{"meta":{"query_hash":"cb33bbf9a2b2","filters":{"topic":"Rocket and propulsion systems research"},"cohort_total":366,"direct_labels_cover":1,"predictions_cover":366,"exported":366,"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/cb33bbf9a2b2","api":"https://metacan.xera.ac/api/v1/cohort?topic=Rocket+and+propulsion+systems+research"},"results":[{"id":"W10141135","doi":"","title":"Development and validation of new cryogenic cavitation model for rocket turbopump inducer","year":2009,"lang":"en","type":"article","venue":"Deep Blue (University of Michigan)","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":13,"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":"Rocket (weapon); Inducer; Cavitation; Aeronautics; Nuclear engineering; Aerospace engineering; Engineering; Mechanics; Physics; Chemistry","score_opus":0.03077677040822216,"score_gpt":0.23116118857381768,"score_spread":0.20038441816559552,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W10141135","genre_codex":"methods","genre_gemma":"methods","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.1367229,0.00027051516,0.852274,0.00014014108,0.000054672695,0.00019851235,0.0001907033,0.0007437859,0.009404748],"genre_scores_gemma":[0.9220701,0.00037722065,0.07021197,0.000032025036,0.000029879095,0.0003217145,0.00025557933,0.0001554991,0.0065460764],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99976,0.00003735024,0.000012118126,0.00004603939,0.00011250489,0.00003193837],"domain_scores_gemma":[0.99960786,0.00012012841,0.000059209317,0.000035864043,0.00016028252,0.000016717584],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00043890032,0.00046612168,0.0005991417,0.0003296426,0.00030878608,0.00057721353,0.0012334395,0.00083974196,0.0010285709],"category_scores_gemma":[0.0010347881,0.00027667917,0.00056688866,0.00017936576,0.0004508544,0.0006710095,0.00050535874,0.0006011755,0.0003668696],"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":[0.000043235923,0.000031591946,0.001029104,0.00006125433,0.000010197777,0.00016683221,0.00008962202,0.9568847,0.028750798,0.004394706,0.00040764723,0.008130284],"study_design_scores_gemma":[0.0000031939599,0.000011206472,0.00008796988,0.0000017886632,0.0000015243395,0.0000091616985,0.0000031400612,0.9974667,0.0019451954,0.00012643596,0.0003408623,0.000002823707],"about_ca_topic_score_codex":0.0072100167,"about_ca_topic_score_gemma":0.0025238874,"teacher_disagreement_score":0.0072100167,"about_ca_system_score_codex":0.0007520255,"about_ca_system_score_gemma":0.0009859435,"threshold_uncertainty_score":0.014336109},"labels":[],"label_agreement":null},{"id":"W11430680","doi":"10.1136/vr.148.23.707","title":"Mechanical Behavior of Advanced Materials for Aerospace Applications","year":2003,"lang":"en","type":"article","venue":"NASA Technical Reports Server (NASA)","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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":"Materials science; Low-cycle fatigue; Memorandum; Aerospace; Ultimate tensile strength; Stress (linguistics); Structural engineering; Composite material; Forensic engineering; Engineering; Aerospace engineering","score_opus":0.023464218493083343,"score_gpt":0.30439739392653464,"score_spread":0.2809331754334513,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W11430680","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":[0.98131263,0.0023760288,0.0072940877,0.00015435708,0.0001238723,0.000053233183,0.00021520164,0.00012383651,0.008346765],"genre_scores_gemma":[0.9906769,0.00050207326,0.0025363439,0.000045516634,0.000017722226,0.00003366473,0.0002957349,0.00001989017,0.0058721323],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9996613,0.000045482993,0.00001571014,0.000027632328,0.00020939963,0.000040484632],"domain_scores_gemma":[0.99965,0.00006154037,0.00005667862,0.000038666283,0.00014899738,0.00004411652],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00037991404,0.00036339185,0.00024979966,0.0008708448,0.00030841274,0.00052403513,0.00022202014,0.0004766856,0.0063842842],"category_scores_gemma":[0.00070822623,0.00019104709,0.00023386831,0.00039127748,0.00022105337,0.00027990286,0.00028381112,0.0001977889,0.0015054689],"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":[0.00032108722,0.0001918243,0.018725602,0.00021140334,0.000044410743,0.00039320622,0.00028435414,0.009357008,0.8770164,0.0013222178,0.0024184545,0.08971399],"study_design_scores_gemma":[0.000073448566,0.004421581,0.37401497,0.0001617007,0.00013493473,0.0020891249,0.0010330586,0.13050483,0.41814393,0.0026398876,0.06663113,0.00015145502],"about_ca_topic_score_codex":0.00046840063,"about_ca_topic_score_gemma":0.0008994871,"teacher_disagreement_score":0.0063842842,"about_ca_system_score_codex":0.00020880763,"about_ca_system_score_gemma":0.0001915688,"threshold_uncertainty_score":0.021357536},"labels":[],"label_agreement":null},{"id":"W1213426171","doi":"","title":"Numerical simulation of cantilevered ramp injector flow fields for hypervelocity fuel/air mixing enhancement","year":2000,"lang":"en","type":"dissertation","venue":"TSpace (University of Toronto)","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":15,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"University of Toronto","keywords":"Hypervelocity; Injector; Aerospace engineering; Mixing (physics); Cantilever; Computer simulation; Mechanics; Engineering; Automotive engineering; Flow (mathematics); Physics; Mechanical engineering","score_opus":0.01976080509288321,"score_gpt":0.27295096545451714,"score_spread":0.25319016036163394,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1213426171","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":[0.91935086,0.00047370148,0.057954572,0.00045640965,0.000096707976,0.00013000655,0.00058662036,0.00042696405,0.020524127],"genre_scores_gemma":[0.9804134,0.0001321519,0.016923938,0.000033679178,0.000008027431,0.00006970028,0.00017886018,0.000027046477,0.0022131712],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99990857,0.000020853866,0.0000052391947,0.000011818684,0.000027656513,0.000025817455],"domain_scores_gemma":[0.99950194,0.00029361277,0.000058692378,0.000022725979,0.000078070996,0.00004491992],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003654442,0.00035272533,0.00041928864,0.0004180223,0.00043191717,0.00063101755,0.0006672369,0.0010318186,0.0030290873],"category_scores_gemma":[0.0009848704,0.0002040315,0.00041763394,0.00036981027,0.00052276393,0.000340092,0.00046883416,0.00054451,0.00021903924],"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":[0.000137176,0.00011627531,0.0027049857,0.000079340905,0.000015044177,0.00021249398,0.000093841845,0.9821347,0.0075203404,0.0023513515,0.00037746236,0.0042570815],"study_design_scores_gemma":[0.0000061234414,0.00001928982,0.00021702127,0.000003069057,0.0000010680545,0.0000049666664,0.000011618643,0.9991223,0.00045729644,0.000057071495,0.00009756378,0.0000025275485],"about_ca_topic_score_codex":0.007664826,"about_ca_topic_score_gemma":0.0057916823,"teacher_disagreement_score":0.007664826,"about_ca_system_score_codex":0.00055467786,"about_ca_system_score_gemma":0.0007764991,"threshold_uncertainty_score":0.015240431},"labels":[],"label_agreement":null},{"id":"W141561937","doi":"","title":"Cryogenic cavitating Flow in 2D Laval Nozzle","year":2003,"lang":"zh","type":"article","venue":"热科学学报：英文版","topic":"Rocket and propulsion systems research","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; Cavitation; Propellant; Liquid-propellant rocket; Rocket engine nozzle; Rocket (weapon); Mechanics; Rocket engine; Flow (mathematics); Liquid nitrogen; Materials science; Thermodynamics; Aerospace engineering; Mechanical engineering; Engineering; Chemistry; Physics","score_opus":0.026263416698223154,"score_gpt":0.2826950492925399,"score_spread":0.2564316325943168,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W141561937","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":[0.9856058,0.0003828608,0.0116884215,0.000069600566,0.000020283953,0.000017503779,0.00004465069,0.00007187426,0.0020988975],"genre_scores_gemma":[0.99692947,0.00011545539,0.0023521879,0.000008160732,0.000008581475,0.000011486065,0.000030138423,0.0000068847967,0.0005376212],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998491,0.000029710909,0.000006429235,0.0000370008,0.00004883113,0.000028833292],"domain_scores_gemma":[0.9998227,0.000051113388,0.000054772638,0.000011735882,0.00003961839,0.000020151207],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00022613535,0.00023966038,0.00034862536,0.00023690186,0.0003076351,0.00058790063,0.00036605875,0.00051981374,0.00040987015],"category_scores_gemma":[0.0005631692,0.00018674301,0.00027591817,0.00015297196,0.0007582414,0.0004114741,0.00041930223,0.00024279633,0.00007975952],"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":[0.00041058764,0.00008239311,0.007902572,0.0001799159,0.000033260632,0.0017063678,0.00048558952,0.22771253,0.74562097,0.009092734,0.00033383694,0.0064392798],"study_design_scores_gemma":[0.00013820537,0.00037907498,0.0076177735,0.000019420882,0.000015469508,0.00040102933,0.00011436492,0.8834953,0.104870684,0.0011852381,0.0016857531,0.000077684796],"about_ca_topic_score_codex":0.0023541208,"about_ca_topic_score_gemma":0.0005715856,"teacher_disagreement_score":0.0023541208,"about_ca_system_score_codex":0.0005960114,"about_ca_system_score_gemma":0.00032239594,"threshold_uncertainty_score":0.004680872},"labels":[],"label_agreement":null},{"id":"W1516034171","doi":"10.4271/2001-01-0848","title":"Accelerated Development of the 2000 Saturn Three-Door Coupe Rear Quarter Panel","year":2001,"lang":"en","type":"article","venue":"SAE technical papers on CD-ROM/SAE technical paper series","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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":"Saturn; Quarter (Canadian coin); Flat panel; Aeronautics; Computer science; Environmental science; Astronomy; Physics; Engineering; Computer graphics (images); History; Archaeology; Planet","score_opus":0.035356623528666066,"score_gpt":0.263869515289266,"score_spread":0.22851289176059994,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1516034171","genre_codex":"other","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":[0.30022877,0.0007365852,0.18087041,0.0023669885,0.002333712,0.0020680146,0.0046856655,0.008844604,0.4978653],"genre_scores_gemma":[0.31121162,0.00076426024,0.13817057,0.0008524162,0.00023459227,0.00043137878,0.006654071,0.0017555887,0.53992546],"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99915254,0.00006836134,0.0000137067855,0.00012075778,0.00055127125,0.00009338827],"domain_scores_gemma":[0.9987698,0.000045108063,0.000024571229,0.00010432315,0.00079346896,0.00026273902],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0017633573,0.00036033144,0.00019819952,0.0006770649,0.0005004642,0.0009214841,0.0009308064,0.00067900727,0.034854107],"category_scores_gemma":[0.0010143665,0.00031574318,0.000422934,0.0003118267,0.0002023838,0.0006174943,0.00065161684,0.001046618,0.015279074],"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":[0.0005478958,0.0010706644,0.005478595,0.00028108258,0.000031097235,0.00069976365,0.00089965813,0.012051458,0.31595078,0.009855115,0.20606233,0.4470715],"study_design_scores_gemma":[0.00015197913,0.002135586,0.029888889,0.00006677137,0.000024141003,0.000733325,0.00030190923,0.018689217,0.097783394,0.00043464024,0.84971005,0.00007993773],"about_ca_topic_score_codex":0.009930444,"about_ca_topic_score_gemma":0.017024303,"teacher_disagreement_score":0.034854107,"about_ca_system_score_codex":0.0010425845,"about_ca_system_score_gemma":0.0016416806,"threshold_uncertainty_score":0.116598606},"labels":[],"label_agreement":null},{"id":"W1542173436","doi":"","title":"Characterization and Fate of Gun and Rocket Propellant Residues on Testing and Training Ranges","year":2011,"lang":"en","type":"article","venue":"US Army Corps of Engineers: Engineer Research and Development Center (Knowledge Core)","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":11,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"Cold Regions Research and Engineering Laboratory; Engineer Research and Development Center; Strategic Environmental Research and Development Program; Ministère de la Défense Nationale; U.S. Department of Defense","keywords":"Propellant; Ammunition; Environmental science; Aeronautics; Aerospace engineering; Waste management; Engineering; Forensic engineering; Materials science","score_opus":0.17312232939801478,"score_gpt":0.29728825201263265,"score_spread":0.12416592261461787,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1542173436","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":[0.9957075,0.00013871465,0.0023389284,0.000012246608,0.0000036748131,0.00003119233,0.00041215756,0.000047605325,0.001307921],"genre_scores_gemma":[0.99285746,0.00019527534,0.003293938,0.000024200772,0.0000024143728,0.000026929461,0.00077728776,0.00004467581,0.0027778358],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997329,0.000017318458,0.000011578133,0.00006026731,0.00014573989,0.000032143333],"domain_scores_gemma":[0.99968743,0.000059420512,0.00005829923,0.000015130028,0.00015320213,0.000026478998],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020222041,0.00026921774,0.0001705656,0.0009716437,0.00040903798,0.0004351925,0.00042170956,0.00032507768,0.0012343444],"category_scores_gemma":[0.00037892678,0.000074058014,0.00017078841,0.0004032045,0.00021398689,0.00026270628,0.00021328068,0.00027542218,0.00036123567],"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":[0.00020664008,0.00007505601,0.030608071,0.00008116371,0.0000134374095,0.00016279895,0.00016840655,0.0013979154,0.9489192,0.000034244582,0.000114634626,0.018218296],"study_design_scores_gemma":[0.000006908512,0.0005972349,0.08195474,0.000020914193,0.000018718418,0.00030754364,0.00031459972,0.004646249,0.91065025,0.000031959844,0.0014384962,0.000012298291],"about_ca_topic_score_codex":0.011984846,"about_ca_topic_score_gemma":0.012018669,"teacher_disagreement_score":0.011984846,"about_ca_system_score_codex":0.00044527784,"about_ca_system_score_gemma":0.00032846807,"threshold_uncertainty_score":0.023830175},"labels":[],"label_agreement":null},{"id":"W1548521662","doi":"10.4271/2010-01-0369","title":"Target Volume Based Shift Controls with High Flow PWM Solenoids","year":2010,"lang":"en","type":"article","venue":"SAE technical papers on CD-ROM/SAE technical paper series","topic":"Rocket and propulsion systems research","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":"Chrysler (Canada)","funders":"","keywords":"Volume (thermodynamics); Flow (mathematics); Computer science; Pulse-width modulation; Physics; Mechanics; Electrical engineering; Voltage; Engineering","score_opus":0.007602294734054139,"score_gpt":0.22678187941251043,"score_spread":0.2191795846784563,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1548521662","genre_codex":"methods","genre_gemma":"methods","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.1713798,0.00032768797,0.81017023,0.00009704774,0.00022196556,0.00013663116,0.000065738845,0.0020810629,0.015519762],"genre_scores_gemma":[0.9418788,0.00009837657,0.05015428,0.000036537058,0.000057652695,0.00006154827,0.000045261702,0.00007334896,0.0075942106],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997092,0.000022404893,0.000016840882,0.000033487842,0.00019970484,0.000018403909],"domain_scores_gemma":[0.99980515,0.000041073883,0.000039189425,0.000022625467,0.000076327975,0.00001568246],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00019754068,0.0003434491,0.00017772548,0.00030555043,0.00019161428,0.00041725632,0.00074772723,0.00017916596,0.0019122434],"category_scores_gemma":[0.0003404855,0.00013319425,0.00013045756,0.000146998,0.00026976835,0.00047386313,0.00039620447,0.00032654783,0.00047741292],"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":[0.0007602316,0.00013567794,0.00078381505,0.00026478822,0.000022558239,0.00011642462,0.0003471891,0.023362132,0.57872593,0.012603496,0.0020874664,0.38079023],"study_design_scores_gemma":[0.00027964215,0.0022789938,0.002590351,0.00003504043,0.00003335514,0.00049635896,0.000080561134,0.33592087,0.62162185,0.0049014995,0.03168486,0.00007655271],"about_ca_topic_score_codex":0.00041572,"about_ca_topic_score_gemma":0.00057527807,"teacher_disagreement_score":0.0019122434,"about_ca_system_score_codex":0.00024871455,"about_ca_system_score_gemma":0.00021026886,"threshold_uncertainty_score":0.0063970685},"labels":[],"label_agreement":null},{"id":"W1598396733","doi":"10.2172/920098","title":"Development/Demonstration of an Advanced Oxy-Fuel Front-End System","year":2007,"lang":"en","type":"report","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":1,"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":"U.S. Department of Energy","keywords":"Natural gas; Combustion; Environmental science; Waste management; Engineering; Chemistry","score_opus":0.046261771088508326,"score_gpt":0.3159349099200992,"score_spread":0.2696731388315909,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1598396733","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":[0.703777,0.0003558806,0.25837475,0.0006895975,0.0004255463,0.0018621414,0.0013363665,0.009505157,0.023673588],"genre_scores_gemma":[0.84856784,0.0002485595,0.119605705,0.00025672148,0.000052110347,0.0005904653,0.0014016564,0.00021379141,0.029063208],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99950624,0.000030914183,0.000018042801,0.00007148702,0.00029349336,0.000079888756],"domain_scores_gemma":[0.99968624,0.000022944347,0.000022251088,0.000034785302,0.00016387526,0.00006995718],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0007795982,0.00039581812,0.00033934886,0.00030384236,0.0004357228,0.00068941736,0.0010838773,0.00081810856,0.004987253],"category_scores_gemma":[0.00035637832,0.0001847643,0.00033915028,0.00014597124,0.00022314984,0.0005952575,0.0005713941,0.0007271275,0.0018203452],"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":[0.0007447567,0.0008709946,0.0031909812,0.00038077217,0.000031900454,0.0007880285,0.00036764782,0.005609661,0.8738006,0.002933608,0.005826447,0.10545462],"study_design_scores_gemma":[0.0002891741,0.0043249945,0.006370713,0.000037048536,0.0000467125,0.0006747439,0.00011219851,0.05637823,0.8813058,0.00039450813,0.050003536,0.00006227671],"about_ca_topic_score_codex":0.0019492093,"about_ca_topic_score_gemma":0.0012717993,"teacher_disagreement_score":0.004987253,"about_ca_system_score_codex":0.00040100078,"about_ca_system_score_gemma":0.0007525238,"threshold_uncertainty_score":0.016683996},"labels":[],"label_agreement":null},{"id":"W1602630007","doi":"10.4271/2006-01-0625","title":"Finite Element Modeling of Fuel Emission for Thermoplastic Multilayer Fuel Tanks with Optimization of Barrier Properties","year":2006,"lang":"en","type":"article","venue":"SAE technical papers on CD-ROM/SAE technical paper series","topic":"Rocket and propulsion systems research","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":"National Research Council Canada","funders":"","keywords":"Finite element method; Materials science; Thermoplastic; Fuel cells; Nuclear engineering; Composite material; Structural engineering; Engineering; Chemical engineering","score_opus":0.01975055223221187,"score_gpt":0.2418759284308471,"score_spread":0.22212537619863523,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1602630007","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":[0.17869465,0.00037100783,0.802989,0.0003483311,0.000063223146,0.00008952292,0.00032546182,0.0005231852,0.016595548],"genre_scores_gemma":[0.90830576,0.0003098066,0.078196816,0.00005481763,0.000016424898,0.00021298566,0.00023265333,0.00013138785,0.012539316],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998466,0.000040906394,0.000007778621,0.00002616726,0.00005742505,0.00002116708],"domain_scores_gemma":[0.99976164,0.00012549077,0.00003308959,0.000017107606,0.0000458899,0.000016726726],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00043837787,0.00048589747,0.00071116764,0.000411852,0.00033759105,0.00080112414,0.0008294161,0.0014072278,0.0025297224],"category_scores_gemma":[0.00075258646,0.0004909802,0.00072214263,0.00034677007,0.00052210636,0.00053862005,0.0004628497,0.0004720337,0.0003846597],"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":[0.000022249282,0.000015074816,0.0002093427,0.000019406907,0.000005016466,0.000023362209,0.000020234394,0.99237764,0.004144112,0.001163466,0.000057336496,0.0019427704],"study_design_scores_gemma":[0.0000019669333,0.0000056943877,0.000038336355,0.0000019511335,0.0000011450569,0.0000030590083,0.0000039449174,0.99923015,0.0005083203,0.00008294737,0.000120946504,0.0000015324176],"about_ca_topic_score_codex":0.007977988,"about_ca_topic_score_gemma":0.00633187,"teacher_disagreement_score":0.007977988,"about_ca_system_score_codex":0.0008090791,"about_ca_system_score_gemma":0.0009603245,"threshold_uncertainty_score":0.01586312},"labels":[],"label_agreement":null},{"id":"W1819109599","doi":"10.5957/jsr.2009.53.1.48","title":"Dynamic Positioning Thruster Near Wake Hydrodynamic Characteristics at Near Bollard Pull","year":2009,"lang":"en","type":"article","venue":"Journal of Ship Research","topic":"Rocket and propulsion systems research","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":"Memorial University of Newfoundland","funders":"","keywords":"Wake; Nozzle; Mechanics; Cavitation; Momentum (technical analysis); Aerospace engineering; Water tunnel; Flow (mathematics); Physics; Marine engineering; Engineering; Vortex","score_opus":0.03579944391231686,"score_gpt":0.33811589209474396,"score_spread":0.3023164481824271,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1819109599","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":[0.99887806,0.000020382713,0.00087159366,0.000008010865,0.0000015392803,0.0000024804174,0.000011681557,0.000025885272,0.00018028804],"genre_scores_gemma":[0.99922085,0.000010276367,0.00039546523,0.0000036793554,8.428135e-7,0.000003107697,0.000027557666,0.0000052550904,0.00033310434],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998679,0.000012423876,0.0000052000164,0.000022272774,0.00006277962,0.000029298713],"domain_scores_gemma":[0.9997167,0.00008788214,0.00006490097,0.00001739835,0.00007734911,0.000035712204],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00019559448,0.00013729493,0.0002637913,0.00023199123,0.0002193772,0.00026608488,0.00015373572,0.00021356536,0.0006508131],"category_scores_gemma":[0.0005674025,0.00010843497,0.00008964471,0.00010459643,0.00031752756,0.0003727823,0.00026652843,0.00023609528,0.00016737115],"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":[0.00042487067,0.00004695215,0.0073622,0.000025380894,0.0000043398945,0.00015121386,0.0001843015,0.0026544959,0.9841084,0.00009100281,0.000059501283,0.004887276],"study_design_scores_gemma":[0.0000739953,0.0021151674,0.10258042,0.00001055202,0.000014680938,0.0003887225,0.0004197356,0.03355137,0.8597789,0.00013728341,0.00087920425,0.000050065097],"about_ca_topic_score_codex":0.0005407082,"about_ca_topic_score_gemma":0.00047922874,"teacher_disagreement_score":0.0006508131,"about_ca_system_score_codex":0.00023841119,"about_ca_system_score_gemma":0.00013130283,"threshold_uncertainty_score":0.0021772385},"labels":[],"label_agreement":null},{"id":"W1840263640","doi":"10.3968/5188","title":"Analysis on U.S. Sealift Innovation Pioneer: Chester Nimitz","year":2014,"lang":"en","type":"article","venue":"Higher education of social science","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Navy; Broadside; Militarism; Aeronautics; Test (biology); World War II; Political science; History; Operations research; Computer science; Law; Engineering; Geology; Visual arts; Art","score_opus":0.025837342756904236,"score_gpt":0.32703943232187754,"score_spread":0.3012020895649733,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1840263640","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":[0.70833796,0.007575889,0.00092280813,0.010901574,0.00034153525,0.00013393546,0.013726725,0.00015094657,0.2579086],"genre_scores_gemma":[0.87329257,0.007795524,0.0007139565,0.002260017,0.00036356345,0.00013831303,0.009018373,0.00008352467,0.106334224],"study_design_codex":"observational","study_design_gemma":"not_applicable","domain_scores_codex":[0.9988545,0.0000767718,0.00004331836,0.00016734634,0.00061093253,0.00024704586],"domain_scores_gemma":[0.9935969,0.0013648875,0.0016778015,0.00020942907,0.001881699,0.0012691853],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0009732002,0.00024446438,0.00023792502,0.0039518657,0.0012756293,0.0017112114,0.000506613,0.00047102393,0.013048255],"category_scores_gemma":[0.004613109,0.00014184797,0.00024164439,0.004943949,0.00051215757,0.0010342785,0.0012379952,0.001014946,0.0021305813],"study_design_candidate":"not_applicable","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":[0.00026024168,0.0002603879,0.58511716,0.0004224188,0.000092653645,0.0008690961,0.006264816,0.0006320922,0.0015635169,0.035890765,0.200072,0.16855484],"study_design_scores_gemma":[0.000012345314,0.0000888805,0.7750907,0.0001822635,0.000033576485,0.0002831159,0.0031384958,0.00029107436,0.00088954956,0.00033112513,0.21963923,0.000019757768],"about_ca_topic_score_codex":0.06621105,"about_ca_topic_score_gemma":0.088355385,"teacher_disagreement_score":0.06621105,"about_ca_system_score_codex":0.003025579,"about_ca_system_score_gemma":0.004441646,"threshold_uncertainty_score":0.13165128},"labels":[],"label_agreement":null},{"id":"W1841578255","doi":"10.1139/juvs-2013-0005","title":"A hybrid propulsion system for a high-endurance UAV: configuration selection, aerodynamic study, and gas turbine bench tests","year":2014,"lang":"en","type":"article","venue":"Journal of Unmanned Vehicle Systems","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":19,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Propulsion; Payload (computing); Automotive engineering; Electrically powered spacecraft propulsion; Battery pack; Propeller; Electric motor; Test bench; Aerodynamics; Range (aeronautics); Engineering; Aerospace engineering; Battery (electricity); Electric generator; Power (physics); Computer science; Marine engineering; Mechanical engineering","score_opus":0.010201107065909524,"score_gpt":0.2415662773789908,"score_spread":0.2313651703130813,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1841578255","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":[0.9786542,0.0003809567,0.019177938,0.000057159996,0.000036230645,0.00010287917,0.00012753955,0.00023690781,0.0012261331],"genre_scores_gemma":[0.9928885,0.00009601201,0.006033307,0.0000111412155,0.0000069914304,0.00004280267,0.000103897815,0.00001607384,0.0008012718],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998547,0.00003386455,0.000012142759,0.000023347504,0.000051632098,0.000024340992],"domain_scores_gemma":[0.99973005,0.00006586709,0.000039797542,0.000045137484,0.000076740085,0.000042351494],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00028508407,0.0004255171,0.00034424584,0.00046892825,0.00031359732,0.00025525867,0.0003335582,0.00038878186,0.0011888501],"category_scores_gemma":[0.0004159872,0.000100459336,0.0002273939,0.0001829614,0.00026282854,0.00039446334,0.00028227887,0.00023264847,0.00029317293],"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":[0.001014267,0.0003464426,0.0074966312,0.00055078784,0.00007605226,0.00092538033,0.0003899656,0.030146165,0.90665025,0.0006533162,0.00082797225,0.050922807],"study_design_scores_gemma":[0.0002224501,0.02413087,0.06000465,0.00009795859,0.00014053642,0.0017212076,0.0006500985,0.124798276,0.77697504,0.0005229864,0.010591627,0.0001443598],"about_ca_topic_score_codex":0.0003457796,"about_ca_topic_score_gemma":0.0003576115,"teacher_disagreement_score":0.0011888501,"about_ca_system_score_codex":0.00015179084,"about_ca_system_score_gemma":0.000110723675,"threshold_uncertainty_score":0.0039770603},"labels":[],"label_agreement":null},{"id":"W1965857624","doi":"10.5589/q03-902","title":"Erratum: CFD Analaysis for Simulated Altitude Testing of Rocket Motors","year":2003,"lang":"en","type":"erratum","venue":"Canadian aeronautics and space journal","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Computational fluid dynamics; Aeronautics; Rocket (weapon); Aerospace engineering; Altitude (triangle); Engineering; Meteorology; Marine engineering; Environmental science; Physics; Mathematics","score_opus":0.028699740398875413,"score_gpt":0.25379083908301653,"score_spread":0.22509109868414112,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1965857624","genre_codex":"empirical","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"other","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.4198125,0.0072487853,0.33077848,0.017711302,0.040696543,0.0007731321,0.018917702,0.018352786,0.14570868],"genre_scores_gemma":[0.6582028,0.003371872,0.12308484,0.0014868851,0.00078040204,0.00040496106,0.008441868,0.002655559,0.20157075],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.99954647,0.000032710457,0.000047074493,0.000031295993,0.00031445778,0.000027928083],"domain_scores_gemma":[0.9982053,0.0007953594,0.00010997674,0.00010141314,0.00074657984,0.00004133097],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00042135714,0.00041132604,0.00033266356,0.00083572353,0.0007231892,0.0007878183,0.00069307716,0.0010147982,0.039262205],"category_scores_gemma":[0.0034190235,0.00020477442,0.00051808986,0.0005726257,0.00024785384,0.0006720828,0.00035506152,0.00059089286,0.004717368],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0016994814,0.0002480481,0.025861822,0.0018417573,0.00008313001,0.0041468814,0.0007087432,0.2730345,0.0677125,0.014002255,0.32662377,0.2840371],"study_design_scores_gemma":[0.00021217941,0.00052881736,0.019930074,0.0006482209,0.00010219389,0.0012918536,0.000853059,0.45436713,0.07282553,0.004658613,0.44440058,0.00018169986],"about_ca_topic_score_codex":0.0056162775,"about_ca_topic_score_gemma":0.0076450305,"teacher_disagreement_score":0.039262205,"about_ca_system_score_codex":0.0008055292,"about_ca_system_score_gemma":0.00095502374,"threshold_uncertainty_score":0.13134515},"labels":[],"label_agreement":null},{"id":"W1970147180","doi":"10.1260/175682709788083399","title":"Simulation of Axial Combustion Instability Development and Suppression in Solid Rocket Motors","year":2009,"lang":"en","type":"article","venue":"International Journal of Spray and Combustion Dynamics","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":13,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Propellant; Instability; Solid-fuel rocket; Mechanics; Combustion; Rocket (weapon); Transient (computer programming); Materials science; Acceleration; Computer simulation; Aerospace engineering; Physics; Classical mechanics; Computer science; Engineering; Chemistry","score_opus":0.014710645113521893,"score_gpt":0.28880205654841273,"score_spread":0.27409141143489085,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1970147180","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":[0.97875273,0.000043837023,0.018001594,0.00004775384,0.000009108862,0.000032958087,0.000075983706,0.0001389339,0.0028970565],"genre_scores_gemma":[0.99577636,0.000022677099,0.0033873199,0.000005734467,0.0000010541299,0.00001567385,0.000047761096,0.000011864257,0.00073153165],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999168,0.000016573635,0.0000037779123,0.000009357488,0.00003151783,0.000021969485],"domain_scores_gemma":[0.99951136,0.00029464246,0.00007035626,0.0000203363,0.00006347356,0.000039840397],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00019249512,0.0002767578,0.00032371414,0.00024764548,0.00024653002,0.00033787102,0.00042920254,0.00048863643,0.0012401751],"category_scores_gemma":[0.0010883481,0.00014432233,0.00024897745,0.0001941502,0.00044170493,0.00027259972,0.00029321987,0.00032957568,0.00008512785],"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":[0.00020278612,0.00006502068,0.0030143065,0.00003618342,0.000009446737,0.00013596615,0.00007535176,0.982141,0.010283971,0.0010935867,0.00011400184,0.0028283105],"study_design_scores_gemma":[0.000009852893,0.00004314909,0.00036755175,0.0000013923197,0.0000015613524,0.000007743143,0.000011650448,0.9974253,0.0019488764,0.00010057917,0.00008015813,0.0000021458914],"about_ca_topic_score_codex":0.0051234425,"about_ca_topic_score_gemma":0.0035795646,"teacher_disagreement_score":0.0051234425,"about_ca_system_score_codex":0.00043290813,"about_ca_system_score_gemma":0.00042701673,"threshold_uncertainty_score":0.010187209},"labels":[],"label_agreement":null},{"id":"W1970811871","doi":"10.1002/1521-4087(200106)26:3<118::aid-prep118>3.0.co;2-0","title":"On the Optimization of GAP-based Ducted Rocket Fuels from Gas Generator Exhaust Characterization","year":2001,"lang":"en","type":"article","venue":"Propellants Explosives Pyrotechnics","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":12,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Bombardier Recreational Products (Canada)","funders":"","keywords":"Gas generator; Exhaust gas; Carbon monoxide; Rocket (weapon); Exhaust gas recirculation; Carbon fibers; Soot; Environmental science; Materials science; Hydrogen; Combustion; Aerospace engineering; Waste management; Chemistry; Engineering; Composite material; Composite number","score_opus":0.04186693361204328,"score_gpt":0.2389748910964752,"score_spread":0.19710795748443194,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1970811871","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":[0.9842852,0.00030158725,0.013681419,0.000021891768,0.0000030940885,0.000040226398,0.00013092416,0.00010312985,0.0014325735],"genre_scores_gemma":[0.9815639,0.00030162637,0.016540315,0.000008307015,0.000001966107,0.00003227529,0.00039409715,0.000052841522,0.0011047011],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99987197,0.000015074874,0.000009470908,0.000029728366,0.00005818595,0.000015608884],"domain_scores_gemma":[0.9998934,0.000029889397,0.000025690208,0.000009974907,0.000033893295,0.000007056828],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016320913,0.00038717812,0.0004065101,0.0002629995,0.00015308287,0.00043294358,0.00031531753,0.00023421038,0.0007512169],"category_scores_gemma":[0.00036809398,0.0001496525,0.00015046421,0.00028941873,0.00012370973,0.00033255448,0.00024437282,0.00021948619,0.00026508493],"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":[0.00032701882,0.0000963506,0.0016095531,0.00020438529,0.000012503672,0.00009819437,0.000030215851,0.015637524,0.95633006,0.0002825131,0.00007579143,0.025295883],"study_design_scores_gemma":[0.00002512283,0.00078652555,0.0045025004,0.000007894882,0.00002091865,0.0001032158,0.000040917254,0.03686972,0.9560891,0.00011444413,0.0014305572,0.0000090725025],"about_ca_topic_score_codex":0.00048252373,"about_ca_topic_score_gemma":0.0012545295,"teacher_disagreement_score":0.0007512169,"about_ca_system_score_codex":0.0002313436,"about_ca_system_score_gemma":0.0002021678,"threshold_uncertainty_score":0.0025131106},"labels":[],"label_agreement":null},{"id":"W1973048364","doi":"10.1115/gt2007-27517","title":"Lycoming T-53 Gas Turbine Engine Modification for Industrial Application","year":2007,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","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":"Magellan Aerospace (Canada)","funders":"","keywords":"Automotive engineering; Rotor (electric); Mechanical engineering; Turbine; Gas compressor; Industrial gas; Aerospace; Combustion chamber; Natural gas; Electricity generation; Exhaust gas; Engineering; Combustion; Power (physics); Aerospace engineering; Waste management","score_opus":0.06721573522141269,"score_gpt":0.31137478164353,"score_spread":0.2441590464221173,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1973048364","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":[0.5550935,0.0033862228,0.21445014,0.0006871493,0.0016049246,0.002150104,0.005680024,0.021305699,0.19564217],"genre_scores_gemma":[0.7667294,0.001506963,0.10052269,0.0004648659,0.0000897642,0.00071750954,0.009044753,0.0019007189,0.119023316],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99967694,0.000016043852,0.000017089182,0.000046436202,0.00019316633,0.000050424675],"domain_scores_gemma":[0.9998375,0.000007371547,0.00001752046,0.00003406333,0.000087988454,0.000015513091],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018818029,0.00042045294,0.00031506692,0.00040768308,0.00027384565,0.00049075985,0.00058829697,0.000444921,0.010012356],"category_scores_gemma":[0.00032239442,0.0002034196,0.0005916472,0.00026093595,0.00011362788,0.00035509263,0.0003851681,0.00061094627,0.0064047677],"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":[0.0006746795,0.00024212814,0.003081773,0.00050856476,0.00003374707,0.0008118321,0.000095901494,0.004434823,0.8172906,0.0022986725,0.016371867,0.15415545],"study_design_scores_gemma":[0.00012717792,0.0013620283,0.014776127,0.00006553773,0.000060102673,0.0017153685,0.000051324285,0.008877751,0.6250358,0.0002487801,0.34760788,0.00007197987],"about_ca_topic_score_codex":0.0020368088,"about_ca_topic_score_gemma":0.0026151724,"teacher_disagreement_score":0.010012356,"about_ca_system_score_codex":0.00038717853,"about_ca_system_score_gemma":0.00063303916,"threshold_uncertainty_score":0.03349465},"labels":[],"label_agreement":null},{"id":"W1977683007","doi":"10.2514/1.b34967","title":"Deep Throttle of a Nitrous Oxide and Hydroxyl-Terminated Polybutadiene Hybrid Rocket Motor","year":2014,"lang":"en","type":"article","venue":"Journal of Propulsion and Power","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":34,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"McMaster University","keywords":"Throttle; Solid-fuel rocket; Aerospace engineering; Injector; Rocket (weapon); Automotive engineering; Chamber pressure; Materials science; Thrust; Combustor; Propellant; Liquid-propellant rocket; Specific impulse; Engineering; Combustion; Mechanical engineering; Chemistry","score_opus":0.005847883386204909,"score_gpt":0.22223677010125098,"score_spread":0.21638888671504608,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1977683007","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":[0.9982855,0.00002718432,0.0011458918,0.0000096056765,0.0000047239264,0.000007386191,0.000055807122,0.00004942794,0.00041432225],"genre_scores_gemma":[0.9981027,0.00001605249,0.0005942842,0.0000041348385,6.716592e-7,0.0000056562963,0.00004417752,0.000012169098,0.001220173],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998275,0.000012440553,0.000010206498,0.000031068466,0.000070942464,0.00004774449],"domain_scores_gemma":[0.99973124,0.00007956045,0.000041222473,0.000029531931,0.0000637568,0.00005461835],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020400016,0.00030508297,0.00029802238,0.00025231828,0.00023560126,0.00020806772,0.00039610744,0.00029912344,0.0020430642],"category_scores_gemma":[0.0003865899,0.00014047878,0.00014639959,0.0001627046,0.00023865091,0.0003488649,0.00029894695,0.00023154971,0.00023760267],"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":[0.0010227113,0.000077925884,0.0030076692,0.00007973742,0.000021711752,0.00035740144,0.00018273412,0.0041157883,0.9789771,0.0001651399,0.0002223856,0.011769781],"study_design_scores_gemma":[0.00004466959,0.0035656814,0.018050727,0.000012301124,0.000019384857,0.0001998566,0.00018811747,0.029321754,0.9466299,0.000083791434,0.0018534524,0.000030295545],"about_ca_topic_score_codex":0.0011376115,"about_ca_topic_score_gemma":0.0021829896,"teacher_disagreement_score":0.0020430642,"about_ca_system_score_codex":0.00028152362,"about_ca_system_score_gemma":0.00016242311,"threshold_uncertainty_score":0.0068347454},"labels":[],"label_agreement":null},{"id":"W1985128390","doi":"10.1007/s11630-003-0058-0","title":"Cryogenic cavitating flow in 2D laval nozzle","year":2003,"lang":"en","type":"article","venue":"Journal of Thermal Science","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":28,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Cavitation; Nozzle; Liquid-propellant rocket; Propellant; Rocket (weapon); Rocket engine nozzle; Liquid nitrogen; Materials science; Rocket engine; Mechanics; Thermodynamics; Flow (mathematics); Cryogenics; Aerospace engineering; Chemistry; Physics; Engineering","score_opus":0.020043407361454418,"score_gpt":0.2813812398773187,"score_spread":0.2613378325158643,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1985128390","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":[0.9890681,0.00032095655,0.005181253,0.00016113839,0.00004466006,0.000026138923,0.00008565467,0.00013984375,0.0049721887],"genre_scores_gemma":[0.9980913,0.00005188443,0.0006995814,0.000014200562,0.000016466594,0.000010070436,0.0000381473,0.000016686776,0.0010618384],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998673,0.000025374657,0.0000048507236,0.0000379497,0.000030796444,0.00003369019],"domain_scores_gemma":[0.99981946,0.00004774333,0.000034650242,0.00002133392,0.000033540695,0.000043333956],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002053007,0.00027872768,0.0005137383,0.00024833163,0.0006447284,0.0009963784,0.0005698862,0.0006348148,0.0016166791],"category_scores_gemma":[0.00047889966,0.00024017961,0.00025734407,0.00014404063,0.0010562525,0.0006114242,0.00074208766,0.00056388247,0.00022021338],"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":[0.0018929952,0.0002631824,0.010059232,0.00016529564,0.000061585364,0.0030261257,0.00069881993,0.117890514,0.83318335,0.022680733,0.0014712736,0.008606883],"study_design_scores_gemma":[0.000614893,0.0009912723,0.026623929,0.000040278836,0.000040358,0.0009102396,0.00036645785,0.77371484,0.18815686,0.003990892,0.0043919384,0.0001580354],"about_ca_topic_score_codex":0.002241657,"about_ca_topic_score_gemma":0.00067123974,"teacher_disagreement_score":0.002241657,"about_ca_system_score_codex":0.00092466123,"about_ca_system_score_gemma":0.0004690004,"threshold_uncertainty_score":0.00670892},"labels":[],"label_agreement":null},{"id":"W1985684554","doi":"10.2514/6.2010-85","title":"A Primer for University-Level Solid Rocket Motor Research and Development","year":2010,"lang":"en","type":"article","venue":"48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"McMaster University","keywords":"Primer (cosmetics); Solid-fuel rocket; Aeronautics; Computer science; Aerospace engineering; Engineering; Physics; Propellant","score_opus":0.08756515238135343,"score_gpt":0.3329067946437156,"score_spread":0.24534164226236216,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1985684554","genre_codex":"methods","genre_gemma":"methods","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0044891825,0.052678023,0.4401114,0.10049339,0.020620253,0.001711951,0.001395474,0.0105921775,0.36790812],"genre_scores_gemma":[0.025523568,0.053108238,0.47861782,0.01598713,0.0029531247,0.0021680922,0.002053388,0.0020908264,0.4174978],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9961132,0.00081425026,0.0004536636,0.00040385747,0.0019502778,0.00026474977],"domain_scores_gemma":[0.9934342,0.0013339277,0.0004171113,0.00096278614,0.0026790686,0.0011729567],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.006439631,0.00091021514,0.0006150453,0.0017616575,0.0014954994,0.004129238,0.00213115,0.0036202557,0.029061249],"category_scores_gemma":[0.007747519,0.000982584,0.00058266975,0.0014816385,0.0012608279,0.0073321783,0.0039012807,0.006634221,0.03674492],"study_design_candidate":"not_applicable","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":[0.00008609076,0.00047198555,0.00050482864,0.000658201,0.0000071425916,0.0004298545,0.0008193494,0.00079895806,0.010837857,0.1571213,0.26365653,0.5646079],"study_design_scores_gemma":[0.0000036719168,0.000065977205,0.00007932645,0.00016507907,0.0000015822566,0.00013534559,0.000066465764,0.00019184181,0.0019510138,0.0045859255,0.9927447,0.000009129464],"about_ca_topic_score_codex":0.00055807823,"about_ca_topic_score_gemma":0.001074185,"teacher_disagreement_score":0.029061249,"about_ca_system_score_codex":0.0019500916,"about_ca_system_score_gemma":0.0049415664,"threshold_uncertainty_score":0.09721959},"labels":[],"label_agreement":null},{"id":"W1989750326","doi":"10.1109/aero.2007.352879","title":"Propulsion System Prognostics R&amp;D Through the Technical Cooperation Program","year":2007,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","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":true,"ca_institutions":"National Research Council Canada","funders":"University of Virginia","keywords":"Prognostics; Propulsion; Aerospace; Work (physics); Engineering management; Key (lock); Systems engineering; Engineering; Process management; Aeronautics; Computer science; Computer security; Aerospace engineering","score_opus":0.03461064730022485,"score_gpt":0.32039188019028936,"score_spread":0.2857812328900645,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1989750326","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.051828284,0.008925774,0.30891487,0.036537345,0.0035180056,0.0021351827,0.006494921,0.0065849093,0.5750608],"genre_scores_gemma":[0.43115297,0.010260145,0.22219755,0.0029961355,0.0011768397,0.0013658213,0.010715609,0.0012142087,0.31892073],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9942729,0.0019987,0.00022381677,0.00043035342,0.0024156645,0.0006586118],"domain_scores_gemma":[0.98693466,0.0017894021,0.0013361675,0.0021972826,0.0063071707,0.0014353022],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.010986658,0.0010147953,0.0005252505,0.003772855,0.0013696084,0.0039478494,0.0009720164,0.0009256353,0.024904598],"category_scores_gemma":[0.01174867,0.0002963182,0.00041898777,0.004828166,0.0011019291,0.0025035953,0.0043445905,0.0014227316,0.0102554485],"study_design_candidate":"not_applicable","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":[0.0003380495,0.00031400303,0.01111298,0.0004241512,0.000051522187,0.00022929661,0.00053718954,0.0068429927,0.0052519087,0.07422687,0.09911009,0.80156094],"study_design_scores_gemma":[0.00013025089,0.0008143709,0.017841209,0.00021752635,0.000039202772,0.0005301121,0.0002969036,0.009660035,0.010141406,0.01703469,0.94325066,0.000043723885],"about_ca_topic_score_codex":0.004772343,"about_ca_topic_score_gemma":0.0032339138,"teacher_disagreement_score":0.024904598,"about_ca_system_score_codex":0.0021474918,"about_ca_system_score_gemma":0.023297917,"threshold_uncertainty_score":0.08331424},"labels":[],"label_agreement":null},{"id":"W1989955604","doi":"10.1115/pvp2004-3113","title":"CFD, Thermal and Stress Analysis for daVinci X-Prize Manned Space Mission: Computational Design Analysis - Part 1 (Keynote Lecture)","year":2004,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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":"Computational fluid dynamics; Software; Aerospace engineering; CAD; Systems engineering; Engineering design process; Computer Aided Design; Engineering; Excavator; Computer science; Simulation; Aeronautics; Mechanical engineering; Operating system; Engineering drawing","score_opus":0.03563623864159362,"score_gpt":0.28156059342853845,"score_spread":0.24592435478694483,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1989955604","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":[0.17247416,0.018964661,0.73962164,0.0022266058,0.0009617818,0.00025322702,0.0015342196,0.0021702072,0.061793525],"genre_scores_gemma":[0.73538244,0.0139817735,0.1846765,0.00025204732,0.00046892537,0.00041726916,0.0021172778,0.0008319129,0.06187192],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998122,0.00003862534,0.000009177411,0.000026660597,0.00009387063,0.000019462925],"domain_scores_gemma":[0.999845,0.00006460312,0.000012837349,0.000013353798,0.00005279002,0.000011260587],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00040360118,0.00053060765,0.000442095,0.0006109273,0.00051041896,0.0009788452,0.00039444433,0.0006594079,0.0035903428],"category_scores_gemma":[0.00064593175,0.00022816402,0.00052328216,0.00046043863,0.00037407724,0.0005286512,0.00044162598,0.0005634777,0.0010004033],"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":[0.00011194817,0.0000888887,0.005532912,0.0004255049,0.000049345235,0.00037681393,0.00023204142,0.6867354,0.02117421,0.019819232,0.022852642,0.24260114],"study_design_scores_gemma":[0.000011600919,0.00010532163,0.005570436,0.00007618208,0.000016457816,0.00021480449,0.00018226395,0.91947496,0.009826713,0.0094146365,0.055056304,0.000050317372],"about_ca_topic_score_codex":0.0038708025,"about_ca_topic_score_gemma":0.003108546,"teacher_disagreement_score":0.0038708025,"about_ca_system_score_codex":0.00065525435,"about_ca_system_score_gemma":0.0008187723,"threshold_uncertainty_score":0.012010872},"labels":[],"label_agreement":null},{"id":"W1993851138","doi":"10.1115/gt2011-45132","title":"Altitude Performance of a Turbojet With Alternate Fuels","year":2011,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"National Research Council Canada","funders":"National Research Council Canada","keywords":"Jet fuel; Kerosene; Turbojet; Environmental science; Aviation fuel; Work (physics); Diesel fuel; Automotive engineering; Aerospace engineering; Engineering; Mechanical engineering","score_opus":0.03340478985759064,"score_gpt":0.2257063702142644,"score_spread":0.19230158035667377,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1993851138","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":[0.99901056,0.00005930433,0.0003020089,0.0000048065494,0.000006219164,0.0000030692581,0.000040543833,0.000025838192,0.00054765353],"genre_scores_gemma":[0.99882,0.000044178036,0.00024147444,0.000004982819,0.0000014401726,0.0000016037063,0.00010020608,0.000007972613,0.0007780675],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.999741,0.000018719513,0.0000137911675,0.00003445394,0.00014040533,0.000051615898],"domain_scores_gemma":[0.99978644,0.000055028297,0.000032383916,0.000019381703,0.000078344754,0.00002839037],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016080764,0.00027270525,0.00027121717,0.00028274537,0.00027942078,0.00046934074,0.00030051006,0.00035050357,0.0018530356],"category_scores_gemma":[0.0003812808,0.00014808663,0.00021991186,0.000276988,0.0002288082,0.00048733148,0.00029851662,0.00025746776,0.0003237249],"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":[0.0025626041,0.0002470833,0.01164499,0.00013833022,0.000040165807,0.00040248266,0.0002399237,0.007115667,0.9616606,0.00015302154,0.0001743883,0.015620653],"study_design_scores_gemma":[0.0000671315,0.003937979,0.026086722,0.000010185212,0.00003915488,0.00017322598,0.00016486563,0.011688802,0.956665,0.00004625599,0.0010953576,0.000025387366],"about_ca_topic_score_codex":0.0017349314,"about_ca_topic_score_gemma":0.0016885502,"teacher_disagreement_score":0.0018530356,"about_ca_system_score_codex":0.00022117101,"about_ca_system_score_gemma":0.00015708478,"threshold_uncertainty_score":0.006199062},"labels":[],"label_agreement":null},{"id":"W2001653310","doi":"10.1115/gt2010-23402","title":"Limited Qualification Tests of an F404 Engine With Blended Fischer Tropsch SPK and NATO F-34 Fuel","year":2010,"lang":"en","type":"article","venue":"Volume 1: Aircraft Engine; Ceramics; Coal, Biomass and Alternative Fuels; Education; Electric Power; Manufacturing Materials and Metallurgy","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"Communications Security Establishment; Department of National Defence; National Research Council Canada","funders":"U.S. Air Force; U.S. Navy; Ministère de la Défense Nationale","keywords":"Operability; Combustor; Engineering; Turbofan; Jet engine; Instrumentation (computer programming); Benchmark (surveying); Test (biology); Automotive engineering; Combustion; Computer science; Mechanical engineering; Systems engineering; Reliability engineering","score_opus":0.008556561406468854,"score_gpt":0.2393123178812021,"score_spread":0.23075575647473326,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2001653310","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":[0.9995491,0.000024932759,0.00024477753,0.0000026411844,0.0000015217379,0.0000056052527,0.000022639484,0.0000073393594,0.0001413859],"genre_scores_gemma":[0.9986198,0.00003533332,0.00057318807,0.000004419157,0.0000010797189,0.0000044929334,0.00009289712,0.000006606678,0.0006622882],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99943405,0.00008378822,0.000038478363,0.000061671,0.0003075861,0.00007433929],"domain_scores_gemma":[0.9995679,0.00011857466,0.00006504485,0.000034895646,0.00016181904,0.00005172852],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006242563,0.00046640262,0.00043170148,0.00047603442,0.00038925395,0.00024294498,0.00043731567,0.00044948614,0.0013795057],"category_scores_gemma":[0.0010062313,0.00017857736,0.0003465832,0.00036319482,0.0002895711,0.00038004355,0.00033812653,0.00021247247,0.00024420742],"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":[0.004087444,0.0004773314,0.020554412,0.00020147723,0.000056195633,0.00039557746,0.0003320178,0.0057357224,0.9524967,0.00010851595,0.000100256584,0.0154543845],"study_design_scores_gemma":[0.00008990262,0.01417826,0.050774604,0.000015377062,0.00007853884,0.0003978574,0.00029354775,0.005314564,0.92761755,0.00005432045,0.0011416305,0.00004390618],"about_ca_topic_score_codex":0.0058690375,"about_ca_topic_score_gemma":0.009504733,"teacher_disagreement_score":0.0058690375,"about_ca_system_score_codex":0.00039457166,"about_ca_system_score_gemma":0.00043172494,"threshold_uncertainty_score":0.011669755},"labels":[],"label_agreement":null},{"id":"W2010728540","doi":"10.3103/s1068799811040118","title":"Generalization of experimental data on two-phase critical efflux through axisymmetric channels","year":2011,"lang":"en","type":"article","venue":"Russian Aeronautics","topic":"Rocket and propulsion systems research","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":"Rotational symmetry; Mechanics; Nozzle; Adiabatic process; Thermodynamics; Atmospheric pressure; Volumetric flow rate; Phase (matter); Generalization; Flow (mathematics); Thrust; Efflux; Chemistry; Materials science; Physics; Mathematics; Meteorology; Mathematical analysis","score_opus":0.15366953202030856,"score_gpt":0.3846296292673284,"score_spread":0.23096009724701985,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2010728540","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":[0.992097,0.0002785896,0.005727613,0.000020272144,0.0000053079243,0.000024009842,0.00023219363,0.00008881444,0.0015261287],"genre_scores_gemma":[0.9985618,0.00013793891,0.0008648937,0.0000052624387,0.0000028346903,0.000020379352,0.00019196613,0.000014440997,0.00020046462],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99980885,0.000017822691,0.0000133346975,0.000037934486,0.00007482475,0.00004727552],"domain_scores_gemma":[0.99898165,0.00041202485,0.00015692401,0.00016954412,0.00023708878,0.00004270234],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00039097044,0.00033057603,0.00033883052,0.00040056757,0.00029987382,0.00034278329,0.00036016147,0.00017542178,0.0023282552],"category_scores_gemma":[0.001401168,0.00012766894,0.00016546508,0.00043493306,0.0005388234,0.00047542132,0.00037024452,0.0005076046,0.00023218134],"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":[0.0002275775,0.000030343752,0.0011510014,0.0000973823,0.0000043313953,0.000056614444,0.00010293344,0.0010095335,0.99513286,0.0002563038,0.00003270065,0.0018984238],"study_design_scores_gemma":[0.000016152246,0.0003216161,0.007467017,0.000007584214,0.0000066639072,0.000090617075,0.00006366333,0.0035308527,0.9877152,0.0001445802,0.0006241134,0.000011903821],"about_ca_topic_score_codex":0.00058018736,"about_ca_topic_score_gemma":0.00024624058,"teacher_disagreement_score":0.0023282552,"about_ca_system_score_codex":0.00025752938,"about_ca_system_score_gemma":0.00016416918,"threshold_uncertainty_score":0.0077887774},"labels":[],"label_agreement":null},{"id":"W2011795239","doi":"10.4271/2014-01-0921","title":"Fuel Tank Strap Fatigue Sensitivity Study under Fuel Level Variation and Payload Variation","year":2014,"lang":"en","type":"article","venue":"SAE technical papers on CD-ROM/SAE technical paper series","topic":"Rocket and propulsion systems research","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":"Chrysler (Canada)","funders":"","keywords":"Payload (computing); Variation (astronomy); Sensitivity (control systems); Automotive engineering; Environmental science; Engineering; Computer science; Physics; Electronic engineering","score_opus":0.03770539074891912,"score_gpt":0.2818851864163722,"score_spread":0.2441797956674531,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2011795239","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":[0.9931202,0.00015220355,0.004905077,0.000040553696,0.000016524618,0.000022470158,0.00042391446,0.00021476836,0.0011041709],"genre_scores_gemma":[0.998765,0.000044453976,0.00047046933,0.00001642136,0.0000024938313,0.0000067331453,0.0002646949,0.000017112421,0.00041250297],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99949884,0.00004941577,0.000028861867,0.00015102042,0.00019515392,0.00007666448],"domain_scores_gemma":[0.9985662,0.00056963274,0.00014870816,0.00020893397,0.00044407995,0.00006244279],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004173315,0.0003149249,0.00033742134,0.0007747714,0.00020085875,0.00024146843,0.00047864637,0.0007026219,0.0013951549],"category_scores_gemma":[0.001644794,0.00021119435,0.00040375703,0.0005021263,0.00021732652,0.0004863938,0.00031473397,0.0003051676,0.00034265209],"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":[0.0021155498,0.00043597963,0.052288778,0.0003405911,0.0001861962,0.0014165017,0.00047158988,0.1626041,0.72240496,0.00020250086,0.0013177473,0.056215547],"study_design_scores_gemma":[0.00004088223,0.0037021262,0.18492371,0.00004385931,0.00014549142,0.0011603122,0.00051920785,0.37982368,0.427521,0.00024992952,0.0017645113,0.000105331186],"about_ca_topic_score_codex":0.0043179975,"about_ca_topic_score_gemma":0.0045865844,"teacher_disagreement_score":0.0043179975,"about_ca_system_score_codex":0.00036391482,"about_ca_system_score_gemma":0.00014917606,"threshold_uncertainty_score":0.008585751},"labels":[],"label_agreement":null},{"id":"W2015480736","doi":"10.1016/j.ast.2003.09.001","title":"Star-grain rocket motor – nonsteady internal ballistics","year":2003,"lang":"en","type":"article","venue":"Aerospace Science and Technology","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":43,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Internal ballistics; Propellant; Solid-fuel rocket; Rocket (weapon); Ballistics; Mechanics; Instability; Internal flow; Combustion; Vibration; Oscillation (cell signaling); Aerospace engineering; Acceleration; Physics; Flow (mathematics); Materials science; Engineering; Classical mechanics; Acoustics; Chemistry","score_opus":0.010361874882998338,"score_gpt":0.24793502016219426,"score_spread":0.23757314527919593,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2015480736","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":[0.7734501,0.00042032474,0.17745894,0.00023161437,0.00012573814,0.00007355135,0.000183257,0.00080910465,0.047247395],"genre_scores_gemma":[0.98257554,0.00007894402,0.0044075046,0.00002185633,0.000008203678,0.000007994037,0.00014325074,0.00006583199,0.012690878],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99990904,0.000008333928,0.0000047068283,0.000022623719,0.000038420287,0.000016943526],"domain_scores_gemma":[0.99981445,0.000026286323,0.000035371442,0.000043099517,0.00005567246,0.000025119114],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012211135,0.00026222382,0.00078498863,0.00021333397,0.0003823486,0.0005252851,0.00043247623,0.00044340483,0.0035105823],"category_scores_gemma":[0.00041641924,0.00016254922,0.00019555366,0.00022152366,0.0005318297,0.0005985604,0.0006663793,0.0002633465,0.0009686406],"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":[0.00400737,0.0003216288,0.017133607,0.00052085856,0.00015968281,0.001956193,0.00028088354,0.3976261,0.38602236,0.065995626,0.0066273124,0.11934842],"study_design_scores_gemma":[0.000087558554,0.0008675931,0.010073658,0.00000905185,0.000025847776,0.0008465543,0.000089541994,0.8945427,0.079773724,0.006018871,0.007633801,0.000031076786],"about_ca_topic_score_codex":0.0019450058,"about_ca_topic_score_gemma":0.002595833,"teacher_disagreement_score":0.0035105823,"about_ca_system_score_codex":0.0003195696,"about_ca_system_score_gemma":0.00058917847,"threshold_uncertainty_score":0.011744082},"labels":[],"label_agreement":null},{"id":"W2020971142","doi":"10.6108/kspe.2014.18.1.008","title":"The Effect of Pressure and Oxidation Mole Fraction on Ablation Rate of Graphite for Nozzle Throat Insert","year":2014,"lang":"en","type":"article","venue":"Journal of the Korean Society of Propulsion Engineers","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":1,"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; Graphite; Mole fraction; Ablation; Materials science; Propulsion; Combustion; Mass fraction; Analytical Chemistry (journal); Composite material; Chemistry; Aerospace engineering; Thermodynamics; Engineering; Physics; Chromatography; Organic chemistry","score_opus":0.006788745791956233,"score_gpt":0.2357489710101248,"score_spread":0.22896022521816856,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2020971142","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":[0.99752325,0.00047578497,0.0010903921,0.0000134901475,0.000008544395,0.000006080254,0.0000903551,0.000050117535,0.0007420548],"genre_scores_gemma":[0.99828416,0.00025238417,0.00067212904,0.000009607451,0.0000034242832,0.0000069311095,0.00011270151,0.000019161438,0.0006394479],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99978334,0.000022239947,0.000015564636,0.000049572023,0.00008608696,0.00004323011],"domain_scores_gemma":[0.99906975,0.00057392614,0.00015118092,0.00004621138,0.00012128385,0.00003780976],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023687906,0.00025128547,0.00025986886,0.00025795453,0.00016718436,0.00026422224,0.00028445665,0.0003362832,0.0015511299],"category_scores_gemma":[0.0011779492,0.00023155128,0.0003123221,0.00024214879,0.00018329194,0.000453656,0.00014953225,0.00028192357,0.0002564256],"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":[0.0006606983,0.00002499277,0.0040763123,0.00011401171,0.000014903342,0.00019372103,0.00009332471,0.0012648369,0.9851548,0.000060370287,0.000077660676,0.008264342],"study_design_scores_gemma":[0.000010439224,0.0010626108,0.033056516,0.000008478616,0.000037203125,0.000247876,0.00008803934,0.0034531213,0.9611918,0.000027437567,0.0007975092,0.00001903959],"about_ca_topic_score_codex":0.00045406868,"about_ca_topic_score_gemma":0.0005889977,"teacher_disagreement_score":0.0015511299,"about_ca_system_score_codex":0.000112976384,"about_ca_system_score_gemma":0.00012217704,"threshold_uncertainty_score":0.0051890016},"labels":[],"label_agreement":null},{"id":"W2026622740","doi":"10.2514/2.854","title":"Convergence Acceleration of an Inverse Design Technique for Constructing Turbomachinery Cascades","year":2000,"lang":"en","type":"article","venue":"AIAA Journal","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Alberta","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Turbomachinery; Acceleration; Convergence (economics); Inverse; Aerospace engineering; Applied mathematics; Computer science; Mechanics; Mathematics; Physics; Engineering; Classical mechanics; Geometry; Economics","score_opus":0.042867125820992565,"score_gpt":0.29638732400188894,"score_spread":0.2535201981808964,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2026622740","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":[0.009444304,0.000027949809,0.987282,0.000024711791,0.000020293313,0.000030036827,0.00000587353,0.00017895992,0.0029859028],"genre_scores_gemma":[0.28681096,0.00013817535,0.70730543,0.000040524577,0.00003348008,0.00012732988,0.000041243493,0.00016924368,0.0053335726],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997385,0.00005621694,0.000011200718,0.000028116689,0.00014812745,0.000017781405],"domain_scores_gemma":[0.99959403,0.00016719241,0.0000299297,0.00006504468,0.00012698748,0.000016789792],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006099824,0.0006195327,0.0005469332,0.00051747536,0.00038024486,0.00048135416,0.00059989735,0.0004997627,0.004043351],"category_scores_gemma":[0.0015108574,0.000365986,0.00055283395,0.00024157227,0.0005729175,0.00060299487,0.0008077933,0.00094950746,0.0008730257],"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":[0.00043032804,0.00022707164,0.001037979,0.00039053857,0.00005651166,0.00020707055,0.0004644078,0.3315405,0.20369089,0.110505305,0.0022333313,0.3492161],"study_design_scores_gemma":[0.000025409701,0.00019910636,0.00016121558,0.000015470843,0.000014722453,0.00008803591,0.00002152774,0.96811914,0.022853421,0.005064603,0.00342713,0.000010225388],"about_ca_topic_score_codex":0.0006974403,"about_ca_topic_score_gemma":0.0009924822,"teacher_disagreement_score":0.004043351,"about_ca_system_score_codex":0.00023749893,"about_ca_system_score_gemma":0.00048147253,"threshold_uncertainty_score":0.01352632},"labels":[],"label_agreement":null},{"id":"W2030245675","doi":"10.2514/1.b34226","title":"Rim-Rotor Rotary Ramjet Engine, Part 2: Quasi-One-Dimensional Aerothermodynamic Design","year":2012,"lang":"en","type":"article","venue":"Journal of Propulsion and Power","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":11,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Ramjet; Windage; Aerospace engineering; Combustion chamber; Rotor (electric); Combustion; Mechanics; Propulsion; Materials science; Mechanical engineering; Aerodynamics; Automotive engineering; Mach number; Engineering; Combustor; Physics","score_opus":0.027710199002971257,"score_gpt":0.25306345249101964,"score_spread":0.22535325348804838,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2030245675","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":[0.15018691,0.003197976,0.81303084,0.0002911,0.00023509112,0.00041453275,0.00068501703,0.0018740749,0.030084508],"genre_scores_gemma":[0.7553079,0.0019497039,0.21953546,0.00008081383,0.00004400741,0.00051296264,0.00074570306,0.00024004662,0.021583429],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998404,0.000025793544,0.000008241117,0.000019575968,0.00009412464,0.000011823785],"domain_scores_gemma":[0.99994755,0.000008064147,0.0000118949965,0.000012937916,0.000016010312,0.0000036005054],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024390958,0.00035207995,0.00036276985,0.00019070803,0.00019496829,0.0004849385,0.00070367934,0.0003669086,0.0016356262],"category_scores_gemma":[0.00015377135,0.00030142482,0.0004576131,0.00014354003,0.0002362018,0.00035257218,0.0002090068,0.00035158487,0.0006537623],"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":[0.00044085967,0.00022590836,0.0024293934,0.0015131416,0.00008126649,0.00035513606,0.00013300017,0.45156026,0.3843596,0.031490132,0.0035609975,0.123850346],"study_design_scores_gemma":[0.00014824646,0.00088360865,0.003728053,0.000032195607,0.00004464868,0.00053396093,0.000022494016,0.871487,0.080774866,0.0024480924,0.03983561,0.00006121393],"about_ca_topic_score_codex":0.00044574158,"about_ca_topic_score_gemma":0.00066619704,"teacher_disagreement_score":0.0016356262,"about_ca_system_score_codex":0.0003585397,"about_ca_system_score_gemma":0.00039409765,"threshold_uncertainty_score":0.005471766},"labels":[],"label_agreement":null},{"id":"W2030676768","doi":"10.1007/s00348-014-1726-4","title":"Study of the behavior of vapor fraction in a turbopump inducer using an X-ray measurement technique","year":2014,"lang":"en","type":"article","venue":"Experiments in Fluids","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Thomson Reuters (Canada)","funders":"","keywords":"Detector; Physics; Optics; Rotational speed; Mechanics; Materials science","score_opus":0.11234767679685859,"score_gpt":0.3593336671976585,"score_spread":0.24698599040079994,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2030676768","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":[0.9904689,0.0004313114,0.0074733635,0.00007765556,0.0000112089065,0.000012392938,0.000073080526,0.00009397022,0.0013581838],"genre_scores_gemma":[0.99524826,0.00022559696,0.0027830754,0.000014366966,0.0000075300386,0.000009283914,0.000061026454,0.000041377316,0.0016094713],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998635,0.00002812562,0.000006496745,0.00003396398,0.00004071381,0.000027041415],"domain_scores_gemma":[0.9994797,0.0002457853,0.00010506951,0.00004998043,0.00008275717,0.000036659272],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00026085708,0.00023161816,0.0002201737,0.00017941675,0.00030109938,0.00029080614,0.0003669693,0.000225925,0.0014570749],"category_scores_gemma":[0.0005114007,0.00016548527,0.00014887823,0.00024412898,0.00035191988,0.00037738224,0.00019590001,0.00044173922,0.0002544044],"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":[0.00011741708,0.000010719189,0.000497354,0.000020565667,0.0000026771156,0.000029929006,0.000046177443,0.00006645057,0.99803156,0.00008459921,0.000019843634,0.0010726625],"study_design_scores_gemma":[0.000003134063,0.000119062424,0.002739828,0.0000017482391,0.0000059702284,0.000036916153,0.000021904078,0.0011802022,0.995567,0.000010648412,0.00031128485,0.000002406593],"about_ca_topic_score_codex":0.00090606057,"about_ca_topic_score_gemma":0.00063752045,"teacher_disagreement_score":0.0014570749,"about_ca_system_score_codex":0.00025986813,"about_ca_system_score_gemma":0.0002785558,"threshold_uncertainty_score":0.0048743486},"labels":[],"label_agreement":null},{"id":"W2030955751","doi":"10.1361/105996300770350140","title":"Design of a New Nozzle for Direct Current Plasma Guns with Improved Spraying Parameters","year":2000,"lang":"en","type":"article","venue":"Journal of Thermal Spray Technology","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":17,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto","funders":"Bộ Giáo dục và Ðào tạo; Ministère de l’Éducation, Gouvernement de l’Ontario; University of Toronto","keywords":"Nozzle; Shroud; Materials science; Coating; Porosity; Gas dynamic cold spray; Microstructure; Thermal spraying; Plasma; Conical surface; Composite material; Jet (fluid); Curvilinear coordinates; Metallurgy; Spray nozzle; Aluminium; Mechanics; Mechanical engineering","score_opus":0.02935207704025971,"score_gpt":0.27044256164301583,"score_spread":0.24109048460275612,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2030955751","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":[0.23148738,0.0033720336,0.75223786,0.0007997993,0.0009790265,0.0009957594,0.0003244463,0.0028128687,0.006990915],"genre_scores_gemma":[0.44794425,0.0008723065,0.5462904,0.00021702705,0.00017207724,0.00032100774,0.00023100646,0.00021078649,0.0037411521],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99952674,0.000022300452,0.00005078646,0.00011892968,0.00023510178,0.000046238158],"domain_scores_gemma":[0.9992557,0.000095205876,0.0001684981,0.00006704936,0.00031170784,0.00010167838],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0008128897,0.0006064628,0.0011438375,0.0005041591,0.00058850244,0.0012466154,0.0019455059,0.0013847484,0.0012114645],"category_scores_gemma":[0.0007015614,0.0008319177,0.00068036333,0.00030179232,0.00038597526,0.0011424364,0.0009272069,0.0006724954,0.00037832325],"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":[0.00029994932,0.00012538688,0.0011980006,0.0004385373,0.000053863874,0.00026903598,0.00009249912,0.005085429,0.94648993,0.0029886249,0.0011351001,0.04182364],"study_design_scores_gemma":[0.0008020179,0.0033335006,0.007450097,0.00006518703,0.00029204492,0.002596377,0.00006738507,0.15698187,0.78321636,0.00094236614,0.04400004,0.00025286098],"about_ca_topic_score_codex":0.00043645402,"about_ca_topic_score_gemma":0.00067296793,"teacher_disagreement_score":0.0019455059,"about_ca_system_score_codex":0.0009027283,"about_ca_system_score_gemma":0.0010193397,"threshold_uncertainty_score":0.0065497756},"labels":[],"label_agreement":null},{"id":"W2031608507","doi":"10.1002/pamm.200810665","title":"Flare gas extraction by a Laval nozzle","year":2008,"lang":"en","type":"article","venue":"PAMM","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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; Gas compressor; Injector; Extraction (chemistry); Flare; Mechanical engineering; Engineering; Nuclear engineering; Materials science; Physics; Chemistry; Aerospace engineering; Chromatography","score_opus":0.021843694459120457,"score_gpt":0.25953677170507666,"score_spread":0.2376930772459562,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2031608507","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":[0.8651172,0.0034736048,0.12142884,0.00046267707,0.00020297985,0.00014799948,0.00031844244,0.0011186039,0.0077296663],"genre_scores_gemma":[0.93434656,0.0007931415,0.05575286,0.00021284078,0.00003755548,0.000034520446,0.00029176462,0.000066609995,0.00846415],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997676,0.000018153993,0.000011739736,0.000060172,0.00008655047,0.000055701716],"domain_scores_gemma":[0.9998853,0.000023120901,0.000025470395,0.0000149547495,0.00003117985,0.000019827552],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023829077,0.0002470439,0.00033510372,0.0003452504,0.00024281068,0.0006390644,0.00046694643,0.0005209007,0.0012116411],"category_scores_gemma":[0.00031527758,0.00015665652,0.0001870481,0.00018862005,0.0002879644,0.000718435,0.000635036,0.0003219303,0.0006272096],"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":[0.00013537293,0.00002009878,0.00028566492,0.00009235057,0.0000069231232,0.00013402605,0.000035095007,0.00021345851,0.98044914,0.00057079614,0.00031089262,0.017746342],"study_design_scores_gemma":[0.000023506316,0.00018744705,0.00093080045,0.000009585492,0.0000052356077,0.00034097728,0.000016308877,0.0028658605,0.98707795,0.000114593255,0.008413658,0.000014093604],"about_ca_topic_score_codex":0.00037446417,"about_ca_topic_score_gemma":0.00033630582,"teacher_disagreement_score":0.0012116411,"about_ca_system_score_codex":0.0002624384,"about_ca_system_score_gemma":0.0002298367,"threshold_uncertainty_score":0.0040533543},"labels":[],"label_agreement":null},{"id":"W2033588043","doi":"10.1155/2012/173129","title":"Multisized Inert Particle Loading for Solid Rocket Axial Combustion Instability Suppression","year":2012,"lang":"en","type":"article","venue":"International Journal of Aerospace Engineering","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Solid-fuel rocket; Propellant; Inert; Mechanics; Materials science; Particle (ecology); Instability; Rocket (weapon); Shock wave; Combustion; Shock (circulatory); Inert gas; Attenuation; Composite material; Aerospace engineering; Physics; Engineering; Chemistry; Geology; Optics","score_opus":0.023056414844616808,"score_gpt":0.304958629871645,"score_spread":0.2819022150270282,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2033588043","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":[0.9925397,0.00006081018,0.0068285437,0.000007991567,0.000004303561,0.000007379716,0.000015843041,0.000060858336,0.00047474875],"genre_scores_gemma":[0.9981312,0.000018390005,0.0016995588,0.0000014744992,5.0491576e-7,0.0000036291792,0.000018587842,0.0000075288253,0.000119128774],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998671,0.000013696824,0.000008952748,0.000021342466,0.00006840521,0.000020450601],"domain_scores_gemma":[0.99961203,0.0001585035,0.000105208965,0.00003429893,0.000068650705,0.000021318878],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021112448,0.00022426128,0.00020986189,0.00024835486,0.0001498767,0.00033512674,0.00032733113,0.00018951781,0.0006410867],"category_scores_gemma":[0.0008302642,0.00009569456,0.00019551412,0.0001341272,0.0002294647,0.0002413232,0.00022613705,0.00017783498,0.000089062916],"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":[0.0012876119,0.0002152729,0.017636962,0.00029551622,0.00004530782,0.00038540506,0.0001913419,0.10803135,0.8388522,0.0009244628,0.00012722303,0.032007404],"study_design_scores_gemma":[0.000042364267,0.0015076029,0.019205796,0.00001227221,0.00007310199,0.00016272983,0.00010155673,0.3819889,0.59560025,0.00020580445,0.0010743478,0.000025186127],"about_ca_topic_score_codex":0.0005773046,"about_ca_topic_score_gemma":0.0008954377,"teacher_disagreement_score":0.0006410867,"about_ca_system_score_codex":0.00018287769,"about_ca_system_score_gemma":0.00022130008,"threshold_uncertainty_score":0.0021446347},"labels":[],"label_agreement":null},{"id":"W2039597596","doi":"10.1021/jp9015596","title":"Primary Steps in the Reaction of OH Radicals with Amino Acids at Low Temperatures in Laval Nozzle Expansions: Perspectives from Experiment and Theory","year":2009,"lang":"en","type":"article","venue":"The Journal of Physical Chemistry A","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":15,"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":"Radical; Nozzle; Primary (astronomy); Chemistry; Aerospace engineering; Physics; Engineering; Organic chemistry; Quantum mechanics","score_opus":0.0073627182707796356,"score_gpt":0.2498999752602158,"score_spread":0.24253725698943615,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2039597596","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":[0.878895,0.007918549,0.10054249,0.0008333419,0.00014101497,0.00013572379,0.00021331527,0.0003091523,0.0110114645],"genre_scores_gemma":[0.9898085,0.001534947,0.00724797,0.00005658797,0.000019116127,0.000060169546,0.00007310335,0.000021885333,0.0011777543],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997483,0.00004422795,0.000009722098,0.00005845588,0.00007351334,0.00006568236],"domain_scores_gemma":[0.9994066,0.00040824298,0.0000808938,0.00004636219,0.000037011694,0.000020900383],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00091954623,0.0007962958,0.0006192157,0.0005003824,0.00063667767,0.0006663437,0.0009821567,0.00084475224,0.0028801798],"category_scores_gemma":[0.0009824422,0.00048786245,0.00062222633,0.0001828592,0.0017318157,0.001976581,0.00060438615,0.0010064006,0.00034951323],"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":[0.0008675565,0.0002698374,0.006140675,0.00086386764,0.00006939931,0.00070000044,0.0006522874,0.04913491,0.8686747,0.060744856,0.00025993452,0.011622088],"study_design_scores_gemma":[0.00013883098,0.0011084707,0.008513384,0.00006430315,0.00005828885,0.00041863398,0.00043656872,0.19471061,0.75488025,0.036954436,0.0025815605,0.00013468247],"about_ca_topic_score_codex":0.0008953895,"about_ca_topic_score_gemma":0.0006017224,"teacher_disagreement_score":0.0028801798,"about_ca_system_score_codex":0.0010807769,"about_ca_system_score_gemma":0.00042973395,"threshold_uncertainty_score":0.00963521},"labels":[],"label_agreement":null},{"id":"W2040258799","doi":"10.1115/fedsm2014-21256","title":"Study of Two Phase Flow Breakup Behavior for Application to Solid Rocket Motor Nozzle","year":2014,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":1,"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; Breakup; Propellant; Solid-fuel rocket; Mechanics; Materials science; Flow (mathematics); Turbulence; Volume fraction; Rocket (weapon); Aerospace engineering; Engineering; Composite material; Physics","score_opus":0.029804576354669366,"score_gpt":0.3666149152323454,"score_spread":0.33681033887767603,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2040258799","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":[0.92056084,0.00043873076,0.076592095,0.00006397698,0.000019963503,0.00005282575,0.000103240964,0.0004929846,0.0016752493],"genre_scores_gemma":[0.9918079,0.00012739412,0.0073243794,0.0000067751184,0.000003284577,0.000017282007,0.00008338917,0.000023002047,0.00060652505],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998448,0.000013021796,0.000007714607,0.00003277662,0.000076972894,0.000024613442],"domain_scores_gemma":[0.9997024,0.00010774088,0.000055969216,0.000023166858,0.00009140161,0.000019199682],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020746945,0.0002397465,0.00026370506,0.0005666302,0.00022042701,0.0004499742,0.0002802914,0.00036884588,0.0010444999],"category_scores_gemma":[0.0007208332,0.00011289713,0.00027301797,0.00034419695,0.00018832766,0.0005672665,0.00020723479,0.0002513111,0.000118444914],"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":[0.0003754541,0.00020205633,0.015993742,0.0002763287,0.000017532613,0.0007338896,0.0003649308,0.076131046,0.83539164,0.0020133145,0.00036798473,0.0681321],"study_design_scores_gemma":[0.000023969707,0.00053708855,0.015701182,0.0000121804105,0.00001034455,0.0002519589,0.00013580412,0.62780917,0.35343778,0.00050140085,0.0015443491,0.0000347068],"about_ca_topic_score_codex":0.0013699249,"about_ca_topic_score_gemma":0.00049479044,"teacher_disagreement_score":0.0013699249,"about_ca_system_score_codex":0.00028977325,"about_ca_system_score_gemma":0.00020423548,"threshold_uncertainty_score":0.0034942627},"labels":[],"label_agreement":null},{"id":"W2040520307","doi":"10.1115/gt2010-23810","title":"CMC Combustor Liner Demonstration in a Small Helicopter Engine","year":2010,"lang":"en","type":"article","venue":"Volume 1: Aircraft Engine; Ceramics; Coal, Biomass and Alternative Fuels; Education; Electric Power; Manufacturing Materials and Metallurgy","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":16,"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":"Combustor; Injector; Materials science; Fabrication; Fuel injection; Combustion; Automotive engineering; Mechanical engineering; Engineering; Chemistry","score_opus":0.008444265342750034,"score_gpt":0.2234562929763996,"score_spread":0.21501202763364957,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2040520307","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":[0.98498756,0.00010548,0.003778726,0.00016549196,0.000052835825,0.00010131943,0.00023759315,0.0004673512,0.010103619],"genre_scores_gemma":[0.98276585,0.000052887255,0.00565045,0.000042255084,0.000011019313,0.000030841275,0.00017901922,0.000071609014,0.011196029],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99984324,0.000013066896,0.0000054471966,0.000020958129,0.00009665152,0.00002054453],"domain_scores_gemma":[0.999845,0.000024519175,0.000009267442,0.00001573774,0.00007762479,0.000027834334],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00033632747,0.000332179,0.00020581442,0.00031087268,0.00047040114,0.00027885445,0.00042673375,0.00057792204,0.004103363],"category_scores_gemma":[0.0003290611,0.00011412554,0.00016068212,0.0001313781,0.0002187633,0.00028269604,0.00033151335,0.00036686508,0.000712572],"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":[0.00059528375,0.00019419314,0.0030465694,0.0000772254,0.000012765769,0.0013562795,0.00037391248,0.0018113942,0.96634656,0.0007576506,0.0017562044,0.023671962],"study_design_scores_gemma":[0.00006904974,0.0020127264,0.010736953,0.000014761217,0.00001743071,0.00068272534,0.00015745735,0.009502911,0.9665042,0.00010478193,0.010173218,0.00002379782],"about_ca_topic_score_codex":0.0031297377,"about_ca_topic_score_gemma":0.005964248,"teacher_disagreement_score":0.004103363,"about_ca_system_score_codex":0.00034916154,"about_ca_system_score_gemma":0.0002206381,"threshold_uncertainty_score":0.0137271285},"labels":[],"label_agreement":null},{"id":"W2040924287","doi":"10.2514/1.26915","title":"Analysis of Increased Compression Through Area Constriction on Ejector-Rocket Performance","year":2007,"lang":"en","type":"article","venue":"Journal of Spacecraft and Rockets","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":27,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Aerospace engineering; Spacecraft; Injector; Rocket (weapon); Missile; Space (punctuation); Spacecraft design; Space launch; Supersonic speed; Compression (physics); Space technology; Rocket engine; Systems engineering; Aeronautics; Engineering; Mechanical engineering; Computer science; Physics; Launch vehicle","score_opus":0.02221137076380233,"score_gpt":0.2686094839992989,"score_spread":0.24639811323549657,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2040924287","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":[0.9819519,0.0011160804,0.004555875,0.00006474071,0.000025478379,0.000027665592,0.0004410941,0.0005093312,0.011307753],"genre_scores_gemma":[0.995884,0.0003592487,0.00057863997,0.000019897589,0.0000130596645,0.000008450436,0.0002752486,0.00008286069,0.002778518],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996662,0.00003406688,0.000010667181,0.000055722205,0.00013935608,0.00009401755],"domain_scores_gemma":[0.99777967,0.0015970867,0.00022712289,0.00009763163,0.00022585026,0.00007268276],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000393031,0.00048543132,0.00051298813,0.0005736221,0.00027565518,0.00044312785,0.0005389148,0.0005402178,0.008353895],"category_scores_gemma":[0.0013634539,0.00018705237,0.00037888324,0.00080180616,0.00028839492,0.0006163947,0.0002625826,0.0003854076,0.0016449704],"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":[0.0044845673,0.00047657432,0.019586481,0.0005055045,0.00010227987,0.0011005102,0.00020942441,0.2430414,0.65965104,0.002010786,0.0015685471,0.067262836],"study_design_scores_gemma":[0.000084180865,0.0044739023,0.08293451,0.000074673124,0.00011152908,0.00091085304,0.00018846944,0.25713032,0.64819515,0.0005652644,0.0052379994,0.00009319474],"about_ca_topic_score_codex":0.00072238117,"about_ca_topic_score_gemma":0.0007706562,"teacher_disagreement_score":0.008353895,"about_ca_system_score_codex":0.00041263876,"about_ca_system_score_gemma":0.00018510147,"threshold_uncertainty_score":0.027946532},"labels":[],"label_agreement":null},{"id":"W2044249852","doi":"10.5589/q10-005","title":"Conceptual design of wrap-around-fin rockets using the MDO methodology","year":2010,"lang":"en","type":"article","venue":"Canadian aeronautics and space journal","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Multidisciplinary design optimization; Aerodynamics; Conceptual design; Aerospace engineering; Payload (computing); Fin; Engineering; Rocket (weapon); Systems engineering; Multidisciplinary approach; Computer science; Mechanical engineering","score_opus":0.11860200626923315,"score_gpt":0.30722623380894365,"score_spread":0.1886242275397105,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2044249852","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":[0.020917965,0.00011432361,0.9689446,0.000089357374,0.000028837858,0.00017374859,0.00005990172,0.00017401739,0.009497246],"genre_scores_gemma":[0.57266694,0.0003455402,0.42105302,0.00006535858,0.000011328151,0.0008720571,0.00014612713,0.00008929711,0.0047502834],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99978,0.00005874987,0.000011799506,0.000038273007,0.00007988694,0.000031302083],"domain_scores_gemma":[0.9997955,0.000083099476,0.000030188483,0.000020052048,0.000051092407,0.000020080446],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0007355504,0.0006213525,0.0007120757,0.00057368743,0.0004978286,0.0009039221,0.00095552974,0.0009007861,0.0034045875],"category_scores_gemma":[0.00086519826,0.0004184513,0.00074550166,0.0003234223,0.00063272245,0.00058235583,0.0010143418,0.00061949436,0.0003486277],"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":[0.0000160965,0.000012212333,0.00016269436,0.000073825526,0.000010754388,0.00006555823,0.000034105873,0.97831035,0.0025733518,0.008839371,0.00011637148,0.009785262],"study_design_scores_gemma":[0.00001882048,0.00007134703,0.00007927936,0.000012912584,0.0000101680325,0.00002295728,0.000035148507,0.99266547,0.0011137901,0.0037916307,0.00217084,0.000007675446],"about_ca_topic_score_codex":0.0018587639,"about_ca_topic_score_gemma":0.0018793985,"teacher_disagreement_score":0.0034045875,"about_ca_system_score_codex":0.00048650368,"about_ca_system_score_gemma":0.0015830148,"threshold_uncertainty_score":0.011389494},"labels":[],"label_agreement":null},{"id":"W2045980217","doi":"10.5589/q02-018","title":"CFD Analysis for Simulated Altitude Testing of Rocket Motors","year":2002,"lang":"en","type":"article","venue":"Canadian aeronautics and space journal","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":29,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Diffuser (optics); Rocket (weapon); Rocket engine; Aerospace engineering; Nozzle; Engineering; Rocket engine nozzle; Vacuum chamber; Computational fluid dynamics; Mach number; Combustion chamber; Mechanical engineering; Flight test; Chamber pressure; Simulation; Mechanics; Physics; Combustion; Optics","score_opus":0.04796689182424609,"score_gpt":0.24344582359205935,"score_spread":0.19547893176781325,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2045980217","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":[0.9226514,0.00023947822,0.053925306,0.00023056682,0.000050739407,0.00012201387,0.00083554484,0.00060048513,0.021344664],"genre_scores_gemma":[0.9880922,0.000087838314,0.009516894,0.000021962529,0.0000063385532,0.000047850637,0.00027818355,0.0000580979,0.0018906597],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99985325,0.000029037172,0.0000071147933,0.000017056422,0.000057457426,0.000035998244],"domain_scores_gemma":[0.99954945,0.00026196646,0.00003924952,0.000030446148,0.00009145215,0.000027395588],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002402456,0.00041476582,0.00054007594,0.00044708827,0.0005031566,0.00064546376,0.0006149535,0.00088744715,0.0033034582],"category_scores_gemma":[0.0012884333,0.00022248995,0.00051217194,0.0003432789,0.0004292602,0.00040033658,0.00037477617,0.0003765754,0.00027210946],"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":[0.00006201186,0.000033822536,0.0024725802,0.00003212874,0.00000777047,0.0001315266,0.000047860223,0.98762494,0.004330245,0.0010831311,0.00020321061,0.0039706836],"study_design_scores_gemma":[0.000012251507,0.000026495552,0.0007817378,0.0000044799,0.000002375643,0.000016272068,0.000019773976,0.9968755,0.0016996431,0.00016555362,0.00038996284,0.0000058691503],"about_ca_topic_score_codex":0.014238179,"about_ca_topic_score_gemma":0.00736797,"teacher_disagreement_score":0.014238179,"about_ca_system_score_codex":0.0008577189,"about_ca_system_score_gemma":0.0010021954,"threshold_uncertainty_score":0.028310597},"labels":[],"label_agreement":null},{"id":"W2047451257","doi":"10.1080/19942060.2012.11015432","title":"CFD Study of Effects of Geometry Variations on Flow in a Nozzle","year":2012,"lang":"en","type":"article","venue":"Engineering Applications of Computational Fluid Mechanics","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":25,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Windsor","funders":"Ontario Ministry of Research and Innovation","keywords":"Nozzle; Turbulence; Reynolds stress; Mechanics; Reynolds number; Turbulence kinetic energy; Computational fluid dynamics; Reynolds-averaged Navier–Stokes equations; Discharge coefficient; Flow (mathematics); Materials science; Physics; Mechanical engineering; Engineering","score_opus":0.008429768771590396,"score_gpt":0.24650146258430375,"score_spread":0.23807169381271334,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2047451257","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":[0.9966967,0.00015636827,0.001984573,0.00002447145,0.000012560164,0.000008668293,0.00007919402,0.00007382546,0.0009635651],"genre_scores_gemma":[0.99888116,0.000051300336,0.00082543556,0.000007825318,0.0000024380627,0.0000034758232,0.00005016188,0.000011216478,0.0001670109],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997248,0.00004444072,0.000017884053,0.00006535055,0.00008160417,0.00006585719],"domain_scores_gemma":[0.9993543,0.00034441025,0.00010465384,0.000056528806,0.00009237316,0.00004784611],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00028581318,0.0003337306,0.00058516755,0.0002887226,0.0003198732,0.0006204111,0.00040128836,0.00048493207,0.00053922413],"category_scores_gemma":[0.0012678818,0.00021157587,0.00042551692,0.00033969097,0.00048188554,0.0003661661,0.00027001693,0.0002331214,0.00010059729],"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":[0.00077663653,0.00021806343,0.022802042,0.0001676333,0.00007615282,0.0017514114,0.0003213157,0.5314951,0.42735502,0.0013657707,0.00054544385,0.01312552],"study_design_scores_gemma":[0.00010302125,0.0012565864,0.047829047,0.000032986343,0.00009635018,0.00058710575,0.00018325704,0.7855764,0.16189203,0.00036554382,0.0019613167,0.00011633761],"about_ca_topic_score_codex":0.002944229,"about_ca_topic_score_gemma":0.0013946374,"teacher_disagreement_score":0.002944229,"about_ca_system_score_codex":0.00062149676,"about_ca_system_score_gemma":0.00040969418,"threshold_uncertainty_score":0.0058541894},"labels":[],"label_agreement":null},{"id":"W2049932988","doi":"10.1155/2008/826070","title":"Transient Burning Rate Model for Solid Rocket Motor Internal Ballistic Simulations","year":2007,"lang":"en","type":"article","venue":"International Journal of Aerospace Engineering","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":41,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Propellant; Solid-fuel rocket; Mechanics; Transient (computer programming); Thermal; Rocket (weapon); Phase (matter); Physics; Materials science; Thermodynamics; Aerospace engineering; Computer science; Engineering","score_opus":0.02066041393424373,"score_gpt":0.30491455341902685,"score_spread":0.2842541394847831,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2049932988","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":[0.06654245,0.00021809412,0.9123698,0.00022973288,0.00006804939,0.00013746749,0.00035576904,0.00071935274,0.019359304],"genre_scores_gemma":[0.9305729,0.0004080481,0.044230957,0.00011270158,0.00002937373,0.00050630927,0.00041882542,0.00026411033,0.023456737],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99982613,0.00002780078,0.000010967642,0.00003319983,0.000069114125,0.000032794956],"domain_scores_gemma":[0.99970955,0.00009750649,0.000054846776,0.000032830278,0.000076753364,0.00002853631],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00042997205,0.00049298856,0.00087625557,0.00045830198,0.0004186231,0.0007353409,0.0019911996,0.0012457727,0.0034266587],"category_scores_gemma":[0.0015186468,0.00039419404,0.00084186945,0.0004003946,0.00057072897,0.0009852584,0.000676407,0.00091484154,0.0008083547],"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":[0.000020397489,0.000011394813,0.00022442557,0.000018070637,0.0000055743158,0.000038029506,0.00002476884,0.98894995,0.0019965668,0.0072146407,0.00014917763,0.0013470352],"study_design_scores_gemma":[0.0000020703728,0.0000026858006,0.000031029915,0.000001239168,9.902365e-7,0.000004734717,0.0000018092935,0.99908507,0.00021765943,0.000508198,0.0001425171,0.0000020192772],"about_ca_topic_score_codex":0.006358688,"about_ca_topic_score_gemma":0.00264279,"teacher_disagreement_score":0.006358688,"about_ca_system_score_codex":0.0010361391,"about_ca_system_score_gemma":0.00091225636,"threshold_uncertainty_score":0.012643337},"labels":[],"label_agreement":null},{"id":"W2056301391","doi":"10.1615/intjenergeticmaterialschemprop.2013005758","title":"A COMPUTATIONAL STUDY OF A DUAL-MODE RAMJET COMBUSTOR WITH A CAVITY FLAMEHOLDER","year":2012,"lang":"en","type":"article","venue":"International Journal of Energetic Materials and Chemical Propulsion","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":9,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Martec (Canada); Defence Research and Development Canada","funders":"","keywords":"Combustor; Ramjet; Reynolds-averaged Navier–Stokes equations; Mechanics; Combustion; Scramjet; Jet (fluid); Aerospace engineering; Wake; Ignition system; Large eddy simulation; Materials science; Turbulence; Physics; Chemistry; Engineering","score_opus":0.013436946366573612,"score_gpt":0.27208961310367297,"score_spread":0.25865266673709936,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2056301391","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":[0.98370636,0.00014561837,0.013673262,0.00006846737,0.000038383023,0.000035076395,0.00005683099,0.00009239072,0.002183629],"genre_scores_gemma":[0.98837876,0.000041263087,0.010495715,0.00001262278,0.0000073829888,0.000022644188,0.000037261605,0.000011929167,0.0009923445],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998783,0.000017772754,0.0000059486038,0.000036107318,0.00003542758,0.000026505757],"domain_scores_gemma":[0.9997174,0.00011729036,0.000045568082,0.000033722972,0.00003289215,0.00005315913],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00038082513,0.00048806923,0.0006834252,0.00026144146,0.0005609348,0.00067877374,0.0010676617,0.0010108786,0.00090764876],"category_scores_gemma":[0.0006403829,0.00034951488,0.0005664874,0.00018676207,0.00064296793,0.00056831207,0.0007571161,0.0005956369,0.00012328991],"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":[0.0005542597,0.00028152205,0.007737517,0.00014089582,0.00005169785,0.0011447846,0.000103990074,0.9240166,0.05590823,0.0026048047,0.00021840671,0.0072372765],"study_design_scores_gemma":[0.000036181653,0.00014204203,0.00096982665,0.0000035326439,0.000007848703,0.00007072103,0.000020534842,0.9952743,0.0031465339,0.0001352997,0.00018191621,0.000011161353],"about_ca_topic_score_codex":0.0048612957,"about_ca_topic_score_gemma":0.0023664604,"teacher_disagreement_score":0.0048612957,"about_ca_system_score_codex":0.00033914752,"about_ca_system_score_gemma":0.0007320086,"threshold_uncertainty_score":0.009666026},"labels":[],"label_agreement":null},{"id":"W2056746067","doi":"10.4028/www.scientific.net/amm.397-400.266","title":"Numerical Simulation of Laval Nozzle","year":2013,"lang":"en","type":"article","venue":"Applied Mechanics and Materials","topic":"Rocket and propulsion systems research","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; Rocket engine; Rocket engine nozzle; Computer simulation; Mechanics; Aerospace engineering; Rocket (weapon); Dimensionless quantity; Flow (mathematics); Section (typography); Engineering; Physics; Mechanical engineering; Computer science","score_opus":0.014140650428057424,"score_gpt":0.23902285938244455,"score_spread":0.22488220895438712,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2056746067","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":[0.5925849,0.001988336,0.3122685,0.0009186746,0.0004286675,0.00025553367,0.0016605621,0.0012853956,0.08860946],"genre_scores_gemma":[0.96022606,0.0005306169,0.028903719,0.00006918569,0.000032572603,0.00017272217,0.0004712202,0.000056057837,0.009537643],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997677,0.00004301292,0.000013655112,0.000033852724,0.000084180676,0.00005757697],"domain_scores_gemma":[0.99974924,0.00007212675,0.000038968654,0.00002214104,0.000084901665,0.000032673623],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002939734,0.00040270222,0.0006815981,0.00045489118,0.00074686407,0.00080814713,0.00094161415,0.0013686566,0.0031075678],"category_scores_gemma":[0.0009037055,0.00020634259,0.00045889016,0.0005847257,0.0005989715,0.0005795175,0.00082366896,0.00053777744,0.00030888768],"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":[0.000071944974,0.000053063468,0.0021183237,0.000110088346,0.0000144972855,0.0003515566,0.00014199938,0.9680195,0.008909129,0.014205479,0.0010414276,0.004963119],"study_design_scores_gemma":[0.000021419468,0.000033269185,0.00039599213,0.000009751579,0.00000403429,0.000050760034,0.000035222838,0.99536914,0.0014600005,0.0009983988,0.0016095923,0.000012395194],"about_ca_topic_score_codex":0.008258993,"about_ca_topic_score_gemma":0.0022450832,"teacher_disagreement_score":0.008258993,"about_ca_system_score_codex":0.000620101,"about_ca_system_score_gemma":0.00075947045,"threshold_uncertainty_score":0.016421854},"labels":[],"label_agreement":null},{"id":"W2058428563","doi":"10.2514/1.j052472","title":"High-g Field Combustor of a Rim–Rotor Rotary Ramjet Engine","year":2014,"lang":"en","type":"article","venue":"AIAA Journal","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"National Research Council Canada","keywords":"Ramjet; Combustor; Combustion; Ignition system; Mechanics; Combustion chamber; Aerospace engineering; Materials science; Automotive engineering; Acceleration; Rotary engine; Rotor (electric); Mechanical engineering; Engineering; Physics; Chemistry; Classical mechanics","score_opus":0.006483325610177238,"score_gpt":0.2155242773289328,"score_spread":0.20904095171875559,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2058428563","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":[0.9488965,0.00054101145,0.037811536,0.000121863006,0.00008840115,0.00007952057,0.00015578937,0.00047042032,0.01183494],"genre_scores_gemma":[0.984262,0.00007806538,0.013515892,0.000013278642,0.000009346496,0.000015514805,0.000049904796,0.000016528797,0.0020393338],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99992406,0.000009610687,0.000004253335,0.000019800578,0.000034169097,0.000007979097],"domain_scores_gemma":[0.99994767,0.000010945129,0.0000115650255,0.000009662894,0.000012166459,0.000008018969],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016277753,0.0002311562,0.00030071064,0.00021585842,0.00032445783,0.0002390843,0.00043806038,0.00030345327,0.0014252511],"category_scores_gemma":[0.00012757402,0.00014960926,0.0002188405,0.000101792495,0.00029390305,0.00021002922,0.00018542171,0.00021229991,0.0003145624],"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":[0.00083777384,0.00011817372,0.0036677162,0.00030399475,0.000020052768,0.00073748245,0.00013463081,0.026884194,0.9306434,0.004486845,0.00086513703,0.03130047],"study_design_scores_gemma":[0.00026579172,0.0014103678,0.020116162,0.000049653536,0.000042351723,0.0012421751,0.00009135418,0.32267588,0.64218175,0.0012755222,0.010566754,0.000082229],"about_ca_topic_score_codex":0.00063963357,"about_ca_topic_score_gemma":0.00048727615,"teacher_disagreement_score":0.0014252511,"about_ca_system_score_codex":0.00022234448,"about_ca_system_score_gemma":0.00020488398,"threshold_uncertainty_score":0.0047678947},"labels":[],"label_agreement":null},{"id":"W2058949849","doi":"10.1002/prep.201100105","title":"Munitions Propellants Residue Deposition Rates On Military Training Ranges","year":2012,"lang":"en","type":"article","venue":"Propellants Explosives Pyrotechnics","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":25,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"Defence Research and Development Canada","funders":"","keywords":"Propellant; Residue (chemistry); Explosive material; Aeronautics; Environmental science; Aerospace engineering; Waste management; Engineering; Chemistry","score_opus":0.08534481205441397,"score_gpt":0.29129524582141547,"score_spread":0.2059504337670015,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2058949849","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":[0.99181014,0.0012276167,0.001034752,0.000015886917,0.000014064067,0.00003395903,0.00052435376,0.00006621405,0.0052729645],"genre_scores_gemma":[0.98911285,0.001238824,0.0010926528,0.000025788646,0.0000075743455,0.000025741198,0.00084557594,0.000039043774,0.007611915],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.9992818,0.000063440595,0.000044868888,0.0001156635,0.00039026904,0.000103932834],"domain_scores_gemma":[0.9989895,0.00027538795,0.00022700438,0.0000679838,0.00039095158,0.000049147853],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00037142192,0.00042778635,0.00025869661,0.0012470542,0.00031019442,0.00044736278,0.0004490583,0.00034129262,0.003580304],"category_scores_gemma":[0.0010395655,0.00017263705,0.00025564837,0.0006410522,0.00022609373,0.00044919833,0.00039278902,0.00034429113,0.0009267614],"study_design_candidate":"observational","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":[0.0021305764,0.00015717708,0.050004635,0.00055273384,0.00012669995,0.00027319026,0.00035379652,0.006263555,0.8347852,0.00020004838,0.0006738086,0.10447855],"study_design_scores_gemma":[0.000015341624,0.0019968343,0.1841324,0.0000775743,0.000069171256,0.00036270637,0.00063537224,0.00273652,0.8059732,0.00009038581,0.0038752158,0.00003537784],"about_ca_topic_score_codex":0.005424144,"about_ca_topic_score_gemma":0.005083878,"teacher_disagreement_score":0.005424144,"about_ca_system_score_codex":0.0005223005,"about_ca_system_score_gemma":0.00018633393,"threshold_uncertainty_score":0.011977315},"labels":[],"label_agreement":null},{"id":"W2063018937","doi":"10.1615/heattransres.v31.i6-8.70","title":"High-Turbulent Gas Screen in a Supersonic Nozzle","year":2000,"lang":"en","type":"article","venue":"Heat Transfer Research","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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; Turbulence; Mechanics; Compressibility; Adiabatic process; Discharge coefficient; Supersonic speed; Materials science; Flow (mathematics); Physics; Pressure gradient; Thermodynamics; Acceleration; Classical mechanics","score_opus":0.05857659168832865,"score_gpt":0.31674874478251824,"score_spread":0.2581721530941896,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2063018937","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":[0.9964574,0.000118963835,0.0025968691,0.000014167854,0.000004658386,0.0000073468505,0.000026438713,0.00010703891,0.00066711503],"genre_scores_gemma":[0.998953,0.000043735552,0.0006237361,0.0000064247843,0.0000019700856,0.0000034818693,0.000040793977,0.000012529046,0.00031427975],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997676,0.00004227557,0.000007648391,0.000036067075,0.00009874801,0.000047611407],"domain_scores_gemma":[0.9996126,0.00015285386,0.00006859976,0.000031988588,0.00007275769,0.00006112688],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00033279837,0.00021268649,0.00035758392,0.00024309722,0.00030083512,0.0007722821,0.00021090658,0.0002503963,0.00064969575],"category_scores_gemma":[0.00069802743,0.0001457943,0.00019442919,0.00023060146,0.00046342585,0.0003036492,0.00028404634,0.00022578826,0.00010372842],"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":[0.0005268228,0.00003766895,0.0032915787,0.000047121815,0.0000103799775,0.00036146972,0.00013131616,0.008114061,0.9828415,0.0007952755,0.000091875285,0.0037509147],"study_design_scores_gemma":[0.000114662456,0.0015344206,0.044359386,0.000019629215,0.000042404237,0.00030105218,0.00013393235,0.091156825,0.86011994,0.00029687732,0.001862035,0.000058846246],"about_ca_topic_score_codex":0.0029709507,"about_ca_topic_score_gemma":0.0016950066,"teacher_disagreement_score":0.0029709507,"about_ca_system_score_codex":0.0006740135,"about_ca_system_score_gemma":0.00030472194,"threshold_uncertainty_score":0.0059073567},"labels":[],"label_agreement":null},{"id":"W2065767335","doi":"10.1109/tmech.2013.2264105","title":"Toward an Accurate Physics-Based UAV Thruster Model","year":2013,"lang":"en","type":"article","venue":"IEEE/ASME Transactions on Mechatronics","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":80,"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":"Thrust; Propeller; Aerodynamics; Aerospace engineering; Propulsion; Torque; Control theory (sociology); Simple (philosophy); Fixed wing; Computer science; Physics; Wing; Marine engineering; Engineering; Control (management)","score_opus":0.06004153803209528,"score_gpt":0.279765880541999,"score_spread":0.21972434250990375,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2065767335","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":[0.019569973,0.00046602578,0.9547054,0.00025317213,0.00009262325,0.00016652879,0.00046543995,0.000864402,0.023416355],"genre_scores_gemma":[0.7610839,0.0019892019,0.20593007,0.00032473,0.00014096806,0.0009060881,0.0012562033,0.00052491744,0.027843967],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99976796,0.00003119082,0.000013377394,0.000035650606,0.00013115631,0.000020777845],"domain_scores_gemma":[0.9997241,0.00007051042,0.00003908178,0.000044763576,0.00010872909,0.0000128551765],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00034545027,0.00063864276,0.00087758957,0.00073805713,0.00046689523,0.0010744465,0.001480193,0.0015799009,0.0024782773],"category_scores_gemma":[0.0010729679,0.00054547883,0.0007393587,0.00044163354,0.00051369914,0.001292341,0.0007995661,0.0011992616,0.0013865208],"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":[0.0000074578847,0.000016642734,0.0002497464,0.000051186144,0.0000069359908,0.00008532143,0.00004709727,0.9813426,0.0041260836,0.008909723,0.0004200559,0.004737095],"study_design_scores_gemma":[0.0000030348422,0.0000067475225,0.000101980935,0.000004950033,0.000002106589,0.000012611997,0.0000057460834,0.9971752,0.0003283563,0.0013236111,0.0010321387,0.0000035399917],"about_ca_topic_score_codex":0.0068803197,"about_ca_topic_score_gemma":0.0035459776,"teacher_disagreement_score":0.0068803197,"about_ca_system_score_codex":0.00068505213,"about_ca_system_score_gemma":0.0009955581,"threshold_uncertainty_score":0.013680518},"labels":[],"label_agreement":null},{"id":"W2069462824","doi":"10.2514/6.2006-4673","title":"Oxygen Rich Hybrid Gas Generator","year":2006,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lockheed Martin (Canada)","funders":"","keywords":"Oxygen; Generator (circuit theory); Computer science; Environmental science; Materials science; Chemistry; Power (physics); Physics; Thermodynamics","score_opus":0.012145957028647781,"score_gpt":0.22535134568018403,"score_spread":0.21320538865153624,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2069462824","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":[0.64224946,0.0022227233,0.2695619,0.00072319614,0.0006859936,0.0002571165,0.0013379556,0.0038303712,0.0791313],"genre_scores_gemma":[0.94615275,0.00036068086,0.02398279,0.00012067432,0.000038384336,0.00007918816,0.00044903407,0.00009611347,0.028720455],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998778,0.000009231104,0.0000052070804,0.00002735057,0.00006084028,0.000019573694],"domain_scores_gemma":[0.99993324,0.000015260126,0.0000129920345,0.000010034766,0.000018661007,0.000009740435],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00011109944,0.00023078204,0.00027549049,0.00024960446,0.00025770674,0.0003601079,0.00059649994,0.00031331612,0.0048744436],"category_scores_gemma":[0.00013787874,0.00013775074,0.000182817,0.00025042277,0.00021986783,0.0008131667,0.0005244141,0.000387618,0.0010377107],"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":[0.00081114116,0.00018072684,0.0028095318,0.0006186233,0.000057877747,0.0009962773,0.00013793653,0.041427515,0.81705457,0.026096607,0.0086117275,0.101197466],"study_design_scores_gemma":[0.00019773576,0.0010985661,0.0028497465,0.000045225468,0.000057446236,0.0014389239,0.00007478624,0.1450295,0.72061574,0.004067161,0.124452636,0.00007251186],"about_ca_topic_score_codex":0.00046442306,"about_ca_topic_score_gemma":0.0011126625,"teacher_disagreement_score":0.0048744436,"about_ca_system_score_codex":0.00022602087,"about_ca_system_score_gemma":0.00014615369,"threshold_uncertainty_score":0.016306639},"labels":[],"label_agreement":null},{"id":"W2069507152","doi":"10.2514/1.b34924","title":"Closed-Loop Precision Throttling of a Hybrid Rocket Motor","year":2014,"lang":"en","type":"article","venue":"Journal of Propulsion and Power","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":29,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"McMaster University","keywords":"Throttle; Control theory (sociology); Bandwidth throttling; Thrust; Rocket engine; Computer science; Engineering; Aerospace engineering; Automotive engineering","score_opus":0.01121724218040833,"score_gpt":0.2517397833819982,"score_spread":0.2405225412015899,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2069507152","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":[0.76170516,0.00018986657,0.22994603,0.00008763794,0.000085961474,0.00020864597,0.00020279559,0.0037147894,0.00385909],"genre_scores_gemma":[0.977571,0.000025502795,0.019979674,0.000017107992,0.0000054233483,0.00006195155,0.000071942144,0.000057349836,0.0022101186],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99967945,0.000020245088,0.000019795356,0.00007800827,0.00017033651,0.000032250333],"domain_scores_gemma":[0.99947315,0.00018934638,0.0000767039,0.00006719865,0.00015376849,0.000039820563],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00037765683,0.000338872,0.00030736424,0.00022461438,0.00030557753,0.00040463748,0.0007739415,0.0003530261,0.0020455683],"category_scores_gemma":[0.0009817928,0.00015431069,0.000114073206,0.00010499455,0.00022463086,0.00029546767,0.00033129097,0.00033243405,0.00032852287],"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":[0.00073526043,0.00013842975,0.0017651493,0.00017825674,0.000029344266,0.0001935913,0.00015982475,0.016757196,0.8927629,0.0005581643,0.0006589493,0.08606292],"study_design_scores_gemma":[0.00015939555,0.0022158793,0.008468309,0.000028706674,0.00003418453,0.0004709318,0.00005199059,0.28038082,0.70017207,0.00026206803,0.0076695974,0.00008597327],"about_ca_topic_score_codex":0.00090004096,"about_ca_topic_score_gemma":0.0009471406,"teacher_disagreement_score":0.0020455683,"about_ca_system_score_codex":0.00026743894,"about_ca_system_score_gemma":0.00031758266,"threshold_uncertainty_score":0.00684309},"labels":[],"label_agreement":null},{"id":"W2069934216","doi":"10.2514/1.b35761","title":"Regression Rate Estimation for Swirling-Flow Hybrid Rocket Engines","year":2015,"lang":"en","type":"article","venue":"Journal of Propulsion and Power","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":10,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Mechanics; Propellant; Mass flow rate; Materials science; Rocket (weapon); Flow (mathematics); Heat transfer; Convection; Volumetric flow rate; Aerospace engineering; Engineering; Physics","score_opus":0.032483695428631186,"score_gpt":0.29761907694775963,"score_spread":0.26513538151912847,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2069934216","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":[0.32535028,0.0004155206,0.67231077,0.000018436847,0.00001097452,0.000046067933,0.000094212155,0.00071388466,0.0010397951],"genre_scores_gemma":[0.9755029,0.0001884235,0.023357404,0.000004385082,0.000004446756,0.000025395482,0.0000851416,0.000042615986,0.0007892339],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99982387,0.000033668333,0.000010119918,0.00004864556,0.00006543061,0.000018233095],"domain_scores_gemma":[0.99957734,0.00021250374,0.00009614947,0.00002615313,0.00007907939,0.000008680117],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006040596,0.00062036316,0.00062301586,0.0006301377,0.00012772605,0.00047157923,0.0007832159,0.00038757862,0.00037660825],"category_scores_gemma":[0.0011436931,0.00028247325,0.00044176975,0.0003593219,0.00020472055,0.0006598268,0.00033271874,0.0003229435,0.00022917522],"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":[0.00023105624,0.0000565784,0.005113266,0.000116043746,0.000041212803,0.00010651635,0.00005009825,0.87120724,0.071000405,0.0008837442,0.00010636085,0.051087502],"study_design_scores_gemma":[0.0000019984152,0.000022743498,0.00056988274,0.0000017403745,0.0000033224326,0.000012575446,0.0000040426967,0.9886,0.010606472,0.000092927854,0.000077833036,0.000006554876],"about_ca_topic_score_codex":0.002455572,"about_ca_topic_score_gemma":0.0015950083,"teacher_disagreement_score":0.002455572,"about_ca_system_score_codex":0.00035434598,"about_ca_system_score_gemma":0.00022944763,"threshold_uncertainty_score":0.004882574},"labels":[],"label_agreement":null},{"id":"W2073156185","doi":"10.1243/09544100jaero513","title":"Prediction of unsteady non-linear combustion instability in solid rocket motors","year":2009,"lang":"en","type":"article","venue":"Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Propellant; Solid-fuel rocket; Mechanics; Instability; Combustion; Combustion chamber; Rocket (weapon); Casing; Transient (computer programming); Computer simulation; Internal flow; Materials science; Flow (mathematics); Aerospace engineering; Physics; Engineering; Chemistry; Mechanical engineering; Computer science","score_opus":0.01992463562151637,"score_gpt":0.2415366294219454,"score_spread":0.22161199380042904,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2073156185","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":[0.990194,0.000028502245,0.009150227,0.000015708552,0.0000027971507,0.0000065638114,0.000015311804,0.000053239302,0.00053355936],"genre_scores_gemma":[0.9990741,0.0000094846455,0.00077161635,0.0000013272803,6.5101244e-7,0.0000024619192,0.000011107926,0.0000047306976,0.00012454407],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998903,0.000027195218,0.000005828684,0.000015105731,0.00004146064,0.00002001671],"domain_scores_gemma":[0.99922514,0.0004719658,0.00011929881,0.00003413873,0.000098945115,0.000050366427],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00028839905,0.00036124466,0.0003001879,0.00026551264,0.0002211847,0.0004571146,0.0003601407,0.00043575952,0.0003610768],"category_scores_gemma":[0.0016648021,0.00021413814,0.00029473758,0.000121960766,0.00048894814,0.00029676492,0.00029845544,0.0002998521,0.00007682968],"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":[0.00011843742,0.000036123198,0.007903347,0.000023778606,0.000009875759,0.00012317658,0.000047427606,0.97242886,0.016268244,0.0003261958,0.000038257836,0.0026762546],"study_design_scores_gemma":[0.0000019203537,0.000020902504,0.0007901202,7.601128e-7,0.0000010243449,0.000006720436,0.0000049875166,0.9967998,0.002334678,0.00002538916,0.000011860312,0.000001806307],"about_ca_topic_score_codex":0.0050997557,"about_ca_topic_score_gemma":0.0023255455,"teacher_disagreement_score":0.0050997557,"about_ca_system_score_codex":0.00044412224,"about_ca_system_score_gemma":0.000352984,"threshold_uncertainty_score":0.010140121},"labels":[],"label_agreement":null},{"id":"W2076415282","doi":"10.1115/gt2013-95602","title":"Thrust Vectoring Design Project at Six Universities: Part I — Project Description and Final Designs","year":2013,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"McMaster University; University of Michigan","keywords":"Thrust vectoring; Outreach; Project-based learning; Workforce; Pound (networking); Engineering management; Thrust; Engineering; Computer science; Mathematics education; Mechanical engineering; Political science; Psychology","score_opus":0.16571044794771642,"score_gpt":0.28962215432236843,"score_spread":0.12391170637465201,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2076415282","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":[0.7204376,0.00068726105,0.17839095,0.0025820816,0.0005135256,0.027638098,0.006831388,0.0028897983,0.060029373],"genre_scores_gemma":[0.6559049,0.000619652,0.23157322,0.00039682622,0.00013408123,0.019661576,0.0060302597,0.0009063108,0.08477314],"study_design_codex":"design_other","study_design_gemma":"design_other","domain_scores_codex":[0.9952922,0.0014386454,0.00025592447,0.0005189575,0.0015584361,0.00093583105],"domain_scores_gemma":[0.9931178,0.00043378235,0.0002450383,0.00083295343,0.002432113,0.00293837],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.007980709,0.0011160541,0.00076483336,0.0016987385,0.0025281818,0.0022363428,0.0014593397,0.0015857628,0.014129724],"category_scores_gemma":[0.0047434345,0.0007130692,0.00051578827,0.00094997167,0.0010069237,0.0011129461,0.0026922647,0.0025574921,0.0056692683],"study_design_candidate":"design_other","study_design_consensus":"design_other","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0039657294,0.013060059,0.024898631,0.0013048718,0.00005633963,0.0009806802,0.014729422,0.016006498,0.10834784,0.011062507,0.042676475,0.76291096],"study_design_scores_gemma":[0.0019902478,0.034511775,0.051691517,0.000426829,0.00008043626,0.0016648286,0.01608101,0.015256848,0.26143515,0.005861248,0.6106577,0.00034235336],"about_ca_topic_score_codex":0.0017409391,"about_ca_topic_score_gemma":0.0025619878,"teacher_disagreement_score":0.014129724,"about_ca_system_score_codex":0.002290649,"about_ca_system_score_gemma":0.0058938847,"threshold_uncertainty_score":0.04726863},"labels":[],"label_agreement":null},{"id":"W2076589408","doi":"10.2514/6.2004-3185","title":"Predictive Momentum Control for High Fuel Efficiency GEO Spacecraft Stationkeeping","year":2004,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","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":"Lockheed Martin (Canada)","funders":"","keywords":"Spacecraft; Aerospace engineering; Momentum (technical analysis); Model predictive control; Computer science; Control (management); Aeronautics; Attitude control; Astrobiology; Automotive engineering; Environmental science; Physics; Engineering; Artificial intelligence; Business","score_opus":0.01090183399381628,"score_gpt":0.2478582550107626,"score_spread":0.23695642101694633,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2076589408","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":[0.05568827,0.0011403015,0.9229923,0.00022843032,0.00017758895,0.00005808583,0.000058323516,0.0022716695,0.017385006],"genre_scores_gemma":[0.95404863,0.000526219,0.040829156,0.000049779406,0.000064389365,0.000046935533,0.000062495805,0.000038208276,0.0043341527],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99988186,0.000011337595,0.000004448393,0.00001679847,0.00007121239,0.000014361851],"domain_scores_gemma":[0.9998915,0.000033484626,0.000023084998,0.000010215195,0.00003527721,0.0000063286443],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00019644189,0.00032248633,0.00019423907,0.00026358743,0.0003075357,0.00048724015,0.00051701715,0.00018355917,0.0014004782],"category_scores_gemma":[0.000372702,0.00014527085,0.00015570433,0.00025287655,0.00026283332,0.00026861188,0.0003282211,0.0005609283,0.00023992098],"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":[0.00021102806,0.000113494374,0.0014592415,0.00016341692,0.00003417639,0.00018192477,0.00014096693,0.6025125,0.060376506,0.01946823,0.0034684478,0.3118701],"study_design_scores_gemma":[0.000022370028,0.00015274432,0.00068078074,0.000012442783,0.000010935978,0.000032978256,0.000012595639,0.9853249,0.007865305,0.0017516658,0.0041220738,0.000011109211],"about_ca_topic_score_codex":0.0046179066,"about_ca_topic_score_gemma":0.005611364,"teacher_disagreement_score":0.0046179066,"about_ca_system_score_codex":0.0003644761,"about_ca_system_score_gemma":0.0005138379,"threshold_uncertainty_score":0.009182036},"labels":[],"label_agreement":null},{"id":"W2078930259","doi":"10.2322/jjsass.58.171","title":"Investigation of an Evaluation Method on the Improvement of Thrust and Specific Impulse by Nozzle Heating","year":2010,"lang":"en","type":"article","venue":"JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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; Specific impulse; Thrust; Materials science; Mechanics; Prandtl number; Heat transfer; Thermodynamics; Inlet; Impulse (physics); Energy transformation; Aerospace engineering; Mechanical engineering; Physics; Engineering; Classical mechanics","score_opus":0.04491491006197865,"score_gpt":0.31764388894593687,"score_spread":0.2727289788839582,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2078930259","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":[0.059471183,0.0004981974,0.9327195,0.00007469956,0.00005117665,0.00007685917,0.000041448893,0.0006285666,0.006438287],"genre_scores_gemma":[0.71101695,0.0005044858,0.28451526,0.000023762288,0.000026972795,0.0001361893,0.00007198744,0.0001573211,0.0035471476],"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9993672,0.00014063084,0.000024838519,0.00008573985,0.00034310072,0.000038557333],"domain_scores_gemma":[0.99913496,0.00042296448,0.000069149195,0.000043982247,0.0003125086,0.000016330598],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00093917444,0.00034005,0.00039642042,0.0006599922,0.00018228542,0.00043375307,0.00054280495,0.00042381202,0.0014286852],"category_scores_gemma":[0.002174037,0.00015878498,0.0003125568,0.0005900265,0.00024170268,0.00055935123,0.0002721772,0.0003477754,0.00018296801],"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":[0.00035974747,0.00016975611,0.007059068,0.0007678624,0.000067286084,0.00021932277,0.00030316866,0.26260725,0.23518272,0.02852079,0.0017080656,0.4630349],"study_design_scores_gemma":[0.000015540516,0.00015153897,0.0020785804,0.00002061562,0.000017246035,0.000107886444,0.00002488137,0.9557583,0.0388824,0.0010216724,0.0019030146,0.000018337101],"about_ca_topic_score_codex":0.0010069823,"about_ca_topic_score_gemma":0.00059585413,"teacher_disagreement_score":0.0014286852,"about_ca_system_score_codex":0.0004156271,"about_ca_system_score_gemma":0.0004908796,"threshold_uncertainty_score":0.0049669147},"labels":[],"label_agreement":null},{"id":"W2079833642","doi":"10.1504/ijep.2007.015675","title":"Pollution reduction from flares by swirl vanes in a cross-flow","year":2007,"lang":"en","type":"article","venue":"International Journal of Environment and Pollution","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":2,"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 Calgary","funders":"","keywords":"Combustor; Crosswind; Nozzle; Mechanics; Flare; Stack (abstract data type); Jet (fluid); Combustion; Environmental science; Airflow; Flow (mathematics); Wake; Meteorology; Combustion chamber; Gas burner; Materials science; Mixing (physics); Atmospheric sciences; Aerospace engineering; Physics; Engineering; Thermodynamics; Chemistry","score_opus":0.009362135900074103,"score_gpt":0.26330387857441534,"score_spread":0.2539417426743412,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2079833642","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":[0.9982249,0.000065514825,0.0014770366,0.00000667562,0.0000033232927,0.000007831476,0.000007690674,0.00003945396,0.00016754786],"genre_scores_gemma":[0.9978676,0.0000658719,0.0016162131,0.000015883155,0.0000022151685,0.000006403558,0.00003407457,0.000013098936,0.0003786179],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997925,0.000019565605,0.000009838128,0.00003805743,0.00008015267,0.000059737],"domain_scores_gemma":[0.99977845,0.000036804417,0.00008073412,0.000015306689,0.000052993204,0.000035739213],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00032208994,0.0004267443,0.0003541577,0.00024469057,0.00033132348,0.00043047665,0.0004076304,0.00044094407,0.0005567093],"category_scores_gemma":[0.00048658205,0.00032113178,0.00030785223,0.00015052348,0.00024389212,0.00038148224,0.0005079357,0.00029198796,0.000111585825],"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":[0.00026089748,0.00007688922,0.0014063783,0.000048941725,0.000014729037,0.000045503166,0.000052051313,0.0014299969,0.9920522,0.000049049144,0.000021212483,0.0045421007],"study_design_scores_gemma":[0.000029477796,0.0018142853,0.008607875,0.0000063438356,0.00002804485,0.000080392114,0.000048503203,0.006983276,0.9818787,0.00003435311,0.0004741613,0.000014499347],"about_ca_topic_score_codex":0.0012409141,"about_ca_topic_score_gemma":0.0016596429,"teacher_disagreement_score":0.0012409141,"about_ca_system_score_codex":0.00021299881,"about_ca_system_score_gemma":0.00021762741,"threshold_uncertainty_score":0.0024673939},"labels":[],"label_agreement":null},{"id":"W2085761776","doi":"10.3390/en3111790","title":"Scale Effects on Quasi-Steady Solid Rocket Internal Ballistic Behaviour","year":2010,"lang":"en","type":"article","venue":"Energies","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Internal ballistics; Propellant; Solid-fuel rocket; Ballistics; Deflection (physics); Aerospace engineering; Engineering; Mechanics; Simulation; Mechanical engineering; Materials science; Physics; Classical mechanics","score_opus":0.008723345265399399,"score_gpt":0.2665378135226148,"score_spread":0.2578144682572154,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2085761776","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":[0.9811866,0.00013134473,0.013891024,0.000028517848,0.000007921681,0.0000140487555,0.0000486596,0.00023715328,0.0044546314],"genre_scores_gemma":[0.99929976,0.000025784984,0.0004337416,0.0000020629077,5.4788273e-7,0.000002382733,0.000014886531,0.000016753856,0.00020401462],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998456,0.000020198386,0.00000792587,0.000023392178,0.00007384543,0.000029040799],"domain_scores_gemma":[0.9992536,0.00042149975,0.000085566084,0.00011547683,0.00009731035,0.000026563976],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00028894923,0.00025369422,0.00021867322,0.00016728976,0.00020096563,0.00031620078,0.00021021214,0.00019058915,0.0017637267],"category_scores_gemma":[0.0020817104,0.00018356985,0.0002594084,0.000121183606,0.0005239562,0.0003882452,0.0003935371,0.0002484408,0.000289907],"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":[0.0007700477,0.00009928006,0.018261684,0.0002094963,0.000044060973,0.0006101288,0.00044388007,0.57878864,0.3629592,0.0027040823,0.00030397234,0.034805503],"study_design_scores_gemma":[0.000032148175,0.0008737737,0.05006801,0.00002157034,0.000038152586,0.0002546599,0.0001857318,0.70554376,0.2408602,0.0010577912,0.0010130865,0.000051221075],"about_ca_topic_score_codex":0.0011938057,"about_ca_topic_score_gemma":0.0013615673,"teacher_disagreement_score":0.0017637267,"about_ca_system_score_codex":0.00027312472,"about_ca_system_score_gemma":0.00015046392,"threshold_uncertainty_score":0.005900264},"labels":[],"label_agreement":null},{"id":"W2089358572","doi":"10.1016/s0895-7177(03)90024-0","title":"Model of the filling of an automotive fuel tank","year":2003,"lang":"en","type":"article","venue":"Mathematical and Computer Modelling","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":8,"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 Windsor","funders":"","keywords":"Automotive industry; Fuel tank; Environmental science; Computer science; Automotive engineering; Mathematics; Engineering; Mechanical engineering; Thermodynamics; Physics","score_opus":0.049298438930562585,"score_gpt":0.23873926526521416,"score_spread":0.1894408263346516,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2089358572","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":[0.22665866,0.00081565883,0.65179235,0.0018364912,0.00040801382,0.00015865771,0.002351822,0.0016046248,0.11437372],"genre_scores_gemma":[0.9365627,0.00038297262,0.011182594,0.00013731621,0.00006075631,0.00016950953,0.0005061322,0.00011669367,0.050881214],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99985504,0.000029749872,0.000008589496,0.000037283964,0.000041090505,0.00002825184],"domain_scores_gemma":[0.99976426,0.000088863715,0.000039006758,0.000016948103,0.00005750017,0.000033526343],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002113309,0.00066652667,0.0012549991,0.00058540626,0.0009476303,0.0018011197,0.0019783182,0.0035080512,0.014043423],"category_scores_gemma":[0.000661682,0.0005157106,0.0007980065,0.0006637413,0.0014527839,0.0010633254,0.001137747,0.0010379703,0.0013757783],"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":[0.000054475644,0.00001723318,0.0001735893,0.000039084025,0.0000112903335,0.00015057756,0.000048565533,0.97977567,0.0021982964,0.015894925,0.00028553486,0.0013508515],"study_design_scores_gemma":[0.000023975523,0.00002105914,0.00009670046,0.000004263049,0.0000075208004,0.000028124587,0.000019144874,0.99561924,0.00040406396,0.0028498727,0.00091665325,0.0000093947265],"about_ca_topic_score_codex":0.02430145,"about_ca_topic_score_gemma":0.0077197244,"teacher_disagreement_score":0.02430145,"about_ca_system_score_codex":0.00105139,"about_ca_system_score_gemma":0.0017968478,"threshold_uncertainty_score":0.048319995},"labels":[],"label_agreement":null},{"id":"W2089387062","doi":"10.1115/pvp2002-1578","title":"Modeling of Structural Vibration for Motor Chamber Internal Flow Studies","year":2002,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","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":"Toronto Metropolitan University","funders":"","keywords":"Mechanics; Vibration; Amplitude; Oscillation (cell signaling); Physics; Internal flow; Flow (mathematics); Asymptote; Acoustics; Classical mechanics; Optics; Mathematics; Chemistry; Geometry","score_opus":0.0809775577094535,"score_gpt":0.3126565756490235,"score_spread":0.23167901793957,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2089387062","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":[0.5307586,0.00012471071,0.45649245,0.000119693854,0.000035914494,0.00007777642,0.00014243634,0.00044696798,0.011801501],"genre_scores_gemma":[0.9851599,0.00006517577,0.01261186,0.0000082131755,0.000006749534,0.000038880356,0.00005920518,0.000027390051,0.0020226825],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99993277,0.000015409698,0.0000021232763,0.000009458341,0.000027141754,0.000013007352],"domain_scores_gemma":[0.9999138,0.000040508337,0.000009796627,0.000011160444,0.000016973478,0.000007818959],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00019382207,0.0002671138,0.00024797535,0.00018761524,0.0002469782,0.0002897346,0.0004302178,0.00048594014,0.0017543973],"category_scores_gemma":[0.00039513217,0.00013867368,0.000256387,0.000108517306,0.00029743084,0.00025518663,0.00027415392,0.00030214727,0.00026423205],"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":[0.00011488897,0.000037249756,0.003088302,0.00006352873,0.000008291357,0.00015622666,0.00013672307,0.90455794,0.066994846,0.0064596776,0.00036129073,0.018021062],"study_design_scores_gemma":[0.000005092495,0.000040104387,0.0008639621,0.000004021034,0.000002549546,0.000018399622,0.000016005622,0.9943718,0.003774056,0.00036103337,0.0005394356,0.0000036124563],"about_ca_topic_score_codex":0.0019134978,"about_ca_topic_score_gemma":0.0014703408,"teacher_disagreement_score":0.0019134978,"about_ca_system_score_codex":0.00023022712,"about_ca_system_score_gemma":0.0004389397,"threshold_uncertainty_score":0.0058690906},"labels":[],"label_agreement":null},{"id":"W2095499640","doi":"10.1243/095765005x31388","title":"Nucleation of steam in high-pressure nozzle experiments","year":2005,"lang":"en","type":"article","venue":"Proceedings of the Institution of Mechanical Engineers Part A Journal of Power and Energy","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":87,"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":"Supersaturation; Subcooling; Nucleation; Superheated steam; Thermodynamics; Nozzle; Mechanics; Materials science; Chemistry; Boiler (water heating); Boiling; Physics","score_opus":0.009914846183560908,"score_gpt":0.22795939012983346,"score_spread":0.21804454394627254,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2095499640","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":[0.9909622,0.00042485626,0.0063946825,0.000016214975,0.000019166151,0.00006424092,0.00018709167,0.00008485505,0.001846702],"genre_scores_gemma":[0.9952814,0.00022084333,0.0034444944,0.000013730067,0.000010403887,0.00003607073,0.00021496166,0.000026498303,0.0007516278],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9994424,0.00007470115,0.000041634234,0.00014176314,0.00019903955,0.00010049963],"domain_scores_gemma":[0.9992143,0.00035991715,0.00008267383,0.000070256974,0.00018837603,0.00008451606],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005804227,0.0002058307,0.0006537374,0.00028222182,0.00037616945,0.00034323309,0.0005175052,0.00038251776,0.0013518352],"category_scores_gemma":[0.0011627687,0.00021463465,0.00032289425,0.00030013896,0.00031902135,0.00043763802,0.0005473347,0.0004737439,0.00020699228],"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":[0.0003382865,0.00008136252,0.00202759,0.00010817865,0.000012902907,0.00015584174,0.0002721863,0.0020709392,0.9915944,0.0005044532,0.00009514339,0.0027387007],"study_design_scores_gemma":[0.00003656305,0.00073850626,0.0052243057,0.0000066164553,0.000011882562,0.00012907696,0.000041796633,0.011889137,0.9809074,0.00012346292,0.00087776803,0.000013373003],"about_ca_topic_score_codex":0.002313051,"about_ca_topic_score_gemma":0.0018643565,"teacher_disagreement_score":0.002313051,"about_ca_system_score_codex":0.0005760668,"about_ca_system_score_gemma":0.00021875644,"threshold_uncertainty_score":0.0045992136},"labels":[],"label_agreement":null},{"id":"W2103336738","doi":"10.1115/ices2009-76147","title":"The Influence of Elliptical Nozzle Holes on Ignition and Combustion of Transient Natural Gas Jets","year":2009,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Nozzle; Combustion; Ignition system; Mechanics; Materials science; Mixing (physics); Cylinder; Nuclear engineering; Mechanical engineering; Physics; Thermodynamics; Chemistry; Engineering","score_opus":0.012563692527454682,"score_gpt":0.2531775924421602,"score_spread":0.24061389991470553,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2103336738","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":[0.9976816,0.00026632915,0.0016239475,0.0000074331506,0.000010375348,0.000014193014,0.000026395164,0.000031657168,0.00033815546],"genre_scores_gemma":[0.998201,0.00011432309,0.0014152478,0.0000072950543,0.0000023711282,0.000006460157,0.000023434643,0.000014941095,0.00021491297],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9995629,0.00005916912,0.000033569657,0.00009050842,0.00014031849,0.00011340386],"domain_scores_gemma":[0.9979971,0.0010859106,0.0005126591,0.00013422167,0.00016994853,0.00010014616],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006646145,0.00037063527,0.00033581018,0.0002344155,0.00026250124,0.000611551,0.0003023651,0.00029196346,0.0008024628],"category_scores_gemma":[0.003160524,0.0002612197,0.00019594634,0.00016847307,0.00053687376,0.00061396,0.00048746224,0.00021057946,0.00009387194],"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":[0.0027875043,0.00010036469,0.0064504617,0.00020444719,0.000016968586,0.00042352788,0.00024983264,0.0044406937,0.97256875,0.00037883018,0.000056111778,0.0123225255],"study_design_scores_gemma":[0.000066063076,0.0020934888,0.024549892,0.00002198752,0.00004582947,0.00031893552,0.00021241956,0.0075931037,0.96411514,0.000112315676,0.00083950534,0.00003125027],"about_ca_topic_score_codex":0.00077422516,"about_ca_topic_score_gemma":0.00086835487,"teacher_disagreement_score":0.0008024628,"about_ca_system_score_codex":0.00029265016,"about_ca_system_score_gemma":0.00022465445,"threshold_uncertainty_score":0.003514886},"labels":[],"label_agreement":null},{"id":"W2107581273","doi":"10.2514/6.2004-3384","title":"Unsteady CFD Calculation for Validation of a Multi-Vane Thrust Vector Control System","year":2004,"lang":"en","type":"article","venue":"40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Defence Research and Development Canada; Université Laval","funders":"Natural Sciences and Engineering Research Council of Canada; Defence Research and Development Canada; Université Laval","keywords":"Computational fluid dynamics; Thrust; Aerospace engineering; Marine engineering; Computer science; Engineering","score_opus":0.04660880103532531,"score_gpt":0.27403543179248,"score_spread":0.22742663075715472,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2107581273","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":[0.8325406,0.00015705971,0.12647367,0.0003710188,0.00019101617,0.00020395363,0.0019377435,0.0030765303,0.03504844],"genre_scores_gemma":[0.98542666,0.00002418692,0.011725225,0.000015723457,0.000003859742,0.000043504417,0.00030569025,0.000084563435,0.0023706327],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998375,0.000028524018,0.000010533435,0.00001840708,0.00008137253,0.000023620285],"domain_scores_gemma":[0.99958736,0.00016288512,0.000021376396,0.000047679063,0.00016007943,0.000020770365],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002709409,0.00038579153,0.00035516697,0.00045978796,0.0006631804,0.00060676347,0.00056553225,0.00061265414,0.004870319],"category_scores_gemma":[0.0008261435,0.00025405874,0.00027701465,0.0003007147,0.00032568412,0.00048316075,0.00033413456,0.00041912778,0.0005205237],"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":[0.00020476428,0.00011262492,0.0021753237,0.00006891284,0.000014836142,0.0001797988,0.00009140027,0.96012574,0.01750071,0.0019794586,0.0015691657,0.015977329],"study_design_scores_gemma":[0.00001951664,0.000037996888,0.0005943991,0.0000023763664,0.0000030586655,0.0000087966455,0.000014805452,0.99330574,0.005359943,0.00010435158,0.0005437348,0.000005276158],"about_ca_topic_score_codex":0.017631046,"about_ca_topic_score_gemma":0.009087866,"teacher_disagreement_score":0.017631046,"about_ca_system_score_codex":0.00048670452,"about_ca_system_score_gemma":0.00092569133,"threshold_uncertainty_score":0.03505689},"labels":[],"label_agreement":null},{"id":"W2110085262","doi":"10.2514/6.2004-4179","title":"Transient Chamber Flowfield Simulation of a Rod-and-Tube Configuration Solid Rocket Motor","year":2004,"lang":"en","type":"article","venue":"40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit","topic":"Rocket and propulsion systems research","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":"Defence Research and Development Canada; Carleton University","funders":"","keywords":"Solid-fuel rocket; Transient (computer programming); Mechanics; Tube (container); Rocket (weapon); Transient analysis; Aerospace engineering; Materials science; Physics; Mechanical engineering; Transient response; Engineering; Computer science; Propellant; Electrical engineering","score_opus":0.03769517690311703,"score_gpt":0.2752617013025815,"score_spread":0.23756652439946446,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2110085262","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":[0.96064943,0.00009416554,0.029982531,0.000102912345,0.00002889637,0.000102687445,0.0005098307,0.00038716267,0.008142489],"genre_scores_gemma":[0.9946457,0.000046393943,0.0034180838,0.000011134737,0.0000025588386,0.00004150849,0.0001624364,0.000020160558,0.0016519916],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99988663,0.000020438252,0.0000060757407,0.000018473755,0.00003377065,0.000034603065],"domain_scores_gemma":[0.99964666,0.00018997058,0.000036994366,0.000021460964,0.000054231685,0.000050682716],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00019333018,0.0003170756,0.000526149,0.00026904044,0.00048466815,0.0006339399,0.00076645275,0.0009952992,0.00280917],"category_scores_gemma":[0.0007239705,0.00020793582,0.0003426655,0.00030036195,0.00054937054,0.000380742,0.00035467264,0.0004081382,0.0002197207],"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":[0.00021144649,0.00006837632,0.0015700555,0.00003587017,0.000009335223,0.00024198364,0.0000622199,0.9852166,0.009095779,0.0011657106,0.00016900465,0.0021536308],"study_design_scores_gemma":[0.00002140907,0.00006732871,0.0005872259,0.000003119899,0.0000035902356,0.000017730692,0.000019766156,0.9952618,0.0037198367,0.00007460096,0.00021613922,0.0000074159566],"about_ca_topic_score_codex":0.012179695,"about_ca_topic_score_gemma":0.0048394077,"teacher_disagreement_score":0.012179695,"about_ca_system_score_codex":0.0009381308,"about_ca_system_score_gemma":0.0008825231,"threshold_uncertainty_score":0.024217606},"labels":[],"label_agreement":null},{"id":"W2113125123","doi":"10.2514/6.2011-6052","title":"A New Ablative Material Offering SRM Nozzle Design Breakthroughs","year":2011,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Safran Electronics (Canada)","funders":"","keywords":"Nozzle; Materials science; Composite material; Propellant; Charring; Mechanical engineering; Structural engineering; Aerospace engineering; Engineering","score_opus":0.08373569570498932,"score_gpt":0.2547520483467125,"score_spread":0.17101635264172318,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2113125123","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":[0.37968677,0.05620283,0.45255655,0.0011628444,0.0017374249,0.00049837976,0.0015648453,0.0060595293,0.10053088],"genre_scores_gemma":[0.6279729,0.012767651,0.3128081,0.0006952354,0.0004078166,0.00023592419,0.000889039,0.0008463335,0.04337702],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99952066,0.000029333401,0.000021245289,0.000099573954,0.00028990264,0.00003929573],"domain_scores_gemma":[0.99973255,0.00004354041,0.0000910172,0.000040405786,0.00006158386,0.000030787596],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004757475,0.00044143302,0.0002963346,0.0007314538,0.0002073332,0.00078212103,0.0005058318,0.0009061629,0.0033386217],"category_scores_gemma":[0.0004330775,0.00032015753,0.00054506614,0.00032314216,0.00021619581,0.0010516214,0.0004350135,0.0007756027,0.0021014262],"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":[0.000058448764,0.00003643165,0.00026561262,0.00043803183,0.000012806667,0.00028420027,0.000082080034,0.0011748888,0.9412059,0.005490204,0.0014938103,0.049457554],"study_design_scores_gemma":[0.000048684673,0.0009375043,0.0025296197,0.00008350508,0.000054813343,0.0033432543,0.000039478946,0.0072436123,0.7449996,0.001300633,0.23933142,0.00008788986],"about_ca_topic_score_codex":0.00011975058,"about_ca_topic_score_gemma":0.00030037542,"teacher_disagreement_score":0.0033386217,"about_ca_system_score_codex":0.00040030433,"about_ca_system_score_gemma":0.0002165482,"threshold_uncertainty_score":0.011168838},"labels":[],"label_agreement":null},{"id":"W2123686872","doi":"10.3390/en4010090","title":"Scale Effects on Solid Rocket Combustion Instability Behaviour","year":2011,"lang":"en","type":"article","venue":"Energies","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":17,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Propellant; Solid-fuel rocket; Combustion; Mechanics; Instability; Transient (computer programming); Rocket (weapon); Internal flow; Aerospace engineering; Internal pressure; Materials science; Flow (mathematics); Engineering; Physics; Chemistry; Computer science; Composite material","score_opus":0.025057025763180273,"score_gpt":0.2533255454654947,"score_spread":0.2282685197023144,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2123686872","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":[0.99203694,0.000141995,0.0059705954,0.000023520415,0.000005593615,0.00000812385,0.00003838945,0.00014151535,0.0016332478],"genre_scores_gemma":[0.99956506,0.000030877996,0.00022770034,0.0000022650459,9.697718e-7,0.0000017426968,0.000013859483,0.0000116098,0.00014593822],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999212,0.000009973757,0.0000045078928,0.000013790259,0.000036365876,0.000014107757],"domain_scores_gemma":[0.99934834,0.00039198215,0.00011435641,0.00004608684,0.000071246104,0.000028028973],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00013193702,0.00019087485,0.00016532725,0.00019192017,0.0001301627,0.00029705281,0.0001186183,0.00017481281,0.001324659],"category_scores_gemma":[0.0016665458,0.00012238878,0.00016376487,0.00010258011,0.0002251118,0.00032354073,0.00025111806,0.00017049976,0.00019037702],"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":[0.00082830933,0.00007245124,0.018738959,0.00016433145,0.00003356989,0.0006889441,0.00021971343,0.11795427,0.83972824,0.00090776983,0.00022912804,0.020434273],"study_design_scores_gemma":[0.000042545213,0.0009884165,0.083523914,0.000017494991,0.000060034195,0.0003830859,0.00017306948,0.41463488,0.4983432,0.00078206894,0.0009923726,0.00005889375],"about_ca_topic_score_codex":0.0008283704,"about_ca_topic_score_gemma":0.0008450075,"teacher_disagreement_score":0.001324659,"about_ca_system_score_codex":0.00015404841,"about_ca_system_score_gemma":0.00010257003,"threshold_uncertainty_score":0.0044314265},"labels":[],"label_agreement":null},{"id":"W2135550419","doi":"10.2514/6.2012-2858","title":"Airfield Performance Evaluation of an Advanced Propeller on the C-130H","year":2012,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","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":"Lockheed Martin (Canada)","funders":"U.S. Air Force","keywords":"Propeller; Aeronautics; Computer science; Marine engineering; Engineering","score_opus":0.08323157262658241,"score_gpt":0.3205184738471631,"score_spread":0.23728690122058066,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2135550419","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":[0.996554,0.0000412504,0.0010834938,0.000017020806,0.000011685918,0.00003449112,0.00013896795,0.000034435052,0.0020846953],"genre_scores_gemma":[0.9966993,0.000050287425,0.0018005056,0.000009584388,0.0000038058022,0.000008165393,0.00032054153,0.0000077946615,0.0010999928],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99970704,0.000027212905,0.000009537827,0.00003108244,0.0001881715,0.000036974096],"domain_scores_gemma":[0.9995665,0.00009383199,0.00003100315,0.000034007266,0.0002140656,0.000060692706],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005345647,0.0003003528,0.00020588528,0.00050186913,0.00028302966,0.0002033426,0.00034940048,0.00021790524,0.00140433],"category_scores_gemma":[0.000573124,0.0000992195,0.00016831524,0.00030467022,0.0002604597,0.00035340304,0.00021986259,0.00026214583,0.00021770918],"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":[0.0057495264,0.0018926333,0.03911524,0.00040345304,0.000047000973,0.0004692383,0.00019036556,0.057569038,0.76378864,0.00087370374,0.0023778726,0.1275234],"study_design_scores_gemma":[0.00071411295,0.052319873,0.21510725,0.000045554163,0.00007682059,0.00070902985,0.0003318233,0.13813739,0.5823351,0.0003813625,0.009698982,0.00014272291],"about_ca_topic_score_codex":0.005814078,"about_ca_topic_score_gemma":0.006989894,"teacher_disagreement_score":0.005814078,"about_ca_system_score_codex":0.0004277354,"about_ca_system_score_gemma":0.00043172494,"threshold_uncertainty_score":0.01156044},"labels":[],"label_agreement":null},{"id":"W2142991290","doi":"10.2514/6.2007-5531","title":"A Transient Model of the VINCI Cryogenic Upper Stage Rocket Engine","year":2007,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":14,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Safran Electronics (Canada)","funders":"","keywords":"Stage (stratigraphy); Transient (computer programming); Rocket (weapon); Aerospace engineering; Aeronautics; Rocket engine; Liquid-propellant rocket; Transient analysis; Engineering; Automotive engineering; Mechanical engineering; Computer science; Electrical engineering; Transient response; Geology; Propellant; Operating system","score_opus":0.02311569837658096,"score_gpt":0.25192008176274944,"score_spread":0.2288043833861685,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2142991290","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":[0.2639023,0.0010238114,0.6180301,0.0006961058,0.00020089051,0.00036582313,0.0024071115,0.0020361678,0.111337714],"genre_scores_gemma":[0.9682675,0.00053672644,0.010142672,0.000084167055,0.00003124936,0.0002533914,0.00077988516,0.00012913684,0.019775234],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99986625,0.000017260072,0.0000070958445,0.000034027165,0.00004687753,0.000028486316],"domain_scores_gemma":[0.9999038,0.000025038555,0.000019050327,0.0000110670735,0.00003053302,0.000010505661],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00014261137,0.00044419087,0.0005782182,0.00046034824,0.0006204714,0.0009193421,0.001195856,0.0008911471,0.0027135762],"category_scores_gemma":[0.00042152384,0.00024042178,0.0007142744,0.00034992615,0.00051072484,0.00064150995,0.00050415687,0.00055991905,0.00051480153],"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":[0.000036766873,0.00001637423,0.0005404914,0.000026037796,0.000007933328,0.0000895545,0.000036331767,0.9865796,0.0028255612,0.007061444,0.00048437735,0.002295623],"study_design_scores_gemma":[0.0000060907373,0.000020795893,0.00030033017,0.0000049123937,0.000004450621,0.000024155495,0.000014242245,0.9967951,0.0008197629,0.0006714552,0.0013310418,0.0000076699525],"about_ca_topic_score_codex":0.017045692,"about_ca_topic_score_gemma":0.0049228123,"teacher_disagreement_score":0.017045692,"about_ca_system_score_codex":0.0010149949,"about_ca_system_score_gemma":0.0011460247,"threshold_uncertainty_score":0.03389293},"labels":[],"label_agreement":null},{"id":"W2144169371","doi":"10.2514/6.2008-4600","title":"Grain Geometry Modifications for Instability Symptom Suppression in Solid Rocket Motor","year":2008,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Solid-fuel rocket; Instability; Materials science; Aerospace engineering; Geometry; Mechanics; Physics; Engineering; Mathematics; Propellant","score_opus":0.04598131770831336,"score_gpt":0.30378240952305385,"score_spread":0.2578010918147405,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2144169371","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":[0.9794742,0.000040535222,0.0195818,0.000017085562,0.000005693214,0.000014046617,0.000017663559,0.00015272817,0.00069612695],"genre_scores_gemma":[0.99691916,0.000012160859,0.0029813282,0.0000017534774,5.280452e-7,0.0000034441869,0.000012913639,0.0000073391525,0.0000613863],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999466,0.0000099205345,0.0000028214104,0.000007772124,0.000022448588,0.000010426161],"domain_scores_gemma":[0.99983823,0.000056029323,0.000045253313,0.000024413963,0.000025091316,0.000010872828],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012509573,0.00020926085,0.0002388346,0.00015373,0.00014809906,0.00020378108,0.00025572808,0.00014855605,0.00051102624],"category_scores_gemma":[0.00070027483,0.00012187264,0.00016410799,0.00012203313,0.00019865186,0.0001712262,0.00017304397,0.00015044097,0.00006137484],"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":[0.00046293624,0.00010183301,0.008997936,0.00008525035,0.000031174106,0.00021190388,0.00012559968,0.6922694,0.26509,0.0012000948,0.00018706034,0.031236859],"study_design_scores_gemma":[0.000027425507,0.00034171902,0.004685546,0.000003560184,0.00002165338,0.00004825663,0.000032365635,0.89570796,0.09846876,0.00024707473,0.00040433495,0.000011412173],"about_ca_topic_score_codex":0.0015003234,"about_ca_topic_score_gemma":0.0021915357,"teacher_disagreement_score":0.0015003234,"about_ca_system_score_codex":0.00021990034,"about_ca_system_score_gemma":0.00022604565,"threshold_uncertainty_score":0.0029831529},"labels":[],"label_agreement":null},{"id":"W2149999973","doi":"10.24908/pceea.v0i0.3581","title":"GeoSurv II Unmanned Aerial Vehicle: A major undergraduate project with","year":2011,"lang":"en","type":"article","venue":"Proceedings of the Canadian Engineering Education Association (CEEA)","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Capstone; Avionics; Aerospace; Engineering; Engineering management; Government (linguistics); Aeronautics; Engineering education; Project management; Project manager; Test (biology); Systems engineering; Computer science; Aerospace engineering","score_opus":0.014583571634648832,"score_gpt":0.21123907580056414,"score_spread":0.19665550416591532,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2149999973","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":[0.7174095,0.00165895,0.1817487,0.005057662,0.0013541796,0.0041207415,0.0012895345,0.0033621318,0.08399878],"genre_scores_gemma":[0.6173341,0.0015421992,0.15536617,0.00095104246,0.00031130423,0.0015294406,0.001959932,0.0006428567,0.22036302],"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9989611,0.0002382521,0.000032542117,0.00014086129,0.00041668827,0.0002106459],"domain_scores_gemma":[0.99790156,0.0000769175,0.00006200503,0.00010355634,0.00067958125,0.0011763832],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.002306357,0.0007744011,0.00034075178,0.00042358102,0.000856595,0.0013795393,0.00046768208,0.00059981877,0.007866566],"category_scores_gemma":[0.0011808139,0.00029330573,0.00038560602,0.00024892972,0.0003874909,0.00071455864,0.001324251,0.00094813784,0.0028357732],"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":[0.0010575345,0.0058437283,0.014163539,0.0005782412,0.000074273594,0.00079766585,0.007048734,0.009362907,0.116319224,0.015404842,0.067432,0.7619174],"study_design_scores_gemma":[0.00037053565,0.02113243,0.022520823,0.0002660322,0.00007759941,0.0016509127,0.006724104,0.01994506,0.11614398,0.006190377,0.8048851,0.00009303568],"about_ca_topic_score_codex":0.0009186224,"about_ca_topic_score_gemma":0.0016453556,"teacher_disagreement_score":0.007866566,"about_ca_system_score_codex":0.0011784278,"about_ca_system_score_gemma":0.0019705044,"threshold_uncertainty_score":0.026316285},"labels":[],"label_agreement":null},{"id":"W2150524741","doi":"10.2514/6.2004-3726","title":"Numerical Transient Burning Rate Model for Solid Rocket Motor Simulations","year":2004,"lang":"en","type":"article","venue":"40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Solid-fuel rocket; Transient (computer programming); Rocket (weapon); Transient analysis; Aerospace engineering; Mechanics; Materials science; Computer science; Transient response; Propellant; Physics; Engineering; Electrical engineering","score_opus":0.057613598569615274,"score_gpt":0.2929326913096195,"score_spread":0.23531909274000423,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2150524741","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":[0.027256431,0.000270864,0.94997114,0.00018899438,0.000088904955,0.0001459479,0.00039966675,0.0008574329,0.020820657],"genre_scores_gemma":[0.7904744,0.0007251448,0.15573852,0.00019893245,0.000068930545,0.0015032637,0.0012370016,0.000683229,0.04937051],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99978584,0.000036873764,0.00001382621,0.00003525774,0.00009501252,0.000033267712],"domain_scores_gemma":[0.999569,0.00013938679,0.000060383987,0.000052044914,0.00014080407,0.00003829958],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00047909375,0.000538072,0.00073389936,0.0004502018,0.0004138318,0.0008471681,0.0020378744,0.0013927135,0.00581308],"category_scores_gemma":[0.0018954274,0.00042240316,0.00072252617,0.00044561923,0.00049168203,0.0010338692,0.0007163395,0.0009945144,0.001564773],"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":[0.000025832722,0.000017176004,0.00019734113,0.00002689677,0.000007676699,0.000047707843,0.0000281483,0.98012537,0.0030996266,0.013758401,0.00031566405,0.0023501995],"study_design_scores_gemma":[0.000002702177,0.0000024970943,0.0000215657,0.0000015064857,8.1777654e-7,0.000003952328,0.0000015057919,0.99851936,0.00024998846,0.0007948902,0.00039939355,0.000001865933],"about_ca_topic_score_codex":0.00555052,"about_ca_topic_score_gemma":0.0023342506,"teacher_disagreement_score":0.00581308,"about_ca_system_score_codex":0.0010645342,"about_ca_system_score_gemma":0.0009521514,"threshold_uncertainty_score":0.01944673},"labels":[],"label_agreement":null},{"id":"W2155611933","doi":"10.3390/en8021195","title":"Numerical Evaluation of the Use of Aluminum Particles for Enhancing Solid Rocket Motor Combustion Stability","year":2015,"lang":"en","type":"article","venue":"Energies","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":15,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Propellant; Solid-fuel rocket; Combustion; Mechanics; Rocket (weapon); Materials science; Internal flow; Transient (computer programming); Instability; Solid fuel; Particle (ecology); Chamber pressure; Flow (mathematics); Aerospace engineering; Chemistry; Physics; Engineering; Geology","score_opus":0.20694164994955488,"score_gpt":0.3360258584657945,"score_spread":0.12908420851623964,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2155611933","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":[0.97836053,0.00009447777,0.017560242,0.00003752719,0.000015124459,0.000033054996,0.000037081674,0.0000961256,0.0037658392],"genre_scores_gemma":[0.9953237,0.000032433367,0.004265541,0.0000022226964,8.094369e-7,0.000006633987,0.000012560649,0.000005123415,0.00035092368],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999074,0.000017770168,0.0000057721004,0.000008822681,0.000043864467,0.000016423252],"domain_scores_gemma":[0.9995728,0.00019808496,0.00007830128,0.00003328639,0.00009585653,0.00002176738],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00032210682,0.00024823696,0.00023123313,0.00029200187,0.00017064466,0.000349937,0.00030172442,0.00029720546,0.00081505603],"category_scores_gemma":[0.001080255,0.00008869864,0.00016341172,0.00019060932,0.00031829224,0.00017584817,0.00022293313,0.0001428832,0.00009194399],"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":[0.00072280236,0.00020529448,0.005702375,0.00023907125,0.000024316269,0.00026713038,0.0001497397,0.7270695,0.23584434,0.002704213,0.00020176444,0.026869392],"study_design_scores_gemma":[0.000032794247,0.00053931103,0.0012695511,0.000005914677,0.000013853868,0.000027889959,0.000038187423,0.9194473,0.07807231,0.00014632817,0.0003978978,0.000008678223],"about_ca_topic_score_codex":0.0017064802,"about_ca_topic_score_gemma":0.0015579462,"teacher_disagreement_score":0.0017064802,"about_ca_system_score_codex":0.00024580382,"about_ca_system_score_gemma":0.00027044743,"threshold_uncertainty_score":0.0033931136},"labels":[],"label_agreement":null},{"id":"W2158471363","doi":"10.2514/6.2011-6133","title":"C2b Rayon Source Requalification for Carbon Phenolic Nozzle Insulators","year":2011,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","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":"Safran Electronics (Canada)","funders":"","keywords":"Nozzle; Carbon fibers; Materials science; Polymer science; Aerospace engineering; Computer science; Environmental science; Engineering; Biochemical engineering; Composite material","score_opus":0.07017224270832065,"score_gpt":0.2665000285642123,"score_spread":0.19632778585589164,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2158471363","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":[0.8971135,0.0017608845,0.04085614,0.00018630558,0.00029198025,0.0005624155,0.0014160795,0.0041448628,0.053667817],"genre_scores_gemma":[0.93755317,0.00059179944,0.026100539,0.000126704,0.000043011994,0.00017370406,0.0017319954,0.0009440083,0.03273513],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9995184,0.000024863893,0.000016925813,0.000095960604,0.00026266402,0.000081223996],"domain_scores_gemma":[0.99956626,0.00004236257,0.00009286155,0.00008212073,0.00017028117,0.000046097637],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00032373512,0.00053297024,0.0002431109,0.001048276,0.00042944562,0.00063676474,0.0005291707,0.0006448246,0.009806256],"category_scores_gemma":[0.0003640087,0.0002082227,0.00031248084,0.0005803497,0.00023958269,0.00044864454,0.0004952892,0.0005044009,0.0033463198],"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":[0.00012054991,0.000031562126,0.00048225623,0.000112921225,0.0000056535237,0.00014737736,0.00004349882,0.0001723966,0.98999435,0.0003514332,0.00094864535,0.007589398],"study_design_scores_gemma":[0.000015923593,0.00020100198,0.003351014,0.000013332196,0.0000073126835,0.00017236476,0.000021921267,0.00071274675,0.9769886,0.000029761703,0.018474454,0.000011410061],"about_ca_topic_score_codex":0.0015951298,"about_ca_topic_score_gemma":0.0027281295,"teacher_disagreement_score":0.009806256,"about_ca_system_score_codex":0.0007017567,"about_ca_system_score_gemma":0.00044121736,"threshold_uncertainty_score":0.032805145},"labels":[],"label_agreement":null},{"id":"W2168728774","doi":"10.1002/prep.200390019","title":"Effect of Porosity on the Burn Rate of a Gas‐Generating Composition","year":2003,"lang":"en","type":"article","venue":"Propellants Explosives Pyrotechnics","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Defence Research and Development Canada","funders":"","keywords":"Propellant; Porosity; Burn rate (chemistry); Materials science; Volume fraction; Composite number; Volume (thermodynamics); Fraction (chemistry); Composite material; Chemistry; Chromatography; Thermodynamics; Organic chemistry","score_opus":0.02090768766323495,"score_gpt":0.2542652801005663,"score_spread":0.23335759243733137,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2168728774","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":[0.99720806,0.00035248295,0.0017354004,0.0000090804815,0.000005507947,0.0000071268964,0.000053099982,0.000041790136,0.0005874492],"genre_scores_gemma":[0.9990294,0.00013918206,0.0004688978,0.000003820882,0.0000012904586,0.0000030710492,0.000030871954,0.000015494064,0.00030792406],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997888,0.00003706864,0.000014967118,0.00003678522,0.00007463446,0.000047723064],"domain_scores_gemma":[0.99886835,0.00067607267,0.00019980154,0.00008573408,0.00009716418,0.00007286733],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00030866396,0.00025365892,0.00019092146,0.00019956409,0.000100259895,0.00031594918,0.0002034681,0.00020590666,0.0010605747],"category_scores_gemma":[0.0013946933,0.0001941378,0.00013794002,0.00015455544,0.00022770718,0.00032979753,0.00020448957,0.000370361,0.00020498344],"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":[0.000929205,0.000076243756,0.0011706485,0.000059543203,0.000014604428,0.00006824547,0.000045689594,0.0026798877,0.9904331,0.00009865989,0.000018604358,0.004405494],"study_design_scores_gemma":[0.0000056720596,0.00031557094,0.0017810072,0.0000043414348,0.000010256688,0.000033420165,0.000012449712,0.0022556498,0.99537945,0.000010469391,0.00018717852,0.0000046210725],"about_ca_topic_score_codex":0.00044017722,"about_ca_topic_score_gemma":0.00042149815,"teacher_disagreement_score":0.0010605747,"about_ca_system_score_codex":0.00015675575,"about_ca_system_score_gemma":0.0001258861,"threshold_uncertainty_score":0.0035479665},"labels":[],"label_agreement":null},{"id":"W2171945004","doi":"10.1134/s0869864313030013","title":"Investigating an annular nozzle on combustion products of hydrocarbon fuels","year":2013,"lang":"en","type":"article","venue":"Thermophysics and Aeromechanics","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":4,"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; Thrust; Jet (fluid); Mechanics; Combustion; Aerospace engineering; Rocket engine nozzle; Materials science; Thermodynamics; Environmental science; Physics; Chemistry; Engineering","score_opus":0.02065569197191327,"score_gpt":0.2275730768501525,"score_spread":0.2069173848782392,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2171945004","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":[0.99528825,0.00019479694,0.0034647319,0.0000105882045,0.0000061371707,0.000007513849,0.000033529665,0.000029605013,0.00096486777],"genre_scores_gemma":[0.997396,0.00011221939,0.0021954305,0.000003682716,0.0000016780529,0.0000036538513,0.00005223765,0.0000061276455,0.0002290256],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998771,0.000014439995,0.0000068967556,0.000024765639,0.000050045768,0.000026651776],"domain_scores_gemma":[0.99986064,0.000052967298,0.000020165584,0.000012979946,0.000040029423,0.000013220424],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00032177626,0.00021238698,0.00042457934,0.00021212873,0.00027365383,0.00051328354,0.00032303066,0.00028104254,0.0006456899],"category_scores_gemma":[0.0004290786,0.00012893247,0.00029383664,0.0002257904,0.00028263917,0.000396393,0.00034406062,0.00016827544,0.00009663494],"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":[0.00096436514,0.0002370931,0.0219926,0.00040058084,0.00004544644,0.0010923822,0.00025511443,0.12195573,0.8278628,0.004051407,0.0002106603,0.020931818],"study_design_scores_gemma":[0.00012056701,0.0014716125,0.030296698,0.000030554027,0.00006681299,0.0005575111,0.00026276245,0.49306044,0.47153565,0.0008009035,0.0017581405,0.000038318693],"about_ca_topic_score_codex":0.0013455662,"about_ca_topic_score_gemma":0.00065068103,"teacher_disagreement_score":0.0013455662,"about_ca_system_score_codex":0.00025198315,"about_ca_system_score_gemma":0.0002939846,"threshold_uncertainty_score":0.0026754737},"labels":[],"label_agreement":null},{"id":"W2228644024","doi":"10.4271/2004-01-2588","title":"Development of NASA High Strength Aluminum Alloy for Use in the Evinrude ETEC Outboard Engine","year":2004,"lang":"en","type":"article","venue":"SAE technical papers on CD-ROM/SAE technical paper series","topic":"Rocket and propulsion systems research","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":"Bombardier Recreational Products (Canada)","funders":"National Aeronautics and Space Administration","keywords":"Alloy; Aluminium; Materials science; Metallurgy","score_opus":0.02673752662776086,"score_gpt":0.2672933299826072,"score_spread":0.24055580335484633,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2228644024","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":[0.9219066,0.0010751748,0.037464637,0.00021984673,0.0002826705,0.00063540513,0.00048226534,0.0011078403,0.036825582],"genre_scores_gemma":[0.90486383,0.00085020816,0.05619895,0.00012869637,0.000031804837,0.00020228523,0.0008143494,0.00020949895,0.03670038],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99963295,0.000029747234,0.000019233881,0.00003471909,0.00025828596,0.000025145184],"domain_scores_gemma":[0.9996506,0.000017626813,0.000045441706,0.0000275564,0.00022402758,0.000034764133],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004992466,0.0003684895,0.00024702388,0.0006174736,0.0003649018,0.000490692,0.0005553362,0.0005160922,0.0013050995],"category_scores_gemma":[0.0005243454,0.00017112485,0.00031082914,0.00024473047,0.00012466691,0.00037218753,0.00026921442,0.0002952092,0.00070246495],"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":[0.00018032077,0.00024107183,0.0019994164,0.00017849689,0.000014541597,0.00049049815,0.00013028696,0.00238297,0.95551723,0.0006405434,0.00092382665,0.037300818],"study_design_scores_gemma":[0.00005006072,0.0017376211,0.0056570317,0.000022433678,0.000029135123,0.00044214405,0.000065996326,0.0033822616,0.9572448,0.00004568756,0.031306285,0.00001660253],"about_ca_topic_score_codex":0.0016124638,"about_ca_topic_score_gemma":0.003945757,"teacher_disagreement_score":0.0016124638,"about_ca_system_score_codex":0.0003702948,"about_ca_system_score_gemma":0.0005446736,"threshold_uncertainty_score":0.0043659806},"labels":[],"label_agreement":null},{"id":"W2234203318","doi":"","title":"수력학적 상사를 적용한 초음속 노즐 내부 유동 연구","year":2009,"lang":"ko","type":"article","venue":"한국추진공학회 학술대회논문집","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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; Rocket (weapon); Mechanics; Hydraulics; Rocket engine nozzle; Flow (mathematics); Aerospace engineering; Supersonic speed; Engineering; Mechanical engineering; Physics","score_opus":0.02416892893313122,"score_gpt":0.2901904527054929,"score_spread":0.26602152377236166,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2234203318","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":[0.8340529,0.00021113582,0.14691149,0.00010762002,0.000048707057,0.00011609985,0.00024736475,0.00037100294,0.01793374],"genre_scores_gemma":[0.9775138,0.00010133213,0.02025115,0.000010032187,0.0000037515151,0.000027570353,0.00010637233,0.000009913606,0.001976086],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99990916,0.000009798925,0.000004118463,0.000021546857,0.000045849032,0.000009371582],"domain_scores_gemma":[0.99992526,0.000018819346,0.000014002271,0.00001373498,0.000023368177,0.000004834521],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016715981,0.00008276412,0.00016868814,0.00010491969,0.00024301356,0.0002733946,0.00017203514,0.0001356092,0.0017279151],"category_scores_gemma":[0.00024317186,0.000062103536,0.00013620807,0.00012947037,0.00034364592,0.00032887602,0.00013906868,0.0001490521,0.00025783968],"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":[0.0002495665,0.000048491816,0.0059828144,0.0001942718,0.000012415497,0.00021399754,0.00013284141,0.027395392,0.8854466,0.020428255,0.0004934208,0.05940186],"study_design_scores_gemma":[0.000045586163,0.00079021265,0.020059032,0.000011076803,0.000017409233,0.00039032675,0.000115482515,0.19997334,0.76179564,0.0043178084,0.012435673,0.000048365157],"about_ca_topic_score_codex":0.0008169774,"about_ca_topic_score_gemma":0.0005758343,"teacher_disagreement_score":0.0017279151,"about_ca_system_score_codex":0.00021305408,"about_ca_system_score_gemma":0.00037971273,"threshold_uncertainty_score":0.0057804585},"labels":[],"label_agreement":null},{"id":"W2260698102","doi":"10.1520/stp159620150079","title":"Evaluation of Containment Boxes as a Fire Mitigation Method in Elevated Oxygen Conditions","year":2016,"lang":"en","type":"book-chapter","venue":"","topic":"Rocket and propulsion systems research","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":"Lockheed Martin (Canada)","funders":"","keywords":"Containment (computer programming); Environmental science; Oxygen; Nuclear engineering; Forensic engineering; Waste management; Computer science; Engineering; Chemistry","score_opus":0.04506943626588627,"score_gpt":0.3436905961300025,"score_spread":0.29862115986411625,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2260698102","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":[0.9349153,0.0034041589,0.040253546,0.00009415022,0.00011859442,0.00031356842,0.00032952256,0.0006368898,0.019934222],"genre_scores_gemma":[0.9188507,0.0026699116,0.06430006,0.00006325269,0.000016395416,0.00018680093,0.00056773337,0.00013261462,0.013212465],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9996749,0.000051635816,0.000012085773,0.000030969422,0.00020127498,0.0000291977],"domain_scores_gemma":[0.9997445,0.000083345636,0.000039613515,0.000028533932,0.00008515394,0.000018817522],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00047922344,0.0003734772,0.0002425379,0.0003910219,0.00022964111,0.000464501,0.00078942464,0.0003206154,0.0010793292],"category_scores_gemma":[0.00052178226,0.00015782134,0.00019004385,0.00023491823,0.00017379833,0.0004363107,0.00026357686,0.00019569728,0.00040785765],"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":[0.00061975664,0.00035855357,0.0032530644,0.00057602033,0.000027344086,0.0002993614,0.00025633638,0.013909435,0.8374021,0.0016928621,0.0010902736,0.14051487],"study_design_scores_gemma":[0.00003111228,0.0020124554,0.005386571,0.0000808976,0.00004027818,0.0002610916,0.00012291691,0.012614613,0.9669056,0.00019082005,0.012331953,0.000021843218],"about_ca_topic_score_codex":0.0007969543,"about_ca_topic_score_gemma":0.0014729769,"teacher_disagreement_score":0.0010793292,"about_ca_system_score_codex":0.0002697038,"about_ca_system_score_gemma":0.0003202256,"threshold_uncertainty_score":0.0036106706},"labels":[],"label_agreement":null},{"id":"W2274365723","doi":"","title":"Heat and Fluid Flow Analysis in a Molten CuCl Heat Exchanger","year":2009,"lang":"en","type":"dissertation","venue":"e-scholar@UOIT (University of Ontario Institute of Technology)","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":9,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Natural Sciences and Engineering Research Council of Canada; Atomic Energy of Canada Limited","keywords":"Heat exchanger; Fluid dynamics; Flow (mathematics); Thermodynamics; Materials science; Mechanics; Mechanical engineering; Petroleum engineering; Engineering; Physics","score_opus":0.01161669008606619,"score_gpt":0.22005199469601117,"score_spread":0.20843530460994497,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2274365723","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":[0.9298783,0.00037495396,0.06013036,0.00025504077,0.00007003522,0.00014426853,0.0006378966,0.0009172571,0.0075917756],"genre_scores_gemma":[0.98151684,0.00020246196,0.011531684,0.000027397555,0.000016147333,0.00006821121,0.00032613578,0.00007431266,0.0062367576],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998802,0.0000112931175,0.000004722434,0.000041117924,0.000036189467,0.000026362113],"domain_scores_gemma":[0.9998778,0.000056529356,0.000022094968,0.000010059602,0.000023310135,0.000010197409],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00026673437,0.0004509543,0.0004324894,0.0006422244,0.0005131823,0.0009788885,0.0005185639,0.0008844247,0.0022714357],"category_scores_gemma":[0.000388208,0.0002535951,0.0006397552,0.00030097543,0.00068536366,0.0006819229,0.0003334628,0.0004949286,0.0003620797],"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":[0.00037823358,0.00042623008,0.014097205,0.00026343335,0.000030012001,0.00035640935,0.0002969983,0.7747056,0.17797638,0.010385461,0.00092147954,0.02016252],"study_design_scores_gemma":[0.0000072931,0.00005256438,0.0009906109,0.0000051213347,0.0000025672923,0.000008926597,0.000016794851,0.9845707,0.013838587,0.00015183025,0.00034684967,0.000008091572],"about_ca_topic_score_codex":0.012727416,"about_ca_topic_score_gemma":0.004814523,"teacher_disagreement_score":0.012727416,"about_ca_system_score_codex":0.0010976901,"about_ca_system_score_gemma":0.0009821492,"threshold_uncertainty_score":0.025306642},"labels":[],"label_agreement":null},{"id":"W2281457697","doi":"10.4271/2001-01-1966","title":"The Flammability of Atmospheres Within Nearly-Empty Liquid Fuel Tanks","year":2001,"lang":"en","type":"article","venue":"SAE technical papers on CD-ROM/SAE technical paper series","topic":"Rocket and propulsion systems research","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":"University of Calgary","funders":"","keywords":"Flammability; Environmental science; Waste management; Materials science; Liquid fuel; Nuclear engineering; Engineering; Combustion; Composite material; Chemistry","score_opus":0.015175017227330471,"score_gpt":0.2576998794230767,"score_spread":0.24252486219574623,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2281457697","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":[0.98602575,0.00007822086,0.011735929,0.000023787157,0.000005541078,0.000005899763,0.00008002735,0.00015772444,0.0018871215],"genre_scores_gemma":[0.99862266,0.000038876144,0.0007734782,0.0000046779032,0.0000014296368,0.0000024012315,0.000062239065,0.00001331122,0.0004809914],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99988747,0.000015214061,0.0000043258838,0.00002405017,0.000048248254,0.000020746922],"domain_scores_gemma":[0.9998141,0.00008877598,0.00003857656,0.000015671207,0.000029010156,0.000013914115],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00014437037,0.00019743692,0.00015755174,0.00018597893,0.00025280204,0.0005499864,0.00025255294,0.00021243315,0.00063390034],"category_scores_gemma":[0.00055937754,0.00013674045,0.0001916174,0.00014889157,0.00040161962,0.0006316412,0.0003413401,0.00025716354,0.0001417252],"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":[0.00058550324,0.00006675127,0.007812887,0.000064884895,0.000017159631,0.0005620187,0.00027607277,0.22198762,0.75190187,0.0024608746,0.00026617842,0.013998311],"study_design_scores_gemma":[0.000026236361,0.0002986241,0.016000357,0.00001257692,0.00002091757,0.00022564536,0.00022062976,0.5245965,0.45644963,0.0011384841,0.0009565198,0.00005390863],"about_ca_topic_score_codex":0.0035307123,"about_ca_topic_score_gemma":0.0017441266,"teacher_disagreement_score":0.0035307123,"about_ca_system_score_codex":0.00043338517,"about_ca_system_score_gemma":0.00018862904,"threshold_uncertainty_score":0.0070202947},"labels":[],"label_agreement":null},{"id":"W2313294797","doi":"10.2514/6.2004-282","title":"Integration of Aerodynamic, Structural, Cost and Manufacturing Cosiderations During the Conceptual Design of a Thrust Reverser Cascade","year":2004,"lang":"en","type":"article","venue":"42nd AIAA Aerospace Sciences Meeting and Exhibit","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Queen's University","funders":"","keywords":"Aerodynamics; Cascade; Conceptual design; Computer science; Aerospace engineering; Engineering; Mechanical engineering","score_opus":0.028936110929447766,"score_gpt":0.26538957823448167,"score_spread":0.23645346730503392,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2313294797","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":[0.8450142,0.00030896804,0.12819962,0.0005709532,0.00006182042,0.0001325296,0.000034381286,0.00013723258,0.025540302],"genre_scores_gemma":[0.9734644,0.000065192384,0.024683334,0.000039645132,0.000012299822,0.000026570604,0.000014232273,0.000040410756,0.0016537256],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99907136,0.00029372878,0.000033056967,0.000062129766,0.00037062657,0.0001690103],"domain_scores_gemma":[0.9986426,0.0007029966,0.00026782413,0.000071453935,0.00026804284,0.000047027625],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0013955834,0.00062608736,0.0004315276,0.00037493426,0.00072633487,0.0014027802,0.0006391497,0.000624251,0.0018771475],"category_scores_gemma":[0.002724883,0.00050436164,0.00029870422,0.00019471638,0.00053456397,0.0010577877,0.00062209024,0.00080231024,0.00016995227],"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":[0.000642962,0.00026360925,0.0067585376,0.0001779505,0.00007949458,0.0008267197,0.0003929758,0.67604595,0.21049596,0.02521239,0.0005348327,0.07856873],"study_design_scores_gemma":[0.00009517572,0.002665851,0.011337293,0.000049369162,0.00022363703,0.00051199424,0.00061079144,0.8598526,0.110607296,0.0055433055,0.008407134,0.00009552817],"about_ca_topic_score_codex":0.00149767,"about_ca_topic_score_gemma":0.0056965896,"teacher_disagreement_score":0.0018771475,"about_ca_system_score_codex":0.0010352919,"about_ca_system_score_gemma":0.0010917078,"threshold_uncertainty_score":0.007511556},"labels":[],"label_agreement":null},{"id":"W2314218311","doi":"10.2514/6.2011-6056","title":"Segmented SRM Pressure Oscillation Demonstrator","year":2011,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":6,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Safran Electronics (Canada)","funders":"","keywords":"Thrust; Oscillation (cell signaling); Acoustics; Vortex; Aerospace engineering; Physics; Solid-fuel rocket; Payload (computing); Rocket (weapon); Engineering; Mechanics; Computer science; Propellant","score_opus":0.040580792079666465,"score_gpt":0.2307743447958728,"score_spread":0.19019355271620633,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2314218311","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":[0.78263485,0.0004637373,0.16459848,0.0016184008,0.00046651898,0.000407721,0.0014593756,0.006426252,0.04192466],"genre_scores_gemma":[0.9319222,0.00012855962,0.046498854,0.00012745142,0.000087279375,0.000192283,0.00051497534,0.00022075375,0.020307763],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9996917,0.000028217446,0.000013163142,0.00006938034,0.0001590346,0.000038669295],"domain_scores_gemma":[0.9997166,0.000047659676,0.00005169848,0.00004799428,0.00008078534,0.000055187735],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00036694427,0.00031975977,0.00035255437,0.0001659924,0.00029737328,0.00035109738,0.00082589436,0.00085396954,0.006964656],"category_scores_gemma":[0.00037426397,0.00012808962,0.00017135263,0.00014789063,0.00027109956,0.00060966745,0.0007110169,0.000449604,0.0018798483],"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":[0.00064951606,0.0001439235,0.0009059604,0.0002648444,0.00002857808,0.0009771517,0.00028210937,0.0033126285,0.93965244,0.0027114039,0.0048934883,0.046178047],"study_design_scores_gemma":[0.00038567488,0.004301536,0.0070499647,0.00004227986,0.000034293716,0.0011631511,0.00019302557,0.07040176,0.8392134,0.0011051946,0.07604794,0.0000618423],"about_ca_topic_score_codex":0.00032683628,"about_ca_topic_score_gemma":0.00040727094,"teacher_disagreement_score":0.006964656,"about_ca_system_score_codex":0.00023259102,"about_ca_system_score_gemma":0.00020758995,"threshold_uncertainty_score":0.023299098},"labels":[],"label_agreement":null},{"id":"W2314403529","doi":"10.2514/6.2005-3546","title":"Accounting for Planned Fuel Expulsion by Hybrid Rockets","year":2005,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lockheed Martin (Canada)","funders":"","keywords":"Aeronautics; Aerospace engineering; Automotive engineering; Environmental science; Engineering","score_opus":0.015791631539260456,"score_gpt":0.2611114049341796,"score_spread":0.24531977339491917,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2314403529","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":[0.74214125,0.00018141366,0.2521782,0.00013127913,0.00005640046,0.000093773924,0.0003334497,0.0010646483,0.0038196049],"genre_scores_gemma":[0.98167634,0.000051570216,0.016885793,0.000007731258,0.000007235461,0.000024321256,0.00014874668,0.000075932316,0.0011224258],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99949396,0.000074166426,0.000028540879,0.00012149793,0.00021280927,0.00006896582],"domain_scores_gemma":[0.9980236,0.0008412275,0.00045078385,0.00022929716,0.0003710052,0.000084118976],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0010249551,0.00088105525,0.00055449706,0.00086487766,0.00035622614,0.0007523936,0.0013066491,0.00054102036,0.0014914023],"category_scores_gemma":[0.0036731337,0.0005641709,0.000615537,0.0005620798,0.00039738786,0.0016801546,0.0006371642,0.00092562294,0.00018932403],"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":[0.00045122567,0.000060863553,0.030174578,0.000057718004,0.00009991684,0.00053241866,0.00007344935,0.91195977,0.0075288955,0.0020729834,0.00032427872,0.04666402],"study_design_scores_gemma":[0.000013390084,0.00010884178,0.0062683206,0.000004424648,0.000026825857,0.00008247853,0.000045474408,0.98665434,0.0053690774,0.001000343,0.00040924197,0.000017215803],"about_ca_topic_score_codex":0.011721495,"about_ca_topic_score_gemma":0.012954212,"teacher_disagreement_score":0.011721495,"about_ca_system_score_codex":0.0009243697,"about_ca_system_score_gemma":0.0011262782,"threshold_uncertainty_score":0.023306549},"labels":[],"label_agreement":null},{"id":"W2314498873","doi":"10.2514/6.2012-3727","title":"Effect of Diminishing Particle Size on Solid Rocket Combustion Instability Symptom Suppression","year":2012,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Propellant; Solid-fuel rocket; Mechanics; Combustion; Internal flow; Rocket (weapon); Particle (ecology); Instability; Particle size; Materials science; Transient (computer programming); Computer simulation; Flow (mathematics); Physics; Aerospace engineering; Engineering; Chemistry; Computer science; Geology","score_opus":0.017020124127252206,"score_gpt":0.30123651309571,"score_spread":0.2842163889684578,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2314498873","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":[0.9930025,0.000077769015,0.006000873,0.000015664584,0.0000055915775,0.000012995675,0.000022121783,0.000120492245,0.0007420159],"genre_scores_gemma":[0.99828655,0.000025916195,0.001522729,0.0000036052152,7.9011164e-7,0.000003472568,0.000015972078,0.000011396629,0.00012943783],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998186,0.000032406864,0.000014420243,0.00003009963,0.000072023,0.00003243286],"domain_scores_gemma":[0.99839896,0.0009306366,0.00026970753,0.000141775,0.00018617818,0.00007283775],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00037074322,0.00027890896,0.0002448005,0.00024324491,0.00016587295,0.00037443367,0.00037711035,0.00023014151,0.0007685774],"category_scores_gemma":[0.0033408452,0.00013515429,0.00019435839,0.00011654356,0.00027705904,0.00027572145,0.00025487834,0.00020635617,0.00012203439],"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":[0.0021514597,0.00037187224,0.026009219,0.0002257895,0.000055119737,0.00041446908,0.00022293115,0.23834348,0.6757324,0.00066270033,0.00016233411,0.055648334],"study_design_scores_gemma":[0.000041900268,0.0021589268,0.017006652,0.000010228812,0.00005535469,0.00013053494,0.00009387816,0.24638696,0.7334929,0.000099763376,0.0005017597,0.000021167585],"about_ca_topic_score_codex":0.0012918925,"about_ca_topic_score_gemma":0.0014028637,"teacher_disagreement_score":0.0012918925,"about_ca_system_score_codex":0.00016503964,"about_ca_system_score_gemma":0.00026628462,"threshold_uncertainty_score":0.002571106},"labels":[],"label_agreement":null},{"id":"W2314783894","doi":"10.2514/6.2011-7057","title":"Flight Test Evaluation and Aerodynamic Performance Modeling of a C-130H with an Advanced Propeller","year":2011,"lang":"en","type":"article","venue":"11th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lockheed Martin (Canada)","funders":"","keywords":"Aerodynamics; Propeller; Aerospace engineering; Computer science; Test (biology); Marine engineering; Aeronautics; Engineering; Automotive engineering; Geology","score_opus":0.03302273290594467,"score_gpt":0.25866617884206455,"score_spread":0.22564344593611987,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2314783894","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":[0.99140316,0.00004497144,0.004813495,0.00002971895,0.000012480498,0.000051839572,0.0003206312,0.00011797839,0.0032056612],"genre_scores_gemma":[0.99650925,0.00003462991,0.0025200057,0.000007439116,0.0000024037554,0.000015514684,0.00023352029,0.000011896191,0.00066540367],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999752,0.000028236915,0.000008531646,0.000034564633,0.00013474342,0.000041888397],"domain_scores_gemma":[0.9996344,0.00013304218,0.000029136685,0.000038264294,0.000129126,0.000035938712],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00048554628,0.0004770085,0.00029766373,0.00044335958,0.0003266568,0.00027821737,0.00061733834,0.00041820903,0.00097654434],"category_scores_gemma":[0.0005692128,0.00014831274,0.0003008414,0.00024770477,0.00026218657,0.00030587282,0.00020698339,0.00030250844,0.00018583234],"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":[0.0012265162,0.00077886943,0.018945765,0.0002217665,0.000066888824,0.00044306475,0.0001726062,0.7991647,0.1399889,0.0009887936,0.0018287626,0.036173414],"study_design_scores_gemma":[0.00011623505,0.0035750682,0.017689236,0.000010698689,0.000025317771,0.00012152147,0.000049719063,0.9418571,0.03525984,0.00013439597,0.0011165788,0.000044325465],"about_ca_topic_score_codex":0.010756955,"about_ca_topic_score_gemma":0.007330647,"teacher_disagreement_score":0.010756955,"about_ca_system_score_codex":0.00055147137,"about_ca_system_score_gemma":0.0005101662,"threshold_uncertainty_score":0.02138871},"labels":[],"label_agreement":null},{"id":"W2314918442","doi":"10.2514/6.2009-6523","title":"Enhancing Human Spaceflight Safety Through Spacecraft Survivability Engineering","year":2009,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lockheed Martin (Canada)","funders":"","keywords":"Survivability; Crew; Spacecraft; Human spaceflight; Engineering; Aeronautics; Systems engineering; Vulnerability (computing); Reliability (semiconductor); Resilience (materials science); Adaptation (eye); Computer science; Reliability engineering; Computer security; Aerospace engineering","score_opus":0.016148565536812563,"score_gpt":0.2711029856316263,"score_spread":0.2549544200948138,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2314918442","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":[0.1388904,0.012263757,0.5212336,0.026910929,0.004186077,0.00049651216,0.00035648423,0.0023301449,0.29333216],"genre_scores_gemma":[0.6384582,0.0068892743,0.15533337,0.003587404,0.0004976133,0.00029419697,0.00036298798,0.00025816626,0.19431886],"study_design_codex":"design_other","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.99926275,0.00018811386,0.000019664902,0.00007252892,0.0003535341,0.00010339305],"domain_scores_gemma":[0.99889934,0.00026980363,0.000085234955,0.00010120096,0.00048262742,0.00016181017],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0018830005,0.00067941315,0.0001817124,0.0008809936,0.0009627985,0.0012270035,0.0005638766,0.0008774946,0.006238855],"category_scores_gemma":[0.0021978782,0.00021709107,0.00036554245,0.0002547221,0.0010820554,0.0012093581,0.0019528908,0.0014553741,0.00096676894],"study_design_candidate":"theoretical_or_conceptual","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":[0.0002286117,0.00022856852,0.003607496,0.00026532853,0.000048551334,0.00030850028,0.0019512532,0.008459912,0.033380136,0.25851145,0.044896375,0.64811385],"study_design_scores_gemma":[0.00007206232,0.0013474723,0.0033983395,0.00030008992,0.000039298797,0.00040960283,0.00068481476,0.016277617,0.03221134,0.047688086,0.8975054,0.00006583845],"about_ca_topic_score_codex":0.0021340705,"about_ca_topic_score_gemma":0.0028726044,"teacher_disagreement_score":0.006238855,"about_ca_system_score_codex":0.0012760302,"about_ca_system_score_gemma":0.001359136,"threshold_uncertainty_score":0.020871043},"labels":[],"label_agreement":null},{"id":"W2315204267","doi":"10.2514/6.2005-3582","title":"Analysis and Simulation of Accelerating Flames","year":2005,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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 Calgary","funders":"","keywords":"Computer science; Environmental science","score_opus":0.03119414194907131,"score_gpt":0.3037925794270687,"score_spread":0.2725984374779974,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2315204267","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":[0.78436106,0.0007855257,0.16656424,0.00059467857,0.00024543758,0.00017602333,0.00053503667,0.0013353676,0.045402713],"genre_scores_gemma":[0.97022074,0.0002046568,0.025407529,0.000039190545,0.000028588322,0.00005643627,0.00017033407,0.00014030164,0.003732377],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99984837,0.000037032012,0.0000061988835,0.000018240462,0.000048506387,0.00004161271],"domain_scores_gemma":[0.9991697,0.00044492187,0.000089846784,0.00005974165,0.0001603575,0.00007557968],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00048229037,0.00074385735,0.0008373561,0.0007934005,0.0009152182,0.0009126807,0.0012783062,0.0013177715,0.0027298203],"category_scores_gemma":[0.0021932675,0.0005140236,0.0007971271,0.00050515507,0.0008834991,0.0005648365,0.00074754946,0.000809992,0.00022538088],"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":[0.000043999193,0.000032879412,0.0005041406,0.00002473395,0.000010851117,0.0000396203,0.000028647919,0.9914938,0.001156696,0.00478057,0.00014583007,0.0017381659],"study_design_scores_gemma":[0.000009197965,0.000005758031,0.00007954586,0.0000014383318,0.0000020710947,0.000004115919,0.00000558847,0.9989685,0.00026551372,0.00052933587,0.00012674135,0.000002233714],"about_ca_topic_score_codex":0.03119425,"about_ca_topic_score_gemma":0.012607598,"teacher_disagreement_score":0.03119425,"about_ca_system_score_codex":0.0010448153,"about_ca_system_score_gemma":0.0013440396,"threshold_uncertainty_score":0.06202531},"labels":[],"label_agreement":null},{"id":"W2316681235","doi":"10.2514/6.2011-5826","title":"Exchange Inlet Design for Enhanced RBCC Rocket-Air Mixing","year":2011,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Carleton University","funders":"","keywords":"Rocket (weapon); Mixing (physics); Inlet; Aerospace engineering; Environmental science; Engineering; Physics; Mechanical engineering","score_opus":0.10506548490240569,"score_gpt":0.28007655346119414,"score_spread":0.17501106855878845,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2316681235","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":[0.72537833,0.00049698335,0.25939566,0.00009284703,0.00017045357,0.00026451083,0.00020921444,0.0016847953,0.012307168],"genre_scores_gemma":[0.9402024,0.00012780653,0.056377623,0.000030306932,0.000017305263,0.00009783374,0.0001624575,0.00008417299,0.0029000938],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997402,0.00003365152,0.000022342387,0.000053124357,0.00011268381,0.000038051374],"domain_scores_gemma":[0.9996921,0.000048202586,0.0000633271,0.000030507901,0.00013203637,0.00003387826],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003937236,0.0003509061,0.0005323115,0.0003247806,0.00031023673,0.00056445383,0.0005909914,0.0004535706,0.0013314582],"category_scores_gemma":[0.00051145826,0.00022010128,0.00021566176,0.00019489469,0.00029322715,0.00037917143,0.00056868617,0.0003129528,0.0004887876],"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":[0.0008638262,0.0003127573,0.004266508,0.0004305479,0.000021776938,0.00027779498,0.00019331893,0.050011855,0.8891396,0.0049888003,0.0008314702,0.048661735],"study_design_scores_gemma":[0.00009323901,0.00068592007,0.0045462367,0.000021823662,0.00003778199,0.0001796761,0.00005420708,0.25619262,0.7291969,0.00027892948,0.00866668,0.00004591571],"about_ca_topic_score_codex":0.00090389623,"about_ca_topic_score_gemma":0.0011237491,"teacher_disagreement_score":0.0013314582,"about_ca_system_score_codex":0.000490249,"about_ca_system_score_gemma":0.00052786496,"threshold_uncertainty_score":0.004454136},"labels":[],"label_agreement":null},{"id":"W2316737403","doi":"10.2514/6.2004-1239","title":"The Effect of the Porous Diverter Fairing on the Aerodynamic Performance of Natural Blockage Thrust Reverser","year":2004,"lang":"en","type":"article","venue":"42nd AIAA Aerospace Sciences Meeting and Exhibit","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Bombardier (Canada)","funders":"","keywords":"Aerodynamics; Porosity; Natural (archaeology); Aerospace engineering; Computer science; Geology; Engineering; Geotechnical engineering","score_opus":0.005988222590292087,"score_gpt":0.2080429914235022,"score_spread":0.2020547688332101,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2316737403","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":[0.9987031,0.000041105995,0.000653343,0.000011844874,0.000007422179,0.000001532834,0.000010545182,0.000020083773,0.00055110606],"genre_scores_gemma":[0.99959975,0.000014239627,0.00013694188,0.000003959371,0.0000015153704,6.150401e-7,0.000009464221,0.0000049850546,0.00022839465],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99982613,0.000023489949,0.000008740031,0.000023390563,0.000053132317,0.00006520694],"domain_scores_gemma":[0.9990497,0.00044908488,0.00013558428,0.000080383215,0.00016687937,0.000118419186],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00032370983,0.00019470784,0.00026297366,0.00019067731,0.0004936431,0.00053112325,0.00024161537,0.00033377734,0.0014919491],"category_scores_gemma":[0.0016056907,0.00014654596,0.00014236504,0.00010701556,0.0006622984,0.0005996464,0.00044299054,0.00026824514,0.00021697806],"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":[0.0033913099,0.00012793661,0.008179795,0.00006889772,0.00002520336,0.0003739087,0.00018582508,0.03789798,0.93184143,0.00078092277,0.00017154179,0.01695525],"study_design_scores_gemma":[0.000121440964,0.0033597148,0.05394713,0.00001784989,0.00008582594,0.00045243118,0.00038276942,0.09513437,0.84466344,0.00043195297,0.0013279355,0.0000751674],"about_ca_topic_score_codex":0.0011826025,"about_ca_topic_score_gemma":0.0010668692,"teacher_disagreement_score":0.0014919491,"about_ca_system_score_codex":0.00024217556,"about_ca_system_score_gemma":0.00026899812,"threshold_uncertainty_score":0.004991114},"labels":[],"label_agreement":null},{"id":"W2317549910","doi":"10.2514/6.2011-5081","title":"Flow-Through Radiator Development for Orion Crew Exploration Vehicle","year":2011,"lang":"en","type":"article","venue":"41st International Conference on Environmental Systems","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lockheed Martin (Canada)","funders":"","keywords":"Crew; Radiator (engine cooling); Aerospace engineering; Flow (mathematics); Marine engineering; Aerodynamics; Automotive engineering; Aeronautics; Computer science; Simulation; Engineering; Physics; Mechanics","score_opus":0.15159822831230374,"score_gpt":0.27657929629533484,"score_spread":0.1249810679830311,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2317549910","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":[0.48206192,0.0009897366,0.46376917,0.00041866564,0.0003599104,0.0012419597,0.0010198394,0.013994045,0.03614472],"genre_scores_gemma":[0.7499068,0.00072509533,0.18438737,0.00015443581,0.000053137912,0.00044018566,0.0017153758,0.0018462081,0.0607714],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9994831,0.000061635925,0.00001831952,0.000070995375,0.00027766565,0.00008831381],"domain_scores_gemma":[0.9993523,0.00006748734,0.000053788466,0.000074943084,0.00038503145,0.00006644016],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0015091067,0.00056013954,0.00044340314,0.0006277798,0.0005585454,0.0008713366,0.0013087378,0.00071614364,0.008233099],"category_scores_gemma":[0.0008878168,0.00040871077,0.00066090334,0.00023455142,0.0002875696,0.0011229524,0.00065980636,0.0006119886,0.0024198396],"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":[0.0011488573,0.00061395305,0.0070629427,0.0004418536,0.00009222461,0.00038715758,0.00085696985,0.023429286,0.7042775,0.004615321,0.008864079,0.24820988],"study_design_scores_gemma":[0.00025237023,0.004055514,0.007977556,0.00008874181,0.00014303003,0.00043270324,0.00024210909,0.051858693,0.8244446,0.00044008569,0.10995782,0.00010686191],"about_ca_topic_score_codex":0.0025480848,"about_ca_topic_score_gemma":0.0028073096,"teacher_disagreement_score":0.008233099,"about_ca_system_score_codex":0.0006487735,"about_ca_system_score_gemma":0.0014813337,"threshold_uncertainty_score":0.027542472},"labels":[],"label_agreement":null},{"id":"W2317698440","doi":"10.2514/6.2007-5804","title":"Particles for Instability Symptom Suppression in Solid Rocket Motor","year":2007,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Solid-fuel rocket; Instability; Rocket (weapon); Control theory (sociology); Aerospace engineering; Materials science; Computer science; Physics; Mechanics; Engineering; Propellant; Control (management); Artificial intelligence","score_opus":0.028139937797312768,"score_gpt":0.31738287017689215,"score_spread":0.2892429323795794,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2317698440","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":[0.9271367,0.0016007014,0.04852993,0.00051997975,0.00014678478,0.00013749523,0.00008156677,0.0009789792,0.020867912],"genre_scores_gemma":[0.99441963,0.00009139362,0.0034868214,0.000052929492,0.0000119823135,0.000013898428,0.00004260514,0.000047908004,0.0018328675],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999094,0.000018332297,0.000004190512,0.000014503853,0.000032848868,0.000020648426],"domain_scores_gemma":[0.9996395,0.00012661087,0.000052576004,0.000035839086,0.00008940163,0.000056145796],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024851333,0.00025408517,0.0005149762,0.0003906212,0.0007276779,0.00081480946,0.00044959973,0.0008045232,0.0033382457],"category_scores_gemma":[0.0007637732,0.000174753,0.00022887388,0.00019269453,0.00041084367,0.00044287046,0.0005835902,0.00038218222,0.00056004524],"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":[0.005668819,0.0004162166,0.006226989,0.0003920958,0.00009845722,0.0013901115,0.00041543177,0.02271327,0.89086485,0.0155897355,0.0032149968,0.05300904],"study_design_scores_gemma":[0.0008175224,0.002141687,0.010216847,0.000053348514,0.00018002995,0.0010313967,0.0003875212,0.3595809,0.6071318,0.009763195,0.0086193755,0.00007639679],"about_ca_topic_score_codex":0.0003453398,"about_ca_topic_score_gemma":0.00038533576,"teacher_disagreement_score":0.0033382457,"about_ca_system_score_codex":0.00021736693,"about_ca_system_score_gemma":0.0002381052,"threshold_uncertainty_score":0.011167526},"labels":[],"label_agreement":null},{"id":"W2319174719","doi":"10.2514/6.2014-3750","title":"Regression Rate Estimation for Swirling-Flow Hybrid Rocket Engines","year":2014,"lang":"en","type":"article","venue":"50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference","topic":"Rocket and propulsion systems research","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":"Toronto Metropolitan University","funders":"","keywords":"Propellant; Mechanics; Mass flow rate; Convection; Rocket (weapon); Flow (mathematics); Heat transfer; Materials science; Volumetric flow rate; Aerospace engineering; Engineering; Physics","score_opus":0.03971017493319882,"score_gpt":0.2760688725277044,"score_spread":0.2363586975945056,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2319174719","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":[0.35258755,0.00034531215,0.64507794,0.000024072498,0.000011380383,0.00004348905,0.00009411606,0.000684624,0.001131435],"genre_scores_gemma":[0.97641057,0.00013127991,0.022434948,0.0000048998086,0.000004180275,0.000020724405,0.00007479768,0.00003800846,0.0008805697],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99983525,0.000035055426,0.000009498962,0.000043779397,0.000058135392,0.000018171399],"domain_scores_gemma":[0.9995819,0.00020928416,0.00009165297,0.000023382061,0.000084869,0.000008929904],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00063804904,0.0005533284,0.00057463197,0.0005650096,0.00013511717,0.00048276622,0.000726804,0.00038679835,0.0004183514],"category_scores_gemma":[0.0011728548,0.00026895246,0.0004039191,0.00031468028,0.00019475017,0.00063623907,0.00031798804,0.00031701033,0.00021856984],"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":[0.00018206718,0.000044152926,0.004245423,0.00006808553,0.000031573272,0.00007917682,0.000034510053,0.9121754,0.04213033,0.00063282467,0.000092282375,0.040284075],"study_design_scores_gemma":[0.0000016546392,0.000016673059,0.00045463804,0.0000013511263,0.000002226471,0.000008662358,0.0000033414399,0.99278706,0.00659139,0.00007033551,0.000057746223,0.0000049525333],"about_ca_topic_score_codex":0.0035076544,"about_ca_topic_score_gemma":0.0021173297,"teacher_disagreement_score":0.0035076544,"about_ca_system_score_codex":0.00040001044,"about_ca_system_score_gemma":0.00024710986,"threshold_uncertainty_score":0.0069744587},"labels":[],"label_agreement":null},{"id":"W2319445259","doi":"10.2514/6.2007-5346","title":"Model for Predicting Fuel Regression Rate in Hybrid Rocket Engines","year":2007,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":9,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Rocket (weapon); Rocket engine; Regression analysis; Regression; Environmental science; Computer science; Automotive engineering; Aeronautics; Aerospace engineering; Engineering; Statistics; Machine learning; Mathematics","score_opus":0.0421246733230068,"score_gpt":0.3034314178560043,"score_spread":0.2613067445329975,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2319445259","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":[0.6439679,0.0007422203,0.34912714,0.00019687852,0.00011774284,0.0000739553,0.0007125903,0.0017558757,0.0033056235],"genre_scores_gemma":[0.9879794,0.00017215403,0.008500469,0.0000239776,0.000016247946,0.000058557103,0.00033606478,0.00004490808,0.002868193],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99988055,0.000023413775,0.000008387374,0.00003652891,0.000029555898,0.000021557833],"domain_scores_gemma":[0.9994375,0.00035771742,0.00004547073,0.000023983885,0.00011716698,0.000018087783],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00063108496,0.0007470719,0.0009007835,0.00051038247,0.00041931,0.00080611627,0.0009709691,0.00092569616,0.001335299],"category_scores_gemma":[0.0011654766,0.0003680405,0.00055096357,0.0003590877,0.00023724341,0.0006561152,0.0003909231,0.00076695834,0.00048829167],"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":[0.00016049412,0.0000580313,0.0021982056,0.000024044944,0.000043980337,0.000023984503,0.000012632813,0.98115784,0.0022709754,0.0003565128,0.00021910707,0.013474256],"study_design_scores_gemma":[0.0000028542886,0.000013246076,0.00023368187,7.1468975e-7,0.0000046173577,0.0000023598384,0.0000013074517,0.99925214,0.00038186772,0.000076149685,0.000028898283,0.0000021380342],"about_ca_topic_score_codex":0.016757866,"about_ca_topic_score_gemma":0.009780813,"teacher_disagreement_score":0.016757866,"about_ca_system_score_codex":0.00062008447,"about_ca_system_score_gemma":0.0005292025,"threshold_uncertainty_score":0.033320665},"labels":[],"label_agreement":null},{"id":"W2320191070","doi":"10.2514/6.2011-2013","title":"Investigation of Shortfalls in Hypersonic Vehicle Structure Combined Environment Analysis Capability","year":2011,"lang":"en","type":"article","venue":"52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":13,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lockheed Martin (Canada)","funders":"","keywords":"Aeronautics; Computer science; Hypersonic speed; Aerospace engineering; Systems engineering; Engineering","score_opus":0.02296570043682811,"score_gpt":0.21439422443923156,"score_spread":0.19142852400240346,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2320191070","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":[0.89807034,0.011394621,0.022455605,0.0014172831,0.00006289841,0.000101551195,0.00036644196,0.00014857837,0.06598258],"genre_scores_gemma":[0.967194,0.0058694724,0.017511781,0.000116216106,0.000022939283,0.000056344405,0.0004130365,0.00003671859,0.008779533],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9990427,0.00022473783,0.000055497963,0.00008542672,0.00053095515,0.00006073743],"domain_scores_gemma":[0.9962387,0.0015429507,0.0004603047,0.00019842369,0.0014321182,0.00012743616],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0021201607,0.00011901224,0.000098884564,0.0014175214,0.00033158512,0.001213032,0.0005020478,0.00027142672,0.0015216765],"category_scores_gemma":[0.004226668,0.0000922885,0.0001384904,0.0014294377,0.0003613149,0.0018945327,0.0005106411,0.00034676696,0.00019042149],"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":[0.0003945095,0.0001960929,0.08588547,0.00078784034,0.000048407233,0.0005160364,0.0026166472,0.018161684,0.021558296,0.028745698,0.0030223394,0.838067],"study_design_scores_gemma":[0.000053311593,0.0068335645,0.4773023,0.0014110239,0.00022602145,0.0034804908,0.018313203,0.09900902,0.08604574,0.030104183,0.27707842,0.0001427796],"about_ca_topic_score_codex":0.0037990871,"about_ca_topic_score_gemma":0.00956888,"teacher_disagreement_score":0.0037990871,"about_ca_system_score_codex":0.0009691022,"about_ca_system_score_gemma":0.0014666135,"threshold_uncertainty_score":0.011212647},"labels":[],"label_agreement":null},{"id":"W2320754164","doi":"10.2514/6.2002-5172","title":"Towards an Integrated Design Environment for Hypersonic Vehicle Design and Synthesis","year":2002,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":13,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lockheed Martin (Canada)","funders":"","keywords":"Computer science; Systems engineering; Aerospace engineering; Human–computer interaction; Automotive engineering; Engineering","score_opus":0.08114648332271873,"score_gpt":0.24772138760774778,"score_spread":0.16657490428502905,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2320754164","genre_codex":"methods","genre_gemma":"methods","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0011520504,0.00007912315,0.99325716,0.000070403315,0.000029723036,0.00007159909,0.000086858425,0.00304949,0.002203558],"genre_scores_gemma":[0.013915558,0.00033918628,0.9793743,0.000090151916,0.000033508262,0.00042475425,0.0008185986,0.0016489902,0.003354857],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99618715,0.000851132,0.0002996902,0.0003415139,0.0020542203,0.00026629184],"domain_scores_gemma":[0.9970193,0.0008675732,0.0002329481,0.0005919925,0.0011289881,0.00015926927],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0062340917,0.0020088828,0.001513749,0.0015608149,0.00080022577,0.0038034513,0.003906788,0.0016710972,0.0076665706],"category_scores_gemma":[0.0055024647,0.0017985788,0.0026395116,0.0010164692,0.0011599731,0.0034461236,0.0032992424,0.0039892513,0.0038812694],"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":[0.00026170662,0.00038221138,0.0015919227,0.00064721296,0.0001562363,0.00032143525,0.0011937774,0.49752694,0.022989409,0.18647529,0.015249846,0.27320397],"study_design_scores_gemma":[0.00016094703,0.000208107,0.0003109776,0.00025252323,0.00008312598,0.0001874776,0.00012777829,0.77460676,0.016957648,0.053779442,0.15323831,0.00008687162],"about_ca_topic_score_codex":0.002769984,"about_ca_topic_score_gemma":0.0033135107,"teacher_disagreement_score":0.0076665706,"about_ca_system_score_codex":0.0015040705,"about_ca_system_score_gemma":0.003270933,"threshold_uncertainty_score":0.032969415},"labels":[],"label_agreement":null},{"id":"W2321064709","doi":"10.2514/6.2013-4081","title":"Uniform Particle Regression and Solid Rocket Combustion Instability Suppression","year":2013,"lang":"en","type":"article","venue":"49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Solid-fuel rocket; Propellant; Mechanics; Combustion; Rocket (weapon); Particle (ecology); Materials science; Instability; Particle size; Computer simulation; Physics; Aerospace engineering; Engineering; Chemistry; Geology","score_opus":0.043733479288001996,"score_gpt":0.27707606161961856,"score_spread":0.23334258233161656,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2321064709","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":[0.9182166,0.000116733165,0.07966928,0.000019162171,0.0000064841583,0.00001914807,0.000024004628,0.00022204156,0.0017065863],"genre_scores_gemma":[0.99606186,0.000022103597,0.0035729532,0.0000026119235,6.5192813e-7,0.0000046859745,0.000019425808,0.000012347546,0.00030335854],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998492,0.000019348881,0.000008189919,0.000028399112,0.000072288014,0.000022621738],"domain_scores_gemma":[0.9996251,0.00013700179,0.00012866911,0.000029452242,0.00006622143,0.000013518391],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00022174555,0.00023088416,0.00019128807,0.00026736857,0.00011966907,0.0002979329,0.0003105818,0.00019441807,0.00061125174],"category_scores_gemma":[0.0011823671,0.00009861403,0.00023999235,0.00016182516,0.0002533056,0.0003645282,0.00027426006,0.00021360163,0.00011286806],"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":[0.0003636271,0.000097665084,0.01755885,0.00010858182,0.00003247665,0.00032846618,0.00013369518,0.64082605,0.2986603,0.0033447922,0.00014056907,0.038404897],"study_design_scores_gemma":[0.000010310794,0.00022389476,0.0059897895,0.0000028683835,0.000008304218,0.000070042486,0.000026720405,0.88597095,0.10707867,0.00034558662,0.0002623095,0.0000105442205],"about_ca_topic_score_codex":0.0016258314,"about_ca_topic_score_gemma":0.0011822691,"teacher_disagreement_score":0.0016258314,"about_ca_system_score_codex":0.00023300386,"about_ca_system_score_gemma":0.00019826925,"threshold_uncertainty_score":0.0032327175},"labels":[],"label_agreement":null},{"id":"W2321209703","doi":"10.2514/6.2001-2413","title":"Investigation of propeller effects on the Aurora aircraft","year":2001,"lang":"en","type":"article","venue":"19th AIAA Applied Aerodynamics Conference","topic":"Rocket and propulsion systems research","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":"National Research Council Canada","funders":"","keywords":"Propeller; Aeronautics; Marine engineering; Environmental science; Aerospace engineering; Computer science; Engineering","score_opus":0.02745828041632807,"score_gpt":0.22050277156046694,"score_spread":0.19304449114413885,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2321209703","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":[0.97182894,0.00044591114,0.0014974655,0.00016209547,0.00020789624,0.00006664005,0.00034784045,0.00017259647,0.02527054],"genre_scores_gemma":[0.9810188,0.00021505106,0.00055766065,0.000043166154,0.000037625494,0.000007858952,0.00030631185,0.00007148302,0.017742096],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9995766,0.000045407887,0.000010262668,0.00003941819,0.00025689183,0.000071376235],"domain_scores_gemma":[0.9982412,0.00047874002,0.00010817693,0.00010425779,0.00097596855,0.00009172936],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003209766,0.00019279157,0.0003138264,0.00059293734,0.0008460205,0.00046338784,0.00037957466,0.00050489296,0.015357819],"category_scores_gemma":[0.0017629947,0.00013503552,0.00023323212,0.00031062294,0.00018777236,0.0003684203,0.0002875186,0.00024154603,0.0025594158],"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":[0.0073327944,0.00036108305,0.049957484,0.0007755688,0.00010902522,0.0046098935,0.00067631574,0.008433482,0.7771341,0.0010105273,0.012182579,0.1374171],"study_design_scores_gemma":[0.00020808457,0.0046792026,0.29321167,0.000059265818,0.00022039347,0.0014750095,0.0013047599,0.022696292,0.6378581,0.00021665878,0.03798189,0.0000886418],"about_ca_topic_score_codex":0.0029915045,"about_ca_topic_score_gemma":0.00410602,"teacher_disagreement_score":0.015357819,"about_ca_system_score_codex":0.00022201528,"about_ca_system_score_gemma":0.00030484164,"threshold_uncertainty_score":0.051377058},"labels":[],"label_agreement":null},{"id":"W2322614412","doi":"10.2514/6.2003-4505","title":"Internal Ballistic Modeling of a Star-Grain Solid Rocket Motor","year":2003,"lang":"en","type":"article","venue":"39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Solid-fuel rocket; Aerospace engineering; Star (game theory); Materials science; Environmental science; Propellant; Physics; Engineering; Astrophysics","score_opus":0.046002772772064264,"score_gpt":0.2717898623647655,"score_spread":0.22578708959270122,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2322614412","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":[0.56400436,0.00045994925,0.28352746,0.0005204884,0.00012954042,0.0001890808,0.0005611228,0.0010253415,0.14958261],"genre_scores_gemma":[0.9835781,0.000118566124,0.003148087,0.000023793622,0.0000069532625,0.000036109177,0.000090671434,0.000061760176,0.012935992],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99988914,0.000017153883,0.0000048382303,0.000018260005,0.00004225257,0.000028355376],"domain_scores_gemma":[0.9998331,0.00003758843,0.000033039796,0.000023968862,0.000040742365,0.000031504973],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00022275804,0.00036415327,0.0009044123,0.00046070386,0.0007271747,0.00097602484,0.0014173021,0.001650923,0.006077937],"category_scores_gemma":[0.0004781279,0.00047386697,0.0005969361,0.0003765984,0.00094564655,0.0008469207,0.00072116137,0.00043001754,0.0010773871],"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":[0.000062075356,0.000015805525,0.00032489354,0.000024681676,0.0000108184295,0.00013177734,0.000042825275,0.99144804,0.0020999871,0.00408418,0.00021239035,0.0015425109],"study_design_scores_gemma":[0.000005188749,0.000017758226,0.00014882458,0.0000018318849,0.0000026500045,0.000009640232,0.000012636475,0.9989153,0.00022022384,0.00029569736,0.000367494,0.0000028490765],"about_ca_topic_score_codex":0.015602626,"about_ca_topic_score_gemma":0.008700924,"teacher_disagreement_score":0.015602626,"about_ca_system_score_codex":0.0008484506,"about_ca_system_score_gemma":0.0011981814,"threshold_uncertainty_score":0.031023622},"labels":[],"label_agreement":null},{"id":"W2322676430","doi":"10.2514/6.2014-3493","title":"Use of Reactive Particles for Solid Rocket Combustion Instability Suppression","year":2014,"lang":"en","type":"article","venue":"50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference","topic":"Rocket and propulsion systems research","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":"Toronto Metropolitan University","funders":"","keywords":"Combustion; Solid-fuel rocket; Rocket (weapon); Instability; Aerospace engineering; Materials science; Environmental science; Nuclear engineering; Mechanics; Propellant; Physics; Engineering; Chemistry","score_opus":0.10168945000457344,"score_gpt":0.30286757985781276,"score_spread":0.20117812985323932,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2322676430","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":[0.9407846,0.000175791,0.056555413,0.00002346246,0.000014058177,0.000040652583,0.000033347136,0.00024604972,0.0021266798],"genre_scores_gemma":[0.9879046,0.00004500161,0.011714098,0.0000037417371,9.769043e-7,0.000007952329,0.00002433626,0.00001330023,0.00028609636],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99982446,0.00002240331,0.000011521957,0.000025311625,0.000098283854,0.000017929415],"domain_scores_gemma":[0.9997167,0.00009147024,0.00007653047,0.00003974057,0.000059894985,0.0000156085],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00029731006,0.0003321977,0.00024151655,0.00026724447,0.00015679581,0.00044294182,0.00046139775,0.00020537531,0.00043757583],"category_scores_gemma":[0.00074872223,0.00013735962,0.00023571607,0.00013373895,0.00026013263,0.0002470632,0.00023176309,0.00019859885,0.0001224084],"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":[0.000492787,0.00014948336,0.0058889464,0.00018940488,0.00003334648,0.0001914702,0.00012563281,0.19884013,0.7536523,0.0016913912,0.00011087365,0.03863423],"study_design_scores_gemma":[0.000033214063,0.0007810805,0.0026900365,0.0000068698023,0.000035233697,0.00006731717,0.00004189,0.43597034,0.55896217,0.00021241225,0.0011795,0.000019896486],"about_ca_topic_score_codex":0.0011210382,"about_ca_topic_score_gemma":0.0015007814,"teacher_disagreement_score":0.0011210382,"about_ca_system_score_codex":0.0002036989,"about_ca_system_score_gemma":0.00025041634,"threshold_uncertainty_score":0.002229035},"labels":[],"label_agreement":null},{"id":"W2322901639","doi":"10.1115/gt2002-30547","title":"Preliminary Design of Ceramic Components for the ST5+ Advanced Microturbine Engine","year":2002,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"Pratt and Whitney Canada; U.S. Department of Energy","keywords":"Ceramic; Rotor (electric); Silicon nitride; Turbine; Mechanical engineering; Aerodynamics; Materials science; Silicon; Stress (linguistics); Engineering; Automotive engineering; Structural engineering; Computer science; Aerospace engineering; Composite material; Optoelectronics","score_opus":0.059527321067337054,"score_gpt":0.2592307269537218,"score_spread":0.19970340588638474,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2322901639","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":[0.66871405,0.002112558,0.29271087,0.0002895998,0.00036626132,0.0008922897,0.00077644293,0.0015769621,0.032560885],"genre_scores_gemma":[0.8775475,0.0007133522,0.1027484,0.000056909772,0.000041164814,0.00023272044,0.00080709293,0.000114321534,0.017738616],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997509,0.000010413061,0.000012347468,0.000026710113,0.00016686882,0.000032707943],"domain_scores_gemma":[0.9997967,0.000015838625,0.000024258821,0.000010895231,0.00012967964,0.000022630065],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00028274886,0.0003589196,0.00023224244,0.00028612916,0.00030770054,0.00035961528,0.00077363255,0.00035301936,0.0018325783],"category_scores_gemma":[0.00031496992,0.00023542295,0.00037072873,0.0002185686,0.0001789155,0.0002595284,0.0002161181,0.0002694843,0.00057076814],"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":[0.00087122136,0.00012601736,0.0035380635,0.0009739794,0.00005484434,0.00069056556,0.00028352893,0.049431093,0.80835,0.0086382255,0.0056930413,0.12134936],"study_design_scores_gemma":[0.00029590962,0.007069874,0.031624474,0.00014337215,0.0002373233,0.0021078915,0.00030085802,0.16576266,0.60413975,0.0012909994,0.18686746,0.00015942982],"about_ca_topic_score_codex":0.0022097025,"about_ca_topic_score_gemma":0.0064175557,"teacher_disagreement_score":0.0022097025,"about_ca_system_score_codex":0.00058611284,"about_ca_system_score_gemma":0.00096006563,"threshold_uncertainty_score":0.006130576},"labels":[],"label_agreement":null},{"id":"W2323181827","doi":"10.2514/6.2012-5846","title":"Thermal Protection Systems : Heritage - Development Status - Perspectives","year":2012,"lang":"en","type":"article","venue":"18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Safran Electronics (Canada)","funders":"","keywords":"Computer science","score_opus":0.0334334976744953,"score_gpt":0.23660588138740024,"score_spread":0.20317238371290494,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2323181827","genre_codex":"review","genre_gemma":"review","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"review","genre_consensus":"review","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.018068545,0.6744711,0.017082669,0.029004183,0.002686442,0.000072951065,0.0009427223,0.0004286129,0.25724283],"genre_scores_gemma":[0.2695586,0.64650214,0.019522596,0.0039026523,0.0020761974,0.0000970458,0.0024099797,0.00022265628,0.055708203],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9992285,0.00013721737,0.000041198593,0.00010872328,0.00030088707,0.0001835137],"domain_scores_gemma":[0.9982413,0.000308188,0.00012764215,0.00011701391,0.0008430881,0.00036271158],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0025442299,0.00077916554,0.00029555982,0.0012205783,0.0005051748,0.0047913454,0.00095402525,0.0015387726,0.018828204],"category_scores_gemma":[0.0012822163,0.00020039792,0.00032956622,0.0015483319,0.0010135329,0.005494171,0.0017802708,0.0017678636,0.005121491],"study_design_candidate":"not_applicable","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":[0.0002538133,0.0002260196,0.0037133195,0.0027957659,0.000030387688,0.0003161669,0.0003906965,0.0016787542,0.005752037,0.13471782,0.046103545,0.80402166],"study_design_scores_gemma":[0.0000122846295,0.00033315964,0.0025116669,0.0012827085,0.000017984008,0.000632843,0.000774902,0.00103152,0.0035991934,0.011686164,0.97809505,0.000022556676],"about_ca_topic_score_codex":0.0022285127,"about_ca_topic_score_gemma":0.0020776025,"teacher_disagreement_score":0.018828204,"about_ca_system_score_codex":0.0016373611,"about_ca_system_score_gemma":0.0034715862,"threshold_uncertainty_score":0.06298667},"labels":[],"label_agreement":null},{"id":"W2323267664","doi":"10.2514/6.2005-5334","title":"Parallel AMR Scheme for Turbulent Multi-Phase Rocket Motor Core Flows","year":2005,"lang":"en","type":"article","venue":"17th AIAA Computational Fluid Dynamics Conference","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":11,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto","funders":"Natural Sciences and Engineering Research Council of Canada; Ontario Innovation Trust","keywords":"Turbulence; Computer science; Core (optical fiber); Scheme (mathematics); Solid-fuel rocket; Aerospace engineering; Phase (matter); Mechanics; Physics; Mathematics; Engineering; Telecommunications","score_opus":0.05686046542384807,"score_gpt":0.32367888593189653,"score_spread":0.2668184205080485,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2323267664","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":[0.02141136,0.0002596457,0.9668687,0.00009322861,0.000093759845,0.00017291614,0.00013973934,0.0016159882,0.009344711],"genre_scores_gemma":[0.2706831,0.00032686468,0.7164513,0.00007325968,0.000048287315,0.00062618894,0.00056776166,0.00037126147,0.010851868],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99977964,0.000048724054,0.000012448906,0.000022681103,0.000111374124,0.000025272791],"domain_scores_gemma":[0.9997975,0.000045145094,0.000024137295,0.00004291459,0.000073916985,0.000016314116],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00041025382,0.0004088857,0.0007617268,0.00032015663,0.0004525986,0.0004424114,0.0011468984,0.0004896811,0.0034640129],"category_scores_gemma":[0.0006089508,0.0001782249,0.0004685558,0.0003297023,0.00026696792,0.0004738945,0.0007247346,0.00068681093,0.0009964553],"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":[0.00020888736,0.00010946726,0.0010026536,0.00026404756,0.000032683613,0.00023739555,0.0001691215,0.69276005,0.050270446,0.05690669,0.005051788,0.19298683],"study_design_scores_gemma":[0.000023616618,0.00003184872,0.0001255136,0.0000075641556,0.0000033369386,0.000036070607,0.000006441344,0.98829854,0.0024652688,0.0021635627,0.006830268,0.000007822972],"about_ca_topic_score_codex":0.0030070907,"about_ca_topic_score_gemma":0.0020173667,"teacher_disagreement_score":0.0034640129,"about_ca_system_score_codex":0.00054402294,"about_ca_system_score_gemma":0.000836137,"threshold_uncertainty_score":0.011588275},"labels":[],"label_agreement":null},{"id":"W2324381607","doi":"10.2514/6.2014-3479","title":"The VINCI Engine Vibration Test campaign","year":2014,"lang":"en","type":"article","venue":"50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference","topic":"Rocket and propulsion systems research","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":"Safran Electronics (Canada)","funders":"","keywords":"Test (biology); Vibration; Automotive engineering; Computer science; Engineering; Aeronautics; Acoustics; Physics; Geology","score_opus":0.02530980728248964,"score_gpt":0.2383671288747165,"score_spread":0.21305732159222687,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2324381607","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":[0.9207589,0.00078803545,0.022318093,0.00019958746,0.00027323124,0.0006462134,0.0061788023,0.0016166408,0.0472205],"genre_scores_gemma":[0.96192294,0.0002690336,0.007955296,0.00014802783,0.000044936663,0.00024988526,0.00738985,0.00022200005,0.021797989],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99928963,0.00004451951,0.00002344866,0.00015768358,0.000380153,0.00010458689],"domain_scores_gemma":[0.99970764,0.000037910573,0.000020763973,0.000049112972,0.00014364244,0.000040929976],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00083130837,0.00052490074,0.0004717984,0.000677485,0.0006594826,0.00040420104,0.0005942975,0.00066169177,0.0036307562],"category_scores_gemma":[0.00043706354,0.00018424883,0.00022510643,0.00037185167,0.00025887226,0.00031095746,0.0006535387,0.00058029743,0.0016095487],"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":[0.0026957318,0.0009892979,0.020040033,0.00060685235,0.000103866005,0.0006567755,0.0006624126,0.013251398,0.8203411,0.0030968646,0.016666004,0.120889604],"study_design_scores_gemma":[0.0003702533,0.014708912,0.18508753,0.0000947988,0.00010163814,0.0009146278,0.00044060973,0.018190319,0.6967512,0.00058288366,0.08257375,0.00018356508],"about_ca_topic_score_codex":0.0017331947,"about_ca_topic_score_gemma":0.0033351884,"teacher_disagreement_score":0.0036307562,"about_ca_system_score_codex":0.00047428362,"about_ca_system_score_gemma":0.00041424565,"threshold_uncertainty_score":0.012146115},"labels":[],"label_agreement":null},{"id":"W2325306875","doi":"10.2514/6.2016-0297","title":"An Optimization Approach to Split-Winglet Design for Sailplanes","year":2016,"lang":"en","type":"article","venue":"54th AIAA Aerospace Sciences Meeting","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Wingtip device; Computer science; Engineering; Aerospace engineering; Aerodynamics","score_opus":0.05894989296216036,"score_gpt":0.29490432844155984,"score_spread":0.23595443547939948,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2325306875","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":[0.01858047,0.0002907584,0.97249156,0.00013139198,0.000041319217,0.00007165295,0.00006334172,0.00013523782,0.008194347],"genre_scores_gemma":[0.48342773,0.00073221297,0.50347555,0.00018408736,0.00009719841,0.0004631274,0.00026771505,0.00033337093,0.011018932],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998184,0.00006400459,0.000006231106,0.000018991233,0.00006619799,0.000026284422],"domain_scores_gemma":[0.9997422,0.00011895644,0.000022926208,0.000013849255,0.000084524356,0.000017589235],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006579383,0.0010142191,0.0011670609,0.0008146608,0.00048338066,0.0009658695,0.0008935895,0.000985857,0.005185441],"category_scores_gemma":[0.0011001334,0.00080733164,0.000772909,0.0005302515,0.0005184322,0.00061641407,0.0008391164,0.0009332458,0.0006447306],"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":[0.000035942212,0.00002807438,0.00015363355,0.000044939334,0.000014865636,0.00002218599,0.000020216743,0.9791189,0.0014263099,0.0041234214,0.0003964323,0.014615118],"study_design_scores_gemma":[0.00000616285,0.000018779496,0.000036374255,0.0000049132464,0.0000032975563,0.0000041771336,0.0000068856743,0.99788123,0.0002139598,0.0013801083,0.0004420056,0.0000019690535],"about_ca_topic_score_codex":0.0030248251,"about_ca_topic_score_gemma":0.0034094367,"teacher_disagreement_score":0.005185441,"about_ca_system_score_codex":0.0005101587,"about_ca_system_score_gemma":0.0009512768,"threshold_uncertainty_score":0.017347097},"labels":[],"label_agreement":null},{"id":"W2326562650","doi":"10.2514/6.2003-5199","title":"Hybrid Sounding Rocket(HYSR)Program","year":2003,"lang":"en","type":"article","venue":"39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lockheed Martin (Canada)","funders":"National Aeronautics and Space Administration","keywords":"Sounding rocket; Rocket (weapon); Depth sounding; Computer science; Aerospace engineering; Aeronautics; Astrobiology; Remote sensing; Geology; Engineering; Physics","score_opus":0.04366670297480852,"score_gpt":0.27295509113369787,"score_spread":0.22928838815888936,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2326562650","genre_codex":"other","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":[0.047441743,0.00073646195,0.2069289,0.0026731442,0.0018960611,0.0008849747,0.011371588,0.032001473,0.6960657],"genre_scores_gemma":[0.17788479,0.00046971033,0.09531583,0.0007644673,0.00060557557,0.0008265636,0.019204162,0.0029848507,0.701944],"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99923587,0.000074823736,0.000010876365,0.000116628784,0.00042934663,0.0001325714],"domain_scores_gemma":[0.9991351,0.000095512485,0.000032998632,0.00014677888,0.0003653645,0.00022422467],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0013216214,0.00073920796,0.0005444361,0.000940398,0.0008600472,0.0010318294,0.0014085606,0.0008227877,0.17431727],"category_scores_gemma":[0.00088592264,0.00021205917,0.000306312,0.0005204488,0.00040051696,0.00095468166,0.0018983969,0.0009961677,0.036516678],"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":[0.0023136698,0.000670549,0.0030262459,0.00023913916,0.00005924932,0.00023933627,0.00025355196,0.0053903665,0.079960056,0.044352062,0.31285688,0.5506389],"study_design_scores_gemma":[0.0006773041,0.0015993648,0.00380174,0.00003965376,0.000060362967,0.00034466427,0.00014544152,0.038746264,0.06231432,0.004787885,0.887423,0.00005996294],"about_ca_topic_score_codex":0.0020249083,"about_ca_topic_score_gemma":0.004051314,"teacher_disagreement_score":0.17431727,"about_ca_system_score_codex":0.0006401043,"about_ca_system_score_gemma":0.0017163352,"threshold_uncertainty_score":0.5831494},"labels":[],"label_agreement":null},{"id":"W2327315414","doi":"10.2514/6.2011-6054","title":"EVALUATION METHOD OF THRUST OSCILLATIONS IN LARGE SRM - APPLICATION TO SEGMENTED SRM's","year":2011,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Safran Electronics (Canada)","funders":"Office National d'études et de Recherches Aérospatiales; Centre National d’Etudes Spatiales","keywords":"Thrust; Computer science; Control theory (sociology); Aerospace engineering; Control engineering; Engineering; Artificial intelligence; Control (management)","score_opus":0.07706405874335527,"score_gpt":0.3671802428570501,"score_spread":0.29011618411369483,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2327315414","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":[0.30179387,0.00029177242,0.6910609,0.000054752712,0.000046136887,0.00029957952,0.00024162396,0.0012798198,0.004931576],"genre_scores_gemma":[0.80771065,0.0001529388,0.1889923,0.0000145559425,0.00001262555,0.00019483439,0.00029980263,0.00012737048,0.0024949373],"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99936575,0.00009820251,0.000044457305,0.00011380506,0.00032302339,0.000054833614],"domain_scores_gemma":[0.9982667,0.0006467169,0.00026439238,0.00009903968,0.0006480885,0.00007503901],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0009853833,0.00057486753,0.0005214474,0.0017226862,0.00025631953,0.0009525429,0.00061132346,0.00048783945,0.0033826241],"category_scores_gemma":[0.0037487599,0.00020940536,0.00034338806,0.0009802595,0.00039629024,0.00055709656,0.00052244985,0.00027608895,0.00047836473],"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":[0.00096661266,0.0002604701,0.020422362,0.0011451213,0.000093987415,0.0008293755,0.001213666,0.19645579,0.22168007,0.006838794,0.0013729181,0.5487208],"study_design_scores_gemma":[0.000015046599,0.00046311424,0.016012335,0.000040330622,0.000024314071,0.00022012835,0.0003330056,0.9459806,0.033894643,0.0007374251,0.0022505773,0.000028422477],"about_ca_topic_score_codex":0.0015990615,"about_ca_topic_score_gemma":0.0009788405,"teacher_disagreement_score":0.0033826241,"about_ca_system_score_codex":0.00044399482,"about_ca_system_score_gemma":0.00041252136,"threshold_uncertainty_score":0.011316001},"labels":[],"label_agreement":null},{"id":"W2329314494","doi":"10.2514/6.2013-4007","title":"Influence of Initial Propellant Temperature on Solid Rocket Internal Ballistics","year":2013,"lang":"en","type":"article","venue":"49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference","topic":"Rocket and propulsion systems research","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":"Toronto Metropolitan University","funders":"","keywords":"Propellant; Internal ballistics; Ballistics; Rocket (weapon); Solid-fuel rocket; Aerospace engineering; Rocket propellant; Materials science; Aeronautics; Engineering; Projectile","score_opus":0.03215441650733007,"score_gpt":0.29335126819048696,"score_spread":0.26119685168315687,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2329314494","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":[0.9882222,0.00019142535,0.006956688,0.000023548091,0.000016931303,0.000017090446,0.00010477796,0.00017983966,0.0042874897],"genre_scores_gemma":[0.9983444,0.000072751645,0.0005159936,0.0000035878047,0.0000010953243,0.000003119955,0.00005834391,0.000028895995,0.0009718798],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998161,0.000019174235,0.0000089363075,0.000033792305,0.000069063426,0.00005293908],"domain_scores_gemma":[0.9994404,0.0002865915,0.000059151767,0.000044510136,0.00013904108,0.000030393598],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024799732,0.0003366595,0.00032455623,0.00028075007,0.00023953174,0.00057314854,0.00030588038,0.00023003534,0.0025154755],"category_scores_gemma":[0.0014187888,0.00020267848,0.00030066565,0.00012176404,0.00030707923,0.00043478963,0.00025173198,0.00030449047,0.0008826261],"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":[0.0030284259,0.00020070914,0.017215272,0.00046227177,0.000048073816,0.0008789339,0.00036894836,0.28008753,0.65067583,0.00091938546,0.00029517725,0.045819346],"study_design_scores_gemma":[0.00003269656,0.001188165,0.019847527,0.000039872906,0.00003416468,0.00018761208,0.00017628558,0.1819532,0.79530936,0.00017023533,0.0010161902,0.000044727785],"about_ca_topic_score_codex":0.002795751,"about_ca_topic_score_gemma":0.001720738,"teacher_disagreement_score":0.002795751,"about_ca_system_score_codex":0.0003528969,"about_ca_system_score_gemma":0.00029074016,"threshold_uncertainty_score":0.008415043},"labels":[],"label_agreement":null},{"id":"W2330037746","doi":"10.2514/6.2005-1348","title":"Experimental Testing of the Quarter-Scale Rocket Chair","year":2005,"lang":"en","type":"article","venue":"43rd AIAA Aerospace Sciences Meeting and Exhibit","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":1,"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":"Aeronautics; Quarter (Canadian coin); Rocket (weapon); Scale (ratio); Aerospace engineering; Computer science; Engineering; History; Geography; Cartography; Archaeology","score_opus":0.022812110108931805,"score_gpt":0.25671795107904166,"score_spread":0.23390584097010986,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2330037746","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":[0.98747337,0.00004641445,0.009664064,0.000035331876,0.00005986198,0.00017084475,0.00037240965,0.00022987921,0.0019477638],"genre_scores_gemma":[0.98951346,0.00007971956,0.006021332,0.000021197702,0.000007008858,0.00009133401,0.00036699598,0.000032040898,0.0038670471],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9996178,0.00004715676,0.00001960099,0.000090897905,0.00013930122,0.00008523983],"domain_scores_gemma":[0.9990005,0.00015169468,0.000053810367,0.00022565052,0.00036545884,0.00020288772],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006258171,0.00067986915,0.0005007476,0.0002548992,0.00038781555,0.00036533308,0.0010298426,0.0006723253,0.005718113],"category_scores_gemma":[0.0011877606,0.0002860307,0.0004864492,0.00019178318,0.00033889076,0.00043053267,0.00056197855,0.0004594414,0.0011249797],"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":[0.0022472967,0.0019004246,0.008130837,0.00050946255,0.00009367394,0.0008233498,0.0010539393,0.051441554,0.89192724,0.0010185909,0.002084614,0.03876894],"study_design_scores_gemma":[0.00059593754,0.057728693,0.05479454,0.00011664925,0.00021166855,0.0007354188,0.0018820438,0.18475905,0.6756327,0.0005335,0.022810485,0.00019926428],"about_ca_topic_score_codex":0.0025733563,"about_ca_topic_score_gemma":0.003336533,"teacher_disagreement_score":0.005718113,"about_ca_system_score_codex":0.00020011513,"about_ca_system_score_gemma":0.00054252875,"threshold_uncertainty_score":0.019128978},"labels":[],"label_agreement":null},{"id":"W2330165364","doi":"10.2514/6.2008-5222","title":"Valentine Glushko - A Pioneer of Rocket Propulsion and Practical Cosmonautics","year":2008,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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 Toronto","funders":"","keywords":"Aeronautics; Propulsion; Aerospace engineering; Rocket (weapon); Spacecraft propulsion; Astrobiology; Engineering; Computer science; Physics","score_opus":0.04534496622634037,"score_gpt":0.27487008367441973,"score_spread":0.22952511744807935,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2330165364","genre_codex":"commentary","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"other","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.011113159,0.24064748,0.044399608,0.27764332,0.14667661,0.00012670297,0.0013168857,0.0013482163,0.27672803],"genre_scores_gemma":[0.11296656,0.106699646,0.017094966,0.030383762,0.031990625,0.00012097061,0.0005286345,0.0010686361,0.6991462],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.9986339,0.00023231399,0.000058032045,0.00044674464,0.0005120263,0.00011700157],"domain_scores_gemma":[0.9978836,0.00055153336,0.00014314454,0.00009678922,0.00069771503,0.0006272974],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0017998008,0.0018188269,0.0012744082,0.0018156179,0.0021243223,0.0033899944,0.0011210158,0.0026661148,0.011294344],"category_scores_gemma":[0.00375993,0.00049612764,0.00055931095,0.00080707704,0.004652753,0.004465051,0.0024719164,0.008031683,0.010151071],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00017863762,0.00008973961,0.0009415539,0.00051640696,0.00006485771,0.00021736145,0.0008930174,0.0018551669,0.0012236164,0.22945806,0.7012243,0.06333716],"study_design_scores_gemma":[0.000017245336,0.000060164937,0.0005089394,0.00020303015,0.000011642369,0.00022957301,0.00016135589,0.0005143555,0.000950867,0.027904466,0.9694027,0.000035748133],"about_ca_topic_score_codex":0.0030618706,"about_ca_topic_score_gemma":0.0035113886,"teacher_disagreement_score":0.011294344,"about_ca_system_score_codex":0.0029954268,"about_ca_system_score_gemma":0.0030823161,"threshold_uncertainty_score":0.037783325},"labels":[],"label_agreement":null},{"id":"W2331265932","doi":"10.2514/6.2006-8089","title":"A Nozzle Concept to Entrain Atmospheric Air for Ejector Operation","year":2006,"lang":"en","type":"article","venue":"14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":11,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Carleton University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Nozzle; Injector; Environmental science; Aerospace engineering; Computer science; Mechanical engineering; Engineering","score_opus":0.013814551955700478,"score_gpt":0.21937143537335804,"score_spread":0.20555688341765757,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2331265932","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":[0.019738838,0.001343562,0.9560208,0.00023171968,0.000528687,0.00028462565,0.00013456077,0.001030871,0.020686353],"genre_scores_gemma":[0.260134,0.0019403867,0.7176797,0.00038511917,0.0001789282,0.0003495105,0.00021688276,0.00018239809,0.01893306],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9996051,0.0000430449,0.000027793812,0.00007177753,0.00022168153,0.000030681644],"domain_scores_gemma":[0.99979836,0.000029197074,0.000026699947,0.000023916244,0.000092911905,0.000028846573],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006862251,0.00046491888,0.00037354644,0.00036410068,0.0005328684,0.00096479204,0.0010815164,0.0008014941,0.0028026989],"category_scores_gemma":[0.00046120715,0.00026137516,0.00050785556,0.00024176191,0.0005032722,0.0012310827,0.0007431609,0.0009125128,0.00083996844],"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":[0.0001978895,0.00014146409,0.0010354774,0.0007584556,0.000043428037,0.00090100017,0.00032193193,0.020186795,0.54524094,0.28658214,0.0033121677,0.14127833],"study_design_scores_gemma":[0.0003379344,0.0033493035,0.0036345893,0.00027387886,0.000104598825,0.0059462935,0.00013523074,0.19679137,0.40317374,0.02954567,0.35646185,0.00024553234],"about_ca_topic_score_codex":0.00038082837,"about_ca_topic_score_gemma":0.00041583375,"teacher_disagreement_score":0.0028026989,"about_ca_system_score_codex":0.00031782317,"about_ca_system_score_gemma":0.0009149514,"threshold_uncertainty_score":0.009375989},"labels":[],"label_agreement":null},{"id":"W2331594232","doi":"10.2514/6.2009-102","title":"F-35 Pre-Flight Store Separation Analyses: Innovative Techniques for Affordability","year":2009,"lang":"en","type":"article","venue":"47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":13,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lockheed Martin (Canada)","funders":"","keywords":"Separation (statistics); Computer science; Machine learning","score_opus":0.04898879488372125,"score_gpt":0.3783437183519215,"score_spread":0.3293549234682002,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2331594232","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":[0.07976416,0.00010078317,0.9000754,0.00008129749,0.000040593946,0.000056679233,0.00047302904,0.0016921108,0.017715884],"genre_scores_gemma":[0.6775748,0.00010552409,0.31160545,0.000021671898,0.00004296142,0.00006183306,0.0007601648,0.00056280696,0.009264754],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996656,0.000025225194,0.000016308495,0.000058342674,0.00016632775,0.00006814018],"domain_scores_gemma":[0.9994392,0.00015412165,0.00006240578,0.000119390614,0.0001954891,0.000029352783],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00029577233,0.0010806296,0.0004979605,0.0029430648,0.0009823289,0.0018591275,0.0008468788,0.00058787374,0.013614751],"category_scores_gemma":[0.0021727702,0.00039024153,0.0009198481,0.0019676108,0.0005127916,0.0021632295,0.00095548603,0.000800124,0.0012791655],"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":[0.0004601345,0.00031553756,0.010962311,0.00019740111,0.00010429724,0.00032549046,0.0007696369,0.12075767,0.05818658,0.076632686,0.0056908885,0.7255974],"study_design_scores_gemma":[0.000028652727,0.00021194915,0.011915593,0.000039545634,0.00008748282,0.0003312952,0.0006032396,0.8899959,0.03203291,0.038539447,0.026127825,0.000086137865],"about_ca_topic_score_codex":0.013438417,"about_ca_topic_score_gemma":0.013290823,"teacher_disagreement_score":0.013614751,"about_ca_system_score_codex":0.00048579904,"about_ca_system_score_gemma":0.001053475,"threshold_uncertainty_score":0.045545876},"labels":[],"label_agreement":null},{"id":"W2333877120","doi":"10.2514/6.2004-4084","title":"Real Time Engine Thrust Calculation For Modern Fighter Aircraft","year":2004,"lang":"en","type":"article","venue":"40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit","topic":"Rocket and propulsion systems research","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":"Lockheed Martin (Canada)","funders":"","keywords":"Aeronautics; Aerospace engineering; Thrust; Computer science; Automotive engineering; Engineering","score_opus":0.031446126121791824,"score_gpt":0.2603208266576596,"score_spread":0.22887470053586778,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2333877120","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":[0.29649132,0.00023637188,0.6867171,0.00009246834,0.000054743377,0.000079201425,0.0005674175,0.0082172295,0.0075441245],"genre_scores_gemma":[0.8583546,0.0001435951,0.136453,0.00001806888,0.000011878962,0.000039572496,0.0005707634,0.0003173576,0.0040910905],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998672,0.000015319365,0.000005713385,0.000020780008,0.0000827322,0.000008270106],"domain_scores_gemma":[0.9998418,0.000046778136,0.00001818334,0.000034025976,0.000049839862,0.00000925607],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020776401,0.00038294133,0.00025747833,0.00046629526,0.00023068965,0.00050826935,0.0004129016,0.000295809,0.0035870979],"category_scores_gemma":[0.00065189827,0.00018233585,0.00015724332,0.00032795305,0.00010169323,0.000563638,0.00024171584,0.0003045912,0.0008417897],"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":[0.000435284,0.00015255604,0.017220935,0.000206134,0.000048560294,0.00021358769,0.00022635265,0.32181582,0.1546866,0.004830874,0.004944841,0.4952185],"study_design_scores_gemma":[0.000034246597,0.00016122925,0.009197771,0.000011982197,0.000011408822,0.00016818372,0.00003721246,0.9326742,0.05066065,0.0013455583,0.0056702304,0.000027254726],"about_ca_topic_score_codex":0.0028572269,"about_ca_topic_score_gemma":0.0038174123,"teacher_disagreement_score":0.0035870979,"about_ca_system_score_codex":0.00033697046,"about_ca_system_score_gemma":0.0003540856,"threshold_uncertainty_score":0.012000024},"labels":[],"label_agreement":null},{"id":"W2333900143","doi":"10.2514/6.2005-5072","title":"A Time-Dependent Sticking Coefficient Model for Multi-Species Spacecraft Material","year":2005,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lockheed Martin (Canada)","funders":"","keywords":"Spacecraft; Sticking coefficient; Biological system; Materials science; Environmental science; Aerospace engineering; Astrobiology; Physics; Chemistry; Engineering; Physical chemistry","score_opus":0.06084135511926671,"score_gpt":0.29669182862860854,"score_spread":0.23585047350934185,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2333900143","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":[0.12386686,0.0023002643,0.82184654,0.0017287575,0.00070534676,0.00020557792,0.0007803643,0.0005130511,0.04805336],"genre_scores_gemma":[0.9293613,0.0017919637,0.025139052,0.00037769976,0.00018179095,0.00023184833,0.0004699561,0.00024720078,0.042199273],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997398,0.000039577008,0.000016481152,0.000070378446,0.00008983505,0.000043947555],"domain_scores_gemma":[0.9993654,0.00020613166,0.00010757491,0.00008135683,0.0001623001,0.000077356744],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005995465,0.0009959029,0.0013467271,0.0012062277,0.0008894323,0.0014313018,0.0030677828,0.003890853,0.0036392375],"category_scores_gemma":[0.0021371169,0.0009141746,0.0011579412,0.001021637,0.0015755309,0.0026896335,0.001212217,0.0015899468,0.0006559889],"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":[0.000021012102,0.00003179108,0.00021112707,0.00007119436,0.000016688333,0.00013499548,0.00004957835,0.95960414,0.0032946744,0.03377695,0.0006098927,0.0021779959],"study_design_scores_gemma":[0.0000048239954,0.0000051794896,0.0000671976,0.0000038119583,0.0000039799274,0.000014632059,0.000005424943,0.99667823,0.00013729048,0.0028050893,0.00026651638,0.000007880565],"about_ca_topic_score_codex":0.012272853,"about_ca_topic_score_gemma":0.006708418,"teacher_disagreement_score":0.012272853,"about_ca_system_score_codex":0.001306506,"about_ca_system_score_gemma":0.0011599747,"threshold_uncertainty_score":0.024402857},"labels":[],"label_agreement":null},{"id":"W2334304186","doi":"10.2514/6.2005-4002","title":"Traveling Shock Wave Interaction with Rocket Motor Head End","year":2005,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","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":"Toronto Metropolitan University","funders":"","keywords":"Head (geology); Aerospace engineering; Shock wave; Physics; Rocket (weapon); Shock (circulatory); Traveling wave; Aeronautics; Computer science; Acoustics; Engineering; Geology; Medicine; Mathematics","score_opus":0.03549899924080189,"score_gpt":0.2763672074864342,"score_spread":0.2408682082456323,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2334304186","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":[0.99243116,0.000039951185,0.005331254,0.000021018752,0.000009619572,0.000012644085,0.000017430226,0.000052880354,0.0020841246],"genre_scores_gemma":[0.9963127,0.00003417715,0.0017268027,0.000011375907,0.0000040961195,0.000007772861,0.00004706866,0.000010299736,0.0018458238],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997924,0.00001783515,0.0000061900296,0.000021419311,0.00010473357,0.00005744577],"domain_scores_gemma":[0.9996686,0.00013146686,0.0000631765,0.000029636389,0.00006692244,0.000040164934],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020694392,0.00021764486,0.0004218885,0.00032048736,0.00038566248,0.0005164765,0.00047183462,0.00040242248,0.002969163],"category_scores_gemma":[0.0006608596,0.00016889576,0.00024636977,0.00017761215,0.00047017343,0.00034746088,0.00061401766,0.00042275648,0.00034856057],"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":[0.0018688872,0.00014880655,0.014928764,0.00016013699,0.000051565545,0.003102589,0.00069789076,0.031643182,0.9154306,0.0045145326,0.00042633284,0.027026545],"study_design_scores_gemma":[0.00006111126,0.000967118,0.025836026,0.000018432642,0.00003176527,0.0006827803,0.00050304865,0.1327645,0.83649504,0.00064290396,0.0019501288,0.000047090052],"about_ca_topic_score_codex":0.0012968921,"about_ca_topic_score_gemma":0.0011284712,"teacher_disagreement_score":0.002969163,"about_ca_system_score_codex":0.00035504493,"about_ca_system_score_gemma":0.00025221534,"threshold_uncertainty_score":0.009932876},"labels":[],"label_agreement":null},{"id":"W2335001156","doi":"10.2514/6.2015-3834","title":"Hybrid Rocket Engine Transient Internal Ballistic Simulation","year":2015,"lang":"en","type":"article","venue":"51st AIAA/SAE/ASEE Joint Propulsion Conference","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Transient (computer programming); Aerospace engineering; Rocket engine; Rocket (weapon); Transient analysis; Environmental science; Automotive engineering; Computer science; Engineering; Transient response; Electrical engineering","score_opus":0.08439625673974123,"score_gpt":0.28967650830623115,"score_spread":0.20528025156648994,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2335001156","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":[0.5830417,0.00022480497,0.21985936,0.00041730897,0.0002766673,0.00035005674,0.0024105993,0.003932698,0.18948682],"genre_scores_gemma":[0.9748931,0.000060304876,0.012091196,0.000072043724,0.000019602696,0.00014808192,0.0007058141,0.00031013068,0.011699564],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997154,0.000050629482,0.000010106446,0.00003786697,0.00010233251,0.00008363886],"domain_scores_gemma":[0.99947006,0.00019624547,0.000049314353,0.00007864697,0.0001394352,0.000066348075],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00036002073,0.00065303553,0.0010912888,0.0006838386,0.0008101124,0.0011317892,0.0021595613,0.0015302708,0.015047059],"category_scores_gemma":[0.0011192402,0.0006367341,0.001051924,0.00059263426,0.00062017015,0.00076092687,0.0010942082,0.000967267,0.0017630678],"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":[0.00007014551,0.00003838492,0.00038033922,0.00002425762,0.000019572219,0.00006192167,0.000023672315,0.99503124,0.0008544931,0.0016465641,0.00033974642,0.0015096667],"study_design_scores_gemma":[0.000018854278,0.000027536531,0.00017269092,0.0000025859504,0.000004114653,0.000009054892,0.000008474114,0.9987602,0.00044505924,0.00024696082,0.00029871543,0.000005673376],"about_ca_topic_score_codex":0.018484056,"about_ca_topic_score_gemma":0.009428003,"teacher_disagreement_score":0.018484056,"about_ca_system_score_codex":0.0010253111,"about_ca_system_score_gemma":0.0012807931,"threshold_uncertainty_score":0.050337493},"labels":[],"label_agreement":null},{"id":"W2335492052","doi":"10.2514/6.2009-5177","title":"Steepness of Grain Geometry Transitions on Instability Symptom Suppression in Solid Rocket Motor","year":2009,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":12,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Solid-fuel rocket; Instability; Aerospace engineering; Rocket (weapon); Materials science; Geometry; Mechanics; Physics; Engineering; Mathematics; Propellant","score_opus":0.016427274863709308,"score_gpt":0.2829837430313083,"score_spread":0.266556468167599,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2335492052","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":[0.9962186,0.000011971751,0.0034719252,0.0000044066524,5.992564e-7,0.000003154586,0.0000055074015,0.000036654663,0.00024710104],"genre_scores_gemma":[0.999524,0.000007599789,0.0004239546,0.0000010128626,1.905597e-7,0.0000010008372,0.0000048442785,0.0000032196565,0.00003403859],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999503,0.00000943969,0.0000029165733,0.0000073035253,0.000016168955,0.000013921957],"domain_scores_gemma":[0.999655,0.00017407924,0.00009051417,0.00002366844,0.000035551788,0.000021179278],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00014038035,0.00014996447,0.00015280505,0.00018882987,0.00011577563,0.00024721024,0.00011580422,0.0001361804,0.0004551304],"category_scores_gemma":[0.0010680616,0.00010217048,0.00014091023,0.00011698135,0.00022161049,0.00022856421,0.0001566295,0.00014442668,0.000049817092],"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":[0.000730482,0.00013339544,0.03704418,0.00006850787,0.000030435778,0.00030080715,0.00021534796,0.772909,0.16214308,0.00084575155,0.0001087279,0.025470154],"study_design_scores_gemma":[0.000025361229,0.0005463384,0.03243576,0.0000069907132,0.000030172749,0.000077934215,0.00009528887,0.87226033,0.094054,0.00027898804,0.00017130174,0.000017467477],"about_ca_topic_score_codex":0.0018057346,"about_ca_topic_score_gemma":0.002251722,"teacher_disagreement_score":0.0018057346,"about_ca_system_score_codex":0.00015904712,"about_ca_system_score_gemma":0.00017550024,"threshold_uncertainty_score":0.003590405},"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":"W2354268437","doi":"","title":"Numerical simulation of flowing field of axial symmetrical turbulence jet flow","year":2008,"lang":"en","type":"article","venue":"Steelmaking","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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":"Turbulence; Mechanics; Jet (fluid); Physics; Flow (mathematics); Computer simulation; Field (mathematics); K-epsilon turbulence model; Turbulence kinetic energy; Mathematics","score_opus":0.034163819998225355,"score_gpt":0.3004932271960264,"score_spread":0.266329407197801,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2354268437","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":[0.7899376,0.00037568697,0.1714932,0.00025469743,0.0001381313,0.00017771458,0.0010236555,0.0015431277,0.035056233],"genre_scores_gemma":[0.9720489,0.00015327819,0.023474876,0.0000186307,0.000013254355,0.0000999154,0.00036332922,0.000047451915,0.0037804553],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998248,0.000030446317,0.000010704595,0.000027038486,0.00006468682,0.00004229662],"domain_scores_gemma":[0.9997003,0.000099613324,0.000035073335,0.000026972797,0.000098555836,0.000039521845],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003001693,0.00037571127,0.000712352,0.0005970943,0.0005439939,0.0006046126,0.0007675052,0.00080609514,0.0025944025],"category_scores_gemma":[0.0006887814,0.0001867651,0.00038481265,0.00068417133,0.0004945104,0.00036723717,0.0003842069,0.00033440767,0.00021513292],"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":[0.00013503953,0.000108135006,0.0020431187,0.00009663494,0.000017650415,0.00023550121,0.00012119558,0.96367246,0.019873085,0.00531781,0.00063739606,0.0077419803],"study_design_scores_gemma":[0.000019440095,0.000032377997,0.0005060242,0.0000036027018,0.0000030551798,0.000020420526,0.000015115292,0.99644756,0.0022406944,0.000347025,0.00035692423,0.000007679162],"about_ca_topic_score_codex":0.00810185,"about_ca_topic_score_gemma":0.0023850459,"teacher_disagreement_score":0.00810185,"about_ca_system_score_codex":0.00052903907,"about_ca_system_score_gemma":0.00072983466,"threshold_uncertainty_score":0.016109407},"labels":[],"label_agreement":null},{"id":"W2356620093","doi":"","title":"Separation Characteristics of Supersonic Swirling Flow Nozzle for Natural Gas","year":2011,"lang":"en","type":"article","venue":"Acta Petrolei Sinica(Petroleum Processing Section)","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":1,"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; Mechanics; Supersonic speed; Discharge coefficient; Tuyere; Choked flow; Materials science; Cylinder; Flow (mathematics); Physics; Thermodynamics; Mechanical engineering; Engineering","score_opus":0.02903100002741074,"score_gpt":0.27600411287917037,"score_spread":0.24697311285175963,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2356620093","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":[0.98616636,0.00032892966,0.0097099375,0.00007644945,0.000021297908,0.000017312004,0.000107330685,0.00013202039,0.0034404255],"genre_scores_gemma":[0.9962063,0.000104734674,0.0025509843,0.000012781216,0.000002277287,0.000007921543,0.00014428141,0.000016428632,0.00095419824],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997603,0.000024344035,0.000013446028,0.000036782625,0.00011449786,0.000050563525],"domain_scores_gemma":[0.9994636,0.00023863556,0.00008019472,0.000021781927,0.00015982304,0.000036018348],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00052604114,0.00024726847,0.00034134678,0.0003126516,0.0005128104,0.00070028956,0.00045080652,0.00070636114,0.0009876329],"category_scores_gemma":[0.001092292,0.00017778005,0.00044039782,0.00029092398,0.00038831052,0.0005403836,0.0002354243,0.0002916847,0.00019739101],"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":[0.0015625663,0.00013488418,0.013319241,0.0003064744,0.000050370385,0.0007372679,0.00047701912,0.45544246,0.50304675,0.004528962,0.0009203509,0.019473733],"study_design_scores_gemma":[0.00008002812,0.00055866153,0.0072520394,0.000017428238,0.000023949891,0.00019354628,0.00014047958,0.8500812,0.13997592,0.00051870936,0.0010825311,0.00007557894],"about_ca_topic_score_codex":0.005325177,"about_ca_topic_score_gemma":0.003006096,"teacher_disagreement_score":0.005325177,"about_ca_system_score_codex":0.00086099375,"about_ca_system_score_gemma":0.000906955,"threshold_uncertainty_score":0.010588348},"labels":[],"label_agreement":null},{"id":"W2368106293","doi":"","title":"Flow characteristics of natural gas in annular supersonic nozzles","year":2011,"lang":"en","type":"article","venue":"Huagong jinzhan","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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; Supersonic speed; Mechanics; Mach number; Flow (mathematics); Discharge coefficient; Choked flow; Jet (fluid); Centrifugal force; Momentum (technical analysis); Natural gas; Materials science; Chemistry; Thermodynamics; Physics","score_opus":0.02649376765600583,"score_gpt":0.22267892768972036,"score_spread":0.19618516003371453,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2368106293","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":[0.9814767,0.00034612344,0.016044987,0.000022432168,0.000015849368,0.000011190159,0.000082413506,0.00009917047,0.0019011536],"genre_scores_gemma":[0.99536127,0.00013513124,0.003634193,0.000008512163,0.0000033973283,0.0000059874324,0.000101800564,0.000008053545,0.000741574],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99989486,0.000010357806,0.000007797549,0.000028610166,0.00004019042,0.000018213219],"domain_scores_gemma":[0.9998665,0.00003724317,0.000028582901,0.000007702983,0.00004499501,0.000014952729],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002280694,0.0001778862,0.00022638687,0.00021224811,0.00017587985,0.00032869485,0.00024079205,0.0002400695,0.000384483],"category_scores_gemma":[0.00030604433,0.00010578324,0.00020819055,0.00017308556,0.00025674904,0.00039796147,0.00015523513,0.0001269631,0.00006764119],"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":[0.0004090079,0.00004284627,0.008569863,0.00011920109,0.000014022936,0.0003305502,0.00029028265,0.04535968,0.9268283,0.0041547483,0.00028198503,0.01359953],"study_design_scores_gemma":[0.00005771121,0.0008265949,0.02879327,0.000021674587,0.00004511749,0.00042092465,0.00020130459,0.55113196,0.41284636,0.00085796503,0.0047061774,0.000090870264],"about_ca_topic_score_codex":0.0026377297,"about_ca_topic_score_gemma":0.0012996206,"teacher_disagreement_score":0.0026377297,"about_ca_system_score_codex":0.00047068959,"about_ca_system_score_gemma":0.0002973713,"threshold_uncertainty_score":0.0052447915},"labels":[],"label_agreement":null},{"id":"W2373166047","doi":"","title":"Further detailed analysis about shock wave reflection outside Laval nozzle in different working states","year":2012,"lang":"en","type":"article","venue":"Journal of Aerospace Power","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":1,"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":"Mach reflection; Shock wave; Oblique shock; Nozzle; Mach number; Reflection (computer programming); Shock (circulatory); Mechanics; Mach wave; Overall pressure ratio; Physics; Optics; Thermodynamics; Computer science","score_opus":0.025853437978307352,"score_gpt":0.2818703477204216,"score_spread":0.2560169097421142,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2373166047","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":[0.9651949,0.00015089799,0.031040829,0.000034341112,0.0000103593675,0.00001835215,0.00013541084,0.00030275667,0.0031122032],"genre_scores_gemma":[0.99748755,0.000057207504,0.0017066445,0.0000075747057,0.0000027200788,0.000008374981,0.00010983459,0.000021553424,0.0005985552],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99965465,0.000024191131,0.000019750214,0.000096309814,0.00011912437,0.00008594637],"domain_scores_gemma":[0.9992047,0.0003457996,0.00013040972,0.00007443487,0.00020693574,0.00003777893],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00037435946,0.00026636434,0.00030266767,0.00075590255,0.00026576567,0.00042884305,0.00036551597,0.00040626238,0.0021367131],"category_scores_gemma":[0.0012448101,0.00019721416,0.000437115,0.0005988939,0.0003870988,0.0007983312,0.00026589035,0.00052432413,0.0001917276],"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":[0.0007723147,0.00012260456,0.04011214,0.0003773529,0.000067833535,0.0019507714,0.0018762075,0.036208123,0.84909683,0.0029203866,0.00092651334,0.06556892],"study_design_scores_gemma":[0.00004622118,0.00095018366,0.19152334,0.00003563469,0.000105092775,0.0011714312,0.0014759481,0.29346684,0.5072407,0.0015234412,0.0023155496,0.00014559217],"about_ca_topic_score_codex":0.00057782896,"about_ca_topic_score_gemma":0.00031014177,"teacher_disagreement_score":0.0021367131,"about_ca_system_score_codex":0.00016717338,"about_ca_system_score_gemma":0.00011712757,"threshold_uncertainty_score":0.0071480274},"labels":[],"label_agreement":null},{"id":"W2375003528","doi":"","title":"Analysis of flow-rate characteristics for a Laval fuel flow-rate control valve","year":2012,"lang":"en","type":"article","venue":"Journal of Mechanical & Electrical Engineering","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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":"Ramjet; Nozzle; Volumetric flow rate; Valve timing; Flow control valve; Flow (mathematics); Flow coefficient; Control valves; Flow control (data); Inlet; Mechanics; Engineering; Materials science; Automotive engineering; Mechanical engineering; Combustor; Internal combustion engine; Chemistry; Combustion; Physics","score_opus":0.013749777082420592,"score_gpt":0.25404340786854385,"score_spread":0.24029363078612326,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2375003528","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":[0.7306642,0.0016643268,0.24823424,0.00025093797,0.00012689103,0.00020954099,0.00053279026,0.0024430014,0.015874067],"genre_scores_gemma":[0.99185246,0.00011439832,0.0052894726,0.00001812898,0.000010417808,0.000025066403,0.00017520905,0.00005217884,0.0024626628],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99944776,0.000041174324,0.000022649196,0.0001104584,0.00031442015,0.00006359106],"domain_scores_gemma":[0.9986191,0.0007444579,0.00014959382,0.00006473964,0.00038346267,0.000038643648],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0007667314,0.00031321694,0.00044119277,0.0011182821,0.00032130664,0.0006587106,0.0006654727,0.00065873476,0.002248627],"category_scores_gemma":[0.00208135,0.00021827704,0.0004697928,0.00040089665,0.0003470051,0.0005932989,0.00015326953,0.0004200978,0.0005500669],"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":[0.0016372338,0.0002605364,0.016553357,0.00051034294,0.00006766335,0.00058784836,0.0010883703,0.080005966,0.7726087,0.008015729,0.002168726,0.11649552],"study_design_scores_gemma":[0.00006596771,0.00087772764,0.019510813,0.000044857887,0.000041688483,0.00042691935,0.00015489297,0.69303364,0.27493122,0.0010689894,0.009724153,0.00011913832],"about_ca_topic_score_codex":0.0027347566,"about_ca_topic_score_gemma":0.00075334596,"teacher_disagreement_score":0.0027347566,"about_ca_system_score_codex":0.00058931246,"about_ca_system_score_gemma":0.00044092414,"threshold_uncertainty_score":0.0075223446},"labels":[],"label_agreement":null},{"id":"W2376865040","doi":"","title":"Effects of throat shape design on propulsion performance of micronozzles","year":2010,"lang":"en","type":"article","venue":"Journal of Aerospace Power","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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":"Throat; Propulsion; Specific impulse; Thrust; Impulse (physics); Mechanics; Rotational symmetry; Expansion ratio; Mechanical engineering; Aerospace engineering; Engineering; Engineering drawing; Structural engineering; Physics; Materials science; Classical mechanics; Anatomy; Composite material; Medicine","score_opus":0.0084959492577615,"score_gpt":0.23100185516823335,"score_spread":0.22250590591047184,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2376865040","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":[0.99276227,0.000102203536,0.0059968736,0.000014166184,0.000005304478,0.000008905136,0.00006327265,0.0000867013,0.00096028286],"genre_scores_gemma":[0.99832577,0.000048438895,0.0013763024,0.0000035860853,6.3240964e-7,0.000007064684,0.00004417256,0.0000109475295,0.00018319949],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99989283,0.000014567391,0.000007068705,0.000020879128,0.000024047433,0.000040609102],"domain_scores_gemma":[0.99973255,0.000120776385,0.00004555187,0.000023881625,0.000040949304,0.000036288246],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00027360138,0.00031034704,0.00036994848,0.00024227348,0.0002471744,0.0004412479,0.00027240408,0.00029203668,0.00087504444],"category_scores_gemma":[0.0008994974,0.00018357267,0.0002824797,0.00014983612,0.0003703112,0.00044515473,0.0003570845,0.00017826365,0.00013465002],"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":[0.0012210766,0.00008131983,0.02790471,0.0003187151,0.000046147437,0.0007990046,0.00024844075,0.28084224,0.6628011,0.0020227728,0.00030747493,0.023407016],"study_design_scores_gemma":[0.00013780947,0.0017810767,0.060689285,0.00003876877,0.000116654846,0.0004746049,0.000447365,0.44816604,0.48460558,0.0007582804,0.0026659037,0.00011861275],"about_ca_topic_score_codex":0.0008473914,"about_ca_topic_score_gemma":0.0011016357,"teacher_disagreement_score":0.00087504444,"about_ca_system_score_codex":0.00043588356,"about_ca_system_score_gemma":0.00027697717,"threshold_uncertainty_score":0.0031626225},"labels":[],"label_agreement":null},{"id":"W2377449772","doi":"","title":"Numerical simulation of swirling flow characteristics of supersonic swirling natural gas separator","year":2007,"lang":"en","type":"article","venue":"Zhongguo Shiyou Daxue xuebao. Ziran kexue ban","topic":"Rocket and propulsion systems research","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":"Supersonic speed; Choked flow; Separator (oil production); Mechanics; Mach number; Supersonic wind tunnel; Nozzle; Cyclonic separation; Wing; Chemistry; Aerospace engineering; Physics; Thermodynamics; Engineering; Mechanical engineering","score_opus":0.016030415476879785,"score_gpt":0.27588491172123586,"score_spread":0.2598544962443561,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2377449772","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":[0.9258507,0.00039627223,0.049234267,0.0003965153,0.000131924,0.000098832614,0.00073251105,0.00063585216,0.022523083],"genre_scores_gemma":[0.98672545,0.00014481462,0.009434643,0.000032369724,0.000009721953,0.00007633479,0.00036502938,0.00003894088,0.0031726086],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998266,0.000028445145,0.0000103107595,0.0000259345,0.000048675025,0.000059998478],"domain_scores_gemma":[0.99952066,0.00021752746,0.000057901456,0.000024126837,0.00012390145,0.000055838667],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003077956,0.00063442776,0.0007329544,0.00061505556,0.0008081217,0.0007270915,0.0006987276,0.0014340286,0.0027713517],"category_scores_gemma":[0.0008496196,0.00033203495,0.0006641052,0.0005784773,0.000649186,0.0005151709,0.00048045127,0.0005267426,0.00023000529],"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":[0.00013372698,0.00007846783,0.0037721677,0.00006596246,0.0000207435,0.00022046675,0.00011305252,0.9850242,0.005351092,0.0013314454,0.00049983134,0.0033887713],"study_design_scores_gemma":[0.000009354076,0.00001741984,0.00044770073,0.0000028030317,0.0000027091387,0.0000060957072,0.000021354188,0.9986337,0.00061001274,0.00010363923,0.00014026053,0.0000049085174],"about_ca_topic_score_codex":0.023103852,"about_ca_topic_score_gemma":0.010356978,"teacher_disagreement_score":0.023103852,"about_ca_system_score_codex":0.0007642388,"about_ca_system_score_gemma":0.00092078984,"threshold_uncertainty_score":0.04593879},"labels":[],"label_agreement":null},{"id":"W2378404170","doi":"","title":"Calculations of Thrust and Torque for Scarfed Nozzles","year":2007,"lang":"en","type":"article","venue":"Journal of Shanghai University of Electric Power","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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; Thrust; Torque; Dimensionless quantity; Rocket engine; Turbine; Rocket (weapon); Aerospace engineering; Engineering; Rocket engine nozzle; Mechanical engineering; Mechanics; Control theory (sociology); Physics; Computer science; Control (management); Thermodynamics","score_opus":0.010367339003040026,"score_gpt":0.22663531513576574,"score_spread":0.21626797613272572,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2378404170","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":[0.16013888,0.0014148218,0.7074319,0.0004098237,0.000248243,0.00019491841,0.0010276706,0.0011666181,0.12796716],"genre_scores_gemma":[0.9201418,0.00079463626,0.061337087,0.00005876171,0.000027271904,0.00012511933,0.00047790457,0.00023796021,0.016799485],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999845,0.000013647028,0.000008664334,0.000015945105,0.00009399582,0.000022620889],"domain_scores_gemma":[0.99977523,0.00007324073,0.00001914469,0.000015584306,0.00010791327,0.000008955888],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023348152,0.00030026576,0.00041717634,0.00051098387,0.00034473778,0.00054781075,0.00063130056,0.0005944037,0.005076835],"category_scores_gemma":[0.0011645112,0.00017144186,0.00049304496,0.00046965294,0.00028362664,0.0005858584,0.00022434918,0.0002739629,0.00088305806],"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":[0.000059461843,0.000015489302,0.0015420105,0.0002725418,0.00001315419,0.00036069646,0.000145237,0.8822835,0.01153398,0.070777,0.002192858,0.030804025],"study_design_scores_gemma":[0.000023120994,0.00003269251,0.0006736776,0.000023588844,0.0000064074698,0.000118365766,0.00004513124,0.9825417,0.0043616216,0.006362602,0.0057959976,0.000015127774],"about_ca_topic_score_codex":0.0034845136,"about_ca_topic_score_gemma":0.002184142,"teacher_disagreement_score":0.005076835,"about_ca_system_score_codex":0.0006729904,"about_ca_system_score_gemma":0.0007080403,"threshold_uncertainty_score":0.016983688},"labels":[],"label_agreement":null},{"id":"W2378609743","doi":"","title":"Numerical Simulation on the Flowfield of Supersonic Combustion and Atomization in Spary Bube","year":2011,"lang":"en","type":"article","venue":"Science Technology and Engineering","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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":"Supersonic speed; Nozzle; Combustion; Computer simulation; Mechanics; Airflow; Materials science; Flow (mathematics); Mixing (physics); Aerospace engineering; Nuclear engineering; Engineering; Mechanical engineering; Physics; Chemistry","score_opus":0.025229329911175824,"score_gpt":0.23519904853025259,"score_spread":0.20996971861907676,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2378609743","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":[0.93305475,0.00028674945,0.041798882,0.00045039476,0.000101836515,0.000089327805,0.0005308853,0.00029206337,0.0233951],"genre_scores_gemma":[0.9909094,0.000117326446,0.005289271,0.000033673594,0.000010584435,0.000058522215,0.00019013947,0.000020232435,0.0033708138],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998523,0.00003193282,0.000006504483,0.000019731411,0.00004524256,0.000044195862],"domain_scores_gemma":[0.9997317,0.00011899854,0.000040780717,0.000015631409,0.00006063551,0.000032258784],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00034048792,0.0003902428,0.00056224165,0.0003662467,0.0008400296,0.00058873,0.0004984271,0.0011013744,0.0026318969],"category_scores_gemma":[0.00085361407,0.00023824736,0.0005415977,0.00041971492,0.0006921851,0.0004431479,0.00047416677,0.0005095857,0.00015788757],"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":[0.00007946604,0.000040376603,0.0020558161,0.000048798793,0.000011942202,0.00014958013,0.00008050334,0.9891606,0.003573122,0.002983837,0.00023316462,0.0015827765],"study_design_scores_gemma":[0.000018841856,0.00002468295,0.0006599461,0.0000041155436,0.0000030781284,0.000012985979,0.000025787605,0.9979309,0.00083728926,0.0002503026,0.00022591163,0.00000616592],"about_ca_topic_score_codex":0.019339157,"about_ca_topic_score_gemma":0.006984422,"teacher_disagreement_score":0.019339157,"about_ca_system_score_codex":0.0006131276,"about_ca_system_score_gemma":0.00091996073,"threshold_uncertainty_score":0.03845316},"labels":[],"label_agreement":null},{"id":"W2381320929","doi":"","title":"Simulation on performance of Laval micronozzle by means of DSMC","year":2007,"lang":"en","type":"article","venue":"Journal of Solid Rocket Technology","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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; Thrust; Mechanics; Rocket engine nozzle; Monte Carlo method; Specific impulse; Discharge coefficient; Direct simulation Monte Carlo; Materials science; Impulse (physics); Rotational symmetry; Flow (mathematics); Physics; Mechanical engineering; Engineering; Classical mechanics; Mathematics","score_opus":0.011024132125339248,"score_gpt":0.27971065327780564,"score_spread":0.2686865211524664,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2381320929","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":[0.9758149,0.00013265928,0.01533798,0.00019881822,0.000030623603,0.000050304126,0.00069716515,0.00046592066,0.007271837],"genre_scores_gemma":[0.99408275,0.000052666284,0.0047480124,0.000018950119,0.0000032142882,0.00003265119,0.00029646928,0.00002438398,0.0007408387],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998548,0.000027849343,0.000006438021,0.000019086854,0.000049442326,0.000042395295],"domain_scores_gemma":[0.99956506,0.0002105123,0.00003856037,0.000026633754,0.00011080415,0.00004840901],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00030416087,0.00044294877,0.00060707063,0.00039643268,0.00055228226,0.0005628789,0.0007080812,0.0009299811,0.0013831385],"category_scores_gemma":[0.0008946131,0.00021575905,0.00051399105,0.00043241482,0.0004430516,0.00031067565,0.0003858434,0.00045324038,0.000114388546],"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":[0.000053483825,0.00003097429,0.0031532987,0.000030386871,0.000011056438,0.00008890035,0.000030843563,0.9917704,0.0023304557,0.000670914,0.00016501333,0.0016643456],"study_design_scores_gemma":[0.0000135371865,0.000018632707,0.0005618256,0.0000018906763,0.0000026682549,0.000008415714,0.000011995753,0.9981437,0.0010243985,0.00007148596,0.00013660644,0.0000048841116],"about_ca_topic_score_codex":0.028327057,"about_ca_topic_score_gemma":0.009568167,"teacher_disagreement_score":0.028327057,"about_ca_system_score_codex":0.00094875233,"about_ca_system_score_gemma":0.00114177,"threshold_uncertainty_score":0.056324303},"labels":[],"label_agreement":null},{"id":"W2394375660","doi":"","title":"Investigation on the transpiration cooling of a liquid rocket nozzle","year":2008,"lang":"en","type":"article","venue":"Journal of Aerospace Power","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":1,"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":"Liquid-propellant rocket; Nozzle; Rocket engine nozzle; Turbulence; Materials science; Mechanics; Propellant; Rocket (weapon); Aerodynamic heating; Thermodynamics; Aerodynamics; Heat transfer; Porosity; Transpiration; Rocket engine; Boundary layer; Compressibility; Aerospace engineering; Chemistry; Composite material; Physics; Engineering","score_opus":0.05423448697183566,"score_gpt":0.24920058075452853,"score_spread":0.19496609378269286,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2394375660","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":[0.99020797,0.00014382275,0.007411047,0.000041064326,0.000012413326,0.000026207135,0.000045493092,0.00007337912,0.0020385804],"genre_scores_gemma":[0.99880457,0.000052695366,0.0007382048,0.000005519576,0.0000016063449,0.000005846587,0.000024983663,0.000008414108,0.0003581927],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998956,0.000016682192,0.000003709776,0.000019344592,0.00003336901,0.000031360443],"domain_scores_gemma":[0.9998603,0.00005761053,0.00002065198,0.0000100525585,0.000035626166,0.000015772299],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024207997,0.00025244773,0.00063006085,0.0001993912,0.0003801528,0.00042658343,0.00037048655,0.0004196403,0.0009404137],"category_scores_gemma":[0.0005034102,0.00016577682,0.0004469497,0.00015683065,0.0005662884,0.00041588172,0.00031763382,0.00027203892,0.00007176528],"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":[0.00044876494,0.00011705807,0.0088719865,0.00019274231,0.00003844947,0.0009294694,0.00021954357,0.62806606,0.35038134,0.0029602689,0.00029602804,0.0074782507],"study_design_scores_gemma":[0.000071122,0.00032466996,0.0056881215,0.000010384456,0.00001647823,0.00008870923,0.00006346544,0.9421336,0.05088961,0.0002137017,0.00047578823,0.000024336412],"about_ca_topic_score_codex":0.005986581,"about_ca_topic_score_gemma":0.0020449462,"teacher_disagreement_score":0.005986581,"about_ca_system_score_codex":0.0005112835,"about_ca_system_score_gemma":0.00060927944,"threshold_uncertainty_score":0.011903465},"labels":[],"label_agreement":null},{"id":"W2464757693","doi":"10.1115/1.4034096","title":"Turbulence Modeling of Cavitating Flows in Liquid Rocket Turbopumps","year":2016,"lang":"en","type":"article","venue":"Journal of Fluids Engineering","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":21,"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 Waterloo","funders":"","keywords":"Turbulence; Reynolds-averaged Navier–Stokes equations; Mechanics; Cavitation; Turbulence modeling; K-epsilon turbulence model; K-omega turbulence model; Rocket engine; Physics; Aerospace engineering; Engineering","score_opus":0.015836164211223205,"score_gpt":0.23739382564770392,"score_spread":0.2215576614364807,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2464757693","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":[0.7744775,0.000501278,0.2201253,0.00017786385,0.000047384587,0.00007703286,0.00012863943,0.0003267099,0.0041383607],"genre_scores_gemma":[0.99431384,0.00017418675,0.004594556,0.000009849189,0.000013326358,0.000026810685,0.00006218251,0.000018465242,0.0007868264],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998591,0.000041568775,0.000010372005,0.000021891003,0.000036694113,0.000030301973],"domain_scores_gemma":[0.9997776,0.000088397144,0.00005753829,0.000014473824,0.000044478216,0.000017489996],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00027623557,0.00048585996,0.00049196446,0.00039368757,0.0003282718,0.00078965415,0.0005657454,0.00061184156,0.0003189876],"category_scores_gemma":[0.0007512885,0.00020197012,0.000494463,0.00030756532,0.0007029022,0.0005003738,0.00040118833,0.00043292152,0.00010560576],"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":[0.000052874035,0.0000312847,0.0018662664,0.000023859553,0.000009617596,0.0001191169,0.000045710734,0.9771817,0.015292113,0.002706686,0.000108171145,0.0025626132],"study_design_scores_gemma":[0.0000024940487,0.000011908725,0.00034009008,0.0000016362517,0.0000011066325,0.000007749651,0.000005528826,0.99835014,0.0010050259,0.00021846702,0.00005199122,0.0000038134297],"about_ca_topic_score_codex":0.0077093104,"about_ca_topic_score_gemma":0.002442751,"teacher_disagreement_score":0.0077093104,"about_ca_system_score_codex":0.00069998263,"about_ca_system_score_gemma":0.00066478713,"threshold_uncertainty_score":0.015328884},"labels":[],"label_agreement":null},{"id":"W2472576502","doi":"10.1088/1757-899x/134/1/012028","title":"Investigation the flushing flow of liquid methane in Laval nozzle","year":2016,"lang":"en","type":"article","venue":"IOP Conference Series Materials Science and Engineering","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":1,"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; Methane; Mechanics; Turbulence; Thermodynamics; Flow (mathematics); Boiling; Conservation of mass; Volume fraction; Momentum (technical analysis); Materials science; Chemistry; Physics","score_opus":0.028897269086566577,"score_gpt":0.23750858830052485,"score_spread":0.20861131921395826,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2472576502","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":[0.99430734,0.0003388979,0.0034877546,0.00004982911,0.000007857546,0.00000854909,0.00004949979,0.00007326451,0.001677031],"genre_scores_gemma":[0.99835604,0.00010166854,0.0007732002,0.0000053395365,0.000002102344,0.000003001657,0.000055793556,0.0000053038634,0.0006973992],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999912,0.000010075999,0.0000030620183,0.000013563188,0.000033478926,0.000027741165],"domain_scores_gemma":[0.99990845,0.000026336322,0.000015809639,0.000006448383,0.000028974238,0.000013940507],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00013037212,0.00015985186,0.00023446356,0.00021895299,0.00027451487,0.00033179953,0.00019725855,0.0003433625,0.0005454565],"category_scores_gemma":[0.0003002815,0.000098081255,0.00021201228,0.00013721391,0.00027766937,0.00021771749,0.00017167546,0.00020003044,0.000063361564],"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":[0.0003725389,0.00006440779,0.012490195,0.00017054626,0.000018930205,0.00082472526,0.00030563166,0.028601823,0.9442745,0.0023513804,0.00031888243,0.010206346],"study_design_scores_gemma":[0.00005859609,0.0007437568,0.04663214,0.00003668707,0.000027786607,0.0005007236,0.00031019954,0.39230555,0.55485505,0.000651417,0.0038255465,0.000052605505],"about_ca_topic_score_codex":0.0027304317,"about_ca_topic_score_gemma":0.0011293896,"teacher_disagreement_score":0.0027304317,"about_ca_system_score_codex":0.0003470671,"about_ca_system_score_gemma":0.00022533082,"threshold_uncertainty_score":0.005429089},"labels":[],"label_agreement":null},{"id":"W2491986785","doi":"10.3182/20070821-3-ca-2919.00050","title":"CALORIMETRIC STUDY OF BURNERS USED IN FLAME-JET DRILLING","year":2007,"lang":"en","type":"article","venue":"IFAC Proceedings Volumes","topic":"Rocket and propulsion systems research","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":"Université du Québec à Chicoutimi","funders":"","keywords":"Mechanics; Drilling; Thermal conduction; Thermal; Materials science; Jet (fluid); Calorimeter (particle physics); Combustor; Transient (computer programming); Nuclear engineering; Mechanical engineering; Petroleum engineering; Thermodynamics; Engineering; Composite material; Combustion; Chemistry; Electrical engineering; Physics; Detector","score_opus":0.02418828753307917,"score_gpt":0.280876268611022,"score_spread":0.25668798107794283,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2491986785","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":[0.9971949,0.00035804044,0.0010030036,0.000022403257,0.000014725745,0.000024837103,0.00018272082,0.000028393823,0.0011708929],"genre_scores_gemma":[0.99659663,0.00021769514,0.000616301,0.00001405262,0.0000042604916,0.000012410527,0.00018510767,0.000027700095,0.0023257683],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99973184,0.000031438758,0.000015457066,0.000043877855,0.00012591152,0.00005140355],"domain_scores_gemma":[0.99941003,0.00024237337,0.000050974857,0.000048635164,0.00020978948,0.000038126844],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003573358,0.0003346456,0.0005286887,0.0008332065,0.0007933635,0.00038158428,0.0006419362,0.00057345507,0.0033645672],"category_scores_gemma":[0.00095128675,0.00023859969,0.00030393217,0.0007983685,0.00060111046,0.000576745,0.0002968371,0.0005319955,0.0003939568],"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":[0.0037631392,0.00020299556,0.009055041,0.00029227987,0.00004196964,0.00037398,0.00047060577,0.0038318788,0.96563476,0.00037054453,0.0003571998,0.0156055605],"study_design_scores_gemma":[0.000028796954,0.0006399912,0.030047594,0.000016840744,0.00003750376,0.00017907389,0.00034959882,0.004928033,0.96190464,0.000072526556,0.0017697607,0.00002563825],"about_ca_topic_score_codex":0.0035760452,"about_ca_topic_score_gemma":0.0045793536,"teacher_disagreement_score":0.0035760452,"about_ca_system_score_codex":0.0004974899,"about_ca_system_score_gemma":0.0003749416,"threshold_uncertainty_score":0.011255562},"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":"W2510341592","doi":"10.4028/www.scientific.net/amm.852.617","title":"Design and Numerical Simulation of Convergent Divergent Nozzle","year":2016,"lang":"en","type":"article","venue":"Applied Mechanics and Materials","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":11,"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":"Mach number; Nozzle; Hypersonic speed; Supersonic speed; Mechanics; Isentropic process; Shock (circulatory); MATLAB; Turbulence; Mach wave; Computational fluid dynamics; Aerospace engineering; Structural engineering; Physics; Computer science; Engineering","score_opus":0.027073371972809363,"score_gpt":0.24839645589474807,"score_spread":0.2213230839219387,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2510341592","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":[0.3976654,0.0009556986,0.5016497,0.00051440735,0.00029627784,0.0005880524,0.0012714748,0.0011810473,0.0958779],"genre_scores_gemma":[0.8913766,0.00046343048,0.09317178,0.0000758603,0.00002075878,0.00048176528,0.00056260376,0.00009020058,0.013756971],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99970144,0.000044718872,0.000015658596,0.00003854423,0.00014246923,0.000057217803],"domain_scores_gemma":[0.99977535,0.00006232564,0.000033189186,0.00002239027,0.0000731336,0.000033649045],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00048352036,0.000456015,0.0008000485,0.00048096315,0.00057749177,0.000960589,0.0010484443,0.0012325265,0.0030797878],"category_scores_gemma":[0.0008053166,0.00028549152,0.0005473535,0.0004468843,0.0005806059,0.0004176258,0.00074417895,0.00047189087,0.0005195789],"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":[0.00007291908,0.00004613489,0.0012489309,0.000103527775,0.0000085921265,0.0002784565,0.00008950333,0.9785694,0.00900643,0.005896172,0.00058681046,0.004093125],"study_design_scores_gemma":[0.000021517604,0.000050810857,0.00027027953,0.000011743497,0.0000031855732,0.00004783204,0.000025703883,0.99559253,0.0018255983,0.0007487108,0.00139181,0.000010181776],"about_ca_topic_score_codex":0.0041042245,"about_ca_topic_score_gemma":0.0016045575,"teacher_disagreement_score":0.0041042245,"about_ca_system_score_codex":0.00062625716,"about_ca_system_score_gemma":0.0012224697,"threshold_uncertainty_score":0.010302961},"labels":[],"label_agreement":null},{"id":"W2516748709","doi":"","title":"First Nations Launch Competition Summary","year":2016,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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":"Competition (biology); Aeronautics; Launched; Propulsion; Political science; Engineering; Aerospace engineering","score_opus":0.01839725819405172,"score_gpt":0.2451482297118834,"score_spread":0.2267509715178317,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2516748709","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0024605035,0.002192244,0.0005547049,0.014050071,0.013710904,0.00044631847,0.015269385,0.0010088164,0.950307],"genre_scores_gemma":[0.004807112,0.0007530359,0.00025709704,0.0030657102,0.0011697519,0.00014447716,0.010436211,0.0002603527,0.9791062],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.9979467,0.000099573524,0.00004403497,0.00015605231,0.0013313702,0.00042233535],"domain_scores_gemma":[0.99670154,0.00016851921,0.000092448136,0.00010988104,0.0017835037,0.0011440819],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0018851005,0.0011959751,0.0006120256,0.0021693087,0.0030977894,0.0087009445,0.001825274,0.0036593406,0.34414232],"category_scores_gemma":[0.003039593,0.0004580731,0.0006988025,0.0016829651,0.00035585786,0.0026985467,0.0018596823,0.003633859,0.18644863],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000022375034,0.00003987355,0.000097972385,0.000037760772,0.0000013846607,0.000018727536,0.000009045928,0.000045028137,0.00007834279,0.0011394065,0.991217,0.007293102],"study_design_scores_gemma":[0.000009810033,0.00002445195,0.0011444148,0.00004337927,0.0000013349744,0.000013414647,0.000041164192,0.00006478266,0.00007311444,0.00018932477,0.9983845,0.000010304335],"about_ca_topic_score_codex":0.039356552,"about_ca_topic_score_gemma":0.08742867,"teacher_disagreement_score":0.34414232,"about_ca_system_score_codex":0.0033355942,"about_ca_system_score_gemma":0.008870772,"threshold_uncertainty_score":0.9355014},"labels":[],"label_agreement":null},{"id":"W2521926985","doi":"10.1115/gt2016-57570","title":"Testing of Synthesized Aromatic Kerosene (SAK) Aviation Fuel Blends at Simulated Altitudes","year":2016,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"National Research Council Canada","funders":"","keywords":"Jet fuel; Kerosene; Environmental science; Jet engine; Aviation fuel; Alternative fuels; Aviation; Process engineering; Waste management; Materials science; Aerospace engineering; Chemistry; Engineering; Combustion; Organic chemistry","score_opus":0.03185273998375164,"score_gpt":0.2602030327134426,"score_spread":0.22835029272969093,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2521926985","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":[0.9990675,0.000054353324,0.00041810045,0.0000053802864,0.000004266133,0.000016363307,0.00011135542,0.000017482891,0.00030515238],"genre_scores_gemma":[0.99772745,0.00015007656,0.0012012064,0.000007674761,0.0000017608807,0.000017131626,0.00022493546,0.000012266082,0.0006574828],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997341,0.000023680675,0.000028716539,0.000042676344,0.0001297419,0.00004105154],"domain_scores_gemma":[0.9998055,0.000038760838,0.000040944095,0.000012751286,0.00007204535,0.000030047097],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000256365,0.0004900304,0.00030375895,0.00031659775,0.0002933695,0.00029077535,0.00046891658,0.00038564406,0.00089498353],"category_scores_gemma":[0.00038148352,0.00016816187,0.00030885,0.00034313495,0.00019056154,0.00040854735,0.00036932193,0.00032595996,0.00017401141],"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":[0.00096959,0.00021977969,0.004278915,0.00013001265,0.000034486868,0.00022023875,0.00011508051,0.004796771,0.9865652,0.000069290225,0.000031850457,0.002568915],"study_design_scores_gemma":[0.000038003152,0.0025295902,0.0059687253,0.0000073346832,0.00003504956,0.00007913786,0.0001192395,0.0028571095,0.987833,0.000018629422,0.0005016443,0.000012527305],"about_ca_topic_score_codex":0.0036498518,"about_ca_topic_score_gemma":0.005557435,"teacher_disagreement_score":0.0036498518,"about_ca_system_score_codex":0.0003846071,"about_ca_system_score_gemma":0.00026817867,"threshold_uncertainty_score":0.007257223},"labels":[],"label_agreement":null},{"id":"W2560871744","doi":"10.1515/ijnsns-2012-0018","title":"Boiling Shocks and Self-Oscillations in Critical Nozzle Flow","year":2012,"lang":"en","type":"article","venue":"International Journal of Nonlinear Sciences and Numerical Simulation","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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":"Boiling; Mechanics; Breakup; Vaporization; Bubble; Nozzle; Shock wave; Thermodynamics; Shock (circulatory); Flow (mathematics); Materials science; Physics","score_opus":0.04192058470576307,"score_gpt":0.3794096360628643,"score_spread":0.3374890513571013,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2560871744","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":[0.9876502,0.000041942672,0.011049243,0.00002749191,0.000007993303,0.000014061541,0.0000128956235,0.00009744145,0.0010987],"genre_scores_gemma":[0.9993413,0.000009089716,0.0005006844,0.000004576117,0.0000018619347,0.000005038359,0.000008361421,0.0000043900195,0.00012457714],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99993265,0.000014491484,0.0000039101883,0.000008522761,0.000018563602,0.000021786807],"domain_scores_gemma":[0.9998306,0.000062794345,0.00004999407,0.000013217997,0.00001938171,0.000024046029],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001602019,0.00018390272,0.00017676958,0.00040646555,0.00018130016,0.00038583527,0.00023627748,0.00036077487,0.00077468343],"category_scores_gemma":[0.00061898795,0.00012129735,0.00027352237,0.00013469614,0.00059612904,0.00024289243,0.00043531987,0.00022672536,0.000061032537],"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":[0.0005511837,0.0003127686,0.025068661,0.00015106481,0.00006463892,0.0024909584,0.0007135603,0.7094238,0.19496515,0.050702617,0.0007057201,0.014849894],"study_design_scores_gemma":[0.00005752745,0.00012928342,0.0052029574,0.0000065989425,0.000008350409,0.00014861966,0.000057874287,0.97623265,0.013058857,0.004790541,0.0002927646,0.000013954567],"about_ca_topic_score_codex":0.0008497232,"about_ca_topic_score_gemma":0.0001853975,"teacher_disagreement_score":0.0008497232,"about_ca_system_score_codex":0.00033574871,"about_ca_system_score_gemma":0.00015402697,"threshold_uncertainty_score":0.0025915504},"labels":[],"label_agreement":null},{"id":"W2581310690","doi":"","title":"20V, 40 Ah Lithium Ion Polymer Battery for the Spacesuit","year":2006,"lang":"en","type":"article","venue":"NASA Technical Reports Server (NASA)","topic":"Rocket and propulsion systems research","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":"Electrovaya (Canada)","funders":"","keywords":"Battery (electricity); Cycling; Aerospace; Temperature cycling; Reliability (semiconductor); Engineering; Automotive engineering; EMI; Power (physics); Electrical engineering; Thermal; Electromagnetic interference; Aerospace engineering; Physics","score_opus":0.020313160198606694,"score_gpt":0.26628296077210606,"score_spread":0.24596980057349938,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2581310690","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":[0.64013857,0.007236204,0.08979269,0.0062712696,0.0013966657,0.0006423789,0.0015435418,0.003875454,0.24910334],"genre_scores_gemma":[0.8029598,0.0022248297,0.029504409,0.0009905422,0.00017513665,0.00020962811,0.00083684287,0.00020064008,0.16289823],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999057,0.000007283884,0.0000044413277,0.000010522546,0.000056595665,0.000015498386],"domain_scores_gemma":[0.9999397,0.0000042831857,0.00000548543,0.000004379865,0.000033963912,0.000012180489],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020294555,0.0002788914,0.0001408248,0.00019356445,0.00041851692,0.0005754267,0.00047897,0.0005417071,0.0089921905],"category_scores_gemma":[0.00021837758,0.0000762914,0.00017002538,0.000104152736,0.00018468188,0.0010033757,0.00034836953,0.00025360016,0.002209117],"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":[0.0017079122,0.0005847335,0.005229417,0.0013468579,0.000057099995,0.0024598183,0.00039450955,0.0058592395,0.600027,0.022046188,0.04263257,0.31765476],"study_design_scores_gemma":[0.00037754077,0.0040032803,0.0067877807,0.00014404966,0.00015360484,0.0043713124,0.00040725805,0.017848376,0.47963127,0.0069537032,0.47925597,0.00006586663],"about_ca_topic_score_codex":0.0007271206,"about_ca_topic_score_gemma":0.0039256625,"teacher_disagreement_score":0.0089921905,"about_ca_system_score_codex":0.00043354012,"about_ca_system_score_gemma":0.00063181133,"threshold_uncertainty_score":0.030081868},"labels":[],"label_agreement":null},{"id":"W2587523433","doi":"10.1088/1742-6596/789/1/012056","title":"Numerical investigation the dynamics of vaporization at the flow of liquid methane in channel with variable section","year":2017,"lang":"en","type":"article","venue":"Journal of Physics Conference Series","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":1,"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":"Vaporization; Diffuser (optics); Mechanics; Nozzle; Methane; Evaporation; Flow (mathematics); Thermodynamics; Momentum (technical analysis); Jet (fluid); Chemistry; Materials science; Physics; Optics","score_opus":0.028178936170813424,"score_gpt":0.25257942499084185,"score_spread":0.22440048882002842,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2587523433","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":[0.9408338,0.0005977893,0.041044436,0.00050808437,0.00009034621,0.00007256441,0.00055354455,0.00038944013,0.01590987],"genre_scores_gemma":[0.99208754,0.0001253561,0.0044280314,0.000022479955,0.000014716545,0.000059095393,0.0001531849,0.000020475183,0.0030890729],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998741,0.0000231003,0.0000062680374,0.000019935744,0.000031457956,0.0000450236],"domain_scores_gemma":[0.99958295,0.00018322164,0.00007929552,0.000021254922,0.00008205134,0.000051253995],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00027205783,0.00038285027,0.0006162317,0.000485976,0.00063743937,0.0007126083,0.0006827446,0.0011701493,0.002265099],"category_scores_gemma":[0.00088394363,0.00023864112,0.00043268697,0.0005309398,0.0007551188,0.00044987196,0.00042476697,0.00049543584,0.00013066597],"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":[0.00014550216,0.0000879352,0.0057687582,0.00010694138,0.000023736042,0.00034823956,0.00009686933,0.97931606,0.006979748,0.003975714,0.00041676548,0.0027337556],"study_design_scores_gemma":[0.000014411587,0.000027152799,0.00080912793,0.0000039816055,0.0000033961867,0.000021210424,0.000024822935,0.998047,0.0006273561,0.0002113661,0.00020421992,0.000006024241],"about_ca_topic_score_codex":0.017528024,"about_ca_topic_score_gemma":0.0060140165,"teacher_disagreement_score":0.017528024,"about_ca_system_score_codex":0.00077230524,"about_ca_system_score_gemma":0.0007369986,"threshold_uncertainty_score":0.034852028},"labels":[],"label_agreement":null},{"id":"W2588732445","doi":"10.1615/ichmt.2015.thmt-15.1880","title":"Two phase flow liquid metal behavior in propulsion chamber","year":2015,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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; Propellant; Breakup; Materials science; Mechanics; Flow (mathematics); Solid-fuel rocket; Liquid metal; Turbulence; Two-phase flow; Combustion; Aerospace engineering; Composite material; Chemistry; Engineering; Physics","score_opus":0.0620591400159658,"score_gpt":0.3488670211022418,"score_spread":0.28680788108627603,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2588732445","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":[0.9717253,0.000132379,0.023955395,0.00007951149,0.000018734127,0.000037297716,0.00021513889,0.0005636908,0.0032725083],"genre_scores_gemma":[0.99542916,0.00004896634,0.002936251,0.000015376383,0.0000031450359,0.000019953512,0.00015249297,0.00003163809,0.0013629206],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99982053,0.000012940061,0.000005175306,0.000053107808,0.00006747815,0.000040887855],"domain_scores_gemma":[0.99976,0.00008048893,0.00004180261,0.000021677355,0.000065898086,0.00003007279],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012679421,0.0002462117,0.00022303093,0.0004967632,0.000354104,0.0007058248,0.0003502402,0.0004166744,0.001833436],"category_scores_gemma":[0.0005824099,0.00016512306,0.00019655918,0.0002906113,0.000466183,0.0007573113,0.00030395767,0.00033553466,0.000329924],"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":[0.0008490275,0.00022986779,0.014582882,0.0001411536,0.000020550395,0.0006603143,0.0005122347,0.061404828,0.8877353,0.0054535866,0.00075027446,0.02765999],"study_design_scores_gemma":[0.000065663684,0.00043948353,0.009872781,0.00001441763,0.000010568442,0.00018535518,0.00017610157,0.44393194,0.5422199,0.00078903005,0.0022499883,0.000044822318],"about_ca_topic_score_codex":0.002378669,"about_ca_topic_score_gemma":0.0006659638,"teacher_disagreement_score":0.002378669,"about_ca_system_score_codex":0.00054269657,"about_ca_system_score_gemma":0.00040326777,"threshold_uncertainty_score":0.006133437},"labels":[],"label_agreement":null},{"id":"W2591619058","doi":"","title":"Laval Nozzle Production of Internal Targets","year":2013,"lang":"de","type":"article","venue":"GSI Repository (German Federal Government)","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Production (economics); Nozzle; Environmental science; Engineering; Mechanical engineering; Economics","score_opus":0.008163199543651979,"score_gpt":0.23119297878524972,"score_spread":0.22302977924159775,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2591619058","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":[0.9668406,0.00059134077,0.0076195365,0.00008229849,0.000046155365,0.000057783134,0.0005154206,0.00029896857,0.023947977],"genre_scores_gemma":[0.99076474,0.00015655083,0.0025387045,0.0000131712595,0.0000060641173,0.00001521016,0.0005462679,0.0000990262,0.005860322],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99946743,0.000053722375,0.000013465941,0.00010207383,0.00025621182,0.000107107095],"domain_scores_gemma":[0.9995907,0.000104203384,0.00006296311,0.00007031924,0.00009881456,0.00007310608],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0007411912,0.00037650397,0.00071523996,0.0005854939,0.0006991019,0.0014742371,0.0005982336,0.00063453865,0.0033988985],"category_scores_gemma":[0.0008641972,0.00018762256,0.0005986,0.0006550701,0.0005242777,0.00043863562,0.0010082398,0.0005908163,0.0009703056],"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":[0.0008201827,0.000071847455,0.004013553,0.0002350942,0.000034457604,0.00048694725,0.0004024161,0.003264808,0.97160137,0.0014881896,0.0009057679,0.01667547],"study_design_scores_gemma":[0.000068726804,0.00049945246,0.0123020895,0.000013429664,0.00003069546,0.00015163298,0.00010869396,0.0032687648,0.97928804,0.00016541826,0.0040854337,0.00001761361],"about_ca_topic_score_codex":0.001411625,"about_ca_topic_score_gemma":0.0013918113,"teacher_disagreement_score":0.0033988985,"about_ca_system_score_codex":0.0012186796,"about_ca_system_score_gemma":0.0006217071,"threshold_uncertainty_score":0.01137042},"labels":[],"label_agreement":null},{"id":"W2612467711","doi":"","title":"Determining Fleet Size for a Modernized Canadian Maritime Patrol Aircraft","year":2014,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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":"Aeronautics; Modernization theory; Range (aeronautics); Meteorology; Engineering; Operations research; Geography; Aerospace engineering; Political science; Law","score_opus":0.01495288103171262,"score_gpt":0.23990029662656495,"score_spread":0.22494741559485232,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2612467711","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":[0.9775598,0.00020414586,0.005569741,0.00013498623,0.000021892829,0.00012700594,0.003450201,0.0001012968,0.012830835],"genre_scores_gemma":[0.99161327,0.00006965275,0.0037143547,0.000019846962,0.000003330135,0.00003199756,0.0022507738,0.000018403096,0.0022785403],"study_design_codex":"observational","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993186,0.00003853083,0.000020660565,0.00009597272,0.00040131787,0.00012495936],"domain_scores_gemma":[0.998137,0.0003811089,0.00016514349,0.00006797762,0.0010993498,0.00014943992],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0007012813,0.00037769353,0.00019383796,0.0020931233,0.0007459223,0.00059554866,0.0007152413,0.0002724924,0.0038655112],"category_scores_gemma":[0.002508863,0.0001708231,0.00042229568,0.0007375607,0.00020279601,0.0006926794,0.00042653285,0.00038039227,0.0004960393],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":true,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.001992728,0.00025663493,0.49140686,0.00035436192,0.00038564796,0.0008498002,0.0006082487,0.30755824,0.06481532,0.0040098806,0.0102462275,0.11751613],"study_design_scores_gemma":[0.000060155915,0.0010709536,0.7310535,0.00007472144,0.0001796484,0.00030635967,0.0011649797,0.21127112,0.03663,0.0006809622,0.01738204,0.00012566634],"about_ca_topic_score_codex":0.43834856,"about_ca_topic_score_gemma":0.51892275,"teacher_disagreement_score":0.56165147,"about_ca_system_score_codex":0.00526403,"about_ca_system_score_gemma":0.0026089079,"threshold_uncertainty_score":0.8715942},"labels":[],"label_agreement":null},{"id":"W2619304673","doi":"","title":"Identity and distribution of residues of energetic compounds at military live-fire training ranges","year":2005,"lang":"en","type":"article","venue":"US Army Corps of Engineers: Engineer Research and Development Center (Knowledge Core)","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":16,"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":"Training (meteorology); Identity (music); Environmental science; Aeronautics; Geography; Engineering; Meteorology; Art; Aesthetics","score_opus":0.07984000931311741,"score_gpt":0.31260969157241086,"score_spread":0.23276968225929345,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2619304673","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":[0.9990526,0.00004577233,0.00014045041,0.0000028876877,4.4810918e-7,0.000008961158,0.00013048392,0.0000028783725,0.0006154446],"genre_scores_gemma":[0.9979526,0.0001300642,0.0008377707,0.000015224134,0.0000011901014,0.000011288644,0.00030067403,0.000005214828,0.000745956],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.9997008,0.000022441529,0.000011703048,0.00008188698,0.00011511302,0.0000681693],"domain_scores_gemma":[0.9996412,0.000054272983,0.000105661995,0.000013646458,0.00013741027,0.000047799913],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017690008,0.00018943415,0.00022336247,0.0011451517,0.0006271785,0.0005604906,0.00036305859,0.00024492914,0.000865849],"category_scores_gemma":[0.0003045166,0.0001886911,0.00016843194,0.00066657685,0.00049905793,0.00029276847,0.00021561405,0.00029243706,0.00017454784],"study_design_candidate":"observational","study_design_consensus":"observational","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0007546888,0.00025807202,0.6723602,0.00008295906,0.00007538963,0.00039778595,0.0008414582,0.0009730833,0.30135,0.00011484053,0.00013111923,0.022660354],"study_design_scores_gemma":[0.0000037230418,0.00027164968,0.9778542,0.000008646413,0.000013847641,0.00014674569,0.0007077953,0.0003619908,0.020329181,0.000019561705,0.00027492314,0.000007801855],"about_ca_topic_score_codex":0.053671204,"about_ca_topic_score_gemma":0.12966359,"teacher_disagreement_score":0.053671204,"about_ca_system_score_codex":0.0010238541,"about_ca_system_score_gemma":0.00049896305,"threshold_uncertainty_score":0.106717646},"labels":[],"label_agreement":null},{"id":"W2620970387","doi":"","title":"The Influence of Elliptical Nozzle Holes on Mixing and Combustion in Direct Injection Natural Gas Engines","year":2008,"lang":"en","type":"dissertation","venue":"Library and Archives Canada (Government of Canada)","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":9,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Nozzle; Combustion; Ignition system; Mechanics; Jet (fluid); Materials science; Mixing (physics); Chemistry; Nuclear engineering; Analytical Chemistry (journal); Thermodynamics; Physics; Engineering; Environmental chemistry","score_opus":0.0031181560333397376,"score_gpt":0.16443220875388834,"score_spread":0.1613140527205486,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2620970387","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":[0.99806076,0.00041324768,0.0009387386,0.000007211643,0.000008346042,0.000019063293,0.000019888017,0.000023874998,0.00050891936],"genre_scores_gemma":[0.9982482,0.0001825571,0.0011938119,0.000009368943,0.0000024862,0.000006903431,0.000024878518,0.000011904489,0.00031989452],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99942845,0.000077830955,0.000047826215,0.00012888767,0.00021301239,0.000104048355],"domain_scores_gemma":[0.99874616,0.0006301923,0.000322496,0.00006476801,0.00015634975,0.000079983765],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00080850685,0.00028627596,0.0002994293,0.0002682899,0.0003177556,0.00090109464,0.00038169615,0.0003200376,0.00076334574],"category_scores_gemma":[0.0027662197,0.000325695,0.0002169911,0.00015264748,0.00046526676,0.0005716463,0.00052660704,0.00021943766,0.00012985092],"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":[0.004557136,0.00029065917,0.021114206,0.0003110251,0.000037702273,0.0004890546,0.00042321198,0.005105953,0.93533397,0.00038307704,0.00011526655,0.03183868],"study_design_scores_gemma":[0.00014261436,0.0032819982,0.071956515,0.000032923806,0.000106842555,0.00042137288,0.0003156458,0.009729732,0.912887,0.00015623336,0.00092083367,0.00004825458],"about_ca_topic_score_codex":0.002176109,"about_ca_topic_score_gemma":0.002433774,"teacher_disagreement_score":0.002176109,"about_ca_system_score_codex":0.0006191142,"about_ca_system_score_gemma":0.00032422188,"threshold_uncertainty_score":0.004491985},"labels":[],"label_agreement":null},{"id":"W2623160192","doi":"10.1021/acs.iecr.7b00693","title":"Reduced-Order Modeling of a Commercial-Scale Gasifier Using a Multielement Injector Feed System","year":2017,"lang":"en","type":"article","venue":"Industrial & Engineering Chemistry Research","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Natural Resources Canada; University of Waterloo","funders":"Natural Resources Canada","keywords":"Injector; Wood gas generator; Process engineering; Scale (ratio); Environmental science; SCALE-UP; Computer science; Nuclear engineering; Waste management; Engineering; Mechanical engineering; Physics","score_opus":0.2210023542790115,"score_gpt":0.3759944514759707,"score_spread":0.15499209719695922,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2623160192","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":[0.40494433,0.0007912877,0.5470276,0.00043894383,0.00009003189,0.0003237844,0.0015498365,0.0016856536,0.04314851],"genre_scores_gemma":[0.95490885,0.00034841607,0.030286185,0.000057025314,0.000015007921,0.00028908518,0.0005309145,0.00013071984,0.013433688],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998301,0.00003190228,0.0000081514245,0.000039387676,0.00006664363,0.00002376517],"domain_scores_gemma":[0.99982136,0.000085616506,0.000026494696,0.000015301348,0.000043430064,0.000007951782],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002779753,0.00061772414,0.0006775225,0.000307233,0.00042399202,0.0008166712,0.0013470786,0.0014524284,0.00251095],"category_scores_gemma":[0.000452085,0.00039295547,0.0009747912,0.00027395927,0.0003683522,0.00060127315,0.0003909218,0.0007139797,0.0005294038],"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":[0.000042157073,0.000032589513,0.00040158798,0.0000441625,0.00001122519,0.0000456974,0.000029558449,0.9902802,0.0058301007,0.0012410906,0.00012537405,0.0019162764],"study_design_scores_gemma":[0.000006010216,0.000015084889,0.000103872044,0.0000016172129,0.0000036926838,0.000006250441,0.000004362745,0.9984812,0.000917842,0.000114089176,0.00034282386,0.0000031370796],"about_ca_topic_score_codex":0.020659357,"about_ca_topic_score_gemma":0.009491068,"teacher_disagreement_score":0.020659357,"about_ca_system_score_codex":0.0009725101,"about_ca_system_score_gemma":0.00091318693,"threshold_uncertainty_score":0.04107821},"labels":[],"label_agreement":null},{"id":"W2715949390","doi":"10.4050/f-0070-2014-9601","title":"Conducting Helicopter Operations in Northern Labrador and the Arctic","year":2014,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","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":true,"ca_institutions":"Government of Newfoundland and Labrador","funders":"","keywords":"Arctic; The arctic; Computer science; Aeronautics; Geography; Oceanography; Engineering; Geology","score_opus":0.03453182215106729,"score_gpt":0.26331107783577273,"score_spread":0.22877925568470545,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2715949390","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":[0.97602016,0.0007964854,0.00055014435,0.0007877092,0.000037923757,0.000096671094,0.00039637848,0.00005791237,0.021256648],"genre_scores_gemma":[0.98130625,0.00115948,0.002256253,0.000381748,0.000016522075,0.00003792317,0.00043837214,0.00002383014,0.014379621],"study_design_codex":"observational","study_design_gemma":"not_applicable","domain_scores_codex":[0.9990414,0.00017326932,0.00003235978,0.00009074002,0.00016135728,0.0005007923],"domain_scores_gemma":[0.9987632,0.000114940034,0.0001825891,0.00003577477,0.00037939925,0.00052404654],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00065058615,0.0003242633,0.00013903725,0.0005400412,0.0042149196,0.0011434882,0.0005884346,0.00035001308,0.0026383006],"category_scores_gemma":[0.0009771916,0.00018482245,0.0001799506,0.0007567151,0.0010978339,0.00037501042,0.0009231177,0.0003274953,0.0006142565],"study_design_candidate":"not_applicable","study_design_consensus":null,"about_ca_topic_candidate":true,"about_ca_topic_consensus":true,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0007829974,0.0005045155,0.6476008,0.00062602584,0.00007333513,0.008748294,0.07182284,0.0027986693,0.018903164,0.0016683972,0.015932508,0.2305384],"study_design_scores_gemma":[0.000012537146,0.00032003337,0.8213407,0.0002070738,0.000025429144,0.0011883059,0.1269149,0.00053208706,0.0015503042,0.0000981974,0.047751404,0.00005903157],"about_ca_topic_score_codex":0.9280866,"about_ca_topic_score_gemma":0.98394185,"teacher_disagreement_score":0.07191342,"about_ca_system_score_codex":0.013029582,"about_ca_system_score_gemma":0.020833813,"threshold_uncertainty_score":0.14467382},"labels":[],"label_agreement":null},{"id":"W2720533985","doi":"","title":"Numerical Modelling of Staged Combustion Aft-injected Hybrid Rocket Motors","year":2012,"lang":"en","type":"dissertation","venue":"Library and Archives Canada (Government of Canada)","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"University of Toronto; Government of Ontario; Compute Canada","keywords":"Combustion; Aerospace engineering; Rocket (weapon); Engineering; Aeronautics; Mechanical engineering; Environmental science; Chemistry","score_opus":0.006988987371934968,"score_gpt":0.16142062903510873,"score_spread":0.15443164166317377,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2720533985","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":[0.7051015,0.0007549217,0.2053104,0.0005757982,0.00017158956,0.0002793063,0.0014485446,0.0010171675,0.08534075],"genre_scores_gemma":[0.96417034,0.00031968125,0.019517705,0.000034667217,0.000016604034,0.00012860158,0.00041612663,0.0000707917,0.01532549],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998338,0.000024042507,0.000009826475,0.00002312904,0.00007706453,0.000032053787],"domain_scores_gemma":[0.9997634,0.000085695676,0.00004209126,0.000018598503,0.00006987405,0.00002041131],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021437203,0.00043766177,0.00059030094,0.00042405128,0.0005027012,0.0011870085,0.0009074766,0.0011827473,0.0029887382],"category_scores_gemma":[0.000697435,0.00026937897,0.0005594525,0.00041292387,0.0006955671,0.00044526215,0.0004897462,0.00047140665,0.00048612445],"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":[0.000031590498,0.000015698275,0.0005083244,0.000021255448,0.00000474232,0.000059386148,0.000034761182,0.99161875,0.0036374764,0.0022632307,0.00016709429,0.0016376857],"study_design_scores_gemma":[0.000005326977,0.000012752287,0.00020962012,0.000003163452,0.000001492523,0.00000807369,0.000010519238,0.99838996,0.00061052607,0.00023389922,0.0005108595,0.0000038392127],"about_ca_topic_score_codex":0.017707553,"about_ca_topic_score_gemma":0.008240099,"teacher_disagreement_score":0.017707553,"about_ca_system_score_codex":0.0011998723,"about_ca_system_score_gemma":0.0012635984,"threshold_uncertainty_score":0.035209},"labels":[],"label_agreement":null},{"id":"W2728170893","doi":"10.4050/f-0072-2016-11514","title":"Mission Ready - Completing 505 Jet Ranger X Optional Equipment Kits Development in Time for 1st Deliveries","year":2016,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","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":"Bell Helicopter Textron (Canada)","funders":"","keywords":"Jet (fluid); Computer science; Aeronautics; Engineering; Aerospace engineering","score_opus":0.05850705911209677,"score_gpt":0.29137143253106346,"score_spread":0.23286437341896668,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2728170893","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.07420751,0.00083684013,0.09135811,0.0018400908,0.0018707231,0.0027323253,0.0066046333,0.040567975,0.7799819],"genre_scores_gemma":[0.17864318,0.0009086911,0.09932669,0.000998021,0.0002637488,0.0007887945,0.0131516475,0.0064215953,0.6994977],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9979242,0.00026596387,0.00012924815,0.00020562821,0.0011772506,0.0002976888],"domain_scores_gemma":[0.99688965,0.0004400041,0.00030863218,0.0005511154,0.0013387474,0.00047194725],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.002343906,0.0007547433,0.0002660656,0.0015618586,0.0009952566,0.0025018526,0.000996782,0.00077240646,0.17459138],"category_scores_gemma":[0.00563523,0.00067037065,0.00041501757,0.0003609417,0.00043262285,0.0017943683,0.0018701142,0.0008286459,0.11838042],"study_design_candidate":"not_applicable","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":[0.00060448004,0.00051684567,0.007341334,0.00067155063,0.00001740405,0.0012443034,0.0013118683,0.0016017006,0.03936152,0.014663808,0.33739856,0.59526664],"study_design_scores_gemma":[0.00009447771,0.0013296084,0.015876131,0.0002470377,0.000013896433,0.0013907577,0.0006579939,0.0011164394,0.028232597,0.0016757944,0.9492932,0.00007215335],"about_ca_topic_score_codex":0.002828538,"about_ca_topic_score_gemma":0.0042607468,"teacher_disagreement_score":0.17459138,"about_ca_system_score_codex":0.0009715501,"about_ca_system_score_gemma":0.003232924,"threshold_uncertainty_score":0.58406633},"labels":[],"label_agreement":null},{"id":"W2728459918","doi":"10.4050/f-0073-2017-12151","title":"Engine Inlet Performance Analysis for the V-280 Demonstrator","year":2017,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","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":"Bell Helicopter Textron (Canada)","funders":"","keywords":"Inlet; Computer science; Automotive engineering; Engineering; Mechanical engineering","score_opus":0.04077467353821627,"score_gpt":0.2897646629452648,"score_spread":0.24898998940704856,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2728459918","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":[0.9787089,0.00016364375,0.013444547,0.000046887268,0.000016747197,0.00006260415,0.0003187814,0.0004323272,0.006805387],"genre_scores_gemma":[0.99197876,0.00007577781,0.0036875585,0.000019234214,0.000004504012,0.000034023964,0.00049412414,0.00007742774,0.0036285415],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995413,0.00004671629,0.000025332634,0.000086020416,0.00023959731,0.00006098894],"domain_scores_gemma":[0.9993594,0.00015612398,0.00006186732,0.00005177907,0.0003345958,0.00003622886],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0007818409,0.00048312597,0.0005457105,0.00080190663,0.0004538606,0.0005705038,0.0010071765,0.0005977953,0.0036669092],"category_scores_gemma":[0.0011166161,0.0001991592,0.0004111643,0.00033549994,0.000307274,0.0005152031,0.0005238693,0.0004724841,0.0010009749],"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":[0.0029987027,0.0004554729,0.018661326,0.0008754973,0.00011982198,0.000971694,0.00080207165,0.0775604,0.8129164,0.0015220457,0.0024067853,0.08070978],"study_design_scores_gemma":[0.00015502903,0.0070250044,0.028899956,0.00006511388,0.00009254594,0.0007742889,0.0004607514,0.100991614,0.8536521,0.00022727823,0.0075494223,0.00010696131],"about_ca_topic_score_codex":0.0013313105,"about_ca_topic_score_gemma":0.0016133194,"teacher_disagreement_score":0.0036669092,"about_ca_system_score_codex":0.00053198886,"about_ca_system_score_gemma":0.00035505794,"threshold_uncertainty_score":0.012267053},"labels":[],"label_agreement":null},{"id":"W2729238602","doi":"10.2514/6.2017-4903","title":"Acceleration Effects on Acoustic Instability of Hybrid Rocket Engine","year":2017,"lang":"en","type":"article","venue":"53rd AIAA/SAE/ASEE Joint Propulsion Conference","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Acceleration; Rocket (weapon); Aerospace engineering; Instability; Rocket engine; Computer science; Acoustics; Aeronautics; Physics; Engineering; Mechanics; Classical mechanics","score_opus":0.05274491058722794,"score_gpt":0.2854943681277771,"score_spread":0.23274945754054918,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2729238602","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":[0.997122,0.00010754921,0.0006904112,0.00003085412,0.000015323036,0.000005384701,0.000027677139,0.000041332878,0.0019595583],"genre_scores_gemma":[0.9994678,0.000025307469,0.000039526032,0.0000046713276,0.0000056056897,0.0000012253524,0.000017411592,0.000007773338,0.00043068244],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999261,0.000010352303,0.0000029933146,0.0000105819645,0.000024031382,0.000025895904],"domain_scores_gemma":[0.99962294,0.00020818257,0.000037764294,0.00001437386,0.00007281341,0.000043882155],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001239876,0.000225009,0.00024420812,0.00032845052,0.00023694409,0.0003753962,0.00018491976,0.00028619875,0.0045739687],"category_scores_gemma":[0.00063048437,0.0001766865,0.00018648342,0.00014292354,0.00022266187,0.0002553614,0.0003012105,0.00032305004,0.00045207923],"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":[0.0058141043,0.00018822613,0.012052702,0.000145494,0.00006555765,0.0014533653,0.000335308,0.035054978,0.9215746,0.0008052006,0.00045749574,0.022052871],"study_design_scores_gemma":[0.00022738008,0.0018434033,0.22803518,0.00003990795,0.00015608301,0.0006293677,0.0005416175,0.33160025,0.43391666,0.0008375427,0.002052057,0.00012058699],"about_ca_topic_score_codex":0.0013428682,"about_ca_topic_score_gemma":0.00084256486,"teacher_disagreement_score":0.0045739687,"about_ca_system_score_codex":0.00019178684,"about_ca_system_score_gemma":0.00011826072,"threshold_uncertainty_score":0.015301466},"labels":[],"label_agreement":null},{"id":"W2731469206","doi":"10.4050/f-0073-2017-12100","title":"Affordable Design and Manufacturing of the V-280 Wing","year":2017,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","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":"Bell Helicopter Textron (Canada)","funders":"","keywords":"Wing; Computer science; Manufacturing engineering; Engineering; Aerospace engineering","score_opus":0.04103172228343997,"score_gpt":0.2643999978200261,"score_spread":0.22336827553658611,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2731469206","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":[0.25291675,0.000820002,0.54261386,0.00063697225,0.00033482668,0.0007269992,0.0010394286,0.0030896363,0.19782157],"genre_scores_gemma":[0.70643383,0.00041042073,0.25116354,0.00017241409,0.000044581073,0.00022782676,0.0009563158,0.00024163061,0.040349483],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9995776,0.00002980107,0.000011083613,0.000041446092,0.0002918928,0.000048197435],"domain_scores_gemma":[0.99981695,0.000010827822,0.000027634023,0.000040299663,0.00007116289,0.000033097036],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00043815814,0.0002998498,0.00021865343,0.00033005673,0.00037068507,0.00061698095,0.00065658306,0.0004288913,0.0058913254],"category_scores_gemma":[0.00029804852,0.000212469,0.00027188024,0.00016733348,0.00023856945,0.00030350272,0.0006683188,0.00045521327,0.002259499],"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":[0.00025390403,0.00010513326,0.003908261,0.00041502013,0.000023205874,0.0005502247,0.0002598999,0.030718569,0.6613224,0.04340671,0.014350875,0.24468566],"study_design_scores_gemma":[0.00013781458,0.0040091285,0.013007402,0.0000909503,0.000036771886,0.002349211,0.00023875282,0.10788576,0.4523866,0.0041810395,0.41557938,0.000097211705],"about_ca_topic_score_codex":0.00065638375,"about_ca_topic_score_gemma":0.001281125,"teacher_disagreement_score":0.0058913254,"about_ca_system_score_codex":0.00053407194,"about_ca_system_score_gemma":0.00067819044,"threshold_uncertainty_score":0.019708455},"labels":[],"label_agreement":null},{"id":"W2734470457","doi":"10.4050/f-0071-2015-10233","title":"V-22 Osprey Maintenance Cost Savings using SAFE for Fatigue Life Calculations","year":2015,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","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":"Bell Helicopter Textron (Canada)","funders":"","keywords":"Reliability engineering; Computer science; Engineering","score_opus":0.19821053636004313,"score_gpt":0.35920795680698,"score_spread":0.16099742044693685,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2734470457","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":[0.49723905,0.0016458309,0.26632077,0.0007767982,0.00031513578,0.00063706556,0.02922033,0.022084884,0.18176018],"genre_scores_gemma":[0.8484867,0.00040130707,0.11158429,0.00009489014,0.00003477194,0.0002431431,0.013829523,0.0018462327,0.02347914],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9992762,0.00012498398,0.000028021579,0.0000571165,0.0004447858,0.00006894574],"domain_scores_gemma":[0.9990771,0.0002284488,0.00008367493,0.00009767973,0.00047754063,0.00003548491],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006188963,0.00077653676,0.0004797989,0.0021031708,0.00031012198,0.0009366776,0.0009396099,0.00034255706,0.012471839],"category_scores_gemma":[0.0026733517,0.00037810585,0.0007419459,0.0009232435,0.00010284387,0.00090503856,0.00036326094,0.0003467329,0.0028295075],"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":[0.00063459127,0.00018244368,0.012167333,0.0003300929,0.00017214924,0.00025088998,0.000107480926,0.5733285,0.0076786024,0.010562717,0.07462592,0.31995934],"study_design_scores_gemma":[0.00009787864,0.00045453227,0.01610552,0.00007309061,0.00014115698,0.0002253001,0.000117780444,0.92911947,0.0087209465,0.0042011095,0.040663794,0.00007945647],"about_ca_topic_score_codex":0.024596522,"about_ca_topic_score_gemma":0.03419125,"teacher_disagreement_score":0.024596522,"about_ca_system_score_codex":0.0018009098,"about_ca_system_score_gemma":0.0015653318,"threshold_uncertainty_score":0.048906684},"labels":[],"label_agreement":null},{"id":"W2743058533","doi":"10.1299/jsmemecjo.2010.5.0_407","title":"G1900-1-3 Effect of heat transfer in supersonic region of Laval nozzle on thrust and specific impulse","year":2010,"lang":"en","type":"article","venue":"The proceedings of the JSME annual meeting","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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":"Isentropic process; Mechanics; Specific impulse; Heat transfer; Propellant; Stagnation temperature; Stagnation point; Thermodynamics; Nozzle; Impulse (physics); Equivalence point; Materials science; Thrust; Chemistry; Physics; Classical mechanics","score_opus":0.008845526445591603,"score_gpt":0.22586737794801837,"score_spread":0.21702185150242675,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2743058533","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":[0.9891984,0.00026289411,0.0020480796,0.00004359561,0.000018179526,0.000007612064,0.00011204916,0.00012901405,0.008180273],"genre_scores_gemma":[0.998466,0.00006396455,0.00039874218,0.000007897727,0.000002415938,0.0000024818332,0.00008302951,0.00002874224,0.0009467228],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99989796,0.000016457368,0.000002131858,0.000012980368,0.000034989487,0.00003537382],"domain_scores_gemma":[0.99977285,0.0001356978,0.000023463197,0.000011254534,0.000034144126,0.000022596145],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020538902,0.00016804293,0.0001916967,0.00017805911,0.000101443744,0.00036204004,0.00019627938,0.00021318269,0.0038040404],"category_scores_gemma":[0.0004374432,0.000074339485,0.0002089596,0.00016414351,0.0003752343,0.00018163498,0.0001885411,0.00018418647,0.00042216523],"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":[0.0018039515,0.00012783926,0.011940694,0.00029458784,0.000070472335,0.00062858383,0.00017896254,0.10764694,0.8512546,0.0022852577,0.0015905938,0.022177644],"study_design_scores_gemma":[0.0001331436,0.001417724,0.057585984,0.000037716753,0.000052073145,0.00037630706,0.00023139085,0.30182046,0.6321979,0.0005471962,0.0055532935,0.0000467559],"about_ca_topic_score_codex":0.0025144648,"about_ca_topic_score_gemma":0.0015563605,"teacher_disagreement_score":0.0038040404,"about_ca_system_score_codex":0.00042326679,"about_ca_system_score_gemma":0.00020408908,"threshold_uncertainty_score":0.0127257705},"labels":[],"label_agreement":null},{"id":"W2743076070","doi":"10.1299/jsmemecjo.2009.5.0_297","title":"S1904-2-2 Improvement of thrust and specific impulse by convective heat transfer in Laval nozzle","year":2009,"lang":"en","type":"article","venue":"The proceedings of the JSME annual meeting","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":1,"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; Specific impulse; Heat transfer; Mechanics; Materials science; Inlet; Thrust; Thermodynamics; Chemistry; Mechanical engineering; Aerospace engineering; Physics; Engineering","score_opus":0.00749549074650265,"score_gpt":0.21968183062879265,"score_spread":0.21218633988229,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2743076070","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":[0.9223474,0.0010931772,0.043336075,0.000115216135,0.000107459426,0.000044419863,0.0003366181,0.0009029716,0.031716608],"genre_scores_gemma":[0.9861222,0.00014456261,0.008590755,0.0000073944975,0.00000894934,0.0000118151665,0.00021761168,0.00008480692,0.0048118844],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99980336,0.000017836823,0.0000061969845,0.00001813635,0.00011723883,0.00003716851],"domain_scores_gemma":[0.99981505,0.000035792404,0.000026744352,0.000016457887,0.00008972956,0.00001633791],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00035470913,0.00019649042,0.0002736191,0.00032443926,0.00017046076,0.000479115,0.00033866047,0.00021458596,0.0028719218],"category_scores_gemma":[0.00038075994,0.000076822944,0.00029118455,0.00029864698,0.00020637542,0.00029935737,0.00028547848,0.0001721111,0.0005800193],"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":[0.000441442,0.00009629174,0.005532128,0.00021070756,0.000024010067,0.00017525455,0.00013512357,0.0229858,0.92211163,0.004146145,0.0016622972,0.042479213],"study_design_scores_gemma":[0.00008913605,0.00048046093,0.0133171,0.000021304817,0.000032798634,0.0002545029,0.000056201527,0.15767542,0.80985653,0.0005248222,0.01765148,0.000040251394],"about_ca_topic_score_codex":0.00072799873,"about_ca_topic_score_gemma":0.0005540364,"teacher_disagreement_score":0.0028719218,"about_ca_system_score_codex":0.000535302,"about_ca_system_score_gemma":0.0003481461,"threshold_uncertainty_score":0.0096075535},"labels":[],"label_agreement":null},{"id":"W2744074458","doi":"10.1299/jsmemecjo.2008.5.0_395","title":"4037 Improvement of the thrust and specific impulse by elongating and heating the Laval nozzle","year":2008,"lang":"en","type":"article","venue":"The proceedings of the JSME annual meeting","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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; Specific impulse; Thrust; Inlet; Impulse (physics); Materials science; Mechanics; Mass flow rate; Rocket engine nozzle; Discharge coefficient; Aerospace engineering; Mechanical engineering; Physics; Engineering; Classical mechanics","score_opus":0.010095303401038733,"score_gpt":0.21083882847789032,"score_spread":0.2007435250768516,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2744074458","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":[0.97313154,0.00048676337,0.01718999,0.00005251107,0.000040655654,0.000018583663,0.00007905174,0.0003119879,0.008689014],"genre_scores_gemma":[0.9891985,0.00012224956,0.0067393584,0.000011358873,0.0000069548864,0.000008463203,0.00008612995,0.000055254848,0.0037716706],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998379,0.000009197607,0.0000077154655,0.000018689574,0.00008374145,0.00004265034],"domain_scores_gemma":[0.9997973,0.000044792137,0.000032635955,0.000033314158,0.000062571125,0.000029360108],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003471343,0.00016632686,0.0002718157,0.0002211691,0.00017104362,0.0003952555,0.00027363191,0.00018708146,0.002284097],"category_scores_gemma":[0.0004855796,0.0000879477,0.0002140522,0.00018815481,0.00025634837,0.00029086188,0.00042695348,0.00028808933,0.00042075367],"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":[0.0002410725,0.000050874907,0.0023777953,0.00007400137,0.000007891922,0.00013647173,0.000113574926,0.005863526,0.9605578,0.0012781628,0.00030003302,0.028998917],"study_design_scores_gemma":[0.000025447285,0.00026072588,0.0064186524,0.000008991341,0.000012996284,0.00013908694,0.000043375723,0.017984573,0.96810424,0.0001231233,0.006858996,0.000019743698],"about_ca_topic_score_codex":0.00048794504,"about_ca_topic_score_gemma":0.00038842438,"teacher_disagreement_score":0.002284097,"about_ca_system_score_codex":0.00044537292,"about_ca_system_score_gemma":0.00027236954,"threshold_uncertainty_score":0.0076411366},"labels":[],"label_agreement":null},{"id":"W2744612681","doi":"10.71781/32193","title":"Effets protecteurs d'un donneur de NO sur la fonction diastolique du coeur défaillant de hamster UM-X7.1","year":2003,"lang":"fr","type":"dissertation","venue":"Open MIND","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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":"Medicine; Biology","score_opus":0.01776202358717232,"score_gpt":0.2833721764625971,"score_spread":0.2656101528754248,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2744612681","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":[0.99188995,0.005351147,0.0008426625,0.00020830406,0.00018650151,0.000028773537,0.0003439486,0.000043124714,0.0011057429],"genre_scores_gemma":[0.9885324,0.0032744682,0.00089297595,0.00018351722,0.000084641506,0.000048648933,0.0005970699,0.000048660622,0.0063377144],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9996075,0.000099916026,0.000028514192,0.00009297562,0.000066601155,0.00010449861],"domain_scores_gemma":[0.99840826,0.0009259784,0.00016304167,0.00015295505,0.00015002466,0.00019970702],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005926998,0.000492671,0.0007974025,0.00019294806,0.000338936,0.00044278285,0.00036042472,0.0008587308,0.006320369],"category_scores_gemma":[0.0016181938,0.0002718587,0.0005244623,0.00014849033,0.000568175,0.00033313708,0.00027438192,0.0005856697,0.00052823185],"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":[0.029568784,0.00036178125,0.0021325643,0.00041179036,0.00027783844,0.00019888626,0.00027109086,0.0004431066,0.9518583,0.0003119844,0.000574393,0.013589524],"study_design_scores_gemma":[0.00048870285,0.015193568,0.017261615,0.00008664509,0.0005557263,0.00029915725,0.00023200034,0.0014476684,0.9591818,0.0002403968,0.004973635,0.000039086564],"about_ca_topic_score_codex":0.0036323608,"about_ca_topic_score_gemma":0.0027657659,"teacher_disagreement_score":0.006320369,"about_ca_system_score_codex":0.00025036643,"about_ca_system_score_gemma":0.0003041397,"threshold_uncertainty_score":0.021143675},"labels":[],"label_agreement":null},{"id":"W2748128571","doi":"10.11159/ffhmt17.110","title":"Computational Analysis of Bell Nozzles","year":2017,"lang":"en","type":"article","venue":"Proceedings of the ... International Conference on Fluid Flow, Heat and Mass Transfer","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":17,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Computer science","score_opus":0.036112962828878284,"score_gpt":0.2787539011926578,"score_spread":0.24264093836377953,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2748128571","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":[0.20909601,0.0013401031,0.6921599,0.0006665751,0.0003942623,0.0004598967,0.0031022863,0.002114615,0.09066638],"genre_scores_gemma":[0.74601096,0.00097311096,0.22062974,0.00027893513,0.00008519694,0.000993924,0.0034176663,0.0005474005,0.027063137],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99965274,0.00005771162,0.000022535134,0.000060172886,0.00012254999,0.00008432236],"domain_scores_gemma":[0.9995011,0.00021139909,0.0000471849,0.000036155736,0.00016354033,0.000040559255],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005388262,0.000633567,0.0010994567,0.0007052772,0.00091795827,0.0014883959,0.001244816,0.0014670136,0.011818588],"category_scores_gemma":[0.0015263647,0.00034742645,0.0009962611,0.0006996132,0.0005612661,0.00068770465,0.0011917118,0.000811705,0.0012734024],"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":[0.00008373583,0.00004778788,0.0018649632,0.00018718383,0.00001967218,0.00034387718,0.00013475455,0.95405436,0.0055209235,0.017972924,0.0027897335,0.01698011],"study_design_scores_gemma":[0.000012191588,0.000029912339,0.00036112376,0.000015700627,0.000004359645,0.000062800354,0.000033287586,0.9927108,0.0010741497,0.0016869853,0.003995025,0.000013668849],"about_ca_topic_score_codex":0.006589697,"about_ca_topic_score_gemma":0.0027957936,"teacher_disagreement_score":0.011818588,"about_ca_system_score_codex":0.0007735935,"about_ca_system_score_gemma":0.0013745917,"threshold_uncertainty_score":0.03953713},"labels":[],"label_agreement":null},{"id":"W2751993223","doi":"10.5281/zenodo.1336050","title":"Application Of De-Laval Nozzle Transonic Flow Field Computation Approaches","year":2013,"lang":"en","type":"article","venue":"Zenodo (CERN European Organization for Nuclear Research)","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":1,"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":"Transonic; Nozzle; Computation; Subsonic and transonic wind tunnel; Mechanics; Field (mathematics); Aerospace engineering; Physics; Computer science; Engineering; Mathematics; Aerodynamics; Algorithm","score_opus":0.03576262147102299,"score_gpt":0.2284127720738489,"score_spread":0.19265015060282592,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2751993223","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":[0.020918254,0.00012102705,0.9680301,0.000048288235,0.000040350875,0.00006453489,0.0000763108,0.00061239046,0.010088811],"genre_scores_gemma":[0.4825461,0.000380924,0.5067255,0.00006316483,0.00004435234,0.00023266127,0.00034577344,0.00045126292,0.009210303],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999765,0.000055133223,0.000017268281,0.000041607767,0.00009147022,0.00002955051],"domain_scores_gemma":[0.9995442,0.00014739232,0.00003848752,0.00007177413,0.00017131645,0.000026735297],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00046476495,0.0006477377,0.00060942315,0.0007983465,0.00035569674,0.0009423645,0.0013864759,0.00073229254,0.002825798],"category_scores_gemma":[0.001430331,0.00030233344,0.0006052234,0.0005304974,0.00045406717,0.00092108076,0.0008801881,0.0007524954,0.0005795995],"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":[0.00011072897,0.00009293243,0.0016330228,0.00013936502,0.000037730984,0.00020775905,0.00018280234,0.8016995,0.02722777,0.09072081,0.0011188383,0.076828726],"study_design_scores_gemma":[0.0000065615,0.000016361731,0.00011287914,0.0000033078516,0.0000017776766,0.000023953773,0.000009163616,0.9940446,0.0027639403,0.0015961372,0.0014152864,0.0000060907637],"about_ca_topic_score_codex":0.0038476835,"about_ca_topic_score_gemma":0.0020873076,"teacher_disagreement_score":0.0038476835,"about_ca_system_score_codex":0.00090143475,"about_ca_system_score_gemma":0.0008565163,"threshold_uncertainty_score":0.009453237},"labels":[],"label_agreement":null},{"id":"W2783054502","doi":"10.2514/6.2018-0409","title":"Multi-Objective Optimization of a Supersonic Rocket Based Combined Cycle Inlet Through Differential Evolution","year":2018,"lang":"en","type":"article","venue":"2018  AIAA Aerospace Sciences Meeting","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Carleton University","funders":"","keywords":"Supersonic speed; Inlet; Rocket (weapon); Differential evolution; Aerospace engineering; Differential (mechanical device); Computer science; Aeronautics; Environmental science; Marine engineering; Engineering; Mechanical engineering; Artificial intelligence","score_opus":0.025991699753187526,"score_gpt":0.27858439909107074,"score_spread":0.2525926993378832,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2783054502","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":[0.46356374,0.00077678816,0.47900486,0.00043778922,0.0002566151,0.0002873682,0.0004951184,0.0005998153,0.054577827],"genre_scores_gemma":[0.95012695,0.0001459014,0.03533245,0.00007025694,0.000027472004,0.00022316964,0.0002685345,0.00008275141,0.013722485],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998196,0.00003585854,0.0000057813554,0.000033804346,0.00005445071,0.000050513216],"domain_scores_gemma":[0.99969995,0.00013650327,0.000032189233,0.0000169034,0.00006203549,0.00005242637],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005173087,0.00088056433,0.0017193558,0.0007687752,0.00092387316,0.001547528,0.0011032379,0.0021387627,0.0059165186],"category_scores_gemma":[0.0008156007,0.00070280273,0.000987965,0.00058105594,0.000611444,0.0006377435,0.0012926427,0.00095167564,0.0004929446],"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":[0.000043455177,0.000023425366,0.0002080151,0.00002350694,0.000013659402,0.00004999228,0.000009401838,0.9959235,0.00078017125,0.0004907932,0.00013184368,0.0023022431],"study_design_scores_gemma":[0.0000092272885,0.000039710743,0.00010612896,0.0000027460237,0.0000056395934,0.0000043888913,0.0000072815183,0.99926263,0.00026580348,0.000113188515,0.00018020273,0.0000031163565],"about_ca_topic_score_codex":0.013358403,"about_ca_topic_score_gemma":0.012285779,"teacher_disagreement_score":0.013358403,"about_ca_system_score_codex":0.0009860412,"about_ca_system_score_gemma":0.001685055,"threshold_uncertainty_score":0.02656132},"labels":[],"label_agreement":null},{"id":"W2783492097","doi":"10.2514/6.2018-1711","title":"AMTech CAPE Turbine Materials Standards Road Map: An Industry-Led Road Map Supporting the Next Generation of Power and Propulsion Manufacturing, Maintenance and Repair","year":2018,"lang":"en","type":"article","venue":"2018  AIAA Aerospace Sciences Meeting","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"National Institute of Standards and Technology; Ontario Advanced Manufacturing Consortium; Coordenação de Aperfeiçoamento de Pessoal de Nível Superior","keywords":"Propulsion; Turbine; Road map; Automotive engineering; Computer science; Engineering; Aerospace engineering; Cartography; Geography","score_opus":0.03795789453056213,"score_gpt":0.30503441901239803,"score_spread":0.2670765244818359,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2783492097","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.013578221,0.001777833,0.058865767,0.009878638,0.0033601003,0.0021836637,0.13228771,0.008813451,0.7692547],"genre_scores_gemma":[0.141115,0.0057943803,0.19178161,0.0032614022,0.00072368444,0.0036902013,0.28846377,0.0039399345,0.36122996],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.9984388,0.00011390169,0.000050439463,0.00008094768,0.0011449442,0.00017094542],"domain_scores_gemma":[0.99238867,0.00035608668,0.0002728146,0.00026899617,0.006223388,0.0004899815],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0013171567,0.0009627527,0.00052240555,0.0051861396,0.0019325828,0.0034830254,0.0013554269,0.002098178,0.06886243],"category_scores_gemma":[0.0053146677,0.00052498427,0.00046945843,0.008010171,0.0006520455,0.0031155488,0.0014515808,0.0021199782,0.02899961],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00013993189,0.00026026097,0.002912594,0.0006693914,0.000018259412,0.00015037159,0.00022667483,0.0046169553,0.0028853947,0.019856172,0.8358155,0.13244851],"study_design_scores_gemma":[0.000027080963,0.000046830504,0.005507777,0.00013531576,0.000008905333,0.0000398497,0.00037282112,0.0023878545,0.0008608073,0.003535579,0.98705196,0.000025215935],"about_ca_topic_score_codex":0.098997295,"about_ca_topic_score_gemma":0.11682862,"teacher_disagreement_score":0.098997295,"about_ca_system_score_codex":0.0025709488,"about_ca_system_score_gemma":0.017478306,"threshold_uncertainty_score":0.23036778},"labels":[],"label_agreement":null},{"id":"W2801482129","doi":"","title":"Two – Dimensional Euler Computations of a Laval Nozzle Done Through the Finite Volume Method","year":2009,"lang":"ru","type":"article","venue":"Механика, Транспорт, Комуникации - Научно списание,","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Nozzle; Euler's formula; Computation; Finite volume method; Mathematics; Volume (thermodynamics); Mathematical analysis; Calculus (dental); Computer science; Mechanical engineering; Mechanics; Engineering; Physics; Algorithm; Medicine; Thermodynamics","score_opus":0.03805763505834117,"score_gpt":0.3414758438139763,"score_spread":0.3034182087556351,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2801482129","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":[0.67137355,0.0006853402,0.27610928,0.0007286431,0.00032335162,0.00017682009,0.00075528724,0.0016330875,0.048214644],"genre_scores_gemma":[0.9491038,0.0001512574,0.044762686,0.00006597928,0.00003323793,0.000059925642,0.00022665987,0.00020650828,0.0053900015],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99986124,0.000034148445,0.000009196462,0.000018134995,0.00004094532,0.000036219644],"domain_scores_gemma":[0.99942976,0.00032037334,0.000059435057,0.00003772806,0.00008784476,0.00006486002],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00039231,0.00050236116,0.0009967663,0.0005409005,0.00088324735,0.0010745913,0.001087918,0.0012740192,0.0053956597],"category_scores_gemma":[0.0015120483,0.0005196153,0.00054968474,0.0006832956,0.000979437,0.00065998785,0.0007098304,0.0007388397,0.00036982188],"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":[0.00009557935,0.00004061468,0.0010127675,0.000048524693,0.000017639293,0.00021004361,0.000094278446,0.9830738,0.00289718,0.008103791,0.0003113066,0.004094408],"study_design_scores_gemma":[0.000024950741,0.000013707011,0.0002663492,0.0000060596026,0.0000030670465,0.000016127735,0.000022147167,0.99783295,0.00052721956,0.00081963284,0.0004588267,0.000009041181],"about_ca_topic_score_codex":0.016697537,"about_ca_topic_score_gemma":0.008350853,"teacher_disagreement_score":0.016697537,"about_ca_system_score_codex":0.00089019316,"about_ca_system_score_gemma":0.0015389171,"threshold_uncertainty_score":0.03320068},"labels":[],"label_agreement":null},{"id":"W2802289436","doi":"10.1139/tcsme-2005-0005","title":"A COMPUTATIONAL STUDY TO PREDICT THE COMBINED EFFECTS OF SURFACE ROUGHNESS AND HEAT FLUX CONDITIONS ON CONVERGING-NOZZLE FLOWS","year":2005,"lang":"en","type":"article","venue":"Transactions of the Canadian Society for Mechanical Engineering","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":6,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Nozzle; Mechanics; Surface roughness; Flux (metallurgy); Heat flux; Materials science; Computational fluid dynamics; Surface finish; Surface (topology); Environmental science; Mechanical engineering; Heat transfer; Physics; Engineering; Geometry; Mathematics; Composite material","score_opus":0.009015049595079596,"score_gpt":0.23267869029165317,"score_spread":0.22366364069657357,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2802289436","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":[0.9178583,0.00023029881,0.07701485,0.000062662366,0.000026492029,0.00006404701,0.00007712757,0.00019606047,0.00447017],"genre_scores_gemma":[0.9761202,0.00018982115,0.022740556,0.000014959237,0.000007235733,0.00002998799,0.000077869394,0.000027068158,0.0007922623],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998598,0.000034355824,0.0000067144265,0.000019233237,0.000061002793,0.000018929853],"domain_scores_gemma":[0.99949753,0.00026265628,0.00003418835,0.00006974083,0.0001097124,0.000026123596],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00045329912,0.00045216584,0.00056190195,0.00021476076,0.0004079945,0.0006764934,0.00046730443,0.00047421918,0.0005026703],"category_scores_gemma":[0.0019250427,0.00023860631,0.00044841308,0.00037930644,0.0004921028,0.00047501113,0.0002824046,0.0005385915,0.00007377501],"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":[0.000055058048,0.000069881564,0.0032642882,0.000047115973,0.00001649709,0.00008609222,0.000045274013,0.97623605,0.010064007,0.0019322631,0.00010938996,0.008074119],"study_design_scores_gemma":[0.0000057615453,0.00005402716,0.000808544,0.000002392383,0.0000041520707,0.0000210629,0.0000077922705,0.9958198,0.0030364671,0.00014692887,0.00008955332,0.0000035958337],"about_ca_topic_score_codex":0.0076032453,"about_ca_topic_score_gemma":0.0039860164,"teacher_disagreement_score":0.0076032453,"about_ca_system_score_codex":0.00037334778,"about_ca_system_score_gemma":0.0010515959,"threshold_uncertainty_score":0.015118003},"labels":[],"label_agreement":null},{"id":"W2806150383","doi":"10.11159/ffhmt18.158","title":"On the Performance Degradation of Centrifugal Pumps","year":2018,"lang":"en","type":"article","venue":"Proceedings of the ... International Conference on Fluid Flow, Heat and Mass Transfer","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":9,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"University of Guelph","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Degradation (telecommunications); Centrifugal pump; Computer science; Process engineering; Environmental science; Mechanical engineering; Engineering; Impeller; Telecommunications","score_opus":0.02959190981581181,"score_gpt":0.24305825345320764,"score_spread":0.21346634363739583,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2806150383","genre_codex":"review","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":[0.0137539385,0.97130865,0.01005968,0.000534184,0.0004642355,0.000030134384,0.00007785065,0.000090533744,0.0036809011],"genre_scores_gemma":[0.081877224,0.9070606,0.004822349,0.0007141574,0.000883445,0.00004611204,0.00019663919,0.000044519074,0.0043549906],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9978434,0.00029519026,0.00021051257,0.00040001963,0.0011259349,0.00012497463],"domain_scores_gemma":[0.9961825,0.0015602913,0.00050336064,0.00009031656,0.0016018049,0.000061699415],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0022611292,0.0010436717,0.0012723433,0.002438205,0.0003342598,0.0012101935,0.00088268326,0.0011684363,0.0010591621],"category_scores_gemma":[0.0030932587,0.00041557022,0.00068327575,0.0020218694,0.0006056943,0.0016892554,0.000538847,0.001114675,0.00086431665],"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":[0.00035436844,0.00016611537,0.002820937,0.016788214,0.00017846732,0.0005512358,0.00036788656,0.00756939,0.066266835,0.004661752,0.011879199,0.8883956],"study_design_scores_gemma":[0.00002369313,0.0030121792,0.01479724,0.006273345,0.00059462676,0.0046293945,0.00045920457,0.01008065,0.1991815,0.0026598389,0.7579974,0.00029081706],"about_ca_topic_score_codex":0.0013199622,"about_ca_topic_score_gemma":0.0005925891,"teacher_disagreement_score":0.002438205,"about_ca_system_score_codex":0.0009108749,"about_ca_system_score_gemma":0.00058975857,"threshold_uncertainty_score":0.011958122},"labels":[],"label_agreement":null},{"id":"W2809936242","doi":"10.2514/6.2018-3803","title":"Low Speed Infrared Development for the Lockheed Martin Aerodynamic Development Facilities","year":2018,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","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":"Lockheed Martin (Canada)","funders":"","keywords":"Aerodynamics; Aerospace engineering; Development (topology); Infrared; Aeronautics; Automotive engineering; Computer science; Engineering; Physics; Optics","score_opus":0.0285747690952125,"score_gpt":0.25620351217613685,"score_spread":0.22762874308092435,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2809936242","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":[0.2897569,0.0030455736,0.33929387,0.00722891,0.0025058526,0.0025053436,0.008280034,0.02539029,0.32199317],"genre_scores_gemma":[0.4174099,0.0009573481,0.19824746,0.00074014475,0.00032745925,0.001065596,0.010391298,0.0025683353,0.36829257],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9978567,0.00020076486,0.000023304672,0.00017325938,0.0013003782,0.0004455157],"domain_scores_gemma":[0.9962255,0.00034727005,0.00021100348,0.00037313424,0.0020940248,0.00074895105],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0040040053,0.0010140521,0.00040952998,0.0021019082,0.0018813807,0.0008113072,0.0016713508,0.0007342793,0.052963722],"category_scores_gemma":[0.0023083824,0.00051729096,0.0005456018,0.0006550558,0.0006822184,0.0012186448,0.0018901799,0.0021011042,0.013601944],"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":[0.0028184336,0.00062059757,0.015061178,0.0006205633,0.000050904408,0.0005782824,0.0011370633,0.0035024448,0.38715294,0.029407745,0.21227881,0.346771],"study_design_scores_gemma":[0.00064596045,0.0050903517,0.028829416,0.00023027313,0.00007162343,0.0009896214,0.00036298166,0.012471322,0.2085799,0.0016627009,0.74096024,0.00010556082],"about_ca_topic_score_codex":0.004507321,"about_ca_topic_score_gemma":0.010171338,"teacher_disagreement_score":0.052963722,"about_ca_system_score_codex":0.002240627,"about_ca_system_score_gemma":0.0058501605,"threshold_uncertainty_score":0.1771813},"labels":[],"label_agreement":null},{"id":"W2810726497","doi":"10.4050/f-0074-2018-12880","title":"Joint Multi-Role Technology Demonstrator Fuselage Proof Test","year":2018,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","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":"Lockheed Martin (Canada)","funders":"","keywords":"Fuselage; Lift (data mining); Flight test; Aerospace engineering; Missile; Engineering; Joint (building); Aeronautics; Flight envelope; Systems engineering; Aviation; Computer science; Automotive engineering; Reliability engineering; Simulation; Structural engineering","score_opus":0.024549591090634003,"score_gpt":0.2597386247441251,"score_spread":0.23518903365349111,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2810726497","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":[0.83594936,0.00032838347,0.10132954,0.0006044573,0.0005499459,0.0013261529,0.00248479,0.00472364,0.052703656],"genre_scores_gemma":[0.94885707,0.00012856582,0.018895097,0.00017286338,0.000031076754,0.00043917773,0.0016614497,0.00029895414,0.029515728],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9989278,0.00008833059,0.00006106735,0.00016858744,0.0005954755,0.00015868711],"domain_scores_gemma":[0.9985089,0.00027962154,0.00010653812,0.00028739023,0.00065910816,0.00015843037],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0010562596,0.000847336,0.00034339982,0.000616598,0.00047390375,0.00049872836,0.0012305294,0.0013134705,0.010633898],"category_scores_gemma":[0.0019136255,0.00022011323,0.0002952765,0.0002607151,0.0003312897,0.0011962759,0.0008765077,0.00069721165,0.004847403],"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":[0.0015478819,0.00063730165,0.0060642236,0.00036168372,0.000055034303,0.0026199047,0.0008616604,0.010877091,0.89269125,0.00335287,0.010035408,0.0708958],"study_design_scores_gemma":[0.00042489238,0.019203877,0.01749683,0.00007517154,0.000052715146,0.002265035,0.0006418404,0.02327291,0.885359,0.0010432132,0.050048962,0.00011560632],"about_ca_topic_score_codex":0.00047648657,"about_ca_topic_score_gemma":0.00088221626,"teacher_disagreement_score":0.010633898,"about_ca_system_score_codex":0.0003678004,"about_ca_system_score_gemma":0.00042425768,"threshold_uncertainty_score":0.0355739},"labels":[],"label_agreement":null},{"id":"W2833684345","doi":"10.2514/6.2018-4442","title":"Geometric Swirl Number and Hybrid Rocket Engine Performance","year":2018,"lang":"en","type":"article","venue":"2018 Joint Propulsion Conference","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Rocket engine; Aerospace engineering; Computer science; Rocket (weapon); Automotive engineering; Engineering","score_opus":0.037894120636156055,"score_gpt":0.25029537295303744,"score_spread":0.2124012523168814,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2833684345","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":[0.99695694,0.000061463725,0.0011437766,0.000013938875,0.000006229672,0.0000033399904,0.00010229667,0.0000879573,0.0016239964],"genre_scores_gemma":[0.99865496,0.00002382646,0.00017789436,0.000005106399,0.0000024903957,0.0000020626603,0.00025010732,0.00002564102,0.00085785484],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998807,0.000013038082,0.000006070006,0.00002978044,0.000034201712,0.00003615716],"domain_scores_gemma":[0.99958557,0.00018708243,0.00006390833,0.000033879624,0.00008336092,0.000046242643],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025471824,0.0003543191,0.0002618286,0.00040385674,0.00015116412,0.0005619454,0.00038969432,0.00035416853,0.005637184],"category_scores_gemma":[0.0010127906,0.0001414359,0.0002219537,0.00031506992,0.00020406241,0.0006963989,0.00038990166,0.00019179909,0.0012959347],"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":[0.016906047,0.0010462947,0.20537078,0.000351285,0.00036141532,0.0011325612,0.00021315474,0.19200055,0.49105942,0.0016407537,0.001820267,0.08809742],"study_design_scores_gemma":[0.00023543986,0.0075831143,0.42697126,0.00004230231,0.00023858731,0.0013067997,0.0005023746,0.24112052,0.31805965,0.001229188,0.0025352973,0.00017539389],"about_ca_topic_score_codex":0.0009403653,"about_ca_topic_score_gemma":0.0012712792,"teacher_disagreement_score":0.005637184,"about_ca_system_score_codex":0.00018044165,"about_ca_system_score_gemma":0.00014036054,"threshold_uncertainty_score":0.018858314},"labels":[],"label_agreement":null},{"id":"W2854053305","doi":"10.2514/6.2018-4837","title":"Development and Testing of a 4.4-kN Paraffin-based Hybrid Rocket Motor and Test Facility","year":2018,"lang":"en","type":"article","venue":"2018 Joint Propulsion Conference","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":6,"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 Calgary","funders":"","keywords":"Test (biology); Rocket (weapon); Automotive engineering; Aeronautics; Computer science; Engineering; Aerospace engineering; Geology","score_opus":0.08016053100836733,"score_gpt":0.25938218606704244,"score_spread":0.1792216550586751,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2854053305","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":[0.73123854,0.00012009012,0.25503874,0.00026029258,0.000104990584,0.0013581946,0.0010334271,0.0036979248,0.0071478863],"genre_scores_gemma":[0.8632505,0.00009955138,0.119679466,0.000091845206,0.00001441107,0.0008554116,0.0011311875,0.00025410013,0.0146235],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9993062,0.00006532879,0.00003246333,0.00010787488,0.00038463259,0.00010342615],"domain_scores_gemma":[0.9988556,0.0001558647,0.00015213682,0.00014275886,0.00050309853,0.000190571],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.001205119,0.00048681008,0.0004683399,0.0005879606,0.000551815,0.00034784304,0.0018878486,0.00064331945,0.0050592762],"category_scores_gemma":[0.0009763621,0.00031337168,0.00035070378,0.00023988211,0.00038078972,0.0009578924,0.00086388807,0.00048457214,0.0014987892],"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":[0.0009162645,0.0006358032,0.008209689,0.0003422244,0.000062916755,0.0005425409,0.000310542,0.010523238,0.9137938,0.0018242457,0.0022191552,0.060619574],"study_design_scores_gemma":[0.00037179637,0.010251681,0.021973541,0.000076110024,0.00010895564,0.0012629768,0.00043938783,0.048273597,0.86650664,0.0005474066,0.050079737,0.0001082433],"about_ca_topic_score_codex":0.0012534442,"about_ca_topic_score_gemma":0.0020491984,"teacher_disagreement_score":0.0050592762,"about_ca_system_score_codex":0.0004890094,"about_ca_system_score_gemma":0.0014035812,"threshold_uncertainty_score":0.016924977},"labels":[],"label_agreement":null},{"id":"W2883008978","doi":"10.4050/f-0074-2018-12769","title":"Establishing Rotorcraft Component Fatigue Lives using SUMS Data and a Partial Usage Spectrum Approach for the UH-60 L/M Blackhawk","year":2018,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","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":"Lockheed Martin (Canada)","funders":"","keywords":"Component (thermodynamics); Spectrum (functional analysis); Computer science; Physics","score_opus":0.14629230149205327,"score_gpt":0.3351808116322968,"score_spread":0.18888851014024352,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2883008978","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":[0.98468256,0.000024630559,0.0070512043,0.000019116284,0.000006000486,0.00008399093,0.0030081049,0.00020845508,0.0049160696],"genre_scores_gemma":[0.9834378,0.00002515091,0.009668294,0.000010940409,0.000008453222,0.00014293002,0.004990111,0.000066238805,0.0016501884],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.99938285,0.00010922712,0.000086553635,0.00014237971,0.00022985571,0.000049123668],"domain_scores_gemma":[0.9969959,0.00080643914,0.0007040474,0.00038696782,0.0010072191,0.0000992999],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0007865802,0.00036721636,0.0002562367,0.0037799447,0.00036786037,0.0004830767,0.0003317192,0.00024778908,0.0023397305],"category_scores_gemma":[0.0037435084,0.00014114448,0.00029666675,0.0011703266,0.00034609338,0.0006843725,0.00079581677,0.00024804438,0.00091261975],"study_design_candidate":"observational","study_design_consensus":"observational","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0009155176,0.00028297596,0.669499,0.00032196374,0.0001210357,0.000345362,0.0056517725,0.011164871,0.0388082,0.0012100507,0.0038120004,0.26786727],"study_design_scores_gemma":[0.000012588276,0.00053465646,0.9413438,0.000058351492,0.000041818024,0.00034035428,0.0031601535,0.02920491,0.016253145,0.00062490563,0.00837107,0.000054257624],"about_ca_topic_score_codex":0.004612266,"about_ca_topic_score_gemma":0.010380734,"teacher_disagreement_score":0.004612266,"about_ca_system_score_codex":0.00040351637,"about_ca_system_score_gemma":0.00019836304,"threshold_uncertainty_score":0.00917083},"labels":[],"label_agreement":null},{"id":"W2887225106","doi":"10.11159/icmie18.108","title":"Pressure Pulsator to Study the Low-Frequency Characteristics of a Liquid Rocket Engine","year":2018,"lang":"en","type":"article","venue":"Proceedings of the World Congress on Mechanical, Chemical, and Material Engineering","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Liquid-propellant rocket; Rocket engine; Aerospace engineering; Materials science; Automotive engineering; Rocket (weapon); Acoustics; Environmental science; Computer science; Physics; Engineering; Propellant","score_opus":0.009347078241560738,"score_gpt":0.23237470744409947,"score_spread":0.2230276292025387,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2887225106","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":[0.85448974,0.0016323967,0.13777806,0.0001272739,0.0000805298,0.00007577458,0.00019894096,0.0005762933,0.0050409148],"genre_scores_gemma":[0.9773382,0.0005300032,0.019276297,0.000029104622,0.00002457694,0.000055274548,0.00014036967,0.000058415535,0.002547672],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99983823,0.00002041969,0.0000083324885,0.000027761058,0.00009006746,0.000015107768],"domain_scores_gemma":[0.99967086,0.00015492272,0.00005170982,0.00002071088,0.00008541989,0.00001637227],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00029887658,0.00021912988,0.00030286712,0.00040942186,0.00012498721,0.0002227334,0.00028762472,0.00028253385,0.0013088413],"category_scores_gemma":[0.0004950719,0.00012248126,0.00010878534,0.0003956095,0.00018815463,0.0004153045,0.00022157562,0.0002828581,0.00026829733],"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":[0.00013610697,0.000031252282,0.001004318,0.00020475089,0.000009504278,0.00013212312,0.00013432899,0.0011378722,0.9709446,0.00041165398,0.00016607186,0.0256874],"study_design_scores_gemma":[0.00002160812,0.000994626,0.0068635116,0.00001772919,0.000019897338,0.00041989348,0.00009202014,0.029447306,0.95418656,0.00017577174,0.0077395164,0.000021557631],"about_ca_topic_score_codex":0.00015425847,"about_ca_topic_score_gemma":0.00013224258,"teacher_disagreement_score":0.0013088413,"about_ca_system_score_codex":0.00009749583,"about_ca_system_score_gemma":0.00010997552,"threshold_uncertainty_score":0.0043784976},"labels":[],"label_agreement":null},{"id":"W2891299362","doi":"10.1088/1757-899x/400/4/042017","title":"Study of full and truncated aerospike nozzles on performances at different working conditions","year":2018,"lang":"en","type":"article","venue":"IOP Conference Series Materials Science and Engineering","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":5,"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; Propulsion; Aerospace engineering; Spark plug; Truncation (statistics); Aerodynamics; Thrust; Marine engineering; Computational fluid dynamics; Mechanical engineering; Engineering; Mechanics; Environmental science; Computer science; Physics","score_opus":0.03525130168871895,"score_gpt":0.2598720465977979,"score_spread":0.22462074490907893,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2891299362","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":[0.9958252,0.00040865826,0.0021113234,0.000025268773,0.000011956836,0.000007702279,0.00017407408,0.00006465049,0.0013710608],"genre_scores_gemma":[0.998453,0.00016548164,0.00075258146,0.000005084027,0.0000027239657,0.0000061441333,0.00014805343,0.000018825898,0.00044799683],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99962807,0.000036247377,0.000025137051,0.00006965515,0.00016239836,0.0000784391],"domain_scores_gemma":[0.9990682,0.0005056475,0.00009938916,0.00007754363,0.00020270282,0.00004651293],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00043895518,0.00033892065,0.0005677033,0.0003430213,0.00026901223,0.00067378685,0.0003701136,0.0005409739,0.0013523207],"category_scores_gemma":[0.001464214,0.00015486435,0.00045802226,0.00036071573,0.000381714,0.0005542189,0.00030631607,0.00023788193,0.00024152163],"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":[0.0016965928,0.00019030253,0.018251885,0.0005700368,0.0000754823,0.0010791845,0.00067698135,0.1755957,0.74129236,0.0008564998,0.0008008209,0.058914166],"study_design_scores_gemma":[0.000054977103,0.0038854901,0.05689723,0.00011466476,0.0001276072,0.0006864137,0.0008225238,0.2843867,0.64851254,0.00063942367,0.0037415158,0.00013081633],"about_ca_topic_score_codex":0.0007274238,"about_ca_topic_score_gemma":0.0005374018,"teacher_disagreement_score":0.0013523207,"about_ca_system_score_codex":0.00020942093,"about_ca_system_score_gemma":0.00018243547,"threshold_uncertainty_score":0.004523933},"labels":[],"label_agreement":null},{"id":"W2891567588","doi":"10.3390/aerospace5030096","title":"Aerodynamic Design of a Laval Nozzle for Real Gas Using Hodograph Method","year":2018,"lang":"en","type":"article","venue":"Aerospace","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":7,"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":"Ministry of Education and Science of the Russian Federation","keywords":"Hodograph; Nozzle; Aerodynamics; Real gas; Rocket engine nozzle; Propellant; Aerospace engineering; Rocket (weapon); Plane (geometry); Rotational symmetry; Mechanical engineering; Mechanics; Computer science; Engineering; Physics; Mathematics; Geometry","score_opus":0.06099717184274695,"score_gpt":0.34936590512346033,"score_spread":0.2883687332807134,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2891567588","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":[0.036509644,0.00028245736,0.9595542,0.0000674042,0.000039548817,0.00007043571,0.00003622523,0.00027717729,0.0031629761],"genre_scores_gemma":[0.538835,0.0002984999,0.45804685,0.000028529643,0.000020215868,0.00011743897,0.00004487615,0.00007377682,0.0025347434],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999874,0.000032347547,0.000005887018,0.000016224409,0.00005875629,0.000012813918],"domain_scores_gemma":[0.99987936,0.000038074893,0.000018094277,0.000012824989,0.00003941787,0.000012210039],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00037297784,0.00023937468,0.00037430465,0.00023040015,0.00021571544,0.0005546583,0.00037254588,0.00041601635,0.0012189199],"category_scores_gemma":[0.0003994314,0.00021521437,0.00033253327,0.000121321886,0.00033960145,0.00029248837,0.0003199461,0.00026105836,0.0002336216],"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":[0.00018897385,0.000043081964,0.0026919595,0.00038448226,0.00003983993,0.00033747812,0.00024147649,0.654875,0.20303904,0.036795538,0.001343616,0.1000196],"study_design_scores_gemma":[0.00005326555,0.00022520406,0.00061085477,0.000017171118,0.00001261694,0.00019162812,0.000037318212,0.97072697,0.01736277,0.0017751121,0.008959584,0.000027458163],"about_ca_topic_score_codex":0.00075066584,"about_ca_topic_score_gemma":0.000673237,"teacher_disagreement_score":0.0012189199,"about_ca_system_score_codex":0.00028521405,"about_ca_system_score_gemma":0.0006678034,"threshold_uncertainty_score":0.004077673},"labels":[],"label_agreement":null},{"id":"W2891678813","doi":"10.1088/1757-899x/400/4/042016","title":"Development of a Laval nozzle for a cold gas propulsion system","year":2018,"lang":"en","type":"article","venue":"IOP Conference Series Materials Science and Engineering","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":5,"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; Propulsion; Aerospace engineering; Mach number; Rocket engine nozzle; Supersonic speed; Jet propulsion; Thermal; Jet (fluid); Mechanical engineering; Spacecraft propulsion; Mechanics; Engineering; Physics; Meteorology","score_opus":0.027092455528298916,"score_gpt":0.24768268650440461,"score_spread":0.2205902309761057,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2891678813","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":[0.2145097,0.0026919467,0.7647654,0.0003340902,0.0003631616,0.00042330884,0.00028715248,0.0019618578,0.014663436],"genre_scores_gemma":[0.6228926,0.00086127425,0.3716717,0.00004419792,0.000038581893,0.00014629343,0.00022437863,0.00014177528,0.003979132],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9995956,0.000032995176,0.000023684215,0.000064844484,0.00025106253,0.000031866337],"domain_scores_gemma":[0.9996704,0.00006890581,0.00004528362,0.000035499248,0.00014414305,0.000035717705],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00074791006,0.00030072528,0.0004959534,0.00030545346,0.00047682715,0.0010977732,0.0012127351,0.00079773046,0.0015737293],"category_scores_gemma":[0.00082551397,0.00026758842,0.0005551264,0.00020046461,0.00026227284,0.000700052,0.00052037265,0.00051193085,0.0004592249],"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":[0.00030699477,0.00017772155,0.008639887,0.001185588,0.00007235558,0.001168225,0.00036975832,0.18675229,0.6355402,0.017266952,0.0021192885,0.14640076],"study_design_scores_gemma":[0.00014425791,0.0013657239,0.0058952617,0.00015462484,0.00008947027,0.0015678549,0.00012598357,0.61738765,0.31531504,0.0013376031,0.05645958,0.0001568881],"about_ca_topic_score_codex":0.0010255743,"about_ca_topic_score_gemma":0.00085786555,"teacher_disagreement_score":0.0015737293,"about_ca_system_score_codex":0.00059885223,"about_ca_system_score_gemma":0.0010714306,"threshold_uncertainty_score":0.0052646995},"labels":[],"label_agreement":null},{"id":"W2894327516","doi":"10.2172/1471904","title":"Analysis and Design of Ex-Service Garter Spring Irradiation Capsules in the High Flux Isotope Reactor","year":2018,"lang":"en","type":"report","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Oak Ridge National Laboratory; CANDU Owners Group; UT-Battelle; Canadian Nuclear Laboratories; Battelle; U.S. Department of Energy","keywords":"Irradiation; Materials science; Embrittlement; Inconel; Oak Ridge National Laboratory; Creep; Nuclear engineering; Neutron flux; Neutron; Flux (metallurgy); Radiochemistry; Composite material; Metallurgy; Nuclear physics; Chemistry; Engineering; Physics","score_opus":0.05662948807707281,"score_gpt":0.29015272141634824,"score_spread":0.23352323333927544,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2894327516","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":[0.9329354,0.00034428266,0.060462426,0.00005764071,0.000022480093,0.0002919386,0.00031221609,0.00051428017,0.005059382],"genre_scores_gemma":[0.95868295,0.00023826558,0.037384782,0.000011484587,0.0000040052,0.0001273834,0.00032222472,0.00010299928,0.0031258776],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9994549,0.00006167529,0.000025130756,0.0000820614,0.0003112997,0.000064826214],"domain_scores_gemma":[0.9994816,0.00009023519,0.00017958575,0.000053206535,0.00014653156,0.000048920236],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0008706752,0.00048690938,0.0005383939,0.0004010876,0.00030909537,0.0006509049,0.00073082955,0.00045453294,0.0011185036],"category_scores_gemma":[0.00066054944,0.00034445347,0.00047533074,0.0002767496,0.0002987233,0.00035669885,0.00024370247,0.00025058686,0.00038688022],"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":[0.0008363051,0.00016849555,0.007236703,0.00037861493,0.000033490698,0.00035053593,0.00012220225,0.08910942,0.8746598,0.00094925164,0.0005204025,0.025634868],"study_design_scores_gemma":[0.00008000964,0.0049277428,0.025927879,0.000027117487,0.00010779615,0.0003044167,0.00017172303,0.189333,0.7727089,0.00013936494,0.0062188213,0.000053255637],"about_ca_topic_score_codex":0.0015529668,"about_ca_topic_score_gemma":0.0025942964,"teacher_disagreement_score":0.0015529668,"about_ca_system_score_codex":0.0009022252,"about_ca_system_score_gemma":0.0012904395,"threshold_uncertainty_score":0.00654608},"labels":[],"label_agreement":null},{"id":"W2894653475","doi":"10.2322/astj.jsass-d-17-00062","title":"Development of CFRP Reinforced Lightweight Hybrid Rocket Engine","year":2018,"lang":"en","type":"article","venue":"AEROSPACE TECHNOLOGY JAPAN THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":5,"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":"Rocket engine; Rocket (weapon); Aerospace engineering; Automotive engineering; Engineering; Aeronautics; Mechanical engineering; Environmental science","score_opus":0.019334373466131264,"score_gpt":0.2640487786799909,"score_spread":0.24471440521385962,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2894653475","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":[0.95246774,0.0009304308,0.031289015,0.00007995203,0.00015544875,0.00022971955,0.00022484451,0.00057328516,0.014049594],"genre_scores_gemma":[0.9393146,0.00091834436,0.047264617,0.000035622987,0.000017779343,0.00011869223,0.0005707671,0.00007462205,0.011684913],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997751,0.0000071043655,0.000013677186,0.000034385823,0.00013840133,0.000031324027],"domain_scores_gemma":[0.99987626,0.0000050771646,0.000017539562,0.000013610385,0.000059054717,0.00002853639],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024032072,0.00025796707,0.0002556418,0.00056162087,0.00020329724,0.00029144005,0.00044197217,0.00032780707,0.00096048234],"category_scores_gemma":[0.00015461439,0.00011997209,0.00037422776,0.00020134657,0.0000912522,0.00032839354,0.00030035822,0.00032089642,0.0005194982],"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":[0.00006173477,0.00014037394,0.0012682867,0.00014032511,0.000017659666,0.00050013274,0.00005338309,0.002772266,0.9657161,0.0006579769,0.0004017486,0.028270062],"study_design_scores_gemma":[0.0000476625,0.0014419592,0.010381606,0.000027979871,0.00004608339,0.00085300265,0.000074293326,0.014320893,0.9537835,0.00013712715,0.018830901,0.000054983542],"about_ca_topic_score_codex":0.0008824314,"about_ca_topic_score_gemma":0.0014971151,"teacher_disagreement_score":0.00096048234,"about_ca_system_score_codex":0.00016996037,"about_ca_system_score_gemma":0.00029864215,"threshold_uncertainty_score":0.0032131076},"labels":[],"label_agreement":null},{"id":"W2897175848","doi":"10.1139/tcsme-2018-0028","title":"Study on creep performance of launch canister under long-term storage","year":2018,"lang":"en","type":"article","venue":"Transactions of the Canadian Society for Mechanical Engineering","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Creep; Deformation (meteorology); Structural engineering; Rocket (weapon); Materials science; Finite element method; Residual; Stress (linguistics); Frame (networking); Term (time); Engineering; Composite material; Mechanical engineering; Aerospace engineering; Computer science; Physics","score_opus":0.030916787931576966,"score_gpt":0.25855596483597176,"score_spread":0.2276391769043948,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2897175848","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":[0.99595624,0.0011523,0.0018304726,0.00004287522,0.000059410482,0.000017517928,0.0001433564,0.00007878285,0.00071906025],"genre_scores_gemma":[0.99743515,0.00034682668,0.0007077114,0.000022304015,0.00001561129,0.000015667845,0.00015340037,0.000029479172,0.0012738738],"study_design_codex":"bench_or_experimental","study_design_gemma":"observational","domain_scores_codex":[0.9994041,0.000038588918,0.00003824114,0.000096265016,0.00032810282,0.000094693874],"domain_scores_gemma":[0.998697,0.00017658745,0.00016444353,0.00018008132,0.00067746785,0.00010450683],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00076519966,0.00046905765,0.00065475435,0.00068719627,0.00065360934,0.0005052651,0.000479419,0.0006174445,0.0015773155],"category_scores_gemma":[0.0014470319,0.00017055098,0.0004283875,0.0006419316,0.00045848114,0.000984603,0.00044090668,0.00048422304,0.00041863165],"study_design_candidate":"observational","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":[0.0005147769,0.00008005948,0.009298974,0.00029466779,0.000043951262,0.00061624486,0.00062339625,0.002932652,0.9651679,0.00017461635,0.00046309363,0.019789618],"study_design_scores_gemma":[0.000014618589,0.0014142635,0.042774413,0.000042469455,0.00013581711,0.000796021,0.0009202915,0.007831479,0.94081295,0.0001194883,0.005073308,0.000064948064],"about_ca_topic_score_codex":0.0012906294,"about_ca_topic_score_gemma":0.0019657575,"teacher_disagreement_score":0.0015773155,"about_ca_system_score_codex":0.00033663976,"about_ca_system_score_gemma":0.00036152388,"threshold_uncertainty_score":0.00527668},"labels":[],"label_agreement":null},{"id":"W2898157671","doi":"10.1115/icone26-81806","title":"Numerical Study of Supersonic Film Cooling in Diverging Section of Nuclear Rocket Laval Nozzle","year":2018,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":9,"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":"Science Fund for Creative Research Groups; National Natural Science Foundation of China","keywords":"Rocket engine nozzle; Coolant; Nozzle; Mach number; Propellant; Specific impulse; Supersonic speed; Inlet; Rocket (weapon); Rocket engine; Mass flow; Mass flow rate; Materials science; Mechanics; Aerospace engineering; Mechanical engineering; Physics; Engineering","score_opus":0.01994616883643278,"score_gpt":0.2655377409369173,"score_spread":0.24559157210048452,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2898157671","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":[0.940489,0.0010775545,0.032091655,0.0004981685,0.00015819968,0.00011074176,0.00038244601,0.00025298784,0.024939174],"genre_scores_gemma":[0.9910097,0.00020016919,0.0054594725,0.00003472287,0.000015024031,0.0000478009,0.00009697123,0.00002829966,0.0031078372],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997876,0.000035615318,0.000009091469,0.000035147823,0.000053103373,0.00007942469],"domain_scores_gemma":[0.9993864,0.00030335248,0.000104530816,0.000022837106,0.000121291865,0.00006158356],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00037366556,0.0005818068,0.00093127345,0.00057770096,0.0010589074,0.0009992046,0.0008328446,0.0017514811,0.0030194463],"category_scores_gemma":[0.0012083022,0.00037919942,0.00067038916,0.00047572303,0.0009963699,0.0005980554,0.0005344597,0.00068187615,0.00018028928],"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":[0.00018705717,0.00008114223,0.0042410176,0.00017271079,0.000023575842,0.0007712287,0.00015569526,0.97780323,0.010500129,0.0027159734,0.0005556332,0.0027926434],"study_design_scores_gemma":[0.000027366139,0.00005822346,0.00081996736,0.000012493015,0.0000078768035,0.000032165888,0.00007092512,0.99724823,0.0012053901,0.0001698108,0.0003372545,0.000010243626],"about_ca_topic_score_codex":0.022538217,"about_ca_topic_score_gemma":0.009495472,"teacher_disagreement_score":0.022538217,"about_ca_system_score_codex":0.000984156,"about_ca_system_score_gemma":0.001051088,"threshold_uncertainty_score":0.04481405},"labels":[],"label_agreement":null},{"id":"W2906369998","doi":"","title":"Non-Flammable R-410A Alternative for Commercial Refrigeration and Air Conditioning","year":2018,"lang":"en","type":"article","venue":"Purdue e-Pubs (Purdue University System)","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":1,"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":"Flammable liquid; Refrigeration; Air conditioning; Environmental science; Waste management; Engineering; Mechanical engineering","score_opus":0.012633264274992019,"score_gpt":0.22300098218514164,"score_spread":0.21036771791014963,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2906369998","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":[0.8103924,0.024129389,0.06240723,0.0012258394,0.00091253855,0.0010923484,0.00278383,0.0018186544,0.09523775],"genre_scores_gemma":[0.9226065,0.0056003034,0.033947017,0.0006517993,0.00016629402,0.00034716394,0.0019629837,0.00021331977,0.034504633],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99947494,0.000059010472,0.00003153724,0.000084694984,0.00028206097,0.00006782121],"domain_scores_gemma":[0.99979883,0.00002376955,0.000051175386,0.000021622449,0.00007502599,0.000029706951],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00038432304,0.00045355156,0.00022616639,0.00078941183,0.00031339587,0.00036503037,0.00043525844,0.00073441153,0.010487671],"category_scores_gemma":[0.00033765187,0.0001578072,0.0005679606,0.00041019125,0.00017522686,0.0008261537,0.00034940278,0.0005536159,0.0034798791],"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":[0.00034253398,0.00026753134,0.0008061784,0.0009008979,0.000030281075,0.00053536,0.000060615912,0.00039643116,0.92143804,0.0022012626,0.003887007,0.069133855],"study_design_scores_gemma":[0.000048478054,0.001982628,0.007155398,0.000121897756,0.0000715214,0.001543503,0.00009348284,0.0025833594,0.8424261,0.0004639602,0.14343838,0.00007130061],"about_ca_topic_score_codex":0.0006093401,"about_ca_topic_score_gemma":0.0011480214,"teacher_disagreement_score":0.010487671,"about_ca_system_score_codex":0.0003280656,"about_ca_system_score_gemma":0.00026705343,"threshold_uncertainty_score":0.035084784},"labels":[],"label_agreement":null},{"id":"W2950207093","doi":"10.2514/6.2019-3570","title":"Nozzle Jet Effects Conceptual Design Tool for a Generic Fighter","year":2019,"lang":"en","type":"article","venue":"AIAA Aviation 2019 Forum","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lockheed Martin (Canada)","funders":"","keywords":"Nozzle; Jet (fluid); Conceptual design; Aerospace engineering; Computer science; Systems engineering; Mechanical engineering; Aeronautics; Engineering; Human–computer interaction","score_opus":0.01795272559280097,"score_gpt":0.24805682478841395,"score_spread":0.23010409919561298,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2950207093","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":[0.015359158,0.00012626455,0.930816,0.00017744655,0.00017842415,0.00031499905,0.0012123183,0.011729698,0.040085677],"genre_scores_gemma":[0.370636,0.00053336855,0.55232114,0.00039877134,0.00011407713,0.0010139995,0.0034507937,0.008055268,0.06347656],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99969137,0.00002816458,0.000014710751,0.000030506017,0.00020346123,0.000031937365],"domain_scores_gemma":[0.99966514,0.00010509962,0.000028829803,0.000057693902,0.00012221467,0.00002091698],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006911376,0.0009337189,0.00066866376,0.0006067571,0.00064196344,0.0013066541,0.0018713055,0.0012940759,0.04594961],"category_scores_gemma":[0.0010971308,0.0007695551,0.0009452539,0.00033322064,0.00031180796,0.00086729444,0.0012297191,0.0013463226,0.004580723],"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":[0.0006810282,0.00029346833,0.0021107937,0.0009748773,0.00014381141,0.00080349605,0.00043278674,0.61689883,0.12761651,0.056436576,0.029921068,0.16368683],"study_design_scores_gemma":[0.00026505798,0.00034174265,0.00096687704,0.0000960864,0.00007290889,0.00025167255,0.00007282494,0.8623487,0.032403495,0.0052316682,0.09786417,0.000084838415],"about_ca_topic_score_codex":0.001775127,"about_ca_topic_score_gemma":0.0022907131,"teacher_disagreement_score":0.04594961,"about_ca_system_score_codex":0.0005366742,"about_ca_system_score_gemma":0.0011763979,"threshold_uncertainty_score":0.15371674},"labels":[],"label_agreement":null},{"id":"W2951338676","doi":"10.22215/etd/2018-13341","title":"Supersonic Multi-Objective Optimization of a Rocket Based Combined Cycle Inlet by Differential Evolution","year":2018,"lang":"en","type":"dissertation","venue":"","topic":"Rocket and propulsion systems research","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":"Carleton University","funders":"","keywords":"Supersonic speed; Inlet; Rocket (weapon); Aerospace engineering; Injector; Engineering; Marine engineering; Mechanics; Mechanical engineering; Physics","score_opus":0.010101999981857861,"score_gpt":0.253973516888542,"score_spread":0.2438715169066841,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2951338676","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":[0.5738983,0.0008313948,0.40129134,0.00024048568,0.00007155607,0.00016754585,0.00015444942,0.00027812365,0.023066724],"genre_scores_gemma":[0.9137525,0.00017147143,0.080149636,0.00006325292,0.000009131838,0.0001778171,0.00016757919,0.00003537939,0.005473179],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99989355,0.000029858516,0.000003780434,0.000020010877,0.00003113714,0.000021684718],"domain_scores_gemma":[0.99973196,0.00017476534,0.000027174889,0.000008736783,0.000041529012,0.000015880145],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00043850328,0.0005459207,0.0006040717,0.00041740926,0.00017169937,0.00053357356,0.0005178151,0.00065207813,0.0011668764],"category_scores_gemma":[0.0008067967,0.000300329,0.00046091818,0.00036235753,0.0003162249,0.00025549144,0.00040280996,0.00040127974,0.00012339858],"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":[0.000057472556,0.000034258494,0.00051107863,0.000037894086,0.000020503163,0.000034706376,0.00001459599,0.98578554,0.0017784787,0.00092918426,0.00019272708,0.010603539],"study_design_scores_gemma":[0.0000067616156,0.00004594589,0.00017060197,0.000003089429,0.0000041674825,0.0000045697743,0.0000058571063,0.99889684,0.00047370885,0.00015423923,0.00023206466,0.0000020071382],"about_ca_topic_score_codex":0.0040604305,"about_ca_topic_score_gemma":0.00441941,"teacher_disagreement_score":0.0040604305,"about_ca_system_score_codex":0.0005216599,"about_ca_system_score_gemma":0.0006149081,"threshold_uncertainty_score":0.008073568},"labels":[],"label_agreement":null},{"id":"W2952270536","doi":"10.1177/1468087419852841","title":"Studies of anaerobic internal combustion engine using direct injection of liquid monopropellant","year":2019,"lang":"en","type":"article","venue":"International Journal of Engine Research","topic":"Rocket and propulsion systems research","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":"Université de Sherbrooke","funders":"","keywords":"Monopropellant; Piston (optics); Combustion; Internal combustion engine; Materials science; Engine power; Mean effective pressure; Isopropyl alcohol; Automotive engineering; Rotary engine; Chemistry; Nuclear engineering; Power (physics); Thermodynamics; Compression ratio; Engineering; Physics; Composite material; Organic chemistry","score_opus":0.10056176798807083,"score_gpt":0.4054816764981763,"score_spread":0.3049199085101055,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2952270536","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":[0.9894856,0.00046993786,0.008554471,0.000015615791,0.000014295935,0.000040032814,0.000048580758,0.000048536116,0.0013229494],"genre_scores_gemma":[0.98874795,0.00066843984,0.008953241,0.00000975643,0.000008306719,0.000028270963,0.00011036591,0.000021562042,0.0014521113],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99962974,0.00004064064,0.00002600723,0.0000654541,0.00019205583,0.00004609683],"domain_scores_gemma":[0.999728,0.00009486768,0.00006472419,0.00001851488,0.00007152027,0.000022372818],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005332365,0.00042392217,0.00053956447,0.00026990444,0.00023965418,0.0004351377,0.0005073437,0.00024392144,0.0004577909],"category_scores_gemma":[0.00049559213,0.00022847965,0.00029909093,0.00020921156,0.00032254905,0.000505752,0.00025466408,0.00033453875,0.00017254375],"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":[0.000521095,0.00020835332,0.0014132157,0.00034706615,0.00001188238,0.00016282548,0.00012581938,0.0027668274,0.98493433,0.00025031218,0.000031883163,0.009226448],"study_design_scores_gemma":[0.000016557042,0.0016714073,0.0030687607,0.000008935518,0.000018693967,0.00013646267,0.000041816256,0.0067774,0.98715186,0.000033296692,0.0010590354,0.000015765396],"about_ca_topic_score_codex":0.00095745263,"about_ca_topic_score_gemma":0.00087610446,"teacher_disagreement_score":0.00095745263,"about_ca_system_score_codex":0.00036247,"about_ca_system_score_gemma":0.0002900751,"threshold_uncertainty_score":0.0028200746},"labels":[],"label_agreement":null},{"id":"W2953671007","doi":"10.18287/2541-7533-2019-18-2-62-74","title":"Technology of computational analysis of the working process parameters of low-thrust rocket engines running on gaseous oxygen-hydrogen fuel with the use of ANSYS CFD","year":2019,"lang":"en","type":"article","venue":"VESTNIK of Samara University Aerospace and Mechanical Engineering","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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":"Rocket engine; Combustion chamber; Rocket engine nozzle; Nozzle; Thrust; Aerospace engineering; Computational fluid dynamics; Combustion; Rocket (weapon); Mechanical engineering; Automotive engineering; Engineering; Nuclear engineering; Chemistry","score_opus":0.014653117711770157,"score_gpt":0.19171247057616259,"score_spread":0.17705935286439242,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2953671007","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":[0.19976307,0.00027917186,0.78692186,0.00021187034,0.000043520613,0.00008985171,0.0007706,0.0013840784,0.010535963],"genre_scores_gemma":[0.8977955,0.00036556445,0.0976713,0.000028023695,0.0000181909,0.0001667834,0.00084886886,0.00024318413,0.0028625894],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99984837,0.000020880429,0.000009852781,0.000023211755,0.000078705256,0.000019001516],"domain_scores_gemma":[0.99976426,0.000099163946,0.000024149891,0.000034130615,0.00006793188,0.00001036746],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00022450153,0.00040717155,0.00043051605,0.0005094077,0.00040630825,0.00079536374,0.00062726997,0.00039660544,0.0017598297],"category_scores_gemma":[0.0007133414,0.00019177586,0.00055948744,0.00046168108,0.00031900342,0.00066978566,0.00037117893,0.00048531403,0.00036033214],"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":[0.0000676366,0.000056650428,0.0058900723,0.00016140714,0.000029624878,0.00016867655,0.00017659746,0.917475,0.024097644,0.0097720865,0.0007123002,0.04139218],"study_design_scores_gemma":[0.0000046051973,0.000011795029,0.0009629293,0.0000059119498,0.000005963992,0.000045203156,0.00002405782,0.9887771,0.007297225,0.0016179184,0.00123998,0.000007233367],"about_ca_topic_score_codex":0.003257137,"about_ca_topic_score_gemma":0.0016455834,"teacher_disagreement_score":0.003257137,"about_ca_system_score_codex":0.00047021732,"about_ca_system_score_gemma":0.00091478496,"threshold_uncertainty_score":0.0064763427},"labels":[],"label_agreement":null},{"id":"W2956164824","doi":"10.21608/iccee.2008.38418","title":"IMPROVEMENT OF THE PROPERTIES OF INSULATING POLYMERS USING ARAMID FIBER FOR SOLID ROCKET MOTOR INSULATION","year":2008,"lang":"en","type":"article","venue":"The International Conference on Chemical and Environmental Engineering","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Concordia University","funders":"Concordia University","keywords":"Aramid; Solid-fuel rocket; Materials science; Composite material; Polymer; Fiber; Propellant; Aerospace engineering; Engineering","score_opus":0.04441379827057433,"score_gpt":0.23057872464743961,"score_spread":0.18616492637686527,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2956164824","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":[0.99629706,0.0009854529,0.0018689851,0.00000927882,0.0000047300637,0.00000827433,0.00003772752,0.000033295917,0.0007552337],"genre_scores_gemma":[0.9943592,0.0008034308,0.0035317293,0.000006593427,0.000004539161,0.000008186034,0.00013614343,0.000023505072,0.0011267441],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999213,0.000014020483,0.00000518475,0.000014056457,0.000029722632,0.00001578265],"domain_scores_gemma":[0.9998004,0.0000556097,0.000071587136,0.000017178405,0.000032485827,0.000022716686],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012613928,0.00043442711,0.00016075828,0.00025224613,0.00010393912,0.00018720672,0.00012510562,0.00018074816,0.00080066663],"category_scores_gemma":[0.00021805175,0.00010364191,0.00014407208,0.00022701091,0.00010926118,0.00024570752,0.00012040656,0.00030601572,0.00022407983],"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":[0.00004383502,0.000018313194,0.00016981227,0.000039526967,0.0000020094096,0.000025303074,0.000010022436,0.0000904632,0.99683183,0.000018088604,0.0000055324663,0.002745185],"study_design_scores_gemma":[0.000001394367,0.0002956707,0.002780624,0.0000039139195,0.000008205574,0.000069506015,0.000008999109,0.00039287738,0.99579215,0.0000059040735,0.00063889055,0.0000018809573],"about_ca_topic_score_codex":0.00018419263,"about_ca_topic_score_gemma":0.00035159543,"teacher_disagreement_score":0.00080066663,"about_ca_system_score_codex":0.00011519067,"about_ca_system_score_gemma":0.00007396853,"threshold_uncertainty_score":0.0026785135},"labels":[],"label_agreement":null},{"id":"W2958721697","doi":"10.2514/6.2019-3570.c1","title":"Correction: Nozzle Jet Effects Conceptual Design Tool for a Generic Fighter","year":2019,"lang":"en","type":"article","venue":"AIAA Aviation 2019 Forum","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lockheed Martin (Canada)","funders":"","keywords":"Nozzle; Jet (fluid); Conceptual design; Computer science; Aerospace engineering; Systems engineering; Aeronautics; Engineering; Human–computer interaction","score_opus":0.016648008675667497,"score_gpt":0.246344869592829,"score_spread":0.22969686091716152,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2958721697","genre_codex":"editorial","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":[0.0006998289,0.00068036217,0.010033314,0.017964464,0.9481983,0.000099056655,0.005643656,0.0058884397,0.010792684],"genre_scores_gemma":[0.059089772,0.0038989137,0.05757575,0.039565556,0.13853246,0.00058163324,0.015534594,0.01622624,0.6689951],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.9975708,0.0002233341,0.00027431897,0.00032959963,0.0013734333,0.00022848931],"domain_scores_gemma":[0.9795608,0.0025270358,0.0008524895,0.0015900164,0.014875929,0.0005938347],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0013031252,0.0023240391,0.0017202016,0.0036736047,0.002900149,0.0035173546,0.0032381385,0.006630096,0.16801508],"category_scores_gemma":[0.031184027,0.0013222371,0.00186873,0.0024566853,0.0016252619,0.0027290261,0.002295079,0.0067866654,0.065531686],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00006355302,0.0000064907344,0.00007070717,0.00013619274,0.000010113927,0.00014761127,0.000028819317,0.00030644043,0.00022194056,0.0012160216,0.9885555,0.009236578],"study_design_scores_gemma":[0.000080709135,0.000021189599,0.00071928476,0.00014628452,0.000026040396,0.00024712118,0.00007433735,0.0014867627,0.00074025686,0.0013947237,0.9950276,0.00003566371],"about_ca_topic_score_codex":0.02533147,"about_ca_topic_score_gemma":0.029926375,"teacher_disagreement_score":0.16801508,"about_ca_system_score_codex":0.0030237597,"about_ca_system_score_gemma":0.0044050226,"threshold_uncertainty_score":0.56206644},"labels":[],"label_agreement":null},{"id":"W2967632412","doi":"10.2514/6.2019-4191","title":"Modification of Paraffin-based Hybrid Rocket Fuels Using Structural Lattices","year":2019,"lang":"en","type":"article","venue":"AIAA Propulsion and Energy 2019 Forum","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 Calgary","funders":"","keywords":"Materials science; Rocket (weapon); Process engineering; Computer science; Aerospace engineering; Engineering","score_opus":0.019780043963481292,"score_gpt":0.2624661750111028,"score_spread":0.24268613104762152,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2967632412","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":[0.9858606,0.00036054017,0.005654141,0.00006731413,0.000059989656,0.000028536242,0.0002277184,0.00010428074,0.0076369103],"genre_scores_gemma":[0.9907582,0.0004214958,0.0030916727,0.000033651057,0.000006253267,0.000030175634,0.0002487034,0.000055009834,0.0053548994],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999453,0.000004704872,0.000003111009,0.000010699067,0.000015113219,0.000021087664],"domain_scores_gemma":[0.9999434,0.000011634192,0.000015260033,0.000010440126,0.000010096842,0.00000912166],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000082640225,0.00021906743,0.00010197582,0.00010455555,0.000094368086,0.00020704693,0.0002950637,0.00015642546,0.00389654],"category_scores_gemma":[0.00014028508,0.00011440459,0.00018592858,0.00014242614,0.00010344404,0.00042506185,0.0003051394,0.0003790303,0.00078518735],"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":[0.00024384142,0.00006799062,0.00020212098,0.00015389347,0.000016058975,0.00018315308,0.000057883623,0.0015450544,0.9875594,0.0020953887,0.0002821995,0.0075930487],"study_design_scores_gemma":[0.000013708849,0.00017886062,0.00025996237,0.000007212429,0.000006320035,0.000045585995,0.000029014605,0.0014806907,0.9937604,0.0001318247,0.0040799943,0.000006399097],"about_ca_topic_score_codex":0.000232913,"about_ca_topic_score_gemma":0.00062684686,"teacher_disagreement_score":0.00389654,"about_ca_system_score_codex":0.00016096322,"about_ca_system_score_gemma":0.00011482426,"threshold_uncertainty_score":0.013035178},"labels":[],"label_agreement":null},{"id":"W2967783566","doi":"10.2514/6.2019-4098","title":"Spectroscopic Techniques for Measuring Regression Rates of Liquefying Hybrid Rocket Fuels","year":2019,"lang":"en","type":"article","venue":"AIAA Propulsion and Energy 2019 Forum","topic":"Rocket and propulsion systems research","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 Calgary","funders":"","keywords":"Rocket (weapon); Environmental science; Computer science; Aerospace engineering; Engineering","score_opus":0.018298952370549407,"score_gpt":0.26892490904835187,"score_spread":0.25062595667780246,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2967783566","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":[0.72390693,0.005929305,0.25639433,0.00043207366,0.0002727531,0.0002320619,0.001681219,0.0016802942,0.009471006],"genre_scores_gemma":[0.8973637,0.0047859047,0.08711956,0.0002906188,0.00007914087,0.00032730572,0.0010968321,0.00024247631,0.008694436],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99921155,0.00014324034,0.00002830556,0.00017885742,0.0003554566,0.00008252307],"domain_scores_gemma":[0.9986626,0.00042224771,0.00032792444,0.0001425305,0.0003892994,0.000055305696],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0011758668,0.00070684636,0.0003273305,0.00149862,0.0006620507,0.00063024403,0.0012483151,0.0009570609,0.0025290186],"category_scores_gemma":[0.0020871179,0.00043275233,0.0003716243,0.0012310012,0.00038566982,0.0012023803,0.0006378605,0.0018168455,0.0008940835],"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":[0.00019516135,0.00009864796,0.0015171991,0.000090785295,0.00003742958,0.000037342586,0.00012658327,0.0003329315,0.9799247,0.00074319827,0.00035558626,0.016540358],"study_design_scores_gemma":[0.000012190553,0.00015657139,0.002358389,0.000017920183,0.000027955275,0.00011761531,0.00009864385,0.0058061727,0.9894405,0.00020775697,0.0017345042,0.000021945443],"about_ca_topic_score_codex":0.0015501812,"about_ca_topic_score_gemma":0.0023181029,"teacher_disagreement_score":0.0025290186,"about_ca_system_score_codex":0.0005544778,"about_ca_system_score_gemma":0.00043722123,"threshold_uncertainty_score":0.0084604025},"labels":[],"label_agreement":null},{"id":"W2967879232","doi":"10.2514/6.2019-4011","title":"Development and Test Flight of The Atlantis I Nitrous Oxide/Paraffin-based Hybrid Rocket","year":2019,"lang":"en","type":"article","venue":"AIAA Propulsion and Energy 2019 Forum","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":11,"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 Calgary","funders":"","keywords":"Nitrous oxide; Rocket (weapon); Aerospace engineering; Flight test; Test (biology); Computer science; Automotive engineering; Aeronautics; Materials science; Environmental science; Engineering; Chemistry; Geology","score_opus":0.005851604525573614,"score_gpt":0.192243881872936,"score_spread":0.18639227734736238,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2967879232","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":[0.96815944,0.0001353802,0.020086199,0.00010137575,0.00007802783,0.00027427712,0.00045129552,0.00056080305,0.010153144],"genre_scores_gemma":[0.956188,0.00016089118,0.023189351,0.00006728814,0.0000068006398,0.00015806634,0.000923764,0.00009004347,0.019215686],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998049,0.00001573522,0.0000061899063,0.000035385747,0.00010658569,0.00003117708],"domain_scores_gemma":[0.999796,0.000015796619,0.000025825753,0.000021050842,0.000091441296,0.00004993297],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00057043554,0.00027253863,0.00018182662,0.00029137894,0.000297848,0.00033983382,0.00073544105,0.00033249744,0.0028021939],"category_scores_gemma":[0.0002449672,0.00012086832,0.00021295354,0.00016928626,0.00017862828,0.00053446204,0.00048225635,0.00025818753,0.00077408575],"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":[0.0009296252,0.0004260329,0.0065665925,0.0001649505,0.00005306385,0.00025956274,0.00019158567,0.00950626,0.94166225,0.0012109713,0.0013431468,0.037686013],"study_design_scores_gemma":[0.00020115115,0.010247816,0.018886127,0.000031034044,0.000095066294,0.00038849187,0.0003334262,0.03391199,0.90524083,0.00024067891,0.030368797,0.00005454624],"about_ca_topic_score_codex":0.0017127335,"about_ca_topic_score_gemma":0.003213877,"teacher_disagreement_score":0.0028021939,"about_ca_system_score_codex":0.0003069443,"about_ca_system_score_gemma":0.00061503943,"threshold_uncertainty_score":0.009374261},"labels":[],"label_agreement":null},{"id":"W2968842602","doi":"10.2514/6.2019-4154","title":"Design of Two-Phase Injectors Using Analytical and Numerical Methods with Application to Hybrid Rockets","year":2019,"lang":"en","type":"article","venue":"AIAA Propulsion and Energy 2019 Forum","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":2,"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 Toronto","funders":"","keywords":"Injector; Computer science; Aerospace engineering; Phase (matter); Physics; Engineering; Mechanical engineering","score_opus":0.021217376730395057,"score_gpt":0.3320137832176104,"score_spread":0.31079640648721535,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2968842602","genre_codex":"methods","genre_gemma":"methods","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.05110654,0.00033370397,0.9393812,0.00013393177,0.000046650115,0.00021026503,0.000036726746,0.0003657001,0.008385354],"genre_scores_gemma":[0.7878897,0.0003480475,0.20444681,0.000058844867,0.00002775349,0.0004251795,0.000046129404,0.000080868725,0.006676636],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999728,0.000071358256,0.00001371973,0.000035512094,0.00012111114,0.000030323556],"domain_scores_gemma":[0.99948347,0.00020423943,0.0001109426,0.000024241903,0.00013873169,0.000038422473],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00081088906,0.00064341177,0.00081911875,0.00047658038,0.0006478121,0.0012379327,0.00093802135,0.00087875896,0.0017776841],"category_scores_gemma":[0.00094533793,0.00060732616,0.0005134583,0.0003268858,0.0006609352,0.00063065323,0.0008643368,0.0004845896,0.0003688856],"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":[0.00030377565,0.0001363104,0.00095064123,0.00030427857,0.000053223048,0.00010837309,0.000153758,0.8999436,0.0399906,0.010965652,0.0004908993,0.046598908],"study_design_scores_gemma":[0.00003146996,0.00014313168,0.00011260266,0.00001119535,0.000010358057,0.000016245236,0.00001891165,0.9923477,0.005461351,0.0007274076,0.0011094635,0.000010163295],"about_ca_topic_score_codex":0.0013128864,"about_ca_topic_score_gemma":0.0018124363,"teacher_disagreement_score":0.0017776841,"about_ca_system_score_codex":0.0005567215,"about_ca_system_score_gemma":0.0011471055,"threshold_uncertainty_score":0.005946934},"labels":[],"label_agreement":null},{"id":"W2972694487","doi":"10.4050/f-0075-2019-14481","title":"Preliminary Design of a Highly Efficient VTOL System Based on Tethered Fixed-Wing Aircraft","year":2019,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Fuselage; Payload (computing); Fixed wing; Wing; Control reconfiguration; Aerospace engineering; Elevator; Automotive engineering; Trajectory; Engineering; Rotor (electric); Computer science; Simulation; Mechanical engineering; Embedded system","score_opus":0.018027545071304857,"score_gpt":0.2325071700434522,"score_spread":0.21447962497214734,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2972694487","genre_codex":"empirical","genre_gemma":"methods","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6071971,0.00040719507,0.34919533,0.00033975666,0.0002349583,0.0005971713,0.0004183279,0.0021804117,0.039429806],"genre_scores_gemma":[0.9515046,0.00008043048,0.037566394,0.000042052845,0.000012098474,0.00012285112,0.00018881679,0.000053851796,0.010428797],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99988866,0.000016089605,0.000004557608,0.000023144363,0.00004653595,0.000021042337],"domain_scores_gemma":[0.99991894,0.000009850921,0.000010317082,0.00001068068,0.00003608506,0.000014013405],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012452423,0.000282816,0.00021448673,0.00019836873,0.0002871378,0.000510352,0.0004989074,0.0002966625,0.0036645562],"category_scores_gemma":[0.00015266116,0.00013200824,0.00023411775,0.00008429325,0.00014288811,0.00026851945,0.00020420877,0.00020752166,0.0008074985],"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":[0.0007123615,0.00025486934,0.00628948,0.0006193373,0.00012395633,0.0014208694,0.0005467447,0.24220783,0.5611784,0.007700816,0.0061272015,0.17281817],"study_design_scores_gemma":[0.00026765838,0.0043859524,0.010226336,0.00006412062,0.00012610292,0.00094236596,0.00030436908,0.7472699,0.16559261,0.0010521939,0.06969595,0.00007239183],"about_ca_topic_score_codex":0.0015911805,"about_ca_topic_score_gemma":0.0026418301,"teacher_disagreement_score":0.0036645562,"about_ca_system_score_codex":0.00038587707,"about_ca_system_score_gemma":0.00051739794,"threshold_uncertainty_score":0.012259126},"labels":[],"label_agreement":null},{"id":"W2980008434","doi":"10.1007/s13369-019-04158-1","title":"New Anti-balling Reamer Blade for Reaming in Soft and Sticky Formation Easy to Hydration and Collapsing","year":2019,"lang":"en","type":"article","venue":"Arabian Journal for Science and Engineering","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":4,"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 Regina","funders":"","keywords":"Reamer; Blade (archaeology); Materials science; Mechanics; Mechanical engineering; Engineering; Engineering drawing; Composite material; Physics","score_opus":0.016192390478546457,"score_gpt":0.2635282885300719,"score_spread":0.24733589805152542,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2980008434","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":[0.49193802,0.004768349,0.47747555,0.00056789647,0.0023692027,0.000452131,0.0003982623,0.00384834,0.01818228],"genre_scores_gemma":[0.61941046,0.00076186884,0.3618619,0.00033481748,0.0002238119,0.00018567473,0.00036556573,0.000268328,0.016587492],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99960595,0.000032474425,0.000031276883,0.0001010312,0.00017063892,0.000058704416],"domain_scores_gemma":[0.9995401,0.000041689196,0.00007116273,0.00010277548,0.00016134702,0.00008305552],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004550955,0.0006669975,0.00061455864,0.00056270993,0.0005578886,0.00046493465,0.0011461917,0.0007498104,0.0038639249],"category_scores_gemma":[0.0004208,0.00043093608,0.00044363798,0.00028452743,0.00036816683,0.00088301394,0.0006242641,0.00073752657,0.0015907024],"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":[0.00043342783,0.00014397482,0.0017738751,0.00055911887,0.000043481206,0.0006617903,0.0002512848,0.0020652579,0.88231075,0.0031121746,0.0049340497,0.10371089],"study_design_scores_gemma":[0.00024515565,0.0041907164,0.010313074,0.00011438804,0.00019909715,0.005130569,0.0004899357,0.07934613,0.79239666,0.002150319,0.10516166,0.00026236626],"about_ca_topic_score_codex":0.0002018419,"about_ca_topic_score_gemma":0.0006534885,"teacher_disagreement_score":0.0038639249,"about_ca_system_score_codex":0.00014589707,"about_ca_system_score_gemma":0.00043795476,"threshold_uncertainty_score":0.012926161},"labels":[],"label_agreement":null},{"id":"W2982439257","doi":"10.17073/1683-4518-2019-9-3-9","title":"Refractories of JSC BKO for the reconstruction of air heaters of JSC EVRAZ ZSMK according to the project of Paul Wurth","year":2019,"lang":"en","type":"article","venue":"NOVYE OGNEUPORY (NEW REFRACTORIES)","topic":"Rocket and propulsion systems research","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":"EVRAZ (Canada)","funders":"","keywords":"Electrical engineering; Engineering; Mechanical engineering; Materials science; Engineering physics","score_opus":0.027043192043304735,"score_gpt":0.28509424023771573,"score_spread":0.258051048194411,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2982439257","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.22347376,0.052158497,0.036005605,0.014208919,0.014471758,0.0024877833,0.020723179,0.003474411,0.632996],"genre_scores_gemma":[0.26926064,0.016094005,0.044845074,0.0010742175,0.0014004399,0.00068765815,0.025011552,0.0010617241,0.6405647],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9981895,0.00013919176,0.00008970472,0.0001463078,0.0012233343,0.00021187504],"domain_scores_gemma":[0.9984591,0.00008501234,0.0001100664,0.00021799677,0.00081903883,0.00030882665],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00247559,0.0007996259,0.00048321785,0.002143225,0.0013629269,0.000974319,0.0010922946,0.0008115638,0.03476703],"category_scores_gemma":[0.0018684783,0.00027797717,0.00046777798,0.0011362995,0.00034603995,0.00063109247,0.0016370985,0.0015152834,0.008438964],"study_design_candidate":"not_applicable","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":[0.0036983665,0.0003932224,0.004386293,0.0021072333,0.00010631652,0.0019993817,0.00088087685,0.005168269,0.19602545,0.08452722,0.27053532,0.43017215],"study_design_scores_gemma":[0.000075340686,0.0002574992,0.008630474,0.00012183682,0.000023334134,0.000546329,0.00011701188,0.00059501163,0.020778218,0.0010655227,0.9677637,0.000025644991],"about_ca_topic_score_codex":0.012392956,"about_ca_topic_score_gemma":0.009197982,"teacher_disagreement_score":0.03476703,"about_ca_system_score_codex":0.0024691136,"about_ca_system_score_gemma":0.0063186176,"threshold_uncertainty_score":0.11630732},"labels":[],"label_agreement":null},{"id":"W2997232336","doi":"10.2514/6.2020-1129","title":"Lockheed Martin Overview of the AFRL EXPEDITE Program: Power and Thermal Management System","year":2020,"lang":"en","type":"article","venue":"AIAA Scitech 2020 Forum","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lockheed Martin (Canada)","funders":"","keywords":"Aerospace; Systems engineering; Multidisciplinary design optimization; Avionics; Multidisciplinary approach; Engineering; Propulsion; Aeronautics; Computer science; Aerospace engineering; Manufacturing engineering","score_opus":0.021915952701007154,"score_gpt":0.2592212634639211,"score_spread":0.23730531076291395,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2997232336","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.014296591,0.0142854955,0.110954106,0.009611504,0.0015869142,0.00074871635,0.0023008112,0.0058779023,0.84033793],"genre_scores_gemma":[0.15075582,0.015641652,0.103097685,0.00234023,0.001195944,0.00093282934,0.0045667165,0.0015467533,0.7199224],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9993293,0.0000842712,0.000016112872,0.00005363203,0.0004523367,0.00006443778],"domain_scores_gemma":[0.9996902,0.000024702516,0.000021081702,0.00002857868,0.000159644,0.000075822834],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00093705294,0.000634298,0.00020896336,0.0009669519,0.0007563183,0.00144448,0.00056677876,0.0006660152,0.042754],"category_scores_gemma":[0.00068514457,0.00029856386,0.00024702813,0.000649393,0.00030940995,0.00092914107,0.0007870608,0.0011972415,0.013125663],"study_design_candidate":"not_applicable","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":[0.00029749778,0.00018800404,0.001498245,0.0004452286,0.0000137186225,0.00016133895,0.00034222426,0.01933151,0.017404165,0.06603346,0.37646157,0.5178229],"study_design_scores_gemma":[0.00001313775,0.0001538786,0.000857297,0.00009758544,0.000003616449,0.000058031517,0.00004087305,0.0028949853,0.001565733,0.0018070524,0.9924981,0.000009800853],"about_ca_topic_score_codex":0.007380836,"about_ca_topic_score_gemma":0.010762385,"teacher_disagreement_score":0.042754,"about_ca_system_score_codex":0.0018736395,"about_ca_system_score_gemma":0.0024410344,"threshold_uncertainty_score":0.14302635},"labels":[],"label_agreement":null},{"id":"W3007784015","doi":"10.2514/6.iac-06-b4.2.08","title":"Free Flyer Capture - New Robotic Challenges from the International Space Station","year":2006,"lang":"en","type":"article","venue":"57th International Astronautical Congress","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Canadian Space Agency","funders":"","keywords":"International Space Station; Aerospace engineering; Aeronautics; Space (punctuation); Systems engineering; Engineering; Computer science; Astrobiology; Environmental science; Physics; Operating system","score_opus":0.02616076684412375,"score_gpt":0.260578384980967,"score_spread":0.23441761813684328,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3007784015","genre_codex":"empirical","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"other","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.57836276,0.03688131,0.056520853,0.08769245,0.0041766497,0.00022488112,0.0037366338,0.0013128419,0.23109171],"genre_scores_gemma":[0.8679271,0.013479147,0.037409484,0.0037267641,0.0012736152,0.00008020798,0.0041131317,0.00017720793,0.07181328],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9997453,0.000027303842,0.000005640606,0.000032503558,0.00014168622,0.000047517624],"domain_scores_gemma":[0.99967575,0.00007444618,0.000014307807,0.0000339532,0.00010472314,0.000096756325],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0010959076,0.00034236116,0.00035533155,0.00043136705,0.0011665018,0.0015618333,0.00045830457,0.0011447901,0.003889635],"category_scores_gemma":[0.00088164903,0.0001806181,0.0002722457,0.00046047685,0.0005501167,0.0016324144,0.0009932631,0.0015844919,0.0005522862],"study_design_candidate":"not_applicable","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":[0.0010593898,0.000335082,0.036295004,0.00056812685,0.00014577685,0.0020372693,0.0035808973,0.030938368,0.02855292,0.027442073,0.19695316,0.67209196],"study_design_scores_gemma":[0.00011746028,0.0010633904,0.088114984,0.00043939214,0.00014419615,0.0015765625,0.008270467,0.05145647,0.009206959,0.017858652,0.8215518,0.0001997836],"about_ca_topic_score_codex":0.018478196,"about_ca_topic_score_gemma":0.07642833,"teacher_disagreement_score":0.018478196,"about_ca_system_score_codex":0.0008579861,"about_ca_system_score_gemma":0.0011972699,"threshold_uncertainty_score":0.036741257},"labels":[],"label_agreement":null},{"id":"W3011597137","doi":"10.22215/etd/2012-06896","title":"Simulation of a rocket base combined cycle exchange inlet at subsonic conditions","year":2012,"lang":"en","type":"dissertation","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Carleton University; Canadian Heritage; Library and Archives Canada","funders":"","keywords":"Rocket (weapon); Base (topology); Aeronautics; Aerospace engineering; Engineering; Physics; Mathematics; Mathematical analysis","score_opus":0.02752607871821001,"score_gpt":0.30555899397679515,"score_spread":0.27803291525858514,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3011597137","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":[0.95089024,0.0001366615,0.0074221264,0.00044111468,0.000121651545,0.00011408841,0.0015555494,0.0003309965,0.03898755],"genre_scores_gemma":[0.989892,0.00005600676,0.0016866913,0.00004730779,0.0000061181636,0.00005240152,0.00065754383,0.0000411034,0.007560827],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99985635,0.000018693217,0.000006411158,0.00002612819,0.000036292462,0.000056099794],"domain_scores_gemma":[0.99948597,0.00022834208,0.000033861652,0.000025628435,0.00011142841,0.000114762],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025344256,0.0005979175,0.0009221833,0.0006452266,0.0012732926,0.0012706666,0.00095035596,0.0021353615,0.010778226],"category_scores_gemma":[0.0008902132,0.0004253973,0.00078212627,0.00053842214,0.00071203505,0.00077540067,0.0007736377,0.0010837131,0.00054725393],"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":[0.00025770935,0.00012803734,0.0032552003,0.00003939698,0.000018791869,0.0002892965,0.00005696097,0.9909863,0.0017144167,0.0006929242,0.00066127983,0.001899622],"study_design_scores_gemma":[0.000045394223,0.00009914868,0.0014766287,0.0000070394462,0.000009442963,0.000014352309,0.000106816864,0.9964798,0.001097702,0.00016999514,0.0004828726,0.000010774939],"about_ca_topic_score_codex":0.06393842,"about_ca_topic_score_gemma":0.045561917,"teacher_disagreement_score":0.06393842,"about_ca_system_score_codex":0.0014128732,"about_ca_system_score_gemma":0.0018421637,"threshold_uncertainty_score":0.12713248},"labels":[],"label_agreement":null},{"id":"W3038172359","doi":"10.26467/2079-0619-2020-23-3-17-28","title":"Substantiation of the ratio of biofuel and kerosin in the mixture for its application as aviation fuel","year":2020,"lang":"en","type":"article","venue":"Civil Aviation High TECHNOLOGIES","topic":"Rocket and propulsion systems research","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":"International Civil Aviation Organization","funders":"","keywords":"Kerosene; Aviation; Aviation fuel; Jet fuel; Quality (philosophy); Civil aviation; Renewable fuels; Engineering; Fossil fuel; Petroleum; Production (economics); Petroleum product; Environmental science; Waste management; Environmental economics; Aerospace engineering; Economics; Chemistry","score_opus":0.017286609914085073,"score_gpt":0.23672192221499147,"score_spread":0.2194353123009064,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3038172359","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":[0.52253747,0.016029317,0.40969878,0.0015042046,0.00045151295,0.00026021173,0.0005670467,0.00055264705,0.048398796],"genre_scores_gemma":[0.9538349,0.0037548966,0.03870715,0.00011619104,0.000034531404,0.00009476953,0.00016949512,0.000055355653,0.0032326535],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99865603,0.00021946963,0.0000827629,0.00039397873,0.0005608786,0.00008688553],"domain_scores_gemma":[0.99936706,0.00028439218,0.00012232033,0.00006182321,0.00014451974,0.000019909565],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0012035221,0.000500395,0.0004292291,0.0013778553,0.0004058505,0.0009566999,0.00085604424,0.0008442534,0.0018522218],"category_scores_gemma":[0.003526936,0.0003276649,0.00076298794,0.00068184047,0.0008005954,0.0015297331,0.0006288796,0.0007164832,0.00072176434],"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":[0.00049721124,0.00016317457,0.012791271,0.0017187151,0.00008743147,0.0009374635,0.00042900504,0.021172842,0.78705794,0.08300713,0.0011008934,0.09103695],"study_design_scores_gemma":[0.000016276004,0.00038504731,0.0041353754,0.0001390179,0.00012348518,0.00077714334,0.00025800613,0.08069824,0.8784591,0.017167747,0.017766478,0.000074078846],"about_ca_topic_score_codex":0.0014507344,"about_ca_topic_score_gemma":0.0013812161,"teacher_disagreement_score":0.0018522218,"about_ca_system_score_codex":0.000589372,"about_ca_system_score_gemma":0.00071001344,"threshold_uncertainty_score":0.006364882},"labels":[],"label_agreement":null},{"id":"W3039770473","doi":"10.1088/1742-6596/1549/4/042117","title":"Structural design and application analysis of Laval nozzle","year":2020,"lang":"en","type":"article","venue":"Journal of Physics Conference Series","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":"Nozzle; Stove; Gambit; Modular design; Combustion; Propulsion; Mechanical engineering; Nuclear engineering; Rocket engine nozzle; Liquid gas; Environmental science; Petroleum engineering; Engineering; Aerospace engineering; Automotive engineering; Computer science; Fluent; Chemistry; Physics; Computational fluid dynamics; Thermodynamics","score_opus":0.04334144229108587,"score_gpt":0.27148861778573025,"score_spread":0.22814717549464436,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3039770473","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":[0.28150004,0.0008570776,0.6716927,0.00028145622,0.00012074668,0.00022150525,0.00031788406,0.0014772419,0.04353134],"genre_scores_gemma":[0.96237755,0.00016900415,0.032320477,0.00002057567,0.000008935324,0.000065354616,0.00009190832,0.00004495537,0.0049012885],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993932,0.00006027235,0.000022983299,0.00008302439,0.00038651115,0.000053935837],"domain_scores_gemma":[0.9996457,0.000057779504,0.000052599604,0.00004888843,0.00017581257,0.000019266421],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005994301,0.00032228808,0.0003528319,0.0006692462,0.00041293429,0.0008522211,0.00087078585,0.0006715709,0.0040466087],"category_scores_gemma":[0.0007925342,0.00023002527,0.00049525994,0.00030282122,0.00040150285,0.00044929277,0.00050503685,0.00022375789,0.0005727758],"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":[0.00022490298,0.00011550347,0.009477274,0.0004738958,0.000042853622,0.0006182642,0.00039097414,0.5980185,0.24180548,0.015972212,0.0017808096,0.13107926],"study_design_scores_gemma":[0.000031138392,0.0006423584,0.0058303424,0.000048335467,0.000037312588,0.0003608958,0.00017553265,0.92067987,0.053894404,0.0016580448,0.016591467,0.000050289505],"about_ca_topic_score_codex":0.0013388353,"about_ca_topic_score_gemma":0.00079056516,"teacher_disagreement_score":0.0040466087,"about_ca_system_score_codex":0.0005814653,"about_ca_system_score_gemma":0.0008021348,"threshold_uncertainty_score":0.013537288},"labels":[],"label_agreement":null},{"id":"W3045678518","doi":"10.2514/1.b37918","title":"Reducing the Ignition Delay of Hypergolic Hybrid Rocket Fuels","year":2020,"lang":"en","type":"article","venue":"Journal of Propulsion and Power","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":20,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Polytechnique Montréal; General Dynamics (Canada)","funders":"Natural Sciences and Engineering Research Council of Canada; Canadian Space Agency","keywords":"Materials science; Propellant; Ignition system; Combustion; Composite material; Polymer; Chemical engineering; Rocket (weapon); Rocket propellant; Organic chemistry; Chemistry; Thermodynamics; Aerospace engineering","score_opus":0.024963739898632223,"score_gpt":0.2516905932241823,"score_spread":0.2267268533255501,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3045678518","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":[0.99799937,0.0003822487,0.0010047236,0.000009756278,0.000004947222,0.000008489588,0.000054650183,0.000019860336,0.0005159592],"genre_scores_gemma":[0.9970354,0.00035053026,0.0014560235,0.000007920283,0.0000014618057,0.00001262775,0.00012211993,0.000019322695,0.0009945964],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99991,0.000007939961,0.0000055412365,0.000016798562,0.00003376043,0.00002603043],"domain_scores_gemma":[0.9998621,0.00003884163,0.000045162393,0.0000069504777,0.000031303727,0.000015644215],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000105567895,0.0002544573,0.00017169722,0.00018429242,0.00007610103,0.00025318968,0.00021675703,0.00019335379,0.001382542],"category_scores_gemma":[0.00024997766,0.00009156932,0.000117369294,0.00017867991,0.00011001769,0.00029846083,0.00019750264,0.0003240334,0.00024113689],"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":[0.00022668387,0.0000205178,0.00025889196,0.000046230518,0.000005038471,0.00003063009,0.000019058818,0.00020810273,0.9972766,0.00003879698,0.000009487474,0.0018599966],"study_design_scores_gemma":[0.000002312228,0.00014887394,0.00072056294,0.0000018541182,0.0000038744397,0.000014527812,0.000011566963,0.00041282392,0.9984541,0.0000046305345,0.00022332433,0.0000016340049],"about_ca_topic_score_codex":0.00053962,"about_ca_topic_score_gemma":0.001427659,"teacher_disagreement_score":0.001382542,"about_ca_system_score_codex":0.00026020405,"about_ca_system_score_gemma":0.00014432205,"threshold_uncertainty_score":0.0046250224},"labels":[],"label_agreement":null},{"id":"W3049297806","doi":"10.22215/etd/2010-09353","title":"An ejector air intake design method for a novel rocket-based combined-cycle rocket nozzle","year":2010,"lang":"en","type":"dissertation","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":7,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Carleton University; Canadian Heritage; Library and Archives Canada","funders":"","keywords":"Rocket (weapon); Injector; Aeronautics; Nozzle; Rocket engine nozzle; Engineering; Aerospace engineering; Mechanical engineering","score_opus":0.03176093729751083,"score_gpt":0.3339758805235247,"score_spread":0.3022149432260139,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3049297806","genre_codex":"methods","genre_gemma":"methods","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.034533143,0.00044727573,0.9556732,0.00005618766,0.00009880897,0.00019024724,0.00004659222,0.00066803163,0.008286486],"genre_scores_gemma":[0.45026937,0.0005359864,0.52549404,0.00006473426,0.00004802382,0.00027834415,0.0001736471,0.00020986107,0.022925954],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99972373,0.000016736014,0.000014519634,0.000046830814,0.00017974408,0.000018389543],"domain_scores_gemma":[0.9998228,0.000030784413,0.000025952659,0.00001408572,0.0000939965,0.000012352138],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00038689162,0.0003227705,0.000534621,0.00037383073,0.00042405206,0.00087838504,0.0012230753,0.0006900017,0.0043299044],"category_scores_gemma":[0.00035372257,0.00032699085,0.00047540572,0.00025710644,0.0001612285,0.0006452033,0.0005571151,0.0004159638,0.0008893891],"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":[0.00036547313,0.00017177165,0.0015249512,0.0008296324,0.00005404277,0.00023242607,0.00025004,0.045770176,0.6924581,0.009651684,0.0023731212,0.24631861],"study_design_scores_gemma":[0.00021298493,0.0016599302,0.0031646625,0.00009802947,0.00009156446,0.000904795,0.00011565674,0.55163103,0.36793473,0.0011674714,0.07290574,0.00011335497],"about_ca_topic_score_codex":0.00043026824,"about_ca_topic_score_gemma":0.000885394,"teacher_disagreement_score":0.0043299044,"about_ca_system_score_codex":0.00030858038,"about_ca_system_score_gemma":0.00067298685,"threshold_uncertainty_score":0.014484942},"labels":[],"label_agreement":null},{"id":"W3094257177","doi":"10.4050/f-0076-2020-16362","title":"Cold Weather Testing of the Bell 525 Relentless","year":2020,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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":"Extreme Cold; Environmental science; Cold weather; Aerospace engineering; Aerodynamics; Aeronautics; Rotor (electric); Meteorology; Engineering; Automotive engineering; Mechanical engineering; Physics; Geology; Climatology","score_opus":0.05462095503080544,"score_gpt":0.23749805136657226,"score_spread":0.18287709633576682,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3094257177","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":[0.9684146,0.0003284826,0.011450609,0.00022175832,0.00011459392,0.00014398883,0.0009422037,0.00053756515,0.017846111],"genre_scores_gemma":[0.9708356,0.00010437916,0.0062494073,0.00027043937,0.000014359262,0.000058152295,0.0015349468,0.00010196298,0.020830683],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9988617,0.00008905587,0.000039363258,0.00025881207,0.0005643118,0.0001867203],"domain_scores_gemma":[0.9990471,0.000086626525,0.00006003804,0.00011507055,0.0005123119,0.00017879318],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0009771283,0.00044429273,0.00030505008,0.0005261048,0.0012185066,0.00065309653,0.0006734305,0.0006619539,0.0063601187],"category_scores_gemma":[0.0009667667,0.00029697292,0.0002819502,0.00023087073,0.0005205748,0.0005281359,0.00068900624,0.0006110799,0.0019756726],"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":[0.0014425332,0.00027923632,0.037397467,0.00018119623,0.00004890682,0.0013295399,0.0019863246,0.0022132716,0.88419247,0.001492446,0.0077872104,0.061649363],"study_design_scores_gemma":[0.00019381984,0.011257346,0.3296411,0.00015669162,0.00015061659,0.0014399498,0.0017203277,0.0095100645,0.55187213,0.00034885172,0.09350923,0.00019998815],"about_ca_topic_score_codex":0.025956329,"about_ca_topic_score_gemma":0.07070463,"teacher_disagreement_score":0.025956329,"about_ca_system_score_codex":0.0010379297,"about_ca_system_score_gemma":0.0006492027,"threshold_uncertainty_score":0.05161053},"labels":[],"label_agreement":null},{"id":"W3105557933","doi":"10.11159/ffhmt20.178","title":"Modeling Combustion and Heat Transfer in a Single-Element GCH4/GOX Rocket Combustor","year":2020,"lang":"en","type":"article","venue":"Proceedings of the ... International Conference on Fluid Flow, Heat and Mass Transfer","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Combustor; Combustion; Rocket (weapon); Heat transfer; Aerospace engineering; Finite element method; Materials science; Mechanical engineering; Engineering; Mechanics; Structural engineering; Physics; Chemistry","score_opus":0.05123383994153683,"score_gpt":0.2478323225472343,"score_spread":0.19659848260569748,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3105557933","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":[0.9500086,0.00019219122,0.0430806,0.00009750222,0.000023615507,0.000120355086,0.00021894526,0.00031771944,0.0059403563],"genre_scores_gemma":[0.9796641,0.0001294842,0.016551651,0.000019602996,0.0000062460626,0.00012894152,0.00013105877,0.00004216605,0.0033266842],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99988616,0.000024085417,0.000005606699,0.000023293973,0.000041423555,0.000019353787],"domain_scores_gemma":[0.9998504,0.000082558436,0.000021092863,0.000013519067,0.000022242606,0.000010138492],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00026786816,0.0005352433,0.00063100917,0.00038998586,0.00050426193,0.00065855053,0.0010086717,0.0010666252,0.0016207016],"category_scores_gemma":[0.00044842137,0.00026867285,0.00052482093,0.0002966758,0.00060902827,0.00043234703,0.00048017525,0.00048314143,0.00025174086],"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":[0.000073842755,0.000046407466,0.0012796586,0.000053928718,0.0000108751165,0.00007204371,0.00006302765,0.9819639,0.012511234,0.0008249307,0.00006318135,0.0030370378],"study_design_scores_gemma":[0.000014479192,0.000039734347,0.0005611305,0.0000035383946,0.0000046308433,0.000014643652,0.000020790887,0.99337363,0.0056131165,0.0001326726,0.00021597887,0.0000056245594],"about_ca_topic_score_codex":0.015645426,"about_ca_topic_score_gemma":0.0054180017,"teacher_disagreement_score":0.015645426,"about_ca_system_score_codex":0.00078699976,"about_ca_system_score_gemma":0.0010647735,"threshold_uncertainty_score":0.031108677},"labels":[],"label_agreement":null},{"id":"W3111935658","doi":"","title":"Numerical investigation of non-equilibrium steam condensing flow in various Laval nozzles","year":2020,"lang":"en","type":"dissertation","venue":"LUTPub (LUT University)","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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; Mechanics; Rocket engine nozzle; Flow (mathematics); Mechanical engineering; Nuclear engineering; Thermodynamics; Engineering; Environmental science; Physics","score_opus":0.012669431558342876,"score_gpt":0.21413957783892404,"score_spread":0.20147014628058116,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3111935658","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":[0.97459275,0.00043642148,0.016065741,0.00019227514,0.00005696231,0.000062143255,0.00025523137,0.00023363525,0.00810502],"genre_scores_gemma":[0.9921138,0.00011479616,0.005899386,0.000018271818,0.000007107888,0.000028923136,0.00011536873,0.000016371616,0.0016860632],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997938,0.000045431883,0.000016541155,0.000032507796,0.000061724575,0.000049960203],"domain_scores_gemma":[0.9993734,0.0003228337,0.00008823122,0.0000323026,0.00012066381,0.000062574916],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00052463886,0.00032936866,0.00062451995,0.00068853324,0.000659246,0.0009420562,0.00068439863,0.0010380425,0.001478558],"category_scores_gemma":[0.0012262504,0.00020606634,0.0004915316,0.0005707972,0.0007257617,0.000359714,0.0004815857,0.00037702243,0.00013244576],"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":[0.0002627891,0.00016944656,0.009829991,0.00016431425,0.000032458647,0.0006209751,0.00024724286,0.95525295,0.023596805,0.0025223123,0.00035547192,0.006945206],"study_design_scores_gemma":[0.000019179266,0.000093887116,0.0015334218,0.000008560206,0.000005846172,0.00002998644,0.000055537912,0.9949414,0.0028186669,0.00015569266,0.00032812636,0.000009659551],"about_ca_topic_score_codex":0.011237178,"about_ca_topic_score_gemma":0.0056508156,"teacher_disagreement_score":0.011237178,"about_ca_system_score_codex":0.00086438004,"about_ca_system_score_gemma":0.00068149803,"threshold_uncertainty_score":0.022343516},"labels":[],"label_agreement":null},{"id":"W3113934359","doi":"10.21611/qirt.2020.157","title":"Temperature Calculation of a Steel Plate under Kerosene Flame Attack using TwoColour Pyrometry","year":2020,"lang":"en","type":"article","venue":"Proceedings of the 2020 International Conference on Quantitative InfraRed Thermography","topic":"Rocket and propulsion systems research","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":"Université Laval","funders":"","keywords":"Pyrometer; Kerosene; Materials science; Metallurgy; Temperature measurement; Physics; Thermodynamics","score_opus":0.08852341066091932,"score_gpt":0.32538030659676187,"score_spread":0.23685689593584255,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3113934359","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":[0.8149041,0.00056275364,0.17694856,0.0000665331,0.00014683652,0.00017539941,0.00069001684,0.0009930838,0.005512607],"genre_scores_gemma":[0.94435316,0.00047624894,0.049965113,0.000022013211,0.000015380276,0.000102697195,0.00044025795,0.00014183178,0.004483258],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99943656,0.000022547458,0.000015279044,0.00012205034,0.00036445528,0.000039139537],"domain_scores_gemma":[0.9996152,0.000059153877,0.00006688453,0.000050107195,0.00018616763,0.000022579914],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00030915372,0.00056518626,0.00038248327,0.00083277666,0.00030207264,0.0004898214,0.00065625523,0.00043996033,0.002123036],"category_scores_gemma":[0.00066257553,0.00035428503,0.0004173184,0.0006415738,0.00039990386,0.00048223592,0.00030034332,0.0006561858,0.0009757785],"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":[0.00010158429,0.000016580587,0.00088829425,0.000063800915,0.0000063691587,0.00008829543,0.000060145507,0.0010214346,0.99137664,0.00018090992,0.00009811357,0.0060977465],"study_design_scores_gemma":[0.000007333411,0.00014852353,0.009320542,0.0000060832535,0.000012919481,0.00012452166,0.000058848927,0.013321877,0.9755492,0.00009847365,0.0013313919,0.000020397336],"about_ca_topic_score_codex":0.0010879055,"about_ca_topic_score_gemma":0.0015171284,"teacher_disagreement_score":0.002123036,"about_ca_system_score_codex":0.0003621308,"about_ca_system_score_gemma":0.00027792866,"threshold_uncertainty_score":0.007102251},"labels":[],"label_agreement":null},{"id":"W3118418716","doi":"10.2514/6.2021-2031","title":"Computational Analysis on De Laval Dual Throat Micronozzle","year":2021,"lang":"en","type":"article","venue":"AIAA Scitech 2021 Forum","topic":"Rocket and propulsion systems research","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":"Aerospace engineering; Mechanical engineering; Thrust; Dual (grammatical number); Propulsion; Satellite; Computer science; Simulation; Engineering","score_opus":0.011599484075840093,"score_gpt":0.26560137580936427,"score_spread":0.25400189173352417,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3118418716","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":[0.8530738,0.0011019029,0.07408977,0.0021816648,0.0002460166,0.00020327102,0.004809776,0.00083024515,0.063463606],"genre_scores_gemma":[0.9753243,0.00020642452,0.015307989,0.0001275089,0.000024534742,0.00014081455,0.0012162491,0.00011743714,0.0075347945],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99989045,0.00002196505,0.000004159131,0.000019801253,0.000024471532,0.00003918798],"domain_scores_gemma":[0.99945563,0.00036112935,0.00004044767,0.00002201055,0.000066916735,0.00005389447],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00022790722,0.0005530197,0.0006991915,0.00051378796,0.0007831704,0.0011008348,0.0009085741,0.0016498311,0.007681321],"category_scores_gemma":[0.00112555,0.0002840989,0.00071814714,0.00036675367,0.0005218178,0.00051943137,0.00075667695,0.00073054066,0.0003834639],"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":[0.000055273547,0.00003816591,0.0015324441,0.000040302508,0.000013081051,0.00010860538,0.000018033163,0.9931826,0.000526056,0.0021891228,0.0007419832,0.0015544234],"study_design_scores_gemma":[0.000012175735,0.000016436608,0.0003704487,0.000005827714,0.0000031373258,0.0000120548,0.000027096725,0.99849856,0.00016428185,0.00037846804,0.0005073647,0.0000041889316],"about_ca_topic_score_codex":0.032988694,"about_ca_topic_score_gemma":0.02046901,"teacher_disagreement_score":0.032988694,"about_ca_system_score_codex":0.0010217115,"about_ca_system_score_gemma":0.0010842661,"threshold_uncertainty_score":0.06559336},"labels":[],"label_agreement":null},{"id":"W3120670561","doi":"10.22214/ijraset.2021.32720","title":"Numerical Analysis of De Laval Nozzle under Surrounding Zone and Compressed Flow","year":2021,"lang":"en","type":"article","venue":"International Journal for Research in Applied Science and Engineering Technology","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":23,"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; Geology; Flow (mathematics); Mechanics; Materials science; Physics; Aerospace engineering; Engineering","score_opus":0.05620046248746868,"score_gpt":0.38175421768065537,"score_spread":0.3255537551931867,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3120670561","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":[0.8773794,0.0027146265,0.06368112,0.0010622998,0.00032930932,0.00015234684,0.00091307826,0.00077266904,0.05299512],"genre_scores_gemma":[0.99157894,0.00030266674,0.004259165,0.000036665155,0.000022524448,0.000027324983,0.00013173456,0.000032755317,0.0036081641],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99971884,0.00003810867,0.000016706304,0.00004349184,0.00010277817,0.0000801372],"domain_scores_gemma":[0.9995547,0.00016660329,0.00006714935,0.00002495778,0.00013804327,0.000048374306],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00047430754,0.0004392848,0.000746354,0.0007362387,0.0008075463,0.0011860428,0.0008674452,0.0013131534,0.0029045867],"category_scores_gemma":[0.0012233969,0.00025054003,0.0006002998,0.00061629893,0.00087318546,0.0005643893,0.00056253,0.00044425394,0.00022376365],"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":[0.00029593127,0.00010053011,0.0075893844,0.00029116136,0.000040987306,0.0011040089,0.00028624796,0.9438143,0.024060387,0.010693077,0.0015807773,0.010143243],"study_design_scores_gemma":[0.000022087163,0.00004157072,0.0014364739,0.000014528652,0.0000069717817,0.000056742407,0.0000586462,0.99551105,0.0017966939,0.0004742514,0.00056352007,0.000017371864],"about_ca_topic_score_codex":0.017225591,"about_ca_topic_score_gemma":0.0051124287,"teacher_disagreement_score":0.017225591,"about_ca_system_score_codex":0.0008340056,"about_ca_system_score_gemma":0.0008233344,"threshold_uncertainty_score":0.034250677},"labels":[],"label_agreement":null},{"id":"W3124074688","doi":"10.13009/eucass2017-64","title":"A numerical analysis of aluminum droplet combustion driven instabilities in solid rocket motors","year":2017,"lang":"en","type":"preprint","venue":"HAL (Le Centre pour la Communication Scientifique Directe)","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Safran Electronics (Canada)","funders":"Centre National d’Etudes Spatiales","keywords":"Mechanics; Combustion; Oscillation (cell signaling); Instability; Solid-fuel rocket; Rocket (weapon); Amplitude; Materials science; Physics; Propellant; Chemistry; Aerospace engineering; Engineering; Optics","score_opus":0.02024563069121027,"score_gpt":0.26458534565956976,"score_spread":0.2443397149683595,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3124074688","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":[0.9125835,0.0003412871,0.06682711,0.0003279956,0.0000390496,0.00006934402,0.00019531019,0.0002718532,0.019344611],"genre_scores_gemma":[0.98995376,0.00007570364,0.007852372,0.000018678,0.000006871475,0.000037490747,0.00006130387,0.000028997556,0.0019648778],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999008,0.000020647145,0.000005203556,0.000013440147,0.000039347055,0.000020523623],"domain_scores_gemma":[0.9995229,0.00025628856,0.00008800087,0.000027301257,0.000069616275,0.00003588553],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00026951768,0.00035042205,0.00041673178,0.0004478878,0.0004415986,0.0006571211,0.0005177046,0.0009173939,0.0021114333],"category_scores_gemma":[0.0013328088,0.0001660627,0.00034483033,0.00040788404,0.0007388671,0.00034355046,0.0004875905,0.00036293623,0.0001666825],"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":[0.00009010392,0.00004405975,0.0022629655,0.00007737803,0.00002038304,0.00025152336,0.00009438929,0.9739855,0.01325306,0.0059370524,0.00019056708,0.0037929486],"study_design_scores_gemma":[0.000005185573,0.0000127385965,0.00025115858,0.000002737462,0.0000017965422,0.000009288026,0.000013394978,0.99870574,0.00056993024,0.00032270816,0.00010245453,0.0000028558554],"about_ca_topic_score_codex":0.0049230475,"about_ca_topic_score_gemma":0.0027038623,"teacher_disagreement_score":0.0049230475,"about_ca_system_score_codex":0.000504834,"about_ca_system_score_gemma":0.00048270868,"threshold_uncertainty_score":0.009788752},"labels":[],"label_agreement":null},{"id":"W3127889972","doi":"10.22034/ijche.2020.253425.1354","title":"Developing a Mathematical Model to Predict the Behavior of a Supersonic Superheated Steam Flow inside a Laval Nozzle","year":2020,"lang":"en","type":"article","venue":"DOAJ (DOAJ: Directory of Open Access Journals)","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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; Superheated steam; Superheating; Mechanics; Supersonic speed; Computational fluid dynamics; Inlet; Mach number; Condensation; Flow (mathematics); Thermodynamics; Engineering; Mechanical engineering; Physics","score_opus":0.3574759100046458,"score_gpt":0.5191873317998676,"score_spread":0.16171142179522185,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3127889972","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":[0.088123515,0.00036111654,0.9026228,0.00024638156,0.00006793577,0.00014983697,0.00022686001,0.00064164033,0.0075599276],"genre_scores_gemma":[0.9353082,0.00055313663,0.05555738,0.000055621924,0.000037529655,0.0005081824,0.00024315958,0.00008240174,0.007654327],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99973124,0.000056327783,0.000016932807,0.00006452213,0.00008687777,0.000044146203],"domain_scores_gemma":[0.9993911,0.00034659004,0.00009764206,0.000018664181,0.00013097141,0.0000150832075],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00076975126,0.00076312246,0.0008426716,0.00063770823,0.00051145186,0.0014061286,0.0011063035,0.001473207,0.0016070557],"category_scores_gemma":[0.0017033799,0.00050187844,0.0011349504,0.0005063924,0.00061956607,0.0010221915,0.0006338167,0.0011219676,0.0004030164],"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":[0.000014387987,0.000017225682,0.0006130271,0.000032282576,0.000008877345,0.00004640638,0.000023007817,0.9930298,0.0016088561,0.0018929235,0.000071501774,0.0026417188],"study_design_scores_gemma":[0.0000016030724,0.000011063014,0.000076651406,0.0000023544455,0.0000028637057,0.000003477774,0.0000029208836,0.99929595,0.0003211533,0.00018857603,0.00009108336,0.0000023408268],"about_ca_topic_score_codex":0.012492435,"about_ca_topic_score_gemma":0.005323538,"teacher_disagreement_score":0.012492435,"about_ca_system_score_codex":0.0010030298,"about_ca_system_score_gemma":0.002134945,"threshold_uncertainty_score":0.02483946},"labels":[],"label_agreement":null},{"id":"W3131490899","doi":"","title":"Towards Automated Thruster Control in a Small Observation Class ROV","year":2015,"lang":"en","type":"article","venue":"The Twenty-fifth International Ocean and Polar Engineering Conference","topic":"Rocket and propulsion systems research","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 Victoria","funders":"","keywords":"Remotely operated underwater vehicle; Class (philosophy); Aeronautics; Control (management); Computer science; Artificial intelligence; Engineering; Mobile robot; Robot","score_opus":0.044451592630611346,"score_gpt":0.2601117555269258,"score_spread":0.21566016289631443,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3131490899","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":[0.096594974,0.00010675643,0.89668477,0.00026805568,0.000077455705,0.00008507794,0.00004053745,0.001144957,0.0049974197],"genre_scores_gemma":[0.90135187,0.000051821913,0.0928839,0.000058700756,0.000039523035,0.000058203186,0.000047033973,0.00005063904,0.0054581785],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99979347,0.000027940048,0.0000065296194,0.00005699639,0.00008406002,0.00003107194],"domain_scores_gemma":[0.9996282,0.000109678185,0.00004868296,0.00007175208,0.00010452958,0.00003706519],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003486912,0.0004114535,0.0003729883,0.00014712645,0.0004299261,0.0007118708,0.00073151203,0.00058239244,0.0020116742],"category_scores_gemma":[0.0007186151,0.00024001708,0.00020300264,0.00010375236,0.00053098024,0.00043380552,0.00074873114,0.00081734103,0.00045346463],"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":[0.0009437559,0.00021542785,0.002866387,0.00016046275,0.00005458892,0.00025099577,0.00044641225,0.30640316,0.42329988,0.012368885,0.0029760532,0.25001395],"study_design_scores_gemma":[0.00005330891,0.00037224495,0.00114096,0.000006650469,0.0000126820005,0.000037552778,0.000036428166,0.97797126,0.013978941,0.0021944123,0.0041845497,0.000010966087],"about_ca_topic_score_codex":0.0038016906,"about_ca_topic_score_gemma":0.00543029,"teacher_disagreement_score":0.0038016906,"about_ca_system_score_codex":0.00028086948,"about_ca_system_score_gemma":0.000694236,"threshold_uncertainty_score":0.0075591207},"labels":[],"label_agreement":null},{"id":"W3135652303","doi":"10.1615/intjenergeticmaterialschemprop.2021036811","title":"DEVELOPMENT OF A PARAFFIN/NITROUS OXIDE HYBRID ROCKET MOTOR FOR FLIGHT-BASED TESTING","year":2021,"lang":"en","type":"article","venue":"International Journal of Energetic Materials and Chemical Propulsion","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":4,"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 Calgary","funders":"","keywords":"Propellant; Injector; Aerospace engineering; Rocket (weapon); Automotive engineering; Combustion; Combustion chamber; Materials science; Environmental science; Process engineering; Mechanical engineering; Engineering; Chemistry","score_opus":0.024070687173046834,"score_gpt":0.2622736579560126,"score_spread":0.23820297078296576,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3135652303","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":[0.79056716,0.00043224028,0.19643085,0.00024407744,0.00009455489,0.0011260504,0.00042431033,0.0016155845,0.0090652695],"genre_scores_gemma":[0.6892512,0.00041518226,0.29260832,0.000069325586,0.000011524144,0.00047738155,0.00067103805,0.00018420581,0.016311862],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99971396,0.000021521808,0.000016641106,0.000043061744,0.00017660904,0.0000281765],"domain_scores_gemma":[0.9995902,0.00005404565,0.000056178058,0.000045820205,0.00018760894,0.00006622871],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00065096695,0.0002971012,0.0002513037,0.00032444825,0.00021404546,0.00028712032,0.00073343795,0.0003370455,0.0020489213],"category_scores_gemma":[0.00056245574,0.00016419392,0.00017919757,0.00012220372,0.00018900658,0.0004748631,0.00033296342,0.00041861448,0.0008218905],"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":[0.00013991694,0.00013998622,0.0022760294,0.00015206958,0.000015477539,0.00027841202,0.000105121464,0.0021025706,0.94486755,0.00093529024,0.00047946034,0.048508078],"study_design_scores_gemma":[0.000055453485,0.0030026168,0.006780486,0.000034745284,0.00002437331,0.0010334187,0.00011397321,0.021177921,0.94224197,0.00017853089,0.02531908,0.00003736758],"about_ca_topic_score_codex":0.0006154006,"about_ca_topic_score_gemma":0.0012941147,"teacher_disagreement_score":0.0020489213,"about_ca_system_score_codex":0.00022502337,"about_ca_system_score_gemma":0.000514896,"threshold_uncertainty_score":0.0068542957},"labels":[],"label_agreement":null},{"id":"W3137868531","doi":"10.54966/jreen.v19i1.546","title":"Physical description of an isentropic flow in a Laval nozzle","year":2023,"lang":"en","type":"article","venue":"Journal of Renewable Energies","topic":"Rocket and propulsion systems research","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; Isentropic process; Computational fluid dynamics; MATLAB; Propeller; Flow (mathematics); Compressibility; Mechanics; Turbine; Computer science; Mechanical engineering; Aerospace engineering; Marine engineering; Engineering; Physics","score_opus":0.02288851650450991,"score_gpt":0.26606423924091777,"score_spread":0.24317572273640786,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3137868531","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":[0.52669734,0.003780187,0.43523657,0.0005496451,0.0002716025,0.00021125027,0.0003904249,0.00040350616,0.032459453],"genre_scores_gemma":[0.9866527,0.0005465907,0.008473016,0.00006637085,0.00004729597,0.000050334485,0.00008149316,0.00001516594,0.004067077],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998667,0.000027548484,0.000010140689,0.000028063661,0.00004469957,0.000022779546],"domain_scores_gemma":[0.9998808,0.0000439178,0.000024483224,0.000010020929,0.00003111872,0.000009721606],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00030114964,0.00035887788,0.0003959991,0.0004947772,0.00044908165,0.0008121518,0.00058623374,0.0007965512,0.0009577601],"category_scores_gemma":[0.0005464939,0.00015278393,0.0003868686,0.00022187055,0.0010642643,0.00075480295,0.00042636658,0.00039365815,0.0001409539],"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":[0.00020011888,0.00012588761,0.006243504,0.00028915217,0.000027757336,0.0020522778,0.00056453014,0.7328941,0.14201975,0.10089291,0.0007524535,0.013937533],"study_design_scores_gemma":[0.00004047952,0.00013733542,0.0027580399,0.000019362586,0.000007493737,0.00048713645,0.00010942403,0.97979945,0.005835392,0.008085896,0.002684138,0.000035908968],"about_ca_topic_score_codex":0.002069365,"about_ca_topic_score_gemma":0.00047890862,"teacher_disagreement_score":0.002069365,"about_ca_system_score_codex":0.00046148468,"about_ca_system_score_gemma":0.0005265855,"threshold_uncertainty_score":0.004114628},"labels":[],"label_agreement":null},{"id":"W3159409249","doi":"","title":"Computational fluid dynamics analysis on the Convergent Nozzle Design","year":2021,"lang":"en","type":"article","venue":"Journal of Emerging Technologies and Innovative Research","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":1,"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; Aerospace engineering; Rocket (weapon); Rocket engine nozzle; Planet; Aerodynamics; Conical surface; Mechanical engineering; Propellant; Liquid-propellant rocket; Computational fluid dynamics; Software; Computer science; Engineering; Physics","score_opus":0.09540125063406986,"score_gpt":0.3653993645254538,"score_spread":0.26999811389138395,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3159409249","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":[0.099869475,0.001919122,0.83775747,0.0009638345,0.00036609918,0.00018835685,0.00041590005,0.00035761035,0.058162257],"genre_scores_gemma":[0.87627244,0.0013849656,0.100723326,0.00016992295,0.00012709128,0.00026742907,0.0004272319,0.00018238297,0.020445205],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99965596,0.00007576905,0.000015449466,0.000046627727,0.00015847433,0.000047618985],"domain_scores_gemma":[0.9994899,0.0001649921,0.00005708335,0.000024482106,0.00023873539,0.000024722172],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00057312613,0.00058350066,0.00067535066,0.0005755792,0.000527746,0.001012452,0.0006308796,0.00090617454,0.0040013553],"category_scores_gemma":[0.0017744615,0.00022773129,0.0009918001,0.0004045208,0.0007384215,0.0006842594,0.00091493136,0.00069548894,0.00040835285],"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":[0.00006677872,0.000035851954,0.0020575444,0.00015064066,0.000019922594,0.00026587336,0.00008917217,0.94608974,0.0063588973,0.023244763,0.001439137,0.02018174],"study_design_scores_gemma":[0.0000060389225,0.000016353539,0.00026544102,0.000008832848,0.0000037161037,0.000031284333,0.000014695344,0.9958198,0.0007852713,0.0016574999,0.0013842091,0.000006867984],"about_ca_topic_score_codex":0.006887544,"about_ca_topic_score_gemma":0.0023773469,"teacher_disagreement_score":0.006887544,"about_ca_system_score_codex":0.0005095663,"about_ca_system_score_gemma":0.0010490987,"threshold_uncertainty_score":0.013694942},"labels":[],"label_agreement":null},{"id":"W3162008140","doi":"10.1061/9780784483374.026","title":"Development and Testing of Prototype Sabatier Reactor for Martian In Situ Propellant Production","year":2021,"lang":"en","type":"article","venue":"Earth and Space 2021","topic":"Rocket and propulsion systems research","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":"University of British Columbia","funders":"","keywords":"Propellant; Mars Exploration Program; Process engineering; Methane; Environmental science; Methanation; Martian; Aerospace engineering; Astrobiology; Engineering; Chemistry","score_opus":0.03251449650331452,"score_gpt":0.24572169352316517,"score_spread":0.21320719701985064,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3162008140","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":[0.9108396,0.000517768,0.07178711,0.000502501,0.0003333597,0.0015793714,0.0019237314,0.004731578,0.0077848625],"genre_scores_gemma":[0.9306569,0.00036776837,0.05956963,0.000116173556,0.00003687837,0.0007531432,0.0013731953,0.00023734619,0.006888979],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99924386,0.000077293436,0.000044947443,0.0001308435,0.00039100784,0.00011219893],"domain_scores_gemma":[0.9993343,0.00011995509,0.00007208684,0.00014120826,0.00020363175,0.00012883301],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0012087782,0.0006858086,0.0007904525,0.0004909112,0.0007096082,0.000924468,0.0020375184,0.0010990865,0.0027234356],"category_scores_gemma":[0.0012981002,0.00042147783,0.00070299767,0.00028384195,0.00039056662,0.0009138563,0.0005953744,0.0010146904,0.0013200338],"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":[0.0009767298,0.0007135567,0.0024929328,0.0007717724,0.00006177551,0.00070115377,0.0003303428,0.008807478,0.95009303,0.0008639605,0.0019538668,0.032233406],"study_design_scores_gemma":[0.00017655047,0.0030195399,0.004053327,0.0000311423,0.000054924287,0.00041957514,0.00015689955,0.019098599,0.9563714,0.00021063547,0.01634291,0.00006443248],"about_ca_topic_score_codex":0.0014865537,"about_ca_topic_score_gemma":0.0010982073,"teacher_disagreement_score":0.0027234356,"about_ca_system_score_codex":0.00063081254,"about_ca_system_score_gemma":0.00085976155,"threshold_uncertainty_score":0.009110749},"labels":[],"label_agreement":null},{"id":"W3162896413","doi":"","title":"7. Thermal Management and Power Generation for Directed Energy Weapons (2010-01-1781)","year":2016,"lang":"en","type":"book","venue":"","topic":"Rocket and propulsion systems research","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":"Boeing (Canada)","funders":"","keywords":"Nuclear engineering; Heat sink; Heat exchanger; Heat transfer; Water cooling; Passive cooling; Internal combustion engine cooling; Thermal energy storage; Environmental science; Air cooling; Process engineering; Thermodynamics; Mechanical engineering; Engineering; Chemistry","score_opus":0.021763830774106343,"score_gpt":0.23592075226548062,"score_spread":0.21415692149137427,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3162896413","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.021198686,0.00407691,0.025998978,0.003241892,0.002221272,0.00089414715,0.0043942826,0.0039008264,0.9340729],"genre_scores_gemma":[0.09582888,0.0033644105,0.017483344,0.0010151122,0.0005195909,0.0003292147,0.008423087,0.00076969276,0.8722666],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9994778,0.0000613592,0.00001341472,0.00004966958,0.00031804494,0.00007971502],"domain_scores_gemma":[0.9996977,0.000019518928,0.000016278624,0.00003016993,0.00019266493,0.00004366855],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00077725266,0.0005315008,0.00023135486,0.00071589253,0.0007259166,0.0012257291,0.0006303991,0.0012406689,0.043196745],"category_scores_gemma":[0.0004165072,0.0002196985,0.00037931136,0.00038018255,0.00024689792,0.0006742609,0.0006163962,0.0010392675,0.025840987],"study_design_candidate":"not_applicable","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":[0.00046653004,0.00062364474,0.0018627329,0.0006413381,0.00002611261,0.00037529238,0.00016702757,0.006907632,0.060620002,0.021751707,0.42247716,0.48408097],"study_design_scores_gemma":[0.00006466097,0.0003714791,0.0048848893,0.00010185751,0.00001391438,0.00024258145,0.00004729511,0.00544291,0.0398321,0.0020837204,0.9468821,0.00003248023],"about_ca_topic_score_codex":0.004635399,"about_ca_topic_score_gemma":0.010034291,"teacher_disagreement_score":0.043196745,"about_ca_system_score_codex":0.0018408861,"about_ca_system_score_gemma":0.0015080083,"threshold_uncertainty_score":0.14450747},"labels":[],"label_agreement":null},{"id":"W3171114255","doi":"10.1016/j.ijmultiphaseflow.2021.103707","title":"Experimental investigation of self-pressurized propellant injection into a simulated rocket motor combustion chamber","year":2021,"lang":"en","type":"article","venue":"International Journal of Multiphase Flow","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":9,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Calgary","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Injector; Materials science; Propellant; Mechanics; Rocket (weapon); Mass flow rate; Volumetric flow rate; Mass flow; Carbon dioxide; Flow (mathematics); Flashing; Thermodynamics; Aerospace engineering; Physics; Chemistry; Engineering","score_opus":0.019121326893565986,"score_gpt":0.2891587641403482,"score_spread":0.2700374372467822,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3171114255","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":[0.99663407,0.00008895689,0.0021741204,0.00002212446,0.000018147904,0.000033391778,0.000115375406,0.00010171973,0.0008120759],"genre_scores_gemma":[0.9979572,0.00006264836,0.0010617257,0.000008821074,0.000005621343,0.000016208107,0.000075893055,0.000017599035,0.00079423335],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997044,0.000035105302,0.000017517794,0.00006546524,0.000111815905,0.00006565393],"domain_scores_gemma":[0.9993543,0.00030795808,0.00008106055,0.000050505503,0.00014913072,0.00005706238],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004260775,0.00045470305,0.0005410183,0.0002747345,0.0005991757,0.00044872475,0.0007264515,0.00074267376,0.0021184909],"category_scores_gemma":[0.00074435095,0.0002584402,0.00032722877,0.0002698288,0.0005499379,0.00055618456,0.00040322237,0.0004441832,0.00022041902],"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":[0.0017752673,0.0002282486,0.0022982804,0.0001730494,0.000017917017,0.00023814678,0.00017162297,0.0018169489,0.98952615,0.00014486269,0.00006525944,0.0035441206],"study_design_scores_gemma":[0.00006892249,0.0014049236,0.0059990017,0.000008592587,0.000022673497,0.00007077407,0.00007199042,0.009607189,0.9822552,0.000021359927,0.00045414982,0.000015030908],"about_ca_topic_score_codex":0.0011679946,"about_ca_topic_score_gemma":0.00094359985,"teacher_disagreement_score":0.0021184909,"about_ca_system_score_codex":0.0003378438,"about_ca_system_score_gemma":0.0004628488,"threshold_uncertainty_score":0.0070871115},"labels":[],"label_agreement":null},{"id":"W3173098105","doi":"10.1139/tcsme-2021-0057","title":"An experimental comparison of the effects of jet fuel (F-34) and diesel (F-54) on the wear of fuel system components and fuel consumption of an internal combustion diesel engine","year":2021,"lang":"en","type":"article","venue":"Transactions of the Canadian Society for Mechanical Engineering","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Diesel fuel; Winter diesel fuel; Jet fuel; Brake specific fuel consumption; Diesel cycle; Automotive engineering; Internal combustion engine; Fuel efficiency; Vapor lock; Truck; Diesel engine; Fuel injection; Aircraft fuel system; Environmental science; Alcohol fuel; Combustion; Thrust specific fuel consumption; Waste management; Engineering; Petrol engine; Combustion chamber; Chemistry","score_opus":0.021726049669438502,"score_gpt":0.2567336174541826,"score_spread":0.2350075677847441,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3173098105","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":[0.9990613,0.000077108445,0.0004429763,0.0000057714146,0.0000152251405,0.000018073162,0.00008989839,0.000010903145,0.00027878679],"genre_scores_gemma":[0.99728394,0.000108392764,0.0010841287,0.000013700633,0.00000920139,0.000024571296,0.00016128186,0.000012686805,0.0013021976],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99951994,0.000058935515,0.000061183964,0.00008930658,0.00016214556,0.00010858379],"domain_scores_gemma":[0.99804556,0.00088450173,0.0002056836,0.00022574849,0.0005406461,0.000097825054],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004501291,0.00056866044,0.000325745,0.000505517,0.00038593923,0.00026176844,0.00050463143,0.00055203674,0.0031165634],"category_scores_gemma":[0.00122599,0.00033701208,0.00045668124,0.00026899914,0.00037431982,0.00041975355,0.00028953023,0.00040337097,0.0002903936],"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":[0.005410004,0.0013957601,0.0036169647,0.00018494343,0.00003539861,0.00010259301,0.00017514484,0.0008442408,0.9801846,0.000042432777,0.00010873871,0.007899138],"study_design_scores_gemma":[0.00010927569,0.019630378,0.024376148,0.000017603283,0.000073856325,0.00013409003,0.00018282651,0.0022653432,0.9525272,0.000032080854,0.00061919464,0.00003206323],"about_ca_topic_score_codex":0.0014105741,"about_ca_topic_score_gemma":0.0021980037,"teacher_disagreement_score":0.0031165634,"about_ca_system_score_codex":0.00021998797,"about_ca_system_score_gemma":0.00021903192,"threshold_uncertainty_score":0.010425985},"labels":[],"label_agreement":null},{"id":"W3173374742","doi":"10.1115/fedsm2020-20197","title":"A Simple Method for the Design of Supersonic Nozzles of Arbitrary Cross Section Shape","year":2020,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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":"Rotational symmetry; Nozzle; Supersonic speed; Wedge (geometry); Cross section (physics); Choked flow; Mechanics; Flow (mathematics); Geometry; Physics; Mechanical engineering; Mathematics; Engineering","score_opus":0.09511706905998464,"score_gpt":0.3473832261562831,"score_spread":0.25226615709629846,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3173374742","genre_codex":"methods","genre_gemma":"methods","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.013178087,0.00006286221,0.9830919,0.00002261488,0.000020948422,0.0001272618,0.000060861756,0.0004899411,0.0029455326],"genre_scores_gemma":[0.14055876,0.00008973732,0.8564659,0.000025988735,0.000010144157,0.00027934,0.000114288414,0.00016596197,0.0022898964],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99972874,0.00003888641,0.000014387876,0.000028053579,0.0001689672,0.000020846019],"domain_scores_gemma":[0.9996985,0.00009049644,0.000049828446,0.00005584573,0.00008597596,0.000019385765],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004845183,0.0005362148,0.00052256737,0.00036989822,0.00023993495,0.00050037616,0.0008554975,0.00039754342,0.0030887432],"category_scores_gemma":[0.00068102445,0.00047584705,0.0004855345,0.00019087267,0.00031881005,0.0002774241,0.00055267196,0.00046521903,0.0007144333],"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":[0.00017837722,0.00010398908,0.0014426546,0.0006313263,0.00007051173,0.0003718646,0.0002289507,0.3325401,0.4235777,0.044123944,0.0031647338,0.19356588],"study_design_scores_gemma":[0.00011655741,0.00035776157,0.00096304965,0.000040856306,0.000028053975,0.00045793387,0.000028705783,0.8694586,0.085182175,0.006087932,0.037212487,0.0000659045],"about_ca_topic_score_codex":0.0004441377,"about_ca_topic_score_gemma":0.0009128699,"teacher_disagreement_score":0.0030887432,"about_ca_system_score_codex":0.00036083526,"about_ca_system_score_gemma":0.0007441484,"threshold_uncertainty_score":0.010332882},"labels":[],"label_agreement":null},{"id":"W3176781912","doi":"","title":"Fuel Flexible Combustor for High-OPR Compact-Core N+3 Propulsion Engine","year":2020,"lang":"en","type":"article","venue":"NASA Technical Reports Server (NASA)","topic":"Rocket and propulsion systems research","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":"Period (music); Quarter (Canadian coin); Work (physics); Core (optical fiber); Propulsion; Aeronautics; Political science; Engineering; Geography; Telecommunications; Aerospace engineering; Mechanical engineering; Archaeology","score_opus":0.06114747334430572,"score_gpt":0.29323052078944256,"score_spread":0.23208304744513686,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3176781912","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":[0.9298947,0.001356484,0.037655227,0.000175328,0.00031804468,0.00015818309,0.0010696953,0.0011786742,0.028193628],"genre_scores_gemma":[0.9827844,0.00023983371,0.0057948367,0.00002570194,0.0000128294605,0.00003638487,0.000490882,0.00006711267,0.010548054],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999002,0.000004571565,0.0000048738925,0.000014085669,0.00006384931,0.000012384566],"domain_scores_gemma":[0.99994254,0.000009946404,0.0000070512547,0.00000852595,0.000022610047,0.000009247968],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020241912,0.00017582501,0.00027774458,0.00033370545,0.00047059532,0.00029531645,0.00065899914,0.00019949635,0.0060203676],"category_scores_gemma":[0.00023040609,0.000099451674,0.00023406351,0.00016103368,0.00015422597,0.00053759734,0.00035633263,0.0002239363,0.0008605685],"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":[0.0047093634,0.000606534,0.009591442,0.0015583241,0.00008581252,0.0015713763,0.00025217276,0.042867806,0.6363729,0.009210467,0.014510911,0.27866298],"study_design_scores_gemma":[0.00027411716,0.0017228532,0.038637552,0.00012890332,0.00010370107,0.0010468141,0.00025092709,0.24326898,0.6748474,0.0022012629,0.037402753,0.0001147039],"about_ca_topic_score_codex":0.0018437708,"about_ca_topic_score_gemma":0.004412249,"teacher_disagreement_score":0.0060203676,"about_ca_system_score_codex":0.00027126036,"about_ca_system_score_gemma":0.00028197357,"threshold_uncertainty_score":0.020140111},"labels":[],"label_agreement":null},{"id":"W3176978852","doi":"10.4271/03-15-01-0003","title":"Helicopter Turboshaft Engine Database as a Conceptual Design Tool","year":2021,"lang":"en","type":"article","venue":"SAE International Journal of Engines","topic":"Rocket and propulsion systems research","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":"University of Windsor","funders":"","keywords":"Conceptual design; Systems engineering; Computer science; Database; Automotive engineering; Engineering; Human–computer interaction","score_opus":0.03452143465907545,"score_gpt":0.3034592261945977,"score_spread":0.2689377915355222,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3176978852","genre_codex":"dataset","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":[0.019431828,0.0029477922,0.1755056,0.00034744517,0.0002121164,0.0008595292,0.7072224,0.049361013,0.044112287],"genre_scores_gemma":[0.04575103,0.0016358366,0.06292597,0.00019919277,0.00004478208,0.0009994148,0.873914,0.002569672,0.011959992],"study_design_codex":"not_applicable","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99925727,0.00007900132,0.00011758595,0.00012782277,0.0003677613,0.000050638966],"domain_scores_gemma":[0.99869907,0.00023591422,0.00012791497,0.00038865051,0.0004940376,0.00005435655],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0009147867,0.001426203,0.0008916423,0.003219811,0.00034749965,0.0013792864,0.0022199831,0.0010036764,0.03350446],"category_scores_gemma":[0.0026881834,0.00052231044,0.0010860773,0.0029215256,0.0002407356,0.0011217602,0.0009789142,0.0008532343,0.021409072],"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":[0.00065056863,0.00036301362,0.008010955,0.0055213342,0.0002479953,0.0005513712,0.00026768018,0.05476209,0.015733114,0.018426064,0.6591826,0.23628324],"study_design_scores_gemma":[0.00019046036,0.00019703634,0.00509348,0.0002768065,0.00008318827,0.0003953584,0.000116152936,0.048152905,0.0122211985,0.005920419,0.9272504,0.0001025975],"about_ca_topic_score_codex":0.0045552356,"about_ca_topic_score_gemma":0.008874089,"teacher_disagreement_score":0.03350446,"about_ca_system_score_codex":0.0008366147,"about_ca_system_score_gemma":0.0012982442,"threshold_uncertainty_score":0.112083554},"labels":[],"label_agreement":null},{"id":"W3184339957","doi":"10.2514/6.2021-3267","title":"MAPLEAF: A Compact, Extensible, Open-Source, 6-Degrees-of-Freedom Rocket Flight Simulation Framework","year":2021,"lang":"en","type":"article","venue":"AIAA Propulsion and Energy 2021 Forum","topic":"Rocket and propulsion systems research","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 Calgary","funders":"","keywords":"Extensibility; Computer science; Rocket (weapon); Open source; Missile; Aerospace engineering; Suite; Wind tunnel; Flight simulator; Systems engineering; Flight test; Monte Carlo method; Probabilistic logic; Simulation; Software; Aeronautics; Engineering; Artificial intelligence","score_opus":0.025611506215172056,"score_gpt":0.28344724332242605,"score_spread":0.257835737107254,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3184339957","genre_codex":"methods","genre_gemma":"software","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"software","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.014622989,0.0004462725,0.79893625,0.00045731064,0.00031325867,0.00046732996,0.0111182835,0.12476737,0.048870847],"genre_scores_gemma":[0.28684038,0.0016640044,0.56642264,0.0007225904,0.00016127476,0.0020078772,0.05628519,0.046445206,0.039450854],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99963975,0.000056464072,0.000022474189,0.000038723894,0.00018359096,0.00005893308],"domain_scores_gemma":[0.99957615,0.00015247847,0.000026730848,0.00006577491,0.00011580122,0.00006311212],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00088389235,0.0010415745,0.0005659687,0.0006802246,0.0005690294,0.0013135374,0.003163106,0.0013369038,0.03661735],"category_scores_gemma":[0.0021495086,0.00070315273,0.0013064482,0.00048520693,0.00046227322,0.0017766452,0.0020392945,0.001945068,0.008920025],"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":[0.00063527626,0.0002922159,0.0047676465,0.0010806784,0.00022156366,0.00050463766,0.0005369179,0.5748882,0.015258668,0.055782437,0.21499623,0.13103548],"study_design_scores_gemma":[0.00022832942,0.00008944775,0.0005675886,0.00010391877,0.000025423267,0.00015095757,0.00006095213,0.7984548,0.0062552844,0.011065726,0.18292779,0.00006972153],"about_ca_topic_score_codex":0.0071551288,"about_ca_topic_score_gemma":0.008546981,"teacher_disagreement_score":0.03661735,"about_ca_system_score_codex":0.0005811011,"about_ca_system_score_gemma":0.0015524278,"threshold_uncertainty_score":0.1224972},"labels":[],"label_agreement":null},{"id":"W3186048982","doi":"10.2514/6.2021-3518","title":"Evaluation of Lattice-Augmented Hybrid Rocket Fuels on a Slab Burner","year":2021,"lang":"en","type":"article","venue":"AIAA Propulsion and Energy 2021 Forum","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":7,"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 Calgary","funders":"","keywords":"Combustor; Wax; Materials science; Slab; Acrylonitrile butadiene styrene; Lattice (music); Combustion; Embedding; Paraffin wax; Composite material; Nuclear engineering; Mechanical engineering; Process engineering; Computer science; Engineering; Structural engineering; Chemistry; Physics; Acoustics; Organic chemistry","score_opus":0.027860273646920827,"score_gpt":0.2733192870833466,"score_spread":0.24545901343642573,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3186048982","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":[0.9855377,0.0002458601,0.009519981,0.000051287974,0.000037900747,0.00008100612,0.00064401847,0.00033070074,0.0035514135],"genre_scores_gemma":[0.98894334,0.00023516074,0.007057875,0.00001273773,0.0000026476166,0.00004885307,0.0003813952,0.000072777046,0.003245254],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99981815,0.00001601157,0.000008544848,0.00002600551,0.00010441991,0.000026915279],"domain_scores_gemma":[0.99972194,0.000082191196,0.00002633028,0.00003371168,0.00010117463,0.000034600635],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00047181212,0.00034566075,0.0004206127,0.00043358916,0.0003072608,0.00059625576,0.0006264258,0.00039564475,0.005007095],"category_scores_gemma":[0.0006646652,0.00014944017,0.0003092902,0.00035344716,0.00020837324,0.00062899676,0.000417995,0.0005496452,0.00093371404],"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":[0.003697532,0.00096152717,0.00738144,0.0006235059,0.000068165806,0.00046755563,0.00023884277,0.16100895,0.7370398,0.0018246344,0.0014493311,0.085238725],"study_design_scores_gemma":[0.00007591557,0.004558702,0.0077207764,0.000055807606,0.00004189798,0.00009616113,0.0003167647,0.25780928,0.72359824,0.00033645768,0.0053339317,0.00005600242],"about_ca_topic_score_codex":0.0018890359,"about_ca_topic_score_gemma":0.003012895,"teacher_disagreement_score":0.005007095,"about_ca_system_score_codex":0.00046714678,"about_ca_system_score_gemma":0.00036076145,"threshold_uncertainty_score":0.016750395},"labels":[],"label_agreement":null},{"id":"W3190439964","doi":"10.1109/icnte51185.2021.9487717","title":"Design and Analysis of Bell-Parabolic De Laval Rocket Exhaust Nozzle","year":2021,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":5,"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":"Rocket engine nozzle; Nozzle; Rocket (weapon); Aerospace engineering; Computational fluid dynamics; Software; Mechanical engineering; Rocket engine; Computer science; Marine engineering; Engineering","score_opus":0.02915919268607086,"score_gpt":0.27930259334458857,"score_spread":0.2501434006585177,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3190439964","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":[0.07560578,0.0020360635,0.8824329,0.00036685547,0.00025336174,0.00049922796,0.00029290805,0.0016400769,0.036872946],"genre_scores_gemma":[0.85058624,0.0010674779,0.12286784,0.00010252094,0.000051771436,0.0003630093,0.0002696195,0.00016869928,0.024522802],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99942255,0.000050081588,0.000026033451,0.00010061088,0.0003516043,0.00004913592],"domain_scores_gemma":[0.99980944,0.00003645782,0.00004094953,0.000012782701,0.00007587441,0.000024364277],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004953409,0.00046762655,0.00076403056,0.0004392264,0.0005974427,0.0015133461,0.001089728,0.0010908096,0.0044395276],"category_scores_gemma":[0.00044788694,0.00038726802,0.0007407325,0.00020896296,0.00033523218,0.00042923997,0.0006355776,0.0003499867,0.0010190319],"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":[0.0004130352,0.000101650105,0.008994719,0.0013064579,0.000105448285,0.0023728502,0.00055646145,0.48631257,0.34800905,0.023908509,0.0049763382,0.12294291],"study_design_scores_gemma":[0.00010219616,0.0011062645,0.006470757,0.0001182469,0.00009402055,0.0015858352,0.00022777433,0.86193585,0.069566265,0.003308684,0.05535377,0.00013037548],"about_ca_topic_score_codex":0.0012665457,"about_ca_topic_score_gemma":0.0006682624,"teacher_disagreement_score":0.0044395276,"about_ca_system_score_codex":0.00065839273,"about_ca_system_score_gemma":0.00091180106,"threshold_uncertainty_score":0.014851689},"labels":[],"label_agreement":null},{"id":"W3194793342","doi":"10.32920/ryerson.14646417.v1","title":"Comparison Of Solid Rocket Motor Thrust Modulation Technique","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Rocket and propulsion systems research","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":"Toronto Metropolitan University; Brandon University","funders":"","keywords":"Thrust; Propellant; Chamber pressure; Nozzle; Solid-fuel rocket; Aerospace engineering; Rocket engine nozzle; Combustion chamber; Rocket (weapon); Acceleration; Propulsion; Mechanical engineering; Materials science; Engineering; Physics; Combustion; Mechanics; Chemistry; Classical mechanics","score_opus":0.062052430989577856,"score_gpt":0.36641397738791487,"score_spread":0.304361546398337,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3194793342","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":[0.87131447,0.0030612098,0.09568494,0.0001621299,0.0001219873,0.0001633244,0.00046993952,0.0012387328,0.027783321],"genre_scores_gemma":[0.9626997,0.00092112983,0.03154843,0.00002532857,0.000012355856,0.000041986616,0.00043941734,0.00011468309,0.0041970164],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9996805,0.000025129742,0.000021670136,0.000046988316,0.000183672,0.000042003885],"domain_scores_gemma":[0.99967825,0.00008796521,0.00006426252,0.000055951426,0.00009570714,0.00001795393],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00029778012,0.0002474463,0.0003218708,0.00050613633,0.00018193344,0.0005026574,0.0005088974,0.00033813267,0.003218541],"category_scores_gemma":[0.0008140563,0.000106183346,0.00023076862,0.0006263192,0.00021106108,0.00058035913,0.00029719246,0.0002670407,0.0005585965],"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":[0.0029548968,0.00022072009,0.003884229,0.0010853154,0.000084162675,0.0002119988,0.00035898742,0.015713722,0.52924204,0.0061216955,0.0019536924,0.4381686],"study_design_scores_gemma":[0.00017047394,0.003603725,0.023535166,0.00012380582,0.00012200572,0.0011434273,0.00034791577,0.123238094,0.7915938,0.0015485672,0.054450247,0.00012273964],"about_ca_topic_score_codex":0.0006544558,"about_ca_topic_score_gemma":0.00075753435,"teacher_disagreement_score":0.003218541,"about_ca_system_score_codex":0.0002732122,"about_ca_system_score_gemma":0.00028536716,"threshold_uncertainty_score":0.010767043},"labels":[],"label_agreement":null},{"id":"W3196763908","doi":"10.1088/1742-6596/2012/1/012023","title":"Investigation of the Influence of Laval Nozzle Throat Width via Euler-based Flow Simulation","year":2021,"lang":"en","type":"article","venue":"Journal of Physics Conference Series","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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; Mechanics; Mach number; Discharge coefficient; Flow (mathematics); Euler equations; Discretization; Euler's formula; Choked flow; Physics; Mechanical engineering; Materials science; Mathematics; Engineering; Supersonic speed; Thermodynamics; Mathematical analysis","score_opus":0.03464567043187961,"score_gpt":0.2607150566477976,"score_spread":0.226069386215918,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3196763908","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":[0.949183,0.00042757098,0.046085402,0.000069167414,0.00004079372,0.000038618593,0.00013543486,0.00049553264,0.0035242816],"genre_scores_gemma":[0.99171066,0.00008835652,0.007883705,0.0000071758054,0.0000026811622,0.0000096083895,0.000050111852,0.000021518435,0.00022611524],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997558,0.00006729822,0.000020354975,0.000034202858,0.00008475992,0.000037531187],"domain_scores_gemma":[0.9987478,0.00077821757,0.00014546889,0.000081230755,0.0002033679,0.000043822547],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0007764013,0.0003902579,0.00053367455,0.0005644517,0.00028086573,0.0006138014,0.00045895774,0.00052728085,0.00072515913],"category_scores_gemma":[0.0015703368,0.00019351295,0.0003836643,0.00037630304,0.00034763385,0.0004715599,0.00031059835,0.0002937896,0.000086278706],"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":[0.00039322267,0.0001664603,0.012912349,0.00019921189,0.000040620802,0.0002790859,0.00013824465,0.87627804,0.08838757,0.0014956254,0.00026531421,0.019444231],"study_design_scores_gemma":[0.000013011749,0.0001102084,0.002288079,0.000009788764,0.000014854541,0.000020851154,0.000024832683,0.98042244,0.016699474,0.00009650391,0.0002859131,0.000014036823],"about_ca_topic_score_codex":0.0031354423,"about_ca_topic_score_gemma":0.0013511356,"teacher_disagreement_score":0.0031354423,"about_ca_system_score_codex":0.0003100661,"about_ca_system_score_gemma":0.00038069044,"threshold_uncertainty_score":0.0062344074},"labels":[],"label_agreement":null},{"id":"W3202448954","doi":"10.11575/prism/39273","title":"Conceptual design methods for small-scale supersonic uncrewed aerial vehicles","year":2021,"lang":"en","type":"dissertation","venue":"Open MIND","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":1,"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":"Supersonic speed; Scale (ratio); Aerospace engineering; Conceptual design; Marine engineering; Aeronautics; Engineering; Environmental science; Computer science; Geography; Cartography; Mechanical engineering","score_opus":0.1473007030233277,"score_gpt":0.409608262273708,"score_spread":0.2623075592503803,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3202448954","genre_codex":"methods","genre_gemma":"methods","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0029077763,0.00018326622,0.98992854,0.000046068526,0.00003458834,0.00036222988,0.000042945096,0.0002223682,0.00627218],"genre_scores_gemma":[0.094574176,0.00064256246,0.89496624,0.00006029584,0.000021236801,0.0015992098,0.00015416801,0.00024030563,0.0077417707],"study_design_codex":"simulation_or_modeling","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.998596,0.00032059033,0.000072094066,0.000110730514,0.000846287,0.000054274904],"domain_scores_gemma":[0.99883336,0.00040176828,0.00016317893,0.00015829412,0.00041160593,0.000031779367],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0028868334,0.00081850705,0.0004349793,0.0008844711,0.00047997595,0.0012779149,0.0013007009,0.0006295126,0.009123525],"category_scores_gemma":[0.002461529,0.000693131,0.0007637168,0.0004862932,0.0006639447,0.00090985664,0.00095010886,0.001082855,0.0019973],"study_design_candidate":"theoretical_or_conceptual","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":[0.0001523854,0.00020934656,0.0012122557,0.00239576,0.00008014138,0.0002589603,0.0008211111,0.4068307,0.06984336,0.14921318,0.0048814924,0.36410126],"study_design_scores_gemma":[0.00019915763,0.001187396,0.0012338442,0.00049271964,0.00007044121,0.00032471228,0.000446013,0.72356105,0.032274753,0.037115116,0.20300482,0.00008994664],"about_ca_topic_score_codex":0.0011552623,"about_ca_topic_score_gemma":0.001933164,"teacher_disagreement_score":0.009123525,"about_ca_system_score_codex":0.0009170238,"about_ca_system_score_gemma":0.0012631767,"threshold_uncertainty_score":0.030521274},"labels":[],"label_agreement":null},{"id":"W3203222894","doi":"10.2514/1.b38330","title":"Hybrid Rocket Engine Performance Assessment Using Plume Luminosity Oscillations","year":2021,"lang":"en","type":"article","venue":"Journal of Propulsion and Power","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Calgary","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Rocket (weapon); Plume; Rocket engine; Solid-fuel rocket; Aerospace engineering; Liquid-propellant rocket; Combustion; Instability; Luminosity; Acoustics; Characteristic velocity; Mechanics; Physics; Propellant; Engineering; Meteorology; Astrophysics","score_opus":0.022186882030998226,"score_gpt":0.2853620725768582,"score_spread":0.26317519054585997,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3203222894","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":[0.9964174,0.000045132652,0.0029907615,0.000005679518,0.0000016404047,0.000011174566,0.00006276023,0.000038786413,0.000426619],"genre_scores_gemma":[0.9979201,0.00004443239,0.001534457,0.0000033174497,0.0000011732484,0.000011286145,0.0000992545,0.000010079767,0.000375876],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999068,0.000008962586,0.000005491855,0.000018725974,0.000043908643,0.000016228669],"domain_scores_gemma":[0.9997261,0.00007835572,0.000051016952,0.000009176394,0.000110649446,0.000024680468],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002525308,0.00032153187,0.00020481387,0.001004971,0.00013792187,0.00029667778,0.00028870304,0.00020393365,0.00096246006],"category_scores_gemma":[0.00048204773,0.000088121815,0.00014054256,0.00034395044,0.00017192117,0.00032721378,0.00039648032,0.00018467693,0.00014047234],"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":[0.0011461497,0.00015383598,0.0364182,0.00014458806,0.000043365788,0.00027600705,0.0003690622,0.009612884,0.91263294,0.00014673983,0.000109640074,0.03894651],"study_design_scores_gemma":[0.000037996513,0.0021041962,0.25241947,0.000028878172,0.00007161615,0.00033247686,0.00078373274,0.100165725,0.6431121,0.00020256893,0.00066169276,0.0000795268],"about_ca_topic_score_codex":0.0013185134,"about_ca_topic_score_gemma":0.0018739295,"teacher_disagreement_score":0.0013185134,"about_ca_system_score_codex":0.0001863549,"about_ca_system_score_gemma":0.00009218559,"threshold_uncertainty_score":0.0032197833},"labels":[],"label_agreement":null},{"id":"W3209233889","doi":"10.32920/ryerson.14645013.v1","title":"Compatibility Of Metallic &amp; Non-Metallic Turbine Engine Materials With Aviation Fuels","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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":"Compatibility (geochemistry); Aerospace; Aviation; Turbine; Mechanical engineering; Materials science; Computer science; Process engineering; Engineering; Composite material; Aerospace engineering","score_opus":0.03262144368006889,"score_gpt":0.2745440959211908,"score_spread":0.2419226522411219,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3209233889","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":[0.99378985,0.00052755995,0.0016295825,0.00001989876,0.000024090798,0.00003036905,0.00012808635,0.000023093162,0.0038274566],"genre_scores_gemma":[0.99481815,0.0002024337,0.002108018,0.000013172355,0.000005185397,0.000017167147,0.00019283687,0.000020475421,0.0026225238],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9991905,0.00012262163,0.00007065503,0.0001129246,0.00044293347,0.000060380233],"domain_scores_gemma":[0.99929607,0.00015491736,0.00014618029,0.000102564074,0.00025968754,0.000040523486],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000511225,0.0002468586,0.00017354033,0.00094002986,0.00027008695,0.00039181573,0.00029325593,0.00037851502,0.0020875828],"category_scores_gemma":[0.0011276734,0.00016153378,0.00019549136,0.00046453328,0.0003168233,0.00034477806,0.0003002463,0.00016318314,0.00043243874],"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":[0.00022378103,0.000044171586,0.0059043407,0.00014372336,0.000014843143,0.0002755763,0.00012559636,0.000361005,0.9863646,0.00033176228,0.000075521384,0.00613511],"study_design_scores_gemma":[0.000005610345,0.0007654382,0.030174451,0.000022386997,0.00003199101,0.0005823055,0.00023178279,0.001011942,0.96405166,0.00009136688,0.003021219,0.000009832377],"about_ca_topic_score_codex":0.00042698538,"about_ca_topic_score_gemma":0.0011810248,"teacher_disagreement_score":0.0020875828,"about_ca_system_score_codex":0.0001513086,"about_ca_system_score_gemma":0.00016958288,"threshold_uncertainty_score":0.0069836974},"labels":[],"label_agreement":null},{"id":"W3209249438","doi":"10.32920/ryerson.14654895.v1","title":"Comparison of cylindrical and non-cylindrical grain internal ballistic behavior of hybrid rocket engines and solid rocket motors","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Rocket and propulsion systems research","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":"Toronto Metropolitan University","funders":"","keywords":"Specific impulse; Solid-fuel rocket; Propellant; Aerospace engineering; Internal ballistics; Propulsion; Rocket (weapon); Combustion; Thrust; Internal flow; Rocket engine; Materials science; Mechanical engineering; Mechanics; Physics; Flow (mathematics); Engineering; Chemistry","score_opus":0.03440304524303126,"score_gpt":0.33529102987715803,"score_spread":0.30088798463412675,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3209249438","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":[0.9687251,0.00033700804,0.011356637,0.00010472436,0.000029301247,0.000057242974,0.00037899904,0.00028959062,0.018721359],"genre_scores_gemma":[0.997154,0.000089087625,0.0015034392,0.000008559849,0.0000018419781,0.000015750895,0.00023454388,0.000031006493,0.00096172385],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99981815,0.0000207008,0.000009248369,0.00002099297,0.00007528849,0.000055580727],"domain_scores_gemma":[0.99943,0.00019297298,0.00008100687,0.00006779198,0.00016378154,0.000064330554],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00039192275,0.0003110909,0.00044572863,0.00069096213,0.00037480207,0.00078324095,0.0007395656,0.00052286906,0.0019813823],"category_scores_gemma":[0.001343321,0.00022318155,0.00063362677,0.0005399156,0.0004970168,0.00047889832,0.0003480248,0.00035068757,0.00033757673],"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":[0.00032764114,0.000088333916,0.0060207946,0.00013355985,0.00004668795,0.00024153032,0.0001604835,0.96349406,0.014777342,0.0056124046,0.0008255694,0.00827155],"study_design_scores_gemma":[0.000017409713,0.00015109435,0.0034553518,0.0000116954525,0.000013850256,0.000042566655,0.00007822124,0.98809004,0.0067155934,0.00060763815,0.0007931348,0.000023355364],"about_ca_topic_score_codex":0.008658819,"about_ca_topic_score_gemma":0.0061566145,"teacher_disagreement_score":0.008658819,"about_ca_system_score_codex":0.0009613067,"about_ca_system_score_gemma":0.0006479588,"threshold_uncertainty_score":0.017216861},"labels":[],"label_agreement":null},{"id":"W3209618046","doi":"10.32920/ryerson.14635701.v1","title":"Design and Analysis of a Rocket-Deployed Flying-Wing UAV","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Rocket and propulsion systems research","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":true,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Payload (computing); Wingspan; Aerospace engineering; Takeoff; Wing loading; Wing; Rocket (weapon); Flight control surfaces; Aerodynamics; Engineering; Airfoil; Power (physics); Volume (thermodynamics); Automotive engineering; Aeronautics; Angle of attack; Computer science","score_opus":0.0537705095298602,"score_gpt":0.2919828896700315,"score_spread":0.2382123801401713,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3209618046","genre_codex":"empirical","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"other","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.57270014,0.0004582358,0.39215687,0.0002070128,0.0000881891,0.00038181402,0.0003327176,0.00091812544,0.03275677],"genre_scores_gemma":[0.94999427,0.00018291351,0.042482752,0.000026457781,0.0000070916567,0.00013149146,0.00012302304,0.000047851045,0.007004126],"study_design_codex":"simulation_or_modeling","study_design_gemma":"not_applicable","domain_scores_codex":[0.9998517,0.00001793172,0.0000051943466,0.0000257085,0.000073079646,0.000026280735],"domain_scores_gemma":[0.9998834,0.000030652107,0.000025929643,0.000012617757,0.00003568384,0.000011698333],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017531459,0.00036525124,0.0003317755,0.00029414496,0.00034825547,0.0006039934,0.00042637065,0.00048643482,0.0024545442],"category_scores_gemma":[0.0002961883,0.00018786207,0.00040032036,0.00011104406,0.0002734608,0.00021219814,0.00026312965,0.00022059101,0.00040781195],"study_design_candidate":"not_applicable","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":[0.00024106726,0.00006866839,0.0020792766,0.00037586005,0.000043010903,0.00091098476,0.0001774585,0.80042225,0.15764771,0.0035677773,0.0006212148,0.033844717],"study_design_scores_gemma":[0.00005139558,0.001053106,0.002661925,0.0000301712,0.000045137098,0.00023676938,0.00014260452,0.9416367,0.04611578,0.00076880556,0.0072349105,0.000022710066],"about_ca_topic_score_codex":0.0025805777,"about_ca_topic_score_gemma":0.0015937771,"teacher_disagreement_score":0.0025805777,"about_ca_system_score_codex":0.00050166226,"about_ca_system_score_gemma":0.0005477494,"threshold_uncertainty_score":0.008211255},"labels":[],"label_agreement":null},{"id":"W3210054541","doi":"10.32920/ryerson.14635638.v1","title":"Aerodynamic Optimization of the Von Karman Nose Cone for a Supersonic Sounding Rocket","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Rocket and propulsion systems research","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":"Toronto Metropolitan University","funders":"","keywords":"Aerodynamics; Sounding rocket; Supersonic speed; Aerospace engineering; Rocket (weapon); Cone (formal languages); Angle of attack; Fluent; Engineering; Computational fluid dynamics; Mechanical engineering; Structural engineering; Computer science","score_opus":0.02610026306870565,"score_gpt":0.2719170150094971,"score_spread":0.24581675194079144,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3210054541","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":[0.529507,0.00043612786,0.44221944,0.00013113872,0.00010221221,0.00026692267,0.00015429492,0.0004384041,0.026744518],"genre_scores_gemma":[0.9315888,0.00016448983,0.063425526,0.000024269933,0.000008722032,0.000068777954,0.00009114797,0.00010063494,0.0045275777],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997603,0.000028543203,0.000007709498,0.000024573043,0.00014127251,0.000037637346],"domain_scores_gemma":[0.9997409,0.000057754154,0.000036847534,0.000020859916,0.00011715673,0.000026559297],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004855944,0.0005920522,0.00044426855,0.0003284856,0.00032602617,0.00078835007,0.00032883842,0.0004325824,0.0016614129],"category_scores_gemma":[0.0006059535,0.00021476197,0.00045780028,0.00023094933,0.00028736214,0.00028298568,0.00027914278,0.00035998895,0.0003534986],"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":[0.00030654765,0.0001950469,0.0033689223,0.00019388483,0.000024244977,0.0005263124,0.00008552017,0.74379575,0.17688996,0.0058552977,0.0010268731,0.06773169],"study_design_scores_gemma":[0.000038607504,0.0006907513,0.0027204116,0.000022941347,0.000017146229,0.00020873728,0.00008410809,0.9469163,0.044500403,0.00096555176,0.0037927758,0.000042307085],"about_ca_topic_score_codex":0.0015313225,"about_ca_topic_score_gemma":0.0033250218,"teacher_disagreement_score":0.0016614129,"about_ca_system_score_codex":0.00037581476,"about_ca_system_score_gemma":0.0010201028,"threshold_uncertainty_score":0.005558014},"labels":[],"label_agreement":null},{"id":"W3211913391","doi":"10.1088/1742-6596/2057/1/012069","title":"The influence of friction on gas parameters in the minimum section of nozzles","year":2021,"lang":"en","type":"article","venue":"Journal of Physics Conference Series","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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":"Polytropic process; Nozzle; Mechanics; Cross section (physics); Thermodynamics; Volume (thermodynamics); Flow (mathematics); Volumetric flow rate; Section (typography); Discharge coefficient; Degree (music); Materials science; Chemistry; Physics","score_opus":0.029322229058786148,"score_gpt":0.2625682456328843,"score_spread":0.23324601657409813,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3211913391","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":[0.99287426,0.00069800176,0.005269224,0.00001982618,0.000011787134,0.000006375393,0.000059283033,0.00005201928,0.0010090944],"genre_scores_gemma":[0.9996126,0.00005250645,0.00022244113,0.000001362289,0.0000015894876,0.0000014857281,0.000022640772,0.0000062185572,0.000079171754],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997266,0.000035099587,0.0000129063355,0.000068252964,0.00008587635,0.00007124813],"domain_scores_gemma":[0.9990079,0.00057524897,0.00017544035,0.00007204866,0.00011488687,0.000054492542],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003346893,0.00027407863,0.0005178319,0.0003642534,0.00030426847,0.00071490294,0.000411123,0.00048023154,0.0007184932],"category_scores_gemma":[0.0024455532,0.00018356531,0.00029850466,0.00023896784,0.00043734335,0.00045088105,0.0002916327,0.00027270525,0.00013884052],"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":[0.0025163232,0.000118361524,0.033732343,0.00030972814,0.00009363069,0.001812851,0.00037092486,0.13510604,0.79742265,0.0024213442,0.00040993787,0.025685871],"study_design_scores_gemma":[0.00005983261,0.0016219264,0.091792196,0.000068962145,0.00007779902,0.001311519,0.00018293838,0.31882396,0.58321714,0.00089886185,0.0018581969,0.000086721586],"about_ca_topic_score_codex":0.0006079392,"about_ca_topic_score_gemma":0.0002784833,"teacher_disagreement_score":0.0007184932,"about_ca_system_score_codex":0.00044412608,"about_ca_system_score_gemma":0.00023447628,"threshold_uncertainty_score":0.003222406},"labels":[],"label_agreement":null},{"id":"W3213123444","doi":"10.32920/ryerson.14644389.v1","title":"Cold flow testing of laboratory-scale hybrid rocket engine test apparatus","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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":"Rocket engine; Nozzle; Thrust; Mechanics; Rocket (weapon); Transient (computer programming); Flow (mathematics); Engineering; Aerospace engineering; Physics; Computer science","score_opus":0.02280089114510181,"score_gpt":0.2494623795760936,"score_spread":0.2266614884309918,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3213123444","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":[0.99037313,0.00006960034,0.008241739,0.000021885877,0.000020847234,0.00013800098,0.00032653692,0.0002290087,0.000579057],"genre_scores_gemma":[0.9924384,0.00006594119,0.0053675883,0.00003093016,0.000011703435,0.00019900782,0.0004612494,0.00004615807,0.0013791352],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99938333,0.0000849613,0.000048949765,0.00014571394,0.00024237082,0.00009470943],"domain_scores_gemma":[0.9988827,0.0003019049,0.00014460464,0.00014089377,0.00043505328,0.000094865056],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00080008054,0.00060064316,0.0004825336,0.000659165,0.00053460215,0.00040326754,0.001086555,0.00067497516,0.0021596404],"category_scores_gemma":[0.001540917,0.00015834333,0.0003658501,0.00030015697,0.00048979477,0.0004992768,0.0005571295,0.0005091774,0.0005236002],"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":[0.0007632304,0.00036636333,0.004224184,0.00013975127,0.000019383668,0.00028075348,0.00024627568,0.0020955363,0.98387724,0.00018501785,0.00021600269,0.0075863795],"study_design_scores_gemma":[0.000076197604,0.004287571,0.018242251,0.000019185356,0.00003237753,0.00018029395,0.00021008839,0.0051314333,0.97070146,0.000049942075,0.0010328334,0.00003639248],"about_ca_topic_score_codex":0.001660426,"about_ca_topic_score_gemma":0.002397398,"teacher_disagreement_score":0.0021596404,"about_ca_system_score_codex":0.00046860785,"about_ca_system_score_gemma":0.00022054768,"threshold_uncertainty_score":0.0072247386},"labels":[],"label_agreement":null},{"id":"W32989260","doi":"10.1038/s41391-020-00288-y","title":"Numerical studies on the separation dynamics of a strap-on rocket booster in the next-generation computing system","year":2008,"lang":"en","type":"dissertation","venue":"Prostate Cancer and Prostatic Diseases","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"McMaster University; Canadian Urological Association","keywords":"Booster (rocketry); Aerospace engineering; Separation (statistics); Aeronautics; Dynamics (music); Rocket (weapon); Astronautics; Computer science; Engineering; Physics; Machine learning; Acoustics","score_opus":0.07264023446706222,"score_gpt":0.34735169655152537,"score_spread":0.2747114620844632,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W32989260","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":[0.9198829,0.0006559223,0.04018087,0.0011449802,0.00019042715,0.00007505537,0.00035748296,0.0002854139,0.037226927],"genre_scores_gemma":[0.98542976,0.00013523747,0.007879314,0.00006832944,0.000012358964,0.000028605908,0.000116814364,0.00003890236,0.0062906207],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99992466,0.000014319043,0.0000024206054,0.000009391132,0.000020886326,0.000028431117],"domain_scores_gemma":[0.99956816,0.00019258671,0.000053753774,0.000022709675,0.00009037823,0.0000724791],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002665292,0.0002852918,0.00044548418,0.00034719866,0.0008185913,0.0006864946,0.0005774807,0.0007581349,0.004536101],"category_scores_gemma":[0.0009691571,0.00015307163,0.00038235314,0.0004140159,0.000561482,0.00049812475,0.00044467702,0.0006174769,0.00029505923],"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":[0.00021201602,0.00010069295,0.0031701792,0.00007803435,0.000036227033,0.00021853615,0.00010793838,0.97291654,0.0068058097,0.009964217,0.0013740106,0.005015804],"study_design_scores_gemma":[0.000009121582,0.0000193184,0.00034966494,0.0000021065887,0.0000034119919,0.000008269894,0.000019138108,0.9984769,0.00047145094,0.00042388844,0.000212079,0.0000046739656],"about_ca_topic_score_codex":0.014721398,"about_ca_topic_score_gemma":0.009490611,"teacher_disagreement_score":0.014721398,"about_ca_system_score_codex":0.00067655626,"about_ca_system_score_gemma":0.0008075247,"threshold_uncertainty_score":0.029271424},"labels":[],"label_agreement":null},{"id":"W35275083","doi":"10.2196/29196","title":"Turbojet Analytical Model Development and Validation","year":2012,"lang":"en","type":"article","venue":"JMIR Formative Research","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"Eunice Kennedy Shriver National Institute of Child Health and Human Development; National Institute on Minority Health and Health Disparities","keywords":"Turbojet; Engineering; Nozzle; Thrust; Thrust vectoring; Aerospace engineering; Automotive engineering","score_opus":0.1316111699990628,"score_gpt":0.41309656291926167,"score_spread":0.28148539292019886,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W35275083","genre_codex":"methods","genre_gemma":"methods","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.12208066,0.0002641303,0.83319116,0.0006042968,0.0005803891,0.0025557075,0.002805524,0.0034070981,0.03451099],"genre_scores_gemma":[0.401431,0.00051205425,0.5762441,0.00022814932,0.00006353645,0.006705515,0.0030252403,0.00069789164,0.011092392],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.997248,0.0015505338,0.00020322484,0.00027126935,0.00055897684,0.000167981],"domain_scores_gemma":[0.9853019,0.0091967005,0.0004058519,0.0007297011,0.004232512,0.00013337235],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0076281955,0.001443716,0.0008144695,0.0017517387,0.0011489093,0.0020774344,0.002236913,0.0013899633,0.017876135],"category_scores_gemma":[0.034310658,0.0007532014,0.001947502,0.0013474181,0.00055291277,0.0014656348,0.0015108349,0.00237329,0.0041056103],"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":[0.00047033056,0.000839847,0.020792108,0.00091452495,0.00040932276,0.00037400398,0.0011428172,0.6946716,0.0016858476,0.033705644,0.014638355,0.23035562],"study_design_scores_gemma":[0.00006902586,0.0001689015,0.0017325791,0.00019355016,0.0000619261,0.000041131625,0.0002691926,0.9848164,0.0012393153,0.0045623817,0.0068108486,0.000034813667],"about_ca_topic_score_codex":0.032261003,"about_ca_topic_score_gemma":0.020727603,"teacher_disagreement_score":0.032261003,"about_ca_system_score_codex":0.00115993,"about_ca_system_score_gemma":0.006970117,"threshold_uncertainty_score":0.06414646},"labels":[],"label_agreement":null},{"id":"W38530340","doi":"10.26077/926p-w978","title":"The Space Technology Research Vehicles: STRV-1A,B,C&D","year":2025,"lang":"en","type":"article","venue":"The Journal of Physical Chemistry A","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"U.S. Naval Research Laboratory; Canadian Space Agency; Office of Naval Research; U.S. Air Force; European Space Agency","keywords":"Space (punctuation); Computer science","score_opus":0.02069391820864622,"score_gpt":0.3373668997254288,"score_spread":0.3166729815167826,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W38530340","genre_codex":"other","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":[0.031815354,0.07103179,0.039341364,0.00718973,0.004074856,0.0008755109,0.006762264,0.003704602,0.8352046],"genre_scores_gemma":[0.16026334,0.052354887,0.04185849,0.0019897576,0.0017106569,0.00044041028,0.031833276,0.00076785765,0.7087813],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9994849,0.000051794956,0.000018438917,0.00006279993,0.00026635366,0.00011574692],"domain_scores_gemma":[0.9997644,0.00001687271,0.0000316561,0.000019402041,0.000100181045,0.00006743185],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00046799117,0.00083693647,0.00029358576,0.0010228534,0.0006460179,0.0013612398,0.0004109543,0.0007149755,0.021027047],"category_scores_gemma":[0.0003737167,0.00015834167,0.00018959462,0.0011017008,0.00026729543,0.00095628755,0.0009195081,0.0007963941,0.013165599],"study_design_candidate":"not_applicable","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":[0.00028550148,0.00009692683,0.003511735,0.00044715838,0.000031489904,0.00014581766,0.0001615425,0.0016779101,0.013126901,0.03883495,0.23108234,0.7105977],"study_design_scores_gemma":[0.0000070429737,0.00013935257,0.0009841894,0.000025004492,0.0000040842892,0.00007835967,0.00003601588,0.0003354452,0.00097315514,0.0008949037,0.9965172,0.000005262508],"about_ca_topic_score_codex":0.0047622095,"about_ca_topic_score_gemma":0.0062103528,"teacher_disagreement_score":0.021027047,"about_ca_system_score_codex":0.0007623923,"about_ca_system_score_gemma":0.0016553963,"threshold_uncertainty_score":0.07034254},"labels":[],"label_agreement":null},{"id":"W4200515333","doi":"10.15407/pmach2021.04.027","title":"Retrospective Review of a Two-Phase Mechanically Pumped Loop for Spacecraft Thermal Control Systems","year":2021,"lang":"en","type":"review","venue":"Journal of Mechanical Engineering","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":13,"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":"Spacecraft; Aerospace engineering; Payload (computing); Aerospace; Engineering; Mechanical engineering; Environmental science; Computer science","score_opus":0.03940682802387865,"score_gpt":0.3502396585595903,"score_spread":0.31083283053571165,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4200515333","genre_codex":"review","genre_gemma":"review","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"review","genre_consensus":"review","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.001665004,0.9882498,0.0041351914,0.00038246036,0.000935378,0.000040046347,0.000108648375,0.000037035334,0.004446424],"genre_scores_gemma":[0.0127044,0.9775603,0.004578061,0.00067829073,0.0010419086,0.000049871112,0.0003627467,0.000034805853,0.0029896896],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9989483,0.00020050185,0.00022077744,0.00017124027,0.00041513622,0.000044107506],"domain_scores_gemma":[0.997022,0.0010430305,0.00029341067,0.00010542808,0.0014590878,0.00007707606],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0012791242,0.00063312723,0.0007281403,0.0028293973,0.0003672666,0.0011778611,0.0008171281,0.0007833518,0.0031181655],"category_scores_gemma":[0.0026063938,0.0003520095,0.00064412534,0.0030915095,0.00039935985,0.0019410842,0.00047699644,0.0007229928,0.0010198797],"study_design_candidate":"not_applicable","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":[0.00016992526,0.00007673747,0.0008043288,0.03764589,0.0001343051,0.0004563963,0.0002979086,0.001605838,0.007888073,0.006752338,0.030633602,0.91353476],"study_design_scores_gemma":[0.0000074035293,0.00031219123,0.0024510764,0.0051248553,0.00017855426,0.0009308104,0.00016119008,0.0005413734,0.0032542446,0.00077754614,0.98622847,0.00003241157],"about_ca_topic_score_codex":0.0015205244,"about_ca_topic_score_gemma":0.0014778747,"teacher_disagreement_score":0.0031181655,"about_ca_system_score_codex":0.00065760664,"about_ca_system_score_gemma":0.002011366,"threshold_uncertainty_score":0.01043129},"labels":[],"label_agreement":null},{"id":"W4206753268","doi":"10.4271/03-15-04-0031","title":"Calculation of Air Velocity on the Helicopter Turboshaft Engines Inlet","year":2021,"lang":"en","type":"article","venue":"SAE International Journal of Engines","topic":"Rocket and propulsion systems research","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":"University of Windsor","funders":"","keywords":"Inlet; Environmental science; Aerospace engineering; Marine engineering; Aeronautics; Automotive engineering; Mechanics; Engineering; Mechanical engineering; Physics","score_opus":0.02236493032371241,"score_gpt":0.28785897485205986,"score_spread":0.26549404452834746,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4206753268","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":[0.6173808,0.00057249854,0.336441,0.000191953,0.00019574883,0.00019861555,0.0005691392,0.0008847649,0.043565422],"genre_scores_gemma":[0.9562686,0.00027651023,0.03496217,0.000021721251,0.000014048335,0.000042593085,0.000210891,0.000082299746,0.008121238],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999187,0.000009284314,0.000004910121,0.000014327536,0.000037228812,0.000015638268],"domain_scores_gemma":[0.99987185,0.00003658409,0.000015030457,0.000007869753,0.00005995052,0.000008719867],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00014226965,0.00043480768,0.00039453333,0.00053965265,0.0004789524,0.0006872343,0.00046920273,0.0006080959,0.001941207],"category_scores_gemma":[0.0005867545,0.00019462599,0.00042452107,0.00030692676,0.00032027753,0.000360048,0.00025887648,0.00032888012,0.0005284293],"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":[0.00013313419,0.00006201153,0.009974358,0.00014828937,0.00001589638,0.0008483165,0.00021215032,0.88858616,0.034377076,0.009789223,0.0014777093,0.054375656],"study_design_scores_gemma":[0.0000067219057,0.000026872805,0.0016910116,0.000016875309,0.000003853103,0.000044973018,0.00004368448,0.9891487,0.0073742913,0.0002852321,0.0013481958,0.0000096805325],"about_ca_topic_score_codex":0.021398108,"about_ca_topic_score_gemma":0.014186475,"teacher_disagreement_score":0.021398108,"about_ca_system_score_codex":0.00065275555,"about_ca_system_score_gemma":0.0011788551,"threshold_uncertainty_score":0.042547107},"labels":[],"label_agreement":null},{"id":"W4223589818","doi":"10.1177/09544100221083714","title":"Efficiency of rocket engine thrust vector control by solid obstacle on the nozzle wall","year":2022,"lang":"en","type":"article","venue":"Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":7,"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; Thrust; Supersonic speed; Aerospace engineering; Obstacle; Rocket engine; Solid-fuel rocket; Mechanics; Rocket engine nozzle; Rocket (weapon); Liquid-propellant rocket; Aerodynamics; Propulsion; Discharge coefficient; Jet (fluid); Missile; Mechanical engineering; Engineering; Physics; Propellant","score_opus":0.010237437851118353,"score_gpt":0.21147044484926023,"score_spread":0.20123300699814187,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4223589818","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":[0.9694699,0.0003283811,0.023294583,0.000039960203,0.000026072177,0.000013522275,0.000030728446,0.00019602735,0.0066007264],"genre_scores_gemma":[0.99901974,0.000034556942,0.0006752227,0.0000027350184,8.0297895e-7,0.000002545989,0.000012990469,0.000005843431,0.0002454811],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997836,0.000021243866,0.00001022413,0.000029539535,0.00007805979,0.000077352815],"domain_scores_gemma":[0.9996082,0.00016695865,0.0000792945,0.000030591487,0.00009020764,0.000024780855],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025905969,0.00033963207,0.00040454397,0.0002899407,0.0002181813,0.0006159713,0.00033017728,0.0003449538,0.0010262277],"category_scores_gemma":[0.00082725025,0.000116191135,0.0003249215,0.00015633884,0.00030150355,0.00039270963,0.00025807458,0.00016828136,0.0001180837],"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":[0.00094027445,0.00015246398,0.008095228,0.00022735924,0.00005787194,0.00039990258,0.00013817046,0.8338443,0.11355451,0.0022747072,0.00040638843,0.039908785],"study_design_scores_gemma":[0.000025018191,0.00043541277,0.004611951,0.000010603071,0.000023600747,0.000048212605,0.00007476634,0.94822305,0.045846123,0.00028453238,0.0003978223,0.000018854993],"about_ca_topic_score_codex":0.0027243735,"about_ca_topic_score_gemma":0.001060905,"teacher_disagreement_score":0.0027243735,"about_ca_system_score_codex":0.00032923493,"about_ca_system_score_gemma":0.00035893449,"threshold_uncertainty_score":0.0054169893},"labels":[],"label_agreement":null},{"id":"W4225905900","doi":"10.2514/1.b38659","title":"Evaluation of a Paraffin/Nitrous Oxide Hybrid Rocket Motor with a Passive Mixing Device","year":2022,"lang":"en","type":"article","venue":"Journal of Propulsion and Power","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":11,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Calgary","funders":"Canadian Network for Research and Innovation in Machining Technology, Natural Sciences and Engineering Research Council of Canada","keywords":"Mixing (physics); Combustion; Materials science; Baffle; Nitrous oxide; Propellant; Combustion chamber; Mass flux; Work (physics); Mechanics; Nuclear engineering; Automotive engineering; Environmental science; Aerospace engineering; Chemistry; Thermodynamics; Physics; Engineering","score_opus":0.024105728297985525,"score_gpt":0.27401205051104954,"score_spread":0.24990632221306402,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4225905900","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":[0.99384636,0.00027870073,0.005016951,0.000030806095,0.00002539394,0.00007372224,0.000051759882,0.00004754254,0.0006287654],"genre_scores_gemma":[0.9899635,0.00029214364,0.0076394184,0.000015243875,0.0000066946363,0.00005567189,0.000107703265,0.00001705053,0.0019025448],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99965286,0.000046738798,0.000030191028,0.000073652845,0.00015426209,0.000042355943],"domain_scores_gemma":[0.999655,0.00008108548,0.00005946331,0.0000274052,0.00013684384,0.000040181014],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000720847,0.0003535478,0.00030724882,0.0003401479,0.00023126729,0.00044513974,0.0005604564,0.0003794869,0.00094041467],"category_scores_gemma":[0.00069062674,0.00016485971,0.00027043995,0.000182574,0.00026039564,0.0006208367,0.00034951986,0.00024372779,0.00023449126],"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":[0.000661594,0.00022136638,0.0016953249,0.00022465199,0.000029939518,0.00009303804,0.000056236047,0.0013385038,0.9840544,0.00019208595,0.00007429455,0.01135857],"study_design_scores_gemma":[0.00006246735,0.0059086215,0.0063077365,0.000014146023,0.00006260732,0.00014469498,0.00009326462,0.012262083,0.9719284,0.000033642507,0.0031613696,0.000021017137],"about_ca_topic_score_codex":0.00049493,"about_ca_topic_score_gemma":0.0007068712,"teacher_disagreement_score":0.00094041467,"about_ca_system_score_codex":0.00032678203,"about_ca_system_score_gemma":0.00024534,"threshold_uncertainty_score":0.0038122535},"labels":[],"label_agreement":null},{"id":"W4229365935","doi":"10.1016/j.ast.2022.107617","title":"Effect of area ratio and heat release method on the Ma∞ = 2-6 operation performance of rocket-based combined cycle engine","year":2022,"lang":"en","type":"article","venue":"Aerospace Science and Technology","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":13,"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 Calgary","funders":"National Natural Science Foundation of China","keywords":"Ramjet; Scramjet; Combustor; Aerospace engineering; Mechanics; Mach number; Specific impulse; Hypersonic speed; Rocket (weapon); Combustion; Materials science; Environmental science; Propulsion; Engineering; Physics; Chemistry","score_opus":0.007122866054960872,"score_gpt":0.2496611824086696,"score_spread":0.24253831635370873,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4229365935","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":[0.99823976,0.00038902936,0.0007399668,0.000010477531,0.0000124499475,0.000002743749,0.000039236013,0.000051010866,0.0005152959],"genre_scores_gemma":[0.99916387,0.00008638452,0.0002588346,0.0000041256735,0.0000038768353,0.000003411706,0.00003308255,0.000018034005,0.0004283765],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998332,0.000021516105,0.0000135912,0.000045205557,0.00005038578,0.000036027952],"domain_scores_gemma":[0.99966323,0.00014513254,0.00005798841,0.000031285414,0.00006679506,0.00003548765],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023988784,0.00032067197,0.00034924576,0.00032088603,0.00021674235,0.00039205264,0.0004196573,0.00023706659,0.0019984941],"category_scores_gemma":[0.0005655128,0.00017811924,0.00019436951,0.00025926303,0.00018765226,0.0004912829,0.00019624345,0.00019392486,0.0003812074],"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":[0.0049325973,0.0001731232,0.0037192584,0.00022739846,0.000039197308,0.00017001967,0.00013743831,0.0061969254,0.9628466,0.00018676874,0.00020778687,0.021163046],"study_design_scores_gemma":[0.00004062757,0.001807497,0.016088134,0.0000114180775,0.000059865662,0.00010537035,0.00011530607,0.013007644,0.9678573,0.000041904237,0.0008278994,0.000037077545],"about_ca_topic_score_codex":0.00040758806,"about_ca_topic_score_gemma":0.00058559043,"teacher_disagreement_score":0.0019984941,"about_ca_system_score_codex":0.00012137719,"about_ca_system_score_gemma":0.00012396515,"threshold_uncertainty_score":0.0066856146},"labels":[],"label_agreement":null},{"id":"W4230070567","doi":"10.32920/ryerson.14635638","title":"Aerodynamic Optimization of the Von Karman Nose Cone for a Supersonic Sounding Rocket","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Aerospace engineering; Sounding rocket; Supersonic speed; Aerodynamics; Rocket (weapon); Cone (formal languages); Angle of attack; Engineering; Mechanical engineering; Computer science","score_opus":0.02610026306870565,"score_gpt":0.2719170150094971,"score_spread":0.24581675194079144,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4230070567","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":[0.529507,0.00043612786,0.44221944,0.00013113872,0.00010221221,0.00026692267,0.00015429492,0.0004384041,0.026744518],"genre_scores_gemma":[0.9315888,0.00016448983,0.063425526,0.000024269933,0.000008722032,0.000068777954,0.00009114797,0.00010063494,0.0045275777],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997603,0.000028543203,0.000007709498,0.000024573043,0.00014127251,0.000037637346],"domain_scores_gemma":[0.9997409,0.000057754154,0.000036847534,0.000020859916,0.00011715673,0.000026559297],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004855944,0.0005920522,0.00044426855,0.0003284856,0.00032602617,0.00078835007,0.00032883842,0.0004325824,0.0016614129],"category_scores_gemma":[0.0006059535,0.00021476197,0.00045780028,0.00023094933,0.00028736214,0.00028298568,0.00027914278,0.00035998895,0.0003534986],"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":[0.00030654765,0.0001950469,0.0033689223,0.00019388483,0.000024244977,0.0005263124,0.00008552017,0.74379575,0.17688996,0.0058552977,0.0010268731,0.06773169],"study_design_scores_gemma":[0.000038607504,0.0006907513,0.0027204116,0.000022941347,0.000017146229,0.00020873728,0.00008410809,0.9469163,0.044500403,0.00096555176,0.0037927758,0.000042307085],"about_ca_topic_score_codex":0.0015313225,"about_ca_topic_score_gemma":0.0033250218,"teacher_disagreement_score":0.0016614129,"about_ca_system_score_codex":0.00037581476,"about_ca_system_score_gemma":0.0010201028,"threshold_uncertainty_score":0.005558014},"labels":[],"label_agreement":null},{"id":"W4230563606","doi":"10.32920/ryerson.14654895","title":"Comparison of cylindrical and non-cylindrical grain internal ballistic behavior of hybrid rocket engines and solid rocket motors","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Rocket and propulsion systems research","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":"Toronto Metropolitan University","funders":"","keywords":"Specific impulse; Propellant; Solid-fuel rocket; Aerospace engineering; Internal ballistics; Propulsion; Rocket (weapon); Combustion; Internal flow; Thrust; Mechanical engineering; Materials science; Mechanics; Physics; Engineering; Flow (mathematics); Chemistry","score_opus":0.03440304524303126,"score_gpt":0.33529102987715803,"score_spread":0.30088798463412675,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4230563606","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":[0.9687251,0.00033700804,0.011356637,0.00010472436,0.000029301247,0.000057242974,0.00037899904,0.00028959062,0.018721359],"genre_scores_gemma":[0.997154,0.000089087625,0.0015034392,0.000008559849,0.0000018419781,0.000015750895,0.00023454388,0.000031006493,0.00096172385],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99981815,0.0000207008,0.000009248369,0.00002099297,0.00007528849,0.000055580727],"domain_scores_gemma":[0.99943,0.00019297298,0.00008100687,0.00006779198,0.00016378154,0.000064330554],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00039192275,0.0003110909,0.00044572863,0.00069096213,0.00037480207,0.00078324095,0.0007395656,0.00052286906,0.0019813823],"category_scores_gemma":[0.001343321,0.00022318155,0.00063362677,0.0005399156,0.0004970168,0.00047889832,0.0003480248,0.00035068757,0.00033757673],"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":[0.00032764114,0.000088333916,0.0060207946,0.00013355985,0.00004668795,0.00024153032,0.0001604835,0.96349406,0.014777342,0.0056124046,0.0008255694,0.00827155],"study_design_scores_gemma":[0.000017409713,0.00015109435,0.0034553518,0.0000116954525,0.000013850256,0.000042566655,0.00007822124,0.98809004,0.0067155934,0.00060763815,0.0007931348,0.000023355364],"about_ca_topic_score_codex":0.008658819,"about_ca_topic_score_gemma":0.0061566145,"teacher_disagreement_score":0.008658819,"about_ca_system_score_codex":0.0009613067,"about_ca_system_score_gemma":0.0006479588,"threshold_uncertainty_score":0.017216861},"labels":[],"label_agreement":null},{"id":"W4231808827","doi":"10.22215/etd/2008-08486","title":"Rocket nozzle design with ejector effect potential","year":2008,"lang":"en","type":"dissertation","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Canadian Heritage; Library and Archives Canada","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Injector; Nozzle; Rocket (weapon); Engineering; Aeronautics; Mechanical engineering","score_opus":0.011620855566443126,"score_gpt":0.24230598354457727,"score_spread":0.23068512797813415,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4231808827","genre_codex":"methods","genre_gemma":"methods","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.07333165,0.0026357349,0.8349217,0.00042268026,0.0005752531,0.0003972899,0.00030398302,0.0020902033,0.085321456],"genre_scores_gemma":[0.78897595,0.0013600853,0.15245035,0.0001597683,0.00009101292,0.00017363038,0.0003514301,0.0005680799,0.055869643],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99943227,0.000042524378,0.000028480388,0.000079500634,0.0003604388,0.000056769968],"domain_scores_gemma":[0.99959,0.00007062983,0.000065052365,0.00003573384,0.00019978653,0.000038722264],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00046270216,0.0003842439,0.0005668633,0.00038725254,0.00033630087,0.0014650605,0.0012533846,0.0009779438,0.011284222],"category_scores_gemma":[0.00092594227,0.00034730972,0.000566665,0.0004071413,0.00024361393,0.0009977862,0.00071831315,0.0005546073,0.0023269963],"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":[0.001153751,0.0001945149,0.0026926498,0.0012110029,0.000100675854,0.0012271557,0.0002235421,0.10283815,0.59646153,0.043978956,0.009028245,0.2408898],"study_design_scores_gemma":[0.00037615735,0.0019101533,0.0052948683,0.00014190316,0.00012554323,0.002862324,0.00011641542,0.43984446,0.4482201,0.0047768685,0.09614794,0.00018331439],"about_ca_topic_score_codex":0.00039636015,"about_ca_topic_score_gemma":0.00056866667,"teacher_disagreement_score":0.011284222,"about_ca_system_score_codex":0.0005299465,"about_ca_system_score_gemma":0.0008478893,"threshold_uncertainty_score":0.03774953},"labels":[],"label_agreement":null},{"id":"W4232284193","doi":"10.32920/ryerson.14645013","title":"Compatibility Of Metallic &amp; Non-Metallic Turbine Engine Materials With Aviation Fuels","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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":"Compatibility (geochemistry); Aerospace; Aviation; Turbine; Mechanical engineering; Materials science; Process engineering; Computer science; Engineering; Composite material; Aerospace engineering","score_opus":0.03262144368006889,"score_gpt":0.2745440959211908,"score_spread":0.2419226522411219,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4232284193","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":[0.99378985,0.00052755995,0.0016295825,0.00001989876,0.000024090798,0.00003036905,0.00012808635,0.000023093162,0.0038274566],"genre_scores_gemma":[0.99481815,0.0002024337,0.002108018,0.000013172355,0.000005185397,0.000017167147,0.00019283687,0.000020475421,0.0026225238],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9991905,0.00012262163,0.00007065503,0.0001129246,0.00044293347,0.000060380233],"domain_scores_gemma":[0.99929607,0.00015491736,0.00014618029,0.000102564074,0.00025968754,0.000040523486],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000511225,0.0002468586,0.00017354033,0.00094002986,0.00027008695,0.00039181573,0.00029325593,0.00037851502,0.0020875828],"category_scores_gemma":[0.0011276734,0.00016153378,0.00019549136,0.00046453328,0.0003168233,0.00034477806,0.0003002463,0.00016318314,0.00043243874],"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":[0.00022378103,0.000044171586,0.0059043407,0.00014372336,0.000014843143,0.0002755763,0.00012559636,0.000361005,0.9863646,0.00033176228,0.000075521384,0.00613511],"study_design_scores_gemma":[0.000005610345,0.0007654382,0.030174451,0.000022386997,0.00003199101,0.0005823055,0.00023178279,0.001011942,0.96405166,0.00009136688,0.003021219,0.000009832377],"about_ca_topic_score_codex":0.00042698538,"about_ca_topic_score_gemma":0.0011810248,"teacher_disagreement_score":0.0020875828,"about_ca_system_score_codex":0.0001513086,"about_ca_system_score_gemma":0.00016958288,"threshold_uncertainty_score":0.0069836974},"labels":[],"label_agreement":null},{"id":"W4234425786","doi":"10.32920/ryerson.14637570.v2","title":"A computational study of soot formation and flame structure of coflow laminar methane/air diffusion flames under microgravity and normal gravity","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Rocket and propulsion systems research","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":"Toronto Metropolitan University","funders":"","keywords":"Soot; Diffusion flame; Laminar flow; Diffusion; Methane; Chemistry; Mechanics; Aerosol; Zero gravity; Premixed flame; Combustion; Thermodynamics; Combustor; Physics; Physical chemistry; Organic chemistry","score_opus":0.015206880568088667,"score_gpt":0.264834750250446,"score_spread":0.24962786968235734,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4234425786","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":[0.99392974,0.000060990897,0.0035902073,0.00005197099,0.000010113562,0.000020033813,0.00019451845,0.00005733615,0.002085244],"genre_scores_gemma":[0.99482626,0.000047509562,0.0044387095,0.000009670784,0.000003295987,0.000017741111,0.0001452911,0.000013874904,0.00049761543],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99991393,0.000013122269,0.0000053908666,0.000019514495,0.000022131218,0.000025870806],"domain_scores_gemma":[0.9996549,0.00016641228,0.000072031544,0.000031039584,0.000038594597,0.000037035403],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00022492577,0.00052921154,0.00058243045,0.00039153552,0.0009012578,0.00064383046,0.0006321574,0.0010072639,0.00093832385],"category_scores_gemma":[0.0007594042,0.00025048797,0.0006234632,0.00038965474,0.0007105729,0.00037881915,0.00041803523,0.00035625228,0.000082151586],"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":[0.00026757678,0.00012116116,0.01089539,0.00010885133,0.000031633044,0.0003171988,0.00014935361,0.9648111,0.01920428,0.0009860191,0.00013227809,0.0029752026],"study_design_scores_gemma":[0.000022820062,0.000090644295,0.004788272,0.0000054620323,0.000009809153,0.00005382187,0.00007294095,0.9905195,0.004036023,0.00018278166,0.00020635573,0.00001149958],"about_ca_topic_score_codex":0.019615695,"about_ca_topic_score_gemma":0.0098971985,"teacher_disagreement_score":0.019615695,"about_ca_system_score_codex":0.0007736444,"about_ca_system_score_gemma":0.0009163552,"threshold_uncertainty_score":0.039003074},"labels":[],"label_agreement":null},{"id":"W4234557154","doi":"10.32920/14640180.v1","title":"Numerical Evaluation of the Use of Aluminum Particles for Enhancing Solid Rocket Motor Combustion Stability","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Rocket and propulsion systems research","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":"Toronto Metropolitan University","funders":"","keywords":"Propellant; Solid-fuel rocket; Combustion; Mechanics; Rocket (weapon); Materials science; Internal flow; Transient (computer programming); Instability; Particle (ecology); Solid fuel; Chamber pressure; Flow (mathematics); Internal pressure; Aerospace engineering; Composite material; Physics; Chemistry; Engineering; Geology; Computer science","score_opus":0.18679492589856944,"score_gpt":0.3491696619787813,"score_spread":0.16237473608021186,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4234557154","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":[0.97684526,0.00010474702,0.018627776,0.000040497966,0.000017310203,0.00003377255,0.00004410895,0.00011540108,0.004171133],"genre_scores_gemma":[0.99489874,0.000034993438,0.004610235,0.0000025377267,9.575111e-7,0.000006785689,0.000014891553,0.000006854973,0.00042409165],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99990153,0.000019217117,0.0000058498163,0.000009564268,0.000046638295,0.000017272174],"domain_scores_gemma":[0.99952996,0.00022138348,0.00008340606,0.000036693054,0.00010483496,0.000023765106],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00033060124,0.00027095148,0.00024281646,0.0002945814,0.00016858667,0.00038236738,0.00030089536,0.0003214522,0.0008870114],"category_scores_gemma":[0.0011143814,0.00008682152,0.0001604754,0.00020781651,0.00034247673,0.00017727967,0.0002374892,0.00015290853,0.00009981813],"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":[0.0007602545,0.00022058947,0.0052233394,0.00026494145,0.000026089996,0.000281951,0.0001649379,0.70753795,0.2555168,0.0027685724,0.00022998349,0.027004706],"study_design_scores_gemma":[0.00003245383,0.00051501795,0.0012311813,0.0000063616485,0.000013382316,0.000029010525,0.000040024293,0.90634185,0.09120756,0.00015642759,0.00041796538,0.000008778012],"about_ca_topic_score_codex":0.0016720694,"about_ca_topic_score_gemma":0.0014035606,"teacher_disagreement_score":0.0016720694,"about_ca_system_score_codex":0.00023896967,"about_ca_system_score_gemma":0.00026488738,"threshold_uncertainty_score":0.0033246875},"labels":[],"label_agreement":null},{"id":"W4235789364","doi":"10.1016/j.carbon.2017.08.057","title":"Ablation performance of a 4D-braided C/C composite in a parameter-variable channel of a Laval nozzle in a solid rocket motor","year":2017,"lang":"en","type":"article","venue":"Carbon","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Solid-fuel rocket; Nozzle; Ablation; Composite number; Materials science; Rocket engine nozzle; Variable (mathematics); Aerospace engineering; Composite material; Engineering; Propellant; Mathematics; Mathematical analysis","score_opus":0.022548505791605684,"score_gpt":0.26823854546421266,"score_spread":0.24569003967260697,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4235789364","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":[0.9981554,0.0001369749,0.00087666686,0.000024499788,0.000013515521,0.000004754567,0.000041105242,0.000068333575,0.0006787416],"genre_scores_gemma":[0.99874026,0.000039384307,0.00052269164,0.0000059293457,0.0000021644166,0.0000031066763,0.00002143118,0.000012043147,0.0006530123],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997532,0.000016126964,0.000010675458,0.00007729043,0.000093559975,0.000049151753],"domain_scores_gemma":[0.9996643,0.00011718541,0.00006269923,0.000029256315,0.000087034736,0.0000395398],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00031426564,0.0002426739,0.00047360457,0.00030485707,0.0004832681,0.00049591943,0.0005573151,0.0006747883,0.0018758195],"category_scores_gemma":[0.00046217453,0.0002074922,0.00023978285,0.00022166882,0.0005342774,0.00037841327,0.00031596332,0.00028655038,0.00022249694],"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":[0.0006117093,0.000045952336,0.0008148797,0.000065480446,0.000009743881,0.00014640953,0.000078300145,0.002562738,0.9932373,0.000109541324,0.00012438478,0.0021937129],"study_design_scores_gemma":[0.000032333075,0.000556058,0.0071204146,0.000009388272,0.000025656162,0.0000657918,0.000088415516,0.022056611,0.96912295,0.000035910554,0.0008586177,0.000027891949],"about_ca_topic_score_codex":0.001738895,"about_ca_topic_score_gemma":0.0020762389,"teacher_disagreement_score":0.0018758195,"about_ca_system_score_codex":0.00043802473,"about_ca_system_score_gemma":0.00034654504,"threshold_uncertainty_score":0.0062752366},"labels":[],"label_agreement":null},{"id":"W4237682015","doi":"10.32920/ryerson.14648736","title":"A Mathematical Method for Predicting the Design Performance of Single and Multi-stage Rockets","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Rocket and propulsion systems research","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":"Toronto Metropolitan University","funders":"","keywords":"Integrator; Range (aeronautics); Set (abstract data type); Computer science; Ordinary differential equation; Tandem; Baseline (sea); Nonlinear system; Path (computing); Multi stage; Aerospace engineering; Rocket (weapon); Mathematical optimization; Simulation; Control theory (sociology); Mathematics; Industrial engineering; Differential equation; Engineering; Mathematical analysis; Control (management); Artificial intelligence; Physics; Telecommunications","score_opus":0.16171363570023883,"score_gpt":0.3602922802790922,"score_spread":0.19857864457885338,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4237682015","genre_codex":"methods","genre_gemma":"methods","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0021652386,0.00012670018,0.9943135,0.000047622212,0.000035089273,0.000025721147,0.00005773124,0.00019215193,0.0030363072],"genre_scores_gemma":[0.27577922,0.0012635177,0.69490504,0.00014198195,0.00013888167,0.00059282745,0.00042292723,0.0005780551,0.026177648],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99956506,0.00007501203,0.000019925763,0.00006910472,0.00023804378,0.000032817334],"domain_scores_gemma":[0.9991067,0.0004880174,0.00009492661,0.00007828163,0.00020763755,0.000024470524],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00093149167,0.00092096976,0.0006260077,0.000961653,0.00041053985,0.0008252005,0.0012693155,0.0010493002,0.004510058],"category_scores_gemma":[0.0032769064,0.0004910319,0.0010185125,0.00078543235,0.0007034457,0.0013125938,0.00072974846,0.0013999942,0.0014919911],"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":[0.000014464292,0.000025421503,0.0003775207,0.00010615825,0.000015153215,0.00003962084,0.000037574093,0.9313037,0.005189722,0.028248582,0.0012026337,0.03343947],"study_design_scores_gemma":[0.000003065411,0.000012453016,0.000071510316,0.000009207567,0.0000044791536,0.000013154222,0.0000040437276,0.9930178,0.00096519105,0.0041456525,0.0017475527,0.0000059698386],"about_ca_topic_score_codex":0.0029216865,"about_ca_topic_score_gemma":0.0020078218,"teacher_disagreement_score":0.004510058,"about_ca_system_score_codex":0.000692161,"about_ca_system_score_gemma":0.0012409065,"threshold_uncertainty_score":0.0150876045},"labels":[],"label_agreement":null},{"id":"W4238976941","doi":"10.32920/14640078","title":"Scale Effects on Quasi-Steady Solid Rocket Internal Ballistic Behaviour","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Rocket and propulsion systems research","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":"Toronto Metropolitan University","funders":"","keywords":"Internal ballistics; Propellant; Solid-fuel rocket; Ballistics; Deflection (physics); Aerospace engineering; Mechanics; Simulation; Engineering; Mechanical engineering; Materials science; Physics; Classical mechanics","score_opus":0.021085191961269737,"score_gpt":0.29954177069246163,"score_spread":0.2784565787311919,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4238976941","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":[0.98081744,0.00015895734,0.013714485,0.00003152981,0.000009608138,0.000014764805,0.000065222455,0.0002694963,0.0049185995],"genre_scores_gemma":[0.99923253,0.000031363,0.00045554191,0.000002338362,6.7797976e-7,0.0000025836107,0.000018277135,0.000021194124,0.00023532078],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998419,0.000019882074,0.000007792282,0.000026037345,0.00007382107,0.000030623018],"domain_scores_gemma":[0.99927336,0.00040167588,0.000090661866,0.00011535353,0.00008975735,0.00002931647],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025750633,0.00026059433,0.00020880882,0.00018556321,0.00017749837,0.0003398831,0.00023012528,0.00020405094,0.0018552161],"category_scores_gemma":[0.0018972143,0.0001678242,0.00025991246,0.00013178185,0.0005454978,0.0003717471,0.00041389253,0.00027704582,0.00027999736],"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":[0.0007309007,0.00010956654,0.016620968,0.00025044294,0.0000456608,0.00060565287,0.00041664435,0.5788279,0.36732104,0.0027909377,0.00033673094,0.03194355],"study_design_scores_gemma":[0.000027328555,0.0007703686,0.046220418,0.000023787183,0.000035769182,0.00021264824,0.0001742655,0.71926916,0.23119423,0.0009946821,0.0010319878,0.00004540311],"about_ca_topic_score_codex":0.0011623972,"about_ca_topic_score_gemma":0.0011666034,"teacher_disagreement_score":0.0018552161,"about_ca_system_score_codex":0.0002635781,"about_ca_system_score_gemma":0.00014650391,"threshold_uncertainty_score":0.0062063336},"labels":[],"label_agreement":null},{"id":"W4239246954","doi":"10.32920/ryerson.14652105.v1","title":"Fluid-structure interaction considerations for solid rocket motor internal ballistics modeling","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Rocket and propulsion systems research","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":"Toronto Metropolitan University","funders":"","keywords":"Internal ballistics; Propellant; Combustion; Mechanics; Solid-fuel rocket; Rocket (weapon); Instability; Combustion chamber; Internal flow; Ballistics; Finite element method; Aerospace engineering; Flow (mathematics); Physics; Materials science; Engineering; Thermodynamics; Chemistry","score_opus":0.06895536003251056,"score_gpt":0.3336702422237189,"score_spread":0.2647148821912083,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4239246954","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":[0.1893275,0.000742491,0.79228246,0.00035970716,0.00005929112,0.00008283756,0.00014416147,0.00046608818,0.016535508],"genre_scores_gemma":[0.94346267,0.0005057261,0.0492093,0.000051208848,0.000045713365,0.00012963101,0.00012425445,0.00019870202,0.0062728724],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998222,0.00005799105,0.0000054057546,0.000013959312,0.00008536986,0.0000151970025],"domain_scores_gemma":[0.9997217,0.00015230766,0.00003839998,0.000021469637,0.00005475509,0.0000113864],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00034531462,0.00045847546,0.0004755775,0.0003136912,0.00047334505,0.00062272797,0.0005371361,0.0005264778,0.002041447],"category_scores_gemma":[0.0011242608,0.00022122309,0.0004803476,0.00024954972,0.0005119587,0.0005019177,0.0005611845,0.00057888875,0.00037119203],"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":[0.000025512034,0.000016346396,0.00046291298,0.000045382716,0.0000065018494,0.000075696924,0.00007950602,0.97383106,0.009108262,0.0113331955,0.00015835381,0.0048573744],"study_design_scores_gemma":[0.0000018101757,0.00001546241,0.000104092906,0.0000035125524,0.0000016151678,0.000010620574,0.000008554682,0.99712723,0.0010178691,0.0010541085,0.00065288343,0.0000023119271],"about_ca_topic_score_codex":0.0067730383,"about_ca_topic_score_gemma":0.004216435,"teacher_disagreement_score":0.0067730383,"about_ca_system_score_codex":0.0004839604,"about_ca_system_score_gemma":0.00067122886,"threshold_uncertainty_score":0.013467193},"labels":[],"label_agreement":null},{"id":"W4240345318","doi":"10.1002/1521-4087(200106)26:3<118::aid-prep118>3.3.co;2-s","title":"On the Optimization of GAP-based Ducted Rocket Fuels from Gas Generator Exhaust Characterization","year":2001,"lang":"en","type":"article","venue":"Propellants Explosives Pyrotechnics","topic":"Rocket and propulsion systems research","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":"Bombardier Recreational Products (Canada)","funders":"","keywords":"Gas generator; Exhaust gas; Exhaust gas recirculation; Carbon monoxide; Rocket (weapon); Environmental science; Carbon fibers; Soot; Materials science; Hydrogen; Combustion; Aerospace engineering; Waste management; Chemistry; Engineering; Composite material; Composite number","score_opus":0.04186693361204328,"score_gpt":0.2389748910964752,"score_spread":0.19710795748443194,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4240345318","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":[0.9842852,0.00030158725,0.013681419,0.000021891768,0.0000030940885,0.000040226398,0.00013092416,0.00010312985,0.0014325735],"genre_scores_gemma":[0.9815639,0.00030162637,0.016540315,0.000008307015,0.000001966107,0.00003227529,0.00039409715,0.000052841522,0.0011047011],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99987197,0.000015074874,0.000009470908,0.000029728366,0.00005818595,0.000015608884],"domain_scores_gemma":[0.9998934,0.000029889397,0.000025690208,0.000009974907,0.000033893295,0.000007056828],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016320913,0.00038717812,0.0004065101,0.0002629995,0.00015308287,0.00043294358,0.00031531753,0.00023421038,0.0007512169],"category_scores_gemma":[0.00036809398,0.0001496525,0.00015046421,0.00028941873,0.00012370973,0.00033255448,0.00024437282,0.00021948619,0.00026508493],"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":[0.00032701882,0.0000963506,0.0016095531,0.00020438529,0.000012503672,0.00009819437,0.000030215851,0.015637524,0.95633006,0.0002825131,0.00007579143,0.025295883],"study_design_scores_gemma":[0.00002512283,0.00078652555,0.0045025004,0.000007894882,0.00002091865,0.0001032158,0.000040917254,0.03686972,0.9560891,0.00011444413,0.0014305572,0.0000090725025],"about_ca_topic_score_codex":0.00048252373,"about_ca_topic_score_gemma":0.0012545295,"teacher_disagreement_score":0.0007512169,"about_ca_system_score_codex":0.0002313436,"about_ca_system_score_gemma":0.0002021678,"threshold_uncertainty_score":0.0025131106},"labels":[],"label_agreement":null},{"id":"W4243390904","doi":"10.35940/ijrte.f7334.038620","title":"Parametric Output of Penetration Length in De-Laval Nozzle using Computational Fluid Dynamics","year":2020,"lang":"en","type":"article","venue":"International Journal of Recent Technology and Engineering (IJRTE)","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":"Nozzle; Computational fluid dynamics; Discharge coefficient; Rocket engine nozzle; Mach number; Mechanics; Conical surface; Angle of attack; Mechanical engineering; Aerospace engineering; Aerodynamics; Physics; Engineering","score_opus":0.02369378789263391,"score_gpt":0.26757702053466703,"score_spread":0.24388323264203313,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4243390904","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":[0.7487901,0.0005101191,0.22076648,0.00034767596,0.00010957412,0.000082055005,0.00090658606,0.0012700297,0.027217245],"genre_scores_gemma":[0.98674357,0.00015394301,0.011335581,0.000013096901,0.000005942158,0.000031011085,0.0002366686,0.000052060437,0.0014280766],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998061,0.000022749682,0.000009283269,0.000029558745,0.00010968588,0.000022661228],"domain_scores_gemma":[0.9996965,0.00014994458,0.000047929094,0.000025009074,0.0000700922,0.000010591346],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000289525,0.00032414027,0.000294992,0.00031168316,0.00027849738,0.00062114,0.00038399344,0.00048759166,0.0016318006],"category_scores_gemma":[0.00082196255,0.00015092158,0.0004265873,0.00038332195,0.00027317888,0.00045368276,0.00034720247,0.00035254462,0.00014939073],"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":[0.00025883812,0.00014463764,0.009288494,0.0003459738,0.00003196015,0.0006442078,0.00042293753,0.8183267,0.11555241,0.005875267,0.0017647044,0.047343917],"study_design_scores_gemma":[0.000018022536,0.0001292999,0.003578253,0.000019831712,0.000011856668,0.00014278002,0.000058002348,0.9574653,0.03590946,0.000816941,0.0018133697,0.000036874197],"about_ca_topic_score_codex":0.0015456834,"about_ca_topic_score_gemma":0.0007768676,"teacher_disagreement_score":0.0016318006,"about_ca_system_score_codex":0.00026788504,"about_ca_system_score_gemma":0.00044022023,"threshold_uncertainty_score":0.0054588914},"labels":[],"label_agreement":null},{"id":"W4244042811","doi":"10.32920/ryerson.14646417","title":"Comparison Of Solid Rocket Motor Thrust Modulation Technique","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Rocket and propulsion systems research","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":"Toronto Metropolitan University; Brandon University","funders":"","keywords":"Thrust; Propellant; Chamber pressure; Nozzle; Solid-fuel rocket; Aerospace engineering; Rocket engine nozzle; Combustion chamber; Rocket (weapon); Propulsion; Acceleration; Mechanical engineering; Materials science; Engineering; Physics; Mechanics; Combustion; Chemistry; Classical mechanics","score_opus":0.062052430989577856,"score_gpt":0.36641397738791487,"score_spread":0.304361546398337,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4244042811","genre_codex":"empirical","genre_gemma":"methods","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.87131447,0.0030612098,0.09568494,0.0001621299,0.0001219873,0.0001633244,0.00046993952,0.0012387328,0.027783321],"genre_scores_gemma":[0.9626997,0.00092112983,0.03154843,0.00002532857,0.000012355856,0.000041986616,0.00043941734,0.00011468309,0.0041970164],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996805,0.000025129742,0.000021670136,0.000046988316,0.000183672,0.000042003885],"domain_scores_gemma":[0.99967825,0.00008796521,0.00006426252,0.000055951426,0.00009570714,0.00001795393],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00029778012,0.0002474463,0.0003218708,0.00050613633,0.00018193344,0.0005026574,0.0005088974,0.00033813267,0.003218541],"category_scores_gemma":[0.0008140563,0.000106183346,0.00023076862,0.0006263192,0.00021106108,0.00058035913,0.00029719246,0.0002670407,0.0005585965],"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":[0.0029548968,0.00022072009,0.003884229,0.0010853154,0.000084162675,0.0002119988,0.00035898742,0.015713722,0.52924204,0.0061216955,0.0019536924,0.4381686],"study_design_scores_gemma":[0.00017047394,0.003603725,0.023535166,0.00012380582,0.00012200572,0.0011434273,0.00034791577,0.123238094,0.7915938,0.0015485672,0.054450247,0.00012273964],"about_ca_topic_score_codex":0.0006544558,"about_ca_topic_score_gemma":0.00075753435,"teacher_disagreement_score":0.003218541,"about_ca_system_score_codex":0.0002732122,"about_ca_system_score_gemma":0.00028536716,"threshold_uncertainty_score":0.010767043},"labels":[],"label_agreement":null},{"id":"W4244352068","doi":"10.32920/14638521","title":"Scale Effects on Solid Rocket Combustion Instability Behaviour","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Rocket and propulsion systems research","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":"Toronto Metropolitan University","funders":"","keywords":"Propellant; Solid-fuel rocket; Mechanics; Instability; Combustion; Transient (computer programming); Rocket (weapon); Internal flow; Aerospace engineering; Materials science; Internal pressure; Flow (mathematics); Physics; Engineering; Chemistry; Computer science; Composite material","score_opus":0.021492884541989544,"score_gpt":0.29078762646330364,"score_spread":0.2692947419213141,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4244352068","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":[0.99112856,0.00016910223,0.0065470086,0.000026974787,0.000007042964,0.000008612677,0.00004975168,0.00016454239,0.0018983143],"genre_scores_gemma":[0.99951255,0.00003488872,0.00025501716,0.0000024617552,0.0000011877711,0.0000017679132,0.000015852831,0.000014743848,0.00016158016],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999174,0.0000104189385,0.0000045176193,0.00001601962,0.000036765363,0.000014925052],"domain_scores_gemma":[0.99929357,0.0004258641,0.00012221363,0.00005325236,0.00007245712,0.000032680106],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012943962,0.0002078613,0.00016697201,0.00020549499,0.0001279745,0.00031044887,0.00012932118,0.00019110704,0.0013773574],"category_scores_gemma":[0.0016571379,0.00012096874,0.00016641,0.00011256389,0.00024344954,0.00033163032,0.0002672947,0.00018701065,0.00018855189],"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":[0.0008403111,0.000076605524,0.016779449,0.00018495512,0.000035004596,0.00070567476,0.00021289809,0.1253731,0.83494955,0.0009744196,0.00025227937,0.019615784],"study_design_scores_gemma":[0.000038786846,0.000876126,0.07644342,0.000017740713,0.000054474578,0.00036406046,0.00015536103,0.42978206,0.490453,0.00080137496,0.0009597068,0.00005392796],"about_ca_topic_score_codex":0.0008197008,"about_ca_topic_score_gemma":0.00072302646,"teacher_disagreement_score":0.0013773574,"about_ca_system_score_codex":0.00015297707,"about_ca_system_score_gemma":0.000104947,"threshold_uncertainty_score":0.0046076775},"labels":[],"label_agreement":null},{"id":"W4244957489","doi":"10.32920/ryerson.14635626.v1","title":"Performance Prediction Analysis for Aero-Naut CAM Folding Propellers and its Application into CREATeV Solar Aircraft","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Rocket and propulsion systems research","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":"Toronto Metropolitan University","funders":"","keywords":"Propeller; Folding (DSP implementation); Parametric statistics; Performance prediction; Marine engineering; Scaling; Work (physics); Engineering; Computer science; Aerospace engineering; Mechanical engineering; Simulation; Mathematics","score_opus":0.023632649936523552,"score_gpt":0.26355376353464544,"score_spread":0.23992111359812188,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4244957489","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":[0.56627834,0.00038692704,0.42327127,0.00020349216,0.000021645179,0.000051024737,0.00012909116,0.0007821316,0.008876178],"genre_scores_gemma":[0.98174435,0.00012369645,0.017165823,0.000008446428,0.0000055406713,0.000015553134,0.0000864506,0.000044238393,0.00080585666],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998186,0.000034034892,0.0000061793507,0.0000276342,0.00009530886,0.000018158571],"domain_scores_gemma":[0.9994081,0.00031602313,0.00007553256,0.000057671645,0.00013052762,0.000012035293],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00044725704,0.00047011202,0.00022718369,0.00037285534,0.00025687023,0.0003294145,0.0003526102,0.00028048013,0.00077420264],"category_scores_gemma":[0.0013400039,0.00012326744,0.00025832074,0.00025692853,0.0002248443,0.00033091026,0.00029748728,0.00043360007,0.00022607303],"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":[0.00016867297,0.000061393235,0.009569321,0.00009744695,0.000015530606,0.0001398568,0.0001303227,0.8305159,0.04186849,0.0016955354,0.00062013726,0.11511739],"study_design_scores_gemma":[0.0000018867187,0.000072703704,0.0025126254,0.000005908546,0.0000029677778,0.000029244082,0.000027655968,0.9794931,0.017283993,0.00016331367,0.00039865,0.000007938581],"about_ca_topic_score_codex":0.0031200158,"about_ca_topic_score_gemma":0.002385739,"teacher_disagreement_score":0.0031200158,"about_ca_system_score_codex":0.00028071448,"about_ca_system_score_gemma":0.00028198567,"threshold_uncertainty_score":0.006203711},"labels":[],"label_agreement":null},{"id":"W4245158397","doi":"10.32920/ryerson.14644173","title":"Hybrid Rocket Engine Research In Support Of Prototype Development &amp; Testing","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Rocket and propulsion systems research","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":true,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Nozzle; Specific impulse; Injector; Rocket engine; Propellant; Mechanical engineering; Propulsion; Thrust; Liquid-propellant rocket; Body orifice; Aerospace engineering; Automotive engineering; Engineering; Nuclear engineering","score_opus":0.2206247826410883,"score_gpt":0.3795355399261545,"score_spread":0.1589107572850662,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4245158397","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":[0.739976,0.0009102557,0.22233792,0.0003535719,0.00037848932,0.0026413454,0.002246389,0.005232813,0.025923245],"genre_scores_gemma":[0.791595,0.0009299267,0.16116028,0.00014190977,0.0000631363,0.0019960345,0.0025878046,0.0008965613,0.04062942],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99837756,0.00014749644,0.000082106424,0.00020792459,0.0010168096,0.00016815876],"domain_scores_gemma":[0.9987519,0.000150137,0.000070731316,0.00026703012,0.00064130913,0.00011892115],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0026238284,0.00060897256,0.00071909564,0.00081092305,0.00048144363,0.0011082196,0.0017535333,0.0007550583,0.0052231424],"category_scores_gemma":[0.0019032402,0.00030293787,0.0005374595,0.0005076327,0.0004437915,0.001259558,0.0007648275,0.00075388676,0.0023661137],"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":[0.0011782204,0.0011701601,0.0035700977,0.0011545009,0.00012022948,0.0011066034,0.0010413091,0.020489017,0.79454046,0.0054350235,0.0057278937,0.1644666],"study_design_scores_gemma":[0.0002521799,0.0075060925,0.005522211,0.00009283676,0.000073454634,0.0011112357,0.00027346003,0.02934431,0.89483476,0.0009933603,0.05989025,0.00010584894],"about_ca_topic_score_codex":0.0006991372,"about_ca_topic_score_gemma":0.000773148,"teacher_disagreement_score":0.0052231424,"about_ca_system_score_codex":0.0005586147,"about_ca_system_score_gemma":0.0006820802,"threshold_uncertainty_score":0.01747322},"labels":[],"label_agreement":null},{"id":"W4245454936","doi":"10.2514/6.2005-4161","title":"Structural Oscillation Considerations for Solid Rocket Internal Ballistics Modeling","year":2005,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Internal ballistics; Ballistics; Solid-fuel rocket; Rocket (weapon); Aerospace engineering; Oscillation (cell signaling); Aeronautics; Computer science; Engineering; Materials science; Propellant; Chemistry; Projectile","score_opus":0.07055856542496501,"score_gpt":0.3235139758683804,"score_spread":0.25295541044341535,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4245454936","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":[0.075768515,0.00026569923,0.8909033,0.00038914772,0.0000728172,0.000041484807,0.00006135907,0.00012125899,0.032376464],"genre_scores_gemma":[0.9542204,0.00044428481,0.03343069,0.00011517065,0.0000662579,0.00010431438,0.00008422554,0.00017016461,0.011364519],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998826,0.000028727789,0.00000486917,0.000016877826,0.000047304442,0.000019648409],"domain_scores_gemma":[0.9997825,0.00008481692,0.000034222143,0.000022666507,0.00005966546,0.000016092223],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00034129195,0.0004580528,0.00042809293,0.0005244029,0.0005213137,0.0007135913,0.00085596106,0.00095523713,0.0040287985],"category_scores_gemma":[0.0014366201,0.00037567614,0.00046729084,0.00032825893,0.00073472725,0.00091731345,0.0009657876,0.0006558898,0.0005698571],"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":[0.000036372025,0.000023347484,0.0006690653,0.00005224571,0.0000115145385,0.00015340556,0.00017296064,0.9027612,0.007761896,0.07097012,0.0006122778,0.016775573],"study_design_scores_gemma":[0.0000027158649,0.000010785994,0.00015413365,0.000005924837,0.0000026485689,0.000013769473,0.000020913543,0.99128973,0.00027229454,0.007601666,0.0006225568,0.0000028011034],"about_ca_topic_score_codex":0.0024831574,"about_ca_topic_score_gemma":0.0029037348,"teacher_disagreement_score":0.0040287985,"about_ca_system_score_codex":0.00034508936,"about_ca_system_score_gemma":0.0004122578,"threshold_uncertainty_score":0.013477683},"labels":[],"label_agreement":null},{"id":"W4246453896","doi":"10.32920/ryerson.14661933.v1","title":"Effects of Grain Geometry and Vibration on the Suppression of Combustion Instability in a Solid Rocket Motor","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Rocket and propulsion systems research","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":"Toronto Metropolitan University","funders":"","keywords":"Solid-fuel rocket; Propellant; Mechanics; Combustion; Instability; Vibration; Rocket (weapon); Materials science; Acceleration; Physics; Classical mechanics; Aerospace engineering; Acoustics; Engineering; Chemistry","score_opus":0.017164046543907727,"score_gpt":0.2692932166422137,"score_spread":0.25212917009830593,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4246453896","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":[0.99567825,0.000032576503,0.0034422711,0.0000093708995,0.0000026663263,0.000007050654,0.000021093856,0.00005075963,0.0007561356],"genre_scores_gemma":[0.99934083,0.000015013966,0.00056600303,0.0000014902078,3.0416462e-7,0.0000021516862,0.000009616299,0.0000035112369,0.00006093654],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999471,0.000009144687,0.0000030867573,0.000008569617,0.000018434957,0.000013616166],"domain_scores_gemma":[0.99979633,0.00010226958,0.000053544634,0.000016800816,0.000018269388,0.000012879028],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000113750706,0.00018273544,0.00021222545,0.00015333736,0.00014746186,0.00027086755,0.00020954697,0.00021539583,0.00054388656],"category_scores_gemma":[0.00058191083,0.00009083998,0.0001581018,0.0001537341,0.00027291544,0.00014925361,0.0001474831,0.00013669768,0.000048239166],"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":[0.00051673834,0.000097509735,0.0063455612,0.00007297099,0.000019357196,0.00020734439,0.00009128222,0.86857754,0.11449663,0.00067698216,0.00006933507,0.0088287415],"study_design_scores_gemma":[0.000033199467,0.0005292384,0.0062437896,0.0000053997237,0.000023944742,0.000042085136,0.000045058103,0.94628376,0.046480257,0.00012867444,0.0001718955,0.000012593827],"about_ca_topic_score_codex":0.0023652283,"about_ca_topic_score_gemma":0.0018684088,"teacher_disagreement_score":0.0023652283,"about_ca_system_score_codex":0.0002151118,"about_ca_system_score_gemma":0.0002185765,"threshold_uncertainty_score":0.0047029257},"labels":[],"label_agreement":null},{"id":"W4246558052","doi":"10.32920/ryerson.14637570.v1","title":"A computational study of soot formation and flame structure of coflow laminar methane/air diffusion flames under microgravity and normal gravity","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"University of Toronto; Government of Ontario; Compute Canada","keywords":"Soot; Diffusion flame; Laminar flow; Diffusion; Methane; Mechanics; Chemistry; Aerosol; Materials science; Combustion; Thermodynamics; Combustor; Physics; Physical chemistry; Organic chemistry","score_opus":0.015206880568088667,"score_gpt":0.264834750250446,"score_spread":0.24962786968235734,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4246558052","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":[0.99392974,0.000060990897,0.0035902073,0.00005197099,0.000010113562,0.000020033813,0.00019451845,0.00005733615,0.002085244],"genre_scores_gemma":[0.99482626,0.000047509562,0.0044387095,0.000009670784,0.000003295987,0.000017741111,0.0001452911,0.000013874904,0.00049761543],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99991393,0.000013122269,0.0000053908666,0.000019514495,0.000022131218,0.000025870806],"domain_scores_gemma":[0.9996549,0.00016641228,0.000072031544,0.000031039584,0.000038594597,0.000037035403],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00022492577,0.00052921154,0.00058243045,0.00039153552,0.0009012578,0.00064383046,0.0006321574,0.0010072639,0.00093832385],"category_scores_gemma":[0.0007594042,0.00025048797,0.0006234632,0.00038965474,0.0007105729,0.00037881915,0.00041803523,0.00035625228,0.000082151586],"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":[0.00026757678,0.00012116116,0.01089539,0.00010885133,0.000031633044,0.0003171988,0.00014935361,0.9648111,0.01920428,0.0009860191,0.00013227809,0.0029752026],"study_design_scores_gemma":[0.000022820062,0.000090644295,0.004788272,0.0000054620323,0.000009809153,0.00005382187,0.00007294095,0.9905195,0.004036023,0.00018278166,0.00020635573,0.00001149958],"about_ca_topic_score_codex":0.019615695,"about_ca_topic_score_gemma":0.0098971985,"teacher_disagreement_score":0.019615695,"about_ca_system_score_codex":0.0007736444,"about_ca_system_score_gemma":0.0009163552,"threshold_uncertainty_score":0.039003074},"labels":[],"label_agreement":null},{"id":"W4247073577","doi":"10.32920/14638521.v1","title":"Scale Effects on Solid Rocket Combustion Instability Behaviour","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Rocket and propulsion systems research","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":"Toronto Metropolitan University","funders":"","keywords":"Propellant; Solid-fuel rocket; Mechanics; Combustion; Instability; Transient (computer programming); Rocket (weapon); Internal flow; Aerospace engineering; Materials science; Internal pressure; Flow (mathematics); Physics; Engineering; Chemistry; Computer science; Composite material","score_opus":0.021492884541989544,"score_gpt":0.29078762646330364,"score_spread":0.2692947419213141,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4247073577","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":[0.99112856,0.00016910223,0.0065470086,0.000026974787,0.000007042964,0.000008612677,0.00004975168,0.00016454239,0.0018983143],"genre_scores_gemma":[0.99951255,0.00003488872,0.00025501716,0.0000024617552,0.0000011877711,0.0000017679132,0.000015852831,0.000014743848,0.00016158016],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999174,0.0000104189385,0.0000045176193,0.00001601962,0.000036765363,0.000014925052],"domain_scores_gemma":[0.99929357,0.0004258641,0.00012221363,0.00005325236,0.00007245712,0.000032680106],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012943962,0.0002078613,0.00016697201,0.00020549499,0.0001279745,0.00031044887,0.00012932118,0.00019110704,0.0013773574],"category_scores_gemma":[0.0016571379,0.00012096874,0.00016641,0.00011256389,0.00024344954,0.00033163032,0.0002672947,0.00018701065,0.00018855189],"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":[0.0008403111,0.000076605524,0.016779449,0.00018495512,0.000035004596,0.00070567476,0.00021289809,0.1253731,0.83494955,0.0009744196,0.00025227937,0.019615784],"study_design_scores_gemma":[0.000038786846,0.000876126,0.07644342,0.000017740713,0.000054474578,0.00036406046,0.00015536103,0.42978206,0.490453,0.00080137496,0.0009597068,0.00005392796],"about_ca_topic_score_codex":0.0008197008,"about_ca_topic_score_gemma":0.00072302646,"teacher_disagreement_score":0.0013773574,"about_ca_system_score_codex":0.00015297707,"about_ca_system_score_gemma":0.000104947,"threshold_uncertainty_score":0.0046076775},"labels":[],"label_agreement":null},{"id":"W4247217679","doi":"10.32920/14640180","title":"Numerical Evaluation of the Use of Aluminum Particles for Enhancing Solid Rocket Motor Combustion Stability","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Rocket and propulsion systems research","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":"Toronto Metropolitan University","funders":"","keywords":"Propellant; Solid-fuel rocket; Mechanics; Combustion; Rocket (weapon); Materials science; Internal flow; Transient (computer programming); Instability; Particle (ecology); Chamber pressure; Flow (mathematics); Internal pressure; Solid fuel; Aerospace engineering; Composite material; Physics; Chemistry; Engineering; Geology","score_opus":0.18679492589856944,"score_gpt":0.3491696619787813,"score_spread":0.16237473608021186,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4247217679","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":[0.97684526,0.00010474702,0.018627776,0.000040497966,0.000017310203,0.00003377255,0.00004410895,0.00011540108,0.004171133],"genre_scores_gemma":[0.99489874,0.000034993438,0.004610235,0.0000025377267,9.575111e-7,0.000006785689,0.000014891553,0.000006854973,0.00042409165],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99990153,0.000019217117,0.0000058498163,0.000009564268,0.000046638295,0.000017272174],"domain_scores_gemma":[0.99952996,0.00022138348,0.00008340606,0.000036693054,0.00010483496,0.000023765106],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00033060124,0.00027095148,0.00024281646,0.0002945814,0.00016858667,0.00038236738,0.00030089536,0.0003214522,0.0008870114],"category_scores_gemma":[0.0011143814,0.00008682152,0.0001604754,0.00020781651,0.00034247673,0.00017727967,0.0002374892,0.00015290853,0.00009981813],"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":[0.0007602545,0.00022058947,0.0052233394,0.00026494145,0.000026089996,0.000281951,0.0001649379,0.70753795,0.2555168,0.0027685724,0.00022998349,0.027004706],"study_design_scores_gemma":[0.00003245383,0.00051501795,0.0012311813,0.0000063616485,0.000013382316,0.000029010525,0.000040024293,0.90634185,0.09120756,0.00015642759,0.00041796538,0.000008778012],"about_ca_topic_score_codex":0.0016720694,"about_ca_topic_score_gemma":0.0014035606,"teacher_disagreement_score":0.0016720694,"about_ca_system_score_codex":0.00023896967,"about_ca_system_score_gemma":0.00026488738,"threshold_uncertainty_score":0.0033246875},"labels":[],"label_agreement":null},{"id":"W4247416352","doi":"10.32920/ryerson.14644173.v1","title":"Hybrid Rocket Engine Research In Support Of Prototype Development &amp; Testing","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Rocket and propulsion systems research","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":true,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Nozzle; Specific impulse; Injector; Rocket engine; Propellant; Mechanical engineering; Propulsion; Thrust; Liquid-propellant rocket; Aerospace engineering; Body orifice; Automotive engineering; Nuclear engineering; Engineering","score_opus":0.2206247826410883,"score_gpt":0.3795355399261545,"score_spread":0.1589107572850662,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4247416352","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":[0.739976,0.0009102557,0.22233792,0.0003535719,0.00037848932,0.0026413454,0.002246389,0.005232813,0.025923245],"genre_scores_gemma":[0.791595,0.0009299267,0.16116028,0.00014190977,0.0000631363,0.0019960345,0.0025878046,0.0008965613,0.04062942],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99837756,0.00014749644,0.000082106424,0.00020792459,0.0010168096,0.00016815876],"domain_scores_gemma":[0.9987519,0.000150137,0.000070731316,0.00026703012,0.00064130913,0.00011892115],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0026238284,0.00060897256,0.00071909564,0.00081092305,0.00048144363,0.0011082196,0.0017535333,0.0007550583,0.0052231424],"category_scores_gemma":[0.0019032402,0.00030293787,0.0005374595,0.0005076327,0.0004437915,0.001259558,0.0007648275,0.00075388676,0.0023661137],"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":[0.0011782204,0.0011701601,0.0035700977,0.0011545009,0.00012022948,0.0011066034,0.0010413091,0.020489017,0.79454046,0.0054350235,0.0057278937,0.1644666],"study_design_scores_gemma":[0.0002521799,0.0075060925,0.005522211,0.00009283676,0.000073454634,0.0011112357,0.00027346003,0.02934431,0.89483476,0.0009933603,0.05989025,0.00010584894],"about_ca_topic_score_codex":0.0006991372,"about_ca_topic_score_gemma":0.000773148,"teacher_disagreement_score":0.0052231424,"about_ca_system_score_codex":0.0005586147,"about_ca_system_score_gemma":0.0006820802,"threshold_uncertainty_score":0.01747322},"labels":[],"label_agreement":null},{"id":"W4247620275","doi":"10.22215/etd/2008-07845","title":"Experimental and numerical investigation of centrifugal compressors for use with alternative working fluids","year":2008,"lang":"en","type":"dissertation","venue":"","topic":"Rocket and propulsion systems research","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":"Canadian Heritage; Library and Archives Canada","funders":"","keywords":"Centrifugal compressor; Gas compressor; Engineering; Mechanical engineering; Computer science","score_opus":0.04846872932321165,"score_gpt":0.29498989581860224,"score_spread":0.2465211664953906,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4247620275","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":[0.9952867,0.00027257137,0.0015344735,0.00010052215,0.000023984298,0.000049917257,0.00037653017,0.00007704118,0.0022781575],"genre_scores_gemma":[0.9950765,0.00024525152,0.0022440136,0.0000140010025,0.000009710705,0.000042423515,0.0002574738,0.000024451901,0.0020861654],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996044,0.00006283824,0.000028528819,0.000050711027,0.00019709907,0.000056458302],"domain_scores_gemma":[0.9982692,0.00059715507,0.00013234654,0.00018832281,0.00073277816,0.00008011256],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0007306896,0.00041465275,0.00043027912,0.0005542115,0.0012987123,0.00060359086,0.00064574985,0.0006044483,0.0038435243],"category_scores_gemma":[0.0024752826,0.00025826064,0.0002503452,0.00088498864,0.0007604234,0.0009586754,0.0003113437,0.0005893445,0.00044491104],"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":[0.0031706651,0.0014678612,0.007765957,0.00068917056,0.000039978804,0.00022912277,0.00093645614,0.010801935,0.93047714,0.0015947288,0.0019993244,0.040827643],"study_design_scores_gemma":[0.00013126431,0.0031332113,0.016782314,0.000028952552,0.00003973928,0.00012508188,0.0005933527,0.030432928,0.94440186,0.00017668126,0.0040986515,0.000055959816],"about_ca_topic_score_codex":0.005519462,"about_ca_topic_score_gemma":0.0061539053,"teacher_disagreement_score":0.005519462,"about_ca_system_score_codex":0.00058380794,"about_ca_system_score_gemma":0.0005226613,"threshold_uncertainty_score":0.012857854},"labels":[],"label_agreement":null},{"id":"W4248777831","doi":"10.32920/ryerson.14665281","title":"Fuel regression rate estimation model for swirling-flow hybrid rocket engines","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Rocket and propulsion systems research","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":"Toronto Metropolitan University","funders":"","keywords":"Mechanics; Propellant; Mass flow rate; Rocket (weapon); Volumetric flow rate; Flow (mathematics); Engineering; Physics; Aerospace engineering","score_opus":0.046412795127424904,"score_gpt":0.30515396186466287,"score_spread":0.25874116673723796,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4248777831","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":[0.05719064,0.00038891283,0.9385162,0.00005921546,0.000023537148,0.00007122266,0.00015363628,0.00061482296,0.0029818881],"genre_scores_gemma":[0.9639145,0.00049255573,0.026761398,0.000033819444,0.00002228615,0.00018207417,0.00030811536,0.000104201325,0.008181029],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99975234,0.000041536838,0.000014024626,0.00008050436,0.00007578736,0.000035780842],"domain_scores_gemma":[0.99947566,0.00024303995,0.00012207303,0.000020347641,0.00012751766,0.000011413317],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00074429385,0.000839982,0.0010258006,0.00059307023,0.00023747967,0.0010166807,0.0015232197,0.00102006,0.001440475],"category_scores_gemma":[0.0014416476,0.00038524208,0.0007957121,0.00039700337,0.00032566613,0.00094420824,0.00042829293,0.0008079623,0.0005115487],"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":[0.000039949424,0.000013712383,0.00041292212,0.000035919198,0.000015200577,0.00004479033,0.000021212041,0.98972404,0.002501895,0.0012511717,0.00007623649,0.00586295],"study_design_scores_gemma":[0.0000010378475,0.00000611913,0.0000671316,0.0000015572435,0.00000276144,0.000005537734,0.0000016917347,0.99916565,0.00050471997,0.00015681435,0.0000845346,0.0000025112595],"about_ca_topic_score_codex":0.007357888,"about_ca_topic_score_gemma":0.0029267194,"teacher_disagreement_score":0.007357888,"about_ca_system_score_codex":0.0006897884,"about_ca_system_score_gemma":0.0006041218,"threshold_uncertainty_score":0.014630139},"labels":[],"label_agreement":null},{"id":"W4249480886","doi":"10.32920/ryerson.14665281.v1","title":"Fuel regression rate estimation model for swirling-flow hybrid rocket engines","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Rocket and propulsion systems research","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":"Toronto Metropolitan University","funders":"","keywords":"Mechanics; Propellant; Mass flow rate; Rocket (weapon); Volumetric flow rate; Flow (mathematics); Engineering; Physics; Aerospace engineering","score_opus":0.046412795127424904,"score_gpt":0.30515396186466287,"score_spread":0.25874116673723796,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4249480886","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":[0.05719064,0.00038891283,0.9385162,0.00005921546,0.000023537148,0.00007122266,0.00015363628,0.00061482296,0.0029818881],"genre_scores_gemma":[0.9639145,0.00049255573,0.026761398,0.000033819444,0.00002228615,0.00018207417,0.00030811536,0.000104201325,0.008181029],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99975234,0.000041536838,0.000014024626,0.00008050436,0.00007578736,0.000035780842],"domain_scores_gemma":[0.99947566,0.00024303995,0.00012207303,0.000020347641,0.00012751766,0.000011413317],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00074429385,0.000839982,0.0010258006,0.00059307023,0.00023747967,0.0010166807,0.0015232197,0.00102006,0.001440475],"category_scores_gemma":[0.0014416476,0.00038524208,0.0007957121,0.00039700337,0.00032566613,0.00094420824,0.00042829293,0.0008079623,0.0005115487],"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":[0.000039949424,0.000013712383,0.00041292212,0.000035919198,0.000015200577,0.00004479033,0.000021212041,0.98972404,0.002501895,0.0012511717,0.00007623649,0.00586295],"study_design_scores_gemma":[0.0000010378475,0.00000611913,0.0000671316,0.0000015572435,0.00000276144,0.000005537734,0.0000016917347,0.99916565,0.00050471997,0.00015681435,0.0000845346,0.0000025112595],"about_ca_topic_score_codex":0.007357888,"about_ca_topic_score_gemma":0.0029267194,"teacher_disagreement_score":0.007357888,"about_ca_system_score_codex":0.0006897884,"about_ca_system_score_gemma":0.0006041218,"threshold_uncertainty_score":0.014630139},"labels":[],"label_agreement":null},{"id":"W4249827837","doi":"10.32920/ryerson.14661933","title":"Effects of Grain Geometry and Vibration on the Suppression of Combustion Instability in a Solid Rocket Motor","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Rocket and propulsion systems research","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":"Toronto Metropolitan University","funders":"","keywords":"Solid-fuel rocket; Propellant; Mechanics; Instability; Combustion; Vibration; Rocket (weapon); Materials science; Acceleration; Physics; Classical mechanics; Acoustics; Aerospace engineering; Engineering; Chemistry","score_opus":0.017164046543907727,"score_gpt":0.2692932166422137,"score_spread":0.25212917009830593,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4249827837","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":[0.99567825,0.000032576503,0.0034422711,0.0000093708995,0.0000026663263,0.000007050654,0.000021093856,0.00005075963,0.0007561356],"genre_scores_gemma":[0.99934083,0.000015013966,0.00056600303,0.0000014902078,3.0416462e-7,0.0000021516862,0.000009616299,0.0000035112369,0.00006093654],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999471,0.000009144687,0.0000030867573,0.000008569617,0.000018434957,0.000013616166],"domain_scores_gemma":[0.99979633,0.00010226958,0.000053544634,0.000016800816,0.000018269388,0.000012879028],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000113750706,0.00018273544,0.00021222545,0.00015333736,0.00014746186,0.00027086755,0.00020954697,0.00021539583,0.00054388656],"category_scores_gemma":[0.00058191083,0.00009083998,0.0001581018,0.0001537341,0.00027291544,0.00014925361,0.0001474831,0.00013669768,0.000048239166],"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":[0.00051673834,0.000097509735,0.0063455612,0.00007297099,0.000019357196,0.00020734439,0.00009128222,0.86857754,0.11449663,0.00067698216,0.00006933507,0.0088287415],"study_design_scores_gemma":[0.000033199467,0.0005292384,0.0062437896,0.0000053997237,0.000023944742,0.000042085136,0.000045058103,0.94628376,0.046480257,0.00012867444,0.0001718955,0.000012593827],"about_ca_topic_score_codex":0.0023652283,"about_ca_topic_score_gemma":0.0018684088,"teacher_disagreement_score":0.0023652283,"about_ca_system_score_codex":0.0002151118,"about_ca_system_score_gemma":0.0002185765,"threshold_uncertainty_score":0.0047029257},"labels":[],"label_agreement":null},{"id":"W4251186870","doi":"10.32920/ryerson.14648736.v1","title":"A Mathematical Method for Predicting the Design Performance of Single and Multi-stage Rockets","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Rocket and propulsion systems research","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":"Toronto Metropolitan University","funders":"","keywords":"Integrator; Range (aeronautics); Set (abstract data type); Computer science; Multi stage; Rocket (weapon); Baseline (sea); Ordinary differential equation; Nonlinear system; Tandem; Aerospace engineering; Path (computing); Stage (stratigraphy); Simulation; Control theory (sociology); Mathematical optimization; Mathematics; Industrial engineering; Differential equation; Engineering; Artificial intelligence; Mathematical analysis; Control (management); Physics; Telecommunications","score_opus":0.16171363570023883,"score_gpt":0.3602922802790922,"score_spread":0.19857864457885338,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4251186870","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":[0.0021652386,0.00012670018,0.9943135,0.000047622212,0.000035089273,0.000025721147,0.00005773124,0.00019215193,0.0030363072],"genre_scores_gemma":[0.27577922,0.0012635177,0.69490504,0.00014198195,0.00013888167,0.00059282745,0.00042292723,0.0005780551,0.026177648],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99956506,0.00007501203,0.000019925763,0.00006910472,0.00023804378,0.000032817334],"domain_scores_gemma":[0.9991067,0.0004880174,0.00009492661,0.00007828163,0.00020763755,0.000024470524],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00093149167,0.00092096976,0.0006260077,0.000961653,0.00041053985,0.0008252005,0.0012693155,0.0010493002,0.004510058],"category_scores_gemma":[0.0032769064,0.0004910319,0.0010185125,0.00078543235,0.0007034457,0.0013125938,0.00072974846,0.0013999942,0.0014919911],"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":[0.000014464292,0.000025421503,0.0003775207,0.00010615825,0.000015153215,0.00003962084,0.000037574093,0.9313037,0.005189722,0.028248582,0.0012026337,0.03343947],"study_design_scores_gemma":[0.000003065411,0.000012453016,0.000071510316,0.000009207567,0.0000044791536,0.000013154222,0.0000040437276,0.9930178,0.00096519105,0.0041456525,0.0017475527,0.0000059698386],"about_ca_topic_score_codex":0.0029216865,"about_ca_topic_score_gemma":0.0020078218,"teacher_disagreement_score":0.004510058,"about_ca_system_score_codex":0.000692161,"about_ca_system_score_gemma":0.0012409065,"threshold_uncertainty_score":0.0150876045},"labels":[],"label_agreement":null},{"id":"W4251810595","doi":"10.32920/ryerson.14644389","title":"Cold flow testing of laboratory-scale hybrid rocket engine test apparatus","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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":"Rocket engine; Thrust; Nozzle; Rocket (weapon); Mechanics; Transient (computer programming); Engineering; Aerospace engineering; Flow (mathematics); Physics; Computer science","score_opus":0.02280089114510181,"score_gpt":0.2494623795760936,"score_spread":0.2266614884309918,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4251810595","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":[0.99037313,0.00006960034,0.008241739,0.000021885877,0.000020847234,0.00013800098,0.00032653692,0.0002290087,0.000579057],"genre_scores_gemma":[0.9924384,0.00006594119,0.0053675883,0.00003093016,0.000011703435,0.00019900782,0.0004612494,0.00004615807,0.0013791352],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99938333,0.0000849613,0.000048949765,0.00014571394,0.00024237082,0.00009470943],"domain_scores_gemma":[0.9988827,0.0003019049,0.00014460464,0.00014089377,0.00043505328,0.000094865056],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00080008054,0.00060064316,0.0004825336,0.000659165,0.00053460215,0.00040326754,0.001086555,0.00067497516,0.0021596404],"category_scores_gemma":[0.001540917,0.00015834333,0.0003658501,0.00030015697,0.00048979477,0.0004992768,0.0005571295,0.0005091774,0.0005236002],"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":[0.0007632304,0.00036636333,0.004224184,0.00013975127,0.000019383668,0.00028075348,0.00024627568,0.0020955363,0.98387724,0.00018501785,0.00021600269,0.0075863795],"study_design_scores_gemma":[0.000076197604,0.004287571,0.018242251,0.000019185356,0.00003237753,0.00018029395,0.00021008839,0.0051314333,0.97070146,0.000049942075,0.0010328334,0.00003639248],"about_ca_topic_score_codex":0.001660426,"about_ca_topic_score_gemma":0.002397398,"teacher_disagreement_score":0.0021596404,"about_ca_system_score_codex":0.00046860785,"about_ca_system_score_gemma":0.00022054768,"threshold_uncertainty_score":0.0072247386},"labels":[],"label_agreement":null},{"id":"W4251940391","doi":"10.32920/ryerson.14663421","title":"Scale effects on hybrid rocket engine performance","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Rocket and propulsion systems research","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":"Toronto Metropolitan University","funders":"","keywords":"Rocket engine; Thrust; Scaling; Aerospace engineering; Rocket (weapon); Scale (ratio); Computer science; Automotive engineering; Environmental science; Mechanics; Simulation; Engineering; Physics; Mathematics; Geometry","score_opus":0.011980333832804757,"score_gpt":0.2355775550800085,"score_spread":0.22359722124720374,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4251940391","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":[0.9895355,0.0006178518,0.0043436717,0.000048303795,0.000047719783,0.000029284382,0.00017137878,0.0004269372,0.0047792587],"genre_scores_gemma":[0.99745756,0.00016553896,0.0010627235,0.000021167536,0.000010147988,0.000011761828,0.00016581595,0.00005038177,0.0010549229],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996736,0.0000213937,0.000020714473,0.00007767346,0.0001601644,0.000046417717],"domain_scores_gemma":[0.99929845,0.00022045668,0.0001187621,0.00012249919,0.00018345985,0.000056365287],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00037637982,0.0004675756,0.00040665662,0.0003541923,0.00020359579,0.00064268155,0.00043948332,0.00040571977,0.0033270766],"category_scores_gemma":[0.001291329,0.00017546762,0.0003112861,0.00031451142,0.00022568538,0.00085357454,0.00067648955,0.00038775403,0.0008733939],"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":[0.0029619243,0.0006946371,0.025010811,0.00054765353,0.00016548166,0.0013144236,0.0002677199,0.082907274,0.768816,0.0008905446,0.0010188842,0.11540465],"study_design_scores_gemma":[0.000099781224,0.0073165786,0.09684036,0.000041881198,0.00017370038,0.00063892966,0.00030935422,0.05939646,0.8265201,0.00055990805,0.007980001,0.00012284823],"about_ca_topic_score_codex":0.00037681044,"about_ca_topic_score_gemma":0.00042003955,"teacher_disagreement_score":0.0033270766,"about_ca_system_score_codex":0.00015753237,"about_ca_system_score_gemma":0.00009136444,"threshold_uncertainty_score":0.011130154},"labels":[{"model":"gemma","categories":[],"domain":null,"study_design":"bench_or_experimental","genre":"empirical","about_ca_system":false,"about_ca_topic":false,"confidence":"low"},{"model":"gpt","categories":[],"domain":null,"study_design":"design_other","genre":"empirical","about_ca_system":false,"about_ca_topic":false,"confidence":"low"}],"label_agreement":"split"},{"id":"W4253687033","doi":"10.31399/asm.hb.v21.a0003475","title":"Space Applications","year":2001,"lang":"en","type":"book-chapter","venue":"Composites","topic":"Rocket and propulsion systems research","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":"Lockheed Martin (Canada)","funders":"","keywords":"Payload (computing); Spacecraft; Aerospace engineering; Spacecraft design; Advanced composite materials; Key (lock); Systems engineering; Engineering; Rocket (weapon); Aeronautics; Computer science; Composite number; Mechanical engineering; Computer security","score_opus":0.024171720620000166,"score_gpt":0.25249186005527025,"score_spread":0.22832013943527008,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4253687033","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0024249386,0.0059471293,0.005435442,0.0013216126,0.001801461,0.00010326782,0.0013557791,0.001344893,0.98026544],"genre_scores_gemma":[0.009375977,0.003825037,0.002410474,0.00073822174,0.00029094768,0.00005637971,0.0018900649,0.00019681605,0.98121613],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.9996954,0.000024554556,0.000010713495,0.000049799834,0.00017896928,0.000040549967],"domain_scores_gemma":[0.9997328,0.000025581987,0.000012721694,0.000040628514,0.00014361003,0.00004463672],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00026363842,0.00093285507,0.0003260588,0.0011941065,0.001119383,0.0018508583,0.0008689269,0.001135052,0.31384444],"category_scores_gemma":[0.00043092828,0.0001964387,0.00043346887,0.0010699217,0.00023290057,0.0011915307,0.0016219482,0.00079867477,0.18640281],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0000702565,0.00008979252,0.00035099286,0.0005365657,0.0000071297536,0.00038985352,0.00017169997,0.0006649792,0.008286556,0.022172825,0.52601486,0.4412445],"study_design_scores_gemma":[0.0000028112593,0.000015725202,0.00011170278,0.00003983626,0.0000015373216,0.00016195209,0.000021818314,0.00009113377,0.0009033523,0.0011291931,0.9975184,0.0000026629393],"about_ca_topic_score_codex":0.0011357907,"about_ca_topic_score_gemma":0.0023350827,"teacher_disagreement_score":0.31384444,"about_ca_system_score_codex":0.00064498134,"about_ca_system_score_gemma":0.0006429232,"threshold_uncertainty_score":0.9787176},"labels":[],"label_agreement":null},{"id":"W4253926358","doi":"10.32920/14640078.v1","title":"Scale Effects on Quasi-Steady Solid Rocket Internal Ballistic Behaviour","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Rocket and propulsion systems research","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":"Toronto Metropolitan University","funders":"","keywords":"Internal ballistics; Propellant; Ballistics; Solid-fuel rocket; Deflection (physics); Aerospace engineering; Engineering; Mechanics; Simulation; Mechanical engineering; Materials science; Physics; Classical mechanics","score_opus":0.021085191961269737,"score_gpt":0.29954177069246163,"score_spread":0.2784565787311919,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4253926358","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":[0.98081744,0.00015895734,0.013714485,0.00003152981,0.000009608138,0.000014764805,0.000065222455,0.0002694963,0.0049185995],"genre_scores_gemma":[0.99923253,0.000031363,0.00045554191,0.000002338362,6.7797976e-7,0.0000025836107,0.000018277135,0.000021194124,0.00023532078],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998419,0.000019882074,0.000007792282,0.000026037345,0.00007382107,0.000030623018],"domain_scores_gemma":[0.99927336,0.00040167588,0.000090661866,0.00011535353,0.00008975735,0.00002931647],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025750633,0.00026059433,0.00020880882,0.00018556321,0.00017749837,0.0003398831,0.00023012528,0.00020405094,0.0018552161],"category_scores_gemma":[0.0018972143,0.0001678242,0.00025991246,0.00013178185,0.0005454978,0.0003717471,0.00041389253,0.00027704582,0.00027999736],"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":[0.0007309007,0.00010956654,0.016620968,0.00025044294,0.0000456608,0.00060565287,0.00041664435,0.5788279,0.36732104,0.0027909377,0.00033673094,0.03194355],"study_design_scores_gemma":[0.000027328555,0.0007703686,0.046220418,0.000023787183,0.000035769182,0.00021264824,0.0001742655,0.71926916,0.23119423,0.0009946821,0.0010319878,0.00004540311],"about_ca_topic_score_codex":0.0011623972,"about_ca_topic_score_gemma":0.0011666034,"teacher_disagreement_score":0.0018552161,"about_ca_system_score_codex":0.0002635781,"about_ca_system_score_gemma":0.00014650391,"threshold_uncertainty_score":0.0062063336},"labels":[],"label_agreement":null},{"id":"W4255016312","doi":"10.32920/ryerson.14663421.v1","title":"Scale effects on hybrid rocket engine performance","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Rocket and propulsion systems research","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":"Toronto Metropolitan University","funders":"","keywords":"Rocket engine; Thrust; Scaling; Aerospace engineering; Rocket (weapon); Scale (ratio); Computer science; Automotive engineering; Environmental science; Mechanics; Simulation; Engineering; Physics; Mathematics; Geometry","score_opus":0.011980333832804757,"score_gpt":0.2355775550800085,"score_spread":0.22359722124720374,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4255016312","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":[0.9895355,0.0006178518,0.0043436717,0.000048303795,0.000047719783,0.000029284382,0.00017137878,0.0004269372,0.0047792587],"genre_scores_gemma":[0.99745756,0.00016553896,0.0010627235,0.000021167536,0.000010147988,0.000011761828,0.00016581595,0.00005038177,0.0010549229],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996736,0.0000213937,0.000020714473,0.00007767346,0.0001601644,0.000046417717],"domain_scores_gemma":[0.99929845,0.00022045668,0.0001187621,0.00012249919,0.00018345985,0.000056365287],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00037637982,0.0004675756,0.00040665662,0.0003541923,0.00020359579,0.00064268155,0.00043948332,0.00040571977,0.0033270766],"category_scores_gemma":[0.001291329,0.00017546762,0.0003112861,0.00031451142,0.00022568538,0.00085357454,0.00067648955,0.00038775403,0.0008733939],"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":[0.0029619243,0.0006946371,0.025010811,0.00054765353,0.00016548166,0.0013144236,0.0002677199,0.082907274,0.768816,0.0008905446,0.0010188842,0.11540465],"study_design_scores_gemma":[0.000099781224,0.0073165786,0.09684036,0.000041881198,0.00017370038,0.00063892966,0.00030935422,0.05939646,0.8265201,0.00055990805,0.007980001,0.00012284823],"about_ca_topic_score_codex":0.00037681044,"about_ca_topic_score_gemma":0.00042003955,"teacher_disagreement_score":0.0033270766,"about_ca_system_score_codex":0.00015753237,"about_ca_system_score_gemma":0.00009136444,"threshold_uncertainty_score":0.011130154},"labels":[],"label_agreement":null},{"id":"W4255180489","doi":"10.32920/ryerson.14635701","title":"Design and Analysis of a Rocket-Deployed Flying-Wing UAV","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Rocket and propulsion systems research","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":true,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Payload (computing); Wingspan; Aerospace engineering; Takeoff; Wing; Wing loading; Rocket (weapon); Flight control surfaces; Engineering; Aerodynamics; Airfoil; Power (physics); Volume (thermodynamics); Automotive engineering; Aeronautics; Marine engineering; Angle of attack; Computer science","score_opus":0.0537705095298602,"score_gpt":0.2919828896700315,"score_spread":0.2382123801401713,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4255180489","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":[0.57270014,0.0004582358,0.39215687,0.0002070128,0.0000881891,0.00038181402,0.0003327176,0.00091812544,0.03275677],"genre_scores_gemma":[0.94999427,0.00018291351,0.042482752,0.000026457781,0.0000070916567,0.00013149146,0.00012302304,0.000047851045,0.007004126],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998517,0.00001793172,0.0000051943466,0.0000257085,0.000073079646,0.000026280735],"domain_scores_gemma":[0.9998834,0.000030652107,0.000025929643,0.000012617757,0.00003568384,0.000011698333],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017531459,0.00036525124,0.0003317755,0.00029414496,0.00034825547,0.0006039934,0.00042637065,0.00048643482,0.0024545442],"category_scores_gemma":[0.0002961883,0.00018786207,0.00040032036,0.00011104406,0.0002734608,0.00021219814,0.00026312965,0.00022059101,0.00040781195],"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":[0.00024106726,0.00006866839,0.0020792766,0.00037586005,0.000043010903,0.00091098476,0.0001774585,0.80042225,0.15764771,0.0035677773,0.0006212148,0.033844717],"study_design_scores_gemma":[0.00005139558,0.001053106,0.002661925,0.0000301712,0.000045137098,0.00023676938,0.00014260452,0.9416367,0.04611578,0.00076880556,0.0072349105,0.000022710066],"about_ca_topic_score_codex":0.0025805777,"about_ca_topic_score_gemma":0.0015937771,"teacher_disagreement_score":0.0025805777,"about_ca_system_score_codex":0.00050166226,"about_ca_system_score_gemma":0.0005477494,"threshold_uncertainty_score":0.008211255},"labels":[],"label_agreement":null},{"id":"W4280539535","doi":"10.1016/j.ast.2022.107637","title":"Ejector mode performance improvement of rocket-based combined cycle engine designed for dual-ramjet mode","year":2022,"lang":"en","type":"article","venue":"Aerospace Science and Technology","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":9,"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 Calgary","funders":"National Natural Science Foundation of China","keywords":"Ramjet; Aerospace engineering; Rocket (weapon); Mechanics; Supersonic speed; Nozzle; Entrainment (biomusicology); Engineering; Automotive engineering; Materials science; Combustion; Physics; Combustor; Chemistry","score_opus":0.009463199488203431,"score_gpt":0.2515093823808216,"score_spread":0.24204618289261817,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4280539535","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":[0.9777654,0.0004859831,0.014991835,0.000054013184,0.00006746943,0.000025563853,0.00013581762,0.0005117273,0.0059621655],"genre_scores_gemma":[0.9930363,0.00012739848,0.0015877022,0.00002212085,0.000009675891,0.000013705224,0.00018597138,0.00004495163,0.004972016],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997919,0.00001570599,0.000008691606,0.00004260285,0.00011004938,0.00003113546],"domain_scores_gemma":[0.9997451,0.00004226498,0.000030569165,0.00002163841,0.00013746112,0.0000231419],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025623426,0.0005351571,0.00052777363,0.0003983156,0.00032270805,0.00039893558,0.0007739227,0.0004999578,0.0029938093],"category_scores_gemma":[0.00019283642,0.00017453652,0.0003827242,0.00021902734,0.00016809469,0.00042568205,0.00030468474,0.00033261636,0.00076802465],"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":[0.0028040493,0.00018590875,0.0038473918,0.0003042198,0.000084000465,0.00024562713,0.00014681368,0.007306552,0.9479078,0.00043228027,0.0009995095,0.035735913],"study_design_scores_gemma":[0.00017486415,0.004667262,0.04802933,0.000046065317,0.0002006905,0.00047252016,0.00017817874,0.08502971,0.854172,0.00015588364,0.0067764744,0.00009707831],"about_ca_topic_score_codex":0.0007665864,"about_ca_topic_score_gemma":0.0012031564,"teacher_disagreement_score":0.0029938093,"about_ca_system_score_codex":0.00018340994,"about_ca_system_score_gemma":0.00024481775,"threshold_uncertainty_score":0.010015309},"labels":[],"label_agreement":null},{"id":"W4281608606","doi":"10.13111/2066-8201.2022.14.2.13","title":"Wernher Von Braun’s Pioneering Work in Modelling and Testing Liquid-Propellant Rockets","year":2022,"lang":"en","type":"article","venue":"INCAS BULLETIN","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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; Aerospace engineering; Rocket engine nozzle; Rocket (weapon); Liquid-propellant rocket; Nozzle; Rocket engine; Chamber pressure; Aeronautics; Engineering; Mechanical engineering; Combustion chamber; Solid-fuel rocket; Combustion; Work (physics); Mechanics; Physics; Chemistry","score_opus":0.03821091244024406,"score_gpt":0.2268218592601129,"score_spread":0.18861094681986884,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4281608606","genre_codex":"methods","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"other","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.030723436,0.006393385,0.9409614,0.0012031716,0.000611892,0.00012930385,0.00027179363,0.0005450898,0.01916056],"genre_scores_gemma":[0.62408274,0.01904139,0.3125198,0.00055684726,0.00042714225,0.0003922712,0.0007393974,0.0006334563,0.041607015],"study_design_codex":"simulation_or_modeling","study_design_gemma":"not_applicable","domain_scores_codex":[0.9982839,0.000338217,0.000093763796,0.00038809626,0.0007665261,0.00012940774],"domain_scores_gemma":[0.9989221,0.00052508473,0.0000664497,0.00013085254,0.00030746547,0.00004808207],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0016780307,0.0013306064,0.00090348086,0.0014778452,0.0006663326,0.0021726452,0.0011481936,0.0019852908,0.0016235582],"category_scores_gemma":[0.003244,0.00087764766,0.0014833898,0.0008637029,0.0018398874,0.0035583375,0.0016486188,0.0022582416,0.0011285497],"study_design_candidate":"not_applicable","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":[0.00023865054,0.00014539603,0.0028262509,0.0007716952,0.00011130191,0.0005698801,0.0008160794,0.4344963,0.08546151,0.28046063,0.005400518,0.1887018],"study_design_scores_gemma":[0.000053725817,0.0009656994,0.0014268861,0.00048853137,0.0001139858,0.0010383187,0.0002457765,0.42751044,0.20404096,0.1413308,0.22243321,0.00035168944],"about_ca_topic_score_codex":0.003040745,"about_ca_topic_score_gemma":0.001206272,"teacher_disagreement_score":0.003040745,"about_ca_system_score_codex":0.0012993185,"about_ca_system_score_gemma":0.0012071542,"threshold_uncertainty_score":0.009427309},"labels":[],"label_agreement":null},{"id":"W4283170067","doi":"10.1142/9781800610996_0002","title":"Laval Nozzles: Design, Characterization, and Applications","year":2022,"lang":"en","type":"book-chapter","venue":"WORLD SCIENTIFIC (EUROPE) eBooks","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":"Characterization (materials science); Materials science; Nanotechnology","score_opus":0.03421536615372337,"score_gpt":0.23302098419990197,"score_spread":0.1988056180461786,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4283170067","genre_codex":"methods","genre_gemma":"methods","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.18040214,0.18389994,0.50076854,0.0032169002,0.0019358963,0.0011091523,0.0024147297,0.004815809,0.12143695],"genre_scores_gemma":[0.59641135,0.052066095,0.17258085,0.000911888,0.0004632776,0.00041519382,0.0024450282,0.00080887706,0.17389746],"study_design_codex":"bench_or_experimental","study_design_gemma":"not_applicable","domain_scores_codex":[0.9990466,0.00004666192,0.000031705888,0.00013421131,0.0006821672,0.000058642534],"domain_scores_gemma":[0.9994723,0.00013206188,0.00007340326,0.00003944988,0.00024011488,0.000042763342],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0010579026,0.00045435925,0.0006607468,0.0007941656,0.0006186265,0.0033963865,0.0014144179,0.0012758437,0.004904845],"category_scores_gemma":[0.0014338141,0.0004128534,0.000478001,0.00096054777,0.00070423115,0.0025352102,0.0008825138,0.00095286826,0.0015504756],"study_design_candidate":"not_applicable","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":[0.00034658992,0.00015266887,0.0034793003,0.0016094435,0.0000351941,0.0003898703,0.0007245615,0.0050221514,0.5452103,0.015920008,0.019716809,0.40739307],"study_design_scores_gemma":[0.000077655444,0.0012880552,0.009306373,0.00027694408,0.00008220797,0.0021178483,0.00043833483,0.02020576,0.48052466,0.0035153108,0.48201555,0.00015120865],"about_ca_topic_score_codex":0.0011257146,"about_ca_topic_score_gemma":0.0017277005,"teacher_disagreement_score":0.004904845,"about_ca_system_score_codex":0.0012446198,"about_ca_system_score_gemma":0.0008214183,"threshold_uncertainty_score":0.016408324},"labels":[],"label_agreement":null},{"id":"W4283208570","doi":"10.2514/6.2022-3781","title":"Development of a facility to test an ejector ramjet at static conditions","year":2022,"lang":"en","type":"article","venue":"AIAA AVIATION 2022 Forum","topic":"Rocket and propulsion systems research","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":"University of Calgary","funders":"","keywords":"Ramjet; Injector; Ignition system; Automotive engineering; Aerospace engineering; Propulsion; Specific impulse; Thrust; Bandwidth throttling; Engineering; Nuclear engineering; Combustion; Combustor; Environmental science; Mechanical engineering","score_opus":0.023008536327035714,"score_gpt":0.28151691802947465,"score_spread":0.25850838170243895,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4283208570","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":[0.53981256,0.00040839677,0.39169598,0.00046018945,0.0011633642,0.007090641,0.0063921665,0.031986784,0.020989873],"genre_scores_gemma":[0.52160394,0.0003297949,0.44163364,0.0003772426,0.00010856352,0.006299516,0.006560416,0.0019261154,0.021160806],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99899,0.000042636853,0.00005184273,0.00015668695,0.0005971886,0.0001616],"domain_scores_gemma":[0.99838114,0.00024210653,0.00014585812,0.0003983326,0.0006078645,0.00022471798],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0018629673,0.0008614545,0.0007756907,0.0010737746,0.0010854654,0.00081407337,0.0023934655,0.0014800085,0.01417268],"category_scores_gemma":[0.0015153361,0.0008491255,0.00072545913,0.00042404782,0.00060314377,0.0013355915,0.0012330395,0.0016791624,0.005430087],"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":[0.0006269761,0.00082010124,0.0029070496,0.0002726923,0.00002300375,0.0005618106,0.00015000958,0.0016361881,0.96106184,0.0011046941,0.0026578642,0.028177705],"study_design_scores_gemma":[0.00022000469,0.0037529315,0.0054252334,0.000053306627,0.00004041039,0.0005824423,0.0001020012,0.009191834,0.96010256,0.00019337606,0.020258714,0.0000772527],"about_ca_topic_score_codex":0.0015116278,"about_ca_topic_score_gemma":0.0017975116,"teacher_disagreement_score":0.01417268,"about_ca_system_score_codex":0.00051500375,"about_ca_system_score_gemma":0.001489538,"threshold_uncertainty_score":0.047412336},"labels":[],"label_agreement":null},{"id":"W4287583214","doi":"10.4271/2022-01-0591","title":"Testing of a Modern Wankel Rotary Engine - Part III: Firing Condition Analysis","year":2022,"lang":"en","type":"article","venue":"SAE technical papers on CD-ROM/SAE technical paper series","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":15,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Kootenay Association for Science & Technology","funders":"","keywords":"Rotary engine; Automotive engineering; Computer science; Mechanical engineering; Engineering","score_opus":0.022773125876709627,"score_gpt":0.2626211237800433,"score_spread":0.2398479979033337,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4287583214","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":[0.9881605,0.0001746686,0.009386,0.000015028028,0.000027927472,0.00006657029,0.00043099493,0.00022829231,0.0015101042],"genre_scores_gemma":[0.99223304,0.00012671502,0.0054296404,0.000015229536,0.0000045944566,0.00004130857,0.00041670073,0.000057863734,0.0016748946],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99940526,0.000030631545,0.000052209376,0.0001325495,0.0003300225,0.000049345876],"domain_scores_gemma":[0.99962103,0.00010313483,0.000033502012,0.00007931745,0.00014156027,0.00002145409],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00056724326,0.0004745233,0.0005703429,0.00067618594,0.00031430877,0.00045104956,0.0007231365,0.00062755577,0.003070044],"category_scores_gemma":[0.0007821315,0.00023232283,0.00044783915,0.00047609163,0.00032272772,0.0005472573,0.00039910048,0.00043847362,0.00058352953],"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":[0.0008702394,0.00018835168,0.0048286524,0.00031847745,0.000028948423,0.00027799673,0.00019953717,0.0060869795,0.9433375,0.0002746956,0.00020764102,0.043380886],"study_design_scores_gemma":[0.00003703803,0.0023948823,0.028155588,0.000036850553,0.000033916127,0.0004029801,0.00020634744,0.017644733,0.94831663,0.00015740797,0.002558125,0.000055450124],"about_ca_topic_score_codex":0.00085494213,"about_ca_topic_score_gemma":0.0011391802,"teacher_disagreement_score":0.003070044,"about_ca_system_score_codex":0.00026960816,"about_ca_system_score_gemma":0.00025207206,"threshold_uncertainty_score":0.010270357},"labels":[],"label_agreement":null},{"id":"W4289490709","doi":"","title":"Laminar kinetic energy model based on the Klebanoff-mode dynamic to predict bypass transition on a turbine blade","year":2018,"lang":"en","type":"preprint","venue":"HAL (Le Centre pour la Communication Scientifique Directe)","topic":"Rocket and propulsion systems research","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":"Safran Electronics (Canada)","funders":"","keywords":"Laminar flow; Kinetic energy; Blade (archaeology); Mechanics; Mode (computer interface); Turbine; Turbine blade; Energy transition; Computer science; Materials science; Physics; Aerospace engineering; Engineering; Mechanical engineering; Classical mechanics; Medicine","score_opus":0.012490734333673214,"score_gpt":0.23219754379088786,"score_spread":0.21970680945721466,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4289490709","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":[0.72712684,0.0005769635,0.24844722,0.0003001482,0.00022679768,0.00014404923,0.00028075985,0.00066732627,0.022229906],"genre_scores_gemma":[0.9937941,0.00009171959,0.0028348067,0.000020627274,0.000012607155,0.000040205818,0.00007768336,0.00004067731,0.0030876198],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99992836,0.000016253864,0.000005122867,0.000013001442,0.000018721039,0.000018603558],"domain_scores_gemma":[0.9998253,0.00006277538,0.000023280607,0.000014391077,0.000045079534,0.000029268338],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020753553,0.00069903897,0.0006402032,0.00047586634,0.0005536476,0.00086281786,0.00086039637,0.0010210862,0.0021883359],"category_scores_gemma":[0.00053914625,0.00032498655,0.0005734157,0.00025913923,0.00051228283,0.00083590794,0.00066368433,0.00075195637,0.00044704796],"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":[0.00008856247,0.000068984555,0.0018088818,0.000035309884,0.000012965968,0.000101613216,0.000033056815,0.9845068,0.0067119882,0.0032228236,0.00025496175,0.0031541262],"study_design_scores_gemma":[0.000004325618,0.000015056882,0.0002268143,0.0000018104366,0.0000017679499,0.0000037486298,0.0000052027744,0.9991178,0.00031534978,0.0002489626,0.00005594721,0.0000031975571],"about_ca_topic_score_codex":0.0058234646,"about_ca_topic_score_gemma":0.0043081907,"teacher_disagreement_score":0.0058234646,"about_ca_system_score_codex":0.00051475514,"about_ca_system_score_gemma":0.00084117305,"threshold_uncertainty_score":0.011579156},"labels":[],"label_agreement":null},{"id":"W4300790825","doi":"","title":"Physical description of an isentropic flow in a Laval nozzle","year":2016,"lang":"en","type":"article","venue":"DOAJ (DOAJ: Directory of Open Access Journals)","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":1,"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":"Isentropic process; Nozzle; Mechanics; Flow (mathematics); Mathematics; Physics; Thermodynamics","score_opus":0.22199307377214994,"score_gpt":0.5178697116051562,"score_spread":0.2958766378330062,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4300790825","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":[0.55571014,0.0037466972,0.40442997,0.00060366845,0.00027599395,0.00020680198,0.00038844257,0.00041063683,0.034227703],"genre_scores_gemma":[0.9863673,0.0005403544,0.008514109,0.00007188933,0.000050955732,0.000045556877,0.00008464956,0.000015803846,0.0043093655],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99986076,0.000028706923,0.0000104964065,0.00002864397,0.00004815875,0.000023252764],"domain_scores_gemma":[0.9998809,0.000043734988,0.000024510562,0.000009782972,0.000030937485,0.000010004984],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00028925543,0.0003567886,0.0003905093,0.0004960135,0.00045401198,0.0008562494,0.0006228835,0.0007856236,0.0009661709],"category_scores_gemma":[0.00055298547,0.00015105965,0.0003756665,0.00021701945,0.0010579837,0.00074383826,0.00044502385,0.00039849427,0.00014406],"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":[0.00022125075,0.00014254921,0.007775815,0.0003128859,0.000030073563,0.0023607127,0.0006584723,0.70452064,0.15859216,0.109325096,0.00087508664,0.0151853],"study_design_scores_gemma":[0.000043250515,0.00015631283,0.0034266582,0.000020257581,0.000008371775,0.0006035394,0.00012900759,0.9769195,0.0061973715,0.009305141,0.003151957,0.000038719034],"about_ca_topic_score_codex":0.0019984324,"about_ca_topic_score_gemma":0.000481189,"teacher_disagreement_score":0.0019984324,"about_ca_system_score_codex":0.00046209432,"about_ca_system_score_gemma":0.00051713246,"threshold_uncertainty_score":0.0039736032},"labels":[],"label_agreement":null},{"id":"W4310386560","doi":"","title":"Travaux de recherche menés dans le cadre projet PIPAA (Pile à combustible pour applications aéronautiques)","year":2019,"lang":"fr","type":"preprint","venue":"HAL (Le Centre pour la Communication Scientifique Directe)","topic":"Rocket and propulsion systems research","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":"Safran Electronics (Canada)","funders":"","keywords":"Pile; Political science; Computer science","score_opus":0.06838760223221915,"score_gpt":0.31087683279914424,"score_spread":0.2424892305669251,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4310386560","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":[0.31154642,0.058555584,0.27497864,0.025365615,0.0070111207,0.00241386,0.0059736148,0.003511079,0.31064403],"genre_scores_gemma":[0.4707107,0.044312447,0.18450737,0.00345559,0.0050149886,0.0019909523,0.011233583,0.0021967548,0.2765776],"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.97220975,0.00949056,0.0006742856,0.002618916,0.013136519,0.0018699885],"domain_scores_gemma":[0.97762805,0.009002479,0.00070896366,0.0026574822,0.0076996805,0.002303272],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.020195644,0.0031607659,0.0018678486,0.0033126401,0.002999059,0.010140186,0.0023939323,0.0061055804,0.019088808],"category_scores_gemma":[0.020435983,0.0008280728,0.003368061,0.0037607965,0.0026644506,0.0049455427,0.0026536235,0.0056608906,0.0059271795],"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":[0.0042131674,0.009202803,0.016612615,0.0045672413,0.0010737507,0.0037600736,0.016555814,0.032161485,0.18004286,0.15866517,0.094541244,0.47860384],"study_design_scores_gemma":[0.0013801423,0.0041535334,0.037043292,0.0016082727,0.0005558492,0.0022633553,0.010151885,0.03222285,0.13396819,0.031731676,0.74450797,0.00041283577],"about_ca_topic_score_codex":0.030283734,"about_ca_topic_score_gemma":0.015821153,"teacher_disagreement_score":0.030283734,"about_ca_system_score_codex":0.0054520564,"about_ca_system_score_gemma":0.009469522,"threshold_uncertainty_score":0.1068061},"labels":[],"label_agreement":null},{"id":"W4312389928","doi":"10.52002/0130-2906-2022-7-94-100","title":"FEATURES OF ICE-FORMING AEROSOL GENERATION DURING THE COMBUSTION OF PYROTECHNIC COMPOSITION IN THE PATH OF THE DE LAVAL NOZZLE","year":2022,"lang":"en","type":"article","venue":"Meteorologiya i Gidrologiya","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":1,"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":"Aerosol; Nozzle; Combustion; Ignition system; Supersonic speed; Aerospace engineering; Environmental science; Chemistry; Materials science; Meteorology; Engineering; Physics; Organic chemistry","score_opus":0.017647992820316923,"score_gpt":0.24176539484292212,"score_spread":0.2241174020226052,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4312389928","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":[0.9964407,0.00031328195,0.0011871443,0.000017569864,0.000007595394,0.000024372015,0.0002155596,0.000058316688,0.0017354299],"genre_scores_gemma":[0.99893135,0.000052920488,0.00036192744,0.0000071873187,0.000005833878,0.0000086443815,0.00022032316,0.000009758778,0.00040210725],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99994075,0.000004592284,0.000001728047,0.000016211663,0.000019956839,0.000016824057],"domain_scores_gemma":[0.9998554,0.000037744525,0.000047817954,0.000008195564,0.00002864521,0.000022267146],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00009131541,0.00015409925,0.00013932752,0.0005011674,0.00019894738,0.00020970928,0.0002415847,0.0002770363,0.0013266249],"category_scores_gemma":[0.00017884762,0.00010326802,0.00018331587,0.00023964411,0.00026954184,0.00017175273,0.0001367896,0.00027234486,0.00020885441],"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":[0.00090584875,0.00013232672,0.029071216,0.000081241,0.000029272096,0.002025688,0.00025357673,0.0011212262,0.96005434,0.00029894378,0.00019452623,0.0058317985],"study_design_scores_gemma":[0.00006144777,0.000955622,0.569648,0.000015757932,0.000038896364,0.0016988253,0.0002968088,0.0126077235,0.41269866,0.00033797885,0.0016039769,0.000036340552],"about_ca_topic_score_codex":0.0010181979,"about_ca_topic_score_gemma":0.00047879812,"teacher_disagreement_score":0.0013266249,"about_ca_system_score_codex":0.00016242651,"about_ca_system_score_gemma":0.00008878454,"threshold_uncertainty_score":0.004437983},"labels":[],"label_agreement":null},{"id":"W4312663132","doi":"10.1049/icp.2022.2020","title":"Iterative feedback design of de Laval nozzle","year":2022,"lang":"en","type":"article","venue":"IET conference proceedings.","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":1,"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; Isentropic process; Iterative and incremental development; Propulsion; Parametric design; Aerospace engineering; Process (computing); Iterative design; Mechanical engineering; Aerodynamics; Computer science; Parametric statistics; Engineering design process; Simulation; Engineering; Physics; Mechanics; Mathematics","score_opus":0.043213591851560366,"score_gpt":0.26526580263722443,"score_spread":0.22205221078566406,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4312663132","genre_codex":"methods","genre_gemma":"methods","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.070578255,0.0004750048,0.91835225,0.00010721623,0.00008886732,0.00021789083,0.000045893325,0.00091408676,0.009220537],"genre_scores_gemma":[0.87767714,0.00022490801,0.118803896,0.00004787993,0.000017207884,0.00022646306,0.000047815727,0.00004373605,0.0029109702],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993691,0.00008300861,0.00003309209,0.00014274563,0.00029786432,0.00007423308],"domain_scores_gemma":[0.99934274,0.00014182406,0.00013094133,0.000045991655,0.00029253445,0.000045869187],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0009185152,0.0005966227,0.00062215194,0.00047439078,0.0005884431,0.0010698176,0.0016749797,0.0010563914,0.0019005854],"category_scores_gemma":[0.0014930974,0.00041717736,0.00060187664,0.0002361268,0.00043281115,0.000670455,0.00097028114,0.00041994784,0.00033296118],"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":[0.00048309017,0.00018837485,0.0020298997,0.0005925343,0.000065825036,0.0005799825,0.00070580665,0.6172072,0.24174589,0.011778841,0.00129937,0.12332317],"study_design_scores_gemma":[0.00007301321,0.00054849626,0.0005581349,0.00003214164,0.000026720763,0.00012804286,0.000043171687,0.95770913,0.03556949,0.0010104518,0.004253964,0.00004729113],"about_ca_topic_score_codex":0.0017680756,"about_ca_topic_score_gemma":0.0008646865,"teacher_disagreement_score":0.0019005854,"about_ca_system_score_codex":0.0008240655,"about_ca_system_score_gemma":0.00094623916,"threshold_uncertainty_score":0.006358087},"labels":[],"label_agreement":null},{"id":"W4312952041","doi":"10.23952/jnva.6.2022.2.08","title":"Dynamic optimization with a non-smooth LPV system in aero-engine transition state acceleration process","year":2022,"lang":"en","type":"article","venue":"Journal of Nonlinear and Variational Analysis","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"Division of Mathematical Sciences; National Natural Science Foundation of China; Chongqing Normal University","keywords":"Acceleration; Process (computing); State (computer science); Transition (genetics); Control theory (sociology); Computer science; Automotive engineering; Mechanical engineering; Control engineering; Engineering; Physics; Algorithm; Classical mechanics; Chemistry; Artificial intelligence","score_opus":0.006295422298800445,"score_gpt":0.23650727673539798,"score_spread":0.23021185443659753,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4312952041","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":[0.0707607,0.00030197014,0.92450166,0.00030137718,0.00003557825,0.000040961953,0.000039925362,0.0001200767,0.0038977235],"genre_scores_gemma":[0.9699433,0.00025010688,0.025270268,0.00005534132,0.000024525125,0.00013547296,0.000074055715,0.00003951183,0.0042074346],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99974483,0.000088245666,0.000010844278,0.00006752544,0.000057110596,0.000031496933],"domain_scores_gemma":[0.99964297,0.00021667554,0.000052082632,0.00001388067,0.000057498233,0.000016811251],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00068030145,0.00073402986,0.0010312486,0.0003257208,0.0004679918,0.0011005837,0.00048673488,0.0011877901,0.00091060903],"category_scores_gemma":[0.0011699883,0.00049172324,0.00061709597,0.00041558885,0.0011216786,0.000704776,0.00086704036,0.0009449165,0.00012265657],"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":[0.000018900608,0.000011043379,0.00018232,0.000030584273,0.000009066095,0.00005164521,0.000028587474,0.99242026,0.00094617764,0.0041886317,0.000109450586,0.002003293],"study_design_scores_gemma":[0.0000023097061,0.000007586456,0.000045802215,8.0149226e-7,0.0000014031953,0.0000023244027,0.0000043218324,0.99931026,0.00008942803,0.00047087166,0.00006293609,0.0000019858799],"about_ca_topic_score_codex":0.009718962,"about_ca_topic_score_gemma":0.0039574574,"teacher_disagreement_score":0.009718962,"about_ca_system_score_codex":0.0005534049,"about_ca_system_score_gemma":0.0009023688,"threshold_uncertainty_score":0.01932478},"labels":[],"label_agreement":null},{"id":"W4313221317","doi":"10.54097/hset.v27i.3858","title":"Principles of Multistage Rocket Vehicle and Concepts of Propulsion Methods for Rocket Applications","year":2022,"lang":"en","type":"article","venue":"Highlights in Science Engineering and Technology","topic":"Rocket and propulsion systems research","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":"Queen's University","funders":"","keywords":"Propulsion; Aerospace engineering; In-space propulsion technologies; Payload (computing); Rocket (weapon); Spacecraft propulsion; Propellant; Thrust; Booster (rocketry); Aeronautics; Electrically powered spacecraft propulsion; Automotive engineering; Engineering; Computer science","score_opus":0.01928534777106881,"score_gpt":0.32999801375072874,"score_spread":0.3107126659796599,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4313221317","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":[0.011129782,0.019562913,0.81916445,0.0012290647,0.00089874514,0.00040331043,0.00034864884,0.00081524695,0.14644776],"genre_scores_gemma":[0.31592718,0.055499397,0.41243932,0.0010214337,0.00088152156,0.0017641817,0.0007106277,0.0004099516,0.21134646],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.9996953,0.000030372024,0.000019756444,0.00005287981,0.0001757239,0.000025855334],"domain_scores_gemma":[0.9998796,0.000025651565,0.000016656742,0.000017539754,0.0000508926,0.000009612468],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00027415864,0.0005371359,0.00032916118,0.0011337677,0.00053164293,0.0009839212,0.0008554205,0.0008302306,0.005966242],"category_scores_gemma":[0.00024546238,0.00031949923,0.000543559,0.0006943492,0.0009931059,0.0014308603,0.0006970931,0.0014773287,0.0029539792],"study_design_candidate":"theoretical_or_conceptual","study_design_consensus":"theoretical_or_conceptual","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00010454569,0.00009306108,0.0008220773,0.0016695134,0.00003095701,0.000494585,0.00065872696,0.022117054,0.06812323,0.614728,0.0128251035,0.27833316],"study_design_scores_gemma":[0.000024474597,0.00057902955,0.0016360839,0.00044389194,0.00002319729,0.0020549563,0.00024087953,0.040958315,0.032076016,0.1586925,0.7631509,0.000119753764],"about_ca_topic_score_codex":0.00053903606,"about_ca_topic_score_gemma":0.0005026054,"teacher_disagreement_score":0.005966242,"about_ca_system_score_codex":0.0004246977,"about_ca_system_score_gemma":0.0006319049,"threshold_uncertainty_score":0.019959092},"labels":[],"label_agreement":null},{"id":"W4313405262","doi":"10.15407/itm2022.04.026","title":"Effect of the length of truncated nozzle with a tip on its thrust characteristics","year":2022,"lang":"en","type":"article","venue":"Technical mechanics","topic":"Rocket and propulsion systems research","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; Conical surface; Discharge coefficient; Supersonic speed; Mechanics; Rocket engine nozzle; Thrust; Bar (unit); Flow (mathematics); Structural engineering; Materials science; Aerospace engineering; Mechanical engineering; Physics; Engineering; Meteorology","score_opus":0.01587878445717541,"score_gpt":0.2522304408786302,"score_spread":0.2363516564214548,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4313405262","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":[0.9906267,0.0014656213,0.0042835306,0.00010770864,0.00007106964,0.000019545174,0.00017862117,0.0001969848,0.003050291],"genre_scores_gemma":[0.99772304,0.000357255,0.0011970305,0.000029813542,0.000013313339,0.000009428407,0.00013181829,0.000046504385,0.0004916383],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9995215,0.00004350698,0.000039184317,0.00012469495,0.00017504444,0.00009602224],"domain_scores_gemma":[0.9969728,0.0016387855,0.00045351393,0.00019756632,0.0005443568,0.00019293907],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000591928,0.00044030545,0.00040161173,0.00038146242,0.000301013,0.00087555445,0.00050857884,0.0006152229,0.0024430996],"category_scores_gemma":[0.0031838543,0.00027533475,0.00034376277,0.00031793345,0.000449227,0.00062830956,0.000434032,0.0005466838,0.0004007992],"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":[0.0030627178,0.00024825183,0.018920999,0.00072288443,0.00007239535,0.0016417602,0.00037912664,0.033325307,0.8993472,0.00095061207,0.0008806641,0.040448125],"study_design_scores_gemma":[0.0001071689,0.003404309,0.045708526,0.00009858928,0.00023914358,0.00071565586,0.0004627525,0.04283052,0.90133554,0.00027671675,0.004709639,0.00011140583],"about_ca_topic_score_codex":0.0006991126,"about_ca_topic_score_gemma":0.0005064356,"teacher_disagreement_score":0.0024430996,"about_ca_system_score_codex":0.00036277695,"about_ca_system_score_gemma":0.00041677765,"threshold_uncertainty_score":0.008172989},"labels":[],"label_agreement":null},{"id":"W4316592872","doi":"","title":"Design and Testing of Temperature Tunable Laval Nozzles for Astrochemical Applications","year":2016,"lang":"en","type":"preprint","venue":"HAL (Le Centre pour la Communication Scientifique Directe)","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Nozzle; Aerospace engineering; Physics; Engineering","score_opus":0.023784869540909855,"score_gpt":0.24539001743372751,"score_spread":0.22160514789281766,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4316592872","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":[0.9462301,0.0023789317,0.046386193,0.00026164844,0.00019329727,0.00044223107,0.00047742724,0.00080500834,0.0028250297],"genre_scores_gemma":[0.97037584,0.00036364302,0.027470848,0.000057039455,0.000015713955,0.0001139222,0.0001358801,0.00007720463,0.0013898247],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99899954,0.00008584623,0.00006972677,0.00024589364,0.0004942515,0.00010482221],"domain_scores_gemma":[0.9978016,0.00042981934,0.0006894771,0.00026686714,0.0006448071,0.00016746178],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0013651048,0.00041112065,0.0005927995,0.0004037041,0.00051940663,0.0011878744,0.0017632666,0.0011032589,0.001345203],"category_scores_gemma":[0.0030612594,0.00042070134,0.00042856476,0.00025603035,0.0006152229,0.001023705,0.00089364743,0.0004664166,0.00031355125],"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":[0.0004085782,0.00009955414,0.0030108716,0.00037166767,0.000033121465,0.00021271645,0.00020836692,0.00810087,0.974952,0.000780323,0.00035144688,0.011470513],"study_design_scores_gemma":[0.00016150596,0.0016324735,0.0057012276,0.000042848074,0.000047615846,0.00024129191,0.00009708993,0.030972809,0.9541958,0.00019119662,0.0066641485,0.000051993426],"about_ca_topic_score_codex":0.0007348988,"about_ca_topic_score_gemma":0.00075054786,"teacher_disagreement_score":0.0017632666,"about_ca_system_score_codex":0.0011270762,"about_ca_system_score_gemma":0.000853077,"threshold_uncertainty_score":0.008177578},"labels":[],"label_agreement":null},{"id":"W4317581693","doi":"10.2514/6.2023-0991","title":"In Silico Studies on Pintle Nozzle with Lucrative SITVC by Creating Sanal Flow Choking and Unchoking Conditions","year":2023,"lang":"en","type":"article","venue":"AIAA SCITECH 2023 Forum","topic":"Rocket and propulsion systems research","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":"University of Calgary","funders":"","keywords":"Nozzle; Choking; Engineering; Mechanical engineering; Thrust; Aerospace engineering; Simulation","score_opus":0.022691957986671046,"score_gpt":0.3114878490406997,"score_spread":0.28879589105402864,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4317581693","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":[0.95700365,0.0028561298,0.024801197,0.00033004247,0.00024423588,0.00012720237,0.00087285327,0.0004355159,0.013329137],"genre_scores_gemma":[0.98930806,0.00046266883,0.008488211,0.00003425556,0.000008599333,0.000047192894,0.0002559739,0.000033183773,0.0013619215],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99969995,0.000021961514,0.000014883703,0.000058488524,0.00013976752,0.000064908054],"domain_scores_gemma":[0.999701,0.000113227696,0.00004974553,0.000029859546,0.00006604406,0.00004014475],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00050814194,0.0003276602,0.0004604597,0.0002961135,0.0003447753,0.000767864,0.00050178013,0.0007844465,0.0034794009],"category_scores_gemma":[0.00078894827,0.00016358227,0.0005071621,0.00027113265,0.00036827143,0.00042184524,0.00033716313,0.0004602357,0.00040493402],"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":[0.0008986219,0.00050973316,0.008285694,0.0020572909,0.00007995635,0.0019061456,0.00037446973,0.3082515,0.63700646,0.0098883165,0.0033507457,0.027391084],"study_design_scores_gemma":[0.00012141671,0.002457171,0.0045175306,0.00008982057,0.000078037985,0.00024471595,0.00028581408,0.5764724,0.40598083,0.001017391,0.008636795,0.00009809323],"about_ca_topic_score_codex":0.0010040173,"about_ca_topic_score_gemma":0.0010187669,"teacher_disagreement_score":0.0034794009,"about_ca_system_score_codex":0.0003493325,"about_ca_system_score_gemma":0.00037212917,"threshold_uncertainty_score":0.011639714},"labels":[],"label_agreement":null},{"id":"W4317634727","doi":"10.2514/6.2023-2018","title":"Thermodynamic Cycle Analysis of an Ejector-Ramjet Propulsion System - Part 1","year":2023,"lang":"en","type":"article","venue":"AIAA SCITECH 2023 Forum","topic":"Rocket and propulsion systems research","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":"University of Calgary","funders":"","keywords":"Ramjet; Injector; Thermodynamic cycle; Gas compressor; Entrainment (biomusicology); Combustion; Propulsion; Aerospace engineering; Mechanics; Thermodynamics; Physics; Engineering; Combustor; Chemistry","score_opus":0.015269973383771113,"score_gpt":0.2670601594623882,"score_spread":0.2517901860786171,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4317634727","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":[0.8847473,0.0007964031,0.08087167,0.00011355937,0.0000863443,0.0003039435,0.0026116564,0.0013871328,0.029082036],"genre_scores_gemma":[0.98830694,0.0001698884,0.0054133628,0.000010374245,0.000003411943,0.000069675734,0.00070602406,0.00007462094,0.005245725],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99990463,0.000009698039,0.000005579205,0.00001409886,0.00005435209,0.000011596964],"domain_scores_gemma":[0.99992526,0.000017089613,0.0000050256926,0.000007644974,0.00003973306,0.0000053134063],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021265121,0.00023924622,0.00034068179,0.00065957906,0.00043223862,0.00043465683,0.00037734353,0.00020946446,0.0032669075],"category_scores_gemma":[0.0002844512,0.00017543885,0.00031083505,0.00025117386,0.00025075057,0.0004931361,0.00022530116,0.00022171004,0.00056770194],"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":[0.00051862205,0.00020911764,0.012029874,0.0004922715,0.00006723785,0.00035964642,0.0002014128,0.70999455,0.14943238,0.013631289,0.004245739,0.1088178],"study_design_scores_gemma":[0.000014574996,0.00022082211,0.0067450716,0.000014949504,0.000012618192,0.00006725823,0.000043215845,0.9259677,0.06064862,0.0018986225,0.0043348945,0.000031608888],"about_ca_topic_score_codex":0.0045923637,"about_ca_topic_score_gemma":0.0040672356,"teacher_disagreement_score":0.0045923637,"about_ca_system_score_codex":0.0007390766,"about_ca_system_score_gemma":0.0006725316,"threshold_uncertainty_score":0.010928869},"labels":[],"label_agreement":null},{"id":"W4317634762","doi":"10.2514/6.2023-2186","title":"Investigation of Baffled-Tube Ram Accelerator Configurations","year":2023,"lang":"en","type":"article","venue":"AIAA SCITECH 2023 Forum","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":2,"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":"Baffle; Projectile; Thrust; Propellant; Mach number; Aerospace engineering; Mechanics; Tube (container); Adiabatic process; Materials science; Hypersonic speed; Nuclear engineering; Physics; Mechanical engineering; Engineering; Thermodynamics","score_opus":0.045396429194377114,"score_gpt":0.28067411892629357,"score_spread":0.23527768973191646,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4317634762","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":[0.99035406,0.00021632244,0.0068254634,0.000023304454,0.0000132838995,0.000074796335,0.00022084435,0.0002220801,0.0020498533],"genre_scores_gemma":[0.9917459,0.00012346983,0.0065229544,0.0000074672826,0.000003960311,0.000051435636,0.00027696934,0.00003605153,0.0012318467],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9996779,0.000058817925,0.000019029283,0.000061967185,0.0001224902,0.000059716425],"domain_scores_gemma":[0.9993579,0.00024739956,0.00012143331,0.000067450535,0.00015600021,0.000049882634],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00057550595,0.00031235514,0.00021401363,0.00047082754,0.00031118433,0.0006020938,0.00064113125,0.0003779064,0.003224859],"category_scores_gemma":[0.0012678251,0.00020245752,0.00017209239,0.00032145373,0.00023512461,0.0006364423,0.0003439327,0.00034022072,0.00068733934],"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":[0.0011215486,0.00017375259,0.0048890156,0.0001895904,0.000025124373,0.00020763875,0.00017372757,0.0097502265,0.9648856,0.001157093,0.00030526015,0.01712146],"study_design_scores_gemma":[0.000058657726,0.002781938,0.009815862,0.000022693079,0.000030718023,0.00021524064,0.00016892595,0.020570073,0.96162313,0.00014760383,0.004522528,0.00004253309],"about_ca_topic_score_codex":0.00049074367,"about_ca_topic_score_gemma":0.0006919885,"teacher_disagreement_score":0.003224859,"about_ca_system_score_codex":0.00033221132,"about_ca_system_score_gemma":0.00019287338,"threshold_uncertainty_score":0.010788202},"labels":[],"label_agreement":null},{"id":"W4318713113","doi":"10.2139/ssrn.4330145","title":"Design and Kinematic Analysis of a Fastening Robot for Narrow Space Aircraft Wing-Box Applications","year":2023,"lang":"en","type":"article","venue":"SSRN Electronic Journal","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Wing; Kinematics; Aerospace engineering; Robot; Space (punctuation); Aeronautics; Engineering; Computer science; Automotive engineering; Physics; Artificial intelligence; Classical mechanics","score_opus":0.019900512832231345,"score_gpt":0.2790311079207043,"score_spread":0.25913059508847297,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4318713113","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":[0.061576985,0.0003191683,0.9251508,0.00013890157,0.000029025385,0.00020771232,0.00006229771,0.0005683328,0.011946768],"genre_scores_gemma":[0.8446749,0.00036595875,0.14279401,0.000045845707,0.000016862492,0.00023278042,0.00008810829,0.00007038613,0.011711266],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998599,0.000023606988,0.0000045218726,0.00002327786,0.000067454566,0.000021172753],"domain_scores_gemma":[0.9997738,0.00008808124,0.000049781425,0.000017810378,0.00005852241,0.000012016101],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00037288663,0.00050594483,0.00046609325,0.0003827742,0.00045296416,0.00044117557,0.00062090263,0.00080269756,0.005418138],"category_scores_gemma":[0.00043876463,0.00038660128,0.0004071178,0.00019325259,0.00033309043,0.00034006327,0.00037992455,0.00040304154,0.000714888],"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":[0.00020800238,0.00006792149,0.00087722763,0.0003679378,0.000045438414,0.00028413368,0.0001545325,0.82329845,0.08303356,0.007379531,0.0007648084,0.08351855],"study_design_scores_gemma":[0.00003698761,0.0005462116,0.00110828,0.000035130324,0.000032561704,0.00013690683,0.000055258053,0.981666,0.011479256,0.0010523048,0.0038319838,0.000019085566],"about_ca_topic_score_codex":0.0026630799,"about_ca_topic_score_gemma":0.0025726454,"teacher_disagreement_score":0.005418138,"about_ca_system_score_codex":0.00032958854,"about_ca_system_score_gemma":0.00095739565,"threshold_uncertainty_score":0.018125534},"labels":[],"label_agreement":null},{"id":"W4323658991","doi":"10.5380/reterm.v21i4.89674","title":"CONVERGENT AND DIVERGENT ANGLES OF A SOLID-FUEL ROCKET NOZZLE AND ITS INFLUENCES ON THE MOTOR’S THRUST CURVE","year":2023,"lang":"en","type":"article","venue":"Revista de Engenharia Térmica","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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; Thrust; Mechanics; Propulsion; Geometry; Specific impulse; Aerospace engineering; Mechanical engineering; Physics; Engineering; Mathematics","score_opus":0.036888161711235434,"score_gpt":0.2894879270053966,"score_spread":0.25259976529416117,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4323658991","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":[0.98050576,0.00058251614,0.0116596045,0.000045027162,0.000048452566,0.00001657724,0.00010904875,0.00010662916,0.0069264327],"genre_scores_gemma":[0.9979917,0.00014320388,0.0012548879,0.000006096909,0.000003942584,0.00000468511,0.00006645673,0.000033493274,0.0004955417],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995454,0.00005669258,0.00002807964,0.00009000098,0.00018827085,0.000091492606],"domain_scores_gemma":[0.99817157,0.0009963068,0.00025655402,0.0001285303,0.00033393843,0.00011312101],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005476826,0.00046291258,0.00041032894,0.0004406714,0.00025081393,0.0012898602,0.00030220518,0.0004985402,0.002353019],"category_scores_gemma":[0.0034232605,0.00018147883,0.00032110605,0.0003264946,0.0004838749,0.00074126397,0.00049720757,0.00043171464,0.00051127275],"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":[0.0039956165,0.00029762913,0.071749315,0.00088242634,0.00011387673,0.002435965,0.0005427613,0.3634641,0.420196,0.005681175,0.0012530702,0.12938806],"study_design_scores_gemma":[0.00012642697,0.0038856943,0.12643762,0.00024233026,0.00023434403,0.0020323964,0.0018173781,0.3003731,0.5499146,0.0026189797,0.012076564,0.00024049464],"about_ca_topic_score_codex":0.0005727739,"about_ca_topic_score_gemma":0.00041470255,"teacher_disagreement_score":0.002353019,"about_ca_system_score_codex":0.00027014903,"about_ca_system_score_gemma":0.00029443792,"threshold_uncertainty_score":0.007871628},"labels":[],"label_agreement":null},{"id":"W4379879067","doi":"10.2514/6.2023-3302","title":"Analysis and Optimisation of an Ejector Ramjet using CFD and a 1D Control Volume Solver","year":2023,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","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 Calgary","funders":"","keywords":"Injector; Ramjet; Computational fluid dynamics; Solver; Aerospace engineering; Volume (thermodynamics); Computer science; Control volume; Automotive engineering; Mechanical engineering; Mechanics; Engineering; Physics; Thermodynamics; Combustion; Combustor; Chemistry","score_opus":0.02488245571419343,"score_gpt":0.2803761132661465,"score_spread":0.255493657551953,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4379879067","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":[0.17467135,0.0005708838,0.779939,0.00035230097,0.00021842949,0.00042533435,0.0011518194,0.0026184693,0.040052395],"genre_scores_gemma":[0.63163203,0.0003653906,0.35153392,0.000095135016,0.00003267944,0.00052552257,0.0011142653,0.0005002649,0.014200908],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999711,0.00003025605,0.000015226761,0.000029042345,0.00018009129,0.0000343863],"domain_scores_gemma":[0.99961025,0.00021543098,0.000033910495,0.000025291027,0.00010007556,0.000015029161],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005620782,0.0006082081,0.00070584845,0.00055821834,0.00040667466,0.0014847423,0.00076615036,0.0010683846,0.004053918],"category_scores_gemma":[0.0010334118,0.0004912494,0.0009456591,0.00040810884,0.00044351703,0.00040457558,0.00054906507,0.00073380535,0.00059476244],"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":[0.000040861894,0.0000353019,0.0006024851,0.00012624408,0.000018303803,0.00008673229,0.00003745945,0.97492695,0.008184176,0.002366183,0.00055523304,0.013020134],"study_design_scores_gemma":[0.000010695523,0.000024035338,0.00021518559,0.0000070721817,0.0000034961356,0.000014533306,0.000008516608,0.9963219,0.0021381166,0.00022552718,0.0010243895,0.0000064313163],"about_ca_topic_score_codex":0.0064176195,"about_ca_topic_score_gemma":0.0047465265,"teacher_disagreement_score":0.0064176195,"about_ca_system_score_codex":0.0007105116,"about_ca_system_score_gemma":0.001959384,"threshold_uncertainty_score":0.013561726},"labels":[],"label_agreement":null},{"id":"W4381619407","doi":"10.11159/ffhmt23.166","title":"Thermal Performance Assessment of Reformed Gas Combustion in O<sub>2</sub> Injection Lance","year":2023,"lang":"en","type":"article","venue":"Proceedings of the ... International Conference on Fluid Flow, Heat and Mass Transfer","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Combustion; Environmental science; Nuclear engineering; Thermal; Materials science; Automotive engineering; Engineering; Chemistry; Thermodynamics; Physics","score_opus":0.02660190358187322,"score_gpt":0.2630356206382468,"score_spread":0.2364337170563736,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4381619407","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":[0.9960561,0.00029981515,0.0024734905,0.000020372634,0.00001138195,0.000013788786,0.00010814951,0.00006845583,0.00094852806],"genre_scores_gemma":[0.9970862,0.00015721259,0.0017773455,0.000008765488,0.0000018912364,0.000010885806,0.00011362065,0.000011896189,0.00083217066],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99984515,0.00001420002,0.000008058846,0.000040279323,0.00006829517,0.000023999986],"domain_scores_gemma":[0.99982053,0.00005685537,0.000032146974,0.000014452901,0.00005788757,0.000018062423],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00028986557,0.0002342881,0.0004049869,0.00019640912,0.00027733546,0.0004076073,0.00025653932,0.0003373615,0.00093695027],"category_scores_gemma":[0.00040145425,0.00014327394,0.00034380326,0.00019127695,0.0002908408,0.0003769741,0.0002392818,0.0002585738,0.00019229937],"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":[0.0014168691,0.00014917302,0.0074405493,0.0003089528,0.000021063173,0.00023663057,0.00020353436,0.025431756,0.9468064,0.00040620257,0.0002717359,0.01730723],"study_design_scores_gemma":[0.000043508804,0.0013693382,0.020116365,0.000016968597,0.000026720083,0.00008959565,0.00017253486,0.09530853,0.8810859,0.00010454942,0.0016227313,0.00004343244],"about_ca_topic_score_codex":0.0015999944,"about_ca_topic_score_gemma":0.0026613658,"teacher_disagreement_score":0.0015999944,"about_ca_system_score_codex":0.0003357337,"about_ca_system_score_gemma":0.0002449574,"threshold_uncertainty_score":0.0031813383},"labels":[],"label_agreement":null},{"id":"W4382203794","doi":"10.4050/f-0079-2023-18034","title":"S-97 RAIDER® Propulsor Flight Loads and Validation","year":2023,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","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":"Lockheed Martin (Canada)","funders":"","keywords":"Propulsor; Wake; Propeller; Aerodynamics; Thrust; Computational fluid dynamics; Rotor (electric); Aerospace engineering; Flight envelope; Airframe; Engineering; Marine engineering; Advance ratio; Envelope (radar); Reynolds-averaged Navier–Stokes equations; Blade pitch; Simulation; Mechanical engineering; Radar","score_opus":0.03629800462796694,"score_gpt":0.27387415298839773,"score_spread":0.23757614836043078,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4382203794","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":[0.954963,0.00007278185,0.021938052,0.0000980901,0.00004787588,0.00021638608,0.0022879776,0.0016234933,0.018752297],"genre_scores_gemma":[0.9843948,0.00006587003,0.008522371,0.000032898995,0.0000048569254,0.00012724538,0.002602629,0.00012166669,0.0041275956],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9996427,0.00003990416,0.00001593972,0.000039283215,0.00020986254,0.00005226702],"domain_scores_gemma":[0.99956626,0.00011863441,0.00003397027,0.000059867587,0.00018984229,0.000031439216],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00068297493,0.0007406058,0.00039192033,0.00048264264,0.00051511516,0.00050419796,0.0010073454,0.00065596914,0.003600235],"category_scores_gemma":[0.000899428,0.00026619955,0.00042504322,0.00031739136,0.00032292504,0.00042951954,0.0004953166,0.00067279063,0.0013785234],"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":[0.001121297,0.00085979875,0.019887675,0.0003411544,0.00007208109,0.0005531455,0.00033175456,0.8290829,0.073576614,0.002109876,0.0074231625,0.064640425],"study_design_scores_gemma":[0.00023515716,0.0021298784,0.0108663,0.00003676828,0.000018179933,0.00011898798,0.00018349949,0.91438407,0.06582913,0.00039933276,0.005754572,0.000044147448],"about_ca_topic_score_codex":0.006071718,"about_ca_topic_score_gemma":0.005554248,"teacher_disagreement_score":0.006071718,"about_ca_system_score_codex":0.00045240924,"about_ca_system_score_gemma":0.00064222136,"threshold_uncertainty_score":0.012072742},"labels":[],"label_agreement":null},{"id":"W4383100603","doi":"10.1016/j.ast.2023.108495","title":"Optimization and parametric studies of two-stage-to-orbit liquid oxygen/paraffin hybrid rocket vehicles","year":2023,"lang":"en","type":"article","venue":"Aerospace Science and Technology","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Calgary","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Payload (computing); Liquid oxygen; Rocket (weapon); Aerospace engineering; Propellant; Parametric statistics; Orbit (dynamics); Particle swarm optimization; Propulsion; Aerodynamics; Trajectory; Conceptual design; Engineering; Automotive engineering; Computer science; Mechanical engineering; Physics; Algorithm; Mathematics; Oxygen","score_opus":0.03368344432810536,"score_gpt":0.3203799089873144,"score_spread":0.286696464659209,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4383100603","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":[0.95351344,0.00024118651,0.026008312,0.00015456986,0.00002260908,0.000070737486,0.00013680164,0.00006280354,0.019789463],"genre_scores_gemma":[0.9956007,0.000061293074,0.00210073,0.000006563892,0.000002399602,0.000032624175,0.000038508882,0.000011930508,0.0021451795],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99989414,0.000023826333,0.0000033769084,0.000013309192,0.000029330879,0.00003603592],"domain_scores_gemma":[0.9997259,0.00016172104,0.000040733215,0.000011872279,0.000040736093,0.000019024317],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00037617373,0.0004979211,0.000620229,0.00047319484,0.0004434923,0.00070541806,0.0005578011,0.0005921978,0.0027218033],"category_scores_gemma":[0.00068233634,0.00032839354,0.00048163434,0.00033720973,0.00043710208,0.00041945235,0.00052523654,0.00031857853,0.00019304264],"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":[0.00016675371,0.000058309513,0.0007178892,0.000052105814,0.000012946915,0.00008000305,0.000027191176,0.9908309,0.0038054376,0.0010757874,0.000098626406,0.003074032],"study_design_scores_gemma":[0.000024393406,0.00018359513,0.0005704137,0.0000039373276,0.000010516515,0.000011732381,0.00005112772,0.9967181,0.0017897371,0.00033160145,0.0002963998,0.000008419906],"about_ca_topic_score_codex":0.0048896405,"about_ca_topic_score_gemma":0.0045835767,"teacher_disagreement_score":0.0048896405,"about_ca_system_score_codex":0.0005019916,"about_ca_system_score_gemma":0.0006167053,"threshold_uncertainty_score":0.009722352},"labels":[],"label_agreement":null},{"id":"W4384822968","doi":"10.1039/9781839162350-00176","title":"Estimating an Enclosure Temperature During Solid Propellant Fires","year":2023,"lang":"en","type":"book-chapter","venue":"","topic":"Rocket and propulsion systems research","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":"General Dynamics (Canada)","funders":"","keywords":"Enclosure; Propellant; Combustion; Mechanics; Event (particle physics); Environmental science; Computer science; Engineering; Aerospace engineering; Physics; Chemistry","score_opus":0.027960648289877803,"score_gpt":0.2680909046889656,"score_spread":0.24013025639908783,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4384822968","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":[0.47472498,0.0020838587,0.50169545,0.0001020551,0.00010667463,0.00008342183,0.0007872847,0.0013896341,0.019026613],"genre_scores_gemma":[0.9270659,0.0012813379,0.06378576,0.000012673136,0.000024610943,0.000027443084,0.00068963814,0.00020260006,0.0069100093],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998609,0.000017967763,0.000004758827,0.000036035788,0.00007022612,0.000010102761],"domain_scores_gemma":[0.99971527,0.00016951805,0.00003946338,0.000024184706,0.000038093855,0.0000133709245],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023318522,0.00032048125,0.00034696885,0.00043526987,0.00021474334,0.00076107413,0.0006076782,0.00055044814,0.0009844425],"category_scores_gemma":[0.0007607351,0.00025486373,0.00032114034,0.00040163376,0.00017251712,0.00070036866,0.00033796395,0.00045095928,0.00061989686],"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":[0.00034126505,0.00008525364,0.027855372,0.00037266532,0.00003872167,0.00054656726,0.00039149262,0.6533409,0.10864183,0.004356438,0.0017176348,0.20231186],"study_design_scores_gemma":[0.000003865169,0.00016534304,0.020489594,0.000048330963,0.000021027483,0.0002618894,0.00016726302,0.9133646,0.05956814,0.0023609449,0.0035073091,0.00004174439],"about_ca_topic_score_codex":0.0019905022,"about_ca_topic_score_gemma":0.0031550648,"teacher_disagreement_score":0.0019905022,"about_ca_system_score_codex":0.00032563944,"about_ca_system_score_gemma":0.00019762489,"threshold_uncertainty_score":0.003957808},"labels":[],"label_agreement":null},{"id":"W4384825731","doi":"10.1039/9781788017855-00176","title":"Estimating an Enclosure Temperature During Solid Propellant Fires","year":2023,"lang":"en","type":"book-chapter","venue":"","topic":"Rocket and propulsion systems research","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":"General Dynamics (Canada)","funders":"","keywords":"Enclosure; Propellant; Combustion; Event (particle physics); Mechanics; Variable (mathematics); Computer science; Environmental science; Applied mathematics; Engineering; Mathematics; Aerospace engineering; Physics; Chemistry; Mathematical analysis","score_opus":0.027960648289877803,"score_gpt":0.2680909046889656,"score_spread":0.24013025639908783,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4384825731","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":[0.47472498,0.0020838587,0.50169545,0.0001020551,0.00010667463,0.00008342183,0.0007872847,0.0013896341,0.019026613],"genre_scores_gemma":[0.9270659,0.0012813379,0.06378576,0.000012673136,0.000024610943,0.000027443084,0.00068963814,0.00020260006,0.0069100093],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998609,0.000017967763,0.000004758827,0.000036035788,0.00007022612,0.000010102761],"domain_scores_gemma":[0.99971527,0.00016951805,0.00003946338,0.000024184706,0.000038093855,0.0000133709245],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023318522,0.00032048125,0.00034696885,0.00043526987,0.00021474334,0.00076107413,0.0006076782,0.00055044814,0.0009844425],"category_scores_gemma":[0.0007607351,0.00025486373,0.00032114034,0.00040163376,0.00017251712,0.00070036866,0.00033796395,0.00045095928,0.00061989686],"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":[0.00034126505,0.00008525364,0.027855372,0.00037266532,0.00003872167,0.00054656726,0.00039149262,0.6533409,0.10864183,0.004356438,0.0017176348,0.20231186],"study_design_scores_gemma":[0.000003865169,0.00016534304,0.020489594,0.000048330963,0.000021027483,0.0002618894,0.00016726302,0.9133646,0.05956814,0.0023609449,0.0035073091,0.00004174439],"about_ca_topic_score_codex":0.0019905022,"about_ca_topic_score_gemma":0.0031550648,"teacher_disagreement_score":0.0019905022,"about_ca_system_score_codex":0.00032563944,"about_ca_system_score_gemma":0.00019762489,"threshold_uncertainty_score":0.003957808},"labels":[],"label_agreement":null},{"id":"W4385907154","doi":"10.1038/d41586-023-02635-0","title":"The Indigenous rocketeer","year":2023,"lang":"en","type":"article","venue":"Nature","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"World Federation of Science Journalists","funders":"","keywords":"Rocket (weapon); Indigenous; Competition (biology); Traditional knowledge; Aeronautics; Engineering; Political science; Ecology; Biology","score_opus":0.011077383174293862,"score_gpt":0.2761328350591973,"score_spread":0.2650554518849034,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4385907154","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.051851593,0.001383325,0.0011890326,0.004777909,0.000803493,0.0000375274,0.00020127441,0.00019035173,0.9395655],"genre_scores_gemma":[0.22076479,0.0013416134,0.0013952393,0.0019520276,0.00028224647,0.000032896605,0.0001923251,0.00012340858,0.77391547],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"not_applicable","domain_scores_codex":[0.999398,0.0000654,0.000010121031,0.00015730351,0.00017886025,0.00019029265],"domain_scores_gemma":[0.9996848,0.00003033928,0.0000279283,0.00006460151,0.0000814079,0.0001110326],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004923881,0.00031726673,0.00031376717,0.0008667909,0.005996656,0.0032081539,0.00079143123,0.0009046661,0.044622403],"category_scores_gemma":[0.00084612577,0.00015205303,0.00018701136,0.0008756225,0.0045920303,0.0020060083,0.0031373969,0.0018572995,0.007966769],"study_design_candidate":"not_applicable","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":[0.00031680116,0.00013439181,0.00956016,0.00035928038,0.000025719817,0.0013134055,0.037350032,0.00018216901,0.007133528,0.4853972,0.15825073,0.29997665],"study_design_scores_gemma":[0.000005515635,0.00006188195,0.006867725,0.00008840373,0.0000067238966,0.00043121225,0.0059732134,0.00007222634,0.0003703316,0.0051972875,0.98090976,0.000015680145],"about_ca_topic_score_codex":0.029990625,"about_ca_topic_score_gemma":0.08651448,"teacher_disagreement_score":0.044622403,"about_ca_system_score_codex":0.0022689116,"about_ca_system_score_gemma":0.0020712693,"threshold_uncertainty_score":0.1492768},"labels":[],"label_agreement":null},{"id":"W4386197724","doi":"10.1016/j.combustflame.2023.113018","title":"The characterization of disruptive combustion of organic gellant-laden ethanol fuel droplets","year":2023,"lang":"en","type":"article","venue":"Combustion and Flame","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":11,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Concordia University","funders":"","keywords":"Propellant; Combustion; Emulsified fuel; Materials science; Ignition system; Transient (computer programming); Chemical engineering; Rocket propellant; Liquid fuel; Chemistry; Thermodynamics; Organic chemistry","score_opus":0.01874761402623313,"score_gpt":0.25045468519890307,"score_spread":0.23170707117266995,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4386197724","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":[0.99690634,0.00024402187,0.001971299,0.000015986023,0.000009598382,0.000010785433,0.00013868854,0.000029744966,0.0006734532],"genre_scores_gemma":[0.9965405,0.00028085386,0.0015183662,0.000026748154,0.000003568724,0.000014060005,0.0002146451,0.000023142196,0.0013781862],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99989223,0.0000043487826,0.000003659445,0.000023735072,0.00005010627,0.000025896856],"domain_scores_gemma":[0.9999049,0.000024194649,0.000028264567,0.0000073399833,0.000025232797,0.000010078176],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00010988149,0.00022345193,0.00012352431,0.00025676689,0.00016650156,0.000265694,0.00020364122,0.00022457798,0.0008968496],"category_scores_gemma":[0.00018545568,0.000091784386,0.0001630612,0.00017052365,0.00022454136,0.00020730948,0.00016544567,0.00031517056,0.00017457746],"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":[0.000037748683,0.000005549387,0.00023221216,0.000011128011,0.0000021344863,0.000030018591,0.000014210863,0.000082666906,0.99898666,0.00002928431,0.000009006144,0.00055932533],"study_design_scores_gemma":[0.0000016422432,0.00003708726,0.0015339784,0.0000012660148,0.0000024925946,0.00002283527,0.000017467846,0.0006051544,0.99758935,0.000006502282,0.00018041435,0.0000018111234],"about_ca_topic_score_codex":0.0014813853,"about_ca_topic_score_gemma":0.001900807,"teacher_disagreement_score":0.0014813853,"about_ca_system_score_codex":0.00030472947,"about_ca_system_score_gemma":0.0001358489,"threshold_uncertainty_score":0.0030002594},"labels":[],"label_agreement":null},{"id":"W4387602506","doi":"10.21608/ejchem.2023.227919.8389","title":"Enhancement in hypergolic properties of paraffin wax hybrid rocket fuel","year":2023,"lang":"en","type":"article","venue":"Egyptian Journal of Chemistry","topic":"Rocket and propulsion systems research","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":"Kootenay Association for Science & Technology","funders":"","keywords":"Paraffin wax; Rocket (weapon); Wax; Rocket propellant; Materials science; Propellant; Aerospace engineering; Composite material; Engineering","score_opus":0.02474802155820923,"score_gpt":0.2392704431613818,"score_spread":0.21452242160317256,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4387602506","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":[0.99698013,0.0005829895,0.0010654064,0.000020400581,0.0000106105335,0.0000066381995,0.00020647346,0.00003012711,0.0010972529],"genre_scores_gemma":[0.9968497,0.00039583983,0.00093396776,0.000010459598,0.0000022003833,0.00001074468,0.00020886984,0.000023234134,0.0015649267],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999205,0.000005622329,0.000004409373,0.000015483603,0.00003766151,0.000016294758],"domain_scores_gemma":[0.99992406,0.000014072162,0.000021362703,0.000005043798,0.000026284017,0.000009145183],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00010549846,0.00024221944,0.0001161568,0.00024547148,0.000090876805,0.00021166727,0.00013189588,0.00017639276,0.0014519984],"category_scores_gemma":[0.00016574426,0.00012183023,0.00016074709,0.00019271199,0.000093249204,0.00027298855,0.00017384141,0.00025199566,0.00026033158],"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":[0.00009855044,0.000007251399,0.0004251206,0.000049314454,0.0000045112297,0.000044503187,0.000015960695,0.0001658263,0.99751425,0.000044423086,0.000029137957,0.0016011648],"study_design_scores_gemma":[0.000002112724,0.00010687942,0.001937326,0.0000032804874,0.0000046505133,0.000036836,0.000021457501,0.0003721692,0.99690646,0.000013713273,0.00059233885,0.0000027819078],"about_ca_topic_score_codex":0.00041081116,"about_ca_topic_score_gemma":0.000996163,"teacher_disagreement_score":0.0014519984,"about_ca_system_score_codex":0.0001279496,"about_ca_system_score_gemma":0.00007323703,"threshold_uncertainty_score":0.004857421},"labels":[],"label_agreement":null},{"id":"W4389256227","doi":"10.1016/j.ijheatmasstransfer.2023.124978","title":"Effect of grain length on GOx-paraffin hybrid rocket engines performance and regression rate","year":2023,"lang":"en","type":"article","venue":"International Journal of Heat and Mass Transfer","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":10,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Ministero dell'Istruzione e del Merito; Ministero dell’Istruzione, dell’Università e della Ricerca; Canadian Internet Registration Authority","keywords":"Propellant; Combustion; Solid fuel; Materials science; Work (physics); Mechanics; Internal ballistics; Entrainment (biomusicology); Grain size; Paraffin wax; Wax; Thermodynamics; Composite material; Aerospace engineering; Physics; Chemistry; Engineering","score_opus":0.010760720834727953,"score_gpt":0.2717109731580858,"score_spread":0.26095025232335783,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4389256227","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":[0.99874496,0.00021609517,0.00047969611,0.000013319326,0.000012219168,0.0000055019036,0.000115417286,0.0000552995,0.0003573814],"genre_scores_gemma":[0.9980769,0.00015535246,0.0004791079,0.0000110186775,0.0000032850562,0.000008775159,0.00012889394,0.00003071847,0.0011059055],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99989176,0.0000069076655,0.000011579752,0.000034549794,0.000026709571,0.000028558881],"domain_scores_gemma":[0.9995339,0.000194531,0.00011489891,0.00003376846,0.000080890844,0.000042056163],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018615618,0.00023614864,0.0002590975,0.00020315172,0.00015351745,0.00046678665,0.00031738714,0.00024311992,0.0022810162],"category_scores_gemma":[0.0006100929,0.00017257815,0.00017765415,0.0002579085,0.00018491728,0.00042609638,0.00019091109,0.00023310451,0.0004591028],"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":[0.0045908736,0.00018388072,0.0033043465,0.00013051275,0.000031309082,0.000115865885,0.00007218034,0.0033860183,0.98051125,0.00009550539,0.000121284516,0.007456973],"study_design_scores_gemma":[0.000031781146,0.0009974882,0.0063769915,0.0000064511732,0.000043951473,0.000028034274,0.000049217586,0.0028581528,0.98885465,0.000017938937,0.0007208079,0.00001454367],"about_ca_topic_score_codex":0.001057282,"about_ca_topic_score_gemma":0.001882373,"teacher_disagreement_score":0.0022810162,"about_ca_system_score_codex":0.00022592585,"about_ca_system_score_gemma":0.00018977314,"threshold_uncertainty_score":0.0076307654},"labels":[],"label_agreement":null},{"id":"W4389540739","doi":"10.17118/11143/21179","title":"Overview of the challenges of alternative propulsion systems applied tobusiness aircraft","year":2023,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","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":"Université de Sherbrooke","funders":"","keywords":"Propulsion; Aeronautics; Aerospace engineering; Computer science; Engineering; Systems engineering","score_opus":0.09308445412227831,"score_gpt":0.3034711724834771,"score_spread":0.2103867183611988,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4389540739","genre_codex":"review","genre_gemma":"review","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"review","genre_consensus":"review","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0064589544,0.7185126,0.033695087,0.009809584,0.003292069,0.0001522018,0.00027064965,0.00016894813,0.22763988],"genre_scores_gemma":[0.069076836,0.846937,0.017863266,0.0019189107,0.0032398733,0.00015586498,0.00056917424,0.00007674025,0.060162324],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9994006,0.00011550836,0.000040430365,0.00007002323,0.00029650648,0.00007696328],"domain_scores_gemma":[0.99946886,0.0001958982,0.000038274964,0.000032031607,0.0002194841,0.000045492845],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0008081228,0.0008491044,0.00047847079,0.001537005,0.0008711403,0.0035943505,0.0008635033,0.0016214735,0.012607907],"category_scores_gemma":[0.0007995558,0.00042169605,0.00075159065,0.0021535235,0.00065319554,0.0039883023,0.0013252427,0.0017262273,0.004121774],"study_design_candidate":"not_applicable","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":[0.00006526856,0.0001589064,0.0014282046,0.0054740272,0.000055112963,0.0005428639,0.00040378977,0.012872049,0.0035557486,0.28693795,0.06364513,0.62486094],"study_design_scores_gemma":[0.0000027987471,0.00011888824,0.0015045295,0.0016731563,0.000020877189,0.0005531667,0.00041226074,0.004658462,0.0005498684,0.033885926,0.9565904,0.00002966067],"about_ca_topic_score_codex":0.0036567494,"about_ca_topic_score_gemma":0.00361745,"teacher_disagreement_score":0.012607907,"about_ca_system_score_codex":0.0015777383,"about_ca_system_score_gemma":0.0017378712,"threshold_uncertainty_score":0.042177618},"labels":[],"label_agreement":null},{"id":"W4390913768","doi":"10.1051/e3sconf/202447700027","title":"CFD Analysis of De Laval Nozzle of a Hybrid Rocket Engine","year":2024,"lang":"en","type":"article","venue":"E3S Web of Conferences","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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":"National Defence University of Malaysia; Universiti Putra Malaysia","keywords":"Computational fluid dynamics; Rocket engine nozzle; Nozzle; Rocket engine; Rocket (weapon); Aerospace engineering; Mechanics; Work (physics); Mechanical engineering; Marine engineering; Computer science; Engineering; Physics","score_opus":0.02075251285138696,"score_gpt":0.2804773677237676,"score_spread":0.2597248548723806,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4390913768","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":[0.90626466,0.0013747265,0.07055119,0.00023957473,0.00014825496,0.00008048454,0.00080504233,0.0007439913,0.01979204],"genre_scores_gemma":[0.9905263,0.0002789686,0.0047328784,0.00002258901,0.00001162765,0.0000139921285,0.0002788207,0.00002910359,0.0041057006],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998528,0.000014337881,0.000008166472,0.000038082966,0.00006350663,0.000022997418],"domain_scores_gemma":[0.99986637,0.000047143436,0.000019763327,0.000010570661,0.000044310524,0.0000117666095],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016854022,0.00024993738,0.00043222422,0.00048323165,0.00040305272,0.00083544804,0.0004156168,0.00069231895,0.0017353684],"category_scores_gemma":[0.00042180484,0.00011266311,0.0005083566,0.00032347412,0.00032532477,0.00034905036,0.00029986267,0.00018358386,0.00024793207],"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":[0.00058001356,0.00013383712,0.025821984,0.00044365047,0.00007379328,0.003410031,0.00040116636,0.7119252,0.19855778,0.010038197,0.0024498324,0.04616459],"study_design_scores_gemma":[0.000035110086,0.00017331471,0.014697405,0.000033823573,0.000018908906,0.0006091812,0.000101871694,0.9246098,0.05356678,0.0010577086,0.0050424016,0.00005385701],"about_ca_topic_score_codex":0.0054508722,"about_ca_topic_score_gemma":0.0014720185,"teacher_disagreement_score":0.0054508722,"about_ca_system_score_codex":0.00055780273,"about_ca_system_score_gemma":0.000474888,"threshold_uncertainty_score":0.01083827},"labels":[],"label_agreement":null},{"id":"W4391054325","doi":"10.2316/j.2024.206-0947","title":"MOTION CHARACTERISTICS OF A REVERSE THRUST ADSORPTION WALL-CLIMBING ROBOT WITH MULTI-DEGREE-OF-FREEDOM PROPELLER, 137-149.","year":2024,"lang":"en","type":"article","venue":"International Journal of Robotics and Automation","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Propeller; Thrust; Climbing; Motion (physics); Robot; Marine engineering; Aerospace engineering; Computer science; Engineering; Artificial intelligence; Structural engineering","score_opus":0.03626775959575965,"score_gpt":0.279702975552054,"score_spread":0.24343521595629433,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4391054325","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":[0.979906,0.00023279789,0.008655255,0.00009820126,0.000025849637,0.00003628104,0.0004003966,0.0001364469,0.010508801],"genre_scores_gemma":[0.995802,0.00003754364,0.0010048249,0.0000063540474,0.0000011420668,0.000008841615,0.00017612394,0.000008845993,0.0029542572],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999677,0.0000028501502,0.0000013867254,0.0000049129517,0.000012842206,0.000010241609],"domain_scores_gemma":[0.999864,0.000034479053,0.000019215022,0.000010854987,0.000049110862,0.000022397979],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00008539307,0.00014220238,0.00017672863,0.00033333883,0.00030684334,0.000127072,0.00023215564,0.00023173213,0.0038764074],"category_scores_gemma":[0.00023843483,0.00009525074,0.00010175463,0.00017826434,0.00017327644,0.00017351088,0.000116101866,0.000105241335,0.00053171563],"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":[0.0021358842,0.00027744228,0.03735917,0.00058456016,0.00005590872,0.0024876134,0.0006614882,0.11070113,0.71530116,0.0045719882,0.0074301125,0.118433535],"study_design_scores_gemma":[0.00011589956,0.0023251623,0.2921304,0.000085663625,0.000051181854,0.0017804821,0.0013160274,0.58400595,0.102550805,0.001398489,0.01412237,0.00011755665],"about_ca_topic_score_codex":0.0031301647,"about_ca_topic_score_gemma":0.0050782324,"teacher_disagreement_score":0.0038764074,"about_ca_system_score_codex":0.00020282369,"about_ca_system_score_gemma":0.00019189164,"threshold_uncertainty_score":0.012967885},"labels":[],"label_agreement":null},{"id":"W4391302720","doi":"10.2514/6.2024-1187","title":"Performance of Paraffin Wax Embedded with Lattice and Protrusion in Hybrid Rocket","year":2024,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","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":"University of Calgary","funders":"","keywords":"Wax; Paraffin wax; Materials science; Computer science; Composite material","score_opus":0.01068341435267788,"score_gpt":0.23698438243192088,"score_spread":0.226300968079243,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4391302720","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":[0.99863064,0.00021852674,0.00065296114,0.000007578463,0.000008306763,0.0000053100503,0.000056229077,0.000040051546,0.00038052487],"genre_scores_gemma":[0.9966719,0.00026134934,0.0015172159,0.000009060016,0.0000027246901,0.000010324528,0.00011823563,0.000027483618,0.0013816305],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99986434,0.000009041616,0.000009730146,0.000033549113,0.00005737188,0.000025911719],"domain_scores_gemma":[0.99982566,0.000032966404,0.00006049576,0.000018340485,0.000036567788,0.000025960111],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00019046907,0.00031119797,0.00019698,0.00035330435,0.00011768657,0.00030973196,0.0003042937,0.00023397179,0.0014311253],"category_scores_gemma":[0.00031318679,0.00016856498,0.00023466817,0.0003110402,0.00015395532,0.0004473112,0.00028374646,0.00027620848,0.0003485534],"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":[0.0002970471,0.000032644708,0.0005594702,0.00007585143,0.000011214772,0.00009907686,0.00003765073,0.00084367103,0.9952549,0.000083343526,0.000035728302,0.0026693912],"study_design_scores_gemma":[0.000010788965,0.00055409316,0.002234718,0.000007746723,0.000011400701,0.00007068471,0.000045329856,0.0030664552,0.9932654,0.000015093166,0.0007082746,0.000010009929],"about_ca_topic_score_codex":0.0005966591,"about_ca_topic_score_gemma":0.0014250808,"teacher_disagreement_score":0.0014311253,"about_ca_system_score_codex":0.00018076196,"about_ca_system_score_gemma":0.00010548649,"threshold_uncertainty_score":0.004787624},"labels":[],"label_agreement":null},{"id":"W4391304822","doi":"10.2514/6.2024-0006","title":"Rapid propeller Performance estimation for eVTOL-Class Aircraft Using a Surface-Vorticity Flow solver","year":2024,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","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":"National Research Council Canada","funders":"","keywords":"Propeller; Solver; Vorticity; Computer science; Propulsor; Flow (mathematics); Class (philosophy); Surface (topology); Marine engineering; Vortex; Engineering; Mechanics; Artificial intelligence; Mathematics; Physics; Geometry","score_opus":0.052157347405012544,"score_gpt":0.2926248512642573,"score_spread":0.24046750385924476,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4391304822","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":[0.41329452,0.00008902229,0.5785234,0.00012999914,0.00004177395,0.000113160306,0.0004217469,0.0016055586,0.005780807],"genre_scores_gemma":[0.8998748,0.000045687353,0.09820171,0.000015523568,0.000008309469,0.00006583033,0.00044997834,0.00010555634,0.0012326525],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998883,0.000024146715,0.0000072973357,0.000014044403,0.000050029437,0.00001615664],"domain_scores_gemma":[0.9996031,0.00023605436,0.000038008442,0.000029972789,0.000076022865,0.000016856045],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00047765076,0.00044379363,0.00030352676,0.0003792475,0.00018842878,0.00041717276,0.00040730298,0.00049769523,0.002363642],"category_scores_gemma":[0.0012329345,0.00017384125,0.0002913934,0.00015575868,0.00022773758,0.00033963448,0.00035237108,0.0005087182,0.00029073018],"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":[0.00025454344,0.00015052763,0.0066563203,0.0001654101,0.000027785314,0.0002068563,0.00014962295,0.86678094,0.05714564,0.002776456,0.0014761497,0.064209655],"study_design_scores_gemma":[0.000011937109,0.000051762916,0.0007724816,0.0000047449225,0.0000018870128,0.000017782375,0.000015987958,0.99207777,0.0065284427,0.00016054783,0.00035158536,0.0000049064092],"about_ca_topic_score_codex":0.0018801205,"about_ca_topic_score_gemma":0.0015391426,"teacher_disagreement_score":0.002363642,"about_ca_system_score_codex":0.0001884444,"about_ca_system_score_gemma":0.00044317983,"threshold_uncertainty_score":0.007907212},"labels":[],"label_agreement":null},{"id":"W4392644351","doi":"10.13111/2066-8201.2024.16.1.8","title":"The impact of the Laval nozzle shape on thrust production, using the method of characteristics","year":2024,"lang":"en","type":"article","venue":"INCAS BULLETIN","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":1,"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; Thrust; Production (economics); Mathematics; Mechanical engineering; Engineering; Economics","score_opus":0.03386975419787199,"score_gpt":0.33942762120338205,"score_spread":0.3055578670055101,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4392644351","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":[0.7377563,0.0013636384,0.24799806,0.00020705687,0.000069747766,0.00013845136,0.00029076502,0.0004375012,0.011738532],"genre_scores_gemma":[0.95952666,0.00044873843,0.03868952,0.000022287106,0.000010614504,0.000036633675,0.00010503039,0.00014456245,0.0010159712],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99905676,0.00016362594,0.00003543326,0.00014237207,0.0005519775,0.000049737177],"domain_scores_gemma":[0.9947172,0.003984773,0.0005038594,0.00028235852,0.0004526057,0.000059190756],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0013332233,0.00038665385,0.00041826742,0.00066488184,0.000296011,0.0013084137,0.0004391554,0.00042665013,0.0008312557],"category_scores_gemma":[0.009492324,0.00018594241,0.00035284285,0.0007569474,0.00049809297,0.0007452711,0.00066928036,0.00038085526,0.00021399914],"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":[0.0013178084,0.00011804036,0.0592322,0.0006690287,0.00010641058,0.0008229837,0.0008693278,0.13867564,0.4342542,0.0078978455,0.00071328937,0.35532328],"study_design_scores_gemma":[0.000066275155,0.0014835675,0.06294004,0.000085109124,0.00012841563,0.0011825252,0.00039662042,0.4597846,0.46150568,0.0016734921,0.010588751,0.0001649108],"about_ca_topic_score_codex":0.00087117474,"about_ca_topic_score_gemma":0.0009819476,"teacher_disagreement_score":0.0013332233,"about_ca_system_score_codex":0.0004286424,"about_ca_system_score_gemma":0.0005552785,"threshold_uncertainty_score":0.0070508122},"labels":[],"label_agreement":null},{"id":"W4392777409","doi":"10.31224/7242","title":"Derivation of a Revised Tsiolkovsky Rocket Equation That Predicts Combustion Oscillations","year":2024,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","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":"Novelis (Canada)","funders":"","keywords":"Rocket (weapon); Propellant; Differential equation; Momentum (technical analysis); Ideal (ethics); Partial differential equation; Physics; Combustion; Collision; Mathematics; Classical mechanics; Mechanics; Mathematical analysis; Aerospace engineering; Law; Engineering; Computer science; Chemistry; Political science","score_opus":0.062480609510744564,"score_gpt":0.2821851802446102,"score_spread":0.21970457073386562,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4392777409","genre_codex":"methods","genre_gemma":"methods","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.03331445,0.0014740025,0.8923945,0.0012553306,0.0005098366,0.00016094316,0.0010777771,0.00023190874,0.069581315],"genre_scores_gemma":[0.7079297,0.0030353954,0.19971706,0.0008455827,0.0004086439,0.00084265973,0.0011131577,0.00034191587,0.08576591],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999762,0.00002832345,0.000023691093,0.00004531343,0.00010830207,0.000032309985],"domain_scores_gemma":[0.99969375,0.00006374566,0.000046824764,0.00003971007,0.00013109781,0.000024893598],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00038338132,0.00046271778,0.0006387828,0.00061114045,0.00043847944,0.000873148,0.0011696245,0.001416286,0.004458688],"category_scores_gemma":[0.0012240182,0.00034589975,0.0009920066,0.0005175341,0.0007668655,0.0010862465,0.0013018003,0.001387734,0.0015158968],"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":[0.00004346285,0.000031649644,0.0019591888,0.00026279257,0.000026880667,0.00075018127,0.0002812666,0.44491804,0.015564294,0.5130768,0.0038691,0.0192164],"study_design_scores_gemma":[0.000010224928,0.000026892661,0.0006387391,0.00003366305,0.000009044541,0.00019550476,0.000040996987,0.9285543,0.0011812043,0.05902953,0.010247841,0.000032081465],"about_ca_topic_score_codex":0.0061198454,"about_ca_topic_score_gemma":0.0031539283,"teacher_disagreement_score":0.0061198454,"about_ca_system_score_codex":0.00091908465,"about_ca_system_score_gemma":0.0015872953,"threshold_uncertainty_score":0.014915824},"labels":[],"label_agreement":null},{"id":"W4392949435","doi":"10.3390/jcs8030109","title":"On the Multidisciplinary Design of a Hybrid Rocket Launcher with a Composite Overwrapped Pressure Vessel","year":2024,"lang":"en","type":"article","venue":"Journal of Composites Science","topic":"Rocket and propulsion systems research","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":"University of Victoria","funders":"Fundação para a Ciência e a Tecnologia","keywords":"Pressure vessel; Composite number; Rocket (weapon); Multidisciplinary approach; Aerospace engineering; Cabin pressurization; Materials science; Aeronautics; Engineering; Mechanical engineering; Composite material","score_opus":0.021861118562271672,"score_gpt":0.2694030108442158,"score_spread":0.24754189228194412,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4392949435","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":[0.383437,0.00078445167,0.58127165,0.0002494339,0.0000672061,0.000314793,0.00014464266,0.00028088826,0.033450086],"genre_scores_gemma":[0.8601186,0.0005261122,0.13021055,0.00005017696,0.000015135038,0.00032600897,0.00008348631,0.00006505022,0.008604856],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997912,0.00005140901,0.0000067586784,0.000038617345,0.000080166625,0.00003181591],"domain_scores_gemma":[0.9998229,0.00009072955,0.000030357396,0.000013823031,0.000026035164,0.000016226055],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00045799254,0.0004909287,0.0007179234,0.00042232123,0.00037356676,0.0011385623,0.00059345755,0.0009953215,0.0026323576],"category_scores_gemma":[0.00053747615,0.00031470097,0.0006651179,0.00023265755,0.0004657522,0.0004346744,0.00094448816,0.0005596976,0.00045245924],"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":[0.000106604,0.000054711738,0.00061217736,0.00023246733,0.000029407356,0.00023458978,0.0000690192,0.94512784,0.03439473,0.0031131993,0.00013717783,0.01588804],"study_design_scores_gemma":[0.000032090542,0.0005729742,0.00088980375,0.000030375122,0.000033200547,0.000110518115,0.000096401025,0.9835772,0.009594328,0.0015431138,0.0034955423,0.000024493489],"about_ca_topic_score_codex":0.00072700105,"about_ca_topic_score_gemma":0.0008436341,"teacher_disagreement_score":0.0026323576,"about_ca_system_score_codex":0.00034829913,"about_ca_system_score_gemma":0.00061853504,"threshold_uncertainty_score":0.008806109},"labels":[],"label_agreement":null},{"id":"W4393419608","doi":"10.5281/zenodo.1068894","title":"Fine Fuel Moisture Code - Era-Interim","year":2017,"lang":"en","type":"dataset","venue":"Zenodo (CERN European Organization for Nuclear Research)","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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":"Interim; Code (set theory); Moisture; Environmental science; Waste management; Computer science; Geography; Engineering; Meteorology; Programming language; Archaeology","score_opus":0.04669369710167657,"score_gpt":0.28636880156164674,"score_spread":0.23967510445997017,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4393419608","genre_codex":"dataset","genre_gemma":"dataset","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"dataset","genre_consensus":"dataset","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0009883455,0.000060267124,0.00062334194,0.0000684246,0.00006681271,0.000019873269,0.9953766,0.0010188275,0.001777588],"genre_scores_gemma":[0.00305875,0.000047824633,0.0023226133,0.000057106918,0.000021954678,0.000101605925,0.9927497,0.0004477253,0.0011927835],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.99945587,0.00006844343,0.00004342487,0.00019485001,0.00014011345,0.0000974087],"domain_scores_gemma":[0.999158,0.00009310289,0.00007888589,0.00023384487,0.0003720945,0.00006408052],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0008378297,0.0010885674,0.0010046188,0.0013619718,0.00053207966,0.0015702508,0.0024421785,0.0011038912,0.032704804],"category_scores_gemma":[0.0021722047,0.00049486686,0.0012496844,0.0023785343,0.00025707434,0.0013833533,0.0008950786,0.0015797437,0.03779524],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00011079305,0.000054754502,0.0057456726,0.00031881614,0.00011065061,0.00004412371,0.000038248214,0.0053640283,0.00070749654,0.001293144,0.9765461,0.009666068],"study_design_scores_gemma":[0.00031937464,0.000022635319,0.022546299,0.00021720136,0.00007062345,0.00006716461,0.00011027539,0.010928405,0.0017717174,0.0033116553,0.96053946,0.00009514795],"about_ca_topic_score_codex":0.05489805,"about_ca_topic_score_gemma":0.06779468,"teacher_disagreement_score":0.05489805,"about_ca_system_score_codex":0.0010468244,"about_ca_system_score_gemma":0.0015190374,"threshold_uncertainty_score":0.10940844},"labels":[],"label_agreement":null},{"id":"W4393598412","doi":"10.5281/zenodo.10355235","title":"Campbell Gas Engine","year":2020,"lang":"en","type":"dataset","venue":"Zenodo (CERN European Organization for Nuclear Research)","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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":"Gas engine; Computer science; Automotive engineering; Engineering","score_opus":0.03247923502319551,"score_gpt":0.23458381584249077,"score_spread":0.20210458081929528,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4393598412","genre_codex":"dataset","genre_gemma":"dataset","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"dataset","genre_consensus":"dataset","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.00013821956,0.00008519026,0.00013856695,0.000039967756,0.000018269802,0.000012872137,0.9927027,0.0019047859,0.0049594413],"genre_scores_gemma":[0.0005135092,0.00011253932,0.00055928226,0.000027936123,0.0000048159786,0.000043427306,0.99636275,0.00052599417,0.0018496481],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.9990866,0.00010491126,0.00007367025,0.0002661833,0.0003065595,0.00016194224],"domain_scores_gemma":[0.9986823,0.00025595093,0.00009673431,0.0003670421,0.00047044316,0.00012743469],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006423022,0.002622028,0.0012417382,0.0033581005,0.00082708476,0.0025025108,0.0025198418,0.001436118,0.12189416],"category_scores_gemma":[0.004021813,0.00072987884,0.0009736244,0.0077144704,0.00032073646,0.0026055707,0.0019605202,0.0016818533,0.23307241],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000030152707,0.000009685435,0.00034837716,0.0002915626,0.000007065461,0.0000090551075,0.00001980409,0.00024864532,0.000053265016,0.0007181604,0.9947232,0.0035410605],"study_design_scores_gemma":[0.000035626315,0.000004776919,0.0009931218,0.00010200955,0.0000055387763,0.00001529645,0.000041690484,0.00025256228,0.00017577577,0.0008495788,0.9975121,0.000011868651],"about_ca_topic_score_codex":0.043285705,"about_ca_topic_score_gemma":0.07527342,"teacher_disagreement_score":0.12189416,"about_ca_system_score_codex":0.001461126,"about_ca_system_score_gemma":0.0020937847,"threshold_uncertainty_score":0.40777653},"labels":[],"label_agreement":null},{"id":"W4393838010","doi":"10.5281/zenodo.10355236","title":"Campbell Gas Engine","year":2020,"lang":"en","type":"dataset","venue":"Zenodo (CERN European Organization for Nuclear Research)","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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":"Gas engine; Computer science; Environmental science; Automotive engineering; Engineering","score_opus":0.03247923502319551,"score_gpt":0.23458381584249077,"score_spread":0.20210458081929528,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4393838010","genre_codex":"dataset","genre_gemma":"dataset","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"dataset","genre_consensus":"dataset","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.00013821956,0.00008519026,0.00013856695,0.000039967756,0.000018269802,0.000012872137,0.9927027,0.0019047859,0.0049594413],"genre_scores_gemma":[0.0005135092,0.00011253932,0.00055928226,0.000027936123,0.0000048159786,0.000043427306,0.99636275,0.00052599417,0.0018496481],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.9990866,0.00010491126,0.00007367025,0.0002661833,0.0003065595,0.00016194224],"domain_scores_gemma":[0.9986823,0.00025595093,0.00009673431,0.0003670421,0.00047044316,0.00012743469],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006423022,0.002622028,0.0012417382,0.0033581005,0.00082708476,0.0025025108,0.0025198418,0.001436118,0.12189416],"category_scores_gemma":[0.004021813,0.00072987884,0.0009736244,0.0077144704,0.00032073646,0.0026055707,0.0019605202,0.0016818533,0.23307241],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000030152707,0.000009685435,0.00034837716,0.0002915626,0.000007065461,0.0000090551075,0.00001980409,0.00024864532,0.000053265016,0.0007181604,0.9947232,0.0035410605],"study_design_scores_gemma":[0.000035626315,0.000004776919,0.0009931218,0.00010200955,0.0000055387763,0.00001529645,0.000041690484,0.00025256228,0.00017577577,0.0008495788,0.9975121,0.000011868651],"about_ca_topic_score_codex":0.043285705,"about_ca_topic_score_gemma":0.07527342,"teacher_disagreement_score":0.12189416,"about_ca_system_score_codex":0.001461126,"about_ca_system_score_gemma":0.0020937847,"threshold_uncertainty_score":0.40777653},"labels":[],"label_agreement":null},{"id":"W4394859682","doi":"","title":"Experimental and Numerical Solution of Formation and Evolution Of Cavitation in Laval Nozzle","year":2010,"lang":"en","type":"article","venue":"DOAJ (DOAJ: Directory of Open Access Journals)","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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; Cavitation; Mechanics; Mechanical engineering; Materials science; Physics; Engineering","score_opus":0.13254781227900275,"score_gpt":0.5059814246632817,"score_spread":0.3734336123842789,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4394859682","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":[0.9660147,0.0003806906,0.02740988,0.00010118417,0.000037502716,0.000079661135,0.00046723947,0.0002874601,0.0052217147],"genre_scores_gemma":[0.98657274,0.00014620574,0.012134408,0.000007668812,0.000008211874,0.00005156555,0.00016320028,0.000024353241,0.00089158857],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99955505,0.000049901802,0.000026052325,0.00008157895,0.00021700721,0.00007039013],"domain_scores_gemma":[0.9993205,0.00023843966,0.00009378922,0.00011801177,0.00018087483,0.000048462654],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006093157,0.00020553006,0.0003130423,0.00031687465,0.00033170212,0.00032282775,0.00070259976,0.000516944,0.0015778353],"category_scores_gemma":[0.0009719595,0.00015500409,0.00021389835,0.00042574253,0.00046326814,0.00038469196,0.00045185778,0.00045565394,0.00012381146],"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":[0.000255081,0.00020520194,0.0052482756,0.00027248095,0.0000125119095,0.00040593464,0.00049296964,0.024040533,0.9562931,0.002132895,0.00044620843,0.010194744],"study_design_scores_gemma":[0.000063828105,0.0009750681,0.01122722,0.000019796951,0.000017178416,0.0002598492,0.00020838609,0.13884303,0.8449323,0.0006201534,0.0027865658,0.00004654603],"about_ca_topic_score_codex":0.0008328342,"about_ca_topic_score_gemma":0.00044810367,"teacher_disagreement_score":0.0015778353,"about_ca_system_score_codex":0.00034947807,"about_ca_system_score_gemma":0.00025416753,"threshold_uncertainty_score":0.005278349},"labels":[],"label_agreement":null},{"id":"W4399281952","doi":"10.21015/vtm.v12i1.1762","title":"Series Solution of Unsteady Tank Drainage for Third Order Fluid using Adomian Decomposition Method","year":2024,"lang":"en","type":"article","venue":"VFAST Transactions on Mathematics","topic":"Rocket and propulsion systems research","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":"Quest University Canada","funders":"","keywords":"Adomian decomposition method; Third order; Decomposition; Series (stratigraphy); Mathematics; Applied mathematics; Calculus (dental); Mechanics; Mathematical analysis; Geology; Physics; Philosophy; Chemistry; Partial differential equation; Medicine","score_opus":0.03894075998628835,"score_gpt":0.3419656480703437,"score_spread":0.30302488808405537,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4399281952","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":[0.03606176,0.0005740372,0.9535026,0.0002507998,0.00012598986,0.00005036142,0.00006968991,0.00010947274,0.009255264],"genre_scores_gemma":[0.7049184,0.0016351738,0.2566275,0.0001612411,0.00018658435,0.00029783414,0.00023669668,0.00022880381,0.035707768],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998443,0.000056793047,0.0000061389624,0.000018931474,0.000055562945,0.000018195113],"domain_scores_gemma":[0.9998173,0.00007140071,0.00002636908,0.000011691582,0.000055463403,0.00001787781],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003407214,0.0006761337,0.0005892835,0.00059533044,0.00031630028,0.000577004,0.00048458943,0.000657774,0.0023203094],"category_scores_gemma":[0.00074128475,0.00021993073,0.0006285707,0.00039092926,0.0006285,0.0006755418,0.0006905866,0.00089919014,0.00034445876],"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":[0.00008445167,0.00010337657,0.0012552441,0.00044437355,0.000052769687,0.000494609,0.00029149567,0.730419,0.020978145,0.1930906,0.0030387964,0.049747113],"study_design_scores_gemma":[0.0000043383784,0.000015297052,0.00005825016,0.0000062331364,0.0000026392258,0.00002838802,0.000023123008,0.9886996,0.00083185453,0.009100755,0.0012248325,0.0000045927886],"about_ca_topic_score_codex":0.0032305077,"about_ca_topic_score_gemma":0.0028611093,"teacher_disagreement_score":0.0032305077,"about_ca_system_score_codex":0.00049476756,"about_ca_system_score_gemma":0.0008780633,"threshold_uncertainty_score":0.0077622533},"labels":[],"label_agreement":null},{"id":"W4399441222","doi":"10.37657/vniipo.pb.2024.115.2.006","title":"CALCULATION OF DEGRADATION MECHANISM OF FREON 227EA IN THE FLAME OF METHANE-OXYGEN MIXTURE","year":2024,"lang":"ru","type":"article","venue":"Pozharnaia bezopasnost`","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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":"Freon; Methane; Degradation (telecommunications); Oxygen; Mechanism (biology); Materials science; Chemistry; Chemical engineering; Organic chemistry; Computer science; Physics; Engineering","score_opus":0.024457117444588977,"score_gpt":0.2883763772320008,"score_spread":0.2639192597874118,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4399441222","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":[0.9639741,0.0017373256,0.02563104,0.00009032823,0.00004924201,0.000046355657,0.0006576951,0.0002942138,0.007519697],"genre_scores_gemma":[0.99230886,0.00064929377,0.00436507,0.000009414618,0.0000022598274,0.000026537315,0.00023149491,0.000026894155,0.0023802146],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999033,0.0000095412015,0.0000059195113,0.000016413915,0.00004551757,0.000019182819],"domain_scores_gemma":[0.9999176,0.000033031025,0.00001238204,0.000005704412,0.000026810687,0.0000043996697],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00019891477,0.00035054918,0.00026931992,0.0004317128,0.0002993782,0.0002899515,0.0004435879,0.00052966445,0.0018778874],"category_scores_gemma":[0.00032841924,0.0002200136,0.0006664206,0.0003791024,0.00014674802,0.0003690469,0.00015967485,0.00032963033,0.00030612428],"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":[0.0011987701,0.00020264881,0.029103275,0.0020052583,0.00017587857,0.0015288532,0.00042121805,0.42314354,0.4784518,0.009999917,0.0012640163,0.052504897],"study_design_scores_gemma":[0.000054327113,0.00035920308,0.017356427,0.000051150153,0.00006952514,0.0002673536,0.00024736734,0.71881545,0.25711522,0.0015810966,0.004020132,0.00006281684],"about_ca_topic_score_codex":0.0082316585,"about_ca_topic_score_gemma":0.005882663,"teacher_disagreement_score":0.0082316585,"about_ca_system_score_codex":0.0005481693,"about_ca_system_score_gemma":0.00047133205,"threshold_uncertainty_score":0.016367495},"labels":[],"label_agreement":null},{"id":"W4399852726","doi":"10.1016/j.actaastro.2024.06.029","title":"Conceptual design of rocket engines using regolith-derived propellants","year":2024,"lang":"en","type":"article","venue":"Acta Astronautica","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":9,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"McGill University; Canadian Space Agency; National Science Foundation","keywords":"Propellant; Regolith; Rocket propellant; Specific impulse; Rocket engine; Rocket (weapon); Aerospace engineering; Liquid-propellant rocket; Oxygen; Materials science; Combustion; Environmental science; Astrobiology; Nuclear engineering; Chemistry; Engineering; Physics","score_opus":0.06058028884312681,"score_gpt":0.2843965819121122,"score_spread":0.2238162930689854,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4399852726","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":[0.10496104,0.0006286297,0.84554404,0.00028759913,0.00017897536,0.0004448292,0.000189205,0.0009209752,0.04684468],"genre_scores_gemma":[0.887335,0.00066409993,0.096822925,0.000058037323,0.000022611517,0.00038190864,0.00020102096,0.00012897342,0.014385405],"study_design_codex":"simulation_or_modeling","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.99983275,0.000017080862,0.0000070574765,0.0000268202,0.00008385122,0.000032330117],"domain_scores_gemma":[0.999908,0.000013868708,0.000017896558,0.000012672094,0.0000345635,0.0000130601165],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002861652,0.00052964885,0.00044720204,0.0003029272,0.00047550583,0.0012504554,0.0014014295,0.00080882706,0.004203962],"category_scores_gemma":[0.00034661358,0.0003283707,0.00052181905,0.00016728148,0.0005376317,0.0006568375,0.0007400777,0.00053635356,0.0011458336],"study_design_candidate":"theoretical_or_conceptual","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":[0.00034377,0.00012588975,0.0009829446,0.0009846006,0.000089096204,0.00096099277,0.00032666337,0.65737617,0.18102328,0.09915106,0.0012688178,0.05736669],"study_design_scores_gemma":[0.0001712294,0.0009740043,0.0010577653,0.00010142047,0.00006581975,0.00040398698,0.00027564343,0.8621189,0.08415401,0.01219,0.038409833,0.000077451885],"about_ca_topic_score_codex":0.0007698925,"about_ca_topic_score_gemma":0.00091421336,"teacher_disagreement_score":0.004203962,"about_ca_system_score_codex":0.00043584575,"about_ca_system_score_gemma":0.0009222114,"threshold_uncertainty_score":0.014063716},"labels":[],"label_agreement":null},{"id":"W4399995805","doi":"10.1109/fpm57590.2023.10565591","title":"Performance Study of a Gas Cannon with a Laval Nozzle Based on CFD Analysis","year":2023,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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; Computational fluid dynamics; Computer science; Mechanical engineering; Aerospace engineering; Engineering","score_opus":0.02051849735800261,"score_gpt":0.261690368934765,"score_spread":0.2411718715767624,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4399995805","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":[0.96571076,0.0005732846,0.028237928,0.00009835355,0.000049901748,0.00005031213,0.00019361856,0.00060403877,0.0044818474],"genre_scores_gemma":[0.99518126,0.00013062234,0.0037872947,0.0000105374675,0.0000028337336,0.00000946254,0.00010082178,0.00002734752,0.0007497156],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994892,0.00006237618,0.00003039233,0.00008293921,0.00025670775,0.0000783075],"domain_scores_gemma":[0.9993106,0.00028624266,0.00006696249,0.00007476179,0.00020427247,0.00005710311],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00087317795,0.00046358554,0.0007040191,0.00061324507,0.0005278204,0.00080635597,0.00079427427,0.0006248284,0.0020690262],"category_scores_gemma":[0.0013983899,0.0002037768,0.00047482576,0.00045116438,0.0005760094,0.0008355129,0.0006861021,0.00025923288,0.00022338016],"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":[0.003025691,0.00022113352,0.03079297,0.0009801107,0.00009482035,0.0016186585,0.00077585765,0.39869148,0.4694495,0.005189131,0.0014475933,0.087712996],"study_design_scores_gemma":[0.0000769294,0.0014700372,0.018139064,0.000045007564,0.00006466754,0.0004712286,0.0002350605,0.8080569,0.168679,0.0003773785,0.002279856,0.0001049879],"about_ca_topic_score_codex":0.0043020262,"about_ca_topic_score_gemma":0.0017884261,"teacher_disagreement_score":0.0043020262,"about_ca_system_score_codex":0.0005880539,"about_ca_system_score_gemma":0.0007686837,"threshold_uncertainty_score":0.008553982},"labels":[],"label_agreement":null},{"id":"W4400001695","doi":"10.2514/1.b38869","title":"Multiple Diagnostics of Hybrid Rocket Ignition and Effect of Hypergolic Additive Granulometry","year":2024,"lang":"en","type":"article","venue":"Journal of Propulsion and Power","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Polytechnique Montréal","funders":"Natural Sciences and Engineering Research Council of Canada; Canadian Space Agency","keywords":"Granulometry; Ignition system; Rocket (weapon); Rocket propellant; Materials science; Combustion; Aerospace engineering; Environmental science; Nuclear engineering; Propellant; Engineering; Chemistry; Geology","score_opus":0.006431775877881867,"score_gpt":0.24724183634911506,"score_spread":0.24081006047123318,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4400001695","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":[0.99450314,0.00033007067,0.0045121745,0.000013971773,0.000008391538,0.000011594402,0.00004821841,0.00007592066,0.00049644907],"genre_scores_gemma":[0.99598134,0.00014118037,0.0034390283,0.000012859529,0.0000026399593,0.000009918252,0.000044943707,0.00001535138,0.00035275205],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99962807,0.00003796295,0.00001652791,0.00007096004,0.0001902682,0.00005606302],"domain_scores_gemma":[0.9994418,0.00019422523,0.00017812707,0.000048016056,0.00009835207,0.000039522176],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00029082247,0.0002755107,0.00026164894,0.00052739674,0.00012769243,0.0003568119,0.00028606315,0.00030297023,0.0008076491],"category_scores_gemma":[0.00052624603,0.0001602812,0.00022478022,0.0003102787,0.0004149865,0.00025811023,0.0003892614,0.00033369556,0.0001249572],"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":[0.0004127421,0.000022976072,0.0019600128,0.000041606992,0.000013047175,0.000106812244,0.000056508445,0.00030920032,0.9926892,0.000063829306,0.000016412212,0.0043076156],"study_design_scores_gemma":[0.00000398606,0.00019727032,0.0064163874,0.0000024855838,0.000011248815,0.00012050523,0.000035351353,0.0019773743,0.9910545,0.000016913968,0.00015786727,0.0000061252604],"about_ca_topic_score_codex":0.0005815515,"about_ca_topic_score_gemma":0.0010187232,"teacher_disagreement_score":0.0008076491,"about_ca_system_score_codex":0.00038048747,"about_ca_system_score_gemma":0.0001200341,"threshold_uncertainty_score":0.0027606487},"labels":[],"label_agreement":null},{"id":"W4401111323","doi":"10.1109/ims40175.2024.10600315","title":"Innovative Development Approach for a High-Power 8-Way Coaxial Radial Combiner","year":2024,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":6,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Polytechnique Montréal; Concordia University; Apollo Microwaves (Canada)","funders":"","keywords":"Coaxial; Power (physics); Computer science; Electrical engineering; Acoustics; Engineering; Physics; Telecommunications","score_opus":0.026015690460292815,"score_gpt":0.26552851885106477,"score_spread":0.23951282839077195,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4401111323","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":[0.29510564,0.0019932922,0.6505843,0.000710132,0.000399471,0.00030214476,0.00018085455,0.0033169808,0.047407128],"genre_scores_gemma":[0.6166872,0.0010436396,0.35726154,0.00020128653,0.00015755948,0.00022343319,0.0002215376,0.00025777813,0.023946121],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9995396,0.00003436094,0.000019648622,0.00009055932,0.00026561282,0.000050191786],"domain_scores_gemma":[0.99978095,0.000012731701,0.00006161039,0.00003708295,0.00007710206,0.000030508634],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00045157937,0.00060030835,0.0002915971,0.00039725154,0.00025352713,0.00077615614,0.00066176837,0.0005535592,0.0023313265],"category_scores_gemma":[0.0002611049,0.00028791197,0.00034145094,0.00027166464,0.0002778852,0.0009210703,0.0007074256,0.0007116873,0.0028219284],"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":[0.00007809008,0.0000723249,0.0004721644,0.00012430915,0.000030064659,0.000419854,0.0001679122,0.001397668,0.95333153,0.0074295425,0.0009387524,0.03553768],"study_design_scores_gemma":[0.000045188008,0.00093321106,0.0010300438,0.000019737714,0.00006151984,0.00249329,0.00007644907,0.01218352,0.9157405,0.0010672342,0.06629946,0.00004981425],"about_ca_topic_score_codex":0.00013753366,"about_ca_topic_score_gemma":0.00024277964,"teacher_disagreement_score":0.0023313265,"about_ca_system_score_codex":0.00026675774,"about_ca_system_score_gemma":0.0003703144,"threshold_uncertainty_score":0.0077990294},"labels":[],"label_agreement":null},{"id":"W4401304685","doi":"10.2316/j.2024.201-0461","title":"STRUCTURAL MECHANICAL PROPERTIES AND MULTI-FIELD COUPLING ANALYSIS OF VARIABLE SWEPT WING AIRCRAFT","year":2024,"lang":"en","type":"article","venue":"Mechatronic systems and control","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Wing; Coupling (piping); Variable (mathematics); Aerospace engineering; Field (mathematics); Structural engineering; Physics; Engineering; Mechanical engineering; Mathematics; Mathematical analysis","score_opus":0.02357447709626632,"score_gpt":0.24292145790021327,"score_spread":0.21934698080394696,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4401304685","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":[0.6900894,0.0007087612,0.2952415,0.0002688355,0.00004737024,0.00003490328,0.00011933013,0.00011556446,0.013374327],"genre_scores_gemma":[0.9957088,0.00014275932,0.0020700719,0.000010072627,0.000014026824,0.000009137706,0.000035468223,0.000020255959,0.0019893227],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99991834,0.000021047315,0.0000025411439,0.000016228747,0.000030403755,0.00001146993],"domain_scores_gemma":[0.99976224,0.000096966076,0.000057451813,0.000021500302,0.000043093976,0.000018656463],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021815655,0.00042161247,0.00023383867,0.000863812,0.00018315567,0.00039627912,0.0003659293,0.00042317397,0.0014417822],"category_scores_gemma":[0.000569146,0.00021356496,0.00031326502,0.00034306134,0.00043400098,0.00064545235,0.00025837912,0.00036130546,0.00020120436],"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":[0.0001351565,0.00012643322,0.0037695053,0.00008389465,0.00007147123,0.00032244038,0.00012493497,0.86784583,0.078552805,0.02231261,0.0005324828,0.026122496],"study_design_scores_gemma":[0.000002283821,0.000028192806,0.0034812095,0.000002959207,0.000004487734,0.000031215168,0.00002042472,0.9923246,0.0009868479,0.0029351006,0.00017739493,0.000005341864],"about_ca_topic_score_codex":0.0009831894,"about_ca_topic_score_gemma":0.00064847735,"teacher_disagreement_score":0.0014417822,"about_ca_system_score_codex":0.00019505438,"about_ca_system_score_gemma":0.00014846711,"threshold_uncertainty_score":0.004823208},"labels":[],"label_agreement":null},{"id":"W4401542731","doi":"10.2139/ssrn.4924684","title":"Reducing Emissions and Fuel Consumption in Supersonic Aviation with Ammonia Hybrid Engines","year":2024,"lang":"en","type":"preprint","venue":"SSRN Electronic Journal","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":3,"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":"Fuel efficiency; Aviation; Supersonic speed; Automotive engineering; Consumption (sociology); Environmental science; Aeronautics; Engineering; Aerospace engineering","score_opus":0.013955713596794324,"score_gpt":0.25919876945401343,"score_spread":0.24524305585721912,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4401542731","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":[0.98596305,0.00031626545,0.0073470487,0.00007205441,0.000020064663,0.000008787019,0.00003647983,0.0000482749,0.0061879945],"genre_scores_gemma":[0.99692106,0.00007417146,0.0007980925,0.000010080803,0.0000035742225,0.000004126038,0.000027617674,0.000011056918,0.0021502522],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998895,0.00001758183,0.0000029520177,0.000013764857,0.000043595322,0.00003255764],"domain_scores_gemma":[0.9999039,0.00003945551,0.000010472322,0.000005355711,0.00003437917,0.000006456489],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001746339,0.00030372996,0.0002887446,0.00019472325,0.000289907,0.0004972315,0.00029256282,0.00030832927,0.0021503628],"category_scores_gemma":[0.00030603877,0.00007944783,0.0001492051,0.0002576458,0.0002230341,0.0004013178,0.00023641404,0.00016579957,0.0001457255],"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":[0.004937715,0.00061774405,0.02153618,0.0004304505,0.00028416715,0.00041621286,0.00018767045,0.442469,0.36270353,0.006179008,0.0010701735,0.15916814],"study_design_scores_gemma":[0.00011764659,0.0017538688,0.038204383,0.000024809879,0.00021356116,0.000114418915,0.0006344494,0.57285005,0.37792915,0.005247363,0.00286679,0.000043570646],"about_ca_topic_score_codex":0.008761276,"about_ca_topic_score_gemma":0.016178006,"teacher_disagreement_score":0.008761276,"about_ca_system_score_codex":0.00038607794,"about_ca_system_score_gemma":0.0002742512,"threshold_uncertainty_score":0.01742059},"labels":[],"label_agreement":null},{"id":"W4401938318","doi":"10.32920/26862379","title":"Numerical and Experimental Modal Analysis of a 1-Stage Rocket Aerostructure","year":2024,"lang":"en","type":"preprint","venue":"","topic":"Rocket and propulsion systems research","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":"Toronto Metropolitan University","funders":"","keywords":"Stage (stratigraphy); Modal; Modal analysis; Rocket (weapon); Aerospace engineering; Engineering; Geology; Structural engineering; Finite element method; Materials science","score_opus":0.019166280168968257,"score_gpt":0.3029427969757264,"score_spread":0.28377651680675814,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4401938318","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":[0.9774721,0.00004094724,0.016767455,0.00004856979,0.000018666073,0.00003181908,0.00016988062,0.00015674454,0.005293928],"genre_scores_gemma":[0.9927087,0.000023699005,0.0053642364,0.000006230339,0.0000021929739,0.000022426771,0.000091383015,0.000012605043,0.0017685327],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998272,0.00001684295,0.000008896102,0.00003033336,0.00009054919,0.00002612606],"domain_scores_gemma":[0.9995152,0.0002045816,0.000039480736,0.000068340574,0.00014174008,0.00003065148],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00040681617,0.00020612097,0.00019411226,0.00048446053,0.00040189366,0.00025744148,0.000366914,0.00047063414,0.004861679],"category_scores_gemma":[0.00065009244,0.00013855564,0.00023572527,0.00022476305,0.0005280159,0.00029272493,0.00026142225,0.00025022755,0.00035810313],"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":[0.0003788966,0.00036401523,0.0042103375,0.00021836613,0.00001327902,0.0003024915,0.00076876977,0.12405817,0.83486474,0.002548596,0.00073737797,0.031535074],"study_design_scores_gemma":[0.000044845685,0.0014079371,0.022804534,0.00003328913,0.000023834067,0.00029785495,0.00076420855,0.66499305,0.30572417,0.00099948,0.0028472024,0.000059584567],"about_ca_topic_score_codex":0.0010155975,"about_ca_topic_score_gemma":0.0017632642,"teacher_disagreement_score":0.004861679,"about_ca_system_score_codex":0.0002616165,"about_ca_system_score_gemma":0.00020106876,"threshold_uncertainty_score":0.016263962},"labels":[],"label_agreement":null},{"id":"W4401938411","doi":"10.32920/26862379.v1","title":"Numerical and Experimental Modal Analysis of a 1-Stage Rocket Aerostructure","year":2024,"lang":"en","type":"preprint","venue":"","topic":"Rocket and propulsion systems research","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":"Toronto Metropolitan University","funders":"","keywords":"Stage (stratigraphy); Modal; Rocket (weapon); Modal analysis; Numerical analysis; Aerospace engineering; Mathematics; Engineering; Geology; Structural engineering; Finite element method; Materials science; Mathematical analysis","score_opus":0.019166280168968257,"score_gpt":0.3029427969757264,"score_spread":0.28377651680675814,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4401938411","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":[0.9774721,0.00004094724,0.016767455,0.00004856979,0.000018666073,0.00003181908,0.00016988062,0.00015674454,0.005293928],"genre_scores_gemma":[0.9927087,0.000023699005,0.0053642364,0.000006230339,0.0000021929739,0.000022426771,0.000091383015,0.000012605043,0.0017685327],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998272,0.00001684295,0.000008896102,0.00003033336,0.00009054919,0.00002612606],"domain_scores_gemma":[0.9995152,0.0002045816,0.000039480736,0.000068340574,0.00014174008,0.00003065148],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00040681617,0.00020612097,0.00019411226,0.00048446053,0.00040189366,0.00025744148,0.000366914,0.00047063414,0.004861679],"category_scores_gemma":[0.00065009244,0.00013855564,0.00023572527,0.00022476305,0.0005280159,0.00029272493,0.00026142225,0.00025022755,0.00035810313],"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":[0.0003788966,0.00036401523,0.0042103375,0.00021836613,0.00001327902,0.0003024915,0.00076876977,0.12405817,0.83486474,0.002548596,0.00073737797,0.031535074],"study_design_scores_gemma":[0.000044845685,0.0014079371,0.022804534,0.00003328913,0.000023834067,0.00029785495,0.00076420855,0.66499305,0.30572417,0.00099948,0.0028472024,0.000059584567],"about_ca_topic_score_codex":0.0010155975,"about_ca_topic_score_gemma":0.0017632642,"teacher_disagreement_score":0.004861679,"about_ca_system_score_codex":0.0002616165,"about_ca_system_score_gemma":0.00020106876,"threshold_uncertainty_score":0.016263962},"labels":[],"label_agreement":null},{"id":"W4402357228","doi":"10.1088/1742-6596/2838/1/012035","title":"Optimization design of hydrogen Laval nozzle based on response surface methodology (RSM)","year":2024,"lang":"en","type":"article","venue":"Journal of Physics Conference Series","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":1,"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":"Response surface methodology; Nozzle; Hydrogen; Design of experiments; Mechanical engineering; Materials science; Computer science; Mathematics; Engineering; Physics; Statistics","score_opus":0.11089418223639727,"score_gpt":0.3253027441468207,"score_spread":0.21440856191042343,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4402357228","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":[0.21156888,0.0008994995,0.77847624,0.00016738652,0.000055116056,0.0002510621,0.00009100006,0.00066914654,0.007821623],"genre_scores_gemma":[0.92780644,0.00024838548,0.070017196,0.000042251326,0.0000072539015,0.0003039396,0.00007805092,0.000036042657,0.0014602763],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99944764,0.00017246092,0.000026114672,0.000084288826,0.00019179666,0.000077720746],"domain_scores_gemma":[0.99963427,0.00016020089,0.000059894275,0.000017658425,0.00011298413,0.00001490777],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0012266039,0.00066662574,0.0009420216,0.0005882515,0.0003277255,0.00096969376,0.0006727948,0.0008618761,0.0014982005],"category_scores_gemma":[0.0010201985,0.00046006442,0.00091788603,0.0004283895,0.00036093895,0.00037549355,0.00044806142,0.0004157404,0.00026965135],"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":[0.00009522499,0.00008463107,0.0011026053,0.00027143845,0.00004224282,0.00011577375,0.000046886333,0.946296,0.028684726,0.0015091308,0.00026437012,0.021487074],"study_design_scores_gemma":[0.000012918752,0.00013226518,0.0003332848,0.0000047391827,0.000010159055,0.000010685994,0.000015497311,0.99516004,0.003857949,0.00016122182,0.00029427238,0.000007028682],"about_ca_topic_score_codex":0.0018922619,"about_ca_topic_score_gemma":0.0011250419,"teacher_disagreement_score":0.0018922619,"about_ca_system_score_codex":0.00044786005,"about_ca_system_score_gemma":0.0010638164,"threshold_uncertainty_score":0.0064869523},"labels":[],"label_agreement":null},{"id":"W4402384545","doi":"","title":"Parametric Analysis on Ignition Assistance by a Shielded Hot Surface under Aircraft Compression Ignition Engine Conditions","year":2023,"lang":"en","type":"article","venue":"HAL (Le Centre pour la Communication Scientifique Directe)","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Army Research Laboratory; York University; New York University Abu Dhabi","keywords":"Ignition system; Shielded cable; Parametric statistics; Compression (physics); Automotive engineering; Aerospace engineering; Nuclear engineering; Materials science; Environmental science; Engineering; Electrical engineering; Composite material","score_opus":0.02034119700222514,"score_gpt":0.25687527305718816,"score_spread":0.23653407605496302,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4402384545","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":[0.9912327,0.000061014616,0.006231604,0.00001906296,0.000006722636,0.000010414696,0.000040325052,0.00004699178,0.0023512647],"genre_scores_gemma":[0.9992065,0.000016387465,0.0003183063,0.0000012589516,0.0000013846593,0.000002348707,0.000011962463,0.0000045396723,0.00043721354],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998677,0.000016693486,0.0000037043553,0.000019736948,0.00006059265,0.000031638185],"domain_scores_gemma":[0.9996569,0.00019689486,0.000033515742,0.000038903494,0.000056286168,0.000017537086],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016392126,0.00025747734,0.00037129605,0.00026465033,0.00024514733,0.00037802928,0.0003404141,0.00044157525,0.0018680886],"category_scores_gemma":[0.0005199475,0.000116416275,0.00029173392,0.00022670503,0.00050323893,0.00024121554,0.00029976948,0.00024595222,0.00015217763],"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":[0.0015718411,0.00011445244,0.005923369,0.00020262672,0.00004213133,0.0009898909,0.00041712288,0.26285207,0.6957024,0.0013263979,0.0002971636,0.030560547],"study_design_scores_gemma":[0.000038753784,0.001191914,0.044282414,0.000016491245,0.000065017455,0.000497149,0.0004816604,0.6380481,0.31326264,0.000627337,0.0014304162,0.000058154463],"about_ca_topic_score_codex":0.0008527113,"about_ca_topic_score_gemma":0.00068814395,"teacher_disagreement_score":0.0018680886,"about_ca_system_score_codex":0.00016920104,"about_ca_system_score_gemma":0.00023840505,"threshold_uncertainty_score":0.006249428},"labels":[],"label_agreement":null},{"id":"W4402638350","doi":"10.4050/f-0073-2017-12099","title":"SB&gt;1 Defiant Joint Multi-Role Technology Demonstrator: The Way Forward for Rotorcraft Manufacturing","year":2017,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","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":"Lockheed Martin (Canada)","funders":"","keywords":"Joint (building); Computer science; Aeronautics; Automotive engineering; Engineering; Aerospace engineering; Structural engineering","score_opus":0.03660866377437489,"score_gpt":0.28195416495159675,"score_spread":0.24534550117722187,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4402638350","genre_codex":"methods","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"other","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.06997273,0.00792002,0.6358577,0.027463092,0.003422832,0.00044151198,0.00053719524,0.00602974,0.24835524],"genre_scores_gemma":[0.32547155,0.0041160462,0.5603351,0.0016867075,0.00050558004,0.00021817604,0.00076149905,0.0011473683,0.105758],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9972013,0.00060588005,0.000053266085,0.00023293376,0.0016462414,0.0002604501],"domain_scores_gemma":[0.99823713,0.00022982835,0.0001238974,0.00032142454,0.0005846265,0.0005030221],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.007880315,0.00071016664,0.00038513375,0.00077129574,0.00090226176,0.0033264172,0.0015106515,0.0024102298,0.012102609],"category_scores_gemma":[0.0021314563,0.00042198523,0.00034210045,0.0004246783,0.001743797,0.004186695,0.002632917,0.0027600361,0.004390333],"study_design_candidate":"not_applicable","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":[0.0006577461,0.0003890121,0.0014200658,0.00059285254,0.000036265188,0.0012329282,0.0011242547,0.010602059,0.2072301,0.2310084,0.09956159,0.44614485],"study_design_scores_gemma":[0.00020686409,0.0023157552,0.0016022376,0.00030089595,0.000019202787,0.001647598,0.00046949595,0.028380657,0.09188577,0.027629666,0.8454573,0.00008463873],"about_ca_topic_score_codex":0.00072299695,"about_ca_topic_score_gemma":0.0011938073,"teacher_disagreement_score":0.012102609,"about_ca_system_score_codex":0.00090720685,"about_ca_system_score_gemma":0.0015527147,"threshold_uncertainty_score":0.041675568},"labels":[],"label_agreement":null},{"id":"W4402675370","doi":"10.4050/f-0074-2018-12777","title":"Further Development and Piloted Simulation Evaluation of the Break Turn ADS-33 Mission Task Element","year":2018,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","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":"Bell Helicopter Textron (Canada); Lockheed Martin (Canada)","funders":"","keywords":"Task (project management); Computer science; Turn (biochemistry); Element (criminal law); Aerospace engineering; Simulation; Aeronautics; Systems engineering; Engineering; Physics; Political science","score_opus":0.062113751305906545,"score_gpt":0.32881282958960767,"score_spread":0.2666990782837011,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4402675370","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":[0.95506424,0.000042323114,0.03134688,0.00013674035,0.00006733893,0.00073516887,0.0010890008,0.0006402467,0.010878156],"genre_scores_gemma":[0.9651483,0.00004531114,0.029794209,0.00003830536,0.0000043968253,0.00031492024,0.0014901039,0.00005213997,0.003112338],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995988,0.00014230119,0.00001802086,0.000033478114,0.00014075832,0.00006667786],"domain_scores_gemma":[0.99890566,0.00038520695,0.00006155498,0.00012035514,0.0003942693,0.00013297817],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0014353592,0.0006297079,0.00030063928,0.00036487172,0.000264669,0.00050105486,0.00074342085,0.00045674611,0.0029654219],"category_scores_gemma":[0.0017055861,0.0001838666,0.00034836424,0.0002316946,0.000289852,0.0004209043,0.00039975613,0.00060543977,0.00045968915],"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":[0.0019171729,0.0033686326,0.018353403,0.00048301573,0.000097290686,0.00045802852,0.0009118894,0.8171428,0.06812234,0.0029771489,0.0065511083,0.07961729],"study_design_scores_gemma":[0.00054277893,0.0062706536,0.012084753,0.000059561713,0.000046299465,0.00007519748,0.0007933927,0.9315098,0.034146823,0.0006839489,0.013730566,0.00005630731],"about_ca_topic_score_codex":0.008046828,"about_ca_topic_score_gemma":0.009286074,"teacher_disagreement_score":0.008046828,"about_ca_system_score_codex":0.00057299423,"about_ca_system_score_gemma":0.00087755854,"threshold_uncertainty_score":0.015999973},"labels":[],"label_agreement":null},{"id":"W4402689818","doi":"10.3233/faia240365","title":"Analysis of the Nozzle Design for Rocket-Candy Using a Systemic Model","year":2024,"lang":"en","type":"book-chapter","venue":"Frontiers in artificial intelligence and applications","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":1,"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":"Rocket (weapon); Nozzle; Aeronautics; Aerospace engineering; Engineering","score_opus":0.10528423134895072,"score_gpt":0.31479869657695464,"score_spread":0.20951446522800393,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4402689818","genre_codex":"methods","genre_gemma":"methods","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.057235077,0.00034774552,0.9215466,0.00009399373,0.000035974397,0.00010869804,0.00011339311,0.00044299322,0.02007558],"genre_scores_gemma":[0.9026563,0.0005546123,0.086698845,0.000053493968,0.0000159868,0.00019235574,0.00018128422,0.00015342695,0.009493692],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997985,0.00004206954,0.0000082210145,0.000046691872,0.00008075915,0.000023808063],"domain_scores_gemma":[0.9997979,0.00009642177,0.000031646356,0.000015045076,0.000045915636,0.000013080017],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00045415552,0.00043138716,0.0006962492,0.00030925896,0.0003343143,0.0008735678,0.00056297384,0.0007623839,0.0048368773],"category_scores_gemma":[0.00078269816,0.0003236117,0.0008483354,0.00020274518,0.00035152354,0.00055618957,0.00045883373,0.00041938497,0.00048325793],"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":[0.000028517234,0.00001802892,0.0006018235,0.000076643046,0.000010691923,0.00008298051,0.000036753016,0.97392184,0.005590629,0.011050002,0.00028718746,0.008294953],"study_design_scores_gemma":[0.0000059192926,0.000031528445,0.00015583255,0.000004740612,0.0000064713795,0.000018716237,0.000007821555,0.9969965,0.00088622107,0.00079833326,0.0010833389,0.0000045581455],"about_ca_topic_score_codex":0.0024962504,"about_ca_topic_score_gemma":0.0016346906,"teacher_disagreement_score":0.0048368773,"about_ca_system_score_codex":0.00073529145,"about_ca_system_score_gemma":0.0011100676,"threshold_uncertainty_score":0.016180992},"labels":[],"label_agreement":null},{"id":"W4402825132","doi":"10.1007/978-3-031-61515-3_15","title":"Fuel Efficiency Monitoring of Military Transport Aircraft Within the Canadian Armed Forces","year":2024,"lang":"en","type":"book-chapter","venue":"Lecture notes in civil engineering","topic":"Rocket and propulsion systems research","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":true,"ca_institutions":"Queen's University; Royal Military College of Canada","funders":"","keywords":"Aeronautics; Aerospace engineering; Engineering; Environmental science; Forensic engineering; Marine engineering","score_opus":0.012701205834129125,"score_gpt":0.22349136105870585,"score_spread":0.21079015522457673,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4402825132","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":[0.9534532,0.0017239064,0.003150674,0.00018990994,0.00003499318,0.000059207112,0.005296918,0.00016110517,0.035930097],"genre_scores_gemma":[0.97876877,0.0008290378,0.002317008,0.00003049797,0.000007955158,0.000017550277,0.0021738447,0.000051443367,0.015803937],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.9994294,0.000012757799,0.00001026051,0.00007305672,0.00035867954,0.00011576523],"domain_scores_gemma":[0.9995466,0.00003201043,0.000033043812,0.000007939823,0.0003453426,0.000035163153],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00030132307,0.00049970887,0.00031613023,0.002871773,0.0016419713,0.001011924,0.0012077793,0.00034561296,0.0018570696],"category_scores_gemma":[0.0006461633,0.00019860831,0.00026104195,0.0028733802,0.00028716985,0.00034286073,0.000345626,0.00033838468,0.00045087523],"study_design_candidate":"observational","study_design_consensus":"observational","about_ca_topic_candidate":true,"about_ca_topic_consensus":true,"about_ca_system_candidate":true,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0007816608,0.00022434257,0.4874807,0.0002630058,0.00020092033,0.00048676447,0.0016750213,0.058132283,0.044092894,0.0021903818,0.01854358,0.38592842],"study_design_scores_gemma":[0.0000041057674,0.000054296837,0.96654934,0.000036733225,0.00003078295,0.000066222485,0.00080899923,0.016930545,0.006136467,0.00010169818,0.009234864,0.000045934572],"about_ca_topic_score_codex":0.9823224,"about_ca_topic_score_gemma":0.99170625,"teacher_disagreement_score":0.985365,"about_ca_system_score_codex":0.014635007,"about_ca_system_score_gemma":0.0071679074,"threshold_uncertainty_score":0.1061849},"labels":[],"label_agreement":null},{"id":"W4403004553","doi":"10.46604/ijeti.2024.13615","title":"Analysis of Atomization Performance of Linear Laval Nozzle under Varied Water Pressures Based on VOF and DPM Models","year":2024,"lang":"en","type":"article","venue":"International Journal of Engineering and Technology Innovation","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":4,"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; Volume of fluid method; Mechanical engineering; Materials science; Mechanics; Engineering; Physics; Flow (mathematics)","score_opus":0.012110108234364739,"score_gpt":0.2541767668607066,"score_spread":0.24206665862634189,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4403004553","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":[0.9855378,0.0004772951,0.011750969,0.0000518551,0.00001504738,0.00002319568,0.0002866217,0.00015724174,0.001700029],"genre_scores_gemma":[0.9967168,0.00021441832,0.002431966,0.0000063449334,0.0000020435834,0.000012812351,0.00013725062,0.00001495763,0.0004633448],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998006,0.0000143547,0.000013016541,0.00003865706,0.00009420234,0.000039228657],"domain_scores_gemma":[0.9997142,0.00014426859,0.00004415303,0.00001897767,0.00006666966,0.00001180071],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00030713488,0.0002663938,0.00026517693,0.00028571862,0.00019361447,0.0002877561,0.0004104608,0.00041130584,0.0011741024],"category_scores_gemma":[0.0006733314,0.00013593248,0.0003774664,0.00030738473,0.00025799853,0.00044722675,0.0002300836,0.00024914937,0.00015732402],"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":[0.00065130554,0.00013028794,0.016245535,0.00045121546,0.000053121545,0.00047601116,0.00029316606,0.20810117,0.7414528,0.001683345,0.00068726396,0.02977474],"study_design_scores_gemma":[0.000028008568,0.0004750655,0.009176517,0.000011886194,0.000025814961,0.000074434596,0.00009575354,0.65609866,0.33291644,0.00018955025,0.00087327557,0.000034541004],"about_ca_topic_score_codex":0.003437509,"about_ca_topic_score_gemma":0.0016907324,"teacher_disagreement_score":0.003437509,"about_ca_system_score_codex":0.00035490107,"about_ca_system_score_gemma":0.0002105923,"threshold_uncertainty_score":0.0068350434},"labels":[],"label_agreement":null},{"id":"W4403318321","doi":"10.1590/1517-7076-rmat-2024-0460","title":"Experimental analysis of the effect of water pressure on the atomization performance of a Linear Laval nozzle and comparison with numerical analysis","year":2024,"lang":"en","type":"article","venue":"Matéria (Rio de Janeiro)","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Nozzle; Mechanics; Materials science; Environmental science; Mechanical engineering; Engineering; Physics","score_opus":0.010294191683607531,"score_gpt":0.2552670191805308,"score_spread":0.24497282749692326,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4403318321","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":[0.9960135,0.000171402,0.002349434,0.00004003678,0.000013498381,0.00002683194,0.00018344594,0.00008260217,0.0011193445],"genre_scores_gemma":[0.9980798,0.000111584704,0.0009927696,0.000011352867,0.000006153322,0.000016465148,0.00008632701,0.000018954559,0.0006765115],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9996773,0.000025680787,0.00001786837,0.00007155457,0.00012439724,0.00008318741],"domain_scores_gemma":[0.99935144,0.00033277826,0.00009301396,0.00007130227,0.000119323224,0.000032085438],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00034718245,0.00032414956,0.00031737168,0.00020158649,0.00059258257,0.00035943565,0.00061617565,0.00054954045,0.0037952971],"category_scores_gemma":[0.0009706384,0.00021156881,0.0002759321,0.00030477977,0.0006258953,0.0005607605,0.00044000457,0.00047115932,0.00030891772],"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":[0.00038413017,0.00008092449,0.001017424,0.00008280288,0.0000073346655,0.000075233926,0.00015922604,0.00094676425,0.9938186,0.000116992145,0.00009398808,0.0032166184],"study_design_scores_gemma":[0.00001979542,0.00067795574,0.0050860452,0.0000034296554,0.000010658458,0.000046484136,0.000081089645,0.0035088104,0.98999023,0.000025897301,0.0005382842,0.000011373766],"about_ca_topic_score_codex":0.001360976,"about_ca_topic_score_gemma":0.00091309124,"teacher_disagreement_score":0.0037952971,"about_ca_system_score_codex":0.00034779863,"about_ca_system_score_gemma":0.00029689624,"threshold_uncertainty_score":0.012696505},"labels":[],"label_agreement":null},{"id":"W4403605384","doi":"10.3390/fluids9100244","title":"Optimization of Rotational Hydrodynamic Cavitation Reactor Geometry","year":2024,"lang":"en","type":"article","venue":"Fluids","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"SAIT Polytechnic","funders":"","keywords":"Cavitation; Mechanics; Physics; Materials science; Geometry; Mathematics","score_opus":0.012251871074860355,"score_gpt":0.2613489838842897,"score_spread":0.2490971128094293,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4403605384","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":[0.82968694,0.002797021,0.14240721,0.0006054751,0.00023163109,0.00045501278,0.0009009639,0.001002648,0.021913156],"genre_scores_gemma":[0.9271104,0.00086767675,0.07006954,0.00004045774,0.000015561833,0.00023769062,0.00037618965,0.000115366194,0.0011670507],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9996019,0.00004933403,0.000030054389,0.00012005154,0.00012739738,0.000071355105],"domain_scores_gemma":[0.9995633,0.00011847566,0.000113447495,0.000042916734,0.0001256595,0.000036140787],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00071381166,0.0009625522,0.0007855589,0.0005379956,0.00029988124,0.00089271675,0.00062957016,0.0006812591,0.0017344309],"category_scores_gemma":[0.0012767233,0.00038530893,0.0004935975,0.00041385903,0.00034079482,0.0005811144,0.00041038034,0.0005585731,0.000733417],"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":[0.0005833484,0.0004218397,0.002830898,0.0009371003,0.000047326896,0.0005288458,0.00013200105,0.20441942,0.7459007,0.006210662,0.0019070021,0.036080927],"study_design_scores_gemma":[0.00033579228,0.0022480255,0.00701934,0.000073710195,0.00019291704,0.00038580204,0.000196758,0.42464322,0.5444403,0.0011033656,0.019213727,0.0001469344],"about_ca_topic_score_codex":0.0010175902,"about_ca_topic_score_gemma":0.0014066142,"teacher_disagreement_score":0.0017344309,"about_ca_system_score_codex":0.0008263072,"about_ca_system_score_gemma":0.00078124995,"threshold_uncertainty_score":0.005995333},"labels":[],"label_agreement":null},{"id":"W4404019580","doi":"10.1016/j.ijheatmasstransfer.2024.126383","title":"Analysis of non-equilibrium condensation characteristics of supercritical carbon dioxide during transcritical flow in the Laval nozzle","year":2024,"lang":"en","type":"article","venue":"International Journal of Heat and Mass Transfer","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":12,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Supercritical carbon dioxide; Materials science; Nozzle; Condensation; Carbon dioxide; Thermodynamics; Supercritical fluid; Mechanics; Flow (mathematics); Chemistry; Physics","score_opus":0.011488282829733609,"score_gpt":0.27145851343774613,"score_spread":0.2599702306080125,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4404019580","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":[0.99734455,0.00015711242,0.0012387182,0.000015340465,0.000009907326,0.0000126831965,0.000102492035,0.00002925168,0.0010899582],"genre_scores_gemma":[0.9995277,0.000028702781,0.00009048056,0.0000033586837,0.0000024497033,0.0000045267116,0.000065624736,0.0000058296773,0.0002713287],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998745,0.000008034701,0.0000040532614,0.000026063288,0.000054743254,0.000032623415],"domain_scores_gemma":[0.9996246,0.00017813299,0.000035429875,0.000013311962,0.00011712467,0.00003140204],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018986526,0.00017679554,0.00023635048,0.0005835231,0.00043654052,0.00037534037,0.00033622215,0.00024847066,0.0012198769],"category_scores_gemma":[0.00048604456,0.000106061314,0.00023455276,0.000347757,0.00042295599,0.00036382067,0.00016131214,0.0002940278,0.00011897491],"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":[0.0007252855,0.00006426706,0.012354259,0.00008382964,0.000023308174,0.0004595573,0.0003537862,0.002253091,0.9774451,0.0004425435,0.00020554871,0.0055893254],"study_design_scores_gemma":[0.000023458915,0.0003945805,0.098687366,0.000009022137,0.00002307351,0.00013477418,0.00030937238,0.038364187,0.86101806,0.00013686759,0.0008586329,0.000040573632],"about_ca_topic_score_codex":0.0065898965,"about_ca_topic_score_gemma":0.0045108115,"teacher_disagreement_score":0.0065898965,"about_ca_system_score_codex":0.00056557934,"about_ca_system_score_gemma":0.00036556073,"threshold_uncertainty_score":0.013103068},"labels":[],"label_agreement":null},{"id":"W4405460903","doi":"10.18287/2541-7533-2024-23-4-125-132","title":"Results of experimental evaluation of the possibility of using an annular nozzle with a flat central body as part of a stand liquid rocket engine chamber","year":2024,"lang":"en","type":"article","venue":"VESTNIK of Samara University Aerospace and Mechanical Engineering","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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; Rocket engine nozzle; Liquid-propellant rocket; Aerospace engineering; Rocket engine; Rocket (weapon); Mechanics; Materials science; Mechanical engineering; Automotive engineering; Engineering; Physics; Propellant","score_opus":0.02432112793057898,"score_gpt":0.25439559298235564,"score_spread":0.23007446505177667,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4405460903","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":[0.99044025,0.00024001508,0.007726064,0.000015111374,0.000021207787,0.00004484814,0.00026659635,0.00011507026,0.0011308867],"genre_scores_gemma":[0.9948087,0.00010626485,0.003922235,0.000007454179,0.0000087482595,0.00003125066,0.00020601218,0.000027857752,0.0008814469],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9992663,0.00010732457,0.000051047642,0.00013751801,0.0003015802,0.00013611017],"domain_scores_gemma":[0.9985476,0.00069079193,0.000100534504,0.00017638618,0.0003802288,0.00010434243],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00081760716,0.0004946758,0.0005343314,0.00028146218,0.00038492362,0.00041480336,0.0005830103,0.0005290068,0.0031505914],"category_scores_gemma":[0.0012396927,0.00017576451,0.00038569813,0.0002522264,0.00038530325,0.00047389066,0.00040318473,0.00032327496,0.00027152197],"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":[0.0012049897,0.00039380157,0.0032140033,0.00031962545,0.000042385087,0.00022657319,0.000216413,0.0048661316,0.9779594,0.00025598853,0.00013412819,0.011166526],"study_design_scores_gemma":[0.000058304457,0.005159387,0.015377023,0.00002113652,0.000083446175,0.00020364349,0.00016188872,0.0077124373,0.9698289,0.000080289145,0.0012751386,0.000038459973],"about_ca_topic_score_codex":0.00032538432,"about_ca_topic_score_gemma":0.00032291733,"teacher_disagreement_score":0.0031505914,"about_ca_system_score_codex":0.00019747384,"about_ca_system_score_gemma":0.00018598745,"threshold_uncertainty_score":0.01053977},"labels":[],"label_agreement":null},{"id":"W4405518944","doi":"10.2316/j.2025.201-0461","title":"STRUCTURAL MECHANICAL PROPERTIES AND MULTI-FIELD COUPLING ANALYSIS OF VARIABLE SWEPT WING AIRCRAFT, 91-101.","year":2024,"lang":"en","type":"article","venue":"Mechatronic systems and control","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Wing; Variable (mathematics); Aerospace engineering; Coupling (piping); Field (mathematics); Wing configuration; Physics; Structural engineering; Engineering; Mechanical engineering; Mathematics; Mathematical analysis","score_opus":0.023428401797951595,"score_gpt":0.24232865020522962,"score_spread":0.218900248407278,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4405518944","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":[0.69408894,0.002107893,0.2612237,0.00054730684,0.00010855092,0.00004689668,0.00026973718,0.0001901391,0.04141681],"genre_scores_gemma":[0.9931617,0.00023544692,0.0019731203,0.00001315732,0.00001236096,0.00000723713,0.000058972753,0.000028379212,0.004509652],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999348,0.000014116482,0.0000018258355,0.000011937778,0.000027391989,0.000009924363],"domain_scores_gemma":[0.9998567,0.000055367498,0.00002501029,0.000015711412,0.000033790035,0.000013393927],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00022149789,0.00033163477,0.0002293678,0.0005557569,0.00023712627,0.00043994674,0.00034051537,0.00033542112,0.0021679376],"category_scores_gemma":[0.0006303005,0.00023418227,0.00027691934,0.00025611726,0.00044958194,0.0006931535,0.00020753751,0.000416198,0.0003538715],"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":[0.0002395983,0.00020436589,0.006419488,0.00013401976,0.000076415345,0.00044656624,0.00017624818,0.77234244,0.1160486,0.050408673,0.0028965985,0.05060705],"study_design_scores_gemma":[0.00000516067,0.000055714136,0.007743749,0.000008466973,0.000008525173,0.00008321531,0.00006203973,0.97980016,0.0038294194,0.0073094186,0.0010867475,0.0000074130307],"about_ca_topic_score_codex":0.0017351287,"about_ca_topic_score_gemma":0.0023104423,"teacher_disagreement_score":0.0021679376,"about_ca_system_score_codex":0.00025526743,"about_ca_system_score_gemma":0.00016380797,"threshold_uncertainty_score":0.0072524548},"labels":[],"label_agreement":null},{"id":"W4405848421","doi":"10.1088/1742-6596/2891/13/132002","title":"Research on the Influence of Cavities in Charge on the Formation and Penetration Performance of Jets","year":2024,"lang":"en","type":"article","venue":"Journal of Physics Conference Series","topic":"Rocket and propulsion systems research","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":"MD Precision (Canada)","funders":"","keywords":"Shaped charge; Penetration (warfare); Materials science; Charge (physics); Mechanics; Physics; Chemistry; Engineering; Operations research; Particle physics","score_opus":0.08539063601741044,"score_gpt":0.3206497456850971,"score_spread":0.23525910966768665,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4405848421","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":[0.9619381,0.0003148423,0.035321046,0.000050353294,0.000016210859,0.000025537138,0.00003362503,0.00012398923,0.002176325],"genre_scores_gemma":[0.99733657,0.00006450425,0.002341348,0.000006479498,0.0000011749016,0.000005508221,0.000009280929,0.0000077765835,0.00022731234],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998264,0.000022752096,0.000007144669,0.00003085465,0.00007315714,0.000039743718],"domain_scores_gemma":[0.9994473,0.00027787397,0.000087622575,0.000056599827,0.000100074416,0.000030535124],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00035706203,0.00029984838,0.00031612633,0.000276941,0.00027024638,0.0005968778,0.00044852227,0.00048361893,0.00094175996],"category_scores_gemma":[0.0017051,0.00022018586,0.00033029597,0.00020215084,0.00049256464,0.0008613893,0.0003585159,0.0002556318,0.00012782584],"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":[0.0002196238,0.00007416048,0.005164954,0.00018850404,0.000035004345,0.000736021,0.00023717157,0.50409347,0.4672884,0.0032650505,0.00016539574,0.018532198],"study_design_scores_gemma":[0.000026683483,0.00046008796,0.0040725926,0.00001969373,0.000033961936,0.00015611708,0.00012666038,0.8453897,0.14848636,0.0004607967,0.0007355446,0.000031654134],"about_ca_topic_score_codex":0.0011709081,"about_ca_topic_score_gemma":0.0007811081,"teacher_disagreement_score":0.0011709081,"about_ca_system_score_codex":0.00040708156,"about_ca_system_score_gemma":0.00036028473,"threshold_uncertainty_score":0.003150463},"labels":[],"label_agreement":null},{"id":"W4405923942","doi":"10.17223/19988621/84/8","title":"On the development of a mathematical model of a two-phase flow in an axisymmetric de Laval nozzle","year":2023,"lang":"en","type":"article","venue":"Vestnik Tomskogo gosudarstvennogo universiteta Matematika i mekhanika","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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":"Tomsk State University","keywords":"Rotational symmetry; Nozzle; Mechanics; Flow (mathematics); Phase (matter); Development (topology); Physics; Engineering; Mechanical engineering; Mathematics; Mathematical analysis","score_opus":0.050862630875812075,"score_gpt":0.2972140369339821,"score_spread":0.24635140605817,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4405923942","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":[0.009903621,0.0018541367,0.9713788,0.00039096543,0.00019612716,0.00012666217,0.00024893082,0.00015015736,0.01575056],"genre_scores_gemma":[0.52486044,0.008167986,0.41826987,0.0005985105,0.0007006642,0.0014670145,0.0009518456,0.00022231988,0.04476133],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996505,0.0000740648,0.00002702011,0.00008904871,0.0001261272,0.000033223514],"domain_scores_gemma":[0.9997671,0.000079761216,0.00006119793,0.000011979248,0.0000665382,0.000013443837],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0007206735,0.0011748587,0.0014434528,0.00090604584,0.0008129374,0.0019350216,0.0020708956,0.0023461394,0.0020370763],"category_scores_gemma":[0.00088681665,0.0005609612,0.0014462548,0.0011271047,0.0011244499,0.0014212,0.0011313386,0.0014901899,0.00081070134],"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":[0.000041022544,0.000065807464,0.0005424062,0.00030700496,0.000026504616,0.0006587631,0.0002732835,0.68377215,0.013569865,0.28780726,0.0010598967,0.0118761165],"study_design_scores_gemma":[0.0000134851825,0.000047705827,0.0001977527,0.000027280308,0.000009360558,0.00010952973,0.000018637755,0.97524023,0.00080000726,0.01720122,0.006313851,0.000020996278],"about_ca_topic_score_codex":0.004429078,"about_ca_topic_score_gemma":0.0018615377,"teacher_disagreement_score":0.004429078,"about_ca_system_score_codex":0.0011695514,"about_ca_system_score_gemma":0.0010734837,"threshold_uncertainty_score":0.008806586},"labels":[],"label_agreement":null},{"id":"W4406392374","doi":"10.1016/s0967-0653(98)80915-0","title":"10.1016/s0967-0653(98)80915-0","year":2000,"lang":"en","type":"article","venue":"Time to knit","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Vaporization; Cavitation; Flow (mathematics); Environmental science; Mechanics; Materials science; Thermodynamics; Physics","score_opus":0.010050461576115405,"score_gpt":0.19643837766929517,"score_spread":0.18638791609317976,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4406392374","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0003919379,0.000282066,0.00065514736,0.0003377595,0.00028720906,0.000096541655,0.00047803053,0.00076075946,0.99671054],"genre_scores_gemma":[0.00043384376,0.00014228112,0.0002413088,0.00014591271,0.000048862934,0.000041680443,0.00023354882,0.00012361408,0.998589],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.99941623,0.000036525562,0.000042226584,0.00022512095,0.00015567847,0.00012422346],"domain_scores_gemma":[0.99806434,0.00040763424,0.00011651527,0.00022474868,0.00052863266,0.000658156],"candidate_categories":["insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.0010101368,0.002588117,0.0016678704,0.0027072292,0.00251119,0.004106679,0.0032291627,0.0055426294,0.9883583],"category_scores_gemma":[0.0015139255,0.0009678768,0.0013675804,0.0024174866,0.0021758738,0.0050014015,0.0028176473,0.0024900613,0.99280035],"study_design_candidate":"not_applicable","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":[0.00033540674,0.00019542937,0.00078095973,0.00053241133,0.000038445458,0.00023587167,0.00013714186,0.00037721443,0.002295586,0.0063584372,0.42688575,0.5618274],"study_design_scores_gemma":[0.000040630486,0.000103789804,0.0005157994,0.00026111002,0.0000114745935,0.00027598577,0.00011895963,0.00016436841,0.00025332283,0.00049539405,0.9977411,0.00001802429],"about_ca_topic_score_codex":0.00453326,"about_ca_topic_score_gemma":0.0035943864,"teacher_disagreement_score":0.011641681,"about_ca_system_score_codex":0.0011484441,"about_ca_system_score_gemma":0.0010850049,"threshold_uncertainty_score":0.016605437},"labels":[],"label_agreement":null},{"id":"W4406411662","doi":"10.1016/j.combustflame.2024.113948","title":"Hypergolic ignition of hybrid rocket fuels in a slab burner experiment","year":2025,"lang":"en","type":"article","venue":"Combustion and Flame","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Polytechnique Montréal","funders":"","keywords":"Combustor; Ignition system; Rocket (weapon); Aerospace engineering; Environmental science; Slab; Nuclear engineering; Combustion; Aeronautics; Engineering; Chemistry; Structural engineering","score_opus":0.013133562827734271,"score_gpt":0.26032951370097523,"score_spread":0.24719595087324098,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4406411662","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":[0.99681133,0.00010832156,0.0021694836,0.000011454524,0.0000057990605,0.000014201923,0.00009309368,0.000067116205,0.0007192079],"genre_scores_gemma":[0.99646795,0.00011033701,0.0020927258,0.000013635662,0.0000021598692,0.000016506738,0.000108455184,0.000025247613,0.0011630728],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998858,0.0000052727837,0.0000044365784,0.000029542189,0.000049803522,0.000025111542],"domain_scores_gemma":[0.9998871,0.00003081424,0.000023272034,0.000014345348,0.000028403982,0.00001613491],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018652288,0.00022239199,0.0002556496,0.00023213682,0.00020274092,0.00021343367,0.00033222017,0.00028149947,0.0017658352],"category_scores_gemma":[0.00020309887,0.00011244974,0.00018652165,0.00018534694,0.0002461751,0.00033936018,0.00038760452,0.0004766519,0.00022670225],"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":[0.00030077825,0.00003315309,0.0006811821,0.000042634376,0.000008432365,0.00007436935,0.00005851927,0.00067072356,0.99569714,0.00011282702,0.000036087313,0.002284096],"study_design_scores_gemma":[0.000009870669,0.00039481904,0.0036745842,0.0000036533913,0.000006724115,0.000061592924,0.000048820435,0.004597554,0.99065876,0.00004577315,0.000488382,0.000009480777],"about_ca_topic_score_codex":0.0009707281,"about_ca_topic_score_gemma":0.0015153468,"teacher_disagreement_score":0.0017658352,"about_ca_system_score_codex":0.00034022622,"about_ca_system_score_gemma":0.00016460932,"threshold_uncertainty_score":0.0059073567},"labels":[],"label_agreement":null},{"id":"W4406513077","doi":"10.1016/s0967-0653(98)81121-6","title":"10.1016/s0967-0653(98)81121-6","year":2000,"lang":"en","type":"article","venue":"Time to knit","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Geology","score_opus":0.010111982514829927,"score_gpt":0.19659215416533257,"score_spread":0.18648017165050265,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4406513077","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0004526255,0.00035484708,0.0007383506,0.00037399807,0.00033562302,0.00010761502,0.000610508,0.000877279,0.9961492],"genre_scores_gemma":[0.00046568786,0.00016512233,0.00025579575,0.00015985184,0.000054577322,0.00004442881,0.00027952853,0.00013355956,0.9984413],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9993185,0.00004062818,0.000051308114,0.00027283013,0.00016895361,0.00014776461],"domain_scores_gemma":[0.997858,0.00048633723,0.00013260831,0.0002508528,0.00059994526,0.00067214906],"candidate_categories":["insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.001114847,0.0029469472,0.0019301956,0.002774771,0.0027437794,0.0044831014,0.0036283405,0.006129401,0.9890377],"category_scores_gemma":[0.0015258532,0.0011129619,0.0015515656,0.002625727,0.0024142805,0.0056132404,0.0031169222,0.0028332705,0.9936407],"study_design_candidate":"not_applicable","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":[0.0004177249,0.00021581391,0.0008446479,0.00066065096,0.000046712015,0.0002781645,0.00014587784,0.0004082922,0.0027442332,0.0065605952,0.43042654,0.55725086],"study_design_scores_gemma":[0.00004981,0.00012140022,0.00051016756,0.0003047005,0.000014266342,0.00032285549,0.0001248115,0.00018891391,0.0003290365,0.00052214804,0.9974899,0.000021900743],"about_ca_topic_score_codex":0.00394853,"about_ca_topic_score_gemma":0.0032440047,"teacher_disagreement_score":0.010962307,"about_ca_system_score_codex":0.0012360694,"about_ca_system_score_gemma":0.0010990215,"threshold_uncertainty_score":0.015636384},"labels":[],"label_agreement":null},{"id":"W4406784137","doi":"10.23967/eccomas.2024.288","title":"One-Shot Optimization for the Inverse Design of a Quasi 1-D De Laval Nozzle","year":2024,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Nozzle; Shot (pellet); Inverse; Computer science; One shot; Mechanical engineering; Physics; Mathematics; Engineering; Materials science; Geometry","score_opus":0.11377546989348448,"score_gpt":0.32014683914687003,"score_spread":0.20637136925338556,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4406784137","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":[0.044168286,0.00032510847,0.9393893,0.00026093918,0.000066080036,0.00008077746,0.000059760194,0.000240421,0.015409264],"genre_scores_gemma":[0.7898481,0.00024074911,0.20049194,0.00012580214,0.000035035853,0.00020366124,0.000083475024,0.00011712716,0.008854114],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99983907,0.000043040196,0.0000044328985,0.000026416848,0.000061198945,0.000025842386],"domain_scores_gemma":[0.999754,0.00014270627,0.00002722415,0.000012181677,0.000048634138,0.000015305279],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006232487,0.0006319718,0.0009915328,0.00030399245,0.00043643778,0.0009854533,0.0006167564,0.0015166518,0.0032111623],"category_scores_gemma":[0.0009933984,0.000605765,0.0006001956,0.0002064904,0.00062352256,0.0005464697,0.00075691275,0.0007524313,0.00040906784],"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":[0.00007750798,0.000028484297,0.00020639645,0.00009379737,0.000015824655,0.00005364435,0.000056178924,0.979042,0.005565229,0.0056650923,0.00035615475,0.008839703],"study_design_scores_gemma":[0.000009188489,0.00004310398,0.00006096144,0.0000042693214,0.0000031111704,0.000010779243,0.000011663925,0.9983896,0.0005284339,0.0005439238,0.00039034433,0.000004675991],"about_ca_topic_score_codex":0.003927561,"about_ca_topic_score_gemma":0.003223779,"teacher_disagreement_score":0.003927561,"about_ca_system_score_codex":0.00066919933,"about_ca_system_score_gemma":0.0012579454,"threshold_uncertainty_score":0.010742426},"labels":[],"label_agreement":null},{"id":"W4407013948","doi":"10.52202/078371-0218","title":"Supercavitating Liquid Oxygen and JET-A Pump Analysis for a 35 KN Rocket Engine Turbopump","year":2024,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Concordia University","funders":"","keywords":"Supercavitation; Rocket engine; Liquid oxygen; Liquid-propellant rocket; Rocket (weapon); Jet (fluid); Aerospace engineering; Mechanics; Engineering; Oxygen; Physics; Propellant; Cavitation","score_opus":0.023051358161453688,"score_gpt":0.2820460097843241,"score_spread":0.2589946516228704,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4407013948","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":[0.99481684,0.00004140358,0.0026799932,0.00003328004,0.0000052094597,0.00000851201,0.00006416474,0.0000854111,0.002265095],"genre_scores_gemma":[0.9982394,0.000026422971,0.00054716866,0.000004419117,0.0000014018921,0.000004296894,0.000033808457,0.000012325686,0.0011306992],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999218,0.000004651187,0.0000031511297,0.0000127369685,0.00003884321,0.000018841045],"domain_scores_gemma":[0.9998739,0.000045035613,0.000013827111,0.000007234831,0.000045189332,0.0000148302215],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00011865879,0.0001819286,0.00037184742,0.00035654413,0.0005643715,0.00046677553,0.00040417816,0.00036590436,0.0016254537],"category_scores_gemma":[0.00028531603,0.00015644754,0.00035259218,0.00026310058,0.0004472937,0.00037560755,0.00028188486,0.00020118708,0.00017588808],"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":[0.0013713337,0.00018242882,0.014017694,0.00012945519,0.00006483506,0.0008190724,0.00033624892,0.26798972,0.68976706,0.0025994952,0.0008586012,0.021864131],"study_design_scores_gemma":[0.000048235215,0.0005574826,0.023917686,0.000012765443,0.00005215346,0.00011692392,0.00034852352,0.8431424,0.12958145,0.0003176646,0.0018638652,0.00004088859],"about_ca_topic_score_codex":0.016202606,"about_ca_topic_score_gemma":0.011165842,"teacher_disagreement_score":0.016202606,"about_ca_system_score_codex":0.0006774844,"about_ca_system_score_gemma":0.000772987,"threshold_uncertainty_score":0.03221655},"labels":[],"label_agreement":null},{"id":"W4407016578","doi":"10.52202/078371-0008","title":"Design and Development of the Largest Student-Built Liquid Rocket Engine for Suborbital Flight: A Comprehensive Overview and Lessons Learned","year":2024,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Concordia University","funders":"","keywords":"Aeronautics; Aerospace engineering; Liquid-propellant rocket; Rocket (weapon); Rocket engine; Engineering; Systems engineering; Computer science; Propellant","score_opus":0.14162506977043626,"score_gpt":0.37080293354200483,"score_spread":0.22917786377156857,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4407016578","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":[0.18552838,0.012384447,0.71243906,0.0014733633,0.00080893637,0.0012726939,0.00064566586,0.0046625407,0.080784984],"genre_scores_gemma":[0.45478573,0.007676264,0.4781633,0.00041317084,0.00013074405,0.0004769438,0.0016839782,0.001712294,0.05495758],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9990213,0.00007148157,0.000042062344,0.000120671466,0.0005993212,0.00014525901],"domain_scores_gemma":[0.9991861,0.000047621394,0.00005373123,0.00007527146,0.00049531006,0.0001420013],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0016103642,0.0009244741,0.0006920258,0.0007911202,0.0005343321,0.0018271209,0.0018397035,0.00095983606,0.003219153],"category_scores_gemma":[0.0011611837,0.00048568446,0.00089708844,0.00037077325,0.00040955184,0.0014886056,0.001013968,0.0014400719,0.0029217766],"study_design_candidate":"not_applicable","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":[0.00052229146,0.0006062722,0.010865892,0.0024425685,0.00021664478,0.0007656006,0.00093129923,0.07971202,0.24996993,0.0148310745,0.012136228,0.6270001],"study_design_scores_gemma":[0.00021117042,0.0049944874,0.010889169,0.0006618378,0.0003231932,0.001862549,0.0006633866,0.09755434,0.29918754,0.0038974525,0.5794818,0.00027308727],"about_ca_topic_score_codex":0.0018294704,"about_ca_topic_score_gemma":0.0038422993,"teacher_disagreement_score":0.003219153,"about_ca_system_score_codex":0.0009234666,"about_ca_system_score_gemma":0.0029567794,"threshold_uncertainty_score":0.010769129},"labels":[],"label_agreement":null},{"id":"W4407017330","doi":"10.52202/078380-0008","title":"Regulation of Rocket Fuel Emissions in Light of SDGs and Space30 Agenda","year":2024,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Bombardier (Canada)","funders":"","keywords":"Rocket (weapon); Environmental science; Aerospace engineering; Aeronautics; Astrobiology; Engineering; Physics","score_opus":0.021258842855105226,"score_gpt":0.27980997616869374,"score_spread":0.25855113331358853,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4407017330","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.109219566,0.0184464,0.03748182,0.15794505,0.010764652,0.00037653773,0.0026539406,0.0007821271,0.6623299],"genre_scores_gemma":[0.7668632,0.011789946,0.022513317,0.056762975,0.0027590806,0.0005471491,0.0016584025,0.00018646693,0.13691945],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"not_applicable","domain_scores_codex":[0.99679166,0.00042335023,0.0001173493,0.00037634824,0.0016560627,0.0006351501],"domain_scores_gemma":[0.9968935,0.00061969337,0.00031761706,0.00016908327,0.0016577237,0.0003423765],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0040424736,0.0006197864,0.00048034464,0.00093298394,0.0011130129,0.0038483301,0.0017423069,0.0042611067,0.010429562],"category_scores_gemma":[0.0042253872,0.00022111554,0.00084989646,0.0006483677,0.0015608141,0.0020367594,0.0024355692,0.0044529624,0.0011163657],"study_design_candidate":"not_applicable","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":[0.00044441613,0.00043048582,0.005821688,0.00072130904,0.00011208495,0.00051237474,0.0008597249,0.011738798,0.026029987,0.81684816,0.06059703,0.07588399],"study_design_scores_gemma":[0.00008644317,0.00051949645,0.01611336,0.00095935015,0.0000635728,0.00017273976,0.0014000364,0.005721586,0.016390001,0.14757155,0.8109025,0.00009943174],"about_ca_topic_score_codex":0.023748362,"about_ca_topic_score_gemma":0.031558458,"teacher_disagreement_score":0.023748362,"about_ca_system_score_codex":0.003836731,"about_ca_system_score_gemma":0.0105894115,"threshold_uncertainty_score":0.04722029},"labels":[],"label_agreement":null},{"id":"W4407397302","doi":"10.2514/6.2025-2789","title":"Analytical Modeling of Regression Rates in Lattice-Protrusion Augmented Hybrid Rocket Fuels","year":2025,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","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":"University of Calgary","funders":"","keywords":"Regression analysis; Regression; Rocket (weapon); Lattice (music); Environmental science; Materials science; Computer science; Aerospace engineering; Statistics; Engineering; Mathematics; Physics; Acoustics; Machine learning","score_opus":0.03437724076741056,"score_gpt":0.32816656440974584,"score_spread":0.2937893236423353,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4407397302","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":[0.7143922,0.0005770955,0.27252433,0.00018850752,0.000039258808,0.00007034399,0.00041344555,0.0006263936,0.011168461],"genre_scores_gemma":[0.9875501,0.00022655225,0.0086958,0.000012458223,0.0000031908337,0.000041921623,0.00008378717,0.000036346493,0.003349907],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999037,0.000011770304,0.0000047882168,0.000021459504,0.00003956047,0.000018751685],"domain_scores_gemma":[0.9997254,0.0001362005,0.00004941877,0.000018289391,0.00006051537,0.0000100750985],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00022704531,0.00041382905,0.00033941632,0.00032495035,0.0001859674,0.0005043559,0.0007883193,0.00071712467,0.0010874439],"category_scores_gemma":[0.0007328528,0.00029192897,0.0004383664,0.00026764686,0.0003974142,0.0005679931,0.00026825257,0.00055356213,0.00029537978],"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":[0.00003214418,0.00002466489,0.0007726767,0.000031202726,0.0000049641585,0.00007791889,0.000034261124,0.9820702,0.012926673,0.0012435163,0.00008113665,0.0027006695],"study_design_scores_gemma":[7.8832306e-7,0.0000051266475,0.00006223239,0.0000010734402,6.608343e-7,0.0000042999036,0.0000028024974,0.9983119,0.0014934052,0.000057496636,0.000058486014,0.000001788058],"about_ca_topic_score_codex":0.0073529542,"about_ca_topic_score_gemma":0.004575536,"teacher_disagreement_score":0.0073529542,"about_ca_system_score_codex":0.0007015303,"about_ca_system_score_gemma":0.00051006465,"threshold_uncertainty_score":0.014620304},"labels":[],"label_agreement":null},{"id":"W4407412552","doi":"10.2514/6.2025-2470","title":"Novel Use of Non-Combustible Propellant Analogs for Rapid, Safe, and Low-Cost Cryogenic Bipropellant Rocket Engine Testing","year":2025,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","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":"Concordia University","funders":"","keywords":"Propellant; Rocket (weapon); Rocket propellant; Rocket engine; Liquid-propellant rocket; Automotive engineering; Aerospace engineering; Waste management; Materials science; Aeronautics; Nuclear engineering; Engineering","score_opus":0.054819022869071,"score_gpt":0.2744929899222721,"score_spread":0.2196739670532011,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4407412552","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":[0.8981781,0.0011548776,0.08409361,0.00019453722,0.00012514426,0.0004472993,0.00012936267,0.0009229953,0.014754053],"genre_scores_gemma":[0.9535117,0.00037535327,0.04169214,0.00012110504,0.000021779884,0.00011914099,0.00017277888,0.00009092876,0.0038948983],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99920183,0.000088903216,0.00004061108,0.000101959246,0.0005037973,0.00006284325],"domain_scores_gemma":[0.9993876,0.00009853093,0.00019547304,0.000116604235,0.00015144984,0.000050270475],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005321083,0.000461687,0.00019877825,0.0004879118,0.00028197005,0.00046915334,0.0009845805,0.00037927862,0.0014316256],"category_scores_gemma":[0.00090139307,0.00024741705,0.00022524898,0.00013514074,0.00050391693,0.0011328544,0.0007690342,0.0005384068,0.0004416885],"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":[0.00024344772,0.00009401666,0.0009441537,0.0001164126,0.00000797799,0.00031125473,0.00009890575,0.0007317829,0.9725433,0.0009899111,0.00015264368,0.023766177],"study_design_scores_gemma":[0.000020504667,0.0011796713,0.0013165569,0.00001633249,0.0000096834565,0.0007070313,0.000044160643,0.0026335095,0.9888598,0.000117680094,0.005076174,0.000018994342],"about_ca_topic_score_codex":0.00031751848,"about_ca_topic_score_gemma":0.00066724734,"teacher_disagreement_score":0.0014316256,"about_ca_system_score_codex":0.00029651573,"about_ca_system_score_gemma":0.00036544696,"threshold_uncertainty_score":0.004789233},"labels":[],"label_agreement":null},{"id":"W4407412763","doi":"10.2514/6.2025-0962","title":"Design of a Kerosene/Nitrous Oxide Liquid Rocket Engine: M-420 \"Swordfish\"","year":2025,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":1,"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":"Nitrous oxide; Kerosene; Swordfish; Environmental science; Rocket (weapon); Automotive engineering; Aerospace engineering; Waste management; Chemistry; Engineering","score_opus":0.016973899992317996,"score_gpt":0.25473423220206665,"score_spread":0.23776033220974865,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4407412763","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":[0.26581568,0.0009398924,0.6778927,0.00036353627,0.0002122488,0.001233549,0.00045729437,0.0019386603,0.05114644],"genre_scores_gemma":[0.8697229,0.00049315667,0.107665546,0.00007819793,0.000023347538,0.0006059085,0.00029838085,0.00009211649,0.021020478],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99984336,0.000012298016,0.000009779376,0.000037966056,0.00007199842,0.000024583007],"domain_scores_gemma":[0.9999399,0.0000045611723,0.00001274658,0.000004748246,0.000020707765,0.000017327166],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025545855,0.0005186395,0.00061269297,0.00039280026,0.00043606973,0.0007624908,0.0012420127,0.0006952851,0.0033067018],"category_scores_gemma":[0.000116532334,0.00032525996,0.00048247335,0.00018690048,0.0003206955,0.0002863715,0.00061524374,0.00031304648,0.0011703599],"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":[0.0007735,0.0002568378,0.0041695433,0.0012663278,0.00014690221,0.0011017439,0.0001628546,0.47964388,0.37219885,0.015983317,0.0033545054,0.12094172],"study_design_scores_gemma":[0.00032564852,0.0017291994,0.00356809,0.0000721813,0.00013104518,0.0005359378,0.000108313056,0.85410947,0.10397593,0.0012852673,0.034065828,0.000093021685],"about_ca_topic_score_codex":0.0024970532,"about_ca_topic_score_gemma":0.001885025,"teacher_disagreement_score":0.0033067018,"about_ca_system_score_codex":0.0005475881,"about_ca_system_score_gemma":0.0015785234,"threshold_uncertainty_score":0.011062086},"labels":[],"label_agreement":null},{"id":"W4407415641","doi":"10.2514/6.2025-0128","title":"Experimental Design, Fabrication and Validation of a Small-Scale Liquid Bi-Propellant Rocket Engine","year":2025,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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; Liquid-propellant rocket; Fabrication; Aerospace engineering; Scale (ratio); Rocket engine; Rocket (weapon); Rocket propellant; Computer science; Materials science; Automotive engineering; Engineering; Physics","score_opus":0.030583764159653658,"score_gpt":0.2741062554310805,"score_spread":0.24352249127142686,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4407415641","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":[0.8779457,0.00063687935,0.110321105,0.00014448036,0.00024125862,0.0018154132,0.0011031934,0.0011088228,0.0066831517],"genre_scores_gemma":[0.85258037,0.0005610769,0.13860595,0.00009349243,0.00002655934,0.00182952,0.00081475166,0.0001560214,0.005332345],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99908364,0.000053390246,0.00005780145,0.00018731387,0.00050995324,0.000107876775],"domain_scores_gemma":[0.99924207,0.00008438681,0.0001424255,0.00015331012,0.00029253092,0.000085228916],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0012953392,0.0006623697,0.0005442249,0.0006001427,0.0005734002,0.0005093053,0.0010838463,0.0008008258,0.0027176025],"category_scores_gemma":[0.0008558884,0.0003280187,0.0004977605,0.00032904948,0.0004226533,0.00045250024,0.00069627014,0.00067739794,0.0010778301],"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":[0.00019427587,0.00027145637,0.00086746993,0.00046104693,0.000016606326,0.0003334393,0.00010152875,0.0053775925,0.9830488,0.00046007865,0.00026630596,0.0086014075],"study_design_scores_gemma":[0.000057360754,0.0025272972,0.0039706156,0.000027287271,0.000037902293,0.00020543771,0.00009692223,0.014489613,0.96934354,0.00011612346,0.009087157,0.00004077639],"about_ca_topic_score_codex":0.000719951,"about_ca_topic_score_gemma":0.0011999849,"teacher_disagreement_score":0.0027176025,"about_ca_system_score_codex":0.00039106418,"about_ca_system_score_gemma":0.00069520395,"threshold_uncertainty_score":0.009091318},"labels":[],"label_agreement":null},{"id":"W4408208341","doi":"10.53555/sfs.v9i3.3421","title":"Advancement of Turbofan Engines Using Composites","year":2022,"lang":"en","type":"article","venue":"Journal of Survey in Fisheries Sciences","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Turbofan; Composite material; Automotive engineering; Materials science; Engineering","score_opus":0.2249714145753667,"score_gpt":0.3140367976589749,"score_spread":0.0890653830836082,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4408208341","genre_codex":"review","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":[0.16176753,0.72345084,0.026698798,0.0010603347,0.0018006937,0.0000858842,0.00021966257,0.00027722333,0.08463903],"genre_scores_gemma":[0.46291375,0.49997133,0.017565545,0.0003353712,0.0005358465,0.000059973667,0.00031313565,0.00007148383,0.018233627],"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998267,0.000014441416,0.000012790458,0.000024439167,0.000098160424,0.000023456116],"domain_scores_gemma":[0.9999161,0.000014645851,0.000017057053,0.0000057077223,0.000037818947,0.000008715597],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00033495712,0.0005353173,0.00034819724,0.001121036,0.00030781436,0.00065041194,0.0002867808,0.00047004054,0.002068787],"category_scores_gemma":[0.00019819687,0.00017503148,0.00074625615,0.000526641,0.0001693434,0.0010004229,0.00034580877,0.0005928786,0.0009167473],"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":[0.00018175521,0.00016323646,0.0020922578,0.009921781,0.00013782312,0.0008415946,0.00018946563,0.0044349725,0.47294027,0.013182748,0.002953651,0.49296042],"study_design_scores_gemma":[0.00001621239,0.001123606,0.0067938115,0.0014963856,0.00023775092,0.0027593428,0.00019691135,0.0032776773,0.432857,0.0025688342,0.5486021,0.00007036743],"about_ca_topic_score_codex":0.000510042,"about_ca_topic_score_gemma":0.001409963,"teacher_disagreement_score":0.002068787,"about_ca_system_score_codex":0.00032739385,"about_ca_system_score_gemma":0.00048053285,"threshold_uncertainty_score":0.006920755},"labels":[],"label_agreement":null},{"id":"W4408646148","doi":"10.5539/mer.v13n1p1","title":"Disruptive ROVA Electropneumatic Valve Technology for Satellite-Delivering Rocket Applications","year":2025,"lang":"en","type":"article","venue":"Mechanical Engineering Research","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"","keywords":"Rocket (weapon); Satellite; Aerospace engineering; Engineering; Aeronautics; Mechanical engineering; Computer science","score_opus":0.026488522593669246,"score_gpt":0.3446298296153097,"score_spread":0.31814130702164045,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4408646148","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":[0.27786294,0.010003097,0.65802115,0.0014025263,0.0012030837,0.00032650775,0.00023687999,0.0035539407,0.047389876],"genre_scores_gemma":[0.8557496,0.0026115566,0.1125348,0.00031345626,0.0002414292,0.00016113019,0.00017863573,0.00020985457,0.027999457],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9995295,0.00003393871,0.000028418635,0.000075384996,0.00029160327,0.00004111691],"domain_scores_gemma":[0.99970895,0.00004078928,0.00010406267,0.000033896154,0.00008195242,0.00003032133],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025533777,0.00033912554,0.00022631565,0.0003391768,0.00025515817,0.00066590187,0.0008880723,0.0005947971,0.0018130098],"category_scores_gemma":[0.0004465222,0.00023185326,0.00026918796,0.00012635849,0.00032740884,0.0010002899,0.0004978853,0.0005392385,0.0012833073],"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":[0.00009972331,0.000047962803,0.0006539519,0.00028314156,0.000010295664,0.00034628794,0.00014007853,0.0013591282,0.9184964,0.004924336,0.0017727168,0.07186602],"study_design_scores_gemma":[0.000052591135,0.0016865458,0.0048707435,0.000072807445,0.000044043358,0.0044719987,0.0001031548,0.02425181,0.7492508,0.0010335534,0.21408246,0.000079367615],"about_ca_topic_score_codex":0.0002795383,"about_ca_topic_score_gemma":0.00039653268,"teacher_disagreement_score":0.0018130098,"about_ca_system_score_codex":0.00036628425,"about_ca_system_score_gemma":0.00031404072,"threshold_uncertainty_score":0.00606519},"labels":[],"label_agreement":null},{"id":"W4409238878","doi":"10.56028/aetr.13.1.447.2025","title":"Optimization design of micro Laval nozzle under viscous force","year":2025,"lang":"en","type":"article","venue":"Advances in Engineering Technology Research","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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; Mechanics; Mechanical engineering; Aerospace engineering; Materials science; Aeronautics; Engineering; Physics","score_opus":0.02053050947766218,"score_gpt":0.33352258576218197,"score_spread":0.3129920762845198,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4409238878","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":[0.22353978,0.0015035259,0.74289745,0.00020127305,0.00008833329,0.00018614679,0.00010629453,0.00046610096,0.03101112],"genre_scores_gemma":[0.9331302,0.00068269094,0.061327547,0.00003360527,0.000021368838,0.00023668661,0.00006567882,0.000071227296,0.004431013],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99978083,0.00003118022,0.000008616802,0.000046887475,0.00009311704,0.000039449224],"domain_scores_gemma":[0.9998398,0.0000552433,0.000034310637,0.0000065209106,0.000052901523,0.000011126324],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00037595574,0.0005385322,0.0007240422,0.00038692722,0.00039379948,0.0009323001,0.0005101137,0.00058828684,0.001496387],"category_scores_gemma":[0.00044767268,0.00043038226,0.00052355754,0.00037019508,0.00029755195,0.000426059,0.00034160525,0.0002656081,0.00023159986],"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":[0.00016079574,0.00006128917,0.0014676499,0.00037480608,0.000035031688,0.00015691013,0.000133018,0.88673097,0.06308638,0.0059764385,0.0010144435,0.040802196],"study_design_scores_gemma":[0.000025028798,0.00014262849,0.0007843532,0.000009677282,0.000018897952,0.00003070449,0.000035367862,0.99017835,0.00664188,0.0004694021,0.001648944,0.000014768498],"about_ca_topic_score_codex":0.0024572264,"about_ca_topic_score_gemma":0.0015471611,"teacher_disagreement_score":0.0024572264,"about_ca_system_score_codex":0.0005297377,"about_ca_system_score_gemma":0.0010462352,"threshold_uncertainty_score":0.005005896},"labels":[],"label_agreement":null},{"id":"W4409273091","doi":"10.1016/j.applthermaleng.2025.126442","title":"Development of an additively manufactured vapor chamber using hybrid wick structures","year":2025,"lang":"en","type":"article","venue":"Applied Thermal Engineering","topic":"Rocket and propulsion systems research","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":"Canadian Institute for Energy Training","funders":"Ministerium für Wissenschaft, Forschung und Kunst Baden-Württemberg","keywords":"Materials science; Mechanical engineering; Composite material; Process engineering; Engineering drawing; Mechanics; Engineering; Physics","score_opus":0.014008802403759901,"score_gpt":0.2432631474530079,"score_spread":0.229254345049248,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4409273091","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":[0.6837995,0.0026716979,0.29635912,0.00023514092,0.0008008408,0.0006289256,0.0008965763,0.004871836,0.00973651],"genre_scores_gemma":[0.760532,0.0007826383,0.23303358,0.000060360544,0.000055600267,0.00018529783,0.00041085665,0.00035137386,0.004588239],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99931943,0.00005051593,0.00003888717,0.0001167476,0.00040120917,0.00007321055],"domain_scores_gemma":[0.99925345,0.00012691734,0.0001859287,0.00016853756,0.00019109834,0.000074097894],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000533748,0.00061712565,0.00037935725,0.0004998868,0.00026145668,0.00079546386,0.0009896891,0.0006076238,0.0012344968],"category_scores_gemma":[0.0009439654,0.00043810508,0.0006055967,0.00025675027,0.00032340104,0.0006880574,0.0005092674,0.0004695755,0.0007557199],"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":[0.000035515877,0.000039190272,0.00040695243,0.00026438644,0.000021934244,0.00038532473,0.000067549416,0.0025973902,0.9802744,0.00075509143,0.00031193154,0.014840229],"study_design_scores_gemma":[0.000006533722,0.0002493895,0.00062223803,0.000011070948,0.00001537826,0.0003600046,0.000014129755,0.0059889234,0.9859642,0.000048543367,0.006694929,0.000024635021],"about_ca_topic_score_codex":0.00057238044,"about_ca_topic_score_gemma":0.0007953959,"teacher_disagreement_score":0.0012344968,"about_ca_system_score_codex":0.00041100194,"about_ca_system_score_gemma":0.0005284922,"threshold_uncertainty_score":0.004129827},"labels":[],"label_agreement":null},{"id":"W4409310219","doi":"10.1007/978-3-031-83721-0_5","title":"Conversion Technologies for Green Aviation Fuels","year":2025,"lang":"en","type":"book-chapter","venue":"Sustainable aviation","topic":"Rocket and propulsion systems research","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":"Dalhousie University","funders":"","keywords":"Aviation; Aeronautics; Environmental science; Business; Engineering; Aerospace engineering","score_opus":0.011763515333252995,"score_gpt":0.24066849534396287,"score_spread":0.22890498001070989,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4409310219","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0017087025,0.05738857,0.017192379,0.0008989609,0.0020547064,0.000051065388,0.00014445261,0.00019543618,0.9203658],"genre_scores_gemma":[0.010458214,0.04492404,0.0056717643,0.00042976023,0.00028960334,0.00004873071,0.00016924035,0.00015128218,0.9378574],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.99981004,0.000014532358,0.000003828458,0.000025617168,0.00012738783,0.000018590395],"domain_scores_gemma":[0.99996066,0.000013893798,0.0000022169968,0.000006699036,0.0000134188585,0.0000030425592],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012761368,0.00092463003,0.00044048345,0.0011423723,0.00072307745,0.002086293,0.00083241926,0.0008274076,0.049838167],"category_scores_gemma":[0.00016807018,0.00036515115,0.00040047764,0.0015364146,0.0005998317,0.0026919574,0.00097321864,0.0018755944,0.016356869],"study_design_candidate":"not_applicable","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":[0.000026976499,0.000107623484,0.00005192473,0.0010109688,0.000012753264,0.00017068756,0.00025223437,0.0020740589,0.018148674,0.3844445,0.16071936,0.43298027],"study_design_scores_gemma":[0.000001959891,0.0000126402165,0.00007647821,0.00020710549,0.0000037832474,0.00013116041,0.000068966096,0.0007388853,0.0050118454,0.031285755,0.9624544,0.000006905768],"about_ca_topic_score_codex":0.0013442438,"about_ca_topic_score_gemma":0.0044297045,"teacher_disagreement_score":0.049838167,"about_ca_system_score_codex":0.0010691743,"about_ca_system_score_gemma":0.00050603406,"threshold_uncertainty_score":0.16672528},"labels":[],"label_agreement":null},{"id":"W4409729140","doi":"10.11159/csp25.127","title":"Advancing Industrial Smokeless Flaring: Experimental Study into a Swirl Air-Assist Burner","year":2025,"lang":"en","type":"article","venue":"Proceedings of the World Congress on Momentum, Heat and Mass Transfer","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"Division of Materials Research; Natural Sciences and Engineering Research Council of Canada; Bundesanstalt für Materialforschung und -Prüfung","keywords":"Combustor; Environmental science; Automotive engineering; Combustion; Engineering; Chemistry","score_opus":0.014913816589615282,"score_gpt":0.26792877308475144,"score_spread":0.25301495649513617,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4409729140","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":[0.9969753,0.000048092228,0.0024991883,0.000011516131,0.000006989118,0.000040677627,0.000031290063,0.000055271157,0.00033156053],"genre_scores_gemma":[0.994611,0.00005783295,0.0044025574,0.000014979304,0.000004585107,0.00002701237,0.000045181197,0.00001634112,0.0008205133],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99971396,0.000031084437,0.000015194822,0.00006356228,0.00011868385,0.000057530837],"domain_scores_gemma":[0.9996873,0.00007568073,0.00003998407,0.000056710578,0.00009449218,0.000045767178],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00062819396,0.0004649661,0.0005487875,0.00025466844,0.000515819,0.00028946705,0.000812928,0.0007213551,0.0013173291],"category_scores_gemma":[0.0005736128,0.00021233961,0.00035617946,0.00017636098,0.0003791286,0.00047877006,0.0004363552,0.00047390896,0.00028010306],"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":[0.0007527483,0.00083838427,0.001969527,0.00016714726,0.000013295898,0.00013123656,0.00022319856,0.002875253,0.9846852,0.000074259195,0.00006051658,0.008209175],"study_design_scores_gemma":[0.00012449232,0.006374396,0.009040618,0.000011982196,0.00003162855,0.00010081205,0.00016816847,0.012463512,0.97076315,0.000044810524,0.00085098145,0.000025438114],"about_ca_topic_score_codex":0.00090053247,"about_ca_topic_score_gemma":0.0015458482,"teacher_disagreement_score":0.0013173291,"about_ca_system_score_codex":0.00023344524,"about_ca_system_score_gemma":0.00022915292,"threshold_uncertainty_score":0.0044068694},"labels":[],"label_agreement":null},{"id":"W4410412446","doi":"10.21203/rs.3.rs-6603661/v1","title":"Decarbonization of Helicopters: Challenges for the Engine Manufacturer of Compatibility with Saf 100% Drop-In","year":2025,"lang":"en","type":"preprint","venue":"Research Square","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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":"Compatibility (geochemistry); Drop (telecommunication); Business; Automotive engineering; Manufacturing engineering; Materials science; Engineering; Mechanical engineering; Composite material","score_opus":0.10173776994616206,"score_gpt":0.3922688710269631,"score_spread":0.29053110108080105,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4410412446","genre_codex":"empirical","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"other","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.57708526,0.010904807,0.07174887,0.029874114,0.004566158,0.00071400433,0.0038242983,0.0039511453,0.2973314],"genre_scores_gemma":[0.9451771,0.0037746874,0.019486876,0.0020740032,0.0001983763,0.00008476527,0.0017992182,0.00058671227,0.026818214],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9975682,0.00022870954,0.00010009815,0.00018841359,0.0015366443,0.00037782054],"domain_scores_gemma":[0.9965327,0.0002013696,0.00016876662,0.00047600927,0.0024231565,0.00019793012],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0038846608,0.00071988243,0.0007278541,0.0007709343,0.0013019162,0.0027699643,0.0015728291,0.001409477,0.010689839],"category_scores_gemma":[0.0036087928,0.00028781453,0.00046787763,0.00077764795,0.00078225636,0.0041070613,0.0017088433,0.0021268234,0.0031926301],"study_design_candidate":"not_applicable","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":[0.0020366232,0.0009271413,0.022398671,0.0018323038,0.00016002197,0.0015456431,0.0015091142,0.024406016,0.2746594,0.050591134,0.09102775,0.5289062],"study_design_scores_gemma":[0.00016490555,0.002318581,0.018452983,0.0009404583,0.00011614488,0.00080695684,0.0034317095,0.027309239,0.3412919,0.019321822,0.58570725,0.0001380697],"about_ca_topic_score_codex":0.0050638574,"about_ca_topic_score_gemma":0.0068127303,"teacher_disagreement_score":0.010689839,"about_ca_system_score_codex":0.0016849283,"about_ca_system_score_gemma":0.0024067287,"threshold_uncertainty_score":0.035761},"labels":[],"label_agreement":null},{"id":"W4411184387","doi":"10.2514/1.b39865","title":"Regression Rates of Protrusion and Lattice Augmented Fuel Grains in Hybrid Rockets","year":2025,"lang":"en","type":"article","venue":"Journal of Propulsion and Power","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Calgary","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Materials science; Aerospace engineering; Lattice (music); Chamber pressure; Engineering; Physics; Acoustics; Metallurgy","score_opus":0.014553767736339979,"score_gpt":0.3041416096605272,"score_spread":0.28958784192418724,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4411184387","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":[0.99750596,0.00020006445,0.0014662694,0.0000073547776,0.000008204863,0.000008363179,0.000088984714,0.00008559012,0.0006293269],"genre_scores_gemma":[0.99803406,0.00009140647,0.0009798046,0.0000039622964,0.000001501234,0.0000073670976,0.000110101624,0.000023784685,0.00074802944],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998498,0.000009064329,0.000008575488,0.00004115696,0.00005691633,0.000034382418],"domain_scores_gemma":[0.9997774,0.000065236665,0.000060529885,0.000023604407,0.00005096058,0.000022187553],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001940016,0.00022405718,0.00020402369,0.00032141295,0.000102336824,0.00037881825,0.0003286206,0.00017971997,0.0012213745],"category_scores_gemma":[0.0005496101,0.00014935754,0.00018491922,0.0002169032,0.00018399305,0.00044663862,0.00024576727,0.00030325228,0.00027460072],"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":[0.00048329786,0.00006326514,0.002909907,0.00010308696,0.000022250066,0.00015200522,0.00008859742,0.008624096,0.9752915,0.00044473237,0.00015874412,0.011658496],"study_design_scores_gemma":[0.000015047668,0.00043583417,0.0044932137,0.0000075869048,0.000013535006,0.00006621902,0.00006341458,0.020800076,0.9726952,0.000057682395,0.0013381402,0.000013991687],"about_ca_topic_score_codex":0.0010603485,"about_ca_topic_score_gemma":0.0017976108,"teacher_disagreement_score":0.0012213745,"about_ca_system_score_codex":0.00033339954,"about_ca_system_score_gemma":0.00008092881,"threshold_uncertainty_score":0.004085958},"labels":[],"label_agreement":null},{"id":"W4411554469","doi":"10.29169/1927-5129.2025.21.13","title":"Numerical Simulation of a Turboprop Engine Inlet with a Bypass Channel","year":2025,"lang":"en","type":"article","venue":"Journal of Basic & Applied Sciences","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"","funders":"National Science and Technology Major Project","keywords":"Turboprop; Inlet; Channel (broadcasting); Marine engineering; Environmental science; Mechanics; Engineering; Computer science; Aerospace engineering; Mechanical engineering; Physics; Electrical engineering","score_opus":0.018984256630767395,"score_gpt":0.27915824746483503,"score_spread":0.2601739908340676,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4411554469","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":[0.9689322,0.0002629333,0.01515354,0.00018776664,0.000094049596,0.000063974374,0.00041048825,0.00017088848,0.014724149],"genre_scores_gemma":[0.9942076,0.000106727806,0.003224716,0.000018563745,0.000005775447,0.00003589641,0.00012872332,0.000010485177,0.0022614896],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998499,0.000020457665,0.000008145144,0.000024361405,0.00003150316,0.0000656181],"domain_scores_gemma":[0.99965084,0.00014653512,0.00005042677,0.000018434064,0.00006649,0.00006725907],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020613472,0.0004714779,0.00069808133,0.00045082666,0.000912505,0.0010475212,0.000631007,0.001357627,0.0024562355],"category_scores_gemma":[0.00054630404,0.00028453098,0.0005117528,0.0005085216,0.0007648964,0.000402939,0.00065772823,0.0005272635,0.000181832],"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":[0.0001297695,0.00010097885,0.0040358542,0.000056287834,0.000014364742,0.00033210395,0.00006612585,0.9872458,0.004323112,0.0014793081,0.00028825787,0.0019279044],"study_design_scores_gemma":[0.000016082484,0.00005093262,0.0008192412,0.0000063620587,0.0000061048854,0.000016716438,0.00005197082,0.9978689,0.000804746,0.000109639484,0.0002417611,0.000007555456],"about_ca_topic_score_codex":0.024193866,"about_ca_topic_score_gemma":0.010628422,"teacher_disagreement_score":0.024193866,"about_ca_system_score_codex":0.0007413607,"about_ca_system_score_gemma":0.001504291,"threshold_uncertainty_score":0.048106074},"labels":[],"label_agreement":null},{"id":"W4411652933","doi":"10.2139/ssrn.5319351","title":"Optimization of Laval Nozzle Structure for Gas Mixture of Nh3-O2 Combustion Products and Co2-H2o by Response Surface Methodology","year":2025,"lang":"en","type":"preprint","venue":"SSRN Electronic Journal","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":false,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Nozzle; Combustion; Response surface methodology; Materials science; Surface (topology); Chemistry; Chemical engineering; Aerospace engineering; Engineering; Chromatography; Mathematics; Physical chemistry; Geometry","score_opus":0.021485668482999345,"score_gpt":0.2990467396877035,"score_spread":0.2775610712047042,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4411652933","genre_codex":"empirical","genre_gemma":"methods","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9657069,0.00065762026,0.03026173,0.00010885041,0.000035292815,0.000120970675,0.00024488074,0.00024916674,0.0026145745],"genre_scores_gemma":[0.98165256,0.00020534298,0.017352438,0.000019034482,0.0000050887716,0.00008106085,0.0001605412,0.000039760504,0.0004842029],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99982065,0.000021377571,0.000008593592,0.00004054917,0.000071380935,0.00003743949],"domain_scores_gemma":[0.9998778,0.000036960348,0.000028871103,0.000009388042,0.000038238224,0.000008760595],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003922771,0.0004291328,0.00041652884,0.00025885255,0.00023232614,0.0005171677,0.000474912,0.0004510513,0.00089663384],"category_scores_gemma":[0.00053543644,0.0001951165,0.00048370147,0.0002413798,0.00015592214,0.00033725216,0.0003117346,0.00038736552,0.00021400364],"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":[0.00051462225,0.0002785296,0.0018959811,0.0004298112,0.00002591065,0.00013633363,0.00006859281,0.049155455,0.9292866,0.00073534134,0.00031632083,0.017156547],"study_design_scores_gemma":[0.00012443538,0.0013173257,0.003796674,0.000014624917,0.000042535186,0.000051184907,0.00010852961,0.19545789,0.79701567,0.00017995707,0.0018592884,0.000031889085],"about_ca_topic_score_codex":0.0006626851,"about_ca_topic_score_gemma":0.0012940149,"teacher_disagreement_score":0.00089663384,"about_ca_system_score_codex":0.00043407778,"about_ca_system_score_gemma":0.00041292957,"threshold_uncertainty_score":0.0031493902},"labels":[],"label_agreement":null},{"id":"W4412479437","doi":"10.1515/rams-2025-0119","title":"Advances in the development and characterization of combustible cartridge cases and propellants: Preparation, performance, and future prospects","year":2025,"lang":"en","type":"article","venue":"REVIEWS ON ADVANCED MATERIALS SCIENCE","topic":"Rocket and propulsion systems research","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":"Ministry of Education and Child Care","funders":"Government of Jiangsu Province; National Natural Science Foundation of China","keywords":"Cartridge; Propellant; Characterization (materials science); Materials science; Process engineering; Chemical engineering; Nanotechnology; Aerospace engineering; Engineering; Metallurgy","score_opus":0.017588611287028474,"score_gpt":0.30087172059043815,"score_spread":0.28328310930340966,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4412479437","genre_codex":"empirical","genre_gemma":"review","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"review","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.51136065,0.2483171,0.2184795,0.0014182883,0.0005696164,0.00037433812,0.00087430846,0.00069788063,0.017908284],"genre_scores_gemma":[0.72348666,0.108009495,0.15571935,0.00035180195,0.0002405349,0.0001902178,0.0013691162,0.00024240247,0.010390404],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9992669,0.00007395248,0.000049985807,0.00013392392,0.0004324484,0.000042809635],"domain_scores_gemma":[0.9992581,0.00014497995,0.00012778338,0.000077429926,0.0003576873,0.00003388193],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0015373161,0.00063694315,0.00038099306,0.0011829924,0.00023061202,0.00083484926,0.000523755,0.00060150586,0.0010849072],"category_scores_gemma":[0.0011016048,0.00026220505,0.0003615563,0.0008235101,0.0004254342,0.0011684068,0.0003926331,0.0006893947,0.0006543763],"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":[0.00006164965,0.000080886835,0.001962499,0.0018815355,0.00004395812,0.00019756278,0.00021750547,0.0013403364,0.87916636,0.0019913479,0.00083980715,0.11221659],"study_design_scores_gemma":[0.0000058090973,0.00034333646,0.0051246365,0.00019079742,0.000051015424,0.0007263641,0.00015038862,0.0039289254,0.9138599,0.0006798227,0.07488633,0.000052756895],"about_ca_topic_score_codex":0.0007570119,"about_ca_topic_score_gemma":0.0012921749,"teacher_disagreement_score":0.0015373161,"about_ca_system_score_codex":0.00036184178,"about_ca_system_score_gemma":0.00043706936,"threshold_uncertainty_score":0.008130252},"labels":[],"label_agreement":null},{"id":"W4412486509","doi":"10.2514/6.2025-3255","title":"A Cessna 172 Retrofitted with a Rotax 916iS for Training Operations: A Conceptual Study","year":2025,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","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":true,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Training (meteorology); Aeronautics; Computer science; Engineering; Aerospace engineering; Environmental science; Meteorology; Physics","score_opus":0.047582689831172434,"score_gpt":0.3118804672984055,"score_spread":0.2642977774672331,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4412486509","genre_codex":"empirical","genre_gemma":"methods","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9959104,0.00016184499,0.0007107075,0.000024552717,0.00002174238,0.00013525557,0.00016211627,0.000029212293,0.0028442552],"genre_scores_gemma":[0.9945034,0.0002757518,0.002353714,0.0000137666075,0.0000037400987,0.0000397254,0.00018014172,0.000015140916,0.002614533],"study_design_codex":"bench_or_experimental","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.9992625,0.000057445443,0.000024008497,0.00009250924,0.0004065251,0.00015689165],"domain_scores_gemma":[0.99968076,0.000028685283,0.000038365604,0.000029040139,0.00015836209,0.00006482614],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0008212974,0.00097001204,0.00068198075,0.00087317626,0.0009245723,0.0011567264,0.0017042933,0.0009445723,0.003010883],"category_scores_gemma":[0.00061892247,0.0002825026,0.00077073264,0.0006337309,0.0008922861,0.0007395222,0.0005618559,0.0006998365,0.0005257081],"study_design_candidate":"theoretical_or_conceptual","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":[0.0059865247,0.0061461786,0.08441485,0.0021601561,0.00018950782,0.007560401,0.001597577,0.15881377,0.5818093,0.00455433,0.002603557,0.14416388],"study_design_scores_gemma":[0.00060694886,0.09392875,0.26514447,0.0003868727,0.00075375754,0.0057572885,0.012063836,0.17925914,0.3998844,0.0008754554,0.04083987,0.00049923727],"about_ca_topic_score_codex":0.041863155,"about_ca_topic_score_gemma":0.05227832,"teacher_disagreement_score":0.041863155,"about_ca_system_score_codex":0.0024866324,"about_ca_system_score_gemma":0.0012292495,"threshold_uncertainty_score":0.08323896},"labels":[],"label_agreement":null},{"id":"W4412986874","doi":"10.1109/itec63604.2025.11098128","title":"Design Space Exploration and Performance Analysis of Low Temperature PEM Fuel Cell Propulsion Aircraft","year":2025,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","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":"Lockheed Martin (Canada)","funders":"","keywords":"Propulsion; Proton exchange membrane fuel cell; Aerospace engineering; Space (punctuation); Fuel cells; Automotive engineering; Aeronautics; Computer science; Environmental science; Engineering; Chemical engineering","score_opus":0.01538540943115589,"score_gpt":0.24149526305387659,"score_spread":0.2261098536227207,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4412986874","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":[0.803571,0.0012024154,0.14350216,0.00021670976,0.000023071132,0.00013907357,0.0006738629,0.00044718926,0.050224427],"genre_scores_gemma":[0.98599607,0.00031144897,0.010190415,0.000030137784,0.00000647648,0.00007900909,0.00027110116,0.00004373595,0.0030716874],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998179,0.000054131728,0.000004730014,0.000019865392,0.00007186933,0.000031497555],"domain_scores_gemma":[0.99983203,0.00008150854,0.00002455761,0.0000139916765,0.000040590992,0.0000072198477],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00041435342,0.0006122823,0.0004221536,0.00040039668,0.00022032048,0.00056974223,0.0003658262,0.00036359008,0.0029258847],"category_scores_gemma":[0.000547407,0.00018808253,0.0006716746,0.00023445794,0.00023007966,0.00027668866,0.00024817756,0.0002985152,0.00037643578],"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":[0.00005355845,0.000023186465,0.0009787773,0.00007692818,0.000026157575,0.000057465586,0.000019938578,0.981155,0.0064438186,0.0011757273,0.00018957631,0.009799925],"study_design_scores_gemma":[0.000010656436,0.00028493625,0.0013369475,0.000011899604,0.000025722147,0.000029034014,0.000025161353,0.99081856,0.00540052,0.00073447137,0.0013152657,0.0000068630375],"about_ca_topic_score_codex":0.0025192783,"about_ca_topic_score_gemma":0.001739582,"teacher_disagreement_score":0.0029258847,"about_ca_system_score_codex":0.00065798627,"about_ca_system_score_gemma":0.00053879205,"threshold_uncertainty_score":0.009788036},"labels":[],"label_agreement":null},{"id":"W4414016511","doi":"10.1063/5.0282385","title":"Performance differences and design method improvement of Laval nozzles under superatmospheric and subatmospheric conditions","year":2025,"lang":"en","type":"article","venue":"Physics of Fluids","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":1,"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":"Fundamental Research Funds for the Central Universities; National Natural Science Foundation of China","keywords":"Physics; Nozzle; Mechanics; Aerospace engineering; Classical mechanics; Thermodynamics; Engineering","score_opus":0.022205067867681574,"score_gpt":0.2780363465124535,"score_spread":0.25583127864477195,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4414016511","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":[0.6541622,0.001161858,0.33978716,0.00012060615,0.00009432043,0.00013742872,0.00013100254,0.0007359967,0.003669349],"genre_scores_gemma":[0.8793057,0.00027862765,0.119364806,0.000029017607,0.000009377863,0.000046472847,0.00011996042,0.000064648346,0.00078141934],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.999097,0.00016192925,0.00008711651,0.00013401356,0.00042418932,0.00009574413],"domain_scores_gemma":[0.9987281,0.00028196067,0.00029380378,0.00019509549,0.0004464028,0.00005460373],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0017231962,0.0004778848,0.00043810927,0.00035776375,0.000249668,0.000857725,0.0006860527,0.0004987289,0.00057853624],"category_scores_gemma":[0.0032011182,0.00020406571,0.00043307734,0.00022105293,0.00020467135,0.00068640104,0.0006001659,0.00031858185,0.00016925398],"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":[0.0008596528,0.00020367686,0.03502118,0.00066316593,0.000090026035,0.00047076793,0.00058099214,0.19887227,0.5122041,0.0031250531,0.00092388113,0.24698539],"study_design_scores_gemma":[0.00009472246,0.0019445976,0.02129786,0.00006678676,0.00008175209,0.00069894304,0.0002259449,0.6062707,0.35881317,0.00066354516,0.009707714,0.00013441595],"about_ca_topic_score_codex":0.0007679207,"about_ca_topic_score_gemma":0.00080501626,"teacher_disagreement_score":0.0017231962,"about_ca_system_score_codex":0.0003602444,"about_ca_system_score_gemma":0.00063458824,"threshold_uncertainty_score":0.009113252},"labels":[],"label_agreement":null},{"id":"W4414498862","doi":"10.46254/na10.20250322","title":"Industrial-Aero Optimization for Agile Rocket Cargo Delivery: Logistics","year":2025,"lang":"en","type":"article","venue":"","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"","funders":"U.S. Air Force; University of Waterloo; Universidad Tecnológica de Panamá; University of Central Florida; U.S. Department of Defense; University of Missouri; Florida Institute of Technology; National Aeronautics and Space Administration","keywords":"Agile software development; Rocket (weapon); Supply chain; Drone; Component (thermodynamics); Plan (archaeology); Adaptability; Resource (disambiguation); Key (lock)","score_opus":0.048335020167727165,"score_gpt":0.28256147219582745,"score_spread":0.23422645202810027,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4414498862","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":[0.031562448,0.0020173532,0.9061947,0.0021746699,0.0003216666,0.00020612788,0.0005591217,0.00067311706,0.05629069],"genre_scores_gemma":[0.76401794,0.0025396913,0.20137835,0.0006982919,0.00022878505,0.00044735387,0.00089861476,0.00053149724,0.029259508],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993274,0.00018585986,0.00002256147,0.00011674765,0.00025398558,0.00009350461],"domain_scores_gemma":[0.9992105,0.00037400858,0.00012034606,0.00006249208,0.00017185479,0.000060778108],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0011351077,0.0012119539,0.0008030801,0.00068621885,0.00053666375,0.0016254104,0.00068685215,0.00082767016,0.009252046],"category_scores_gemma":[0.0025368943,0.00039662604,0.00083388673,0.00086314505,0.0005435318,0.0011507466,0.0014444304,0.0014171306,0.0010152052],"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":[0.00004829544,0.0000627939,0.00056011084,0.00014333271,0.0000370484,0.000047252906,0.000024917279,0.95279896,0.00103505,0.016782274,0.0039704135,0.024489539],"study_design_scores_gemma":[0.00001422824,0.000043491807,0.00022247968,0.00002128155,0.0000091423235,0.000019789402,0.00002531929,0.9844752,0.00049765216,0.009455238,0.005208427,0.000007822461],"about_ca_topic_score_codex":0.0062911063,"about_ca_topic_score_gemma":0.0048512463,"teacher_disagreement_score":0.009252046,"about_ca_system_score_codex":0.0015465631,"about_ca_system_score_gemma":0.0022531066,"threshold_uncertainty_score":0.030951142},"labels":[],"label_agreement":null},{"id":"W4415333575","doi":"10.48550/arxiv.2506.15195","title":"An efficient co-simulation and control approach to tackle complex multi-domain energetic systems: concepts and applications of the PEGASE platform","year":2025,"lang":"en","type":"preprint","venue":"ArXiv.org","topic":"Rocket and propulsion systems research","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":"Hatch (Canada)","funders":"Horizon 2020 Framework Programme","keywords":"Interface (matter); Software deployment; Energy (signal processing); Control (management); Efficient energy use; Integer programming","score_opus":0.06294158173535305,"score_gpt":0.34207799232766417,"score_spread":0.2791364105923111,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4415333575","genre_codex":"methods","genre_gemma":"methods","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.004440776,0.00011405764,0.9913141,0.00009844985,0.00004063559,0.000050160077,0.000025762198,0.00047135123,0.0034447075],"genre_scores_gemma":[0.3185101,0.0006363166,0.67460805,0.00012910289,0.000069315734,0.000532342,0.00017995207,0.00038481902,0.0049499376],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996941,0.00008025668,0.000013990533,0.000066025714,0.00011784262,0.0000277943],"domain_scores_gemma":[0.99969244,0.000110748326,0.000036541616,0.000078756275,0.00005098503,0.000030450476],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006197595,0.0009298592,0.0006231427,0.00039276452,0.00040204462,0.0008894306,0.0013540566,0.0010095523,0.0029633164],"category_scores_gemma":[0.0009436813,0.0003836599,0.0007596463,0.00031829072,0.0009539788,0.0011034812,0.0015569251,0.0013930822,0.00062278676],"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":[0.000062475134,0.00006932807,0.0005739133,0.00014648952,0.000059341757,0.00014104067,0.00010098195,0.8616228,0.014764734,0.08633348,0.0011483011,0.03497713],"study_design_scores_gemma":[0.00001303863,0.000031532538,0.000070038564,0.000009347126,0.0000073686674,0.000033401946,0.000008265891,0.9808312,0.0032239098,0.008522494,0.0072410763,0.000008359651],"about_ca_topic_score_codex":0.0017566453,"about_ca_topic_score_gemma":0.0010810853,"teacher_disagreement_score":0.0029633164,"about_ca_system_score_codex":0.00045458798,"about_ca_system_score_gemma":0.00088720076,"threshold_uncertainty_score":0.009913266},"labels":[],"label_agreement":null},{"id":"W4416716225","doi":"10.2514/1.b40192","title":"Modeling the Regression Rates of Protrusion-and-Lattice Hybrid Rocket Fuel Grains","year":2025,"lang":"en","type":"article","venue":"Journal of Propulsion and Power","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Calgary","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Propellant; Combustion; Solid fuel; Volume fraction; Thrust; Heat transfer; Ramjet; Boiler (water heating); Combustion chamber; Convection","score_opus":0.02194099581075127,"score_gpt":0.3072547218707166,"score_spread":0.28531372605996536,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4416716225","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":[0.90700644,0.00022160633,0.087454885,0.00009730821,0.000023819832,0.00004448811,0.00036322518,0.000325697,0.0044626025],"genre_scores_gemma":[0.994058,0.00007380387,0.0045929914,0.0000071081918,0.0000020735317,0.000022160044,0.0000964647,0.000023620807,0.0011238806],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999188,0.000008459417,0.0000043333403,0.000026688855,0.000022577016,0.000019172016],"domain_scores_gemma":[0.9996332,0.00020764359,0.00006853513,0.000024004785,0.00005133641,0.000015267598],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023207995,0.0004067072,0.00030181475,0.00030370132,0.00016798078,0.00053337676,0.00069922156,0.0006800133,0.0010249697],"category_scores_gemma":[0.0010541214,0.00022355848,0.00044684796,0.00022051488,0.0003079867,0.0005845569,0.0002445392,0.00047597903,0.00021036052],"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":[0.00003204246,0.000024975074,0.0023018136,0.00001689779,0.0000046699356,0.000038284503,0.00001102599,0.99065524,0.0038496105,0.0006332896,0.00006450417,0.0023677147],"study_design_scores_gemma":[9.947823e-7,0.0000059749705,0.00018168561,7.887363e-7,0.000001080945,0.0000044302005,0.000002068592,0.998599,0.0011037549,0.000057876314,0.000040649255,0.0000016837755],"about_ca_topic_score_codex":0.0101214545,"about_ca_topic_score_gemma":0.005710007,"teacher_disagreement_score":0.0101214545,"about_ca_system_score_codex":0.00067310006,"about_ca_system_score_gemma":0.00041377696,"threshold_uncertainty_score":0.020125091},"labels":[],"label_agreement":null},{"id":"W5378779","doi":"","title":"Propellant residues deposition from firing of AT4 rockets","year":2009,"lang":"en","type":"article","venue":"This Digital Resource was created in Microsoft Word and Adobe Acrobat","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":5,"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; Environmental science; Rocket (weapon); Snow; Deposition (geology); Atmospheric sciences; Aerospace engineering; Meteorology; Physics; Geology; Engineering","score_opus":0.00948300902909832,"score_gpt":0.2217768528942148,"score_spread":0.2122938438651165,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W5378779","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":[0.9982212,0.00003150618,0.00038274846,0.0000033770827,0.000002534118,0.000014861858,0.0002702661,0.00001128898,0.0010621118],"genre_scores_gemma":[0.9938253,0.00007219903,0.0018432915,0.000012190316,0.0000018550211,0.000018600513,0.0008076032,0.000021902051,0.003397148],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99967897,0.000017530783,0.000019585297,0.00006138097,0.00017416675,0.000048445978],"domain_scores_gemma":[0.99970275,0.000033973323,0.00006477504,0.000016800494,0.0001526203,0.00002899083],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021057323,0.00042557126,0.00029109683,0.00078690035,0.0008656774,0.000576301,0.0004331436,0.0003005066,0.002434354],"category_scores_gemma":[0.00031641818,0.00014504718,0.0003030569,0.0006042335,0.00024176399,0.00022058637,0.00038761226,0.00032250411,0.0005690676],"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":[0.0010161581,0.00010096324,0.105620235,0.00019739763,0.00007342928,0.0005148693,0.00047731795,0.0018990451,0.8697902,0.000041051153,0.00016927507,0.020100102],"study_design_scores_gemma":[0.000015555128,0.001398319,0.35906103,0.000039996085,0.0000652028,0.00051413645,0.0009837773,0.00240405,0.6328093,0.00005622334,0.0026236305,0.000028745008],"about_ca_topic_score_codex":0.019557549,"about_ca_topic_score_gemma":0.028832067,"teacher_disagreement_score":0.019557549,"about_ca_system_score_codex":0.00069734064,"about_ca_system_score_gemma":0.00043266983,"threshold_uncertainty_score":0.03888738},"labels":[],"label_agreement":null},{"id":"W6930340185","doi":"10.5281/zenodo.12340220","title":"ocean of pdfs","year":2024,"lang":"en","type":"other","venue":"Zenodo (CERN European Organization for Nuclear Research)","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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":"Upload; Download; Payment; Reading (process); Icon; Pacific ocean; Certificate","score_opus":0.02717822318800364,"score_gpt":0.24095813940082403,"score_spread":0.2137799162128204,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6930340185","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.00047609105,0.0011614342,0.0017756646,0.0052407617,0.005230878,0.00021295056,0.0074127563,0.006508728,0.97198063],"genre_scores_gemma":[0.0034081505,0.0010684445,0.0014097213,0.003445989,0.0024300874,0.00010688759,0.006212608,0.0051610186,0.9767571],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.99707556,0.00026862844,0.00016654166,0.00030579686,0.0018451852,0.00033830848],"domain_scores_gemma":[0.9896881,0.0013266754,0.00044524428,0.0016914908,0.0047805817,0.0020679417],"candidate_categories":["insufficient_payload"],"consensus_categories":["insufficient_payload"],"category_scores_codex":[0.0016896888,0.0013092228,0.001104857,0.0058127223,0.004002332,0.016966125,0.0016650693,0.0029058713,0.7960337],"category_scores_gemma":[0.015403176,0.0007088725,0.0010151496,0.005060865,0.0012055252,0.012265711,0.006795211,0.0027936287,0.69046885],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000013927468,0.0000120682635,0.00008177607,0.00008908162,0.0000018226975,0.000035923575,0.000048164344,0.000015494184,0.00007359344,0.0023047398,0.96153915,0.035784338],"study_design_scores_gemma":[0.0000029972462,0.0000038164353,0.0001834556,0.00005565332,9.0687547e-7,0.000052881387,0.00006003618,0.00001435667,0.000043188946,0.0004934268,0.99908376,0.000005564777],"about_ca_topic_score_codex":0.0029445945,"about_ca_topic_score_gemma":0.0049558096,"teacher_disagreement_score":0.20396632,"about_ca_system_score_codex":0.0018726714,"about_ca_system_score_gemma":0.0020943347,"threshold_uncertainty_score":0.2909332},"labels":[],"label_agreement":null},{"id":"W6980384573","doi":"","title":"Canada – Ontario Province – Long Sault – Steamer \"Algerian\" running Long Sault Rapids – Saint Lawrence River","year":2014,"lang":"en","type":"article","venue":"Digital USD (University of San Diego)","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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":"SAINT; Assemblage (archaeology); Flake; Prehistory","score_opus":0.008505301539165677,"score_gpt":0.17155106355769514,"score_spread":0.16304576201852947,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6980384573","genre_codex":"other","genre_gemma":"other","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"other","genre_consensus":"other","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.07333531,0.0016572841,0.0022375777,0.0040191733,0.00062790787,0.0002182727,0.04448054,0.0015732024,0.8718508],"genre_scores_gemma":[0.16485599,0.0012468807,0.004034384,0.0005645282,0.000063101375,0.00006861795,0.016083237,0.0006626265,0.81242055],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.99973124,0.000013339933,0.0000064954206,0.000041159616,0.00012343841,0.000084205145],"domain_scores_gemma":[0.99924755,0.000015724647,0.00002849319,0.000028140965,0.0005661537,0.00011392418],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00026032142,0.00034531395,0.0002144859,0.0007893916,0.004365005,0.0015837053,0.00052401586,0.00053847913,0.09740311],"category_scores_gemma":[0.0005948761,0.00025068483,0.00019888084,0.0018566039,0.0005547231,0.00040836123,0.0007279592,0.00043837662,0.01725719],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":true,"about_ca_topic_consensus":true,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0004359211,0.000070977025,0.035456102,0.00030455814,0.000049976934,0.00047335713,0.001433783,0.0009881711,0.0028077622,0.008576623,0.8028254,0.14657731],"study_design_scores_gemma":[0.000018567465,0.000017407423,0.079320155,0.00006932114,0.000008833692,0.00007545665,0.0009086527,0.00026344118,0.00059634907,0.0001710627,0.91853476,0.000016086311],"about_ca_topic_score_codex":0.9660691,"about_ca_topic_score_gemma":0.99007785,"teacher_disagreement_score":0.09740311,"about_ca_system_score_codex":0.013010384,"about_ca_system_score_gemma":0.026122706,"threshold_uncertainty_score":0.32584584},"labels":[],"label_agreement":null},{"id":"W6999227294","doi":"","title":"A CFD Analysis of Thrust Losses in a Solid Rocket Motor Nozzle","year":2025,"lang":"en","type":"article","venue":"DiVA at Umeå University (Umeå University)","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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; Rocket (weapon); Propellant; Propulsion; Thrust; Internal ballistics; Rocket engine nozzle; Computational fluid dynamics; Solid-fuel rocket","score_opus":0.010274390660781426,"score_gpt":0.2200938954028093,"score_spread":0.20981950474202787,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6999227294","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":[0.9458566,0.00032747284,0.041728973,0.0001705465,0.00003434739,0.000047610472,0.00020165782,0.00029438888,0.011338457],"genre_scores_gemma":[0.9961421,0.0000828489,0.0021084242,0.00001042271,0.000003015018,0.000010450549,0.000055220433,0.000013717533,0.0015738716],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999186,0.000008051671,0.0000043579735,0.000014088225,0.000037246886,0.000017693037],"domain_scores_gemma":[0.9998128,0.000095872594,0.000024692852,0.000009699026,0.000043946573,0.000012984241],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015070515,0.00024657868,0.00037758177,0.00040194247,0.00035072168,0.00055606716,0.00035916557,0.0006245408,0.0011326013],"category_scores_gemma":[0.0006014603,0.00011370483,0.00032130693,0.0002698458,0.00039692412,0.0003546983,0.00024658948,0.00025707507,0.00015122525],"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":[0.00026893098,0.00008671588,0.010690074,0.00008151262,0.000019130419,0.0008926017,0.00015732316,0.91020507,0.05438675,0.0037076697,0.00052693463,0.018977424],"study_design_scores_gemma":[0.000007505895,0.000058503294,0.0023912985,0.0000048932425,0.000003426252,0.000041349922,0.000032392876,0.9926023,0.0042550103,0.0002051041,0.00039010137,0.000008066123],"about_ca_topic_score_codex":0.0069985143,"about_ca_topic_score_gemma":0.0017413185,"teacher_disagreement_score":0.0069985143,"about_ca_system_score_codex":0.0006281048,"about_ca_system_score_gemma":0.0005654872,"threshold_uncertainty_score":0.013915539},"labels":[],"label_agreement":null},{"id":"W7084610551","doi":"10.1386/public_00234_1","title":"Tryleather.net: Performance Research and the Embodied Archive","year":2025,"lang":"en","type":"article","venue":"Public","topic":"Rocket and propulsion systems research","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":true,"ca_institutions":"Queen's University","funders":"","keywords":"Expansive; Embodied cognition; Process (computing); Work (physics)","score_opus":0.052643289962386555,"score_gpt":0.3095905396208,"score_spread":0.2569472496584135,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7084610551","genre_codex":"other","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":[0.05393229,0.015239822,0.01061673,0.042049542,0.0010927839,0.00014350483,0.00069334236,0.00061913405,0.8756128],"genre_scores_gemma":[0.69298023,0.015911609,0.0107842125,0.0020928723,0.00054437935,0.00026317663,0.0005613567,0.0006817054,0.2761805],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"qualitative","domain_scores_codex":[0.99591464,0.0016301001,0.00007629753,0.000336377,0.0014819247,0.00056064146],"domain_scores_gemma":[0.9958347,0.0018519571,0.00024292714,0.00064822653,0.0007230111,0.00069921394],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.006990192,0.0006664199,0.00036186885,0.0041578645,0.015395266,0.022795025,0.0019915095,0.0019632268,0.022138828],"category_scores_gemma":[0.007103279,0.0002567647,0.00019980532,0.0061832042,0.027555045,0.008755025,0.007995862,0.0024920604,0.0022337895],"study_design_candidate":"qualitative","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":[0.00006736105,0.000053667536,0.0014283194,0.00036801797,0.000011399192,0.0002810506,0.1595015,0.00049274485,0.0008085204,0.6375465,0.057394158,0.14204685],"study_design_scores_gemma":[0.0000061749292,0.000026354468,0.0017224897,0.00055519724,0.0000067009687,0.00012031685,0.11233747,0.00017946692,0.0007305834,0.021160707,0.86312926,0.000025190935],"about_ca_topic_score_codex":0.30914092,"about_ca_topic_score_gemma":0.4778164,"teacher_disagreement_score":0.30914092,"about_ca_system_score_codex":0.03184607,"about_ca_system_score_gemma":0.032356393,"threshold_uncertainty_score":0.61468303},"labels":[],"label_agreement":null},{"id":"W893095983","doi":"","title":"Design and Atomization Characteristic of Laval-style Annular Slot Nozzle","year":2013,"lang":"zh","type":"article","venue":"哈尔滨工业大学学报：英文版","topic":"Rocket and propulsion systems research","field":"Engineering","cited_by":0,"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; Materials science; Mechanics; Mechanical engineering; Physics; Engineering","score_opus":0.020267516470596297,"score_gpt":0.24247992329792778,"score_spread":0.22221240682733148,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W893095983","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":[0.7726155,0.001729832,0.21157518,0.00025950067,0.00016829408,0.0004072867,0.0007250751,0.0011489774,0.01137036],"genre_scores_gemma":[0.94742084,0.0003509295,0.04995819,0.000039623996,0.000018533088,0.00014974232,0.00021336043,0.00005810553,0.0017907127],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9996747,0.000018806411,0.000024838579,0.00008605249,0.00015360059,0.00004206971],"domain_scores_gemma":[0.9997316,0.000043648175,0.00007511201,0.00002299235,0.00009773459,0.000028891614],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003991231,0.00027586764,0.00027545422,0.00022461716,0.00022392391,0.000574767,0.00066974,0.0005725698,0.0008268152],"category_scores_gemma":[0.00056136743,0.00021418897,0.00023372407,0.00020155843,0.00024507326,0.0003906027,0.00025325222,0.00017675896,0.0002446593],"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":[0.00019570361,0.000027484677,0.0029572453,0.00025671205,0.000014669569,0.00032330136,0.00014731826,0.004343299,0.9774974,0.0018750164,0.00042362357,0.011938288],"study_design_scores_gemma":[0.00017028104,0.0012855185,0.017175592,0.000027099253,0.00006218884,0.0015513473,0.0000948709,0.062300745,0.89919597,0.0005425643,0.017467847,0.00012600239],"about_ca_topic_score_codex":0.0003868129,"about_ca_topic_score_gemma":0.0003785749,"teacher_disagreement_score":0.0008268152,"about_ca_system_score_codex":0.00033733272,"about_ca_system_score_gemma":0.00052609784,"threshold_uncertainty_score":0.0027659535},"labels":[],"label_agreement":null}]}