{"meta":{"query_hash":"89a144da100c","filters":{"venue":"CEAS Aeronautical Journal"},"cohort_total":9,"direct_labels_cover":0,"predictions_cover":9,"exported":9,"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/89a144da100c","api":"https://metacan.xera.ac/api/v1/cohort?venue=CEAS+Aeronautical+Journal"},"results":[{"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":"methods","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.00094497885,0.000028015784,0.9829071,0.000022591728,0.000015926145,0.000043029308,0.00015391939,0.012837067,0.0030473296],"genre_scores_gemma":[0.057630263,0.00018500701,0.92223376,0.00008107,0.000035678095,0.0005106727,0.0014056457,0.00617975,0.0117381085],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991627,0.00020685267,0.00006590873,0.00016362956,0.00032464223,0.00007627478],"domain_scores_gemma":[0.99790597,0.0009344502,0.00007132527,0.00055851915,0.0003988031,0.0001309821],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0017216637,0.0019796225,0.0011119918,0.0011846771,0.0008106418,0.0017339423,0.0031297212,0.0012243942,0.0601693],"category_scores_gemma":[0.0042062225,0.0011616362,0.001441472,0.00068716385,0.00067836983,0.0019742674,0.0033407738,0.002033162,0.020080252],"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":[0.00064780196,0.0004319765,0.0012093489,0.00057398644,0.00011001291,0.0005417512,0.0006052837,0.16567042,0.028084652,0.05366681,0.03912096,0.709337],"study_design_scores_gemma":[0.00028469818,0.0001258647,0.00041294954,0.00015380976,0.000051206756,0.0003847586,0.00011112606,0.8225366,0.01830384,0.0741411,0.08343443,0.000059623242],"about_ca_topic_score_codex":0.001064775,"about_ca_topic_score_gemma":0.0017712918,"teacher_disagreement_score":0.0601693,"about_ca_system_score_codex":0.0005873909,"about_ca_system_score_gemma":0.0010024122,"threshold_uncertainty_score":0.20128632},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.06379119,0.000109363384,0.9196491,0.00068707066,0.000024102615,0.00020842819,0.00053072453,0.001384555,0.013615506],"genre_scores_gemma":[0.47354004,0.00013037559,0.5230288,0.0000522279,0.000009031167,0.00027266835,0.00075791863,0.00027954875,0.0019293997],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99734277,0.0013357373,0.00022832534,0.0004039226,0.0005674837,0.000121800906],"domain_scores_gemma":[0.9864813,0.007762761,0.00081265764,0.0033833187,0.0010488626,0.0005110981],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.003946254,0.00064589083,0.00079753925,0.0021275126,0.002033275,0.006615938,0.0026677866,0.0011835903,0.00859307],"category_scores_gemma":[0.01843032,0.00076191983,0.0011383757,0.0015639412,0.0020153192,0.008433193,0.009241365,0.0023407938,0.0011743075],"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":[0.00017479525,0.0004690886,0.026188826,0.00084619905,0.00027318546,0.001228363,0.03720316,0.35834172,0.010598254,0.39759496,0.0051480066,0.16193344],"study_design_scores_gemma":[0.00003557749,0.000058926373,0.0059133405,0.0002492057,0.00005090353,0.00017812205,0.007461894,0.71599525,0.0021369786,0.24278262,0.025042875,0.000094357],"about_ca_topic_score_codex":0.013949216,"about_ca_topic_score_gemma":0.026470527,"teacher_disagreement_score":0.013949216,"about_ca_system_score_codex":0.0016753075,"about_ca_system_score_gemma":0.005492243,"threshold_uncertainty_score":0.028746724},"labels":[],"label_agreement":null},{"id":"W2164108194","doi":"10.1007/s13272-013-0066-z","title":"Development of a PZT phased array and FBG network for structural health monitoring based on guided Lamb waves","year":2013,"lang":"en","type":"article","venue":"CEAS Aeronautical Journal","topic":"Ultrasonics and Acoustic Wave Propagation","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Victoria","funders":"","keywords":"Lamb waves; Phased array; Beamforming; Structural health monitoring; Acoustics; Transducer; Interference (communication); SIGNAL (programming language); Phased-array optics; Noise (video); Electronic engineering; Optics; Engineering; Computer science; Surface wave; Physics; Telecommunications; Electrical engineering; Channel (broadcasting)","score_opus":0.022994723440098255,"score_gpt":0.2646475261999248,"score_spread":0.24165280275982656,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2164108194","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.16334948,0.0009132778,0.8277193,0.0003961818,0.00019488769,0.00021125322,0.00017828096,0.0012621552,0.005775174],"genre_scores_gemma":[0.4174323,0.00055273983,0.5757194,0.00013745326,0.000057304835,0.00012000657,0.00013698386,0.000037667724,0.0058061224],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99961036,0.000035777193,0.000011673745,0.00008573095,0.0002354414,0.00002102272],"domain_scores_gemma":[0.99969983,0.000072986855,0.000053077445,0.000029327193,0.00012087061,0.000023974377],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00031664062,0.00032760555,0.00033009765,0.00039290416,0.00015881087,0.00031981527,0.0006513489,0.0006095608,0.0008776041],"category_scores_gemma":[0.00048119033,0.0002979397,0.00019356831,0.00025801675,0.00023955847,0.00070489687,0.00033453363,0.00032936144,0.00044728068],"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":[0.00007979941,0.000058950765,0.0011137523,0.00010161261,0.000013068218,0.00011009293,0.00005104109,0.0025080799,0.9228292,0.0010801761,0.00029971774,0.07175448],"study_design_scores_gemma":[0.000030021822,0.00070726365,0.0049758065,0.000018826777,0.00005251676,0.001010149,0.000042544136,0.09794306,0.8844108,0.00049389753,0.010277234,0.000037913294],"about_ca_topic_score_codex":0.00064565166,"about_ca_topic_score_gemma":0.0014390594,"teacher_disagreement_score":0.0008776041,"about_ca_system_score_codex":0.00031002884,"about_ca_system_score_gemma":0.00044263093,"threshold_uncertainty_score":0.002935946},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.69908535,0.0002344613,0.2913455,0.000070663875,0.00005419455,0.00016814237,0.00023400449,0.0003816561,0.008426115],"genre_scores_gemma":[0.95545554,0.000088977744,0.041371882,0.000008574261,0.0000055671107,0.00007603473,0.00016178211,0.000035951292,0.0027956457],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9995857,0.00007684785,0.000027322352,0.00003360434,0.0002535792,0.000022970215],"domain_scores_gemma":[0.99950206,0.0001298987,0.00006427736,0.000065887754,0.00022224056,0.000015655532],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00066834426,0.0004279593,0.00027092954,0.0008270509,0.00031101055,0.00037398277,0.00053730275,0.0004102689,0.0015941937],"category_scores_gemma":[0.00079102325,0.00017946704,0.00027650566,0.00046174557,0.00023808613,0.0005181914,0.00040701087,0.0002953111,0.00026370454],"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":[0.0009947813,0.0010110213,0.02386007,0.0005754205,0.00007592697,0.00029030404,0.00042673398,0.2393688,0.40122014,0.0037721165,0.00094228116,0.3274624],"study_design_scores_gemma":[0.00006792813,0.0033216497,0.03689302,0.000045589743,0.00004768414,0.00027056236,0.00031593445,0.8108455,0.14489646,0.00054237375,0.0026913653,0.000061872386],"about_ca_topic_score_codex":0.0016878166,"about_ca_topic_score_gemma":0.0028518345,"teacher_disagreement_score":0.0016878166,"about_ca_system_score_codex":0.0002681454,"about_ca_system_score_gemma":0.00035066603,"threshold_uncertainty_score":0.005333066},"labels":[],"label_agreement":null},{"id":"W3119513293","doi":"10.1007/s13272-020-00484-5","title":"CFD-based prediction of wall-pressure spectra under a turbulent boundary layer with adverse pressure gradient","year":2021,"lang":"en","type":"article","venue":"CEAS Aeronautical Journal","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":4,"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; Université de Sherbrooke","funders":"Horizon 2020; Canadian Network for Research and Innovation in Machining Technology, Natural Sciences and Engineering Research Council of Canada","keywords":"Turbulence; Boundary layer; Direct numerical simulation; Airfoil; Mechanics; Computational fluid dynamics; Pressure gradient; Turbulence modeling; Statistical physics; Physics; Wind tunnel; Adverse pressure gradient; Flow separation; Classical mechanics; Reynolds number","score_opus":0.01018194260158959,"score_gpt":0.2068171236100554,"score_spread":0.1966351810084658,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3119513293","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.95497465,0.0002022838,0.034985002,0.0001642739,0.00014456875,0.000047303976,0.00031275698,0.0007690876,0.008400082],"genre_scores_gemma":[0.99609935,0.000038931394,0.0028798054,0.000011861373,0.000009485796,0.000008898995,0.00010042602,0.000028262508,0.00082292955],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999064,0.000014269271,0.000005681166,0.000020242733,0.00003056559,0.000022806884],"domain_scores_gemma":[0.9996165,0.00018055335,0.000029985658,0.000023732531,0.00010096166,0.000048186994],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020814709,0.00057405856,0.0006033168,0.0004936968,0.00055445824,0.00081807113,0.00059028383,0.0010396339,0.0012119844],"category_scores_gemma":[0.0008412195,0.00032309562,0.00047973168,0.00034952787,0.0005739467,0.00053178763,0.00045603697,0.00048801288,0.0002848735],"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":[0.0002883901,0.00016311531,0.0052826186,0.000067894,0.000023435563,0.00030993338,0.00005518954,0.9650486,0.018893663,0.00087300554,0.00054099347,0.008453192],"study_design_scores_gemma":[0.00000807426,0.00001133576,0.0007497691,0.000001538559,0.0000022210145,0.0000064526107,0.0000046543255,0.99772364,0.0014128269,0.000041892086,0.000033834356,0.000003753283],"about_ca_topic_score_codex":0.014250511,"about_ca_topic_score_gemma":0.0050577135,"teacher_disagreement_score":0.014250511,"about_ca_system_score_codex":0.00052060286,"about_ca_system_score_gemma":0.00078262016,"threshold_uncertainty_score":0.028335154},"labels":[],"label_agreement":null},{"id":"W4388557166","doi":"10.1007/s13272-023-00694-7","title":"Trim Strategies and Dynamic Cross-Coupling During Aerial Refueling","year":2023,"lang":"en","type":"article","venue":"CEAS Aeronautical Journal","topic":"Aerospace Engineering and Control Systems","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Royal Military College of Canada","funders":"Ministère de la Défense Nationale","keywords":"Trim; Coupling (piping); Aerospace engineering; Aeronautics; Engineering; Marine engineering; Computer science; Structural engineering; Mechanical engineering","score_opus":0.00733137643158387,"score_gpt":0.2417328795335935,"score_spread":0.2344015031020096,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4388557166","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.87720674,0.0003689182,0.103659056,0.00016957028,0.00007003672,0.00004769253,0.000054518234,0.00024129197,0.018182103],"genre_scores_gemma":[0.9982906,0.000019448711,0.00095869426,0.0000063562493,0.000002151086,0.0000031816953,0.000008004198,0.0000075704797,0.0007040385],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999155,0.000013292656,0.000003191491,0.000013919746,0.000017044815,0.000037069058],"domain_scores_gemma":[0.99974066,0.00009988132,0.000051883064,0.00002006874,0.00005038016,0.000037076075],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020919801,0.00035400208,0.0003121679,0.00041649706,0.000474562,0.0004834724,0.0003271664,0.0003584242,0.0035686265],"category_scores_gemma":[0.0009335526,0.00018680356,0.00012337034,0.00020410502,0.00021194718,0.0005338694,0.00069256115,0.00033109458,0.00030930495],"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":[0.0020822664,0.00030345347,0.010785141,0.00021408818,0.000101555466,0.0012521265,0.0006270608,0.7154909,0.09723072,0.010736835,0.0013540072,0.15982193],"study_design_scores_gemma":[0.000017465105,0.0003520578,0.008164817,0.000023098524,0.000016276861,0.00013711047,0.0003516902,0.9784008,0.009514908,0.0022248416,0.0007789113,0.000018075994],"about_ca_topic_score_codex":0.002360407,"about_ca_topic_score_gemma":0.0025899138,"teacher_disagreement_score":0.0035686265,"about_ca_system_score_codex":0.00021067848,"about_ca_system_score_gemma":0.00027924022,"threshold_uncertainty_score":0.011938214},"labels":[],"label_agreement":null},{"id":"W4393391783","doi":"10.1007/s13272-024-00731-z","title":"New smart twisting active rotor (STAR): pretest predictions","year":2024,"lang":"en","type":"article","venue":"CEAS Aeronautical Journal","topic":"Aerospace and Aviation Technology","field":"Engineering","cited_by":9,"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":"U.S. Army Combat Capabilities Development Command Aviation and Missile Center; Engineering and Physical Sciences Research Council; Korea Aerospace Research Institute; National Research Foundation of Korea; Defence Science and Technology Laboratory; Ministry of Science and ICT, South Korea; Deutsches Zentrum für Luft- und Raumfahrt; Konkuk University; National Research Foundation; U.S. Army Combat Capabilities Development Command; U.S. Army Combat Capabilities Development Command Soldier Center; University of Guelph; National Aeronautics and Space Administration","keywords":"Aerospace; Aeronautics; Aerospace engineering; Engineering; Aviation; Flight test; Rotor (electric); Test (biology); Missile; Wind tunnel; Payload (computing); Computer science; Mechanical engineering; Computer security","score_opus":0.008530611840009658,"score_gpt":0.2265668057849158,"score_spread":0.21803619394490614,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4393391783","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.94327176,0.00011882272,0.03738903,0.000093837974,0.000042135696,0.00016030937,0.0014002336,0.00067072094,0.016853057],"genre_scores_gemma":[0.9956708,0.000022764787,0.0031412246,0.0000060371785,0.0000024581911,0.000026843383,0.00024436903,0.000023651866,0.0008618533],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99984384,0.000031391406,0.0000073646793,0.000026387313,0.00006657435,0.000024396642],"domain_scores_gemma":[0.99929774,0.00029188898,0.00004381783,0.00009528792,0.00023811929,0.000033065786],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006013546,0.00034908982,0.00040100596,0.00029604966,0.00019373099,0.00027481967,0.00052346947,0.00048441923,0.0039991685],"category_scores_gemma":[0.0011975386,0.00013489202,0.00025816562,0.00021463895,0.00028387932,0.0003973231,0.00021151135,0.0002450333,0.0006947327],"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":[0.0005987579,0.00024467558,0.0074948985,0.00020813881,0.00001641303,0.00021021607,0.000093856324,0.93893945,0.021701258,0.0017602678,0.0014780755,0.02725399],"study_design_scores_gemma":[0.00006844225,0.0009224437,0.0037392015,0.000009924095,0.000012648644,0.000018696623,0.00003707234,0.9831072,0.010779222,0.00035780927,0.0009345521,0.000012671583],"about_ca_topic_score_codex":0.002150758,"about_ca_topic_score_gemma":0.0022873373,"teacher_disagreement_score":0.0039991685,"about_ca_system_score_codex":0.0002152308,"about_ca_system_score_gemma":0.00025493227,"threshold_uncertainty_score":0.013378561},"labels":[],"label_agreement":null},{"id":"W4411744189","doi":"10.1007/s13272-025-00861-y","title":"Relative kinematics for a jerk-level trajectory generation system","year":2025,"lang":"en","type":"article","venue":"CEAS Aeronautical Journal","topic":"Robotic Mechanisms and Dynamics","field":"Engineering","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 Rehabilitation Institute; University of Toronto","funders":"Technische Universität München","keywords":"Jerk; Kinematics; Trajectory; Control theory (sociology); Physics; Computer science; Classical mechanics; Artificial intelligence; Acceleration","score_opus":0.033935117927052005,"score_gpt":0.2497045880047709,"score_spread":0.2157694700777189,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4411744189","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.05854131,0.000029895795,0.9383535,0.00006318169,0.000016405618,0.000035331832,0.00003801025,0.0005646192,0.0023578345],"genre_scores_gemma":[0.93036944,0.00003072975,0.06644866,0.000016540584,0.000005562839,0.000052486466,0.00007811531,0.00003983512,0.0029585548],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99981314,0.000045402183,0.000010105102,0.00003281562,0.00008503878,0.000013532946],"domain_scores_gemma":[0.999754,0.00009185778,0.00004325746,0.000026221342,0.00007268295,0.0000119159895],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003484936,0.00040212166,0.00023614684,0.00021448285,0.00030618437,0.0004966749,0.00027966464,0.0004394726,0.0026027707],"category_scores_gemma":[0.0008066918,0.0001411932,0.00021188172,0.00014427885,0.0003256441,0.00021346296,0.00037190446,0.00035103678,0.0004004952],"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":[0.00010341033,0.000028383572,0.000816605,0.00007941368,0.0000135797045,0.00012952712,0.00018089688,0.93552214,0.02607883,0.010523213,0.00029912958,0.026224986],"study_design_scores_gemma":[0.0000057072743,0.00005758753,0.00016192927,0.0000037589946,0.0000018788297,0.00001795736,0.000007757675,0.9973188,0.0016596903,0.00034200112,0.00041926978,0.0000036051226],"about_ca_topic_score_codex":0.004062105,"about_ca_topic_score_gemma":0.002462453,"teacher_disagreement_score":0.004062105,"about_ca_system_score_codex":0.00037734173,"about_ca_system_score_gemma":0.0005728585,"threshold_uncertainty_score":0.008707106},"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":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.56457216,0.0007435317,0.40578952,0.000115305884,0.00009652543,0.00008034386,0.00020288215,0.0010125117,0.027387159],"genre_scores_gemma":[0.9052468,0.00018217484,0.091133706,0.000018225714,0.000007681419,0.000056758985,0.00009852051,0.00008133374,0.0031748007],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999163,0.000007625864,0.0000026732437,0.0000145592485,0.00004166728,0.0000170921],"domain_scores_gemma":[0.99992776,0.000019914258,0.000017626086,0.000008244149,0.000021903199,0.000004453759],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012787715,0.00039717258,0.00018077264,0.0002645164,0.0001136166,0.0003707146,0.0002502834,0.00025838675,0.0018333016],"category_scores_gemma":[0.00022334927,0.00014024616,0.00020143412,0.00020685041,0.00013875635,0.00018024613,0.00022338635,0.00022398883,0.0003430005],"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":[0.00013952848,0.00010063459,0.0009801151,0.0003153975,0.00002889938,0.00020403386,0.000050459126,0.39720744,0.5223893,0.0047879103,0.0011086959,0.07268753],"study_design_scores_gemma":[0.000028247205,0.00041255832,0.0010856132,0.000017380042,0.000018593395,0.00010201879,0.00003573343,0.8489447,0.13984585,0.0006528748,0.008836256,0.000020119176],"about_ca_topic_score_codex":0.00040089953,"about_ca_topic_score_gemma":0.0009346593,"teacher_disagreement_score":0.0018333016,"about_ca_system_score_codex":0.00021102928,"about_ca_system_score_gemma":0.00024395587,"threshold_uncertainty_score":0.0061329603},"labels":[],"label_agreement":null}]}