0.000030021403,0.00015974324],"category_scores_gemma":[0.00001942127,0.000041631658,0.000010278609,0.000015558104,0.00010960157,0.0001684906,0.00007568912,0.00003439251,0.000007419401],"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":[0.000019934649,0.000034311706,0.05523352,0.0000016274523,0.0000034359703,0.0000016783498,0.000055026787,0.00002043948,0.9329289,0.00006798586,0.000007470927,0.011625677],"study_design_scores_gemma":[0.00020270444,0.00008087801,0.7873866,0.000012435132,0.0000048628003,0.0000012617768,0.000012325208,0.0025587785,0.20851824,0.001130113,0.000035780817,0.00005603215],"about_ca_topic_score_codex":0.00011708648,"about_ca_topic_score_gemma":0.000012711286,"teacher_disagreement_score":0.73215306,"about_ca_system_score_codex":0.000014932613,"about_ca_system_score_gemma":0.0000011846403,"threshold_uncertainty_score":0.17490765},"labels":[],"label_agreement":null},{"id":"W2747590803","doi":"10.1115/gt2017-63978","title":"Reducing Nacelle Pressure Drag","year":2017,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Queen's University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Nacelle; Fuselage; Drag; Parasitic drag; Turbulence; Mechanics; Flow separation; Reynolds number; Aerospace engineering; Materials science; Engineering; Physics; Turbine","score_opus":0.014922645617243161,"score_gpt":0.24643990699026733,"score_spread":0.23151726137302417,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2747590803","genre_codex":"other","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":[0.113919675,0.000078278004,0.010390765,0.0019011337,0.00016588486,0.00015945522,0.0000011819119,0.00044258655,0.872941],"genre_scores_gemma":[0.94708353,0.000012484866,0.010178876,0.000044450535,0.000011320451,0.0000050653384,1.6699464e-7,0.0000048400016,0.042659234],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9995486,0.0000037549926,0.000051424195,0.00016923665,0.0000870951,0.00013987307],"domain_scores_gemma":[0.99938965,0.000008641657,0.00004043732,0.0005337835,0.000001328807,0.000026138421],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.000049267466,0.00005669742,0.000053328353,0.0000061876444,0.00038491015,0.000041485342,0.00039864954,0.000041514806,0.0026971085],"category_scores_gemma":[0.00006784089,0.00004415302,0.000018847617,0.000016361193,0.00020477458,0.0002475824,0.0003200257,0.00006390003,0.0006736258],"study_design_candidate":"not_applicable","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":[0.000021330376,0.00013291968,0.11348056,0.000015189984,0.000031253956,0.00005127968,0.00035804574,0.0030544715,0.2430283,0.01070217,0.102816835,0.52630764],"study_design_scores_gemma":[0.00042997458,0.000080352984,0.0787361,0.000016922608,0.000016067466,0.000012092681,0.00020420285,0.0035352404,0.22763643,0.031618923,0.6572592,0.00045445404],"about_ca_topic_score_codex":0.00017101261,"about_ca_topic_score_gemma":0.000019870235,"teacher_disagreement_score":0.83316386,"about_ca_system_score_codex":0.000012441507,"about_ca_system_score_gemma":0.000001408153,"threshold_uncertainty_score":0.99821454},"labels":[],"label_agreement":null},{"id":"W2756227111","doi":"10.2514/1.g002806","title":"Electric Aircraft Flight Management Systems: Economy Mode and Maximum Endurance","year":2017,"lang":"en","type":"article","venue":"Journal of Guidance Control and Dynamics","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":19,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Concordia University","funders":"Natural Sciences and Engineering Research Council of Canada; Mitacs","keywords":"Aeronautics; Engineering","score_opus":0.004999437935183998,"score_gpt":0.21627480080221384,"score_spread":0.21127536286702983,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2756227111","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":[0.43274772,0.008780331,0.5254895,0.0053236717,0.00061566604,0.0007357556,0.000021541817,0.00008801904,0.026197765],"genre_scores_gemma":[0.99470097,0.0014551319,0.0032368475,0.00012648836,0.00004019912,0.0000081759545,1.9017322e-7,0.000009754508,0.00042222065],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9990908,0.00001974666,0.00033234575,0.00018795455,0.00013558938,0.00023359983],"domain_scores_gemma":[0.99908805,0.000034912162,0.00049231027,0.0002782189,0.000020960093,0.00008555804],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002315436,0.00014876852,0.0002937493,0.00005577569,0.000281746,0.00013675184,0.00036056284,0.00006828247,0.00000494472],"category_scores_gemma":[0.00003984422,0.00011810182,0.000046925208,0.000038060425,0.00019313706,0.0005779291,0.00010996249,0.00016411596,0.0000050911685],"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":[0.0007306418,0.00025148905,0.3605353,0.00032589692,0.00047239094,0.000909393,0.00015271596,0.015885701,0.009452899,0.051422015,0.0025616793,0.55729985],"study_design_scores_gemma":[0.0068810238,0.0005439371,0.30281863,0.00024985755,0.0002024264,0.0008436215,0.00029265764,0.56936973,0.00017299555,0.09084093,0.026954588,0.0008296336],"about_ca_topic_score_codex":0.000019126535,"about_ca_topic_score_gemma":0.000020688842,"teacher_disagreement_score":0.56195325,"about_ca_system_score_codex":0.00012972619,"about_ca_system_score_gemma":0.0000065318186,"threshold_uncertainty_score":0.48160526},"labels":[],"label_agreement":null},{"id":"W2769844601","doi":"10.2514/6.2015-0695","title":"Aerodynamic Optimization Trade Study of a Box-Wing Aircraft Configuration","year":2015,"lang":"en","type":"article","venue":"56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":25,"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":"Aerodynamics; Transonic; Wing; Wing configuration; Lift-induced drag; Inviscid flow; Lift-to-drag ratio; Aerospace engineering; Airfoil; Control theory (sociology); Drag; Wing loading; Longitudinal static stability; Wing twist; Mach number; Computer science; Mathematics; Engineering; Angle of attack","score_opus":0.01716698949224949,"score_gpt":0.2383157896229099,"score_spread":0.2211488001306604,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2769844601","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":[0.9751938,0.000053669326,0.021687813,0.00017179146,0.0008237812,0.0011474876,0.00019556526,0.0002663314,0.0004597875],"genre_scores_gemma":[0.9889443,0.000055415592,0.010440739,0.000068756926,0.00006691938,0.00003763868,0.00023792361,0.000048607548,0.00009968001],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.99646306,0.0002606309,0.0010320839,0.00095561857,0.000685204,0.00060339505],"domain_scores_gemma":[0.99827415,0.00006524764,0.0006443664,0.0006977024,0.000083669824,0.00023486775],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00033811084,0.0006230643,0.0008679674,0.00015579665,0.00027605702,0.0002303832,0.0006525259,0.00032447686,0.0006168035],"category_scores_gemma":[0.00022048017,0.00052734034,0.000070319365,0.00028441745,0.0006229338,0.0007393489,0.00034480757,0.0002768366,0.000008631421],"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":[0.0026704813,0.0005697258,0.04542149,0.0007484881,0.00072587613,0.00022999576,0.018964104,0.15325996,0.47029778,0.10348475,0.00077301706,0.20285432],"study_design_scores_gemma":[0.010817171,0.0033439964,0.6448154,0.0002037419,0.0004754048,0.00038724657,0.01223292,0.1555573,0.050697096,0.11725324,0.00022323897,0.0039932714],"about_ca_topic_score_codex":0.0010830424,"about_ca_topic_score_gemma":0.0011954751,"teacher_disagreement_score":0.5993939,"about_ca_system_score_codex":0.0002656942,"about_ca_system_score_gemma":0.000062332976,"threshold_uncertainty_score":0.99971783},"labels":[],"label_agreement":null},{"id":"W2771707279","doi":"10.2514/1.c034605","title":"Aerostructural Optimization of Drooped Wings","year":2017,"lang":"en","type":"article","venue":"Journal of Aircraft","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":9,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto","funders":"Compute Canada; University of Michigan; National Aeronautics and Space Administration","keywords":"Wing; Wing loading; Wing twist; Camber (aerodynamics); Swept wing; Transonic; Aerospace engineering; Drag; Washout; Structural engineering; Aerodynamics; Lift-induced drag; Wing configuration; Span (engineering); Lift-to-drag ratio; Angle of attack; Engineering; Physics","score_opus":0.012513717518117702,"score_gpt":0.24874385191770648,"score_spread":0.2362301343995888,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2771707279","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":[0.9422186,0.000047351237,0.054250006,0.0011402249,0.0002914821,0.0000796618,0.0000017693667,0.000024413139,0.001946494],"genre_scores_gemma":[0.9406733,0.000037897727,0.059034433,0.000026107155,0.000030529034,3.5907604e-7,2.0337345e-7,0.000006863821,0.00019030705],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.99925554,0.000011460539,0.0002819229,0.00008137181,0.0002491941,0.00012048331],"domain_scores_gemma":[0.99898434,0.000020571028,0.00066471705,0.0002598647,0.000027068847,0.000043434495],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015434984,0.000079043726,0.00017761596,0.00003637392,0.00013596387,0.000027990462,0.0005096805,0.0000579964,0.00030892066],"category_scores_gemma":[0.0002328314,0.000060403163,0.00007708936,0.000048184975,0.0003007895,0.0006706731,0.00013587107,0.00013380735,0.000009682396],"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":[0.00024622848,0.00018418588,0.37818754,0.00003611627,0.000101490456,0.00016107532,0.0008076458,0.25040948,0.24582453,0.0004481361,0.005277375,0.118316196],"study_design_scores_gemma":[0.0049364436,0.0020273034,0.60618967,0.00032111947,0.00016527645,0.0007599158,0.00077599415,0.012187258,0.3373647,0.021697348,0.012588242,0.0009866949],"about_ca_topic_score_codex":0.000014566454,"about_ca_topic_score_gemma":0.000004145092,"teacher_disagreement_score":0.23822223,"about_ca_system_score_codex":0.00004830519,"about_ca_system_score_gemma":0.000009947769,"threshold_uncertainty_score":0.33824646},"labels":[],"label_agreement":null},{"id":"W2776508864","doi":"10.1016/j.enpol.2017.12.007","title":"Aviation CO2 emissions reductions from the use of alternative jet fuels","year":2017,"lang":"en","type":"article","venue":"Energy Policy","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":301,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Gastops (Canada)","funders":"Federal Aviation Administration","keywords":"Jet fuel; Aviation; Oil refinery; Aviation biofuel; Biofuel; Investment (military); Natural resource economics; Raw material; Production (economics); Greenhouse gas; Capital investment; Environmental science; Waste management; Engineering; Bioenergy; Business; Economics; Finance","score_opus":0.05172039148113045,"score_gpt":0.29188930362341975,"score_spread":0.2401689121422893,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2776508864","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":[0.9147279,0.00006586851,0.041810025,0.021914026,0.00040788134,0.00017694927,0.00019842548,0.00020689795,0.020491987],"genre_scores_gemma":[0.9943934,0.00012936108,0.0026358427,0.00017938144,0.00011355972,0.000012215246,0.0000061961273,0.0000063865305,0.002523635],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"not_applicable","domain_scores_codex":[0.9995111,0.00002419446,0.00009745602,0.00013889075,0.00011343332,0.00011491696],"domain_scores_gemma":[0.99917,0.000087272434,0.00014740207,0.0005589053,0.0000054419265,0.000031001102],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000026466061,0.00007105292,0.000071328795,0.000019652407,0.0003840278,0.00003065939,0.00038056652,0.000044187822,0.00018866213],"category_scores_gemma":[0.00043004192,0.000046794357,0.00003513106,0.00006906581,0.00040162657,0.0003044166,0.00021621436,0.000062735075,0.000023638902],"study_design_candidate":"theoretical_or_conceptual","study_design_consensus":null,"about_ca_topic_candidate":true,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00004078269,0.0002680332,0.06500662,0.0000021320595,0.00012255266,0.000009634471,0.0020859912,0.015355536,0.23967758,0.31596124,0.055744424,0.30572549],"study_design_scores_gemma":[0.00033000333,0.000050966133,0.18936785,0.00002784051,0.000020603575,0.0000034726668,0.00017377781,0.0010219774,0.21363682,0.27297416,0.32214832,0.00024421778],"about_ca_topic_score_codex":0.021435572,"about_ca_topic_score_gemma":0.00041038173,"teacher_disagreement_score":0.30548126,"about_ca_system_score_codex":0.00005763092,"about_ca_system_score_gemma":0.0000104423725,"threshold_uncertainty_score":0.9850808},"labels":[],"label_agreement":null},{"id":"W2781661029","doi":"10.2514/6.2018-1006","title":"Development of a Preliminary Design Methodology for Transitional UAV","year":2018,"lang":"en","type":"article","venue":"2018  AIAA Aerospace Sciences Meeting","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":11,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Calgary","funders":"","keywords":"Computer science; Systems engineering; Engineering","score_opus":0.11834559779501048,"score_gpt":0.32562519918690885,"score_spread":0.20727960139189838,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2781661029","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":[0.13532723,0.00004631126,0.86123866,0.00043161522,0.00017430571,0.0003733979,0.0000027671,0.00010472478,0.0023009987],"genre_scores_gemma":[0.32744494,0.0000028032855,0.6722725,0.00006341022,0.00002639858,0.000041588166,6.458663e-7,0.00000665492,0.00014104189],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9984292,0.00008901977,0.00028157912,0.0004500527,0.00032172984,0.0004284672],"domain_scores_gemma":[0.9991162,0.00047273972,0.00017472377,0.00015685684,0.00002685074,0.00005262308],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0022009462,0.0001449673,0.00019268712,0.00006023522,0.00059303414,0.000015431251,0.00046421864,0.00008859864,0.00016669383],"category_scores_gemma":[0.0003861454,0.00012138379,0.00004898554,0.00041788095,0.0020435762,0.00023331102,0.00014866842,0.00006309355,0.0000595753],"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":[0.00018473966,0.00009800063,0.0022203173,0.000026605343,0.000016601925,0.0000012836981,0.004448541,0.0028965455,0.9305842,0.0016388657,0.002431455,0.055452827],"study_design_scores_gemma":[0.00045493073,0.0011485908,0.003368236,0.00008387577,0.0000179436,0.000014452369,0.002311566,0.007999215,0.9650645,0.013221459,0.005907853,0.00040735852],"about_ca_topic_score_codex":0.0000132777905,"about_ca_topic_score_gemma":0.000030277328,"teacher_disagreement_score":0.1921177,"about_ca_system_score_codex":0.000067048575,"about_ca_system_score_gemma":0.000059647587,"threshold_uncertainty_score":0.75296414},"labels":[],"label_agreement":null},{"id":"W2789533535","doi":"10.22261/s5wgld","title":"Benchmarking data from the experience gained in engine performance and emissions testing on alternative fuels for aviation","year":2017,"lang":"en","type":"article","venue":"Journal of the Global Power and Propulsion Society","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":9,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"Environment and Climate Change Canada; National Research Council Canada","funders":"","keywords":"Benchmarking; Aviation; Jet fuel; Engineering; Fuel efficiency; Certification; Alternative fuels; Renewable fuels; Energy security; Civil aviation; Environmental economics; Renewable energy; Fossil fuel; Automotive engineering; Waste management; Business; Economics","score_opus":0.05026730048601594,"score_gpt":0.3114356268615895,"score_spread":0.2611683263755735,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2789533535","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":[0.9960556,0.00009524594,0.0017667408,0.0015695611,0.00015687136,0.00013827569,0.000021857042,0.000004396733,0.00019144733],"genre_scores_gemma":[0.99210864,0.00014546403,0.0075183837,0.00017010876,0.00003933966,0.000002031616,6.8317695e-7,0.000002192953,0.000013167499],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.99944425,0.000018234807,0.00014335435,0.00013090757,0.00016313302,0.00010012485],"domain_scores_gemma":[0.999311,0.000118312986,0.00025460595,0.00027729583,0.000012806668,0.00002598499],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00031926142,0.00006946128,0.00008271952,0.0000027511303,0.00052010745,0.000054566077,0.00054963207,0.00003640698,0.000007315825],"category_scores_gemma":[0.00046440164,0.00003398125,0.000028708906,0.00004817152,0.00017829167,0.00037136558,0.00047241643,0.00014098533,3.083451e-7],"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":[0.000081718186,0.000041117288,0.78017783,0.0000057173133,0.000014315435,0.0000015586257,0.0017630431,0.00016616462,0.0052196374,0.000026855556,0.002055832,0.21044618],"study_design_scores_gemma":[0.00062616344,0.00015609179,0.96954286,0.00020431259,0.000010816017,0.000013974779,0.0009878612,0.013477408,0.001455032,0.012022256,0.0013993668,0.00010383282],"about_ca_topic_score_codex":0.000034707846,"about_ca_topic_score_gemma":0.0000068384647,"teacher_disagreement_score":0.21034235,"about_ca_system_score_codex":0.00005967371,"about_ca_system_score_gemma":0.0000058262003,"threshold_uncertainty_score":0.40002987},"labels":[],"label_agreement":null},{"id":"W2792640202","doi":"","title":"Probing Uncertainty in Aerosol Radiative Forcing: Sensitivity Analysis with a Single Climate Model","year":2013,"lang":"en","type":"article","venue":"93rd American Meteorological Society Annual Meeting","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"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":"","keywords":"Climate sensitivity; Radiative forcing; Aerosol; Climatology; Forcing (mathematics); Environmental science; Sensitivity (control systems); Climate model; Atmospheric sciences; Meteorology; Climate change; Geography; Geology; Oceanography","score_opus":0.01147184001236297,"score_gpt":0.22471338933168641,"score_spread":0.21324154931932343,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2792640202","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":[0.944534,0.000013257093,0.053042095,0.0005461187,0.0000070064016,0.00045867593,0.000017289676,0.00030219273,0.0010793434],"genre_scores_gemma":[0.9048714,0.000024462917,0.09415072,0.0007724127,0.000010990118,0.00012629741,0.0000071689387,0.000017164792,0.000019392413],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9973092,0.00023362273,0.00035906423,0.00079883676,0.0003575259,0.0009417572],"domain_scores_gemma":[0.99877214,0.00046195835,0.00032389196,0.00027249535,0.000033077064,0.00013641671],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00069027493,0.00033225195,0.00064516056,0.000047763093,0.00029139314,0.000050585928,0.00023302065,0.00013544723,0.00008031677],"category_scores_gemma":[0.0002629062,0.00023844009,0.00025890113,0.0019394644,0.0013744313,0.00046229476,0.0003715382,0.00046185788,0.00003546499],"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":[0.000044005472,0.00015559306,0.08576836,0.0000054814927,0.00010085888,0.000011641868,0.0019409948,0.8746222,0.023101948,0.00003667182,0.000031155076,0.014181066],"study_design_scores_gemma":[0.00048643877,0.0007495931,0.02565992,0.000023725115,0.00014108141,0.000003701761,0.01449336,0.9544671,0.002261538,0.0009878405,0.000030205192,0.00069545873],"about_ca_topic_score_codex":0.0013679574,"about_ca_topic_score_gemma":0.00035235492,"teacher_disagreement_score":0.07984491,"about_ca_system_score_codex":0.00035836722,"about_ca_system_score_gemma":0.00000920926,"threshold_uncertainty_score":0.9723305},"labels":[],"label_agreement":null},{"id":"W2802297912","doi":"10.1139/tcsme-2002-0022","title":"OPTIMAL GEOMETRICAL DESIGN OF AIRCRAFT USING GENETIC ALGORITHMS","year":2003,"lang":"en","type":"article","venue":"Transactions of the Canadian Society for Mechanical Engineering","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":13,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Sizing; Genetic algorithm; Crossover; Selection (genetic algorithm); Computer science; Aerodynamics; Conceptual design; Propulsion; Process (computing); Engineering design process; Optimal design; Algorithm; Mathematical optimization; Engineering; Aerospace engineering; Artificial intelligence; Mathematics","score_opus":0.019919143854136553,"score_gpt":0.2151085321399221,"score_spread":0.19518938828578553,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2802297912","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.008748107,0.000052735566,0.99070674,0.00004839892,0.00010335063,0.00027906682,0.00002165771,0.000030773914,0.000009159612],"genre_scores_gemma":[0.50368625,0.000006833205,0.49624506,0.000013090546,0.0000028819334,0.000012111077,1.5685536e-7,0.000012165088,0.000021438109],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992151,0.0000100086345,0.00019272824,0.00015188134,0.00014739872,0.00028285844],"domain_scores_gemma":[0.9995365,0.000089197754,0.000040876672,0.00021137597,0.000012355158,0.00010969144],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015706205,0.00010650924,0.00015066664,0.000041874693,0.0001366075,0.0000047358517,0.00024730727,0.00013409532,0.000090724905],"category_scores_gemma":[0.00007303189,0.000094719275,0.00029499098,0.00056204974,0.000097937416,0.00005887344,0.0000076124047,0.00014898629,9.1847545e-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":[0.00000136307,0.000013389729,0.0000072290363,0.000011396964,0.00002968666,2.1477659e-7,0.000026988871,0.9737633,0.024437388,0.00029129762,0.000017271977,0.0014005044],"study_design_scores_gemma":[0.00032912928,0.00009665179,0.00006799224,0.000019036517,0.000085828615,0.000016470665,0.0000917083,0.85190123,0.1454215,0.0007873753,0.00097535294,0.0002077013],"about_ca_topic_score_codex":0.0017756657,"about_ca_topic_score_gemma":0.00025989718,"teacher_disagreement_score":0.49493816,"about_ca_system_score_codex":0.00033008485,"about_ca_system_score_gemma":0.000063314386,"threshold_uncertainty_score":0.38625398},"labels":[],"label_agreement":null},{"id":"W2803511726","doi":"10.1177/1468087418772228","title":"Aero-thermodynamic and chemical process interactions in an axial high-pressure turbine of aircraft engines","year":2018,"lang":"en","type":"article","venue":"International Journal of Engine Research","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Montréal; École de Technologie Supérieure; Université du Québec à Montréal","funders":"","keywords":"Turbine; Thermodynamic process; Mechanics; Rotor (electric); Turbine blade; Flow (mathematics); Chemical process; Thermodynamic equilibrium; Thermodynamic system; Chemical species; Materials science; Thermodynamics; Chemistry; Mechanical engineering; Physics; Material properties; Engineering","score_opus":0.02600363959778053,"score_gpt":0.3642968012738251,"score_spread":0.33829316167604456,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2803511726","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":[0.9964935,0.00006298104,0.0022271941,0.0007126224,0.00015107678,0.00006731807,0.0000059955623,0.000012184778,0.00026710454],"genre_scores_gemma":[0.9971202,0.000042220032,0.0025722282,0.0000083135155,0.00018553132,0.0000040748196,0.0000018960873,0.000009327842,0.000056220993],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9987611,0.000042852058,0.00028036276,0.00013917538,0.00060542277,0.00017106562],"domain_scores_gemma":[0.99935675,0.0001257444,0.000088163426,0.000103718136,0.00026467862,0.00006096354],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00040217274,0.00007924967,0.00013661606,0.00030074685,0.000024580435,0.000020176494,0.00053098606,0.000046254332,0.00031629315],"category_scores_gemma":[0.00035307443,0.00006543143,0.000026858723,0.0002489001,0.00033880875,0.00045745407,0.00015755431,0.00040961712,0.0000064733536],"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":[0.0005401754,0.00052866485,0.029899353,0.000022547058,0.00009459666,0.000092927046,0.0006844946,0.0040836288,0.9174643,0.0010800853,0.00026489512,0.045244306],"study_design_scores_gemma":[0.004901068,0.0022566407,0.20362094,0.0006643089,0.000039621405,0.00083367474,0.0014199256,0.11835631,0.5974953,0.06513735,0.004570961,0.0007039071],"about_ca_topic_score_codex":0.000047599413,"about_ca_topic_score_gemma":0.00005539612,"teacher_disagreement_score":0.31996903,"about_ca_system_score_codex":0.000090483234,"about_ca_system_score_gemma":0.000022710808,"threshold_uncertainty_score":0.34631884},"labels":[],"label_agreement":null},{"id":"W2806226253","doi":"10.1016/j.ast.2018.05.060","title":"Comparison of box-wing and conventional aircraft mission performance using multidisciplinary analysis and optimization","year":2018,"lang":"en","type":"article","venue":"Aerospace Science and Technology","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":46,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Royal Military College of Canada","funders":"U.S. Department of Energy","keywords":"Wing; Wing configuration; Thrust vectoring; Wing loading; Longitudinal static stability; Lift-to-drag ratio; Aerodynamics; Fuel efficiency; Drag; Aerospace engineering; Wing twist; Thrust; Parametric statistics; Thrust specific fuel consumption; Engineering; Lift-induced drag; Airplane; Automotive engineering; Angle of attack; Mathematics","score_opus":0.019718460651085092,"score_gpt":0.30367457158445094,"score_spread":0.28395611093336587,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2806226253","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":[0.95797026,0.00014270218,0.041183777,0.0004233822,0.000024029405,0.00009615158,9.836874e-7,0.000073131225,0.00008559168],"genre_scores_gemma":[0.90967476,0.0000824036,0.09019998,0.000008518695,0.0000033692886,0.0000017781136,5.949126e-7,0.000003577586,0.0000250019],"study_design_codex":"observational","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99899715,0.000008060643,0.00015969759,0.00039472294,0.00021824494,0.00022209993],"domain_scores_gemma":[0.99958616,0.000021133274,0.0001158294,0.00017734693,0.000049641294,0.00004987034],"candidate_categories":["sts"],"consensus_categories":[],"category_scores_codex":[0.00023699447,0.000103425264,0.0001928843,0.00033036622,0.0005265115,0.000020045361,0.0001659261,0.00010624377,0.000027361231],"category_scores_gemma":[0.00008713655,0.00008976185,0.000012069171,0.0020295323,0.005294946,0.00041712483,0.0005174985,0.000093304494,0.0000015158378],"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":[0.000007266125,0.00002627176,0.8099038,0.000006814511,0.0000088447,5.323065e-7,0.0001533475,0.0021314186,0.17722125,0.00023750837,0.0000051982925,0.0102977455],"study_design_scores_gemma":[0.0003097617,0.0003721701,0.11841523,0.000033537555,0.000073259034,0.000022053147,0.0013296569,0.6877803,0.19045584,0.00094467856,0.00005143981,0.00021204894],"about_ca_topic_score_codex":0.00002361455,"about_ca_topic_score_gemma":0.000015828256,"teacher_disagreement_score":0.69148856,"about_ca_system_score_codex":0.000039661456,"about_ca_system_score_gemma":0.000016620357,"threshold_uncertainty_score":0.9974121},"labels":[],"label_agreement":null},{"id":"W2809972697","doi":"10.2514/6.2018-3249","title":"AGILE the Next Generation of Collaborative MDO: Achievements and Open Challenges","year":2018,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":19,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"Deutsches Zentrum für Luft- und Raumfahrt; European Commission","keywords":"Agile software development; Software deployment; Blueprint; Agile usability engineering; Systems engineering; Agile Unified Process; Agile manufacturing; Computer science; Multidisciplinary approach; Multidisciplinary design optimization; Paradigm shift; Engineering management; Process management; Engineering; Software engineering; Software; Software development; Software development process; Mechanical engineering","score_opus":0.10835969535328306,"score_gpt":0.299235339978557,"score_spread":0.19087564462527395,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2809972697","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":[0.8238791,0.0006575888,0.003218158,0.0048372224,0.00008816358,0.00082672393,0.000005764744,0.00006991162,0.16641735],"genre_scores_gemma":[0.99174654,0.0005732268,0.0065081404,0.0001612849,0.000013397691,0.00001779443,6.958331e-7,0.000002999746,0.000975889],"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99962986,0.000021355572,0.000068908004,0.00013024142,0.000077378114,0.00007227996],"domain_scores_gemma":[0.9997738,0.000018875371,0.000038249276,0.00014741851,0.000009203228,0.000012441143],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00010028242,0.000049360657,0.00005826958,0.0000069490216,0.00010814916,0.000022327838,0.00022721257,0.000024738783,0.00038949086],"category_scores_gemma":[0.00002181336,0.00002884236,0.000004745578,0.0000937645,0.00036045114,0.00026634266,0.00036037157,0.000025276668,0.000040242423],"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":[0.000029266826,0.00010802222,0.004700718,0.000004407198,0.000024493222,9.834663e-7,0.0030024524,0.00001915255,0.4700999,0.024061715,0.009571225,0.48837766],"study_design_scores_gemma":[0.0010015317,0.0013451218,0.0397854,0.00001715617,0.000018376833,0.000003547118,0.011473687,0.0027753378,0.74731517,0.033980697,0.16189758,0.00038639974],"about_ca_topic_score_codex":0.00005255245,"about_ca_topic_score_gemma":0.00040726046,"teacher_disagreement_score":0.48799127,"about_ca_system_score_codex":0.0000132309615,"about_ca_system_score_gemma":0.000003057283,"threshold_uncertainty_score":0.42646518},"labels":[],"label_agreement":null},{"id":"W2810176269","doi":"10.2514/6.2018-4137","title":"Conceptual design framework for an aircraft auxiliary photovoltaic system","year":2018,"lang":"en","type":"article","venue":"2018 Aviation Technology, Integration, and Operations Conference","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":"Concordia University","funders":"","keywords":"Photovoltaic system; Conceptual design; Systems engineering; Computer science; Aerospace engineering; Engineering; Electrical engineering; Human–computer interaction","score_opus":0.03806499088771819,"score_gpt":0.2825026135112657,"score_spread":0.2444376226235475,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2810176269","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.031538866,0.00004508088,0.9651147,0.0006716401,0.00022239343,0.0009973625,0.000032219777,0.0008938649,0.00048383116],"genre_scores_gemma":[0.68904376,0.000030264895,0.31005695,0.0001228766,0.000056192857,0.00039479777,0.000034340243,0.000015038506,0.00024579072],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.99847865,0.00008157709,0.0003792277,0.00059298344,0.00016301828,0.0003045542],"domain_scores_gemma":[0.9989836,0.0001001435,0.00010574017,0.0005045682,0.00022795904,0.000077940625],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00033524857,0.00025255815,0.00022520004,0.00018260267,0.0008752744,0.00012386541,0.0003821347,0.0004565072,0.00031980625],"category_scores_gemma":[0.00047758105,0.00022300762,0.00003255781,0.0004937477,0.001679366,0.0007958989,0.00008637309,0.00023458937,0.00016127159],"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":[0.00002697216,0.00007724711,0.0017789367,0.0000056261542,0.000014238573,5.870804e-7,0.00092475564,0.00013566714,0.058108594,0.9128569,0.0014616661,0.024608834],"study_design_scores_gemma":[0.0011640339,0.0030377456,0.0027274312,0.00018698667,0.000086254186,0.000054971526,0.018765643,0.24548574,0.3243821,0.39619255,0.006729577,0.0011869653],"about_ca_topic_score_codex":0.00010249914,"about_ca_topic_score_gemma":0.00066607195,"teacher_disagreement_score":0.65750486,"about_ca_system_score_codex":0.00015660678,"about_ca_system_score_gemma":0.00006664175,"threshold_uncertainty_score":0.9093987},"labels":[],"label_agreement":null},{"id":"W2811115836","doi":"10.4050/f-0074-2018-12805","title":"Additively Manufactured Composite Ply Placement Templates","year":2018,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lockheed Martin (Canada)","funders":"","keywords":"Template; Computer science; Fabrication; Simple (philosophy); Composite number; Manufacturing engineering; Engineering drawing; Mechanical engineering; Engineering; Algorithm","score_opus":0.011637679002179912,"score_gpt":0.23356627882436404,"score_spread":0.22192859982218413,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2811115836","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":[0.6041541,0.00002318507,0.0661916,0.0011065032,0.00021582148,0.00048264622,0.000026858186,0.0011935978,0.32660568],"genre_scores_gemma":[0.9737818,0.0000050190743,0.02092413,0.00053345447,0.000024418145,0.000013021681,0.0000052688706,0.000007984281,0.004704884],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9992824,0.000009832078,0.00010074404,0.00023532783,0.00014898837,0.00022265958],"domain_scores_gemma":[0.9997114,0.000030457639,0.000033060376,0.00017671929,0.0000042893885,0.000044083103],"candidate_categories":["insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.000043099368,0.0001114609,0.000084280626,0.00002089402,0.00013881447,0.00001625034,0.00019551652,0.000050403276,0.010697523],"category_scores_gemma":[0.0000110315805,0.0000837748,0.000023841694,0.00009271462,0.00036237383,0.00013890529,0.00017410156,0.00006457135,0.003563974],"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":[0.00025509106,0.00036675725,0.046446547,0.00000979403,0.00008864128,0.00006339934,0.00078614696,0.00049792696,0.45553493,0.003678264,0.30528933,0.18698317],"study_design_scores_gemma":[0.00044230765,0.0003392257,0.05236156,0.00000899063,0.0000075432513,0.000012896568,0.0002581806,0.00038804207,0.76326925,0.008029001,0.17454343,0.00033957534],"about_ca_topic_score_codex":0.000040514642,"about_ca_topic_score_gemma":0.000044420693,"teacher_disagreement_score":0.3696277,"about_ca_system_score_codex":0.00006657267,"about_ca_system_score_gemma":0.0000018457222,"threshold_uncertainty_score":0.9972119},"labels":[],"label_agreement":null},{"id":"W2811504441","doi":"10.2514/6.2018-3661","title":"Technical Viability and Operational Assessment of a Supersonic Business Jet","year":2018,"lang":"en","type":"article","venue":"2018 Aviation Technology, Integration, and Operations Conference","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Royal Military College of Canada","funders":"","keywords":"Supersonic speed; Jet (fluid); Computer science; Systems engineering; Aerospace engineering; Engineering","score_opus":0.01613595777026563,"score_gpt":0.27754727482640645,"score_spread":0.26141131705614085,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2811504441","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":[0.39194164,0.00003573144,0.6008664,0.0042348043,0.000074649295,0.00046902752,0.00002760669,0.00023348923,0.0021166531],"genre_scores_gemma":[0.91141504,0.00010420388,0.08811127,0.000060635914,0.00001784611,0.00009905242,0.000025959247,0.0000071087898,0.00015887903],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"observational","domain_scores_codex":[0.9988353,0.00004895773,0.00035532005,0.00041912633,0.0001788336,0.00016242889],"domain_scores_gemma":[0.999238,0.000043975815,0.000072249044,0.00032302315,0.0002816448,0.000041112347],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00029120417,0.00017364418,0.00020202121,0.0001607064,0.00039261283,0.00006479585,0.00020128944,0.00023921236,0.0006309254],"category_scores_gemma":[0.00038548058,0.00014231102,0.00001804717,0.00062803115,0.001974542,0.0005341234,0.00015867552,0.00018455056,0.000017704966],"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":[0.000010852248,0.00020240512,0.22796431,0.000013853006,0.000013883272,5.8943397e-7,0.0003108341,0.00004455068,0.23084244,0.50303227,0.00060869404,0.03695532],"study_design_scores_gemma":[0.00095401984,0.0008229713,0.7891176,0.00008563667,0.00005301272,0.00006525483,0.0014862722,0.060283065,0.06503299,0.07915556,0.0022701556,0.0006735011],"about_ca_topic_score_codex":0.00014906297,"about_ca_topic_score_gemma":0.0018773387,"teacher_disagreement_score":0.56115323,"about_ca_system_score_codex":0.000091878865,"about_ca_system_score_gemma":0.0000838294,"threshold_uncertainty_score":0.7275282},"labels":[],"label_agreement":null},{"id":"W2824042642","doi":"10.1016/j.jairtraman.2018.06.001","title":"“Problematizing” carbon emissions from international aviation and the role of alternative jet fuels in meeting ICAO's mid-century aspirational goals","year":2018,"lang":"en","type":"article","venue":"Journal of Air Transport Management","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":30,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"Consejo Nacional de Ciencia y Tecnología; McGill University","keywords":"Aviation; Civil aviation; Sustainability; Greenhouse gas; Sustainable development; Political science; Economics; Engineering","score_opus":0.006863027142080606,"score_gpt":0.21955656606004786,"score_spread":0.21269353891796725,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2824042642","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":[0.9798428,0.00024049578,0.005447317,0.0012944662,0.00016372546,0.00025750336,0.00000804061,0.000012932152,0.012732752],"genre_scores_gemma":[0.9922387,0.00036179315,0.0072379378,0.00007321227,0.000047331585,0.0000066317916,0.0000031693278,0.0000057007987,0.000025506813],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.9988359,0.00003354705,0.00048293604,0.0001335763,0.00041063194,0.00010336236],"domain_scores_gemma":[0.99938804,0.0000605176,0.00040010636,0.00009753511,0.000025525296,0.000028286446],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004288867,0.00009562587,0.00017020981,0.00009398511,0.000046749687,0.000007652566,0.00026639734,0.000035264573,0.000114174065],"category_scores_gemma":[0.000022251486,0.00006405979,0.000054544114,0.00012920298,0.00022506765,0.00020471434,0.000058412814,0.00012046814,0.0000016741682],"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":[0.0010475906,0.00060521974,0.81008744,0.000055899614,0.0005907558,0.00010919505,0.008379021,0.011380333,0.05330655,0.013841115,0.00013630756,0.10046056],"study_design_scores_gemma":[0.006441465,0.00035493533,0.69232845,0.0008410906,0.00021607958,0.000016616192,0.004654045,0.008178949,0.052908543,0.22170344,0.011924688,0.00043165789],"about_ca_topic_score_codex":0.00011016742,"about_ca_topic_score_gemma":0.0000733964,"teacher_disagreement_score":0.20786233,"about_ca_system_score_codex":0.00008216292,"about_ca_system_score_gemma":0.0000051398647,"threshold_uncertainty_score":0.26122823},"labels":[],"label_agreement":null},{"id":"W2884668967","doi":"10.2514/6.2018-3637.c1","title":"Correction: A Parametric Study of Multimodality in Aerodynamic Shape Optimization of Wings","year":2018,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"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; Multimodality; Parametric statistics; Computer science; Aerospace engineering; Engineering; Mathematics; World Wide Web; Statistics","score_opus":0.014072481676935223,"score_gpt":0.2550930477150551,"score_spread":0.24102056603811986,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2884668967","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":[0.9722832,0.0000021827861,0.025087163,0.000010440478,0.0000699505,0.00022790587,3.452623e-7,0.00004973134,0.0022690909],"genre_scores_gemma":[0.98748344,0.0000034154837,0.012392369,0.0000073243414,0.0000023685666,0.0000073779875,4.0568915e-7,0.0000035555784,0.00009974041],"study_design_codex":"observational","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99937874,0.000024894181,0.00020414211,0.0001682174,0.00013536392,0.00008861577],"domain_scores_gemma":[0.99966794,0.000050768,0.00008693669,0.00017096272,0.000011728907,0.000011690592],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012520942,0.000059366866,0.00011874535,0.0000888498,0.000021819986,0.0000020432524,0.00012590352,0.000041146595,0.00073908124],"category_scores_gemma":[0.00014906592,0.000051020965,0.000014239637,0.00093821174,0.00019021994,0.00012420479,0.00008784096,0.00005054742,0.000010378624],"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":[0.00004324573,0.0009769609,0.7730741,0.00000432305,0.000005992532,0.0000010417745,0.00045796874,0.18486772,0.00299566,0.000018637547,0.00006710246,0.03748724],"study_design_scores_gemma":[0.00039799674,0.0005172681,0.41732723,0.000005459104,0.000003624416,6.9848096e-7,0.0010560596,0.5775806,0.0028875347,0.00015273334,0.000004253316,0.00006659164],"about_ca_topic_score_codex":0.0009899567,"about_ca_topic_score_gemma":0.00061684736,"teacher_disagreement_score":0.39271283,"about_ca_system_score_codex":0.000057471607,"about_ca_system_score_gemma":0.0000026286205,"threshold_uncertainty_score":0.8092421},"labels":[],"label_agreement":null},{"id":"W2885808831","doi":"10.23919/acc.2018.8431244","title":"Maximum Endurance of a Turbofan in Cruise with Head or Tail-Wind","year":2018,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Concordia University","funders":"Mitacs","keywords":"Turbofan; Cruise; Control theory (sociology); Computer science; Optimal control; Head (geology); Mathematical optimization; Mathematics; Engineering; Control (management); Automotive engineering; Aerospace engineering; Artificial intelligence; Geology","score_opus":0.01740420496884346,"score_gpt":0.25044542695647165,"score_spread":0.2330412219876282,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2885808831","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":[0.9689785,0.000012182493,0.00486268,0.0003147723,0.000021711605,0.00018367439,0.0000015164233,0.00009734765,0.025527574],"genre_scores_gemma":[0.97342217,0.0000080308855,0.02475754,0.00011296801,0.0000069579155,0.000006865392,1.9916767e-7,0.000007042231,0.0016782517],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.99930936,0.000010039795,0.00012529519,0.00021460839,0.00013777499,0.00020290675],"domain_scores_gemma":[0.9996592,0.0000279674,0.000040629322,0.00023885323,0.0000047987946,0.000028587621],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00005781367,0.00009269435,0.0001227414,0.000033186247,0.000028115363,0.0000040782897,0.00019728778,0.00004840034,0.0014910672],"category_scores_gemma":[0.000035806497,0.00005630251,0.000013137135,0.00034226978,0.0005543104,0.00015101794,0.00008167234,0.0000711603,0.00008225891],"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":[0.0012232861,0.0005725747,0.6241417,0.000036326845,0.000021551496,0.00018644985,0.0010172501,0.00022839541,0.14339001,0.0028377108,0.0033908745,0.22295389],"study_design_scores_gemma":[0.002991517,0.00235884,0.51390505,0.00013478735,0.000011333801,0.000066758716,0.0012310869,0.0004995155,0.39657637,0.059010997,0.022375057,0.00083867507],"about_ca_topic_score_codex":0.0001665113,"about_ca_topic_score_gemma":0.0019211057,"teacher_disagreement_score":0.25318637,"about_ca_system_score_codex":0.00004148813,"about_ca_system_score_gemma":0.00000721499,"threshold_uncertainty_score":0.9994217},"labels":[],"label_agreement":null},{"id":"W2888995238","doi":"10.1115/gt2018-75204","title":"Estimating the Drag Developed by a High Bypass Ratio Turbofan Engine","year":2018,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Queen's University","funders":"","keywords":"Turbofan; Computational fluid dynamics; Thrust; Reynolds-averaged Navier–Stokes equations; Drag; Nozzle; Stall (fluid mechanics); Aerospace engineering; Engineering; Mechanics; Simulation; Physics","score_opus":0.009390444864843228,"score_gpt":0.226700556808483,"score_spread":0.21731011194363978,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2888995238","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":[0.20692037,0.000019124142,0.76859915,0.004037673,0.0001755367,0.00024765774,0.0000025823153,0.00057394913,0.019423967],"genre_scores_gemma":[0.8519146,0.0000016315888,0.14438486,0.00046595105,0.000032519994,0.00001820528,0.0000022609051,0.00000813461,0.003171857],"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99931186,0.000014014278,0.000120361314,0.00019685602,0.00014376476,0.00021315768],"domain_scores_gemma":[0.9996394,0.00005120898,0.00003751387,0.00023816321,0.0000057677444,0.000027953487],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00010917788,0.00010179449,0.000073374984,0.00000979245,0.00023245242,0.000028939472,0.00030446137,0.000044418382,0.0015721496],"category_scores_gemma":[0.00010254187,0.000059814865,0.000014743269,0.00020852382,0.00033698816,0.00015652025,0.00016752949,0.00008916024,0.00073030236],"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":[0.000021135675,0.00010345673,0.006256692,0.0000060265324,0.000036674966,0.000010492086,0.0009060156,0.0020869896,0.19410889,0.0061259507,0.15711862,0.63321906],"study_design_scores_gemma":[0.0010106086,0.00040276107,0.014821236,0.000024540932,0.000025857744,0.000033107575,0.00049441267,0.12784117,0.6620085,0.062588476,0.12966134,0.0010879487],"about_ca_topic_score_codex":0.000107055705,"about_ca_topic_score_gemma":0.000056676763,"teacher_disagreement_score":0.6449942,"about_ca_system_score_codex":0.000050184994,"about_ca_system_score_gemma":0.000004832549,"threshold_uncertainty_score":0.99934053},"labels":[],"label_agreement":null},{"id":"W2889106594","doi":"10.1109/ccece.2018.8447674","title":"Maximum Endurance of a Turboprop in Cruise with Head and Tail-Wind","year":2018,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Concordia University","funders":"","keywords":"Turboprop; Cruise; Airspeed; Aeronautics; Head (geology); Aerospace engineering; Control theory (sociology); Engineering; Computer science; Control (management); Geology; Artificial intelligence","score_opus":0.010863020955498142,"score_gpt":0.2265433812678262,"score_spread":0.21568036031232804,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2889106594","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":[0.98118746,0.000032171985,0.002137166,0.00021413932,0.000009415332,0.00012297089,8.3660996e-7,0.00004635009,0.016249508],"genre_scores_gemma":[0.986368,0.0000132039695,0.01305243,0.00007675827,0.000003903973,0.0000040242194,1.311763e-7,0.0000045158376,0.00047702712],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.9995019,0.0000062362583,0.0000855283,0.00017527283,0.00009112888,0.000139944],"domain_scores_gemma":[0.9997862,0.000012561245,0.000027158729,0.00014821033,0.0000034647842,0.000022421153],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000043925214,0.00006939718,0.00009090639,0.000024110715,0.000022733702,0.00000387756,0.000094158626,0.000036241512,0.000337084],"category_scores_gemma":[0.000014193306,0.000046790723,0.0000064990986,0.00017885801,0.00060464477,0.00012401318,0.0000735302,0.000053762138,0.000035576762],"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":[0.00017773145,0.00014114995,0.7085611,0.000016984557,0.000006736537,0.00003319637,0.000516952,0.000060458995,0.14241998,0.0011130366,0.00034862763,0.14660403],"study_design_scores_gemma":[0.001327933,0.000805012,0.78408486,0.000054605534,0.0000046939012,0.00003060384,0.00050404615,0.00045572643,0.18397875,0.024040671,0.0043784375,0.000334665],"about_ca_topic_score_codex":0.00014735952,"about_ca_topic_score_gemma":0.0005451091,"teacher_disagreement_score":0.14626937,"about_ca_system_score_codex":0.00001918413,"about_ca_system_score_gemma":0.0000027619228,"threshold_uncertainty_score":0.36908334},"labels":[],"label_agreement":null},{"id":"W2892015826","doi":"10.5194/acp-2018-601","title":"Tracer study to estimate the transport of cruise altitude aviationemissions in Northern Hemisphere","year":2018,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Office of Defense Programs; Federal Aviation Administration; University of North Carolina at Chapel Hill; Transport Canada; National Aeronautics and Space Administration; U.S. Department of Defense","keywords":"Environmental science; Cruise; Altitude (triangle); Northern Hemisphere; Troposphere; TRACER; Atmospheric sciences; Southern Hemisphere; Air quality index; Meteorology; Climatology; Geography; Geology; Oceanography; Physics","score_opus":0.012377016629334731,"score_gpt":0.2979581370178975,"score_spread":0.28558112038856276,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2892015826","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":[0.9848248,0.000004636917,0.0048773587,0.0005364923,0.000017231634,0.00039406374,0.0000010985002,0.000066769586,0.009277575],"genre_scores_gemma":[0.9941587,0.0000013636848,0.004844105,0.000058390622,0.000005039455,0.000026915073,3.2971948e-7,0.0000063043253,0.00089887704],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.9993498,0.000011903894,0.00016502176,0.00017602282,0.00015831795,0.00013893183],"domain_scores_gemma":[0.9996455,0.0000234088,0.000029918447,0.0002594652,0.0000072254415,0.000034503948],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.000114917966,0.00007724594,0.00009016142,0.000014301309,0.000068911104,0.0000029697487,0.00024860536,0.000024179055,0.0010700948],"category_scores_gemma":[0.00003178246,0.000046733494,0.000019635132,0.0002778923,0.0001337943,0.000068385365,0.00005407815,0.000063546904,0.00014053722],"study_design_candidate":"observational","study_design_consensus":"observational","about_ca_topic_candidate":true,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000017888835,0.0003572191,0.9691476,0.0000013996811,0.000004015525,0.0000041165395,0.0017594977,0.0017281555,0.013438385,0.000054922475,0.00012972952,0.013357054],"study_design_scores_gemma":[0.00031101846,0.00022551796,0.9782992,0.000010024957,0.000008018057,0.0000011043056,0.0021052535,0.000284026,0.016278725,0.0013143541,0.0010346705,0.00012807577],"about_ca_topic_score_codex":0.00034680808,"about_ca_topic_score_gemma":0.022580223,"teacher_disagreement_score":0.022233415,"about_ca_system_score_codex":0.000037247562,"about_ca_system_score_gemma":0.000005790436,"threshold_uncertainty_score":0.99984306},"labels":[],"label_agreement":null},{"id":"W2895771111","doi":"10.1155/2018/2560370","title":"Experimental Analysis of a Small-Scale Rotor at Various Inflow Angles","year":2018,"lang":"en","type":"article","venue":"International Journal of Aerospace Engineering","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":47,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"Natural Sciences and Engineering Research Council of Canada; Ontario Centres of Excellence","keywords":"Freestream; Inflow; Thrust; Rotor (electric); Wind tunnel; Aerodynamics; Tip-speed ratio; Degree of reaction; Advance ratio; Mechanics; Multirotor; Aerospace engineering; Engineering; Marine engineering; Physics; Blade pitch; Reynolds number; Mechanical engineering; Turbulence","score_opus":0.006925143196248066,"score_gpt":0.22912065229986633,"score_spread":0.22219550910361827,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2895771111","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":[0.93952805,0.00008417054,0.059677377,0.000094929455,0.00029162862,0.000038507675,0.0000046825267,0.00002643778,0.0002542015],"genre_scores_gemma":[0.9703641,0.000012206391,0.029388083,0.000020292655,0.00007238982,0.0000022422034,9.46543e-7,0.000008820528,0.0001309141],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99919415,0.0000060125126,0.00025120354,0.0001009635,0.00032906156,0.00011861053],"domain_scores_gemma":[0.9995703,0.000037679732,0.0001902268,0.00010301832,0.000050213665,0.000048566984],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00009422037,0.00009554417,0.00017803867,0.00018721468,0.00002302586,0.000014431294,0.00037261168,0.000044618166,0.0004035581],"category_scores_gemma":[0.00005775901,0.00008570196,0.0001331841,0.00027145157,0.000098863,0.00016724654,0.00017599814,0.00008821316,0.000013978684],"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":[0.0000647261,0.0000853438,0.050753586,0.0000017092194,0.0005352315,0.000032916483,0.0006316528,0.087330885,0.8591564,0.000086564185,0.00016774655,0.0011531909],"study_design_scores_gemma":[0.0005807767,0.00033750405,0.07781166,0.000040006613,0.00012710429,0.00007625531,0.00019295426,0.025168508,0.8923043,0.000052650736,0.0030876382,0.00022062667],"about_ca_topic_score_codex":0.000022461936,"about_ca_topic_score_gemma":0.000040199473,"teacher_disagreement_score":0.062162377,"about_ca_system_score_codex":0.00026428455,"about_ca_system_score_gemma":0.0000053509048,"threshold_uncertainty_score":0.4418678},"labels":[],"label_agreement":null},{"id":"W2896096635","doi":"10.1108/aeat-08-2017-0189","title":"Proof-of-concept analysis of a supplemental solar power system for aircraft","year":2018,"lang":"en","type":"article","venue":"Aircraft Engineering and Aerospace Technology","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":7,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Ontario Tech University; Concordia University","funders":"","keywords":"Sizing; Engineering; Electric power system; Photovoltaic system; Parametric statistics; Systems engineering; Conceptual design; Power (physics); Air conditioning; Automotive engineering; Reliability engineering; Computer science; Aerospace engineering; Electrical engineering; Mechanical engineering","score_opus":0.0055995062112936715,"score_gpt":0.2159591365086179,"score_spread":0.2103596302973242,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2896096635","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":[0.64245266,0.00025648353,0.3554513,0.0004431272,0.000117196745,0.0004906331,0.00009322513,0.0006068161,0.00008858315],"genre_scores_gemma":[0.95865357,0.000005598118,0.04115375,0.000008925772,0.0000099794925,0.00007356157,0.000008934156,0.00002436611,0.00006129038],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99868214,0.0000075108087,0.00034237522,0.00041406832,0.00015309635,0.0004008347],"domain_scores_gemma":[0.99927026,0.00006406649,0.00014690743,0.00043526228,0.00003385654,0.000049652856],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00014492043,0.00022789292,0.0005136448,0.0004022076,0.00007739437,0.0000065308955,0.00032441274,0.00024493755,0.000073240495],"category_scores_gemma":[0.00009051774,0.00021553459,0.00012164379,0.0013553987,0.00070246577,0.00010899069,0.00023760376,0.00013206096,0.0000031134477],"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":[0.00016066647,0.00051348004,0.09494853,0.0004961929,0.0026375675,0.000024302502,0.002020062,0.03710352,0.79046834,0.024598684,0.0021118107,0.044916876],"study_design_scores_gemma":[0.00077376876,0.0012003117,0.0016135802,0.00007442488,0.00037906348,0.000016557506,0.0013030687,0.02586968,0.96308184,0.00033966027,0.0049151685,0.0004328507],"about_ca_topic_score_codex":0.000032159005,"about_ca_topic_score_gemma":0.000030654162,"teacher_disagreement_score":0.31620094,"about_ca_system_score_codex":0.000077377415,"about_ca_system_score_gemma":0.0000076982515,"threshold_uncertainty_score":0.87892455},"labels":[],"label_agreement":null},{"id":"W2896151495","doi":"10.1155/2018/6320197","title":"Approach to the Weight Estimation in the Conceptual Design of Hybrid-Electric-Powered Unconventional Regional Aircraft","year":2018,"lang":"en","type":"article","venue":"Journal of Advanced Transportation","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":42,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"Horizon 2020 Framework Programme; European Commission","keywords":"Airframe; Propulsion; Context (archaeology); Sizing; Payload (computing); Engineering; Electrically powered spacecraft propulsion; Aviation; Aircraft noise; Range (aeronautics); Automotive engineering; Systems engineering; Aerospace engineering; Computer science; Noise reduction","score_opus":0.019490927655843454,"score_gpt":0.2459420528333575,"score_spread":0.22645112517751403,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2896151495","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":[0.2604443,0.00008834835,0.73780894,0.0010187761,0.00010437966,0.00035965146,0.000003748337,0.000012391017,0.00015943662],"genre_scores_gemma":[0.92499924,0.00003800075,0.07467865,0.00019517676,0.000038584367,0.000016870907,0.0000073922683,0.0000073265055,0.0000187389],"study_design_codex":"simulation_or_modeling","study_design_gemma":"observational","domain_scores_codex":[0.998597,0.00007730113,0.0004943655,0.00014669845,0.00052376033,0.00016085441],"domain_scores_gemma":[0.99923813,0.00015077955,0.0003671324,0.00014744086,0.00006544624,0.00003105931],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000508084,0.00011277931,0.00015803872,0.000088156994,0.00008946913,0.000007855925,0.00038209843,0.000035072004,0.000044267967],"category_scores_gemma":[0.000068657144,0.00006826735,0.000073849114,0.0005218828,0.0002587831,0.0004028021,0.0000044939925,0.00019029972,0.0000098729115],"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":[0.0006242672,0.0003384139,0.0016401297,0.000008806838,0.000029201135,0.000015881531,0.006772449,0.9343497,0.030907061,0.004007482,0.0012452313,0.020061383],"study_design_scores_gemma":[0.0074505503,0.0056184456,0.6647103,0.0003063826,0.00024617955,0.00043007074,0.01234015,0.029481238,0.11203329,0.138236,0.028054869,0.001092549],"about_ca_topic_score_codex":0.0000067626793,"about_ca_topic_score_gemma":0.000012968751,"teacher_disagreement_score":0.9048685,"about_ca_system_score_codex":0.000077883065,"about_ca_system_score_gemma":0.00003147725,"threshold_uncertainty_score":0.27838618},"labels":[],"label_agreement":null},{"id":"W2908704155","doi":"10.2514/6.2019-0008","title":"Multi–Objective Design Optimization of an MoM Aircraft using an Asynchronous Constrained PSO","year":2019,"lang":"en","type":"article","venue":"AIAA Scitech 2019 Forum","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":"Royal Military College of Canada","funders":"","keywords":"Computer science; Asynchronous communication; Particle swarm optimization; Mathematical optimization; Mathematics; Algorithm; Telecommunications","score_opus":0.01638111948842478,"score_gpt":0.252172728559829,"score_spread":0.2357916090714042,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2908704155","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.2536154,0.000029100373,0.745019,0.00004306257,0.00010358231,0.0006701278,0.00001820308,0.00024444913,0.00025705682],"genre_scores_gemma":[0.6113895,0.000009010275,0.38840812,0.0000581465,0.0000063022367,0.000008133579,0.000011796244,0.000024143874,0.00008480821],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9983192,0.000084369894,0.00028831715,0.0005443741,0.00028816878,0.0004755497],"domain_scores_gemma":[0.99901205,0.00005826497,0.0001969002,0.00060199277,0.000031281368,0.00009950115],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002776476,0.00023811105,0.000273831,0.00011666595,0.00013892479,0.000029545155,0.0004543124,0.00021072282,0.00052699534],"category_scores_gemma":[0.000054446053,0.00022483288,0.000058977508,0.00037124706,0.00043498317,0.0011788097,0.00017521004,0.00016918164,0.00014172976],"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":[0.000045828077,0.00022699368,0.007536251,0.0000059975223,0.000014154301,0.000004952808,0.00012841923,0.7883721,0.19300188,0.000086633234,0.00005277433,0.010524011],"study_design_scores_gemma":[0.0011319683,0.0010519618,0.0020481807,0.0000339235,0.000022262782,0.000030079222,0.0010958435,0.8970807,0.095204584,0.0017250112,0.000078430356,0.0004970224],"about_ca_topic_score_codex":0.00021056665,"about_ca_topic_score_gemma":0.000027702667,"teacher_disagreement_score":0.3577741,"about_ca_system_score_codex":0.00019410597,"about_ca_system_score_gemma":0.000042593663,"threshold_uncertainty_score":0.91684186},"labels":[],"label_agreement":null},{"id":"W2909838564","doi":"10.2514/6.2019-0173","title":"Lockheed Martin Overview of the AFRL EXPEDITE Program","year":2019,"lang":"en","type":"article","venue":"AIAA Scitech 2019 Forum","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":10,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lockheed Martin (Canada)","funders":"Air Force Research Laboratory","keywords":"Computer science; Systems engineering; Engineering","score_opus":0.012192911073662048,"score_gpt":0.2542497295439433,"score_spread":0.24205681847028127,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2909838564","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":[0.97297996,0.0007716738,0.0007143157,0.0036564006,0.000745386,0.0021213414,0.000018132707,0.00059678964,0.018395972],"genre_scores_gemma":[0.9906495,0.000054728822,0.0026336242,0.00028568684,0.000012405087,0.0000495058,0.000002158523,0.000018775467,0.0062935846],"study_design_codex":"observational","study_design_gemma":"not_applicable","domain_scores_codex":[0.9987267,0.000024423238,0.00021699406,0.00029193505,0.00034336356,0.00039655392],"domain_scores_gemma":[0.9990426,0.00003124416,0.00014456398,0.000734442,0.000009101622,0.00003807571],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00014838939,0.00014824398,0.00017485867,0.000030679817,0.00007231743,0.000015655782,0.00067769235,0.00010779526,0.0008041876],"category_scores_gemma":[0.00004175746,0.00009682962,0.00011054087,0.00047895324,0.00028773677,0.00022931439,0.0006156029,0.00016370889,0.0011469824],"study_design_candidate":"not_applicable","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":[0.00003503678,0.00030502662,0.5439799,0.00005979453,0.000025703092,0.000003220466,0.00013623336,0.000298336,0.09132822,0.003361689,0.06270017,0.2977667],"study_design_scores_gemma":[0.0011384519,0.00070081954,0.09875256,0.0002072404,0.000029183526,0.000017565473,0.0006240688,0.001446885,0.1236396,0.032555137,0.74013144,0.00075705023],"about_ca_topic_score_codex":0.00004281592,"about_ca_topic_score_gemma":0.000025779804,"teacher_disagreement_score":0.6774313,"about_ca_system_score_codex":0.000055687204,"about_ca_system_score_gemma":0.000009154861,"threshold_uncertainty_score":0.99963075},"labels":[],"label_agreement":null},{"id":"W2911329704","doi":"","title":"Review of Absent Aviators - Gender Issues in Aviation edited by Donna Bridges, Jane Neal-Smith and Albert J. Mills","year":2019,"lang":"en","type":"article","venue":"International Journal of Gender, Science, and Technology","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"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 Ottawa","funders":"","keywords":"Aviation; Sociology; Engineering; Aeronautics; Law and economics; Management; Economics; Aerospace engineering","score_opus":0.009287019377506863,"score_gpt":0.2643821853483212,"score_spread":0.25509516597081433,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2911329704","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":[0.95160496,0.037750583,0.0014015698,0.0065575805,0.0006751582,0.00030889292,0.000012528518,0.000040552168,0.001648151],"genre_scores_gemma":[0.95571285,0.042247593,0.001549353,0.00034522483,0.00002101334,0.0000027887195,0.0000014686088,0.0000058520536,0.00011382846],"study_design_codex":"observational","study_design_gemma":"not_applicable","domain_scores_codex":[0.9984444,0.000018368899,0.00044406988,0.0002631453,0.0006298065,0.00020022858],"domain_scores_gemma":[0.99923134,0.000041866704,0.00036698123,0.00014843185,0.00015846388,0.000052896317],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006332575,0.00011990917,0.00025152214,0.00048963964,0.00004081821,0.000020127252,0.00057883584,0.00008696969,0.00008981946],"category_scores_gemma":[0.00024526299,0.00009676415,0.000028159997,0.00065922714,0.0008413936,0.0004371342,0.00024353503,0.00020586296,0.000009054698],"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":[0.000063615276,0.00034281026,0.7127199,0.00025640806,0.00008341025,0.00006128876,0.00041279948,0.000048184276,0.11917329,0.0083838375,0.017259484,0.14119494],"study_design_scores_gemma":[0.0074092797,0.0018816035,0.35287538,0.0047852364,0.00012666124,0.0034199127,0.0047031636,0.0041562105,0.14011866,0.12178701,0.35687357,0.0018632822],"about_ca_topic_score_codex":0.00006426112,"about_ca_topic_score_gemma":0.000008692131,"teacher_disagreement_score":0.35984454,"about_ca_system_score_codex":0.00016465226,"about_ca_system_score_gemma":0.000053523054,"threshold_uncertainty_score":0.39459276},"labels":[],"label_agreement":null},{"id":"W2913237003","doi":"","title":"Research in the Past, Present and Future Solar Electric Aircraft","year":2018,"lang":"en","type":"article","venue":"Khazar University Institutional Repository (Khazar University)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":9,"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 Windsor","funders":"","keywords":"Aviation; Electric motor; Automotive engineering; Engineering; Miles per gallon gasoline equivalent; Internal combustion engine; Battery electric vehicle; Aeronautics; Electric vehicle; Aerospace engineering; Fuel efficiency; Electrical engineering; Green vehicle","score_opus":0.015982871068452528,"score_gpt":0.22457405652957524,"score_spread":0.2085911854611227,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2913237003","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":[0.745644,0.00011517612,0.0022359174,0.004844096,0.0002785421,0.0005509288,0.000010143227,0.00020026768,0.24612094],"genre_scores_gemma":[0.994592,0.00015964967,0.0007200057,0.00006360935,0.00043554907,4.409358e-7,0.0000040962823,0.000007043716,0.0040176166],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"not_applicable","domain_scores_codex":[0.99799097,0.0003219839,0.00011120299,0.00052560616,0.000592958,0.0004572659],"domain_scores_gemma":[0.9992436,0.00012811851,0.00005802045,0.00039735116,0.00006363902,0.00010925642],"candidate_categories":["sts"],"consensus_categories":[],"category_scores_codex":[0.00034665677,0.00017732235,0.00014153664,0.00048525044,0.0019264496,0.00004189306,0.0008866277,0.00019609663,0.00006441285],"category_scores_gemma":[0.000009585708,0.00016630825,0.00006275753,0.0019636555,0.0019894256,0.0007060143,0.0005287327,0.0005768957,0.0001125978],"study_design_candidate":"not_applicable","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":[0.0026509298,0.0026275332,0.26167154,0.00015151949,0.00035648892,0.028155856,0.007232189,0.0028891892,0.042717673,0.49723998,0.07421287,0.08009425],"study_design_scores_gemma":[0.0006412033,0.0002271812,0.044494312,0.000017286637,0.000024151966,0.00015225905,0.0050152517,0.00040465253,0.0008405775,0.0008537624,0.947069,0.0002603922],"about_ca_topic_score_codex":0.00035940716,"about_ca_topic_score_gemma":0.00011059034,"teacher_disagreement_score":0.8728561,"about_ca_system_score_codex":0.00081022084,"about_ca_system_score_gemma":0.00011881495,"threshold_uncertainty_score":0.9993729},"labels":[],"label_agreement":null},{"id":"W2914617555","doi":"10.21608/jes.2016.25105","title":"THE ASSUMPTION EFFECT OF USING BIODIESEL AS AN AIRCRAFT FUEL ON AIR QUALITY IN SOME EGYPTIAN AIRPORTS","year":2016,"lang":"en","type":"article","venue":"Journal of Environmental Science","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"International Civil Aviation Organization","funders":"","keywords":"Air quality index; Biodiesel; Environmental science; Quality (philosophy); Aeronautics; Aviation; Jet fuel; Aircraft fuel system; Automotive engineering; Engineering; Waste management; Aerospace engineering; Meteorology; Chemistry; Geography; Physics; Combustion; Vapor lock; Catalysis","score_opus":0.015182184431382103,"score_gpt":0.287206726315819,"score_spread":0.2720245418844369,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2914617555","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":[0.99883586,0.0000763212,0.00023781158,0.00030826902,0.00015896547,0.00015806445,0.000004185901,0.000011499577,0.00020902544],"genre_scores_gemma":[0.9988907,0.00022633371,0.00075242255,0.0000608039,0.000022580783,0.000002378402,1.11298036e-7,0.000007824507,0.00003684273],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.99765694,0.00015242881,0.0005252977,0.00030036934,0.0009871162,0.00037782578],"domain_scores_gemma":[0.99872345,0.00023620304,0.0005396169,0.00036367011,0.0000040081145,0.0001330324],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00247728,0.00016973742,0.00023624966,0.00012143299,0.00023096563,0.000018434348,0.00073628116,0.00006854513,0.0001070892],"category_scores_gemma":[0.00024127268,0.00008711349,0.00008886921,0.00025966807,0.0024850185,0.0014083696,0.00021830921,0.00018285216,0.000050015653],"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":[0.00013602588,0.00014463255,0.15300137,0.0000033669385,0.0000036360593,0.000021362179,0.00007422504,0.00066855253,0.79181767,0.00013641705,0.000008331006,0.053984433],"study_design_scores_gemma":[0.00081118324,0.0015362035,0.7823919,0.00007947029,0.000009501552,0.00006711298,0.00022637189,0.00009465506,0.2073565,0.0068486207,0.0003696955,0.0002087644],"about_ca_topic_score_codex":0.000038673024,"about_ca_topic_score_gemma":0.000019498584,"teacher_disagreement_score":0.62939054,"about_ca_system_score_codex":0.00077258464,"about_ca_system_score_gemma":0.000022224636,"threshold_uncertainty_score":0.9156154},"labels":[],"label_agreement":null},{"id":"W2920952290","doi":"10.1504/ijsa.2018.10019853","title":"Sustainable flight test project tools","year":2018,"lang":"en","type":"article","venue":"International Journal of Sustainable Aviation","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université du Québec à Trois-Rivières","funders":"","keywords":"Certification; Aviation; Key (lock); Sample (material); Product (mathematics); Cost reduction; New product development; Flight test; Manufacturing engineering; Systems engineering; Engineering; Computer science; Aeronautics; Business; Simulation; Aerospace engineering; Marketing; Computer security; Economics","score_opus":0.01135626202321967,"score_gpt":0.26723557713324586,"score_spread":0.2558793151100262,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2920952290","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":[0.7385348,0.00021347254,0.14478445,0.0093741035,0.0014006482,0.0013116621,0.00001142464,0.0003115171,0.10405791],"genre_scores_gemma":[0.9795789,0.000038360937,0.0034931984,0.00019196462,0.00032636255,0.000009501749,0.000003402696,0.000012819327,0.016345505],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"not_applicable","domain_scores_codex":[0.99851793,0.00002633357,0.00037226168,0.00015560359,0.0005985644,0.00032928062],"domain_scores_gemma":[0.9986376,0.00011762579,0.0003929098,0.00013379431,0.00067444344,0.000043619024],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00045915475,0.00011842795,0.00012853988,0.00023897723,0.00014203611,0.00014842667,0.00058303546,0.00007542169,0.00052973244],"category_scores_gemma":[0.0014865762,0.0001005648,0.00006942923,0.0003725561,0.00018401809,0.0020149131,0.00023072194,0.00016023229,0.00010251989],"study_design_candidate":"not_applicable","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":[0.0013794865,0.0021767593,0.23847404,0.00010905385,0.0004675197,0.0073890844,0.007636557,0.0018887245,0.056178477,0.30324063,0.19209336,0.18896632],"study_design_scores_gemma":[0.0020760794,0.0017232287,0.043406725,0.000059895534,0.00004758061,0.00049929053,0.023206066,0.0005613705,0.060042433,0.14836925,0.7194527,0.0005553817],"about_ca_topic_score_codex":0.00012277662,"about_ca_topic_score_gemma":0.0000065609715,"teacher_disagreement_score":0.52735937,"about_ca_system_score_codex":0.0009108473,"about_ca_system_score_gemma":0.00009090339,"threshold_uncertainty_score":0.58001983},"labels":[],"label_agreement":null},{"id":"W2925215074","doi":"10.18372/38234","title":"Models for assessment of NOx emissions from turbofan engine of aircraft","year":2019,"lang":"en","type":"book-chapter","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Aviation; Aeronautics; Environmental science; Engineering; Civil aviation; Turbofan; Emission inventory; Meteorology; Air quality index; Aerospace engineering; Geography","score_opus":0.02863469481818803,"score_gpt":0.26219070232110503,"score_spread":0.233556007502917,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2925215074","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.00018651629,0.00010274624,0.4076846,0.00014252748,0.00009544324,0.00069105485,0.00036007146,0.0001116303,0.5906254],"genre_scores_gemma":[0.10430574,0.00028864376,0.32501897,0.000065827626,0.00002557665,0.000027758626,0.000116568415,0.00007464162,0.5700763],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.99874026,0.0000036883914,0.00039005527,0.00039131337,0.0002982767,0.0001764041],"domain_scores_gemma":[0.99891233,0.00016623958,0.00025783197,0.0005954058,0.000017927863,0.000050240313],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00006757878,0.000261957,0.00049970875,0.000060838494,0.000025935837,0.0000031627164,0.0004029737,0.0003327749,0.0029631592],"category_scores_gemma":[0.000014164163,0.00021031572,0.00019174938,0.000025817673,0.00019620062,0.00010672083,0.0002660875,0.0001877193,0.00002786924],"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":[0.00008642469,0.0003453217,0.00089048187,0.00031048481,0.00046208611,0.000008666108,0.00014973192,0.07003718,0.08120316,0.6603496,0.017060667,0.16909616],"study_design_scores_gemma":[0.0009358319,0.00047736062,0.00030827388,0.00033686013,0.00016030963,0.000001289687,0.000057959474,0.034401987,0.021617936,0.831998,0.10884906,0.0008551648],"about_ca_topic_score_codex":0.00006049568,"about_ca_topic_score_gemma":0.000016815598,"teacher_disagreement_score":0.17164832,"about_ca_system_score_codex":0.000094033916,"about_ca_system_score_gemma":0.000033961933,"threshold_uncertainty_score":0.9979483},"labels":[],"label_agreement":null},{"id":"W2925510744","doi":"10.22215/etd/2014-10450","title":"A Process for the Design and Manufacture of Propellers for Small Unmanned Aerial Vehicles","year":2014,"lang":"en","type":"dissertation","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Carleton University","funders":"","keywords":"Propeller; Engineering; Thrust; Process (computing); Instrumentation (computer programming); Systems engineering; Manufacturing engineering; Manufacturing process; Design process; Marine engineering; Mechanical engineering; Computer science; Work in process; Operations management","score_opus":0.02419187541223525,"score_gpt":0.25894615057957887,"score_spread":0.23475427516734362,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2925510744","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":[0.23698863,0.0003111705,0.7486942,0.00061674416,0.00039700698,0.010883651,0.000037392998,0.00025651988,0.0018147331],"genre_scores_gemma":[0.94566804,0.00009666841,0.043324146,0.00009010019,0.00005368708,0.0013448165,0.00008490285,0.00005530045,0.009282357],"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99930155,0.000011474609,0.00015720876,0.00026743763,0.00009285028,0.0001695012],"domain_scores_gemma":[0.9994042,0.00025842903,0.00014963224,0.0001525755,0.000015516142,0.00001965178],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015214583,0.00017148184,0.00019513103,0.000021647253,0.00012062039,0.000013497016,0.00027109467,0.00020237299,0.000033153156],"category_scores_gemma":[0.00009816647,0.0000976413,0.000053938333,0.000044366487,0.00012804793,0.00004443945,0.000019801148,0.0000741682,0.0000022052147],"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":[0.008668431,0.00028148055,0.00035061475,0.003396926,0.00034801624,0.0000014704541,0.0040436625,0.02307633,0.116118036,0.003619227,0.014241895,0.8258539],"study_design_scores_gemma":[0.0015640358,0.000898507,0.0009752258,0.00009870065,0.00018685739,0.0000015499638,0.0033892947,0.0075187627,0.904708,0.06771653,0.012361823,0.00058071024],"about_ca_topic_score_codex":0.000015178578,"about_ca_topic_score_gemma":0.00012500804,"teacher_disagreement_score":0.8252732,"about_ca_system_score_codex":0.000015770067,"about_ca_system_score_gemma":0.000012790518,"threshold_uncertainty_score":0.39816967},"labels":[],"label_agreement":null},{"id":"W2935124386","doi":"10.1016/j.combustflame.2019.03.018","title":"Aircraft and MiniCAST soot at the nanoscale","year":2019,"lang":"en","type":"article","venue":"Combustion and Flame","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":57,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Canadian Light Source (Canada)","funders":"National Research Council Canada; Western Economic Diversification Canada; Natural Sciences and Engineering Research Council of Canada; Canadian Institutes of Health Research; University of Saskatchewan; Canadian Light Source","keywords":"Soot; X-ray photoelectron spectroscopy; XANES; Fourier transform infrared spectroscopy; Materials science; Nanoscopic scale; Infrared; Infrared spectroscopy; Absorption (acoustics); Analytical Chemistry (journal); Chemical engineering; Spectroscopy; Nanotechnology; Chemistry; Combustion; Environmental chemistry; Optics; Organic chemistry; Physics; Composite material","score_opus":0.008857524115935687,"score_gpt":0.2139593796043538,"score_spread":0.2051018554884181,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2935124386","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":[0.9932091,0.00021048156,0.000530368,0.0017151984,0.000074483694,0.00014117366,0.0000015846502,0.00006862336,0.0040489887],"genre_scores_gemma":[0.98944175,0.00015187815,0.00036372984,0.00030991444,0.0000064129486,0.0000052842356,0.0000014056183,0.00000469774,0.009714942],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.99955493,0.000013408312,0.000068524045,0.00017394242,0.00007721945,0.00011196813],"domain_scores_gemma":[0.99973434,0.000043568023,0.000024552384,0.00016450537,0.0000020441414,0.00003098212],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00007056369,0.00006760163,0.00006757926,0.000009256736,0.00011914199,0.000014678188,0.000076567856,0.000048409973,0.00063060917],"category_scores_gemma":[0.000017310975,0.00004419286,0.000013910879,0.000059100646,0.00030325825,0.00007790146,0.0002236001,0.00007303174,0.00047108374],"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":[0.00008773825,0.00009343754,0.43690383,0.000031522264,0.000017871118,0.000011426161,0.000747041,0.0003450174,0.13602749,0.0031312855,0.023403164,0.39920017],"study_design_scores_gemma":[0.0015316267,0.00034919512,0.5990249,0.00003914196,0.00002756851,0.0001109596,0.0010057099,0.0030870796,0.020380462,0.010102726,0.36377624,0.00056438294],"about_ca_topic_score_codex":0.0000065782124,"about_ca_topic_score_gemma":0.000019544505,"teacher_disagreement_score":0.3986358,"about_ca_system_score_codex":0.00002400054,"about_ca_system_score_gemma":0.0000012592996,"threshold_uncertainty_score":0.6904728},"labels":[],"label_agreement":null},{"id":"W2954561314","doi":"10.2514/1.i010663","title":"Identification and Validation of an Engine Performance Database Model for the Flight Management System","year":2019,"lang":"en","type":"article","venue":"Journal of Aerospace Information Systems","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":25,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université du Québec à Montréal","funders":"Ministère du Développement Économique, de l’Innovation et de l’Exportation","keywords":"Climb; Flight simulator; Takeoff; Descent (aeronautics); Engineering; Flight management system; Trajectory; Aircraft flight mechanics; Fly-by-wire; Simulation; Takeoff and landing; Computer science; Aerodynamics; Aerospace engineering","score_opus":0.010820033217070459,"score_gpt":0.2208430893755751,"score_spread":0.21002305615850464,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2954561314","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":[0.5829632,0.000037275884,0.41608554,0.0000565465,0.00018407262,0.00050340215,0.000009361402,0.000017106304,0.0001434431],"genre_scores_gemma":[0.99563235,0.00007375905,0.0040785996,0.0000072291964,0.000011249553,0.000017096014,0.000005925527,0.0000037803354,0.000170037],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9990699,0.000013300724,0.00048547125,0.000053810472,0.00029593444,0.00008154319],"domain_scores_gemma":[0.9989368,0.00003432679,0.00072908733,0.00021436508,0.000060256694,0.000025219415],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0007700132,0.00006956382,0.000121936995,0.00006653897,0.00006802426,0.00005454863,0.00018838418,0.000034531015,0.0000024601804],"category_scores_gemma":[0.000013786528,0.000045647565,0.00002554658,0.00011195163,0.000032111653,0.0026814304,0.000040337884,0.000056340108,0.000015127092],"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":[0.00010807782,0.000026230118,0.0030405119,0.0009452352,0.000043994492,2.8029035e-7,0.0012820712,0.96144694,0.011415086,0.0023390488,0.0004986624,0.018853858],"study_design_scores_gemma":[0.0004937738,0.00009984506,0.0015103634,0.00011590847,0.000027864713,0.00003174798,0.0035462317,0.977913,0.014951529,0.000014873269,0.0012202789,0.00007455577],"about_ca_topic_score_codex":0.0000035684614,"about_ca_topic_score_gemma":3.4777528e-7,"teacher_disagreement_score":0.41266906,"about_ca_system_score_codex":0.00008506792,"about_ca_system_score_gemma":0.0000052239443,"threshold_uncertainty_score":0.19439723},"labels":[],"label_agreement":null},{"id":"W2967734124","doi":"10.2514/1.c035114","title":"Generalized Sizing Methodology for Hybrid Aircraft Using Integrated Performance Constraints","year":2019,"lang":"en","type":"article","venue":"Journal of Aircraft","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":10,"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 Calgary","funders":"","keywords":"Sizing; Wing; Engineering; Automotive engineering; Aerospace engineering; Propeller; Fixed wing; Power (physics); Takeoff and landing; Process (computing); Airworthiness; Computer science; Marine engineering","score_opus":0.05073694616835252,"score_gpt":0.2958325674696148,"score_spread":0.24509562130126228,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2967734124","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":[0.795145,0.0001233981,0.20339112,0.00024844098,0.0005112489,0.00027306695,0.0000068170507,0.00005504136,0.00024586424],"genre_scores_gemma":[0.6213471,0.0000659911,0.37804782,0.00021712885,0.000053084867,0.000003445967,0.0000015410266,0.000022582855,0.00024128665],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99821585,0.000117573516,0.0006458827,0.00027202923,0.00029846872,0.0004501931],"domain_scores_gemma":[0.99871165,0.00032789368,0.00052092207,0.00025569645,0.00007813379,0.000105711064],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0009774894,0.00023714876,0.0005348921,0.00015256021,0.00011480156,0.000026473203,0.00047777707,0.00012744287,0.00080629694],"category_scores_gemma":[0.00033883192,0.00019039528,0.0002170966,0.00024289486,0.00037136202,0.0005473424,0.00012064071,0.00037857488,0.00007367737],"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":[0.0005672767,0.000157249,0.050801646,0.00007706453,0.00016995851,0.000081119375,0.00023815513,0.035421412,0.7187293,0.00035721195,0.0019376591,0.1914619],"study_design_scores_gemma":[0.012665422,0.0043959613,0.012706018,0.00063873554,0.0004050826,0.0054077674,0.0021073767,0.08152076,0.725023,0.018405898,0.13443546,0.0022885827],"about_ca_topic_score_codex":0.000013627467,"about_ca_topic_score_gemma":0.0000026831708,"teacher_disagreement_score":0.18917333,"about_ca_system_score_codex":0.0002677443,"about_ca_system_score_gemma":0.000070543945,"threshold_uncertainty_score":0.8828386},"labels":[],"label_agreement":null},{"id":"W2973081103","doi":"10.1115/gt2019-90617","title":"Capacity Matching of Aeroderivative Gas Generator With Free Power Turbine: Challenges, Uncertainties, and Opportunities","year":2019,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Siemens (Canada)","funders":"","keywords":"Turbine; Power (physics); Generator (circuit theory); Range (aeronautics); Matching (statistics); Electricity generation; Automotive engineering; Sensitivity (control systems); Computer science; Gas turbines; Electric generator; Gas generator; Engineering; Mechanical engineering; Aerospace engineering; Mathematics; Electronic engineering","score_opus":0.030207471179393996,"score_gpt":0.20483275689031286,"score_spread":0.17462528571091887,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2973081103","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":[0.97454995,0.00043323927,0.0015450488,0.0009860827,0.000027137745,0.00017428385,0.000008337108,0.00010525157,0.022170695],"genre_scores_gemma":[0.98518264,0.0007228869,0.013125954,0.00012727205,0.0000035231528,0.000007885071,0.0000012354811,0.0000113117,0.0008172944],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99926186,0.000020403353,0.00011891066,0.00023963941,0.00018309338,0.00017609392],"domain_scores_gemma":[0.9995079,0.00004087674,0.000068831505,0.0003297205,0.000010437463,0.000042228014],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000089976566,0.00013815695,0.0001748431,0.000027557293,0.000042871343,0.000009177864,0.00018889052,0.00005750538,0.00067579345],"category_scores_gemma":[0.000013634804,0.00009568692,0.000015722446,0.00005559492,0.00037503717,0.000254813,0.00020822801,0.000098143886,0.000012209546],"study_design_candidate":"theoretical_or_conceptual","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":[0.0004514628,0.0005446322,0.07334105,0.00038260067,0.00035512092,0.00008808889,0.017829897,0.0025595787,0.26796132,0.45084593,0.0058873603,0.17975296],"study_design_scores_gemma":[0.006783048,0.0053387387,0.114623174,0.00047839314,0.00009601961,0.0002025271,0.0831121,0.0015395195,0.37677836,0.33342308,0.073530816,0.0040941956],"about_ca_topic_score_codex":0.00019443755,"about_ca_topic_score_gemma":0.00013439715,"teacher_disagreement_score":0.17565878,"about_ca_system_score_codex":0.000038723952,"about_ca_system_score_gemma":0.000007798641,"threshold_uncertainty_score":0.7399464},"labels":[],"label_agreement":null},{"id":"W2978421172","doi":"10.2514/6.2014-2592","title":"Stability and Control Effects on the Design Optimization of a Box-Wing Aircraft","year":2014,"lang":"en","type":"article","venue":"14th AIAA Aviation Technology, Integration, and Operations Conference","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":12,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Royal Military College of Canada","funders":"","keywords":"Wing; Stability (learning theory); Computer science; Control (management); Aerospace engineering; Engineering; Artificial intelligence","score_opus":0.012693553746400747,"score_gpt":0.21832001479687996,"score_spread":0.20562646105047921,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2978421172","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":[0.06779046,0.000029341292,0.92633766,0.004668144,0.0000398937,0.00067023124,0.00000506829,0.00017703387,0.0002821471],"genre_scores_gemma":[0.9605616,0.00008080404,0.03890431,0.0002176279,0.000009771842,0.00017071771,0.0000070842266,0.000008178775,0.00003992202],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9988715,0.00019560121,0.00028715,0.0003384079,0.00015119468,0.00015613958],"domain_scores_gemma":[0.9990221,0.000409677,0.0001008062,0.00033345266,0.00010049461,0.000033441036],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00047520793,0.0001732604,0.00019202838,0.00011374167,0.00040817528,0.00006281243,0.00018917568,0.00018041114,0.00009929591],"category_scores_gemma":[0.0013485982,0.00012059674,0.000020799294,0.00035903315,0.0005939151,0.00030437563,0.00005366854,0.00020788258,0.000008732717],"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":[0.00007148496,0.0002256937,0.028659584,0.0000420927,0.000047346126,8.244085e-7,0.0015211204,0.053489815,0.20206659,0.5369322,0.00024175119,0.17670152],"study_design_scores_gemma":[0.0008765305,0.00069520815,0.0069479314,0.00008692135,0.000044194927,0.0000060241646,0.00097562274,0.56019634,0.38396263,0.04568946,0.00018493153,0.00033421596],"about_ca_topic_score_codex":0.00003745787,"about_ca_topic_score_gemma":0.00009516419,"teacher_disagreement_score":0.8927711,"about_ca_system_score_codex":0.000047408525,"about_ca_system_score_gemma":0.000021797827,"threshold_uncertainty_score":0.49177924},"labels":[],"label_agreement":null},{"id":"W2985522692","doi":"","title":"Impact of aviation emissions on UTLS and air quality in current and future climate - GEM-AC model simulations","year":2015,"lang":"en","type":"article","venue":"AGU Fall Meeting Abstracts","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"York University","funders":"","keywords":"Environmental science; Air quality index; Climatology; Meteorology; Aviation; Atmospheric sciences; Engineering; Geography; Geology; Aerospace engineering","score_opus":0.04438650877500772,"score_gpt":0.3363386037587766,"score_spread":0.2919520949837689,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2985522692","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":[0.9979755,0.000089200985,0.00010920913,0.00016792942,0.000026062615,0.00012487796,0.000020015104,0.00005201739,0.0014351571],"genre_scores_gemma":[0.99797106,0.00011489102,0.0018658211,0.000013054751,0.000012739031,0.0000033962017,0.0000069884168,0.00000650841,0.0000055158557],"study_design_codex":"simulation_or_modeling","study_design_gemma":"observational","domain_scores_codex":[0.9991764,0.00003074414,0.00024353368,0.00020798648,0.00016334248,0.00017798287],"domain_scores_gemma":[0.9995015,0.00011151959,0.00014476242,0.00014308559,0.000010362272,0.00008873425],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00030127008,0.000108906876,0.00013199003,0.0000436274,0.000060936767,0.000009131169,0.00006502806,0.0000756441,0.000001539783],"category_scores_gemma":[0.00026403132,0.000088696106,0.000021229727,0.00010486295,0.00007712478,0.00017753955,0.000078804434,0.00015062667,0.0000040604245],"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":[0.00003214238,0.00011089101,0.48762754,0.000014484509,0.0000028081333,0.0000012298062,0.0005340016,0.48826638,0.0039108484,0.00012796608,0.000038773036,0.01933296],"study_design_scores_gemma":[0.00033394527,0.00006962084,0.9659411,0.000055177978,0.000004716186,9.138543e-7,0.00018291222,0.025838975,0.00039368073,0.0070160893,0.00003597443,0.00012693145],"about_ca_topic_score_codex":0.00068442157,"about_ca_topic_score_gemma":0.0004387591,"teacher_disagreement_score":0.47831354,"about_ca_system_score_codex":0.000087654094,"about_ca_system_score_gemma":0.000012143331,"threshold_uncertainty_score":0.36169222},"labels":[],"label_agreement":null},{"id":"W2995976509","doi":"10.2514/1.c035437","title":"Systematic Methodology for Aircraft Concept Development with Application to Transitional Aircraft","year":2019,"lang":"en","type":"article","venue":"Journal of Aircraft","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":7,"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 Calgary","funders":"","keywords":"Aerospace engineering; Aeronautics; Development (topology); Computer science; Aileron; Systems engineering; Engineering; Environmental science; Aerodynamics; Mathematics","score_opus":0.01745604679409369,"score_gpt":0.26432237426545824,"score_spread":0.24686632747136456,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2995976509","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.08079887,0.00009768331,0.91548705,0.0016394698,0.00017607161,0.0015107208,0.000006808339,0.00007773598,0.00020560209],"genre_scores_gemma":[0.51106495,0.0000054175493,0.48759428,0.0006046536,0.000052736028,0.0001411334,0.0000046574633,0.000032570802,0.00049957796],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9976978,0.00011511418,0.00084373774,0.00036386008,0.0005766157,0.00040292143],"domain_scores_gemma":[0.9983968,0.00050012034,0.00048481103,0.00032757936,0.0001131919,0.00017747222],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00094958226,0.00027035887,0.0006811396,0.00017029449,0.000118605014,0.000024492718,0.0005331936,0.00014842187,0.00022500439],"category_scores_gemma":[0.00015156151,0.0001995085,0.0001534414,0.00035245356,0.00013903483,0.00035463873,0.00006891235,0.00024123043,0.0002752983],"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":[0.0048140287,0.0023964725,0.03657752,0.010264379,0.0022149426,0.00024007028,0.016297208,0.32599765,0.46370527,0.01043631,0.020342886,0.10671327],"study_design_scores_gemma":[0.031135455,0.021576524,0.087084964,0.013865719,0.0019143723,0.0068361363,0.016637716,0.0077390703,0.4478399,0.04315952,0.31359765,0.008612999],"about_ca_topic_score_codex":0.000005145201,"about_ca_topic_score_gemma":0.000019436537,"teacher_disagreement_score":0.4302661,"about_ca_system_score_codex":0.00033348726,"about_ca_system_score_gemma":0.00009070348,"threshold_uncertainty_score":0.8135721},"labels":[],"label_agreement":null},{"id":"W2997352881","doi":"10.26467/2079-0619-2019-22-6-8-16","title":"The impact of physico-chemical properties of the jet fuel and biofuels on the characteristics of gas-turbine engines","year":2019,"lang":"en","type":"article","venue":"Civil Aviation High TECHNOLOGIES","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"International Civil Aviation Organization","funders":"","keywords":"Jet fuel; Renewable fuels; Work (physics); Fuel oil; Fuel efficiency; Renewable energy; Aviation biofuel; Fossil fuel; Jet engine; Aviation; Biofuel; Turboprop; Environmental science; Coal; Aviation fuel; Natural gas; Engineering; Waste management; Automotive engineering; Bioenergy; Mechanical engineering; Aerospace engineering","score_opus":0.00862423145562451,"score_gpt":0.1997832961661647,"score_spread":0.19115906471054017,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2997352881","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":[0.9978437,0.00018836168,0.000046230845,0.0013047551,0.0000397966,0.00031592164,0.000019109453,0.00012856636,0.00011358423],"genre_scores_gemma":[0.9995124,0.00032823757,0.00008125239,0.0000072172647,0.0000037918526,0.000022072783,9.794264e-7,0.000007700438,0.000036347148],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9992499,0.000021817788,0.00023383339,0.00015246945,0.0001974443,0.0001445523],"domain_scores_gemma":[0.9989381,0.00017170736,0.00030589537,0.0005515343,0.000026832553,0.0000059755425],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00011496155,0.00013633305,0.00019882881,0.000031008043,0.000063956904,0.000009519095,0.00053448405,0.00010816003,0.00001551125],"category_scores_gemma":[0.0004517557,0.000053865566,0.000071913695,0.00029819176,0.00115693,0.00008366345,0.000326574,0.00016206963,0.0000060668767],"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":[0.000031778374,0.00006158665,0.05884635,0.00003625492,0.000025372243,8.3924135e-8,0.00013380377,0.000038252183,0.91750723,0.0058391546,0.000088540284,0.0173916],"study_design_scores_gemma":[0.00012363371,0.00014848137,0.09949425,0.00006339736,0.000009380412,9.627341e-7,0.0003739526,0.00017008383,0.86223364,0.037236627,0.000058975354,0.000086596265],"about_ca_topic_score_codex":0.000033087512,"about_ca_topic_score_gemma":0.000003466089,"teacher_disagreement_score":0.055273563,"about_ca_system_score_codex":0.000040191015,"about_ca_system_score_gemma":0.000007921909,"threshold_uncertainty_score":0.42627567},"labels":[],"label_agreement":null},{"id":"W3000390911","doi":"10.1108/aeat-11-2018-0286","title":"NRC particle detection probe: test cell to flight","year":2020,"lang":"en","type":"article","venue":"Aircraft Engineering and Aerospace Technology","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"National Research Council Canada","funders":"","keywords":"Flight test; Engineering; Fuselage; Aeronautics; Aerospace engineering; European union; Pitot tube; Takeoff; Environmental science; Physics","score_opus":0.00514125014989617,"score_gpt":0.1788113341669535,"score_spread":0.17367008401705733,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3000390911","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":[0.73754567,0.00020661183,0.24138783,0.017234998,0.00006468523,0.00036877912,0.000003119729,0.0029774413,0.00021087736],"genre_scores_gemma":[0.9798863,0.000033448527,0.019566227,0.00025958577,0.000018905053,0.000067741086,3.0065908e-7,0.000026567433,0.00014093118],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9989208,0.000003964843,0.00013684234,0.00041627733,0.0001407583,0.0003813874],"domain_scores_gemma":[0.99955875,0.00003529867,0.000028804889,0.00022482203,0.000009610122,0.00014272596],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000059885708,0.00018761634,0.00016957402,0.00005193289,0.000085365195,0.000018954368,0.00021400081,0.00016814271,0.000035226847],"category_scores_gemma":[0.00033469914,0.00018303897,0.000024246274,0.00079522544,0.00010558372,0.0001472692,0.0002782248,0.00024841234,0.00030859586],"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":[0.0000048411844,0.000028185394,0.0067368397,0.000015351927,0.000003306228,0.000013531076,0.00010910384,0.004683289,0.97476435,0.00017672496,0.0003606058,0.013103873],"study_design_scores_gemma":[0.00032705374,0.00059608684,0.0016598736,0.000013743602,0.000010786772,0.000019287221,0.00016921677,0.014923434,0.94358295,0.00036902074,0.037946504,0.00038202375],"about_ca_topic_score_codex":0.000010007987,"about_ca_topic_score_gemma":0.000012241135,"teacher_disagreement_score":0.24234064,"about_ca_system_score_codex":0.00006814553,"about_ca_system_score_gemma":0.0000035954288,"threshold_uncertainty_score":0.74641126},"labels":[],"label_agreement":null},{"id":"W3009722352","doi":"10.5539/jms.v10n1p83","title":"Decision Support System for Selecting Sustainable Alternatives to Conventional Jet Fuel: Impact of Emissions, Production Costs and Carbon Pricing","year":2020,"lang":"en","type":"article","venue":"Journal of Management and Sustainability","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Greenhouse gas; Jet fuel; Emissions trading; Profitability index; Carbon offset; Production (economics); Aviation; Business; Natural resource economics; Environmental economics; Aviation biofuel; Aviation fuel; Environmental science; European union; Waste management; Finance; Economics; Biofuel; Engineering; International trade; Microeconomics","score_opus":0.010164424121041566,"score_gpt":0.2783195766320218,"score_spread":0.2681551525109802,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3009722352","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":[0.97268146,0.00009252204,0.025527675,0.00067575247,0.00003406637,0.0007404796,9.0019654e-7,0.000019092071,0.00022806037],"genre_scores_gemma":[0.99467254,0.00004008639,0.005123909,0.000010316062,0.000021963187,0.0000088924835,3.9896344e-7,0.0000058273636,0.00011609344],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.9990124,0.000038597653,0.00033583344,0.00020703078,0.00021767057,0.00018844611],"domain_scores_gemma":[0.999362,0.00008210172,0.00023831255,0.000080909245,0.00013684356,0.00009984912],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00083130127,0.00010160626,0.00020888218,0.00008439672,0.000092950526,0.000022289494,0.00010336283,0.00003131952,0.000006830091],"category_scores_gemma":[0.00079229445,0.000075658725,0.00006226677,0.0002309718,0.000069714675,0.00023858064,0.0001964142,0.00008816208,8.7312614e-8],"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":[0.001506848,0.00015189743,0.8894171,0.0022219736,0.0001333946,0.00005885982,0.0014363544,0.0052330326,0.001288501,0.0014158533,0.0007698402,0.096366316],"study_design_scores_gemma":[0.0044959164,0.0069653764,0.80308694,0.0004398451,0.00029834727,0.00012576183,0.11841888,0.0071868417,0.00873345,0.04244518,0.007059175,0.0007442696],"about_ca_topic_score_codex":0.00003013851,"about_ca_topic_score_gemma":0.0000016096415,"teacher_disagreement_score":0.11698253,"about_ca_system_score_codex":0.00062884303,"about_ca_system_score_gemma":0.000030148936,"threshold_uncertainty_score":0.30852732},"labels":[],"label_agreement":null},{"id":"W3013279455","doi":"10.1108/aeat-06-2019-0119","title":"Optimum sub-megawatt electric-hybrid power source selection","year":2020,"lang":"en","type":"article","venue":"Aircraft Engineering and Aerospace Technology","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Automotive engineering; Turbine; Engineering; Recuperator; Power density; Overall pressure ratio; Power (physics); Mechanical engineering; Gas compressor","score_opus":0.004118394180605377,"score_gpt":0.17746423195518155,"score_spread":0.17334583777457616,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3013279455","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":[0.7734001,0.0003749596,0.2164289,0.0062502148,0.000054611824,0.00019060235,0.0000014569326,0.0031374814,0.00016166834],"genre_scores_gemma":[0.98845994,0.00013804845,0.010936444,0.00024337067,0.00002156312,0.000034214976,0.000001343289,0.000043224267,0.0001218617],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99863106,0.0000080903355,0.00017178182,0.0005268003,0.00014469105,0.00051759667],"domain_scores_gemma":[0.99957675,0.000033792272,0.00005217979,0.00020942063,0.000009306724,0.00011853342],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.000062866966,0.00026902132,0.00024988645,0.00011367389,0.00012126749,0.00002556496,0.0002677171,0.00021826263,0.00006398527],"category_scores_gemma":[0.00016488107,0.00027266156,0.000043764583,0.000919695,0.00014270135,0.00016937879,0.0002388672,0.0004906264,0.00015248563],"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":[0.000018378018,0.000039198287,0.015089614,0.00001950258,0.000031784824,0.000025464957,0.00009623221,0.032583654,0.92859924,0.00093445624,0.003189324,0.019373158],"study_design_scores_gemma":[0.0009834951,0.0011944858,0.0027127774,0.000035936606,0.000040486964,0.00031077812,0.00023412002,0.115577534,0.7627594,0.0011729022,0.11369144,0.0012866722],"about_ca_topic_score_codex":0.000008760008,"about_ca_topic_score_gemma":0.0000018642883,"teacher_disagreement_score":0.21505983,"about_ca_system_score_codex":0.00007686231,"about_ca_system_score_gemma":0.000006337646,"threshold_uncertainty_score":0.9999726},"labels":[],"label_agreement":null},{"id":"W3019164457","doi":"10.3390/atmos11040418","title":"Aircraft Takeoff Performance in a Changing Climate for Canadian Airports","year":2020,"lang":"en","type":"article","venue":"Atmosphere","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":15,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"McGill University","funders":"Trottier Institute for Sustainability in Engineering and Design; Transport Canada; Compute Canada","keywords":"Takeoff; Crosswind; Environmental science; Takeoff and landing; Atmospheric sciences; Climate change; Climatology; Meteorology; Geography; Aerospace engineering; Geology; Engineering","score_opus":0.012815735190220303,"score_gpt":0.20742825475280968,"score_spread":0.19461251956258938,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3019164457","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":[0.97715425,0.00011361924,0.0028311291,0.003539147,0.0000902752,0.00062070624,0.000013217994,0.0002602716,0.0153774],"genre_scores_gemma":[0.98807955,0.000046708556,0.010340593,0.0012168478,0.000022949182,0.00007283826,0.000004748393,0.000018508688,0.00019728173],"study_design_codex":"observational","study_design_gemma":"not_applicable","domain_scores_codex":[0.9988468,0.0000057217785,0.00013586882,0.00028081718,0.00008908541,0.00064167514],"domain_scores_gemma":[0.9996595,0.00001606672,0.000035822064,0.00014422934,0.0000033191047,0.00014107962],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00009240451,0.00012114575,0.00012571891,0.0000065117993,0.00015993179,0.000012723678,0.0002017197,0.00007434714,0.00048323654],"category_scores_gemma":[0.000036720165,0.000118759024,0.00003393725,0.0004755289,0.000065053086,0.0002088427,0.00009988059,0.00010665649,0.00023842149],"study_design_candidate":"observational","study_design_consensus":null,"about_ca_topic_candidate":true,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000040235358,0.000026600357,0.8065214,0.00006947227,0.00000746356,0.00010447861,0.0012136495,0.01816911,0.0007080157,0.0010188813,0.0029080487,0.16921261],"study_design_scores_gemma":[0.001894347,0.0006276488,0.18340851,0.00013417748,0.00002249845,0.000025655798,0.0029522993,0.16105404,0.005559509,0.0019794472,0.6409582,0.0013836953],"about_ca_topic_score_codex":0.001726538,"about_ca_topic_score_gemma":0.020720867,"teacher_disagreement_score":0.63805014,"about_ca_system_score_codex":0.00014705988,"about_ca_system_score_gemma":0.000020305924,"threshold_uncertainty_score":0.99714845},"labels":[],"label_agreement":null},{"id":"W3022081099","doi":"10.1021/acs.energyfuels.0c00260","title":"Comparison of Particle Number Emissions from In-Flight Aircraft Fueled with Jet A1, JP-5 and an Alcohol-to-Jet Fuel Blend","year":2020,"lang":"en","type":"article","venue":"Energy & Fuels","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":33,"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; University of Alberta","funders":"","keywords":"Jet fuel; Environmental science; Greenhouse gas; Aviation fuel; Kerosene; Particle number; Waste management; Nuclear engineering; Chemistry; Physics; Engineering; Nuclear physics","score_opus":0.02562985094672684,"score_gpt":0.28227288494067,"score_spread":0.25664303399394317,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3022081099","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":[0.99239075,0.00014772215,0.0035212152,0.0012559308,0.00002362444,0.00010806275,0.000018298975,0.00013632551,0.0023980464],"genre_scores_gemma":[0.98978335,0.000047097346,0.009504303,0.0004548512,0.000024363551,0.000025387557,0.000010358157,0.000022645281,0.00012762393],"study_design_codex":"observational","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9985727,0.000053870488,0.0002906165,0.00049873017,0.00025706197,0.00032703325],"domain_scores_gemma":[0.99922395,0.000076847835,0.00008730345,0.0003337721,0.0000081447415,0.0002699759],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00005713576,0.00021343188,0.00035898984,0.000019389108,0.00006652627,0.000019582838,0.00028963864,0.00009751662,0.0008145313],"category_scores_gemma":[0.000041365438,0.00016497988,0.00003027018,0.00041876984,0.00021839459,0.000279561,0.00022831808,0.00014398342,0.0000648877],"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":[0.00014084062,0.00019873587,0.64396155,0.000007881078,0.000017948856,0.000027707016,0.001233774,0.00073083304,0.34460202,0.0007188593,0.000622683,0.007737173],"study_design_scores_gemma":[0.0014597306,0.00066484,0.14846818,0.000051789855,0.000035103865,0.0000044195976,0.0013211631,0.0015651494,0.8232675,0.005190941,0.01741848,0.00055269874],"about_ca_topic_score_codex":0.00044153442,"about_ca_topic_score_gemma":0.00082517683,"teacher_disagreement_score":0.49549335,"about_ca_system_score_codex":0.0000343878,"about_ca_system_score_gemma":0.000011075333,"threshold_uncertainty_score":0.89185464},"labels":[],"label_agreement":null},{"id":"W3033221360","doi":"10.1177/1687814020923178","title":"Design optimization of multi-objective proportional–integral–derivative controllers for enhanced handling quality of a twin-engine, propeller-driven airplane","year":2014,"lang":"en","type":"article","venue":"Advances in Mechanical Engineering","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":14,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"Mitacs","keywords":"Propeller; Airplane; Particle swarm optimization; Control theory (sociology); Genetic algorithm; Sensitivity (control systems); Engineering; Stability (learning theory); Propulsion; Stability derivatives; Aerodynamics; Range (aeronautics); Computer science; Mathematical optimization; Mathematics; Aerospace engineering; Control (management); Marine engineering","score_opus":0.017433959111397564,"score_gpt":0.2669283205936873,"score_spread":0.24949436148228976,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3033221360","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0059753885,0.00009326515,0.9928342,0.000019454339,0.00007731718,0.00085239875,0.0000065860254,0.000087402484,0.00005397608],"genre_scores_gemma":[0.576166,0.00004913385,0.42364195,0.000005297714,0.0000060025836,0.00010661543,0.0000037263305,0.0000124711505,0.00000881697],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9986165,0.000054043383,0.0005421316,0.00032640854,0.00020912125,0.0002517964],"domain_scores_gemma":[0.99893904,0.0005377398,0.00026252744,0.00017770434,0.00004512925,0.000037882844],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00048912904,0.0001856176,0.00044247945,0.00007986857,0.000031854044,0.0000037377276,0.00021663871,0.0001021355,0.00002354824],"category_scores_gemma":[0.0015311458,0.00016274599,0.000071263275,0.00028522976,0.00012213827,0.00030778983,0.00006221021,0.00015559701,0.0000014025981],"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":[0.00012333211,0.000061972256,0.000045239904,0.000051964864,0.000010833335,2.2915157e-7,0.000071909104,0.8268818,0.16527417,0.0015231434,4.0436356e-7,0.0059549822],"study_design_scores_gemma":[0.0011091398,0.00021821224,0.00006230169,0.00008584374,0.000006051503,3.8326533e-7,0.00007808366,0.694445,0.3024184,0.0013971943,0.000026406371,0.00015295557],"about_ca_topic_score_codex":0.000009247665,"about_ca_topic_score_gemma":0.0000087961525,"teacher_disagreement_score":0.5701906,"about_ca_system_score_codex":0.000105699015,"about_ca_system_score_gemma":0.000010755189,"threshold_uncertainty_score":0.66365886},"labels":[],"label_agreement":null},{"id":"W3034259591","doi":"10.2514/6.2020-2646","title":"Mainstream Flow Prediction for the Thermal Risk Assessment of Aircraft Systems in Conceptual Design","year":2020,"lang":"en","type":"article","venue":"AIAA AVIATION 2020 FORUM","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Concordia University","funders":"","keywords":"Conceptual design; Computer science; Risk assessment; Thermal; Systems engineering; Engineering; Mechanical engineering; Meteorology","score_opus":0.018325564742757934,"score_gpt":0.24071805732336932,"score_spread":0.2223924925806114,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3034259591","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":[0.022987906,0.00010472664,0.9721198,0.0028549626,0.00017119518,0.0012548526,0.00008787089,0.0001268268,0.00029182932],"genre_scores_gemma":[0.98811007,0.00006302916,0.011340949,0.00017697246,0.000034727484,0.00021094576,0.000016154754,0.0000121994,0.000034944336],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99896204,0.000080465055,0.00028558235,0.00023458745,0.00022870017,0.00020861538],"domain_scores_gemma":[0.9993691,0.00024404991,0.0001744297,0.00016318036,0.000012942317,0.000036321388],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002546735,0.00011288265,0.00014479923,0.000017044173,0.00011305317,0.000015201826,0.00021585183,0.00008185588,0.00007626513],"category_scores_gemma":[0.00014148236,0.000083460145,0.000052820687,0.00024789834,0.00015384528,0.00022901526,0.00007538379,0.00013883162,0.000018261759],"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":[0.00007498576,0.000071326875,0.24483022,0.000014580504,0.000033625187,0.0000018881295,0.0006740224,0.699902,0.0096006645,0.0016218692,0.005478986,0.03769585],"study_design_scores_gemma":[0.00091163546,0.00048312006,0.08659862,0.000013667926,0.000028818073,0.0000010199986,0.002294665,0.9020578,0.0025007555,0.000927825,0.0040445062,0.00013752813],"about_ca_topic_score_codex":0.00006765576,"about_ca_topic_score_gemma":0.000017421211,"teacher_disagreement_score":0.96512216,"about_ca_system_score_codex":0.000112344744,"about_ca_system_score_gemma":0.000018728679,"threshold_uncertainty_score":0.3403406},"labels":[],"label_agreement":null},{"id":"W3036544735","doi":"10.7939/r3-3f0w-pw98","title":"Particle Number Emission Indices from In-flight Aircraft","year":2020,"lang":"en","type":"article","venue":"University of Alberta Library","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Aeronautics; Environmental science; Meteorology; Physics; Engineering","score_opus":0.007997026067008119,"score_gpt":0.17489452666080943,"score_spread":0.16689750059380132,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3036544735","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":[0.9691706,0.0000241553,0.00015805547,0.00472976,0.000011443044,0.00005784886,0.0000023665252,0.00007259556,0.025773186],"genre_scores_gemma":[0.9947523,0.00004474593,0.0032269296,0.00028919516,0.0000062661234,6.906398e-8,0.0000071698773,0.000005791564,0.0016675224],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.9994912,0.000019511312,0.00007227765,0.0002020722,0.000093150404,0.00012179142],"domain_scores_gemma":[0.9996808,0.000075993485,0.000044139124,0.00011855342,7.570568e-7,0.00007976526],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.000009296024,0.0000701975,0.000105053216,0.000008245889,0.00004149421,0.000005082013,0.00030365636,0.000064278494,0.007709973],"category_scores_gemma":[0.000016493703,0.00007314805,0.00003141688,0.00023411613,0.00014532504,0.0007979561,0.00033328656,0.000089318295,0.000494217],"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":[0.000066083616,0.000049992934,0.98276985,0.0000043455702,0.0000059502095,0.000039453724,0.0033100196,0.00008002695,0.0049498924,0.00019633825,0.0059580654,0.0025699735],"study_design_scores_gemma":[0.0021826106,0.00019488094,0.47376212,0.000094292336,0.00003168091,0.0000022194088,0.006834291,0.004203925,0.1823941,0.009346656,0.3202569,0.0006963006],"about_ca_topic_score_codex":0.00095894764,"about_ca_topic_score_gemma":0.00008797775,"teacher_disagreement_score":0.5090077,"about_ca_system_score_codex":0.000012080032,"about_ca_system_score_gemma":0.0000070370256,"threshold_uncertainty_score":0.99319714},"labels":[],"label_agreement":null},{"id":"W3041912093","doi":"","title":"Electrification of Airport Operations:Electric Powered Tow-Truck Utilizationin Taxiing Operations","year":2019,"lang":"en","type":"dissertation","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Aviation; Fuel efficiency; Civil aviation; Electrification; Truck; Transport engineering; Engineering; Airplane; Greenhouse gas; Aviation engineering; Aeronautics; Consumption (sociology); Environmental science; Automotive engineering; Electricity","score_opus":0.010904413578999487,"score_gpt":0.2536550594265774,"score_spread":0.2427506458475779,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3041912093","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":[0.7190312,0.0010028317,0.1350556,0.00042234952,0.000949846,0.0042208694,0.000046232213,0.001053454,0.13821763],"genre_scores_gemma":[0.946569,0.00042007142,0.008999689,0.000052140305,0.000015376354,0.000106816056,0.0012250559,0.000045736535,0.04256608],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99806845,0.00004177442,0.0006117441,0.00056841876,0.00041730911,0.0002923251],"domain_scores_gemma":[0.9990935,0.000035829744,0.00017221917,0.0005684433,0.00008447354,0.00004555993],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00014617981,0.00030137875,0.00034445667,0.00023390849,0.00025753674,0.000052668893,0.00043821643,0.00038918635,0.002283537],"category_scores_gemma":[0.0002080926,0.00029079453,0.00009858047,0.0010100757,0.000054006006,0.00043590943,0.000025431626,0.00028933524,0.0004260187],"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":[0.0000608936,0.0002911908,0.006186206,0.00008418211,0.00007357655,0.000002598155,0.000613462,0.034606155,0.8930524,0.024897862,0.001995969,0.038135517],"study_design_scores_gemma":[0.0007867539,0.00043581123,0.042175487,0.00012583357,0.00015728881,0.000013007475,0.0018660395,0.048427913,0.8982763,0.003961589,0.0023316096,0.0014423332],"about_ca_topic_score_codex":0.00039760547,"about_ca_topic_score_gemma":0.0011693682,"teacher_disagreement_score":0.22753786,"about_ca_system_score_codex":0.00022303636,"about_ca_system_score_gemma":0.000125493,"threshold_uncertainty_score":0.9999544},"labels":[],"label_agreement":null},{"id":"W3048177207","doi":"10.1007/s13272-020-00462-x","title":"Blade element momentum new methodology and wind tunnel test performance evaluation for the UAS-S45 Bàlaam propeller","year":2020,"lang":"en","type":"article","venue":"CEAS Aeronautical Journal","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":16,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure","funders":"Canada Research Chairs","keywords":"Propeller; Blade element momentum theory; Wind tunnel; Computational fluid dynamics; Propulsion; Engineering; Aerodynamics; Blade element theory; Thrust; Aerospace engineering; Marine engineering; Performance prediction; Turbulence; Advance ratio; Lift coefficient; Lift (data mining); Structural engineering; Blade pitch; Simulation; Reynolds number; Computer science; Mechanics; Physics","score_opus":0.11265947582411362,"score_gpt":0.3061058789933794,"score_spread":0.19344640316926576,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3048177207","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":[0.4110998,0.0017997714,0.48010355,0.1028927,0.00042617158,0.0023539232,0.000008526292,0.00014936474,0.0011662231],"genre_scores_gemma":[0.9658392,0.00031636644,0.032235388,0.0011220505,0.00019760798,0.000019456342,0.0000015157524,0.000015391266,0.00025302352],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9986489,0.00008222474,0.00026875152,0.00026199265,0.00038444993,0.0003537084],"domain_scores_gemma":[0.9991417,0.000397814,0.000098224955,0.00013217832,0.000019832205,0.00021025502],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0008388156,0.00014886053,0.00016517464,0.000016013342,0.0003194945,0.000051599476,0.00028860668,0.00007564834,0.001014394],"category_scores_gemma":[0.00078071066,0.00009125046,0.000048890048,0.00012115913,0.00031105865,0.00019374334,0.00018845001,0.00034668535,0.00006464818],"study_design_candidate":"design_other","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":[0.00025146906,0.00013181687,0.016899131,0.000020835223,0.00007815512,0.00000883865,0.00075459445,0.006395258,0.039757468,0.0009490118,0.013512676,0.92124075],"study_design_scores_gemma":[0.0074090892,0.005115355,0.30741313,0.00007969631,0.0006429666,0.0005015176,0.0020868182,0.41571414,0.021710876,0.054877892,0.18333125,0.0011172495],"about_ca_topic_score_codex":0.0000020639948,"about_ca_topic_score_gemma":0.0000022082068,"teacher_disagreement_score":0.9201235,"about_ca_system_score_codex":0.000119524135,"about_ca_system_score_gemma":0.000042542975,"threshold_uncertainty_score":0.9998988},"labels":[],"label_agreement":null},{"id":"W3049392569","doi":"10.1016/j.cja.2020.07.017","title":"Review of hybrid electric powered aircraft, its conceptual design and energy management methodologies","year":2020,"lang":"en","type":"article","venue":"Chinese Journal of Aeronautics","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":205,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Dalhousie University; York University","funders":"Science and Technology Department of Zhejiang Province; Innovate UK; China Scholarship Council; Cranfield University","keywords":"Propulsion; Context (archaeology); Systems engineering; Energy management; Electrically powered spacecraft propulsion; Conceptual design; Hybrid system; Engineering; Hybrid vehicle; Computer science; Aerospace engineering; Energy (signal processing); Mechanical engineering; Power (physics)","score_opus":0.04121203505086997,"score_gpt":0.2806293417995385,"score_spread":0.23941730674866857,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3049392569","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.043960154,0.14312688,0.8067199,0.0046781646,0.0001623569,0.00031211326,0.0000057475618,0.00010047957,0.0009342284],"genre_scores_gemma":[0.64140445,0.16069394,0.19545192,0.0023267427,0.000035517092,0.0000037056875,0.000001021208,0.000020556496,0.00006215193],"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9986378,0.00015738129,0.00053136406,0.00017521174,0.0002997738,0.00019846395],"domain_scores_gemma":[0.9990205,0.00025579194,0.00043770214,0.00014341822,0.000036716352,0.00010585924],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00046018857,0.00019377972,0.00048742833,0.00005171267,0.000042292395,0.000007407722,0.00039999894,0.00003927457,0.00012383306],"category_scores_gemma":[0.00064465776,0.0001314986,0.00009679444,0.00039562583,0.00022489026,0.00019569635,0.00023873217,0.00019301442,0.00000572116],"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":[0.0012170206,0.0005684525,0.0045935316,0.005085804,0.0010992932,0.0015998734,0.0011976719,0.014772617,0.25615555,0.008280693,0.058033008,0.6473965],"study_design_scores_gemma":[0.011103433,0.017099556,0.021082679,0.00875546,0.0021820278,0.0036377832,0.0016711473,0.020483049,0.563633,0.1350249,0.21123217,0.004094746],"about_ca_topic_score_codex":6.8628987e-7,"about_ca_topic_score_gemma":1.1393825e-7,"teacher_disagreement_score":0.6433017,"about_ca_system_score_codex":0.00005155142,"about_ca_system_score_gemma":0.000014922788,"threshold_uncertainty_score":0.53623575},"labels":[],"label_agreement":null},{"id":"W3052774193","doi":"10.2514/6.2020-3521","title":"Book-keeping Investigations for BLI Aircraft","year":2020,"lang":"en","type":"article","venue":"AIAA Propulsion and Energy 2020 Forum","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Safran Electronics (Canada)","funders":"","keywords":"Propulsor; Airframe; Aerodynamics; Fuselage; Context (archaeology); Computational fluid dynamics; Aerospace engineering; Engineering; Coupling (piping); Propulsion; Boundary layer; Computer science; Mechanical engineering; Geology","score_opus":0.014842328139927159,"score_gpt":0.22173065546237333,"score_spread":0.20688832732244616,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3052774193","genre_codex":"commentary","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":[0.02473268,0.0065513956,0.403656,0.5437342,0.000603244,0.0010950107,0.0000615272,0.0023752663,0.017190682],"genre_scores_gemma":[0.87504166,0.0011152915,0.04386018,0.07468462,0.00011546747,0.00025506987,0.000051416253,0.000059522685,0.0048167855],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.9990794,0.000012880993,0.00016367005,0.0003477324,0.00012212619,0.00027419082],"domain_scores_gemma":[0.99962175,0.000028552628,0.000051595554,0.0001307561,0.0000064748665,0.00016084981],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000036275058,0.00013534541,0.00013260549,0.000018894878,0.00023053735,0.000021425007,0.00015378048,0.000085609776,0.0002622227],"category_scores_gemma":[0.00010177584,0.00011748853,0.000046870213,0.00019868038,0.00019251657,0.0002647909,0.00022917886,0.00008405963,0.00004533115],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00008257039,0.000064244225,0.0071568578,0.000046059216,0.00002605007,0.000016989634,0.00031323003,0.001067352,0.08011984,0.024692805,0.5288499,0.35756412],"study_design_scores_gemma":[0.00034091886,0.00020464198,0.0002778679,0.000012197586,0.000009305354,0.0000047405556,0.00016344003,0.0077059767,0.016451938,0.015819209,0.9587978,0.00021194194],"about_ca_topic_score_codex":0.000037552367,"about_ca_topic_score_gemma":0.00002274979,"teacher_disagreement_score":0.85030895,"about_ca_system_score_codex":0.000022961354,"about_ca_system_score_gemma":0.000007103019,"threshold_uncertainty_score":0.47910434},"labels":[],"label_agreement":null},{"id":"W3081085996","doi":"10.1111/cag.12649","title":"A not‐so‐green choice? The high carbon footprint of long‐distance passenger rail travel in Canada","year":2020,"lang":"en","type":"article","venue":"Canadian Geographies / Géographies canadiennes","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":true,"ca_institutions":"University of Ottawa","funders":"","keywords":"Train; Carbon footprint; Greenhouse gas; Transport engineering; Windsor; Footprint; Environmental science; Air travel; Aviation; Business; Meteorology; Engineering; Geography","score_opus":0.007865743650289522,"score_gpt":0.1693773672385305,"score_spread":0.16151162358824098,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3081085996","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":[0.98663473,0.000783068,0.00001485774,0.010636054,0.00020600323,0.00054819265,0.00016625503,0.000058655372,0.00095220935],"genre_scores_gemma":[0.9975934,0.00044354002,0.00010961001,0.0016112053,0.00004107994,0.00009659932,0.0000126775685,0.000042743526,0.00004915109],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.9970216,0.000073888,0.0005447355,0.00069745304,0.0004287371,0.0012335986],"domain_scores_gemma":[0.99813515,0.00020559982,0.00019586222,0.00066622626,0.000035891233,0.00076130073],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00014161046,0.00044720728,0.00052042166,0.0005921562,0.00029379874,0.000036150162,0.0011448252,0.00014761626,0.0001067812],"category_scores_gemma":[0.00015996769,0.0003854256,0.0001607876,0.0050734417,0.0020626206,0.000095892676,0.00013805907,0.0004552317,0.0000023783157],"study_design_candidate":"observational","study_design_consensus":"observational","about_ca_topic_candidate":true,"about_ca_topic_consensus":true,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00003776799,0.000015054246,0.96228135,0.00005677385,0.00008496196,0.00042711495,0.0010740353,0.00064146414,0.0005851438,0.0016234455,0.00088393665,0.03228897],"study_design_scores_gemma":[0.0004032945,0.00008960696,0.9740323,0.000037133854,0.000031191277,0.000013416592,0.0056510665,0.00013357021,0.000947267,0.00074942823,0.017316228,0.00059549743],"about_ca_topic_score_codex":0.99968934,"about_ca_topic_score_gemma":0.9999963,"teacher_disagreement_score":0.03169347,"about_ca_system_score_codex":0.00052825443,"about_ca_system_score_gemma":0.00047197344,"threshold_uncertainty_score":0.99985975},"labels":[],"label_agreement":null},{"id":"W3087194450","doi":"10.48550/arxiv.2009.09650","title":"Exploring Collaborative and Multidisciplinary Aircraft Optimization\\n through the AGILE Academy Challenge -- A case study for an aircraft auxiliary\\n solar power system","year":2020,"lang":"en","type":"preprint","venue":"arXiv (Cornell University)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Concordia University","funders":"","keywords":"Agile software development; Toolchain; Systems engineering; Engineering management; Scrum; Multidisciplinary approach; Engineering; New product development; Process (computing); Computer science; Process management; Software engineering; Software development; Software","score_opus":0.17840876416738322,"score_gpt":0.2516057562831207,"score_spread":0.07319699211573749,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3087194450","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":[0.59551024,0.00013312681,0.3981319,0.0005839219,0.00022971546,0.003881493,0.00014487478,0.00075879705,0.00062592333],"genre_scores_gemma":[0.9889012,0.0003523127,0.010378981,0.000040741557,0.000043920583,0.00010292255,0.000013912803,0.00005998127,0.000106032836],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99728894,0.00024430436,0.00030909298,0.0015727191,0.0001480559,0.00043687128],"domain_scores_gemma":[0.9985529,0.0002096996,0.00028476302,0.0007330787,0.000050867413,0.00016865272],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00025908597,0.00052295707,0.0004908078,0.00007612292,0.0009206212,0.00007540775,0.0008394538,0.00031897792,0.00002431451],"category_scores_gemma":[0.000056838282,0.0004693571,0.00012014901,0.00058882084,0.00050540635,0.0011675791,0.0025715502,0.0007900528,0.00001892948],"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":[0.00014925153,0.00034058793,0.0016304638,0.000104548584,0.0001513876,0.0019704904,0.013035778,0.9796696,0.000032595064,0.0025648875,0.000078055826,0.00027235853],"study_design_scores_gemma":[0.0020467842,0.0013257053,0.00045027726,0.00013296076,0.00041423092,0.00012965707,0.26868168,0.7171474,0.00013595234,0.007590488,0.00065857416,0.0012862796],"about_ca_topic_score_codex":0.0002196724,"about_ca_topic_score_gemma":0.00016825776,"teacher_disagreement_score":0.39339095,"about_ca_system_score_codex":0.00039713614,"about_ca_system_score_gemma":0.00004666578,"threshold_uncertainty_score":0.9997758},"labels":[],"label_agreement":null},{"id":"W3112559140","doi":"10.1016/j.ast.2020.106401","title":"Ventilation considerations for an enhanced thermal risk prediction in aircraft conceptual design","year":2020,"lang":"en","type":"article","venue":"Aerospace Science and Technology","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":28,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Concordia University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Conceptual design; Thermal; Engineering; Computer science; Simulation; Automotive engineering; Mechanical engineering; Meteorology","score_opus":0.029527869242331865,"score_gpt":0.25269906224756694,"score_spread":0.22317119300523508,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3112559140","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":[0.8239985,0.00004132302,0.1719202,0.0027302061,0.000051603034,0.00066793326,0.000009363917,0.00040162166,0.00017922501],"genre_scores_gemma":[0.95949966,0.000022346423,0.040154774,0.00018325496,0.000010340533,0.00010485411,0.000001194576,0.0000072965195,0.000016301414],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9987935,0.000023863995,0.0001640199,0.00051969127,0.0001855662,0.00031339208],"domain_scores_gemma":[0.99953616,0.000084480336,0.000083993735,0.0001878297,0.000036743393,0.00007079434],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00032161968,0.00011485293,0.00012925365,0.00010761217,0.00037250994,0.0000333899,0.00021362223,0.00013847904,0.00005195179],"category_scores_gemma":[0.0010163059,0.00010877169,0.000012429925,0.0009967214,0.0023034106,0.0007096278,0.00012218759,0.00017486891,0.000022571207],"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":[0.000039425402,0.000042098265,0.0155293625,0.0000019299275,0.0000023622276,0.0000018452512,0.0010432443,0.0038752246,0.9541823,0.0040856176,0.0002742543,0.020922301],"study_design_scores_gemma":[0.0014220391,0.0020761832,0.022556255,0.000012396117,0.000019335097,0.000010437192,0.0043538995,0.049486745,0.86926,0.049633585,0.00075625035,0.00041286953],"about_ca_topic_score_codex":0.000016081594,"about_ca_topic_score_gemma":0.000057876285,"teacher_disagreement_score":0.1355011,"about_ca_system_score_codex":0.00007292248,"about_ca_system_score_gemma":0.000045736597,"threshold_uncertainty_score":0.84870124},"labels":[],"label_agreement":null},{"id":"W3113084141","doi":"10.1016/j.jaerosci.2020.105734","title":"Assessment of a regulatory measurement system for the determination of the non-volatile particulate matter emissions from commercial aircraft engines","year":2020,"lang":"en","type":"article","venue":"Journal of Aerosol Science","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":27,"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":"Federal Aviation Administration; U.S. Environmental Protection Agency","keywords":"Particulates; Environmental science; Sampling (signal processing); Combustion; Engineering; Air pollution; Aerospace; Meteorology; Automotive engineering; Aerospace engineering; Electrical engineering; Chemistry; Physics","score_opus":0.025044988754047287,"score_gpt":0.2602910965490657,"score_spread":0.2352461077950184,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3113084141","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":[0.8496332,0.000037062062,0.14690638,0.0026925209,0.0002513517,0.00034954032,0.000007688309,0.000009472376,0.00011277458],"genre_scores_gemma":[0.98758554,0.0000030906886,0.012281726,0.00008927164,0.000023451676,0.0000071723566,5.177945e-8,0.0000043697455,0.000005327558],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9984435,0.000029804365,0.0004031067,0.00012795224,0.0008516213,0.00014400561],"domain_scores_gemma":[0.9989751,0.000109813765,0.00053046574,0.00022575639,0.000098390796,0.00006045547],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006997663,0.00008267086,0.00017231771,0.000018870756,0.00020420857,0.000017165274,0.000728869,0.000031327378,0.00003110423],"category_scores_gemma":[0.00017344076,0.000042484382,0.00010331995,0.00031869777,0.00053548417,0.0002507295,0.00017566781,0.00011487845,0.0000014324511],"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":[0.000014666954,0.000035452653,0.029232182,0.000019754687,0.000007919146,6.330652e-7,0.00033615113,0.004379086,0.9629481,0.00001723175,0.0003496798,0.0026591371],"study_design_scores_gemma":[0.00037938487,0.00015911298,0.30518022,0.00017137655,0.000057220765,0.0000055569376,0.00046842298,0.046703197,0.64660645,0.00010480395,0.00007466876,0.00008960168],"about_ca_topic_score_codex":0.000013088562,"about_ca_topic_score_gemma":0.000005555713,"teacher_disagreement_score":0.31634167,"about_ca_system_score_codex":0.00015521524,"about_ca_system_score_gemma":0.00008477049,"threshold_uncertainty_score":0.19730137},"labels":[],"label_agreement":null},{"id":"W3118682277","doi":"10.2514/6.2021-0463","title":"Influence of Carbon Pricing on Regional Aircraft and Route Network Design","year":2021,"lang":"en","type":"article","venue":"AIAA Scitech 2021 Forum","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Royal Military College of Canada","funders":"","keywords":"Carbon tax; Turboprop; Environmental economics; Business; Environmental science; Greenhouse gas; Computer science; Industrial organization; Automotive engineering; Economics; Engineering","score_opus":0.012327291595006685,"score_gpt":0.2218808986314415,"score_spread":0.20955360703643483,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3118682277","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":[0.97467136,0.00048862095,0.020447241,0.002039679,0.00006359038,0.00024386495,0.0000028316865,0.00011795339,0.0019248776],"genre_scores_gemma":[0.9717264,0.00020022427,0.02709187,0.00050370186,0.000018950795,0.000016554672,0.0000021424896,0.000014746349,0.00042540982],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9986469,0.000046601075,0.00020775535,0.00041405187,0.00029404444,0.00039065184],"domain_scores_gemma":[0.9993111,0.00015320646,0.000092250615,0.00036448194,0.000017988894,0.00006095746],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018186141,0.00015712503,0.0001936376,0.000037348687,0.00011984452,0.0000161077,0.00020320504,0.0001113951,0.000052498253],"category_scores_gemma":[0.00011961018,0.00014646925,0.0000391188,0.0005929262,0.00028792417,0.00015679497,0.0003144399,0.000187761,0.000018826804],"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":[0.000071735485,0.00013960125,0.20554684,0.000027570584,0.000048353522,0.0001974121,0.00018758912,0.5612697,0.15441105,0.0054980232,0.0036167414,0.06898537],"study_design_scores_gemma":[0.0020167746,0.001436782,0.24229352,0.00090804667,0.00008831003,0.00023885697,0.0011009898,0.018639244,0.50347066,0.18433313,0.043561004,0.0019126582],"about_ca_topic_score_codex":0.000064862965,"about_ca_topic_score_gemma":0.000036486574,"teacher_disagreement_score":0.5426305,"about_ca_system_score_codex":0.00007843796,"about_ca_system_score_gemma":0.00002475299,"threshold_uncertainty_score":0.59728426},"labels":[],"label_agreement":null},{"id":"W3118825139","doi":"10.2514/6.2021-0213","title":"‘Switchblade’: Wide-Mission Performance Design of a Multi-Variant Unmanned Aerial System","year":2021,"lang":"en","type":"article","venue":"AIAA Scitech 2021 Forum","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":9,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lockheed Martin (Canada)","funders":"","keywords":"Aerodynamics; Takeoff; Propulsion; Flexibility (engineering); Computational fluid dynamics; Aerospace engineering; Computer science; Takeoff and landing; Lift (data mining); Conceptual design; Range (aeronautics); Drag; Simulation; Systems engineering; Control engineering; Engineering; Human–computer interaction","score_opus":0.016664874790750506,"score_gpt":0.22760964588547514,"score_spread":0.21094477109472462,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3118825139","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":[0.20355217,0.00057990866,0.78908014,0.0016105708,0.0009351736,0.0009923419,0.000025555219,0.00060641195,0.0026177056],"genre_scores_gemma":[0.9423128,0.000118678436,0.056277648,0.000087241395,0.000023409608,0.000028562796,0.000007800476,0.000027321455,0.0011165532],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99798375,0.00008303431,0.00041117833,0.00055174483,0.00041613873,0.0005541795],"domain_scores_gemma":[0.99895054,0.00009477167,0.00017731053,0.00063563435,0.00003551558,0.00010620903],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00030122345,0.0002446277,0.00033291566,0.00006892641,0.00022816047,0.000032333282,0.0004473572,0.00020646179,0.0005483435],"category_scores_gemma":[0.0002021012,0.00021479759,0.00009512015,0.00075394555,0.00023161093,0.00036470895,0.00052652817,0.00021290613,0.00027577564],"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":[0.00026347837,0.0004419957,0.01689193,0.00018424811,0.00007259081,0.0005243715,0.00029666192,0.024680013,0.8546796,0.0017425594,0.0050997003,0.09512288],"study_design_scores_gemma":[0.0018670387,0.00043229517,0.002900454,0.00043662774,0.000045039153,0.00018867328,0.002102284,0.08425777,0.89298236,0.0009494215,0.013106352,0.0007316606],"about_ca_topic_score_codex":0.000037367947,"about_ca_topic_score_gemma":0.000013650403,"teacher_disagreement_score":0.7387606,"about_ca_system_score_codex":0.00019687836,"about_ca_system_score_gemma":0.00005614568,"threshold_uncertainty_score":0.8759191},"labels":[],"label_agreement":null},{"id":"W3119159932","doi":"10.2514/6.2021-0014","title":"Further Exploration of Regional-Class Hybrid Wing-Body Aircraft Through Multifidelity Optimization","year":2021,"lang":"en","type":"article","venue":"AIAA Scitech 2021 Forum","topic":"Advanced Aircraft Design and Technologies","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":"University of Toronto","funders":"","keywords":"Takeoff; Aerospace engineering; Aerodynamics; Angle of attack; Wing configuration; Longitudinal static stability; Computer science; Engineering; Control theory (sociology)","score_opus":0.024062633092221442,"score_gpt":0.2566821357807613,"score_spread":0.23261950268853987,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3119159932","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.026458848,0.00029584212,0.9584535,0.01059384,0.00022349054,0.0003389334,0.000024294133,0.00023972112,0.0033715458],"genre_scores_gemma":[0.8996291,0.00033453034,0.098071784,0.00051428966,0.000029170113,0.00004775195,0.00007868621,0.000029732882,0.0012649184],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99830544,0.00006003081,0.00035699923,0.00051823474,0.0004139302,0.00034537795],"domain_scores_gemma":[0.9990778,0.00006233292,0.00016614652,0.00058165286,0.00006543021,0.00004666445],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0001590595,0.00018865077,0.00021921487,0.000042122425,0.00015038683,0.000029500477,0.00026146322,0.00011415696,0.001178995],"category_scores_gemma":[0.0001759144,0.0001856645,0.00012738268,0.00059265073,0.00030355764,0.0012943862,0.00030665728,0.00016575276,0.00014356179],"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":[0.00010814116,0.0010039653,0.018044943,0.000063106985,0.00013824791,0.00016357894,0.0011452521,0.5645254,0.28944433,0.007715304,0.022344997,0.09530271],"study_design_scores_gemma":[0.001406322,0.00024812677,0.0014530383,0.00014193449,0.0000655872,0.000057761896,0.0045548044,0.0928367,0.70543396,0.10509877,0.08766698,0.0010360247],"about_ca_topic_score_codex":0.00007717836,"about_ca_topic_score_gemma":0.00006689359,"teacher_disagreement_score":0.8731703,"about_ca_system_score_codex":0.00012944794,"about_ca_system_score_gemma":0.000029517621,"threshold_uncertainty_score":0.99973404},"labels":[],"label_agreement":null},{"id":"W3123970377","doi":"10.1016/j.trd.2020.102688","title":"On the design of environmentally sustainable aircraft for urban air mobility","year":2021,"lang":"en","type":"article","venue":"Transportation Research Part D Transport and Environment","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":63,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Victoria","funders":"Universidade de Lisboa; University of Victoria","keywords":"Aviation; Renewable energy; Ecological footprint; Greenhouse gas; Sustainable transport; Electricity; Environmental science; Fossil fuel; Battery electric vehicle; Propulsion; Battery (electricity); Automotive engineering; Engineering; Sustainable development; Sustainability; Aerospace engineering; Waste management; Power (physics)","score_opus":0.04048352433370669,"score_gpt":0.27599226999320925,"score_spread":0.23550874565950256,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3123970377","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":[0.86426115,0.0002669445,0.12933391,0.0025723737,0.00002766643,0.0026674184,0.00012901802,0.000072999544,0.0006685182],"genre_scores_gemma":[0.99288297,0.0007585368,0.0033821985,0.000113338494,0.000010492325,0.0006104735,0.000080359285,0.000025648093,0.0021359723],"study_design_codex":"simulation_or_modeling","study_design_gemma":"observational","domain_scores_codex":[0.9976754,0.00011533083,0.00038640315,0.00057768484,0.0006876707,0.0005574989],"domain_scores_gemma":[0.9988424,0.00048843893,0.00006723336,0.00047280316,0.000015222343,0.000113857015],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0010136794,0.0002066995,0.00023026267,0.000043757158,0.00039006633,0.0000079479305,0.00023343609,0.00011177376,0.0017065884],"category_scores_gemma":[0.000029643745,0.00016074181,0.00010064301,0.00020042557,0.0010445971,0.00015665898,0.00001909432,0.00026293614,0.00003314518],"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":[0.0030841134,0.0068812207,0.33912846,0.0009569706,0.00045810244,0.00063612784,0.008161548,0.35219613,0.119546175,0.13798144,0.014651865,0.016317844],"study_design_scores_gemma":[0.0025659048,0.0017721083,0.61779267,0.00009712243,0.00011334733,0.000003470961,0.005983133,0.0008875622,0.13271779,0.07204114,0.16517316,0.000852606],"about_ca_topic_score_codex":0.00005742065,"about_ca_topic_score_gemma":0.000034145116,"teacher_disagreement_score":0.35130855,"about_ca_system_score_codex":0.0001253721,"about_ca_system_score_gemma":0.000025943966,"threshold_uncertainty_score":0.999206},"labels":[],"label_agreement":null},{"id":"W3132452891","doi":"10.1177/1468087421993961","title":"Eulerian–Lagrangian CFD-microphysics modeling of a near-field contrail from a realistic turbofan","year":2021,"lang":"en","type":"article","venue":"International Journal of Engine Research","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":15,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure; Université du Québec à Montréal","funders":"","keywords":"Turbofan; Nozzle; Turbulence; Mechanics; Jet (fluid); Aerospace engineering; Computational fluid dynamics; Environmental science; Meteorology; Downwash; Radiative transfer; Airplane; Physics; Engineering; Vortex; Optics","score_opus":0.038484697003730806,"score_gpt":0.33683104567156424,"score_spread":0.29834634866783344,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3132452891","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":[0.8445845,0.0005878343,0.14659628,0.004071266,0.00038490279,0.00008848323,0.00004466292,0.000022788134,0.0036192194],"genre_scores_gemma":[0.98589414,0.00021576838,0.0135809565,0.000049692764,0.0001336949,0.0000014925553,0.000005315265,0.00001006007,0.00010889305],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9983893,0.00006473286,0.0003301946,0.00013944822,0.0008837082,0.0001926358],"domain_scores_gemma":[0.99898034,0.00033269674,0.000101612895,0.0001576428,0.00035931013,0.000068395486],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003604285,0.00007828676,0.00016881624,0.00008618295,0.000043566866,0.000050380677,0.00055673154,0.000063438594,0.0005363148],"category_scores_gemma":[0.0009200835,0.00006902668,0.0000964485,0.00024331066,0.00013564577,0.0001817509,0.00020712406,0.00044388542,0.00002260116],"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":[0.00043960856,0.0004381263,0.0024434442,0.000015023951,0.00036659153,0.0014717896,0.0007201329,0.12894838,0.7280858,0.0027120395,0.002357631,0.13200144],"study_design_scores_gemma":[0.0040356847,0.00088263804,0.0040205894,0.00075955945,0.00006401637,0.00039277028,0.0018771789,0.3607005,0.44004074,0.17247531,0.0141208805,0.00063013437],"about_ca_topic_score_codex":0.00034064378,"about_ca_topic_score_gemma":0.00003584888,"teacher_disagreement_score":0.28804505,"about_ca_system_score_codex":0.0001333748,"about_ca_system_score_gemma":0.00007892953,"threshold_uncertainty_score":0.58722705},"labels":[],"label_agreement":null},{"id":"W3132697398","doi":"10.1016/j.ast.2021.106602","title":"HNN-based generalized predictive control for turbofan engine direct performance optimization","year":2021,"lang":"en","type":"article","venue":"Aerospace Science and Technology","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":31,"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":"China Scholarship Council","keywords":"Turbofan; Artificial neural network; Control theory (sociology); Model predictive control; Controller (irrigation); Nonlinear system; Computer science; Optimal control; Engineering; Optimization problem; Mathematical optimization; Control engineering; Control (management); Algorithm; Artificial intelligence; Mathematics; Automotive engineering","score_opus":0.005027967187623656,"score_gpt":0.20779269867375713,"score_spread":0.20276473148613347,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3132697398","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":[0.46852946,0.00069895707,0.5076518,0.016131116,0.00031272913,0.0012215392,0.000035556917,0.001496074,0.0039227954],"genre_scores_gemma":[0.9407179,0.00012315458,0.05849527,0.00026513322,0.000008940233,0.00013476842,0.0000036731394,0.000010489793,0.00024072088],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99861795,0.000010702769,0.000131008,0.0005646405,0.00024684725,0.00042883275],"domain_scores_gemma":[0.999369,0.00005716287,0.00007020512,0.00033725222,0.00010644599,0.0000599187],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025081934,0.00014951055,0.00019171266,0.00013535835,0.00041075895,0.00003715022,0.00030978696,0.00014429461,0.000050976585],"category_scores_gemma":[0.00052767486,0.00013238161,0.000023459217,0.0016042076,0.0017206545,0.0003287234,0.0001406767,0.00011985527,0.000007762901],"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":[0.00013375752,0.0002132311,0.061224416,0.00003557356,0.000029725992,0.000023038721,0.00011222216,0.41723016,0.42979896,0.0041901614,0.0010183492,0.085990414],"study_design_scores_gemma":[0.0015975639,0.0004473047,0.0015666445,0.000018356093,0.000023629518,0.000018392473,0.00014985008,0.5560205,0.43474638,0.0017873158,0.0033151254,0.00030893297],"about_ca_topic_score_codex":0.0000048295947,"about_ca_topic_score_gemma":0.00000887351,"teacher_disagreement_score":0.47218838,"about_ca_system_score_codex":0.00012121261,"about_ca_system_score_gemma":0.000080564,"threshold_uncertainty_score":0.63398236},"labels":[],"label_agreement":null},{"id":"W3133507058","doi":"","title":"Modeling capabilities on the formation of contrails in a commercial CFD code","year":2019,"lang":"en","type":"article","venue":"Espace ÉTS (ETS)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Compute Canada","keywords":"Radiative transfer; Context (archaeology); Computational fluid dynamics; Meteorology; Mechanics; Environmental science; Aerospace engineering; Forcing (mathematics); Turbulence; Flow (mathematics); Physics; Geology; Atmospheric sciences; Engineering; Optics","score_opus":0.017723927803011297,"score_gpt":0.23598239568582344,"score_spread":0.21825846788281214,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3133507058","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":[0.9884556,0.000017434597,0.004315596,0.001859214,0.000042154406,0.00031717125,0.0000055379414,0.00004429282,0.00494299],"genre_scores_gemma":[0.99915016,0.000012797981,0.00038749154,0.00018084263,0.000004877585,0.000018033148,0.0000010350531,0.00000600908,0.00023877481],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99935764,0.00003825632,0.00014377183,0.00012663356,0.00016629373,0.00016738396],"domain_scores_gemma":[0.9995649,0.00012908397,0.000046499994,0.00024057149,0.0000048111983,0.000014149565],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020827103,0.00008367504,0.00012200563,0.00003219618,0.000039999064,0.000008755568,0.00019117461,0.000055296085,0.00020795726],"category_scores_gemma":[0.000091359114,0.00005818457,0.0000298017,0.000118821656,0.00011741446,0.00020210221,0.00006544892,0.00013340077,0.00016806553],"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":[0.00044796016,0.00036655008,0.04786998,0.00008912963,0.000017935474,0.0000065178506,0.019531514,0.7422649,0.084206074,0.06268545,0.0018152694,0.040698696],"study_design_scores_gemma":[0.002200646,0.0005332532,0.019086061,0.00023686294,0.000013748115,0.000006461229,0.019696262,0.82217616,0.08452734,0.045448247,0.0053686197,0.00070634414],"about_ca_topic_score_codex":0.00014218067,"about_ca_topic_score_gemma":0.0007064823,"teacher_disagreement_score":0.079911225,"about_ca_system_score_codex":0.00008932743,"about_ca_system_score_gemma":0.0000044609183,"threshold_uncertainty_score":0.23726979},"labels":[],"label_agreement":null},{"id":"W3144622163","doi":"10.3390/su13073656","title":"Climate Change Mitigation Pathways for the Aviation Sector","year":2021,"lang":"en","type":"article","venue":"Sustainability","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":81,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Wilfrid Laurier University","funders":"","keywords":"Greenhouse gas; Aviation; Climate change mitigation; Climate change; Context (archaeology); Emissions trading; Environmental economics; Natural resource economics; Business; Environmental science; Engineering; Economics","score_opus":0.022163272797967582,"score_gpt":0.254533966833253,"score_spread":0.23237069403528543,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3144622163","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":[0.8765676,0.00029415346,0.101751044,0.016795246,0.00030247116,0.0026661232,0.000057172878,0.0004939417,0.0010722692],"genre_scores_gemma":[0.9979314,0.000027775113,0.001321959,0.00018776079,0.00003523351,0.0003954141,0.000010416216,0.000006354312,0.000083657666],"study_design_codex":"design_other","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.99929816,0.00003473319,0.00010281846,0.00023030148,0.00010712781,0.00022688803],"domain_scores_gemma":[0.99941003,0.00015789378,0.000041723855,0.0003040644,0.000065469685,0.000020815638],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025861728,0.00007106401,0.000065068816,0.0000073584156,0.00023665732,0.000019142657,0.00010896108,0.00005245904,0.00015408405],"category_scores_gemma":[0.00078096054,0.0000519657,0.00005057047,0.00018169206,0.00014405338,0.00018960857,0.0001198504,0.000063746935,0.000013900509],"study_design_candidate":"design_other","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":[0.000059729966,0.00019329549,0.15412243,0.00019114459,0.000010168965,0.000012893084,0.0017939641,0.00032192058,0.006503182,0.090717755,0.0005763861,0.7454971],"study_design_scores_gemma":[0.00028836992,0.000068596,0.37211084,0.000005010527,0.000015298005,0.0000026966084,0.0026472688,0.0023032175,0.020691909,0.592724,0.008967726,0.00017503058],"about_ca_topic_score_codex":0.000021268053,"about_ca_topic_score_gemma":0.000056135108,"teacher_disagreement_score":0.7453221,"about_ca_system_score_codex":0.00046166184,"about_ca_system_score_gemma":0.000019319272,"threshold_uncertainty_score":0.21190996},"labels":[],"label_agreement":null},{"id":"W3146605210","doi":"10.22215/etd/2015-10913","title":"Development of a Simulation and Optimization Framework for Improved Aerodynamic Performance of R/C Helicopter Rotor Blades","year":2015,"lang":"en","type":"dissertation","venue":"","topic":"Advanced Aircraft Design and Technologies","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":"Carleton University","funders":"","keywords":"Airfoil; Aerodynamics; Blade element theory; Blade element momentum theory; Helicopter rotor; Aeroelasticity; Rotor (electric); Chord (peer-to-peer); MATLAB; Blade (archaeology); Engineering; Aerospace engineering; Computer science; Mechanical engineering","score_opus":0.015634075010619624,"score_gpt":0.28195265851257373,"score_spread":0.2663185835019541,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3146605210","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":[0.5942382,0.00004390177,0.40461642,0.0000054342436,0.000054927357,0.0007306276,0.000006280942,0.00004427271,0.00025987683],"genre_scores_gemma":[0.5089183,0.000017691402,0.49053085,0.000003977587,0.0000035501494,0.00006154377,0.00010379379,0.0000123010805,0.0003479786],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991975,0.0000052424753,0.00032427174,0.00022039213,0.00013610463,0.00011648515],"domain_scores_gemma":[0.99944246,0.000053450185,0.00029717764,0.00013798004,0.000044322456,0.000024638062],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00010274905,0.00015109636,0.00021805296,0.000058774025,0.00004514979,0.0000058627766,0.00011151885,0.00024908088,0.0000692256],"category_scores_gemma":[0.000091267975,0.00013116545,0.000026135765,0.00010535323,0.000058977304,0.00014235986,0.000032553147,0.00007390932,0.0000017659992],"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":[0.00051598065,0.00010189835,0.0008281771,0.0005657724,0.000044264325,6.1489466e-8,0.0015075665,0.71273863,0.03672745,0.00018943177,0.000019088808,0.24676166],"study_design_scores_gemma":[0.0004674917,0.00028125307,0.0039000302,0.00022560095,0.00003758057,2.2865088e-7,0.00075270404,0.9426634,0.048303124,0.002714256,0.00028408147,0.0003702651],"about_ca_topic_score_codex":0.000004488548,"about_ca_topic_score_gemma":0.000042499687,"teacher_disagreement_score":0.2463914,"about_ca_system_score_codex":0.00007260815,"about_ca_system_score_gemma":0.000025702751,"threshold_uncertainty_score":0.5348772},"labels":[],"label_agreement":null},{"id":"W3155322643","doi":"10.1007/s11270-021-05087-2","title":"Overview of Emissions at Montreal’s Pierre Elliott Trudeau International Airport and Impact of Local Weather on Related Pollutant Concentrations","year":2021,"lang":"en","type":"article","venue":"Water Air & Soil Pollution","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":6,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"École de Technologie Supérieure","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Pollutant; Environmental science; Meteorology; Air pollutants; International airport; Air pollution; Engineering; Geography; Transport engineering; Ecology; Biology","score_opus":0.012708672238390617,"score_gpt":0.2567992747512154,"score_spread":0.24409060251282477,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3155322643","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":[0.98953074,0.00038459033,0.0015292373,0.001433021,0.000095155076,0.0001385325,0.00010005534,0.00005964775,0.006729023],"genre_scores_gemma":[0.997432,0.00046454364,0.00017699055,0.00004980779,0.000007153026,0.0000051132906,0.00003187352,0.000009863961,0.0018226601],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9990182,0.000036466612,0.00028925075,0.00024175257,0.00022283853,0.00019148829],"domain_scores_gemma":[0.9995878,0.000014650506,0.00009873087,0.00021802176,0.000017383365,0.00006341166],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.000074689764,0.00013345575,0.00017827371,0.000043455526,0.000082492435,0.0000047189014,0.00010487137,0.00010841949,0.0016321454],"category_scores_gemma":[0.000019533009,0.00009214112,0.00010438978,0.00014785057,0.00032101755,0.00011872801,0.00013826729,0.00009751918,0.000039842762],"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":[0.00023180507,0.00061133225,0.04388217,0.000027877571,0.00023628958,0.000070864,0.0016009801,0.03834009,0.77960885,0.0017719531,0.0026448292,0.13097297],"study_design_scores_gemma":[0.0012817999,0.00034394307,0.45461062,0.00017358546,0.00006177027,0.000091806796,0.000434039,0.0053899866,0.52747995,0.0077632964,0.002045491,0.00032375482],"about_ca_topic_score_codex":0.0003684002,"about_ca_topic_score_gemma":0.00019473596,"teacher_disagreement_score":0.41072845,"about_ca_system_score_codex":0.00024795622,"about_ca_system_score_gemma":0.000022964405,"threshold_uncertainty_score":0.9992805},"labels":[],"label_agreement":null},{"id":"W3159663946","doi":"10.1016/j.enconman.2021.114172","title":"Novel hybrid aircraft propulsion systems using hydrogen, methane, methanol, ethanol and dimethyl ether as alternative fuels","year":2021,"lang":"en","type":"article","venue":"Energy Conversion and Management","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":73,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Ontario Tech University","funders":"Natural Sciences and Engineering Research Council of Canada; Transport Canada","keywords":"Turbofan; Dimethyl ether; Hydrogen; Methanol; Methane; Thermal efficiency; Waste management; Hydrogen fuel; Environmental science; Chemistry; Engineering; Combustion; Automotive engineering; Organic chemistry","score_opus":0.017008843845283568,"score_gpt":0.2371567457032842,"score_spread":0.22014790185800065,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3159663946","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":[0.8102585,0.0025520723,0.17324944,0.00066180545,0.0006394197,0.000615356,0.00000979518,0.0003015167,0.011712081],"genre_scores_gemma":[0.97775465,0.002552299,0.011735004,0.00050096883,0.000022583788,0.000038002254,0.000009066775,0.00002978654,0.0073576244],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99848884,0.00009250367,0.0001951618,0.0006088386,0.00033093238,0.00028369925],"domain_scores_gemma":[0.99943495,0.00004480027,0.0001067881,0.00028626103,0.000015515661,0.000111675996],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00019426036,0.00022980591,0.00023137164,0.00009521881,0.00015045874,0.00004242769,0.00015625986,0.00008233381,0.00022308831],"category_scores_gemma":[0.000021325734,0.00020304277,0.000046545847,0.000218499,0.00023848384,0.0002588484,0.0008515162,0.000108414424,0.000024058532],"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":[0.000121633355,0.00039473953,0.0017262145,0.00031179923,0.0005837471,0.001210088,0.0005132942,0.0083348295,0.81955236,0.026153285,0.0011022692,0.13999575],"study_design_scores_gemma":[0.0017955572,0.0001454381,0.00034492477,0.00015306851,0.0001580132,0.00014951221,0.0016075153,0.021355646,0.8728429,0.0060563525,0.094692774,0.00069829874],"about_ca_topic_score_codex":0.00071159797,"about_ca_topic_score_gemma":0.000012618,"teacher_disagreement_score":0.16749614,"about_ca_system_score_codex":0.00010293357,"about_ca_system_score_gemma":0.0000063588977,"threshold_uncertainty_score":0.8279844},"labels":[],"label_agreement":null},{"id":"W3161526324","doi":"10.1016/j.compind.2021.103467","title":"Improving aircraft conceptual design through parametric CAD modellers – A case study for thermal analysis of aircraft systems","year":2021,"lang":"en","type":"article","venue":"Computers in Industry","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":19,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Bombardier (Canada); Concordia University","funders":"Natural Sciences and Engineering Research Council of Canada; Consortium de Recherche et d’innovation en Aérospatiale au Québec","keywords":"CAD; Parametric statistics; Conceptual design; Systems engineering; Engineering; Parametric design; Computer Aided Design; Computer science; Manufacturing engineering; Aerospace engineering; Engineering drawing; Mechanical engineering; Mathematics","score_opus":0.06014688102861573,"score_gpt":0.2863997120968466,"score_spread":0.22625283106823088,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3161526324","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":[0.54630405,0.0001172954,0.45281696,0.000015835027,0.00014035121,0.0004844472,0.000010894976,0.000064230255,0.000045950044],"genre_scores_gemma":[0.93564576,0.00000422176,0.06410029,0.000047858215,0.000019686968,0.000107315114,0.0000046968785,0.000019658717,0.00005052341],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9979248,0.0001930717,0.000527076,0.0006440352,0.00028661627,0.00042439927],"domain_scores_gemma":[0.9985131,0.0006167115,0.00020904645,0.0005614596,0.000033454075,0.000066203975],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00035373116,0.00024998246,0.0005697578,0.00024214297,0.00011996433,0.000035920213,0.00039689557,0.0003794693,0.00003722966],"category_scores_gemma":[0.00013654566,0.0002452256,0.00014713408,0.0026433433,0.000338434,0.000262037,0.0003419072,0.00050775614,0.000002953105],"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":[0.000020439915,0.0003489093,0.03995853,0.0000138773,0.000271348,0.0012722512,0.0015681664,0.9472651,0.00070278684,0.000062574305,0.00012627052,0.0083897635],"study_design_scores_gemma":[0.001506637,0.00048542296,0.0014366128,0.000035689252,0.00041640058,0.0001612816,0.03554188,0.95766956,0.0020528957,0.00015925098,0.000047238438,0.000487151],"about_ca_topic_score_codex":0.001104461,"about_ca_topic_score_gemma":0.00006816823,"teacher_disagreement_score":0.3893417,"about_ca_system_score_codex":0.00025662643,"about_ca_system_score_gemma":0.00005573655,"threshold_uncertainty_score":1},"labels":[],"label_agreement":null},{"id":"W3166064711","doi":"10.1007/s42401-021-00097-8","title":"Flight management system for hydrogen-powered aircraft in cruise","year":2021,"lang":"en","type":"article","venue":"Aerospace Systems","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Concordia University","funders":"","keywords":"Cruise; Minification; Pontryagin's minimum principle; Optimal control; Control theory (sociology); Computer science; Aerospace engineering; Automotive engineering; Mathematical optimization; Engineering; Control (management); Mathematics","score_opus":0.010729803044207011,"score_gpt":0.22490295785281728,"score_spread":0.21417315480861027,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3166064711","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":[0.642952,0.00853652,0.20880632,0.0029587084,0.0049728234,0.009815648,0.000121190336,0.003529706,0.118307054],"genre_scores_gemma":[0.9855553,0.000060687482,0.005160807,0.00003784279,0.000028971413,0.00049756316,0.000009262009,0.000032522064,0.008617066],"study_design_codex":"bench_or_experimental","study_design_gemma":"not_applicable","domain_scores_codex":[0.9982976,0.000056286808,0.00032241788,0.00056574057,0.00028153902,0.00047647263],"domain_scores_gemma":[0.99917495,0.00005095396,0.000099157885,0.00058583263,0.000013438777,0.00007564638],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023594806,0.00021243372,0.00030869283,0.000050453902,0.00011010857,0.00004825066,0.0002930862,0.0001292904,0.00004109828],"category_scores_gemma":[0.000027299535,0.00020132774,0.000087152046,0.0004544572,0.00007614479,0.00016361967,0.00021810758,0.00009785583,0.00036145197],"study_design_candidate":"not_applicable","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":[0.00040539863,0.0017608864,0.17747563,0.0057994584,0.00069405575,0.0063566323,0.0027238296,0.08077688,0.4642429,0.15421425,0.06579771,0.039752353],"study_design_scores_gemma":[0.008543577,0.00043685606,0.010620772,0.0017194779,0.00016063775,0.00047647458,0.028091071,0.016573196,0.24303244,0.0029473118,0.6843307,0.0030674997],"about_ca_topic_score_codex":0.00008673262,"about_ca_topic_score_gemma":0.00013140045,"teacher_disagreement_score":0.61853296,"about_ca_system_score_codex":0.00045650694,"about_ca_system_score_gemma":0.000008950875,"threshold_uncertainty_score":0.8209907},"labels":[],"label_agreement":null},{"id":"W3167853685","doi":"10.1080/01441647.2021.1938284","title":"Transition policies for climatically sustainable aviation","year":2021,"lang":"en","type":"article","venue":"Transport Reviews","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":123,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"International Air Transport Association; Transport Canada","funders":"","keywords":"Aviation; Subsidy; Civil aviation; Business; Greenhouse gas; Emissions trading; Sustainable transport; Sustainable development; Environmental economics; Economics; Natural resource economics; Engineering; Sustainability; Market economy; Political science","score_opus":0.021821428487014963,"score_gpt":0.27421938842221166,"score_spread":0.2523979599351967,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3167853685","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.02235621,0.003387573,0.9579566,0.0031182996,0.00005310743,0.001574558,0.000015284739,0.00026098863,0.011277373],"genre_scores_gemma":[0.8187913,0.016434604,0.14924595,0.0028455274,0.000081643564,0.0009301034,0.0002912447,0.000055624983,0.011324018],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.99915546,0.000020037,0.00027616465,0.00020364129,0.000097986536,0.00024668477],"domain_scores_gemma":[0.9996811,0.000022310223,0.00005025309,0.00019682037,0.000014129513,0.000035345452],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002249015,0.00010269184,0.00021287208,0.00001479334,0.0000995211,0.000008344274,0.00009176879,0.000056346307,0.00061184267],"category_scores_gemma":[0.00004443904,0.000087140725,0.0001202735,0.00021989306,0.000068803914,0.0002044151,0.000007432736,0.000057687957,0.00010283242],"study_design_candidate":"not_applicable","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":[0.00015304558,0.0011086708,0.01815894,0.0039358465,0.00006333205,0.00023221388,0.0054464485,0.0017684224,0.14063995,0.19340211,0.019822055,0.61526895],"study_design_scores_gemma":[0.00037068856,0.00008284548,0.008142326,0.000061862636,0.00006537245,0.000010716582,0.00035721855,0.00013704521,0.011001749,0.041355744,0.9381354,0.0002790665],"about_ca_topic_score_codex":0.000016383672,"about_ca_topic_score_gemma":0.000044525623,"teacher_disagreement_score":0.9183133,"about_ca_system_score_codex":0.000062105275,"about_ca_system_score_gemma":0.000009555098,"threshold_uncertainty_score":0.66992486},"labels":[],"label_agreement":null},{"id":"W3169690126","doi":"10.1038/s43247-021-00175-x","title":"Process-oriented analysis of aircraft soot-cirrus interactions constrains the climate impact of aviation","year":2021,"lang":"en","type":"article","venue":"Communications Earth & Environment","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":44,"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 British Columbia","funders":"European Commission","keywords":"Cirrus; Soot; Radiative forcing; Atmospheric sciences; Environmental science; Ice crystals; Aerosol; Radiative transfer; Climatology; Climate model; Optical depth; Climate change; Meteorology; Combustion; Chemistry; Geography; Geology; Physics; Optics","score_opus":0.021090656691578273,"score_gpt":0.2995975667845528,"score_spread":0.2785069100929745,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3169690126","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":[0.96996415,0.0004013725,0.023480045,0.001006123,0.000025541323,0.00035618598,0.00018531023,0.000064969754,0.004516329],"genre_scores_gemma":[0.9919667,0.0012013003,0.006540944,0.000025465763,0.0000020745786,0.000047911562,0.000120813485,0.000008243422,0.00008654678],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.9988465,0.00012966267,0.00040483655,0.00021088772,0.00022757557,0.00018056529],"domain_scores_gemma":[0.9976262,0.00019510213,0.0003030164,0.001816733,0.000019603054,0.000039372466],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00018017899,0.00012581352,0.00023266928,0.00009080398,0.00023210846,0.0000080271775,0.00053488964,0.000047176243,0.0012408405],"category_scores_gemma":[0.00007513248,0.00009893421,0.00023036411,0.00086132734,0.00091344427,0.00015559186,0.00048202017,0.00018992834,0.000053303014],"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":[0.000032012456,0.0017034735,0.67219967,0.000017654409,0.0013955976,0.0000028253014,0.0023818011,0.15124084,0.1277126,0.0040532444,0.00007962576,0.03918064],"study_design_scores_gemma":[0.00029428172,0.00009680324,0.95816827,0.000022106587,0.00060834084,0.0000067934766,0.0017175127,0.0174657,0.01719188,0.0008501559,0.0033706736,0.00020745731],"about_ca_topic_score_codex":0.00007496187,"about_ca_topic_score_gemma":0.00019483315,"teacher_disagreement_score":0.28596863,"about_ca_system_score_codex":0.000106509025,"about_ca_system_score_gemma":0.000023157885,"threshold_uncertainty_score":0.9996722},"labels":[],"label_agreement":null},{"id":"W3170862003","doi":"10.1016/j.energy.2021.121037","title":"Investigation of two hybrid aircraft propulsion and powering systems using alternative fuels","year":2021,"lang":"en","type":"article","venue":"Energy","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":34,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Ontario Tech University","funders":"Natural Sciences and Engineering Research Council of Canada; Transport Canada","keywords":"Turbofan; Propulsion; Thrust specific fuel consumption; Thrust; Fuel efficiency; Automotive engineering; Environmental science; Engineering; Aerospace engineering","score_opus":0.021369836742371806,"score_gpt":0.2398339468309678,"score_spread":0.21846411008859598,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3170862003","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":[0.94848406,0.00030491178,0.050368104,0.00004363783,0.00010351862,0.000036242527,0.0000020131838,0.000044775235,0.00061274396],"genre_scores_gemma":[0.9907689,0.000053740983,0.008940626,0.000024449197,0.000015887896,0.0000041870776,0.0000026367632,0.000007251417,0.00018228289],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9994331,0.000031040287,0.000121392884,0.00018461185,0.00012632378,0.000103552156],"domain_scores_gemma":[0.99974906,0.000019622707,0.00006998876,0.000121553116,0.000009353263,0.000030410272],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000048121623,0.00007080701,0.000098081146,0.000023364275,0.000047373644,0.000011155206,0.00006173763,0.000021304546,0.000023597058],"category_scores_gemma":[0.000027346869,0.00006505736,0.000014016248,0.00011640149,0.00013125374,0.00016428922,0.00014393049,0.000039529426,0.0000019172285],"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":[0.000002711488,0.000006817202,0.008386484,0.000011979748,0.0000066108355,0.000032973716,0.00007519119,0.012826097,0.9659197,0.0036487016,0.000016352535,0.009066389],"study_design_scores_gemma":[0.00017536744,0.00002779606,0.00084919645,0.000056728833,0.0000053980593,0.000046931065,0.00012820553,0.016105514,0.9651657,0.01676757,0.00056079734,0.00011083466],"about_ca_topic_score_codex":0.0004922015,"about_ca_topic_score_gemma":0.000023007433,"teacher_disagreement_score":0.042284887,"about_ca_system_score_codex":0.000055176442,"about_ca_system_score_gemma":0.000006605628,"threshold_uncertainty_score":0.26529622},"labels":[],"label_agreement":null},{"id":"W3172732923","doi":"10.1109/tte.2021.3089605","title":"Review of Electric Machines in More-/Hybrid-/Turbo-Electric Aircraft","year":2021,"lang":"en","type":"article","venue":"IEEE Transactions on Transportation Electrification","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":313,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Upgrade; Automotive engineering; Electrification; Propulsion; Turbofan; Electrically powered spacecraft propulsion; Electric motor; Takeoff; Electric machine; Controllability; Aerospace; Battery electric vehicle; Engineering; Computer science; Battery (electricity); Aerospace engineering; Electricity; Mechanical engineering; Electrical engineering","score_opus":0.01005837640623753,"score_gpt":0.24671860813296861,"score_spread":0.2366602317267311,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3172732923","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":[0.17598808,0.0070963628,0.8133964,0.0016024457,0.00013719566,0.0009188346,0.00003856386,0.00032746542,0.00049463107],"genre_scores_gemma":[0.9755801,0.02192456,0.0015279502,0.00053531106,0.000006057798,0.00015547646,0.000057558074,0.00002560944,0.0001873741],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99814016,0.00008512952,0.0006268959,0.00048838113,0.00035290717,0.0003065344],"domain_scores_gemma":[0.9992154,0.00009783227,0.0001911103,0.00038162776,0.00006129873,0.00005272392],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020878865,0.00021751749,0.00030127625,0.0002534184,0.00009513761,0.000007417982,0.00019852386,0.00011144008,0.00043413902],"category_scores_gemma":[0.000026562586,0.00022903357,0.00013807348,0.0027460488,0.00006039557,0.00027486318,5.813296e-8,0.00038970384,0.000052089094],"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":[0.000052018888,0.0004674091,0.0004598771,0.00033352544,0.00001752988,0.000013065714,0.000087373686,0.0056625814,0.83640224,0.000097063465,0.0001719205,0.15623538],"study_design_scores_gemma":[0.00038851824,0.00010543227,0.012373622,0.00029918394,0.000055856315,0.000010988409,0.000015873165,0.0009814869,0.9842973,0.000844119,0.0003891903,0.00023844311],"about_ca_topic_score_codex":0.000078220975,"about_ca_topic_score_gemma":0.00013383127,"teacher_disagreement_score":0.8118685,"about_ca_system_score_codex":0.00020515184,"about_ca_system_score_gemma":0.00006725448,"threshold_uncertainty_score":0.9339718},"labels":[],"label_agreement":null},{"id":"W3173374578","doi":"10.22215/etd/2021-14416","title":"Multi-Objective Shape Optimization of a Boundary Layer Ingesting Engine Intake","year":2021,"lang":"en","type":"dissertation","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Carleton University","funders":"","keywords":"Wake; Inlet; Propulsion; Inflow; Boundary layer; Offset (computer science); Distortion (music); Mechanics; Engineering; Environmental science; Marine engineering; Automotive engineering; Control theory (sociology); Mechanical engineering; Computer science; Aerospace engineering; Physics; Artificial intelligence","score_opus":0.01686226147139513,"score_gpt":0.25732623136656635,"score_spread":0.24046396989517121,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3173374578","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":[0.6628928,0.0013601419,0.2589034,0.00010492784,0.00093744276,0.0012965482,0.00003355369,0.0011569787,0.07331419],"genre_scores_gemma":[0.5288307,0.00019641872,0.46265793,0.000047078673,0.0000206415,0.000054841137,0.0004942221,0.00005443175,0.0076437662],"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9989426,0.000020928112,0.0002648943,0.00038073366,0.00021387821,0.00017697635],"domain_scores_gemma":[0.9994823,0.000054596974,0.00019698325,0.00020699632,0.000033126853,0.000026030253],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00007695295,0.00020694513,0.00025234613,0.000076603785,0.00008066181,0.000019823021,0.00018454564,0.00025791465,0.0023202389],"category_scores_gemma":[0.00026531902,0.00019687024,0.0000653389,0.00036509387,0.00008138707,0.00017425469,0.00008546506,0.00026078348,0.000024022918],"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":[0.00012778286,0.00054671493,0.005633656,0.00033391028,0.0001654928,0.00007945125,0.0043611443,0.22660497,0.2279941,0.00014446548,0.0006142118,0.5333941],"study_design_scores_gemma":[0.0013525301,0.00030759885,0.027992964,0.00073946844,0.00016195772,0.000021205815,0.019875223,0.4438054,0.5017696,0.0008797303,0.001387777,0.0017065228],"about_ca_topic_score_codex":0.00011673711,"about_ca_topic_score_gemma":0.00050120754,"teacher_disagreement_score":0.53168756,"about_ca_system_score_codex":0.00012302314,"about_ca_system_score_gemma":0.000029963148,"threshold_uncertainty_score":0.9985918},"labels":[],"label_agreement":null},{"id":"W3177503117","doi":"10.1177/09544100211029450","title":"Vertical tail sizing of propeller-driven aircraft considering the asymmetric blade effect","year":2021,"lang":"en","type":"article","venue":"Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":7,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"Mitacs","keywords":"Rudder; Propeller; Thrust; Blade pitch; Aerodynamics; Propulsor; Sizing; Structural engineering; Aerospace engineering; Blade (archaeology); Blade element theory; Deflection (physics); Engineering; Longitudinal static stability; Marine engineering; Turbine; Physics","score_opus":0.008904832680772877,"score_gpt":0.20145244330928827,"score_spread":0.1925476106285154,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3177503117","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":[0.94097453,0.00058048003,0.056085475,0.00094095117,0.0006410084,0.0003061736,0.0000025467743,0.000057665555,0.00041119647],"genre_scores_gemma":[0.9868864,0.000106440006,0.012918751,0.000009956353,0.0000394072,0.0000040573677,1.145157e-7,0.000016361017,0.00001853658],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9983211,0.000013334528,0.0006357713,0.00016330066,0.0006081048,0.00025835008],"domain_scores_gemma":[0.99906516,0.0002318958,0.00033222197,0.00015542921,0.00013444656,0.000080874386],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00060640345,0.00019326345,0.0004526184,0.0000904501,0.00006520359,0.000013881648,0.00052360824,0.00012765809,0.000019210038],"category_scores_gemma":[0.0029440844,0.00012557452,0.00025320478,0.00087823236,0.00024456324,0.000296437,0.00030457877,0.0005262742,0.0000020554044],"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":[0.000040524086,0.00006437149,0.000819996,0.00018072395,0.00009553193,0.000007804281,0.00010075283,0.28353703,0.7081421,0.006174886,0.000110417095,0.0007258343],"study_design_scores_gemma":[0.00052897783,0.00023581133,0.0003226148,0.0005150019,0.000089945315,0.00016100147,0.00017444705,0.018217623,0.9788276,0.00016089858,0.00062673003,0.00013934533],"about_ca_topic_score_codex":0.000002979455,"about_ca_topic_score_gemma":4.3175157e-7,"teacher_disagreement_score":0.27068546,"about_ca_system_score_codex":0.0001271002,"about_ca_system_score_gemma":0.00003952624,"threshold_uncertainty_score":0.51207805},"labels":[],"label_agreement":null},{"id":"W3183350353","doi":"10.1017/aer.2021.63","title":"Design and performance quantification of VTOL systems for a canard aircraft","year":2021,"lang":"en","type":"article","venue":"The Aeronautical Journal","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":10,"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 Victoria","funders":"","keywords":"Tilt (camera); Rotor (electric); Aerodynamics; Aerospace engineering; Sizing; Equidistant; Range (aeronautics); Engineering; Automotive engineering; Lift-to-drag ratio; Structural engineering; Mechanical engineering","score_opus":0.033755285026767494,"score_gpt":0.2547614786132281,"score_spread":0.22100619358646062,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3183350353","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":[0.2525268,0.0004972801,0.74474907,0.0017918235,0.000093917486,0.0002049173,0.0000016932861,0.000021942697,0.00011256721],"genre_scores_gemma":[0.9832072,0.0003412613,0.016180983,0.00004694595,0.000017803615,0.000012948671,5.14355e-7,0.000006129213,0.00018615928],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99930584,0.00006172892,0.00018974878,0.00011210877,0.00016275702,0.00016778661],"domain_scores_gemma":[0.9995114,0.00018939891,0.00007611502,0.0001533768,0.00002262112,0.000047081125],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00041629787,0.00006727185,0.00011324608,0.00001168436,0.00017940767,0.000025618945,0.0001588185,0.000042215634,0.000027301763],"category_scores_gemma":[0.000104179344,0.00004290313,0.00002604872,0.000095075775,0.00025597506,0.0001033781,0.00005947703,0.00013368939,0.000012229468],"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":[0.0008803493,0.00046874463,0.024193304,0.0002467123,0.00021562383,0.000077347024,0.0011362298,0.12414583,0.41768327,0.03669803,0.010537435,0.38371712],"study_design_scores_gemma":[0.002764859,0.0018187336,0.097551204,0.0003068986,0.00026893214,0.003952572,0.0022141882,0.6066716,0.20760694,0.047042403,0.028937882,0.00086379744],"about_ca_topic_score_codex":0.000006962161,"about_ca_topic_score_gemma":0.0000023531877,"teacher_disagreement_score":0.73068047,"about_ca_system_score_codex":0.000047592217,"about_ca_system_score_gemma":0.00002343653,"threshold_uncertainty_score":0.1749539},"labels":[],"label_agreement":null},{"id":"W3184644817","doi":"10.2514/6.2021-3080","title":"An MBSE Certification-Driven Design of a UAV MALE Configuration in the AGILE 4.0 Design Environment","year":2021,"lang":"en","type":"article","venue":"AIAA AVIATION 2021 FORUM","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":12,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Concordia University","funders":"Concordia University; European Commission; Natural Sciences and Engineering Research Council of Canada; Consortium de Recherche et d’innovation en Aérospatiale au Québec","keywords":"Certification; Agile software development; Systems engineering; Scope (computer science); Computer science; Engineering design process; Unified Modeling Language; Software engineering; Engineering; Software; Mechanical engineering; Operating system","score_opus":0.025422282930172773,"score_gpt":0.24148749996683988,"score_spread":0.21606521703666712,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3184644817","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.020008994,0.0000707678,0.97634435,0.0023145985,0.00004821072,0.00054933265,0.0000062878876,0.00003126761,0.0006261736],"genre_scores_gemma":[0.9770479,0.00011083019,0.022120643,0.00020048257,0.000008103767,0.00012772108,0.000050763134,0.000010166504,0.00032333977],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99864763,0.00026718536,0.00028542866,0.00030381378,0.00029139986,0.00020451253],"domain_scores_gemma":[0.99920154,0.00014529208,0.00014272645,0.00046926553,0.000013034282,0.000028127664],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00030495288,0.00011530664,0.00011928087,0.00003906985,0.00010650109,0.000027433001,0.00025920023,0.00008602555,0.0022204728],"category_scores_gemma":[0.00008009988,0.0000974533,0.000034134056,0.0003010408,0.00011619365,0.0003703179,0.000044404176,0.000104630344,0.00024931025],"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":[0.00004266781,0.0005151104,0.024608133,0.0000064395053,0.000012975581,0.000026674637,0.001301153,0.23556763,0.6957447,0.0036877776,0.0019739757,0.036512773],"study_design_scores_gemma":[0.0012880609,0.0006448988,0.12727416,0.00004307176,0.000052985135,0.000044050877,0.0075693424,0.12782855,0.6871463,0.04035986,0.007034368,0.0007143212],"about_ca_topic_score_codex":0.000030515208,"about_ca_topic_score_gemma":0.000021978782,"teacher_disagreement_score":0.95703894,"about_ca_system_score_codex":0.00011703455,"about_ca_system_score_gemma":0.000021026677,"threshold_uncertainty_score":0.9986916},"labels":[],"label_agreement":null},{"id":"W3187069526","doi":"10.2514/6.2021-2443","title":"Parallel Hybrid-Electric Powertrain Sizing on Regional Turboprop Aircraft with Consideration for Certification Performance Requirements","year":2021,"lang":"en","type":"article","venue":"AIAA AVIATION 2021 FORUM","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":14,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Powertrain; Propulsion; Automotive engineering; Alternator; Climb; Engineering; Turboprop; Fuel efficiency; Sizing; Battery (electricity); Electric motor; Aerospace engineering; Power (physics); Mechanical engineering; Torque","score_opus":0.027051258768597736,"score_gpt":0.24881972846861664,"score_spread":0.2217684697000189,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3187069526","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":[0.58949465,0.00013052192,0.3884076,0.017085012,0.0002474826,0.0012772819,0.000013246054,0.0002956995,0.0030485278],"genre_scores_gemma":[0.98407143,0.000069963484,0.013467025,0.0008170593,0.00002678744,0.00017627375,0.00012671389,0.000021434313,0.0012233125],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9985015,0.000032650758,0.00025214584,0.0004653006,0.00041412466,0.0003343018],"domain_scores_gemma":[0.99935603,0.000085061634,0.00015674702,0.00029539873,0.00006068452,0.000046068173],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016408693,0.00016833191,0.00013430745,0.00005764598,0.00033758083,0.00005085514,0.000113700844,0.000069631125,0.00023622847],"category_scores_gemma":[0.00015044941,0.00015294598,0.00004743269,0.00032462587,0.00006468243,0.0004772007,0.000036544418,0.00011949837,0.00012463803],"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":[0.0004992483,0.0007321518,0.12156959,0.00006527219,0.00012234677,0.000035487865,0.00042039447,0.020779245,0.46523297,0.011721152,0.020123208,0.35869893],"study_design_scores_gemma":[0.0036162876,0.0015317824,0.15141,0.0001722295,0.0000754697,0.00010869344,0.0007529954,0.06152133,0.7045341,0.034089737,0.040870573,0.0013167678],"about_ca_topic_score_codex":0.000008972913,"about_ca_topic_score_gemma":0.00003158884,"teacher_disagreement_score":0.3945768,"about_ca_system_score_codex":0.0003043131,"about_ca_system_score_gemma":0.000058137244,"threshold_uncertainty_score":0.6236956},"labels":[],"label_agreement":null},{"id":"W3189482161","doi":"10.1109/itherm51669.2021.9503205","title":"Hybrid Electric Aircraft Thermal Management: Now, New Visions and Future Concepts and Formulation","year":2021,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":13,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Turbofan; Jet fuel; Automotive engineering; Aviation; Fuel efficiency; Range (aeronautics); Aeronautics; Auxiliary power unit; On board; Environmental science; Engineering; Aerospace engineering; Electrical engineering","score_opus":0.006137990566140747,"score_gpt":0.23004915966648518,"score_spread":0.22391116910034442,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3189482161","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":[0.89317995,0.0012896847,0.042976726,0.0040840423,0.000093311784,0.00034915103,0.0000021336518,0.0003800454,0.05764497],"genre_scores_gemma":[0.97736377,0.00096703565,0.01666861,0.0003322871,0.000032660915,0.000004391489,0.000003876106,0.000007818904,0.0046195583],"study_design_codex":"design_other","study_design_gemma":"observational","domain_scores_codex":[0.99938226,0.000008461777,0.00008487535,0.00024931366,0.00010656761,0.00016850805],"domain_scores_gemma":[0.9997591,0.000017207845,0.000021342275,0.00014113919,0.0000031141124,0.000058131922],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000030263827,0.000093409595,0.00008057711,0.000023834305,0.000113219634,0.00002750534,0.000063141495,0.00003831419,0.00071305165],"category_scores_gemma":[0.00000480811,0.00007698465,0.000015904556,0.00016103646,0.000043031036,0.00024249186,0.0001705301,0.00007197085,0.000050417726],"study_design_candidate":"design_other","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":[0.0000095832465,0.000029581193,0.010029695,0.000008072704,0.0000152570265,0.000059421458,0.00007121358,0.0000745169,0.030644078,0.011495057,0.0035260583,0.94403744],"study_design_scores_gemma":[0.0021978365,0.00022343214,0.5025432,0.000023479815,0.0000719857,0.00017838695,0.00086364377,0.0069847032,0.106775,0.0745473,0.30473417,0.0008568348],"about_ca_topic_score_codex":0.0000069997127,"about_ca_topic_score_gemma":0.000013046959,"teacher_disagreement_score":0.9431806,"about_ca_system_score_codex":0.000023523377,"about_ca_system_score_gemma":0.0000035223002,"threshold_uncertainty_score":0.7807416},"labels":[],"label_agreement":null},{"id":"W3204572865","doi":"10.1029/2021gl095882","title":"An Observational Constraint on Aviation‐Induced Cirrus From the COVID‐19‐Induced Flight Disruption","year":2021,"lang":"en","type":"article","venue":"Geophysical Research Letters","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":19,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Environment and Climate Change Canada; University of Victoria","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Cirrus; Aviation; Environmental science; Radiative forcing; Climatology; Atmospheric sciences; Meteorology; Radiative transfer; Coronavirus disease 2019 (COVID-19); Satellite; Aeronautics; Geography; Physics; Aerospace engineering; Aerosol; Engineering; Geology; Medicine","score_opus":0.15602217845571906,"score_gpt":0.37374135924038704,"score_spread":0.21771918078466798,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3204572865","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":[0.9096543,0.000004428221,0.0029266176,0.086510405,0.00007993439,0.00024653572,0.000032125306,0.000114758375,0.00043089167],"genre_scores_gemma":[0.9870911,0.0000057082116,0.0008054346,0.011623831,0.00018422682,0.0000794689,0.00011189827,0.000014167961,0.00008414912],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.9971439,0.00042343882,0.00017761147,0.00058877753,0.0011708299,0.00049543375],"domain_scores_gemma":[0.997767,0.0012344643,0.00004616077,0.00064435403,0.000035612557,0.00027244785],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0003948607,0.00014984139,0.00013599273,0.00003222931,0.0005756272,0.00011509576,0.00052191166,0.00008889697,0.0008048251],"category_scores_gemma":[0.0016900824,0.00011137555,0.00007252418,0.0005755078,0.0005321335,0.000293435,0.00021843026,0.00067418267,0.00096821116],"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":[0.000035065572,0.00016421382,0.002526772,0.0000016338141,0.000012931688,0.00007518665,0.00020571814,0.00020876476,0.96957856,0.007945619,0.00529317,0.013952364],"study_design_scores_gemma":[0.0014509569,0.00060435105,0.66527456,0.000035904734,0.00001950728,0.000012201141,0.001412688,0.0027120295,0.15674295,0.14923972,0.02171556,0.00077956653],"about_ca_topic_score_codex":0.00066213106,"about_ca_topic_score_gemma":0.00008322445,"teacher_disagreement_score":0.81283563,"about_ca_system_score_codex":0.00041252302,"about_ca_system_score_gemma":0.00009668144,"threshold_uncertainty_score":0.9998096},"labels":[],"label_agreement":null},{"id":"W3206347031","doi":"10.1080/02786826.2021.1971152","title":"Experimental verification of principal losses in a regulatory particulate matter emissions sampling system for aircraft turbine engines","year":2021,"lang":"en","type":"article","venue":"Aerosol Science and Technology","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":7,"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":"Air Force Research Laboratory; U.S. Air Force; Federal Aviation Administration; U.S. Environmental Protection Agency","keywords":"Particulates; Principal (computer security); Environmental science; Turbine; Sampling (signal processing); Gas turbines; Aerospace engineering; Engineering; Computer science; Chemistry; Mechanical engineering; Telecommunications","score_opus":0.016859095381352343,"score_gpt":0.26316156890382714,"score_spread":0.2463024735224748,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3206347031","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":[0.99631256,0.00021860702,0.0022921963,0.00065758463,0.000054832024,0.00021075319,0.0000026676405,0.00010646605,0.00014435001],"genre_scores_gemma":[0.98649,0.000009794411,0.01332383,0.000023427627,0.0000034128027,0.0000899386,0.0000012315589,0.000006188095,0.000052150426],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9989089,0.00000729257,0.00021919851,0.00040745563,0.00016982041,0.00028734084],"domain_scores_gemma":[0.9995042,0.00003158812,0.00007162507,0.00031600246,0.000037448237,0.000039142353],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00019174069,0.00010102415,0.00015995385,0.000112543865,0.00014789883,0.000013894494,0.00023228345,0.00010668406,0.000029218814],"category_scores_gemma":[0.00015149699,0.000089262256,0.000018283079,0.00096263026,0.0011064741,0.00021050782,0.00024926115,0.00007808342,0.000009620556],"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":[0.0000048043303,0.000046067522,0.023123078,0.000016703218,0.0000015417874,0.0000036690337,0.00006458761,0.00011395613,0.9732435,0.0015431312,0.000016801436,0.0018221746],"study_design_scores_gemma":[0.00023661884,0.00004991035,0.0059002605,0.000046731053,0.000003719819,0.000033120807,0.0010180261,0.0009667864,0.99088633,0.0005508265,0.00019800941,0.000109685185],"about_ca_topic_score_codex":0.000010088201,"about_ca_topic_score_gemma":0.000008577243,"teacher_disagreement_score":0.01764282,"about_ca_system_score_codex":0.00011834296,"about_ca_system_score_gemma":0.000038263628,"threshold_uncertainty_score":0.40768498},"labels":[],"label_agreement":null},{"id":"W3208568930","doi":"10.32920/ryerson.14648193.v1","title":"Multidisciplinary Design Optimization of a Helicopter Rotor Blade","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Natural Sciences and Engineering Research Council of Canada; Queen's University","keywords":"Sequential quadratic programming; Particle swarm optimization; Aerodynamics; Rotor (electric); Blade element momentum theory; Finite element method; Blade element theory; Reduction (mathematics); Blade (archaeology); Helicopter rotor; Engineering; Structural engineering; Control theory (sociology); Computer science; Mathematics; Mathematical optimization; Quadratic programming; Mechanical engineering; Aerospace engineering; Turbine blade; Geometry","score_opus":0.026597527439121364,"score_gpt":0.25850918207742474,"score_spread":0.23191165463830338,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3208568930","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":[0.00549311,0.00007208501,0.9779075,0.000092236485,0.000070045426,0.0005703825,0.0000027453796,0.0002539275,0.0155379595],"genre_scores_gemma":[0.27325737,0.000096079915,0.7229164,0.000019493695,0.000008459299,0.00009526308,0.000010222718,0.000032066073,0.003564627],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99895036,0.00004305273,0.00022761108,0.0004311433,0.00018494361,0.00016290655],"domain_scores_gemma":[0.9992858,0.000035054763,0.0001427055,0.00048996217,0.0000086805285,0.000037776736],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00008205063,0.00018827278,0.00023083933,0.000047978796,0.00003152264,0.000016191107,0.0003121402,0.00025652925,0.0070006833],"category_scores_gemma":[0.00004730905,0.00016467964,0.00007873887,0.00012571947,0.00016921894,0.00008265737,0.0016470051,0.00019287023,0.00007602337],"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":[0.000010225728,0.000091012516,0.0012270758,0.000024468744,0.000014745898,0.000011776883,0.00011851011,0.9853005,0.008610417,0.000019853866,0.0002988331,0.0042726197],"study_design_scores_gemma":[0.00071133557,0.00023014066,0.005247758,0.0003319899,0.000074023796,0.00001447499,0.0010856396,0.6866407,0.29903534,0.005092707,0.00031831756,0.0012176244],"about_ca_topic_score_codex":0.00004401608,"about_ca_topic_score_gemma":0.000010835234,"teacher_disagreement_score":0.2986598,"about_ca_system_score_codex":0.000077332144,"about_ca_system_score_gemma":0.000015788033,"threshold_uncertainty_score":0.99390703},"labels":[],"label_agreement":null},{"id":"W3209823934","doi":"10.32920/ryerson.14649783.v1","title":"Development of UAV derivative MDO methodology for flight simulation","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Multidisciplinary design optimization; Process (computing); Flight simulator; Derivative (finance); Computer science; Simulation; Time derivative; Engineering; Multidisciplinary approach; Mathematics","score_opus":0.1339321546614659,"score_gpt":0.3571032787808954,"score_spread":0.22317112411942946,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3209823934","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":[0.068565756,0.000042672298,0.92882216,0.00011105943,0.0001220018,0.00045025235,0.0000039753872,0.00010300293,0.0017790972],"genre_scores_gemma":[0.34801573,0.000007598486,0.65153813,0.000036502413,0.000005634658,0.00008321126,0.000026146492,0.000008950189,0.00027809813],"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9988497,0.000052472922,0.0003445108,0.0004332025,0.00014224373,0.00017789517],"domain_scores_gemma":[0.9990527,0.0003990651,0.00020301556,0.00029521793,0.000025680603,0.0000242923],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00027677332,0.00017395115,0.00032178103,0.000043367847,0.000059120997,0.000008500449,0.00026151043,0.00027646893,0.000600466],"category_scores_gemma":[0.00034087864,0.0001514933,0.00007808279,0.00010232579,0.00013660533,0.000062321735,0.0009900241,0.00015203521,0.000010680345],"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":[0.00007689151,0.00019428371,0.0020125567,0.000237204,0.00018956691,0.0000048356305,0.0043563484,0.2973307,0.1993279,0.0021382673,0.000333936,0.4937975],"study_design_scores_gemma":[0.00029883787,0.00004524424,0.0042641745,0.000056025197,0.000028169257,9.1662844e-7,0.001242732,0.01258184,0.9251108,0.039726175,0.01617716,0.00046790062],"about_ca_topic_score_codex":0.00001320391,"about_ca_topic_score_gemma":0.00006386895,"teacher_disagreement_score":0.72578293,"about_ca_system_score_codex":0.00015182963,"about_ca_system_score_gemma":0.000039663784,"threshold_uncertainty_score":0.65746814},"labels":[],"label_agreement":null},{"id":"W3210444428","doi":"10.32920/ryerson.14649630.v1","title":"A design methodology for rotors of small multirotor vehicles","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":6,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"Natural Sciences and Engineering Research Council of Canada; Ontario Centres of Excellence","keywords":"Multirotor; Aerodynamics; Rotor (electric); Wake; Inflow; Blade element momentum theory; Power (physics); Wake turbulence; Flow (mathematics); Operating point; Point (geometry); Control theory (sociology); Computer science; Aerospace engineering; Engineering; Mechanical engineering; Mechanics; Physics; Mathematics; Turbine","score_opus":0.15452912609874733,"score_gpt":0.3211829899589272,"score_spread":0.16665386386017986,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3210444428","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":[0.07343775,0.00011167658,0.92397434,0.00010136337,0.00015654402,0.0017345955,0.000009411532,0.00018896158,0.00028536568],"genre_scores_gemma":[0.09371646,0.000042589,0.90476274,0.000064319596,0.000013810419,0.00083318196,0.000008970385,0.000024425037,0.00053349393],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9984968,0.00017969724,0.00033525363,0.000587142,0.0001232072,0.0002779124],"domain_scores_gemma":[0.9983979,0.0007835802,0.00021058608,0.0005433477,0.000020128002,0.000044482153],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005079598,0.0002412327,0.00047670922,0.000053332256,0.000043528245,0.000013574968,0.0005394771,0.00044656286,0.00042371554],"category_scores_gemma":[0.0005325065,0.00020801369,0.00017686385,0.00009752475,0.000249137,0.000042787,0.0011659764,0.00026029284,0.000010780195],"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":[0.00030840066,0.00046077688,0.010811844,0.00051655236,0.00023695576,0.000030671374,0.0010991464,0.09986878,0.57222503,0.0009005207,0.0011633977,0.31237793],"study_design_scores_gemma":[0.0005633273,0.00026012323,0.002617497,0.00007226011,0.00006521644,0.0000054570523,0.00063064246,0.013304603,0.9328625,0.047855973,0.0011853372,0.00057706767],"about_ca_topic_score_codex":0.00025387754,"about_ca_topic_score_gemma":0.00007601026,"teacher_disagreement_score":0.3606375,"about_ca_system_score_codex":0.00009337378,"about_ca_system_score_gemma":0.000030779054,"threshold_uncertainty_score":0.8482552},"labels":[],"label_agreement":null},{"id":"W3211902531","doi":"10.1115/imece2001/aes-23645","title":"Exergy Analysis of a Turbojet Engine Over a Complete Flight Cycle","year":2001,"lang":"en","type":"article","venue":"Advanced Energy Systems","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Cruise; Turbojet; Exergy; Environmental science; Work (physics); Sensitivity (control systems); Descent (aeronautics); Climb; Computer science; Marine engineering; Automotive engineering; Engineering; Aerospace engineering; Mechanical engineering; Process engineering","score_opus":0.007653383759632937,"score_gpt":0.21334101970542962,"score_spread":0.2056876359457967,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3211902531","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":[0.61722744,0.0022529191,0.3458405,0.00014257575,0.0006026513,0.00035319795,0.00008088949,0.00091893994,0.032580845],"genre_scores_gemma":[0.99571353,0.00025583504,0.0022020398,0.00005773887,0.000020341911,0.000057061574,0.000026814876,0.000021922233,0.0016446881],"study_design_codex":"simulation_or_modeling","study_design_gemma":"not_applicable","domain_scores_codex":[0.9984294,0.000043596076,0.00040065602,0.00042211762,0.0003313312,0.00037287347],"domain_scores_gemma":[0.9990195,0.00007941493,0.00020235985,0.0006013711,0.000014708557,0.000082650105],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00008857191,0.0002204999,0.00050693227,0.00020809233,0.000072966664,0.000012361514,0.00035129787,0.000098827746,0.0003497179],"category_scores_gemma":[0.00002207122,0.00019330789,0.00015760382,0.0017440724,0.00016356492,0.000261776,0.00013859701,0.00007585053,0.000029471476],"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":[0.000040607272,0.00008154288,0.0072564553,0.000008498463,0.00028753607,0.000040039806,0.00006650676,0.92949486,0.039011817,0.0034751429,0.0001713749,0.020065604],"study_design_scores_gemma":[0.0017599835,0.00031864436,0.031082826,0.00009301503,0.00054087135,0.000049135906,0.0004904398,0.364977,0.010401745,0.0037704324,0.5851987,0.0013172209],"about_ca_topic_score_codex":0.0012923548,"about_ca_topic_score_gemma":0.0003475626,"teacher_disagreement_score":0.5850273,"about_ca_system_score_codex":0.00012677477,"about_ca_system_score_gemma":0.000003985204,"threshold_uncertainty_score":0.7882867},"labels":[],"label_agreement":null},{"id":"W367300435","doi":"","title":"Alternative jet fuel scenario analysis report","year":2012,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Jet fuel; Aviation; Greenhouse gas; Aviation biofuel; European union; Alternative fuels; Production (economics); Environmental science; Engineering; Natural resource economics; Environmental economics; Biofuel; Waste management; Business; Economics; International trade; Diesel fuel; Bioenergy","score_opus":0.018648202615824467,"score_gpt":0.2622846474265711,"score_spread":0.24363644481074662,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W367300435","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":[0.33026543,0.00010840143,0.33936876,0.00040703296,0.00016813044,0.0001640175,0.0000024552103,0.0005143689,0.32900143],"genre_scores_gemma":[0.9785826,0.000014255632,0.016299598,0.00012615098,0.000019944686,0.000008166791,0.0000036427275,0.00000466811,0.0049409317],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.9992528,0.000010953742,0.0001250342,0.00018162918,0.00017866172,0.00025093174],"domain_scores_gemma":[0.99955463,0.000021919015,0.00005798178,0.00029590525,0.000003280689,0.00006626548],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00014570165,0.0000870724,0.00011577887,0.00004988838,0.000045783756,0.000008676598,0.00015740162,0.000040488998,0.0036541028],"category_scores_gemma":[0.00005219012,0.00006251044,0.000071371185,0.00048779685,0.0001262538,0.0003090807,0.00015455828,0.00007025815,0.0007512932],"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":[0.0000021759288,0.000056769713,0.99104136,6.490015e-7,0.00008099852,0.000031734926,0.00010999777,0.00033240547,0.0010154239,0.0013770645,0.0009473149,0.0050041014],"study_design_scores_gemma":[0.00025915774,0.000056734727,0.85618424,0.0000025832362,0.00029627123,0.00009677088,0.00042162396,0.0021754417,0.028273087,0.023845222,0.087777294,0.0006115773],"about_ca_topic_score_codex":0.00029444322,"about_ca_topic_score_gemma":0.00009411723,"teacher_disagreement_score":0.6483172,"about_ca_system_score_codex":0.00008124459,"about_ca_system_score_gemma":0.0000015152092,"threshold_uncertainty_score":0.9972567},"labels":[],"label_agreement":null},{"id":"W4200199696","doi":"10.1016/j.fuel.2021.122781","title":"IVOC/SVOC and size distribution characteristics of particulate matter emissions from a modern aero-engine combustor in different operational modes","year":2021,"lang":"en","type":"article","venue":"Fuel","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":28,"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 Alberta","funders":"","keywords":"Combustor; Scanning mobility particle sizer; Particulates; Combustion; Chemistry; Aerosol; NOx; Analytical Chemistry (journal); Environmental chemistry; Particle size; Particle-size distribution; Organic chemistry","score_opus":0.008868988847188754,"score_gpt":0.2102973127241504,"score_spread":0.20142832387696163,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4200199696","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":[0.98236215,0.00006406331,0.016609179,0.0006378097,0.000022563727,0.000062568055,0.00016081343,0.000021124542,0.00005970121],"genre_scores_gemma":[0.99736756,0.000048592057,0.0022373095,0.000063351945,0.0000073844258,0.000012611002,0.00010794769,0.0000050565386,0.00015018391],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.99944067,0.000018775028,0.00015319212,0.00017219165,0.00010219097,0.00011296076],"domain_scores_gemma":[0.9997279,0.000064923246,0.00003347049,0.0001307435,0.000007025463,0.000035948786],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000021939375,0.000084523825,0.00013394347,0.0000042846045,0.000032996162,0.000012003372,0.00005558861,0.00005186493,0.0005497724],"category_scores_gemma":[0.00006978105,0.00006868877,0.000018180646,0.000059947495,0.000082502615,0.00008479464,0.000117822565,0.000080277874,0.000016048813],"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":[0.000027662516,0.00028524655,0.5990887,0.000021966687,0.000013356149,0.000023949275,0.00027464985,0.0013147956,0.3930846,0.00022152103,0.0004182432,0.005225267],"study_design_scores_gemma":[0.00027659113,0.000012268484,0.955122,0.000028112083,0.000007806455,0.0000021545154,0.000048894963,0.022125116,0.015941864,0.006160822,0.00017363646,0.000100763595],"about_ca_topic_score_codex":0.000023427703,"about_ca_topic_score_gemma":0.000015086074,"teacher_disagreement_score":0.37714273,"about_ca_system_score_codex":0.000050753362,"about_ca_system_score_gemma":0.0000049918453,"threshold_uncertainty_score":0.60196227},"labels":[],"label_agreement":null},{"id":"W4205909405","doi":"10.3390/su14010414","title":"Technical Advances in Aviation Electrification: Enhancing Strategic R&amp;D Investment Analysis through Simulation Decomposition","year":2021,"lang":"en","type":"article","venue":"Sustainability","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":9,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"York University","funders":"Natural Sciences and Engineering Research Council of Canada; Liikesivistysrahasto","keywords":"Monte Carlo method; Aviation; Electrification; Computer science; Range (aeronautics); Visualization; Generalizability theory; Process (computing); Operations research; Simulation; Engineering; Artificial intelligence","score_opus":0.01578577334523623,"score_gpt":0.32480670597614447,"score_spread":0.30902093263090824,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4205909405","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":[0.51790476,0.0004145781,0.47874832,0.0006074219,0.000020073006,0.00037522105,0.0000016584703,0.00017295907,0.0017550236],"genre_scores_gemma":[0.9867368,0.00008821203,0.01291327,0.00007301497,0.000007749638,0.00006586271,0.000053635267,0.000005224149,0.000056230856],"study_design_codex":"simulation_or_modeling","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.99858826,0.00013392762,0.00032874287,0.00047664554,0.00022324642,0.0002491905],"domain_scores_gemma":[0.9992564,0.00013273694,0.00009993671,0.00039849416,0.000082183105,0.000030271018],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00029285564,0.00012053239,0.00017793273,0.00006759064,0.0001122615,0.000026194944,0.000110063826,0.00010645833,0.00019535399],"category_scores_gemma":[0.00042447238,0.00012271771,0.00007329749,0.00195621,0.00012657151,0.0006409936,0.000046773264,0.0001572129,0.000014443282],"study_design_candidate":"theoretical_or_conceptual","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":[0.00007785451,0.00073341944,0.21027505,0.00008243608,0.000027777385,0.000024560737,0.00054740167,0.6614281,0.06050558,0.043960128,0.00000620863,0.022331491],"study_design_scores_gemma":[0.00024410935,0.00005525346,0.13854077,0.0000063109105,0.000062393556,0.000002067506,0.00087612984,0.0059213624,0.024156757,0.8285349,0.0013387535,0.00026121],"about_ca_topic_score_codex":0.000057873665,"about_ca_topic_score_gemma":0.0015820139,"teacher_disagreement_score":0.78457475,"about_ca_system_score_codex":0.002068228,"about_ca_system_score_gemma":0.00006746555,"threshold_uncertainty_score":0.5408344},"labels":[],"label_agreement":null},{"id":"W4205939837","doi":"10.5194/acp-2021-343-rc2","title":"Comment on acp-2021-343","year":2021,"lang":"en","type":"peer-review","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"York University; Environment and Climate Change Canada","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Environmental science; Meteorology; Air quality index; Sampling (signal processing); Emission inventory; Daytime; Remote sensing; Atmospheric sciences; Computer science; Geography; Geology","score_opus":0.031076206789500613,"score_gpt":0.28859035718675374,"score_spread":0.2575141503972531,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4205939837","genre_codex":"commentary","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"other","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0000025066488,0.009564773,0.0018012896,0.52608323,0.0011577131,0.00058870646,0.00006937568,0.00030185745,0.46043056],"genre_scores_gemma":[0.000072882896,0.029490618,0.00742527,0.13255684,0.000112137255,0.00015643964,0.0004209093,0.000050237988,0.82971466],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.9981456,0.000048626112,0.00027284416,0.00063565915,0.000549542,0.0003477234],"domain_scores_gemma":[0.998808,0.00009253428,0.000111279835,0.00090418354,0.000009723938,0.00007422768],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.00015937582,0.00034768006,0.00048258313,0.000032455762,0.00008703808,0.000023881448,0.0005933586,0.00025624275,0.059539095],"category_scores_gemma":[0.00013918124,0.0002690607,0.00016970499,0.00026453193,0.00015884226,0.000055240638,0.0006691754,0.0005408219,0.0052615223],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[9.683891e-7,0.0000597401,0.0000087658955,0.00010038561,0.000011462623,0.00003914549,0.0000022833021,0.000008483351,0.000023630444,0.0003478635,0.9193243,0.08007299],"study_design_scores_gemma":[0.00008145181,0.00007121571,0.000015404605,0.00081868627,0.000027263308,0.000004804914,0.000015538986,0.000006232324,0.00059958606,0.0011018262,0.9969226,0.0003353868],"about_ca_topic_score_codex":0.00008873166,"about_ca_topic_score_gemma":0.00006652794,"teacher_disagreement_score":0.39352638,"about_ca_system_score_codex":0.00031072582,"about_ca_system_score_gemma":0.000015657988,"threshold_uncertainty_score":0.99997616},"labels":[],"label_agreement":null},{"id":"W4206052991","doi":"10.2514/6.2022-1823","title":"Eulerian-Lagrangian CFD-microphysics modeling of Aircraft-Emitted Aerosol Formation at Ground Level","year":2022,"lang":"en","type":"article","venue":"AIAA SCITECH 2022 Forum","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"École de Technologie Supérieure","funders":"","keywords":"Plume; Context (archaeology); Environmental science; Soot; Particulates; Aerosol; Meteorology; Computational fluid dynamics; Jet engine; Air quality index; Lagrangian particle tracking; Aerospace engineering; Lagrangian; Atmospheric sciences; Combustion; Physics; Chemistry; Engineering; Geology","score_opus":0.020797899331294785,"score_gpt":0.22259735489991295,"score_spread":0.20179945556861817,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4206052991","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":[0.8367454,0.00013750033,0.1586544,0.0010808058,0.0002748377,0.00061581813,0.00017379176,0.0003881293,0.0019293424],"genre_scores_gemma":[0.99276674,0.000029561745,0.005618144,0.0002949473,0.0000127108115,0.00011479227,0.00007098246,0.00003351296,0.0010586127],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9980446,0.000048543614,0.00038375534,0.00040863742,0.0005889607,0.00052549894],"domain_scores_gemma":[0.99919057,0.00003391663,0.00019271587,0.00050563493,0.00001595775,0.000061176375],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00022740323,0.00021991177,0.00023604039,0.000105835454,0.00078694936,0.000020651833,0.0006349925,0.00008390857,0.0010049025],"category_scores_gemma":[0.00002752218,0.0002305874,0.00012666338,0.00086967373,0.0001920987,0.00058335584,0.0014037698,0.0003146439,0.000099613644],"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":[0.00009852184,0.00019061139,0.0016581415,0.000029407682,0.000027535203,0.000016753553,0.0005633157,0.07819601,0.88594806,0.001003666,0.0053205984,0.02694738],"study_design_scores_gemma":[0.0029893129,0.0011596696,0.0009501816,0.00005785858,0.00009224069,0.00016216892,0.008577505,0.5546753,0.35488853,0.04763528,0.026794031,0.0020179355],"about_ca_topic_score_codex":0.00017776637,"about_ca_topic_score_gemma":0.00008877671,"teacher_disagreement_score":0.5310595,"about_ca_system_score_codex":0.000588051,"about_ca_system_score_gemma":0.0000139753265,"threshold_uncertainty_score":0.9999083},"labels":[],"label_agreement":null},{"id":"W4206587744","doi":"10.2514/6.2022-2050","title":"Feasibility Study of a Serial Hybrid Electric Powertrain for a Light Sports Aircraft","year":2022,"lang":"en","type":"article","venue":"AIAA SCITECH 2022 Forum","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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; Toronto Metropolitan University","funders":"","keywords":"Powertrain; Automotive engineering; Range (aeronautics); Propulsion; Aerodynamics; Battery (electricity); MATLAB; Battery electric vehicle; Aerospace engineering; Engineering; Electric vehicle; Electrically powered spacecraft propulsion; Computer science; Torque; Power (physics)","score_opus":0.010384173398702871,"score_gpt":0.24270500417195445,"score_spread":0.23232083077325158,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4206587744","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":[0.9926175,0.000060891827,0.0030769578,0.00077527104,0.0002949781,0.0022775976,0.000061804836,0.00027629078,0.00055869715],"genre_scores_gemma":[0.99731535,0.0000040330046,0.0013216444,0.00014565769,0.000014904778,0.00059520756,0.000010814636,0.000028501705,0.0005639066],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9975984,0.00007059871,0.0003984526,0.0006710209,0.00068015774,0.0005813672],"domain_scores_gemma":[0.99900055,0.00006561458,0.00019038403,0.0006615511,0.000013811534,0.00006806244],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0006591511,0.00021380461,0.00031198264,0.00014409822,0.00047052553,0.0000134816055,0.00066670706,0.000044631302,0.001257982],"category_scores_gemma":[0.0001236725,0.00021037563,0.00013147912,0.0009997798,0.00008782965,0.00019278354,0.0007830751,0.0002781716,0.000008729033],"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":[0.0021257172,0.009032056,0.327899,0.00005541617,0.00012959944,0.0002539445,0.0016347017,0.005039842,0.5117735,0.00120184,0.045441624,0.09541271],"study_design_scores_gemma":[0.020477077,0.037206974,0.09098536,0.00003692719,0.0003312897,0.0004360359,0.036068484,0.008488315,0.3351174,0.26530352,0.20120375,0.004344876],"about_ca_topic_score_codex":0.000068019544,"about_ca_topic_score_gemma":0.00008071238,"teacher_disagreement_score":0.26410168,"about_ca_system_score_codex":0.0003293908,"about_ca_system_score_gemma":0.000032512173,"threshold_uncertainty_score":0.999655},"labels":[],"label_agreement":null},{"id":"W4212954296","doi":"10.25242/885x113420212349","title":"Análise de Eficiência Térmica dos Motores Aeronáuticos TURBOFAN","year":2021,"lang":"pt","type":"article","venue":"Exatas & Engenharia","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Discovery Air (Canada)","funders":"","keywords":"Physics; Humanities; Turbofan; Philosophy; Aerospace engineering; Engineering","score_opus":0.016436953066416526,"score_gpt":0.2510834113491904,"score_spread":0.23464645828277386,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4212954296","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":[0.869304,0.034693226,0.059105586,0.006010179,0.0036913916,0.0025878646,0.0016303039,0.0025372023,0.020440271],"genre_scores_gemma":[0.9806571,0.0012323426,0.0121426135,0.00069156213,0.00022260575,0.00007755745,0.00009941716,0.00008969477,0.004787113],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9960249,0.00024369181,0.00056325766,0.0012335527,0.0006012964,0.0013332982],"domain_scores_gemma":[0.9977029,0.00020604052,0.00021013057,0.0014668833,0.000035666784,0.00037836106],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.00037817835,0.00060825556,0.00054154015,0.000092713984,0.00043795,0.00018292975,0.0010269398,0.0005144764,0.013715451],"category_scores_gemma":[0.00056564034,0.0006283061,0.00022154758,0.0007094119,0.0005489075,0.00045395474,0.00096458255,0.00083698076,0.0039481907],"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":[0.00017745663,0.0012922414,0.012881525,0.00016269159,0.00031777055,0.002523917,0.0027658776,0.001147019,0.7841088,0.008893403,0.063432164,0.122297116],"study_design_scores_gemma":[0.0019364136,0.00040279652,0.06189811,0.00022606846,0.0003788669,0.00024271442,0.002729801,0.003105818,0.6363904,0.011857034,0.27859387,0.0022381418],"about_ca_topic_score_codex":0.00015326113,"about_ca_topic_score_gemma":0.00016486963,"teacher_disagreement_score":0.2151617,"about_ca_system_score_codex":0.0006200805,"about_ca_system_score_gemma":0.0001585488,"threshold_uncertainty_score":0.9996168},"labels":[],"label_agreement":null},{"id":"W4220713072","doi":"10.1016/j.jclepro.2022.131246","title":"Emissions of future conventional aircrafts adopting evolutionary technologies","year":2022,"lang":"en","type":"article","venue":"Journal of Cleaner Production","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":16,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université du Québec à Trois-Rivières","funders":"","keywords":"Aviation; Prosperity; Aeronautics; Business; Operations research; Engineering; Economics; Economic growth","score_opus":0.009720507021206344,"score_gpt":0.2255528280410687,"score_spread":0.21583232101986236,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4220713072","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":[0.97409123,0.0016394724,0.0046462156,0.015894337,0.0021284425,0.0002868328,0.000010063546,0.00026660098,0.0010368322],"genre_scores_gemma":[0.9835375,0.00011492726,0.015472471,0.000017628874,0.00013741883,0.0000064680803,0.0000019198426,0.000008517249,0.0007031308],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.99882287,0.000048251855,0.00036395245,0.00015197303,0.0004839784,0.00012896639],"domain_scores_gemma":[0.9992619,0.000019942001,0.00048857153,0.00016718257,0.000041303578,0.000021059412],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003649441,0.000082803905,0.00014359783,0.0001304355,0.0002467422,0.0000035176454,0.00026810679,0.000049542203,0.00044306892],"category_scores_gemma":[0.00020166163,0.00007088711,0.00009382717,0.00034385192,0.000204857,0.0003006887,0.00023274886,0.00041871768,0.000004412768],"study_design_candidate":"not_applicable","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":[0.00040693293,0.00089169777,0.0531235,0.000050613344,0.00009358818,0.00006747677,0.0005062143,0.24069527,0.23306994,0.0014348954,0.121224456,0.3484354],"study_design_scores_gemma":[0.0009838718,0.0012523236,0.041454773,0.000080772945,0.00008418377,0.0028952414,0.027745115,0.0005092697,0.07554736,0.029625898,0.81934714,0.0004740477],"about_ca_topic_score_codex":0.0000020858358,"about_ca_topic_score_gemma":5.407645e-7,"teacher_disagreement_score":0.6981227,"about_ca_system_score_codex":0.00019297836,"about_ca_system_score_gemma":0.000024613435,"threshold_uncertainty_score":0.48512942},"labels":[],"label_agreement":null},{"id":"W4221066289","doi":"10.3390/aerospace9030160","title":"A Multidisciplinary Possibilistic Approach to Size the Empennage of Multi-Engine Propeller-Driven Light Aircraft","year":2022,"lang":"en","type":"article","venue":"Aerospace","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":9,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"Mitacs","keywords":"Airworthiness; Airframe; Propeller; Sizing; Propulsion; Multidisciplinary design optimization; Aerodynamics; Stability (learning theory); Controllability; Longitudinal static stability; Computer science; Flight envelope; Flight control surfaces; Aerospace engineering; Engineering; Control engineering; Multidisciplinary approach; Marine engineering; Mathematics","score_opus":0.016045170277475946,"score_gpt":0.23827073903078336,"score_spread":0.2222255687533074,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4221066289","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":[0.80935967,0.0004752616,0.103894606,0.008493851,0.00034544317,0.005249487,0.000065221975,0.0013727049,0.07074376],"genre_scores_gemma":[0.91779625,0.0000048058696,0.053186327,0.00007974725,0.000007736137,0.00021150635,0.0000015979202,0.00003736163,0.028674658],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.998716,0.00006817485,0.00017572663,0.00041852935,0.0003187641,0.00030277984],"domain_scores_gemma":[0.9991222,0.0000893183,0.00008757403,0.0006274015,0.000005912523,0.0000675745],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00019005062,0.00017114852,0.00018286619,0.000028430677,0.00031291207,0.000010824498,0.0007081355,0.000039048133,0.00064492825],"category_scores_gemma":[0.00014105768,0.00011954888,0.00006468264,0.0005704014,0.00021168766,0.00007271148,0.0014625317,0.00024387192,0.00023337058],"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":[0.00025447638,0.0035629468,0.052803382,0.000090491965,0.000104236,0.00009372711,0.016410727,0.3533498,0.5275306,0.0017662649,0.028923804,0.015109496],"study_design_scores_gemma":[0.009343209,0.0050525493,0.41611648,0.00014753129,0.00027825226,0.00030609115,0.050081857,0.20222329,0.10955699,0.0046672835,0.19704418,0.005182297],"about_ca_topic_score_codex":0.00006122146,"about_ca_topic_score_gemma":0.000029795,"teacher_disagreement_score":0.41797364,"about_ca_system_score_codex":0.00012954963,"about_ca_system_score_gemma":0.000009631653,"threshold_uncertainty_score":0.70615125},"labels":[],"label_agreement":null},{"id":"W4223957595","doi":"10.3390/aerospace9040224","title":"Feasibility Study of Electrified Light-Sport Aircraft Powertrains","year":2022,"lang":"en","type":"article","venue":"Aerospace","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"National Research Council Canada; Toronto Metropolitan University","funders":"National Research Council Canada","keywords":"Powertrain; Propulsion; Automotive engineering; Range (aeronautics); Battery (electricity); Aerodynamics; MATLAB; Engineering; Aerospace engineering; Power (physics); Computer science; Torque","score_opus":0.015796446850229455,"score_gpt":0.24917163262744432,"score_spread":0.23337518577721486,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4223957595","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":[0.99397916,0.0000364711,0.00032501132,0.00043446067,0.000075930424,0.00061589194,0.0000038843696,0.00024172866,0.0042874906],"genre_scores_gemma":[0.9974377,0.0000041086523,0.00052373344,0.00007782525,0.000004419456,0.000069510505,0.0000017769702,0.000014015801,0.0018668841],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.9986396,0.000040961768,0.00020193959,0.00040278168,0.0004368417,0.00027791265],"domain_scores_gemma":[0.9992439,0.000023576462,0.00010746307,0.00057188194,0.000006156097,0.000047017962],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00026426077,0.00013442841,0.00020523884,0.000032773267,0.0002260689,0.000005565684,0.00043170922,0.00003526437,0.0009100435],"category_scores_gemma":[0.000034992296,0.00012867097,0.0000530922,0.00055496034,0.000095807765,0.00010298514,0.00038981385,0.0002507784,0.00003990985],"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":[0.00015852053,0.0030953102,0.8301288,0.0000059741196,0.00002905891,0.00006178865,0.0024867516,0.0020029005,0.15415128,0.00060544885,0.0050754934,0.0021986698],"study_design_scores_gemma":[0.0048747486,0.007831179,0.820605,0.000007708685,0.00007858056,0.00005456766,0.029392602,0.00031598957,0.091660485,0.0075487276,0.0362955,0.0013349106],"about_ca_topic_score_codex":0.00019197848,"about_ca_topic_score_gemma":0.0001888676,"teacher_disagreement_score":0.062490795,"about_ca_system_score_codex":0.00024156223,"about_ca_system_score_gemma":0.0000122727415,"threshold_uncertainty_score":0.9964338},"labels":[],"label_agreement":null},{"id":"W4224997346","doi":"10.18280/mmep.090204","title":"The Difference in the Wall Thickness of the Helicopter Structure Are Made of Composite Materials with Another Made of Steel","year":2022,"lang":"en","type":"article","venue":"Mathematical Modelling and Engineering Problems","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":6,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Aluminium; Composite number; Materials science; Aerodynamics; Layer (electronics); Composite material; Alloy; Welding; Structural engineering; Engineering; Aerospace engineering","score_opus":0.012873949392556004,"score_gpt":0.18240720874010977,"score_spread":0.16953325934755376,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4224997346","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":[0.91225904,0.000081079146,0.087179884,0.0001796699,0.000013217008,0.00023249275,0.00001055903,0.000014990783,0.000029040304],"genre_scores_gemma":[0.9950764,0.000017517074,0.004812356,0.000014277604,0.0000015002562,0.000029941746,3.29138e-7,0.000010079683,0.00003760994],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99927,0.000033301305,0.00022233954,0.000109278204,0.00023010063,0.00013497994],"domain_scores_gemma":[0.9994988,0.00013678508,0.00010447322,0.0002470501,0.0000044905723,0.000008433342],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020175106,0.000100621,0.00017680909,0.000015739419,0.00007157925,0.000010081466,0.00034822448,0.000032746644,0.000018688223],"category_scores_gemma":[0.000008782345,0.00004491138,0.000020522883,0.00013429309,0.0001662749,0.000023825965,0.00014244222,0.00016127818,1.9463408e-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":[0.000014904654,0.000039033148,0.00076695386,0.00023550495,0.000009448833,4.3446855e-7,0.0016821834,0.774777,0.2195674,0.0027047172,0.000001235863,0.00020121057],"study_design_scores_gemma":[0.0007976295,0.00028072688,0.013947143,0.0010237563,0.00006445014,0.000068231864,0.0016549423,0.61220396,0.23547165,0.13385628,0.00013308623,0.00049813563],"about_ca_topic_score_codex":0.00002252714,"about_ca_topic_score_gemma":0.000003121272,"teacher_disagreement_score":0.162573,"about_ca_system_score_codex":0.000013104681,"about_ca_system_score_gemma":0.000002062481,"threshold_uncertainty_score":0.18314329},"labels":[],"label_agreement":null},{"id":"W4226000714","doi":"10.1016/j.enconman.2022.115573","title":"Erratum to “Design, simulation, and validation of additively manufactured high-temperature combustion chambers for micro gas turbines” [Energy Convers. Manage., 248 (2021) 114805]","year":2022,"lang":"en","type":"erratum","venue":"Energy Conversion and Management","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Simon Fraser University","funders":"","keywords":"Gas turbines; Combustion; Process engineering; Energy (signal processing); Nuclear engineering; Environmental science; Mechanical engineering; Automotive engineering; Aerospace engineering; Engineering; Chemistry; Physics; Organic chemistry","score_opus":0.008418122814323714,"score_gpt":0.21224900540507885,"score_spread":0.20383088259075513,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4226000714","genre_codex":"methods","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.016661456,0.0069204075,0.8095516,0.0263166,0.07901422,0.017052073,0.0029268258,0.0025653706,0.03899143],"genre_scores_gemma":[0.4172373,0.020093882,0.026834283,0.005384397,0.00042428912,0.0011194231,0.009226726,0.00030280655,0.5193769],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.99773294,0.00011152899,0.00038908835,0.00093926553,0.00045503676,0.00037215362],"domain_scores_gemma":[0.9989581,0.00011094156,0.0003527626,0.00040703666,0.000040804287,0.00013035668],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00020494769,0.00049035304,0.00048646974,0.00029072663,0.00041551772,0.00007033849,0.00030765092,0.00036000038,0.0011573514],"category_scores_gemma":[0.000029389723,0.0004920049,0.00009665332,0.00036659453,0.00023721832,0.00021933098,0.00075102324,0.00024180253,0.000006287971],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00024024626,0.00006152675,0.0000073233987,0.0001924579,0.0001445993,0.000026663336,0.0001059995,0.049182605,0.0005504821,0.0011521679,0.93848586,0.009850087],"study_design_scores_gemma":[0.0011949033,0.00034339508,0.00019256424,0.000102400685,0.00017761921,0.0000025346044,0.00042317458,0.0049889297,0.007157467,0.0016364426,0.98317057,0.0006099858],"about_ca_topic_score_codex":0.00023450989,"about_ca_topic_score_gemma":0.0000216939,"teacher_disagreement_score":0.78271735,"about_ca_system_score_codex":0.0002551953,"about_ca_system_score_gemma":0.000015565598,"threshold_uncertainty_score":0.99975574},"labels":[],"label_agreement":null},{"id":"W4232146310","doi":"10.1115/gt2013-94079","title":"Assessment and Characterization of Volcanic Ash Threat to Gas Turbine Engine Performance","year":2013,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"National Research Council Canada","funders":"National Research Council Canada; Ministère de la Défense Nationale","keywords":"Volcanic ash; Environmental science; Volcano; Turbine; Geology; Explosive eruption; Meteorology; Engineering; Aerospace engineering; Magma; Seismology; Physics","score_opus":0.007264361122001855,"score_gpt":0.21573475716330728,"score_spread":0.20847039604130543,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4232146310","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":[0.98474306,0.0000031269087,0.011976025,0.0004159451,0.000019047578,0.00021405435,0.0000010216492,0.00006817314,0.002559567],"genre_scores_gemma":[0.9898405,0.000071202616,0.009027545,0.00010429482,0.0000047564367,0.000027207001,0.0000034547359,0.0000049527516,0.00091608363],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.999553,0.0000040312166,0.00009697958,0.00013488859,0.00009666176,0.000114418624],"domain_scores_gemma":[0.9997898,0.000007877122,0.000027504395,0.00013270923,0.0000059461345,0.000036185516],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00003688125,0.00006916518,0.000081391554,0.000023467412,0.000027730375,0.0000083093455,0.000082228034,0.000027591752,0.0013273065],"category_scores_gemma":[0.000004627781,0.000052432504,0.00000833401,0.00012223978,0.00005073713,0.00024895603,0.00011140852,0.000038896218,0.00011630682],"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":[0.0000013724245,0.000020229372,0.087517805,0.00000575147,0.000002130803,1.8727819e-7,0.00002834606,0.000049272196,0.7386875,0.00010721743,0.00007793627,0.17350227],"study_design_scores_gemma":[0.000091577036,0.00012855645,0.8864678,0.000006801344,0.0000020712882,0.000001729109,0.000025050696,0.0029228216,0.109616786,0.0002992129,0.00035786207,0.00007973231],"about_ca_topic_score_codex":0.00003301092,"about_ca_topic_score_gemma":0.000006700189,"teacher_disagreement_score":0.79895,"about_ca_system_score_codex":0.0000379351,"about_ca_system_score_gemma":0.0000020973496,"threshold_uncertainty_score":0.9995856},"labels":[],"label_agreement":null},{"id":"W4234334879","doi":"10.1016/b978-0-12-824372-5.00019-1","title":"Exergy analyses of aircraft flight systems","year":2020,"lang":"en","type":"book-chapter","venue":"Elsevier eBooks","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Ontario Tech University","funders":"","keywords":"Exergy; Aerospace; Aerospace engineering; Environmental science; Engineering; Propulsion; Automotive engineering; Process engineering","score_opus":0.02922452052985294,"score_gpt":0.2571515408947478,"score_spread":0.22792702036489484,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4234334879","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.000023010862,0.0016312567,0.00027132663,0.00006154551,0.00018670797,0.0004013936,0.00003356804,0.00024423056,0.99714696],"genre_scores_gemma":[0.018014185,0.00020712984,0.0013346432,0.00010801249,0.00008136656,0.00003254387,0.000012643816,0.00007991087,0.98012954],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9980714,0.000020102367,0.00055739825,0.0005961493,0.00048896094,0.0002659938],"domain_scores_gemma":[0.9987431,0.000053813223,0.00039476537,0.0006773577,0.000016292204,0.000114649614],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.000082402476,0.0004439554,0.0007643846,0.000092797665,0.000069655885,0.00001849383,0.0006114324,0.00037334376,0.0006666182],"category_scores_gemma":[0.000025451776,0.0003781555,0.00026307628,0.0000377423,0.00051406276,0.00006179121,0.00042100885,0.00037226238,0.0007760636],"study_design_candidate":"design_other","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":[0.00001805819,0.000011718858,0.000033631917,0.0001351306,0.00015879858,0.00011291453,0.00007760463,0.0001778297,0.00691612,0.008968903,0.0010898347,0.98229945],"study_design_scores_gemma":[0.000133932,0.000102466074,0.0000129498485,0.0002084933,0.00011972656,0.000011842128,0.000019001196,0.00005158327,0.003912952,0.014230867,0.98074436,0.00045185132],"about_ca_topic_score_codex":0.000004383414,"about_ca_topic_score_gemma":0.0000088698325,"teacher_disagreement_score":0.9818476,"about_ca_system_score_codex":0.00012687105,"about_ca_system_score_gemma":0.000021140955,"threshold_uncertainty_score":0.999867},"labels":[],"label_agreement":null},{"id":"W4234550733","doi":"10.5383/ijtee.13.02.003","title":"The Future of Conventional Aircraft Ground Propulsion Systems in Relation to Fuel Consumption and CO2 Emission","year":2017,"lang":"en","type":"article","venue":"International Journal of Thermal and Environmental Engineering","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Fuel efficiency; Aircraft fuel system; Automotive engineering; Runway; Propulsion; Aeronautics; Thrust specific fuel consumption; Engineering; Block (permutation group theory); Fuel tank; Environmental science; Marine engineering; Aerospace engineering; Combustion","score_opus":0.007362281175477395,"score_gpt":0.21586249404757948,"score_spread":0.20850021287210208,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4234550733","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":[0.99748206,0.0008279796,0.0008104,0.00042704146,0.00034212336,0.000075927645,0.0000036648353,0.0000038055064,0.000027000178],"genre_scores_gemma":[0.9986772,0.000750917,0.00046137994,0.0000064750543,0.000054172688,0.0000025345264,0.0000012043407,0.0000047506414,0.000041355655],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.9994177,0.000009346322,0.0002051012,0.00007572821,0.00022191672,0.00007018633],"domain_scores_gemma":[0.99969596,0.000026550728,0.00017000987,0.00006736296,0.0000036376002,0.000036484365],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000163131,0.00006701158,0.000078065255,0.00003661974,0.00007249007,0.000036999387,0.00018284898,0.000039690654,0.000014601789],"category_scores_gemma":[0.000020501475,0.000047255115,0.000021703458,0.000009971419,0.00009678963,0.00029222335,0.00014292485,0.00010419327,0.00000195601],"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":[0.0002431429,0.00007124235,0.39124662,0.000025784804,0.00004720717,0.00003454436,0.00025749922,0.04555039,0.4839897,0.00066175876,0.00003342149,0.07783871],"study_design_scores_gemma":[0.00048234029,0.00006704213,0.98746854,0.0001058826,0.0000051608727,0.00008917118,0.00016066922,0.0074306913,0.0013882278,0.0002509336,0.0024760605,0.000075294396],"about_ca_topic_score_codex":0.000013932615,"about_ca_topic_score_gemma":0.0000022231059,"teacher_disagreement_score":0.5962219,"about_ca_system_score_codex":0.00008443514,"about_ca_system_score_gemma":0.0000015083101,"threshold_uncertainty_score":0.19270076},"labels":[],"label_agreement":null},{"id":"W4238179141","doi":"10.32920/ryerson.14649570","title":"Structural repair on a composite aircraft fuselage damaged by fire.","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Fuselage; Durability; Structural engineering; Composite number; Suite; Forensic engineering; Aerospace engineering; Computer science; Engineering; Aeronautics","score_opus":0.013158346653004738,"score_gpt":0.236651291777103,"score_spread":0.22349294512409826,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4238179141","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":[0.975955,0.0002521074,0.002767419,0.00067902025,0.00036874606,0.00049863994,0.000054016087,0.0022253531,0.017199686],"genre_scores_gemma":[0.96405727,0.00012453519,0.028477686,0.00078391924,0.000027124848,0.000054554377,0.00017880434,0.00004535339,0.0062507484],"study_design_codex":"not_applicable","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9975382,0.00009303435,0.0003398512,0.0011076549,0.00046990288,0.00045133792],"domain_scores_gemma":[0.99841946,0.000085715874,0.00014309183,0.0012280138,0.000009731558,0.00011395433],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00011320122,0.00047930013,0.000430906,0.000037314345,0.00019703903,0.00009631193,0.0007293993,0.00045877302,0.003447186],"category_scores_gemma":[0.00006305536,0.00041386357,0.0002565402,0.00019182578,0.00034455836,0.00015887425,0.0022299683,0.0010862886,0.0003003249],"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":[0.00030117494,0.0010105143,0.10575438,0.00042095454,0.0006239175,0.001783972,0.0016684339,0.048237946,0.2714758,0.001015629,0.44292653,0.124780744],"study_design_scores_gemma":[0.0057386276,0.0019460875,0.2623132,0.0014873942,0.0005275136,0.00026703658,0.0039159264,0.103276454,0.45270622,0.04941058,0.10420769,0.014203261],"about_ca_topic_score_codex":0.0003104122,"about_ca_topic_score_gemma":0.00008027009,"teacher_disagreement_score":0.33871883,"about_ca_system_score_codex":0.00029225816,"about_ca_system_score_gemma":0.000017401431,"threshold_uncertainty_score":0.9998313},"labels":[],"label_agreement":null},{"id":"W4243734136","doi":"10.1115/1.4025007","title":"Evaluation of Gas Turbine Outboard Bleed Air on Overall Engine Efficiency and CO2e Emission in Natural Gas Compressor Stations","year":2013,"lang":"en","type":"article","venue":"Journal of Engineering for Gas Turbines and Power","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"TransCanada (Canada); Nova Chemicals (Canada)","funders":"","keywords":"Gas compressor; Automotive engineering; Natural gas; Bleed; Compressor station; Turbine; Engineering; Industrial gas; Overall pressure ratio; Marine engineering; Axial compressor; Environmental science; Mechanical engineering; Waste management","score_opus":0.009796182782037746,"score_gpt":0.23871583322829112,"score_spread":0.22891965044625337,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4243734136","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":[0.9959948,0.0007363124,0.0022592144,0.0005158941,0.00015820579,0.0002630771,0.0000039426473,0.00001561962,0.00005290618],"genre_scores_gemma":[0.9947512,0.00011359395,0.005033426,0.000024743505,0.000017733582,0.000008673948,0.0000017913735,0.000010229442,0.00003857634],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991341,0.000013799838,0.00028913154,0.000114569,0.00029239545,0.00015597974],"domain_scores_gemma":[0.9995348,0.00011637443,0.0001345222,0.00008263916,0.000077290606,0.00005439959],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00032985938,0.00012580726,0.00019730406,0.000119009426,0.000029904384,0.000013051657,0.0000844246,0.0000532384,0.000046257894],"category_scores_gemma":[0.00025993853,0.00009246798,0.00004209505,0.000103094244,0.000045163328,0.00022690109,0.000032203534,0.00015367598,8.058131e-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":[0.00017696898,0.0002790396,0.0047794073,0.0001162583,0.000061804276,0.0000064458827,0.0009313396,0.6252429,0.33892733,0.0002769903,0.0017112656,0.027490241],"study_design_scores_gemma":[0.0067138616,0.0021182802,0.13570555,0.0006333761,0.00014717586,0.00009557054,0.00029454136,0.79513127,0.046386886,0.0078991745,0.004234445,0.00063986983],"about_ca_topic_score_codex":0.000015151024,"about_ca_topic_score_gemma":0.000002076594,"teacher_disagreement_score":0.29254046,"about_ca_system_score_codex":0.0000612663,"about_ca_system_score_gemma":0.000007545818,"threshold_uncertainty_score":0.37707347},"labels":[],"label_agreement":null},{"id":"W4244238897","doi":"10.32920/ryerson.14649570.v1","title":"Structural repair on a composite aircraft fuselage damaged by fire.","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Fuselage; Durability; Structural engineering; Composite number; Forensic engineering; Engineering; Aerospace engineering; Aeronautics; Computer science; Materials science; Composite material","score_opus":0.013158346653004738,"score_gpt":0.236651291777103,"score_spread":0.22349294512409826,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4244238897","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":[0.975955,0.0002521074,0.002767419,0.00067902025,0.00036874606,0.00049863994,0.000054016087,0.0022253531,0.017199686],"genre_scores_gemma":[0.96405727,0.00012453519,0.028477686,0.00078391924,0.000027124848,0.000054554377,0.00017880434,0.00004535339,0.0062507484],"study_design_codex":"not_applicable","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9975382,0.00009303435,0.0003398512,0.0011076549,0.00046990288,0.00045133792],"domain_scores_gemma":[0.99841946,0.000085715874,0.00014309183,0.0012280138,0.000009731558,0.00011395433],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00011320122,0.00047930013,0.000430906,0.000037314345,0.00019703903,0.00009631193,0.0007293993,0.00045877302,0.003447186],"category_scores_gemma":[0.00006305536,0.00041386357,0.0002565402,0.00019182578,0.00034455836,0.00015887425,0.0022299683,0.0010862886,0.0003003249],"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":[0.00030117494,0.0010105143,0.10575438,0.00042095454,0.0006239175,0.001783972,0.0016684339,0.048237946,0.2714758,0.001015629,0.44292653,0.124780744],"study_design_scores_gemma":[0.0057386276,0.0019460875,0.2623132,0.0014873942,0.0005275136,0.00026703658,0.0039159264,0.103276454,0.45270622,0.04941058,0.10420769,0.014203261],"about_ca_topic_score_codex":0.0003104122,"about_ca_topic_score_gemma":0.00008027009,"teacher_disagreement_score":0.33871883,"about_ca_system_score_codex":0.00029225816,"about_ca_system_score_gemma":0.000017401431,"threshold_uncertainty_score":0.9998313},"labels":[],"label_agreement":null},{"id":"W4245913177","doi":"10.32920/ryerson.14635626","title":"Performance Prediction Analysis for Aero-Naut CAM Folding Propellers and its Application into CREATeV Solar Aircraft","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Propeller; Folding (DSP implementation); Parametric statistics; Marine engineering; Performance prediction; Scaling; Engineering; Work (physics); Computer science; Aerospace engineering; Mechanical engineering; Simulation; Mathematics","score_opus":0.014718819737504841,"score_gpt":0.23461629631757155,"score_spread":0.21989747658006673,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4245913177","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":[0.5660978,0.00024565437,0.4307857,0.0001883463,0.00007009616,0.0012066333,0.0000136260005,0.0003831676,0.0010089896],"genre_scores_gemma":[0.9634314,0.0010469051,0.0337328,0.00003744223,0.000027033926,0.0007371364,0.00014298223,0.000024204706,0.00082005275],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9981802,0.000023642733,0.00032342406,0.0009401608,0.0002462796,0.00028631],"domain_scores_gemma":[0.99919343,0.000038422208,0.00017358645,0.00048712548,0.000031900636,0.00007551124],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00023958713,0.00029172905,0.00036484023,0.00014198807,0.00026361985,0.000078422294,0.00030307902,0.0003447642,0.00013882232],"category_scores_gemma":[0.00005352188,0.00026332206,0.00014363033,0.0004433524,0.00011902018,0.0003576965,0.0008150105,0.0002892375,0.000019197025],"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":[0.00008422564,0.00021027595,0.33113104,0.00077682664,0.0009475182,0.0000037107486,0.001117714,0.34379277,0.07518517,0.00017781332,0.00029715302,0.24627578],"study_design_scores_gemma":[0.00040574625,0.00015042826,0.042274654,0.00008254559,0.00081743853,0.000004652628,0.0005935843,0.88625413,0.06492357,0.0012679162,0.002470442,0.0007549089],"about_ca_topic_score_codex":0.00014272828,"about_ca_topic_score_gemma":0.00013520244,"teacher_disagreement_score":0.54246134,"about_ca_system_score_codex":0.00028141958,"about_ca_system_score_gemma":0.000019671557,"threshold_uncertainty_score":0.9999819},"labels":[],"label_agreement":null},{"id":"W4246345031","doi":"10.1088/1757-899x/842/1/011002","title":"Conference Chairs","year":2020,"lang":"en","type":"article","venue":"IOP Conference Series Materials Science and Engineering","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Library science; China; Technical university; Political science; Law","score_opus":0.01837547454596238,"score_gpt":0.20023500590283394,"score_spread":0.18185953135687155,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4246345031","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":[0.98671716,0.000020214391,0.0072271507,0.00247508,0.00021620584,0.00017593498,0.000009869432,0.00047095126,0.0026874298],"genre_scores_gemma":[0.99486,0.00008823642,0.004722379,0.00020989713,0.000031874482,0.000019389248,0.0000011430759,0.000010981529,0.000056120738],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9985919,0.000007257022,0.00018520055,0.00045266046,0.00033262392,0.00043033055],"domain_scores_gemma":[0.9995243,0.0000120204,0.00004827638,0.00018419136,0.000034972712,0.00019624624],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021085431,0.00019210891,0.00020637308,0.000040226638,0.00018367368,0.00024457157,0.00047516418,0.000056633857,0.0008460354],"category_scores_gemma":[0.00026244752,0.0001722168,0.000012262237,0.00043058032,0.0008706889,0.0011802351,0.00045052107,0.00009325581,0.00013092795],"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":[0.0000096641525,0.0000033287804,0.0000792247,0.00001686517,0.000001406091,0.0000073968426,0.00039109154,0.00024492148,0.9892873,0.006462312,0.00005008749,0.0034463597],"study_design_scores_gemma":[0.00014377362,0.00015184554,0.003414662,0.00002754224,0.0000048009506,0.000023567329,0.00049611554,0.0028054917,0.98557544,0.00089944544,0.0060692024,0.00038810444],"about_ca_topic_score_codex":0.00002329645,"about_ca_topic_score_gemma":0.0000032474773,"teacher_disagreement_score":0.008142815,"about_ca_system_score_codex":0.00004264044,"about_ca_system_score_gemma":0.000038048172,"threshold_uncertainty_score":0.9263494},"labels":[],"label_agreement":null},{"id":"W4246374729","doi":"10.1504/ijsa.2018.098424","title":"Sustainable flight test project tools","year":2018,"lang":"en","type":"article","venue":"International Journal of Sustainable Aviation","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université du Québec à Trois-Rivières","funders":"","keywords":"Certification; Aviation; Sample (material); Key (lock); Product (mathematics); Cost reduction; New product development; Flight test; Sustainable development; Manufacturing engineering; Engineering; Business; Aeronautics; Systems engineering; Computer science; Simulation; Marketing; Aerospace engineering; Computer security; Economics","score_opus":0.01135626202321967,"score_gpt":0.26723557713324586,"score_spread":0.2558793151100262,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4246374729","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":[0.7385348,0.00021347254,0.14478445,0.0093741035,0.0014006482,0.0013116621,0.00001142464,0.0003115171,0.10405791],"genre_scores_gemma":[0.9795789,0.000038360937,0.0034931984,0.00019196462,0.00032636255,0.000009501749,0.000003402696,0.000012819327,0.016345505],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"not_applicable","domain_scores_codex":[0.99851793,0.00002633357,0.00037226168,0.00015560359,0.0005985644,0.00032928062],"domain_scores_gemma":[0.9986376,0.00011762579,0.0003929098,0.00013379431,0.00067444344,0.000043619024],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00045915475,0.00011842795,0.00012853988,0.00023897723,0.00014203611,0.00014842667,0.00058303546,0.00007542169,0.00052973244],"category_scores_gemma":[0.0014865762,0.0001005648,0.00006942923,0.0003725561,0.00018401809,0.0020149131,0.00023072194,0.00016023229,0.00010251989],"study_design_candidate":"not_applicable","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":[0.0013794865,0.0021767593,0.23847404,0.00010905385,0.0004675197,0.0073890844,0.007636557,0.0018887245,0.056178477,0.30324063,0.19209336,0.18896632],"study_design_scores_gemma":[0.0020760794,0.0017232287,0.043406725,0.000059895534,0.00004758061,0.00049929053,0.023206066,0.0005613705,0.060042433,0.14836925,0.7194527,0.0005553817],"about_ca_topic_score_codex":0.00012277662,"about_ca_topic_score_gemma":0.0000065609715,"teacher_disagreement_score":0.52735937,"about_ca_system_score_codex":0.0009108473,"about_ca_system_score_gemma":0.00009090339,"threshold_uncertainty_score":0.58001983},"labels":[],"label_agreement":null},{"id":"W4246591708","doi":"10.24124/2012/bpgub819","title":"A sky-high challenge: The carbon footprint of aviation in British Columbia, Canada, and measures to mitigate it.","year":2012,"lang":"en","type":"dissertation","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Civil aviation; Greenhouse gas; Carbon footprint; Aviation; Business; Government (linguistics); Incentive; Transport engineering; Environmental science; Engineering; Economics","score_opus":0.007872811149733767,"score_gpt":0.20250446987139273,"score_spread":0.19463165872165897,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4246591708","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":[0.9922901,0.00027186025,0.000015141458,0.0002951212,0.00012175062,0.0004480239,0.000008026159,0.000025439711,0.0065245507],"genre_scores_gemma":[0.99565786,0.00015737116,0.00017611509,0.000041899526,0.000007762014,0.000086639135,0.000015153678,0.000013855882,0.0038433415],"study_design_codex":"design_other","study_design_gemma":"observational","domain_scores_codex":[0.998957,0.000028878607,0.00022781809,0.0002513281,0.00031792637,0.00021704283],"domain_scores_gemma":[0.9996042,0.000038554754,0.00010185446,0.00019248645,0.000012956401,0.000049897815],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00014494329,0.000106040716,0.00019361166,0.000021283731,0.000052146723,0.000026861137,0.00019743077,0.00014255477,0.00008491984],"category_scores_gemma":[0.00007638141,0.00012447148,0.000018619638,0.00014402386,0.0000599299,0.000030181409,0.000062088526,0.0001711707,0.0000013331884],"study_design_candidate":"observational","study_design_consensus":null,"about_ca_topic_candidate":true,"about_ca_topic_consensus":true,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00002707115,0.00012876108,0.2172543,0.00013243336,0.000041363845,0.000023577224,0.0017896222,0.00020739181,0.010962397,0.00027163027,0.0007367346,0.7684247],"study_design_scores_gemma":[0.00012389955,0.000039408606,0.992295,0.00008023139,0.0000125067145,0.000002196429,0.0017146828,0.000012719124,0.0019482512,0.0026841008,0.00088423747,0.00020273536],"about_ca_topic_score_codex":0.9884709,"about_ca_topic_score_gemma":0.99992454,"teacher_disagreement_score":0.77504075,"about_ca_system_score_codex":0.00019714246,"about_ca_system_score_gemma":0.00004220969,"threshold_uncertainty_score":0.50758},"labels":[],"label_agreement":null},{"id":"W4251381540","doi":"10.32920/ryerson.14648193","title":"Multidisciplinary Design Optimization of a Helicopter Rotor Blade","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Natural Sciences and Engineering Research Council of Canada; Queen's University","keywords":"Sequential quadratic programming; Particle swarm optimization; Blade element momentum theory; Aerodynamics; Rotor (electric); Finite element method; Blade element theory; Reduction (mathematics); Blade (archaeology); Helicopter rotor; Engineering; Structural engineering; Control theory (sociology); Mathematics; Computer science; Mathematical optimization; Quadratic programming; Mechanical engineering; Aerospace engineering; Turbine blade; Geometry","score_opus":0.026597527439121364,"score_gpt":0.25850918207742474,"score_spread":0.23191165463830338,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4251381540","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":[0.00549311,0.00007208501,0.9779075,0.000092236485,0.000070045426,0.0005703825,0.0000027453796,0.0002539275,0.0155379595],"genre_scores_gemma":[0.27325737,0.000096079915,0.7229164,0.000019493695,0.000008459299,0.00009526308,0.000010222718,0.000032066073,0.003564627],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99895036,0.00004305273,0.00022761108,0.0004311433,0.00018494361,0.00016290655],"domain_scores_gemma":[0.9992858,0.000035054763,0.0001427055,0.00048996217,0.0000086805285,0.000037776736],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00008205063,0.00018827278,0.00023083933,0.000047978796,0.00003152264,0.000016191107,0.0003121402,0.00025652925,0.0070006833],"category_scores_gemma":[0.00004730905,0.00016467964,0.00007873887,0.00012571947,0.00016921894,0.00008265737,0.0016470051,0.00019287023,0.00007602337],"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":[0.000010225728,0.000091012516,0.0012270758,0.000024468744,0.000014745898,0.000011776883,0.00011851011,0.9853005,0.008610417,0.000019853866,0.0002988331,0.0042726197],"study_design_scores_gemma":[0.00071133557,0.00023014066,0.005247758,0.0003319899,0.000074023796,0.00001447499,0.0010856396,0.6866407,0.29903534,0.005092707,0.00031831756,0.0012176244],"about_ca_topic_score_codex":0.00004401608,"about_ca_topic_score_gemma":0.000010835234,"teacher_disagreement_score":0.2986598,"about_ca_system_score_codex":0.000077332144,"about_ca_system_score_gemma":0.000015788033,"threshold_uncertainty_score":0.99390703},"labels":[],"label_agreement":null},{"id":"W4251794209","doi":"10.32920/ryerson.14647884","title":"Bleed Air Temperature Regulation System: Modeling, Control, and Simulation","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Heat exchanger; Control theory (sociology); Temperature control; System dynamics; Control system; State-space representation; Nonlinear system; Control (management); Control valves; Engineering; Computer science; Control engineering; Automotive engineering; Simulation; Mechanical engineering; Physics","score_opus":0.010451318765617572,"score_gpt":0.2271680632020485,"score_spread":0.2167167444364309,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4251794209","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":[0.50127184,0.0003445243,0.49246126,0.00041744215,0.0001950952,0.00065758644,0.000008680514,0.00083526777,0.003808303],"genre_scores_gemma":[0.99008256,0.00002805753,0.0091740005,0.00008612479,0.00003007735,0.000031079864,0.000039073744,0.000017694176,0.000511312],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99877244,0.000043840286,0.00023718493,0.00055251725,0.000227334,0.00016666374],"domain_scores_gemma":[0.99939907,0.000035748675,0.000096134536,0.0004030137,0.000021777058,0.00004427524],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00011747428,0.0002207449,0.00026109198,0.00003886051,0.00010902734,0.00006879755,0.0001407578,0.00046060196,0.0001296659],"category_scores_gemma":[0.00003961913,0.00019081596,0.000053655498,0.000092517985,0.000075952805,0.00018901058,0.00042097826,0.00033071762,0.000016566422],"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":[0.000009071169,0.000009727689,0.0005759054,0.000052844065,0.000012304404,0.0000043131463,0.00004532722,0.9905258,0.0071785217,0.00015244915,0.000048001828,0.0013857655],"study_design_scores_gemma":[0.0002648808,0.000012725036,0.0013727332,0.00009282628,0.000029292383,0.000004046943,0.0002884109,0.9948107,0.00064135104,0.0021834825,0.0000671847,0.0002323647],"about_ca_topic_score_codex":0.00011514685,"about_ca_topic_score_gemma":0.000040308976,"teacher_disagreement_score":0.48881072,"about_ca_system_score_codex":0.00018350164,"about_ca_system_score_gemma":0.000010727498,"threshold_uncertainty_score":0.7781249},"labels":[],"label_agreement":null},{"id":"W4252499335","doi":"10.32920/ryerson.14649783","title":"Development of UAV derivative MDO methodology for flight simulation","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Multidisciplinary design optimization; Derivative (finance); Process (computing); Flight simulator; Simulation; Computer science; Engineering; Multidisciplinary approach","score_opus":0.1339321546614659,"score_gpt":0.3571032787808954,"score_spread":0.22317112411942946,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4252499335","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":[0.068565756,0.000042672298,0.92882216,0.00011105943,0.0001220018,0.00045025235,0.0000039753872,0.00010300293,0.0017790972],"genre_scores_gemma":[0.34801573,0.000007598486,0.65153813,0.000036502413,0.000005634658,0.00008321126,0.000026146492,0.000008950189,0.00027809813],"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9988497,0.000052472922,0.0003445108,0.0004332025,0.00014224373,0.00017789517],"domain_scores_gemma":[0.9990527,0.0003990651,0.00020301556,0.00029521793,0.000025680603,0.0000242923],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00027677332,0.00017395115,0.00032178103,0.000043367847,0.000059120997,0.000008500449,0.00026151043,0.00027646893,0.000600466],"category_scores_gemma":[0.00034087864,0.0001514933,0.00007808279,0.00010232579,0.00013660533,0.000062321735,0.0009900241,0.00015203521,0.000010680345],"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":[0.00007689151,0.00019428371,0.0020125567,0.000237204,0.00018956691,0.0000048356305,0.0043563484,0.2973307,0.1993279,0.0021382673,0.000333936,0.4937975],"study_design_scores_gemma":[0.00029883787,0.00004524424,0.0042641745,0.000056025197,0.000028169257,9.1662844e-7,0.001242732,0.01258184,0.9251108,0.039726175,0.01617716,0.00046790062],"about_ca_topic_score_codex":0.00001320391,"about_ca_topic_score_gemma":0.00006386895,"teacher_disagreement_score":0.72578293,"about_ca_system_score_codex":0.00015182963,"about_ca_system_score_gemma":0.000039663784,"threshold_uncertainty_score":0.65746814},"labels":[],"label_agreement":null},{"id":"W4254457941","doi":"10.32920/ryerson.14647884.v1","title":"Bleed Air Temperature Regulation System: Modeling, Control, and Simulation","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Toronto Metropolitan University","funders":"","keywords":"Heat exchanger; Control theory (sociology); Temperature control; System dynamics; Control system; State-space representation; Nonlinear system; Control (management); Engineering; Control valves; Control engineering; Computer science; Automotive engineering; Mechanical engineering; Physics","score_opus":0.010451318765617572,"score_gpt":0.2271680632020485,"score_spread":0.2167167444364309,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4254457941","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":[0.50127184,0.0003445243,0.49246126,0.00041744215,0.0001950952,0.00065758644,0.000008680514,0.00083526777,0.003808303],"genre_scores_gemma":[0.99008256,0.00002805753,0.0091740005,0.00008612479,0.00003007735,0.000031079864,0.000039073744,0.000017694176,0.000511312],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99877244,0.000043840286,0.00023718493,0.00055251725,0.000227334,0.00016666374],"domain_scores_gemma":[0.99939907,0.000035748675,0.000096134536,0.0004030137,0.000021777058,0.00004427524],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00011747428,0.0002207449,0.00026109198,0.00003886051,0.00010902734,0.00006879755,0.0001407578,0.00046060196,0.0001296659],"category_scores_gemma":[0.00003961913,0.00019081596,0.000053655498,0.000092517985,0.000075952805,0.00018901058,0.00042097826,0.00033071762,0.000016566422],"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":[0.000009071169,0.000009727689,0.0005759054,0.000052844065,0.000012304404,0.0000043131463,0.00004532722,0.9905258,0.0071785217,0.00015244915,0.000048001828,0.0013857655],"study_design_scores_gemma":[0.0002648808,0.000012725036,0.0013727332,0.00009282628,0.000029292383,0.000004046943,0.0002884109,0.9948107,0.00064135104,0.0021834825,0.0000671847,0.0002323647],"about_ca_topic_score_codex":0.00011514685,"about_ca_topic_score_gemma":0.000040308976,"teacher_disagreement_score":0.48881072,"about_ca_system_score_codex":0.00018350164,"about_ca_system_score_gemma":0.000010727498,"threshold_uncertainty_score":0.7781249},"labels":[],"label_agreement":null},{"id":"W4255394472","doi":"10.32920/ryerson.14649630","title":"A design methodology for rotors of small multirotor vehicles","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":15,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"Natural Sciences and Engineering Research Council of Canada; Ontario Centres of Excellence","keywords":"Multirotor; Aerodynamics; Rotor (electric); Wake; Blade element momentum theory; Inflow; Power (physics); Wake turbulence; Operating point; Flow (mathematics); Control theory (sociology); Point (geometry); Computer science; Engineering; Aerospace engineering; Mechanical engineering; Mechanics; Physics; Mathematics; Turbine; Electronic engineering","score_opus":0.15452912609874733,"score_gpt":0.3211829899589272,"score_spread":0.16665386386017986,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4255394472","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":[0.07343775,0.00011167658,0.92397434,0.00010136337,0.00015654402,0.0017345955,0.000009411532,0.00018896158,0.00028536568],"genre_scores_gemma":[0.09371646,0.000042589,0.90476274,0.000064319596,0.000013810419,0.00083318196,0.000008970385,0.000024425037,0.00053349393],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9984968,0.00017969724,0.00033525363,0.000587142,0.0001232072,0.0002779124],"domain_scores_gemma":[0.9983979,0.0007835802,0.00021058608,0.0005433477,0.000020128002,0.000044482153],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005079598,0.0002412327,0.00047670922,0.000053332256,0.000043528245,0.000013574968,0.0005394771,0.00044656286,0.00042371554],"category_scores_gemma":[0.0005325065,0.00020801369,0.00017686385,0.00009752475,0.000249137,0.000042787,0.0011659764,0.00026029284,0.000010780195],"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":[0.00030840066,0.00046077688,0.010811844,0.00051655236,0.00023695576,0.000030671374,0.0010991464,0.09986878,0.57222503,0.0009005207,0.0011633977,0.31237793],"study_design_scores_gemma":[0.0005633273,0.00026012323,0.002617497,0.00007226011,0.00006521644,0.0000054570523,0.00063064246,0.013304603,0.9328625,0.047855973,0.0011853372,0.00057706767],"about_ca_topic_score_codex":0.00025387754,"about_ca_topic_score_gemma":0.00007601026,"teacher_disagreement_score":0.3606375,"about_ca_system_score_codex":0.00009337378,"about_ca_system_score_gemma":0.000030779054,"threshold_uncertainty_score":0.8482552},"labels":[],"label_agreement":null},{"id":"W4280591100","doi":"10.2514/1.i011050","title":"Aircraft Mathematical Model Identification for Flight Trajectories and Performance Analysis in Cruise","year":2022,"lang":"en","type":"article","venue":"Journal of Aerospace Information Systems","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":9,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure","funders":"Canada Research Chairs","keywords":"Cruise; Fuel efficiency; Range (aeronautics); Civil aviation; Crew; Aircraft flight mechanics; Trajectory; Engineering; Flight simulator; Operations research; Aviation; Aerodynamics; Aerospace engineering; Computer science; Aeronautics","score_opus":0.012464974202225872,"score_gpt":0.23366402588566956,"score_spread":0.2211990516834437,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4280591100","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":[0.7056235,0.000054943117,0.29344153,0.00020750302,0.000085434105,0.00028631662,0.000011812978,0.000021336331,0.00026763082],"genre_scores_gemma":[0.9962399,0.000030165369,0.0034312527,0.000021227539,0.000007965565,0.0000601523,0.0000036883348,0.0000039041793,0.00020176583],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99874586,0.000024794386,0.0006531133,0.00006809864,0.0003800836,0.00012806492],"domain_scores_gemma":[0.9991986,0.000053650703,0.00055227056,0.00012277928,0.000035673147,0.000036997695],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00079940347,0.0000837757,0.00022903304,0.0002459437,0.00015242238,0.000065339766,0.00017246768,0.00003795924,0.000021515429],"category_scores_gemma":[0.00007108912,0.00007163443,0.00006581049,0.0005390633,0.000053083375,0.0015816181,0.00006288058,0.00013869411,0.0000059025538],"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":[0.00008842206,0.000041880816,0.029907152,0.00007839181,0.00004563208,8.3473884e-7,0.0030982555,0.96191657,0.0009852761,0.0012005307,0.00070162275,0.0019354618],"study_design_scores_gemma":[0.0006509823,0.00020511514,0.014916932,0.000020268966,0.000081001745,0.000060571223,0.0053614965,0.97472113,0.000730834,0.0009724829,0.002105746,0.00017343446],"about_ca_topic_score_codex":0.000005541496,"about_ca_topic_score_gemma":0.0000033255676,"teacher_disagreement_score":0.2906164,"about_ca_system_score_codex":0.00022761255,"about_ca_system_score_gemma":0.000015061625,"threshold_uncertainty_score":0.29211673},"labels":[],"label_agreement":null},{"id":"W4281633404","doi":"10.1139/dsa-2021-0031","title":"Aerodynamics effect of holes in UAV wings modified for VTOL capability","year":2022,"lang":"en","type":"article","venue":"Drone Systems and Applications","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Drag; Lift-to-drag ratio; Aerodynamics; Wing; Lift-induced drag; Lift (data mining); Aerospace engineering; Turbulence; Wind tunnel; Angle of attack; Computational fluid dynamics; Marine engineering; Wing configuration; Mechanics; Wing twist; Drag coefficient; Lift coefficient; Wingtip vortices; Physics; Engineering; Computer science; Vortex; Horseshoe vortex; Reynolds number; Vorticity","score_opus":0.0077411009870517015,"score_gpt":0.23214944367279286,"score_spread":0.22440834268574117,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4281633404","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":[0.92053324,0.0001248392,0.0771696,0.00007561362,0.000017438417,0.0015540957,0.000067576315,0.000050809245,0.00040679393],"genre_scores_gemma":[0.9965982,0.0000045755355,0.00034429517,0.0000044666567,0.0000049531536,0.0029355066,0.000010658355,0.0000055228784,0.000091810376],"study_design_codex":"observational","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994473,0.000027259273,0.00015321467,0.00019209806,0.00007957369,0.000100553916],"domain_scores_gemma":[0.99963015,0.00009216428,0.00006400059,0.00019425135,0.0000026047517,0.000016810793],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024326918,0.000062413324,0.00013520282,0.000024016965,0.00012495913,0.0000048230745,0.00011791957,0.000025713518,0.0000055941014],"category_scores_gemma":[0.000012037367,0.00005697854,0.000021351454,0.00015996833,0.00014046492,0.000038055583,0.00009689481,0.000061727296,0.000001327379],"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":[0.00016242226,0.0007140679,0.24811406,0.0010462881,0.00003773401,0.0000021880046,0.000992618,0.2337871,0.219328,0.17294621,0.0005254921,0.122343816],"study_design_scores_gemma":[0.010708999,0.003553833,0.16808024,0.00012607046,0.00020468148,0.000101827296,0.00959462,0.5166269,0.020599842,0.13231644,0.1352318,0.002854776],"about_ca_topic_score_codex":0.00024631244,"about_ca_topic_score_gemma":0.00002592966,"teacher_disagreement_score":0.28283978,"about_ca_system_score_codex":0.00007583354,"about_ca_system_score_gemma":0.0000026828254,"threshold_uncertainty_score":0.23235175},"labels":[],"label_agreement":null},{"id":"W4281986019","doi":"10.1016/j.ast.2022.107681","title":"A methodology to integrate reliability into the conceptual design of safety-critical multirotor unmanned aerial vehicles","year":2022,"lang":"en","type":"article","venue":"Aerospace Science and Technology","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":24,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Concordia University","funders":"Fondation Sciences et Technologies pour l’Aéronautique et l’Espace; Concordia University; Agence Nationale de la Recherche","keywords":"Multirotor; Sizing; Conceptual design; Reliability engineering; Reliability (semiconductor); Controllability; Payload (computing); Multidisciplinary design optimization; Computer science; Engineering; Systems engineering; Multidisciplinary approach; Aerospace engineering","score_opus":0.03009952464244506,"score_gpt":0.29588903665969557,"score_spread":0.2657895120172505,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4281986019","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":[0.896908,0.00014135097,0.068244025,0.03285391,0.0003102664,0.0010650863,0.000009671169,0.00032722813,0.00014045788],"genre_scores_gemma":[0.8936304,0.000021290736,0.10571206,0.00032772293,0.0000067157557,0.00022320166,3.0224143e-7,0.000008519199,0.00006979274],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9977716,0.00025414897,0.00027824272,0.00070138596,0.0004732119,0.0005213606],"domain_scores_gemma":[0.99841475,0.00072040065,0.00009018291,0.0006240994,0.00006652985,0.000084033505],"candidate_categories":["sts"],"consensus_categories":[],"category_scores_codex":[0.0024165711,0.00017229075,0.0002876514,0.00018236175,0.0010290553,0.000017298782,0.0013014937,0.0001164969,0.00014794043],"category_scores_gemma":[0.005153798,0.00012434724,0.000028145942,0.0025500811,0.01397309,0.00019192504,0.0022121142,0.00044121363,0.000020676021],"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":[0.00023833428,0.000100832964,0.003747468,0.000003946135,0.0000056301437,0.000009573176,0.0030357963,0.0017730347,0.88880724,0.051449064,0.0004339134,0.050395187],"study_design_scores_gemma":[0.0014152189,0.0051937583,0.003421775,0.000020223699,0.000044056113,0.00012929399,0.06695848,0.00549041,0.6393166,0.24983254,0.02725306,0.00092454226],"about_ca_topic_score_codex":0.0002483518,"about_ca_topic_score_gemma":0.000045405286,"teacher_disagreement_score":0.24949057,"about_ca_system_score_codex":0.00024306162,"about_ca_system_score_gemma":0.000088657674,"threshold_uncertainty_score":0.9887103},"labels":[],"label_agreement":null},{"id":"W4283399194","doi":"10.1016/j.fuel.2022.124764","title":"Aircraft engine particulate matter emissions from sustainable aviation fuels: Results from ground-based measurements during the NASA/DLR campaign ECLIF2/ND-MAX","year":2022,"lang":"en","type":"article","venue":"Fuel","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":101,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"National Research Council Canada","funders":"Division of Loan Repayment; Adelaide Research and Innovation, University of Adelaide; National Research Council Canada; U.S. Air Force; Deutsches Zentrum für Luft- und Raumfahrt; Transport Canada; U.S. Environmental Protection Agency; Federal Aviation Administration; Aeronautics Research Mission Directorate; H2020 Fast Track to Innovation; Langley Research Center; National Aeronautics and Space Administration","keywords":"Environmental science; Jet fuel; Particulates; Aviation fuel; Fossil fuel; Particle number; Renewable fuels; Waste management; Chemistry; Engineering; Volume (thermodynamics); Physics","score_opus":0.016658599904827813,"score_gpt":0.21910858626355295,"score_spread":0.20244998635872513,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4283399194","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":[0.9881063,0.00023521135,0.005320757,0.0025885466,0.0002334057,0.0006417207,0.00022537935,0.00041345748,0.002235204],"genre_scores_gemma":[0.9933309,0.0000068056734,0.0023951489,0.00054448686,0.0000411435,0.00020196848,0.00013697318,0.00003195572,0.0033106145],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.99767685,0.00016601158,0.0003653173,0.0005677865,0.0006789948,0.00054506405],"domain_scores_gemma":[0.99881315,0.00017357191,0.00017180748,0.00073321036,0.000017763366,0.00009051737],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0003773804,0.00023548662,0.00018378717,0.000050582832,0.000879134,0.000067027184,0.0005507318,0.00007559356,0.0039652823],"category_scores_gemma":[0.00017225285,0.00018708632,0.000086389984,0.00039170045,0.000121525125,0.00029619716,0.00048771847,0.0003535376,0.00043533533],"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":[0.0015001647,0.0011848601,0.40787062,0.000087220775,0.00026662313,0.00043994735,0.005903562,0.286434,0.2608497,0.00014988927,0.03165908,0.0036543359],"study_design_scores_gemma":[0.0054724505,0.00019805858,0.82522833,0.000061179555,0.00013988443,0.0000068669074,0.0071236445,0.0074754087,0.040463097,0.03448045,0.07807684,0.0012738134],"about_ca_topic_score_codex":0.0018371093,"about_ca_topic_score_gemma":0.00007331994,"teacher_disagreement_score":0.41735768,"about_ca_system_score_codex":0.0007025801,"about_ca_system_score_gemma":0.000029937099,"threshold_uncertainty_score":0.9969452},"labels":[],"label_agreement":null},{"id":"W4283829435","doi":"10.5281/zenodo.6801154","title":"Multidisciplinary design of a more electric regional aircraft including certification constraints","year":2022,"lang":"en","type":"paratext","venue":"Zenodo (CERN European Organization for Nuclear Research)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Concordia University","funders":"Concordia University; European Commission; Natural Sciences and Engineering Research Council of Canada; Horizon 2020 Framework Programme; Consortium de Recherche et d’innovation en Aérospatiale au Québec","keywords":"Multidisciplinary approach; Certification; Aeronautics; Computer science; Systems engineering; Engineering; Political science","score_opus":0.07442986725937376,"score_gpt":0.2843360046581465,"score_spread":0.20990613739877276,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4283829435","genre_codex":"other","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"other","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0017045051,0.00080462184,0.30447382,0.0014217797,0.00036068677,0.003080772,0.00059561216,0.0020386314,0.6855196],"genre_scores_gemma":[0.6920851,0.0046761096,0.0284309,0.00032178374,0.00033488625,0.000004511282,0.012507029,0.0121853305,0.24945435],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.9977775,0.00033308537,0.0003456509,0.000623842,0.0005474536,0.00037247417],"domain_scores_gemma":[0.9989205,0.000054219927,0.00032920248,0.00053442846,0.0000690073,0.00009266527],"candidate_categories":["metaepi_narrow","sts","insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.00045061286,0.0002310198,0.00024556718,0.00031896084,0.0015900262,0.000089338,0.0013599484,0.00015373348,0.19752225],"category_scores_gemma":[0.00028725812,0.00025082816,0.00006776978,0.0009664021,0.00066262565,0.00015791629,0.0023317242,0.0005028046,0.0227914],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00007742565,0.00019018498,0.0000027691126,0.000056120247,0.000041542065,0.000013177679,0.00048967294,0.0053569167,0.05209277,0.00024160257,0.82720643,0.11423137],"study_design_scores_gemma":[0.00029499797,0.0002685116,0.00016642587,0.000040013256,0.000017820441,0.00009607586,0.00035363328,0.0016296048,0.0019182538,0.00026965377,0.99463046,0.00031453063],"about_ca_topic_score_codex":0.000012365843,"about_ca_topic_score_gemma":5.986626e-8,"teacher_disagreement_score":0.6903806,"about_ca_system_score_codex":0.0004959307,"about_ca_system_score_gemma":0.0000066656326,"threshold_uncertainty_score":0.9999944},"labels":[],"label_agreement":null},{"id":"W4284897253","doi":"10.1109/itec53557.2022.9813971","title":"Implementation of a 200 kW Adaptable Testing Platform for Experimental Research in Electrification of Aircraft Propulsion","year":2022,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":5,"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":"Propulsion; Electrification; Automotive engineering; Systems engineering; Reliability (semiconductor); Certification; Battery (electricity); Electrically powered spacecraft propulsion; Engineering; Aviation; Avionics; Computer science; Aerospace engineering; Power (physics); Electrical engineering","score_opus":0.11883537616525629,"score_gpt":0.37823786190615927,"score_spread":0.25940248574090297,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4284897253","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":[0.9936314,0.00004902768,0.0037985507,0.00008474506,0.000015246327,0.00094744103,0.000007859079,0.000034463315,0.0014312158],"genre_scores_gemma":[0.97272646,0.0000027444446,0.026702644,0.000005629606,0.0000025527609,0.0004160651,0.0000086931095,0.0000069220255,0.00012826902],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99898744,0.000028573737,0.0002527131,0.00018909611,0.00032381518,0.00021836637],"domain_scores_gemma":[0.99964565,0.00010422199,0.000087165994,0.00013429447,0.000014989004,0.000013704742],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005872397,0.0000542949,0.00009097241,0.00012224082,0.00013157619,0.0000029538435,0.00017318835,0.000022054586,0.0005075623],"category_scores_gemma":[0.000038311267,0.00005221262,0.000018401986,0.0007076724,0.00007787704,0.00017495929,0.00011734957,0.00010076374,0.0000020638474],"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":[0.000051577557,0.00013423307,0.025763221,0.000009341841,0.0000013501823,3.4138105e-7,0.00021447573,0.000754221,0.9363545,0.00088927476,0.00022880272,0.035598624],"study_design_scores_gemma":[0.00053201255,0.00085640774,0.0062479763,0.0000051601237,0.0000011903144,0.0000017090871,0.010280774,0.0032324833,0.972962,0.0054613454,0.00034914733,0.00006979268],"about_ca_topic_score_codex":0.0013218439,"about_ca_topic_score_gemma":0.00012534883,"teacher_disagreement_score":0.036607463,"about_ca_system_score_codex":0.00030413872,"about_ca_system_score_gemma":0.000022594531,"threshold_uncertainty_score":0.5557451},"labels":[],"label_agreement":null},{"id":"W4285464739","doi":"10.32920/ryerson.14653626","title":"Preliminary Sailplane Design Using MDO And Multi-Fidelity Analysis","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Aerodynamics; Airworthiness; Multidisciplinary design optimization; Solver; Finite element method; Aerospace; Engineering; Aeroelasticity; Aerospace engineering; Wing; Computer science; Multidisciplinary approach; Structural engineering","score_opus":0.05925819300300604,"score_gpt":0.2871872764832746,"score_spread":0.22792908348026852,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4285464739","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.15084854,0.00038090904,0.84778744,0.000050829713,0.00004957302,0.00024773352,0.000007381856,0.00023025316,0.00039733577],"genre_scores_gemma":[0.50321305,0.00016063225,0.49627507,0.000051654355,0.0000058369087,0.000012352707,0.000019696221,0.000010949356,0.0002507521],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9982036,0.00012704139,0.00028574734,0.000875658,0.00022788359,0.000280101],"domain_scores_gemma":[0.9989593,0.00011685744,0.00013657493,0.0006933391,0.00001098918,0.00008293671],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00029837975,0.00029645854,0.00044439881,0.00010691125,0.00011736832,0.00008244769,0.00031230744,0.00035015531,0.00079784845],"category_scores_gemma":[0.00012397775,0.00026771484,0.00013072985,0.0003967011,0.00027801708,0.00014295775,0.0021953406,0.0004158194,0.000015107825],"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":[0.000060124654,0.00031705783,0.106448755,0.00009491726,0.0007483294,0.00015944791,0.00037860204,0.78084975,0.018078439,0.000054371485,0.00023436526,0.09257586],"study_design_scores_gemma":[0.00021388223,0.000063252526,0.07706858,0.00003844288,0.0007808552,0.000016970322,0.00039955744,0.9121009,0.006165801,0.0023837266,0.00009136311,0.0006766587],"about_ca_topic_score_codex":0.0009897698,"about_ca_topic_score_gemma":0.0001261961,"teacher_disagreement_score":0.3523645,"about_ca_system_score_codex":0.00016140462,"about_ca_system_score_gemma":0.000016332491,"threshold_uncertainty_score":0.9999775},"labels":[],"label_agreement":null},{"id":"W4287646011","doi":"","title":"Green house gas (GHG) reduction study for the rotorcraft industry","year":2020,"lang":"en","type":"article","venue":"HAL (Le Centre pour la Communication Scientifique Directe)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Cégep Marie-Victorin; Safran Electronics (Canada); National Research Council Canada","funders":"Office National d'études et de Recherches Aérospatiales","keywords":"Aviation; Fuel efficiency; Greenhouse gas; Software deployment; Fossil fuel; Engineering; Civil aviation; Aerospace; Aeronautics; Automotive engineering; Aerospace engineering; Waste management","score_opus":0.021944498654121184,"score_gpt":0.23232955031332408,"score_spread":0.2103850516592029,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4287646011","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":[0.6171151,0.00024055786,0.27888206,0.088366084,0.00015858306,0.0029996973,0.000020955646,0.0014732612,0.010743704],"genre_scores_gemma":[0.9862383,0.000041969794,0.010639908,0.00019440548,0.000022359642,0.00019191769,0.0000065017484,0.000031195254,0.0026334596],"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.998139,0.0006944194,0.00022697655,0.00043518233,0.00026143176,0.00024297697],"domain_scores_gemma":[0.99832386,0.0005018398,0.00014179041,0.00082430436,0.00010823851,0.00009997531],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0013163167,0.00015492523,0.00013588037,0.00002500941,0.00045251765,0.000085004285,0.0008484316,0.00012797932,0.00020424987],"category_scores_gemma":[0.0008162267,0.00012470447,0.00007232424,0.00043806553,0.00029450553,0.00020513525,0.00042740378,0.0003635465,0.00009310454],"study_design_candidate":"design_other","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":[0.00016705203,0.0024428125,0.08680617,0.00006336365,0.00019962642,0.000014834535,0.04469244,0.0014864228,0.08673716,0.021877598,0.022907648,0.73260486],"study_design_scores_gemma":[0.006103246,0.00003703093,0.06845555,0.00033241103,0.00030316794,0.000055066044,0.019022882,0.068858504,0.45529488,0.027787348,0.35153568,0.0022142583],"about_ca_topic_score_codex":0.00057836995,"about_ca_topic_score_gemma":0.0003574982,"teacher_disagreement_score":0.7303906,"about_ca_system_score_codex":0.00006980016,"about_ca_system_score_gemma":0.000019677824,"threshold_uncertainty_score":0.5085301},"labels":[],"label_agreement":null},{"id":"W4288047865","doi":"10.1109/icuas54217.2022.9836217","title":"In-Flight Validation of Propeller Slipstream Model","year":2022,"lang":"en","type":"article","venue":"2022 International Conference on Unmanned Aircraft Systems (ICUAS)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Propeller; Computer science; Marine engineering; Aeronautics; Aerospace engineering; Engineering","score_opus":0.029336230192139462,"score_gpt":0.26008477785534856,"score_spread":0.2307485476632091,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4288047865","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":[0.79254156,0.00009347298,0.0100570815,0.005741821,0.0026267841,0.0020389664,0.0003699549,0.00040878978,0.18612154],"genre_scores_gemma":[0.98747057,0.00003003513,0.00031854646,0.00013213973,0.000030320265,0.0003459802,0.000058541613,0.000023142775,0.011590756],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9974634,0.00013083266,0.00055626885,0.00055061816,0.0010054099,0.00029347977],"domain_scores_gemma":[0.99915177,0.00005001651,0.0002957649,0.00039953252,0.000047950492,0.000054982436],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0003952363,0.0002330903,0.00028370193,0.00027240996,0.00014301614,0.000033687822,0.00090120314,0.00008061712,0.00407527],"category_scores_gemma":[0.00006197699,0.00022445123,0.00008309106,0.00040032814,0.00012798111,0.0003680665,0.00051931594,0.00037871493,0.00023486454],"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":[0.00033762085,0.00097073783,0.013140811,0.000044656805,0.00007900176,0.00008369714,0.0008896094,0.7366728,0.08949827,0.14042436,0.015636783,0.0022216483],"study_design_scores_gemma":[0.0024395518,0.000916528,0.0015202706,0.00017387151,0.000026578595,0.00007285925,0.0036251396,0.88692796,0.0418401,0.03566674,0.025598025,0.0011923827],"about_ca_topic_score_codex":0.00017623928,"about_ca_topic_score_gemma":0.000022313945,"teacher_disagreement_score":0.19492896,"about_ca_system_score_codex":0.0005503952,"about_ca_system_score_gemma":0.00004857725,"threshold_uncertainty_score":0.9968351},"labels":[],"label_agreement":null},{"id":"W4288085652","doi":"10.1504/ijsa.2022.124482","title":"Assessing the discursive foundations for emissions abatement in aviation: a post-normal science primer on alternative jet fuels","year":2022,"lang":"en","type":"article","venue":"International Journal of Sustainable Aviation","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"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":"Aviation; Jet fuel; Sustainability; Carbon neutrality; Misrepresentation; Economics; Natural resource economics; Greenhouse gas; Debt; Emissions trading; Business; Political science; Finance; Engineering; Waste management","score_opus":0.018511409699831758,"score_gpt":0.33270987141535674,"score_spread":0.31419846171552496,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4288085652","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":[0.8794033,0.000035954654,0.099485695,0.017162167,0.00086109433,0.00087232806,0.00002050719,0.000025477066,0.0021334775],"genre_scores_gemma":[0.9973397,0.000008999462,0.0016235146,0.00033436535,0.000073737385,0.00010511256,0.000012339869,0.000008207631,0.00049401185],"study_design_codex":"simulation_or_modeling","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.9980836,0.00006800794,0.0003922322,0.00018682494,0.0010211644,0.00024819814],"domain_scores_gemma":[0.9987181,0.00023803495,0.0005402741,0.00012157398,0.00034182792,0.00004023221],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0011295867,0.00010247945,0.000099965015,0.00033712026,0.0006910001,0.00017756161,0.00077647803,0.000020838388,0.00029793457],"category_scores_gemma":[0.0007341479,0.00007580934,0.00007061538,0.0005045339,0.00018627464,0.0019106622,0.00032158074,0.0002600973,0.0000042408374],"study_design_candidate":"theoretical_or_conceptual","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":[0.00091175555,0.0022116364,0.0989835,0.000024190225,0.00023691884,0.0003833969,0.016833937,0.38581854,0.047916763,0.35643563,0.0027197325,0.087524004],"study_design_scores_gemma":[0.005032959,0.0020858643,0.34789893,0.00012168428,0.000081750026,0.00021946148,0.14721893,0.012819517,0.030628972,0.41560176,0.037508275,0.0007818961],"about_ca_topic_score_codex":0.00009425169,"about_ca_topic_score_gemma":0.000007850204,"teacher_disagreement_score":0.372999,"about_ca_system_score_codex":0.002398721,"about_ca_system_score_gemma":0.00020042958,"threshold_uncertainty_score":0.62725717},"labels":[],"label_agreement":null},{"id":"W4288096147","doi":"10.1017/aer.2022.67","title":"An altitude capable rig for studying engine inlet velocity profile effects: Boundary layer generator","year":2022,"lang":"en","type":"article","venue":"The Aeronautical Journal","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"National Research Council Canada","funders":"","keywords":"Boundary layer; Boundary layer suction; Fuselage; Boundary layer control; Boundary layer thickness; Thrust; Parametric statistics; Aerospace engineering; Propulsion; Boundary (topology); Aerodynamics; Vortex generator; Generator (circuit theory); Flow separation; Layer (electronics); Mechanical engineering; Materials science; Engineering; Mechanics; Power (physics); Physics; Vortex; Mathematics; Composite material","score_opus":0.019325552706885213,"score_gpt":0.26318311438141584,"score_spread":0.24385756167453063,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4288096147","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":[0.90715283,0.0003254887,0.08943215,0.0017261492,0.00034240246,0.0006417128,0.000019674902,0.00015402025,0.00020556072],"genre_scores_gemma":[0.9667519,0.000013214703,0.03195004,0.00080792204,0.0001321752,0.00015681228,0.000004335015,0.000023133845,0.00016046956],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9985053,0.00017046806,0.00021096214,0.00023343183,0.0004236419,0.0004562292],"domain_scores_gemma":[0.99933386,0.00017364822,0.00007577201,0.00028430088,0.000010131368,0.00012230247],"candidate_categories":["sts","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00083021703,0.00015075994,0.00017176743,0.000026652833,0.0016369894,0.00007814191,0.0006627433,0.000043338303,0.0011628342],"category_scores_gemma":[0.00008777587,0.000102555045,0.00006873919,0.00017616141,0.0002645818,0.00022352852,0.0003669493,0.00065479707,0.00004678328],"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":[0.0009534816,0.0022587727,0.016708631,0.00007425196,0.0003481767,0.00039634944,0.0029189729,0.05842728,0.41377804,0.008711989,0.046466485,0.4489576],"study_design_scores_gemma":[0.01004836,0.010353481,0.06485613,0.00006633326,0.000456004,0.0022785435,0.0044659027,0.15137309,0.13602145,0.19246277,0.42486346,0.002754478],"about_ca_topic_score_codex":0.00000766826,"about_ca_topic_score_gemma":0.0000068044756,"teacher_disagreement_score":0.4462031,"about_ca_system_score_codex":0.00035250912,"about_ca_system_score_gemma":0.000034520253,"threshold_uncertainty_score":0.99975026},"labels":[],"label_agreement":null},{"id":"W4288256162","doi":"","title":"Helicopter engine particulate matter emissions characterization","year":2019,"lang":"fr","type":"preprint","venue":"HAL (Le Centre pour la Communication Scientifique Directe)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Safran Electronics (Canada)","funders":"","keywords":"Particulates; Environmental science; Characterization (materials science); Computer science; Materials science; Chemistry; Nanotechnology","score_opus":0.010421222183409972,"score_gpt":0.21193587893926752,"score_spread":0.20151465675585756,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4288256162","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":[0.27494583,0.00040441,0.6397686,0.03995985,0.00057461,0.0009556676,0.00014510842,0.00044991876,0.042796027],"genre_scores_gemma":[0.8383469,0.0012035625,0.059794556,0.00038909225,0.000021505717,0.000111953326,0.00070057076,0.00007980054,0.09935207],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.995012,0.0020916006,0.0006587805,0.0011252814,0.00046728278,0.0006450445],"domain_scores_gemma":[0.9958672,0.0005864377,0.00053045846,0.0024578874,0.00031957505,0.00023845537],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.0018151824,0.0005251732,0.00046318833,0.00011924795,0.00038345507,0.00027892328,0.0012723404,0.00053636293,0.0072265556],"category_scores_gemma":[0.0005022748,0.0005372355,0.00023230884,0.00042936567,0.0005484776,0.00039247092,0.00202277,0.0007990034,0.006727393],"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":[0.00003726614,0.0017580162,0.12480497,0.00041398048,0.00018855836,0.000026503789,0.0066797766,0.0048536127,0.53289926,0.058770955,0.0036680575,0.26589903],"study_design_scores_gemma":[0.001027339,0.0000015003441,0.20256123,0.0037166825,0.00013815245,0.000040244893,0.00013275337,0.07664163,0.45434207,0.010057028,0.24964945,0.001691917],"about_ca_topic_score_codex":0.00037664428,"about_ca_topic_score_gemma":0.00012611064,"teacher_disagreement_score":0.57997406,"about_ca_system_score_codex":0.00029571078,"about_ca_system_score_gemma":0.000066762856,"threshold_uncertainty_score":0.99970794},"labels":[],"label_agreement":null},{"id":"W4289517154","doi":"10.1108/aeat-02-2022-0051","title":"Impact of OEI requirement on parallel hybrid electric turboprop regional aircraft optimization","year":2022,"lang":"en","type":"article","venue":"Aircraft Engineering and Aerospace Technology","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Institut interdisciplinaire d'innovation technologique; Université de Sherbrooke","funders":"","keywords":"Climb; Powertrain; Overshoot (microwave communication); Automotive engineering; Sizing; Propulsion; Engineering; Turboprop; Simulation; Aerospace engineering; Torque; Electrical engineering","score_opus":0.00828420159302002,"score_gpt":0.21955098149734628,"score_spread":0.21126677990432627,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4289517154","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":[0.91576207,0.0004650313,0.08037,0.00175529,0.00007949056,0.0003915923,0.000010904207,0.00103439,0.00013125516],"genre_scores_gemma":[0.97824466,0.00019070049,0.021188466,0.000045188342,0.000010080188,0.00013340863,0.000009382475,0.00003571904,0.00014242156],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.998499,0.000018984734,0.0002512047,0.00047313428,0.0003034299,0.00045427054],"domain_scores_gemma":[0.99933857,0.000044939767,0.00012235934,0.0004216134,0.000012045591,0.00006050284],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00013723495,0.0002693445,0.0002893903,0.00031840167,0.00018252905,0.000009021025,0.00035697268,0.00010682064,0.00018413398],"category_scores_gemma":[0.000073144656,0.00025814743,0.0000884867,0.0008845217,0.00016782638,0.000109812805,0.00035760272,0.00044657683,0.000010778929],"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":[0.000036505728,0.0001150456,0.005167496,0.000007664194,0.000032672397,0.000018466892,0.000024410436,0.95432454,0.033926133,0.0008609575,0.000823206,0.0046629244],"study_design_scores_gemma":[0.0047661224,0.013051717,0.023744643,0.00013380912,0.00012919531,0.00088718755,0.0005110201,0.8828723,0.047394916,0.008455744,0.0151236495,0.0029296977],"about_ca_topic_score_codex":0.000040267867,"about_ca_topic_score_gemma":0.0000013137454,"teacher_disagreement_score":0.071452215,"about_ca_system_score_codex":0.00035733622,"about_ca_system_score_gemma":0.000017929813,"threshold_uncertainty_score":0.99998707},"labels":[],"label_agreement":null},{"id":"W4292168494","doi":"10.1017/aer.2022.28","title":"Design of a sub-scale fan for a boundary layer ingestion test with by-pass flow","year":2022,"lang":"en","type":"article","venue":"The Aeronautical Journal","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"National Research Council Canada","funders":"","keywords":"Transonic; Computational fluid dynamics; Scale model; Nozzle; Boundary layer; Scale (ratio); Marine engineering; Full scale; Distortion (music); Mechanical fan; Engineering; Aerospace engineering; Simulation; Mechanical engineering; Aerodynamics; Structural engineering; Physics","score_opus":0.016036675257542578,"score_gpt":0.22793611785120707,"score_spread":0.2118994425936645,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4292168494","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":[0.16806361,0.00013657828,0.82744485,0.0037392941,0.000053964246,0.000353085,0.00002106576,0.000055943226,0.00013159814],"genre_scores_gemma":[0.9675662,0.000018389675,0.03200626,0.00020971043,0.000017296035,0.000053517997,0.000002089882,0.000014201497,0.00011232475],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9990009,0.000081059276,0.00017057174,0.00013759697,0.000353513,0.00025635478],"domain_scores_gemma":[0.9993644,0.0003176127,0.00009492728,0.0001573683,0.000009614109,0.000056097517],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005019214,0.00009916455,0.00012463065,0.000019124416,0.0005368904,0.000023928951,0.00035891793,0.00003104655,0.0003164838],"category_scores_gemma":[0.00006334033,0.00006106343,0.000038436287,0.00016318102,0.00042124942,0.000107223954,0.00016739409,0.00036939798,0.000008603694],"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":[0.0023711617,0.001195033,0.0091067245,0.000018285653,0.00009287955,0.000058666636,0.0009040723,0.080324695,0.6846869,0.0007013376,0.033077992,0.18746229],"study_design_scores_gemma":[0.010479154,0.024589695,0.032205004,0.00015447508,0.00055319077,0.005511541,0.0048423004,0.19501804,0.35248253,0.28507286,0.08691356,0.002177645],"about_ca_topic_score_codex":0.0000030524209,"about_ca_topic_score_gemma":0.0000035579246,"teacher_disagreement_score":0.7995026,"about_ca_system_score_codex":0.00015545211,"about_ca_system_score_gemma":0.000026290876,"threshold_uncertainty_score":0.41293812},"labels":[],"label_agreement":null},{"id":"W4295280091","doi":"10.1016/j.toxlet.2022.07.193","title":"SOC-V-04 A high throughput screening concept for read-across of a large inventory of related structures","year":2022,"lang":"en","type":"article","venue":"Toxicology Letters","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Health Canada","funders":"","keywords":"Cone calorimeter; Carbon nanotube; Materials science; Composite material; Epoxy; Combustion; Carbon fibers; Particle (ecology); Composite number; Polymer; Chemical engineering; Chemistry; Char; Organic chemistry","score_opus":0.015938993408811802,"score_gpt":0.2724642631854239,"score_spread":0.25652526977661205,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4295280091","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":[0.98264265,0.000076740704,0.014544863,0.0018919077,0.00015927615,0.00036740804,0.00012476322,0.00009410658,0.000098264034],"genre_scores_gemma":[0.9874125,0.0000027537,0.010706399,0.0016516068,0.000008364691,0.00008073595,0.000019782805,0.000015757472,0.000102065635],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9988364,0.000068335474,0.0002886259,0.00028224598,0.00016969597,0.00035472354],"domain_scores_gemma":[0.9993596,0.000110183755,0.00025200102,0.00024829851,0.0000052336495,0.000024673285],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00022042493,0.000120772886,0.00026430583,0.000035568755,0.00021113853,0.0000022179408,0.00035882238,0.00009316806,0.0010945278],"category_scores_gemma":[0.00006569251,0.000121249774,0.00008489793,0.00020105732,0.000802309,0.00008419189,0.00043798817,0.00022256153,0.0000022275055],"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":[0.00023348452,0.00018241197,0.024244197,0.00003234783,0.00012656489,0.00003319463,0.0038415908,0.019962715,0.9211565,0.012054549,0.01155857,0.0065738447],"study_design_scores_gemma":[0.015789073,0.0050328323,0.14519222,0.000056044577,0.00022231926,0.00015291903,0.01514265,0.0031900888,0.6221938,0.11068553,0.0802857,0.002056847],"about_ca_topic_score_codex":0.00005139376,"about_ca_topic_score_gemma":0.000016367414,"teacher_disagreement_score":0.29896274,"about_ca_system_score_codex":0.00010440692,"about_ca_system_score_gemma":0.00000755084,"threshold_uncertainty_score":0.9998186},"labels":[],"label_agreement":null},{"id":"W4295548916","doi":"10.3390/applmech3030064","title":"Aerodynamic Shape Optimization of an Aircraft Propulsor Air Intake with Boundary Layer Ingestion","year":2022,"lang":"en","type":"article","venue":"Applied Mechanics","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":7,"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; Carleton University","funders":"","keywords":"Nacelle; Propulsor; Wake; Propulsion; Aerodynamics; Engineering; Automotive engineering; Marine engineering; Environmental science; Computer science; Aerospace engineering","score_opus":0.008610074621552753,"score_gpt":0.20460610283407663,"score_spread":0.19599602821252388,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4295548916","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":[0.58502734,0.000017650837,0.41235307,0.0001664412,0.00008204963,0.0007848271,0.000017788523,0.0004431285,0.0011077218],"genre_scores_gemma":[0.9099222,0.000007645324,0.08962209,0.00014299588,0.0000061768683,0.00017563804,0.00005258798,0.000028297405,0.000042409803],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99889207,0.00002579987,0.00017549266,0.00034655537,0.0003529956,0.00020707457],"domain_scores_gemma":[0.9994786,0.0000136144545,0.00013757,0.00032164535,0.000007932746,0.000040647166],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017705651,0.00014351337,0.00014525707,0.000055977904,0.00024547536,0.000008338834,0.000293817,0.00006148916,0.0006923781],"category_scores_gemma":[0.000008842335,0.00013258636,0.00002000819,0.0004081172,0.00007452774,0.00016674638,0.00028015822,0.00022099853,0.000013102032],"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":[0.00025181234,0.00024802273,0.000099149685,0.000014520102,0.000012697233,0.000009503549,0.00021278714,0.8473008,0.061576147,0.01184413,0.000048475504,0.07838195],"study_design_scores_gemma":[0.0016838926,0.0020478654,0.00069740415,0.000018403238,0.00007526616,0.00007049471,0.002669399,0.88856465,0.04797716,0.05101051,0.004261912,0.000923071],"about_ca_topic_score_codex":0.000016016575,"about_ca_topic_score_gemma":0.000043827502,"teacher_disagreement_score":0.32489485,"about_ca_system_score_codex":0.00019947528,"about_ca_system_score_gemma":0.000021450087,"threshold_uncertainty_score":0.75810546},"labels":[],"label_agreement":null},{"id":"W4297970645","doi":"","title":"Aero-propulsive and structural methods for pre-design of distributed propulsion aircraft","year":2018,"lang":"en","type":"preprint","venue":"HAL (Le Centre pour la Communication Scientifique Directe)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Safran Electronics (Canada)","funders":"","keywords":"Propulsion; Aerospace engineering; Computer science; Aeronautics; Engineering; Automotive engineering; Marine engineering","score_opus":0.018073495779510985,"score_gpt":0.2875011112659765,"score_spread":0.2694276154864655,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4297970645","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":[0.03865011,0.00035335467,0.95686,0.0014141751,0.00013964958,0.0014865176,0.00013796093,0.00022828644,0.00072996813],"genre_scores_gemma":[0.3049279,0.00016840827,0.6936653,0.00001577992,0.000008431137,0.00016732064,0.00019882199,0.000032028696,0.00081601104],"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99572146,0.0023308692,0.00049622194,0.0008470999,0.00025805278,0.00034627743],"domain_scores_gemma":[0.9963586,0.0011159923,0.00059832,0.0013766141,0.00043972387,0.00011079453],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0028890707,0.00034626308,0.0004405962,0.000082819635,0.0002908808,0.00008975682,0.0009899093,0.00036383572,0.00011919095],"category_scores_gemma":[0.0024169958,0.00031374107,0.00012706447,0.00025431724,0.0010410026,0.0001576252,0.002060736,0.0003718428,0.0000060869056],"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":[0.0003452356,0.0005134633,0.008128866,0.0007637736,0.0002052295,0.0000036897748,0.005996848,0.0017370777,0.19134307,0.014813721,0.0029840108,0.77316505],"study_design_scores_gemma":[0.0009940726,0.000010280834,0.010458953,0.0010941854,0.00011763927,0.000014065464,0.00015050852,0.11894292,0.6137548,0.24940094,0.0041751387,0.0008864603],"about_ca_topic_score_codex":0.0002651688,"about_ca_topic_score_gemma":0.00009176307,"teacher_disagreement_score":0.77227855,"about_ca_system_score_codex":0.00014453399,"about_ca_system_score_gemma":0.00005106506,"threshold_uncertainty_score":0.99993145},"labels":[],"label_agreement":null},{"id":"W4303628770","doi":"10.3390/designs6050091","title":"Improved Local Scale Generic Cycle Model for Aerothermodynamic Simulations of Gas Turbine Engines for Propulsion","year":2022,"lang":"en","type":"article","venue":"Designs","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":9,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure","funders":"","keywords":"Thrust specific fuel consumption; Propulsion; Gas compressor; Turbine; Combustor; Turbofan; Thrust; Turbomachinery; Environmental science; Fuel efficiency; Aerospace engineering; Engineering; Combustion; Chemistry","score_opus":0.02223468354710386,"score_gpt":0.24547577748101732,"score_spread":0.22324109393391345,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4303628770","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":[0.14964274,0.0000238168,0.84904,0.000110239685,0.000032343432,0.00092364993,0.000110408146,0.00009089987,0.00002591571],"genre_scores_gemma":[0.86874753,0.0000021752483,0.13033135,0.000036273384,0.000007694155,0.00050510064,0.00002825845,0.00002197952,0.00031963774],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992544,0.000013520311,0.00016448478,0.00023491141,0.00012315687,0.00020953099],"domain_scores_gemma":[0.99962574,0.00006475828,0.00007111763,0.00019959528,0.000011518679,0.00002727829],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000094111885,0.000105136096,0.00013089919,0.0000406131,0.00020644093,0.000004179005,0.00017196476,0.00004391181,0.00006822256],"category_scores_gemma":[0.000024395851,0.000097653334,0.00006972934,0.00016862099,0.00010716718,0.000084427484,0.000103998726,0.000062405634,8.842755e-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":[0.000040330906,0.00006039715,0.000036297908,0.000008383733,0.0000031827476,1.3098291e-7,0.000055431567,0.6472366,0.33299664,0.000088563604,0.00007624169,0.019397834],"study_design_scores_gemma":[0.00043754835,0.00025298345,0.000048822632,0.0000018339562,0.000012384482,0.000001399439,0.000057939327,0.96522325,0.020285051,0.013350229,0.00020640274,0.00012216016],"about_ca_topic_score_codex":0.000017422168,"about_ca_topic_score_gemma":0.0000227865,"teacher_disagreement_score":0.71910477,"about_ca_system_score_codex":0.00013712602,"about_ca_system_score_gemma":0.000012307762,"threshold_uncertainty_score":0.39821875},"labels":[],"label_agreement":null},{"id":"W4306362656","doi":"10.1016/j.jweia.2022.105208","title":"High-fidelity CFD modeling of pollutant dispersion from aircraft auxiliary power units (APUs) at a realistic airport and the effects on airport air quality","year":2022,"lang":"en","type":"article","venue":"Journal of Wind Engineering and Industrial Aerodynamics","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":9,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure; Université du Québec à Montréal","funders":"","keywords":"Computational fluid dynamics; Aerospace engineering; Auxiliary power unit; Environmental science; Fidelity; Dispersion (optics); Engineering; Power (physics); Marine engineering; Physics; Telecommunications","score_opus":0.014423267601110923,"score_gpt":0.20891448444662142,"score_spread":0.1944912168455105,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4306362656","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":[0.9961996,0.00014887463,0.0023491348,0.0005044272,0.00049481884,0.00017486996,0.00006904738,0.000031015305,0.000028196022],"genre_scores_gemma":[0.99918085,0.00012577785,0.0005041108,0.000059994418,0.00007479883,0.0000027085903,0.000007326655,0.000017143904,0.000027265916],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.998376,0.000115082286,0.0005909763,0.00022031798,0.00048575885,0.00021186292],"domain_scores_gemma":[0.99890226,0.0003923027,0.00034716883,0.0002377601,0.00002145755,0.00009902842],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0010356251,0.00020151367,0.0004472222,0.00007537081,0.00021636319,0.000011613799,0.00023933218,0.00013123527,0.000021016118],"category_scores_gemma":[0.0006334081,0.00014523935,0.00007975628,0.00025799515,0.0001584539,0.00014361834,0.00035465288,0.000760058,4.2526352e-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":[0.0009047202,0.000059269674,0.0047344,0.000015674792,0.00008627217,0.000048447306,0.0002675972,0.9820585,0.00689792,0.0004979039,0.0001356347,0.004293632],"study_design_scores_gemma":[0.018043246,0.0035921203,0.09153207,0.00070072873,0.0005810938,0.00039744607,0.0024579423,0.87007767,0.0019759953,0.0076104207,0.0014936916,0.0015375693],"about_ca_topic_score_codex":0.00048520387,"about_ca_topic_score_gemma":0.000014940318,"teacher_disagreement_score":0.11198085,"about_ca_system_score_codex":0.00030783194,"about_ca_system_score_gemma":0.00003053872,"threshold_uncertainty_score":0.5922689},"labels":[],"label_agreement":null},{"id":"W4307609291","doi":"","title":"A common framework for the design optimization of fixed-wing, multicopter and VTOL UAV configurations","year":2022,"lang":"en","type":"preprint","venue":"HAL (Le Centre pour la Communication Scientifique Directe)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Concordia University","funders":"","keywords":"Fixed wing; Computer science; Aerospace engineering; Wing; Control theory (sociology); Engineering; Artificial intelligence; Control (management)","score_opus":0.02140661193629839,"score_gpt":0.25051080384256275,"score_spread":0.22910419190626435,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4307609291","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":[0.0028545358,0.00045235676,0.98769486,0.0043235538,0.000090573856,0.0011321246,0.000060677554,0.00014485349,0.003246437],"genre_scores_gemma":[0.44617406,0.00047925083,0.5520211,0.000078578276,0.000004713623,0.0003929249,0.00009174374,0.000025596173,0.0007320577],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99744743,0.0012511122,0.0003655737,0.0004683462,0.00026134963,0.00020619377],"domain_scores_gemma":[0.9941013,0.004025555,0.00042789348,0.0012397724,0.00015413032,0.000051382714],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0019455152,0.0002116694,0.00024907757,0.000061635816,0.0005506978,0.00011173464,0.00089113234,0.0001986868,0.0005926077],"category_scores_gemma":[0.001575212,0.00018388896,0.00010123625,0.00021723675,0.0005359158,0.000104545135,0.0012837687,0.00047210886,0.000003747268],"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":[0.00008704546,0.0008971604,0.006601825,0.00023402611,0.00020369986,0.000003231156,0.01505422,0.5567275,0.0060111713,0.26592222,0.0019369805,0.14632088],"study_design_scores_gemma":[0.0006943715,0.0000036337929,0.0032267836,0.0006411017,0.00014551675,0.0000066621715,0.00090600253,0.8474047,0.04041505,0.09469848,0.011211682,0.00064598286],"about_ca_topic_score_codex":0.0003067183,"about_ca_topic_score_gemma":0.00013314624,"teacher_disagreement_score":0.4433195,"about_ca_system_score_codex":0.00009304507,"about_ca_system_score_gemma":0.000038874063,"threshold_uncertainty_score":0.74987745},"labels":[],"label_agreement":null},{"id":"W4307988338","doi":"10.3390/jrfm15110505","title":"Towards True Climate Neutrality for Global Aviation: A Negative Emissions Fund for Airlines","year":2022,"lang":"en","type":"article","venue":"Journal of risk and financial management","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":9,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Aviation; Carbon neutrality; Greenhouse gas; Business; Environmental economics; Environmental science; Emissions trading; Natural resource economics; Finance; Economics; Engineering","score_opus":0.01808755392952957,"score_gpt":0.27151008784049796,"score_spread":0.25342253391096836,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4307988338","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":[0.075967535,0.0002673303,0.91924113,0.0014113429,0.000551172,0.00092373614,0.00034254513,0.000039167382,0.0012560477],"genre_scores_gemma":[0.9551621,0.0005836267,0.043815114,0.00014169577,0.00007227756,0.00009064363,0.000002632563,0.0000054800053,0.00012640031],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9992595,0.000022380504,0.00024696588,0.00013731868,0.00015837741,0.000175463],"domain_scores_gemma":[0.99957436,0.00004850991,0.00024125747,0.0000775554,0.000015152206,0.00004314794],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00035516595,0.00008726251,0.00015282787,0.000029456081,0.00045559026,0.000016034337,0.00015520063,0.00002548163,0.000031164436],"category_scores_gemma":[0.00008972013,0.000072849034,0.00009919287,0.00016142616,0.000059348116,0.00012308916,0.00020821723,0.00009304429,5.664962e-7],"study_design_candidate":"design_other","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":[0.00068680133,0.00015986449,0.019221526,0.000045484987,0.000021097012,0.000016706781,0.0003416232,0.004016841,0.000022165108,0.028644225,0.0063001104,0.94052356],"study_design_scores_gemma":[0.0021526366,0.00095950154,0.16856389,0.000016865244,0.00013022083,0.00001776505,0.0018954661,0.0006987187,0.000097053635,0.38763496,0.43761623,0.00021669228],"about_ca_topic_score_codex":0.000009343411,"about_ca_topic_score_gemma":0.000014035153,"teacher_disagreement_score":0.94030684,"about_ca_system_score_codex":0.00013969767,"about_ca_system_score_gemma":0.000009166461,"threshold_uncertainty_score":0.3504078},"labels":[],"label_agreement":null},{"id":"W4311974987","doi":"10.3390/aerospace9120806","title":"Influence of Ventilation Flow Rate and Gap Distance on the Radiative Heat Transfer in Aircraft Avionics Bays","year":2022,"lang":"en","type":"article","venue":"Aerospace","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":6,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Siemens (Canada); Concordia University","funders":"Natural Sciences and Engineering Research Council of Canada; Bombardier","keywords":"Avionics; Heat transfer; Radiative transfer; Computational fluid dynamics; Thermal; Aerospace engineering; Thermal radiation; Thermal mass; Environmental science; Mechanical engineering; Computer science; Automotive engineering; Engineering; Meteorology; Mechanics; Physics","score_opus":0.010313729070454572,"score_gpt":0.21363906181822268,"score_spread":0.2033253327477681,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4311974987","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":[0.99403083,0.000094199866,0.0041292463,0.0012198574,0.000019107027,0.00023412413,0.000012971414,0.000032544332,0.00022711736],"genre_scores_gemma":[0.99928874,0.00008538348,0.00027632187,0.00017371315,0.0000015800784,0.00005333718,0.0000016584185,0.000006684047,0.00011256973],"study_design_codex":"simulation_or_modeling","study_design_gemma":"observational","domain_scores_codex":[0.9993196,0.000071198854,0.00010927962,0.00019479635,0.00016509718,0.00014004241],"domain_scores_gemma":[0.999659,0.00012224584,0.000016610258,0.00018201201,0.000003012256,0.000017138898],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002102352,0.00008459671,0.00009420778,0.000018708903,0.00014553011,0.0000060717634,0.00015119607,0.000024495595,0.000093171584],"category_scores_gemma":[0.000039889703,0.000067181834,0.000019819723,0.0002959835,0.00020928991,0.00012229689,0.00008275667,0.00018512353,0.000007826736],"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":[0.000106097235,0.000076942146,0.053190593,0.0000063228804,0.000004436257,0.000007971404,0.001563861,0.9004073,0.03839185,0.0044915956,0.00019722067,0.0015558129],"study_design_scores_gemma":[0.0013388839,0.0006708528,0.8331498,0.000066078406,0.000016833512,0.000007068473,0.0019740802,0.039058343,0.10215073,0.014531784,0.0064945742,0.0005410134],"about_ca_topic_score_codex":0.000048650054,"about_ca_topic_score_gemma":0.00010218766,"teacher_disagreement_score":0.8613489,"about_ca_system_score_codex":0.00012379988,"about_ca_system_score_gemma":0.0000054182588,"threshold_uncertainty_score":0.27395958},"labels":[],"label_agreement":null},{"id":"W4312211170","doi":"10.1016/j.xpro.2022.101952","title":"Protocol to calculate aircraft emissions for international air routes in South America","year":2022,"lang":"en","type":"article","venue":"STAR Protocols","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":8,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"Fundamental Research Funds for the Central Universities; National Natural Science Foundation of China","keywords":"Descent (aeronautics); Cruise; Protocol (science); Kyoto Protocol; Climb; Aviation; Pollutant; Air pollution; Environmental science; International airport; Air pollutants; Montreal Protocol; Aeronautics; Computer science; Transport engineering; Engineering; Meteorology; Greenhouse gas; Ozone layer; Geography; Aerospace engineering; Ozone; Chemistry; Geology","score_opus":0.02581337416803776,"score_gpt":0.32613064258381297,"score_spread":0.3003172684157752,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4312211170","genre_codex":"protocol","genre_gemma":"protocol","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"protocol","genre_consensus":"protocol","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0022399602,2.6686072e-7,0.025400368,0.0016457448,0.000043800806,0.96885616,0.00011069431,0.0002612215,0.0014418156],"genre_scores_gemma":[0.016937988,1.8665169e-8,0.034409612,0.0005030123,0.000018674673,0.947109,0.000007174822,0.000020282434,0.0009942406],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.99862605,0.00004292131,0.0002609462,0.00041007026,0.00032474415,0.0003352671],"domain_scores_gemma":[0.9994998,0.00003681351,0.0000892618,0.00028352163,0.000012336052,0.000078277044],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00018568255,0.00014692963,0.00015051536,0.00008957128,0.00021379752,0.000016560034,0.00058237213,0.00003563419,0.0015272263],"category_scores_gemma":[0.00019048213,0.000134328,0.000060708877,0.00038876326,0.00007908706,0.00012641931,0.000693513,0.00019292893,0.000078997095],"study_design_candidate":"not_applicable","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":[0.00443992,0.003167589,0.19836348,0.00022938619,0.000096235926,0.0001786616,0.011665667,0.22961695,0.118133,0.0030544412,0.084266625,0.34678802],"study_design_scores_gemma":[0.0013267812,0.0005756176,0.0042855362,0.000027423655,0.0000014856683,0.0000020263603,0.00060793816,0.0019081803,0.0047047823,0.0069795707,0.97929287,0.00028778982],"about_ca_topic_score_codex":0.00003305788,"about_ca_topic_score_gemma":0.000012918259,"teacher_disagreement_score":0.89502627,"about_ca_system_score_codex":0.00035627122,"about_ca_system_score_gemma":0.000027318934,"threshold_uncertainty_score":0.99938554},"labels":[],"label_agreement":null},{"id":"W4312612419","doi":"10.1109/access.2022.3213068","title":"Model-Based Analysis of Lithium-Ion Battery Technology Predictions in Light-Sport Aircraft","year":2022,"lang":"en","type":"article","venue":"IEEE Access","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"National Research Council Canada; Toronto Metropolitan University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Lithium (medication); Ion; Computer science; Battery (electricity); Aeronautics; Aerospace engineering; Automotive engineering; Environmental science; Physics; Engineering; Thermodynamics","score_opus":0.01856643824873884,"score_gpt":0.2686210470645881,"score_spread":0.2500546088158493,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4312612419","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":[0.89594096,0.000032686246,0.100827396,0.0010405171,0.0001164776,0.00020849844,0.00003237961,0.00027154284,0.001529532],"genre_scores_gemma":[0.99819094,0.000009012298,0.0012383761,0.0001583667,0.0000046079485,0.00019941857,0.000011497778,0.000011220124,0.00017653183],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9987745,0.000019145527,0.0003020655,0.0003729076,0.0002908865,0.00024048793],"domain_scores_gemma":[0.99931425,0.000024124605,0.00012958795,0.0004953937,0.000008349307,0.00002830695],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015578479,0.00012197169,0.00026474748,0.000844972,0.00013301507,0.000009468654,0.00078614976,0.000091848575,0.00045285354],"category_scores_gemma":[0.000015592715,0.00012384415,0.000088383524,0.0039248955,0.00017559045,0.00026442637,0.00034399348,0.0002795032,0.0000078563535],"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":[0.0000133415715,0.00013021166,0.2844253,0.0000028677903,0.000026548669,0.000010946976,0.000029764362,0.7032074,0.010727928,0.00007128756,0.00030602975,0.0010484004],"study_design_scores_gemma":[0.0006706498,0.00019603035,0.0846559,0.000013542464,0.00028842042,0.0000049336163,0.00028788982,0.796517,0.10324896,0.009187926,0.0044486998,0.00048002918],"about_ca_topic_score_codex":0.00011272464,"about_ca_topic_score_gemma":0.00018691973,"teacher_disagreement_score":0.19976938,"about_ca_system_score_codex":0.00021908934,"about_ca_system_score_gemma":0.000019169085,"threshold_uncertainty_score":0.50502175},"labels":[],"label_agreement":null},{"id":"W4312884652","doi":"10.1115/gt2022-83031","title":"Performance Improvement of Heat Exchangers Used in a Hybrid Electric Aircraft","year":2022,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"National Research Council Canada","funders":"","keywords":"Radiator (engine cooling); Coolant; Heat exchanger; Mechanical engineering; Nuclear engineering; Fin; Heat transfer; Thermal resistance; Active cooling; Automotive engineering; Water cooling; Materials science; Engineering; Mechanics; Physics","score_opus":0.009490765741445679,"score_gpt":0.20584024208676618,"score_spread":0.19634947634532052,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4312884652","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":[0.9954034,0.000031970012,0.001064534,0.00017398415,0.000036105193,0.0002494918,0.0000020977905,0.000086698215,0.0029517105],"genre_scores_gemma":[0.9982773,0.000036712558,0.0008316376,0.00013423462,0.000002377133,0.0001185038,0.0000015719904,0.000007744652,0.0005898977],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99908894,0.000013762363,0.00016724173,0.00021503298,0.0002598691,0.00025517482],"domain_scores_gemma":[0.99972194,0.000019106934,0.000031942058,0.00020264724,0.0000016693356,0.000022672326],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00015287967,0.000088707595,0.00011953112,0.0000926565,0.000073430376,0.0000024584222,0.00025629354,0.000014009998,0.0020695014],"category_scores_gemma":[0.000008029335,0.00008247783,0.000029422104,0.00050740957,0.000057241254,0.00011154608,0.0003060185,0.00013781522,0.000026112348],"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":[0.000056692163,0.00029861252,0.15952396,0.000018066114,0.0000071755444,0.000020778887,0.00020601717,0.019615931,0.6654916,0.00006198218,0.00110981,0.15358943],"study_design_scores_gemma":[0.0015281732,0.0021702559,0.050515655,0.000008456334,0.000008577497,0.000022464748,0.00095690717,0.045589816,0.88758963,0.0012231986,0.00983704,0.000549843],"about_ca_topic_score_codex":0.00019421973,"about_ca_topic_score_gemma":0.000027521774,"teacher_disagreement_score":0.22209805,"about_ca_system_score_codex":0.0002836159,"about_ca_system_score_gemma":0.000007645685,"threshold_uncertainty_score":0.9988427},"labels":[],"label_agreement":null},{"id":"W4317254315","doi":"10.1016/j.paerosci.2022.100878","title":"Strategies towards a more sustainable aviation: A systematic review","year":2023,"lang":"en","type":"review","venue":"Progress in Aerospace Sciences","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":191,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Victoria","funders":"Fundação para a Ciência e a Tecnologia; Natural Sciences and Engineering Research Council of Canada; Canada Research Chairs","keywords":"Aviation; Renewable energy; Fossil fuel; Propulsion; Greenhouse gas; Environmental economics; Engineering; Production (economics); Business; Waste management; Aerospace engineering; Economics","score_opus":0.05099422530307525,"score_gpt":0.37587382305916645,"score_spread":0.3248795977560912,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4317254315","genre_codex":"review","genre_gemma":"review","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"review","genre_consensus":"review","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[8.251371e-7,0.9933724,0.00010064954,0.00045313273,0.00008837211,0.0039015082,0.0000047874582,0.00047378507,0.001604556],"genre_scores_gemma":[0.000022974975,0.9935714,0.001466007,0.000045392895,0.000013611593,0.002832004,0.0000057662473,0.000034761997,0.0020080938],"study_design_codex":"systematic_review","study_design_gemma":"systematic_review","domain_scores_codex":[0.9961789,0.00022198429,0.000842913,0.000933182,0.00094963535,0.00087334577],"domain_scores_gemma":[0.99844396,0.00016820861,0.0006694181,0.00062059733,0.000021356544,0.0000764375],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0019292098,0.00052579754,0.0020607933,0.00022221473,0.00029627595,0.00031197793,0.0017995677,0.00023807857,0.00009040802],"category_scores_gemma":[0.00048595955,0.0003490688,0.00025429085,0.0045093643,0.0018837593,0.00079948985,0.00082950684,0.0004048593,0.00045344548],"study_design_candidate":"systematic_review","study_design_consensus":"systematic_review","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[2.850012e-7,0.000035287507,0.00006673445,0.9140382,0.000017619477,0.00011496105,0.00010380421,0.000008221636,1.3372833e-8,0.0034715568,0.00051618787,0.08162716],"study_design_scores_gemma":[0.0001024899,0.00015829531,0.000014424631,0.8947058,0.00057538797,0.00006381934,0.004958913,0.00006284412,9.003482e-7,0.0058462634,0.092355266,0.0011555954],"about_ca_topic_score_codex":0.000051995983,"about_ca_topic_score_gemma":0.00004161056,"teacher_disagreement_score":0.091839075,"about_ca_system_score_codex":0.00051140354,"about_ca_system_score_gemma":0.00028925223,"threshold_uncertainty_score":0.9998961},"labels":[],"label_agreement":null},{"id":"W4317568620","doi":"10.2514/6.2023-0213","title":"A Conceptual Sizing Tool for Regional and Commuter Aircraft with Hybrid-Electric Propulsion","year":2023,"lang":"en","type":"article","venue":"AIAA SCITECH 2023 Forum","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Concordia University","funders":"","keywords":"Sizing; Propulsion; Electrically powered spacecraft propulsion; Aviation; Conceptual design; Automotive engineering; Systems engineering; Engineering; Carbon footprint; Fuel efficiency; Computer science; Aerospace engineering; Greenhouse gas; Mechanical engineering","score_opus":0.017223022838202543,"score_gpt":0.23788509490446702,"score_spread":0.22066207206626448,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4317568620","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":[0.9554659,0.00019561507,0.033196315,0.008004891,0.0000995264,0.001373113,0.000030981293,0.0011608746,0.00047279964],"genre_scores_gemma":[0.9851654,0.000075354714,0.011333978,0.0006621141,0.000024384368,0.00026387,0.000026915895,0.00003386229,0.0024140931],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9985518,0.000016829272,0.00016347693,0.00043255556,0.00027270644,0.00056264614],"domain_scores_gemma":[0.9994451,0.00014970393,0.0000639041,0.0002700495,0.000012641174,0.000058609756],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017059727,0.00018348022,0.0001701287,0.00010443093,0.00034796356,0.000038259903,0.00025653405,0.000076859076,0.000052126295],"category_scores_gemma":[0.0000637409,0.00014271786,0.000044155826,0.0006943531,0.0003986675,0.000312352,0.00028173928,0.00016625154,0.00015069335],"study_design_candidate":"not_applicable","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":[0.00053462904,0.00018487472,0.114532374,0.000074960604,0.00009855423,0.00019357105,0.00053909747,0.0009832208,0.18969642,0.009974873,0.24119684,0.44199058],"study_design_scores_gemma":[0.005642119,0.0041476735,0.046836015,0.00028739282,0.000091086564,0.00039400626,0.0033850607,0.025401779,0.09745536,0.12873837,0.6850526,0.0025685362],"about_ca_topic_score_codex":0.000026156,"about_ca_topic_score_gemma":0.000034430752,"teacher_disagreement_score":0.44385573,"about_ca_system_score_codex":0.00007620385,"about_ca_system_score_gemma":0.000012478096,"threshold_uncertainty_score":0.5819866},"labels":[],"label_agreement":null},{"id":"W4317583742","doi":"10.2514/6.2023-1361","title":"Systems Integration Considerations for Hybrid-electric Commuter Aircraft: Case Study for the DO-228","year":2023,"lang":"en","type":"article","venue":"AIAA SCITECH 2023 Forum","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Concordia University","funders":"","keywords":"Sizing; Maintainability; Systems engineering; Electrification; Avionics; Aerospace; Engineering; System integration; Retrofitting; Conceptual design; Propulsion; Workflow; Hybrid system; Automotive engineering; Computer science; Aerospace engineering; Reliability engineering; Electricity; Mechanical engineering","score_opus":0.037480322633598094,"score_gpt":0.28888308443244837,"score_spread":0.2514027617988503,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4317583742","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":[0.30332008,0.0003204608,0.66665757,0.012543778,0.0014150743,0.013044898,0.0002776378,0.0019592317,0.00046126524],"genre_scores_gemma":[0.99331886,0.000024600211,0.001843401,0.00022061358,0.000042071584,0.0029295871,0.00001675639,0.000031557764,0.0015725561],"study_design_codex":"not_applicable","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9984902,0.000045626064,0.00031742614,0.00040784094,0.00022705148,0.0005118646],"domain_scores_gemma":[0.9978882,0.0013720073,0.00009890834,0.00055522553,0.000037972375,0.000047671823],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006122714,0.00019974732,0.0001956377,0.00013601071,0.0011451168,0.00017224344,0.00030434455,0.00007507639,0.000047027195],"category_scores_gemma":[0.00038149735,0.00014068047,0.00010316908,0.0007670325,0.00013502789,0.00028199513,0.00019751646,0.00017420224,0.00020215534],"study_design_candidate":"not_applicable","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":[0.000106903935,0.0006016455,0.01097682,0.00006723144,0.00027739082,0.0008067139,0.0015921036,0.020519175,0.019800832,0.012194251,0.7916137,0.14144325],"study_design_scores_gemma":[0.004986,0.0038261905,0.0021576444,0.00008982949,0.00037243668,0.0023383426,0.073590495,0.58051366,0.020918729,0.1875742,0.12175185,0.0018806509],"about_ca_topic_score_codex":0.00028092653,"about_ca_topic_score_gemma":0.0011252173,"teacher_disagreement_score":0.6899988,"about_ca_system_score_codex":0.00013433912,"about_ca_system_score_gemma":0.000018272014,"threshold_uncertainty_score":0.88074285},"labels":[],"label_agreement":null},{"id":"W4317583802","doi":"10.2514/6.2023-1362","title":"Estimation of Battery Pack Layout and Dimensions for the Conceptual Design of Hybrid-Electric Aircraft","year":2023,"lang":"en","type":"article","venue":"AIAA SCITECH 2023 Forum","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Concordia University","funders":"","keywords":"Battery pack; Battery (electricity); Automotive engineering; Conceptual design; Sizing; Fuselage; Aerospace; Aviation; Engineering; Computer science; Aerospace engineering; Mechanical engineering; Power (physics)","score_opus":0.023294535031601202,"score_gpt":0.2525523368816123,"score_spread":0.22925780185001113,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4317583802","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":[0.30225727,0.00022095793,0.6936201,0.0023412083,0.00011574837,0.0010428034,0.000053489577,0.00024529174,0.0001031204],"genre_scores_gemma":[0.9919974,0.00010034931,0.007381959,0.00008881409,0.0000055144164,0.000082135135,0.0000068471563,0.000013902658,0.00032306073],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9990421,0.00002405319,0.00021900125,0.00022286267,0.00019756061,0.00029440766],"domain_scores_gemma":[0.9988567,0.0007307321,0.00010978243,0.00026060455,0.000012328601,0.00002983102],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002948936,0.000113820985,0.00016387837,0.00008590669,0.00015826536,0.00000794375,0.00022519022,0.000048718382,0.00004078488],"category_scores_gemma":[0.00027002423,0.00008238964,0.000048141268,0.0006231006,0.00047378638,0.0001475808,0.0001939471,0.00008393798,0.00004390617],"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":[0.00013781196,0.000120994446,0.0103925,0.00006837711,0.000107018765,0.000012965949,0.00047984632,0.2803752,0.34535575,0.005183906,0.07663556,0.28113008],"study_design_scores_gemma":[0.00085745635,0.0007751994,0.0063352273,0.00005805634,0.00007292667,0.0000145575195,0.0015534888,0.5973678,0.32717374,0.06268727,0.0027309973,0.00037323445],"about_ca_topic_score_codex":0.000026412037,"about_ca_topic_score_gemma":0.000004986499,"teacher_disagreement_score":0.6897401,"about_ca_system_score_codex":0.00002679887,"about_ca_system_score_gemma":0.000011701284,"threshold_uncertainty_score":0.33597523},"labels":[],"label_agreement":null},{"id":"W4317583844","doi":"10.2514/6.2023-1357","title":"Top Level Aircraft Requirements relaxation for a single-aisle aircraft: a case study on fleet-wide CO2 emissions and economic impacts","year":2023,"lang":"en","type":"article","venue":"AIAA SCITECH 2023 Forum","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Toronto Baptist Seminary and Bible College","funders":"","keywords":"Payload (computing); Range (aeronautics); Fuel efficiency; Aviation; Operating cost; Baseline (sea); Automotive engineering; Commercial aviation; Aviation fuel; Environmental science; Aeronautics; Engineering; Computer science; Aerospace engineering","score_opus":0.05946170800333946,"score_gpt":0.3074507668151185,"score_spread":0.24798905881177905,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4317583844","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":[0.98872036,0.000024549312,0.004215561,0.003214985,0.00027776972,0.001655753,0.00011506788,0.0006919606,0.0010840179],"genre_scores_gemma":[0.9951354,0.000019262648,0.002021252,0.0002673533,0.00002528823,0.0002994921,0.000023711564,0.000048968333,0.0021592616],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.99777937,0.00004037466,0.00042126945,0.00075258844,0.00026891904,0.0007374696],"domain_scores_gemma":[0.99877304,0.00029868315,0.00017587388,0.0005559291,0.000012886219,0.00018360671],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0004951639,0.00030389274,0.0002746189,0.00023099528,0.0006464698,0.00007981407,0.00029371944,0.00016583988,0.000104766885],"category_scores_gemma":[0.0004923113,0.0002799577,0.000085319945,0.0005509597,0.00019791363,0.00050332467,0.00046295582,0.00019503535,0.00047666885],"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":[0.00052014034,0.0018694691,0.4501458,0.00011857559,0.0003103512,0.0033468727,0.0040557673,0.0067694336,0.1916235,0.0011275355,0.19806649,0.14204606],"study_design_scores_gemma":[0.0294621,0.02966038,0.20598124,0.0011622888,0.0007007163,0.0030110856,0.13408536,0.048795152,0.19379504,0.14994633,0.19401169,0.009388619],"about_ca_topic_score_codex":0.0003637987,"about_ca_topic_score_gemma":0.000876907,"teacher_disagreement_score":0.24416459,"about_ca_system_score_codex":0.0004560752,"about_ca_system_score_gemma":0.000029246023,"threshold_uncertainty_score":0.99996525},"labels":[],"label_agreement":null},{"id":"W4317632366","doi":"10.2514/6.2023-2328","title":"Cost estimation of the use of low-carbon fuels in prospective scenarios for air transport","year":2023,"lang":"en","type":"article","venue":"AIAA SCITECH 2023 Forum","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Baptist Seminary and Bible College","funders":"","keywords":"Environmental science; Aviation; Production (economics); Greenhouse gas; Carbon fibers; Capital cost; Revenue; Environmental economics; Natural resource economics; Computer science; Engineering; Business; Economics","score_opus":0.02885692149098108,"score_gpt":0.25681787219314617,"score_spread":0.2279609507021651,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4317632366","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":[0.9877109,0.000007959827,0.009185407,0.0009482774,0.000098280725,0.0016425627,0.000061497645,0.00013952916,0.00020558342],"genre_scores_gemma":[0.99632794,0.000010473726,0.0029888728,0.000038307673,0.0000024301912,0.00016852934,0.0000066664447,0.000012818765,0.0004439433],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.99903876,0.000011305477,0.00024480006,0.0002236062,0.0002185983,0.0002629453],"domain_scores_gemma":[0.9994799,0.00009578228,0.00011006734,0.0002842789,0.000011919742,0.000018070119],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015755362,0.00010207534,0.00015852437,0.00008784143,0.000051169358,0.0000031436032,0.0002533921,0.00008770616,0.000014877919],"category_scores_gemma":[0.00014846513,0.00007749234,0.00006909423,0.0011285713,0.00027779187,0.000201593,0.00010110368,0.00010017174,0.000009635283],"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":[0.00013850327,0.00019193644,0.5614894,0.00012968646,0.000022168737,0.0000061924384,0.00064196036,0.30591935,0.082403645,0.0014069848,0.0010125077,0.046637677],"study_design_scores_gemma":[0.0011256683,0.00024196248,0.5800724,0.00024211075,0.00001910856,0.0000018327895,0.0005705239,0.09359782,0.27761173,0.044990644,0.0012108176,0.00031538296],"about_ca_topic_score_codex":0.00013791103,"about_ca_topic_score_gemma":0.00045937314,"teacher_disagreement_score":0.21232152,"about_ca_system_score_codex":0.00009273443,"about_ca_system_score_gemma":0.0000135401515,"threshold_uncertainty_score":0.31600457},"labels":[],"label_agreement":null},{"id":"W4317634703","doi":"10.2514/6.2023-1578","title":"Multi-Material Topology Optimization of an Urban Air Mobility Vehicle Battery Pack","year":2023,"lang":"en","type":"article","venue":"AIAA SCITECH 2023 Forum","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Queen's University","funders":"","keywords":"Battery pack; Battery (electricity); Topology optimization; Automotive engineering; Finite element method; Takeoff; Acceleration; Power (physics); Engineering; Topology (electrical circuits); Computer science; Electrical engineering; Structural engineering","score_opus":0.01383457302992999,"score_gpt":0.2509223519420292,"score_spread":0.23708777891209923,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4317634703","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":[0.97533107,0.000007578497,0.021930667,0.0010516463,0.0002991518,0.00034466173,0.00006875712,0.00069975166,0.00026672106],"genre_scores_gemma":[0.9827957,0.000014929232,0.016339952,0.00014797159,0.000019189612,0.00004331932,0.000054002998,0.000019625926,0.0005653181],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99871063,0.00004684517,0.00024810934,0.00039388594,0.00018629964,0.00041424422],"domain_scores_gemma":[0.9993327,0.000043598662,0.000087979955,0.0004644668,0.000011079766,0.000060139944],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002204474,0.00014068029,0.00018063639,0.00008523701,0.00012760669,0.00001132975,0.0003620724,0.0001595269,0.00078283926],"category_scores_gemma":[0.000085630425,0.00013126351,0.000048991515,0.00063603395,0.00043655105,0.00037041228,0.0003801779,0.00010379457,0.0002966499],"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":[0.00015108082,0.0005417755,0.12832236,0.000050215745,0.000030265366,0.000051327515,0.00031358283,0.25922173,0.57521504,0.00036233026,0.011985241,0.023755059],"study_design_scores_gemma":[0.0018500821,0.0012509825,0.1692029,0.000048338014,0.000027622424,0.000015993168,0.002154893,0.32619143,0.4796762,0.011967793,0.0065582786,0.0010555218],"about_ca_topic_score_codex":0.00013975031,"about_ca_topic_score_gemma":0.00008586192,"teacher_disagreement_score":0.09553884,"about_ca_system_score_codex":0.00007070668,"about_ca_system_score_gemma":0.00000774464,"threshold_uncertainty_score":0.85715413},"labels":[],"label_agreement":null},{"id":"W4317932566","doi":"10.3390/aerospace10020113","title":"On the Study of Thermal-Propulsive Systems for Regional Aircraft","year":2023,"lang":"en","type":"article","venue":"Aerospace","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":7,"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 Victoria","funders":"Fundação para a Ciência e a Tecnologia","keywords":"Powertrain; Propulsion; Electrification; Automotive engineering; Context (archaeology); Electrically powered spacecraft propulsion; Computer science; Engineering; Systems engineering; Aerospace engineering; Electrical engineering; Electricity","score_opus":0.033164324559985796,"score_gpt":0.2617347410955849,"score_spread":0.22857041653559912,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4317932566","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":[0.995849,0.000023393206,0.0004942014,0.0015979744,0.00008771602,0.0009993097,0.00000450108,0.00019306193,0.00075085193],"genre_scores_gemma":[0.9968772,0.000013064377,0.00008806757,0.00007581039,0.000011186217,0.0002449217,0.0000012492907,0.000012218156,0.0026762695],"study_design_codex":"not_applicable","study_design_gemma":"observational","domain_scores_codex":[0.9992798,0.000029230614,0.00010346202,0.00019830992,0.0002121747,0.00017703263],"domain_scores_gemma":[0.99926597,0.0003109041,0.000070571936,0.00032698596,0.000007841139,0.000017717604],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016751268,0.000089554866,0.000106907566,0.00001879697,0.00012704752,0.000008716238,0.00027772386,0.000038222122,0.000033756583],"category_scores_gemma":[0.00008947079,0.000054420965,0.00003505179,0.00027155358,0.00013426464,0.000048293077,0.00010026772,0.00007104229,0.000203634],"study_design_candidate":"not_applicable","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":[0.00047272746,0.0017019114,0.083113,0.00008781888,0.00025114202,0.00005628631,0.0099850595,0.17376557,0.15060146,0.0709276,0.49521783,0.013819588],"study_design_scores_gemma":[0.011016587,0.018177869,0.46260825,0.000425631,0.00023128027,0.00002815699,0.20695812,0.035946455,0.06387587,0.098154075,0.099326506,0.0032512192],"about_ca_topic_score_codex":0.0001012788,"about_ca_topic_score_gemma":0.000025898546,"teacher_disagreement_score":0.39589134,"about_ca_system_score_codex":0.000039255126,"about_ca_system_score_gemma":0.0000029622788,"threshold_uncertainty_score":0.2617371},"labels":[],"label_agreement":null},{"id":"W4318614074","doi":"10.3390/app13031799","title":"New Validation Methodology of an Adaptive Wing for UAV S45 for Fuel Reduction and Climate Improvement","year":2023,"lang":"en","type":"article","venue":"Applied Sciences","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure","funders":"Natural Sciences and Engineering Research Council of Canada; Canada Research Chairs; École de technologie supérieure","keywords":"Drag; Lift-to-drag ratio; Airfoil; Wing; Lift (data mining); Aerodynamics; Wing configuration; Reduction (mathematics); Computer science; Simulation; Engineering; Aerospace engineering; Mathematics; Data mining","score_opus":0.09343989066996895,"score_gpt":0.3313343014611452,"score_spread":0.23789441079117624,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4318614074","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":[0.62047213,0.000020893374,0.37721592,0.00031566079,0.0001411737,0.0009787973,0.000010762067,0.0001662749,0.0006783962],"genre_scores_gemma":[0.70684236,0.00002505339,0.2929636,0.000014815593,0.000016156744,0.00009815815,0.000003707763,0.0000036844442,0.000032466516],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9992305,0.000011073759,0.00012942393,0.00030885494,0.000110907145,0.0002092092],"domain_scores_gemma":[0.99963677,0.0001527103,0.00009129812,0.00008491747,0.000005321658,0.000028969976],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00085077964,0.00006704516,0.00010236602,0.00005593981,0.00018781555,0.000013780228,0.00014511796,0.000041439827,0.0000090864405],"category_scores_gemma":[0.000045804263,0.00005625917,0.000017745402,0.00029914515,0.00031926463,0.00020880983,0.00008194256,0.000024381412,0.00000317466],"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":[0.00003671229,0.000007895937,0.00008310484,0.000013487022,0.0000027207832,4.4913442e-8,0.00029102204,0.0013963028,0.6665939,0.011433467,0.00008035757,0.32006097],"study_design_scores_gemma":[0.00044012244,0.0010238676,0.0013371325,0.0000053616955,0.000015768876,0.0000014428143,0.0053339275,0.00614022,0.6460604,0.3389951,0.0004900504,0.0001565841],"about_ca_topic_score_codex":0.000029700484,"about_ca_topic_score_gemma":0.000014536388,"teacher_disagreement_score":0.32756162,"about_ca_system_score_codex":0.000021128173,"about_ca_system_score_gemma":0.000009275743,"threshold_uncertainty_score":0.22941823},"labels":[],"label_agreement":null},{"id":"W4319324439","doi":"10.1016/j.ast.2023.108148","title":"Comparison studies on aerodynamic performances of a rotating propeller for small-size UAVs","year":2023,"lang":"en","type":"article","venue":"Aerospace Science and Technology","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":63,"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":"Department of Mechanical Engineering, University of Alberta; College of Engineering, University of Canterbury; Ministry of Business, Innovation and Employment","keywords":"Propeller; Aerodynamics; Advance ratio; Computational fluid dynamics; Blade element momentum theory; Thrust; Aerospace engineering; Stall (fluid mechanics); Wind tunnel; Performance prediction; Rotor (electric); Freestream; Marine engineering; Computer science; Blade pitch; Mechanics; Engineering; Simulation; Physics; Mechanical engineering; Turbulence; Turbine; Reynolds number; Turbine blade","score_opus":0.04049464582443197,"score_gpt":0.3230844294784939,"score_spread":0.28258978365406195,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4319324439","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":[0.99669594,0.00013134156,0.00017887399,0.0016552341,0.00010244275,0.00041574275,0.0000020228158,0.00040419935,0.0004142254],"genre_scores_gemma":[0.9886867,0.00015714997,0.010567591,0.000038421607,0.0000043956825,0.00011048438,3.4822367e-7,0.000008507744,0.00042644312],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9986415,0.0000069051985,0.0002108573,0.00045749545,0.00025303935,0.00043020563],"domain_scores_gemma":[0.99924815,0.0002367641,0.00015266787,0.00027309003,0.000057903868,0.000031419506],"candidate_categories":["sts"],"consensus_categories":[],"category_scores_codex":[0.0005539541,0.0001405268,0.0002569497,0.00021624612,0.00040189057,0.00001533112,0.00046090252,0.00009103901,0.0000039907222],"category_scores_gemma":[0.001692788,0.000106456304,0.00002074122,0.0024127155,0.003429643,0.0001765982,0.0004404025,0.0001387634,0.000042254585],"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":[0.000036133242,0.00013117015,0.25171858,0.00011905509,0.0000336048,0.0000061123123,0.0023055496,0.0021413665,0.5331161,0.017124688,0.0016729509,0.1915947],"study_design_scores_gemma":[0.0015737523,0.00423963,0.04712129,0.00025707722,0.000043031858,0.000020993279,0.0473913,0.05595659,0.7838662,0.05526286,0.003502035,0.0007652426],"about_ca_topic_score_codex":0.0000055653336,"about_ca_topic_score_gemma":0.000057634494,"teacher_disagreement_score":0.2507501,"about_ca_system_score_codex":0.000054159533,"about_ca_system_score_gemma":0.000023142382,"threshold_uncertainty_score":0.9992825},"labels":[],"label_agreement":null},{"id":"W4319456104","doi":"10.1016/j.biombioe.2023.106727","title":"Economic opportunities and challenges in biojet production: A literature review and analysis","year":2023,"lang":"en","type":"review","venue":"Biomass and Bioenergy","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":35,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Alberta","funders":"Natural Resources Canada; FORGE Hydrocarbons","keywords":"Production (economics); Business; Economics; Microeconomics","score_opus":0.12674123802652035,"score_gpt":0.29953796166851643,"score_spread":0.17279672364199608,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4319456104","genre_codex":"review","genre_gemma":"review","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"review","genre_consensus":"review","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.00002188542,0.9972317,9.750996e-7,0.0022331988,0.0000414753,0.00022011215,0.000054148284,0.00007203971,0.00012442496],"genre_scores_gemma":[0.000008244638,0.9991143,0.00016063989,0.000021935499,0.00002635885,0.000076702905,0.000059176713,0.000016222411,0.0005164247],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.99876755,0.00006394546,0.00029855943,0.0006268215,0.0000592393,0.0001838848],"domain_scores_gemma":[0.9995155,0.000030921594,0.00014158327,0.0002489399,0.0000028420964,0.00006025201],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020550583,0.00029034706,0.0009788362,0.00029243203,0.00005687775,0.000042503267,0.000112816066,0.0002128486,0.000020080393],"category_scores_gemma":[0.0000134670745,0.0002048559,0.0000878775,0.00051755377,0.00028879542,0.00013087325,0.000204925,0.00009066432,0.000005413747],"study_design_candidate":"not_applicable","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":[6.788042e-7,0.000007114586,0.000034638026,0.0115389,0.00012697175,0.000034233883,0.000018034782,1.0198648e-7,8.302951e-7,0.0005084784,0.0001708038,0.9875592],"study_design_scores_gemma":[0.00003179828,0.000031112588,0.00010557402,0.0054422263,0.00060632045,0.000062673105,0.000047643873,0.0000023928555,0.0000012328775,0.00016844377,0.993236,0.0002645961],"about_ca_topic_score_codex":0.00004864349,"about_ca_topic_score_gemma":0.00057995174,"teacher_disagreement_score":0.9930652,"about_ca_system_score_codex":0.00004743013,"about_ca_system_score_gemma":0.000011381299,"threshold_uncertainty_score":0.8353781},"labels":[],"label_agreement":null},{"id":"W4322210231","doi":"10.5194/egusphere-egu23-14974","title":"Sensitivities of atmospheric ozone to supersonic emissions above the transatlantic flight corridor","year":2023,"lang":"en","type":"preprint","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"NOx; Environmental science; Ozone; Atmospheric sciences; Emission inventory; Ozone layer; Montreal Protocol; Greenhouse gas; Civil aviation; Meteorology; Tropospheric ozone; Aviation; Air quality index; Combustion; Engineering; Chemistry; Geography; Aerospace engineering; Geology","score_opus":0.02283982934443887,"score_gpt":0.2438406837580063,"score_spread":0.22100085441356743,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4322210231","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":[0.7775239,0.00025187543,0.18422043,0.019648235,0.0011411584,0.0022413062,0.00015958454,0.001883989,0.012929534],"genre_scores_gemma":[0.96254545,0.00032742263,0.016977008,0.0002560533,0.000037278885,0.00008651945,0.000010323961,0.000046420708,0.019713499],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9983793,0.000049946968,0.00032424784,0.0005183008,0.00035998132,0.0003682183],"domain_scores_gemma":[0.9988264,0.00023137261,0.000091060894,0.0007596222,0.000010223244,0.00008131552],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00019416699,0.00029124744,0.00037201063,0.00001662583,0.000132258,0.000023517312,0.00061900116,0.00022022656,0.0009802912],"category_scores_gemma":[0.00009981921,0.00018463096,0.00016716274,0.00038659314,0.0004066073,0.000050963674,0.00087578857,0.00043584732,0.00051491905],"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":[0.0002841212,0.00089254533,0.042281132,0.00083844754,0.00057224126,0.0005416912,0.022518506,0.305653,0.26649672,0.0028385478,0.2569277,0.10015533],"study_design_scores_gemma":[0.0026228018,0.001822782,0.2027245,0.003032719,0.0011253657,0.00022908069,0.06272326,0.07886401,0.38294685,0.10435658,0.1506179,0.0089341635],"about_ca_topic_score_codex":0.0007183351,"about_ca_topic_score_gemma":0.00032457887,"teacher_disagreement_score":0.22678901,"about_ca_system_score_codex":0.000110488196,"about_ca_system_score_gemma":0.00002702215,"threshold_uncertainty_score":0.99993294},"labels":[],"label_agreement":null},{"id":"W4328107213","doi":"10.2514/1.c036330","title":"Optimization and Decision-Making Framework for Small Unmanned Aircraft Systems Fleet Design","year":2023,"lang":"en","type":"article","venue":"Journal of Aircraft","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"University of British Columbia; Purdue University","keywords":"Bespoke; Sizing; Systems engineering; Computer science; Fleet management; Profiling (computer programming); Operations research; Engineering","score_opus":0.02727747201250736,"score_gpt":0.2783196002042202,"score_spread":0.25104212819171284,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4328107213","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":[0.020734485,0.00029870833,0.9774217,0.00046962633,0.00047758294,0.0003851822,0.0000046120617,0.00016274561,0.000045335102],"genre_scores_gemma":[0.28623652,0.00030534784,0.7131484,0.00009443231,0.00009759665,0.000018711922,9.70994e-7,0.00003252395,0.00006549076],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99843746,0.00005110842,0.000542643,0.0002611068,0.00034473883,0.0003629428],"domain_scores_gemma":[0.99786097,0.0013646364,0.00038609645,0.00022892933,0.000054695687,0.00010468705],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00085688056,0.00019562687,0.00033559737,0.00021603424,0.00021137985,0.000087274464,0.00037035072,0.000207266,0.000049559836],"category_scores_gemma":[0.00104924,0.00016209253,0.000105409104,0.00057186215,0.00013834605,0.00037710846,0.00015242067,0.00025405412,0.000036200163],"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":[0.00015188105,0.00003699686,0.0013362909,0.000024824365,0.000033317738,0.000060826613,0.00014038157,0.94642246,0.0005304803,0.00054458034,0.0039997455,0.046718232],"study_design_scores_gemma":[0.0024008402,0.002184019,0.004363436,0.0017032801,0.00018597154,0.00056053494,0.0021244392,0.63251835,0.0014407417,0.33868697,0.012721101,0.0011102943],"about_ca_topic_score_codex":0.000002557421,"about_ca_topic_score_gemma":0.0000018182712,"teacher_disagreement_score":0.3381424,"about_ca_system_score_codex":0.00012991842,"about_ca_system_score_gemma":0.000023605691,"threshold_uncertainty_score":0.6609942},"labels":[],"label_agreement":null},{"id":"W4360616018","doi":"10.1016/j.applthermaleng.2023.120427","title":"A review on the recent developments in thermal management systems for hybrid-electric aircraft","year":2023,"lang":"en","type":"review","venue":"Applied Thermal Engineering","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":113,"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 Victoria","funders":"Horizon 2020; Fundação para a Ciência e a Tecnologia; Horizon 2020 Framework Programme; European Commission","keywords":"Electrification; Heat exchanger; Thermal management of electronic devices and systems; Propulsion; Automotive engineering; Engineering; Mechanical engineering; Systems engineering; Aerospace engineering; Electricity; Electrical engineering","score_opus":0.035149766195931624,"score_gpt":0.2565016060403896,"score_spread":0.22135183984445794,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4360616018","genre_codex":"review","genre_gemma":"review","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"review","genre_consensus":"review","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0000111018,0.99020404,0.00092768774,0.000040724964,0.00017855197,0.005272111,0.000008610264,0.0004392994,0.0029178641],"genre_scores_gemma":[0.00008837717,0.99245465,0.00045420413,0.00014116196,0.000032514552,0.006481917,0.000021818187,0.00012929224,0.0001960849],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9978942,0.000031151045,0.00059788866,0.0005634921,0.0002822438,0.0006309802],"domain_scores_gemma":[0.9989787,0.00027548982,0.00017718789,0.00051745476,0.000003777724,0.000047402562],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00056578394,0.00053488085,0.00090864295,0.00015259736,0.000081212005,0.000027707089,0.00082023675,0.000129575,0.00003501047],"category_scores_gemma":[0.00004028378,0.0003562703,0.00015764456,0.0009427905,0.00002639658,0.000039839935,0.00029239722,0.00044040734,0.0005949775],"study_design_candidate":"not_applicable","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":[0.0000034864267,0.000024134475,1.99985e-7,0.013674203,0.00010012553,0.000020289926,0.000006584555,0.006177062,0.000025425737,0.0017324241,0.00060993567,0.97762614],"study_design_scores_gemma":[0.00012360587,0.000016576003,0.0000067870465,0.015118991,0.00010129291,0.000004810425,0.0000058643777,0.00028737317,0.00002558658,0.000034666355,0.9838206,0.00045382805],"about_ca_topic_score_codex":0.0000039061083,"about_ca_topic_score_gemma":4.1699772e-7,"teacher_disagreement_score":0.9832107,"about_ca_system_score_codex":0.0005492192,"about_ca_system_score_gemma":0.000015960519,"threshold_uncertainty_score":0.99988896},"labels":[],"label_agreement":null},{"id":"W4362509600","doi":"10.2514/1.c037090","title":"Statistical Approach for Electric Taxiing Requirements for Regional Turboprop Aircraft","year":2023,"lang":"en","type":"article","venue":"Journal of Aircraft","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Natural Sciences and Engineering Research Council of Canada; Consortium de Recherche et d’innovation en Aérospatiale au Québec; Pratt and Whitney Canada; Université de Sherbrooke; Université Laval","keywords":"Turboprop; Fuel efficiency; Automotive engineering; Payload (computing); Acceleration; Aeronautics; Runway; Landing gear; Engineering; Computer science; Aerospace engineering; Physics","score_opus":0.043878926602767196,"score_gpt":0.29632948285782545,"score_spread":0.25245055625505824,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4362509600","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":[0.02755322,0.0001090534,0.96951693,0.0013180716,0.0002336917,0.00072494237,0.000024170437,0.0001725932,0.00034730212],"genre_scores_gemma":[0.49236643,0.00013139327,0.5050548,0.00039692683,0.00033591967,0.00014625968,0.000033640998,0.00007012544,0.0014645524],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.99799025,0.00003128004,0.00057003216,0.0003111737,0.0005272264,0.000570023],"domain_scores_gemma":[0.998929,0.00034472928,0.00033946626,0.00020249483,0.000051027542,0.00013325344],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0007555345,0.00020310495,0.00033936457,0.00020118685,0.0002121291,0.000034416888,0.00046684267,0.0001313591,0.00005030813],"category_scores_gemma":[0.00055240875,0.00016757594,0.00019961964,0.00055252167,0.0001501461,0.00036465997,0.00009329943,0.00024302697,0.000038593866],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0012634672,0.0008417584,0.013694934,0.0002675688,0.00034217542,0.00013157443,0.00041367073,0.012977638,0.173891,0.0051871357,0.5458254,0.24516365],"study_design_scores_gemma":[0.013005826,0.0074925064,0.04593737,0.00023216015,0.0005123495,0.0007880904,0.0016436973,0.12806241,0.037259106,0.26236054,0.50015277,0.0025531875],"about_ca_topic_score_codex":0.0000040277578,"about_ca_topic_score_gemma":0.0000013896,"teacher_disagreement_score":0.4648132,"about_ca_system_score_codex":0.00023392512,"about_ca_system_score_gemma":0.000047794238,"threshold_uncertainty_score":0.68335485},"labels":[],"label_agreement":null},{"id":"W4366777812","doi":"10.54097/hset.v43i.7430","title":"Current Status of Jet Engines and Their future","year":2023,"lang":"en","type":"article","venue":"Highlights in Science Engineering and Technology","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Kensington Health","funders":"","keywords":"Jet engine; Aerospace; Turbofan; Spacecraft; Jet (fluid); Aerospace engineering; Jet propulsion; Mechanical engineering; Computer science; Aeronautics; Engineering","score_opus":0.006990476818477538,"score_gpt":0.21973262765535953,"score_spread":0.212742150836882,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4366777812","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":[0.9967337,0.0011175318,0.0005416242,0.0007640983,0.00020820991,0.00008728954,0.0000041380154,0.00047811345,0.00006527172],"genre_scores_gemma":[0.99398947,0.0040903455,0.0018775857,0.0000020508683,0.000011118974,0.000014609778,4.779808e-7,0.0000062823574,0.000008041931],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9990242,0.0000029110588,0.00013127751,0.00030867613,0.000109561755,0.00042337133],"domain_scores_gemma":[0.9996756,0.00003719636,0.000028851306,0.00019933029,0.0000074821637,0.00005157113],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015123226,0.00012348796,0.00015286474,0.0005792092,0.00006464793,0.0000094794395,0.00023611475,0.00008453788,0.000003619689],"category_scores_gemma":[0.000099169294,0.00008766568,0.000008981865,0.0025111586,0.00083624135,0.00015533325,0.00032181252,0.00014606185,0.00001707782],"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":[0.000006041322,0.000056900306,0.08515891,0.0000654275,0.0000063230586,0.000023826928,0.00087711914,0.003279365,0.42392877,0.19924955,0.00021884266,0.28712893],"study_design_scores_gemma":[0.0009622348,0.00032518327,0.20444123,0.00018850362,0.000008016036,0.00006169763,0.0019111572,0.04521594,0.37723413,0.03427522,0.3343875,0.0009891599],"about_ca_topic_score_codex":0.000007863946,"about_ca_topic_score_gemma":0.000007865407,"teacher_disagreement_score":0.33416867,"about_ca_system_score_codex":0.000038438953,"about_ca_system_score_gemma":0.000009336904,"threshold_uncertainty_score":0.35749027},"labels":[],"label_agreement":null},{"id":"W4375866158","doi":"10.2514/1.c037158","title":"Aerodynamic Optimization and Fuel Burn Evaluation of a Transonic Strut-Braced-Wing Single-Aisle Aircraft","year":2023,"lang":"en","type":"article","venue":"Journal of Aircraft","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":11,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto","funders":"Natural Sciences and Engineering Research Council of Canada; University of Toronto; Government of Ontario","keywords":"Transonic; Wing; Wing loading; Aerodynamics; Engineering; Structural engineering; Aerospace engineering; Fuel efficiency; Aileron; Mach number; Angle of attack","score_opus":0.025580446816077965,"score_gpt":0.2634515939579263,"score_spread":0.23787114714184832,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4375866158","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":[0.92946464,0.000700836,0.06781005,0.00078868907,0.00022196607,0.00029226296,0.0000053623053,0.000112753194,0.00060346257],"genre_scores_gemma":[0.98298323,0.00044304744,0.016408684,0.000026614633,0.00003123908,0.0000052356695,0.0000031047082,0.000022385186,0.00007643275],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99802136,0.00010873149,0.00055963086,0.00021925516,0.000827146,0.0002638797],"domain_scores_gemma":[0.9990938,0.00012018683,0.00041539397,0.00019766478,0.000093835144,0.00007914167],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0011834503,0.00016734039,0.00029495457,0.00023375556,0.00008691845,0.000025855768,0.00022626038,0.00012462173,0.00023968102],"category_scores_gemma":[0.00028942002,0.00014779207,0.000107689295,0.00066768675,0.00021075619,0.00076383573,0.000081896615,0.00022900674,0.00001758264],"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":[0.000056857993,0.00011827423,0.004639667,0.00003704765,0.000043579825,0.000021427672,0.0006126534,0.8371373,0.07928422,0.00004659966,0.00022940607,0.07777297],"study_design_scores_gemma":[0.008285634,0.0030025463,0.103774235,0.0006457245,0.0007729276,0.000521462,0.0038083557,0.8256707,0.019342005,0.029957497,0.002993292,0.0012255887],"about_ca_topic_score_codex":0.000008872789,"about_ca_topic_score_gemma":0.000030105055,"teacher_disagreement_score":0.09913457,"about_ca_system_score_codex":0.0002135559,"about_ca_system_score_gemma":0.000039569157,"threshold_uncertainty_score":0.6026786},"labels":[],"label_agreement":null},{"id":"W4377861320","doi":"10.1016/j.isci.2023.106944","title":"Multi-criteria decision analysis for the evaluation and screening of sustainable aviation fuel production pathways","year":2023,"lang":"en","type":"review","venue":"iScience","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":81,"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 Calgary","funders":"","keywords":"Aviation; Production (economics); Biochemical engineering; Sustainable production; Engineering; Operations research; Aeronautics; Environmental science; Aerospace engineering; Economics","score_opus":0.13711331071664926,"score_gpt":0.38407387058233566,"score_spread":0.2469605598656864,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4377861320","genre_codex":"review","genre_gemma":"review","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"review","genre_consensus":"review","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.000112135414,0.5796322,0.4183582,0.000025915238,0.000088221335,0.0016993529,0.000010250547,0.00006002454,0.0000136616645],"genre_scores_gemma":[0.006864032,0.9607216,0.03154922,0.000003840509,0.000019778206,0.00047038798,0.000018373861,0.000015105942,0.00033764134],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9984431,0.00006226995,0.0003253461,0.0005096526,0.00044119416,0.00021839056],"domain_scores_gemma":[0.9988516,0.0003618022,0.00033082734,0.0003759035,0.000057645713,0.000022243301],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0021633285,0.00015160882,0.00038055005,0.00020893363,0.000287751,0.000047102894,0.00035844464,0.00009407052,0.000019749536],"category_scores_gemma":[0.0017375234,0.00009578824,0.00013576617,0.002263312,0.00030988175,0.0003332866,0.00025846926,0.00008550626,0.000007168799],"study_design_candidate":"design_other","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":[0.000001999438,0.000010100027,0.000053555315,0.00036086494,0.000021875405,3.402116e-7,0.00008910038,0.000991358,0.000058400696,0.00008371157,0.000033035445,0.99829566],"study_design_scores_gemma":[0.0010459364,0.00048079027,0.02570785,0.0048536602,0.010973419,0.000026764139,0.0059092776,0.3506129,0.00035033716,0.046837557,0.5511779,0.0020235858],"about_ca_topic_score_codex":0.000045376935,"about_ca_topic_score_gemma":0.00004510744,"teacher_disagreement_score":0.9962721,"about_ca_system_score_codex":0.00013316137,"about_ca_system_score_gemma":0.00003082213,"threshold_uncertainty_score":0.3906131},"labels":[],"label_agreement":null},{"id":"W4379385269","doi":"10.3390/aerospace10060533","title":"Systems Integration Framework for Hybrid-Electric Commuter and Regional Aircraft","year":2023,"lang":"en","type":"article","venue":"Aerospace","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":6,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Concordia University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Electrification; Sizing; Systems engineering; System integration; Retrofitting; Engineering; Electric power system; Avionics; Multidisciplinary approach; Propulsion; Key (lock); Hybrid system; Computer science; Aerospace engineering; Electricity; Power (physics); Electrical engineering","score_opus":0.02402155604513454,"score_gpt":0.26335205045760035,"score_spread":0.23933049441246582,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4379385269","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":[0.29821342,0.00028258484,0.69443804,0.0048827697,0.00021435508,0.0006324954,0.000008065514,0.00093386945,0.00039437215],"genre_scores_gemma":[0.9815114,0.00017186563,0.016400635,0.0002046716,0.000030061194,0.00012675887,0.000010720485,0.000015847187,0.0015280052],"study_design_codex":"not_applicable","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.99931896,0.000015157676,0.000091946764,0.00022397323,0.00012551241,0.0002244342],"domain_scores_gemma":[0.99950653,0.0002117185,0.00004322825,0.00019537743,0.0000063922844,0.00003677389],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00011946601,0.000100383084,0.00010421515,0.000035968485,0.00014452545,0.00003471315,0.00013393053,0.0000712317,0.000014220731],"category_scores_gemma":[0.00010176971,0.00008615539,0.000026901282,0.0003064057,0.00009710047,0.00013894404,0.00008185844,0.0001215681,0.00014929746],"study_design_candidate":"theoretical_or_conceptual","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":[0.00015304162,0.00015148352,0.04263434,0.000112957605,0.000071476614,0.000047622638,0.0012270323,0.0045262724,0.12118508,0.19505288,0.4603586,0.17447923],"study_design_scores_gemma":[0.0017625733,0.0011225676,0.062716156,0.0003179286,0.000065863074,0.00015192488,0.0026252281,0.12360444,0.055916734,0.51597553,0.23399334,0.0017476991],"about_ca_topic_score_codex":0.000041707433,"about_ca_topic_score_gemma":0.000012141511,"teacher_disagreement_score":0.683298,"about_ca_system_score_codex":0.000064943,"about_ca_system_score_gemma":0.0000032455164,"threshold_uncertainty_score":0.3513315},"labels":[],"label_agreement":null},{"id":"W4379793346","doi":"10.2514/6.2023-3393","title":"Aerodynamic evaluation of distributed propulsion for a regional aircraft","year":2023,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Safran Electronics (Canada)","funders":"","keywords":"Propulsion; Wing; Aerodynamics; Aerospace engineering; Lift-to-drag ratio; Lift (data mining); Drag; Marine engineering; Limiting; Engineering; Cruise; Wing loading; Leading edge; Aeronautics; Computer science; Angle of attack; Mechanical engineering","score_opus":0.04580652788945342,"score_gpt":0.30182463863209974,"score_spread":0.2560181107426463,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4379793346","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":[0.90062326,0.000010652023,0.094625495,0.0022827538,0.000070457994,0.0010620769,0.00003462823,0.0005197711,0.0007708825],"genre_scores_gemma":[0.9918683,0.0000057749926,0.0074667726,0.0000184908,0.0000045106194,0.00013056702,0.00009382703,0.0000059236927,0.0004058366],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992392,0.000017076844,0.00011971401,0.0001689768,0.0003195379,0.00013548063],"domain_scores_gemma":[0.9997213,0.000045784374,0.000045829605,0.00014842078,0.000021703143,0.000016976515],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003527875,0.000058964586,0.00007132406,0.00003235284,0.00005035908,0.0000027481035,0.000113814865,0.00004621671,0.00021320379],"category_scores_gemma":[0.00015830346,0.000046398607,0.00003673546,0.00035035523,0.00010145837,0.0000887272,0.00006604199,0.000028753338,0.00007867015],"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":[0.00012412942,0.00022016974,0.020983186,0.000049635095,0.000029096054,0.0000020528732,0.000117447635,0.0493046,0.3482021,0.008198194,0.06277182,0.50999755],"study_design_scores_gemma":[0.0020904609,0.00036552284,0.25736642,0.000029868188,0.000066193534,0.0000050441245,0.0005340868,0.47871134,0.02944175,0.21352336,0.017449781,0.00041616592],"about_ca_topic_score_codex":0.000013945502,"about_ca_topic_score_gemma":0.00004111909,"teacher_disagreement_score":0.5095814,"about_ca_system_score_codex":0.000089284134,"about_ca_system_score_gemma":0.000008217817,"threshold_uncertainty_score":0.2334432},"labels":[],"label_agreement":null},{"id":"W4382055809","doi":"10.4050/f-0079-2023-18146","title":"Implications of Sustainable Aviation Fuel for the Rotorcraft Industry","year":2023,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Lockheed Martin (Canada)","funders":"","keywords":"Aviation; Original equipment manufacturer; Jet fuel; Aviation fuel; Engineering; Aeronautics; Certification; Kerosene; Waste management; Computer science; Aerospace engineering","score_opus":0.02066443885557692,"score_gpt":0.2728195144965687,"score_spread":0.2521550756409918,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4382055809","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":[0.13671014,0.000082581304,0.74808955,0.035525925,0.0001285638,0.004704817,0.000033334174,0.001723087,0.07300198],"genre_scores_gemma":[0.98275304,0.000013596183,0.0014284848,0.00007722695,0.0000069098983,0.00032261838,0.0000032646035,0.00000493286,0.015389945],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.9996054,0.00000402574,0.00008223151,0.00009732848,0.00006243332,0.00014857005],"domain_scores_gemma":[0.99960977,0.00013142286,0.000033528282,0.00020303481,0.00000977181,0.000012468324],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00011776112,0.00004035022,0.00004116815,0.000021407926,0.000106962245,0.000006047525,0.00018082796,0.00007103806,0.0002481327],"category_scores_gemma":[0.00010031597,0.00002635005,0.000023773693,0.00040584517,0.00009725764,0.000098610515,0.000103027356,0.00006321955,0.0000611454],"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":[0.000019272313,0.00009165063,0.13037267,0.000049771552,0.000027147624,0.0000014794507,0.00045304126,0.00587639,0.03472162,0.6518155,0.10793908,0.0686324],"study_design_scores_gemma":[0.00025313842,0.00007051243,0.37232018,0.0000024721098,0.000012804182,0.0000010861772,0.004641979,0.0015953967,0.015626382,0.52472436,0.08061481,0.00013684083],"about_ca_topic_score_codex":0.000055147015,"about_ca_topic_score_gemma":0.000013157814,"teacher_disagreement_score":0.8460429,"about_ca_system_score_codex":0.0000403023,"about_ca_system_score_gemma":0.000005434653,"threshold_uncertainty_score":0.27168792},"labels":[],"label_agreement":null},{"id":"W4384625943","doi":"","title":"EFFECTS OF COSMIC RADIATION IN AIRCRAFTS: A DISCUSSION ABOUT AIRCREW OVER SOUTH AMERICA DOI 10.5028/jatm.2012.04021012","year":2012,"lang":"en","type":"article","venue":"DOAJ (DOAJ: Directory of Open Access Journals)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Aircrew; Aeronautics; COSMIC cancer database; Aerospace engineering; Radiation; Physics; Environmental science; Meteorology; Engineering; Astronomy; Nuclear physics","score_opus":0.06366329118097251,"score_gpt":0.4446554267799187,"score_spread":0.3809921355989462,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4384625943","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":[0.97501016,0.015800422,0.0045660087,0.00015168177,0.00042704356,0.0010802916,0.000026529038,0.000112861315,0.0028250213],"genre_scores_gemma":[0.99370074,0.004491837,0.0008814748,0.00017173043,0.000067614375,0.00008571794,0.000008615161,0.000052933752,0.00053931243],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.996842,0.0002931068,0.0008717398,0.00048375616,0.0007990705,0.0007102838],"domain_scores_gemma":[0.9977947,0.0003538014,0.0010006321,0.0005506272,0.000030320534,0.00026992016],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0007094622,0.00040990734,0.0008231429,0.00053924567,0.0001639739,0.00016209211,0.0018504026,0.00019690911,0.010585265],"category_scores_gemma":[0.00048145937,0.00029647618,0.00019319185,0.001490492,0.00047674248,0.0045325207,0.0011477282,0.00046541283,0.00016252503],"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":[0.00019156781,0.00052920653,0.6920452,0.00010213959,0.000048667116,0.000014855132,0.0005410423,0.0005554605,0.1697166,0.000023791425,0.00929704,0.12693442],"study_design_scores_gemma":[0.0009199796,0.000030686475,0.9245083,0.00039218,0.000054890923,0.0000042837987,0.00013226109,0.00011951082,0.058679137,0.0027594208,0.011933059,0.0004662882],"about_ca_topic_score_codex":0.00044739922,"about_ca_topic_score_gemma":0.00001949909,"teacher_disagreement_score":0.23246309,"about_ca_system_score_codex":0.00034339444,"about_ca_system_score_gemma":0.000035658588,"threshold_uncertainty_score":0.99994874},"labels":[],"label_agreement":null},{"id":"W4385582373","doi":"10.1017/aer.2023.64","title":"A methodology to determine the precision uncertainty in gas turbine engine cycle models","year":2023,"lang":"en","type":"article","venue":"The Aeronautical Journal","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Computer science; Thrust; Engineering; Aerospace engineering","score_opus":0.07320909941032405,"score_gpt":0.31113617912803115,"score_spread":0.2379270797177071,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4385582373","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":[0.8750051,0.00006655491,0.09420888,0.029505543,0.00015218729,0.0002895806,0.000002123031,0.00013118464,0.0006387959],"genre_scores_gemma":[0.98731524,0.00011231217,0.011525377,0.0007246924,0.000052036386,0.000020811069,6.081051e-7,0.000012916274,0.0002359851],"study_design_codex":"simulation_or_modeling","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.9984785,0.00027077695,0.00027003896,0.0001992432,0.0003163737,0.0004651151],"domain_scores_gemma":[0.99850535,0.001016923,0.000045746714,0.00032750302,0.0000074922627,0.00009695177],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.001732028,0.0001310487,0.0001755953,0.00006178618,0.00020348176,0.000027881455,0.00073018833,0.00007080469,0.00030575515],"category_scores_gemma":[0.0006458723,0.00006316815,0.00005954513,0.00064715795,0.00027290033,0.00012323508,0.0005210849,0.0005516519,0.00036702203],"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":[0.000131159,0.000038306698,0.00021470476,0.0000011632603,0.000008581739,0.00008645969,0.00054165174,0.60340697,0.009592044,0.0015701763,0.001539577,0.38286918],"study_design_scores_gemma":[0.0005285771,0.00027462852,0.011681339,0.000026404154,0.000015465674,0.00036060656,0.00037193648,0.32700697,0.0016563091,0.65454096,0.003343462,0.00019334756],"about_ca_topic_score_codex":0.000029736293,"about_ca_topic_score_gemma":0.00007151906,"teacher_disagreement_score":0.6529708,"about_ca_system_score_codex":0.00013254106,"about_ca_system_score_gemma":0.000009506935,"threshold_uncertainty_score":0.4717448},"labels":[],"label_agreement":null},{"id":"W4385873037","doi":"10.3390/aerospace10080718","title":"EVTOL Tilt-Wing Aircraft Design under Uncertainty Using a Multidisciplinary Possibilistic Approach","year":2023,"lang":"en","type":"article","venue":"Aerospace","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":17,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"Mitacs","keywords":"Multidisciplinary design optimization; Conceptual design; Wing configuration; Aerodynamics; Computer science; Stability (learning theory); Airworthiness; Tilt (camera); Automotive engineering; Simulation; Engineering; Aerospace engineering; Multidisciplinary approach; Mechanical engineering","score_opus":0.056496230109593336,"score_gpt":0.2916827803596675,"score_spread":0.23518655025007415,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4385873037","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":[0.52540785,0.00005268481,0.47099563,0.00033681246,0.00012539297,0.0005491753,0.000005030636,0.0014083853,0.0011190464],"genre_scores_gemma":[0.8983579,0.000016137594,0.099677466,0.00006574375,0.000023792038,0.000043714113,0.000007911854,0.00004210547,0.0017651793],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9980781,0.000079259014,0.00021066357,0.00064691785,0.0003535433,0.00063148583],"domain_scores_gemma":[0.9990347,0.00019836552,0.000084403786,0.00056499505,0.0000096120475,0.0001079355],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00035448218,0.0002652769,0.00023136796,0.00007274593,0.00040629247,0.00004470277,0.0004232003,0.00015552768,0.00010409655],"category_scores_gemma":[0.000130436,0.00023372527,0.00008114514,0.0010078351,0.00040102104,0.0002960252,0.00058657804,0.00024785733,0.0006372449],"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":[0.00002607543,0.000074147276,0.0055676387,0.000014000564,0.000014388305,0.000041915853,0.0005667353,0.9114938,0.079456724,0.00021676348,0.0009900066,0.0015378002],"study_design_scores_gemma":[0.0007535104,0.00013926014,0.022724854,0.000054699645,0.000043922602,0.00004854017,0.004128797,0.94619757,0.005243254,0.019600406,0.00023824547,0.00082695176],"about_ca_topic_score_codex":0.00015686755,"about_ca_topic_score_gemma":0.00002106954,"teacher_disagreement_score":0.3729501,"about_ca_system_score_codex":0.00038032536,"about_ca_system_score_gemma":0.000025071753,"threshold_uncertainty_score":0.953104},"labels":[],"label_agreement":null},{"id":"W4386036986","doi":"10.1007/978-3-031-32639-4_2","title":"Design Considerations for Hybrid-Electric Propulsion Systems for FW-VTOL Aircraft","year":2023,"lang":"en","type":"book-chapter","venue":"Sustainable aviation","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":3,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Victoria","funders":"","keywords":"Propulsion; Takeoff; Takeoff and landing; Sizing; Fuel efficiency; Aerospace engineering; Aerospace; Automotive engineering; Engineering; Runway; Test bench; Hybrid system; Hybrid vehicle; Aeronautics; Power (physics); Computer science; Mechanical engineering","score_opus":0.029668419649212473,"score_gpt":0.2440508503417349,"score_spread":0.21438243069252244,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4386036986","genre_codex":"methods","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.000032538093,0.00039150578,0.972287,0.0007342379,0.00038025563,0.01183768,0.00007717578,0.0011096083,0.013149988],"genre_scores_gemma":[0.030050717,0.00025489088,0.015384338,0.000092001996,0.0001726381,0.003694996,0.0002686763,0.00021060006,0.9498711],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.99793273,0.00002593356,0.00045417922,0.00066140335,0.0003157828,0.0006099884],"domain_scores_gemma":[0.99834704,0.00066314306,0.00035946726,0.00039699965,0.00016957802,0.00006378483],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0004707757,0.00036850682,0.00037427119,0.000253201,0.0006352308,0.00011359273,0.00019402582,0.00035256214,0.000081274666],"category_scores_gemma":[0.0007216509,0.0003662414,0.00013721616,0.00012490623,0.00008579775,0.0003519086,0.000103464394,0.00020190676,0.00017533425],"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":[0.00022961422,0.00007596083,0.00001900369,0.0011012623,0.0001259316,0.00010228502,0.00016342236,0.045209005,0.0014830148,0.7887787,0.14487676,0.017835002],"study_design_scores_gemma":[0.0005259143,0.00044963017,0.000008270325,0.000057917692,0.0001015377,0.0000125499055,0.00015834392,0.019557076,0.0015354065,0.90458345,0.0724823,0.0005275842],"about_ca_topic_score_codex":0.00004652669,"about_ca_topic_score_gemma":0.000007037313,"teacher_disagreement_score":0.9569027,"about_ca_system_score_codex":0.0010623819,"about_ca_system_score_gemma":0.00012035526,"threshold_uncertainty_score":0.99987894},"labels":[],"label_agreement":null},{"id":"W4386099030","doi":"10.3390/aerospace10090745","title":"A Study on Thermal Management Systems for Hybrid–Electric Aircraft","year":2023,"lang":"en","type":"article","venue":"Aerospace","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":22,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Victoria","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Automotive engineering; Powertrain; Context (archaeology); Internal combustion engine cooling; Heat exchanger; Heat transfer; Mechanical engineering; Engineering; Environmental science; Computer science; Combustion","score_opus":0.02147601722656125,"score_gpt":0.257713842993961,"score_spread":0.23623782576739974,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4386099030","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":[0.98361534,0.000040967418,0.005741449,0.00045519494,0.00021348041,0.0019207973,0.000004502803,0.001208487,0.006799776],"genre_scores_gemma":[0.9899434,0.000028989218,0.00032019787,0.000064310785,0.00001807426,0.00051936833,0.0000023615228,0.000023843804,0.009079442],"study_design_codex":"not_applicable","study_design_gemma":"observational","domain_scores_codex":[0.99886066,0.000022542623,0.0001139667,0.000370095,0.00025378738,0.00037892594],"domain_scores_gemma":[0.99947894,0.0000726421,0.000042979027,0.00036328114,0.000003573648,0.00003860703],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00019153093,0.00014401744,0.00013167612,0.00006144055,0.00015315693,0.000029011238,0.00028270393,0.00003047097,0.000019738261],"category_scores_gemma":[0.000020542413,0.00012122926,0.000043574466,0.0005015041,0.000038442926,0.000078879246,0.00015522324,0.00008123227,0.0012680626],"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":[0.0005620614,0.0033439165,0.1734832,0.0002156243,0.00062146096,0.0017730977,0.002749912,0.16874304,0.06934005,0.01732836,0.3866421,0.17519718],"study_design_scores_gemma":[0.010575725,0.010117295,0.7176658,0.00016582481,0.00028365824,0.000044684675,0.026245259,0.02910884,0.043169867,0.009637518,0.14946114,0.0035244068],"about_ca_topic_score_codex":0.000023750641,"about_ca_topic_score_gemma":0.0000043979617,"teacher_disagreement_score":0.5441826,"about_ca_system_score_codex":0.00012220135,"about_ca_system_score_gemma":0.0000019350325,"threshold_uncertainty_score":0.9995096},"labels":[],"label_agreement":null},{"id":"W4386391511","doi":"10.1115/1.4063330","title":"Effect of Tip-Mounted Propeller and Trailing-Edge Flap on Wing's Lift and Drag Coefficients and Vortical Wake","year":2023,"lang":"en","type":"article","venue":"Journal of Fluids Engineering","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Drag; Stall (fluid mechanics); Wingtip vortices; Lift-to-drag ratio; Wake; Propeller; Vortex lift; Lift (data mining); Wing; Trailing edge; Mechanics; Airfoil; Lift coefficient; Physics; Vortex; Marine engineering; Lift-induced drag; Aerospace engineering; Engineering; Horseshoe vortex; Turbulence; Computer science; Vortex ring; Reynolds number","score_opus":0.005763302722501548,"score_gpt":0.22901826987762317,"score_spread":0.2232549671551216,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4386391511","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":[0.9953734,0.00020083877,0.0040972573,0.00006165582,0.00007218491,0.000088539615,9.960291e-7,0.00004420856,0.00006088333],"genre_scores_gemma":[0.99897236,0.00012682463,0.00082658953,0.000007741393,0.00001745608,0.0000012305015,1.8955984e-7,0.000012090652,0.00003549541],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99931926,0.00001446484,0.00020694078,0.00011883978,0.00018056377,0.0001599591],"domain_scores_gemma":[0.9996451,0.00016084143,0.00004363002,0.000069721944,0.000006670612,0.00007403184],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00032888376,0.000112277,0.0002053778,0.00009963573,0.00003352132,0.000014716671,0.00007303558,0.000058463687,0.000007650613],"category_scores_gemma":[0.00025252067,0.00008176385,0.000026340344,0.00017875544,0.00011179645,0.000103003586,0.00007681844,0.0001746491,0.000003593105],"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":[0.00013372397,0.00004209501,0.014958651,0.00018567422,0.00003765644,0.00011156665,0.0003823966,0.022749426,0.8931102,0.00009712801,0.00018433134,0.06800711],"study_design_scores_gemma":[0.004417725,0.00653301,0.18229611,0.00095181906,0.00015033255,0.00046357838,0.00019294297,0.34774825,0.45236325,0.00016923941,0.003970713,0.00074302824],"about_ca_topic_score_codex":9.4771184e-7,"about_ca_topic_score_gemma":1.8445262e-7,"teacher_disagreement_score":0.440747,"about_ca_system_score_codex":0.00001873413,"about_ca_system_score_gemma":0.0000026532343,"threshold_uncertainty_score":0.3334233},"labels":[],"label_agreement":null},{"id":"W4387052921","doi":"10.2514/1.i011220","title":"Performance Model Identification of the General Electric CF34-8C5B1 Turbofan Using Neural Networks","year":2023,"lang":"en","type":"article","venue":"Journal of Aerospace Information Systems","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université du Québec; Université du Québec à Montréal","funders":"","keywords":"Turbofan; Artificial neural network; Takeoff; Flight simulator; Computer science; Simulation; Climb; Engineering; Artificial intelligence; Automotive engineering; Aerospace engineering","score_opus":0.017165159261434887,"score_gpt":0.23742513319650976,"score_spread":0.22025997393507488,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4387052921","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":[0.95393497,0.000038917253,0.045129992,0.00009789996,0.00043217055,0.00017352514,0.0000016139443,0.00003941788,0.00015149561],"genre_scores_gemma":[0.9993881,0.00006364212,0.00032314265,0.000025097368,0.000038696075,0.0000031415418,0.0000010592919,0.0000058250484,0.00015131931],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9985525,0.000032359578,0.00071442744,0.0000542298,0.00046440362,0.00018208615],"domain_scores_gemma":[0.9984968,0.000020680756,0.0011846554,0.00019836331,0.000066786735,0.000032716816],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005530459,0.000094772906,0.00015860499,0.000112801856,0.0001443523,0.000055888966,0.0003458454,0.00007675785,0.000002750161],"category_scores_gemma":[0.00005592244,0.00006387617,0.00007796663,0.0008716874,0.00006267854,0.0017405057,0.00007982082,0.00019452086,0.00001512627],"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":[0.000009029285,0.000003968307,0.009647571,0.000014271209,0.0000053351832,2.0577637e-7,0.00020000312,0.9770394,0.010938161,0.00005889804,0.0004924567,0.0015907292],"study_design_scores_gemma":[0.00014687359,0.000031570507,0.0140828835,0.00002580113,0.000009425399,0.00004422706,0.00023373378,0.98157704,0.0036423577,0.000029579758,0.00010737788,0.000069109774],"about_ca_topic_score_codex":0.000013303264,"about_ca_topic_score_gemma":7.967666e-7,"teacher_disagreement_score":0.045453113,"about_ca_system_score_codex":0.00016327189,"about_ca_system_score_gemma":0.000018627969,"threshold_uncertainty_score":0.26047948},"labels":[],"label_agreement":null},{"id":"W4387127410","doi":"10.1115/gt2023-102238","title":"Thrust Rebalance to Extend Engine Time On-Wing With Consideration of Engine Degradation and Creep Life Consumption","year":2023,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Fuel efficiency; Automotive engineering; Thrust; Thrust specific fuel consumption; Engineering; Schedule; Aeronautics; Jet engine; Turbine; Computer science; Aerospace engineering","score_opus":0.016617655664355458,"score_gpt":0.2298894978739158,"score_spread":0.21327184220956033,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4387127410","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":[0.96724594,0.000013785172,0.030359177,0.00080485165,0.000014958898,0.0002190373,0.0000040527448,0.0002899265,0.0010482966],"genre_scores_gemma":[0.9852388,0.000043438853,0.013926839,0.00014118681,0.0000059860467,0.000013296077,0.000009796729,0.000007643298,0.0006130348],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.99942297,0.0000109183175,0.00011181668,0.00019233095,0.00014176533,0.000120207726],"domain_scores_gemma":[0.9996763,0.00010463218,0.0000361081,0.00013284157,0.0000065394474,0.000043598357],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000092151764,0.00008618197,0.00010389471,0.00006000044,0.00005665496,0.000011112619,0.00004627037,0.00003582004,0.00033466605],"category_scores_gemma":[0.00011952202,0.00006516241,0.000008296458,0.00020498758,0.00008845883,0.00015749835,0.000042086547,0.000050028255,0.0002199469],"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":[0.00023701627,0.00011720275,0.07209356,0.000058251506,0.000042861004,0.00002583234,0.00038520168,0.091289945,0.6205384,0.0039023564,0.007587929,0.2037214],"study_design_scores_gemma":[0.0013794963,0.0010425948,0.5384232,0.0001489366,0.000028146665,0.000021009117,0.00036040077,0.076872796,0.37747738,0.002440307,0.001172531,0.0006332227],"about_ca_topic_score_codex":0.000009989566,"about_ca_topic_score_gemma":0.000017310018,"teacher_disagreement_score":0.46632963,"about_ca_system_score_codex":0.000026475469,"about_ca_system_score_gemma":0.0000029268836,"threshold_uncertainty_score":0.36643586},"labels":[],"label_agreement":null},{"id":"W4387334057","doi":"10.2514/1.c036927","title":"Off-Design Performance Analysis of a Parallel Hybrid Electric Regional Turboprop Aircraft","year":2023,"lang":"en","type":"article","venue":"Journal of Aircraft","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"Natural Sciences and Engineering Research Council of Canada; Consortium de Recherche et d’innovation en Aérospatiale au Québec","keywords":"Turboprop; Propulsion; Fuel efficiency; Automotive engineering; Sizing; Payload (computing); Aircraft fuel system; Powertrain; Robustness (evolution); Engineering; Aerospace engineering; Computer science; Torque; Combustion","score_opus":0.02185126728758321,"score_gpt":0.2438250574854183,"score_spread":0.22197379019783509,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4387334057","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":[0.9490505,0.00044370117,0.048430454,0.0011936754,0.0001331693,0.00021071061,0.000004505605,0.00016964482,0.00036362716],"genre_scores_gemma":[0.9806668,0.0017116242,0.016657332,0.00014575379,0.000051161962,0.000008294857,0.0000039559472,0.00002497417,0.00073009625],"study_design_codex":"simulation_or_modeling","study_design_gemma":"observational","domain_scores_codex":[0.9974516,0.00008771597,0.00080774026,0.0002925269,0.0008817544,0.00047864506],"domain_scores_gemma":[0.9985269,0.00022228625,0.000675599,0.00038589517,0.00005832134,0.00013102175],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00082810747,0.00024290642,0.0006359941,0.0009133282,0.00011793444,0.000018336406,0.0007244259,0.000103769285,0.0002894459],"category_scores_gemma":[0.00016730007,0.00019582076,0.00041440417,0.0037688534,0.00024349493,0.0004921129,0.00014088122,0.00040459668,0.00015931962],"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":[0.0007125186,0.0005867273,0.109537706,0.000055511708,0.0020783735,0.0005708631,0.0005187828,0.55500156,0.09326875,0.00012903077,0.062424365,0.1751158],"study_design_scores_gemma":[0.002845332,0.0031021857,0.6788808,0.00017245635,0.0021013052,0.00060049415,0.00044295713,0.20534621,0.058963653,0.007632981,0.038518943,0.0013926923],"about_ca_topic_score_codex":0.000012030177,"about_ca_topic_score_gemma":0.0000039403285,"teacher_disagreement_score":0.5693431,"about_ca_system_score_codex":0.00018058346,"about_ca_system_score_gemma":0.000063924315,"threshold_uncertainty_score":0.7985339},"labels":[],"label_agreement":null},{"id":"W4387742956","doi":"10.1115/1.4063791","title":"Thrust Rebalance to Extend Engine Time On-Wing With Consideration of Engine Degradation and Creep Life Consumption","year":2023,"lang":"en","type":"article","venue":"Journal of Engineering for Gas Turbines and Power","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Fuel efficiency; Thrust; Automotive engineering; Thrust specific fuel consumption; Engineering; Aeronautics; Limiting; Creep; Turbine; Jet engine; Aerospace engineering; Mechanical engineering","score_opus":0.010342040427117557,"score_gpt":0.21917806939001433,"score_spread":0.20883602896289677,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4387742956","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":[0.9746671,0.00013572001,0.024478367,0.0004716095,0.00006463934,0.000120990364,0.000005264452,0.000037660513,0.00001865536],"genre_scores_gemma":[0.9853768,0.0001330227,0.014348985,0.000036254314,0.000024537096,0.000003852472,0.0000022340068,0.000011203559,0.000063117055],"study_design_codex":"simulation_or_modeling","study_design_gemma":"observational","domain_scores_codex":[0.99951494,0.0000037108755,0.00017341002,0.000091541275,0.00010828537,0.00010811271],"domain_scores_gemma":[0.9996478,0.00013070028,0.000081910584,0.000061443636,0.00002113196,0.00005701634],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00013592653,0.0000936345,0.00015639154,0.00009751586,0.00003243346,0.000014195699,0.000038820435,0.0000355963,0.000024288007],"category_scores_gemma":[0.00018628594,0.000068378344,0.000020540609,0.00011160117,0.000030253033,0.00015481039,0.000018308727,0.0000695432,0.0000024839553],"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":[0.0004972484,0.00006774156,0.012198675,0.00016719426,0.00010536948,0.000029922805,0.0004536576,0.614179,0.3438021,0.0008275945,0.0032500334,0.024421431],"study_design_scores_gemma":[0.006479919,0.007874186,0.5295361,0.0016826799,0.00021175052,0.0005828478,0.0003960314,0.27073538,0.16122732,0.001893448,0.01787192,0.0015084107],"about_ca_topic_score_codex":9.17634e-7,"about_ca_topic_score_gemma":7.342715e-7,"teacher_disagreement_score":0.51733744,"about_ca_system_score_codex":0.000017058595,"about_ca_system_score_gemma":0.0000031422337,"threshold_uncertainty_score":0.27883878},"labels":[],"label_agreement":null},{"id":"W4387903656","doi":"10.3390/designs7060120","title":"Correction: Gurrola Arrieta, M.d.J.; Botez, R.M. Improved Local Scale Generic Cycle Model for Aerothermodynamic Simulations of Gas Turbine Engines for Propulsion. Designs 2022, 6, 91","year":2023,"lang":"en","type":"article","venue":"Designs","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure","funders":"","keywords":"Gas turbines; Aerospace engineering; Propulsion; Scale (ratio); Turbine; Marine propulsion; Physics; Mechanical engineering; Engineering","score_opus":0.028059576832048724,"score_gpt":0.2597519138093122,"score_spread":0.23169233697726344,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4387903656","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.059673432,0.00004755079,0.93749833,0.00022164402,0.000272199,0.0016433658,0.00012022268,0.00045602917,0.00006722067],"genre_scores_gemma":[0.9205843,0.000025553598,0.075454876,0.000050912327,0.000045569257,0.000647808,0.000072278104,0.00006496683,0.003053723],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9983647,0.000029173125,0.00037298625,0.00050844107,0.00022533165,0.0004993974],"domain_scores_gemma":[0.9990401,0.00026332482,0.00014828109,0.00040930978,0.000049898234,0.00008903206],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00022831718,0.00026364895,0.00030545105,0.00012723934,0.0002953738,0.000018722949,0.00028267608,0.00020131764,0.000070083544],"category_scores_gemma":[0.00015200784,0.00024174563,0.00016493189,0.0006654853,0.00026981073,0.00023241724,0.000094832256,0.0001337946,0.000020569352],"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":[0.000081595,0.00007219275,0.000078805686,0.000023307064,0.000013822436,7.2762055e-7,0.0000996329,0.5934085,0.38063997,0.000044462093,0.0026330713,0.022903895],"study_design_scores_gemma":[0.00071450847,0.00029235255,0.00019014871,0.000015014029,0.000037200778,0.0000035426765,0.00010434883,0.94351906,0.04366278,0.010830033,0.0003514879,0.00027950233],"about_ca_topic_score_codex":0.00002692723,"about_ca_topic_score_gemma":0.00009372755,"teacher_disagreement_score":0.86204344,"about_ca_system_score_codex":0.00016817014,"about_ca_system_score_gemma":0.000037282465,"threshold_uncertainty_score":0.98581004},"labels":[],"label_agreement":null},{"id":"W4387975000","doi":"10.5194/ar-2023-15","title":"Opinion: Eliminating aircraft soot emissions","year":2023,"lang":"en","type":"preprint","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Natural Sciences and Engineering Research Council of Canada; Eidgenössische Technische Hochschule Zürich; Schweizerischer Nationalfonds zur Förderung der Wissenschaftlichen Forschung; National Science Foundation","keywords":"Soot; NOx; Combustion; Pollutant; Environmental science; Combustor; Particulates; Chemistry","score_opus":0.04946838640854983,"score_gpt":0.3009243800260294,"score_spread":0.25145599361747956,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4387975000","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.028900584,0.0005872559,0.5442065,0.032829348,0.00794156,0.003049157,0.00012572517,0.023557309,0.3588026],"genre_scores_gemma":[0.67583203,0.0010965805,0.23821762,0.0006846158,0.0003630817,0.00051636476,0.00014419878,0.00021319011,0.08293232],"study_design_codex":"not_applicable","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.9981994,0.000026765838,0.00029506822,0.00072906236,0.00034842233,0.00040126554],"domain_scores_gemma":[0.99891394,0.00011749428,0.00012074243,0.00074003974,0.000007316935,0.00010045492],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.0001823234,0.00029121706,0.00025076407,0.00006962364,0.00019338397,0.000043016615,0.0007496516,0.00038820918,0.0023727373],"category_scores_gemma":[0.00026372567,0.00024970423,0.00012583593,0.00023547442,0.00022238257,0.000089347835,0.0042285323,0.0007126305,0.0028099641],"study_design_candidate":"not_applicable","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":[0.000021559019,0.00031999857,0.031004352,0.00031433345,0.0001110057,0.00018475724,0.0008352063,0.05635893,0.0117365755,0.00585184,0.45447516,0.43878627],"study_design_scores_gemma":[0.0007862958,0.00023886227,0.04412868,0.0010298362,0.00006626285,0.000040668987,0.0027322625,0.031289227,0.02115328,0.6301947,0.26453948,0.0038004455],"about_ca_topic_score_codex":0.00014752416,"about_ca_topic_score_gemma":0.000032171745,"teacher_disagreement_score":0.6469314,"about_ca_system_score_codex":0.00017176919,"about_ca_system_score_gemma":0.000020001737,"threshold_uncertainty_score":0.9999955},"labels":[],"label_agreement":null},{"id":"W4388107690","doi":"10.1115/1.4063934","title":"Aerodynamics and Flowfield of Distributed Electric Propulsion Tiltwing During Transition With Deflected Trailing-Edge Flap","year":2023,"lang":"en","type":"article","venue":"Journal of Fluids Engineering","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":3,"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":"Stall (fluid mechanics); Lift coefficient; Wing; Wing loading; Angle of attack; Vortex lift; Wing twist; Mechanics; Wingtip vortices; Trailing edge; Aerodynamics; Leading edge; Airfoil; Aerospace engineering; Lift-to-drag ratio; Deflection (physics); Physics; Engineering; Optics; Vortex; Horseshoe vortex; Turbulence; Vorticity; Reynolds number","score_opus":0.004469445896320751,"score_gpt":0.18539695311749613,"score_spread":0.18092750722117537,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4388107690","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":[0.87603635,0.00007029418,0.123648845,0.000055394266,0.000033263685,0.00006135332,0.0000016417705,0.00008101695,0.000011837122],"genre_scores_gemma":[0.99403006,0.000119332166,0.005809197,0.0000021275646,0.000016867694,0.0000016419741,0.0000018316703,0.000012970519,0.00000595516],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99930286,0.000007456883,0.00023622093,0.00009660549,0.0001798896,0.00017695296],"domain_scores_gemma":[0.9997662,0.00003571074,0.0000683833,0.00007073443,0.000015842465,0.000043179913],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000114303075,0.00010331636,0.00016979764,0.00014500011,0.000042246622,0.000008996951,0.00009100702,0.00006023974,0.00000580538],"category_scores_gemma":[0.000063528845,0.0000810019,0.000036630885,0.0006558425,0.000024927278,0.00020537674,0.000022605065,0.00019858118,9.4620964e-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":[0.000036993857,0.000010984449,0.00095690857,0.00004324629,0.0000115283065,0.00003814976,0.00012184841,0.09492418,0.90133595,0.000010021214,0.000006197437,0.0025039967],"study_design_scores_gemma":[0.0014721472,0.0009218261,0.10884854,0.00042041676,0.00007826757,0.00047068848,0.00024288011,0.29239467,0.5944927,0.00020489104,0.00005095415,0.0004020171],"about_ca_topic_score_codex":0.0000019984157,"about_ca_topic_score_gemma":0.0000017062239,"teacher_disagreement_score":0.30684325,"about_ca_system_score_codex":0.00005472044,"about_ca_system_score_gemma":0.000005987084,"threshold_uncertainty_score":0.33031616},"labels":[],"label_agreement":null},{"id":"W4388669109","doi":"10.1088/1742-6596/2633/1/011001","title":"Preface","year":2023,"lang":"en","type":"article","venue":"Journal of Physics Conference Series","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Astronautics; Aerospace; Engineering; Aeronautics; China; Globe; Aviation; Engineering management; Library science; Engineering ethics; Aerospace engineering; Political science; Computer science","score_opus":0.02688936405653916,"score_gpt":0.24975522439168318,"score_spread":0.22286586033514402,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4388669109","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":[0.8696918,0.000052441825,0.10594293,0.0034231613,0.0005894871,0.00017529039,0.000008307276,0.00040210926,0.019714499],"genre_scores_gemma":[0.9957281,0.00014205601,0.002666565,0.0000291782,0.000044973116,0.0000015289114,5.2837476e-7,0.0000066330686,0.0013804665],"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9993797,0.000013824597,0.00015843315,0.000079377074,0.0002171868,0.00015147623],"domain_scores_gemma":[0.99964154,0.000026472335,0.00014982594,0.00011876098,0.000025493291,0.000037895163],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000099643796,0.000078507015,0.00013076088,0.000023115383,0.000058033052,0.000024562902,0.00025475296,0.000031830878,0.00021137451],"category_scores_gemma":[0.000050056387,0.00006139506,0.000049750473,0.000306558,0.00020291115,0.0006319894,0.00011399128,0.00014172756,0.00030010784],"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":[0.00006296886,0.00006899191,0.010282657,0.000016072769,0.00003583846,0.00009584524,0.0011780241,0.0029321865,0.21841747,0.038207766,0.010906152,0.717796],"study_design_scores_gemma":[0.00026363423,0.0003527042,0.015663613,0.00003845325,0.000013942425,0.000042304047,0.0013914034,0.0001378072,0.52548295,0.43077958,0.025611244,0.00022236592],"about_ca_topic_score_codex":0.0000024224955,"about_ca_topic_score_gemma":0.000002924447,"teacher_disagreement_score":0.71757364,"about_ca_system_score_codex":0.000027669323,"about_ca_system_score_gemma":0.000017970835,"threshold_uncertainty_score":0.38573793},"labels":[],"label_agreement":null},{"id":"W4388821914","doi":"10.1007/978-3-031-39767-7_5","title":"A Unified Hybrid Control Approach to Maximum Endurance of Aircraft","year":2023,"lang":"en","type":"book-chapter","venue":"Advances in industrial control","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Concordia University","funders":"","keywords":"Turbofan; Turboprop; Climb; Cruise; Turbojet; Runway; Aerospace engineering; Engineering; Computer science; Aeronautics; Automotive engineering","score_opus":0.027957611105411413,"score_gpt":0.23673809452042044,"score_spread":0.20878048341500902,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4388821914","genre_codex":"other","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"other","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0003600752,0.0016544586,0.07506135,0.000888347,0.0019435033,0.006303694,0.0011001785,0.00092873746,0.9117597],"genre_scores_gemma":[0.8800572,0.0011215156,0.0034360106,0.00091648655,0.0005741543,0.0007587302,0.0000677311,0.00031492466,0.11275322],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9964788,0.000065422275,0.0010118105,0.001034186,0.0007053753,0.00070438685],"domain_scores_gemma":[0.99790823,0.00052437844,0.0005475937,0.0008270993,0.000031329844,0.00016135648],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00046665224,0.00065360655,0.0012949198,0.00031649406,0.000082137325,0.000020351781,0.0010455527,0.0006503527,0.0002855985],"category_scores_gemma":[0.0005158119,0.000630039,0.00023358004,0.000290722,0.00060932804,0.0003783055,0.00022649062,0.0011654064,0.0004025498],"study_design_candidate":"design_other","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":[0.0042788805,0.00040620894,0.003939975,0.00015568269,0.0003775407,0.0004539707,0.0001555714,0.12362534,0.00282714,0.12172945,0.009895599,0.73215467],"study_design_scores_gemma":[0.015966725,0.00082063285,0.00020692116,0.00057422393,0.000195652,0.000026277336,0.000101099016,0.0010851132,0.00087152305,0.28552264,0.6924474,0.0021817647],"about_ca_topic_score_codex":0.00004956372,"about_ca_topic_score_gemma":0.000055392004,"teacher_disagreement_score":0.87969714,"about_ca_system_score_codex":0.00033145497,"about_ca_system_score_gemma":0.000055079407,"threshold_uncertainty_score":0.9996151},"labels":[],"label_agreement":null},{"id":"W4388861606","doi":"10.5194/ar-2023-15-rc1","title":"Comment on ar-2023-15","year":2023,"lang":"en","type":"peer-review","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Natural Sciences and Engineering Research Council of Canada; Eidgenössische Technische Hochschule Zürich; Schweizerischer Nationalfonds zur Förderung der Wissenschaftlichen Forschung; National Science Foundation","keywords":"Soot; NOx; Pollutant; Combustion; Environmental science; Particulates; Radiative forcing; Atmospheric sciences; Meteorology; Aerosol; Chemistry; Physics","score_opus":0.04291062927988296,"score_gpt":0.2984492002144269,"score_spread":0.2555385709345439,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4388861606","genre_codex":"commentary","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"other","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0000019282418,0.0024881205,0.0009814921,0.57950556,0.0018539642,0.00090700045,0.00014502225,0.0015059557,0.41261098],"genre_scores_gemma":[0.000021282827,0.01226765,0.0016456067,0.06524339,0.00006504661,0.0001738571,0.00023142101,0.00005338992,0.92029834],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.99820155,0.000030391833,0.00026795865,0.00056449557,0.0005611708,0.00037446307],"domain_scores_gemma":[0.99892884,0.00013090274,0.00010938204,0.0007557056,0.0000055975843,0.00006959311],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.00021124777,0.00033119126,0.00041865368,0.000054688142,0.000086098225,0.000015768124,0.0006712173,0.00023695442,0.015658593],"category_scores_gemma":[0.00014827293,0.0002493113,0.00014042879,0.0003616812,0.00016711399,0.000044642948,0.0005954948,0.0004916853,0.03729929],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000012276304,0.00003019602,0.000009901785,0.00011448979,0.000009753237,0.000021456079,0.0000016789747,0.000017465414,0.0000055118044,0.00029326652,0.9660059,0.033489104],"study_design_scores_gemma":[0.00007078297,0.00008677999,0.00003310088,0.00064939563,0.000020960348,0.0000017523241,0.000009666546,0.000013576107,0.000099052035,0.0036186588,0.99508363,0.000312621],"about_ca_topic_score_codex":0.0001950669,"about_ca_topic_score_gemma":0.00015496316,"teacher_disagreement_score":0.51426214,"about_ca_system_score_codex":0.0002684583,"about_ca_system_score_gemma":0.000008276954,"threshold_uncertainty_score":0.9999959},"labels":[],"label_agreement":null},{"id":"W4389191896","doi":"10.22215/etd/2023-15782","title":"Thermo-Elastic mechanics of Morphing Lattice Structures with Application in Shape Optimization of BLI Engine Intakes","year":2023,"lang":"en","type":"dissertation","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Carleton University","funders":"Mitacs","keywords":"Morphing; Mechanics; Materials science; Pressure drop; Duct (anatomy); Offset (computer science); Aerodynamics; Airflow; Mechanical engineering; Structural engineering; Engineering; Physics; Computer science; Anatomy","score_opus":0.008764255102329503,"score_gpt":0.2282010503405872,"score_spread":0.2194367952382577,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4389191896","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":[0.5791429,0.000091949034,0.41741896,0.000030879353,0.00009214018,0.0008522201,0.000013418702,0.00029010337,0.0020673797],"genre_scores_gemma":[0.96426797,0.000100875135,0.035181902,0.0000049365863,0.0000043309938,0.000043774082,0.00016598203,0.00003274387,0.00019748598],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9990882,0.000012439017,0.0002807824,0.00025608155,0.00024103581,0.00012146219],"domain_scores_gemma":[0.99941146,0.0000770957,0.00027353506,0.00020441737,0.000018727995,0.000014783229],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00007689631,0.00016112455,0.00022625425,0.00014935144,0.000021202004,0.000004961973,0.00022153363,0.00017868793,0.00023915835],"category_scores_gemma":[0.000065190274,0.00012840524,0.000024228892,0.0005805001,0.000041228028,0.00011139801,0.00003243741,0.00015103206,0.0000058829282],"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":[0.00009176608,0.000048171732,0.0006143942,0.00017321525,0.000023760045,0.000002057024,0.00051603315,0.90942204,0.027259039,0.004700794,0.000009421755,0.057139307],"study_design_scores_gemma":[0.00060011615,0.0002841584,0.014176559,0.00029121584,0.00010001615,0.0000025984784,0.0056186407,0.867972,0.07462039,0.035753082,0.00001382027,0.00056738674],"about_ca_topic_score_codex":0.0001758256,"about_ca_topic_score_gemma":0.00068772613,"teacher_disagreement_score":0.385125,"about_ca_system_score_codex":0.00005523171,"about_ca_system_score_gemma":0.0000109053335,"threshold_uncertainty_score":0.5236214},"labels":[],"label_agreement":null},{"id":"W4389490931","doi":"10.1139/dsa-2023-0014","title":"Taiwan solar-powered UAV flight endurance record","year":2023,"lang":"en","type":"article","venue":"Drone Systems and Applications","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":10,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"National Science and Technology Council","keywords":"Wingspan; Aeronautics; Solar powered; Flight test; Aerospace engineering; Environmental science; Meteorology; Engineering; Solar energy; Geography; Electrical engineering; Aerodynamics","score_opus":0.01253328722339466,"score_gpt":0.2327288606727313,"score_spread":0.22019557344933663,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4389490931","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":[0.42770934,0.0024676635,0.44557947,0.007496557,0.000876319,0.00709874,0.00028448136,0.0071842014,0.10130323],"genre_scores_gemma":[0.9935824,0.00015265882,0.00075110595,0.000028246084,0.00004679971,0.0005164007,0.000014723102,0.000013562019,0.004894054],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9992062,0.000012632532,0.00016210787,0.00029565048,0.00011309626,0.00021034945],"domain_scores_gemma":[0.9995372,0.000023509852,0.00005993955,0.00031715416,0.0000049308983,0.000057242323],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.000094573545,0.000099385376,0.00011908187,0.000034356668,0.00023603799,0.000030969917,0.00016150014,0.000064485655,0.000059112575],"category_scores_gemma":[0.000008448898,0.00008849043,0.000021669142,0.00042867614,0.00013324479,0.000107273685,0.000101670055,0.00007993832,0.0011474388],"study_design_candidate":"not_applicable","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":[0.000019400091,0.00029896115,0.046721503,0.00019964378,0.000058846817,0.000027418582,0.0008394118,0.0012633597,0.24272545,0.09482014,0.051983047,0.56104285],"study_design_scores_gemma":[0.00021294932,0.000034247376,0.013173875,0.000016113096,0.00000828906,0.000014143301,0.0007750138,0.0017372932,0.0010278454,0.0074371374,0.9752877,0.00027538728],"about_ca_topic_score_codex":0.000092954375,"about_ca_topic_score_gemma":0.000024888675,"teacher_disagreement_score":0.9233047,"about_ca_system_score_codex":0.000035575693,"about_ca_system_score_gemma":0.0000033922859,"threshold_uncertainty_score":0.9996303},"labels":[],"label_agreement":null},{"id":"W4389584793","doi":"10.17118/11143/20868","title":"Aerodynamic optimization of eVTOL rotor profiles","year":2023,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Concordia University","funders":"","keywords":"Aerodynamics; Rotor (electric); Computer science; Aerospace engineering; Control theory (sociology); Engineering; Mechanical engineering; Artificial intelligence","score_opus":0.010302476501441725,"score_gpt":0.22943873163490827,"score_spread":0.21913625513346655,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4389584793","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":[0.6298406,0.000012369921,0.32290015,0.00058888254,0.000112809896,0.00080879114,0.000008876204,0.0019425682,0.04378497],"genre_scores_gemma":[0.9564481,0.000020652564,0.04073525,0.000017122004,0.0000028526233,0.0000306783,0.000005841175,0.0000061959145,0.00273332],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999601,0.0000061816736,0.00008265688,0.00011123559,0.0000984109,0.00010051127],"domain_scores_gemma":[0.9998139,0.000017313081,0.000027938557,0.00012551004,0.0000025684194,0.000012731485],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00004629841,0.000045337256,0.000054813885,0.000029395482,0.000026296695,0.0000027033905,0.0001102454,0.000032682783,0.0011040036],"category_scores_gemma":[0.00003593143,0.00003597461,0.000016441752,0.0003342596,0.00009004409,0.000096566335,0.00008890546,0.000026474381,0.0003612851],"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":[0.000011787828,0.000053155934,0.037641656,0.000016962329,0.0000074337836,0.0000058270452,0.00008860907,0.7922677,0.13125764,0.002286454,0.0048611686,0.031501602],"study_design_scores_gemma":[0.00051904813,0.0002128656,0.09070174,0.000023090664,0.000010485162,0.0000039911793,0.0006431917,0.7679251,0.12650238,0.010828678,0.0021950174,0.0004344091],"about_ca_topic_score_codex":0.000017073227,"about_ca_topic_score_gemma":0.000007604088,"teacher_disagreement_score":0.3266075,"about_ca_system_score_codex":0.000021542826,"about_ca_system_score_gemma":0.0000018332352,"threshold_uncertainty_score":0.99980915},"labels":[],"label_agreement":null},{"id":"W4390977476","doi":"10.1002/gch2.202300205","title":"Thermodynamics, Environmental and Sustainability Impacts of a Turbofan Engine Under Different Design Conditions Considering Variable Needs in the Aviation Industry","year":2024,"lang":"en","type":"article","venue":"Global Challenges","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":13,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Ministry of Education and Child Care","funders":"","keywords":"Exergy; Turbofan; Combustor; Environmental science; Sustainability; Gas compressor; Thermodynamics; Automotive engineering; Engineering; Process engineering; Chemistry; Mechanical engineering; Physics; Combustion","score_opus":0.016824190091391338,"score_gpt":0.24665409321178275,"score_spread":0.22982990312039142,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4390977476","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":[0.9836527,0.0027419082,0.010113074,0.0021980156,0.000038320475,0.00035784452,0.000036887403,0.00008210658,0.000779119],"genre_scores_gemma":[0.9989888,0.000644151,0.00028556597,0.0000308312,0.0000068393642,0.000026289295,0.0000043248488,0.000005543303,0.000007659635],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.99925697,0.000073909,0.00013810126,0.00019240775,0.00014214337,0.00019647536],"domain_scores_gemma":[0.99961615,0.00015178032,0.000028832033,0.00017044609,0.0000021362614,0.00003064172],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00019407517,0.00012706926,0.00011661487,0.000034324185,0.00004746628,0.000020130217,0.00011816032,0.0001455596,0.00007206647],"category_scores_gemma":[0.000036878875,0.00008989469,0.000021130147,0.00013732254,0.00026866753,0.00015131358,0.0001011068,0.00021625348,0.0000030963047],"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":[0.00016659906,0.0018201965,0.17244592,0.0008763834,0.0002914627,0.00019706899,0.016704936,0.06295092,0.0453458,0.5284069,0.00037160094,0.1704222],"study_design_scores_gemma":[0.00031141308,0.00017949744,0.3639631,0.000059563114,0.000029569164,0.000046014982,0.022101453,0.00611221,0.0006621867,0.606158,0.0001379889,0.00023896845],"about_ca_topic_score_codex":0.00005797619,"about_ca_topic_score_gemma":0.000043864202,"teacher_disagreement_score":0.19151717,"about_ca_system_score_codex":0.00038756797,"about_ca_system_score_gemma":0.0000129592,"threshold_uncertainty_score":0.3665799},"labels":[],"label_agreement":null},{"id":"W4391300999","doi":"10.2514/6.2024-1538","title":"System Integration Study for a Hybrid-Electric Commuter Aircraft Concept with a Solar Auxiliary Power System","year":2024,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Concordia University","funders":"","keywords":"Auxiliary power unit; Aerospace engineering; Power (physics); Electric power system; Computer science; Hybrid power; Automotive engineering; Electrical engineering; Engineering; Physics; Voltage","score_opus":0.008350815686289889,"score_gpt":0.227031294366191,"score_spread":0.2186804786799011,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4391300999","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":[0.114101596,0.00026305552,0.8755003,0.00018778337,0.00022707245,0.002354745,0.000015237137,0.0026677654,0.004682448],"genre_scores_gemma":[0.993274,0.0000013882238,0.005193169,0.000049113125,0.000018218847,0.00042056033,0.000005842823,0.00003334162,0.0010043739],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99861884,0.000054271062,0.0002508068,0.0004872815,0.00026785964,0.00032095987],"domain_scores_gemma":[0.9993854,0.00011802859,0.000043963006,0.0003838905,0.000015394799,0.000053327258],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023123954,0.00023124999,0.00023777054,0.00008863151,0.00017092377,0.00010593987,0.0002915923,0.00006120379,0.00007148808],"category_scores_gemma":[0.000013948415,0.00014929191,0.00006645572,0.0004045477,0.00009236528,0.0003664936,0.000098821765,0.00018717111,0.00019932562],"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":[0.0018688873,0.0041079656,0.0452177,0.002919775,0.002173914,0.0046057533,0.01898335,0.006859003,0.090398,0.15570892,0.12249478,0.54466194],"study_design_scores_gemma":[0.0072833626,0.018682146,0.007340602,0.0022948212,0.000822556,0.0019897635,0.1541257,0.5866237,0.1848657,0.0021095087,0.029532254,0.004329879],"about_ca_topic_score_codex":0.00009547152,"about_ca_topic_score_gemma":0.000053843436,"teacher_disagreement_score":0.8791724,"about_ca_system_score_codex":0.00051096274,"about_ca_system_score_gemma":0.000018307152,"threshold_uncertainty_score":0.60879475},"labels":[],"label_agreement":null},{"id":"W4391330108","doi":"10.2514/6.2024-2313","title":"Design and performances of a Turbo-Electric and Distributed Propulsion aircraft in the Small and Medium Range segment: intermediate results from the European project IMOTHEP","year":2024,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Safran Electronics (Canada)","funders":"European Commission","keywords":"Propulsion; Turbofan; Electrically powered spacecraft propulsion; Automotive engineering; Aerospace engineering; Conceptual design; Engineering; Range (aeronautics); Computer science; Aeronautics; Mechanical engineering","score_opus":0.017906338142563802,"score_gpt":0.2224474856899026,"score_spread":0.20454114754733882,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4391330108","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":[0.9894566,0.0012557696,0.0062223924,0.0015828355,0.00003379291,0.0007921693,0.000029622499,0.000098495104,0.0005283222],"genre_scores_gemma":[0.99675286,0.0015842286,0.0015150702,0.000060287686,0.000014566667,0.0000208548,0.000007495312,0.00000836322,0.00003626148],"study_design_codex":"design_other","study_design_gemma":"observational","domain_scores_codex":[0.999001,0.00020188269,0.0001964921,0.0002961894,0.00013472486,0.00016966408],"domain_scores_gemma":[0.99937636,0.00039656626,0.000043965698,0.0001617475,0.000002976718,0.00001839682],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0007853421,0.00012954169,0.000111405985,0.00004162094,0.00007797652,0.00005747066,0.00021212803,0.00003682961,0.0000061901364],"category_scores_gemma":[0.00008601222,0.000058946905,0.000012838101,0.00031714025,0.00033103916,0.00014782973,0.00019524767,0.00017755784,0.0000034805419],"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":[0.00053447,0.00012557273,0.07455187,0.0001116724,0.000047916994,0.00011801853,0.01601776,0.00009642687,0.03808877,0.000045780795,0.0024092689,0.86785245],"study_design_scores_gemma":[0.0021383786,0.0009340046,0.9334307,0.0003525578,0.000071776354,0.00006216973,0.003911472,0.03397394,0.016982514,0.0049857264,0.0026775536,0.0004792242],"about_ca_topic_score_codex":0.00027705112,"about_ca_topic_score_gemma":0.00012639062,"teacher_disagreement_score":0.8673732,"about_ca_system_score_codex":0.000020395579,"about_ca_system_score_gemma":0.000006997173,"threshold_uncertainty_score":0.2403785},"labels":[],"label_agreement":null},{"id":"W4391857844","doi":"10.33737/gpps23-tc-080","title":"Deriving Sensitivities of Distributed Propeller Propulsion in Overwing Configuration by using DoE in CFD Simulations","year":2023,"lang":"en","type":"article","venue":"Proceedings","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Innovation Cluster (Canada)","funders":"Technische Universiteit Delft; Deutsche Forschungsgemeinschaft","keywords":"Propeller; Wing; Chord (peer-to-peer); Advance ratio; Propulsion; Angle of attack; Computational fluid dynamics; Airfoil; Lift-to-drag ratio; Trailing edge; Aerodynamics; Aerospace engineering; Marine engineering; Lift (data mining); Engineering; Blade pitch; Drag; Wing configuration; Structural engineering; Computer science; Turbine","score_opus":0.019657506189451827,"score_gpt":0.2506240763711641,"score_spread":0.23096657018171224,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4391857844","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":[0.9978934,0.000008251805,0.0012642823,0.00012256984,0.00001521517,0.00025719186,0.000008240656,0.000107641616,0.00032319227],"genre_scores_gemma":[0.99915993,0.000009116771,0.00073870696,0.000008846695,0.0000041167914,0.000008382459,0.000012754402,0.000008858653,0.00004931366],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99926347,0.0000057967372,0.00019853596,0.00018864626,0.0001497245,0.00019383094],"domain_scores_gemma":[0.99982625,0.000031054493,0.00007581412,0.00004099407,0.0000110289675,0.0000148652425],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012757668,0.000084870946,0.000115327486,0.000081415325,0.00005387589,0.000016219063,0.000063485844,0.000060136652,0.00002543143],"category_scores_gemma":[0.0001672335,0.000079516394,0.000013482205,0.00078612467,0.00009254656,0.00044926925,0.000088877205,0.000095698706,0.000007922459],"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":[0.000008268207,0.000025431566,0.1325514,0.000025483476,0.0000011292282,0.0000024213966,0.00065969495,0.0077973064,0.8542283,0.000047704965,0.000088780616,0.0045640534],"study_design_scores_gemma":[0.0005484713,0.000055179815,0.0806924,0.0002929761,0.000005862421,0.000003993036,0.0033950661,0.44514534,0.46520227,0.004017087,0.00030958763,0.00033176446],"about_ca_topic_score_codex":0.0001294944,"about_ca_topic_score_gemma":0.000021305841,"teacher_disagreement_score":0.43734804,"about_ca_system_score_codex":0.00013820293,"about_ca_system_score_gemma":0.0000048991064,"threshold_uncertainty_score":0.32425842},"labels":[],"label_agreement":null},{"id":"W4391916408","doi":"","title":"Stratégie fréquentielle adaptative pour une alimentation hybride à base de pile à combustible, supercondensateurs et batteries pour un drone de grande endurance.","year":2023,"lang":"fr","type":"article","venue":"HAL (Le Centre pour la Communication Scientifique Directe)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Institut National d'Excellence en Santé et en Services Sociaux","funders":"","keywords":"Pile; Engineering; Structural engineering","score_opus":0.021072183291184703,"score_gpt":0.24432923461791267,"score_spread":0.22325705132672796,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4391916408","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":[0.5761864,0.0011011955,0.34304407,0.068477586,0.00022726206,0.00054488034,0.00025832636,0.00067712343,0.009483137],"genre_scores_gemma":[0.8894119,0.0043934803,0.08304269,0.0005588419,0.000017988603,0.00010339571,0.0002963446,0.000075436656,0.022099882],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99323285,0.0038131732,0.00058536563,0.00085313595,0.0005142652,0.0010012101],"domain_scores_gemma":[0.99614334,0.0019165785,0.00032348276,0.0010508847,0.00027109345,0.00029461048],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.0035730593,0.00046864885,0.00039728792,0.00020933649,0.000770036,0.00027791338,0.0009537636,0.0002490406,0.0017798133],"category_scores_gemma":[0.00088474434,0.0005411883,0.00018585178,0.0013600653,0.0011662628,0.00081576395,0.00051463256,0.0005973413,0.00083921495],"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":[0.00009775156,0.001512591,0.026899986,0.0002013913,0.00022320304,0.0002601083,0.021303928,0.005431833,0.64396477,0.123311296,0.015490884,0.16130225],"study_design_scores_gemma":[0.0021300511,0.000006230108,0.058000665,0.0009332787,0.00012136645,0.00008705229,0.009894141,0.033722345,0.8030337,0.08517452,0.006018221,0.00087840186],"about_ca_topic_score_codex":0.005494047,"about_ca_topic_score_gemma":0.0033523806,"teacher_disagreement_score":0.31322554,"about_ca_system_score_codex":0.00048546214,"about_ca_system_score_gemma":0.00024905967,"threshold_uncertainty_score":0.9999387},"labels":[],"label_agreement":null},{"id":"W4392367249","doi":"10.32920/25336327.v1","title":"Prediction Model Validation for Circular Flight Paths for CREATeV","year":2024,"lang":"en","type":"preprint","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Flight test; Power (physics); Renewable energy; Aerospace engineering; Position (finance); Model validation; Simulation; Computer science; Engineering; Electrical engineering; Physics","score_opus":0.03494839569492215,"score_gpt":0.2618950676299619,"score_spread":0.22694667193503976,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4392367249","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0074263443,0.00009987153,0.9833485,0.00052177155,0.00038341392,0.0019380647,0.00035080255,0.0009240436,0.0050071864],"genre_scores_gemma":[0.7700195,0.00014250599,0.2150785,0.000095541756,0.00012476016,0.0036791333,0.000534697,0.000083287865,0.010242085],"study_design_codex":"simulation_or_modeling","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.99868435,0.0000069397884,0.000239271,0.0006649567,0.00017032062,0.00023416075],"domain_scores_gemma":[0.9994433,0.000043016793,0.000072212475,0.00038881451,0.000014913505,0.000037727412],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017276972,0.00022169869,0.00018676769,0.000057565165,0.00009414204,0.000057179062,0.00025276636,0.0003697654,0.00007839956],"category_scores_gemma":[0.00006376441,0.00018988042,0.00018160805,0.00006777691,0.000071449336,0.00009075772,0.0005465158,0.00020086876,0.00006873704],"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":[0.00007617425,0.00015787315,0.00031297322,0.0010175398,0.000134996,0.0000034973887,0.0003044255,0.7930567,0.068801805,0.0230567,0.044433277,0.068643995],"study_design_scores_gemma":[0.00011781745,0.000041442207,0.000012950224,0.000029773237,0.00005960737,8.674157e-7,0.000022085535,0.44745094,0.039653704,0.5078681,0.004575807,0.00016692726],"about_ca_topic_score_codex":0.000013348661,"about_ca_topic_score_gemma":0.0000029998387,"teacher_disagreement_score":0.76827,"about_ca_system_score_codex":0.00026202225,"about_ca_system_score_gemma":0.00001998934,"threshold_uncertainty_score":0.7743099},"labels":[],"label_agreement":null},{"id":"W4392383245","doi":"10.32920/25336327","title":"Prediction Model Validation for Circular Flight Paths for CREATeV","year":2024,"lang":"en","type":"preprint","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Toronto Metropolitan University","funders":"","keywords":"Flight test; Power (physics); Position (finance); Renewable energy; Aerospace engineering; Heading (navigation); Simulation; Computer science; Engineering; Electrical engineering; Physics","score_opus":0.03494839569492215,"score_gpt":0.2618950676299619,"score_spread":0.22694667193503976,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4392383245","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0074263443,0.00009987153,0.9833485,0.00052177155,0.00038341392,0.0019380647,0.00035080255,0.0009240436,0.0050071864],"genre_scores_gemma":[0.7700195,0.00014250599,0.2150785,0.000095541756,0.00012476016,0.0036791333,0.000534697,0.000083287865,0.010242085],"study_design_codex":"simulation_or_modeling","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.99868435,0.0000069397884,0.000239271,0.0006649567,0.00017032062,0.00023416075],"domain_scores_gemma":[0.9994433,0.000043016793,0.000072212475,0.00038881451,0.000014913505,0.000037727412],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017276972,0.00022169869,0.00018676769,0.000057565165,0.00009414204,0.000057179062,0.00025276636,0.0003697654,0.00007839956],"category_scores_gemma":[0.00006376441,0.00018988042,0.00018160805,0.00006777691,0.000071449336,0.00009075772,0.0005465158,0.00020086876,0.00006873704],"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":[0.00007617425,0.00015787315,0.00031297322,0.0010175398,0.000134996,0.0000034973887,0.0003044255,0.7930567,0.068801805,0.0230567,0.044433277,0.068643995],"study_design_scores_gemma":[0.00011781745,0.000041442207,0.000012950224,0.000029773237,0.00005960737,8.674157e-7,0.000022085535,0.44745094,0.039653704,0.5078681,0.004575807,0.00016692726],"about_ca_topic_score_codex":0.000013348661,"about_ca_topic_score_gemma":0.0000029998387,"teacher_disagreement_score":0.76827,"about_ca_system_score_codex":0.00026202225,"about_ca_system_score_gemma":0.00001998934,"threshold_uncertainty_score":0.7743099},"labels":[],"label_agreement":null},{"id":"W4393476566","doi":"10.5281/zenodo.10385726","title":"Nieuport 12 - First World War Airplane","year":2017,"lang":"en","type":"dataset","venue":"Zenodo (CERN European Organization for Nuclear Research)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Airplane; Aeronautics; Engineering; Aerospace engineering","score_opus":0.030506811926566374,"score_gpt":0.2505227079321022,"score_spread":0.2200158960055358,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4393476566","genre_codex":"dataset","genre_gemma":"dataset","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"dataset","genre_consensus":"dataset","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.000053689404,0.00009892046,0.00038121143,0.0007059229,0.0002534651,0.0006587071,0.91729474,0.001426099,0.07912722],"genre_scores_gemma":[0.0008560453,0.0006630173,0.0002692943,0.00013040937,0.00013642033,1.1678012e-7,0.9906938,0.0009588547,0.006292031],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.9977931,0.00009370571,0.00028156865,0.00073196227,0.0005554388,0.0005442486],"domain_scores_gemma":[0.9978664,0.000023695682,0.00028221263,0.0016043084,0.000045106524,0.00017830399],"candidate_categories":["metaepi_narrow","sts","insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.0004031497,0.00030441704,0.00027243636,0.00021497149,0.003685497,0.00045864697,0.0033197855,0.00019361528,0.075293474],"category_scores_gemma":[0.0006173409,0.00030397734,0.00007440526,0.00026604402,0.0006715576,0.00033660216,0.0041113286,0.0006813778,0.084714726],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000021007347,0.00007936662,0.000005170175,0.00004454967,0.000020694659,0.00009059893,0.00002686579,0.00004223014,0.00004832797,0.000019188312,0.9781404,0.021461587],"study_design_scores_gemma":[0.00022590767,0.00012306588,0.00027050838,0.000051407507,0.000022229722,0.000090560425,0.000023591756,0.000016438129,0.00004943673,0.0002032044,0.998573,0.00035062977],"about_ca_topic_score_codex":0.00015372391,"about_ca_topic_score_gemma":0.000049264436,"teacher_disagreement_score":0.073399045,"about_ca_system_score_codex":0.00031018545,"about_ca_system_score_gemma":0.0000020718485,"threshold_uncertainty_score":0.99994123},"labels":[],"label_agreement":null},{"id":"W4393612039","doi":"10.5281/zenodo.10234308","title":"Bristol F.2B - First World War Airplane","year":2017,"lang":"en","type":"dataset","venue":"Zenodo (CERN European Organization for Nuclear Research)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Airplane; Aeronautics; Geography; History; Engineering; Aerospace engineering","score_opus":0.027552415108774247,"score_gpt":0.2498015598332875,"score_spread":0.22224914472451326,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4393612039","genre_codex":"dataset","genre_gemma":"dataset","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"dataset","genre_consensus":"dataset","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.00005804736,0.000120754215,0.0004921886,0.0007692772,0.00023147493,0.0006276142,0.94880825,0.001330262,0.047562145],"genre_scores_gemma":[0.0010398041,0.0005256274,0.00028779227,0.0001314457,0.00012730295,1.1269633e-7,0.9919834,0.00095878984,0.0049457178],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.99784166,0.00011400823,0.00026920976,0.00072371354,0.0005265055,0.0005249124],"domain_scores_gemma":[0.9979045,0.000027096692,0.00027987416,0.0015643411,0.000051697407,0.00017252933],"candidate_categories":["metaepi_narrow","sts","insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.00035517995,0.0002997122,0.00027244102,0.00021216202,0.0039607254,0.000511987,0.0034535192,0.0001895338,0.05571844],"category_scores_gemma":[0.00071242487,0.00030471018,0.00007332765,0.0003315141,0.0007238332,0.00032153653,0.004035022,0.00069284823,0.1229377],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000023406992,0.00007732183,0.0000030089561,0.000046363122,0.000018879931,0.00008055323,0.000028226515,0.00004338869,0.000055356555,0.00001753707,0.9797079,0.019898085],"study_design_scores_gemma":[0.0002572132,0.00011783301,0.00014556675,0.0000525535,0.00002171393,0.00008460504,0.000023913839,0.000028466653,0.00005360256,0.00022956783,0.99863267,0.00035229107],"about_ca_topic_score_codex":0.00014712721,"about_ca_topic_score_gemma":0.00003388267,"teacher_disagreement_score":0.067219265,"about_ca_system_score_codex":0.00035810066,"about_ca_system_score_gemma":0.000001937051,"threshold_uncertainty_score":0.9999405},"labels":[],"label_agreement":null},{"id":"W4393891457","doi":"10.5281/zenodo.10385725","title":"Nieuport 12 - First World War Airplane","year":2017,"lang":"en","type":"dataset","venue":"Zenodo (CERN European Organization for Nuclear Research)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Airplane; Aeronautics; History; Geography; Engineering; Aerospace engineering","score_opus":0.030506811926566374,"score_gpt":0.2505227079321022,"score_spread":0.2200158960055358,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4393891457","genre_codex":"dataset","genre_gemma":"dataset","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"dataset","genre_consensus":"dataset","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.000053689404,0.00009892046,0.00038121143,0.0007059229,0.0002534651,0.0006587071,0.91729474,0.001426099,0.07912722],"genre_scores_gemma":[0.0008560453,0.0006630173,0.0002692943,0.00013040937,0.00013642033,1.1678012e-7,0.9906938,0.0009588547,0.006292031],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.9977931,0.00009370571,0.00028156865,0.00073196227,0.0005554388,0.0005442486],"domain_scores_gemma":[0.9978664,0.000023695682,0.00028221263,0.0016043084,0.000045106524,0.00017830399],"candidate_categories":["metaepi_narrow","sts","insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.0004031497,0.00030441704,0.00027243636,0.00021497149,0.003685497,0.00045864697,0.0033197855,0.00019361528,0.075293474],"category_scores_gemma":[0.0006173409,0.00030397734,0.00007440526,0.00026604402,0.0006715576,0.00033660216,0.0041113286,0.0006813778,0.084714726],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000021007347,0.00007936662,0.000005170175,0.00004454967,0.000020694659,0.00009059893,0.00002686579,0.00004223014,0.00004832797,0.000019188312,0.9781404,0.021461587],"study_design_scores_gemma":[0.00022590767,0.00012306588,0.00027050838,0.000051407507,0.000022229722,0.000090560425,0.000023591756,0.000016438129,0.00004943673,0.0002032044,0.998573,0.00035062977],"about_ca_topic_score_codex":0.00015372391,"about_ca_topic_score_gemma":0.000049264436,"teacher_disagreement_score":0.073399045,"about_ca_system_score_codex":0.00031018545,"about_ca_system_score_gemma":0.0000020718485,"threshold_uncertainty_score":0.99994123},"labels":[],"label_agreement":null},{"id":"W4394041342","doi":"10.5281/zenodo.10234307","title":"Bristol F.2B - First World War Airplane","year":2017,"lang":"en","type":"dataset","venue":"Zenodo (CERN European Organization for Nuclear Research)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Airplane; Aeronautics; History; Engineering; Aerospace engineering","score_opus":0.027552415108774247,"score_gpt":0.2498015598332875,"score_spread":0.22224914472451326,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4394041342","genre_codex":"dataset","genre_gemma":"dataset","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"dataset","genre_consensus":"dataset","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.00005804736,0.000120754215,0.0004921886,0.0007692772,0.00023147493,0.0006276142,0.94880825,0.001330262,0.047562145],"genre_scores_gemma":[0.0010398041,0.0005256274,0.00028779227,0.0001314457,0.00012730295,1.1269633e-7,0.9919834,0.00095878984,0.0049457178],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.99784166,0.00011400823,0.00026920976,0.00072371354,0.0005265055,0.0005249124],"domain_scores_gemma":[0.9979045,0.000027096692,0.00027987416,0.0015643411,0.000051697407,0.00017252933],"candidate_categories":["metaepi_narrow","sts","insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.00035517995,0.0002997122,0.00027244102,0.00021216202,0.0039607254,0.000511987,0.0034535192,0.0001895338,0.05571844],"category_scores_gemma":[0.00071242487,0.00030471018,0.00007332765,0.0003315141,0.0007238332,0.00032153653,0.004035022,0.00069284823,0.1229377],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000023406992,0.00007732183,0.0000030089561,0.000046363122,0.000018879931,0.00008055323,0.000028226515,0.00004338869,0.000055356555,0.00001753707,0.9797079,0.019898085],"study_design_scores_gemma":[0.0002572132,0.00011783301,0.00014556675,0.0000525535,0.00002171393,0.00008460504,0.000023913839,0.000028466653,0.00005360256,0.00022956783,0.99863267,0.00035229107],"about_ca_topic_score_codex":0.00014712721,"about_ca_topic_score_gemma":0.00003388267,"teacher_disagreement_score":0.067219265,"about_ca_system_score_codex":0.00035810066,"about_ca_system_score_gemma":0.000001937051,"threshold_uncertainty_score":0.9999405},"labels":[],"label_agreement":null},{"id":"W4394601285","doi":"10.1080/02786826.2024.2316190","title":"Rapid assessment of jet engine-like soot from combustion of conventional and sustainable aviation fuels using flame spray pyrolysis","year":2024,"lang":"en","type":"article","venue":"Aerosol Science and Technology","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Carleton University; National Research Council Canada","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Jet fuel; Combustion; Soot; Pyrolysis; Jet (fluid); Environmental science; Waste management; Jet engine; Aviation; Aerospace engineering; Chemistry; Engineering; Organic chemistry","score_opus":0.010597940244597141,"score_gpt":0.25597316066736925,"score_spread":0.2453752204227721,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4394601285","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":[0.9782566,0.0005077586,0.02024026,0.00048732173,0.0000638767,0.0001655563,0.000008264565,0.00011736566,0.00015299469],"genre_scores_gemma":[0.98865354,0.00017514218,0.011098995,0.00001236125,0.0000043487757,0.000010193425,0.000002943944,0.000005109338,0.000037380974],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9988522,0.000011240332,0.00020957168,0.00036995995,0.00029950126,0.0002575493],"domain_scores_gemma":[0.9995806,0.000057700847,0.00009389805,0.00018698533,0.00005040219,0.000030417063],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00043599878,0.00010465134,0.00017539533,0.0002609604,0.00015745625,0.000028288443,0.00020428658,0.00011978796,0.000080073085],"category_scores_gemma":[0.00008618322,0.000090562746,0.000020616368,0.0013088931,0.0021050319,0.0004953723,0.00033571816,0.00012733585,0.000002016939],"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":[0.00000297101,0.00003152939,0.016315665,0.000027594806,0.000010766741,0.00000625827,0.000039929924,0.000062858584,0.94506633,0.017115736,0.00002240705,0.021297956],"study_design_scores_gemma":[0.00042474427,0.00032545527,0.0110088615,0.00008268364,0.00006354634,0.0000224155,0.0016010632,0.017073754,0.9141721,0.05451695,0.00044332325,0.00026509707],"about_ca_topic_score_codex":0.00010556551,"about_ca_topic_score_gemma":0.000010758077,"teacher_disagreement_score":0.037401214,"about_ca_system_score_codex":0.0001097108,"about_ca_system_score_gemma":0.000057696612,"threshold_uncertainty_score":0.7756078},"labels":[],"label_agreement":null},{"id":"W4396775211","doi":"10.1017/aer.2024.42","title":"Effects of distortion on a BLI fan","year":2024,"lang":"en","type":"article","venue":"The Aeronautical Journal","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":3,"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":"GKN Aerospace Services","keywords":"Distortion (music); Fan-out; Geology; Mathematics; Computer science; Telecommunications","score_opus":0.007170496853023384,"score_gpt":0.23689360108771773,"score_spread":0.22972310423469436,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4396775211","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":[0.89865154,0.0007711481,0.089735776,0.005070538,0.00048230623,0.000184603,0.0000011808087,0.00017461974,0.0049282564],"genre_scores_gemma":[0.99910545,0.00005853675,0.00044464946,0.000101572215,0.000037727856,0.000002744608,1.1504599e-7,0.0000060492484,0.0002431673],"study_design_codex":"design_other","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.999398,0.000035212983,0.00011305303,0.00008866387,0.00022554443,0.00013952682],"domain_scores_gemma":[0.9996391,0.00019777328,0.000023228833,0.00009811926,0.0000020098466,0.000039770057],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015422484,0.00006375804,0.00006959268,0.00002007981,0.00008058351,0.000020712503,0.00018615792,0.000034409044,0.00024441164],"category_scores_gemma":[0.000084204716,0.000033574895,0.000054131695,0.00012748789,0.00027548507,0.00007771504,0.00006243144,0.00029321655,0.0002655464],"study_design_candidate":"design_other","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":[0.0001096375,0.00022454355,0.0007295677,0.0000488477,0.00005298663,0.0002642763,0.00041708606,0.0004567212,0.158365,0.04734089,0.007442836,0.7845476],"study_design_scores_gemma":[0.0008154702,0.0019622454,0.103076644,0.00047718504,0.00016572172,0.0006502221,0.00017148994,0.0036250416,0.2963522,0.54911214,0.04312404,0.00046756575],"about_ca_topic_score_codex":0.0000017899456,"about_ca_topic_score_gemma":7.781599e-7,"teacher_disagreement_score":0.78408,"about_ca_system_score_codex":0.00008531239,"about_ca_system_score_gemma":0.000004884958,"threshold_uncertainty_score":0.34131503},"labels":[],"label_agreement":null},{"id":"W4396827656","doi":"10.2172/2348933","title":"Development of R&amp;D GREET 2023 Rev1 to Estimate Greenhouse Gas Emissions of Sustainable Aviation Fuels for 40B Provision of the Inflation Reduction Act","year":2024,"lang":"en","type":"report","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Cascades (Canada)","funders":"U.S. Department of Energy; Office of Energy Efficiency and Renewable Energy; University of Chicago; Argonne National Laboratory; Office of Energy Efficiency; Purdue University; U.S. Department of Agriculture","keywords":"Greenhouse gas; Aviation; Waste management; Environmental science; Natural resource economics; Sustainable development; Reduction (mathematics); Business; Environmental economics; Engineering; Economics; Political science; Law; Aerospace engineering","score_opus":0.03189249509617711,"score_gpt":0.32157175244318403,"score_spread":0.28967925734700695,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4396827656","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":[0.71260244,0.00042150333,0.23683803,0.0015629908,0.0012770469,0.012580741,0.00014146436,0.0006281634,0.033947613],"genre_scores_gemma":[0.6990921,0.00020200331,0.22088926,0.0000063442144,0.000041684958,0.00039210424,0.00012898218,0.000083125844,0.07916438],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9978937,0.000020696714,0.0007838624,0.00037732619,0.0006935182,0.00023092092],"domain_scores_gemma":[0.99862677,0.000048376238,0.0006532895,0.0004722496,0.00015828831,0.00004101731],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00066217943,0.00021085281,0.00033570785,0.00017786911,0.0001062993,0.000009547975,0.00029175798,0.00025229796,0.00010473176],"category_scores_gemma":[0.00068721554,0.00014353494,0.000120280805,0.0006375373,0.00011252236,0.00017781433,0.00043221394,0.00015259122,0.00001023599],"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":[0.00014556789,0.00026583637,0.001832858,0.0037664406,0.00010828771,0.0000025307634,0.0015772423,0.0061292094,0.64649045,0.0017145942,0.025566015,0.31240094],"study_design_scores_gemma":[0.00034148293,0.00035286063,0.008268086,0.0017219192,0.00021015166,0.00001872244,0.0012621981,0.00026189754,0.77606875,0.03304304,0.17780252,0.0006483893],"about_ca_topic_score_codex":0.00022672182,"about_ca_topic_score_gemma":0.00016585522,"teacher_disagreement_score":0.31175256,"about_ca_system_score_codex":0.00063410617,"about_ca_system_score_gemma":0.0003431944,"threshold_uncertainty_score":0.5853185},"labels":[],"label_agreement":null},{"id":"W4396922420","doi":"10.3390/air2020010","title":"Quantifying the Environmental Impact of Private and Commercial Pilot License Training in Canada","year":2024,"lang":"en","type":"article","venue":"Air","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":7,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"University of Waterloo","funders":"","keywords":"Aviation; License; Training (meteorology); Greenhouse gas; Sustainability; Commercial aviation; Aeronautics; Flight training; Engineering; Environmental science; Business; Environmental economics; Flight simulator; Meteorology; Economics; Simulation; Computer science; Geography","score_opus":0.03443303037218599,"score_gpt":0.26096460346738065,"score_spread":0.22653157309519467,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4396922420","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":[0.99915093,0.00019983324,0.00006581407,0.00024590665,0.00003559369,0.000084143,0.0000091826805,0.000022080056,0.00018648642],"genre_scores_gemma":[0.99969554,0.000058356378,0.0001629128,0.000057080408,0.000005368978,0.0000031680306,8.8068225e-7,0.000006503641,0.000010178882],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.9995131,0.000016886004,0.00009923366,0.00012566253,0.00009527325,0.00014985495],"domain_scores_gemma":[0.9997733,0.0000867755,0.00001834463,0.000100771824,1.9756811e-7,0.000020560316],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00007814715,0.00007174802,0.00007993643,0.000015763017,0.000040888615,0.0000055773944,0.00010494978,0.000015236731,0.00011555028],"category_scores_gemma":[0.000010695369,0.000046968707,0.000017653696,0.00009632418,0.00015030122,0.00008328021,0.00009658561,0.00011720615,0.000006706498],"study_design_candidate":"observational","study_design_consensus":"observational","about_ca_topic_candidate":true,"about_ca_topic_consensus":true,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000026640762,0.000021921618,0.6869516,0.000010960747,0.000019682533,0.00006819689,0.0018191849,0.0014593299,0.051393017,0.00038558544,0.00032678,0.2575171],"study_design_scores_gemma":[0.000107570995,0.00009412373,0.993402,0.000022404183,0.0000039449924,0.000012926914,0.0005654429,0.002073239,0.0021974675,0.00047653358,0.00095291703,0.000091424095],"about_ca_topic_score_codex":0.25233424,"about_ca_topic_score_gemma":0.4115076,"teacher_disagreement_score":0.30645043,"about_ca_system_score_codex":0.0002683,"about_ca_system_score_gemma":0.000034402412,"threshold_uncertainty_score":0.75264454},"labels":[],"label_agreement":null},{"id":"W4398237079","doi":"10.1088/1742-6596/2746/1/011001","title":"Preface","year":2024,"lang":"en","type":"article","venue":"Journal of Physics Conference Series","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Philosophy","score_opus":0.018917679504270028,"score_gpt":0.24587342636161927,"score_spread":0.22695574685734923,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4398237079","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":[0.23913543,0.001078192,0.71385825,0.004436347,0.0013574173,0.0001943124,0.0000110530455,0.00039619123,0.039532803],"genre_scores_gemma":[0.9933458,0.00016845141,0.00519779,0.00002565022,0.00007025875,0.0000011479352,2.3273724e-7,0.000007236548,0.0011834075],"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.999438,0.000011531834,0.0001539459,0.00009027571,0.00018924553,0.00011703716],"domain_scores_gemma":[0.9997556,0.00002660558,0.000068186324,0.00009712908,0.000018280045,0.00003417001],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00007777827,0.000082740335,0.00011642723,0.000018342458,0.000036956033,0.000067018445,0.00020708461,0.00003197985,0.00038374364],"category_scores_gemma":[0.000023635941,0.000060696184,0.000058895792,0.00016359045,0.000202998,0.0009248881,0.000072339644,0.00019274719,0.00013751321],"study_design_candidate":"design_other","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":[0.00002335096,0.000036321486,0.00078288047,0.00002514377,0.000032111522,0.00009320957,0.00069539744,0.0004496231,0.10729433,0.0858514,0.0035479022,0.8011683],"study_design_scores_gemma":[0.00009707498,0.00030947052,0.0010781888,0.00011169818,0.000021983244,0.000114639435,0.00053315307,0.00019768215,0.46967146,0.45831525,0.069365665,0.00018374271],"about_ca_topic_score_codex":0.000002337189,"about_ca_topic_score_gemma":0.000002378416,"teacher_disagreement_score":0.80098456,"about_ca_system_score_codex":0.00004204369,"about_ca_system_score_gemma":0.000028849192,"threshold_uncertainty_score":0.4201724},"labels":[],"label_agreement":null},{"id":"W4399843117","doi":"10.4050/f-0080-2024-1250","title":"Transitioning eVTOL Aircraft with Augmentative Cross-Modal Elements","year":2024,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"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 Calgary","funders":"","keywords":"Modal; Airplane; Propeller; Wing; Aerodynamics; Computer science; Drag; Mode (computer interface); Range (aeronautics); Lift (data mining); Aerospace engineering; Aeronautics; Engineering; Marine engineering; Human–computer interaction; Materials science","score_opus":0.009727682368278727,"score_gpt":0.2742556993854509,"score_spread":0.2645280170171722,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4399843117","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":[0.43080178,0.00009008833,0.50654787,0.00074333564,0.00011166584,0.00038864405,0.000012156266,0.0013813648,0.059923097],"genre_scores_gemma":[0.96262455,0.000008808357,0.033246815,0.00016674724,0.000011263611,0.000045086173,0.000005644672,0.000015566056,0.0038755487],"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99905324,0.000010750018,0.0001304697,0.00033113567,0.0002295364,0.00024486717],"domain_scores_gemma":[0.99978054,0.000029171639,0.00001544634,0.00012855732,0.0000036396216,0.00004266905],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0000739688,0.00012903889,0.00008227369,0.000033187254,0.0001272155,0.00008497006,0.000130773,0.000040668863,0.003931209],"category_scores_gemma":[0.0000046070445,0.000091816466,0.00003147084,0.00026395076,0.00027815232,0.0005210894,0.000049361515,0.00012476886,0.0007440973],"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":[0.00033819219,0.00047849212,0.19725879,0.00015524963,0.00040703124,0.0013177948,0.0058881356,0.019830251,0.2570136,0.03048558,0.011651385,0.4751755],"study_design_scores_gemma":[0.004489388,0.0027749063,0.0828511,0.0004891774,0.0001824599,0.00034263715,0.006448969,0.042176988,0.6701538,0.084914535,0.10196809,0.0032079658],"about_ca_topic_score_codex":0.00003445476,"about_ca_topic_score_gemma":0.000040791794,"teacher_disagreement_score":0.53182274,"about_ca_system_score_codex":0.00012424389,"about_ca_system_score_gemma":0.000008096679,"threshold_uncertainty_score":0.99697936},"labels":[],"label_agreement":null},{"id":"W4400493660","doi":"10.1007/s00158-024-03833-8","title":"Bayesian optimization with hidden constraints for aircraft design","year":2024,"lang":"en","type":"article","venue":"Structural and Multidisciplinary Optimization","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":10,"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; Bombardier (Canada); McGill University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Bayesian optimization; Engineering design process; Bayesian probability; Computer science; Mathematical optimization; Multidisciplinary design optimization; Engineering; Artificial intelligence; Mathematics; Mechanical engineering","score_opus":0.012265878201582267,"score_gpt":0.24980511399173555,"score_spread":0.2375392357901533,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4400493660","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":[0.004215289,0.00011834969,0.9936569,0.0004835521,0.00012636713,0.00071146816,0.000020723997,0.00036626504,0.00030111332],"genre_scores_gemma":[0.4295824,0.000044643923,0.5700329,0.00001283718,0.000023869427,0.000050058985,0.00004993173,0.000019033301,0.00018435846],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9990322,0.000022167755,0.0001597804,0.00042998738,0.00012555969,0.00023028492],"domain_scores_gemma":[0.99967974,0.00007796938,0.00004151142,0.000121274636,0.000015057112,0.0000644151],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0000766964,0.0001936528,0.0001301084,0.000058264075,0.00032471027,0.00007927543,0.000097079355,0.00009422376,0.0002841387],"category_scores_gemma":[0.000020266953,0.00013861415,0.000029239509,0.0002282956,0.00039211463,0.00054783496,0.00008420961,0.00008577316,0.0000041165927],"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":[0.00006883336,0.000005283706,0.00037161904,0.000033165226,0.0000125926645,0.0000080980035,0.00022561633,0.9685935,0.00039239632,0.0003250199,0.00007986643,0.029884059],"study_design_scores_gemma":[0.00037445314,0.00023267872,0.0003705916,0.00004000909,0.00004335311,0.000057584235,0.00021390777,0.99446666,0.00052249973,0.0034013146,0.000038022732,0.00023891895],"about_ca_topic_score_codex":0.0000041092994,"about_ca_topic_score_gemma":0.0000033583246,"teacher_disagreement_score":0.42536712,"about_ca_system_score_codex":0.00006441521,"about_ca_system_score_gemma":0.000015161867,"threshold_uncertainty_score":0.5652521},"labels":[],"label_agreement":null},{"id":"W4400568674","doi":"10.5194/ar-2-207-2024","title":"Opinion: Eliminating aircraft soot emissions","year":2024,"lang":"en","type":"article","venue":"Aerosol Research","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":9,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Institute of Particle Physics","funders":"Natural Sciences and Engineering Research Council of Canada; Schweizerischer Nationalfonds zur Förderung der Wissenschaftlichen Forschung","keywords":"Soot; Environmental science; Aeronautics; Aerospace engineering; Business; Engineering; Combustion; Chemistry","score_opus":0.08375020731480161,"score_gpt":0.3912719187445121,"score_spread":0.3075217114297105,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4400568674","genre_codex":"other","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":[0.43273422,0.008588817,0.044666924,0.049609907,0.0023710735,0.0026410234,0.000042211144,0.006431066,0.45291477],"genre_scores_gemma":[0.9846191,0.00028644974,0.0059328186,0.00004658757,0.00008329101,0.00008397726,0.0000037208795,0.000025757985,0.008918305],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9980423,0.00007638264,0.0001486229,0.000451861,0.0006955564,0.0005852888],"domain_scores_gemma":[0.9990654,0.00042265313,0.000010101657,0.00036717832,0.00001598599,0.00011866853],"candidate_categories":["insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.00073738385,0.00010917387,0.00009175007,0.00008820981,0.00039376062,0.000104686034,0.0004575251,0.00010583443,0.0022385383],"category_scores_gemma":[0.00048020473,0.00008869569,0.000049480204,0.00090680475,0.0004853644,0.00026779083,0.00067026255,0.0006589143,0.004061626],"study_design_candidate":"not_applicable","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":[0.000014957028,0.00010359546,0.002539795,0.00008332057,0.000017293694,0.00019798512,0.0006710706,0.00021599163,0.34863228,0.0075424477,0.14088735,0.49909392],"study_design_scores_gemma":[0.0004548942,0.0006930788,0.003306287,0.0006953727,0.000008549255,0.00010946423,0.002599664,0.016685402,0.31351393,0.061082553,0.59989506,0.0009557347],"about_ca_topic_score_codex":0.000063505824,"about_ca_topic_score_gemma":0.000009572661,"teacher_disagreement_score":0.5518849,"about_ca_system_score_codex":0.00017977909,"about_ca_system_score_gemma":0.00003217721,"threshold_uncertainty_score":0.99867356},"labels":[],"label_agreement":null},{"id":"W4400836103","doi":"10.1088/1742-6596/2784/1/012004","title":"Enhancing VTOL Performance: Shrouded Rotor BLDC Motor Model and Validation","year":2024,"lang":"en","type":"article","venue":"Journal of Physics Conference Series","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"University of Calgary","funders":"","keywords":"Rotor (electric); Computer science; Automotive engineering; Aeronautics; Aerospace engineering; Engineering; Electrical engineering","score_opus":0.01929603557681929,"score_gpt":0.24241638025092968,"score_spread":0.2231203446741104,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4400836103","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":[0.7959729,0.000113587324,0.20286281,0.00022672488,0.0001278457,0.00009720652,0.00000443901,0.000059929727,0.00053455046],"genre_scores_gemma":[0.9899607,0.00030415846,0.009184518,0.00001922437,0.00006457337,0.0000055685273,8.5311467e-7,0.000009943208,0.00045051562],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99926686,0.000012069575,0.00022098725,0.00013260162,0.00022462287,0.00014283869],"domain_scores_gemma":[0.9996955,0.000025871537,0.00010679432,0.00009760605,0.000029656394,0.000044617642],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012403802,0.000117239295,0.00015512796,0.00003379523,0.000083413426,0.00010371816,0.00014703714,0.0000481219,0.000080606056],"category_scores_gemma":[0.000024123618,0.00009270702,0.000042543466,0.0001237865,0.00018288055,0.0016556835,0.000079411366,0.00020611599,0.000018961335],"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":[0.000055838576,0.000032087748,0.0012690957,0.0000944089,0.000028168903,0.0000144139085,0.0012409803,0.004594275,0.78087056,0.00830627,0.00015239975,0.2033415],"study_design_scores_gemma":[0.00015516994,0.00034576326,0.00081981695,0.00019250916,0.000030010633,0.000051974897,0.00046053808,0.02880125,0.9030274,0.06520042,0.00070652063,0.00020861151],"about_ca_topic_score_codex":0.000002485628,"about_ca_topic_score_gemma":0.0000024167964,"teacher_disagreement_score":0.20313288,"about_ca_system_score_codex":0.00006353908,"about_ca_system_score_gemma":0.000043540884,"threshold_uncertainty_score":0.37804824},"labels":[],"label_agreement":null},{"id":"W4401416825","doi":"10.3390/aerospace11080644","title":"Number of Blades’ Influence on the Performance of Rotor with Equal Solidity in Open and Shrouded Configurations: Experimental Analysis","year":2024,"lang":"en","type":"article","venue":"Aerospace","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":5,"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 Calgary","funders":"","keywords":"Solidity; Rotor (electric); Structural engineering; Engineering; Mathematics; Computer science; Mechanical engineering","score_opus":0.016827974073830656,"score_gpt":0.28813866565568697,"score_spread":0.27131069158185633,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4401416825","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":[0.99791694,0.00003856723,0.00026773312,0.00018990552,0.000006566865,0.0002698007,0.0000052988676,0.000021190552,0.0012839857],"genre_scores_gemma":[0.9987772,0.000026135995,0.00096771825,0.000032924316,0.0000014665079,0.000053815103,8.490948e-7,0.000004427933,0.00013542494],"study_design_codex":"observational","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9994257,0.000021776728,0.00012108152,0.00018560489,0.0001464651,0.00009937065],"domain_scores_gemma":[0.9996395,0.00009108492,0.000048550886,0.000200741,0.00000476523,0.000015327194],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012380768,0.00007968823,0.00013532024,0.000024980201,0.000041679814,0.000026292373,0.00022573075,0.00003146047,0.00025331022],"category_scores_gemma":[0.000018568793,0.000049348448,0.00001780647,0.00052555883,0.00038306142,0.0002848627,0.00014242443,0.00008651162,0.000013263865],"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":[0.0001472744,0.00019113287,0.6663066,0.000031342195,0.00012393431,0.000008996911,0.0024404551,0.0110727465,0.30632976,0.012190691,0.0001674598,0.0009895964],"study_design_scores_gemma":[0.00033961545,0.00040061615,0.20740184,0.00011670825,0.000044801196,0.0000047275407,0.0019660564,0.0082953945,0.7806653,0.00040518132,0.00016210433,0.00019768892],"about_ca_topic_score_codex":0.00033091957,"about_ca_topic_score_gemma":0.00013059912,"teacher_disagreement_score":0.4743355,"about_ca_system_score_codex":0.0000441036,"about_ca_system_score_gemma":0.00000862551,"threshold_uncertainty_score":0.27735695},"labels":[],"label_agreement":null},{"id":"W4401468492","doi":"10.1108/aeat-06-2023-0167","title":"Conceptual design and analysis of a box fan-in-split-wing tiltrotor eVTOL aircraft","year":2024,"lang":"en","type":"article","venue":"Aircraft Engineering and Aerospace Technology","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Toronto Metropolitan University","funders":"","keywords":"Thrust; Propeller; Aerodynamics; Engineering; Aerospace engineering; Wing; Conceptual design; Cruise; Lift (data mining); Marine engineering; Propulsion; Aeronautics; Automotive engineering; Wing loading; Computer science; Mechanical engineering; Angle of attack","score_opus":0.008317845852306755,"score_gpt":0.22026771561597247,"score_spread":0.21194986976366573,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4401468492","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":[0.72378284,0.0030016596,0.2708876,0.0008123069,0.000068882,0.0003339997,0.000008166079,0.0010552204,0.000049315677],"genre_scores_gemma":[0.9491248,0.0004223198,0.05020106,0.000019090392,0.0000068757704,0.00008343708,0.0000021605256,0.000028799474,0.00011143639],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99850726,0.00001758604,0.00029238898,0.0005855827,0.0001560237,0.00044116782],"domain_scores_gemma":[0.999349,0.00020780737,0.000043574983,0.00032613653,0.000007641017,0.00006584942],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00021728482,0.00027487116,0.00048289006,0.00072605157,0.000049986076,0.000027256883,0.00022548702,0.0003019683,0.000042126943],"category_scores_gemma":[0.00012460482,0.00026169815,0.00007031036,0.0021175742,0.0006102226,0.00020068459,0.00024764304,0.0003722057,0.000011076257],"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":[0.00005044005,0.00013983872,0.09427385,0.0002152209,0.0009126097,0.00036326703,0.0020313475,0.14386699,0.6578613,0.03777757,0.00044723722,0.06206035],"study_design_scores_gemma":[0.0017801372,0.0012467597,0.047897834,0.0007482869,0.0011041799,0.00018596626,0.0031649945,0.78146636,0.13405064,0.0062733307,0.019691346,0.0023901851],"about_ca_topic_score_codex":0.000041785264,"about_ca_topic_score_gemma":0.000017881877,"teacher_disagreement_score":0.63759935,"about_ca_system_score_codex":0.00008828237,"about_ca_system_score_gemma":0.000010335921,"threshold_uncertainty_score":0.99998355},"labels":[],"label_agreement":null},{"id":"W4401537999","doi":"10.1109/remar61031.2024.10618077","title":"Application of Mechanisms to Aircraft Flexible Trailing Edge Design","year":2024,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Toronto Metropolitan University","funders":"","keywords":"Trailing edge; Computer science; Aerospace engineering; Engineering; Structural engineering","score_opus":0.019418046134920385,"score_gpt":0.25856830191173924,"score_spread":0.23915025577681887,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4401537999","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0010311694,0.000043964774,0.99044085,0.00037703157,0.000048729897,0.00029974882,0.0000014339638,0.0006219326,0.0071351514],"genre_scores_gemma":[0.682422,0.0000054942225,0.31621683,0.00008380586,0.0000055952028,0.00005013309,6.459657e-7,0.000009461059,0.0012060668],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99929994,0.000009421901,0.00013277138,0.00026299068,0.0001402328,0.000154611],"domain_scores_gemma":[0.9996924,0.000050988256,0.000013931084,0.00019855631,0.0000032933071,0.000040830866],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0001514026,0.00008432912,0.000086272405,0.00005095042,0.0000340298,0.000012538781,0.0001929502,0.000052852363,0.0004942798],"category_scores_gemma":[0.00001865615,0.00006989033,0.000031666394,0.00037461144,0.0000521806,0.00013159284,0.000087228495,0.000059919268,0.001059927],"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":[0.000005726976,0.0000203102,0.00003425697,0.000010991541,0.0000042221973,0.0000020359607,0.00008577587,0.0105695855,0.7180589,0.04261441,0.0010337628,0.22756006],"study_design_scores_gemma":[0.000049635495,0.000115268245,0.00014243372,0.000014496722,0.00000683684,0.0000036589104,0.000117136486,0.027303288,0.8512732,0.10824149,0.0125867,0.00014588011],"about_ca_topic_score_codex":0.00002813255,"about_ca_topic_score_gemma":0.0000042786323,"teacher_disagreement_score":0.6813908,"about_ca_system_score_codex":0.000042262902,"about_ca_system_score_gemma":0.0000057963457,"threshold_uncertainty_score":0.9997179},"labels":[],"label_agreement":null},{"id":"W4401542152","doi":"10.3390/aerospace11080664","title":"Propeller Effects and Elasticity in Aerodynamic Analysis of Small Propeller-Driven Aircraft and UAVs","year":2024,"lang":"en","type":"article","venue":"Aerospace","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Propeller; Aerodynamics; Aeroelasticity; Wing; Aerospace engineering; Wind tunnel; Engineering; Deflection (physics); Aerodynamic force; Marine engineering; Structural engineering; Physics","score_opus":0.006837605099646079,"score_gpt":0.21559963218694642,"score_spread":0.20876202708730035,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4401542152","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":[0.99089366,0.00063021155,0.007107462,0.00025265242,0.00003260857,0.00031004212,0.0000034200627,0.00012043386,0.0006495229],"genre_scores_gemma":[0.99393904,0.0002541533,0.004976324,0.000020731613,0.000003198909,0.000018377506,0.0000016529912,0.000012447134,0.00077406276],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.9990667,0.000035495763,0.00014639238,0.00041286225,0.00012512898,0.00021343993],"domain_scores_gemma":[0.9995828,0.0001433181,0.00003517662,0.00018682891,0.0000040424366,0.00004778247],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00011556797,0.0001485161,0.0002635822,0.00013297524,0.000034761997,0.000024322006,0.00011427462,0.000085770844,0.000045032382],"category_scores_gemma":[0.00006588389,0.0001156857,0.0000396392,0.0008809394,0.00035491606,0.00012641026,0.0002384989,0.00016162459,0.00003176538],"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":[0.0000557761,0.00018678528,0.76514536,0.00046428453,0.0003903133,0.00016298042,0.0017554774,0.01619149,0.15819584,0.0013721334,0.00026491645,0.05581466],"study_design_scores_gemma":[0.000508749,0.00032851248,0.8221423,0.0002205395,0.0003917852,0.000008905149,0.00018256682,0.16602416,0.007757816,0.0011458615,0.0008292226,0.00045958982],"about_ca_topic_score_codex":0.00021181273,"about_ca_topic_score_gemma":0.0014077463,"teacher_disagreement_score":0.15043801,"about_ca_system_score_codex":0.000063429085,"about_ca_system_score_gemma":0.0000062407807,"threshold_uncertainty_score":0.4717526},"labels":[],"label_agreement":null},{"id":"W4401800056","doi":"10.1016/j.ast.2024.109479","title":"Hybrid electric aircraft design with optimal power management","year":2024,"lang":"en","type":"article","venue":"Aerospace Science and Technology","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Royal Military College of Canada","funders":"","keywords":"Power (physics); Optimal design; Electric power; Automotive engineering; Aerospace engineering; Engineering; Computer science; Aeronautics; Physics","score_opus":0.00538023738645495,"score_gpt":0.21237035116589895,"score_spread":0.20699011377944398,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4401800056","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":[0.68553185,0.0017823268,0.28519377,0.010605755,0.00021571224,0.0010042082,0.000002115436,0.0035416093,0.012122642],"genre_scores_gemma":[0.9454704,0.00021985765,0.05328274,0.00010415624,0.000003894466,0.000063873136,1.9394437e-7,0.000016356686,0.0008385316],"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9979908,0.000008421386,0.0001134816,0.00080619374,0.00044042218,0.0006407184],"domain_scores_gemma":[0.99943745,0.000029295472,0.000028533846,0.00040831015,0.000020682979,0.0000757426],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00032853746,0.00020117465,0.0001428189,0.00043351826,0.0003222745,0.00011663428,0.0005948243,0.00008115657,0.000092050715],"category_scores_gemma":[0.000038847294,0.00014885855,0.00001535019,0.00330354,0.0023527325,0.0005407163,0.00045180364,0.00026061945,0.00026866118],"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":[0.000065987166,0.0001756421,0.0047682137,0.00004096645,0.00009063697,0.0018632933,0.00025541658,0.0011977633,0.38118008,0.14673151,0.011735929,0.45189458],"study_design_scores_gemma":[0.0009228689,0.0032076226,0.003257579,0.0001701878,0.000097986005,0.0018156379,0.0016666785,0.014896305,0.80817366,0.07825285,0.085796855,0.0017417548],"about_ca_topic_score_codex":0.000005791935,"about_ca_topic_score_gemma":0.0000023412363,"teacher_disagreement_score":0.4501528,"about_ca_system_score_codex":0.00017091897,"about_ca_system_score_gemma":0.000040925635,"threshold_uncertainty_score":0.8668741},"labels":[],"label_agreement":null},{"id":"W4401908032","doi":"10.3390/modelling5030053","title":"Integrating Null Controllability and Model-Based Safety Assessment for Enhanced Reliability in Drone Design","year":2024,"lang":"en","type":"article","venue":"Modelling—International Open Access Journal of Modelling in Engineering Science","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Concordia University","funders":"Office National d'études et de Recherches Aérospatiales; Natural Sciences and Engineering Research Council of Canada; Norges Teknisk-Naturvitenskapelige Universitet","keywords":"Drone; Controllability; Reliability engineering; Reliability (semiconductor); Computer science; Systems engineering; Distributed computing; Engineering","score_opus":0.03788321399457088,"score_gpt":0.3460823174965387,"score_spread":0.30819910350196783,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4401908032","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.11359206,0.00009617071,0.88488513,0.00044844902,0.00025371602,0.00052073307,0.000005527764,0.00003321701,0.00016498838],"genre_scores_gemma":[0.5995983,0.00006420254,0.40025294,0.000019264538,0.000011475731,0.000030424171,6.748499e-7,0.000011841187,0.000010902693],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99754524,0.000026903777,0.00088338414,0.00058180344,0.0005996608,0.00036297602],"domain_scores_gemma":[0.99879014,0.00058345834,0.00019646215,0.00021475092,0.00012243645,0.00009276387],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.004630637,0.00021869836,0.00035493704,0.00042168584,0.000093218034,0.0007181831,0.002111067,0.00007733169,0.000014035222],"category_scores_gemma":[0.0003203605,0.00019163958,0.00006714098,0.0006821059,0.00024763469,0.0032922712,0.00041549077,0.000482436,6.195104e-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":[0.00012881089,0.000071891096,0.00051279715,0.000027875654,0.000005115234,0.0000066463263,0.00013639056,0.98979807,0.0054432177,0.0014577098,0.0000025115378,0.0024089883],"study_design_scores_gemma":[0.00066677376,0.00006510204,0.00008670097,0.00033968364,0.0000062478316,0.000004231628,0.000022881406,0.9641239,0.0044099293,0.030044835,0.00003201073,0.00019768075],"about_ca_topic_score_codex":0.000072029325,"about_ca_topic_score_gemma":0.000009252075,"teacher_disagreement_score":0.4860062,"about_ca_system_score_codex":0.001189426,"about_ca_system_score_gemma":0.0002531316,"threshold_uncertainty_score":0.78148353},"labels":[],"label_agreement":null},{"id":"W4401942596","doi":"10.1115/gt2024-121815","title":"Innovative Synergies in Aircraft Propulsion: the Concept of Hybrid Power Systems With Contra-Rotating Propellers","year":2024,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Propulsion; Aerospace engineering; Aeronautics; Power (physics); Engineering; Systems engineering; Electrically powered spacecraft propulsion; Propulsor; Propeller; Automotive engineering; Computer science; Marine engineering; Physics","score_opus":0.008535462847015188,"score_gpt":0.22186273774837,"score_spread":0.21332727490135484,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4401942596","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":[0.91899294,0.0012425124,0.02796678,0.002042501,0.0002707136,0.002126457,0.0000135621,0.00062468107,0.046719883],"genre_scores_gemma":[0.9967479,0.000007878289,0.001611005,0.00004074554,0.0000039765564,0.00007625368,0.0000010369582,0.000013519661,0.0014976562],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99896705,0.00004126484,0.00025162954,0.00027606604,0.0002463039,0.00021766043],"domain_scores_gemma":[0.9995775,0.00012263113,0.00006152585,0.00020407866,0.000017930757,0.000016304873],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018810593,0.00013989462,0.0001720687,0.000048722817,0.00005464606,0.000035533354,0.00022987653,0.000028335064,0.00017214948],"category_scores_gemma":[0.000056074914,0.00006753613,0.0000188108,0.0007665322,0.0006921879,0.0002451005,0.00010614862,0.00019604868,0.000035987683],"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":[0.0006179704,0.000748068,0.12992133,0.0007210721,0.0005606213,0.002567034,0.025713116,0.22393054,0.13082571,0.2520751,0.028791213,0.20352821],"study_design_scores_gemma":[0.0042437105,0.0045243544,0.020778392,0.004530289,0.0000837206,0.0007312703,0.12212713,0.10528798,0.6629743,0.019197999,0.052153077,0.0033677714],"about_ca_topic_score_codex":0.00015525823,"about_ca_topic_score_gemma":0.000024522276,"teacher_disagreement_score":0.5321486,"about_ca_system_score_codex":0.00006446646,"about_ca_system_score_gemma":0.000021960725,"threshold_uncertainty_score":0.27540436},"labels":[],"label_agreement":null},{"id":"W4402031473","doi":"10.32920/26884153","title":"Preliminary Design, Modelling, and Motion Planning of a Robotic Fastening System for Aircraft Wing Interior Assembly","year":2024,"lang":"en","type":"preprint","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Wing; Motion planning; Motion (physics); Aerospace engineering; Engineering; Computer science; Aeronautics; Robot; Artificial intelligence","score_opus":0.04169136758311823,"score_gpt":0.26496490435629594,"score_spread":0.2232735367731777,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4402031473","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.06289448,0.00071299786,0.9341804,0.000052441806,0.00023655989,0.0009751864,0.0000060212938,0.00054067135,0.00040126403],"genre_scores_gemma":[0.7279547,0.000014211405,0.2716188,0.0000060517723,0.00001875832,0.00014633597,0.000005038399,0.00003803571,0.00019805049],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9982684,0.000040264254,0.0004599251,0.0007210585,0.00020509794,0.00030521338],"domain_scores_gemma":[0.999238,0.00016006238,0.0002093674,0.00032372863,0.000015132803,0.0000536742],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0003519093,0.00033025467,0.00047105414,0.00014083604,0.000088675624,0.0000641399,0.00030319774,0.0003259591,0.00000772648],"category_scores_gemma":[0.00003848586,0.00029310235,0.00011814486,0.00010673499,0.00013736553,0.00012776,0.001592769,0.00040833332,0.00001009517],"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":[0.000056679684,0.000012433749,0.00021549962,0.001273184,0.000042301257,0.000016395294,0.00039602615,0.9778883,0.01064699,0.00017368671,0.00006536666,0.009213136],"study_design_scores_gemma":[0.000143423,0.0002440666,0.000059673068,0.0020920525,0.00011224635,0.000026257901,0.0011674084,0.9693027,0.017497055,0.009030568,0.000012170094,0.0003123703],"about_ca_topic_score_codex":0.000047977304,"about_ca_topic_score_gemma":9.229322e-7,"teacher_disagreement_score":0.6650602,"about_ca_system_score_codex":0.00024159139,"about_ca_system_score_gemma":0.000015795895,"threshold_uncertainty_score":0.99995214},"labels":[],"label_agreement":null},{"id":"W4402031523","doi":"10.32920/26884153.v1","title":"Preliminary Design, Modelling, and Motion Planning of a Robotic Fastening System for Aircraft Wing Interior Assembly","year":2024,"lang":"en","type":"preprint","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Wing; Aerospace engineering; Motion (physics); Motion planning; Engineering; Aeronautics; Computer science; Robot; Artificial intelligence","score_opus":0.04169136758311823,"score_gpt":0.26496490435629594,"score_spread":0.2232735367731777,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4402031523","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.06289448,0.00071299786,0.9341804,0.000052441806,0.00023655989,0.0009751864,0.0000060212938,0.00054067135,0.00040126403],"genre_scores_gemma":[0.7279547,0.000014211405,0.2716188,0.0000060517723,0.00001875832,0.00014633597,0.000005038399,0.00003803571,0.00019805049],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9982684,0.000040264254,0.0004599251,0.0007210585,0.00020509794,0.00030521338],"domain_scores_gemma":[0.999238,0.00016006238,0.0002093674,0.00032372863,0.000015132803,0.0000536742],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0003519093,0.00033025467,0.00047105414,0.00014083604,0.000088675624,0.0000641399,0.00030319774,0.0003259591,0.00000772648],"category_scores_gemma":[0.00003848586,0.00029310235,0.00011814486,0.00010673499,0.00013736553,0.00012776,0.001592769,0.00040833332,0.00001009517],"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":[0.000056679684,0.000012433749,0.00021549962,0.001273184,0.000042301257,0.000016395294,0.00039602615,0.9778883,0.01064699,0.00017368671,0.00006536666,0.009213136],"study_design_scores_gemma":[0.000143423,0.0002440666,0.000059673068,0.0020920525,0.00011224635,0.000026257901,0.0011674084,0.9693027,0.017497055,0.009030568,0.000012170094,0.0003123703],"about_ca_topic_score_codex":0.000047977304,"about_ca_topic_score_gemma":9.229322e-7,"teacher_disagreement_score":0.6650602,"about_ca_system_score_codex":0.00024159139,"about_ca_system_score_gemma":0.000015795895,"threshold_uncertainty_score":0.99995214},"labels":[],"label_agreement":null},{"id":"W4402261491","doi":"10.62973/14-008","title":"OGC Testbed 10 Report on Aviation Architecture","year":2014,"lang":"en","type":"report","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"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":"National Weather Service; Natural Resources Canada; U.S. Geological Survey; Defence Science and Technology Group; National Oceanic and Atmospheric Administration; National Geospatial-Intelligence Agency; U.S. Army Corps of Engineers; Defence Science and Technology Laboratory; European Space Agency","keywords":"Testbed; Architecture; Aviation; Computer science; Aeronautics; Engineering; World Wide Web; Aerospace engineering; Geography; Archaeology","score_opus":0.01977088200865213,"score_gpt":0.2674600951618896,"score_spread":0.2476892131532375,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4402261491","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0005264827,0.00001529598,0.047067683,0.00041949376,0.00038719462,0.0003511361,0.000006391237,0.00084675616,0.95037955],"genre_scores_gemma":[0.24072364,0.0002115926,0.024866357,0.0004989238,0.00047457646,0.00014972546,0.00031933695,0.0001329087,0.7326229],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9974995,0.000034743116,0.00039853042,0.0007312753,0.0010208307,0.00031511506],"domain_scores_gemma":[0.9984673,0.00012857666,0.00038035228,0.0009310519,0.000025065283,0.000067622204],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.00055882236,0.00034307953,0.00035163327,0.00006875392,0.00009650912,0.000025043562,0.0003567494,0.0005078528,0.008829051],"category_scores_gemma":[0.0013539675,0.00025642844,0.00012737053,0.00019441424,0.00017871798,0.00005468882,0.00020280904,0.00052254426,0.0038130227],"study_design_candidate":"not_applicable","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":[0.000020384814,0.000114941446,0.011317757,0.000049950337,0.000034975845,0.0004964838,0.000015678444,0.00079131697,0.0009342049,0.00027071853,0.4899405,0.49601308],"study_design_scores_gemma":[0.000079582,0.000098509736,0.003468332,0.000044080363,0.000019388488,0.000406135,0.0000043660325,0.000024307032,0.0015155607,0.009499039,0.98443985,0.0004008608],"about_ca_topic_score_codex":0.00018461165,"about_ca_topic_score_gemma":0.00006847058,"teacher_disagreement_score":0.49561223,"about_ca_system_score_codex":0.00048101647,"about_ca_system_score_gemma":0.000049935217,"threshold_uncertainty_score":0.9999888},"labels":[],"label_agreement":null},{"id":"W4402452648","doi":"10.11159/eee24.105","title":"Innovative Integration Of Solar &amp; Wind Energy For Future Automotive Propulsion Systems","year":2024,"lang":"en","type":"article","venue":"Proceedings of the World Congress on Electrical Engineering and Computer Systems and Science","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Propulsion; Automotive industry; Wind power; Aerospace engineering; Solar energy; Automotive engineering; Computer science; Engineering; Systems engineering; Environmental science; Aeronautics; Electrical engineering","score_opus":0.006972362571296954,"score_gpt":0.20998083692111352,"score_spread":0.20300847434981656,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4402452648","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":[0.8306364,0.00272129,0.15957786,0.0006519314,0.004230171,0.0012474388,0.000012593874,0.00036314462,0.00055918616],"genre_scores_gemma":[0.998564,0.000022495027,0.0009609839,0.000008648849,0.00007009853,0.000020605483,2.0324653e-7,0.0000062733707,0.00034667132],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99913687,0.000003151866,0.00018557449,0.00027868937,0.00022829651,0.00016743717],"domain_scores_gemma":[0.9996726,0.000059144393,0.00008268687,0.000061443425,0.00009080402,0.000033329703],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024604474,0.00011519841,0.00016986705,0.000161095,0.000096698626,0.00010151539,0.00022691069,0.000039825263,2.6787507e-7],"category_scores_gemma":[0.00004364172,0.00006998918,0.000021828811,0.0012699236,0.00020443978,0.00021301149,0.00010730758,0.00011756049,1.4341408e-7],"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":[0.00006282817,0.000086641994,0.0016218094,0.00082716666,0.0000557682,9.758663e-7,0.00062388385,0.01595758,0.19108361,0.6324864,0.002647489,0.15454586],"study_design_scores_gemma":[0.00012386365,0.000259645,0.0010961425,0.0007005616,0.000008755329,0.00001832695,0.00005712437,0.96031123,0.02991797,0.0005045669,0.0068355626,0.00016627625],"about_ca_topic_score_codex":0.000020908805,"about_ca_topic_score_gemma":0.0000010917108,"teacher_disagreement_score":0.94435364,"about_ca_system_score_codex":0.000067864334,"about_ca_system_score_gemma":0.000009879042,"threshold_uncertainty_score":0.2854076},"labels":[],"label_agreement":null},{"id":"W4402471561","doi":"10.1080/02786826.2024.2395940","title":"Eulerian–Lagrangian CFD-microphysics modeling of aircraft-emitted aerosol formation at ground-level","year":2024,"lang":"en","type":"article","venue":"Aerosol Science and Technology","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure; Université du Québec à Montréal","funders":"Alliance de recherche numérique du Canada; Safran Aircraft Engines","keywords":"Aerosol; Eulerian path; Lagrangian; Computational fluid dynamics; Environmental science; Atmospheric sciences; Meteorology; Mechanics; Physics; Theoretical physics","score_opus":0.017910751416525723,"score_gpt":0.2358253044045292,"score_spread":0.21791455298800347,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4402471561","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":[0.9540418,0.00035384868,0.041718427,0.001471033,0.00015940145,0.00029832436,0.0000135262635,0.0006882974,0.001255389],"genre_scores_gemma":[0.9934236,0.00018500848,0.006076125,0.00007340632,0.000011246492,0.000032530243,0.0000033815165,0.000015939513,0.0001787806],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9981341,0.000010017646,0.0003092614,0.00059996406,0.00041884655,0.0005278102],"domain_scores_gemma":[0.99934334,0.000031679123,0.00007722207,0.00042893438,0.000051067975,0.00006775107],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002918321,0.00020845028,0.00022202791,0.0002663899,0.0004066892,0.0000625056,0.0006270371,0.0002163112,0.0000556774],"category_scores_gemma":[0.000099627454,0.00017971871,0.000041620322,0.0025840665,0.0024939869,0.0010570087,0.0007486992,0.00023982649,0.00012599892],"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":[0.000006071707,0.000025681347,0.00030896717,0.000026551033,0.00000539189,0.0000102261965,0.00017882371,0.00025241764,0.9467854,0.003207776,0.00015593575,0.049036764],"study_design_scores_gemma":[0.00033322404,0.0002558153,0.00010624155,0.00010766473,0.000027271668,0.00014386549,0.00066374877,0.1251955,0.8540534,0.01788565,0.0007348024,0.0004928085],"about_ca_topic_score_codex":0.00007083341,"about_ca_topic_score_gemma":0.000060387247,"teacher_disagreement_score":0.124943085,"about_ca_system_score_codex":0.00026932047,"about_ca_system_score_gemma":0.000040965762,"threshold_uncertainty_score":0.91891986},"labels":[],"label_agreement":null},{"id":"W4402488917","doi":"10.2514/1.c037876","title":"Blended-Wing-Body Regional Aircraft Optimization with High-Fidelity Aerodynamics and Critical Design Requirements","year":2024,"lang":"en","type":"article","venue":"Journal of Aircraft","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":8,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto","funders":"Natural Sciences and Engineering Research Council of Canada; Alliance de recherche numérique du Canada; University of Toronto; Transport Canada","keywords":"Aerodynamics; Wing; Aerospace engineering; High fidelity; Aeronautics; Computer science; Fidelity; Engineering; Multidisciplinary design optimization; Simulation","score_opus":0.019946939811179235,"score_gpt":0.2684770986148443,"score_spread":0.24853015880366508,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4402488917","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.048809376,0.000505696,0.9451741,0.0047538825,0.00026114786,0.0001766265,0.0000043496625,0.00015471857,0.00016013253],"genre_scores_gemma":[0.6984573,0.0003168178,0.30083063,0.00018487456,0.00007360718,0.000004828827,0.0000019338795,0.000027963475,0.00010207876],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99808806,0.00008820233,0.000495717,0.00035111554,0.00064201263,0.0003348745],"domain_scores_gemma":[0.99915016,0.00027239352,0.00013799708,0.00021521919,0.00006548335,0.0001587537],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005869651,0.00023319758,0.0002827123,0.00014096306,0.00015294997,0.0001042625,0.00027161304,0.00013689468,0.00021163048],"category_scores_gemma":[0.00020277682,0.00017511605,0.000071165996,0.0003528582,0.0006520295,0.0011090229,0.000121546735,0.00043135762,0.000022380726],"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":[0.0010522999,0.0007827526,0.010718839,0.00029969757,0.00044789092,0.0026449934,0.0006788944,0.87651086,0.033090554,0.010395949,0.019138385,0.04423887],"study_design_scores_gemma":[0.0071085757,0.012467133,0.06057632,0.003529374,0.0014214169,0.009398525,0.0021700207,0.68088514,0.012384655,0.17753223,0.028444847,0.0040817955],"about_ca_topic_score_codex":0.00001350324,"about_ca_topic_score_gemma":0.0000064770493,"teacher_disagreement_score":0.6496479,"about_ca_system_score_codex":0.00026951294,"about_ca_system_score_gemma":0.0000773618,"threshold_uncertainty_score":0.7141025},"labels":[],"label_agreement":null},{"id":"W4402686200","doi":"10.2514/6.2024-3507","title":"Application of Aerodynamic Shape Optimization to Swept Natural Laminar Flow Wings","year":2024,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Institute for Christian Studies; University of Toronto","funders":"","keywords":"Laminar flow; Aerodynamics; Computer science; Swept wing; Flow (mathematics); Aerospace engineering; Engineering; Mechanics; Physics","score_opus":0.004146135951947951,"score_gpt":0.21798731859407444,"score_spread":0.21384118264212648,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4402686200","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0789637,0.0000750972,0.91692615,0.00061815843,0.000074095355,0.00023449013,0.0000023027524,0.00042978305,0.0026762313],"genre_scores_gemma":[0.86567485,0.000009172012,0.13345957,0.00009013937,0.0000063054986,0.000021095868,0.0000068693244,0.000007842258,0.00072414987],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994518,0.0000048578845,0.00010305868,0.00021535005,0.00011879496,0.00010610191],"domain_scores_gemma":[0.9997968,0.000020203566,0.000015114431,0.00014339523,0.000004270582,0.000020233952],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000050630108,0.000070198075,0.0000635811,0.000041259776,0.000027443342,0.000012248967,0.00014277936,0.00004049311,0.0005452822],"category_scores_gemma":[0.000018704362,0.000057762914,0.00002344257,0.00037033734,0.000059442467,0.00017967321,0.00009228884,0.00005912448,0.00030218586],"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":[0.000010803059,0.000025648817,0.00069244526,0.00002005158,0.000006232101,0.000002586753,0.00014247723,0.29212078,0.12254941,0.0020252983,0.0014610532,0.5809432],"study_design_scores_gemma":[0.00003304481,0.000043890293,0.0013344362,0.000009371824,0.000003896526,0.000002227099,0.000047084894,0.98954195,0.005759195,0.00088504615,0.0022527215,0.00008716227],"about_ca_topic_score_codex":0.000022913177,"about_ca_topic_score_gemma":0.00001728979,"teacher_disagreement_score":0.78671116,"about_ca_system_score_codex":0.00007377562,"about_ca_system_score_gemma":0.0000023873292,"threshold_uncertainty_score":0.5970458},"labels":[],"label_agreement":null},{"id":"W4402686231","doi":"10.2514/6.2024-4322","title":"Definition of Minimum Design Requirements for Hydrogen Aircraft From an Air Transportation Network Perspective","year":2024,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Perspective (graphical); Systems engineering; Computer science; Air travel; Transport engineering; Engineering; Aviation; Aeronautics; Aerospace engineering","score_opus":0.03915837347028284,"score_gpt":0.2814745958798537,"score_spread":0.24231622240957085,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4402686231","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.13127027,0.00020382213,0.8643857,0.0003075767,0.000102223574,0.00055712723,0.000061714294,0.0004029356,0.0027085918],"genre_scores_gemma":[0.81013775,0.000023100962,0.18953371,0.00007676824,0.00002795557,0.00006869426,0.000050137245,0.000015286643,0.000066586654],"study_design_codex":"bench_or_experimental","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.99908954,0.000022789223,0.00019288741,0.0003469316,0.00015705363,0.00019082357],"domain_scores_gemma":[0.9996441,0.00010945771,0.000040836898,0.00015827447,0.00001132124,0.00003599818],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012423127,0.000117408636,0.00012096217,0.000029142537,0.00006239011,0.000008876289,0.00013647255,0.0000823581,0.00032650883],"category_scores_gemma":[0.000015997653,0.000104582774,0.00006344571,0.00020190167,0.000116436655,0.00040734012,0.000010291006,0.00005440198,0.000043322932],"study_design_candidate":"theoretical_or_conceptual","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":[0.0009681315,0.0008595965,0.013506787,0.000112208894,0.00046325798,0.0000711656,0.007490402,0.07993103,0.534752,0.28512868,0.013837973,0.06287875],"study_design_scores_gemma":[0.00031512717,0.00046294436,0.0037437049,0.000041217096,0.00006353985,6.505852e-7,0.0010861002,0.008763288,0.06660482,0.91810787,0.0005824212,0.00022829488],"about_ca_topic_score_codex":0.00018257432,"about_ca_topic_score_gemma":0.00014568256,"teacher_disagreement_score":0.67886746,"about_ca_system_score_codex":0.000119163684,"about_ca_system_score_gemma":0.000010812945,"threshold_uncertainty_score":0.42647618},"labels":[],"label_agreement":null},{"id":"W4402687774","doi":"10.2514/6.2024-3623","title":"Heat Pipe-Based Air-Cooled Battery Thermal Management Strategies for an Electric Trainer Aircraft","year":2024,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Université de Sherbrooke","funders":"","keywords":"Trainer; Battery (electricity); Thermal management of electronic devices and systems; Heat pipe; Automotive engineering; Computer cooling; Thermal; Environmental science; Aeronautics; Computer science; Electrical engineering; Aerospace engineering; Engineering; Mechanical engineering; Heat transfer; Meteorology; Mechanics; Physics; Operating system","score_opus":0.014263748154916411,"score_gpt":0.24648234045545636,"score_spread":0.23221859230053996,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4402687774","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":[0.12689179,0.00016185266,0.83108616,0.0019308447,0.00020129127,0.0009738274,0.00000947733,0.00206461,0.036680136],"genre_scores_gemma":[0.9796013,0.000011203615,0.017170247,0.0009264192,0.00003312366,0.0002288989,0.000012190652,0.000033220957,0.0019833737],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9986648,0.000021508553,0.00017710954,0.00049738464,0.00020122144,0.00043799766],"domain_scores_gemma":[0.9995511,0.00006427913,0.000009261167,0.00031025324,0.000004078108,0.000060997703],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001419133,0.000216909,0.00014216926,0.000099987796,0.00011173221,0.000094104464,0.00030973885,0.0000833498,0.00090092374],"category_scores_gemma":[0.0000039097763,0.00016451433,0.00009193099,0.00035403454,0.00011087123,0.0005433578,0.00005623206,0.00011779601,0.00020057053],"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":[0.00016255517,0.0004204911,0.00049117143,0.00023250059,0.00011255159,0.00014349404,0.00023262475,0.04524333,0.4794957,0.019123415,0.020510254,0.4338319],"study_design_scores_gemma":[0.0034558477,0.0031871053,0.014942764,0.00015254796,0.00028175872,0.000034539975,0.0039834105,0.40640372,0.26905924,0.07932203,0.21618499,0.0029920507],"about_ca_topic_score_codex":0.000028049682,"about_ca_topic_score_gemma":0.0000341089,"teacher_disagreement_score":0.85270953,"about_ca_system_score_codex":0.000115491646,"about_ca_system_score_gemma":0.000015893931,"threshold_uncertainty_score":0.9864483},"labels":[],"label_agreement":null},{"id":"W4402936998","doi":"10.1038/s41598-024-73484-8","title":"Trade-off between soot and NO emissions during enclosed spray combustion of jet fuel","year":2024,"lang":"en","type":"article","venue":"Scientific Reports","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Institute of Particle Physics","funders":"Natural Sciences and Engineering Research Council of Canada; Schweizerischer Nationalfonds zur Förderung der Wissenschaftlichen Forschung","keywords":"Soot; Combustion; Combustor; Environmental science; NOx; Jet fuel; Jet (fluid); Fuel injection; Waste management; Chemistry; Aerospace engineering; Engineering","score_opus":0.012942843803924882,"score_gpt":0.24145486396899973,"score_spread":0.22851202016507485,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4402936998","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":[0.99391353,0.00038705126,0.0005290052,0.0001926193,0.0011335134,0.00019208892,0.000005001772,0.00024337131,0.0034038315],"genre_scores_gemma":[0.9966013,0.000024393607,0.0012354616,0.000002961333,0.00002081165,0.000006588522,0.000009585638,0.000009679951,0.0020892406],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9985452,0.00001744011,0.00031570726,0.00056684343,0.00034110842,0.00021364688],"domain_scores_gemma":[0.9993686,0.000043803197,0.00009646246,0.0004032,0.0000065810364,0.00008134275],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004529085,0.00011382698,0.00014437335,0.00009123272,0.00019531682,0.00008282355,0.000109200126,0.000075858276,0.00023280994],"category_scores_gemma":[0.00013054801,0.00009055467,0.000049485934,0.00043570393,0.0006031092,0.00027213394,0.0001581118,0.00013119586,0.00004378139],"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":[0.0000036466922,0.000040473133,0.07046107,0.000119377226,0.000013547322,0.00025326002,0.0004414671,0.00009369735,0.89789367,0.00007142513,0.005976783,0.02463159],"study_design_scores_gemma":[0.00020635601,0.00008924521,0.14088856,0.00032311186,0.00006580611,0.0002879338,0.00030413253,0.00044062748,0.69418514,0.052752662,0.109930776,0.0005256817],"about_ca_topic_score_codex":0.000007921012,"about_ca_topic_score_gemma":0.0000041113835,"teacher_disagreement_score":0.20370854,"about_ca_system_score_codex":0.0000521832,"about_ca_system_score_gemma":0.000016996344,"threshold_uncertainty_score":0.36927122},"labels":[],"label_agreement":null},{"id":"W4403416176","doi":"10.4050/f-0070-2014-9615","title":"Turboshaft After-Market Positioning: A Strategy Based Approach","year":2014,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Computer science","score_opus":0.007401378126925409,"score_gpt":0.20494630359576754,"score_spread":0.19754492546884214,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4403416176","genre_codex":"other","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":[0.025774334,0.000010833948,0.4699146,0.00018256462,0.000018520606,0.0001266483,0.0000015824542,0.0003966277,0.5035743],"genre_scores_gemma":[0.943569,0.0000010081724,0.053358972,0.00041934132,0.000010568733,0.00004519003,0.0000032757712,0.000009200285,0.002583449],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99922705,0.000032528817,0.000099619334,0.00026854157,0.00015150754,0.00022076184],"domain_scores_gemma":[0.9996146,0.000038612437,0.000026352087,0.00026444244,0.0000028815612,0.00005314175],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00011807967,0.00011279988,0.00008987104,0.000024893452,0.00006648598,0.00002810789,0.0001837372,0.00006881327,0.004089383],"category_scores_gemma":[0.000027575737,0.00009022504,0.000037254795,0.00015090505,0.00015291559,0.00014687638,0.00007166125,0.000092282564,0.00026580138],"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":[0.00058425654,0.0020301277,0.2023987,0.00011779449,0.000068684465,0.000083408384,0.0002456372,0.07649538,0.05953018,0.033311862,0.07235819,0.5527758],"study_design_scores_gemma":[0.002213641,0.0009914183,0.22199087,0.00004098897,0.000045256158,0.000043749063,0.00038008255,0.60342884,0.03420914,0.072137006,0.06262896,0.0018900089],"about_ca_topic_score_codex":0.00002431336,"about_ca_topic_score_gemma":0.0000077225695,"teacher_disagreement_score":0.91779464,"about_ca_system_score_codex":0.000042216787,"about_ca_system_score_gemma":0.000003158609,"threshold_uncertainty_score":0.996821},"labels":[],"label_agreement":null},{"id":"W4404276054","doi":"10.26434/chemrxiv-2024-lnmv4","title":"Greenhouse Gas Accounting Procedures in Low Carbon Fuel Policies Lead to Undervalued Benefits of Miscanthus-based Sustainable Aviation Fuel","year":2024,"lang":"en","type":"preprint","venue":"ChemRxiv","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"U.S. Department of Energy","keywords":"Miscanthus; Greenhouse gas; Lead (geology); Aviation; Environmental science; Aviation fuel; Carbon fibers; Carbon accounting; Fuel efficiency; Natural resource economics; Environmental economics; Business; Waste management; Engineering; Economics; Biofuel; Bioenergy; Materials science; Aerospace engineering","score_opus":0.014485059719010361,"score_gpt":0.2465076468074017,"score_spread":0.23202258708839132,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4404276054","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":[0.9920366,0.0010081733,0.00019219439,0.0012833935,0.00010160701,0.0008996546,0.000005913022,0.0003915063,0.0040809754],"genre_scores_gemma":[0.99742746,0.00011856639,0.0013181716,0.00012314295,0.000042274005,0.00018891547,0.000011104105,0.00006439758,0.00070593704],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9977158,0.00002281826,0.0004617414,0.00076915,0.0004209703,0.0006095269],"domain_scores_gemma":[0.99900126,0.000064521475,0.00022939249,0.00059735944,0.000041668518,0.0000658139],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0002715801,0.0003995967,0.0004386686,0.0003348714,0.000047035977,0.000068472575,0.0006226372,0.00038847915,0.000032190634],"category_scores_gemma":[0.000400823,0.00039520318,0.000110251975,0.00078306074,0.00022721982,0.00009839774,0.0013377963,0.00055587495,0.000033659926],"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":[0.00037493932,0.0012985109,0.16838855,0.030102422,0.00015317448,0.00018499172,0.00982403,0.6799845,0.08742531,0.005633892,0.0017193633,0.014910304],"study_design_scores_gemma":[0.0018905803,0.00045749627,0.12587905,0.0060185934,0.00022945032,0.0000105959225,0.0069567664,0.032127034,0.47010174,0.35230818,0.00048189575,0.003538637],"about_ca_topic_score_codex":0.0022874826,"about_ca_topic_score_gemma":0.0018411182,"teacher_disagreement_score":0.6478575,"about_ca_system_score_codex":0.0007048063,"about_ca_system_score_gemma":0.00013707494,"threshold_uncertainty_score":0.99985},"labels":[],"label_agreement":null},{"id":"W4404967222","doi":"10.1080/15568318.2024.2435558","title":"National climate change mitigation efforts for aviation: Lessons from post-Covid state action plans","year":2024,"lang":"en","type":"article","venue":"International Journal of Sustainable Transportation","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"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":"Coronavirus disease 2019 (COVID-19); 2019-20 coronavirus outbreak; Climate change; Aviation; Severe acute respiratory syndrome coronavirus 2 (SARS-CoV-2); Aeronautics; Action (physics); Pandemic; State (computer science); Business; Environmental planning; Environmental science; Engineering; Computer science; Medicine; Aerospace engineering; Virology","score_opus":0.022533016329110755,"score_gpt":0.30704932479267305,"score_spread":0.2845163084635623,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4404967222","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":[0.68967897,0.00027978598,0.29293552,0.012893843,0.0016640171,0.0007990773,0.0011501205,0.00022506119,0.00037357133],"genre_scores_gemma":[0.9954252,0.0002599678,0.0030424243,0.0002572039,0.00026915784,0.00007193792,0.0004744599,0.000020154966,0.00017949092],"study_design_codex":"design_other","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.9984287,0.00001777785,0.0004515463,0.00021358066,0.0006748453,0.00021354445],"domain_scores_gemma":[0.99908745,0.00014767953,0.0002631856,0.000057254587,0.0003853507,0.000059069313],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003474466,0.0001344148,0.00012614237,0.00024412197,0.00010789547,0.00010869524,0.00022496106,0.00008015812,0.0002074548],"category_scores_gemma":[0.00008230667,0.00012704275,0.00012671472,0.00018998965,0.00006270104,0.0019888582,0.000010179692,0.0001543332,0.000019073339],"study_design_candidate":"theoretical_or_conceptual","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":[0.0038550391,0.000823616,0.050306097,0.0006587742,0.0012764347,0.0025489952,0.020329336,0.077452205,0.057253778,0.31245884,0.0055019152,0.46753496],"study_design_scores_gemma":[0.0028837023,0.00066688814,0.31710157,0.00040575888,0.00024386637,0.00009977858,0.0060452293,0.008463415,0.019641003,0.55493134,0.08874075,0.0007767093],"about_ca_topic_score_codex":0.00014582064,"about_ca_topic_score_gemma":0.00028760676,"teacher_disagreement_score":0.46675825,"about_ca_system_score_codex":0.00064133765,"about_ca_system_score_gemma":0.00008482823,"threshold_uncertainty_score":0.5180653},"labels":[],"label_agreement":null},{"id":"W4405098997","doi":"10.22215/etd/2024-16346","title":"Life Cycle Analysis Frameworks in Sustainable Aviation","year":2024,"lang":"en","type":"dissertation","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Carleton University","funders":"Natural Sciences and Engineering Research Council of Canada; Mitacs","keywords":"Airframe; Life-cycle assessment; Aviation; Engineering; Environmental impact assessment; Retrofitting; Propulsion; Global warming; Global-warming potential; Sustainable development; Environmental economics; Environmental science; Climate change; Greenhouse gas; Aerospace engineering","score_opus":0.004083063534343364,"score_gpt":0.24614340223799458,"score_spread":0.2420603387036512,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4405098997","genre_codex":"other","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":[0.4366383,0.0012630931,0.034329537,0.0011736865,0.0004733206,0.0010585014,0.000006297984,0.0014643216,0.52359295],"genre_scores_gemma":[0.88022304,0.00008724309,0.0014899934,0.0001258914,0.00001158356,0.00006639013,0.00018939112,0.000019891855,0.117786564],"study_design_codex":"simulation_or_modeling","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.99884534,0.000014204887,0.00022377618,0.00041648233,0.00022381349,0.0002763588],"domain_scores_gemma":[0.9995856,0.000034980072,0.000065552296,0.00025192415,0.0000073098677,0.000054578533],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00011104983,0.00017286045,0.00023554631,0.00035154936,0.000047543042,0.000054908025,0.00020973657,0.00066331046,0.0031581004],"category_scores_gemma":[0.00022050437,0.0001547782,0.00011027724,0.0020335398,0.000030922405,0.00018367867,0.000066191555,0.000666287,0.00063054846],"study_design_candidate":"theoretical_or_conceptual","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":[0.0003074812,0.0009467264,0.14153941,0.0011969346,0.0020120617,0.0010778954,0.011502244,0.32640913,0.001957631,0.23189677,0.056271784,0.22488192],"study_design_scores_gemma":[0.00037989163,0.00011993643,0.20334822,0.00014296245,0.001255067,9.727579e-7,0.044550583,0.055265315,0.002234006,0.67090344,0.019890029,0.0019095631],"about_ca_topic_score_codex":0.00083665515,"about_ca_topic_score_gemma":0.0027523288,"teacher_disagreement_score":0.44358477,"about_ca_system_score_codex":0.00027682685,"about_ca_system_score_gemma":0.000022002087,"threshold_uncertainty_score":0.99775314},"labels":[],"label_agreement":null},{"id":"W4405099007","doi":"10.22215/etd/2024-16304","title":"Converting Carbon Dioxide into Synthetic Aviation Fuels: A Techno-Economic Assessment","year":2024,"lang":"en","type":"dissertation","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"Transport Canada","keywords":"Electricity; Waste management; Environmental science; Greenhouse gas; Syngas; Electricity generation; Aviation; Engineering; Cost of electricity by source; Resource (disambiguation); Environmental engineering; Environmental economics; Power (physics); Economics; Chemistry","score_opus":0.006632887823899182,"score_gpt":0.25723004302423347,"score_spread":0.25059715520033427,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4405099007","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":[0.6934504,0.0004924509,0.0015830375,0.00044140962,0.0010266948,0.0008687724,0.0000052744676,0.002069018,0.30006292],"genre_scores_gemma":[0.9828341,0.00012715938,0.0031245581,0.000031303796,0.000029945513,0.00020116725,0.00008842109,0.00006232334,0.013501038],"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99836195,0.000018157652,0.00039423574,0.00068580045,0.0002496192,0.00029027148],"domain_scores_gemma":[0.9993206,0.000048360584,0.00018000959,0.00039934748,0.000005402541,0.000046280486],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0001661931,0.00033298574,0.00029222295,0.00014170918,0.00009143594,0.00004332083,0.0003489588,0.00037587772,0.0007877703],"category_scores_gemma":[0.000038718455,0.0003026652,0.00010242018,0.00017383469,0.00008790573,0.00014781895,0.00013077552,0.00045189244,0.00084437145],"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":[0.00005510282,0.0001561276,0.006233795,0.00077897345,0.00021681465,0.00009997121,0.001545979,0.0015234976,0.48234499,0.018961795,0.0007244807,0.48735848],"study_design_scores_gemma":[0.0006035826,0.00036987197,0.0076500727,0.0010177641,0.00044669188,0.00002708424,0.016479021,0.03151316,0.5389686,0.38899678,0.01081482,0.0031125555],"about_ca_topic_score_codex":0.0012257128,"about_ca_topic_score_gemma":0.0014739571,"teacher_disagreement_score":0.48424593,"about_ca_system_score_codex":0.0012272809,"about_ca_system_score_gemma":0.000041749634,"threshold_uncertainty_score":0.99994254},"labels":[],"label_agreement":null},{"id":"W4405099181","doi":"10.1175/bams-d-23-0311.1","title":"Airborne Soil-Derived Dust Hazards in Aviation","year":2024,"lang":"en","type":"article","venue":"Bulletin of the American Meteorological Society","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"International Civil Aviation Organization; Air Canada","funders":"Barcelona Supercomputing Center; Österreichische Forschungsförderungsgesellschaft; AXA Research Fund; Belgian Federal Science Policy Office; University of Twente; European Commission","keywords":"Aviation; Visibility; Environmental science; Dust control; Aeronautics; Meteorology; Engineering; Aerospace engineering; Waste management","score_opus":0.009027092378836168,"score_gpt":0.23009669820725137,"score_spread":0.2210696058284152,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4405099181","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":[0.980329,0.00015739069,0.0030439554,0.014077894,0.000074901836,0.00019635296,0.000006059163,0.00021570447,0.0018987507],"genre_scores_gemma":[0.9880147,0.0001652847,0.0101640895,0.001285606,0.000016565487,0.000030696825,0.0000010328615,0.0000103766015,0.00031163855],"study_design_codex":"design_other","study_design_gemma":"observational","domain_scores_codex":[0.9988132,0.0001084812,0.00022271504,0.0003347406,0.0002518474,0.00026900086],"domain_scores_gemma":[0.9993863,0.00020178349,0.00010931695,0.00026521512,0.000005161126,0.00003223882],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00035775476,0.00013895323,0.00023637507,0.000011811038,0.00007026252,0.0000138365085,0.0004355159,0.00008143465,0.0010710324],"category_scores_gemma":[0.00020177555,0.00008423333,0.00023585913,0.00053651055,0.0013801854,0.000024874358,0.00038399443,0.00031495176,0.00018424162],"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":[0.00017760787,0.0005404546,0.07149802,0.000065037406,0.00014032367,0.000038042854,0.0009102757,0.007594075,0.3398976,0.003976628,0.12129802,0.45386392],"study_design_scores_gemma":[0.00046812434,0.0005753982,0.81525093,0.00005534533,0.00004872778,0.000010444164,0.0010276337,0.0046658525,0.023902297,0.02427586,0.12918511,0.00053426943],"about_ca_topic_score_codex":0.0003064093,"about_ca_topic_score_gemma":0.000009554679,"teacher_disagreement_score":0.7437529,"about_ca_system_score_codex":0.00013052284,"about_ca_system_score_gemma":0.000008327393,"threshold_uncertainty_score":0.9998421},"labels":[],"label_agreement":null},{"id":"W4405420564","doi":"10.1017/aer.2024.126","title":"Small aircraft flight trajectory optimisation using a multidisciplinary approach","year":2024,"lang":"en","type":"article","venue":"The Aeronautical Journal","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Toronto Metropolitan University","funders":"","keywords":"Trajectory; Multidisciplinary approach; Aeronautics; Aerospace engineering; Computer science; Engineering; Physics; Political science","score_opus":0.04724385846862859,"score_gpt":0.27054380358036645,"score_spread":0.22329994511173787,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4405420564","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":[0.48094153,0.00088284747,0.51096016,0.002125638,0.00033380406,0.00022410536,0.000002126759,0.00031755003,0.004212238],"genre_scores_gemma":[0.90775794,0.000053742337,0.09156432,0.00007913124,0.00013867315,0.000006488749,0.0000010749284,0.00002210226,0.0003765386],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.998818,0.00008441173,0.00022637933,0.00024036728,0.00028868695,0.0003421897],"domain_scores_gemma":[0.99953824,0.000114926064,0.000036730224,0.00020690521,0.00000543184,0.0000977392],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00044930167,0.00015469453,0.00012276179,0.000043236556,0.0003804864,0.00010608915,0.0003852146,0.00009339833,0.00041745536],"category_scores_gemma":[0.000039306626,0.00009120312,0.00010458975,0.00024369625,0.00044669057,0.00023919651,0.00022278696,0.00064213236,0.00018551975],"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":[0.00029368026,0.00089296576,0.0043062973,0.00011338653,0.00030273307,0.0010069722,0.005495241,0.26605907,0.28805062,0.016532987,0.0045913323,0.41235468],"study_design_scores_gemma":[0.0006908706,0.00033066308,0.0132329995,0.00015287109,0.00020343023,0.004732985,0.0014700853,0.89128083,0.006465714,0.07323034,0.0074272654,0.0007819209],"about_ca_topic_score_codex":0.000007340839,"about_ca_topic_score_gemma":0.000002469034,"teacher_disagreement_score":0.6252218,"about_ca_system_score_codex":0.0002617503,"about_ca_system_score_gemma":0.000026335692,"threshold_uncertainty_score":0.45708436},"labels":[],"label_agreement":null},{"id":"W4406106693","doi":"10.54097/3fb71s08","title":"Innovative Wing Design: Advancements in Aerodynamics, Materials, and Computational Analysis","year":2024,"lang":"en","type":"article","venue":"Highlights in Science Engineering and Technology","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Aurora College","funders":"","keywords":"Aerodynamics; Wing; Aerospace engineering; Engineering; Computer science; Aeronautics","score_opus":0.007121115417521487,"score_gpt":0.23042222399039222,"score_spread":0.22330110857287072,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4406106693","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":[0.9089694,0.00023862481,0.08963259,0.000617615,0.00010236771,0.0001246408,0.0000031073603,0.00026657045,0.000045088218],"genre_scores_gemma":[0.9560126,0.00011277339,0.043821342,0.0000072028624,0.0000030908138,0.000022246742,0.0000013610078,0.000005936583,0.000013438026],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989262,0.000007134559,0.00019092594,0.00045502683,0.00014278383,0.00027790418],"domain_scores_gemma":[0.999772,0.000058215934,0.000021490361,0.00011613285,0.000008986131,0.000023135413],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003358913,0.00012224572,0.00016904404,0.0013865957,0.00006131117,0.00004951048,0.00018567576,0.00008161477,0.000009131378],"category_scores_gemma":[0.00007654344,0.00010797466,0.000005922914,0.0065273335,0.00061727763,0.00035304797,0.00021869299,0.00013901298,0.000012235565],"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":[0.00000985168,0.000053687952,0.030577607,0.00003556434,0.00004257416,0.00020209585,0.0004865828,0.39533818,0.29978627,0.2521127,0.000014186303,0.021340705],"study_design_scores_gemma":[0.00053296116,0.00016241534,0.10338365,0.00019381102,0.000028148013,0.000048671616,0.00029431374,0.7917436,0.050043203,0.051159713,0.0016621654,0.00074736757],"about_ca_topic_score_codex":0.000018480474,"about_ca_topic_score_gemma":0.000017238703,"teacher_disagreement_score":0.3964054,"about_ca_system_score_codex":0.00014956297,"about_ca_system_score_gemma":0.000012882308,"threshold_uncertainty_score":0.4403079},"labels":[],"label_agreement":null},{"id":"W4406470873","doi":"10.1016/0967-0653(95)95770-7","title":"10.1016/0967-0653(95)95770-7","year":2000,"lang":"en","type":"article","venue":"Time to knit","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Environmental science; Marine stratocumulus; Atmospheric sciences; Radiation; Absorption (acoustics); Meteorology; Physics; Optics; Aerosol","score_opus":0.00598983555716176,"score_gpt":0.17105178600554774,"score_spread":0.16506195044838598,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4406470873","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.00068439485,0.000035544934,0.000022118034,0.0002565748,9.320683e-7,0.00015302614,0.0000051274537,0.00042563985,0.99841666],"genre_scores_gemma":[0.00069409685,8.126877e-7,0.0014591798,0.00005868736,0.000020402056,0.000022330843,0.0000037116745,0.000016582077,0.9977242],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9991084,0.000015514568,0.00011991166,0.00027950783,0.00017739894,0.00029930653],"domain_scores_gemma":[0.9995293,0.000026380942,0.000019288915,0.0003301738,0.0000028012225,0.000092079244],"candidate_categories":["insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.00006860582,0.00013245574,0.00011628014,0.000021350537,0.00008969884,0.000018882058,0.00033944572,0.0000700879,0.99878114],"category_scores_gemma":[0.000028057812,0.000119756136,0.000039168586,0.0002504196,0.00012772209,0.0001527697,0.00010941811,0.00010502718,0.9989076],"study_design_candidate":"not_applicable","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":[0.000015910446,0.000026708762,8.8917807e-7,7.094992e-7,0.000002577555,0.0000071608592,0.000006015676,0.00036350783,0.0003133097,0.0000013143999,0.16752851,0.8317334],"study_design_scores_gemma":[0.00010632001,0.00009940646,0.00007333473,0.0000044787234,0.000004237295,0.0000070280526,0.0000015457455,0.00015285365,0.0008289662,0.00022698677,0.99831784,0.00017700878],"about_ca_topic_score_codex":0.000021496484,"about_ca_topic_score_gemma":4.0017767e-7,"teacher_disagreement_score":0.8315564,"about_ca_system_score_codex":0.000069269525,"about_ca_system_score_gemma":0.0000031357072,"threshold_uncertainty_score":0.48835135},"labels":[],"label_agreement":null},{"id":"W4406681403","doi":"10.1051/e3sconf/202560601002","title":"Critical Development of Electric Fixed-Wing Manned Civil Aircraft","year":2025,"lang":"en","type":"article","venue":"E3S Web of Conferences","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Western University","funders":"","keywords":"Fixed wing; Aerospace engineering; Aeronautics; Wing; Environmental science; Engineering","score_opus":0.014330230513006895,"score_gpt":0.26087513301394366,"score_spread":0.24654490250093677,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4406681403","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":[0.7993094,0.00037618954,0.042854127,0.000870043,0.00017610725,0.00022482329,0.0000029916635,0.00017801991,0.15600835],"genre_scores_gemma":[0.98867464,0.000031574036,0.010863055,0.000039879396,0.0000035826677,0.000013298137,9.720287e-7,0.0000034411632,0.00036955113],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9989803,0.000024556568,0.00032365823,0.0002188691,0.00022646927,0.00022618941],"domain_scores_gemma":[0.99951327,0.00019086791,0.00006883212,0.00017345145,0.000024768538,0.000028783583],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015387055,0.000116745905,0.00022441131,0.00010808763,0.00007790272,0.000009899258,0.00035983193,0.00007952313,0.0006908471],"category_scores_gemma":[0.00025813817,0.00010016438,0.000041332496,0.00040248397,0.0003382372,0.000119118275,0.00015959938,0.00010292076,0.000026784503],"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":[0.000066902314,0.00033602625,0.23293248,0.0001695333,0.000076129,0.000008801549,0.00037958962,0.00010284223,0.36042204,0.10275481,0.0016008418,0.30115002],"study_design_scores_gemma":[0.0003787298,0.00015000234,0.11730739,0.0001702586,0.000024699058,0.000001476725,0.00057925103,0.0009641378,0.8156929,0.04577802,0.018659076,0.00029405928],"about_ca_topic_score_codex":0.000019617457,"about_ca_topic_score_gemma":0.00007875106,"teacher_disagreement_score":0.45527086,"about_ca_system_score_codex":0.00003666705,"about_ca_system_score_gemma":0.00024329066,"threshold_uncertainty_score":0.75642914},"labels":[],"label_agreement":null},{"id":"W4407412982","doi":"10.2514/6.2025-0849","title":"New Methodology for Aerodynamic Forces Calculations in Unmanned Aerial Systems Optimization Design","year":2025,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure","funders":"","keywords":"Aerodynamics; Aerospace engineering; Aerodynamic force; Computer science; Design methods; Control engineering; Engineering; Systems engineering; Mechanical engineering","score_opus":0.04451065656571073,"score_gpt":0.30643295466822984,"score_spread":0.2619222981025191,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4407412982","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":[0.001336953,0.000036715934,0.9953168,0.00035708834,0.00022816262,0.00073887483,0.0000014219214,0.00015875406,0.0018252184],"genre_scores_gemma":[0.19204453,0.000012109359,0.80362165,0.00005492635,0.000010767106,0.000119177355,0.000007127873,0.0000066276857,0.0041230875],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99924153,0.00008562804,0.00019661456,0.00023176082,0.000055969485,0.00018851784],"domain_scores_gemma":[0.99943,0.00035384778,0.000041443367,0.00014824703,0.00000540718,0.000021037657],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002596653,0.00009044135,0.0001469681,0.00009064003,0.00007283043,0.00001740314,0.00015924551,0.00011308852,0.00011401128],"category_scores_gemma":[0.00022865502,0.00007957308,0.000027851585,0.00034682013,0.000055701774,0.00014430254,0.000060247712,0.00004586584,0.000009345675],"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":[0.00003420664,0.000009279187,0.00049341144,0.000004208728,0.0000045967026,3.5642435e-7,0.000019445783,0.97286355,0.0032084496,0.018094353,0.00086221006,0.004405909],"study_design_scores_gemma":[0.0009248933,0.000083324965,0.0012177945,0.000016339009,0.000015775438,0.0000014680916,0.0002217617,0.9586941,0.0025919585,0.034865208,0.0011923714,0.00017498026],"about_ca_topic_score_codex":0.00044772998,"about_ca_topic_score_gemma":0.00033182613,"teacher_disagreement_score":0.19169517,"about_ca_system_score_codex":0.00013559905,"about_ca_system_score_gemma":0.000018750265,"threshold_uncertainty_score":0.32448962},"labels":[],"label_agreement":null},{"id":"W4407414111","doi":"10.2514/6.2025-1718","title":"Thermodynamic Analysis of Commercial Aircraft Environmental Control Systems","year":2025,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Safran Electronics (Canada)","funders":"","keywords":"Environmental control system; Environmental science; Control (management); Computer science; Aerospace engineering; Engineering","score_opus":0.004913712552356404,"score_gpt":0.2157540363009392,"score_spread":0.2108403237485828,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4407414111","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":[0.7289259,0.00013852178,0.23885837,0.00020432322,0.00009680596,0.0003125669,0.000044138105,0.0001599353,0.031259436],"genre_scores_gemma":[0.99797624,0.000019166213,0.00037925164,0.00014113187,0.0000024662102,0.000019861001,0.000006930074,0.0000046932973,0.0014502393],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.9991725,0.000036958572,0.00023192282,0.0002227833,0.00016200313,0.000173823],"domain_scores_gemma":[0.999507,0.00007960801,0.00006627063,0.00032196188,0.000001540448,0.000023632687],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00009838124,0.00011461161,0.00029157806,0.00014200623,0.0000612312,0.000007824416,0.0002722228,0.00007749955,0.0008669798],"category_scores_gemma":[0.000011521202,0.000093379495,0.00012252448,0.00056716776,0.00029918822,0.00007908456,0.000110889174,0.00007529015,0.000056108565],"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":[0.00006458629,0.0003208178,0.7785976,0.00001166161,0.0012439957,0.0000066932375,0.000074398915,0.05303076,0.119709946,0.008799947,0.0008560722,0.037283536],"study_design_scores_gemma":[0.000806024,0.00006839381,0.7736874,0.000009069768,0.0008183589,8.28909e-7,0.00044928215,0.21813571,0.0022504532,0.0011906907,0.0023218072,0.00026198817],"about_ca_topic_score_codex":0.00022073944,"about_ca_topic_score_gemma":0.00008256414,"teacher_disagreement_score":0.26905036,"about_ca_system_score_codex":0.00012455368,"about_ca_system_score_gemma":0.0000033738606,"threshold_uncertainty_score":0.9492821},"labels":[],"label_agreement":null},{"id":"W4407414623","doi":"10.2514/6.2025-0600","title":"Contrail Formation Simulation via FANS-Based Turbulence Modelling Combined With Two-Equation Soot/Ice Particle Transport Modelling","year":2025,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Institute for Christian Studies; University of Toronto","funders":"","keywords":"Turbulence; Soot; Smoothed-particle hydrodynamics; Environmental science; Particle (ecology); Meteorology; Mechanics; Computer science; Physics; Geology; Chemistry; Combustion","score_opus":0.023633458804663495,"score_gpt":0.23672829292035552,"score_spread":0.21309483411569202,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4407414623","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":[0.21086974,0.000011750337,0.78705764,0.00021291319,0.000015354799,0.0003529213,9.852625e-7,0.00031268192,0.001165985],"genre_scores_gemma":[0.9558435,0.000005460993,0.043704867,0.00020469792,0.0000034848513,0.0000395073,0.000015548903,0.000009621947,0.00017327607],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989012,0.000022788397,0.0002795377,0.0002831704,0.00025793526,0.00025537206],"domain_scores_gemma":[0.9995286,0.00010145383,0.000082044375,0.00022344092,0.000026028965,0.00003846047],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016511361,0.00015572662,0.00014080525,0.000044712815,0.00019197637,0.000022880287,0.00014262152,0.00006894025,0.00007538121],"category_scores_gemma":[0.0000069748485,0.00012956565,0.000034953322,0.0003837748,0.00011228438,0.00079255895,0.000013402584,0.00011029954,0.00003073516],"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":[0.00015027485,0.00005018632,0.0013024609,0.000010858329,0.0000044432545,0.0000012391863,0.0001022809,0.98906004,0.0018535001,0.0014552686,0.000002229182,0.006007186],"study_design_scores_gemma":[0.0010710115,0.000088095956,0.000116779695,0.00003128544,0.000022120696,2.8001347e-7,0.00007939126,0.95841753,0.029691156,0.010259696,0.00005370094,0.00016894966],"about_ca_topic_score_codex":0.00013788926,"about_ca_topic_score_gemma":0.000089074674,"teacher_disagreement_score":0.7449738,"about_ca_system_score_codex":0.00012617737,"about_ca_system_score_gemma":0.000013017176,"threshold_uncertainty_score":0.5283534},"labels":[],"label_agreement":null},{"id":"W4407415519","doi":"10.2514/6.2025-1435","title":"Parallel Hybrid Turboprop Performance Modeling and Optimization","year":2025,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":6,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Turboprop; Computer science; Aerospace engineering; Engineering","score_opus":0.009579715257347963,"score_gpt":0.2124295789683685,"score_spread":0.20284986371102054,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4407415519","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":[0.145645,0.00004307162,0.8356256,0.00024301317,0.00001842639,0.00007359198,1.542884e-7,0.00014807336,0.018203063],"genre_scores_gemma":[0.86171037,0.00018245004,0.13629408,0.00014689678,0.0000017111486,0.0000076982615,7.6630204e-7,0.0000024304923,0.0016536019],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996358,0.0000032933208,0.00006746773,0.00014446162,0.000050637886,0.000098345554],"domain_scores_gemma":[0.99987066,0.0000060950583,0.000009639276,0.00009838606,0.000002305946,0.000012911613],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000035250603,0.000054920005,0.000048264497,0.000019881601,0.000078778976,0.000011582878,0.0000731926,0.000021380305,0.0001342918],"category_scores_gemma":[0.000011411897,0.000044219752,0.000007373805,0.0000886358,0.000060816634,0.00017344006,0.0001053747,0.000046382986,0.000019322057],"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":[0.0000040411724,0.0000057629995,0.0029808737,0.0000030060148,0.0000012780358,4.5364368e-7,0.000005592267,0.96468586,0.00020828833,0.00042463234,0.000116990006,0.03156322],"study_design_scores_gemma":[0.000099734076,0.000011343019,0.00028342826,0.000005219402,0.0000020903162,0.000001505884,0.000023304472,0.9951514,0.0013471835,0.0027804708,0.00023534794,0.000058952606],"about_ca_topic_score_codex":0.000011886783,"about_ca_topic_score_gemma":0.0000016310153,"teacher_disagreement_score":0.71606535,"about_ca_system_score_codex":0.000024047078,"about_ca_system_score_gemma":0.0000020390257,"threshold_uncertainty_score":0.18032292},"labels":[],"label_agreement":null},{"id":"W4407415718","doi":"10.2514/6.2025-1823","title":"Withdrawn: Conceptual Design of a Piloted Quarter-Scale Flying-V Research Airplane","year":2025,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Airplane; Aeronautics; Quarter (Canadian coin); Scale (ratio); Computer science; Conceptual design; Engineering; Aerospace engineering; Human–computer interaction; History; Geography; Cartography","score_opus":0.046765206380885625,"score_gpt":0.31450903568805977,"score_spread":0.26774382930717416,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4407415718","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":[0.15164594,0.00011520813,0.76717776,0.0011584198,0.000090430905,0.0008101158,0.000005000869,0.00046397457,0.078533135],"genre_scores_gemma":[0.96827656,0.000015298698,0.0259048,0.00008402267,0.000004418577,0.000033564986,0.000001439111,0.0000061885216,0.005673706],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99874896,0.00010863267,0.00020010713,0.00029759633,0.00031540138,0.0003293265],"domain_scores_gemma":[0.9992795,0.0002671774,0.00003438298,0.00036032483,0.00001963068,0.000038975475],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0004084979,0.00010473223,0.00016541911,0.00009800783,0.00016602076,0.000012204375,0.00039170322,0.00009268724,0.0009952452],"category_scores_gemma":[0.00009872345,0.00008511675,0.000026137996,0.0006927762,0.0012923331,0.00012255284,0.00020997976,0.00021265208,0.0002343622],"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":[0.0005388471,0.0007849415,0.04902192,0.000050955645,0.0000730599,0.00004967613,0.0026059244,0.004387243,0.68627447,0.035596833,0.1301341,0.090482056],"study_design_scores_gemma":[0.0037008922,0.0035245619,0.028803814,0.0002382307,0.000040865354,0.00002182919,0.026538707,0.017165167,0.7582273,0.13217723,0.02848668,0.0010747268],"about_ca_topic_score_codex":0.00019588675,"about_ca_topic_score_gemma":0.000052950083,"teacher_disagreement_score":0.8166306,"about_ca_system_score_codex":0.00008147685,"about_ca_system_score_gemma":0.000023082051,"threshold_uncertainty_score":0.999918},"labels":[],"label_agreement":null},{"id":"W4407416714","doi":"10.2514/6.2025-0427","title":"Withdrawn: Design and Wind Tunnel Testing of a Whirl Flutter Model to Evaluate Distributed Propulsion Arrangements","year":2025,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"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":"","keywords":"Flutter; Propulsion; Wind tunnel; Aerospace engineering; Aerodynamics; Computer science; Aeronautics; Marine engineering; Engineering; Automotive engineering","score_opus":0.03543245911132181,"score_gpt":0.27017529586017497,"score_spread":0.23474283674885316,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4407416714","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":[0.31000564,0.0000096443755,0.687416,0.00044920848,0.000013925889,0.0004822609,0.0000046089754,0.000088116794,0.0015305757],"genre_scores_gemma":[0.7834441,0.0000020436826,0.21548735,0.00016913748,0.0000014116822,0.000021271288,0.0000013081942,0.0000051040365,0.00086829474],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991397,0.000023067309,0.00017211265,0.00028975453,0.0001746144,0.00020073084],"domain_scores_gemma":[0.9996513,0.000047899204,0.00004133064,0.00020235703,0.000015687105,0.000041412324],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001846388,0.00012033261,0.00013433771,0.000047775975,0.00008548738,0.000014228696,0.0001608631,0.000047960995,0.000049551858],"category_scores_gemma":[0.00015996926,0.00009211198,0.0000141550845,0.0004015269,0.0001211982,0.0001373884,0.00027789918,0.0000632211,0.000019929164],"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":[0.000091845875,0.000108017455,0.032546673,0.00003069883,0.000018971803,0.0000036467468,0.00012691341,0.18022588,0.7021537,0.00013735335,0.0038144975,0.0807418],"study_design_scores_gemma":[0.0013404816,0.00038209258,0.053203844,0.0002167783,0.000059060843,0.0000034147702,0.00023070097,0.6777702,0.21053338,0.055469405,0.00032394024,0.00046671354],"about_ca_topic_score_codex":0.000030288746,"about_ca_topic_score_gemma":0.000008168129,"teacher_disagreement_score":0.49754432,"about_ca_system_score_codex":0.000062157626,"about_ca_system_score_gemma":0.00000948014,"threshold_uncertainty_score":0.37562177},"labels":[],"label_agreement":null},{"id":"W4407679334","doi":"10.2514/6.2024-1538.c1","title":"Correction: System Integration Study for a Hybrid-Electric Commuter Aircraft Concept with a Solar Auxiliary Power System","year":2024,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Concordia University","funders":"","keywords":"Computer science; Auxiliary power unit; Electric power system; Power (physics); Aerospace engineering; Electrical engineering; Automotive engineering; Aeronautics; Engineering; Physics; Voltage","score_opus":0.007812901066922479,"score_gpt":0.22455265610330347,"score_spread":0.216739755036381,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4407679334","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":[0.045890357,0.00021311229,0.94042,0.00015278274,0.000991637,0.0021080826,0.000009120391,0.0029349,0.007280057],"genre_scores_gemma":[0.99403524,0.0000015355173,0.0026242025,0.000043832017,0.000030376477,0.00044293533,0.000006050495,0.000031863277,0.0027839672],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9986387,0.00005821639,0.0002538226,0.0004930104,0.0002630532,0.0002932084],"domain_scores_gemma":[0.9993762,0.00014949417,0.00004896831,0.0003532573,0.000019959236,0.00005213204],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002179289,0.00023020776,0.00023222077,0.00009312305,0.00021860874,0.00011313928,0.0002397237,0.0000654867,0.00009299301],"category_scores_gemma":[0.000018306027,0.00015418384,0.000068117246,0.00048416914,0.00008999773,0.00038461087,0.000080618614,0.00021966602,0.00019216163],"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":[0.001538902,0.0027492826,0.03179198,0.0013048282,0.0013806635,0.0023354904,0.012024027,0.008750547,0.026859181,0.03309728,0.35179773,0.52637005],"study_design_scores_gemma":[0.0035861284,0.0115881255,0.004777446,0.0014812284,0.00046852193,0.0022499897,0.104625754,0.75366896,0.089615576,0.000500011,0.025102306,0.0023359745],"about_ca_topic_score_codex":0.000119310105,"about_ca_topic_score_gemma":0.000081509024,"teacher_disagreement_score":0.94814485,"about_ca_system_score_codex":0.000629664,"about_ca_system_score_gemma":0.000021205024,"threshold_uncertainty_score":0.62874347},"labels":[],"label_agreement":null},{"id":"W4407766134","doi":"10.3390/aerospace12030164","title":"Exploration of Solar Power System Integration for Sustainable Air Transportation—A Case Study for Seaplane Air Taxi Operations","year":2025,"lang":"en","type":"article","venue":"Aerospace","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Concordia University","funders":"Natural Sciences and Engineering Research Council of Canada; Concordia University","keywords":"Solar power; Air transport; Power (physics); Sustainable transport; Environmental science; Meteorology; Transport engineering; Engineering; Geography; Sustainability; Physics","score_opus":0.013711535656431845,"score_gpt":0.26586513739831535,"score_spread":0.2521536017418835,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4407766134","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":[0.3135406,0.000017105196,0.6834642,0.0004611,0.000052774154,0.0021376433,0.000028734099,0.00013777426,0.00016004026],"genre_scores_gemma":[0.98218966,0.0000021464493,0.013686888,0.00003614878,0.000004954957,0.0009224072,0.000041940388,0.000010384149,0.0031054511],"study_design_codex":"simulation_or_modeling","study_design_gemma":"qualitative","domain_scores_codex":[0.99922913,0.00002016417,0.0002285486,0.00024618531,0.00009896026,0.0001769852],"domain_scores_gemma":[0.9995406,0.00007702461,0.000063249274,0.00021700753,0.00008029098,0.000021782373],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018897443,0.000115750845,0.00015445382,0.000052768624,0.00028443002,0.00001595373,0.00010626553,0.000068361056,0.000008071674],"category_scores_gemma":[0.00007827595,0.000105119405,0.000047363712,0.00027970027,0.000058922207,0.0006761129,0.000014892079,0.000053316562,0.0000030916917],"study_design_candidate":"qualitative","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":[0.0010412354,0.003293408,0.025610907,0.001408203,0.00037827482,0.00057897106,0.040286977,0.47274074,0.07632357,0.33290562,0.03096392,0.0144681875],"study_design_scores_gemma":[0.005001724,0.0029951509,0.004301537,0.00014140306,0.0002835204,0.00003503147,0.78657794,0.01866213,0.16629069,0.005414001,0.009517073,0.0007798062],"about_ca_topic_score_codex":0.0005420629,"about_ca_topic_score_gemma":0.0027458568,"teacher_disagreement_score":0.746291,"about_ca_system_score_codex":0.00016945347,"about_ca_system_score_gemma":0.000023500526,"threshold_uncertainty_score":0.4286645},"labels":[],"label_agreement":null},{"id":"W4407779780","doi":"10.3390/act14030104","title":"Optimized Structural Design of a Reciprocating Wing for the Reciprocating Airfoil (RA)-Driven Vertical Take-Off and Landing (VTOL) Aircraft","year":2025,"lang":"en","type":"article","venue":"Actuators","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"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 Alberta","funders":"","keywords":"Reciprocating motion; Airfoil; Wing; Aerospace engineering; Engineering; Aerodynamics; Computer science; Aeronautics","score_opus":0.018836817251302866,"score_gpt":0.26730205468525503,"score_spread":0.24846523743395216,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4407779780","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":[0.30302772,0.00023156704,0.6947388,0.0006754325,0.00013011013,0.0007454192,0.0000024084322,0.00015681062,0.0002917656],"genre_scores_gemma":[0.84347147,0.0000462925,0.15619382,0.00010992222,0.000014701324,0.00008517787,0.0000012435311,0.0000141538585,0.00006319461],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9988021,0.000046631463,0.00031063406,0.00034277228,0.00016638958,0.00033146288],"domain_scores_gemma":[0.9982492,0.0013319165,0.000092142735,0.00027007132,0.000015574285,0.000041123432],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00034765463,0.00017930093,0.00024483318,0.000053649943,0.00039260526,0.0000314572,0.00033058532,0.00010420938,0.000028015007],"category_scores_gemma":[0.0012405922,0.00012575033,0.00005864086,0.0003175774,0.00033496562,0.00020102093,0.00023614282,0.00018200814,0.000002814567],"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":[0.00039918744,0.000041709387,0.03901229,0.0001133358,0.00017234377,0.0000047072926,0.002385961,0.033127207,0.061699122,0.0023123142,0.00070505106,0.8600268],"study_design_scores_gemma":[0.0036664056,0.0004486071,0.0166142,0.0005370928,0.00030528547,0.000024726896,0.0061924676,0.840134,0.100048624,0.029339295,0.001728449,0.0009608144],"about_ca_topic_score_codex":0.000035004297,"about_ca_topic_score_gemma":0.000006717695,"teacher_disagreement_score":0.85906595,"about_ca_system_score_codex":0.0001074738,"about_ca_system_score_gemma":0.000023411962,"threshold_uncertainty_score":0.512795},"labels":[],"label_agreement":null},{"id":"W4407803427","doi":"10.5281/zenodo.14755156","title":"IMOTHEP European project: An investigation of the potential of hybrid electric propulsion for reducing emissions of commercial aircraft","year":2024,"lang":"en","type":"article","venue":"elib (German Aerospace Center)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Safran Electronics (Canada)","funders":"European Commission","keywords":"Propulsion; Electrically powered spacecraft propulsion; Aerospace engineering; Aeronautics; Automotive engineering; Environmental science; Engineering","score_opus":0.013157506990989514,"score_gpt":0.2594092476285445,"score_spread":0.24625174063755498,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4407803427","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":[0.9938824,0.00007152785,0.0041864053,0.00061687524,0.00021691831,0.0006549323,0.00003755147,0.0001067928,0.00022660244],"genre_scores_gemma":[0.99683076,0.000029973717,0.0027665047,0.000026520052,0.00003115089,0.00001262763,0.000014830919,0.000029765168,0.000257864],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9988333,0.00010474637,0.0003248702,0.0002794067,0.00024610836,0.00021159711],"domain_scores_gemma":[0.9993647,0.000026645796,0.00019451139,0.00035357967,0.000020227928,0.000040384144],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024091921,0.00013929678,0.00017270051,0.000071537455,0.00010228734,0.000012723519,0.00037846706,0.00003773552,0.000021291547],"category_scores_gemma":[0.000053229785,0.000099612946,0.0001136401,0.0003951434,0.00028386933,0.00021740339,0.00019447932,0.00015058891,0.000003686797],"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":[0.000031780477,0.00008874374,0.004715088,0.000103993414,0.000009922222,0.0000021498668,0.0006565568,0.00013879173,0.97631675,0.0001272323,0.0024485607,0.015360436],"study_design_scores_gemma":[0.00038463817,0.0003412654,0.03146523,0.00032488213,0.000037969538,0.000016838003,0.00013947922,0.004429156,0.96037054,0.0012082536,0.0011071018,0.00017462908],"about_ca_topic_score_codex":0.000035764366,"about_ca_topic_score_gemma":0.0000067273972,"teacher_disagreement_score":0.026750142,"about_ca_system_score_codex":0.000057123827,"about_ca_system_score_gemma":0.000029655777,"threshold_uncertainty_score":0.4062098},"labels":[],"label_agreement":null},{"id":"W4408308061","doi":"10.2514/1.c037774","title":"Zonal Safety and Particular Risk Analysis for Early Aircraft Design","year":2025,"lang":"en","type":"article","venue":"Journal of Aircraft","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Bombardier (Canada); Concordia University","funders":"Natural Sciences and Engineering Research Council of Canada; Consortium de Recherche et d’innovation en Aérospatiale au Québec; Bombardier","keywords":"Aeronautics; Computer science; Aerospace engineering; Engineering; Risk analysis (engineering); Environmental science; Business","score_opus":0.010930005779953612,"score_gpt":0.2439142501430028,"score_spread":0.23298424436304918,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4408308061","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.114953764,0.0004289413,0.88304454,0.0010169668,0.00009387407,0.00021336938,0.000009370719,0.0000409921,0.00019819872],"genre_scores_gemma":[0.86454153,0.0004086019,0.13422775,0.00017814574,0.000030147454,0.000009264742,8.4076925e-7,0.000011292539,0.0005924236],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.9985149,0.000094350224,0.0005514253,0.00025135666,0.0002836688,0.0003042891],"domain_scores_gemma":[0.99887884,0.00039595287,0.00033465624,0.00023532586,0.000049233597,0.000106005864],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00085214974,0.0001788751,0.00043509665,0.00024494095,0.00021190986,0.000042863445,0.00030588618,0.00012102983,0.0001174861],"category_scores_gemma":[0.00039608264,0.0001428434,0.00028435374,0.0007801554,0.0002616082,0.00032805777,0.00011724534,0.00026525525,0.000011215585],"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":[0.0012308147,0.00030859662,0.7705995,0.000031374868,0.0022130047,0.000086738306,0.00035775686,0.10875858,0.0058033643,0.0009321834,0.006341327,0.10333678],"study_design_scores_gemma":[0.0032860097,0.0013206706,0.850245,0.00007870213,0.0029027702,0.000051741994,0.00032879997,0.014195629,0.011308132,0.049295023,0.06635434,0.0006332051],"about_ca_topic_score_codex":0.00002436588,"about_ca_topic_score_gemma":0.000017314254,"teacher_disagreement_score":0.7495878,"about_ca_system_score_codex":0.00012614127,"about_ca_system_score_gemma":0.000030562536,"threshold_uncertainty_score":0.5824985},"labels":[],"label_agreement":null},{"id":"W4408430456","doi":"10.5194/egusphere-egu25-14302","title":"Stochastic modeling of contrail formation","year":2025,"lang":"en","type":"preprint","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"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":"Computer science; Environmental science","score_opus":0.023012017962649206,"score_gpt":0.2504769932797772,"score_spread":0.22746497531712798,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4408430456","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":[0.0066967546,0.00004450898,0.96379864,0.00009434998,0.000070184,0.00022310115,0.000011012783,0.00015460413,0.028906861],"genre_scores_gemma":[0.97920024,0.000019454914,0.020003954,0.00003610773,0.0000034284192,0.000024773675,0.0000069426883,0.0000029286782,0.0007021916],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99938464,0.0000076053907,0.0002036679,0.0001717292,0.00012548674,0.00010684217],"domain_scores_gemma":[0.99962825,0.000023829181,0.000075442076,0.0002515455,0.0000073268848,0.000013620519],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00006336856,0.00010265597,0.0001561709,0.00004007855,0.00002392591,0.000005871574,0.00024063628,0.0001424848,0.00020813657],"category_scores_gemma":[0.000049143724,0.00008888525,0.000048181886,0.00006295085,0.000067054614,0.00008159792,0.000642734,0.00017507772,0.000023068678],"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":[0.0000042265588,0.000012400617,0.000017177308,0.00003254538,0.0000046277455,2.2600771e-7,0.00005209075,0.98282444,0.0004809575,0.0014320556,0.00012796829,0.0150113],"study_design_scores_gemma":[0.00008783947,0.000009056129,0.000014099539,0.00005955618,0.00001036691,3.9002987e-7,0.00008292696,0.9097871,0.0014365723,0.08838011,0.000035146502,0.000096786294],"about_ca_topic_score_codex":0.00009157568,"about_ca_topic_score_gemma":0.000028315731,"teacher_disagreement_score":0.9725035,"about_ca_system_score_codex":0.000076391014,"about_ca_system_score_gemma":0.000008997243,"threshold_uncertainty_score":0.36246353},"labels":[],"label_agreement":null},{"id":"W4408964180","doi":"10.1016/j.fuel.2025.135186","title":"Multi-objective optimization of hybridized turbofan engines using eco-friendly fuels","year":2025,"lang":"en","type":"article","venue":"Fuel","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":3,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Ontario Tech University","funders":"Natural Sciences and Engineering Research Council of Canada; Research and Development; Transport Canada","keywords":"Turbofan; Environmentally friendly; Environmental science; Process engineering; Biochemical engineering; Computer science; Automotive engineering; Engineering; Ecology; Biology","score_opus":0.011981606919077407,"score_gpt":0.25086866087350096,"score_spread":0.23888705395442356,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4408964180","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.14264263,0.00021121593,0.85128444,0.00008232762,0.00019025934,0.000288773,0.000011151315,0.00021219227,0.0050769835],"genre_scores_gemma":[0.7679001,0.000032355183,0.23169962,0.000029700162,0.000005184139,0.0000075410744,0.0000024891763,0.000006632288,0.0003163457],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993799,0.000018540983,0.00015148224,0.00020732115,0.00009227145,0.00015049551],"domain_scores_gemma":[0.99967015,0.000039773637,0.00006728252,0.00019194222,0.000012440622,0.000018384844],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000061885796,0.000101007994,0.00013706161,0.000066819906,0.000055385837,0.000007923042,0.00016079897,0.000057543235,0.0001572687],"category_scores_gemma":[0.00012403745,0.00009286836,0.000040216684,0.00034603337,0.00014907391,0.0001716665,0.0001277217,0.0000698535,0.000013335319],"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":[0.0000679028,0.00024877465,0.016934536,0.00007902468,0.000052195617,0.000010950531,0.00042241774,0.674439,0.29024917,0.00062938035,0.00035999712,0.01650663],"study_design_scores_gemma":[0.0029829775,0.00018861209,0.02782207,0.00014993752,0.000092883536,0.000010503887,0.0011586568,0.49795696,0.45379612,0.011971725,0.0031027745,0.0007667617],"about_ca_topic_score_codex":0.00006302636,"about_ca_topic_score_gemma":0.00001186104,"teacher_disagreement_score":0.6252575,"about_ca_system_score_codex":0.00009535122,"about_ca_system_score_gemma":0.000011598113,"threshold_uncertainty_score":0.37870616},"labels":[],"label_agreement":null},{"id":"W4409293456","doi":"10.2139/ssrn.5211074","title":"A Lifecycle Assessment of Waste-Based Sustainable Aviation Fuels Blends for Advancing the Circular Aviation Economy","year":2025,"lang":"en","type":"preprint","venue":"SSRN Electronic Journal","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Ontario Tech University","funders":"","keywords":"Aviation; Circular economy; Waste management; Commercial aviation; Business; Environmental science; Engineering; Aerospace engineering","score_opus":0.006078269855005775,"score_gpt":0.2566304565729963,"score_spread":0.25055218671799057,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4409293456","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":[0.017151337,0.0007718059,0.9771324,0.0018214773,0.00014875055,0.0010411423,0.00000941453,0.00006391356,0.0018597748],"genre_scores_gemma":[0.99393564,0.00057232677,0.0037079817,0.00009892982,0.000076829754,0.00021791215,0.000022614882,0.000020547614,0.0013471951],"study_design_codex":"simulation_or_modeling","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.9972666,0.000105725136,0.00048736887,0.00037840696,0.0002560011,0.0015059044],"domain_scores_gemma":[0.99859434,0.00017541363,0.00068656396,0.00042825082,0.000076515375,0.000038934377],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0022063358,0.0002519478,0.00032024272,0.00014634854,0.00035523917,0.000062787294,0.00064809964,0.00020842026,0.00003404383],"category_scores_gemma":[0.00015602556,0.00020592417,0.00024593886,0.0002127737,0.000099253855,0.00025227174,0.00031303594,0.0016884048,0.0000018407424],"study_design_candidate":"theoretical_or_conceptual","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":true,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000104769046,0.00026433414,0.012761088,0.0006004951,0.0004254032,0.0000043745326,0.0002116022,0.5578811,0.003576572,0.35710323,0.00024837835,0.066818655],"study_design_scores_gemma":[0.0006578017,0.00023674163,0.0003830773,0.00007636079,0.00011743936,0.000007602762,0.0024970933,0.023194252,0.0034431298,0.96729374,0.0018346804,0.0002580685],"about_ca_topic_score_codex":0.0000701516,"about_ca_topic_score_gemma":0.00011997018,"teacher_disagreement_score":0.97678435,"about_ca_system_score_codex":0.0047606328,"about_ca_system_score_gemma":0.0024502482,"threshold_uncertainty_score":0.9990599},"labels":[],"label_agreement":null},{"id":"W4409303737","doi":"10.1021/acsestair.4c00288","title":"Investigating the Impact of Aviation Activity on Fine Particulate Matter, Black Carbon, and Ultrafine Particles Using Flight Track Data at the Ottawa International Airport","year":2025,"lang":"en","type":"article","venue":"ACS ES&T Air","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"Carleton University; Health Canada","funders":"","keywords":"Particulates; Track (disk drive); Ultrafine particle; Carbon black; Aviation; Environmental science; Aeronautics; Aerospace engineering; Meteorology; Engineering; Geography; Materials science; Chemistry; Chemical engineering; Mechanical engineering","score_opus":0.028931939956512883,"score_gpt":0.29396515519128136,"score_spread":0.26503321523476847,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4409303737","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":[0.99566483,0.000023686682,0.00026042646,0.0033844216,0.00004369374,0.00016697911,0.000017063534,0.000033661043,0.00040524284],"genre_scores_gemma":[0.9994723,0.0000107214055,0.00021992877,0.00012018185,0.000013551353,0.0000041136364,0.000009069783,0.0000059532063,0.00014416383],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.99922794,0.000046342855,0.00017258343,0.00023812066,0.00016608005,0.00014891707],"domain_scores_gemma":[0.99919,0.00015598201,0.0001378586,0.000486418,0.000008095852,0.000021678343],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024540056,0.00011034011,0.000102313155,0.000019459947,0.00012785643,0.00001741666,0.00034871046,0.000040712985,0.000046954014],"category_scores_gemma":[0.00016867531,0.00006160032,0.000025741478,0.00018371906,0.00047726472,0.00020024943,0.00037450195,0.000114495306,0.00000997155],"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":[0.000018963441,0.00006365956,0.7229701,0.0000063792204,0.000049940343,0.0000016669893,0.00022229551,0.021048442,0.24523179,0.000119269105,0.0019799955,0.008287473],"study_design_scores_gemma":[0.00021087381,0.000031806325,0.7713235,0.00003166048,0.000024683433,0.0000037554942,0.000047003796,0.04916042,0.17657626,0.002322131,0.00017915606,0.00008874613],"about_ca_topic_score_codex":0.0003686428,"about_ca_topic_score_gemma":0.00023224292,"teacher_disagreement_score":0.068655536,"about_ca_system_score_codex":0.00010788105,"about_ca_system_score_gemma":0.000011972925,"threshold_uncertainty_score":0.25119883},"labels":[],"label_agreement":null},{"id":"W4409898387","doi":"10.26434/chemrxiv-2024-lnmv4-v2","title":"Greenhouse Gas Accounting Procedures in Low Carbon Fuel Policies Overlook the Spatial Variability of Miscanthus-derived Sustainable Aviation Fuel","year":2025,"lang":"en","type":"preprint","venue":"ChemRxiv","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"Biological and Environmental Research; Office of Science; U.S. Department of Energy","keywords":"Miscanthus; Greenhouse gas; Aviation; Business; Natural resource economics; Environmental economics; Environmental science; Economics; Waste management; Biofuel; Engineering; Bioenergy; Aerospace engineering","score_opus":0.007277525502589957,"score_gpt":0.2264852241695192,"score_spread":0.21920769866692924,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4409898387","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":[0.9855294,0.00021413607,0.0011026516,0.0006477948,0.00011568958,0.0011541276,0.0000065159247,0.00020807183,0.011021587],"genre_scores_gemma":[0.99841666,0.00022442122,0.00046208524,0.000059674305,0.00004052716,0.00017280653,0.000007934794,0.000018958073,0.0005969353],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.99801356,0.0000784049,0.0004730176,0.00062415167,0.00033246176,0.00047839893],"domain_scores_gemma":[0.99854064,0.00018719635,0.00038162098,0.0008131488,0.000046276495,0.000031120984],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00054386107,0.00033176635,0.00040443623,0.00010564016,0.00008519983,0.000044137145,0.0008015484,0.00037701597,0.00006238181],"category_scores_gemma":[0.0011250386,0.00026863004,0.00010826738,0.00039560033,0.0005602947,0.00013034578,0.0016132803,0.0006028389,0.0000029907992],"study_design_candidate":"observational","study_design_consensus":"observational","about_ca_topic_candidate":true,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0003058369,0.001181626,0.8779751,0.010541846,0.00014078285,0.000040310806,0.01142572,0.030774934,0.056365296,0.0030354771,0.00041509804,0.0077979807],"study_design_scores_gemma":[0.0012524038,0.000104617124,0.5345233,0.0009756376,0.00013799271,0.0000044234907,0.004365013,0.012297659,0.120803565,0.32373473,0.00040705007,0.0013935906],"about_ca_topic_score_codex":0.00935095,"about_ca_topic_score_gemma":0.0020128482,"teacher_disagreement_score":0.34345177,"about_ca_system_score_codex":0.0005434608,"about_ca_system_score_gemma":0.00016916063,"threshold_uncertainty_score":0.9999766},"labels":[],"label_agreement":null},{"id":"W4409957956","doi":"10.5194/egusphere-2025-1346","title":"Transport of Biomass Burning Aerosol into the Extratropical Tropopause Region over Europe via Warm Conveyor Belt Uplift","year":2025,"lang":"en","type":"preprint","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"Deutsche Forschungsgemeinschaft","keywords":"Extratropical cyclone; Aerosol; Biomass burning; Environmental science; Tropopause; Atmospheric sciences; Conveyor belt; Climatology; Biomass (ecology); Geology; Meteorology; Geography; Oceanography; Stratosphere","score_opus":0.014447667097034558,"score_gpt":0.24669575710450073,"score_spread":0.23224809000746616,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4409957956","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":[0.4788653,0.0003781373,0.5054821,0.0020444558,0.00046005004,0.0011023763,0.000015298396,0.00064373855,0.011008585],"genre_scores_gemma":[0.9885545,0.00037476252,0.0077388133,0.00021262738,0.000030323672,0.00006326413,0.000022234597,0.000025441233,0.0029780485],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9978451,0.00007904909,0.0005555654,0.00076302554,0.00040190737,0.00035535527],"domain_scores_gemma":[0.998544,0.000102009835,0.0002513475,0.0010119485,0.000022521297,0.00006818938],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00014764273,0.0004004042,0.00047035812,0.000071047885,0.00015356156,0.000019979814,0.0011065997,0.00037894765,0.00043302245],"category_scores_gemma":[0.000054587807,0.00026414558,0.00018829541,0.00037146072,0.00095111964,0.000110335684,0.0009603759,0.00074910437,0.000038822436],"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":[0.00061313476,0.0010576658,0.23651047,0.0009330547,0.0005466535,0.0005942515,0.0036968496,0.005984871,0.58103377,0.011919441,0.007082275,0.15002756],"study_design_scores_gemma":[0.0034096565,0.0011497181,0.10506369,0.0009894161,0.00082150137,0.00008066828,0.0010345958,0.00905921,0.75340945,0.059753116,0.061143063,0.004085912],"about_ca_topic_score_codex":0.0013008459,"about_ca_topic_score_gemma":0.0003081293,"teacher_disagreement_score":0.50968915,"about_ca_system_score_codex":0.00013163408,"about_ca_system_score_gemma":0.000036252135,"threshold_uncertainty_score":0.99998105},"labels":[],"label_agreement":null},{"id":"W4410033753","doi":"10.1007/978-3-031-89444-2_15","title":"Advances on the Next Generation Short-Medium Range Aircraft Rear End: The CleanSky 2 Project IMPACT","year":2025,"lang":"en","type":"book-chapter","venue":"Lecture notes in mobility","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Q & T Research","funders":"European Commission; Clean Aviation","keywords":"Aeronautics; Range (aeronautics); Aerospace engineering; Engineering","score_opus":0.03762990693663228,"score_gpt":0.28228356444094066,"score_spread":0.24465365750430837,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4410033753","genre_codex":"other","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":[0.08090584,0.017667642,0.14919743,0.034204822,0.0041026236,0.030398075,0.00090147945,0.002991734,0.67963034],"genre_scores_gemma":[0.99171746,0.0016055373,0.001029891,0.0013332056,0.00025569476,0.0002948201,0.00004554833,0.000055048375,0.0036627727],"study_design_codex":"design_other","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.997734,0.00012847774,0.00038714136,0.0008445344,0.00050091115,0.00040492835],"domain_scores_gemma":[0.99747956,0.001021758,0.00012983185,0.0013208683,0.000016633197,0.000031326534],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00061378506,0.0005304262,0.00039772806,0.00007875582,0.00028074134,0.00006027732,0.0008180966,0.00051412685,0.00084593165],"category_scores_gemma":[0.0006592274,0.00027120084,0.00024100277,0.00019743963,0.00090263813,0.00017802561,0.0002739916,0.0013724482,0.000056584853],"study_design_candidate":"design_other","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":[0.00026943066,0.00013647585,0.0035314693,0.00005796859,0.0000578607,0.000027852448,0.0004790524,0.015881883,0.00271914,0.0020168314,0.002590492,0.97223157],"study_design_scores_gemma":[0.0010000597,0.0018639972,0.018264892,0.00069845596,0.00026973677,0.000037352198,0.0001285333,0.010740428,0.023877528,0.5060276,0.43387413,0.0032172892],"about_ca_topic_score_codex":0.00017153501,"about_ca_topic_score_gemma":0.0022893308,"teacher_disagreement_score":0.9690142,"about_ca_system_score_codex":0.0006193589,"about_ca_system_score_gemma":0.0000673549,"threshold_uncertainty_score":0.999974},"labels":[],"label_agreement":null},{"id":"W4410105379","doi":"10.21203/rs.3.rs-6538724/v1","title":"Potential benefits of great circle routes to reduce fuel consumption and aircraft emissions in mainland China","year":2025,"lang":"en","type":"preprint","venue":"Research Square","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"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":"Hong Kong Polytechnic University; National Natural Science Foundation of China","keywords":"Mainland China; China; Consumption (sociology); Fuel efficiency; China mainland; Business; Natural resource economics; Mainland; Environmental economics; Environmental science; Economics; Automotive engineering; Engineering; Geography; Sociology","score_opus":0.033981509186276515,"score_gpt":0.34142917607746265,"score_spread":0.30744766689118613,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4410105379","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":[0.9931414,0.0011789,0.0011780555,0.0013395285,0.00007246632,0.0011868005,0.00019614826,0.00008657466,0.0016201292],"genre_scores_gemma":[0.99415284,0.0018475234,0.0028397809,0.000010636276,0.00001793893,0.00013530719,0.000024345292,0.000012779753,0.0009588307],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.9977581,0.0001673604,0.00028586457,0.00070194295,0.0005999409,0.00048683016],"domain_scores_gemma":[0.9990413,0.00014703984,0.000057044166,0.00057306956,0.000034191704,0.00014735776],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00059787586,0.00019070023,0.0003087324,0.0003973259,0.00013008589,0.000041168823,0.0004853846,0.00032206485,0.00022188746],"category_scores_gemma":[0.00046335324,0.00018931119,0.000056428587,0.0004774404,0.00039281638,0.00009543056,0.002805811,0.00086519023,0.000037100897],"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":[0.00041837283,0.00050863245,0.54538286,0.0027424605,0.00005455906,0.00011440599,0.0019534957,0.05047647,0.03269312,0.0008802463,0.0030206316,0.36175475],"study_design_scores_gemma":[0.00039563695,0.00012917569,0.9752469,0.0012720595,0.00000798034,0.0000051714883,0.00021085603,0.00059332006,0.0048855683,0.016607776,0.00039954184,0.00024599038],"about_ca_topic_score_codex":0.0007601042,"about_ca_topic_score_gemma":0.0002597807,"teacher_disagreement_score":0.42986405,"about_ca_system_score_codex":0.0002585302,"about_ca_system_score_gemma":0.00005560293,"threshold_uncertainty_score":0.77198863},"labels":[],"label_agreement":null},{"id":"W4410195530","doi":"10.21203/rs.3.rs-6559440/v1","title":"Substantial aircraft contrail formation at low soot emission levels","year":2025,"lang":"en","type":"preprint","venue":"Research Square","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":4,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Safran Electronics (Canada)","funders":"HORIZON EUROPE Framework Programme; Deutsche Forschungsgemeinschaft; Science Foundation Ireland; European Commission; National Science Foundation","keywords":"Ice crystals; Soot; Environmental science; Cirrus; Aerosol; Meteorology; Atmospheric sciences; Particle number; Cloud condensation nuclei; Radiative forcing; Combustion; Chemistry; Geography; Physics","score_opus":0.0605002799901205,"score_gpt":0.360630556610268,"score_spread":0.3001302766201475,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4410195530","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":[0.9287227,0.0001644067,0.051933203,0.0013180416,0.00016078739,0.001760538,0.0001251363,0.00065596495,0.015159266],"genre_scores_gemma":[0.99250525,0.00012302017,0.0021350102,0.00003586966,0.000028838136,0.00019642476,0.000051739204,0.000014311588,0.004909559],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99691826,0.00021580831,0.00032848734,0.0006473107,0.0011494774,0.0007406383],"domain_scores_gemma":[0.998687,0.00025585564,0.00008344884,0.00075260655,0.00007492485,0.00014616088],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00087106734,0.00024033067,0.0002557164,0.00019863312,0.0005724642,0.00007415495,0.00078831805,0.00037666693,0.0021599152],"category_scores_gemma":[0.0004923722,0.00020870822,0.00011991704,0.00049629767,0.000477924,0.00029912978,0.0031241642,0.0010153468,0.0007312019],"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":[0.00064548716,0.000552931,0.047964357,0.0014493479,0.00006088128,0.00022679985,0.0025700622,0.010585796,0.6956103,0.0020807262,0.027214507,0.21103878],"study_design_scores_gemma":[0.001994342,0.00034007055,0.07159099,0.0014270889,0.000016841508,0.000021869593,0.0014830009,0.017160576,0.8017239,0.07512381,0.027926018,0.001191499],"about_ca_topic_score_codex":0.00009452111,"about_ca_topic_score_gemma":0.00012508933,"teacher_disagreement_score":0.20984729,"about_ca_system_score_codex":0.001105513,"about_ca_system_score_gemma":0.000064153974,"threshold_uncertainty_score":0.99875224},"labels":[],"label_agreement":null},{"id":"W4410210664","doi":"10.70671/hjf9f116","title":"Hydrogen in Aviation: Evaluating the Feasibility and Benefits of a Green Fuel Alternative","year":2025,"lang":"en","type":"article","venue":"Journal of High School Research","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Hillsborough Hospital","funders":"","keywords":"Aviation; Alternative fuels; Hydrogen fuel; Environmental science; Aeronautics; Engineering; Waste management; Fuel cells; Aerospace engineering; Chemical engineering","score_opus":0.12185281397894855,"score_gpt":0.4123855888094879,"score_spread":0.29053277483053935,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4410210664","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":[0.995979,0.0010614326,0.0001604986,0.0020019617,0.000021618738,0.00019555843,0.0000015527337,0.000003385799,0.0005749644],"genre_scores_gemma":[0.9982226,0.0003052662,0.0011821769,0.000024652476,0.000016532487,0.0000053423078,9.6900436e-8,0.0000026369396,0.0002407196],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.9984667,0.00024622364,0.00030436533,0.00012913892,0.00068487757,0.00016872238],"domain_scores_gemma":[0.9991022,0.00045385852,0.00013028097,0.00017841347,0.000095012205,0.000040245555],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0032737274,0.00005528004,0.00013779632,0.00015430257,0.0000831846,0.000016924543,0.00039121724,0.00004282304,0.00009401326],"category_scores_gemma":[0.001683396,0.000034950335,0.000028520453,0.0005994001,0.0002962344,0.00022032262,0.00030914924,0.0005255795,0.000006319152],"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":[0.0002910339,0.0001189888,0.9070138,0.000032222313,0.000030243851,0.000013605111,0.00042385166,0.0040573073,0.011585807,0.0020035142,0.00021095446,0.07421869],"study_design_scores_gemma":[0.0005995075,0.00039543252,0.78558165,0.00008200739,0.000004975983,0.000007636696,0.00039002864,0.0006287011,0.005278821,0.2069596,0.000033021366,0.000038641185],"about_ca_topic_score_codex":0.00045907407,"about_ca_topic_score_gemma":0.00018776163,"teacher_disagreement_score":0.20495608,"about_ca_system_score_codex":0.00025788927,"about_ca_system_score_gemma":0.000057240748,"threshold_uncertainty_score":0.22834106},"labels":[],"label_agreement":null},{"id":"W4410440292","doi":"10.32920/29078597.v1","title":"Beam Design Optimization of a Tandem Wing Aircraft","year":2025,"lang":"en","type":"preprint","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Tandem; Wing; Aerospace engineering; Aeronautics; Beam (structure); Wing configuration; Computer science; Engineering; Structural engineering","score_opus":0.0224302599020392,"score_gpt":0.25032283439613695,"score_spread":0.22789257449409775,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4410440292","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":[0.00048882957,0.000077212804,0.975415,0.00014198376,0.0001309598,0.00044900543,0.000005882292,0.0003622462,0.022928912],"genre_scores_gemma":[0.1759415,0.00020508206,0.81982976,0.00010665972,0.000011736687,0.00006271964,0.000011282522,0.000013602115,0.0038176375],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9988226,0.00003416199,0.0002952647,0.0004310883,0.00022124636,0.00019558909],"domain_scores_gemma":[0.99924594,0.00009074199,0.0001530137,0.00046855092,0.0000123063055,0.000029458099],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017969706,0.00020794642,0.00028072085,0.00008154838,0.000054965676,0.00001439052,0.00048228784,0.00031401488,0.0008467004],"category_scores_gemma":[0.00011377214,0.00018896096,0.00008511744,0.00023374046,0.0001887248,0.00009331266,0.001223328,0.00028056896,0.000021226731],"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":[0.0000054263887,0.00003421722,0.0010969861,0.00002269835,0.000014613202,0.0000018515774,0.000034899414,0.9885029,0.0008941131,0.00013899324,0.00093310216,0.008320171],"study_design_scores_gemma":[0.0011439832,0.00030245192,0.0027837453,0.00087948097,0.00023402346,0.000007663558,0.00039076144,0.6104905,0.24372132,0.13425627,0.0037725405,0.0020172377],"about_ca_topic_score_codex":0.00006581451,"about_ca_topic_score_gemma":0.0000054059965,"teacher_disagreement_score":0.3780124,"about_ca_system_score_codex":0.00015435331,"about_ca_system_score_gemma":0.000033582073,"threshold_uncertainty_score":0.92707753},"labels":[],"label_agreement":null},{"id":"W4410495004","doi":"10.1016/j.rineng.2025.105337","title":"Hydrogen fuel cell integrated turbofan engines offer lower costs when climate impact accounted for aviation purposes","year":2025,"lang":"en","type":"article","venue":"Results in Engineering","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":5,"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":"Turbofan; Aviation; Aeronautics; Environmental science; Automotive engineering; Engineering; Aerospace engineering","score_opus":0.0055392404235449656,"score_gpt":0.2303090525890085,"score_spread":0.22476981216546352,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4410495004","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":[0.89317775,0.0008076057,0.09579243,0.000344447,0.0006460188,0.0016998826,0.0002775135,0.001245933,0.0060083927],"genre_scores_gemma":[0.9933628,0.00011412741,0.006113083,0.00002659209,0.000014210377,0.000075197095,0.0000482146,0.000021126478,0.00022464411],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99891025,0.0000088153,0.00028313248,0.0003036637,0.00011167689,0.00038243836],"domain_scores_gemma":[0.9995117,0.00013713638,0.00005232286,0.0002513427,0.000013199611,0.000034293207],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018120657,0.00020625192,0.00018489303,0.00016392842,0.000036486646,0.000030232015,0.00023820586,0.0001317612,0.00002160384],"category_scores_gemma":[0.0002902068,0.00017784654,0.00006524474,0.00042650994,0.000030961637,0.0002503472,0.00009705944,0.0001649443,0.00001992049],"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":[0.0006450594,0.0002608446,0.013186599,0.00030433157,0.000061867024,0.000028026561,0.00049066765,0.7123049,0.2350842,0.00033659147,0.0018367969,0.03546014],"study_design_scores_gemma":[0.0055555115,0.00035254343,0.033137534,0.00065447827,0.00005596809,0.0000062484187,0.00029262155,0.7080628,0.220594,0.0027260487,0.02722881,0.0013334154],"about_ca_topic_score_codex":0.000074855496,"about_ca_topic_score_gemma":0.000043391112,"teacher_disagreement_score":0.10018503,"about_ca_system_score_codex":0.0004912104,"about_ca_system_score_gemma":0.000010097765,"threshold_uncertainty_score":0.72523713},"labels":[],"label_agreement":null},{"id":"W4410707781","doi":"10.12968/s1478-2774(25)50070-4","title":"Fit &amp; Fly","year":2025,"lang":"en","type":"article","venue":"Aerospace Testing International","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Computer science","score_opus":0.03486973499333234,"score_gpt":0.2926448097636591,"score_spread":0.25777507477032674,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4410707781","genre_codex":"other","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":[0.41624847,0.000050383336,0.098234706,0.017416187,0.0009954834,0.00020844517,0.000007967003,0.0012501073,0.46558827],"genre_scores_gemma":[0.8897655,0.0000036778592,0.08264395,0.0006170156,0.000020540208,0.000014985944,0.0000032436064,0.0000057895436,0.02692528],"study_design_codex":"observational","study_design_gemma":"not_applicable","domain_scores_codex":[0.9993745,0.000009044348,0.000097750766,0.00020343394,0.00017577689,0.00013947797],"domain_scores_gemma":[0.9995461,0.00022274561,0.000041033694,0.0001546149,0.000016683409,0.000018836336],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00010018536,0.00007905767,0.00005681361,0.000033039312,0.000103215425,0.0000295699,0.00032826627,0.000048775724,0.00069387665],"category_scores_gemma":[0.0013681422,0.0000755806,0.00002254731,0.00023484553,0.00011886056,0.00012677626,0.00024535757,0.00015667327,0.0006493192],"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":[0.000011241152,0.00009564751,0.8175532,0.000005346419,0.000028610597,0.000010131745,0.00012502032,0.0051593916,0.049582385,0.0075524473,0.06571305,0.054163527],"study_design_scores_gemma":[0.0007425949,0.000052858282,0.37179032,0.00014771141,0.000015609025,0.000027026223,0.00012643285,0.006128551,0.0096616335,0.059040587,0.5517493,0.000517417],"about_ca_topic_score_codex":0.00011428113,"about_ca_topic_score_gemma":0.00008945951,"teacher_disagreement_score":0.48603624,"about_ca_system_score_codex":0.000121841804,"about_ca_system_score_gemma":0.000009584281,"threshold_uncertainty_score":0.83459014},"labels":[],"label_agreement":null},{"id":"W4410738454","doi":"10.1109/iraset64571.2025.11008199","title":"Comparison of the Genetic Algorithm and the Particle Swarm Optimization for Minimizing Fuel Consumption for UAVs","year":2025,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Royal Military College of Canada","funders":"","keywords":"Particle swarm optimization; Genetic algorithm; Fuel efficiency; Computer science; Mathematical optimization; Consumption (sociology); Algorithm; Engineering; Mathematics; Automotive engineering; Machine learning","score_opus":0.023741494514712195,"score_gpt":0.2942674264681193,"score_spread":0.27052593195340713,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4410738454","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.039215524,0.00026567865,0.9586081,0.00095883314,0.000046682624,0.0007085667,0.0000031810964,0.000030558345,0.00016290568],"genre_scores_gemma":[0.7375053,0.00004850073,0.26199242,0.000105791914,0.0000027138976,0.00010412963,6.343064e-7,0.000002805808,0.0002376871],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995996,0.000015225456,0.00013347312,0.00010957055,0.00005110991,0.000091071466],"domain_scores_gemma":[0.9995855,0.00022216566,0.00005282363,0.00012482073,0.000007202709,0.0000074737204],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000081270024,0.000049166603,0.000086558975,0.0000056211084,0.00012327169,0.0000104487035,0.00011057365,0.000030500612,0.000017204178],"category_scores_gemma":[0.00007260463,0.000026853788,0.000030506459,0.00007648362,0.00033730245,0.000040947467,0.00007589948,0.000024967887,7.2258996e-7],"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":[0.00025717288,0.00018472163,0.110583626,0.00014223007,0.00005291468,7.027509e-8,0.0008743492,0.3038614,0.00662579,0.02041312,0.0020092304,0.55499536],"study_design_scores_gemma":[0.0011085463,0.000031773878,0.007450717,0.000009116148,0.00003048214,2.9456928e-7,0.00036137982,0.9374738,0.0417434,0.011078086,0.00066327414,0.00004916345],"about_ca_topic_score_codex":0.000008342183,"about_ca_topic_score_gemma":0.0000089072755,"teacher_disagreement_score":0.6982898,"about_ca_system_score_codex":0.0000169956,"about_ca_system_score_gemma":0.0000028799313,"threshold_uncertainty_score":0.12428049},"labels":[],"label_agreement":null},{"id":"W4410765932","doi":"10.2514/6.2025-1650.c1","title":"Correction: Aerodynamic Optimization of Adaptive Wing Configurations with Different Leading-Edge Shapes – Application to the UAS-S45","year":2025,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"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":"Aerodynamics; Enhanced Data Rates for GSM Evolution; Computer science; Wing; Aerospace engineering; Computer vision; Engineering","score_opus":0.007610267972787119,"score_gpt":0.22335811794757932,"score_spread":0.21574784997479218,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4410765932","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":[0.013403192,0.000008361365,0.9657276,0.0009662394,0.000058381615,0.00043538178,0.0000016418387,0.00012405861,0.019275142],"genre_scores_gemma":[0.9902769,0.0000074158147,0.0067209173,0.0001297495,0.0000050589847,0.000117491276,0.000004467814,0.000004872682,0.0027331752],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999452,0.000015943671,0.0001258266,0.00019904602,0.00010668123,0.00010048901],"domain_scores_gemma":[0.99967265,0.000070650654,0.000053508058,0.00017042835,0.000016245978,0.000016510443],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00004297566,0.00008899137,0.00009196801,0.000041836036,0.00015832981,0.0000134311595,0.00016365702,0.000035712987,0.00012670095],"category_scores_gemma":[0.000026890588,0.000054610446,0.000018171686,0.00042287383,0.0001246067,0.00010724524,0.000060236587,0.000069816466,0.000023878358],"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":[0.000030353196,0.00004638051,0.0026158718,0.0000027115175,0.000013308939,1.4335468e-7,0.00014330988,0.948457,0.013282918,0.0067034205,0.0011360407,0.027568525],"study_design_scores_gemma":[0.0002751075,0.00025360606,0.05164854,0.000057488724,0.0000400779,0.0000031620962,0.0018536671,0.92217875,0.020719903,0.0010905446,0.0016532043,0.00022594244],"about_ca_topic_score_codex":0.000054354703,"about_ca_topic_score_gemma":0.0006207712,"teacher_disagreement_score":0.97687364,"about_ca_system_score_codex":0.0001034208,"about_ca_system_score_gemma":0.000006773461,"threshold_uncertainty_score":0.22269493},"labels":[],"label_agreement":null},{"id":"W4411047518","doi":"10.20944/preprints202505.2431.v2","title":"HEFA-to-Jet: Are We Heading in the Right Direction for Sustainable Aviation Fuel Production?","year":2025,"lang":"en","type":"preprint","venue":"Preprints.org","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Natural Sciences and Engineering Research Council of Canada; Université de Sherbrooke","keywords":"Heading (navigation); Aviation; Jet (fluid); Aeronautics; Production (economics); Aerospace engineering; Jet fuel; Environmental science; Engineering; Economics","score_opus":0.057570616373923654,"score_gpt":0.32618256725276185,"score_spread":0.2686119508788382,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4411047518","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":[0.84826386,0.00044255183,0.04646052,0.041952457,0.0019460311,0.013591561,0.00003658786,0.0015256706,0.045780767],"genre_scores_gemma":[0.98214555,0.00019487839,0.0011449265,0.00016379135,0.000084920735,0.0020304048,0.000014060168,0.000018262124,0.014203233],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.9977462,0.00011490698,0.00035672967,0.0010659314,0.00028078826,0.00043541743],"domain_scores_gemma":[0.99857014,0.000115486495,0.0002246907,0.0010054025,0.00004570385,0.000038595965],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0009954191,0.00028478302,0.000285149,0.00020142137,0.00025744986,0.000036495756,0.00073168287,0.00026016624,0.0001739212],"category_scores_gemma":[0.0009313131,0.00023311611,0.00011266384,0.00057177164,0.00010053698,0.00024390926,0.0012796208,0.0005989243,0.000196999],"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":[0.00013321139,0.00043239506,0.93701714,0.00084664306,0.000047446243,0.000020903815,0.0036065718,0.038276285,0.0043658908,0.005224448,0.0027862315,0.007242821],"study_design_scores_gemma":[0.00034988913,0.000041070663,0.5377186,0.00039480918,0.000053670796,0.000006613193,0.0029268588,0.00043619852,0.04614774,0.2733822,0.13784857,0.00069379044],"about_ca_topic_score_codex":0.00028947523,"about_ca_topic_score_gemma":0.0002992833,"teacher_disagreement_score":0.39929855,"about_ca_system_score_codex":0.0008557421,"about_ca_system_score_gemma":0.00003243959,"threshold_uncertainty_score":0.9506199},"labels":[],"label_agreement":null},{"id":"W4411217978","doi":"10.3390/en18123074","title":"A Study on Thermal Management Systems for Fuel-Cell Powered Regional Aircraft","year":2025,"lang":"en","type":"article","venue":"Energies","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Victoria","funders":"Fundação para a Ciência e a Tecnologia; Natural Sciences and Engineering Research Council of Canada","keywords":"Fuel cells; Thermal management of electronic devices and systems; Thermal; Aerospace engineering; Automotive engineering; Aeronautics; Environmental science; Engineering; Systems engineering; Nuclear engineering; Meteorology; Mechanical engineering; Chemical engineering; Physics","score_opus":0.01651558942868664,"score_gpt":0.25034577771891786,"score_spread":0.23383018829023122,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4411217978","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":[0.81510425,0.0015462467,0.004885297,0.00088117336,0.0006868859,0.0020526773,0.000009204401,0.0008063911,0.17402789],"genre_scores_gemma":[0.98061335,0.00009532003,0.0010888048,0.00016771059,0.000014737722,0.0003874289,0.0000026112612,0.000011313392,0.017618742],"study_design_codex":"simulation_or_modeling","study_design_gemma":"not_applicable","domain_scores_codex":[0.99907786,0.000025984154,0.00014957832,0.00033024154,0.0001874376,0.00022888489],"domain_scores_gemma":[0.9995192,0.00007101393,0.00004261706,0.00034223084,0.0000048409147,0.000020093936],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000103099446,0.00014708687,0.00013673665,0.00006884492,0.00012046018,0.000029984512,0.00031127594,0.00004828205,0.000029393841],"category_scores_gemma":[0.000008720401,0.000119900615,0.0000518677,0.00017777707,0.000095402036,0.000078620265,0.00017577605,0.00006377548,0.00006653844],"study_design_candidate":"not_applicable","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":[0.0010351922,0.005207767,0.045633875,0.0006839006,0.0005956296,0.00031879442,0.0028041305,0.61464304,0.015388171,0.099101454,0.17051786,0.044070214],"study_design_scores_gemma":[0.0071543814,0.002148191,0.0883533,0.00019914076,0.00017166923,0.0000050068047,0.03943601,0.001635029,0.0102515975,0.021949753,0.82729703,0.0013988593],"about_ca_topic_score_codex":0.00003224151,"about_ca_topic_score_gemma":0.000008604823,"teacher_disagreement_score":0.6567792,"about_ca_system_score_codex":0.000092103546,"about_ca_system_score_gemma":0.0000039273223,"threshold_uncertainty_score":0.4889405},"labels":[],"label_agreement":null},{"id":"W4411267627","doi":"10.26434/chemrxiv-2024-lnmv4-v3","title":"Greenhouse Gas Accounting Procedures in Low Carbon Fuel Policies Overlook the Spatial Variability of Miscanthus-derived Sustainable Aviation Fuel","year":2025,"lang":"en","type":"preprint","venue":"ChemRxiv","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"Biological and Environmental Research; Office of Science; U.S. Department of Energy","keywords":"Miscanthus; Greenhouse gas; Aviation; Environmental science; Aviation fuel; Natural resource economics; Carbon accounting; Environmental economics; Business; Biofuel; Waste management; Economics; Engineering; Bioenergy; Aerospace engineering","score_opus":0.007277525502589957,"score_gpt":0.2264852241695192,"score_spread":0.21920769866692924,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4411267627","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":[0.9855294,0.00021413607,0.0011026516,0.0006477948,0.00011568958,0.0011541276,0.0000065159247,0.00020807183,0.011021587],"genre_scores_gemma":[0.99841666,0.00022442122,0.00046208524,0.000059674305,0.00004052716,0.00017280653,0.000007934794,0.000018958073,0.0005969353],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.99801356,0.0000784049,0.0004730176,0.00062415167,0.00033246176,0.00047839893],"domain_scores_gemma":[0.99854064,0.00018719635,0.00038162098,0.0008131488,0.000046276495,0.000031120984],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00054386107,0.00033176635,0.00040443623,0.00010564016,0.00008519983,0.000044137145,0.0008015484,0.00037701597,0.00006238181],"category_scores_gemma":[0.0011250386,0.00026863004,0.00010826738,0.00039560033,0.0005602947,0.00013034578,0.0016132803,0.0006028389,0.0000029907992],"study_design_candidate":"observational","study_design_consensus":"observational","about_ca_topic_candidate":true,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0003058369,0.001181626,0.8779751,0.010541846,0.00014078285,0.000040310806,0.01142572,0.030774934,0.056365296,0.0030354771,0.00041509804,0.0077979807],"study_design_scores_gemma":[0.0012524038,0.000104617124,0.5345233,0.0009756376,0.00013799271,0.0000044234907,0.004365013,0.012297659,0.120803565,0.32373473,0.00040705007,0.0013935906],"about_ca_topic_score_codex":0.00935095,"about_ca_topic_score_gemma":0.0020128482,"teacher_disagreement_score":0.34345177,"about_ca_system_score_codex":0.0005434608,"about_ca_system_score_gemma":0.00016916063,"threshold_uncertainty_score":0.9999766},"labels":[],"label_agreement":null},{"id":"W4411439296","doi":"10.1139/dsa-2025-0003","title":"Mermoz<sup>©</sup> simulator: use of a database to estimate the photovoltaic input on a UAV. <i>Application to a transatlantic voyage</i>","year":2025,"lang":"en","type":"article","venue":"Drone Systems and Applications","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Modular design; Photovoltaic system; Simulation; Computer science; Propulsion; Automotive engineering; Aerospace engineering; Flight simulator; Engineering; Electrical engineering","score_opus":0.012439426257529026,"score_gpt":0.27520215271363097,"score_spread":0.26276272645610194,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4411439296","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":[0.23792875,0.00009896594,0.7569258,0.00093933183,0.00001507088,0.0033920275,0.00014034499,0.00016668247,0.00039297697],"genre_scores_gemma":[0.99593925,0.0000161512,0.0019158707,0.00033270897,0.000011669545,0.001376278,0.000016690976,0.000011696143,0.00037967594],"study_design_codex":"simulation_or_modeling","study_design_gemma":"not_applicable","domain_scores_codex":[0.9989579,0.000025085816,0.00026987892,0.00039440166,0.0001631864,0.00018958792],"domain_scores_gemma":[0.9989851,0.00014459163,0.00006291074,0.0007177714,0.000013749864,0.00007584047],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00013437495,0.00014705869,0.00018677766,0.00007054499,0.00020508967,0.00003965284,0.00026752005,0.00005347545,0.000006169072],"category_scores_gemma":[0.000027041027,0.00011008896,0.000030400208,0.0006642902,0.00011755533,0.0000928567,0.000117885036,0.00009411227,0.00008598977],"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":[0.000081112674,0.00044978329,0.005005364,0.0002279062,0.000056820925,0.0000020083073,0.00089570455,0.5140352,0.37273043,0.043422945,0.004707203,0.058385495],"study_design_scores_gemma":[0.00088478014,0.00025720923,0.0055704084,0.00031342986,0.00015190832,0.000013269363,0.00089058344,0.26806304,0.029272906,0.0027685333,0.6910714,0.0007425323],"about_ca_topic_score_codex":0.0006095888,"about_ca_topic_score_gemma":0.00005410299,"teacher_disagreement_score":0.7580105,"about_ca_system_score_codex":0.000053702697,"about_ca_system_score_gemma":0.000009672293,"threshold_uncertainty_score":0.44892973},"labels":[],"label_agreement":null},{"id":"W4411786598","doi":"10.1021/acssusresmgt.4c00486","title":"Greenhouse Gas Accounting Procedures in Low Carbon Fuel Policies Overlook the Spatial Variability of Miscanthus-Derived Sustainable Aviation Fuel","year":2025,"lang":"en","type":"article","venue":"ACS Sustainable Resource Management","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"Biological and Environmental Research","keywords":"Miscanthus; Greenhouse gas; Aviation; Environmental science; Carbon accounting; Natural resource economics; Biofuel; Waste management; Economics; Engineering; Bioenergy; Aerospace engineering","score_opus":0.003375834428046105,"score_gpt":0.20611428596702766,"score_spread":0.20273845153898157,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4411786598","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":[0.8279214,0.00034519692,0.0037211862,0.002864887,0.000037636888,0.0030946336,0.0000020168134,0.00030381026,0.16170925],"genre_scores_gemma":[0.9850076,0.00012784226,0.0002353236,0.000194032,0.000015106267,0.00022503333,0.0000031220536,0.000022583776,0.014169381],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.9974873,0.0001429343,0.0004744624,0.00054467574,0.00043926272,0.0009113585],"domain_scores_gemma":[0.99874514,0.0001645498,0.00023303619,0.0007657259,0.000056103057,0.00003546851],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0010245267,0.00028236522,0.0002950501,0.0002709288,0.00024944032,0.00008480403,0.0007575831,0.0001248227,0.00004248458],"category_scores_gemma":[0.00052774325,0.00023299632,0.000067385576,0.0012995929,0.00043740936,0.0002491477,0.0015388376,0.00024415835,0.00000349824],"study_design_candidate":"observational","study_design_consensus":"observational","about_ca_topic_candidate":true,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0011262922,0.002564193,0.4561305,0.020403488,0.0004240134,0.00071395375,0.014860446,0.14132226,0.003228237,0.3076736,0.00419032,0.04736271],"study_design_scores_gemma":[0.003276312,0.00032822625,0.36943713,0.00045058667,0.00024013457,0.0000052280743,0.21798414,0.0063073095,0.0063722725,0.34058318,0.053721577,0.0012938953],"about_ca_topic_score_codex":0.0072182966,"about_ca_topic_score_gemma":0.00051060936,"teacher_disagreement_score":0.20312369,"about_ca_system_score_codex":0.0010239367,"about_ca_system_score_gemma":0.000055147964,"threshold_uncertainty_score":0.99939275},"labels":[],"label_agreement":null},{"id":"W4411850717","doi":"10.4050/f-0081-2025-0097","title":"Dragonfly Preparation for Powered Flight Wind Tunnel and CFD Modeling","year":2025,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Lockheed Martin (Canada)","funders":"","keywords":"Wind tunnel; Dragonfly; Computational fluid dynamics; Marine engineering; Aerospace engineering; Aerodynamics; Aeronautics; Engineering; Environmental science; Computer science; Geology","score_opus":0.011993807875593943,"score_gpt":0.26217682572187695,"score_spread":0.250183017846283,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4411850717","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":[0.28827524,0.000096495954,0.68189955,0.00090166513,0.00006160787,0.00042174564,0.000002220567,0.00022648278,0.028114974],"genre_scores_gemma":[0.9609272,0.000020810226,0.034912236,0.00016694183,0.00000404371,0.000018330513,0.0000019287788,0.0000035500505,0.0039449716],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995343,0.000004039991,0.00009293959,0.00020060941,0.000050231236,0.00011789192],"domain_scores_gemma":[0.99981946,0.000025821006,0.000014512124,0.00011968384,0.0000040419604,0.000016455539],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000054510696,0.000066009576,0.000066227796,0.00002366356,0.00009736269,0.00001840541,0.00007682325,0.000052710184,0.00006305029],"category_scores_gemma":[0.000036613208,0.000054639684,0.000017310127,0.00008264262,0.000052423246,0.00016794681,0.00007314933,0.000032066033,0.00001375419],"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":[0.000507289,0.0002948245,0.012146308,0.00010355408,0.00008384079,0.0000056299173,0.0012901096,0.09489782,0.5380856,0.09102861,0.01704665,0.24450979],"study_design_scores_gemma":[0.0007775571,0.00013468435,0.0016839362,0.000019890818,0.000018575634,0.0000022150996,0.0004002706,0.7663647,0.022395836,0.18846188,0.019462584,0.00027786978],"about_ca_topic_score_codex":0.00001711257,"about_ca_topic_score_gemma":0.00003406866,"teacher_disagreement_score":0.67265195,"about_ca_system_score_codex":0.000032504926,"about_ca_system_score_gemma":0.000003841925,"threshold_uncertainty_score":0.22281417},"labels":[],"label_agreement":null},{"id":"W4412486523","doi":"10.2514/6.2025-3627","title":"Business Aviation Turbofan Efficiency Improvement by Electrical Assistance During Transient Operations","year":2025,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Turbofan; Transient (computer programming); Aviation; Aeronautics; Automotive engineering; Transient analysis; Computer science; Aerospace engineering; Engineering; Electrical engineering; Transient response; Operating system","score_opus":0.0033355148552873487,"score_gpt":0.2082721315418197,"score_spread":0.20493661668653235,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4412486523","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":[0.4286518,0.00008485301,0.55773485,0.0016251014,0.00007973906,0.00032444083,0.0000032455218,0.0002877705,0.01120818],"genre_scores_gemma":[0.9929445,0.000075958196,0.0022367702,0.0001857793,0.0000039307847,0.000055971177,0.0000047760896,0.000004730431,0.0044876207],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99913853,0.0000096713875,0.00016990253,0.00029270444,0.00016574061,0.00022343903],"domain_scores_gemma":[0.9997504,0.00001354442,0.000017524439,0.0001813423,0.000011063669,0.000026177486],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000052972624,0.00010448086,0.000085704196,0.0000660337,0.0002247892,0.00003058693,0.00017441032,0.000054300213,0.00023129476],"category_scores_gemma":[0.000035965342,0.00008759699,0.000023720902,0.001128422,0.000078178746,0.00016899317,0.000039156006,0.000085748965,0.000039787898],"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":[0.000011429508,0.00019328202,0.0028633762,0.0000066895086,0.0000053341582,0.0000015261988,0.00002729843,0.003443748,0.96919394,0.001995019,0.0027247404,0.019533608],"study_design_scores_gemma":[0.0012294153,0.00016971151,0.20249397,0.00002594942,0.000026165262,0.0000024459612,0.00012760462,0.013741859,0.7703528,0.0018679168,0.009393483,0.0005686992],"about_ca_topic_score_codex":0.00009263889,"about_ca_topic_score_gemma":0.00010684741,"teacher_disagreement_score":0.56429267,"about_ca_system_score_codex":0.00019229823,"about_ca_system_score_gemma":0.00000900625,"threshold_uncertainty_score":0.35721016},"labels":[],"label_agreement":null},{"id":"W4412486603","doi":"10.2514/6.2025-3256","title":"Impact of Hydrogen Availability at Airports on the Potential Environmental Benefits of Hydrogen-Kerosene Dual-Fuel Business Jets Using ADS-B Data","year":2025,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Université de Sherbrooke","funders":"","keywords":"Kerosene; Hydrogen; Dual (grammatical number); Hydrogen fuel; Environmental science; Jet fuel; Liquid hydrogen; Waste management; Aerospace engineering; Automotive engineering; Aeronautics; Computer science; Engineering; Chemistry","score_opus":0.026560668014581713,"score_gpt":0.25862842551826737,"score_spread":0.23206775750368566,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4412486603","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":[0.997445,0.00017109551,0.0004298975,0.00013534227,0.000052203075,0.00042563546,0.00026131174,0.000064072745,0.0010154373],"genre_scores_gemma":[0.9986661,0.00011604954,0.0007912192,0.000047739242,0.000008968897,0.000005775956,0.000055757064,0.00001656296,0.00029181797],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.99804807,0.00005659206,0.00046787233,0.0006388116,0.00044126465,0.00034740337],"domain_scores_gemma":[0.997863,0.000097022305,0.0002466653,0.0017319401,0.000008063933,0.000053309534],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0003081649,0.0002753662,0.00032669748,0.000061543695,0.00015958559,0.000008985271,0.000773045,0.0001380099,0.0018817458],"category_scores_gemma":[0.00010021539,0.00018407326,0.00012517723,0.00041506276,0.0008560545,0.0002847315,0.0019954378,0.00013114935,0.000052490017],"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":[0.000143766,0.00066993054,0.20790349,0.000025791896,0.00012221735,0.000015958432,0.000040381066,0.04564642,0.73684025,0.00011543645,0.00045931258,0.008017054],"study_design_scores_gemma":[0.00059341005,0.00015312535,0.6406104,0.00005220954,0.000090840156,0.000028555689,0.000084769104,0.008173572,0.347516,0.0021534953,0.00018782784,0.00035583173],"about_ca_topic_score_codex":0.00040603502,"about_ca_topic_score_gemma":0.000060165396,"teacher_disagreement_score":0.4327069,"about_ca_system_score_codex":0.00034925385,"about_ca_system_score_gemma":0.000027960246,"threshold_uncertainty_score":0.99903065},"labels":[],"label_agreement":null},{"id":"W4412486671","doi":"10.2514/6.2025-3098","title":"The Effect of Altitude Upon Jet Transport Emissions of Nitrogen Oxides: A Flight and Empirical Data Study","year":2025,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"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":"Nitrogen; Altitude (triangle); Jet (fluid); Environmental science; Atmospheric sciences; Nitrogen oxides; Aerospace engineering; Meteorology; Chemistry; Physics; Engineering; Waste management; Mathematics","score_opus":0.01850557594340234,"score_gpt":0.3134325252467769,"score_spread":0.29492694930337454,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4412486671","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":[0.9948583,0.0001388025,0.0022424124,0.00028596137,0.000015310912,0.00039245846,0.000009050591,0.00004738306,0.0020103168],"genre_scores_gemma":[0.9988153,0.000049123188,0.00090791105,0.000014514893,0.0000011985132,0.000012624029,0.00000228883,0.0000031322836,0.00019393534],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.9992739,0.000046534726,0.00018989417,0.00022781876,0.00014529655,0.000116560834],"domain_scores_gemma":[0.9990455,0.00029825474,0.000038647275,0.0005900669,0.0000026905338,0.000024869098],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00031172225,0.00008910853,0.00016941017,0.000021567515,0.00008913751,0.0000033583249,0.0005004365,0.00003995873,0.000051700077],"category_scores_gemma":[0.0001124112,0.000045130924,0.00002357179,0.00020980644,0.00022940167,0.00007553433,0.00033148052,0.00007470687,0.0000025434715],"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":[0.000050429542,0.00008785293,0.97727203,0.000010940517,0.000033420773,0.000004065784,0.0000599952,0.000014694975,0.012517542,0.00005214534,0.0006410451,0.009255832],"study_design_scores_gemma":[0.0024339622,0.0019294712,0.5807723,0.000083304374,0.00029736722,0.0000075167395,0.0022688915,0.001273655,0.3887519,0.0063902806,0.015437345,0.0003540414],"about_ca_topic_score_codex":0.00008962272,"about_ca_topic_score_gemma":0.0002611282,"teacher_disagreement_score":0.39649975,"about_ca_system_score_codex":0.000012793637,"about_ca_system_score_gemma":0.0000070461665,"threshold_uncertainty_score":0.18403856},"labels":[],"label_agreement":null},{"id":"W4412746074","doi":"10.1016/j.ast.2025.110703","title":"Numerical investigation of engine position effects on contrail formation and evolution in the near-field of a realistic aircraft configuration","year":2025,"lang":"en","type":"article","venue":"Aerospace Science and Technology","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure; Université du Québec à Montréal","funders":"Office National d'études et de Recherches Aérospatiales","keywords":"Aerospace engineering; Position (finance); Field (mathematics); Aeronautics; Engineering; Mechanics; Automotive engineering; Physics; Mathematics","score_opus":0.0039911054660181355,"score_gpt":0.22687270560908396,"score_spread":0.22288160014306582,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4412746074","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":[0.9707045,0.00005694004,0.020405045,0.008161302,0.000021387292,0.00028118104,6.169177e-7,0.000038034475,0.0003310208],"genre_scores_gemma":[0.99878967,0.000023025075,0.0010041562,0.0001532467,0.0000010653006,0.000021936232,8.509563e-7,0.0000012215959,0.000004809566],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99941444,0.000022966422,0.00012261026,0.00016161303,0.00016209614,0.00011627054],"domain_scores_gemma":[0.9995977,0.0001451362,0.00007764951,0.00014146407,0.000026862284,0.00001115439],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002920283,0.00006227926,0.000100654106,0.00016392398,0.00010597998,0.000011199522,0.00013397481,0.00009011398,0.0000011731235],"category_scores_gemma":[0.00050295464,0.000046811867,0.000006501688,0.0013224925,0.0010662965,0.00024139106,0.00004006448,0.00010420223,8.662231e-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":[0.000035729954,0.00003558518,0.051254034,0.00005799732,0.0000025173708,0.0000016947821,0.0005639224,0.00021365778,0.76813334,0.10770623,0.00012200545,0.071873315],"study_design_scores_gemma":[0.0005031734,0.0007494615,0.22147034,0.00012609371,0.000011291012,0.000010759274,0.00070906035,0.009305561,0.6991193,0.06787331,0.000027657848,0.0000939742],"about_ca_topic_score_codex":0.00010889536,"about_ca_topic_score_gemma":0.00004242339,"teacher_disagreement_score":0.1702163,"about_ca_system_score_codex":0.000059955517,"about_ca_system_score_gemma":0.00002114157,"threshold_uncertainty_score":0.3928814},"labels":[],"label_agreement":null},{"id":"W4412792350","doi":"10.1016/j.ijhydene.2025.150540","title":"Reducing emissions and fuel consumption in supersonic aviation with ammonia hybrid engines","year":2025,"lang":"en","type":"article","venue":"International Journal of Hydrogen Energy","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":3,"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":"Fuel efficiency; Aviation; Supersonic speed; Environmental science; Ammonia; Automotive engineering; Consumption (sociology); Greenhouse gas; Nitrogen oxides; Thrust specific fuel consumption; Waste management; Chemistry; Aerospace engineering; Engineering","score_opus":0.007556167779140669,"score_gpt":0.23598107560020118,"score_spread":0.2284249078210605,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4412792350","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":[0.9876782,0.00042936174,0.010638749,0.0006861778,0.000098794495,0.000020974769,0.0000014485207,0.000014276308,0.00043204695],"genre_scores_gemma":[0.99697423,0.00049272086,0.0022391977,0.00007548242,0.000017359456,0.0000024811511,0.0000016975561,0.0000040755667,0.00019272664],"study_design_codex":"observational","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9994231,0.000016335598,0.00019071865,0.00010199154,0.00018412442,0.00008374744],"domain_scores_gemma":[0.9997625,0.000040629846,0.00009804351,0.00005324542,0.000019391151,0.00002622257],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00008691202,0.00006834466,0.00008736247,0.00016115796,0.000024192845,0.000016748048,0.0001629492,0.000026963586,0.000048652175],"category_scores_gemma":[0.000045279954,0.000054278295,0.000022530588,0.000090376976,0.00007467964,0.0002371621,0.0000556459,0.00008897045,0.0000019678973],"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":[0.00044564134,0.0003237394,0.46136752,0.000017759518,0.00027249553,0.00062445033,0.00044178902,0.06687559,0.23903936,0.009996417,0.0005964113,0.2199988],"study_design_scores_gemma":[0.007427828,0.0005945188,0.2070068,0.0014361306,0.00012886454,0.0028436189,0.00077256333,0.03550894,0.616347,0.091855265,0.03509714,0.0009812918],"about_ca_topic_score_codex":0.000094839495,"about_ca_topic_score_gemma":0.00010179785,"teacher_disagreement_score":0.37730768,"about_ca_system_score_codex":0.0001517979,"about_ca_system_score_gemma":0.000015397218,"threshold_uncertainty_score":0.22134046},"labels":[],"label_agreement":null},{"id":"W4412973918","doi":"10.3390/en18154156","title":"Hydroprocessed Ester and Fatty Acids to Jet: Are We Heading in the Right Direction for Sustainable Aviation Fuel Production?","year":2025,"lang":"en","type":"article","venue":"Energies","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Nexen (Canada); Université de Sherbrooke","funders":"Natural Sciences and Engineering Research Council of Canada; Université de Sherbrooke","keywords":"Jet fuel; Heading (navigation); Aviation; Aviation biofuel; Jet (fluid); Production (economics); Sustainable production; Aerospace engineering; Aeronautics; Chemistry; Environmental science; Automotive engineering; Engineering; Waste management; Biofuel; Economics; Bioenergy","score_opus":0.008317841137511143,"score_gpt":0.24676782318890159,"score_spread":0.23844998205139045,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4412973918","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":[0.93433404,0.0005254947,0.042152856,0.017712967,0.00015949654,0.00087831006,0.0000010659759,0.00023427891,0.0040014805],"genre_scores_gemma":[0.99310607,0.00007526094,0.001572623,0.00015556793,0.000016921325,0.000244611,0.0000012084163,0.0000044854423,0.0048232735],"study_design_codex":"observational","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.9994423,0.000016607008,0.00008760895,0.0002197963,0.00007511627,0.00015861234],"domain_scores_gemma":[0.999786,0.000038545662,0.000029090088,0.00012698409,0.000010047695,0.000009289243],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00014898613,0.0000784599,0.00007604229,0.00007174292,0.00017078267,0.00004250544,0.000099882935,0.000039731593,0.0000059563495],"category_scores_gemma":[0.000113400456,0.000053986598,0.000013239324,0.00040180728,0.000061139246,0.00030614465,0.00005867221,0.00005265448,0.0000021941687],"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":[0.00034559984,0.0005429227,0.42243713,0.001162339,0.000057789857,0.000035828703,0.01462366,0.14089167,0.1251889,0.09257568,0.025426563,0.1767119],"study_design_scores_gemma":[0.0006599183,0.00016155714,0.2275993,0.00014512871,0.000027386342,0.0000069139455,0.016912816,0.0012992513,0.25501496,0.28803775,0.2096694,0.00046562759],"about_ca_topic_score_codex":0.000034741664,"about_ca_topic_score_gemma":0.00020367265,"teacher_disagreement_score":0.19546208,"about_ca_system_score_codex":0.00009776901,"about_ca_system_score_gemma":0.000004094146,"threshold_uncertainty_score":0.22015096},"labels":[],"label_agreement":null},{"id":"W4412986467","doi":"10.1109/itec63604.2025.11097944","title":"Framework for Technical Performance Uncertainty in Hybrid-Electric Aircraft Development","year":2025,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Computer science; Systems engineering; Aerospace engineering; Aeronautics; Engineering","score_opus":0.01242985545051471,"score_gpt":0.2604213978353074,"score_spread":0.24799154238479268,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4412986467","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":[0.29091918,0.000052840373,0.69749683,0.00078107696,0.000069895796,0.000572386,6.271607e-7,0.000381176,0.009725978],"genre_scores_gemma":[0.8218935,0.000027191194,0.1763973,0.00037397674,0.000003816744,0.00021133237,0.0000015728875,0.000006048795,0.0010852733],"study_design_codex":"design_other","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.99893844,0.000008289651,0.00023104451,0.00033200622,0.00012298483,0.00036725478],"domain_scores_gemma":[0.9995588,0.0001531643,0.000029187786,0.00022605884,0.00000524267,0.000027521239],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017609914,0.00013338211,0.0001474575,0.000101062695,0.00011047967,0.000011530088,0.00033409815,0.00010323922,0.00015164008],"category_scores_gemma":[0.00013970869,0.00011264616,0.000032004275,0.0006343831,0.00008856688,0.00010497295,0.00017243803,0.00020745303,0.00007537582],"study_design_candidate":"design_other","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":[0.000116032046,0.00028305413,0.10272262,0.0000528271,0.000013377649,0.00000797365,0.00004810459,0.009346091,0.008828523,0.03132899,0.004524493,0.8427279],"study_design_scores_gemma":[0.0014746466,0.00031926742,0.25243104,0.0002300487,0.000015504573,0.000012343492,0.00014369175,0.030747587,0.24810964,0.3145351,0.15086634,0.0011147554],"about_ca_topic_score_codex":0.000012487597,"about_ca_topic_score_gemma":0.00004848541,"teacher_disagreement_score":0.8416132,"about_ca_system_score_codex":0.00040309815,"about_ca_system_score_gemma":0.000034287223,"threshold_uncertainty_score":0.4593577},"labels":[],"label_agreement":null},{"id":"W4413080361","doi":"10.2514/1.c038376","title":"Evaluating Bypass Effects of Advanced Turbofan Engines on Contrail Formation Using Large Eddy Simulations","year":2025,"lang":"en","type":"article","venue":"Journal of Aircraft","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université du Québec","funders":"","keywords":"Turbofan; Jet (fluid); Condensation; Mechanics; Environmental science; Atmospheric sciences; Mixing (physics); Materials science; Meteorology; Physics","score_opus":0.01630617452643361,"score_gpt":0.3173503661267706,"score_spread":0.30104419160033696,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4413080361","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":[0.8407472,0.00017142876,0.15810446,0.0002492466,0.00025088622,0.00021957823,0.0000034766279,0.000032224954,0.00022149835],"genre_scores_gemma":[0.96635085,0.000017854109,0.033419248,0.000107048,0.000021806734,0.0000019467896,8.2334026e-7,0.000007353758,0.00007307038],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99889094,0.000053689622,0.0004451268,0.00010499742,0.00031684423,0.00018842975],"domain_scores_gemma":[0.9990043,0.00036849995,0.0003833387,0.0001547284,0.000055212993,0.000033920176],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00027342702,0.000119343764,0.00023979764,0.00015424755,0.00010975423,0.000011940644,0.00018586832,0.00007107194,0.00004469353],"category_scores_gemma":[0.0007460185,0.0000986021,0.00009166804,0.00033238757,0.000061525294,0.00050899317,0.000058138932,0.00019319306,0.0000051504444],"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":[0.000079212215,0.00015236114,0.0017452949,0.00006286888,0.00003484476,0.000008832604,0.00019309607,0.5034729,0.4446066,0.00030373636,0.00015147805,0.049188767],"study_design_scores_gemma":[0.007376734,0.0017776034,0.026469532,0.001482554,0.00025833747,0.00003815437,0.00070540875,0.2426694,0.69809127,0.015740974,0.004876702,0.0005133323],"about_ca_topic_score_codex":0.0000028668148,"about_ca_topic_score_gemma":0.000004634523,"teacher_disagreement_score":0.26080352,"about_ca_system_score_codex":0.00017053475,"about_ca_system_score_gemma":0.000022991022,"threshold_uncertainty_score":0.40208766},"labels":[],"label_agreement":null},{"id":"W4413215600","doi":"10.1115/gt2025-152175","title":"Aerodynamic Force Modelling of Free and Shrouded Propellers in Incidence for Low Subsonic VTOL Operations","year":2025,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Safran Electronics (Canada)","funders":"","keywords":"Aerodynamics; Aerospace engineering; Propeller; Shroud; Rotor (electric); Blade element theory; Aerodynamic force; Range (aeronautics); Blade element momentum theory; Engineering; Mechanics; Marine engineering; Physics; Structural engineering; Mechanical engineering; Turbine blade; Turbine","score_opus":0.013737079679682495,"score_gpt":0.23527995015024594,"score_spread":0.22154287047056345,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4413215600","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":[0.4741532,0.00004272362,0.52407694,0.000190156,0.000010570136,0.00033741898,0.0000019450995,0.00003332621,0.0011537345],"genre_scores_gemma":[0.93214613,0.000057711088,0.06622237,0.000045568147,8.30725e-7,0.000053030155,0.000001013799,0.0000038064584,0.0014695126],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994369,0.000007582563,0.0001576826,0.00019926197,0.00006208098,0.00013646623],"domain_scores_gemma":[0.9997101,0.00005288478,0.0000181408,0.00019984244,0.0000059605463,0.000013104724],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00009422431,0.00007108302,0.00010510277,0.000048527905,0.000054644403,0.000008794314,0.00020538247,0.00004894704,0.000025784651],"category_scores_gemma":[0.00006377722,0.00006007373,0.000017298795,0.0002156883,0.00015510364,0.00019051203,0.00014843723,0.000056495508,0.0000022176382],"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":[0.000030903288,0.00006773952,0.013755235,0.000055074226,0.000007225589,0.0000012287181,0.00018866741,0.89614964,0.05985264,0.020423584,0.00010494111,0.009363118],"study_design_scores_gemma":[0.0003978479,0.000038088372,0.0015672427,0.000040330466,0.0000039046527,5.0825776e-7,0.00021859794,0.95425314,0.015428842,0.027942054,0.000020357267,0.000089100984],"about_ca_topic_score_codex":0.00023998405,"about_ca_topic_score_gemma":0.0023320247,"teacher_disagreement_score":0.45799297,"about_ca_system_score_codex":0.000065132495,"about_ca_system_score_gemma":0.000012825323,"threshold_uncertainty_score":0.24497356},"labels":[],"label_agreement":null},{"id":"W4413215695","doi":"10.1115/gt2025-153993","title":"Preliminary Design and Performance Analysis of Aircraft Propellers Using a 0-D Model","year":2025,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Safran Electronics (Canada)","funders":"","keywords":"Lift (data mining); Parametric statistics; Propeller; Airfoil; Range (aeronautics); Angle of attack; Marine engineering; Computer science; Aerospace engineering; Aerodynamics; Engineering; Mathematics; Data mining","score_opus":0.02429109721658541,"score_gpt":0.24857170676729684,"score_spread":0.22428060955071144,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4413215695","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":[0.4316896,0.000033467855,0.5662179,0.000034400404,0.000004048951,0.000112168345,3.9262102e-7,0.00004331803,0.0018646905],"genre_scores_gemma":[0.81781787,0.00004748211,0.18110698,0.000043470387,3.4953797e-7,0.0000056134386,3.0543248e-7,0.0000028468087,0.000975076],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994228,0.000013471133,0.00013662741,0.0002044452,0.000092058326,0.00013061002],"domain_scores_gemma":[0.99972045,0.00003210342,0.000037679998,0.0001859665,0.0000051368966,0.000018682902],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00010687113,0.00008427509,0.00015624685,0.00014649185,0.00006466663,0.0000053231997,0.00012923547,0.000047978712,0.00006381633],"category_scores_gemma":[0.000015113253,0.00006686105,0.00003417686,0.0008157145,0.0002304202,0.00015663813,0.0001746292,0.000050793464,0.0000027173787],"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":[0.000043488486,0.000027069029,0.027886443,0.0000102172635,0.000071118855,6.4494907e-7,0.00006002284,0.9445006,0.011491592,0.0001354741,0.000069789436,0.015703533],"study_design_scores_gemma":[0.00008358833,0.00006024625,0.009402717,0.000009443106,0.0001732053,4.8189276e-7,0.00005901574,0.97388,0.015466595,0.00077504053,0.000014106298,0.00007557933],"about_ca_topic_score_codex":0.000024827947,"about_ca_topic_score_gemma":0.0000024873239,"teacher_disagreement_score":0.38612828,"about_ca_system_score_codex":0.000043015985,"about_ca_system_score_gemma":0.00001042332,"threshold_uncertainty_score":0.27265143},"labels":[],"label_agreement":null},{"id":"W4413217136","doi":"10.1115/gt2025-151174","title":"Experimental Investigation of Enhanced Heat Sinks for Hybrid Electric Aircraft","year":2025,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Carleton University; National Research Council Canada","funders":"","keywords":"Heat sink; Airflow; Fin; Mechanical engineering; Materials science; Thermal; Heat transfer; Automotive engineering; Environmental science; Mechanics; Engineering; Thermodynamics; Physics","score_opus":0.009689999784663937,"score_gpt":0.2465665447659464,"score_spread":0.23687654498128244,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4413217136","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":[0.70654655,0.00009090926,0.2860276,0.00026343873,0.00005368758,0.00035477578,0.0000015837105,0.0001555039,0.006505982],"genre_scores_gemma":[0.97814226,0.0000063871707,0.020288378,0.00025118436,0.0000040534333,0.00008056368,0.0000034783682,0.0000053285357,0.0012183409],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.999359,0.0000094094985,0.00016066802,0.00021383702,0.000091798574,0.00016528061],"domain_scores_gemma":[0.99972504,0.00005595291,0.000027128186,0.00016301603,0.0000064720216,0.000022362721],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00005672668,0.0000904415,0.00011476948,0.000055228316,0.00006164743,0.0000056239537,0.00015251184,0.00004426562,0.00015857724],"category_scores_gemma":[0.000040419036,0.000080437116,0.000043520155,0.00026731,0.00013518336,0.00012902809,0.00006819544,0.000048787355,0.000018373881],"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":[0.000015862837,0.000025573372,0.00067024364,0.0000055043424,0.00000426301,1.7700829e-7,0.000027823531,0.00013530684,0.9887031,0.0013404085,0.0014716834,0.0076001002],"study_design_scores_gemma":[0.00027255953,0.0001204314,0.00095560245,0.0000074403956,0.0000042642823,5.0159235e-7,0.00006345978,0.00089333585,0.98098475,0.01589831,0.0007168974,0.00008246936],"about_ca_topic_score_codex":0.00002822996,"about_ca_topic_score_gemma":0.0000036474753,"teacher_disagreement_score":0.27159578,"about_ca_system_score_codex":0.00010253096,"about_ca_system_score_gemma":0.000010666409,"threshold_uncertainty_score":0.32801303},"labels":[],"label_agreement":null},{"id":"W4413218849","doi":"10.1115/gt2025-153051","title":"Optimum Pressure Ratio in a Turbojet Engine: Mathematical Expression to Determine the Pressure Ratio Required for Optimization of the Specific Thrust","year":2025,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Carleton University","funders":"","keywords":"Turbojet; Thrust; Overall pressure ratio; Gas compressor; Combustor; Turbine; Jet engine; Aerospace engineering; Computer science; Engineering; Automotive engineering; Combustion","score_opus":0.014935040739777349,"score_gpt":0.24421788216964274,"score_spread":0.22928284142986538,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4413218849","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0027028972,0.00012729212,0.9887532,0.002261249,0.00008431618,0.0018553886,0.000010803683,0.000079981095,0.0041248733],"genre_scores_gemma":[0.86415106,0.000021860065,0.1294269,0.00016569582,0.0000152210305,0.0003142488,0.0000032141404,0.000012954893,0.0058888565],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99901676,0.000046599896,0.00029526014,0.00026476997,0.00018871741,0.00018789433],"domain_scores_gemma":[0.9991468,0.00020989522,0.00007433918,0.00053343707,0.00001492234,0.000020591693],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020308307,0.00013692443,0.00016961223,0.000039603023,0.00011318237,0.00002708888,0.0005134678,0.000100033736,0.00047520315],"category_scores_gemma":[0.00025214278,0.000072626244,0.000054088974,0.0003836083,0.00014843389,0.0001795104,0.0002946156,0.00010425011,0.000005360759],"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":[0.00006713332,0.0000902124,0.00027640696,0.000045088425,0.000010260091,3.9103418e-7,0.00031922868,0.93176043,0.053474467,0.0037068587,0.006386661,0.0038628336],"study_design_scores_gemma":[0.0008608411,0.0001026274,0.001705634,0.00019302787,0.000046240566,0.000001984098,0.0004532664,0.58857805,0.3846482,0.010468097,0.012693358,0.00024867503],"about_ca_topic_score_codex":0.000003406927,"about_ca_topic_score_gemma":0.0000050386843,"teacher_disagreement_score":0.86144817,"about_ca_system_score_codex":0.000027771983,"about_ca_system_score_gemma":0.000010527012,"threshold_uncertainty_score":0.52031416},"labels":[],"label_agreement":null},{"id":"W4413219341","doi":"10.1115/gt2025-153546","title":"Surrogate Modelling of a Turboprop Engine Performance","year":2025,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Safran Electronics (Canada)","funders":"","keywords":"Turboprop; Perceptron; Artificial neural network; Computer science; Fuel efficiency; Thrust specific fuel consumption; Mean absolute percentage error; Latin hypercube sampling; Design of experiments; Surrogate model; Performance prediction; Simulation; Machine learning; Engineering; Monte Carlo method; Automotive engineering; Statistics; Mathematics","score_opus":0.013962774381100928,"score_gpt":0.20596436221609532,"score_spread":0.19200158783499438,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4413219341","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":[0.65961254,0.000038215803,0.2977447,0.000108307235,0.000028181326,0.000068815105,3.8309295e-7,0.00012396596,0.042274933],"genre_scores_gemma":[0.96608925,0.000060353465,0.030019946,0.000036924543,0.000001318352,0.0000045113766,3.117708e-7,0.0000024198964,0.0037849525],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99961144,0.0000031372163,0.000095290656,0.00011186533,0.000069202164,0.00010906654],"domain_scores_gemma":[0.9998064,0.000015111132,0.000018635845,0.00014637904,0.0000033448323,0.000010149025],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000052857933,0.000054224456,0.00007287582,0.000027726659,0.00002836018,0.000002329385,0.0001325273,0.000030701303,0.00022793801],"category_scores_gemma":[0.000007650401,0.00004235772,0.000018375395,0.00022147874,0.00009307752,0.00009327477,0.000089804125,0.000053432606,0.00004453171],"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":[0.000027672535,0.00008034378,0.032945137,0.000048245307,0.000014519762,0.0000023396997,0.00007930539,0.5639078,0.02240927,0.0041083065,0.00052526535,0.3758518],"study_design_scores_gemma":[0.000257796,0.000053693813,0.0030442425,0.000031741147,0.000006827218,0.0000010030302,0.00006694611,0.4833842,0.49964607,0.009861139,0.0035054418,0.00014090393],"about_ca_topic_score_codex":0.000025261168,"about_ca_topic_score_gemma":0.0000021999222,"teacher_disagreement_score":0.4772368,"about_ca_system_score_codex":0.00002336886,"about_ca_system_score_gemma":0.0000029155663,"threshold_uncertainty_score":0.24957614},"labels":[],"label_agreement":null},{"id":"W4413329722","doi":"10.1007/s13272-025-00880-9","title":"Tailored composites and digital optimization for efficient eVTOL propellers","year":2025,"lang":"en","type":"article","venue":"CEAS Aeronautical Journal","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Centre for Excellence in Mining Innovation","funders":"","keywords":"Composite material; Materials science; Mechanical engineering; Computer science; Engineering","score_opus":0.007994452008816893,"score_gpt":0.23138368548269675,"score_spread":0.22338923347387984,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4413329722","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":[0.10528233,0.00016746417,0.88960224,0.0018327839,0.00010291626,0.0003017494,0.0000037817956,0.0000737673,0.0026329427],"genre_scores_gemma":[0.96234804,0.0000200569,0.037204564,0.00011828553,0.000013398062,0.000007701482,0.000002606379,0.0000065416502,0.00027880174],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993202,0.000010651063,0.00016302805,0.00016805221,0.0001265938,0.00021145216],"domain_scores_gemma":[0.99971336,0.00007621427,0.000039393297,0.00007953304,0.0000128655465,0.0000786423],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000081993916,0.000096213495,0.00010795525,0.00003573864,0.00022101424,0.0001152987,0.00013277837,0.00005675429,0.0001136635],"category_scores_gemma":[0.00013104896,0.00007290161,0.000038753642,0.00011898401,0.00031860228,0.00013433384,0.00011826008,0.0001324168,0.000012531286],"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":[0.00046304014,0.0005513643,0.024766793,0.00004896293,0.00008929707,0.000033703018,0.00015413963,0.62986773,0.010660701,0.014356886,0.004875979,0.31413138],"study_design_scores_gemma":[0.0023892743,0.00039704537,0.009800146,0.00010699182,0.00006871747,0.00013678714,0.00031877434,0.9469168,0.004372346,0.024445701,0.010615714,0.00043166167],"about_ca_topic_score_codex":2.9921424e-7,"about_ca_topic_score_gemma":1.7159493e-7,"teacher_disagreement_score":0.85706574,"about_ca_system_score_codex":0.000089498055,"about_ca_system_score_gemma":0.000011257438,"threshold_uncertainty_score":0.29728413},"labels":[],"label_agreement":null},{"id":"W4413513824","doi":"10.1109/isie62713.2025.11124611","title":"Aerodynamic Modelling of a Small Electric Aircraft","year":2025,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"University of Waterloo","funders":"","keywords":"Aerodynamics; Aerospace engineering; Computer science; Aeronautics; Environmental science; Automotive engineering; Engineering","score_opus":0.014310990809577734,"score_gpt":0.21576903774027426,"score_spread":0.20145804693069652,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4413513824","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":[0.18921515,0.00005987926,0.7728632,0.00013270564,0.000021240585,0.000090155365,2.8569067e-7,0.00015549886,0.037461884],"genre_scores_gemma":[0.93646413,0.00004344439,0.05961419,0.00008333025,0.0000012600107,0.00000756785,3.8416084e-7,0.000003935686,0.0037817429],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994507,0.00000822666,0.00013265025,0.00017482921,0.00007126841,0.00016236088],"domain_scores_gemma":[0.99971926,0.000036093516,0.000028052355,0.00019867125,0.0000038735534,0.000014066403],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00005957159,0.00007391483,0.00010082615,0.000062353734,0.000035575566,0.0000035926623,0.0002080365,0.00005276991,0.00016745419],"category_scores_gemma":[0.000017420685,0.00006253297,0.00003550745,0.0004915042,0.00007041465,0.000053981967,0.00010314261,0.00007746154,0.000054074582],"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":[0.000039030478,0.00022343265,0.02556311,0.00003866539,0.000035447236,0.000007527157,0.00006376391,0.5281437,0.19523278,0.039155208,0.0011568317,0.2103405],"study_design_scores_gemma":[0.0005030022,0.0001280998,0.00714059,0.000034665652,0.000027028515,0.0000032170287,0.00011293482,0.7520145,0.09871178,0.13691042,0.0040585604,0.00035516915],"about_ca_topic_score_codex":0.00011223673,"about_ca_topic_score_gemma":0.000055502984,"teacher_disagreement_score":0.747249,"about_ca_system_score_codex":0.000056878358,"about_ca_system_score_gemma":0.000006701348,"threshold_uncertainty_score":0.25500205},"labels":[],"label_agreement":null},{"id":"W4414043843","doi":"10.1016/j.applthermaleng.2025.128096","title":"A study on the potential of skin heat exchangers for hybrid-electric aircraft","year":2025,"lang":"en","type":"article","venue":"Applied Thermal Engineering","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":3,"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 Victoria","funders":"Fundação para a Ciência e a Tecnologia","keywords":"Heat transfer; Aerodynamics; Heat exchanger; Convective heat transfer; Aerodynamic heating; Thermal; Work (physics); Plate heat exchanger","score_opus":0.006864961742216793,"score_gpt":0.20436836546402765,"score_spread":0.19750340372181086,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4414043843","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":[0.90719855,0.000027068012,0.08954636,0.00013756676,0.00006560071,0.00086740346,0.0000021116402,0.00015144165,0.002003885],"genre_scores_gemma":[0.9989406,0.0000026628913,0.0006271251,0.00006757432,0.000013384437,0.00026977374,6.163812e-7,0.000014192045,0.00006408326],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9993406,0.000005673854,0.00012549484,0.00019017748,0.00011912188,0.00021892134],"domain_scores_gemma":[0.9996246,0.00010198877,0.000020063122,0.00023521336,0.0000028351494,0.000015296397],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012031394,0.00012622857,0.00012833031,0.000058171303,0.00006550233,0.0000074744657,0.0002645793,0.000031294992,0.000030563846],"category_scores_gemma":[0.000019765848,0.0000927501,0.000048082817,0.00026017506,0.000033718174,0.00002727861,0.00008969768,0.000109350476,0.000011973955],"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":[0.000054047985,0.0001348227,0.00010216324,0.000013053772,0.000050158047,0.0000036247145,0.0001244566,0.17592339,0.7987672,0.0039261384,0.00013108489,0.020769862],"study_design_scores_gemma":[0.0012114742,0.00034720023,0.015863836,0.000023771508,0.00005796863,0.000002148684,0.0007986868,0.027896592,0.9500428,0.0020915156,0.001291629,0.0003723839],"about_ca_topic_score_codex":0.000009553548,"about_ca_topic_score_gemma":6.8052765e-7,"teacher_disagreement_score":0.15127559,"about_ca_system_score_codex":0.000053470027,"about_ca_system_score_gemma":0.000003503263,"threshold_uncertainty_score":0.37822396},"labels":[],"label_agreement":null},{"id":"W4414217981","doi":"10.2514/1.c037723","title":"Weight Estimation and Architecture Definition of Fuel Systems for Aircraft Conceptual Design","year":2025,"lang":"en","type":"article","venue":"Journal of Aircraft","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Concordia University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Propulsion; Conceptual design; Aircraft fuel system; Component (thermodynamics); Multidisciplinary design optimization; Key (lock); Systems design; Range (aeronautics); Electric power system","score_opus":0.01914006974081563,"score_gpt":0.24609643522282698,"score_spread":0.22695636548201134,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4414217981","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.021767927,0.0014972133,0.97482204,0.00067884626,0.00022436505,0.00034513735,0.000008560664,0.000033912736,0.0006219898],"genre_scores_gemma":[0.7649344,0.00024691303,0.23456839,0.0000656413,0.000027063337,0.000014302197,0.0000015554106,0.000009528912,0.00013219238],"study_design_codex":"simulation_or_modeling","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.99892926,0.00005949239,0.0004722643,0.00014957612,0.00021932778,0.00017008463],"domain_scores_gemma":[0.9990512,0.00036046383,0.00035493803,0.00013445436,0.000051027055,0.000047904683],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00037436237,0.00013630248,0.00029708908,0.00014265033,0.000071587805,0.000018333923,0.00019273024,0.00012006781,0.000020164869],"category_scores_gemma":[0.00027353456,0.000108761786,0.00008259446,0.00020486966,0.0003571457,0.00024002562,0.00005568492,0.00017411081,0.0000030772937],"study_design_candidate":"theoretical_or_conceptual","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":[0.0024840864,0.0009801103,0.018804686,0.0014319826,0.00064174755,0.00009754351,0.0036129444,0.34951487,0.15391442,0.07928299,0.041872945,0.34736165],"study_design_scores_gemma":[0.008875477,0.004600563,0.013903476,0.0016391525,0.00060734234,0.0006217873,0.0032093674,0.031407412,0.0526691,0.8275302,0.05380773,0.0011283571],"about_ca_topic_score_codex":0.0000074789673,"about_ca_topic_score_gemma":0.000002171592,"teacher_disagreement_score":0.74824727,"about_ca_system_score_codex":0.00009137287,"about_ca_system_score_gemma":0.00003805095,"threshold_uncertainty_score":0.44351768},"labels":[],"label_agreement":null},{"id":"W4415046404","doi":"10.1029/2025ef006201","title":"A Stylized Study of the Climate Response to Longwave and Shortwave Forcing at the Altitude of Aviation‐Induced Cirrus","year":2025,"lang":"en","type":"article","venue":"Earth s Future","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Merck Canada Inc. (Canada)","funders":"Carnegie Institution for Science; Gates Ventures","keywords":"Longwave; Shortwave; Cirrus; Radiative forcing; Cloud forcing; Shortwave radiation; Forcing (mathematics); Latitude","score_opus":0.007369614039987669,"score_gpt":0.2437703646511604,"score_spread":0.23640075061117272,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4415046404","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":[0.9973277,0.0000678807,0.00013404942,0.0012714114,0.00009600622,0.00065657,0.000006456576,0.000025101686,0.00041485525],"genre_scores_gemma":[0.99888325,0.000013938106,0.00036771063,0.00015106844,0.000008214505,0.000019094332,3.023999e-7,0.000004625922,0.0005517732],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.9992045,0.00010435972,0.0001701169,0.00018797269,0.00019032638,0.00014269544],"domain_scores_gemma":[0.99935585,0.00011826268,0.00008121426,0.0004165169,0.000009482102,0.000018658078],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000302148,0.00009103782,0.00013585252,0.000031349962,0.00018942294,0.000007678196,0.00022012398,0.000051609873,0.000057862762],"category_scores_gemma":[0.00010973813,0.000050805582,0.00003341144,0.00035335208,0.000096386495,0.000047936006,0.0004908067,0.00011199259,0.0000051755596],"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":[0.0016016565,0.0002478716,0.41691548,0.000030948002,0.00008035815,0.00000846011,0.0096095195,0.0013864209,0.53070766,0.0006874496,0.00053417037,0.038190033],"study_design_scores_gemma":[0.0005593343,0.00019891288,0.95398974,0.000024091585,0.00002264264,0.000001741218,0.0037011844,0.00005954433,0.039921034,0.00035706788,0.0010904596,0.000074242926],"about_ca_topic_score_codex":0.00003609949,"about_ca_topic_score_gemma":0.0010077565,"teacher_disagreement_score":0.53707427,"about_ca_system_score_codex":0.000027889237,"about_ca_system_score_gemma":0.000008143628,"threshold_uncertainty_score":0.20717916},"labels":[],"label_agreement":null},{"id":"W4415070958","doi":"10.1016/j.treng.2025.100397","title":"Blended wing body designs for aerodynamic, stability, and control optimization: A comprehensive review","year":2025,"lang":"en","type":"review","venue":"Transportation Engineering","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Carleton University","funders":"United Arab Emirates University","keywords":"Propulsion; Aerospace; Fuselage; Airworthiness; Payload (computing); Aviation; Aerodynamics; Control (management)","score_opus":0.026455799688963094,"score_gpt":0.27247036313493733,"score_spread":0.24601456344597425,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4415070958","genre_codex":"review","genre_gemma":"review","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"review","genre_consensus":"review","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[8.479577e-7,0.5564228,0.4419576,0.000026157873,0.00003976397,0.0013100537,0.0000714704,0.00015803568,0.000013256311],"genre_scores_gemma":[0.00009747531,0.9688835,0.030113239,0.000048697304,0.000008735902,0.00056771364,0.00022554773,0.00003265378,0.00002244505],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9987094,0.000022983859,0.0005000806,0.00041869335,0.00012411935,0.0002247214],"domain_scores_gemma":[0.99923307,0.00033808962,0.00013927647,0.00022196029,0.000019245395,0.000048385697],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.000114148825,0.0003359672,0.0009329183,0.000071288014,0.000066017215,0.000013455337,0.00016505655,0.00015260644,0.00008783407],"category_scores_gemma":[0.00005694129,0.00031974053,0.00018023675,0.00030556964,0.000051193143,0.00014959484,0.0000093342915,0.0001707827,0.00000267155],"study_design_candidate":"not_applicable","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":[0.000013354678,0.000057887086,0.00002948114,0.262865,0.00024502858,0.000015434467,0.00006354772,0.20109217,0.0001226807,0.0006023234,0.00015548493,0.5347376],"study_design_scores_gemma":[0.0014272076,0.00014669084,0.00015796062,0.07164808,0.0034372772,0.000013034411,0.00003013891,0.036442913,0.000029553437,0.00016636492,0.8847213,0.0017794962],"about_ca_topic_score_codex":0.0000029094701,"about_ca_topic_score_gemma":0.0000042590086,"teacher_disagreement_score":0.8845658,"about_ca_system_score_codex":0.00010727334,"about_ca_system_score_gemma":0.000028895973,"threshold_uncertainty_score":0.9999255},"labels":[],"label_agreement":null},{"id":"W4415823959","doi":"10.1016/j.ecolecon.2025.108842","title":"Fixed capital and growth imperatives: Is commercial aviation trapped in a treadmill?","year":2025,"lang":"en","type":"article","venue":"Ecological Economics","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","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":"Université du Québec à Montréal; University of Waterloo","funders":"","keywords":"Aviation; Profitability index; Capital (architecture); Fixed cost; Investment (military); Commercial aviation; Fixed asset; Fixed capital","score_opus":0.008525398701143041,"score_gpt":0.2224778743092361,"score_spread":0.21395247560809305,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4415823959","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":[0.99215466,0.000017908937,0.00047823854,0.0021640034,0.000045774086,0.00018685336,0.00000780609,0.000051598145,0.004893157],"genre_scores_gemma":[0.9972715,0.00018238221,0.0011499843,0.001147998,0.000006031971,0.000034551787,0.0000035509497,0.0000031440684,0.00020087049],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.99933946,0.000022936592,0.00018007935,0.00026585246,0.000018998117,0.00017268017],"domain_scores_gemma":[0.9997387,0.000108027954,0.000037382226,0.00008452403,0.0000020631182,0.000029281393],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00008326449,0.0001025228,0.00016740993,0.0000424552,0.00007501598,0.000020482319,0.00011563197,0.00013405,0.00044614394],"category_scores_gemma":[0.00007408362,0.00008721229,0.000028050996,0.00009757006,0.00020666105,0.00015330054,0.0001235982,0.00012118517,0.00004795247],"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":[0.00007697994,0.00030070217,0.9092678,0.000007175956,0.000016434255,0.000009278425,0.0008536769,0.00022782687,0.00085948844,0.03602165,0.0013280676,0.05103094],"study_design_scores_gemma":[0.0005996674,0.00012008333,0.9084076,0.0000024561584,0.0000033731023,0.000001145187,0.0002571525,0.0014185517,0.0011028597,0.08738631,0.0005663105,0.00013447886],"about_ca_topic_score_codex":0.0000427842,"about_ca_topic_score_gemma":0.00047349575,"teacher_disagreement_score":0.051364657,"about_ca_system_score_codex":0.00018869039,"about_ca_system_score_gemma":0.000008521329,"threshold_uncertainty_score":0.48849633},"labels":[],"label_agreement":null},{"id":"W4416342587","doi":"10.1109/epec65543.2025.11230450","title":"Energy Management and Control of a Hybrid-Electric Aircraft Propulsion System","year":2025,"lang":"","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"National Research Council Canada; University of Waterloo","funders":"","keywords":"Aerospace; Propulsion; Aviation; Certification; Energy management; Control (management); Control system; Task (project management)","score_opus":0.003913570827253053,"score_gpt":0.19371331834131794,"score_spread":0.1897997475140649,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4416342587","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":[0.018794077,0.004468494,0.941365,0.0006278093,0.00021521644,0.00094395055,0.000010759567,0.00029276917,0.033281937],"genre_scores_gemma":[0.98644054,0.0013581557,0.003396387,0.00015673022,0.000006070055,0.00006826223,5.971218e-7,0.000012166888,0.008561115],"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9979942,0.000058888552,0.00052890927,0.00065174454,0.00030834568,0.00045790098],"domain_scores_gemma":[0.9992046,0.0000612335,0.00016323624,0.00048687326,0.000015281834,0.000068806665],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00017677901,0.00030228737,0.00044335818,0.00027464243,0.00017720334,0.000029340572,0.00037813067,0.00009586575,0.00012444446],"category_scores_gemma":[0.00001157433,0.00025393793,0.0000838023,0.0007607442,0.00033421614,0.00016764946,0.00041911745,0.00012373665,0.000021795438],"study_design_candidate":"design_other","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":[0.00016444661,0.0002505077,0.0053651426,0.0008455237,0.00019528325,0.000104051025,0.000014434271,0.00026822017,0.044238526,0.11921741,0.00069807365,0.8286384],"study_design_scores_gemma":[0.0063883914,0.00121447,0.017293897,0.0013816253,0.0006920517,0.00008540035,0.0015536221,0.15575482,0.76463073,0.029190313,0.020575505,0.001239189],"about_ca_topic_score_codex":0.00011884207,"about_ca_topic_score_gemma":0.0000074624104,"teacher_disagreement_score":0.9676464,"about_ca_system_score_codex":0.00027930547,"about_ca_system_score_gemma":0.000013641486,"threshold_uncertainty_score":0.9999913},"labels":[],"label_agreement":null},{"id":"W4416342600","doi":"10.1109/epec65543.2025.11230438","title":"Modelling the Powertrain and Aerodynamic Behaviour of a Small Electric Aircraft","year":2025,"lang":"","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"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":"Powertrain; Torque; Aerodynamics; Battery (electricity); Battery electric vehicle; MATLAB; Electric vehicle; Electric motor","score_opus":0.01155559169618348,"score_gpt":0.2228719074901155,"score_spread":0.21131631579393204,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4416342600","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":[0.4696688,0.0021166932,0.5214382,0.0014622106,0.00008879965,0.0005389878,0.0000066506036,0.000104711624,0.004574952],"genre_scores_gemma":[0.98082334,0.0016047808,0.013515637,0.00016831033,0.0000040410364,0.00001836893,5.543707e-7,0.000013766381,0.0038511828],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.998247,0.000055571996,0.0004492161,0.0005494646,0.0002028113,0.00049588917],"domain_scores_gemma":[0.99907535,0.0001855111,0.0001253301,0.0005486962,0.000015251024,0.000049833707],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00033681744,0.00028972627,0.00030790342,0.00014269384,0.00026435166,0.00003821617,0.0005978657,0.00020907591,0.00022226876],"category_scores_gemma":[0.000041128733,0.00020506613,0.00010052482,0.00095587457,0.00070632424,0.00013268026,0.00040759993,0.000401268,0.000017039345],"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":[0.00016482853,0.00078744994,0.03922933,0.00017642378,0.00019914164,0.000031165015,0.0010319811,0.32996845,0.10041649,0.062031727,0.0003642795,0.46559873],"study_design_scores_gemma":[0.00065712584,0.00032549113,0.017501362,0.00011526305,0.00017200399,0.000015326548,0.0013792788,0.92548954,0.014174368,0.039222583,0.00046211586,0.00048555495],"about_ca_topic_score_codex":0.0005962616,"about_ca_topic_score_gemma":0.00014945908,"teacher_disagreement_score":0.5955211,"about_ca_system_score_codex":0.000116312694,"about_ca_system_score_gemma":0.00003908895,"threshold_uncertainty_score":0.8362354},"labels":[],"label_agreement":null},{"id":"W4417306678","doi":"10.1080/15567036.2025.2601825","title":"ZA novel carbon-reducing aviation fuel and mechanism for small gas turbine","year":2025,"lang":"en","type":"article","venue":"Energy Sources Part A Recovery Utilization and Environmental Effects","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"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":"Fundamental Research Funds for the Central Universities","keywords":"Mechanism (biology); Gas turbines; Aviation; Turbine; Electricity generation","score_opus":0.010627009839188491,"score_gpt":0.2038602151963456,"score_spread":0.1932332053571571,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4417306678","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":[0.8290435,0.00082822,0.16806677,0.00015353397,0.00025431055,0.00038480424,0.000014298758,0.00013306593,0.0011214556],"genre_scores_gemma":[0.9944264,0.0012904727,0.0019506027,0.00045883324,0.000024918521,0.00012031474,0.000070786955,0.000019999878,0.0016376151],"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99900496,0.000029273235,0.0001800431,0.00044463214,0.000107993474,0.00023307008],"domain_scores_gemma":[0.9995595,0.00013648318,0.00008470796,0.0001556404,0.0000018509542,0.00006181167],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000089578585,0.00021010434,0.00018219643,0.00007158314,0.0001859563,0.00003654176,0.000080971084,0.000134553,0.00002381948],"category_scores_gemma":[0.000054624143,0.00020470245,0.00004089195,0.00011908507,0.00016404365,0.00014541399,0.00016107371,0.00006318019,0.0000019020192],"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":[0.0003484837,0.00059879734,0.03006685,0.00036857586,0.00018138115,0.0000075303874,0.0008463796,0.008953922,0.37844732,0.035694107,0.0004365801,0.54405004],"study_design_scores_gemma":[0.007424151,0.0015580065,0.032135744,0.00045875684,0.00036238012,0.000047501097,0.0011838028,0.29413104,0.4692832,0.12466843,0.06665631,0.0020906902],"about_ca_topic_score_codex":0.000074589014,"about_ca_topic_score_gemma":0.00005533614,"teacher_disagreement_score":0.54195935,"about_ca_system_score_codex":0.00010891161,"about_ca_system_score_gemma":0.0000035976832,"threshold_uncertainty_score":0.8347524},"labels":[],"label_agreement":null},{"id":"W585237834","doi":"","title":"NOISES FROM MONTREAL","year":2001,"lang":"en","type":"article","venue":"Airline business","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Advertising; Business; Subtitle; Aeronautics; Marketing; Engineering; Computer science","score_opus":0.010033234873477723,"score_gpt":0.21254367675568853,"score_spread":0.2025104418822108,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W585237834","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":[0.94083756,0.00013859282,0.037247077,0.0018964002,0.00016156638,0.000120602985,0.0000086768205,0.0005379678,0.019051567],"genre_scores_gemma":[0.9927827,0.00015870438,0.0051845736,0.00029409974,0.000075070835,0.000011386225,0.000016818,0.000013457842,0.0014631761],"study_design_codex":"design_other","study_design_gemma":"observational","domain_scores_codex":[0.99928916,0.000007529191,0.00011544651,0.0002472252,0.00014038266,0.0002002523],"domain_scores_gemma":[0.99960744,0.000034135202,0.000037428566,0.0002734934,0.000010633966,0.000036889676],"candidate_categories":["insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.000027720338,0.000116315634,0.000112922804,0.000020672951,0.000070753784,0.000013594293,0.0002305141,0.000060854138,0.0016058141],"category_scores_gemma":[0.000060894545,0.00009632574,0.000023740971,0.00040147497,0.00013917973,0.00022064228,0.00014586371,0.00006494693,0.0009540268],"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":[0.00008698443,0.0002639414,0.30562818,0.0000034975797,0.000016883954,0.0002624346,0.00013582189,0.005573959,0.017454145,0.00013317341,0.014896011,0.655545],"study_design_scores_gemma":[0.00038722344,0.000017585413,0.9202604,0.0000091308575,0.000010084692,0.000012872995,0.000056152116,0.00077870034,0.0017458745,0.011094927,0.06539855,0.00022845737],"about_ca_topic_score_codex":0.003767775,"about_ca_topic_score_gemma":0.0010983718,"teacher_disagreement_score":0.65531653,"about_ca_system_score_codex":0.00003743662,"about_ca_system_score_gemma":0.000004006697,"threshold_uncertainty_score":0.99982387},"labels":[],"label_agreement":null},{"id":"W598313066","doi":"","title":"Avro Canada C102 Jetliner : in color","year":2008,"lang":"en","type":"article","venue":"Airliners","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Comet; Aeronautics; Meteorology; Geography; Engineering; Astronomy; Physics","score_opus":0.009988945221754208,"score_gpt":0.19284523969015355,"score_spread":0.18285629446839935,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W598313066","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":[0.98383933,0.00004211037,0.00044823904,0.001490345,0.00010848827,0.00011626731,0.0000028538443,0.00011157237,0.013840814],"genre_scores_gemma":[0.9935604,0.000039033606,0.0027573772,0.00072181766,0.000011533662,0.000013714302,0.0000024483652,0.000008483128,0.0028852357],"study_design_codex":"observational","study_design_gemma":"not_applicable","domain_scores_codex":[0.9992603,0.000010115023,0.00012759211,0.00019420902,0.00016591627,0.00024184118],"domain_scores_gemma":[0.9997229,0.000033732365,0.000026896518,0.00016814051,0.000002730005,0.00004559475],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000040688326,0.000092201204,0.00009904972,0.000023017927,0.00005557087,0.000001967542,0.00018257833,0.00004749581,0.00033532866],"category_scores_gemma":[0.000059453843,0.00008035708,0.00001733822,0.00025218958,0.0001643678,0.000087716755,0.000077428354,0.00011768642,0.00010745727],"study_design_candidate":"observational","study_design_consensus":null,"about_ca_topic_candidate":true,"about_ca_topic_consensus":true,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00004561306,0.00013422623,0.6920247,0.000006058649,0.000011462159,0.0011670764,0.00029484453,0.05094836,0.010615307,0.0003688863,0.21685755,0.027525933],"study_design_scores_gemma":[0.0018077097,0.00017148798,0.3050513,0.000020522259,0.00000844123,0.00011379262,0.0008602279,0.009628259,0.018409954,0.0018582068,0.6610067,0.001063448],"about_ca_topic_score_codex":0.20754069,"about_ca_topic_score_gemma":0.56826586,"teacher_disagreement_score":0.4441491,"about_ca_system_score_codex":0.00026057067,"about_ca_system_score_gemma":0.000048744456,"threshold_uncertainty_score":0.79773635},"labels":[],"label_agreement":null},{"id":"W636920640","doi":"","title":"Bombardier Learjet 60XR : $13.3 mil, Mach .81, FL510, 2365 nm, 6-9 seats","year":2008,"lang":"en","type":"article","venue":"Professional pilot","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Aeronautics; Mach number; Aerospace engineering; Engineering; Automotive engineering; Physics; Environmental science","score_opus":0.0353628134350401,"score_gpt":0.2680893417485068,"score_spread":0.23272652831346669,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W636920640","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":[0.94860697,0.00052949414,0.002099934,0.0047753435,0.0009819529,0.00070822204,0.000027895177,0.0008666006,0.041403588],"genre_scores_gemma":[0.95969003,0.00012013458,0.0067901877,0.00070402125,0.0000786851,0.000081179394,0.000014409054,0.000033658907,0.032487664],"study_design_codex":"not_applicable","study_design_gemma":"observational","domain_scores_codex":[0.99803776,0.000073348296,0.00025108532,0.0005276351,0.0005740203,0.00053617184],"domain_scores_gemma":[0.9992534,0.00009137978,0.00008186691,0.0004179299,0.000014179044,0.00014127417],"candidate_categories":["insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.0001690235,0.00025224267,0.00023180502,0.00005363243,0.00054129417,0.000009830301,0.00046184604,0.00012930084,0.0029825657],"category_scores_gemma":[0.00008912585,0.00019879008,0.00007566149,0.0002933234,0.00052207644,0.00032098783,0.0005516671,0.00043783893,0.0034373489],"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":[0.00059221504,0.0017866617,0.33078945,0.000059587048,0.00007931893,0.0005573086,0.00080613274,0.0008296373,0.12116129,0.003271549,0.48530707,0.0547598],"study_design_scores_gemma":[0.0025251752,0.0009828918,0.61701137,0.00014037348,0.000032497843,0.00027262108,0.0004788246,0.0009889415,0.027861698,0.047598965,0.30055478,0.0015518846],"about_ca_topic_score_codex":0.000066558685,"about_ca_topic_score_gemma":0.000022546781,"teacher_disagreement_score":0.28622192,"about_ca_system_score_codex":0.00013514391,"about_ca_system_score_gemma":0.00003120819,"threshold_uncertainty_score":0.99792886},"labels":[],"label_agreement":null},{"id":"W656213694","doi":"","title":"AIR CANADA ACQUISITION NEARS COMPLETION","year":2000,"lang":"en","type":"article","venue":"Commercial Aviation Report","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Aeronautics; Business; Air travel; Operations management; Advertising; Aviation; Engineering; Aerospace engineering","score_opus":0.008847305354522134,"score_gpt":0.21954952797062163,"score_spread":0.2107022226160995,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W656213694","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":[0.9484758,0.000013129581,0.008149699,0.0034003723,0.00021911097,0.00023876742,0.000010850073,0.00026217592,0.03923014],"genre_scores_gemma":[0.99606067,0.000007681484,0.00091899396,0.0011707629,0.00004458675,0.000015686888,0.00009045313,0.000007445223,0.0016837043],"study_design_codex":"design_other","study_design_gemma":"observational","domain_scores_codex":[0.9991315,0.000020702826,0.00021599302,0.00019796338,0.00028012902,0.0001537214],"domain_scores_gemma":[0.9996225,0.000016719281,0.000084357554,0.00022341091,0.0000098316905,0.000043164524],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00009143092,0.00008613051,0.00009624175,0.000013484651,0.00018067884,0.000008939962,0.00010873006,0.00005086671,0.0045039337],"category_scores_gemma":[0.000023604709,0.000087626955,0.00002583937,0.00016444252,0.00006800482,0.00015846064,0.000033084583,0.000082314844,0.0002417889],"study_design_candidate":"observational","study_design_consensus":null,"about_ca_topic_candidate":true,"about_ca_topic_consensus":true,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00004013383,0.00010376202,0.34630615,0.000004560634,0.00001075737,0.00036145924,0.000079452235,0.0034762858,0.0027701452,0.00045045547,0.08057872,0.56581813],"study_design_scores_gemma":[0.00010793863,0.000018110635,0.82721525,0.0000032914652,0.000004741271,0.000066058376,0.000013372971,0.0002061592,0.00089252245,0.002423926,0.16891809,0.00013053766],"about_ca_topic_score_codex":0.07585476,"about_ca_topic_score_gemma":0.07734645,"teacher_disagreement_score":0.5656876,"about_ca_system_score_codex":0.00030432458,"about_ca_system_score_gemma":0.00002917575,"threshold_uncertainty_score":0.9964061},"labels":[],"label_agreement":null},{"id":"W6893160424","doi":"10.5281/zenodo.1459677","title":"Helicopters Market Overview, Challenges, Opportunities, Trends and Market Analysis by 2023","year":2018,"lang":"en","type":"article","venue":"Zenodo (CERN European Organization for Nuclear Research)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Work (physics); Government (linguistics); Staring; Product (mathematics)","score_opus":0.05727625105437764,"score_gpt":0.25165827448681066,"score_spread":0.19438202343243302,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6893160424","genre_codex":"other","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"other","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0073960233,0.0011034326,0.0027795136,0.0031360004,0.000051331222,0.00019875032,0.0003292164,0.001006417,0.9839993],"genre_scores_gemma":[0.91492057,0.016407855,0.0015937502,0.0006759771,0.00011397641,2.6215287e-7,0.0010074907,0.0012104678,0.064069666],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9986008,0.00018293974,0.0001667788,0.0004405871,0.00028449498,0.0003244225],"domain_scores_gemma":[0.99930185,0.000016552545,0.00007500034,0.00041641956,0.000042467585,0.00014773087],"candidate_categories":["insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.0004913327,0.00014267689,0.00015348186,0.00022341074,0.0009654715,0.00019070665,0.0006025082,0.000067252186,0.11539411],"category_scores_gemma":[0.00012365845,0.00014237914,0.00004336051,0.00082085317,0.00058130425,0.0002704147,0.001177633,0.00013050063,0.0014900706],"study_design_candidate":"not_applicable","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":[0.000025560174,0.00003613226,0.00001951117,0.0000079286665,0.000057465473,0.0000065497966,0.0001368901,0.0000015310089,0.00051851117,0.00024052981,0.4785852,0.52036417],"study_design_scores_gemma":[0.00018920068,0.00018432204,0.006051264,0.0000066158414,0.000037456553,0.000019157073,0.00036128334,0.00058497884,0.00013024906,0.00020585812,0.9920579,0.00017171701],"about_ca_topic_score_codex":0.000033380304,"about_ca_topic_score_gemma":0.000003632801,"teacher_disagreement_score":0.9199296,"about_ca_system_score_codex":0.00012216186,"about_ca_system_score_gemma":6.331571e-7,"threshold_uncertainty_score":0.99928737},"labels":[],"label_agreement":null},{"id":"W6907639279","doi":"10.25316/ir-19243","title":"Optimization of a Hydrogen Alternative Aviation Fuel Supply Chain Under Demand and Emissions Constraints - A Case Study of Canada","year":2023,"lang":"en","type":"article","venue":"VIUSpace (Vancouver Island University Library)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Greenhouse gas; Jet fuel; Aviation; Supply chain; Steam reforming; Hydrogen production; Production (economics); Alternative fuels; Hydrogen","score_opus":0.007704980488657737,"score_gpt":0.18730990034044426,"score_spread":0.17960491985178653,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6907639279","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":[0.9856281,0.000009486095,0.007074314,0.0001686419,0.000040406198,0.0003075467,0.00006579207,0.000070748894,0.006634946],"genre_scores_gemma":[0.9957104,0.00005374505,0.0008077885,0.000012167322,0.000002758089,7.023769e-7,0.0000037563714,0.0000072110447,0.0034014704],"study_design_codex":"simulation_or_modeling","study_design_gemma":"qualitative","domain_scores_codex":[0.999358,0.000048405796,0.00009889054,0.0001981625,0.00016053468,0.00013599453],"domain_scores_gemma":[0.99961853,0.00007406044,0.000110792935,0.00012926351,0.0000074148024,0.000059923543],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000033961653,0.00009748094,0.00014065008,0.00009481323,0.00010821041,0.00000444819,0.00011407207,0.000046132864,0.00015688925],"category_scores_gemma":[0.000014019029,0.00009356719,0.000016913475,0.0004798747,0.00016576773,0.0003966158,0.0002085706,0.00006376921,5.674551e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":true,"about_ca_topic_consensus":true,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00021571433,0.0005152825,0.14361799,0.00008852272,0.00023163969,0.0036121325,0.012801432,0.6705395,0.0014997153,0.0006760363,0.16431253,0.0018894903],"study_design_scores_gemma":[0.018962162,0.0024651263,0.04376277,0.00033065485,0.0004597705,0.00025512552,0.6354214,0.2600878,0.0197513,0.01063499,0.005463865,0.002405056],"about_ca_topic_score_codex":0.031928275,"about_ca_topic_score_gemma":0.7603178,"teacher_disagreement_score":0.7283895,"about_ca_system_score_codex":0.00005528391,"about_ca_system_score_gemma":0.00005327826,"threshold_uncertainty_score":0.9745182},"labels":[],"label_agreement":null},{"id":"W6912696240","doi":"10.5281/zenodo.8412101","title":"Hydrogen-Enabled Airport Ecosystem Assessment","year":2023,"lang":"en","type":"article","venue":"Zenodo (CERN European Organization for Nuclear Research)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Software deployment; Aviation; International airport; Energy consumption; Consumption (sociology); Ecosystem","score_opus":0.028084918417780668,"score_gpt":0.24975546820917985,"score_spread":0.2216705497913992,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6912696240","genre_codex":"other","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":[0.3805402,0.00002488823,0.014956342,0.001888688,0.00018262262,0.0011156469,0.00016415687,0.010852288,0.59027517],"genre_scores_gemma":[0.995837,0.000054012242,0.0006047783,0.000063890446,0.000031174884,1.2208436e-7,0.00036101154,0.0006243366,0.0024236934],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.9985287,0.00011513042,0.00018841233,0.00039511066,0.000377897,0.0003947545],"domain_scores_gemma":[0.99932504,0.000015821259,0.00007174271,0.00043987675,0.00003879104,0.0001087505],"candidate_categories":["sts","insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.0005663281,0.000119019314,0.000115898765,0.00012346821,0.0014831512,0.00019857498,0.0008453748,0.00005850274,0.016794102],"category_scores_gemma":[0.0001688867,0.000117347794,0.00004121251,0.0009160282,0.00012507552,0.00025289285,0.0015844285,0.00018607065,0.046525043],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00003505081,0.00021971353,0.0003628168,0.00007086102,0.00006457444,0.00021236563,0.00057309325,0.0045645996,0.0804391,0.0077647762,0.59165794,0.31403515],"study_design_scores_gemma":[0.00024159059,0.00011009791,0.0024305917,0.000010361797,0.0000051240468,0.000051130388,0.0002732731,0.002358893,0.0019312119,0.0012471525,0.99117726,0.00016332389],"about_ca_topic_score_codex":0.000006749968,"about_ca_topic_score_gemma":5.5235694e-7,"teacher_disagreement_score":0.6152968,"about_ca_system_score_codex":0.0002620307,"about_ca_system_score_gemma":0.0000013768745,"threshold_uncertainty_score":0.9998168},"labels":[],"label_agreement":null},{"id":"W6923500374","doi":"10.14288/1.0169562","title":"The Atlin Claim","year":2011,"lang":"en","type":"article","venue":"Open Collections","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Publishing; George (robot); Subject (documents); Project commissioning; Privilege (computing)","score_opus":0.03336358064636911,"score_gpt":0.2446836482968526,"score_spread":0.2113200676504835,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6923500374","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0004157468,0.000010946215,0.0032137996,0.00019630794,0.00010042438,0.0002483636,0.0000014194037,0.00008657951,0.9957264],"genre_scores_gemma":[0.13320018,0.00008175729,0.013433331,0.00014996152,0.000011721171,0.00024571366,4.819795e-7,0.00001124783,0.8528656],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.9996086,0.000016035709,0.00006739577,0.000120023935,0.000058706402,0.000129249],"domain_scores_gemma":[0.99969494,0.00003651265,0.000022306624,0.00021975086,0.0000032505357,0.000023211613],"candidate_categories":["sts","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.000086661275,0.000046116926,0.000039545437,0.000005987399,0.002759471,0.00018587941,0.00046709186,0.000027815286,0.0034230608],"category_scores_gemma":[0.00003881436,0.000030454212,0.000018212288,0.00051789806,0.00017547353,0.0001435995,0.0003214799,0.00007648524,0.00031529652],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00002362407,0.00007795658,0.0015112229,2.472801e-7,0.000010725146,0.0000028718798,0.00014568846,0.000029700652,0.0003063071,0.0024028185,0.9678468,0.027642049],"study_design_scores_gemma":[0.00015213719,0.00007738094,0.0020395322,0.0000017191633,0.000005034256,0.000010253364,0.00043049577,0.0001497486,0.0033603774,0.11131029,0.8823549,0.000108093234],"about_ca_topic_score_codex":0.0036020419,"about_ca_topic_score_gemma":0.0044140248,"teacher_disagreement_score":0.14286081,"about_ca_system_score_codex":0.00005347661,"about_ca_system_score_gemma":0.0000069832467,"threshold_uncertainty_score":0.9985388},"labels":[],"label_agreement":null},{"id":"W6926524261","doi":"10.25446/oxford.16975951.v1","title":"Chartham Down Grave 46","year":2021,"lang":"en","type":"other","venue":"Figshare","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Quarter (Canadian coin); Natural (archaeology); Period (music); Feature (linguistics)","score_opus":0.024857629579026458,"score_gpt":0.23736040330585778,"score_spread":0.21250277372683132,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6926524261","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[4.6073723e-7,0.0009252728,0.00000892899,0.000045424513,0.000059284153,0.00019535715,0.06522973,0.0005776368,0.9329579],"genre_scores_gemma":[0.00016234891,0.00004418817,0.0007911678,0.00020197073,0.000104866434,0.0001719989,0.05967178,0.00021161637,0.93864006],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.99910426,0.0000109468065,0.000082699305,0.000391035,0.00017160046,0.00023945741],"domain_scores_gemma":[0.99940604,0.00001678099,0.00008590758,0.00043896414,0.0000026316895,0.000049655275],"candidate_categories":["insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.000008285718,0.00020665658,0.00018020497,0.000036672056,0.000033329237,0.000019824347,0.00033247485,0.00029407963,0.9682043],"category_scores_gemma":[0.00015393473,0.00018829167,0.000070835165,0.00016083437,0.000022560893,0.000025223648,0.00035937713,0.00020210653,0.03387046],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[2.859899e-7,0.000008905112,0.000013455376,0.000031915017,0.00000633998,0.00006208613,0.000004657784,0.0000023925686,0.000048255697,0.000010785668,0.9893723,0.010438623],"study_design_scores_gemma":[0.00005903574,0.000010725709,0.00012958783,0.0007920842,0.0000025106613,0.0000066364496,0.000007517363,0.0000070301558,0.00042778708,0.00021255123,0.9981004,0.00024415972],"about_ca_topic_score_codex":0.00001953019,"about_ca_topic_score_gemma":0.00009681794,"teacher_disagreement_score":0.93433386,"about_ca_system_score_codex":0.00004771193,"about_ca_system_score_gemma":0.000008298171,"threshold_uncertainty_score":0.9668818},"labels":[],"label_agreement":null},{"id":"W6948906283","doi":"10.5281/zenodo.11524119","title":"Highlights of the Airbus A220 from a Pilot's Perspective","year":2024,"lang":"en","type":"article","venue":"Zenodo (CERN European Organization for Nuclear Research)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Air Canada","funders":"","keywords":"Cockpit; Cruise; Aisle; Avionics; Airplane; Perspective (graphical); Climb; Crew; Aircraft industry","score_opus":0.023174637831209245,"score_gpt":0.23051924081095412,"score_spread":0.20734460297974489,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6948906283","genre_codex":"other","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":[0.16556707,0.0009856402,0.028441021,0.012675428,0.00057960907,0.001331657,0.00056574156,0.0049742586,0.78487957],"genre_scores_gemma":[0.99821585,0.00005465373,0.0003800354,0.00004502037,0.000031692434,2.771542e-8,0.00002949623,0.00030730705,0.00093591714],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.9990697,0.0000917919,0.000113259826,0.000297876,0.00025895494,0.00016839954],"domain_scores_gemma":[0.9995156,0.00002587375,0.000035603505,0.0003415027,0.00004033556,0.00004109762],"candidate_categories":["insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.00012918026,0.000084019186,0.00007465369,0.000048746562,0.00063023047,0.00014828816,0.0008205297,0.000032602846,0.012201129],"category_scores_gemma":[0.00021735142,0.00006126273,0.000040007642,0.00052663346,0.00037787293,0.00018517415,0.001163237,0.00017440325,0.005494469],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00014607696,0.0004367025,0.00005042745,0.000058832353,0.00015928877,0.00006837728,0.008516587,0.0006651586,0.27202463,0.18511403,0.31455317,0.21820673],"study_design_scores_gemma":[0.0001546311,0.0001755701,0.0018323691,0.000035691824,0.000012095208,0.000017601476,0.00068541215,0.00044760542,0.011073129,0.015439896,0.9700074,0.00011860643],"about_ca_topic_score_codex":0.00011227338,"about_ca_topic_score_gemma":0.0000015347224,"teacher_disagreement_score":0.83264875,"about_ca_system_score_codex":0.00021346686,"about_ca_system_score_gemma":0.000001301215,"threshold_uncertainty_score":0.99527985},"labels":[],"label_agreement":null},{"id":"W6950515791","doi":"10.5281/zenodo.8412100","title":"Hydrogen-Enabled Airport Ecosystem Assessment","year":2023,"lang":"en","type":"article","venue":"Zenodo (CERN European Organization for Nuclear Research)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Software deployment; Aviation; International airport; Energy consumption; Consumption (sociology); Ecosystem","score_opus":0.028084918417780668,"score_gpt":0.24975546820917985,"score_spread":0.2216705497913992,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6950515791","genre_codex":"other","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":[0.3805402,0.00002488823,0.014956342,0.001888688,0.00018262262,0.0011156469,0.00016415687,0.010852288,0.59027517],"genre_scores_gemma":[0.995837,0.000054012242,0.0006047783,0.000063890446,0.000031174884,1.2208436e-7,0.00036101154,0.0006243366,0.0024236934],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.9985287,0.00011513042,0.00018841233,0.00039511066,0.000377897,0.0003947545],"domain_scores_gemma":[0.99932504,0.000015821259,0.00007174271,0.00043987675,0.00003879104,0.0001087505],"candidate_categories":["sts","insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.0005663281,0.000119019314,0.000115898765,0.00012346821,0.0014831512,0.00019857498,0.0008453748,0.00005850274,0.016794102],"category_scores_gemma":[0.0001688867,0.000117347794,0.00004121251,0.0009160282,0.00012507552,0.00025289285,0.0015844285,0.00018607065,0.046525043],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00003505081,0.00021971353,0.0003628168,0.00007086102,0.00006457444,0.00021236563,0.00057309325,0.0045645996,0.0804391,0.0077647762,0.59165794,0.31403515],"study_design_scores_gemma":[0.00024159059,0.00011009791,0.0024305917,0.000010361797,0.0000051240468,0.000051130388,0.0002732731,0.002358893,0.0019312119,0.0012471525,0.99117726,0.00016332389],"about_ca_topic_score_codex":0.000006749968,"about_ca_topic_score_gemma":5.5235694e-7,"teacher_disagreement_score":0.6152968,"about_ca_system_score_codex":0.0002620307,"about_ca_system_score_gemma":0.0000013768745,"threshold_uncertainty_score":0.9998168},"labels":[],"label_agreement":null},{"id":"W6958374115","doi":"10.6084/m9.figshare.8867306.v1","title":"Additional file 2: of Prevalence of, and factors associated with health supplement use in Dubai, United Arab Emirates: a population-based cross-sectional study","year":2019,"lang":"en","type":"article","venue":"Figshare","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Table (database); Public health; Health information; MEDLINE; Population; Quarter (Canadian coin)","score_opus":0.04607434351991498,"score_gpt":0.27946255545273324,"score_spread":0.23338821193281825,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6958374115","genre_codex":"dataset","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":[0.4060336,0.0000013315685,4.5441598e-7,0.000002350779,0.0000017328844,0.00027641817,0.5936568,0.000018200908,0.000009147732],"genre_scores_gemma":[0.650318,6.8157355e-8,0.00012388018,0.000011947016,7.323856e-7,0.00011006828,0.34933084,0.000004403955,0.00010002442],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.99915576,0.00003725846,0.0002142304,0.00020893158,0.00025334093,0.0001304806],"domain_scores_gemma":[0.99873704,0.00087104674,0.00022027364,0.000120818775,0.000023620074,0.000027225971],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.000033145043,0.00009244884,0.00012337838,0.00007671487,0.00003931272,0.0000107737715,0.00009543543,0.000043978383,0.9023111],"category_scores_gemma":[0.0009204382,0.000077875986,0.000016457696,0.00033720123,0.000023785984,0.00017403938,0.00005276984,0.00008325019,0.000029635297],"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":[0.000011368836,0.00013873693,0.9386028,0.000034427798,0.00000530044,5.8581134e-7,0.000036605852,0.0020694663,0.0000036993208,5.4396264e-7,0.059063744,0.000032710614],"study_design_scores_gemma":[0.00037512986,0.0002922069,0.9971546,0.00048016378,8.3279315e-7,1.643282e-7,0.00006424301,0.00091145013,0.00003195654,0.0000113373535,0.00059656496,0.00008135012],"about_ca_topic_score_codex":0.00014410279,"about_ca_topic_score_gemma":0.0003148583,"teacher_disagreement_score":0.90228146,"about_ca_system_score_codex":0.0001329209,"about_ca_system_score_gemma":0.000036979836,"threshold_uncertainty_score":0.31756905},"labels":[],"label_agreement":null},{"id":"W6959606922","doi":"10.1021/es8013985.s001","title":"Particle and Gaseous Emissions from Commercial Aircraft at Each Stage of the Landing and Takeoff Cycle","year":2016,"lang":"en","type":"article","venue":"Figshare","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Range (aeronautics); Thrust; Airframe; Particle (ecology); Takeoff; Jet engine; Propulsion; Particle number","score_opus":0.025315771505728144,"score_gpt":0.23547810030273295,"score_spread":0.2101623287970048,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6959606922","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":[0.97681236,0.0001242212,0.000019277946,0.0005009082,0.00001176934,0.000111683665,0.021842469,0.00005586747,0.00052146247],"genre_scores_gemma":[0.99882495,0.0000085368665,0.000118309785,0.00005630733,0.000007130402,0.000014243064,0.00009525432,0.0000060376938,0.0008692073],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.9995355,0.000017520691,0.00007658988,0.00014852226,0.00009133746,0.00013054698],"domain_scores_gemma":[0.9995959,0.0001377242,0.000043728938,0.00017460388,0.000002488463,0.00004557883],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.000018307597,0.000065996726,0.00007275563,0.0000049395553,0.00013421646,0.0000070123333,0.00012166888,0.000043683285,0.031920865],"category_scores_gemma":[0.00025878465,0.000036026544,0.000016643307,0.000052250496,0.00006827396,0.00008539916,0.00045235423,0.000045089033,0.000117847376],"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":[0.000038942737,0.00006904799,0.56181055,0.000032096756,0.000015238801,0.000020000996,0.0005436963,0.000032305034,0.27895963,0.00004263057,0.059290707,0.09914514],"study_design_scores_gemma":[0.0007119516,0.000056029992,0.7511663,0.00045902064,0.000008399002,0.000006955142,0.00013425155,0.00035830736,0.16301541,0.0012393362,0.08261506,0.00022898604],"about_ca_topic_score_codex":0.000024856108,"about_ca_topic_score_gemma":0.00011385211,"teacher_disagreement_score":0.18935572,"about_ca_system_score_codex":0.000029433044,"about_ca_system_score_gemma":0.0000025419754,"threshold_uncertainty_score":0.9689641},"labels":[],"label_agreement":null},{"id":"W6976667098","doi":"10.6068/dp16e7a04e97856","title":"TREND: Federal Housing Finance Agency. House Price Index: House Price Index - All Transactions | Seasonally Adjusted: Non-Seasonally Adj, 1975/1 - 2019/2. Data Planet™ Statistical Datasets: A SAGE Publishing Resource Dataset-ID: 057-001-001","year":2019,"lang":"en","type":"other","venue":"Data Planet","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Underwriting; Index (typography); Mortgage insurance; Quarter (Canadian coin); Loan-to-value ratio; Loan; Mortgage underwriting; Real estate","score_opus":0.025114391429050614,"score_gpt":0.24937870139576715,"score_spread":0.22426430996671654,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6976667098","genre_codex":"dataset","genre_gemma":"dataset","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"dataset","genre_consensus":"dataset","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.000008944305,0.0008585374,0.009665922,0.00011573262,0.00035017828,0.0013897199,0.9808458,0.001606135,0.005159007],"genre_scores_gemma":[0.00035769484,0.001955823,0.0071367803,0.0011641395,0.0002816894,0.00004051316,0.9830282,0.00085480086,0.0051803687],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.99153346,0.00026177702,0.0009864421,0.0034646408,0.0018738405,0.0018798279],"domain_scores_gemma":[0.9899297,0.00071476086,0.0009655051,0.007868743,0.0000023263735,0.0005189872],"candidate_categories":["metaepi_narrow","scholarly_communication","open_science","research_integrity","insufficient_payload"],"consensus_categories":["metaepi_narrow","research_integrity","insufficient_payload"],"category_scores_codex":[0.00084497593,0.001393228,0.0011652962,0.0003375981,0.00045453163,0.0011370521,0.009140386,0.0013242032,0.009178803],"category_scores_gemma":[0.00012964837,0.0013745785,0.000018296932,0.00046372737,0.0007020599,0.004081923,0.0035875735,0.0027373359,0.0025029457],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":true,"about_ca_topic_consensus":true,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00020937897,0.00057161273,0.00024217741,0.00016635998,0.000249767,0.00089125667,0.000026453969,0.00075408677,0.00002156895,0.000009897185,0.9748864,0.021971043],"study_design_scores_gemma":[0.0018607782,0.00013868768,0.0012585934,0.00014295793,0.0002410606,0.00021586525,0.00007398902,0.0070794392,6.0422923e-7,0.000008193866,0.9873267,0.0016531362],"about_ca_topic_score_codex":0.03262775,"about_ca_topic_score_gemma":0.03474952,"teacher_disagreement_score":0.020317908,"about_ca_system_score_codex":0.00024683992,"about_ca_system_score_gemma":0.00021121382,"threshold_uncertainty_score":0.9999723},"labels":[],"label_agreement":null},{"id":"W6976892359","doi":"10.60692/86zhz-hbn68","title":"Las tres partes de la Silva de varios romances de Vicenç Beltran","year":2019,"lang":"es","type":"article","venue":"Greater South Information System","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Derogation; Context (archaeology); Period (music); Section (typography); Sequence (biology)","score_opus":0.010106842347598354,"score_gpt":0.20444325484932413,"score_spread":0.19433641250172579,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6976892359","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":[0.9611278,0.000026045303,0.019613013,0.000081451544,0.00014005523,0.0004326779,0.000074228956,0.00050040375,0.0180043],"genre_scores_gemma":[0.9973091,0.000007574468,0.0021464266,0.00016897368,0.000037652775,0.000059950533,0.0000053276235,0.000015942724,0.00024908353],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.99823815,0.00014846625,0.00048887957,0.00022109618,0.00030568786,0.0005976987],"domain_scores_gemma":[0.9990869,0.000057217203,0.00030291727,0.00041361348,0.000015982663,0.00012333559],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0005450307,0.00028120686,0.00028729741,0.00013216391,0.00019217252,0.0003478268,0.00043275705,0.00031328146,0.00015826368],"category_scores_gemma":[0.000033274966,0.00024168144,0.000094021205,0.00024163202,0.00019050537,0.0011697754,0.000106732325,0.00021439682,0.003264936],"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":[0.00003840027,0.0000061673063,0.9524356,0.00040747516,0.000036646066,0.000008577378,0.039196335,0.0034786933,0.00025209718,0.0011228011,0.00009055602,0.00292665],"study_design_scores_gemma":[0.0014280304,0.00020469644,0.91834676,0.00065956323,0.00007305473,0.00018350221,0.041362494,0.013799818,0.01764202,0.00017888591,0.005406363,0.0007147931],"about_ca_topic_score_codex":0.000071662886,"about_ca_topic_score_gemma":0.0000010661612,"teacher_disagreement_score":0.03618124,"about_ca_system_score_codex":0.0005349662,"about_ca_system_score_gemma":0.000053931046,"threshold_uncertainty_score":0.99751115},"labels":[],"label_agreement":null},{"id":"W6979719646","doi":"","title":"Acciones frente al clima y el \"desarrollo\"","year":2013,"lang":"es","type":"other","venue":"Repositorio Institucional UN - Biblioteca Digital","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Partenariat Canadien Contre Le Cancer; Henan Institute of Science and Technology; Ministerio de Economía y Competitividad","keywords":"Context (archaeology); Work (physics); Ven; Period (music)","score_opus":0.011769422843715318,"score_gpt":0.23974452713214825,"score_spread":0.22797510428843293,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6979719646","genre_codex":"other","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"other","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.031424146,0.0036024728,0.00704897,0.0024221824,0.007389042,0.0022460357,0.00092102546,0.0021531207,0.942793],"genre_scores_gemma":[0.7760101,0.0043603103,0.004310141,0.0004638314,0.00258898,0.0002638898,0.00038265556,0.00072964566,0.21089046],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.993669,0.000058169717,0.0011114272,0.001994859,0.0018513674,0.0013152],"domain_scores_gemma":[0.9969904,0.00017780435,0.0008214008,0.00142085,0.00008383362,0.00050574646],"candidate_categories":["metaepi_narrow","scholarly_communication","research_integrity","insufficient_payload"],"consensus_categories":["metaepi_narrow","insufficient_payload"],"category_scores_codex":[0.00015230101,0.0014157484,0.0010390924,0.0026618056,0.00064185297,0.0018720696,0.0018001233,0.0014371035,0.004201487],"category_scores_gemma":[0.00023896866,0.0012617169,0.0006139084,0.004102653,0.0011293672,0.0026503252,0.0014355225,0.0012893446,0.013431168],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00036170147,0.0028616078,0.066583216,0.00027770086,0.0013939831,0.001781017,0.00014472262,0.0008850862,0.02474879,0.029859778,0.6701967,0.20090568],"study_design_scores_gemma":[0.00097437866,0.00034954623,0.011850098,0.000466728,0.00008752003,0.00041963873,0.000069814094,0.00025079836,0.003685058,0.0021781581,0.9779785,0.0016897161],"about_ca_topic_score_codex":0.00015838117,"about_ca_topic_score_gemma":0.000011258817,"teacher_disagreement_score":0.74458593,"about_ca_system_score_codex":0.000579933,"about_ca_system_score_gemma":0.00014610193,"threshold_uncertainty_score":0.9998593},"labels":[],"label_agreement":null},{"id":"W6980423292","doi":"","title":"Canadian Solar Secures Massive 10-Year Power Deal for 300MW Spanish Solar Project","year":2024,"lang":"en","type":"other","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Power (physics); Solar power; Solar energy; Photovoltaic system; Government (linguistics)","score_opus":0.009877598597626394,"score_gpt":0.23844977966821437,"score_spread":0.22857218107058797,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6980423292","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.000009166139,0.00031060155,0.002999627,0.0005322548,0.000305702,0.0012988743,0.00043780907,0.00094160205,0.99316436],"genre_scores_gemma":[0.0015647158,0.00006737502,0.02856905,0.0002946976,0.0000900316,0.00017686977,0.00004440787,0.0004820428,0.9687108],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.9982189,0.000015394846,0.00016392404,0.0007133196,0.00022987863,0.00065856206],"domain_scores_gemma":[0.9993518,0.000021934124,0.000073564326,0.00040587282,0.000006199211,0.00014064956],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.000085746746,0.0003810182,0.00029050597,0.00022227498,0.000082447186,0.000077524266,0.00048669832,0.0005559585,0.030791052],"category_scores_gemma":[0.000042499785,0.00031372203,0.00013647825,0.00021293534,0.00019352815,0.000078860925,0.00018066721,0.00028654037,0.0057084854],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":true,"about_ca_topic_consensus":true,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000050039084,0.000010597113,0.00008290573,0.00003185612,0.000046052857,0.000050765095,0.000045102617,0.0000022166564,0.00007132842,0.0011220922,0.99620634,0.0023257204],"study_design_scores_gemma":[0.00013678493,0.00010994449,0.000017489672,0.000053294945,0.000029979701,0.0000048561833,0.00030636287,0.000027289901,0.00030373436,0.0055088364,0.99304885,0.0004525894],"about_ca_topic_score_codex":0.058481332,"about_ca_topic_score_gemma":0.30707732,"teacher_disagreement_score":0.248596,"about_ca_system_score_codex":0.00043585792,"about_ca_system_score_gemma":0.000119023665,"threshold_uncertainty_score":0.9999315},"labels":[],"label_agreement":null},{"id":"W6982740498","doi":"","title":"June 10: Prof Sylvain Charlebois, Bank of Canada Raises Interest Rate to 4.75%.","year":2023,"lang":"en","type":"other","venue":"Bulletin of Miscellaneous Information (Royal Gardens Kew)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Interest rate; Monetary policy; Public interest; National interest","score_opus":0.007794794663476059,"score_gpt":0.18414620475623397,"score_spread":0.17635141009275793,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6982740498","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.000099651596,0.000051654937,0.000002467307,0.00054370274,0.00026975022,0.0005712602,0.00018442434,0.00034678253,0.9979303],"genre_scores_gemma":[0.0019718078,0.00014322519,0.0006479559,0.00018327123,0.000031036838,0.000034268738,0.000031396525,0.00014382633,0.99681324],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.99843967,0.00004302576,0.0005561291,0.00024487046,0.00036475508,0.00035156196],"domain_scores_gemma":[0.99886066,0.00011843575,0.0004568283,0.0004201348,0.000031715645,0.00011223227],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.00019345609,0.00031455257,0.00042347334,0.00007466201,0.00004762096,0.0000143462,0.00051551807,0.00023548654,0.32901287],"category_scores_gemma":[0.00036297718,0.00029473484,0.00007897673,0.000029244395,0.00020274491,3.862424e-7,0.00027954785,0.00018403499,0.008701453],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":true,"about_ca_topic_consensus":true,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00003477346,0.000017633547,0.000006214938,0.00015617216,0.000026370606,0.000017163824,0.0000404657,0.00056325615,0.000008132369,0.000014024983,0.9965382,0.0025775873],"study_design_scores_gemma":[0.00020733564,0.0000991662,0.000033910866,0.00023902892,0.000014869906,0.000007780412,0.0001217843,0.000010759629,0.0002849257,0.000013815003,0.9986697,0.0002969227],"about_ca_topic_score_codex":0.19421262,"about_ca_topic_score_gemma":0.6137186,"teacher_disagreement_score":0.419506,"about_ca_system_score_codex":0.00016305565,"about_ca_system_score_gemma":0.000037702946,"threshold_uncertainty_score":0.99995047},"labels":[],"label_agreement":null},{"id":"W6992564995","doi":"","title":"Letter from the Government of Quebec, Canada","year":2012,"lang":"en","type":"other","venue":"VTechWorks (Virginia Tech)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Government (linguistics); Work (physics); Public policy; Legislation","score_opus":0.005176115784433824,"score_gpt":0.17768716754377978,"score_spread":0.17251105175934595,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6992564995","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.00057989784,0.0037731512,0.010794661,0.0071788514,0.0013945253,0.0012395772,0.00065404264,0.0010804554,0.9733048],"genre_scores_gemma":[0.08930142,0.000474633,0.007959583,0.0033840963,0.00058698904,0.000121802215,0.00004176519,0.00064943446,0.89748025],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.99793833,0.000036212372,0.00026724295,0.0004050366,0.00092141196,0.00043177625],"domain_scores_gemma":[0.99837047,0.000128064,0.00033565317,0.0011006502,0.00000240799,0.00006274334],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00009434646,0.00037497154,0.00035424493,0.000020780551,0.000061427876,0.000013085436,0.0010687652,0.00043363156,0.018501421],"category_scores_gemma":[0.000039163584,0.00025782533,0.000084152,0.00023143673,0.00039690748,0.000055965844,0.0005255433,0.00052778673,0.00018742273],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":true,"about_ca_topic_consensus":true,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000048409834,0.000024628202,0.001846683,0.000005084936,0.000031878826,0.000008140659,0.000013142269,0.000009772642,0.00049756415,0.00012313554,0.9537335,0.043701615],"study_design_scores_gemma":[0.00012156286,0.000007077978,0.0021688677,0.00010435879,0.000036280206,9.386137e-7,0.00004543103,0.0000057180127,0.0018765854,0.00036565049,0.99494755,0.00031998302],"about_ca_topic_score_codex":0.6302943,"about_ca_topic_score_gemma":0.8608365,"teacher_disagreement_score":0.23054218,"about_ca_system_score_codex":0.00049068884,"about_ca_system_score_gemma":0.000036718393,"threshold_uncertainty_score":0.9999874},"labels":[],"label_agreement":null},{"id":"W6995602193","doi":"","title":"Organisation et dynamiques de l’occupation du sol au nord-ouest de Cenabum-Orléans (Loiret) du ier s. av. n. è. au ve s. de n. è.","year":2024,"lang":"en","type":"article","venue":"DOAJ (DOAJ: Directory of Open Access Journals)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Human settlement; Quarter (Canadian coin); Rural settlement; Settlement (finance); Work (physics); Documentation","score_opus":0.08916242684532784,"score_gpt":0.4680605607698844,"score_spread":0.37889813392455657,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6995602193","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":[0.8988138,0.0009971252,0.093610235,0.00084868295,0.0003325396,0.0004202335,0.00003036463,0.00032788818,0.004619129],"genre_scores_gemma":[0.9912129,0.004282509,0.0034835357,0.00044369185,0.00015209947,0.00006354748,0.000018652407,0.000070028735,0.00027301387],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.99753696,0.00026720326,0.00054802594,0.00051089784,0.00050055014,0.00063633977],"domain_scores_gemma":[0.9987082,0.0003080289,0.0003263728,0.00038099688,0.000045785597,0.00023062756],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0015630159,0.00033762847,0.00038985978,0.00034464992,0.00037529622,0.0007943842,0.0015923473,0.00021694672,0.0039405385],"category_scores_gemma":[0.00048506472,0.00031147272,0.00013532456,0.0006441117,0.00031601498,0.003005565,0.0007392555,0.0005092585,0.00010348531],"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":[0.000058863767,0.00013841635,0.75426185,0.00006416218,0.000058457706,0.00008948565,0.002213681,0.0016641149,0.21176295,0.00024480114,0.010364985,0.019078264],"study_design_scores_gemma":[0.00026317223,0.000027869757,0.84169203,0.0003238821,0.0000751787,0.00007370504,0.00032658782,0.005316283,0.11763146,0.026185239,0.007580492,0.000504123],"about_ca_topic_score_codex":0.0051758992,"about_ca_topic_score_gemma":0.001961115,"teacher_disagreement_score":0.09413149,"about_ca_system_score_codex":0.0021066386,"about_ca_system_score_gemma":0.00039761685,"threshold_uncertainty_score":0.9999337},"labels":[],"label_agreement":null},{"id":"W6995931973","doi":"","title":"Pratt &amp;amp; Whitney Canada Expands Carbon Offset Service to Include Helicopter Engines","year":2021,"lang":"en","type":"other","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Service (business); Offset (computer science); Carbon offset","score_opus":0.015725666411633556,"score_gpt":0.23844442742037472,"score_spread":0.22271876100874116,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6995931973","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.004277967,0.00049636344,0.002214008,0.0034685652,0.0005626875,0.0005667745,0.000078351804,0.0007308618,0.98760444],"genre_scores_gemma":[0.0065744817,0.000101856254,0.018167516,0.0042619407,0.00012572588,0.0001024005,0.00015423703,0.00025521888,0.9702566],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.99827325,0.000024685867,0.00020516095,0.0006254517,0.00043666328,0.00043476172],"domain_scores_gemma":[0.9989122,0.000028468261,0.00008248999,0.0008044103,0.000011605173,0.00016080226],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.000050001854,0.0003954522,0.00035275196,0.00008382816,0.000051523868,0.000026457285,0.00053166156,0.00029733937,0.022742834],"category_scores_gemma":[0.000047834255,0.00034114206,0.000038515827,0.00051403174,0.00004786717,0.000034136385,0.0006755873,0.00023404812,0.00043077522],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":true,"about_ca_topic_consensus":true,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000004016868,0.000029232897,0.002074525,0.00004866437,0.00002868538,0.00002345074,0.00006962402,0.00019900504,0.0034120395,0.00002170696,0.99110353,0.0029855086],"study_design_scores_gemma":[0.000107902095,0.0000085612155,0.00026541416,0.00008198646,0.000009982243,0.00000744098,0.00006687002,0.000016729615,0.0011877468,0.000050654315,0.9977188,0.00047791423],"about_ca_topic_score_codex":0.6645579,"about_ca_topic_score_gemma":0.98979884,"teacher_disagreement_score":0.325241,"about_ca_system_score_codex":0.00039505365,"about_ca_system_score_gemma":0.00009846914,"threshold_uncertainty_score":0.99990404},"labels":[],"label_agreement":null},{"id":"W7000738101","doi":"","title":"Green house gas (GHG) reduction study for the rotorcraft industry","year":2020,"lang":"en","type":"article","venue":"NPARC","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"Safran Electronics (Canada); National Research Council Canada; Bell Helicopter Textron (Canada)","funders":"Office National d'études et de Recherches Aérospatiales","keywords":"Fuel efficiency; Aviation; Software deployment; Aerospace; Civil aviation; Propulsion; Greenhouse gas; Aircraft fuel system","score_opus":0.03347062003780704,"score_gpt":0.25645740030690245,"score_spread":0.2229867802690954,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7000738101","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":[0.95304847,0.000023281262,0.014453791,0.0255949,0.00017514512,0.0025706582,0.0000075166454,0.0009963346,0.0031299244],"genre_scores_gemma":[0.99655044,0.000005907569,0.002374569,0.00028331502,0.00009481505,0.00019984064,3.9860305e-7,0.000017894445,0.00047284152],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.99930614,0.00001861015,0.0001038328,0.00023978537,0.00015989374,0.00017174755],"domain_scores_gemma":[0.99964285,0.000041696727,0.000039197406,0.00022453627,0.0000041628055,0.00004753097],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00009265272,0.00009175631,0.0000815792,0.000008596301,0.00016393159,0.00001559961,0.00030509662,0.000087690074,0.00041906018],"category_scores_gemma":[0.00007422369,0.000062965424,0.00003348706,0.00017994965,0.00013491377,0.000119412114,0.00014087395,0.00024716643,0.00013232713],"study_design_candidate":"not_applicable","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":[0.0002637295,0.00049762434,0.061422616,0.000018809109,0.00009016461,0.000024861354,0.0049850685,0.0022570505,0.30790925,0.00057584007,0.0773634,0.5445916],"study_design_scores_gemma":[0.007509719,0.0071295784,0.10464902,0.000038206425,0.00038466143,0.00007088717,0.045843445,0.022419024,0.19580951,0.1378154,0.47591183,0.0024187278],"about_ca_topic_score_codex":0.000033794593,"about_ca_topic_score_gemma":0.00000945366,"teacher_disagreement_score":0.54217285,"about_ca_system_score_codex":0.00004237343,"about_ca_system_score_gemma":0.0000046899168,"threshold_uncertainty_score":0.4588415},"labels":[],"label_agreement":null},{"id":"W7008499874","doi":"","title":"Canada Carbon Adds Dr. Roger Roberts, Former SVP and CTO at the Boeing Company and Vice Admiral Richard H. Truly, Former Director of NASA and NREL to the Company's Advisory Board","year":2014,"lang":"en","type":"other","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Advisory committee; On board; Vice president; Aircraft industry; Carbon fibers","score_opus":0.007823330541457583,"score_gpt":0.2055595457958444,"score_spread":0.1977362152543868,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7008499874","genre_codex":"other","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":[0.38596398,0.0148945395,0.0014979909,0.010131674,0.0007801509,0.0046599465,0.0004337626,0.00064830465,0.58098966],"genre_scores_gemma":[0.7587396,0.0008766713,0.0013586072,0.0023090702,0.00008518799,0.000115122035,0.0000145252525,0.0002490653,0.23625214],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.99823874,0.000059728278,0.00028246062,0.00055028865,0.00040074342,0.00046800895],"domain_scores_gemma":[0.9989443,0.00019603348,0.00019500921,0.0005046544,0.000008949813,0.00015109181],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016691517,0.00043376588,0.00052201306,0.000061622355,0.00021355547,0.000033513625,0.0003653988,0.00019553438,0.00073027937],"category_scores_gemma":[0.00003762908,0.00024351041,0.00004540942,0.00016382617,0.000581386,0.000059649028,0.0006619623,0.0002539176,0.000011262869],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":true,"about_ca_topic_consensus":true,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00013564735,0.000055037443,0.07085662,0.00020351355,0.00023751045,0.00001210101,0.0006236874,0.00007213563,0.0036327024,0.0003061138,0.87032807,0.05353684],"study_design_scores_gemma":[0.00040388756,0.00008824487,0.02164999,0.000096722026,0.00006538089,0.000018215638,0.00029928295,0.00040231086,0.0007797273,0.00008506161,0.9756251,0.00048610152],"about_ca_topic_score_codex":0.32384568,"about_ca_topic_score_gemma":0.8170684,"teacher_disagreement_score":0.4932227,"about_ca_system_score_codex":0.00015870274,"about_ca_system_score_gemma":0.000033308814,"threshold_uncertainty_score":0.99300665},"labels":[],"label_agreement":null},{"id":"W7011107766","doi":"","title":"L’intégration en emploi des personnes ayant un trouble du spectre de l’autisme : évaluation d’un programme de soutien à l’emploi et exploration des facteurs soutenant l’intégration en entreprise","year":2020,"lang":"fr","type":"dissertation","venue":"Papyrus : Institutional Repository (Université de Montréal)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Population; Context (archaeology); Research methodology; Social environment","score_opus":0.012757528033164345,"score_gpt":0.19198086139994566,"score_spread":0.1792233333667813,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7011107766","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":[0.8863175,0.0015717063,0.10644243,0.0025277932,0.00032526258,0.0011888678,0.00006569706,0.00056131626,0.0009994212],"genre_scores_gemma":[0.95570505,0.0032948223,0.0380449,0.00008738153,0.00015326774,0.00021109266,0.0009097127,0.000075511474,0.0015182464],"study_design_codex":"qualitative","study_design_gemma":"observational","domain_scores_codex":[0.99517643,0.00076050084,0.0007118314,0.001213216,0.0010230307,0.001114997],"domain_scores_gemma":[0.9979194,0.00025461207,0.00068955304,0.00044468668,0.00019382244,0.00049796497],"candidate_categories":["metaepi_narrow","sts"],"consensus_categories":[],"category_scores_codex":[0.0007760954,0.0008284276,0.0005564048,0.00032451024,0.007016415,0.00025796524,0.0006478676,0.00079500355,0.00019115473],"category_scores_gemma":[0.0006143615,0.0008969114,0.00040379446,0.00072201464,0.00080379593,0.002330223,0.0002673358,0.00075384916,0.00015458096],"study_design_candidate":"observational","study_design_consensus":null,"about_ca_topic_candidate":true,"about_ca_topic_consensus":false,"about_ca_system_candidate":true,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0010951234,0.0009042026,0.14122632,0.00022445587,0.0003895948,0.001122616,0.3987362,0.036908783,0.28554526,0.019664558,0.00008731047,0.114095554],"study_design_scores_gemma":[0.002498085,0.0007744415,0.5368022,0.000383404,0.00076768186,0.0007641453,0.20751859,0.04214771,0.18075946,0.023821836,0.0022635506,0.001498895],"about_ca_topic_score_codex":0.022721173,"about_ca_topic_score_gemma":0.015090835,"teacher_disagreement_score":0.39557588,"about_ca_system_score_codex":0.012316173,"about_ca_system_score_gemma":0.0010317843,"threshold_uncertainty_score":0.99934816},"labels":[],"label_agreement":null},{"id":"W7011279407","doi":"","title":"Living with Strangers: The Nineteenth-Century Sioux and the Canadian-American Borderlands. By David G. McCrady","year":2006,"lang":"en","type":"article","venue":"eScholarship (California Digital Library)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Perspective (graphical); Indigenous; Ethnography; Identity (music)","score_opus":0.0039012326658594333,"score_gpt":0.17126196959687706,"score_spread":0.16736073693101763,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7011279407","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":[0.8909624,0.0028064656,0.0005549388,0.012335646,0.000064916705,0.0011278003,0.0015729584,0.0007716888,0.08980319],"genre_scores_gemma":[0.997884,0.00010472896,0.00046658117,0.00084285985,0.000027797274,0.000034135377,0.00007605157,0.000043294745,0.0005205523],"study_design_codex":"observational","study_design_gemma":"not_applicable","domain_scores_codex":[0.99845046,0.000067796864,0.00021334364,0.0003949392,0.0003365993,0.0005368733],"domain_scores_gemma":[0.999042,0.0002882851,0.00010907547,0.00039265634,0.0000046523805,0.00016333774],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00014851276,0.0002730304,0.00020001511,0.00004266458,0.0005145582,0.00093143026,0.0005836675,0.00007329534,0.00026192097],"category_scores_gemma":[0.00006844176,0.00014299765,0.00005545735,0.00049450266,0.0016383431,0.0012458588,0.00022084887,0.00042958415,0.00021120126],"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":[0.00009599892,0.00008167793,0.93742967,0.000009442415,0.000038826653,0.00003501092,0.0000727919,0.00007194791,0.00013049434,0.0019327607,0.014650837,0.045450572],"study_design_scores_gemma":[0.0012506364,0.00020886934,0.1262912,0.000068849426,0.00004125135,0.000049330625,0.0005096304,0.00021288694,0.00038373083,0.0103503615,0.85982174,0.00081154006],"about_ca_topic_score_codex":0.0059601916,"about_ca_topic_score_gemma":0.0059462283,"teacher_disagreement_score":0.84517086,"about_ca_system_score_codex":0.000064539396,"about_ca_system_score_gemma":0.00003442474,"threshold_uncertainty_score":0.9010067},"labels":[],"label_agreement":null},{"id":"W7011369152","doi":"","title":"Measurement of the cross section for the production of a W boson in association with b-jets in pp collisions at root s=7 TeV with the ATLAS detector","year":2012,"lang":"en","type":"article","venue":"Lancaster EPrints (Lancaster University)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Fundação para a Ciência e a Tecnologia; Institut National de Physique Nucléaire et de Physique des Particules; Agencia Nacional de Promoción Científica y Tecnológica; Science and Technology Facilities Council; Natural Sciences and Engineering Research Council of Canada; H. Lundbeck A/S; State Atomic Energy Corporation ROSATOM; Centre National pour la Recherche Scientifique et Technique; Centre National de la Recherche Scientifique; Max-Planck-Gesellschaft; Israel Science Foundation; Lundbeckfonden; Leverhulme Trust; General Secretariat for Research and Technology; Ministry of Education, Culture, Sports, Science and Technology; Nederlandse Organisatie voor Wetenschappelijk Onderzoek; Bundesministerium für Bildung und Forschung; Joint Institute for Nuclear Research; National Science Council; Japan Society for the Promotion of Science; Conselho Nacional de Desenvolvimento Científico e Tecnológico; U.S. Department of Energy; National Natural Science Foundation of China; Fundação de Amparo à Pesquisa do Estado de São Paulo; Bundesministerium für Wissenschaft und Forschung; Javna Agencija za Raziskovalno Dejavnost RS; Schweizerischer Nationalfonds zur Förderung der Wissenschaftlichen Forschung; Ministerstwo Edukacji i Nauki; CERN; Deutsche Forschungsgemeinschaft; Services Fédéraux des Affaires Scientifiques, Techniques et Culturelles; Department of Science and Technology, Ministry of Science and Technology, India; Ministerio de Ciencia e Innovación; European Commission; Comisión Nacional de Investigación Científica y Tecnológica; Danmarks Grundforskningsfond; TRIUMF; Alexander von Humboldt-Stiftung; Türkiye Atom Enerjisi Kurumu; National Science Foundation","keywords":"Lepton; Muon; Cross section (physics); Atlas detector; Atlas (anatomy); Boson; Large Hadron Collider; Quantum chromodynamics; Detector; ATLAS experiment","score_opus":0.018489262784219463,"score_gpt":0.20728281345722532,"score_spread":0.18879355067300585,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7011369152","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":[0.99663067,0.000018316303,0.0015902121,0.0005132233,0.00009369046,0.0007041116,0.0000037174118,0.000010970736,0.00043507206],"genre_scores_gemma":[0.99874914,0.0000053783083,0.00014666258,0.000008937906,0.00002333712,0.000011622149,3.6685603e-7,0.0000074859354,0.0010470541],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.99907374,0.00007589637,0.00011858493,0.00018507557,0.00032114136,0.00022558002],"domain_scores_gemma":[0.99935603,0.00007610855,0.0002053184,0.00030883838,0.000036416677,0.000017261147],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003878323,0.00010314584,0.0001229555,0.00005677681,0.00012402053,0.0000075761054,0.00024883045,0.00006273502,0.00002202466],"category_scores_gemma":[0.00006236878,0.00005223138,0.00003457531,0.0006483941,0.00015821036,0.00023759365,0.00017389552,0.00014101042,0.0000058851715],"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":[0.00029441397,0.00006686144,0.98823875,0.00001195521,0.000016983695,5.817767e-7,0.0005358621,0.0002812263,0.009823955,0.000026555866,0.00003292861,0.00066994474],"study_design_scores_gemma":[0.00057151855,0.000070003895,0.94210285,0.000061428706,0.000017871955,0.0000036399442,0.0005174437,0.000079130965,0.052723937,0.000012610321,0.003768729,0.00007085554],"about_ca_topic_score_codex":0.00012041868,"about_ca_topic_score_gemma":0.0056266263,"teacher_disagreement_score":0.046135902,"about_ca_system_score_codex":0.0007586715,"about_ca_system_score_gemma":0.000015475222,"threshold_uncertainty_score":0.31397894},"labels":[],"label_agreement":null},{"id":"W7017055929","doi":"","title":"Advanced BioFuels USA – New Order for Alfa Laval to Unlock Potential of Biofuels in Aviation","year":2024,"lang":"en","type":"other","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Biofuel; Aviation; Aviation biofuel; Order (exchange); Renewable energy","score_opus":0.009964582640016572,"score_gpt":0.2576397469719589,"score_spread":0.24767516433194234,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7017055929","genre_codex":"methods","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"other","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0018760704,0.0011701196,0.5724781,0.0017511913,0.0016313146,0.004293218,0.00022339028,0.0011197139,0.41545683],"genre_scores_gemma":[0.00752275,0.00015755497,0.12021549,0.00014420324,0.00006626653,0.00007650061,0.000020347281,0.0002198035,0.8715771],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.99866235,0.000010188223,0.0002740155,0.00053410657,0.00021558095,0.0003037466],"domain_scores_gemma":[0.99949074,0.000018210289,0.00010616255,0.00031193648,0.000006184255,0.00006677134],"candidate_categories":["insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.0000616141,0.00025928137,0.00031271423,0.00026056287,0.0000131843435,0.000013887649,0.0003139308,0.00031290643,0.004519128],"category_scores_gemma":[0.00005910531,0.0002208524,0.00007827635,0.00057583203,0.00008695914,0.00007993725,0.00019473778,0.00012559228,0.0011794158],"study_design_candidate":"not_applicable","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":[0.00010425316,0.00017201406,0.00092221034,0.00027410893,0.00006413376,0.00002041961,0.00013612263,0.0013874047,0.09106507,0.0018733885,0.40105128,0.50292957],"study_design_scores_gemma":[0.001136869,0.00039753228,0.00034353219,0.00029377866,0.00004898592,0.0000037180805,0.0001549076,0.00019437396,0.024518488,0.10552709,0.86649734,0.0008833945],"about_ca_topic_score_codex":0.00082809885,"about_ca_topic_score_gemma":0.0018931363,"teacher_disagreement_score":0.50204617,"about_ca_system_score_codex":0.00009558388,"about_ca_system_score_gemma":0.000023762652,"threshold_uncertainty_score":0.99959826},"labels":[],"label_agreement":null},{"id":"W7018871301","doi":"","title":"Electrification of Airport Operations:&#13;\\nElectric Powered Tow-Truck Utilization&#13;\\nin Taxiing Operations","year":2019,"lang":"en","type":"dissertation","venue":"Spectrum Research Repository (Concordia University)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Aviation; Fuel efficiency; Electrification; Civil aviation; Airplane; Greenhouse gas; Runway; Consumption (sociology)","score_opus":0.02991956285942992,"score_gpt":0.28120034322421544,"score_spread":0.2512807803647855,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7018871301","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":[0.90891415,0.00030149246,0.002511409,0.00021536605,0.0004870092,0.0016878244,0.000027895123,0.0002764775,0.08557837],"genre_scores_gemma":[0.91167915,0.00059253105,0.00023083533,0.0000069032258,0.00005915807,0.000021393504,0.00049237325,0.00005950756,0.08685816],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9961014,0.00038757376,0.00057642587,0.00107078,0.0010818044,0.00078203593],"domain_scores_gemma":[0.998147,0.00015625685,0.0002414695,0.0010358306,0.00024077555,0.00017866826],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00047737724,0.0004093649,0.00051733205,0.0012647581,0.0010235901,0.00013293076,0.0012115128,0.00058361725,0.00056374643],"category_scores_gemma":[0.00025404614,0.0004671714,0.00018517922,0.0028724987,0.0003981454,0.00084526354,0.00014696068,0.001150137,0.00027423946],"study_design_candidate":"bench_or_experimental","study_design_consensus":"bench_or_experimental","about_ca_topic_candidate":true,"about_ca_topic_consensus":true,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0008306931,0.00075586693,0.12475586,0.0002796942,0.00035806932,0.00028074358,0.0013659842,0.014239568,0.82884794,0.013556496,0.0035415594,0.011187541],"study_design_scores_gemma":[0.0015522714,0.0013375212,0.2508498,0.00021452628,0.00019273502,0.000044531134,0.005404313,0.008281814,0.71360314,0.001512443,0.015426572,0.0015803188],"about_ca_topic_score_codex":0.016696423,"about_ca_topic_score_gemma":0.03382622,"teacher_disagreement_score":0.12609395,"about_ca_system_score_codex":0.001332565,"about_ca_system_score_gemma":0.000778705,"threshold_uncertainty_score":0.999778},"labels":[],"label_agreement":null},{"id":"W7019121994","doi":"","title":"Estudo paramétrico de um motor turbohélice PW150A","year":2015,"lang":"pt","type":"dissertation","venue":"UBibliorum repositorio digital da ubi (University of Beira Interior)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Power consumption; Propulsive efficiency; Power (physics); Turbine","score_opus":0.01443033113422771,"score_gpt":0.23625689650048412,"score_spread":0.22182656536625642,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7019121994","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":[0.9729638,0.00063251855,0.0023500044,0.0002185154,0.00199474,0.0009052238,0.00043600224,0.0004829585,0.020016233],"genre_scores_gemma":[0.9677087,0.00024048467,0.0018034423,0.000028318107,0.00010888512,0.0000046928826,0.00030335737,0.00009328454,0.029708805],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9953186,0.000096538344,0.00072891114,0.0014211495,0.0012941917,0.0011406254],"domain_scores_gemma":[0.9965194,0.00015443559,0.0011990522,0.0012682077,0.00026945083,0.00058949407],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00028572584,0.00094239635,0.0011579909,0.0021249156,0.0005723054,0.0008037894,0.002436109,0.001104748,0.00031496526],"category_scores_gemma":[0.00026630308,0.00115678,0.00064838916,0.0039592898,0.00092335633,0.0028809477,0.0012507281,0.0010017738,0.00075615436],"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":[0.005228846,0.003556892,0.24276695,0.0015551572,0.0021425625,0.0042820615,0.02397262,0.0006292881,0.27579582,0.0009976777,0.07490979,0.36416236],"study_design_scores_gemma":[0.010054455,0.012950132,0.27553052,0.005422268,0.0026872896,0.00092261354,0.21757904,0.0055863834,0.035933264,0.0071199597,0.41387782,0.012336278],"about_ca_topic_score_codex":0.0017851597,"about_ca_topic_score_gemma":0.00014801021,"teacher_disagreement_score":0.35182607,"about_ca_system_score_codex":0.0013832429,"about_ca_system_score_gemma":0.00027808693,"threshold_uncertainty_score":0.9990882},"labels":[],"label_agreement":null},{"id":"W7019312550","doi":"","title":"Historical and future trends in aircraft performance, cost, and emissions","year":2001,"lang":"en","type":"article","venue":"DSpace@MIT (Massachusetts Institute of Technology)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":10,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Glenn Research Center; Canadian Institute for Theoretical Astrophysics; H2020 European Research Council; Ames Research Center; National Aeronautics and Space Administration","keywords":"Work (physics); Climate change; Air pollution; Government (linguistics)","score_opus":0.012736051455123536,"score_gpt":0.235004440194344,"score_spread":0.22226838873922045,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7019312550","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":[0.9703201,0.0015316707,0.00054096355,0.017971097,0.0002561587,0.0002704668,0.000007457168,0.00052086945,0.008581182],"genre_scores_gemma":[0.9805475,0.002944691,0.014377312,0.00006371666,0.0000312227,0.00005272896,0.0000032374662,0.000020174986,0.001959431],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.99848926,0.000011561651,0.00031823674,0.0005216529,0.00021106355,0.00044823607],"domain_scores_gemma":[0.99928343,0.000014137681,0.00012572232,0.00046349608,0.000010366529,0.0001028604],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00011696919,0.0002731241,0.00038684456,0.00069133966,0.00016303404,0.000010431998,0.0003585739,0.00050299295,0.000101660225],"category_scores_gemma":[0.000062121115,0.00024205651,0.000041892737,0.0014997724,0.00094566843,0.0004423967,0.0004093039,0.0005136489,0.000011316357],"study_design_candidate":"not_applicable","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":[0.000026043048,0.000093598894,0.43997538,0.000011489802,0.000010769484,0.00006452323,0.00006303586,0.00004675914,0.0027485855,0.0008145673,0.0028572662,0.553288],"study_design_scores_gemma":[0.00075347984,0.00016923992,0.10993671,0.000038328086,0.000016804066,0.00012210342,0.0001031419,0.00023948755,0.0012441819,0.0010904404,0.88596946,0.00031659915],"about_ca_topic_score_codex":0.000040809664,"about_ca_topic_score_gemma":0.00014821759,"teacher_disagreement_score":0.88311225,"about_ca_system_score_codex":0.00034617042,"about_ca_system_score_gemma":0.000012458971,"threshold_uncertainty_score":0.98707783},"labels":[],"label_agreement":null},{"id":"W7022042448","doi":"","title":"Erik R. Lindbergh","year":2021,"lang":"en","type":"article","venue":"Scholarly Commons (Embry–Riddle Aeronautical University)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Thriving; Craft; Plan (archaeology); Siege; Plank; Wife; Carving; German; Cruise","score_opus":0.01815695076446903,"score_gpt":0.20403296811518493,"score_spread":0.1858760173507159,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7022042448","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":[0.5528086,0.00038509248,0.024907598,0.0061236843,0.0003834743,0.0003500893,0.00004601219,0.0011646355,0.41383082],"genre_scores_gemma":[0.9633181,0.000080807,0.012834021,0.00045002502,0.000027149244,0.0000015941083,0.000019535122,0.000027578477,0.023241209],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"not_applicable","domain_scores_codex":[0.9979841,0.00015496238,0.00019950114,0.000649936,0.00041821002,0.00059328723],"domain_scores_gemma":[0.99861366,0.0001792372,0.000063504755,0.00080522284,0.000046891793,0.0002915],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.000158789,0.00025959322,0.00027698238,0.000110892244,0.00049532723,0.00016353924,0.00082580635,0.00027135847,0.002046739],"category_scores_gemma":[0.00031983032,0.00028397434,0.00015370417,0.0013298563,0.0006171405,0.0017576715,0.0013027249,0.0009007551,0.0016217222],"study_design_candidate":"not_applicable","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":[0.00043858457,0.0025918975,0.14882568,0.00005202026,0.0003368321,0.010742828,0.0004087137,0.0013577888,0.090219304,0.48148498,0.018899351,0.24464202],"study_design_scores_gemma":[0.0015564164,0.0002405243,0.048293866,0.0000427149,0.00010252274,0.00011772717,0.0008696605,0.00033017955,0.018628124,0.015501452,0.91340363,0.00091317476],"about_ca_topic_score_codex":0.000048054662,"about_ca_topic_score_gemma":0.00026530473,"teacher_disagreement_score":0.8945043,"about_ca_system_score_codex":0.0003758552,"about_ca_system_score_gemma":0.000065861685,"threshold_uncertainty_score":0.99996126},"labels":[],"label_agreement":null},{"id":"W7023677098","doi":"","title":"Operation Green Skies","year":2023,"lang":"en","type":"article","venue":"Scholarly Commons (Embry–Riddle Aeronautical University)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Aviation; Greenhouse gas; Global warming; Climate change; Commercial aviation; Greenhouse effect; Atmosphere (unit); Carbon neutrality","score_opus":0.023964804832856602,"score_gpt":0.21706687876655667,"score_spread":0.19310207393370007,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7023677098","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":[0.8252992,0.000058212743,0.0115600815,0.007973291,0.00026364689,0.0005591675,0.00004553853,0.0027004797,0.1515404],"genre_scores_gemma":[0.97696114,0.000042993048,0.0023264685,0.00018646599,0.000022472523,0.0000027039478,0.000028781249,0.000022136725,0.020406863],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"not_applicable","domain_scores_codex":[0.9983647,0.000110819936,0.00016366999,0.0004757084,0.00037982166,0.00050527445],"domain_scores_gemma":[0.999088,0.00014647987,0.000046138943,0.0005170284,0.000021387777,0.00018097428],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00022668221,0.0002100743,0.00019990336,0.00023316724,0.0005899293,0.00013977621,0.0007900372,0.00019602265,0.00060131686],"category_scores_gemma":[0.000149048,0.00021633424,0.000092019596,0.0015497019,0.0005367309,0.0022719468,0.0009646884,0.0005455811,0.0048818463],"study_design_candidate":"not_applicable","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":[0.00043031963,0.0009194235,0.15506534,0.00006023611,0.00023090585,0.0025300407,0.0010207582,0.0058324123,0.06811171,0.50717556,0.031207535,0.22741574],"study_design_scores_gemma":[0.002434452,0.0006434088,0.20787181,0.00005415662,0.0001222416,0.000041604275,0.0023185585,0.005813625,0.0077996603,0.034526758,0.7368688,0.0015049262],"about_ca_topic_score_codex":0.0001821911,"about_ca_topic_score_gemma":0.00034861648,"teacher_disagreement_score":0.70566124,"about_ca_system_score_codex":0.00027776507,"about_ca_system_score_gemma":0.000024110703,"threshold_uncertainty_score":0.99589294},"labels":[],"label_agreement":null},{"id":"W7027200611","doi":"","title":"Code One, Volume 17, Number 1, First Quarter 2002","year":2002,"lang":"en","type":"other","venue":"The Portal to Texas History (University of North Texas)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Code (set theory); Volume (thermodynamics); Quarter (Canadian coin); Measure (data warehouse)","score_opus":0.014430917222466798,"score_gpt":0.18165008999063925,"score_spread":0.16721917276817244,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7027200611","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0015513995,0.00025149668,0.0016872224,0.00057208457,0.00022946367,0.0005312665,0.00016281613,0.00049769244,0.99451655],"genre_scores_gemma":[0.010043189,0.00016778478,0.0023602068,0.00019603389,0.000045397726,9.295104e-7,0.00001875367,0.00013868696,0.987029],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.9982803,0.00003795779,0.00018269006,0.0005919241,0.00048106987,0.00042609178],"domain_scores_gemma":[0.9984664,0.000026727334,0.0003562755,0.0009802057,0.00001234505,0.00015804979],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.00007934416,0.0003685678,0.00045709047,0.00013922033,0.00016592475,0.000005057922,0.001317398,0.0002667602,0.23201138],"category_scores_gemma":[0.000013348959,0.00037864345,0.00019321458,0.00028115633,0.0010494407,0.00014357195,0.00040933423,0.0003736603,0.025666464],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":true,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000013916485,0.0001130802,0.04165397,0.00001828004,0.000044573695,0.00007915508,0.00013162642,0.00008873458,0.0000010470471,0.00003240246,0.9561817,0.0016414841],"study_design_scores_gemma":[0.00020030422,0.000059384518,0.096039146,0.00004222072,0.000075900825,0.00000870565,0.000032762407,0.00003810121,6.794223e-7,0.000025404855,0.9030583,0.00041910337],"about_ca_topic_score_codex":0.0019838396,"about_ca_topic_score_gemma":0.02651425,"teacher_disagreement_score":0.20634492,"about_ca_system_score_codex":0.00049821875,"about_ca_system_score_gemma":0.000020070764,"threshold_uncertainty_score":0.99986655},"labels":[],"label_agreement":null},{"id":"W7028621966","doi":"","title":"FLYING WHALES QUÉBEC chooses Pratt &amp;amp; Whitney Canada to develop a propulsion system for electric aircraft","year":2022,"lang":"en","type":"other","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Propulsion; Electrically powered spacecraft propulsion; Airframe; Weapon system","score_opus":0.015879093974161033,"score_gpt":0.23257734112884926,"score_spread":0.21669824715468822,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7028621966","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0036591215,0.00323704,0.25293124,0.0054114973,0.0019939619,0.014562805,0.00044026363,0.0081323935,0.7096317],"genre_scores_gemma":[0.008904776,0.000046814308,0.0747064,0.0005558608,0.00008440823,0.0016747055,0.000100750236,0.00046055453,0.91346574],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.99760765,0.000046388745,0.00033438686,0.0008226513,0.0005460362,0.00064291665],"domain_scores_gemma":[0.9989305,0.00009202012,0.0002043008,0.00060677476,0.000018436616,0.00014795008],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00014480522,0.0004552917,0.00044480152,0.00019800206,0.00043445497,0.000037728223,0.00073768245,0.0002058473,0.007207499],"category_scores_gemma":[0.00034174786,0.00038343068,0.000057231155,0.0010254412,0.000048635993,0.000076726305,0.00047551855,0.0002642109,0.00043179037],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":true,"about_ca_topic_consensus":true,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000015214371,0.000024678257,0.0016635916,0.00014747256,0.000028319691,0.000009507397,0.00005260699,0.00008397875,0.0015848769,0.00008360898,0.96848017,0.02782599],"study_design_scores_gemma":[0.00015364168,0.00004042425,0.00013027241,0.000085411615,0.000019981297,0.000020086947,0.00029242874,0.000015455931,0.00042655264,0.00002725159,0.9982075,0.00058097235],"about_ca_topic_score_codex":0.8105099,"about_ca_topic_score_gemma":0.9925331,"teacher_disagreement_score":0.20383404,"about_ca_system_score_codex":0.0037520905,"about_ca_system_score_gemma":0.0007486493,"threshold_uncertainty_score":0.9998618},"labels":[],"label_agreement":null},{"id":"W7037224315","doi":"","title":"Dietary intake and anthropometry of DeneMÃ©tis and Yukon children","year":2004,"lang":"en","type":"other","venue":"Library and Archives Canada (Government of Canada)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Anthropometry; Nutrient; Vitamin; Food intake; Sugar; Dietary Sucrose; Vitamin C; Malnutrition; Added sugar; Food frequency questionnaire","score_opus":0.0025538024401003867,"score_gpt":0.14379945121366308,"score_spread":0.1412456487735627,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7037224315","genre_codex":"other","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":[0.07748344,0.0062903143,0.00016226817,0.0013580499,0.00014442277,0.000516633,0.00077565585,0.00006471399,0.9132045],"genre_scores_gemma":[0.92152107,0.0060817143,0.0063720876,0.00035442348,0.00003246596,0.0000062375525,0.000014053315,0.00012459229,0.065493345],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.9985372,0.000017907314,0.00018511547,0.0003166556,0.00073124026,0.0002118851],"domain_scores_gemma":[0.9994376,0.000055761277,0.00017891602,0.00019387538,6.652127e-8,0.00013379367],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0000053829963,0.00023149796,0.00031567662,0.000035028046,0.000067331915,0.0000070316873,0.0001786003,0.00006979036,0.00025890928],"category_scores_gemma":[0.0000028322331,0.0002118946,0.000016211963,0.00008490225,0.000599723,0.00013517804,0.00034522542,0.00013632947,4.60946e-9],"study_design_candidate":"observational","study_design_consensus":"observational","about_ca_topic_candidate":true,"about_ca_topic_consensus":true,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00029420282,0.00013276578,0.54497653,0.00086810923,0.00044664284,0.00022587247,0.000121586854,0.000072474,0.024594449,0.014593444,0.02938026,0.38429365],"study_design_scores_gemma":[0.001353896,0.0005261572,0.81060314,0.00097151595,0.0001233198,0.00007185359,0.0016934006,0.000104440114,0.08949538,0.009629116,0.08401546,0.0014122948],"about_ca_topic_score_codex":0.013234892,"about_ca_topic_score_gemma":0.04125622,"teacher_disagreement_score":0.84771115,"about_ca_system_score_codex":0.000008370945,"about_ca_system_score_gemma":0.00013113281,"threshold_uncertainty_score":0.9933361},"labels":[],"label_agreement":null},{"id":"W7040768367","doi":"","title":"P. Barry Butler","year":2020,"lang":"en","type":"article","venue":"Scholarly Commons (Embry–Riddle Aeronautical University)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Aviation; Aerospace; Vice president; Institution; Georgia tech; Engineering education; Higher education; The arts","score_opus":0.02671612614433902,"score_gpt":0.19690352859999505,"score_spread":0.17018740245565603,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7040768367","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":[0.4921586,0.00027526886,0.061424438,0.037053514,0.00028540174,0.00082103454,0.00007434371,0.0025015296,0.40540588],"genre_scores_gemma":[0.98920226,0.000028931063,0.0062001585,0.0013287356,0.00003178957,0.000001248977,0.000008229204,0.000025255273,0.0031733792],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"not_applicable","domain_scores_codex":[0.9981694,0.00011288372,0.00018391003,0.0006018459,0.00039694156,0.000534984],"domain_scores_gemma":[0.9988406,0.00012864714,0.00006027772,0.00048420834,0.000021860955,0.000464409],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.000119614415,0.00025876862,0.00026403458,0.00008387726,0.00039343903,0.00011897234,0.001078981,0.0002226803,0.0018645006],"category_scores_gemma":[0.00028950235,0.00026922784,0.000131115,0.0010789264,0.00062935083,0.0018541845,0.0011212815,0.00090049446,0.0032153751],"study_design_candidate":"not_applicable","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":[0.0013626385,0.001655828,0.22833659,0.00009793586,0.00039110077,0.004547489,0.0013335524,0.0026559767,0.102703564,0.37304473,0.09004182,0.19382879],"study_design_scores_gemma":[0.0015305317,0.00047884492,0.025407776,0.00002069496,0.00008278428,0.000019545545,0.0007608602,0.0011288223,0.004806991,0.0052104085,0.95970374,0.0008489665],"about_ca_topic_score_codex":0.00004994239,"about_ca_topic_score_gemma":0.000048387017,"teacher_disagreement_score":0.8696619,"about_ca_system_score_codex":0.00023548992,"about_ca_system_score_gemma":0.000029161674,"threshold_uncertainty_score":0.999976},"labels":[],"label_agreement":null},{"id":"W7042779085","doi":"","title":"Randomized experimental design for casual graph discovery","year":2015,"lang":"en","type":"dissertation","venue":"eScholarship@McGill (McGill)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"McGill University","keywords":"Graph; Minimax; Logarithm; Clique; Causal inference; Adversarial system; Upper and lower bounds; Cardinality (data modeling)","score_opus":0.029683976088733233,"score_gpt":0.2758303895534643,"score_spread":0.24614641346473104,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7042779085","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":[0.9152868,0.0012774729,0.00026576436,0.00001949746,0.002397762,0.006864284,0.0010984177,0.0012467427,0.07154329],"genre_scores_gemma":[0.9670192,0.00016862895,0.014365639,0.00014206047,0.000038616927,0.0022763158,0.000710522,0.0002613127,0.01501771],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9953509,0.00042646396,0.00091603847,0.0014115572,0.00096544414,0.0009295797],"domain_scores_gemma":[0.9975744,0.0006532704,0.00062265445,0.00078362017,0.00007538533,0.00029067797],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0015546748,0.0009809167,0.0013582684,0.00024758631,0.00090631976,0.00011915381,0.0010041625,0.00090812595,0.00030617078],"category_scores_gemma":[0.0013502324,0.00089481706,0.00069572503,0.00046593102,0.00041486212,0.0015669647,0.00024472742,0.0008609686,0.00034920065],"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":[0.13599363,0.001688062,0.000017030663,0.00031062248,0.00097198866,0.0002547049,0.00010089565,0.0022558204,0.53467387,0.13527514,0.0006910263,0.1877672],"study_design_scores_gemma":[0.059229456,0.0004925693,0.000016079406,0.00015437235,0.00030369565,0.000028276138,0.0011094307,0.00010957478,0.52610683,0.3977322,0.0128210075,0.0018965035],"about_ca_topic_score_codex":0.00018607179,"about_ca_topic_score_gemma":0.00019186418,"teacher_disagreement_score":0.26245704,"about_ca_system_score_codex":0.001175247,"about_ca_system_score_gemma":0.000035259378,"threshold_uncertainty_score":0.99935025},"labels":[],"label_agreement":null},{"id":"W7043735215","doi":"","title":"Study of particulate matter formation and evolution in near-field aircraft plumes using a one-dimensional microphysical model","year":2007,"lang":"en","type":"dissertation","venue":"DSpace@MIT (Massachusetts Institute of Technology)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Federal Aviation Administration; Transport Canada","keywords":"Relative humidity; Particulates; Plume; Soot; Nucleation; Aerosol; Sulfur dioxide; Combustion","score_opus":0.015812924845042205,"score_gpt":0.2708014844217718,"score_spread":0.2549885595767296,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7043735215","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":[0.99419785,0.00014188305,0.004181727,0.00022285279,0.000116788295,0.00078311574,0.000013084354,0.00013080954,0.00021191119],"genre_scores_gemma":[0.97012126,0.00001596035,0.029633263,0.000022674687,0.00000591987,0.00003974016,0.000024853356,0.000029273442,0.000107061336],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9978958,0.000021581145,0.0006893367,0.00055149593,0.00044265672,0.00039917542],"domain_scores_gemma":[0.9988777,0.000024761895,0.0005124392,0.0004983335,0.00004342108,0.000043348395],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00014904168,0.00036892382,0.0006166261,0.0006043999,0.0001331791,0.000014201605,0.0003481604,0.0008130431,0.000018727982],"category_scores_gemma":[0.00008676735,0.00037514846,0.00007871126,0.00075795973,0.00050219876,0.0005334488,0.00024262507,0.0006205251,0.00001411988],"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":[0.00077500375,0.0032360873,0.26669043,0.00053664355,0.00028191507,0.00012658961,0.0028260367,0.134273,0.5671584,0.0011075683,0.0003699209,0.022618372],"study_design_scores_gemma":[0.008878949,0.0029823193,0.27035046,0.0028233721,0.0010689234,0.00009308373,0.009081273,0.21393344,0.4476408,0.03864278,0.00066694047,0.0038376544],"about_ca_topic_score_codex":0.00029587132,"about_ca_topic_score_gemma":0.0013757872,"teacher_disagreement_score":0.11951762,"about_ca_system_score_codex":0.0002800235,"about_ca_system_score_gemma":0.000046437337,"threshold_uncertainty_score":0.99987006},"labels":[],"label_agreement":null},{"id":"W7067729300","doi":"","title":"New order for Alfa Laval to unlock potential of biofuels in aviation","year":2024,"lang":"en","type":"other","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Aviation; Order (exchange); Biofuel; Production (economics); Work (physics)","score_opus":0.00813725402896295,"score_gpt":0.24658741101008627,"score_spread":0.23845015698112332,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7067729300","genre_codex":"methods","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"other","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.00009105372,0.00025433718,0.60992366,0.00076651137,0.0004397397,0.001043346,0.000036875615,0.0004100917,0.38703442],"genre_scores_gemma":[0.0025070384,0.000038027545,0.10350312,0.00006727481,0.000041232637,0.000024572213,0.0000074747313,0.00010951307,0.89370173],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.99934316,0.0000041821513,0.00012962836,0.00026301257,0.000116842544,0.00014318997],"domain_scores_gemma":[0.99976325,0.0000070525657,0.000041288382,0.0001576198,0.0000020083742,0.00002878896],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00003423187,0.00012068867,0.00014904902,0.00012912737,0.0000051160396,0.0000066346392,0.00016195759,0.00017885167,0.0043109474],"category_scores_gemma":[0.00002234052,0.00009964637,0.000037037356,0.00027343992,0.000031283635,0.000027066762,0.0001090645,0.00006403925,0.00075240136],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00001316055,0.000027710432,0.00019298203,0.000052294676,0.000013744416,0.0000041285416,0.000038437865,0.00018544632,0.0077247,0.0010907004,0.88191694,0.10873977],"study_design_scores_gemma":[0.00042168715,0.00016805269,0.00020232487,0.00012387011,0.000024609462,0.0000015860454,0.000086251865,0.00015377997,0.007190762,0.084940396,0.9062951,0.00039153325],"about_ca_topic_score_codex":0.00096746616,"about_ca_topic_score_gemma":0.0011404944,"teacher_disagreement_score":0.5066673,"about_ca_system_score_codex":0.00004631868,"about_ca_system_score_gemma":0.000010217099,"threshold_uncertainty_score":0.99659926},"labels":[],"label_agreement":null},{"id":"W7100322589","doi":"","title":"Aviation and the Global Atmosphere: A Special Report of IPCC Working","year":2014,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Aviation; Civil aviation; Montreal Protocol; Product (mathematics); Revenue; Passenger transport; Tropospheric ozone; Climate change","score_opus":0.007104203070786609,"score_gpt":0.21094072381217904,"score_spread":0.20383652074139244,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7100322589","genre_codex":"other","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":[0.4140836,0.00003067958,0.13481043,0.0012146714,0.00013048435,0.00019062334,2.8619402e-7,0.000111017165,0.4494282],"genre_scores_gemma":[0.9908199,0.000008146053,0.008653592,0.000064224696,0.00004615528,0.0000027531587,2.3810604e-7,0.0000015930902,0.00040343814],"study_design_codex":"observational","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.99959886,0.00001469867,0.000103178645,0.00010650681,0.00010499147,0.00007175007],"domain_scores_gemma":[0.9997521,0.00003607059,0.00006268604,0.00013622442,0.000001820915,0.000011121286],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017431758,0.000042112948,0.00006744417,6.261429e-7,0.000043902877,0.000006944088,0.00008034324,0.000028514356,0.00023677044],"category_scores_gemma":[0.00010448435,0.000024751755,0.000016675594,0.00009569516,0.000291038,0.00004840845,0.00009213188,0.00003022686,0.000016527007],"study_design_candidate":"theoretical_or_conceptual","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":[0.000047089998,0.000019897165,0.40058422,0.0000021495257,0.0000068350655,0.0000071617023,0.00008913469,0.00021416183,0.00027060334,0.21037361,0.0012740502,0.3871111],"study_design_scores_gemma":[0.0013568,0.0000705926,0.26109734,0.000013510293,0.00001907302,0.000112404945,0.00024998575,0.0037674748,0.0022276118,0.65139294,0.07948187,0.00021038367],"about_ca_topic_score_codex":0.000066098975,"about_ca_topic_score_gemma":0.00008061616,"teacher_disagreement_score":0.5767363,"about_ca_system_score_codex":0.000027743978,"about_ca_system_score_gemma":0.0000012870186,"threshold_uncertainty_score":0.25924703},"labels":[],"label_agreement":null},{"id":"W7100365052","doi":"","title":"Screening for HIV during pregnancy Screening for HIV during pregnancy Survey of physicians ’ practices","year":2014,"lang":"en","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Pregnancy; Prenatal care; Human immunodeficiency virus (HIV); Prenatal screening; HIV screening; MEDLINE","score_opus":0.042483001044178056,"score_gpt":0.28227745319479924,"score_spread":0.23979445215062117,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7100365052","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":[0.17521137,0.00029889125,0.82024413,0.0003424386,0.000063623665,0.0014171707,0.00007801176,0.00045831176,0.0018860239],"genre_scores_gemma":[0.83186525,0.00006082105,0.1652251,0.000012304877,0.000029618439,0.00023947044,0.00002342386,0.000051323237,0.0024927135],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.99795794,0.000067696594,0.00042606844,0.0006448044,0.00027522398,0.00062826404],"domain_scores_gemma":[0.9980978,0.0006202703,0.000687995,0.00050300447,0.000038230457,0.000052729156],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00023136947,0.00028497877,0.00037469447,0.00007590743,0.00039289694,0.00003986013,0.0005170844,0.00012520648,0.000060908587],"category_scores_gemma":[0.0010648587,0.00026663716,0.00013319084,0.0002915127,0.0001954711,0.0009272579,0.00028398377,0.00014844527,0.000012258674],"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":[0.00047875135,0.00037494308,0.56125194,0.0009396868,0.00015347256,0.000008450917,0.000489437,0.0068275942,0.16371232,0.0010054647,0.0003370694,0.26442084],"study_design_scores_gemma":[0.0039850054,0.0003890358,0.5747738,0.0023992474,0.0000884137,0.000014116332,0.0006444092,0.020852894,0.39286113,0.0016646226,0.0012088361,0.0011184979],"about_ca_topic_score_codex":0.0001445574,"about_ca_topic_score_gemma":0.00025910215,"teacher_disagreement_score":0.6566538,"about_ca_system_score_codex":0.000048343412,"about_ca_system_score_gemma":0.0000059096296,"threshold_uncertainty_score":0.9999786},"labels":[],"label_agreement":null},{"id":"W7103576024","doi":"","title":"P. Barry Butler","year":2020,"lang":"","type":"article","venue":"Scholarly Commons (Embry–Riddle Aeronautical University)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Aviation; Aerospace; Vice president; Georgia tech; Institution; Engineering education; Higher education; The arts","score_opus":0.033397398422139755,"score_gpt":0.20687930766713072,"score_spread":0.17348190924499096,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7103576024","genre_codex":"other","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":[0.3212027,0.0040072417,0.10699353,0.13083203,0.0017213003,0.0034305516,0.00093464804,0.00422702,0.42665097],"genre_scores_gemma":[0.98409563,0.00043357594,0.0059631374,0.0021408352,0.000118481345,0.0000021271112,0.000016103188,0.00008113245,0.0071489713],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"not_applicable","domain_scores_codex":[0.99459946,0.00038707125,0.00060421217,0.0017604446,0.0010694397,0.001579358],"domain_scores_gemma":[0.9964681,0.00035191787,0.00023702142,0.0012826084,0.000087418775,0.0015728816],"candidate_categories":["metaepi_narrow","research_integrity","insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.00033186976,0.0008596946,0.0008430785,0.0002780177,0.0012806731,0.0005479652,0.0030938569,0.0008647907,0.0065494245],"category_scores_gemma":[0.00067967415,0.0009810103,0.0004635669,0.0029764653,0.0024671718,0.004984698,0.0034398243,0.0032011361,0.0088916],"study_design_candidate":"not_applicable","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":[0.0033938277,0.0038837742,0.08163943,0.00041355137,0.0012685019,0.010526635,0.0025974435,0.003159869,0.07349133,0.38913342,0.044310812,0.38618138],"study_design_scores_gemma":[0.0038531786,0.0017723046,0.025809657,0.0001401086,0.00048670126,0.00004788837,0.003165785,0.0037126695,0.0073344805,0.005225134,0.94603294,0.002419128],"about_ca_topic_score_codex":0.00009756339,"about_ca_topic_score_gemma":0.00008029085,"teacher_disagreement_score":0.90172213,"about_ca_system_score_codex":0.00083712966,"about_ca_system_score_gemma":0.0001750273,"threshold_uncertainty_score":0.99926406},"labels":[],"label_agreement":null},{"id":"W7108464075","doi":"10.5281/zenodo.17776620","title":"Evolution of Utility and Bush Aircraft: Structural and Aerodynamic Trends from Fairchild to Murdern STOL types","year":2025,"lang":"","type":"article","venue":"Zenodo (CERN European Organization for Nuclear Research)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Aerodynamics; Lift (data mining); Wing; Key (lock)","score_opus":0.012037379672632997,"score_gpt":0.23100332263921283,"score_spread":0.21896594296657984,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7108464075","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":[0.94790715,0.0010788244,0.032412212,0.0015334823,0.00013985088,0.0006136653,0.0009716486,0.00054011634,0.014803069],"genre_scores_gemma":[0.99744576,0.00017525967,0.001372013,0.00004482331,0.000018602705,4.8283734e-8,0.00011577187,0.00024369523,0.0005840203],"study_design_codex":"design_other","study_design_gemma":"observational","domain_scores_codex":[0.9980027,0.00019815603,0.0003471763,0.0007586684,0.00031144966,0.00038183224],"domain_scores_gemma":[0.99907213,0.000040787578,0.00011740244,0.0005201761,0.000094312694,0.00015516703],"candidate_categories":["metaepi_narrow","sts","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00028991682,0.00023325933,0.00026806447,0.00031064363,0.0014041325,0.00023570922,0.0007152908,0.00013513389,0.0039020902],"category_scores_gemma":[0.00040430998,0.00024567032,0.000040520335,0.0009599165,0.0009286381,0.00031784902,0.0025490653,0.00031269842,0.00026578878],"study_design_candidate":"design_other","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":[0.00019759659,0.00008456397,0.0014458881,0.00007841172,0.000067584646,0.000004565091,0.0010082384,0.00029483164,0.026930265,0.002793882,0.0036151335,0.96347904],"study_design_scores_gemma":[0.0014335591,0.0007375075,0.8305554,0.0002046659,0.00010910598,0.00003297144,0.0019670567,0.014114392,0.0022509333,0.010294084,0.13767949,0.00062086445],"about_ca_topic_score_codex":0.00022931301,"about_ca_topic_score_gemma":0.00001903966,"teacher_disagreement_score":0.9628582,"about_ca_system_score_codex":0.00027918426,"about_ca_system_score_gemma":0.0000038126386,"threshold_uncertainty_score":0.9999996},"labels":[],"label_agreement":null},{"id":"W7108481733","doi":"10.5281/zenodo.17776621","title":"Evolution of Utility and Bush Aircraft: Structural and Aerodynamic Trends from Fairchild to Murdern STOL types","year":2025,"lang":"","type":"article","venue":"Zenodo (CERN European Organization for Nuclear Research)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Aerodynamics; Lift (data mining); Wing; Key (lock)","score_opus":0.012037379672632997,"score_gpt":0.23100332263921283,"score_spread":0.21896594296657984,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7108481733","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":[0.94790715,0.0010788244,0.032412212,0.0015334823,0.00013985088,0.0006136653,0.0009716486,0.00054011634,0.014803069],"genre_scores_gemma":[0.99744576,0.00017525967,0.001372013,0.00004482331,0.000018602705,4.8283734e-8,0.00011577187,0.00024369523,0.0005840203],"study_design_codex":"design_other","study_design_gemma":"observational","domain_scores_codex":[0.9980027,0.00019815603,0.0003471763,0.0007586684,0.00031144966,0.00038183224],"domain_scores_gemma":[0.99907213,0.000040787578,0.00011740244,0.0005201761,0.000094312694,0.00015516703],"candidate_categories":["metaepi_narrow","sts","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00028991682,0.00023325933,0.00026806447,0.00031064363,0.0014041325,0.00023570922,0.0007152908,0.00013513389,0.0039020902],"category_scores_gemma":[0.00040430998,0.00024567032,0.000040520335,0.0009599165,0.0009286381,0.00031784902,0.0025490653,0.00031269842,0.00026578878],"study_design_candidate":"design_other","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":[0.00019759659,0.00008456397,0.0014458881,0.00007841172,0.000067584646,0.000004565091,0.0010082384,0.00029483164,0.026930265,0.002793882,0.0036151335,0.96347904],"study_design_scores_gemma":[0.0014335591,0.0007375075,0.8305554,0.0002046659,0.00010910598,0.00003297144,0.0019670567,0.014114392,0.0022509333,0.010294084,0.13767949,0.00062086445],"about_ca_topic_score_codex":0.00022931301,"about_ca_topic_score_gemma":0.00001903966,"teacher_disagreement_score":0.9628582,"about_ca_system_score_codex":0.00027918426,"about_ca_system_score_gemma":0.0000038126386,"threshold_uncertainty_score":0.9999996},"labels":[],"label_agreement":null},{"id":"W7111486241","doi":"","title":"The use of sustainable aviation fuels (SAF) in developing countries: A practical approach for distributing the green premium","year":2024,"lang":"en","type":"article","venue":"Document Server@UHasselt (UHasselt)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"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":"Transport Canada; Washington State University; Massachusetts Institute of Technology; National Aeronautics and Space Administration; U.S. Department of Defense","keywords":"Aviation; Sustainability; Sustainable development; Sustainable energy; Production (economics); Greenhouse gas","score_opus":0.03176449160220429,"score_gpt":0.29096905145553864,"score_spread":0.25920455985333435,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7111486241","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":[0.24862738,0.0008506609,0.70878744,0.03374576,0.0003642608,0.006136376,0.00005875386,0.00070216466,0.00072721374],"genre_scores_gemma":[0.9822793,0.0003591893,0.0145136,0.00024481278,0.00005013063,0.0006883165,0.000063940985,0.000044818404,0.0017559176],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"not_applicable","domain_scores_codex":[0.9972097,0.00015954461,0.00062954857,0.00058886653,0.0005916956,0.00082061504],"domain_scores_gemma":[0.99744135,0.0016405452,0.00023010955,0.0005676959,0.00006538391,0.00005494365],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0017495584,0.00029931735,0.00027842572,0.00007337079,0.00056045793,0.0004613678,0.00057958625,0.000173329,0.000040510604],"category_scores_gemma":[0.00071253104,0.00019182291,0.00011909653,0.00091277284,0.0003237499,0.0016537094,0.0004768062,0.00035928586,0.000018645873],"study_design_candidate":"theoretical_or_conceptual","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":[0.00038590547,0.0003131626,0.029550942,0.0012071864,0.0002609848,0.00009045026,0.0027960804,0.0046793674,0.001251873,0.9330669,0.0119040385,0.01449313],"study_design_scores_gemma":[0.0012269933,0.0003291088,0.011639787,0.00024769205,0.00014794832,0.000040075593,0.006676993,0.02693168,0.009413604,0.1035582,0.8387868,0.0010011666],"about_ca_topic_score_codex":0.0006699168,"about_ca_topic_score_gemma":0.0002166874,"teacher_disagreement_score":0.82950866,"about_ca_system_score_codex":0.0010179593,"about_ca_system_score_gemma":0.00013990689,"threshold_uncertainty_score":0.7822311},"labels":[],"label_agreement":null},{"id":"W7112424414","doi":"","title":"The use of sustainable aviation fuels (SAF) - Supply Chain Challenges","year":2025,"lang":"en","type":"article","venue":"Document Server@UHasselt (UHasselt)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"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":"Transport Canada; Washington State University; Massachusetts Institute of Technology; National Aeronautics and Space Administration; U.S. Department of Defense","keywords":"Supply chain; Aviation; Sustainability; Production (economics); Sustainable development; Supply chain risk management","score_opus":0.01877463909007706,"score_gpt":0.24963931028304046,"score_spread":0.2308646711929634,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7112424414","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":[0.9109105,0.00638778,0.017856587,0.041322242,0.0011068779,0.005228972,0.000033696317,0.0016261132,0.015527238],"genre_scores_gemma":[0.9786866,0.003255092,0.0015595442,0.00027261887,0.00002450936,0.00023194055,0.000019634872,0.000033212607,0.015916878],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"not_applicable","domain_scores_codex":[0.99696857,0.00020118701,0.0006335197,0.00067526376,0.00064661267,0.00087482884],"domain_scores_gemma":[0.9978306,0.0005491745,0.000327017,0.0011244292,0.00007549304,0.000093272196],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.000861479,0.00039225395,0.0003971192,0.00016056903,0.00059262355,0.00019405538,0.00094881543,0.00023301833,0.0002805766],"category_scores_gemma":[0.00038108256,0.0003069868,0.0001681448,0.0008469476,0.00040148638,0.001357002,0.0007199128,0.0003212868,0.00011001234],"study_design_candidate":"theoretical_or_conceptual","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":[0.00028640815,0.0006911354,0.04004575,0.00037435736,0.00030841434,0.00008549149,0.0011017615,0.0030090963,0.009169462,0.8406937,0.024949115,0.079285294],"study_design_scores_gemma":[0.0020342653,0.00053997274,0.10216022,0.00018170585,0.00013363152,0.0000085966085,0.006056886,0.0006764763,0.03908077,0.29884458,0.54922616,0.0010567289],"about_ca_topic_score_codex":0.00058220647,"about_ca_topic_score_gemma":0.00043755976,"teacher_disagreement_score":0.54184914,"about_ca_system_score_codex":0.0005687912,"about_ca_system_score_gemma":0.00005708926,"threshold_uncertainty_score":0.99993825},"labels":[],"label_agreement":null},{"id":"W7114984454","doi":"10.1016/j.ijhydene.2025.153000","title":"Estimating the demand and cost-effectiveness of a hydrogen-based decarbonization strategy for airports","year":2025,"lang":"en","type":"article","venue":"International Journal of Hydrogen Energy","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"Carleton University","funders":"Transport Canada; Carleton University","keywords":"Aviation; Hydrogen vehicle; Range (aeronautics); Hydrogen; Greenhouse gas; Emissions trading; Baseline (sea); Supply and demand","score_opus":0.013711949198830451,"score_gpt":0.2797712562804669,"score_spread":0.26605930708163644,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7114984454","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":[0.56403065,0.00024066208,0.43502593,0.0001593035,0.00012097751,0.00010851552,0.0000040004606,0.000009916918,0.00030003904],"genre_scores_gemma":[0.9965155,0.000016868313,0.003320422,0.00007489474,0.000021423051,0.000018371391,0.000003302678,0.0000059869785,0.00002319013],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9992733,0.000047260517,0.00027358482,0.00010548862,0.00021265207,0.00008772533],"domain_scores_gemma":[0.99927664,0.00028045732,0.00027079813,0.00007856092,0.00007203366,0.000021493768],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003504586,0.00008140704,0.00012910951,0.00008069862,0.00005176201,0.000016247257,0.00027278464,0.000043180222,0.000011767401],"category_scores_gemma":[0.00014533577,0.00005838339,0.00006260017,0.00011359824,0.00014177704,0.00012275716,0.00005845909,0.000053823085,1.8596681e-7],"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":[0.00016468872,0.000072049916,0.012746898,0.000013079519,0.00012704119,0.000017042898,0.000016882452,0.8850513,0.039002728,0.005002828,0.000030727657,0.057754718],"study_design_scores_gemma":[0.0015420185,0.0002090629,0.004187622,0.0002118976,0.000066057204,0.00008844074,0.00004085678,0.3127622,0.5977663,0.0813892,0.001593793,0.00014256689],"about_ca_topic_score_codex":0.00003832317,"about_ca_topic_score_gemma":0.000023295805,"teacher_disagreement_score":0.5722891,"about_ca_system_score_codex":0.00008658852,"about_ca_system_score_gemma":0.000037630947,"threshold_uncertainty_score":0.23808055},"labels":[],"label_agreement":null},{"id":"W7116776169","doi":"10.18280/mmep.121122","title":"Ka4-55 Series Based Toroidal Propeller Design","year":2025,"lang":"","type":"article","venue":"Mathematical Modelling and Engineering Problems","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"","score_opus":0.02295428348137415,"score_gpt":0.20493207061332605,"score_spread":0.1819777871319519,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7116776169","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.00198923,0.0012461968,0.9932072,0.0007069556,0.00013599789,0.0007342593,0.00000419193,0.00048614648,0.0014897813],"genre_scores_gemma":[0.60712016,0.00032139927,0.38983077,0.000044513698,0.000017570897,0.00011002835,9.0194743e-7,0.00004581803,0.002508863],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9978077,0.000028697146,0.0005535809,0.0006347797,0.00028219758,0.0006930559],"domain_scores_gemma":[0.9991085,0.00022298822,0.00006646741,0.0004376696,0.000017985658,0.00014637414],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.0004652584,0.00048992416,0.0004958061,0.00012877725,0.0002345709,0.00016841294,0.0003317777,0.00030598784,0.0002371757],"category_scores_gemma":[0.00008996594,0.00042978878,0.00009000244,0.00039412724,0.00032156517,0.00029773082,0.00021288055,0.00045268572,0.00014827533],"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":[0.000022797285,0.000114720984,0.000012572993,0.0010167966,0.000033724024,0.000006421773,0.00020865176,0.97758746,0.0026480998,0.013849782,0.000088305744,0.004410637],"study_design_scores_gemma":[0.00031415047,0.00010414731,0.0000053271783,0.0008953154,0.000054501335,0.000007820243,0.000046540095,0.91645414,0.0059211715,0.07412547,0.0016282849,0.0004431142],"about_ca_topic_score_codex":0.000006873641,"about_ca_topic_score_gemma":3.24277e-7,"teacher_disagreement_score":0.6051309,"about_ca_system_score_codex":0.0001215215,"about_ca_system_score_gemma":0.000028732045,"threshold_uncertainty_score":0.9998154},"labels":[],"label_agreement":null},{"id":"W7132889418","doi":"","title":"Fischer-Tropsch Sustainable Aviation Fuel: An Assessment of Pioneer Plants and Canadian Supply","year":2022,"lang":"","type":"dissertation","venue":"TSpace","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Aviation; Greenhouse gas; Production (economics); Investment (military); Capital investment; Aviation fuel; Aviation biofuel; Biomass (ecology)","score_opus":0.01035608526055637,"score_gpt":0.31939381296412084,"score_spread":0.30903772770356447,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7132889418","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":[0.98093134,0.00090351584,0.0010179924,0.00061578566,0.0002853932,0.0013418234,0.000129055,0.00010965932,0.014665407],"genre_scores_gemma":[0.973706,0.0010097949,0.0026551003,0.00005100567,0.000016442347,0.00012690011,0.00083242584,0.000053059575,0.02154925],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.9972374,0.0001424023,0.00040389143,0.0007769821,0.0006451197,0.0007941906],"domain_scores_gemma":[0.99860907,0.000072124654,0.00039724825,0.0005512198,0.00004478159,0.0003255615],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00038625856,0.0004334488,0.00045069432,0.00035036216,0.00058539456,0.0000743905,0.00048295228,0.00037446,0.006535471],"category_scores_gemma":[0.0000749074,0.0004852343,0.00006388325,0.0004631748,0.00020962788,0.0005478657,0.00016904375,0.0006584427,0.00001577059],"study_design_candidate":"observational","study_design_consensus":"observational","about_ca_topic_candidate":true,"about_ca_topic_consensus":true,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00074279244,0.002011962,0.5181877,0.0033953914,0.00059226004,0.0012963851,0.13289817,0.012901522,0.13821062,0.06421453,0.005451091,0.120097585],"study_design_scores_gemma":[0.00093766866,0.0012579052,0.6128677,0.000086541,0.000099959216,0.000020427115,0.34860182,0.003062261,0.004274589,0.006588269,0.020990018,0.001212828],"about_ca_topic_score_codex":0.19647849,"about_ca_topic_score_gemma":0.11001139,"teacher_disagreement_score":0.21570364,"about_ca_system_score_codex":0.0012649898,"about_ca_system_score_gemma":0.00042564177,"threshold_uncertainty_score":0.9997599},"labels":[],"label_agreement":null},{"id":"W7133061775","doi":"","title":"Propuesta de procedimiento para una alteración mayor basada en certificado tipo suplementario (STC) SA00863SE en la Aeronave Piper Cheyenne II","year":2020,"lang":"es","type":"dissertation","venue":"Repositorio Institucional FULL","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Cheyenne; Power (physics); Piper; Class (philosophy)","score_opus":0.014201797662148996,"score_gpt":0.27046276231913513,"score_spread":0.2562609646569861,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7133061775","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":[0.9787971,0.0008073778,0.0020505749,0.00396065,0.002982241,0.0030364718,0.0002975848,0.0007644232,0.0073035844],"genre_scores_gemma":[0.9757287,0.00060495205,0.014268137,0.00023242102,0.0011474628,0.00059003895,0.0020810494,0.00015807086,0.005189163],"study_design_codex":"bench_or_experimental","study_design_gemma":"not_applicable","domain_scores_codex":[0.99360484,0.00027812517,0.0012825297,0.0020334085,0.0016145093,0.0011865903],"domain_scores_gemma":[0.99750537,0.00033608387,0.00067285844,0.0008455373,0.0001078284,0.0005323264],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00047718902,0.0012100972,0.00089988037,0.00021803535,0.0010615094,0.00030003441,0.0014213374,0.0011175438,0.00090457336],"category_scores_gemma":[0.0004929455,0.0011662119,0.00037731032,0.0006381995,0.0003827597,0.00085552235,0.00071634696,0.0017343035,0.00052427064],"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":[0.0028378319,0.002200298,0.030337116,0.0016649438,0.0007938483,0.0020944597,0.01702772,0.0021065671,0.8955118,0.017052682,0.0076275505,0.02074517],"study_design_scores_gemma":[0.0019596482,0.0019592354,0.03417196,0.0017441526,0.00062768377,0.00061043934,0.0032461085,0.0015516059,0.27108398,0.0017914176,0.67806196,0.0031918054],"about_ca_topic_score_codex":0.0009925663,"about_ca_topic_score_gemma":0.0004972334,"teacher_disagreement_score":0.6704344,"about_ca_system_score_codex":0.002399179,"about_ca_system_score_gemma":0.00061324873,"threshold_uncertainty_score":0.9990788},"labels":[],"label_agreement":null},{"id":"W7135298989","doi":"","title":"Serial number index for Cessna T-50s","year":2015,"lang":"en","type":"article","venue":"Holmes Museum Of Anthropology (Wichita State University)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Index (typography); Listing (finance); Training (meteorology); Airplane; Air traffic control radar beacon system","score_opus":0.018749587943462407,"score_gpt":0.24835165597370865,"score_spread":0.22960206803024624,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7135298989","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":[0.86365294,0.000045130975,0.098125875,0.0026709007,0.00090935995,0.0005713999,0.00012297825,0.0003783627,0.03352304],"genre_scores_gemma":[0.99213076,0.000106499785,0.0059387097,0.000053247586,0.00001865702,0.0000012330422,0.000007867481,0.000016491518,0.0017265513],"study_design_codex":"observational","study_design_gemma":"not_applicable","domain_scores_codex":[0.9989192,0.000050110517,0.00016155432,0.00034989128,0.00014784683,0.00037139776],"domain_scores_gemma":[0.9993504,0.00007002417,0.00014307143,0.00028836256,0.000032957425,0.00011518031],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00010030722,0.00017149032,0.00026420693,0.000110719135,0.00014268575,0.0000067869746,0.00044446936,0.00014582076,0.0005462022],"category_scores_gemma":[0.000062642,0.00017344725,0.000076130025,0.00035707382,0.0020400798,0.0003426106,0.00032616657,0.00012224642,0.00009219549],"study_design_candidate":"not_applicable","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":[0.0066211782,0.0022034985,0.74343646,0.00016772353,0.0006660832,0.00084766804,0.011038376,0.015140404,0.018647356,0.055885427,0.076098695,0.06924712],"study_design_scores_gemma":[0.011832135,0.002756965,0.022864634,0.00005129016,0.00018571636,0.000068196,0.02558843,0.0011720674,0.02768324,0.05806574,0.84794307,0.0017885038],"about_ca_topic_score_codex":0.00051906635,"about_ca_topic_score_gemma":0.00043901565,"teacher_disagreement_score":0.7718444,"about_ca_system_score_codex":0.0001235618,"about_ca_system_score_gemma":0.000042922216,"threshold_uncertainty_score":0.7516759},"labels":[],"label_agreement":null},{"id":"W7135348537","doi":"","title":"Production records for Cessna T-50, serial numbers 1000-1118","year":2015,"lang":"en","type":"article","venue":"Holmes Museum Of Anthropology (Wichita State University)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Production (economics); Sound production; Plane (geometry); Historical record; Electronic equipment","score_opus":0.02036979551199635,"score_gpt":0.2442273811163029,"score_spread":0.22385758560430655,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7135348537","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":[0.93277216,0.000072827235,0.03612177,0.0058475635,0.0025498213,0.00082761166,0.00008844968,0.0004804227,0.021239363],"genre_scores_gemma":[0.9822202,0.00030386815,0.012615549,0.000041068648,0.000051369145,0.0000025001193,0.000015479682,0.000024032259,0.0047259685],"study_design_codex":"observational","study_design_gemma":"not_applicable","domain_scores_codex":[0.99875575,0.00006735711,0.000185444,0.00046116885,0.00015652853,0.00037372357],"domain_scores_gemma":[0.9992839,0.000048492282,0.00018421991,0.00033435028,0.000043559616,0.00010544172],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015416495,0.00018454342,0.0002677399,0.00016850588,0.00019010337,0.000007180384,0.00038933865,0.00013597595,0.00024845803],"category_scores_gemma":[0.0000981247,0.00019061183,0.00007734412,0.00041195782,0.0020324446,0.00046098814,0.00023205971,0.0001253092,0.000047065907],"study_design_candidate":"not_applicable","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":[0.015940841,0.0041894186,0.30598173,0.00045022712,0.0013270328,0.0006631637,0.025244169,0.03536427,0.11584482,0.041393183,0.27544552,0.1781556],"study_design_scores_gemma":[0.005828956,0.004064009,0.006816012,0.00006419257,0.00022318795,0.00007939872,0.030547166,0.00028443025,0.09119619,0.023163226,0.8362164,0.0015168308],"about_ca_topic_score_codex":0.000845694,"about_ca_topic_score_gemma":0.0010084326,"teacher_disagreement_score":0.56077087,"about_ca_system_score_codex":0.00019666213,"about_ca_system_score_gemma":0.000049777307,"threshold_uncertainty_score":0.7772925},"labels":[],"label_agreement":null},{"id":"W7139353566","doi":"","title":"Ellen Ebner","year":2022,"lang":"","type":"article","venue":"Scholarly Commons (Embry–Riddle Aeronautical University)","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Portfolio; Sustainability; Work (physics); Renewable energy; Product (mathematics); Advanced manufacturing; Road map","score_opus":0.02141780046840429,"score_gpt":0.2038616750283377,"score_spread":0.18244387455993344,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7139353566","genre_codex":"other","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":[0.43162712,0.0032428757,0.020955296,0.024867494,0.0029198306,0.0035883614,0.0014219352,0.002660827,0.5087163],"genre_scores_gemma":[0.94956267,0.00024039579,0.003001671,0.0006370901,0.00005182595,0.000011248217,0.000028821227,0.00008036007,0.046385944],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"not_applicable","domain_scores_codex":[0.99367845,0.00079071865,0.00058420975,0.0016734586,0.0015743823,0.0016987865],"domain_scores_gemma":[0.9966759,0.00041107257,0.00028540893,0.0018361051,0.000060135193,0.0007313507],"candidate_categories":["metaepi_narrow","sts","open_science","research_integrity","insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.0007813449,0.00076898304,0.00073064934,0.0006358205,0.0041771904,0.00039959128,0.003908939,0.00043688502,0.017710647],"category_scores_gemma":[0.00023695035,0.0009381028,0.00047117812,0.0034444989,0.002111221,0.0035517297,0.008640717,0.004299291,0.0025152494],"study_design_candidate":"not_applicable","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":[0.0024853228,0.007388385,0.05189346,0.0001228512,0.00089934247,0.008974892,0.0015269772,0.012922299,0.01999251,0.56065416,0.027995424,0.30514434],"study_design_scores_gemma":[0.0026932925,0.0014985402,0.012420061,0.000036314214,0.00029167515,0.00012310993,0.005323473,0.0015929998,0.0012021615,0.009641902,0.9635654,0.0016110475],"about_ca_topic_score_codex":0.00018891894,"about_ca_topic_score_gemma":0.000111882546,"teacher_disagreement_score":0.93557,"about_ca_system_score_codex":0.0026299155,"about_ca_system_score_gemma":0.00022048203,"threshold_uncertainty_score":0.9993772},"labels":[],"label_agreement":null},{"id":"W7155374041","doi":"10.13182/t133-49010","title":"Control of Once-Through Steam Generator During Turbine Power Ramp Change in i-SMR","year":2025,"lang":"","type":"article","venue":"Transactions of the American Nuclear Society","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Kootenay Association for Science & Technology","funders":"","keywords":"Steam turbine; Boiler (water heating); Steam-electric power station; Turbine; Heat recovery steam generator; Power (physics); Steam drum","score_opus":0.009373423337084057,"score_gpt":0.23993590853441119,"score_spread":0.23056248519732714,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7155374041","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":[0.984177,0.00042620458,0.011345443,0.002661403,0.00022372905,0.0006994849,0.00012227439,0.00007846833,0.00026601763],"genre_scores_gemma":[0.99304926,0.0017056084,0.004364033,0.00060141826,0.000010538861,0.000026252932,1.9671397e-7,0.000029908966,0.00021278398],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.9982222,0.0000968022,0.0005298355,0.00042176674,0.0003045845,0.00042486747],"domain_scores_gemma":[0.99867886,0.000073327334,0.0004185437,0.00076548004,0.000023930192,0.00003986234],"candidate_categories":["sts"],"consensus_categories":[],"category_scores_codex":[0.00014050258,0.0002740231,0.00060471316,0.00004752075,0.00027701526,0.000011142404,0.00076616183,0.0001292989,0.00055663486],"category_scores_gemma":[0.000016122678,0.00023603204,0.00056332664,0.0015844607,0.0030469699,0.00030699742,0.00008295444,0.0005225958,0.000011639295],"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":[0.0006315202,0.0018784761,0.011097742,0.00029395826,0.0007511922,0.000004041758,0.014136093,0.01837219,0.86601514,0.00057607703,0.00034238264,0.08590119],"study_design_scores_gemma":[0.012432173,0.002081565,0.49563473,0.0012758656,0.0009409638,0.000021244114,0.05536162,0.029828025,0.38655707,0.0015791052,0.012155292,0.0021323338],"about_ca_topic_score_codex":0.0013847732,"about_ca_topic_score_gemma":0.00006567562,"teacher_disagreement_score":0.484537,"about_ca_system_score_codex":0.00037015395,"about_ca_system_score_gemma":0.0000352538,"threshold_uncertainty_score":0.99966615},"labels":[],"label_agreement":null},{"id":"W7162077266","doi":"10.82308/34349","title":"Alternative jet fuels and the business of freedom: a socio-environmental perspective for mitigating the climate impact of aviation","year":2021,"lang":"en","type":"dissertation","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Normative; Environmental policy; Perspective (graphical); Context (archaeology); Descriptive research","score_opus":0.009585092700546279,"score_gpt":0.2719851414911757,"score_spread":0.2624000487906294,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7162077266","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":[0.99043304,0.0006191875,0.003430942,0.00020632712,0.000092576796,0.0011458311,0.00020987936,0.00002558358,0.0038366562],"genre_scores_gemma":[0.9971638,0.0005774253,0.0017227696,0.000010778471,0.000018589973,0.00009615159,0.00011629738,0.000017777866,0.00027645583],"study_design_codex":"bench_or_experimental","study_design_gemma":"qualitative","domain_scores_codex":[0.99901617,0.000055731067,0.0002648273,0.00026855606,0.00022923034,0.00016551484],"domain_scores_gemma":[0.99889034,0.0003825646,0.00048015025,0.00020257667,0.000029806544,0.000014564801],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00022309659,0.00019826909,0.00030871417,0.000025872656,0.00017090102,0.00001672563,0.00022857319,0.000114113194,0.00018361371],"category_scores_gemma":[0.00017633056,0.00010144098,0.00017476501,0.00013758053,0.0007348665,0.00013826437,0.00010137824,0.00014412592,0.0000016264997],"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":[0.0040417514,0.0010961795,0.1687762,0.00096611393,0.0029254686,0.000011948067,0.12118754,0.013778414,0.47310585,0.14987925,0.0007787166,0.06345257],"study_design_scores_gemma":[0.004691112,0.00046552002,0.36759397,0.00032556598,0.0005171525,0.00001277857,0.37563887,0.0065259673,0.055016603,0.18838541,0.00001738593,0.0008096475],"about_ca_topic_score_codex":0.000940165,"about_ca_topic_score_gemma":0.00015077143,"teacher_disagreement_score":0.41808924,"about_ca_system_score_codex":0.0001936982,"about_ca_system_score_gemma":0.000016849603,"threshold_uncertainty_score":0.4136643},"labels":[],"label_agreement":null},{"id":"W7163892210","doi":"10.4050/sm-2024-tvf-5058","title":"50 Years of Progress in Rotorcraft Design: A Retrospective from the Vertical Flight Society's Aircraft Design Technical Committee","year":2024,"lang":"","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lockheed Martin (Canada)","funders":"","keywords":"Takeoff and landing; Propulsion; Avionics; Cockpit; Takeoff; Range (aeronautics); Aerodynamics; Turbine; Engineering design process","score_opus":0.019882090033380984,"score_gpt":0.260004136095401,"score_spread":0.24012204606202003,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7163892210","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.020170527,0.020189425,0.94175255,0.009814437,0.0006551749,0.005359859,0.000107131236,0.0012815028,0.00066941296],"genre_scores_gemma":[0.8402464,0.00064254395,0.15825044,0.00020795593,0.00007532527,0.00030338645,0.000002643652,0.000073125804,0.00019821642],"study_design_codex":"design_other","study_design_gemma":"observational","domain_scores_codex":[0.9949606,0.0004017674,0.0010065202,0.0014397276,0.0011286781,0.0010626714],"domain_scores_gemma":[0.99664545,0.0018745783,0.00009639277,0.0011912587,0.00002801141,0.00016429351],"candidate_categories":["metaepi_narrow","sts","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0010602492,0.0006227776,0.00077843084,0.00009977659,0.00020126607,0.00019453668,0.0017220543,0.000787919,0.0017529886],"category_scores_gemma":[0.00022946147,0.00046781282,0.00046191568,0.0017544946,0.004255185,0.0005627887,0.0010621039,0.0016337612,0.00045970484],"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":[0.0019780167,0.005140479,0.19721945,0.00035710243,0.0014160654,0.0015305607,0.0139391385,0.0047934395,0.21113689,0.024367861,0.085240304,0.45288068],"study_design_scores_gemma":[0.0030408432,0.0036485838,0.5815715,0.0018268118,0.00060427876,0.00008400398,0.004583099,0.10287987,0.1381268,0.14791113,0.012630612,0.003092435],"about_ca_topic_score_codex":0.00019462976,"about_ca_topic_score_gemma":0.00006526784,"teacher_disagreement_score":0.8200758,"about_ca_system_score_codex":0.0010680278,"about_ca_system_score_gemma":0.00016774792,"threshold_uncertainty_score":0.9997774},"labels":[],"label_agreement":null},{"id":"W7164166619","doi":"10.4050/f-0079-2023-0092","title":"S-97 RAIDER&amp;reg; Propulsor Flight Loads and Validation","year":2023,"lang":"","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lockheed Martin (Canada)","funders":"","keywords":"Propulsor; Wake; Aerodynamics; Propeller; Airframe; Thrust; Rotor (electric); Computational fluid dynamics; Wind tunnel; Detached eddy simulation","score_opus":0.0347064693557108,"score_gpt":0.2631210750959487,"score_spread":0.22841460574023786,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7164166619","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":[0.88195986,0.0011018107,0.056579225,0.017871568,0.0010835136,0.0025802625,0.000049043305,0.00391108,0.034863625],"genre_scores_gemma":[0.92649215,0.0017946383,0.0079804985,0.00018128834,0.0000469386,0.00005268746,0.000016040956,0.000034689478,0.06340106],"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9976847,0.00004795951,0.00037811816,0.00080253324,0.00043290466,0.00065376057],"domain_scores_gemma":[0.99909484,0.000096519965,0.00011381778,0.0005345463,0.000012054975,0.00014823023],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.00031662578,0.0003172679,0.00026791473,0.0001571272,0.00038327984,0.0001251111,0.00034220403,0.00026019258,0.0041266927],"category_scores_gemma":[0.00016195426,0.00028067693,0.000067307235,0.001076392,0.00070182467,0.00068090745,0.0006142209,0.00024268884,0.012406728],"study_design_candidate":"design_other","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":[0.000046131918,0.00013359208,0.028405378,0.00009243552,0.000041052986,0.00004743483,0.00060727965,0.0004973129,0.13345776,0.0044480516,0.007555204,0.82466835],"study_design_scores_gemma":[0.001951104,0.0006253547,0.096615665,0.0001577236,0.000113651055,0.00006978737,0.0020879956,0.005662559,0.4860789,0.12253612,0.28193992,0.002161224],"about_ca_topic_score_codex":0.00004841948,"about_ca_topic_score_gemma":0.000034539207,"teacher_disagreement_score":0.82250714,"about_ca_system_score_codex":0.00012037525,"about_ca_system_score_gemma":0.0000148585095,"threshold_uncertainty_score":0.99996454},"labels":[],"label_agreement":null},{"id":"W7164577401","doi":"10.4050/sm_helmot_2018-4242","title":"Sikorsky - Boeing Team: Defiant","year":2018,"lang":"","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lockheed Martin (Canada)","funders":"","keywords":"Airframe; Point (geometry); Feature (linguistics); Pilotage","score_opus":0.014470131917732255,"score_gpt":0.2397857849729171,"score_spread":0.22531565305518486,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7164577401","genre_codex":"other","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":[0.10980831,0.0005209723,0.11032885,0.0017011598,0.0010550205,0.0006445057,0.000013133273,0.0011436372,0.7747844],"genre_scores_gemma":[0.9530337,0.0002254079,0.029668229,0.0006285154,0.00014060854,0.00000936328,5.408074e-7,0.00002834778,0.016265297],"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99767184,0.000026680444,0.00035627058,0.0007319577,0.00037777808,0.00083545095],"domain_scores_gemma":[0.9989598,0.00005156202,0.00010664183,0.0007053974,0.000014185599,0.00016243599],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.00020884468,0.00032916036,0.0002471634,0.00007110047,0.00054812897,0.00007934603,0.00066516554,0.0002373606,0.023669288],"category_scores_gemma":[0.00010228351,0.0002803596,0.00009825681,0.00055089407,0.0021178725,0.00050399045,0.00070953515,0.00026824593,0.018152917],"study_design_candidate":"design_other","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":[0.000056601762,0.00030076757,0.025079696,0.000020621294,0.0000452354,0.000055023233,0.0006593678,0.000056114517,0.12241929,0.019349938,0.018044192,0.81391317],"study_design_scores_gemma":[0.0010960398,0.0018767584,0.025082896,0.00013120752,0.000070531445,0.0000984861,0.002943393,0.010183618,0.52001023,0.08562509,0.35098773,0.0018939996],"about_ca_topic_score_codex":0.0001780119,"about_ca_topic_score_gemma":0.00016389626,"teacher_disagreement_score":0.84322536,"about_ca_system_score_codex":0.00023006972,"about_ca_system_score_gemma":0.000018789486,"threshold_uncertainty_score":0.99996483},"labels":[],"label_agreement":null},{"id":"W7164809668","doi":"10.4050/sm_struct_2001-4039","title":"Reducing The Risk Of Innovative Designs To Assess Affordability","year":2001,"lang":"","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Bell Helicopter Textron (Canada)","funders":"","keywords":"Aerospace; Procurement; Process (computing); Emerging technologies; Order (exchange); Technology readiness level; Profitability index; Reliability (semiconductor)","score_opus":0.05983523397154222,"score_gpt":0.29847747655013546,"score_spread":0.23864224257859323,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7164809668","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":[0.6333693,0.00004983013,0.3503616,0.0012279669,0.00012427577,0.0007926359,0.000021651984,0.000100711135,0.013951974],"genre_scores_gemma":[0.9604441,0.0002858842,0.0378827,0.00017932168,0.00002012091,0.000036401754,5.026738e-7,0.000016031547,0.001134927],"study_design_codex":"design_other","study_design_gemma":"observational","domain_scores_codex":[0.99754167,0.00019640554,0.00060434215,0.00064050505,0.00044936265,0.000567691],"domain_scores_gemma":[0.99791163,0.0005316366,0.0003115515,0.0010793614,0.000073536095,0.00009228681],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0012961125,0.0003005756,0.000340524,0.00007906992,0.00039193197,0.000036317077,0.00095527305,0.00015351239,0.0028712775],"category_scores_gemma":[0.001094208,0.00018959463,0.00009397133,0.0030248044,0.0012634757,0.00035206566,0.00068197085,0.0004464412,0.00021662324],"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":[0.0001568945,0.00044697165,0.36610994,0.00001734317,0.000087684086,0.000009640272,0.0017031212,0.01437781,0.10214348,0.0044158306,0.0010329856,0.5094983],"study_design_scores_gemma":[0.00040731474,0.0009633473,0.49813,0.00006910266,0.000051024414,0.000016085687,0.009357599,0.0021630374,0.44316044,0.040076572,0.0049330983,0.0006723572],"about_ca_topic_score_codex":0.0005414278,"about_ca_topic_score_gemma":0.00012138062,"teacher_disagreement_score":0.5088259,"about_ca_system_score_codex":0.0002750903,"about_ca_system_score_gemma":0.000041827258,"threshold_uncertainty_score":0.99804026},"labels":[],"label_agreement":null},{"id":"W7164846531","doi":"10.4050/sm_prop_2015-3600","title":"Next Generations Of Turboshaft Engines","year":2015,"lang":"","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Safran Electronics (Canada)","funders":"","keywords":"","score_opus":0.043799985011542635,"score_gpt":0.25683455556813023,"score_spread":0.2130345705565876,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7164846531","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":[0.3931694,0.005372226,0.4507868,0.0051792366,0.0015314533,0.0011249755,0.000061498875,0.0008020774,0.14197233],"genre_scores_gemma":[0.9413422,0.00023677186,0.053194895,0.00008649777,0.00003852381,0.000008532771,0.0000016586674,0.000011331902,0.005079585],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9988359,0.000019181047,0.00030510765,0.00028222954,0.00028776366,0.00026976783],"domain_scores_gemma":[0.99929786,0.00003225591,0.00008904761,0.00041943588,0.000026027863,0.0001353775],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00013151577,0.00017330878,0.00019693766,0.000057060388,0.00006393337,0.000026214377,0.00034733405,0.00012986003,0.0024683734],"category_scores_gemma":[0.0001293794,0.00014724639,0.00006220851,0.00038590567,0.00048275577,0.0004929667,0.0002442868,0.00011421532,0.0006955733],"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":[0.000049488306,0.0008182075,0.019575538,0.000045386583,0.000088663684,0.00002854224,0.001738673,0.07081596,0.4107848,0.057637352,0.031502448,0.40691492],"study_design_scores_gemma":[0.0015407964,0.0009866264,0.007004333,0.000048483267,0.000089061985,0.000032221058,0.005458636,0.08079896,0.77298707,0.05737327,0.07251338,0.0011671634],"about_ca_topic_score_codex":0.00006755323,"about_ca_topic_score_gemma":0.000033788685,"teacher_disagreement_score":0.5481728,"about_ca_system_score_codex":0.000083146435,"about_ca_system_score_gemma":0.000032118853,"threshold_uncertainty_score":0.9984435},"labels":[],"label_agreement":null},{"id":"W7164866859","doi":"10.4050/sm_struct_2009-3722","title":"Operations Support &amp;amp; Sustainment Technology for Airframe Structures","year":2009,"lang":"","type":"article","venue":"","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Bell Helicopter Textron (Canada)","funders":"","keywords":"Airframe; Component (thermodynamics); Key (lock); Technology assessment","score_opus":0.015959798258768632,"score_gpt":0.28641366693618714,"score_spread":0.2704538686774185,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7164866859","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.027918266,0.00043894604,0.9196921,0.035869665,0.0003003522,0.0030754409,0.00012630361,0.0012557447,0.01132317],"genre_scores_gemma":[0.73740464,0.00021915406,0.23305793,0.0011824373,0.000048699287,0.000110415596,0.000030891875,0.000026435435,0.02791941],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.99689555,0.000019863193,0.000620593,0.0009823415,0.0003745071,0.0011071585],"domain_scores_gemma":[0.99852896,0.00005310895,0.000105529674,0.001099309,0.000048623202,0.00016449076],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.0001893177,0.0005111529,0.00043824947,0.00026458525,0.0007123767,0.00012553712,0.00093147624,0.00063642906,0.015027681],"category_scores_gemma":[0.00025385368,0.00045299565,0.00017220003,0.00073876826,0.000930839,0.00044758763,0.00029891205,0.00044386488,0.0015997015],"study_design_candidate":"theoretical_or_conceptual","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":[0.0001000963,0.0006593697,0.0010276899,0.000031958385,0.000075491254,0.000016316275,0.00046023598,0.013476784,0.080466494,0.27821153,0.03669388,0.58878016],"study_design_scores_gemma":[0.00087237393,0.00085341797,0.001321377,0.000011428635,0.000060369875,0.000048092523,0.0013133928,0.0004500237,0.034524564,0.394812,0.5648806,0.0008523415],"about_ca_topic_score_codex":0.000022049078,"about_ca_topic_score_gemma":0.00025604325,"teacher_disagreement_score":0.70948637,"about_ca_system_score_codex":0.00050672883,"about_ca_system_score_gemma":0.000071631315,"threshold_uncertainty_score":0.99979216},"labels":[],"label_agreement":null},{"id":"W806970725","doi":"10.4271/2015-01-2562","title":"Characterization of the Ultrafine and Black Carbon Emissions from Different Aviation Alternative Fuels","year":2015,"lang":"en","type":"article","venue":"SAE international journal of fuels and lubricants","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":7,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"National Research Council Canada; Environment and Climate Change Canada","funders":"National Research Council Canada; U.S. Air Force; Clean Air Regulatory Agenda; Transport Canada","keywords":"Carbon black; Alternative fuels; Aviation; Environmental science; Waste management; Characterization (materials science); Carbon fibers; Engineering; Materials science; Aerospace engineering; Diesel fuel; Nanotechnology","score_opus":0.017142339586515565,"score_gpt":0.24311879075564427,"score_spread":0.2259764511691287,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W806970725","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":[0.9973349,0.000046510966,0.00090140454,0.0010107447,0.00025916126,0.0000607154,0.00002626803,0.000005100343,0.00035522046],"genre_scores_gemma":[0.9993366,0.00030492622,0.00015391484,0.00006107652,0.000059841066,8.8888544e-7,0.0000031690563,0.0000043937985,0.000075182536],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.99920064,0.000032980515,0.00024074753,0.00009705451,0.00036094236,0.00006763184],"domain_scores_gemma":[0.9994105,0.000046748046,0.0003579797,0.00006518953,0.00005885429,0.000060702303],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00008253123,0.00007836589,0.00012448657,0.000039359496,0.000021983426,0.000016935914,0.00020971258,0.000033788434,0.000037137484],"category_scores_gemma":[0.0001092184,0.00004817129,0.00002859081,0.00005613607,0.00017749921,0.00016153419,0.00011649102,0.00010006346,8.8809065e-7],"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":[0.00008121348,0.00008951752,0.2522319,0.000002311497,0.00006474868,0.000006760483,0.0011461709,0.000048938764,0.7127746,0.00014688748,0.000051563235,0.033355426],"study_design_scores_gemma":[0.0008241876,0.00010944759,0.88123095,0.000086864566,0.000023438915,0.00003290942,0.00037707097,0.00048621028,0.09912341,0.01715575,0.0004565586,0.00009321022],"about_ca_topic_score_codex":0.0000690997,"about_ca_topic_score_gemma":0.000016650762,"teacher_disagreement_score":0.62899905,"about_ca_system_score_codex":0.00006424085,"about_ca_system_score_gemma":0.00001009744,"threshold_uncertainty_score":0.19643682},"labels":[],"label_agreement":null},{"id":"W825349975","doi":"10.4271/2015-01-2564","title":"Development of a Multi-Disciplinary Optimization Framework for Nonconventional Aircraft Configurations in PACELAB APD","year":2015,"lang":"en","type":"article","venue":"SAE technical papers on CD-ROM/SAE technical paper series","topic":"Advanced Aircraft Design and Technologies","field":"Environmental Science","cited_by":7,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Safran Electronics (Canada)","funders":"","keywords":"Computer science; Discipline; Systems engineering; Aeronautics; Engineering; Sociology","score_opus":0.035186306141179284,"score_gpt":0.2953176075000203,"score_spread":0.260131301358841,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W825349975","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":[0.8106888,0.0012869457,0.064591564,0.025422618,0.0015653468,0.016739001,0.00052037364,0.010934759,0.0682506],"genre_scores_gemma":[0.60011023,0.000029019582,0.39890605,0.00016275092,0.000016612332,0.00053046906,0.00004954583,0.000038096758,0.00015723782],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.99666077,0.00007200349,0.0010711903,0.00087866967,0.0006946166,0.00062272674],"domain_scores_gemma":[0.9983207,0.0003714273,0.0002901096,0.00071842805,0.00006295279,0.00023636957],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00062835147,0.0004722354,0.0006019018,0.00017354247,0.00026583526,0.00003216349,0.000742409,0.00072282733,0.00048111845],"category_scores_gemma":[0.0011574549,0.00042597004,0.00021003578,0.00082073273,0.0011421054,0.000497087,0.0004918713,0.0006530986,0.000074494776],"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":[0.00039692014,0.0011053606,0.00082218956,0.000037055568,0.00002539176,0.000015443902,0.00019358068,0.0078000007,0.96183413,0.0205963,0.000830752,0.006342859],"study_design_scores_gemma":[0.0019835588,0.0010752853,0.94760513,0.0003233556,0.00003890207,0.000028883,0.000892977,0.000017301214,0.0011070409,0.029285712,0.016761668,0.0008802102],"about_ca_topic_score_codex":0.000011308469,"about_ca_topic_score_gemma":0.017294504,"teacher_disagreement_score":0.9607271,"about_ca_system_score_codex":0.00059664046,"about_ca_system_score_gemma":0.0001330471,"threshold_uncertainty_score":0.9998192},"labels":[],"label_agreement":null}]}