{"meta":{"query_hash":"376ecd9ee52c","filters":{"venue":"International Journal of Aeroacoustics"},"cohort_total":14,"direct_labels_cover":0,"predictions_cover":14,"exported":14,"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/376ecd9ee52c","api":"https://metacan.xera.ac/api/v1/cohort?venue=International+Journal+of+Aeroacoustics"},"results":[{"id":"W1967371752","doi":"10.1260/1475-472x.10.2-3.201","title":"Aeroacoustics of Pipe Systems with Closed Branches","year":2011,"lang":"en","type":"article","venue":"International Journal of Aeroacoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":102,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McMaster University","funders":"","keywords":"Aeroacoustics; Acoustics; Flow (mathematics); Mode (computer interface); Power (physics); Sound power; Computer science; Physics; Mechanics; Sound (geography); Sound pressure","score_opus":0.013423053502439218,"score_gpt":0.18866285994513748,"score_spread":0.17523980644269826,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1967371752","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.20419507,0.00049662904,0.7855314,0.000018004119,0.004093462,0.000104173625,0.000108145316,0.000051574898,0.0054015378],"genre_scores_gemma":[0.97674996,0.00041589918,0.022163225,0.000018791961,0.000520704,0.0000017155116,0.0000056450826,0.00005506168,0.000068985246],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9981157,0.000019226914,0.0007936517,0.000108622655,0.0007503296,0.0002124489],"domain_scores_gemma":[0.99790776,0.00011131654,0.00040656363,0.00019746597,0.001278853,0.0000980504],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00027992172,0.0002140109,0.0003626299,0.00023571345,0.000024660796,0.00004201337,0.0006463496,0.000116653726,0.000042489566],"category_scores_gemma":[0.00009478607,0.00017825651,0.00013398117,0.0001345221,0.00011545012,0.0001546368,0.00004233971,0.00034344493,0.0000045466854],"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":[0.00036988882,0.00043033285,0.0018863499,0.00028181644,0.0022208786,0.000607839,0.0014000594,0.92703044,0.05574276,0.002549516,0.0028851747,0.0045949593],"study_design_scores_gemma":[0.0042443327,0.0012940796,0.00740504,0.0013465072,0.0011697724,0.0021558662,0.0023651759,0.95877606,0.015561611,0.0018203782,0.0026188542,0.0012423025],"about_ca_topic_score_codex":0.000008549175,"about_ca_topic_score_gemma":0.000004596218,"teacher_disagreement_score":0.77255493,"about_ca_system_score_codex":0.000108860986,"about_ca_system_score_gemma":0.00008243241,"threshold_uncertainty_score":0.7269089},"labels":[],"label_agreement":null},{"id":"W1995486294","doi":"10.1260/1475-472x.9.3.273","title":"Extensions and limitations of analytical airfoil broadband noise models","year":2010,"lang":"en","type":"article","venue":"International Journal of Aeroacoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":154,"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":"Airfoil; Trailing edge; Noise (video); Vortex shedding; Computer science; Wake; Aeroacoustics; Turbulence; Boundary layer; Acoustics; Physics; Aerospace engineering; Mechanics; Engineering; Reynolds number","score_opus":0.023996430981278398,"score_gpt":0.2447403246448237,"score_spread":0.2207438936635453,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1995486294","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.73591167,0.00011288611,0.25743085,0.00022819066,0.0022961402,0.00003733831,0.00005750773,0.000018403676,0.00390701],"genre_scores_gemma":[0.97494656,0.00079046853,0.023825841,0.0000334447,0.00031059203,5.4173563e-7,0.000003971452,0.000019902782,0.00006868902],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989713,0.0000070222577,0.00046346785,0.0000712536,0.00037542664,0.00011154292],"domain_scores_gemma":[0.9984691,0.00032612894,0.00012676536,0.00010855911,0.00085716,0.00011230136],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017661315,0.00010608256,0.00018258467,0.00017680108,0.000026559706,0.0000374129,0.00024534925,0.00008635909,0.000015471269],"category_scores_gemma":[0.0004421147,0.00009789831,0.00007798651,0.00007200928,0.00010764593,0.00014844025,0.00004378134,0.00040323945,0.0000013181459],"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":[0.000025107043,0.000109373206,0.0002297936,0.000017484856,0.00025741087,0.000057850968,0.00022536927,0.9206042,0.05194126,0.015131999,0.0020644802,0.009335653],"study_design_scores_gemma":[0.00036097263,0.0000392669,0.0014471562,0.000036301906,0.00009269131,0.00019144322,0.000083498795,0.99141055,0.00022768525,0.005405451,0.000602475,0.00010249431],"about_ca_topic_score_codex":0.0000019095282,"about_ca_topic_score_gemma":0.000014881118,"teacher_disagreement_score":0.23903488,"about_ca_system_score_codex":0.000023522438,"about_ca_system_score_gemma":0.000045659523,"threshold_uncertainty_score":0.3992177},"labels":[],"label_agreement":null},{"id":"W2097081826","doi":"10.1260/147547204323022248","title":"Airframe Noise Study of a Bombardier CRJ-700 Aircraft Model in the NASA Ames 7-by 10-Foot Wind Tunnel","year":2004,"lang":"en","type":"article","venue":"International Journal of Aeroacoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":24,"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 (Canada)","funders":"","keywords":"Wind tunnel; Airframe; Landing gear; Takeoff; Aerodynamics; Scale model; Acoustics; Noise (video); Aircraft noise; Aeroacoustics; Aerospace engineering; Fuselage; Mach number; Airplane; Marine engineering; Full scale; Ceiling (cloud); Computer science; Structural engineering; Engineering; Physics; Sound pressure; Noise reduction","score_opus":0.00933754788906673,"score_gpt":0.24008540946208876,"score_spread":0.23074786157302202,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2097081826","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9105922,0.00013804711,0.08718723,0.00021139893,0.0008479795,0.00014656146,0.00008119591,0.000016362765,0.00077904516],"genre_scores_gemma":[0.99627984,0.00013285043,0.003089926,0.00010084004,0.00027558996,0.0000031773845,0.0000058728165,0.00003887396,0.00007302841],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99784684,0.000029828887,0.000809612,0.00013160473,0.00095961324,0.00022248861],"domain_scores_gemma":[0.9988455,0.000118209544,0.00023402997,0.00021353495,0.00051835977,0.00007036479],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00045147643,0.0002145499,0.00031572752,0.00021530244,0.00003489058,0.000070142756,0.0009163237,0.00010181312,0.000017187936],"category_scores_gemma":[0.00015795682,0.00017080597,0.00012844778,0.00016009425,0.00006794401,0.00016430287,0.000069589936,0.00055090064,0.0000045058896],"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":[0.00004649129,0.000752259,0.00032186613,0.000013769695,0.00021887964,0.000091039,0.0019993456,0.9887024,0.0052163927,0.00021344937,0.0020896117,0.00033450645],"study_design_scores_gemma":[0.0042710453,0.0004509419,0.005404354,0.00022309228,0.00020686607,0.00018600488,0.0035646202,0.9787285,0.00027982122,0.0059925485,0.00025934685,0.0004328735],"about_ca_topic_score_codex":0.000023379349,"about_ca_topic_score_gemma":0.000034182136,"teacher_disagreement_score":0.08568766,"about_ca_system_score_codex":0.00022979871,"about_ca_system_score_gemma":0.000088908404,"threshold_uncertainty_score":0.6965265},"labels":[],"label_agreement":null},{"id":"W2371654762","doi":"10.1177/1475472x16630870","title":"Noise mechanisms in a transonic high-pressure turbine stage","year":2016,"lang":"en","type":"article","venue":"International Journal of Aeroacoustics","topic":"Combustion and flame dynamics","field":"Engineering","cited_by":18,"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":"Grand Équipement National De Calcul Intensif; Compute Canada","keywords":"Physics; Wake; Acoustics; Mechanics; Transonic; Turbine; Stator; Inflow; Noise (video); Computer science; Aerodynamics","score_opus":0.005294063876808898,"score_gpt":0.2089405668552548,"score_spread":0.20364650297844591,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2371654762","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.26440233,0.00012761426,0.7316889,0.0007623177,0.002575947,0.000047395446,0.00010333491,0.00004024501,0.000251935],"genre_scores_gemma":[0.9951948,0.00033374663,0.0036657343,0.000053792945,0.00018864087,9.957039e-7,0.0000022781317,0.000021596856,0.00053839444],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99901915,0.000014569469,0.00038906976,0.00006650531,0.0003784396,0.00013228435],"domain_scores_gemma":[0.9994519,0.00007327404,0.00008486508,0.00008544066,0.0002368531,0.000067716006],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016538549,0.00010678425,0.00015342288,0.00023389755,0.000008489032,0.000026677815,0.00033215235,0.0000692852,0.0002629154],"category_scores_gemma":[0.000068520945,0.00008059076,0.00007173044,0.000075008546,0.000020034639,0.00015398434,0.000019004327,0.00018990957,0.000012071042],"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":[0.0002120307,0.0001812706,0.00042336842,0.000043910757,0.00043360257,0.00052803423,0.00032415375,0.7671046,0.18541098,0.020152142,0.0014056532,0.023780232],"study_design_scores_gemma":[0.016623976,0.0005451412,0.024121638,0.0014190512,0.00031700183,0.0007503206,0.00044109722,0.88734263,0.020303575,0.024109827,0.022675257,0.0013505052],"about_ca_topic_score_codex":0.0000030398505,"about_ca_topic_score_gemma":0.000019633479,"teacher_disagreement_score":0.7307925,"about_ca_system_score_codex":0.00013648377,"about_ca_system_score_gemma":0.000033449705,"threshold_uncertainty_score":0.3286396},"labels":[],"label_agreement":null},{"id":"W2378862251","doi":"10.1177/1475472x16630861","title":"Numerical assessment of the tonal noise of Counter-Rotating Open Rotors at approach","year":2016,"lang":"en","type":"article","venue":"International Journal of Aeroacoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":10,"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":"Safran; École Centrale de Lyon; Compute Canada","keywords":"Rotor (electric); Aerodynamics; Vortex; Physics; Noise (video); Mechanics; Front (military); Acoustics; Chord (peer-to-peer); Helicopter rotor; Aerospace engineering; Computer science; Engineering; Meteorology","score_opus":0.011623381857338353,"score_gpt":0.2743577837076645,"score_spread":0.26273440185032615,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2378862251","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.44831985,0.000031006144,0.5443844,0.00017638369,0.002165885,0.00016876493,0.0001538762,0.000008472625,0.004591363],"genre_scores_gemma":[0.9701265,0.00004456078,0.0293986,0.000027545731,0.00022412749,0.0000034590134,0.0000022559382,0.000024774052,0.00014816246],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99818814,0.00003190361,0.00074773043,0.000092261645,0.0008021267,0.00013781562],"domain_scores_gemma":[0.9983684,0.00021621406,0.0005105083,0.00017352773,0.000671648,0.000059729995],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004067569,0.00013225096,0.00027213938,0.00007440959,0.000031802636,0.00003102549,0.0012270601,0.00006186652,0.00007570243],"category_scores_gemma":[0.0001654311,0.00007963043,0.00014676365,0.00008613089,0.00009550746,0.0001329986,0.0002826024,0.00018955034,8.7047937e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00007646082,0.00028441413,0.022267722,0.000075968,0.0006129873,0.000016954968,0.00019455847,0.8739905,0.09165009,0.0025281182,0.0024281286,0.005874119],"study_design_scores_gemma":[0.001837476,0.0001696817,0.0318427,0.0005856759,0.00012721591,0.0002080883,0.0001279451,0.95742047,0.0058935108,0.0007456084,0.0007656751,0.0002759751],"about_ca_topic_score_codex":0.000005583081,"about_ca_topic_score_gemma":0.0000018169343,"teacher_disagreement_score":0.52180666,"about_ca_system_score_codex":0.00026289493,"about_ca_system_score_gemma":0.00010772745,"threshold_uncertainty_score":0.32472348},"labels":[],"label_agreement":null},{"id":"W2394905731","doi":"10.1177/1475472x16630669","title":"The effect of upstream edge geometry on the acoustic resonance excitation in shallow rectangular cavities","year":2016,"lang":"en","type":"article","venue":"International Journal of Aeroacoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":19,"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 Guelph; Ontario Tech University","funders":"","keywords":"Resonance (particle physics); Vortex; Acoustic resonance; Mach number; Excited state; Excitation; Materials science; Physics; Vibration; Optics; Enhanced Data Rates for GSM Evolution; Geometry; Amplitude; Acoustics; Mechanics; Atomic physics; Telecommunications","score_opus":0.004733736576609895,"score_gpt":0.21648861377286838,"score_spread":0.2117548771962585,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2394905731","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.96828467,0.0005583676,0.027307237,0.0005215978,0.0025253352,0.00010970341,0.000055072578,0.000014742715,0.0006232546],"genre_scores_gemma":[0.99821633,0.0009654763,0.00024690913,0.000025170191,0.0003651065,0.000003983603,0.0000012358166,0.000026424548,0.00014933622],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99855137,0.000070337956,0.0005198389,0.00008280295,0.0005982173,0.00017745732],"domain_scores_gemma":[0.99658453,0.0026950638,0.00021503799,0.00017685432,0.00029343826,0.00003507744],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0008823882,0.0001497201,0.00019103088,0.00015686676,0.00004860147,0.000042549793,0.0006075138,0.000072716226,0.0000166138],"category_scores_gemma":[0.0013149604,0.00007277536,0.00010467057,0.00013585135,0.00012305265,0.00008504246,0.000037391725,0.00027632635,0.000004502319],"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":[0.0008905895,0.00013992234,0.009791169,0.00011178059,0.00069750095,0.00027454374,0.0007179815,0.73919326,0.11695569,0.0082041845,0.008022084,0.11500129],"study_design_scores_gemma":[0.010585689,0.00455968,0.09783989,0.007551147,0.00061262987,0.0006179793,0.0022036997,0.7803843,0.05763888,0.027026715,0.009109401,0.001869989],"about_ca_topic_score_codex":0.0000031104444,"about_ca_topic_score_gemma":0.000025361727,"teacher_disagreement_score":0.1131313,"about_ca_system_score_codex":0.00022446323,"about_ca_system_score_gemma":0.000030959098,"threshold_uncertainty_score":0.2967693},"labels":[],"label_agreement":null},{"id":"W2790776643","doi":"10.1177/1475472x17743657","title":"Low-dissipation low-dispersion explicit Taylor-Galerkin schemes from the Runge-Kutta kernels","year":2018,"lang":"en","type":"article","venue":"International Journal of Aeroacoustics","topic":"Computational Fluid Dynamics and Aerodynamics","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":"McGill University","funders":"National Institutes of Health; Pennsylvania State University","keywords":"Runge–Kutta methods; Galerkin method; Taylor series; Dissipative system; Applied mathematics; Dissipation; Mathematics; Dispersion (optics); Discontinuous Galerkin method; Grid; Mathematical analysis; Physics; Differential equation; Geometry; Finite element method; Nonlinear system; Quantum mechanics","score_opus":0.007168614359035631,"score_gpt":0.23044375247182355,"score_spread":0.22327513811278793,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2790776643","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.6959491,0.00016042274,0.29978424,0.0004752776,0.0031882285,0.000060014914,0.000099629215,0.000036836107,0.0002462626],"genre_scores_gemma":[0.99246705,0.00017266428,0.0043008304,0.00022840584,0.0026670299,0.0000017786771,0.00006786715,0.000038207298,0.0000561623],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9983041,0.000025664842,0.00057570986,0.00013746749,0.0007763051,0.00018069452],"domain_scores_gemma":[0.9982858,0.00026366694,0.00020616382,0.00017209438,0.0009796924,0.000092630224],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00022537315,0.00018796338,0.00018091811,0.000120245335,0.0000871502,0.00016452176,0.00068413606,0.00009027019,0.0001411879],"category_scores_gemma":[0.00013512524,0.00015007812,0.00014459589,0.00013673757,0.000072189076,0.00024595647,0.00008808797,0.00029742674,0.000047868503],"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":[0.00030847825,0.00039331222,0.0042804233,0.000038368184,0.0014350564,0.0001377288,0.0019189392,0.7619321,0.15403143,0.007740621,0.017423876,0.05035967],"study_design_scores_gemma":[0.0005888543,0.000066538116,0.009561919,0.00017120158,0.000053524313,0.00004222456,0.00015000034,0.98313075,0.0022863767,0.0021216404,0.001625198,0.0002017955],"about_ca_topic_score_codex":0.000014317194,"about_ca_topic_score_gemma":0.000024890365,"teacher_disagreement_score":0.29651797,"about_ca_system_score_codex":0.00022665304,"about_ca_system_score_gemma":0.000056414563,"threshold_uncertainty_score":0.6120008},"labels":[],"label_agreement":null},{"id":"W2883570416","doi":"10.1177/1475472x18785224","title":"Philip J Morris: Some history and professional achievements","year":2018,"lang":"en","type":"article","venue":"International Journal of Aeroacoustics","topic":"Aerodynamics and Acoustics in Jet Flows","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":"Honor; Classics; Library science; Sociology; Art history; History; Computer science","score_opus":0.008893642041900351,"score_gpt":0.23141570310008047,"score_spread":0.22252206105818012,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2883570416","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9010427,0.0013271751,0.060438126,0.00046338982,0.032136884,0.00010439905,0.000061578976,0.00007114045,0.004354629],"genre_scores_gemma":[0.9910734,0.00040988447,0.0050221104,0.0002865422,0.002474993,0.0000011049056,0.000004484823,0.000027048633,0.0007003883],"study_design_codex":"not_applicable","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99891335,0.000012180525,0.0003734991,0.00008473768,0.00047689694,0.0001393382],"domain_scores_gemma":[0.99915224,0.00005179697,0.00013302438,0.000086176435,0.0004826059,0.0000941407],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002246317,0.00012018136,0.0001399489,0.00014615689,0.00003252841,0.00002382831,0.00032364225,0.00007075296,0.00018166026],"category_scores_gemma":[0.00008919603,0.0001102169,0.000048132682,0.000028708191,0.000119886034,0.00019263124,0.00007252479,0.00026178098,0.000018700393],"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":[0.0005211885,0.0010305183,0.006660061,0.00026348565,0.003132367,0.00088919734,0.003962865,0.094236426,0.19731505,0.021236531,0.6149998,0.055752523],"study_design_scores_gemma":[0.0031998581,0.0004540278,0.01118268,0.00055653247,0.000259352,0.00071228103,0.00045485,0.83542436,0.001437375,0.0116706025,0.13378781,0.0008602682],"about_ca_topic_score_codex":0.0000012320005,"about_ca_topic_score_gemma":0.0000017833177,"teacher_disagreement_score":0.74118793,"about_ca_system_score_codex":0.00028199572,"about_ca_system_score_gemma":0.000063227984,"threshold_uncertainty_score":0.44945148},"labels":[],"label_agreement":null},{"id":"W2884047390","doi":"10.1177/1475472x18789005","title":"Advanced noise modeling for future propulsion systems","year":2018,"lang":"en","type":"article","venue":"International Journal of Aeroacoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":49,"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":"Agence Nationale de la Recherche","keywords":"Turbomachinery; Airfoil; Acoustics; Noise (video); Turbofan; Rotor (electric); Solidity; Propulsion; Computer science; Aeroacoustics; Physics; Aerospace engineering; Mechanics; Engineering; Sound pressure","score_opus":0.008337794306489385,"score_gpt":0.2450104443787152,"score_spread":0.23667265007222582,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2884047390","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.20193918,0.00027722793,0.78183293,0.00010574663,0.015274161,0.000109992085,0.000055362834,0.00003564347,0.00036977258],"genre_scores_gemma":[0.9613637,0.00024861138,0.031434327,0.00003133211,0.006802123,0.0000041797343,0.000009040159,0.000039205697,0.00006749093],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9988838,0.000006670403,0.00047030646,0.00008573874,0.0003912293,0.00016227602],"domain_scores_gemma":[0.99807495,0.00003961958,0.0001380229,0.000100754274,0.0015723512,0.00007432639],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020239546,0.00012979913,0.0001720508,0.00012316609,0.000049699123,0.00007630697,0.0003766468,0.000087959066,0.000007836285],"category_scores_gemma":[0.00008860592,0.000113911585,0.00009091791,0.000055886758,0.000026346985,0.00014739498,0.000027786466,0.0001824439,0.000004399905],"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":[0.00006256168,0.000024336814,0.000011697988,0.000031960903,0.00010273414,0.00001208864,0.000108170825,0.9818042,0.010430733,0.00070382433,0.0014521193,0.00525558],"study_design_scores_gemma":[0.00051615393,0.000114958195,0.000011484805,0.00011315495,0.000038337705,0.00008246248,0.00026390186,0.99471736,0.00022946957,0.0005877975,0.0031987005,0.00012619267],"about_ca_topic_score_codex":7.7119756e-7,"about_ca_topic_score_gemma":0.0000016709738,"teacher_disagreement_score":0.7594245,"about_ca_system_score_codex":0.00014281172,"about_ca_system_score_gemma":0.000036073554,"threshold_uncertainty_score":0.46451798},"labels":[],"label_agreement":null},{"id":"W2904473351","doi":"10.1177/1475472x18812798","title":"Modal analysis of the laminar boundary layer instability and tonal noise of an airfoil at Reynolds number 150,000","year":2018,"lang":"en","type":"article","venue":"International Journal of Aeroacoustics","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":58,"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":"Physics; Reynolds number; Airfoil; Mechanics; Boundary layer; Vortex; Vortex shedding; Turbulence; Lattice Boltzmann methods; Acoustics","score_opus":0.007788386799962314,"score_gpt":0.24881192007862918,"score_spread":0.24102353327866685,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2904473351","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98512965,0.000049834598,0.012143253,0.0000632097,0.0011872912,0.000040761977,0.0003081308,0.000008886974,0.0010689914],"genre_scores_gemma":[0.99555284,0.000074161915,0.003905384,0.000035923065,0.00031767177,5.8802556e-7,0.000008481056,0.000019406585,0.000085517655],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9983713,0.000036625614,0.00066608714,0.00011742882,0.00067034294,0.00013822119],"domain_scores_gemma":[0.99823016,0.00011112629,0.00031661004,0.00024203552,0.0010210981,0.0000789466],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00040485378,0.00014237028,0.00031766715,0.00015815918,0.00005545974,0.000030422718,0.0004913651,0.000100609985,0.00017950777],"category_scores_gemma":[0.00013258451,0.000111834386,0.00017967683,0.00025363668,0.00035200542,0.00014413755,0.00015530303,0.00022530729,0.0000010695662],"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":[0.00039441194,0.00049424934,0.09885028,0.00010112294,0.004178988,0.000044249526,0.0017133733,0.805359,0.081950136,0.0012111256,0.0010614484,0.004641617],"study_design_scores_gemma":[0.0005644605,0.00013542552,0.17119752,0.00006690959,0.000821366,0.000097572774,0.00014997854,0.8212914,0.004099867,0.00084573805,0.0005498678,0.00017992781],"about_ca_topic_score_codex":0.000020608253,"about_ca_topic_score_gemma":0.00013832486,"teacher_disagreement_score":0.07785027,"about_ca_system_score_codex":0.00016498935,"about_ca_system_score_gemma":0.00006352348,"threshold_uncertainty_score":0.4560474},"labels":[],"label_agreement":null},{"id":"W3015395998","doi":"10.1177/1475472x20905060","title":"An experimental investigation of the use of an outlet silencer to quiet ejectors","year":2020,"lang":"en","type":"article","venue":"International Journal of Aeroacoustics","topic":"Refrigeration and Air Conditioning Technologies","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":"Carleton University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Silencer; Injector; Offset (computer science); Acoustics; Noise control; Noise (video); Jet noise; Noise reduction; Computer science; Mechanical engineering; Physics; Mechanics; Engineering; Turbulence; Inlet","score_opus":0.04810153757626352,"score_gpt":0.26947833503057494,"score_spread":0.22137679745431144,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3015395998","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.98166436,0.000013206616,0.017126624,0.00053013983,0.00053747126,0.000044352342,0.00003815035,0.000029619989,0.00001605179],"genre_scores_gemma":[0.9866209,0.0000066406305,0.012999491,0.00022860385,0.00012565168,9.1857044e-7,0.0000049320233,0.000009075258,0.000003769833],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99922776,0.000020196509,0.00032458827,0.000050286686,0.00032840707,0.00004876185],"domain_scores_gemma":[0.99938816,0.000026942405,0.00015194449,0.00008831222,0.00028644645,0.000058218917],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000053456402,0.000063590014,0.00009770949,0.00008092904,0.000015236376,0.00003551961,0.00031721167,0.00004028183,0.000030152187],"category_scores_gemma":[0.00014782247,0.00004954072,0.000046434965,0.000097491975,0.000053995904,0.00030122127,0.000026866288,0.00010774807,9.854616e-7],"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":[0.0000178261,0.00002386505,0.0014754017,0.0000053190784,0.00003992561,0.0000027537135,0.0011905266,0.43811914,0.55687875,0.00029263337,0.0016464846,0.0003073811],"study_design_scores_gemma":[0.00026732366,0.0003395664,0.00737349,0.00007431295,0.00001757775,0.000013975808,0.00087815203,0.09642571,0.89396197,0.00013192034,0.00042042506,0.000095574585],"about_ca_topic_score_codex":0.0000035917324,"about_ca_topic_score_gemma":0.0000015737257,"teacher_disagreement_score":0.34169343,"about_ca_system_score_codex":0.000039271916,"about_ca_system_score_gemma":0.000030176385,"threshold_uncertainty_score":0.20202118},"labels":[],"label_agreement":null},{"id":"W3175024409","doi":"10.1177/1475472x211023873","title":"Influence of the liner-type treatment on the trailing-edge noise generated by a flat plate","year":2021,"lang":"en","type":"article","venue":"International Journal of Aeroacoustics","topic":"Aerodynamics and Acoustics in Jet Flows","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":true,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Trailing edge; Noise (video); Physics; Acoustics; Optics; Dipole; Airfoil; Wind tunnel; Anechoic chamber; Materials science; Scattering; Directivity; Geometry; Mechanics; Antenna (radio); Mathematics","score_opus":0.010944151868659383,"score_gpt":0.22979931090810396,"score_spread":0.21885515903944458,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3175024409","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99268055,0.00027660298,0.0043982295,0.00047511264,0.0016586896,0.00005250088,0.00010777508,0.000011024768,0.0003395348],"genre_scores_gemma":[0.99787545,0.0006134402,0.0007010042,0.00016977573,0.00029683838,0.0000010535065,0.000008168636,0.000022347658,0.00031191928],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989005,0.0000294951,0.00043358782,0.00008045522,0.0004350746,0.00012091156],"domain_scores_gemma":[0.99856895,0.00019394356,0.0001754122,0.00018215048,0.00083340204,0.000046158977],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001327477,0.00014019944,0.0001632093,0.000041019557,0.000045136843,0.000044542987,0.00043298258,0.0000664158,0.000028263832],"category_scores_gemma":[0.00024304561,0.00008256435,0.00011523014,0.00014507514,0.000054965494,0.00004508524,0.000039601648,0.000269671,0.0000038365433],"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":[0.000020921316,0.000054183914,0.00006270814,0.000005043108,0.00022746573,0.000059030757,0.00011281395,0.8113079,0.18579431,0.0002616648,0.001556688,0.00053727184],"study_design_scores_gemma":[0.0009838659,0.00022606248,0.0010090793,0.00028105904,0.00018015034,0.00029079695,0.00012386174,0.8438266,0.14804174,0.000371569,0.00443624,0.00022896127],"about_ca_topic_score_codex":0.0000032045746,"about_ca_topic_score_gemma":0.0000073205824,"teacher_disagreement_score":0.03775258,"about_ca_system_score_codex":0.00012493362,"about_ca_system_score_gemma":0.00011564209,"threshold_uncertainty_score":0.33668765},"labels":[],"label_agreement":null},{"id":"W3201363867","doi":"10.1177/1475472x211043339","title":"Swirling mean flow effects on locally reacting interstage liner","year":2021,"lang":"en","type":"article","venue":"International Journal of Aeroacoustics","topic":"Aerodynamics and Acoustics in Jet Flows","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 de Sherbrooke","funders":"","keywords":"Mechanics; Transmission loss; Physics; Duct (anatomy); Attenuation; Axial compressor; Parametric statistics; Optics; Mathematics; Thermodynamics","score_opus":0.0066020399960872245,"score_gpt":0.22524477150301891,"score_spread":0.2186427315069317,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3201363867","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.3081669,0.00022004418,0.675172,0.00030453547,0.0114654815,0.000052926862,0.000029454122,0.00007329391,0.0045153904],"genre_scores_gemma":[0.9672798,0.00025018267,0.029995449,0.00028259226,0.0019488159,8.1220776e-7,0.000012667643,0.000052722397,0.00017693774],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99847203,0.000026360363,0.0005401029,0.00012939492,0.00062711345,0.00020501671],"domain_scores_gemma":[0.998367,0.00037546843,0.00016437694,0.00015702589,0.0008245194,0.000111597285],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002817221,0.00018538411,0.0002383145,0.00016248565,0.000038162263,0.00012517227,0.0003796997,0.00010010118,0.000040378214],"category_scores_gemma":[0.0005309182,0.00017909822,0.0001574749,0.00010547488,0.000022593313,0.000121178935,0.00007050513,0.00062608975,0.000016017202],"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":[0.00003443424,0.000066825385,0.000053384218,0.000044924145,0.00034431144,0.0016053629,0.00025693665,0.93026614,0.038993057,0.00032534028,0.0017693408,0.026239963],"study_design_scores_gemma":[0.0008036928,0.0001087497,0.00011375966,0.0006298543,0.00008807028,0.00043353467,0.00029029828,0.98037475,0.014293404,0.0005137734,0.0020862692,0.00026386743],"about_ca_topic_score_codex":9.279993e-7,"about_ca_topic_score_gemma":0.000006767797,"teacher_disagreement_score":0.65911293,"about_ca_system_score_codex":0.0002648432,"about_ca_system_score_gemma":0.00007160357,"threshold_uncertainty_score":0.7303414},"labels":[],"label_agreement":null},{"id":"W4390451705","doi":"10.1177/1475472x231225628","title":"Supersonic jet noise and screech tone suppression using cross-wire","year":2023,"lang":"en","type":"article","venue":"International Journal of Aeroacoustics","topic":"Aerodynamics and Acoustics in Jet Flows","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; Strouhal number; Supersonic speed; Acoustics; Jet (fluid); Physics; Sound pressure; Noise (video); Mach number; Shock (circulatory); Schlieren imaging; Jet noise; Schlieren; Mechanics; Computer science; Turbulence","score_opus":0.01745822576005184,"score_gpt":0.3054249021978505,"score_spread":0.28796667643779866,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4390451705","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9533574,0.00018437742,0.042668976,0.00009070924,0.0031464326,0.000041066105,0.00008263536,0.00006457481,0.0003638273],"genre_scores_gemma":[0.9914131,0.00068684475,0.0070029777,0.00003212918,0.00068685564,5.739777e-7,0.000012699281,0.00003995552,0.00012486201],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9987743,0.000011811657,0.00040297463,0.00010206199,0.00050539075,0.00020347584],"domain_scores_gemma":[0.99917835,0.0001079951,0.00009955453,0.0001019566,0.00040545393,0.00010666549],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002775978,0.00014727157,0.00018349038,0.00018482644,0.00006254728,0.0001443995,0.0003182704,0.000100032616,0.000053586245],"category_scores_gemma":[0.00015245377,0.00013472277,0.00007589654,0.0001430063,0.00006808752,0.00020638554,0.00010309784,0.00030404818,0.000008830866],"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":[0.000037657104,0.000031138366,0.004606868,0.000042530173,0.00019781145,0.00037508586,0.00019299862,0.8694646,0.118314154,0.00019870554,0.003880176,0.0026582994],"study_design_scores_gemma":[0.00056909537,0.000036864618,0.0060466737,0.0001457082,0.000047209083,0.00031490313,0.00015574774,0.99040294,0.0011477639,0.00044772323,0.00051557395,0.00016977204],"about_ca_topic_score_codex":0.000004237281,"about_ca_topic_score_gemma":0.0000020856469,"teacher_disagreement_score":0.12093839,"about_ca_system_score_codex":0.00011937015,"about_ca_system_score_gemma":0.000040141163,"threshold_uncertainty_score":0.54938346},"labels":[],"label_agreement":null}]}