{"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9539272,0.00019902109,0.02192379,0.00035395703,0.0000804144,0.000059405305,0.0007641207,0.00028982433,0.02240219],"genre_scores_gemma":[0.9937941,0.000072544615,0.00380172,0.000036309804,0.000008078211,0.000051465828,0.00022931001,0.000028455135,0.0019780404],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99986327,0.000023807266,0.0000056084905,0.000020295016,0.000041826508,0.00004520804],"domain_scores_gemma":[0.9996132,0.00018525904,0.00003269218,0.000027416627,0.00007669183,0.00006475453],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020413246,0.00039987813,0.0005948798,0.00028025213,0.00073621905,0.00085211097,0.00076741376,0.0013815266,0.0032016963],"category_scores_gemma":[0.00090452953,0.00031155156,0.0004726433,0.0004602763,0.00089959893,0.00048786035,0.0006335736,0.000705836,0.00018665295],"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":[0.000111769594,0.00005554726,0.0016741842,0.000033175587,0.000016009606,0.0002208303,0.00008212767,0.99150157,0.002472735,0.0024604325,0.0002783061,0.0010932493],"study_design_scores_gemma":[0.000020628226,0.000023696866,0.0005878814,0.000003657082,0.0000044400845,0.000018067762,0.000033022083,0.9981856,0.0005588603,0.00032358512,0.0002332375,0.0000074511536],"about_ca_topic_score_codex":0.013539472,"about_ca_topic_score_gemma":0.0054260506,"teacher_disagreement_score":0.013539472,"about_ca_system_score_codex":0.00057748903,"about_ca_system_score_gemma":0.00078109885,"threshold_uncertainty_score":0.026921332},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.25559732,0.00037062741,0.7145405,0.00027391576,0.00010275241,0.00018057358,0.00013260033,0.00090059586,0.027901042],"genre_scores_gemma":[0.8892999,0.0001650282,0.10518556,0.000034153098,0.000014114821,0.00017936855,0.000054065447,0.000024550407,0.005043291],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99988365,0.0000119612705,0.0000054250877,0.000016556593,0.0000666734,0.000015751923],"domain_scores_gemma":[0.99991107,0.000021738975,0.000020662328,0.000011037094,0.000025084602,0.0000104601995],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016624822,0.00020513007,0.00042321553,0.00016887514,0.00028544472,0.00040407563,0.0004541109,0.00059636775,0.0024649035],"category_scores_gemma":[0.00021930694,0.00020846089,0.0003178968,0.00012620882,0.0003244671,0.00024316771,0.00029830323,0.00026664385,0.00036680876],"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":[0.0001313788,0.00003988614,0.0011132596,0.00020467045,0.000030167137,0.0002723637,0.000109532346,0.8388133,0.12378198,0.013262071,0.00051890727,0.021722494],"study_design_scores_gemma":[0.000022701854,0.00008010059,0.0003572409,0.0000058988303,0.000008072262,0.00005143744,0.000014457299,0.9910404,0.006114368,0.00054116215,0.0017555354,0.0000085903885],"about_ca_topic_score_codex":0.0011008243,"about_ca_topic_score_gemma":0.0006140455,"teacher_disagreement_score":0.0024649035,"about_ca_system_score_codex":0.00031474957,"about_ca_system_score_gemma":0.00052185834,"threshold_uncertainty_score":0.008245885},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99231344,0.00030709064,0.0048933355,0.000049047794,0.000018493918,0.000021655384,0.000078556695,0.0001105423,0.0022079519],"genre_scores_gemma":[0.99828976,0.00008998897,0.00082528446,0.000009670298,0.000004741486,0.0000072196913,0.000047321464,0.0000066743983,0.0007193994],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99985623,0.00001498458,0.000005424768,0.000022015363,0.0000674715,0.00003379424],"domain_scores_gemma":[0.99961627,0.00016683871,0.000053438634,0.000020557778,0.00009466079,0.000048278704],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00032229145,0.00025720743,0.0003517579,0.00041276155,0.00029198406,0.00050244754,0.0003554398,0.0005574033,0.0009794029],"category_scores_gemma":[0.00079621613,0.00018840811,0.00025496533,0.00022636766,0.00046908,0.00040992527,0.00030035223,0.00024394308,0.00017003382],"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":[0.0019908582,0.00021209163,0.010476453,0.00019933004,0.000033004282,0.0014630235,0.00030882086,0.2829897,0.67889696,0.0024520354,0.0007392623,0.020238338],"study_design_scores_gemma":[0.00019769317,0.0026024918,0.017956324,0.00003762849,0.000031870964,0.00049014954,0.00019369277,0.764082,0.21229063,0.00054029067,0.0014447006,0.00013254442],"about_ca_topic_score_codex":0.0027517173,"about_ca_topic_score_gemma":0.000929188,"teacher_disagreement_score":0.0027517173,"about_ca_system_score_codex":0.00046112365,"about_ca_system_score_gemma":0.00041661598,"threshold_uncertainty_score":0.0054714084},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.97405505,0.00080854975,0.022261133,0.000113883114,0.00004987203,0.00005500162,0.000052125913,0.0002705354,0.0023336578],"genre_scores_gemma":[0.9965144,0.00019314744,0.002075835,0.0000149103325,0.0000056663444,0.000009953701,0.000031973763,0.000008964711,0.0011451573],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99970704,0.000027724345,0.000011181497,0.000057231657,0.00015380874,0.000042951237],"domain_scores_gemma":[0.9997727,0.000044167995,0.000029892344,0.00001406751,0.00012373572,0.000015361675],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00034834497,0.0002446901,0.0003701764,0.00026048828,0.0003711363,0.000380051,0.0005390805,0.00037715654,0.0016234971],"category_scores_gemma":[0.0004882028,0.00015450033,0.00019827267,0.00013911458,0.00025087228,0.00049757573,0.0002895123,0.00020283122,0.00027307472],"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":[0.00069292524,0.000063554326,0.0030146288,0.0004335192,0.000020814023,0.0005303217,0.00030831725,0.0041128,0.96245104,0.0010967137,0.00039990697,0.026875557],"study_design_scores_gemma":[0.00007430576,0.0015683384,0.008505211,0.00002813382,0.000064575455,0.0005013255,0.00021324569,0.08154056,0.90266716,0.0002105367,0.0045785746,0.00004795162],"about_ca_topic_score_codex":0.0019806845,"about_ca_topic_score_gemma":0.0015836444,"teacher_disagreement_score":0.0019806845,"about_ca_system_score_codex":0.00032830215,"about_ca_system_score_gemma":0.00031077754,"threshold_uncertainty_score":0.005431175},"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":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.29826272,0.00064489886,0.67915934,0.0004478174,0.00011553967,0.00018536263,0.0009025659,0.0015343664,0.01874735],"genre_scores_gemma":[0.87101173,0.00044702692,0.121497355,0.000043356034,0.000036280504,0.00022319445,0.00067696825,0.00017440587,0.0058896965],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997743,0.00005124582,0.000015028861,0.000029723904,0.00009323168,0.00003649414],"domain_scores_gemma":[0.9997764,0.00005584699,0.00004270209,0.000024619038,0.000071440976,0.000029077253],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003454213,0.000697662,0.0010714526,0.0005559805,0.0006320221,0.00081134046,0.001033466,0.000832089,0.0015009714],"category_scores_gemma":[0.000664239,0.0002941304,0.0006474448,0.00064459175,0.0003592022,0.00086293655,0.0004955173,0.00054216816,0.00034776164],"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":[0.00011126278,0.0000705309,0.0014885837,0.0000958357,0.000023872004,0.000401867,0.0000754015,0.94462734,0.017139401,0.023609566,0.001424438,0.0109319175],"study_design_scores_gemma":[0.000007187822,0.000015054796,0.000113937276,0.0000015575131,0.0000011298529,0.000017452114,0.0000046956675,0.9983089,0.00067402964,0.0005607686,0.0002912347,0.000004001186],"about_ca_topic_score_codex":0.007108521,"about_ca_topic_score_gemma":0.0030519583,"teacher_disagreement_score":0.007108521,"about_ca_system_score_codex":0.00051036273,"about_ca_system_score_gemma":0.0010150437,"threshold_uncertainty_score":0.014134288},"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":"metacan-v3-hybrid-931329e0061c","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.91855377,0.0006914731,0.07043094,0.00033417606,0.000070341215,0.00012510749,0.00019635,0.00019327526,0.009404602],"genre_scores_gemma":[0.9943598,0.00026971684,0.0025686836,0.00003199049,0.000013814159,0.000033531116,0.000046856312,0.000010384008,0.0026652375],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999131,0.000014158294,0.0000032243831,0.000019142255,0.00002028941,0.000030169238],"domain_scores_gemma":[0.99992967,0.000017136852,0.000018796649,0.0000045677857,0.00001479703,0.000015009567],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001265991,0.00036684092,0.00054218806,0.000372564,0.00049537205,0.0006426534,0.00040470404,0.00086895295,0.0010074053],"category_scores_gemma":[0.0005266821,0.00023485441,0.00056316465,0.00025285003,0.00071189523,0.00086793303,0.00067163556,0.00035526295,0.00010814141],"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":[0.00015773921,0.000059166363,0.0056516714,0.00013558423,0.00002678184,0.0010685038,0.00035531016,0.88865346,0.060866166,0.034100816,0.00044945363,0.008475296],"study_design_scores_gemma":[0.00005616725,0.00011011297,0.0019752206,0.0000075574985,0.000008858332,0.00010827977,0.00006305371,0.99119604,0.003304728,0.002297668,0.00084434875,0.000027918422],"about_ca_topic_score_codex":0.009667859,"about_ca_topic_score_gemma":0.0020025698,"teacher_disagreement_score":0.009667859,"about_ca_system_score_codex":0.0010046805,"about_ca_system_score_gemma":0.0006661063,"threshold_uncertainty_score":0.019223213},"labels":[],"label_agreement":null}]}