{"meta":{"query_hash":"1b50d9397fbb","filters":{"venue":"Frontiers in Aerospace Engineering"},"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/1b50d9397fbb","api":"https://metacan.xera.ac/api/v1/cohort?venue=Frontiers+in+Aerospace+Engineering"},"results":[{"id":"W4292582824","doi":"10.3389/fpace.2022.951987","title":"Design and test a converging and de Laval nozzle using additive manufacturing","year":2022,"lang":"en","type":"article","venue":"Frontiers in Aerospace Engineering","topic":"Fluid Dynamics and Turbulent Flows","field":"Engineering","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":"Division of Electrical, Communications and Cyber Systems; North Carolina State University; National Science Foundation","keywords":"Nozzle; Surface roughness; Mechanical engineering; Aerospace; Fused filament fabrication; Surface finish; Fluent; Compressibility; Isentropic process; Computer science; Engineering; 3D printing; Materials science; Aerospace engineering; Computational fluid dynamics; Mechanics; Physics; Composite material","score_opus":0.004062776365238085,"score_gpt":0.16501469668515995,"score_spread":0.16095192031992187,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4292582824","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.67646575,0.0015566046,0.32094598,0.000019196968,0.00060534326,0.00019069579,0.00001811351,0.00017343406,0.000024881885],"genre_scores_gemma":[0.91471726,0.00026953127,0.08481734,0.000013377996,0.000037266465,0.000039171773,0.000004460085,0.00006625267,0.000035322242],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9991331,0.00001796118,0.00013976842,0.00020826602,0.00011382883,0.00038708633],"domain_scores_gemma":[0.9996815,0.00010139552,0.000017458557,0.00010375793,0.000004697076,0.00009119827],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00021276869,0.00019663954,0.00020800032,0.00019920131,0.00010303424,0.000047102807,0.000085263644,0.000047378846,0.0000088875995],"category_scores_gemma":[0.000026516764,0.0002559677,0.000022056898,0.00012842208,0.000020357325,0.00012221797,0.00010538351,0.00034745794,2.4310555e-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":[0.0000052717705,0.0000066893203,0.0035973194,0.000047647412,0.000022744387,0.000041850657,0.0005934239,0.99050164,0.0041540735,0.00003082715,0.00033244846,0.00066603493],"study_design_scores_gemma":[0.00041242392,0.000022883487,0.0016416756,0.000036868423,0.00001196249,0.000047528476,0.00015838188,0.99434584,0.0023844873,0.00002758972,0.0006365015,0.0002738696],"about_ca_topic_score_codex":0.000024732244,"about_ca_topic_score_gemma":0.0000015242356,"teacher_disagreement_score":0.2382515,"about_ca_system_score_codex":0.00029276792,"about_ca_system_score_gemma":0.000014244387,"threshold_uncertainty_score":0.9999893},"labels":[],"label_agreement":null},{"id":"W4309215747","doi":"10.3389/fpace.2022.975158","title":"Review of experimental investigations of wings in ground effect at low Reynolds numbers","year":2022,"lang":"en","type":"article","venue":"Frontiers in Aerospace Engineering","topic":"Aerodynamics and Fluid Dynamics Research","field":"Engineering","cited_by":20,"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":"Ground effect (cars); Lift-induced drag; Vortex lift; Delta wing; Wing; Lift-to-drag ratio; Drag; Aerodynamics; Reynolds number; Chord (peer-to-peer); Wing twist; Lift (data mining); Wingtip vortices; Vortex; Mechanics; Aerospace engineering; Angle of attack; Physics; Lift coefficient; Engineering; Horseshoe vortex; Computer science; Turbulence; Vorticity","score_opus":0.004355994453751945,"score_gpt":0.2158733679977959,"score_spread":0.21151737354404396,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4309215747","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9658332,0.029819183,0.0029809347,0.000032858326,0.00059645384,0.0004338184,0.00002668398,0.000057528556,0.00021937562],"genre_scores_gemma":[0.9922845,0.00240431,0.004963553,0.000012571205,0.000010233416,0.00015072119,0.00003465841,0.00005915859,0.00008032246],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9987822,0.00004347821,0.00038973385,0.00018422864,0.00029176482,0.00030860226],"domain_scores_gemma":[0.99956936,0.000047738908,0.000044952732,0.00025758176,0.000014456181,0.00006589806],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000489646,0.00017610639,0.0004272243,0.0002969725,0.000030329506,0.0000054283346,0.00025150654,0.00005267641,0.000027436272],"category_scores_gemma":[0.000062136,0.00022016723,0.00008512052,0.00085390266,0.000055834458,0.00009623638,0.0001751605,0.0003590419,7.043922e-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":[0.000016754257,0.00005097421,0.021996876,0.004976496,0.000047927788,0.000014046846,0.0009499916,0.8421323,0.12630817,0.0002915322,0.0030780833,0.00013684429],"study_design_scores_gemma":[0.0008427256,0.00011447682,0.004628688,0.0025033378,0.000010504327,0.0000070708584,0.00028966204,0.98247075,0.008111632,0.00001377739,0.000637791,0.0003695649],"about_ca_topic_score_codex":0.00006468832,"about_ca_topic_score_gemma":0.000020604064,"teacher_disagreement_score":0.14033847,"about_ca_system_score_codex":0.00096165336,"about_ca_system_score_gemma":0.000020772413,"threshold_uncertainty_score":0.89781594},"labels":[],"label_agreement":null}]}