{"meta":{"query_hash":"29d06922e570","filters":{"venue":"Journal of Propulsion Technology"},"cohort_total":6,"direct_labels_cover":0,"predictions_cover":6,"exported":6,"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/29d06922e570","api":"https://metacan.xera.ac/api/v1/cohort?venue=Journal+of+Propulsion+Technology"},"results":[{"id":"W2348839502","doi":"","title":"Three-dimensional simulation of continuous spin detonation","year":2010,"lang":"en","type":"article","venue":"Journal of Propulsion Technology","topic":"Combustion and Detonation Processes","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":"L'Alliance Boviteq","funders":"","keywords":"Detonation; Combustor; Mechanics; Deflagration to detonation transition; Combustion; Euler equations; Limiter; Flow (mathematics); Physics; Materials science; Classical mechanics; Engineering; Explosive material; Chemistry; Thermodynamics","score_opus":0.0068171579083908165,"score_gpt":0.2457380547497738,"score_spread":0.23892089684138298,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2348839502","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":[0.9578956,0.00019698046,0.040375154,0.00048056757,0.0007300512,0.00008022496,0.0000014603047,0.00011030311,0.00012965727],"genre_scores_gemma":[0.99312913,0.000009286329,0.0067601046,0.000013415374,0.00005542266,0.0000015591664,0.0000012826392,0.000011567727,0.000018240946],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9991474,0.000005182843,0.00047732927,0.00006176023,0.00022218225,0.000086152635],"domain_scores_gemma":[0.9989909,0.00004512349,0.0002628597,0.0001039904,0.0005653331,0.00003177152],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00019261293,0.00007892951,0.00018239474,0.00059474766,0.000028151126,0.000006895226,0.00013498716,0.00018994881,0.0001564662],"category_scores_gemma":[0.0003165555,0.00006733411,0.00004920773,0.00034610668,0.00005586819,0.00014697497,0.000021335563,0.00035919968,0.000008521018],"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":[0.0000641091,0.0001548696,0.0037046836,0.000089843226,0.000042217493,0.000012492057,0.0000480061,0.10333652,0.56247175,0.004334293,0.0007796133,0.32496163],"study_design_scores_gemma":[0.001730962,0.0005178974,0.0074756513,0.00012964435,0.0000475558,0.00032438766,0.000072800634,0.40492648,0.51434374,0.05618436,0.013949852,0.00029671311],"about_ca_topic_score_codex":9.424731e-7,"about_ca_topic_score_gemma":0.000016621449,"teacher_disagreement_score":0.32466492,"about_ca_system_score_codex":0.000019767835,"about_ca_system_score_gemma":0.000029424453,"threshold_uncertainty_score":0.27458057},"labels":[],"label_agreement":null},{"id":"W2349220867","doi":"","title":"Design and numerical analysis on a solid micro-thruster","year":2007,"lang":"en","type":"article","venue":"Journal of Propulsion Technology","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":3,"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":"","keywords":"Propellant; Nozzle; Solid-fuel rocket; Microelectromechanical systems; Internal ballistics; Specific impulse; Mechanical engineering; Ballistics; Impulse (physics); Materials science; Aerospace engineering; Engineering; Projectile; Nanotechnology; Physics","score_opus":0.018024932248729635,"score_gpt":0.2955215888165763,"score_spread":0.27749665656784667,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2349220867","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":[0.6801881,0.00097100664,0.3175549,0.000595047,0.00020438507,0.000167664,5.62658e-7,0.000091714704,0.00022660664],"genre_scores_gemma":[0.98585874,0.0001231585,0.013773577,0.000025446618,0.00007753679,0.0000027184183,3.1932504e-7,0.000019785111,0.00011872386],"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9986554,0.00005198857,0.00056479214,0.00012878148,0.00029629303,0.00030277966],"domain_scores_gemma":[0.99931633,0.00008950069,0.00013468576,0.00018823447,0.00015416976,0.00011709799],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00096605235,0.00013509458,0.00042045282,0.0019421771,0.00006217401,0.000024985706,0.00022210907,0.00026363065,0.000065028886],"category_scores_gemma":[0.00007497958,0.00009695552,0.000099392826,0.0011761002,0.000052954012,0.00007562227,0.000047131332,0.00057009247,0.000027927297],"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":[0.00032730744,0.00008131967,0.0043298774,0.00005613386,0.00056518515,0.0003398456,0.00018151289,0.0011657816,0.26248178,0.000025096448,0.0025399348,0.7279062],"study_design_scores_gemma":[0.0011502152,0.0015148869,0.0026091267,0.00011684069,0.00019565642,0.000888962,0.0003382857,0.0077571194,0.97326756,0.001416547,0.010398089,0.00034672534],"about_ca_topic_score_codex":0.0000010980937,"about_ca_topic_score_gemma":5.727193e-7,"teacher_disagreement_score":0.7275595,"about_ca_system_score_codex":0.000066751774,"about_ca_system_score_gemma":0.000014496958,"threshold_uncertainty_score":0.39537314},"labels":[],"label_agreement":null},{"id":"W2357486924","doi":"","title":"Cold flow field and propulsive performance of a micro Laval nozzle","year":2004,"lang":"en","type":"article","venue":"Journal of Propulsion Technology","topic":"Computational Fluid Dynamics and Aerodynamics","field":"Engineering","cited_by":2,"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":"","keywords":"Nozzle; Discharge coefficient; Supersonic speed; Mechanics; Slip (aerodynamics); Rocket engine nozzle; Mechanical engineering; Boundary value problem; Range (aeronautics); Materials science; Engineering; Structural engineering; Aerospace engineering; Physics","score_opus":0.002336803819893925,"score_gpt":0.18485696959734524,"score_spread":0.1825201657774513,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2357486924","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":[0.99094796,0.0005049496,0.007530688,0.0006665004,0.00020255316,0.000081082726,0.000004093031,0.000031149717,0.00003101108],"genre_scores_gemma":[0.9621379,0.00036661708,0.037419602,0.000017512575,0.0000298289,0.0000015182392,7.253272e-7,0.000011182933,0.000015148702],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9993844,0.0000038282346,0.00032475987,0.00006478655,0.0001121841,0.000110046116],"domain_scores_gemma":[0.99961525,0.000016779193,0.00010466557,0.00007885679,0.00015375999,0.000030681527],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000078861536,0.00008517767,0.00019379478,0.00025742882,0.000027749473,0.000006613864,0.00012476135,0.000119527926,0.0000037075754],"category_scores_gemma":[0.000037929283,0.00007191391,0.0000350218,0.0002087925,0.000046015495,0.00007402815,0.000041471405,0.00025397225,0.0000011415078],"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":[0.000098521145,0.00013318914,0.0057773665,0.00034295162,0.00009237392,0.000052242638,0.0001436345,0.10707968,0.8080108,0.0068364763,0.0002089092,0.07122387],"study_design_scores_gemma":[0.0039306125,0.004172194,0.005834242,0.0010034516,0.000089383575,0.0018079899,0.00019487005,0.37804365,0.57682884,0.025948593,0.0015553229,0.00059084425],"about_ca_topic_score_codex":0.0000023279886,"about_ca_topic_score_gemma":0.0000042309575,"teacher_disagreement_score":0.27096397,"about_ca_system_score_codex":0.000044661083,"about_ca_system_score_gemma":0.000039678558,"threshold_uncertainty_score":0.29325643},"labels":[],"label_agreement":null},{"id":"W2359159465","doi":"","title":"Investigation on common-rail fuel system for rotary valved pulse detonation engine","year":2011,"lang":"en","type":"article","venue":"Journal of Propulsion Technology","topic":"Combustion and Detonation Processes","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":"L'Alliance Boviteq","funders":"","keywords":"Common rail; Automotive engineering; Diesel fuel; Engineering; Fuel injection; Diesel engine; Fuel supply; Detonation; Microsecond; Explosive material","score_opus":0.03498713509961497,"score_gpt":0.22443672960015196,"score_spread":0.189449594500537,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2359159465","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":[0.94022685,0.0011996593,0.051004592,0.0016347052,0.0022021946,0.00073622086,0.000012720121,0.0011062542,0.0018767936],"genre_scores_gemma":[0.9911331,0.000056635945,0.008579603,0.000046684723,0.00007580476,0.000030554158,0.000006310619,0.000026378157,0.00004495028],"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9990032,0.000019091665,0.00054289756,0.00010148815,0.00019048058,0.00014287065],"domain_scores_gemma":[0.9991094,0.000043934262,0.0002512097,0.00014466346,0.0003861695,0.00006463356],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00028007923,0.00013308498,0.00023184202,0.0008198853,0.00005747389,0.000012567565,0.00020477788,0.00020792503,0.000036702862],"category_scores_gemma":[0.0001654899,0.000115262425,0.000076381955,0.00039005248,0.000038937163,0.00020324095,0.000018175188,0.00026916128,0.000015267975],"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":[0.00078974676,0.00041493564,0.006330173,0.0033233662,0.00038619043,0.00008649445,0.0016565347,0.0067963735,0.117832616,0.060997374,0.008461136,0.79292506],"study_design_scores_gemma":[0.0033785058,0.0017313975,0.0043767984,0.0007582555,0.000131617,0.0004970375,0.0010749768,0.030337384,0.88806194,0.060131382,0.0089475345,0.00057319546],"about_ca_topic_score_codex":0.0000015380748,"about_ca_topic_score_gemma":0.0000041290623,"teacher_disagreement_score":0.79235184,"about_ca_system_score_codex":0.0001398126,"about_ca_system_score_gemma":0.000032235475,"threshold_uncertainty_score":0.47002652},"labels":[],"label_agreement":null},{"id":"W2381359814","doi":"","title":"Computation of axisymmetric jet flow with Spalart-Allmaras turbulence model","year":2001,"lang":"en","type":"article","venue":"Journal of Propulsion Technology","topic":"Computational Fluid Dynamics and Aerodynamics","field":"Engineering","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":"CAE (Canada)","funders":"","keywords":"Turbulence; Jet (fluid); Nozzle; Mechanics; Rotational symmetry; K-epsilon turbulence model; Physics; Flow (mathematics); Computation; Boundary value problem; External flow; Internal flow; Finite volume method; Turbulence modeling; Classical mechanics; Aerospace engineering; Engineering; Mathematics","score_opus":0.005582673827023597,"score_gpt":0.20526173159923733,"score_spread":0.19967905777221373,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2381359814","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":[0.5659515,0.0002716885,0.4332574,0.00025446023,0.000093648,0.000053932945,0.0000024752426,0.00004307404,0.00007179057],"genre_scores_gemma":[0.9214262,0.00026694633,0.078236975,0.0000092075325,0.000023799867,0.0000012969798,0.0000027814147,0.000018170755,0.000014646681],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99904954,0.0000091865395,0.00044383638,0.00009131609,0.0002598347,0.00014625446],"domain_scores_gemma":[0.9992933,0.000026555359,0.00019278334,0.00010349784,0.0003419682,0.000041845655],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00013776193,0.00012218211,0.00026195004,0.0008086674,0.000028760525,0.000009572974,0.0001919497,0.00012042334,0.0000040368827],"category_scores_gemma":[0.000040665505,0.00009447494,0.00005492384,0.00089240045,0.000052009214,0.000114043694,0.000030465073,0.0002839132,0.0000023062835],"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":[0.000030158577,0.000049196093,0.0019203608,0.000031283143,0.00003089929,0.00003032985,0.000019034569,0.9407037,0.0031880962,0.0010382739,0.00006642197,0.05289224],"study_design_scores_gemma":[0.00042926538,0.00028392355,0.0011799746,0.0000930501,0.00001845691,0.00036048036,0.00002062538,0.9863229,0.0004957904,0.010647685,0.000046752033,0.00010109563],"about_ca_topic_score_codex":0.0000013359703,"about_ca_topic_score_gemma":0.000005610281,"teacher_disagreement_score":0.35547465,"about_ca_system_score_codex":0.00007219003,"about_ca_system_score_gemma":0.00003976137,"threshold_uncertainty_score":0.3852576},"labels":[],"label_agreement":null},{"id":"W2387154195","doi":"","title":"Nozzle flows of the missile launching under water","year":2001,"lang":"en","type":"article","venue":"Journal of Propulsion Technology","topic":"Electromagnetic Launch and Propulsion Technology","field":"Engineering","cited_by":3,"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":"","keywords":"Nozzle; Throat; Mechanics; Missile; Overall pressure ratio; Discharge coefficient; Physics; Materials science; Engineering; Thermodynamics; Aerospace engineering; Medicine; Anatomy","score_opus":0.00428120794643157,"score_gpt":0.19029867142587165,"score_spread":0.18601746347944006,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2387154195","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":[0.9879269,0.0015608311,0.0023898513,0.0064308066,0.00064093556,0.00013835642,0.0000010549628,0.00016170005,0.0007495813],"genre_scores_gemma":[0.9959405,0.0003209407,0.0032547938,0.000058177546,0.00006803805,0.0000042688084,4.668899e-7,0.000027881608,0.00032491138],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99864674,0.000034247183,0.00061620754,0.00011164294,0.0002375537,0.00035363965],"domain_scores_gemma":[0.9992265,0.000020660736,0.00016749777,0.00038815278,0.0001469407,0.000050225844],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024412796,0.00016025719,0.0003396171,0.00044204338,0.000075608055,0.000008498112,0.0006598287,0.00036167723,0.0003025405],"category_scores_gemma":[0.00007312146,0.000084460036,0.00013787008,0.00048267035,0.0001223403,0.00008548207,0.00011523684,0.0007451475,0.000018027462],"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":[0.000025983232,0.000054830656,0.0009923934,0.000033172222,0.000042412397,0.000027178396,0.000046946803,0.00037134832,0.9289188,0.00069565704,0.0016796037,0.06711169],"study_design_scores_gemma":[0.00064322096,0.0005629667,0.0003191521,0.00009289122,0.00003644741,0.0013064805,0.000110381734,0.00078399264,0.9145542,0.05933563,0.022098841,0.0001558103],"about_ca_topic_score_codex":0.00000379957,"about_ca_topic_score_gemma":0.000008366143,"teacher_disagreement_score":0.06695588,"about_ca_system_score_codex":0.000060900107,"about_ca_system_score_gemma":0.000027879774,"threshold_uncertainty_score":0.34441805},"labels":[],"label_agreement":null}]}