{"meta":{"query_hash":"239f9a13f26c","filters":{"venue":"52nd AIAA/SAE/ASEE Joint Propulsion Conference"},"cohort_total":5,"direct_labels_cover":0,"predictions_cover":5,"exported":5,"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/239f9a13f26c","api":"https://metacan.xera.ac/api/v1/cohort?venue=52nd+AIAA%2FSAE%2FASEE+Joint+Propulsion+Conference"},"results":[{"id":"W2484810407","doi":"10.2514/6.2016-4801","title":"Numerical Investigation of the Effect of Wing Position on the Aeroacoustic Field of a Propeller","year":2016,"lang":"en","type":"article","venue":"52nd AIAA/SAE/ASEE Joint Propulsion Conference","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":"Carleton University","funders":"Pratt and Whitney Canada","keywords":"Propeller; Wing; Acoustics; Propulsor; Position (finance); Marine engineering; Aerospace engineering; Engineering; Field (mathematics); Aeronautics; Computer science; Physics; Mathematics","score_opus":0.013004399093189055,"score_gpt":0.2102289880899683,"score_spread":0.19722458899677922,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2484810407","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":[0.97938603,0.0001589215,0.008901942,0.0001390791,0.000047510013,0.000025878013,0.000112714035,0.00013553434,0.011092319],"genre_scores_gemma":[0.9980831,0.00003756915,0.0011990258,0.000011386334,0.0000056905533,0.0000054471266,0.000021716645,0.000009120967,0.000626918],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99986255,0.000032224696,0.00000776014,0.000019962225,0.0000442333,0.000033296703],"domain_scores_gemma":[0.9986046,0.0009878677,0.00010580065,0.000084355495,0.000142153,0.00007523383],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002944146,0.00032803745,0.00046870657,0.00039190447,0.0005220469,0.000538658,0.0004878471,0.00094429153,0.002813742],"category_scores_gemma":[0.001995607,0.00031236676,0.0003969188,0.00040282012,0.0008447828,0.0004220224,0.00038218807,0.00046061448,0.00017521484],"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":[0.0004366084,0.00017967123,0.0036136282,0.00009201658,0.000027012633,0.00052179146,0.00007758356,0.95506173,0.03315489,0.0012173615,0.00023566511,0.00538198],"study_design_scores_gemma":[0.00005210623,0.00012329669,0.0023532833,0.000005748954,0.00001079258,0.000051888932,0.000038674454,0.9929047,0.004187121,0.00010812952,0.00015137358,0.000012779755],"about_ca_topic_score_codex":0.0068106954,"about_ca_topic_score_gemma":0.0031832657,"teacher_disagreement_score":0.0068106954,"about_ca_system_score_codex":0.0003791582,"about_ca_system_score_gemma":0.000433417,"threshold_uncertainty_score":0.013542116},"labels":[],"label_agreement":null},{"id":"W2485266855","doi":"10.2514/6.2016-4543","title":"Performance and Plume Characterization of the PPS 1350-G Hall Thruster","year":2016,"lang":"en","type":"article","venue":"52nd AIAA/SAE/ASEE Joint Propulsion Conference","topic":"Plasma Diagnostics and Applications","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":"Safran Electronics (Canada)","funders":"","keywords":"Characterization (materials science); Aerospace engineering; Plume; Astrobiology; Environmental science; Physics; Nuclear engineering; Computer science; Aeronautics; Engineering; Meteorology; Optics","score_opus":0.01646229331238019,"score_gpt":0.1856945877141072,"score_spread":0.16923229440172702,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2485266855","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":[0.9942893,0.00014242723,0.002607839,0.00008595013,0.000009867862,0.000017733886,0.00023090921,0.00020659875,0.0024094554],"genre_scores_gemma":[0.9970772,0.0000465078,0.00087678496,0.000025469473,0.0000027421984,0.0000067803817,0.00024121178,0.00002308906,0.0017001298],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99988043,0.000009859696,0.0000045509687,0.000021043226,0.000057451103,0.00002665001],"domain_scores_gemma":[0.99991524,0.000018871637,0.000009794744,0.000008199838,0.000030401572,0.000017561],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023865592,0.00025707996,0.00028206847,0.00032509162,0.00036508692,0.00046248848,0.00032986232,0.0003224085,0.0018420279],"category_scores_gemma":[0.0002346326,0.00011195042,0.00018656878,0.00021618325,0.00019948228,0.00036459512,0.000310379,0.00024403543,0.0003796639],"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":[0.0010851962,0.00005233332,0.0052121393,0.000046509565,0.000013610169,0.00006005758,0.00013325604,0.0021029725,0.9785866,0.00019721591,0.00039731752,0.012112797],"study_design_scores_gemma":[0.00008212091,0.001861226,0.067498595,0.000010921567,0.000033953373,0.00019241271,0.0002846492,0.01892687,0.9074367,0.00013175502,0.0035067105,0.000034047862],"about_ca_topic_score_codex":0.0030310696,"about_ca_topic_score_gemma":0.0018148334,"teacher_disagreement_score":0.0030310696,"about_ca_system_score_codex":0.00035629235,"about_ca_system_score_gemma":0.0003432221,"threshold_uncertainty_score":0.0061621666},"labels":[],"label_agreement":null},{"id":"W2501543565","doi":"10.2514/6.2016-4789","title":"Sub- or Supercritical? A flamelet analysis of high pressure rocket propellant injection","year":2016,"lang":"en","type":"article","venue":"52nd AIAA/SAE/ASEE Joint Propulsion Conference","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":15,"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":"Propellant; Supercritical fluid; Rocket (weapon); Aerospace engineering; Rocket engine; Liquid-propellant rocket; Rocket propellant; Materials science; Aeronautics; Environmental science; Engineering; Thermodynamics; Physics","score_opus":0.038499974438419314,"score_gpt":0.2623093735577036,"score_spread":0.2238093991192843,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2501543565","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":[0.98068064,0.00020970561,0.010326587,0.000071837385,0.00001967181,0.00002287561,0.000077265664,0.00013737874,0.00845403],"genre_scores_gemma":[0.9977101,0.000066021494,0.0007051634,0.000008351899,0.000005528739,0.0000045188335,0.000039095594,0.00002035964,0.0014409553],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999553,0.000002887236,0.0000013205009,0.0000058658625,0.000020941316,0.000013637369],"domain_scores_gemma":[0.9999356,0.00001913336,0.000012665605,0.0000048540724,0.000019200204,0.0000085551155],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000105235216,0.00023424746,0.00021263458,0.0006106281,0.00032199998,0.0003943724,0.00027945515,0.00029504683,0.001978258],"category_scores_gemma":[0.00021260945,0.0001125727,0.00028546786,0.00021175812,0.00034998002,0.00040861825,0.00027636255,0.000381615,0.00022834683],"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":[0.0011132968,0.00023496643,0.0141519755,0.0001501922,0.00004119982,0.0006476189,0.00031186856,0.04463285,0.8974992,0.012607511,0.0004877773,0.028121475],"study_design_scores_gemma":[0.000041829022,0.00031112437,0.038973812,0.000017714361,0.000022851904,0.00018544505,0.00014179687,0.65352136,0.30275604,0.0026052138,0.0013851172,0.000037671496],"about_ca_topic_score_codex":0.0036263429,"about_ca_topic_score_gemma":0.0023948334,"teacher_disagreement_score":0.0036263429,"about_ca_system_score_codex":0.0002933161,"about_ca_system_score_gemma":0.00028871652,"threshold_uncertainty_score":0.007210493},"labels":[],"label_agreement":null},{"id":"W2503960968","doi":"10.2514/6.2016-4813","title":"Experimental Investigation of a Baffled-Tube Ram Accelerator","year":2016,"lang":"en","type":"article","venue":"52nd AIAA/SAE/ASEE Joint Propulsion Conference","topic":"Combustion and Detonation Processes","field":"Engineering","cited_by":10,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"Joint Center for Aerospace Technology Innovation; University of Washington","keywords":"Computer science; Electrical engineering; Nuclear engineering; Engineering","score_opus":0.04046101639532247,"score_gpt":0.2462438166492507,"score_spread":0.20578280025392826,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2503960968","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":[0.99481815,0.000074753465,0.0023611845,0.00007673016,0.0000181109,0.000087135086,0.00020047369,0.00029111144,0.0020722144],"genre_scores_gemma":[0.99582916,0.000038141403,0.0023264564,0.000024814066,0.000012286653,0.00003988632,0.00015652236,0.00003299264,0.0015398099],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9995053,0.00010820613,0.000018981196,0.00009442083,0.00014816635,0.00012492802],"domain_scores_gemma":[0.99920064,0.0002938923,0.00007301325,0.0001396523,0.00015037229,0.00014243834],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0009732724,0.0004073323,0.0007407128,0.00037897663,0.0012740217,0.00048636735,0.0012263814,0.0009773211,0.0044084997],"category_scores_gemma":[0.0010195363,0.00035214692,0.00035673063,0.0003664751,0.00089092547,0.00078758446,0.0007995444,0.0007056396,0.0008563668],"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":[0.006853542,0.0010766223,0.009462005,0.00025877624,0.00007065905,0.0008336604,0.00078265276,0.0030956732,0.9679785,0.0014523102,0.0005175059,0.0076180752],"study_design_scores_gemma":[0.0009407854,0.023217332,0.038892098,0.000048388356,0.00013619053,0.0009956518,0.00077885104,0.022457473,0.9015651,0.00051673397,0.010339282,0.000112072164],"about_ca_topic_score_codex":0.0007933302,"about_ca_topic_score_gemma":0.00053796585,"teacher_disagreement_score":0.0044084997,"about_ca_system_score_codex":0.00047111197,"about_ca_system_score_gemma":0.00059457595,"threshold_uncertainty_score":0.014747918},"labels":[],"label_agreement":null},{"id":"W2742737388","doi":"10.2514/6.2016-4788","title":"Trajectory and Breakup of Cryogenic Jets in Crossflow","year":2016,"lang":"en","type":"article","venue":"52nd AIAA/SAE/ASEE Joint Propulsion Conference","topic":"Cyclone Separators and Fluid Dynamics","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":"University of Toronto","funders":"","keywords":"Breakup; Trajectory; Mechanics; Aerospace engineering; Physics; Computer science; Engineering; Astronomy","score_opus":0.014855183326583133,"score_gpt":0.21070415244280044,"score_spread":0.1958489691162173,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2742737388","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":[0.9986185,0.00011311651,0.0007626047,0.000012019123,0.0000045796246,0.0000052091236,0.00005938727,0.000025140253,0.00039949076],"genre_scores_gemma":[0.99834144,0.00009233218,0.00071547163,0.000009562579,0.000002510909,0.00000626096,0.00020274747,0.000014429455,0.0006152638],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999043,0.0000050778685,0.0000032031028,0.00002234699,0.000035700174,0.000029314593],"domain_scores_gemma":[0.99976164,0.000046948855,0.000074951684,0.00001822445,0.00005845577,0.00003977838],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001449168,0.00018982291,0.00019262913,0.00052120315,0.00039158572,0.00053968997,0.00016839373,0.00027426583,0.0009776969],"category_scores_gemma":[0.00037817887,0.00014845932,0.00021863486,0.0002095124,0.00027899514,0.00040069965,0.00026119506,0.00058040366,0.00015108746],"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":[0.000406092,0.000062373525,0.017981108,0.000026080672,0.000017772774,0.0003814783,0.00041906626,0.0024469295,0.97077775,0.00053026696,0.00013810814,0.006812852],"study_design_scores_gemma":[0.000026896421,0.00083350873,0.17809165,0.000024649482,0.000023831588,0.0002814757,0.00031939923,0.023534719,0.7945009,0.00024577242,0.0020725098,0.00004467307],"about_ca_topic_score_codex":0.0028270264,"about_ca_topic_score_gemma":0.0017171018,"teacher_disagreement_score":0.0028270264,"about_ca_system_score_codex":0.000660069,"about_ca_system_score_gemma":0.0002111581,"threshold_uncertainty_score":0.005621195},"labels":[],"label_agreement":null}]}