{"meta":{"query_hash":"4ffe033ac168","filters":{"venue":"41st  Structures, Structural Dynamics, and Materials Conference and Exhibit"},"cohort_total":2,"direct_labels_cover":0,"predictions_cover":2,"exported":2,"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/4ffe033ac168","api":"https://metacan.xera.ac/api/v1/cohort?venue=41st++Structures%2C+Structural+Dynamics%2C+and+Materials+Conference+and+Exhibit"},"results":[{"id":"W2323523344","doi":"10.2514/6.2000-1438","title":"A Dynamic Finite Element (DFE) formulation for coupled flap-lag vibrations of propeller blades","year":2000,"lang":"en","type":"article","venue":"41st  Structures, Structural Dynamics, and Materials Conference and Exhibit","topic":"Cavitation Phenomena in Pumps","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Waterloo","funders":"","keywords":"Finite element method; Lag; Vibration; Propeller; Structural engineering; Engineering; Computer science; Mechanical engineering; Acoustics; Marine engineering; Physics","score_opus":0.012066843325514632,"score_gpt":0.22232170810040702,"score_spread":0.21025486477489239,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2323523344","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99185985,0.00014525294,0.0056576272,0.00007087784,0.00032743625,0.0007599077,0.00092002924,0.00009266924,0.00016637186],"genre_scores_gemma":[0.994783,0.00028371284,0.0036850355,0.000030667055,0.00005512083,0.000048352747,0.0008948726,0.000035050798,0.00018421479],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9987432,0.00002071726,0.0005304394,0.00028221688,0.0001372004,0.0002862788],"domain_scores_gemma":[0.9994675,0.00005603316,0.000105029125,0.00018432365,0.00010361637,0.00008353006],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.000082313556,0.000284094,0.00038160064,0.000100320896,0.00015505397,0.00016407453,0.000104009145,0.00012637902,0.0006898668],"category_scores_gemma":[0.000018270683,0.00025284867,0.00004006489,0.00006755158,0.000089165005,0.00029588176,0.000029093439,0.000072089024,0.00000185551],"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":[0.0008179149,0.00002788992,0.00049819786,0.0032792045,0.00052333606,0.0000036528888,0.0070161396,0.023974866,0.47244206,0.3547332,0.00017795955,0.13650559],"study_design_scores_gemma":[0.0022830712,0.00023812515,0.03627566,0.00011235237,0.00014184952,0.000024636924,0.00041208678,0.83329344,0.013475536,0.11257446,0.00032650502,0.00084228517],"about_ca_topic_score_codex":0.00007443349,"about_ca_topic_score_gemma":0.000263449,"teacher_disagreement_score":0.8093186,"about_ca_system_score_codex":0.000049430608,"about_ca_system_score_gemma":0.000026421514,"threshold_uncertainty_score":0.9999924},"labels":[],"label_agreement":null},{"id":"W2332044052","doi":"10.2514/6.2000-1637","title":"Inflatable spacecraft using 'Rigidization-On-Command' concept","year":2000,"lang":"en","type":"article","venue":"41st  Structures, Structural Dynamics, and Materials Conference and Exhibit","topic":"Structural Analysis and Optimization","field":"Engineering","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":"","funders":"","keywords":"Inflatable; Spacecraft; Aeronautics; Aerospace engineering; Computer science; Engineering; Mechanical engineering","score_opus":0.011783122934602774,"score_gpt":0.2080441680956406,"score_spread":0.19626104516103784,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2332044052","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9971537,0.00028926868,0.00068210927,0.00006277705,0.00043305513,0.00020552064,0.00030655763,0.00014878261,0.00071824604],"genre_scores_gemma":[0.9969504,0.0006988457,0.001308246,0.000101604084,0.00021143316,0.000004149631,0.00043887238,0.000037772377,0.00024867093],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99859244,0.000039610568,0.0004128666,0.00039320617,0.0001774744,0.00038440537],"domain_scores_gemma":[0.9994433,0.000024324645,0.00007785471,0.0002358534,0.00006773956,0.00015093535],"candidate_categories":["metaepi_narrow","insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00005004466,0.00041146428,0.00051555166,0.000105318446,0.00031345582,0.00041830025,0.00013551948,0.00019334465,0.002258838],"category_scores_gemma":[0.000010494808,0.00033750536,0.00004378036,0.00012863446,0.00017421503,0.0003684432,0.0000406698,0.00014215717,0.000005263443],"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":[0.00064244226,0.00001987074,0.0056845415,0.0012733334,0.0010843448,0.00006754487,0.004816486,0.2528453,0.095521964,0.2938229,0.001238309,0.34298298],"study_design_scores_gemma":[0.0027938609,0.00018648179,0.07956683,0.00025161647,0.00038005607,0.00029519745,0.0005605871,0.8318707,0.027321486,0.052686382,0.0013966394,0.0026902151],"about_ca_topic_score_codex":0.00033302468,"about_ca_topic_score_gemma":0.00010119302,"teacher_disagreement_score":0.5790254,"about_ca_system_score_codex":0.00005096348,"about_ca_system_score_gemma":0.000018161429,"threshold_uncertainty_score":0.9999077},"labels":[],"label_agreement":null}]}