{"meta":{"query_hash":"e7a9a9730da4","filters":{"venue":"54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference"},"cohort_total":17,"direct_labels_cover":0,"predictions_cover":17,"exported":17,"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/e7a9a9730da4","api":"https://metacan.xera.ac/api/v1/cohort?venue=54th+AIAA%2FASME%2FASCE%2FAHS%2FASC+Structures%2C+Structural+Dynamics%2C+and+Materials+Conference"},"results":[{"id":"W2141202363","doi":"10.2514/6.2013-1629","title":"An implicit model for Lagrangian vortex dynamics for Horizontal Axis Wind Turbine design optimization","year":2013,"lang":"en","type":"article","venue":"54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference","topic":"Wind Energy Research and Development","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":"University of Victoria","funders":"","keywords":"Vortex; Lagrangian; Dynamics (music); Horizontal axis; Turbine; Computational fluid dynamics; Mechanics; Physics; Computer science; Aerospace engineering; Meteorology; Marine engineering; Engineering; Theoretical physics","score_opus":0.013817357028531778,"score_gpt":0.2316476632517665,"score_spread":0.2178303062232347,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2141202363","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.50018626,0.00009970314,0.49388656,0.00010500801,0.0010467757,0.0020297251,0.0022158728,0.000338802,0.00009130712],"genre_scores_gemma":[0.89837664,0.00015390712,0.096737646,0.00007244455,0.0003456307,0.00031760868,0.0036236062,0.00016654223,0.00020598093],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9961263,0.000090913694,0.0009466622,0.000985289,0.00043635338,0.0014145082],"domain_scores_gemma":[0.99786276,0.00011791944,0.00021292017,0.0006423149,0.00053113594,0.0006329695],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00029399095,0.0009412321,0.000982282,0.00029451662,0.0004893781,0.0009271055,0.0007112413,0.0005471784,0.0002940659],"category_scores_gemma":[0.000086938555,0.00084436435,0.00015233854,0.00017647102,0.00021896744,0.00091307214,0.00013196515,0.00027184718,0.000004361982],"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":[0.0011635345,0.00005057383,0.00020518848,0.0016555812,0.0007327526,0.000012359121,0.0013892445,0.74427146,0.07190532,0.09576879,0.0012327897,0.0816124],"study_design_scores_gemma":[0.0017573143,0.00034563526,0.0059626736,0.00004902364,0.000073368814,0.000040035688,0.00015365612,0.9533684,0.003835423,0.033306915,0.000029738498,0.0010777621],"about_ca_topic_score_codex":0.0005611065,"about_ca_topic_score_gemma":0.00096057274,"teacher_disagreement_score":0.39819038,"about_ca_system_score_codex":0.00038823317,"about_ca_system_score_gemma":0.00021788031,"threshold_uncertainty_score":0.99940073},"labels":[],"label_agreement":null},{"id":"W2143811188","doi":"10.2514/6.2013-1684","title":"Structural Reliability Analysis of the Advanced Composite Cargo Aircraft","year":2013,"lang":"en","type":"article","venue":"54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference","topic":"Probabilistic and Robust Engineering Design","field":"Decision Sciences","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":"Lockheed Martin (Canada)","funders":"","keywords":"Reliability (semiconductor); Composite number; Reliability engineering; Computer science; Aerospace engineering; Engineering; Physics","score_opus":0.02307055820163893,"score_gpt":0.27343284840695986,"score_spread":0.2503622902053209,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2143811188","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9872615,0.00025768564,0.005446361,0.00052981003,0.0032057355,0.0012881572,0.0015983983,0.00016325967,0.00024909808],"genre_scores_gemma":[0.9914883,0.000053281885,0.0073177507,0.0001681919,0.0001555028,0.000045852175,0.00020902455,0.000054148775,0.00050793955],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"observational","domain_scores_codex":[0.99230325,0.0007163415,0.0023712046,0.0017518983,0.0017634828,0.0010938263],"domain_scores_gemma":[0.99360985,0.00086770934,0.0012513766,0.0024237267,0.0013814062,0.0004659064],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0010546703,0.0010231099,0.0022046624,0.00055623514,0.0006690309,0.00093726564,0.002578083,0.00050773984,0.002011295],"category_scores_gemma":[0.0017083546,0.0006322774,0.00053131714,0.0014980031,0.0014289679,0.00081378926,0.0008868703,0.0005598452,0.000017900922],"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":[0.0015663729,0.000116108524,0.085166894,0.0013734368,0.0043552117,0.00004641873,0.006893795,0.13671654,0.18385181,0.42720369,0.0020600623,0.15064968],"study_design_scores_gemma":[0.0008867309,0.00010954473,0.78980815,0.000061968385,0.00058507035,0.000044305474,0.00031974984,0.08386714,0.0036757872,0.119641036,0.00008269274,0.00091778755],"about_ca_topic_score_codex":0.0019792614,"about_ca_topic_score_gemma":0.0006137309,"teacher_disagreement_score":0.7046413,"about_ca_system_score_codex":0.00022617557,"about_ca_system_score_gemma":0.0002543195,"threshold_uncertainty_score":0.99961287},"labels":[],"label_agreement":null},{"id":"W2163210830","doi":"10.2514/6.2013-1502","title":"Aircraft Wind Tunnel Characterization using Modern Design of Experiments","year":2013,"lang":"en","type":"article","venue":"54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference","topic":"Aerospace and Aviation Technology","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Canadian Society of Intestinal Research; University of Victoria","funders":"","keywords":"Wind tunnel; Characterization (materials science); Aerospace engineering; Marine engineering; Aerodynamics; Engineering; Computer science; Environmental science; Materials science; Nanotechnology","score_opus":0.0169085886172531,"score_gpt":0.21921147585183437,"score_spread":0.20230288723458126,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2163210830","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9285085,0.00015915382,0.06827173,0.000057916608,0.0012689033,0.00085043145,0.0004735585,0.00036724302,0.00004253973],"genre_scores_gemma":[0.99071515,0.0002059084,0.0081279585,0.000064698725,0.00015785111,0.000032677188,0.00050980935,0.00009816073,0.0000878185],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99737173,0.00010308476,0.00087679125,0.00061751367,0.0003306005,0.0007002592],"domain_scores_gemma":[0.99859506,0.000037193135,0.00038222727,0.0005511044,0.00024517268,0.00018926016],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.000107495514,0.0006727243,0.0008761579,0.00024594812,0.00020919723,0.0002767869,0.0004700632,0.000519278,0.00075261487],"category_scores_gemma":[0.000041141022,0.0006355493,0.000076103875,0.00017749591,0.00030222733,0.0007251414,0.00017611314,0.0002580597,0.00001164506],"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":[0.000043633678,0.000008173752,0.00046408913,0.00023015126,0.00011814544,0.0000039442207,0.00069889677,0.0015440378,0.9814535,0.006082893,0.00003389334,0.009318687],"study_design_scores_gemma":[0.0022053777,0.00024173914,0.16452959,0.00023939648,0.00017369275,0.00013008456,0.00049616594,0.3841244,0.40359986,0.04227232,0.00003130144,0.0019560757],"about_ca_topic_score_codex":0.0003530797,"about_ca_topic_score_gemma":0.000039774284,"teacher_disagreement_score":0.5778536,"about_ca_system_score_codex":0.0001453599,"about_ca_system_score_gemma":0.000071370814,"threshold_uncertainty_score":0.9996096},"labels":[],"label_agreement":null},{"id":"W2313700874","doi":"10.2514/6.2013-1467","title":"Two-Level Domain Decomposition Method for Uncertainty Quantification","year":2013,"lang":"en","type":"article","venue":"54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference","topic":"Probabilistic and Robust Engineering Design","field":"Decision Sciences","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":"Carleton University","funders":"Natural Sciences and Engineering Research Council of Canada; Canada Research Chairs; Ontario Innovation Trust","keywords":"Computer science; Decomposition; Domain (mathematical analysis); Domain decomposition methods; Mathematics; Physics; Chemistry; Finite element method","score_opus":0.06990014270604977,"score_gpt":0.3629099515374286,"score_spread":0.29300980883137884,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2313700874","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":[0.41428736,0.00011823132,0.5785492,0.0006428117,0.0027711645,0.0016688367,0.0015826313,0.00019164116,0.00018813957],"genre_scores_gemma":[0.79324424,0.00003615318,0.20488362,0.00018887379,0.0003447695,0.0001699674,0.00065204845,0.00005689609,0.00042342173],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.993907,0.00059652614,0.001786792,0.0016623841,0.0010279997,0.0010193161],"domain_scores_gemma":[0.99504125,0.0012442629,0.00085806,0.001211294,0.0011924937,0.00045260933],"candidate_categories":["metaepi_narrow","scholarly_communication","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0019495888,0.0008554184,0.0012803457,0.00040822013,0.0007159029,0.0017604149,0.0013528379,0.00046330717,0.0011560762],"category_scores_gemma":[0.001259672,0.00064009224,0.00022172226,0.0003903525,0.00046420388,0.00080009596,0.00028665666,0.00032153726,0.000052105297],"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":[0.00039302823,0.00002563168,0.00016728051,0.0002459367,0.00015166242,0.0000064493215,0.00078390294,0.0041634864,0.108964145,0.7949925,0.0014113152,0.08869468],"study_design_scores_gemma":[0.0018566384,0.00020018275,0.044860624,0.0000820645,0.00010664242,0.00013828736,0.0006197402,0.16720422,0.005668065,0.777734,0.0003702184,0.0011593245],"about_ca_topic_score_codex":0.0013787455,"about_ca_topic_score_gemma":0.0005482177,"teacher_disagreement_score":0.3789569,"about_ca_system_score_codex":0.00022985888,"about_ca_system_score_gemma":0.00023272348,"threshold_uncertainty_score":0.999757},"labels":[],"label_agreement":null},{"id":"W2315270790","doi":"10.2514/6.2013-1876","title":"Crack Arrestment of Bonded Composite Joints","year":2013,"lang":"en","type":"article","venue":"54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference","topic":"Mechanical Behavior of Composites","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lockheed Martin (Canada)","funders":"","keywords":"Composite number; Materials science; Structural engineering; Composite material; Forensic engineering; Engineering","score_opus":0.009577686842825787,"score_gpt":0.21375840391921516,"score_spread":0.20418071707638938,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2315270790","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99286324,0.00037018565,0.0008826995,0.00014166918,0.002686448,0.001207649,0.000825446,0.00045667164,0.0005659795],"genre_scores_gemma":[0.9909409,0.00021984053,0.007678907,0.00011710999,0.00021218833,0.00007293092,0.0004860473,0.00012452957,0.00014750626],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.995777,0.00017191084,0.0014491333,0.0008806532,0.00066988094,0.0010514223],"domain_scores_gemma":[0.99757487,0.00012905334,0.00042026438,0.0009899994,0.00034988121,0.0005359473],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00017560956,0.0010258885,0.0014761194,0.0002550833,0.00022354633,0.0005261343,0.0008932983,0.00048581895,0.002554571],"category_scores_gemma":[0.000060927356,0.0009109138,0.0001871053,0.00019336141,0.00040063052,0.0005384235,0.00038201877,0.0004710951,0.000057946072],"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":[0.00012991106,0.000025271367,0.00084604765,0.0007669684,0.00024333077,0.000023586384,0.00034049727,0.0001919026,0.92273176,0.060852084,0.0004964325,0.0133521985],"study_design_scores_gemma":[0.0030001514,0.00042048446,0.34818998,0.00043121388,0.0003649422,0.00024790916,0.00016426765,0.022646626,0.52641875,0.09530762,0.00022784524,0.0025802108],"about_ca_topic_score_codex":0.0006584504,"about_ca_topic_score_gemma":0.00015691943,"teacher_disagreement_score":0.39631304,"about_ca_system_score_codex":0.0001830266,"about_ca_system_score_gemma":0.00006792737,"threshold_uncertainty_score":0.99933416},"labels":[],"label_agreement":null},{"id":"W2316665742","doi":"10.2514/6.2013-1699","title":"A Robust ASE Correlation and Analysis Method","year":2013,"lang":"en","type":"article","venue":"54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference","topic":"Probabilistic and Robust Engineering Design","field":"Decision Sciences","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; Correlation; Mathematics","score_opus":0.048360729124806774,"score_gpt":0.29882363635840925,"score_spread":0.2504629072336025,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2316665742","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6032028,0.00031633314,0.39217165,0.0003574782,0.0017440057,0.0008794071,0.0007622086,0.00019969077,0.0003664241],"genre_scores_gemma":[0.94048166,0.00011813784,0.057437472,0.0001660794,0.00021662262,0.00004891293,0.00031478822,0.00004997161,0.001166371],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9939324,0.0006278802,0.0016474649,0.0017052343,0.0011645108,0.0009224673],"domain_scores_gemma":[0.9956899,0.00096405635,0.0007791776,0.0011687077,0.0007996277,0.00059849216],"candidate_categories":["metaepi_narrow","scholarly_communication","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0014915653,0.0008784335,0.001626871,0.00078456855,0.00057030166,0.002026769,0.0010005395,0.0005458243,0.0032009934],"category_scores_gemma":[0.0016535805,0.0006423314,0.00022310957,0.0009613244,0.0005706479,0.00094568543,0.0004753366,0.00043599782,0.00004577825],"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":[0.0005982487,0.000061954524,0.01509015,0.00057761587,0.002041712,0.000090790614,0.0034169813,0.03972209,0.019362241,0.6156948,0.0028879743,0.30045545],"study_design_scores_gemma":[0.0010348441,0.00014244036,0.3514943,0.000045276465,0.000559118,0.00015817962,0.00042806077,0.4419566,0.00054728525,0.20229937,0.0002050772,0.0011294273],"about_ca_topic_score_codex":0.0014655923,"about_ca_topic_score_gemma":0.00041859676,"teacher_disagreement_score":0.41339543,"about_ca_system_score_codex":0.0001331612,"about_ca_system_score_gemma":0.00015970664,"threshold_uncertainty_score":0.9996028},"labels":[],"label_agreement":null},{"id":"W2316937867","doi":"10.2514/6.2013-1809","title":"Smeared Stiffeners in Panel for Mesh Simplification at Conceptual Design Phase","year":2013,"lang":"en","type":"article","venue":"54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference","topic":"Innovations in Concrete and Construction Materials","field":"Engineering","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":"Bombardier (Canada)","funders":"","keywords":"Computer science; Phase (matter); Engineering drawing; Engineering; Physics","score_opus":0.03937969892610799,"score_gpt":0.25494365450591716,"score_spread":0.21556395557980917,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2316937867","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97694653,0.00012311508,0.015007454,0.0001355191,0.0034390895,0.002092329,0.0016703935,0.00040239806,0.00018316777],"genre_scores_gemma":[0.98740345,0.00016412168,0.00964193,0.00015748196,0.00036922767,0.0004194683,0.0014835784,0.00011046957,0.00025024946],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9962352,0.00019631156,0.0013808549,0.00088113436,0.00034975706,0.0009567339],"domain_scores_gemma":[0.9980764,0.00019957755,0.0003765419,0.00065078767,0.00046655713,0.00023013153],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00033257788,0.00081909384,0.0010099108,0.00036114192,0.00038605655,0.00062431616,0.0005481546,0.0005233444,0.001745258],"category_scores_gemma":[0.00016452553,0.0007865228,0.00009861996,0.00028403706,0.00057332375,0.0006649157,0.00014746837,0.0002594515,0.000025826756],"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":[0.00052322226,0.000014147227,0.0002110064,0.0005517901,0.00024576002,0.0000097251295,0.0012458491,0.001048923,0.77266943,0.1623858,0.0016881952,0.059406143],"study_design_scores_gemma":[0.020877333,0.0009711581,0.04863154,0.00045793387,0.00047424404,0.0005651735,0.0041342876,0.2149368,0.53819096,0.16123165,0.002657338,0.0068716053],"about_ca_topic_score_codex":0.00032437334,"about_ca_topic_score_gemma":0.0001344815,"teacher_disagreement_score":0.23447847,"about_ca_system_score_codex":0.00037045605,"about_ca_system_score_gemma":0.00013350934,"threshold_uncertainty_score":0.99945855},"labels":[],"label_agreement":null},{"id":"W2319226720","doi":"10.2514/6.2013-1861","title":"Strouhal Frequency Influence on the Vibration Specification for a Flat Blade Antenna Subject to Upstream Proturbances","year":2013,"lang":"en","type":"article","venue":"54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference","topic":"Fluid Dynamics and Vibration Analysis","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":"Lockheed Martin (Canada)","funders":"","keywords":"Strouhal number; Blade (archaeology); Vibration; Acoustics; Upstream (networking); Antenna (radio); Subject (documents); Structural engineering; Computer science; Physics; Engineering; Electrical engineering; Telecommunications; Mechanics; Turbulence","score_opus":0.01029652864183235,"score_gpt":0.2122709893049326,"score_spread":0.20197446066310026,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2319226720","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9779778,0.00009305334,0.015744468,0.0011749627,0.00097648305,0.0025561934,0.0009270192,0.00029485673,0.0002551749],"genre_scores_gemma":[0.9936218,0.0001702345,0.0042201527,0.0003535098,0.00034043728,0.00043642276,0.00063520344,0.00008261843,0.00013960345],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99690026,0.0001293612,0.00094804104,0.0008489505,0.00043572753,0.000737658],"domain_scores_gemma":[0.9980792,0.00015361713,0.0002890166,0.00077204773,0.00043899356,0.0002671418],"candidate_categories":["metaepi_narrow","scholarly_communication"],"consensus_categories":[],"category_scores_codex":[0.00022832691,0.0007428938,0.0007016042,0.0002680594,0.00046553698,0.0012504715,0.0006665411,0.00029549169,0.00056140806],"category_scores_gemma":[0.00017744517,0.00054891163,0.0001425414,0.00032411393,0.0002347316,0.00078318105,0.00009038014,0.00029247743,0.000032747437],"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":[0.00022670186,0.000016932041,0.001117548,0.0004397103,0.00032503638,0.00000382969,0.0012030314,0.0051421113,0.539767,0.43907037,0.00059507263,0.012092645],"study_design_scores_gemma":[0.0015572672,0.0006133107,0.23767966,0.0002690425,0.0002191462,0.00005107854,0.000730473,0.57811445,0.069739014,0.10849073,0.0002388354,0.0022969856],"about_ca_topic_score_codex":0.00067009515,"about_ca_topic_score_gemma":0.0010504158,"teacher_disagreement_score":0.57297236,"about_ca_system_score_codex":0.00019083622,"about_ca_system_score_gemma":0.000081537786,"threshold_uncertainty_score":0.9997863},"labels":[],"label_agreement":null},{"id":"W2319817956","doi":"10.2514/6.2013-1631","title":"Micromechanics Investigation of Wind Turbine Blade Fatigue Behavior Considering Multi-Axial Loading","year":2013,"lang":"en","type":"article","venue":"54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference","topic":"Mechanical Behavior of Composites","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Victoria","funders":"","keywords":"Micromechanics; Turbine blade; Materials science; Blade (archaeology); Structural engineering; Turbine; Mechanical engineering; Composite material; Engineering; Composite number","score_opus":0.02462247627852474,"score_gpt":0.2363132315132509,"score_spread":0.21169075523472616,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2319817956","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9917237,0.00024408965,0.0029836874,0.000066600696,0.0024119061,0.0013746879,0.00072404876,0.00043659227,0.00003467498],"genre_scores_gemma":[0.98014593,0.000119208955,0.018707182,0.000060744387,0.0002013649,0.000067871515,0.00050641556,0.00014078473,0.000050470757],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9959723,0.00015824512,0.0014884401,0.00088451063,0.0005248751,0.0009716815],"domain_scores_gemma":[0.9977673,0.00013302667,0.00048468096,0.0007442546,0.00036328737,0.00050744246],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00020280239,0.000996057,0.0012970368,0.00032356207,0.00025302023,0.0005296198,0.0007052874,0.0006156816,0.0010923394],"category_scores_gemma":[0.00011631097,0.0009597495,0.0001550743,0.00022687759,0.00040390404,0.0006986666,0.000333997,0.0005615523,0.000015910833],"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":[0.000033139,0.000009226253,0.0011783313,0.0004580234,0.0000933217,0.00001496784,0.0004191337,0.0002339743,0.982173,0.01039296,0.000042633917,0.004951288],"study_design_scores_gemma":[0.0022699528,0.0002204229,0.12915887,0.00036555433,0.0003464063,0.00024523007,0.0002174354,0.03925496,0.8119078,0.014184475,0.000022626158,0.0018062484],"about_ca_topic_score_codex":0.0007433843,"about_ca_topic_score_gemma":0.00024050858,"teacher_disagreement_score":0.17026518,"about_ca_system_score_codex":0.00019621736,"about_ca_system_score_gemma":0.00009395695,"threshold_uncertainty_score":0.99982077},"labels":[],"label_agreement":null},{"id":"W2320594082","doi":"10.2514/6.2013-1938","title":"Model Selection Methods for Nonlinear Aeroelastic Systems Using Wind Tunnel Data","year":2013,"lang":"en","type":"article","venue":"54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference","topic":"Probabilistic and Robust Engineering Design","field":"Decision Sciences","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; Carleton University","funders":"","keywords":"Aeroelasticity; Wind tunnel; Nonlinear system; Selection (genetic algorithm); Computer science; Aerodynamics; Structural engineering; Aerospace engineering; Marine engineering; Engineering; Physics; Artificial intelligence","score_opus":0.17896040813205374,"score_gpt":0.39520401450306974,"score_spread":0.216243606371016,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2320594082","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":[0.35728002,0.0002762884,0.6348913,0.00008752185,0.0036468667,0.0015259805,0.0020684092,0.0001797177,0.0000439012],"genre_scores_gemma":[0.7415689,0.000044874843,0.25678122,0.00006269096,0.00051455514,0.00004172139,0.0005072365,0.0000794393,0.0003993367],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99340683,0.00055306865,0.0019094254,0.0020170095,0.00093633303,0.0011773254],"domain_scores_gemma":[0.99462044,0.0010974115,0.00087589474,0.001703574,0.0011966596,0.00050600106],"candidate_categories":["metaepi_narrow","scholarly_communication"],"consensus_categories":[],"category_scores_codex":[0.002096124,0.00095850247,0.0015660853,0.00042468775,0.0007361538,0.0023115615,0.0021977432,0.00059408287,0.00036161704],"category_scores_gemma":[0.002724051,0.00071948225,0.00014473457,0.00044713297,0.00048270533,0.0013678723,0.0007815302,0.0004166524,0.000017493505],"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":[0.0009510578,0.00008732405,0.00056109345,0.001977077,0.0008713448,0.000017795539,0.0015340919,0.32204166,0.27092606,0.27948925,0.003558165,0.11798506],"study_design_scores_gemma":[0.0008270831,0.000113951304,0.0031805863,0.000090414076,0.00016425607,0.00017057871,0.00021193235,0.90257823,0.0006156419,0.09103043,0.00017238564,0.0008444959],"about_ca_topic_score_codex":0.0009689248,"about_ca_topic_score_gemma":0.00016343877,"teacher_disagreement_score":0.58053654,"about_ca_system_score_codex":0.00022791015,"about_ca_system_score_gemma":0.00045849066,"threshold_uncertainty_score":0.9995256},"labels":[],"label_agreement":null},{"id":"W2320736119","doi":"10.2514/6.2013-1468","title":"Data Assimilation for Large-Scale Computational Models","year":2013,"lang":"en","type":"article","venue":"54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference","topic":"Meteorological Phenomena and Simulations","field":"Earth and Planetary Sciences","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":"Carleton University","funders":"Natural Sciences and Engineering Research Council of Canada; Canada Research Chairs; Ontario Innovation Trust","keywords":"Data assimilation; Computer science; Scale (ratio); Assimilation (phonology); Meteorology; Physics","score_opus":0.046164506877801874,"score_gpt":0.25758933367872117,"score_spread":0.21142482680091929,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2320736119","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.93340075,0.0002026763,0.04247128,0.0005547219,0.0015285579,0.0014359053,0.019092562,0.00016400695,0.0011495425],"genre_scores_gemma":[0.9557674,0.000056994828,0.023370542,0.00047076866,0.0003457684,0.00001680138,0.019755362,0.000019678651,0.0001966701],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99654895,0.00020204345,0.00086577435,0.0010753878,0.00047657875,0.00083129253],"domain_scores_gemma":[0.9978581,0.00036445807,0.0003876113,0.00068603794,0.0003293576,0.00037444232],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00038456646,0.0005471176,0.00071924296,0.0001466936,0.00073495245,0.00076040655,0.0008535786,0.00032222996,0.0060959663],"category_scores_gemma":[0.00012742328,0.00042637758,0.000083124876,0.00015021801,0.00026177304,0.0013059292,0.00017478892,0.00023232042,0.00003525952],"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":[0.001305905,0.00009374401,0.04016753,0.0011097956,0.00067384564,0.00001895384,0.0026029071,0.19774644,0.002566707,0.5564943,0.00537365,0.19184624],"study_design_scores_gemma":[0.000608897,0.00008329994,0.24490327,0.00001094095,0.00003857584,0.00001155437,0.00008757644,0.48808488,0.000018552342,0.26563296,0.00017294253,0.00034656117],"about_ca_topic_score_codex":0.0010610749,"about_ca_topic_score_gemma":0.0026858496,"teacher_disagreement_score":0.29086134,"about_ca_system_score_codex":0.000023978115,"about_ca_system_score_gemma":0.00012180003,"threshold_uncertainty_score":0.9998188},"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":"W2329298154","doi":"10.2514/6.2013-1678","title":"Knowledge Based Approach to Wing Weight and Stiffness Estimation at Early Stages of Aircraft Design","year":2013,"lang":"en","type":"article","venue":"54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference","topic":"Aerospace and Aviation Technology","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Bombardier (Canada)","funders":"","keywords":"Leverage (statistics); Computer science; Stiffness; Flexibility (engineering); Multidisciplinary approach; Wing; Conceptual design; Artificial neural network; Artificial intelligence; Industrial engineering; Engineering; Aerospace engineering; Structural engineering; Mathematics; Human–computer interaction","score_opus":0.011130950516241073,"score_gpt":0.2115943773050595,"score_spread":0.20046342678881843,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2329298154","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9346009,0.00028419253,0.062472623,0.000101972764,0.0006918215,0.0010177006,0.0002901701,0.00039705288,0.00014357138],"genre_scores_gemma":[0.9766732,0.000082617546,0.022609109,0.000042555705,0.00008672304,0.000090272726,0.00019701169,0.00007833041,0.00014017538],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.99756616,0.00011950759,0.00072030525,0.00067931943,0.0002709551,0.00064371986],"domain_scores_gemma":[0.99866205,0.00009494001,0.00023581569,0.00050526974,0.00024260732,0.0002593391],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00016634629,0.0006441931,0.00086059474,0.00030493693,0.00024621468,0.00029099005,0.00040901618,0.00043608874,0.000220757],"category_scores_gemma":[0.00008241729,0.0005789874,0.00005961778,0.00022892053,0.00032007287,0.0004706404,0.00022167778,0.00023960508,0.000013277152],"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":[0.00046902147,0.00006998884,0.008315424,0.0050399154,0.00057725736,0.000014903415,0.00566146,0.01998362,0.66658884,0.114936724,0.0012960756,0.17704676],"study_design_scores_gemma":[0.00276075,0.0003414382,0.5239955,0.0003367863,0.000204516,0.00007354376,0.00037434377,0.3059918,0.14072828,0.022996409,0.0000917373,0.0021048565],"about_ca_topic_score_codex":0.00031872452,"about_ca_topic_score_gemma":0.0001066205,"teacher_disagreement_score":0.52586055,"about_ca_system_score_codex":0.00014859518,"about_ca_system_score_gemma":0.0000635522,"threshold_uncertainty_score":0.99966615},"labels":[],"label_agreement":null},{"id":"W2330124367","doi":"10.2514/6.2013-1810","title":"Impact of Wing Box Geometrical Parameters on Stick Model Prediction Accuracy","year":2013,"lang":"en","type":"article","venue":"54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference","topic":"Probabilistic and Robust Engineering Design","field":"Decision Sciences","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":"Bombardier (Canada)","funders":"","keywords":"Wing; Computer science; Engineering; Structural engineering","score_opus":0.05763931188743964,"score_gpt":0.3186414711913,"score_spread":0.26100215930386034,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2330124367","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9365922,0.00009520845,0.05868058,0.000106035644,0.0017373003,0.0009969687,0.0013917545,0.0001921543,0.000207782],"genre_scores_gemma":[0.9871954,0.000096872674,0.011955416,0.000075969634,0.0001868576,0.000041720188,0.00018541311,0.00006254733,0.00019981572],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99376065,0.00031737192,0.0019003077,0.0014049555,0.0015617759,0.0010549597],"domain_scores_gemma":[0.99501574,0.0013970392,0.00091640063,0.0012525271,0.00083780737,0.0005804926],"candidate_categories":["metaepi_narrow","scholarly_communication","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00090661505,0.00091064326,0.0014873552,0.0008309035,0.00035667836,0.001260491,0.0013450732,0.0005316959,0.0009970726],"category_scores_gemma":[0.004619989,0.0006252077,0.0003172114,0.00072589674,0.000626164,0.0011401933,0.00038091955,0.0005106694,0.000035040168],"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":[0.002269665,0.00023176747,0.012347488,0.0008347494,0.0013114837,0.000061685794,0.0030301407,0.3859037,0.10183459,0.23638089,0.0060445936,0.24974926],"study_design_scores_gemma":[0.0013270652,0.00067833083,0.3234404,0.00012607074,0.00012132204,0.000089255016,0.0001851734,0.4878608,0.0018610966,0.18337041,0.000012056824,0.0009280079],"about_ca_topic_score_codex":0.0010726061,"about_ca_topic_score_gemma":0.000029272835,"teacher_disagreement_score":0.3110929,"about_ca_system_score_codex":0.00031082082,"about_ca_system_score_gemma":0.00033235128,"threshold_uncertainty_score":0.99991614},"labels":[],"label_agreement":null},{"id":"W2330592822","doi":"10.2514/6.2013-1523","title":"Ultra-Thin Highly Deformable Composite Mirrors","year":2013,"lang":"en","type":"article","venue":"54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference","topic":"Adaptive optics and wavefront sensing","field":"Physics and Astronomy","cited_by":17,"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; California Institute of Technology","keywords":"Composite number; Materials science; Computer science; Composite material","score_opus":0.010928476290403728,"score_gpt":0.2234983020090184,"score_spread":0.21256982571861469,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2330592822","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9863518,0.00011752472,0.0032024365,0.0003227397,0.0021020342,0.0010416075,0.0013284902,0.00017189492,0.0053614876],"genre_scores_gemma":[0.9891256,0.000048474016,0.0074341316,0.0002331709,0.0005016791,0.000033111348,0.001274386,0.00011169309,0.001237727],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.9956331,0.00018801176,0.0011390196,0.0011461478,0.0005214351,0.0013722309],"domain_scores_gemma":[0.997418,0.00010079352,0.00068526744,0.000776796,0.00046953905,0.00054962235],"candidate_categories":["metaepi_narrow","scholarly_communication","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00019432591,0.0011127677,0.0012593219,0.0002055876,0.00081959175,0.0012000275,0.0006574148,0.00032350147,0.0019419641],"category_scores_gemma":[0.000020656504,0.0009396306,0.00021538431,0.00018313868,0.0005818688,0.0009248976,0.0003032616,0.0005503606,0.00008166222],"study_design_candidate":"theoretical_or_conceptual","study_design_consensus":"theoretical_or_conceptual","about_ca_topic_candidate":true,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0003488212,0.000065149514,0.008800527,0.00038637585,0.0007963687,0.000032843953,0.0019696928,0.0003086352,0.2090282,0.7378188,0.0009287625,0.03951587],"study_design_scores_gemma":[0.0068974914,0.0006578848,0.37489873,0.00055184023,0.0006733909,0.0002661067,0.0034605504,0.06267416,0.10857827,0.43275845,0.0021484143,0.006434697],"about_ca_topic_score_codex":0.00726672,"about_ca_topic_score_gemma":0.00028293312,"teacher_disagreement_score":0.36609823,"about_ca_system_score_codex":0.00013830332,"about_ca_system_score_gemma":0.00015275549,"threshold_uncertainty_score":0.9998368},"labels":[],"label_agreement":null},{"id":"W2333505503","doi":"10.2514/6.2013-1715","title":"Blade Sailing Phenomenon Modeling for Feedback Control","year":2013,"lang":"en","type":"article","venue":"54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference","topic":"Aeroelasticity and Vibration Control","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":"Carleton University","funders":"","keywords":"Control theory (sociology); Aeroelasticity; Nonlinear system; Rotor (electric); Aerodynamics; Helicopter rotor; Discretization; Blade (archaeology); Galerkin method; Flapping; Computer science; Blade element theory; Controller (irrigation); Elevator; Actuator; Engineering; Physics; Aerospace engineering; Structural engineering; Mathematics; Mechanical engineering; Mathematical analysis; Control (management)","score_opus":0.009321421201920421,"score_gpt":0.1972072194385199,"score_spread":0.18788579823659948,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2333505503","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.7781915,0.00037983342,0.21448264,0.0002603693,0.0026109212,0.001868401,0.0012930136,0.00055553165,0.00035775412],"genre_scores_gemma":[0.99225557,0.000168282,0.0053831683,0.00029940982,0.0008686642,0.00020835652,0.0005124958,0.00014309649,0.00016095839],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99617374,0.0001189667,0.0012067575,0.000894601,0.00038998402,0.0012159526],"domain_scores_gemma":[0.9981093,0.00021826917,0.00028112743,0.0005626268,0.0003991455,0.00042954742],"candidate_categories":["metaepi_narrow","scholarly_communication","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00022745678,0.0009640436,0.0012344578,0.00020739733,0.00051928207,0.0010454537,0.0005940947,0.0005510967,0.0011945552],"category_scores_gemma":[0.00015286666,0.0008859097,0.0001724558,0.00013386745,0.00023749111,0.000908363,0.0001198388,0.0004507305,0.00003230269],"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":[0.0014018525,0.00005227984,0.000436282,0.0037148732,0.0017663264,0.000021820793,0.003443136,0.20142598,0.41744554,0.265423,0.0013255102,0.103543386],"study_design_scores_gemma":[0.0033195643,0.00014993853,0.0031103026,0.0000998832,0.00017399275,0.000038447204,0.00034083222,0.9493654,0.0037632647,0.03836083,0.000120681754,0.0011568955],"about_ca_topic_score_codex":0.0003937046,"about_ca_topic_score_gemma":0.00035950597,"teacher_disagreement_score":0.7479394,"about_ca_system_score_codex":0.00019429385,"about_ca_system_score_gemma":0.00010298306,"threshold_uncertainty_score":0.99999154},"labels":[],"label_agreement":null},{"id":"W2333643134","doi":"10.2514/6.2013-1892","title":"Vibration Analysis of String-Harnessed Beam Structures: A Homogenization Approach","year":2013,"lang":"en","type":"article","venue":"54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference","topic":"Vibration and Dynamic Analysis","field":"Engineering","cited_by":12,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Waterloo","funders":"Air Force Office of Scientific Research","keywords":"Homogenization (climate); Vibration; Structural engineering; Computer science; Beam (structure); Materials science; Mechanical engineering; Physics; Engineering; Acoustics","score_opus":0.0072392042085846235,"score_gpt":0.1973002006304121,"score_spread":0.19006099642182747,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2333643134","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.8542298,0.0001992469,0.14164446,0.00006115064,0.0008182023,0.00086294074,0.0011526496,0.00040354452,0.0006279885],"genre_scores_gemma":[0.98878807,0.0002494557,0.005931922,0.000088030036,0.00018602039,0.000067320616,0.0044449717,0.00009772599,0.00014645711],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9958677,0.00018038302,0.0015218012,0.0009852033,0.0006730358,0.00077187],"domain_scores_gemma":[0.997531,0.000078517456,0.0006130719,0.00089221157,0.0005364864,0.00034868895],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0002009468,0.00093481893,0.0016080745,0.000986866,0.00033086524,0.00075299386,0.00064756564,0.0005681332,0.0016157833],"category_scores_gemma":[0.00010090449,0.0008429895,0.0003082206,0.0012828854,0.0003467853,0.0009598405,0.00016615666,0.00034272386,0.0000081677945],"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":[0.00031153802,0.00007999945,0.0061025284,0.0024469052,0.008739725,0.000013847992,0.004311262,0.30495834,0.18331645,0.44458714,0.00050177553,0.044630483],"study_design_scores_gemma":[0.0011098963,0.000081515675,0.1608777,0.000038385988,0.0015962487,0.000024522797,0.00068338827,0.80948865,0.009522367,0.015305571,0.000029521532,0.0012422166],"about_ca_topic_score_codex":0.0009557519,"about_ca_topic_score_gemma":0.00065055286,"teacher_disagreement_score":0.5045303,"about_ca_system_score_codex":0.00018543273,"about_ca_system_score_gemma":0.00011023929,"threshold_uncertainty_score":0.9994021},"labels":[],"label_agreement":null}]}