{"meta":{"query_hash":"49ba8094b9e8","filters":{"topic":"Aeroelasticity and Vibration Control"},"cohort_total":364,"direct_labels_cover":0,"predictions_cover":364,"exported":364,"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/49ba8094b9e8","api":"https://metacan.xera.ac/api/v1/cohort?topic=Aeroelasticity+and+Vibration+Control"},"results":[{"id":"W103970286","doi":"10.1007/978-90-481-9887-0_21","title":"Experimental Investigation and Theoretical Modeling of Piezoelectric Actuators Used in Fuel Injectors","year":2010,"lang":"en","type":"book-chapter","venue":"IUTAM bookseries","topic":"Aeroelasticity and Vibration Control","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 British Columbia","funders":"","keywords":"Piezoelectricity; Lead zirconate titanate; Actuator; Injector; Materials science; Electric field; Coupling (piping); Nonlinear system; Field (mathematics); Mechanics; Mechanical engineering; Ferroelectricity; Engineering; Electrical engineering; Optoelectronics; Composite material; Physics","score_opus":0.011159554116023571,"score_gpt":0.1998576878015024,"score_spread":0.18869813368547883,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W103970286","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":[0.52672446,0.004498868,0.40226912,0.0007170289,0.00028278359,0.00034952283,0.0015739969,0.0011625361,0.06242177],"genre_scores_gemma":[0.9568398,0.0019060494,0.027870823,0.000031654068,0.00003505457,0.0001373952,0.00051301846,0.000058776728,0.012607358],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999655,0.000038789945,0.000012380631,0.00004760441,0.0002180178,0.000028244785],"domain_scores_gemma":[0.99973994,0.00014069551,0.000018495159,0.000039688395,0.000054829878,0.0000063229922],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003898368,0.00045255263,0.00033466282,0.00026863467,0.000485083,0.00046772332,0.001237279,0.0006741372,0.0048100036],"category_scores_gemma":[0.00084435433,0.0003111105,0.0002942471,0.0003393254,0.00055736984,0.0010842383,0.000275687,0.0005076247,0.0008162534],"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":[0.00040055608,0.0004050103,0.0011424216,0.0006552129,0.00001589889,0.00030168376,0.00023957262,0.06033241,0.8436333,0.019952338,0.0019283507,0.07099325],"study_design_scores_gemma":[0.000057597095,0.00062202784,0.004339265,0.000048050108,0.000024330322,0.0003954106,0.00021086512,0.3010224,0.674507,0.0056109424,0.013119441,0.000042603748],"about_ca_topic_score_codex":0.0009239946,"about_ca_topic_score_gemma":0.0007543679,"teacher_disagreement_score":0.0048100036,"about_ca_system_score_codex":0.00044582953,"about_ca_system_score_gemma":0.00032927355,"threshold_uncertainty_score":0.016091049},"labels":[],"label_agreement":null},{"id":"W108752441","doi":"10.5220/0002878500130019","title":"A MORPHING WING USED SHAPE MEMORY ALLOY ACTUATORS NEW CONTROL TECHNIQUE WITH BI-POSITIONAL AND PI LAWS OPTIMUM COMBINATION - Part 2: Experimental Validation","year":2010,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":13,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure","funders":"Natural Sciences and Engineering Research Council of Canada; Consortium de Recherche et d’innovation en Aérospatiale au Québec","keywords":"Actuator; Airfoil; Test bench; Data acquisition; Wind tunnel; Morphing; Computer science; Controller (irrigation); Control system; Control theory (sociology); Engineering; Mechanical engineering; Structural engineering; Electrical engineering; Aerospace engineering; Artificial intelligence; Control (management)","score_opus":0.008101937190038669,"score_gpt":0.20845280766062502,"score_spread":0.20035087047058636,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W108752441","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":[0.80863065,0.0003535164,0.18382998,0.000080877624,0.00010172819,0.00020667957,0.00009107228,0.00093856157,0.005766956],"genre_scores_gemma":[0.95840704,0.00007174084,0.039648447,0.000011724993,0.000006141445,0.000050466166,0.000032607717,0.000021321126,0.0017504585],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99970454,0.000022190907,0.000019913894,0.00004683563,0.00018361479,0.000022892396],"domain_scores_gemma":[0.9998301,0.00003246709,0.000020924423,0.000057762223,0.000046446243,0.000012113349],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021598689,0.00028291796,0.00022890224,0.00022212516,0.0001312838,0.00024051442,0.00035955012,0.00023998047,0.0010731269],"category_scores_gemma":[0.00033399666,0.00011293772,0.00017657685,0.00013467237,0.00026782145,0.00020481816,0.00018959698,0.00022240214,0.00015381035],"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":[0.00022712963,0.00008727148,0.00078026135,0.00020256637,0.000016391508,0.00010910736,0.0001211551,0.008074954,0.9265273,0.0012374219,0.00018847549,0.062428005],"study_design_scores_gemma":[0.00005234737,0.0012246834,0.00493882,0.000012496357,0.000026676975,0.00028472024,0.000038283913,0.07761968,0.9094534,0.00016875875,0.00615744,0.000022688937],"about_ca_topic_score_codex":0.0005756708,"about_ca_topic_score_gemma":0.000600123,"teacher_disagreement_score":0.0010731269,"about_ca_system_score_codex":0.000121009805,"about_ca_system_score_gemma":0.00016573857,"threshold_uncertainty_score":0.0035899282},"labels":[],"label_agreement":null},{"id":"W1480318605","doi":"10.5772/48778","title":"Fuzzy Logic Control of a Smart Actuation System in a Morphing Wing","year":2012,"lang":"en","type":"book-chapter","venue":"InTech eBooks","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":9,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure; Bombardier (Canada); Polytechnique Montréal; National Research Council Canada; Consortium For Research and Innovation In Aerospace In Quebec; Natural Sciences and Engineering Research Council of Canada","funders":"Natural Sciences and Engineering Research Council of Canada; Consortium de Recherche et d’innovation en Aérospatiale au Québec","keywords":"Morphing; Fuzzy logic; Computer science; Wing; Fuzzy control system; Control engineering; Artificial intelligence; Engineering; Structural engineering","score_opus":0.019223291474691033,"score_gpt":0.20742392778506127,"score_spread":0.18820063631037023,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1480318605","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":[0.07252475,0.00096632243,0.8940583,0.00033547665,0.00023016547,0.00010152641,0.00007675435,0.00047133712,0.031235483],"genre_scores_gemma":[0.94174504,0.00028938678,0.0467695,0.0001084013,0.000031430693,0.000079766614,0.00004197008,0.000013805291,0.010920635],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998894,0.00001690041,0.0000055808973,0.000029025736,0.000045074292,0.000014057603],"domain_scores_gemma":[0.9999379,0.000022774715,0.000011267755,0.00000574524,0.000016695709,0.00000556989],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00019435078,0.0003084057,0.00021589446,0.00014854073,0.00021896635,0.00059855264,0.00042707025,0.0005205465,0.0021978144],"category_scores_gemma":[0.00024816385,0.000119018354,0.00023291435,0.00012221841,0.00039042218,0.00023757003,0.00024030812,0.00030341075,0.0002499314],"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":[0.00045664544,0.00016587331,0.0004643307,0.00040291285,0.00007327917,0.0006559816,0.00030198414,0.5938915,0.17458303,0.038071573,0.0027389426,0.18819392],"study_design_scores_gemma":[0.00003165298,0.00019074562,0.00036329124,0.00001917117,0.00001881773,0.00006220416,0.000017462044,0.98480785,0.00784212,0.0038505502,0.0027845094,0.000011591962],"about_ca_topic_score_codex":0.00228376,"about_ca_topic_score_gemma":0.002931199,"teacher_disagreement_score":0.00228376,"about_ca_system_score_codex":0.00037885885,"about_ca_system_score_gemma":0.0002753261,"threshold_uncertainty_score":0.007352352},"labels":[],"label_agreement":null},{"id":"W1483110893","doi":"","title":"Simulation method for rigid and control modes aeroservoelastic interactions","year":2007,"lang":"en","type":"article","venue":"International Conference on Modelling, Identification and Control","topic":"Aeroelasticity and Vibration Control","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 du Québec à Montréal","funders":"","keywords":"Aerodynamics; Aeroelasticity; MATLAB; Rigid body; Aerodynamic force; Computer science; Finite element method; Inertial frame of reference; Software; Control theory (sociology); Structural engineering; Physics; Engineering; Aerospace engineering; Classical mechanics; Control (management)","score_opus":0.04204490354584215,"score_gpt":0.31990545288302413,"score_spread":0.27786054933718196,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1483110893","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":[0.0031979159,0.00007738171,0.98368233,0.00007581802,0.000084256986,0.00012399215,0.00027373512,0.0023308492,0.010153729],"genre_scores_gemma":[0.19600025,0.00046082094,0.7758999,0.000108561886,0.000059908758,0.001692496,0.0011966438,0.0014049516,0.023176512],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997129,0.000059216276,0.000016868447,0.000030447556,0.00015846945,0.000022003476],"domain_scores_gemma":[0.99963963,0.00013624532,0.000027242932,0.000041826686,0.00013240216,0.000022658469],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00044460088,0.0006552475,0.0006329173,0.00059335487,0.0005308092,0.0006674554,0.0015020545,0.0008966082,0.018600529],"category_scores_gemma":[0.0010473711,0.00031942857,0.00061695214,0.00038965585,0.00034162658,0.0006135344,0.000790671,0.0009642609,0.0031773204],"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":[0.00014019277,0.0001063525,0.0010246481,0.0002855452,0.000062520805,0.00022616702,0.00024908307,0.8443568,0.019469535,0.07277542,0.0095080035,0.051795702],"study_design_scores_gemma":[0.00003127557,0.000019087054,0.00006536703,0.00001768715,0.0000060592247,0.000040498264,0.000010105051,0.9796102,0.0023341922,0.0032125001,0.014644319,0.000008630048],"about_ca_topic_score_codex":0.003493483,"about_ca_topic_score_gemma":0.0021590188,"teacher_disagreement_score":0.018600529,"about_ca_system_score_codex":0.00042825195,"about_ca_system_score_gemma":0.001078153,"threshold_uncertainty_score":0.062224925},"labels":[],"label_agreement":null},{"id":"W1489535156","doi":"","title":"Méthode des impédances mécaniques virtuelles optimales pour le contrôle actif vibroacoustique d'un panneau aéronautique","year":2014,"lang":"fr","type":"dissertation","venue":"HAL (Le Centre pour la Communication Scientifique Directe)","topic":"Aeroelasticity and Vibration Control","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":"Natural Sciences and Engineering Research Council of Canada; Schweizerischer Nationalfonds zur Förderung der Wissenschaftlichen Forschung; National Science Foundation","keywords":"Humanities; Physics; Philosophy","score_opus":0.012395032230273502,"score_gpt":0.2215847046055091,"score_spread":0.2091896723752356,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1489535156","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":[0.0129599115,0.000770007,0.9808317,0.00009233675,0.00006506616,0.000087039174,0.00003761954,0.00041488008,0.0047414266],"genre_scores_gemma":[0.2618025,0.0014362463,0.71985257,0.00008322719,0.00003335184,0.00054214045,0.00011473496,0.00018930202,0.015945988],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99928075,0.00006470436,0.000032110136,0.00020219276,0.00036829538,0.00005187429],"domain_scores_gemma":[0.99958044,0.0001843086,0.000053215346,0.00004480925,0.000121516314,0.000015679921],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006060445,0.000718938,0.00073476613,0.0005197986,0.00030017388,0.0013043557,0.00073498883,0.0008776133,0.004404215],"category_scores_gemma":[0.0011770205,0.00065283116,0.00045580007,0.0004897453,0.0005010568,0.0007304428,0.00076347817,0.0011503932,0.0012422807],"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":[0.00020336203,0.00007451366,0.00033574263,0.00063986395,0.000046719542,0.00009387787,0.00021623632,0.060763415,0.6821267,0.01414319,0.0009125586,0.2404438],"study_design_scores_gemma":[0.00012167548,0.00039287363,0.0013003614,0.00012057672,0.00006476771,0.0001830819,0.00010475307,0.5220736,0.43671423,0.004335239,0.03450044,0.000088439534],"about_ca_topic_score_codex":0.0021948237,"about_ca_topic_score_gemma":0.0027960541,"teacher_disagreement_score":0.004404215,"about_ca_system_score_codex":0.0009877034,"about_ca_system_score_gemma":0.0010951901,"threshold_uncertainty_score":0.014733553},"labels":[],"label_agreement":null},{"id":"W1491371101","doi":"","title":"Active sound radation control of cylindrical structures using piezoelectric actuators","year":2002,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":1,"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 British Columbia","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Actuator; Acoustics; Piezoelectricity; Bending; Noise (video); Active noise control; Noise control; Range (aeronautics); Structural engineering; Materials science; Engineering; Aerospace engineering; Computer science; Noise reduction; Physics; Electrical engineering","score_opus":0.015048884247837931,"score_gpt":0.19885494565792095,"score_spread":0.18380606141008302,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1491371101","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":[0.51837385,0.00043587945,0.4738518,0.00019857893,0.00009612889,0.000030754803,0.000024528708,0.00028451224,0.006704008],"genre_scores_gemma":[0.98877454,0.000073576724,0.00989966,0.000009801738,0.000008949702,0.000013881479,0.000007348714,0.000005383802,0.001206743],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999261,0.00001265626,0.0000033902595,0.000011623011,0.000036666905,0.000009554685],"domain_scores_gemma":[0.99988437,0.000044354063,0.000027743017,0.00000881839,0.000023430013,0.000011179226],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00014830481,0.00026147612,0.00013313991,0.0001164307,0.00016122618,0.00024577032,0.00028219412,0.00017671716,0.0005010725],"category_scores_gemma":[0.00032527422,0.00012178866,0.00008759182,0.00006887976,0.00042339426,0.00024647784,0.00030530264,0.00013045632,0.00008706843],"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":[0.0002594913,0.000060359693,0.00029741946,0.00008883494,0.0000083508385,0.00013160893,0.00013820043,0.083767444,0.85541636,0.011447651,0.0004099403,0.047974266],"study_design_scores_gemma":[0.00009253963,0.000714177,0.0012954033,0.000010640783,0.00001350865,0.00009440586,0.000046394664,0.84756213,0.14340305,0.003383454,0.003358989,0.000025318237],"about_ca_topic_score_codex":0.00047312176,"about_ca_topic_score_gemma":0.0008278752,"teacher_disagreement_score":0.0005010725,"about_ca_system_score_codex":0.0001374871,"about_ca_system_score_gemma":0.00016707265,"threshold_uncertainty_score":0.0016762614},"labels":[],"label_agreement":null},{"id":"W1495974298","doi":"10.1109/cdc.2003.1272351","title":"Location and coverage of enhanced self-sensing piezoelectric actuators for active-passive hybrid vibration control of beam structures","year":2004,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Atomic Energy of Canada Limited","keywords":"Actuator; Vibration control; Constrained-layer damping; Vibration; Active vibration control; Control theory (sociology); Beam (structure); Piezoelectricity; Control system; Computer science; Engineering; Acoustics; Structural engineering; Control (management); Physics; Electrical engineering","score_opus":0.0033257798926069598,"score_gpt":0.18998606358468167,"score_spread":0.1866602836920747,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1495974298","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":[0.8585859,0.00034049753,0.14014055,0.000038991115,0.000009624717,0.0000098810215,0.000012056488,0.00006127907,0.0008013511],"genre_scores_gemma":[0.991098,0.00004650798,0.008610626,0.0000047092317,0.000003629367,0.000008515712,0.000006344002,0.0000030299343,0.00021857042],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99993026,0.000015585667,0.000003760074,0.000012436232,0.00002883379,0.000009089324],"domain_scores_gemma":[0.9997863,0.00010487845,0.00005212066,0.000022793534,0.000023663311,0.000010266328],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012206292,0.0002497711,0.00014151185,0.00008313019,0.00006992589,0.00015830544,0.00030357423,0.00018962247,0.0003101347],"category_scores_gemma":[0.00034335925,0.00011843034,0.00009253418,0.00005805926,0.00020827354,0.00030898192,0.00027395063,0.00011651467,0.000044936005],"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":[0.0002503377,0.000058330203,0.0009462596,0.00012009444,0.000021949136,0.00007506236,0.000093381874,0.07209678,0.89010334,0.0012940529,0.0000822354,0.034858156],"study_design_scores_gemma":[0.00005402202,0.000662472,0.0029644428,0.000010639881,0.000037451664,0.00010959735,0.00005379099,0.64426327,0.3503433,0.0006717161,0.0008131091,0.000016158487],"about_ca_topic_score_codex":0.00021501172,"about_ca_topic_score_gemma":0.0004022353,"teacher_disagreement_score":0.0003101347,"about_ca_system_score_codex":0.000077094475,"about_ca_system_score_gemma":0.00007983805,"threshold_uncertainty_score":0.0010374784},"labels":[],"label_agreement":null},{"id":"W1528877777","doi":"10.1002/0471216275.esm082","title":"Truss Structures with Piezoelectric Actuators and Sensors","year":2002,"lang":"en","type":"other","venue":"","topic":"Aeroelasticity and Vibration Control","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":"McMaster University; BAH Enterprises (Canada); University of Waterloo","funders":"","keywords":"Truss; Actuator; Finite element method; Piezoelectricity; Control theory (sociology); Vibration control; Modal; Vibration; Piezoelectric sensor; Flexibility (engineering); Controller (irrigation); Engineering; Active vibration control; Smart material; Modal analysis; Control engineering; Computer science; Structural engineering; Acoustics; Control (management); Materials science; Physics; Mathematics; Artificial intelligence","score_opus":0.004197591978186411,"score_gpt":0.16393134807296209,"score_spread":0.15973375609477566,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1528877777","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":[0.54489595,0.0006175465,0.43788657,0.00020951455,0.00006204252,0.0000940216,0.00009743174,0.000643539,0.015493423],"genre_scores_gemma":[0.95428705,0.00019011302,0.04181045,0.000034279183,0.000010445352,0.00003338871,0.000049527964,0.00000917821,0.003575499],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99975425,0.000020370206,0.000009734161,0.000027737131,0.00017669737,0.0000111362],"domain_scores_gemma":[0.99974424,0.00004041728,0.00007504021,0.000052422896,0.00007353745,0.000014343325],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00013066187,0.00030097543,0.00021267676,0.00028586687,0.00013218938,0.00019715042,0.000575754,0.00033296627,0.0007833843],"category_scores_gemma":[0.0003472392,0.00015458078,0.000116185816,0.00014814454,0.00046406194,0.00033789504,0.000369273,0.00020572123,0.00022207943],"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":[0.00012626701,0.00007757519,0.0011202443,0.00019566914,0.000025358308,0.00035725444,0.00010103276,0.14109543,0.7850311,0.007996624,0.00038762524,0.06348594],"study_design_scores_gemma":[0.000062566825,0.000780188,0.004900129,0.000045213324,0.000038926653,0.00074353785,0.00005919337,0.6344276,0.3420259,0.0074226367,0.009458795,0.00003527627],"about_ca_topic_score_codex":0.00062136294,"about_ca_topic_score_gemma":0.00073438283,"teacher_disagreement_score":0.0007833843,"about_ca_system_score_codex":0.00014164361,"about_ca_system_score_gemma":0.0001650557,"threshold_uncertainty_score":0.002620697},"labels":[],"label_agreement":null},{"id":"W1573506672","doi":"","title":"Comparison of wave sensing strategies for active structural acoustic control","year":2000,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Attenuation; Acceleration; Piezoelectric sensor; Acoustics; Actuator; Piezoelectricity; Intensity (physics); Vibration control; Harmonic; Control theory (sociology); Vibration; Physics; Engineering; Computer science; Control (management); Optics; Electrical engineering","score_opus":0.016574844117819603,"score_gpt":0.24382131989945627,"score_spread":0.22724647578163668,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1573506672","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":[0.17695849,0.0055256025,0.7574688,0.0002326786,0.00037719734,0.00030622294,0.00009371052,0.00092551083,0.05811174],"genre_scores_gemma":[0.9521594,0.0009733257,0.040757094,0.00007656683,0.000042602078,0.00010138369,0.0000493229,0.000038811948,0.005801541],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996234,0.000049094317,0.000025356228,0.000059938022,0.00019930679,0.000042763324],"domain_scores_gemma":[0.9995592,0.00021087537,0.00004211221,0.00004297127,0.0001224175,0.000022435739],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00035156746,0.00059531484,0.0003976867,0.0004740942,0.00021930797,0.00083355635,0.0008835631,0.0005744274,0.004641161],"category_scores_gemma":[0.0008493387,0.00018660133,0.00029589617,0.00020384054,0.00028690934,0.000834473,0.00035293726,0.00031513482,0.00056762533],"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":[0.0011385059,0.00067838805,0.00054012716,0.0008481258,0.000099896475,0.00010655334,0.00019267543,0.09246436,0.09464061,0.02658183,0.0013346563,0.7813742],"study_design_scores_gemma":[0.00017271993,0.0028800687,0.0022905373,0.00009392804,0.00015818533,0.00018428631,0.00018049317,0.90573514,0.07104067,0.0069035906,0.010301733,0.00005868703],"about_ca_topic_score_codex":0.00062800304,"about_ca_topic_score_gemma":0.0009328946,"teacher_disagreement_score":0.004641161,"about_ca_system_score_codex":0.00022363396,"about_ca_system_score_gemma":0.0002450139,"threshold_uncertainty_score":0.015526295},"labels":[],"label_agreement":null},{"id":"W1576780245","doi":"10.1109/cdc.2003.1272254","title":"Control of a positioning system with structural flexibility using piezoelectric transducers","year":2004,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Western University","funders":"","keywords":"Actuator; Lead zirconate titanate; Compensation (psychology); Flexibility (engineering); Piezoelectricity; Transducer; Control theory (sociology); Torque; Nonlinear system; Controller (irrigation); Control system; Control engineering; Computer science; Materials science; Engineering; Control (management); Electrical engineering; Ferroelectricity","score_opus":0.007980919692755516,"score_gpt":0.2008793623632182,"score_spread":0.1928984426704627,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1576780245","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":[0.16385517,0.00023779372,0.8301532,0.0002564644,0.00013881516,0.000061517305,0.000036784633,0.0005542115,0.0047060135],"genre_scores_gemma":[0.97181374,0.00010551764,0.025309151,0.000026477855,0.000039883562,0.000049575534,0.000020446709,0.000009648363,0.00262553],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998259,0.000021981654,0.000010051752,0.00005030096,0.000072341434,0.000019454916],"domain_scores_gemma":[0.9997713,0.00008017176,0.00006222918,0.00002263536,0.000044963534,0.000018732866],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002541123,0.00037489904,0.00023287859,0.00011633914,0.0003072948,0.00045961555,0.0005377672,0.00039289723,0.0009775697],"category_scores_gemma":[0.0005685967,0.00019645144,0.00016754233,0.00017258966,0.000550656,0.00036161227,0.00046182284,0.00038728002,0.00021166205],"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":[0.000278107,0.00008650179,0.0009872263,0.0002622959,0.00003920208,0.00050548156,0.00031242706,0.37520042,0.4650819,0.016315425,0.0012085898,0.13972247],"study_design_scores_gemma":[0.000073326366,0.00036437955,0.00081757223,0.000008516499,0.000020088053,0.00010900994,0.000019216639,0.97089165,0.023514787,0.0015660146,0.0025980026,0.00001738433],"about_ca_topic_score_codex":0.0019515017,"about_ca_topic_score_gemma":0.001903809,"teacher_disagreement_score":0.0019515017,"about_ca_system_score_codex":0.00022452339,"about_ca_system_score_gemma":0.00029648578,"threshold_uncertainty_score":0.003880322},"labels":[],"label_agreement":null},{"id":"W1599718628","doi":"10.1109/robot.1999.772396","title":"Study on piezoelectric actuators in control of a single-link flexible manipulator","year":2003,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":26,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto","funders":"","keywords":"Actuator; Control theory (sociology); Vibration; Piezoelectricity; Voltage; Vibration control; Controller (irrigation); Stability (learning theory); Lyapunov stability; Control system; Computer science; Engineering; Control engineering; Control (management); Acoustics; Physics","score_opus":0.023045773586502342,"score_gpt":0.22744886635537004,"score_spread":0.2044030927688677,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1599718628","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":[0.09016371,0.008517945,0.87703305,0.0007771967,0.00018099124,0.00010875336,0.000026948679,0.00013713051,0.023054171],"genre_scores_gemma":[0.8534867,0.010888977,0.108706005,0.0004423814,0.0004405815,0.00024572547,0.00004646986,0.000047732465,0.025695387],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998791,0.000027652903,0.0000067746064,0.000039330524,0.000034096436,0.000012982018],"domain_scores_gemma":[0.9998166,0.00010800865,0.000017340617,0.000010807659,0.000037037367,0.000010314413],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00029779942,0.0003532971,0.00038392117,0.00015421979,0.00031037605,0.0006159281,0.00039830402,0.0008991962,0.001743865],"category_scores_gemma":[0.00040549104,0.00017577373,0.00039194926,0.00018573474,0.0007052429,0.0007081834,0.000206866,0.0005308596,0.00041708455],"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":[0.0002029888,0.00037206753,0.002007303,0.001606842,0.00013841392,0.0038825423,0.0012771705,0.31550765,0.30076507,0.19525467,0.0022931646,0.17669213],"study_design_scores_gemma":[0.000044364566,0.0019727573,0.0015443381,0.00012720576,0.00005827515,0.0014960503,0.00021767704,0.9112044,0.032011334,0.024287984,0.026972432,0.000063075866],"about_ca_topic_score_codex":0.0007511324,"about_ca_topic_score_gemma":0.0006059264,"teacher_disagreement_score":0.001743865,"about_ca_system_score_codex":0.00020762718,"about_ca_system_score_gemma":0.00026285008,"threshold_uncertainty_score":0.005833745},"labels":[],"label_agreement":null},{"id":"W163346187","doi":"10.1007/978-3-642-19539-6_4","title":"Design and Experimental Validation of a Combined PI and Bi-Positional Laws Controller for Delaying the Transition from Laminar Flow to Turbulent Flow over a Morphing Wing","year":2011,"lang":"en","type":"book-chapter","venue":"Lecture notes in electrical engineering","topic":"Aeroelasticity and Vibration Control","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":"National Research Council Canada; École de Technologie Supérieure","funders":"","keywords":"Airfoil; Wind tunnel; Morphing; Aerodynamics; Actuator; Laminar flow; Wing; Turbulence; Engineering; Controller (irrigation); Law; Structural engineering; Control theory (sociology); Aerospace engineering; Computer science; Mechanics; Physics; Control (management); Electrical engineering","score_opus":0.010447858840144937,"score_gpt":0.19291380001071712,"score_spread":0.1824659411705722,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W163346187","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":[0.64415586,0.0005635776,0.33938038,0.00029311405,0.0005937827,0.0012228674,0.00034487984,0.0028352817,0.010610219],"genre_scores_gemma":[0.95099974,0.00007111343,0.045287594,0.00005347526,0.000011994579,0.00025817414,0.00008664864,0.000031088348,0.003200083],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99964297,0.00003747327,0.000030759922,0.000078073004,0.00016196522,0.000048809008],"domain_scores_gemma":[0.9992035,0.00018652431,0.00009759674,0.00013384085,0.00032066143,0.00005797125],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00068918744,0.0005712506,0.0004024724,0.00038694477,0.0005528203,0.00060900796,0.0012131967,0.00093119044,0.0027470472],"category_scores_gemma":[0.000949921,0.00029739624,0.00025042493,0.00017665062,0.00036126774,0.00040280077,0.0004228133,0.00048686643,0.00059230055],"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":[0.0020409124,0.0011212117,0.0015210134,0.00070125,0.00007549954,0.00018558714,0.00025538195,0.022764742,0.84155834,0.0009824706,0.001165456,0.12762813],"study_design_scores_gemma":[0.0006724401,0.008505524,0.007369472,0.000040697567,0.00014470707,0.0002586319,0.00012621323,0.26325646,0.7114244,0.0003161263,0.007814656,0.000070658294],"about_ca_topic_score_codex":0.0019209572,"about_ca_topic_score_gemma":0.0019260581,"teacher_disagreement_score":0.0027470472,"about_ca_system_score_codex":0.00033381267,"about_ca_system_score_gemma":0.0006232261,"threshold_uncertainty_score":0.009189844},"labels":[],"label_agreement":null},{"id":"W166197139","doi":"","title":"Optimization of unsteady aerodynamic forces for aeroservoelastic analysis","year":2001,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Aerodynamic force; Realization (probability); Aerodynamics; Domain (mathematical analysis); State space; Mathematics; Elasticity (physics); Dimension (graph theory); Control theory (sociology); Computer science; Mathematical analysis; Physics; Engineering; Aerospace engineering; Combinatorics","score_opus":0.007825210137250781,"score_gpt":0.2110000778228325,"score_spread":0.2031748676855817,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W166197139","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":[0.05334872,0.00022956295,0.9411405,0.00021369601,0.000018651885,0.00003343198,0.00006369714,0.00014326608,0.0048084925],"genre_scores_gemma":[0.9160421,0.0002404473,0.07949936,0.00003780176,0.000017235388,0.00010771769,0.00012206468,0.00007967511,0.0038535628],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998294,0.000058601687,0.000005816397,0.000018673201,0.000059729522,0.000027771059],"domain_scores_gemma":[0.99973255,0.0001798319,0.000026539983,0.000014350657,0.00003289544,0.000013738935],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004547568,0.0006485441,0.0004899461,0.00031939356,0.00022086965,0.00066811085,0.00036664514,0.0005058335,0.0022947395],"category_scores_gemma":[0.0010974946,0.0003433139,0.0004979622,0.00020661013,0.0005141226,0.00043059365,0.0007371433,0.00073815027,0.00027255138],"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":[0.000047460555,0.000021926218,0.00027907873,0.000033411976,0.000012780634,0.00001942559,0.00002724965,0.97807544,0.0023240268,0.0071757985,0.0002478866,0.01173551],"study_design_scores_gemma":[0.0000019678325,0.000009920514,0.000050646202,0.000002236971,9.986213e-7,0.0000016102883,0.0000043082864,0.9982475,0.0002394125,0.0012891243,0.00015096822,0.0000013897819],"about_ca_topic_score_codex":0.0029169244,"about_ca_topic_score_gemma":0.002599747,"teacher_disagreement_score":0.0029169244,"about_ca_system_score_codex":0.00061225577,"about_ca_system_score_gemma":0.0006277598,"threshold_uncertainty_score":0.0076767206},"labels":[],"label_agreement":null},{"id":"W1762780633","doi":"10.1007/s10999-015-9323-0","title":"Complete morphing wing design using flexible-rib system","year":2015,"lang":"en","type":"article","venue":"International Journal of Mechanics and Materials in Design","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":62,"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":"Natural Sciences and Engineering Research Council of Canada","keywords":"Morphing; Airfoil; Wing; Camber (aerodynamics); Aileron; Aerodynamics; Engineering; Servomotor; Computer science; Aerospace engineering; Structural engineering; Mechanical engineering","score_opus":0.09079226422727875,"score_gpt":0.26564845793382097,"score_spread":0.1748561937065422,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1762780633","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":[0.14081034,0.00015982469,0.84660435,0.00003681335,0.00004736743,0.00006418,0.00006291188,0.00051848276,0.011695724],"genre_scores_gemma":[0.8844478,0.00007898494,0.11035282,0.000017997627,0.000013397309,0.000060288898,0.00007393968,0.00007017533,0.004884661],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999366,0.000009682288,0.000003509509,0.000013208723,0.000025893656,0.000011198249],"domain_scores_gemma":[0.99996376,0.000004462913,0.0000065760796,0.000010950767,0.000009492793,0.0000047066515],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00010396152,0.0003284167,0.00034268512,0.00022501608,0.00024067843,0.00022206016,0.0004210217,0.00034653742,0.0025367336],"category_scores_gemma":[0.00008265662,0.0001642694,0.00041656836,0.000113108974,0.00015285169,0.00017640639,0.0003831159,0.00017889163,0.0004933832],"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":[0.00016220473,0.000054959644,0.0011297375,0.00020332725,0.000060177317,0.0003318457,0.00007686337,0.58583754,0.26706183,0.011623548,0.00075366994,0.1327043],"study_design_scores_gemma":[0.000025077992,0.0004869967,0.00168663,0.000011797886,0.00003880124,0.00031222764,0.000025600113,0.97107106,0.019659113,0.0016883408,0.004976413,0.000017924469],"about_ca_topic_score_codex":0.000263607,"about_ca_topic_score_gemma":0.0003649331,"teacher_disagreement_score":0.0025367336,"about_ca_system_score_codex":0.000087405424,"about_ca_system_score_gemma":0.00019114533,"threshold_uncertainty_score":0.008486271},"labels":[],"label_agreement":null},{"id":"W1770513535","doi":"","title":"Type synthesis and kinematics of a modular variable geometry truss mechanism for aircraft wing morphing","year":2009,"lang":"en","type":"article","venue":"ASME/IFToMM International Conference on Reconfigurable Mechanisms and Robots","topic":"Aeroelasticity and Vibration Control","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":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Morphing; Truss; Wing; Kinematics; Modular design; Structural engineering; Computer science; Engineering; Aerospace engineering; Artificial intelligence; Physics","score_opus":0.02152008323863575,"score_gpt":0.23682829535327554,"score_spread":0.2153082121146398,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1770513535","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":[0.11441917,0.00018908996,0.870675,0.00006672004,0.000084107654,0.00014154946,0.000087108514,0.0004594516,0.013877862],"genre_scores_gemma":[0.6769023,0.00014335077,0.31642988,0.000021142463,0.000015338037,0.00010851034,0.00011236556,0.00004258673,0.0062244777],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999337,0.000008014011,0.0000033328506,0.000011463327,0.0000356888,0.000007783952],"domain_scores_gemma":[0.99993384,0.000008079701,0.000019615063,0.0000127479125,0.000020822636,0.000004843705],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00014143334,0.0002240482,0.00015600675,0.00028613053,0.00011371915,0.00017950863,0.00039959213,0.00029408975,0.0022188344],"category_scores_gemma":[0.00016576954,0.00012132454,0.00040012464,0.00010775078,0.00020485527,0.0001136359,0.00017206467,0.00016471169,0.0003920857],"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":[0.00008631611,0.000043642955,0.001158157,0.00031350908,0.00003449519,0.00050621136,0.0001535523,0.35070187,0.45538485,0.050022047,0.0010119849,0.14058341],"study_design_scores_gemma":[0.00010167949,0.0013427172,0.0042607198,0.000087116765,0.000059692255,0.0013541675,0.00010546016,0.8220009,0.12326847,0.014477629,0.032884758,0.00005666742],"about_ca_topic_score_codex":0.00040137596,"about_ca_topic_score_gemma":0.00063001283,"teacher_disagreement_score":0.0022188344,"about_ca_system_score_codex":0.00013376471,"about_ca_system_score_gemma":0.00020226343,"threshold_uncertainty_score":0.007422745},"labels":[],"label_agreement":null},{"id":"W1851020071","doi":"10.1115/imece2014-40082","title":"Active Vibration Control Using Self-Sensing Actuators: An Experimental Comparison of Piezoelectric and Electromagnetic Technologies","year":2014,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Université de Sherbrooke","funders":"Institute of Nuclear Energy Research; Schweizerischer Nationalfonds zur Förderung der Wissenschaftlichen Forschung","keywords":"Exciter; Actuator; Vibration control; Vibration; Harmonic; Active vibration control; Computer science; Piezoelectricity; Engineering; Control theory (sociology); Control engineering; Acoustics; Electrical engineering; Control (management); Physics","score_opus":0.00882707305202415,"score_gpt":0.23570481945762178,"score_spread":0.22687774640559763,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1851020071","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":[0.97092324,0.00089770317,0.023351083,0.000076089236,0.00012588881,0.00012608034,0.00008854598,0.00012836834,0.004282937],"genre_scores_gemma":[0.9898443,0.0004055192,0.007556599,0.000017566468,0.000028088649,0.00007194865,0.000055489014,0.000022629758,0.0019978923],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99938834,0.000083734216,0.000038617804,0.00010046122,0.0003160419,0.00007276454],"domain_scores_gemma":[0.999461,0.00021826483,0.00009329121,0.00008052405,0.00010927848,0.000037626723],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00051465014,0.00038350196,0.0003320438,0.00040527154,0.0002809718,0.00036830374,0.0005810318,0.00043221595,0.0024411702],"category_scores_gemma":[0.00077328575,0.00015398761,0.00017468202,0.00023946984,0.00058286806,0.0007260588,0.0004257482,0.00033683045,0.00018589277],"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":[0.00038818852,0.00048136013,0.00025471844,0.00018659697,0.000008320795,0.0000311897,0.00010584264,0.0004896145,0.9819758,0.0003816112,0.000077718745,0.015619097],"study_design_scores_gemma":[0.000080500045,0.00581706,0.004585359,0.000023873368,0.000029395258,0.00011673044,0.00013293888,0.0057792924,0.9808107,0.00018809618,0.0024140642,0.00002213935],"about_ca_topic_score_codex":0.00017171541,"about_ca_topic_score_gemma":0.00019160642,"teacher_disagreement_score":0.0024411702,"about_ca_system_score_codex":0.00013602362,"about_ca_system_score_gemma":0.00014547518,"threshold_uncertainty_score":0.008166492},"labels":[],"label_agreement":null},{"id":"W1894762943","doi":"10.1109/acc.1995.533850","title":"Sensor effectiveness coefficients for piezoelectric materials","year":2005,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"University of Waterloo","funders":"","keywords":"Piezoelectricity; Piezoelectric sensor; Measure (data warehouse); Materials science; Voltage; Piezoelectric coefficient; Electronic engineering; Acoustics; Computer science; Electrical engineering; Composite material; Engineering; Physics; Data mining","score_opus":0.007910817805355042,"score_gpt":0.2203712965422841,"score_spread":0.21246047873692905,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1894762943","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":[0.022704758,0.0032712102,0.9478652,0.00023173504,0.0002721145,0.00023029177,0.00027162084,0.00069349766,0.024459507],"genre_scores_gemma":[0.5420844,0.0043220026,0.44039646,0.0003039395,0.00021491497,0.00047571695,0.00044296804,0.0004100948,0.0113494955],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9978011,0.0002648948,0.00011311742,0.00021808737,0.0014715516,0.0001313134],"domain_scores_gemma":[0.99688977,0.0018936909,0.00027948117,0.00015717711,0.0007080742,0.00007177861],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0015272894,0.0010256652,0.0006412877,0.0017800719,0.00030519147,0.0013137402,0.0007832921,0.0009006436,0.003818214],"category_scores_gemma":[0.008427628,0.00045995438,0.0004067803,0.00067604514,0.000676594,0.0018415072,0.0006399604,0.0012534478,0.0010288483],"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":[0.00025829306,0.00012772015,0.0016518133,0.0014942405,0.00004629292,0.00035780776,0.000390536,0.047681022,0.48262337,0.18335645,0.0069381106,0.2750744],"study_design_scores_gemma":[0.00007484265,0.00046591714,0.003348824,0.00027304338,0.00011968184,0.0023517427,0.00020742037,0.2681988,0.6179536,0.034521565,0.07223921,0.00024535792],"about_ca_topic_score_codex":0.00026892964,"about_ca_topic_score_gemma":0.00041176527,"teacher_disagreement_score":0.003818214,"about_ca_system_score_codex":0.0005196344,"about_ca_system_score_gemma":0.00047679007,"threshold_uncertainty_score":0.012773216},"labels":[],"label_agreement":null},{"id":"W1927480537","doi":"10.1109/imtc.1997.610195","title":"Instrumentation and data fusion architecture for systems control","year":2002,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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 Ottawa; Canadian Space Agency","funders":"","keywords":"Instrumentation (computer programming); Sensor fusion; Computer science; Key (lock); Architecture; Control engineering; Control system; Fusion; Robust control; Systems engineering; Engineering; Artificial intelligence; Electrical engineering","score_opus":0.023474991388147955,"score_gpt":0.2238610955630837,"score_spread":0.20038610417493574,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1927480537","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":[0.0021507964,0.0008609973,0.9923369,0.0002646862,0.0000683936,0.000044505672,0.000029353734,0.00045921849,0.0037851762],"genre_scores_gemma":[0.387316,0.0036353727,0.5981971,0.0004878199,0.000451602,0.00047939623,0.00040856932,0.000098007185,0.008926179],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9993243,0.00014346404,0.000046955625,0.00012280155,0.00031100473,0.000051433635],"domain_scores_gemma":[0.9996854,0.00006317576,0.000029198287,0.00008074986,0.00012618359,0.00001526557],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00090374507,0.0006226766,0.00049812853,0.0004201266,0.0004324313,0.0011113129,0.00078342867,0.00083017163,0.002139052],"category_scores_gemma":[0.0009480565,0.00021253647,0.0003589612,0.00056061056,0.0007068059,0.0012773363,0.001016121,0.0012129147,0.00097372604],"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":[0.00018963082,0.000066887114,0.00040121403,0.00039693512,0.0000973122,0.00015393156,0.00022327856,0.09775506,0.0363797,0.5406188,0.00557979,0.31813747],"study_design_scores_gemma":[0.000058459307,0.00029451234,0.0005337662,0.00009257967,0.000087725006,0.00019611213,0.00005301109,0.61719793,0.024271535,0.27053246,0.086629264,0.000052763236],"about_ca_topic_score_codex":0.0009431945,"about_ca_topic_score_gemma":0.0009283313,"teacher_disagreement_score":0.002139052,"about_ca_system_score_codex":0.0005610799,"about_ca_system_score_gemma":0.0008776468,"threshold_uncertainty_score":0.0071558952},"labels":[],"label_agreement":null},{"id":"W1940359528","doi":"10.1109/acc.1995.533859","title":"Structural property changes due to piezoelectric material bonding: a numerical example","year":2005,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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 Waterloo","funders":"","keywords":"Piezoelectricity; Property (philosophy); Materials science; Transducer; PMUT; Piezoelectric sensor; Structural engineering; Computer science; Mechanical engineering; Acoustics; Composite material; Engineering; Physics","score_opus":0.01723169032536361,"score_gpt":0.21099769345269537,"score_spread":0.19376600312733175,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1940359528","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":[0.91134274,0.00027892613,0.045762427,0.00076301116,0.00007507188,0.000097355296,0.00030259768,0.00027923405,0.04109871],"genre_scores_gemma":[0.99138427,0.00008238961,0.006096538,0.00003445878,0.000004789448,0.000051802555,0.000033859575,0.000012013785,0.0022998757],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999859,0.000028913488,0.000005762307,0.00001509715,0.000055463173,0.00003589793],"domain_scores_gemma":[0.99928814,0.0004419948,0.00007913428,0.00004312278,0.00009901394,0.000048657486],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00038110692,0.0003121313,0.00040921703,0.0004656552,0.0006991073,0.00054729014,0.0007437922,0.0024655436,0.0063594864],"category_scores_gemma":[0.0014681037,0.00029818466,0.00039104518,0.00053761323,0.001049699,0.00047897044,0.0006190806,0.0006077448,0.00034995965],"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":[0.00012254503,0.00010832396,0.0013743173,0.00007852865,0.000011703407,0.0005422519,0.000103745835,0.983067,0.0052124765,0.0052002617,0.0003803588,0.0037984352],"study_design_scores_gemma":[0.00008246967,0.0001492076,0.00068240886,0.000009759583,0.000013691242,0.000063250875,0.00007571128,0.9952384,0.0016607675,0.0013690133,0.00064036716,0.000014933194],"about_ca_topic_score_codex":0.007880605,"about_ca_topic_score_gemma":0.0044340203,"teacher_disagreement_score":0.007880605,"about_ca_system_score_codex":0.00045373337,"about_ca_system_score_gemma":0.0004907119,"threshold_uncertainty_score":0.021274626},"labels":[],"label_agreement":null},{"id":"W1944684427","doi":"10.2514/1.j053686","title":"Study on Blade Property Measurement and Its Influence on Air/Structural Loads","year":2015,"lang":"en","type":"article","venue":"AIAA Journal","topic":"Aeroelasticity and Vibration Control","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":"","keywords":"Aeroelasticity; Helicopter rotor; Structural engineering; Rotor (electric); Engineering; Aeroacoustics; Aerodynamics; Aerospace engineering; Mechanical engineering","score_opus":0.05443908103050564,"score_gpt":0.24749172747471895,"score_spread":0.19305264644421333,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1944684427","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":[0.9256882,0.000670065,0.07180145,0.00003828122,0.00006344438,0.000037094902,0.00015004635,0.00025830008,0.0012931006],"genre_scores_gemma":[0.99212086,0.00021615582,0.007005891,0.000024592002,0.000030695766,0.000017161845,0.00016605928,0.000046367888,0.00037222911],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99828196,0.00032372255,0.00007304936,0.0004007689,0.0008430046,0.000077483426],"domain_scores_gemma":[0.9957651,0.0019278957,0.0006474275,0.00071530143,0.00087099127,0.00007334843],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0008812442,0.00068887556,0.00053638656,0.0006036423,0.00022619787,0.00036882164,0.00045895032,0.00062547036,0.000847064],"category_scores_gemma":[0.003877549,0.0002560616,0.00032745535,0.00070234574,0.0003651278,0.00057577423,0.00031105767,0.00034456054,0.0006769045],"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":[0.0004468837,0.0002668952,0.054205883,0.00033990457,0.0000848966,0.000305335,0.0002670538,0.011272632,0.8214475,0.00024234939,0.00022405235,0.110896505],"study_design_scores_gemma":[0.000012563481,0.0021536578,0.19072948,0.000032984775,0.000101930236,0.0012060694,0.00019928254,0.08080218,0.72220945,0.00017148208,0.0023183266,0.00006257668],"about_ca_topic_score_codex":0.0004686154,"about_ca_topic_score_gemma":0.00049093016,"teacher_disagreement_score":0.0008812442,"about_ca_system_score_codex":0.00014089303,"about_ca_system_score_gemma":0.00015527332,"threshold_uncertainty_score":0.004660487},"labels":[],"label_agreement":null},{"id":"W1964297633","doi":"10.2514/6.2013-4918","title":"Control of Actuation System Based Smart Material Actuators in a Morphing Wing Experimental Model","year":2013,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":true,"ca_institutions":"Université du Québec","funders":"Università di Catania; Consortium de Recherche et d’innovation en Aérospatiale au Québec","keywords":"Morphing; Actuator; Wing; Computer science; Smart material; Pneumatic actuator; Control system; Control engineering; Aerospace engineering; Engineering; Materials science; Computer graphics (images); Artificial intelligence; Electrical engineering; Composite material","score_opus":0.007311334665134013,"score_gpt":0.18552043040908403,"score_spread":0.17820909574395002,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1964297633","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":[0.81060785,0.00012444623,0.17320065,0.00015060409,0.00008686645,0.00032546447,0.00047647284,0.0010594336,0.013968135],"genre_scores_gemma":[0.99158114,0.000030905212,0.006266856,0.000007960091,0.0000023340908,0.00010594756,0.000056005465,0.000008431918,0.001940456],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999013,0.000011739312,0.0000062583576,0.000027798016,0.00003643246,0.00001634674],"domain_scores_gemma":[0.9998801,0.000034352815,0.000023670449,0.000023903925,0.000026405338,0.0000114175755],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020725986,0.00034715544,0.00023246308,0.00016179043,0.00022754724,0.00039885018,0.0005261638,0.0004312482,0.0030814104],"category_scores_gemma":[0.00024275744,0.00013186796,0.0002856963,0.00006701832,0.0003734389,0.00022222579,0.00029713183,0.00025154292,0.00024390935],"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":[0.0005641273,0.00017078583,0.0018355071,0.00033736325,0.000028763712,0.0004142881,0.00017660168,0.702459,0.27160698,0.0028784503,0.00044505877,0.019083057],"study_design_scores_gemma":[0.000039027338,0.0003561666,0.0015770432,0.000009535171,0.0000126034,0.000026256293,0.000023438442,0.9641644,0.032535013,0.00021646803,0.001029254,0.000010752433],"about_ca_topic_score_codex":0.0020724237,"about_ca_topic_score_gemma":0.001732943,"teacher_disagreement_score":0.0030814104,"about_ca_system_score_codex":0.000258648,"about_ca_system_score_gemma":0.000303411,"threshold_uncertainty_score":0.010308325},"labels":[],"label_agreement":null},{"id":"W1966115056","doi":"10.1117/12.2044550","title":"Implementation of a self-sensing piezoelectric actuator for vibro-acoustic active control","year":2014,"lang":"en","type":"article","venue":"Proceedings of SPIE, the International Society for Optical Engineering/Proceedings of SPIE","topic":"Aeroelasticity and Vibration Control","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":"Université de Sherbrooke","funders":"","keywords":"Acoustics; Actuator; Capacitive sensing; Resistor; Piezoelectric sensor; Electrical impedance; Transducer; Voltage; Piezoelectricity; Current (fluid); Vibration; Engineering; Electronic engineering; Electrical engineering; Physics","score_opus":0.00647760767597425,"score_gpt":0.220976012214139,"score_spread":0.21449840453816477,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1966115056","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":[0.14842781,0.00049225974,0.8342826,0.00026636507,0.00046995698,0.00019903683,0.00023994118,0.0029534006,0.012668653],"genre_scores_gemma":[0.71119666,0.00025510884,0.2785394,0.00008124242,0.000047636495,0.00022010744,0.00018269644,0.00010268906,0.009374447],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998259,0.000011575059,0.000010234631,0.000028757519,0.000107095344,0.000016361042],"domain_scores_gemma":[0.99984384,0.000037554866,0.000021213846,0.000027176582,0.00006009469,0.000010083261],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018358718,0.0002468487,0.00020491486,0.00016468797,0.00013292984,0.0002577576,0.0006930435,0.00034262467,0.0030042687],"category_scores_gemma":[0.00028008837,0.00014277724,0.00016992036,0.00010254813,0.00015790187,0.00028934536,0.00026463266,0.00032652388,0.000695536],"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":[0.000065213906,0.000104199404,0.0005567123,0.0002593512,0.000019378424,0.00011419459,0.00006334156,0.006415047,0.9211594,0.002796506,0.0012369908,0.067209706],"study_design_scores_gemma":[0.000047472644,0.00055953866,0.002876023,0.000033529537,0.00003038904,0.000458879,0.000028103876,0.15393725,0.8123477,0.0005189431,0.029128868,0.000033222892],"about_ca_topic_score_codex":0.0002655433,"about_ca_topic_score_gemma":0.0003617821,"teacher_disagreement_score":0.0030042687,"about_ca_system_score_codex":0.00014418711,"about_ca_system_score_gemma":0.0002751988,"threshold_uncertainty_score":0.010050356},"labels":[],"label_agreement":null},{"id":"W1966847917","doi":"10.1007/s00466-004-0549-1","title":"Optimal gains for active vibration control by the beam analogy","year":2004,"lang":"en","type":"article","venue":"Computational Mechanics","topic":"Aeroelasticity and Vibration Control","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 Saskatchewan","funders":"","keywords":"Finite element method; Optimal control; Analogy; Mathematics; Vibration; Boundary value problem; Domain (mathematical analysis); Control theory (sociology); Beam (structure); Mathematical analysis; Applied mathematics; Computer science; Mathematical optimization; Control (management); Physics; Engineering; Structural engineering","score_opus":0.01191692361966933,"score_gpt":0.2307735694725807,"score_spread":0.21885664585291137,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1966847917","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":[0.048335038,0.00022989407,0.9388701,0.00028564053,0.000071385475,0.000026391026,0.00001581496,0.00012541657,0.012040295],"genre_scores_gemma":[0.95169413,0.00013917549,0.041512873,0.00010751788,0.00005528174,0.00008991452,0.0000130684375,0.0000326059,0.006355536],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99981743,0.00006357825,0.000006616166,0.0000307819,0.00005778232,0.0000237249],"domain_scores_gemma":[0.999716,0.00019253713,0.000023553668,0.000022258182,0.000034673958,0.000010945098],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00055184367,0.0003548077,0.00044805798,0.00021112185,0.0002827214,0.0005708911,0.0005607733,0.00072126545,0.004194479],"category_scores_gemma":[0.0016384599,0.00029533842,0.00023302407,0.000172366,0.0005572857,0.00087564375,0.00066061114,0.00070852565,0.0003523348],"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":[0.00037663584,0.00016031481,0.00020861201,0.00012895066,0.000049624676,0.000062835774,0.00013814993,0.49998826,0.028687704,0.370925,0.0019136772,0.09736027],"study_design_scores_gemma":[0.000052212574,0.00007055696,0.00014298328,0.000007717176,0.000009000148,0.000013200197,0.000009665376,0.939469,0.0011045225,0.058137417,0.0009749158,0.000008813024],"about_ca_topic_score_codex":0.000583129,"about_ca_topic_score_gemma":0.0006955489,"teacher_disagreement_score":0.004194479,"about_ca_system_score_codex":0.0002812114,"about_ca_system_score_gemma":0.0002925369,"threshold_uncertainty_score":0.014031887},"labels":[],"label_agreement":null},{"id":"W1966939403","doi":"10.1177/1045389x05050105","title":"Actuator Placement Optimization and Adaptive Vibration Control of Plate Smart Structures","year":2005,"lang":"en","type":"article","venue":"Journal of Intelligent Material Systems and Structures","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":149,"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 Space Agency","funders":"","keywords":"Actuator; Controllability; Vibration control; Control theory (sociology); Active vibration control; Vibration; Finite element method; Engineering; Genetic algorithm; Optimization problem; Control engineering; Computer science; Structural engineering; Mathematics; Control (management); Acoustics; Algorithm","score_opus":0.008262381157899961,"score_gpt":0.20430923091114034,"score_spread":0.19604684975324038,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1966939403","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":[0.09520244,0.00014727445,0.9026427,0.00006221148,0.000017397902,0.000015183015,0.000010315084,0.00014065226,0.0017618478],"genre_scores_gemma":[0.9284955,0.00006717513,0.0695091,0.000018103337,0.000011150516,0.00003116578,0.000015531134,0.000018696,0.0018335094],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99989486,0.000021825892,0.0000043686596,0.000025504183,0.00004460093,0.000008759341],"domain_scores_gemma":[0.9998727,0.00005408712,0.00003369137,0.000009315549,0.000024217878,0.0000059856734],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018011866,0.00035400884,0.00020211247,0.00014091883,0.00011000604,0.00016963399,0.000286678,0.00029406,0.000674905],"category_scores_gemma":[0.00040417927,0.00016263015,0.00011868709,0.000090188245,0.00028592136,0.00021919927,0.00019373506,0.00017252467,0.00012367801],"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":[0.000078088175,0.000026805792,0.00041974167,0.00007297627,0.000019110777,0.00008963609,0.000046051988,0.8138035,0.12044874,0.005012796,0.0002932543,0.059689276],"study_design_scores_gemma":[0.0000072515413,0.00007110413,0.00026452294,0.00000202472,0.00000390329,0.000020941947,0.000006378843,0.9870524,0.011651967,0.0006364901,0.00027941298,0.0000035149633],"about_ca_topic_score_codex":0.0006272054,"about_ca_topic_score_gemma":0.0008677685,"teacher_disagreement_score":0.000674905,"about_ca_system_score_codex":0.0001818809,"about_ca_system_score_gemma":0.00021435242,"threshold_uncertainty_score":0.0022577643},"labels":[],"label_agreement":null},{"id":"W1967769531","doi":"10.2514/2.4975","title":"Method of Unsteady Aerodynamic Forces Approximation for Aeroservoelastic Interactions","year":2002,"lang":"en","type":"article","venue":"Journal of Guidance Control and Dynamics","topic":"Aeroelasticity and Vibration Control","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":"École de Technologie Supérieure","funders":"Office of Naval Research; National Aeronautics and Space Administration; National Science Foundation","keywords":"Aerodynamics; Aeroelasticity; Aerodynamic force; Aerospace engineering; Control theory (sociology); Computer science; Physics; Engineering","score_opus":0.010468721825092004,"score_gpt":0.23801109329728407,"score_spread":0.22754237147219206,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1967769531","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":[0.0015630318,0.00030190236,0.99428284,0.00006365939,0.000091932874,0.000039207338,0.000071168244,0.0001784827,0.0034078711],"genre_scores_gemma":[0.13665573,0.0009029419,0.8321898,0.0001315383,0.00020461097,0.0005318225,0.0003299817,0.00054350286,0.02851011],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99955875,0.00012997647,0.000015405372,0.000034567343,0.0002307385,0.00003068862],"domain_scores_gemma":[0.99946207,0.00021304311,0.000040851915,0.00007472977,0.0001743262,0.00003504248],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005276343,0.0005691609,0.0005109853,0.0006530387,0.00039648238,0.0006016825,0.0017831028,0.00072239526,0.012448476],"category_scores_gemma":[0.0015955445,0.00018332532,0.0005381913,0.00047517577,0.00056989974,0.0005826917,0.0008088602,0.0010748114,0.004244726],"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":[0.00018986077,0.00015817236,0.0017154618,0.00064274174,0.00008090887,0.0004680032,0.0003083006,0.27800468,0.017513167,0.390765,0.017313836,0.2928397],"study_design_scores_gemma":[0.0000137852985,0.000023114648,0.00015444038,0.00002234585,0.000004098138,0.00008905506,0.000020435951,0.95933473,0.001317673,0.019400856,0.019607985,0.000011369668],"about_ca_topic_score_codex":0.002716339,"about_ca_topic_score_gemma":0.0025756056,"teacher_disagreement_score":0.012448476,"about_ca_system_score_codex":0.0004611887,"about_ca_system_score_gemma":0.0008404752,"threshold_uncertainty_score":0.041644335},"labels":[],"label_agreement":null},{"id":"W1967833674","doi":"10.1023/b:nody.0000040033.85421.4d","title":"The Secondary Bifurcation of an Aeroelastic Airfoil Motion: Effect of High Harmonics","year":2004,"lang":"en","type":"article","venue":"Nonlinear Dynamics","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":96,"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 Research Council Canada","keywords":"Bifurcation; Flutter; Harmonic balance; Mathematics; Aeroelasticity; Saddle-node bifurcation; Bifurcation diagram; Hopf bifurcation; Airfoil; Control theory (sociology); Transcritical bifurcation; Limit cycle; Period-doubling bifurcation; Nonlinear system; Classical mechanics; Mechanics; Mathematical analysis; Physics; Limit (mathematics); Aerodynamics; Computer science","score_opus":0.0027751411125080455,"score_gpt":0.1936778991863945,"score_spread":0.19090275807388646,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1967833674","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":[0.95829445,0.0001840259,0.019836428,0.00041480985,0.00013736164,0.00003146706,0.000054031643,0.00019152976,0.020855926],"genre_scores_gemma":[0.99690706,0.000036652124,0.0009438736,0.000020161235,0.000018893616,0.000005010809,0.000019307683,0.000028229535,0.0020207716],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999424,0.0000115724,0.0000021842973,0.000010861596,0.000016547272,0.000016473883],"domain_scores_gemma":[0.9997018,0.000092166585,0.000033372093,0.000026477937,0.000043855616,0.00010225289],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016108144,0.0002248846,0.00042670546,0.00046925776,0.00074496225,0.00059408264,0.00025430231,0.0007904887,0.0057245498],"category_scores_gemma":[0.0010038796,0.0002019913,0.000333418,0.000115662304,0.00069894374,0.0003862224,0.00056204817,0.00053226633,0.0004892209],"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":[0.0030357137,0.0003711835,0.013145457,0.00037378355,0.00009583786,0.0051225107,0.002093541,0.18114874,0.5606875,0.18128365,0.0070648855,0.045577228],"study_design_scores_gemma":[0.000115696625,0.00035480026,0.013468119,0.000044075055,0.000038965307,0.0012446296,0.0003592579,0.91091067,0.046958797,0.023440732,0.0030117969,0.000052451356],"about_ca_topic_score_codex":0.0008712079,"about_ca_topic_score_gemma":0.00061171595,"teacher_disagreement_score":0.0057245498,"about_ca_system_score_codex":0.0003836089,"about_ca_system_score_gemma":0.00024013474,"threshold_uncertainty_score":0.019150496},"labels":[],"label_agreement":null},{"id":"W1969048729","doi":"10.1557/proc-655-cc13.6.1","title":"Macroscopic Actuators Using Thick Piezoelectric Coatings","year":2000,"lang":"en","type":"article","venue":"MRS Proceedings","topic":"Aeroelasticity and Vibration Control","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":"Royal Military College of Canada; Queen's University","funders":"","keywords":"Materials science; Wafer dicing; Lapping; Fabrication; Piezoelectricity; Composite material; Ceramic; Coating; Actuator; Laser; Unimorph; Voltage; Optoelectronics; Optics; Wafer","score_opus":0.009887807081179036,"score_gpt":0.21627594263717875,"score_spread":0.20638813555599972,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1969048729","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":[0.79251194,0.0036613655,0.17038433,0.00058696454,0.000892738,0.00008504194,0.00011873231,0.0010759279,0.030682907],"genre_scores_gemma":[0.95079505,0.00091998203,0.03832279,0.00013024014,0.00009172378,0.000023471512,0.000071431896,0.00006861412,0.0095767835],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998233,0.00000873086,0.0000068307454,0.00003835556,0.00008883668,0.000034100354],"domain_scores_gemma":[0.9998535,0.000031489395,0.000030159583,0.000037892143,0.00002052508,0.000026437492],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016264721,0.00043366145,0.00035778747,0.00015182399,0.00024977847,0.0005667158,0.00048181275,0.0004995065,0.0015406287],"category_scores_gemma":[0.00023081528,0.0004882933,0.00018863568,0.00012948913,0.0005627638,0.0006578226,0.0009241724,0.0007822429,0.00044292238],"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":[0.00002577419,0.000011069506,0.00010403952,0.00005529973,0.0000080732225,0.00005883651,0.000022240174,0.00074997026,0.9922421,0.0015027253,0.00023313472,0.0049866755],"study_design_scores_gemma":[0.000055259243,0.00036110578,0.0035407175,0.000018713876,0.00003103096,0.00036043933,0.000057999896,0.021268295,0.9610017,0.0014051379,0.011864409,0.000035230252],"about_ca_topic_score_codex":0.00027128935,"about_ca_topic_score_gemma":0.00090782554,"teacher_disagreement_score":0.0015406287,"about_ca_system_score_codex":0.00024851167,"about_ca_system_score_gemma":0.00017368949,"threshold_uncertainty_score":0.005153954},"labels":[],"label_agreement":null},{"id":"W1969547495","doi":"10.1177/1077546308094246","title":"Direct Optimal Vibration Control of a Piezoelastic Plate","year":2009,"lang":"en","type":"article","venue":"Journal of Vibration and Control","topic":"Aeroelasticity and Vibration Control","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":"University of Victoria; British Columbia Institute of Technology","funders":"","keywords":"Optimal control; Control theory (sociology); Controller (irrigation); Mathematics; Algebraic equation; Parametric statistics; Linear-quadratic regulator; Vibration; Vibration control; Active vibration control; Actuator; Mathematical optimization; Nonlinear system; Computer science; Control (management); Physics","score_opus":0.004922316592041683,"score_gpt":0.19701703256230688,"score_spread":0.1920947159702652,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1969547495","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":[0.040914956,0.00034044182,0.9522253,0.00015569283,0.00008352638,0.000058420792,0.000014774781,0.00014791425,0.0060589667],"genre_scores_gemma":[0.9247333,0.00034759357,0.06786608,0.0000427654,0.000031002222,0.00012634926,0.000022912072,0.000020987278,0.0068089664],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998585,0.000030779644,0.0000046159666,0.000035114397,0.00005566472,0.000015303578],"domain_scores_gemma":[0.99989665,0.000050909875,0.000014913958,0.0000069189796,0.000022833035,0.000007735408],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00027382452,0.0004798737,0.0004177518,0.0001582262,0.0002513279,0.0004595115,0.0005173311,0.0004200115,0.0012670428],"category_scores_gemma":[0.00038860698,0.0002640754,0.00023692852,0.00012257893,0.0007371307,0.00023586625,0.00055791653,0.000453448,0.00012183685],"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":[0.00008814519,0.0000658505,0.00025503174,0.000183002,0.000025673813,0.00014340557,0.00009865356,0.87429154,0.03799446,0.013777181,0.00061778136,0.072459325],"study_design_scores_gemma":[0.000023116043,0.00008651713,0.0001314474,0.0000054464167,0.000006895718,0.000022036182,0.000008329874,0.99436766,0.003047475,0.0015279363,0.00076675636,0.0000063339526],"about_ca_topic_score_codex":0.002633805,"about_ca_topic_score_gemma":0.0019081242,"teacher_disagreement_score":0.002633805,"about_ca_system_score_codex":0.00032528138,"about_ca_system_score_gemma":0.00069136824,"threshold_uncertainty_score":0.0052369833},"labels":[],"label_agreement":null},{"id":"W1971118600","doi":"10.1007/s10999-011-9169-z","title":"Flutter boundary prediction of an adaptive morphing wing for unmanned aerial vehicle","year":2011,"lang":"en","type":"article","venue":"International Journal of Mechanics and Materials in Design","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":21,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Canada Research Chairs; University of Toronto","funders":"","keywords":"Morphing; Flutter; Wing; Aerodynamics; Solid mechanics; Structural engineering; Computer science; Aerospace engineering; Aeroelasticity; Flexibility (engineering); Actuator; Aerodynamic force; Wing twist; Angle of attack; Control theory (sociology); Engineering; Mathematics; Materials science; Artificial intelligence","score_opus":0.0383970342078778,"score_gpt":0.22950524507910225,"score_spread":0.19110821087122445,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1971118600","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":[0.7208846,0.00014987687,0.2748309,0.00019122653,0.00008601321,0.00004211869,0.000038606187,0.00045719778,0.0033193736],"genre_scores_gemma":[0.9933031,0.000013626125,0.0061119273,0.000010027977,0.000004524435,0.0000082554625,0.000014484145,0.000010476608,0.00052345585],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99996054,0.000008295312,0.0000020472253,0.000010133326,0.000011257678,0.000007819263],"domain_scores_gemma":[0.99983287,0.00009049635,0.000016420257,0.000009809651,0.000036396734,0.00001402597],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001605968,0.00028291903,0.00036495854,0.00020885462,0.00031787617,0.0002665521,0.00035948004,0.00069228036,0.0010579242],"category_scores_gemma":[0.0004825021,0.00017572346,0.00027070774,0.00006301797,0.00024839037,0.0002568127,0.00032882116,0.00030957223,0.00010011726],"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":[0.00024816653,0.000059210197,0.002126982,0.00003376628,0.00001355267,0.00015754836,0.0000702702,0.94758606,0.020572258,0.0004965033,0.00037681652,0.028258897],"study_design_scores_gemma":[0.0000020025086,0.000009353603,0.00014239876,5.6777736e-7,6.8706504e-7,0.0000021037208,0.0000026163605,0.99945,0.00035178554,0.000022338883,0.000015261481,8.273293e-7],"about_ca_topic_score_codex":0.008818066,"about_ca_topic_score_gemma":0.0047617736,"teacher_disagreement_score":0.008818066,"about_ca_system_score_codex":0.00022289804,"about_ca_system_score_gemma":0.00026044928,"threshold_uncertainty_score":0.017533481},"labels":[],"label_agreement":null},{"id":"W1973342232","doi":"10.2514/2.4530","title":"Vibration Suppression of Flexible Beams with Bonded Piezotransducers Using Wave-Absorbing Controllers","year":2000,"lang":"en","type":"article","venue":"Journal of Guidance Control and Dynamics","topic":"Aeroelasticity and Vibration Control","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":"Canadian Space Agency","funders":"","keywords":"Vibration; Vibration control; Acoustics; Structural engineering; Physics; Control theory (sociology); Computer science; Engineering; Control (management)","score_opus":0.007771174958388248,"score_gpt":0.20103568663351176,"score_spread":0.1932645116751235,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1973342232","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":[0.34332666,0.00023069464,0.65395164,0.000059627746,0.000039502294,0.000022482585,0.000015740763,0.00035515972,0.0019985426],"genre_scores_gemma":[0.9633142,0.000083495186,0.035465207,0.000018484941,0.000008638001,0.000027490129,0.000011249952,0.000010755746,0.0010604551],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999925,0.00000945805,0.0000040651967,0.00001392312,0.000039070965,0.000008408756],"domain_scores_gemma":[0.9999031,0.000032783413,0.000027523065,0.000013875175,0.000015497044,0.0000071902637],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012196146,0.00030132566,0.00019090253,0.000111949455,0.000110281,0.0001849023,0.0004376153,0.00024373521,0.00054131594],"category_scores_gemma":[0.00020700826,0.00016611305,0.00015259202,0.00008983092,0.0002773426,0.0003091664,0.00029070745,0.00022607863,0.00010098807],"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":[0.00014994272,0.00008863121,0.0004305124,0.00007249366,0.000031005315,0.00008631409,0.00011565313,0.09036216,0.83385617,0.0045991116,0.00025827406,0.06994979],"study_design_scores_gemma":[0.000041970503,0.00032820023,0.0005509542,0.000008128395,0.000017702785,0.000043959044,0.000018079041,0.8456312,0.1512351,0.0011209283,0.0009890738,0.000014741379],"about_ca_topic_score_codex":0.00032071568,"about_ca_topic_score_gemma":0.0005991571,"teacher_disagreement_score":0.00054131594,"about_ca_system_score_codex":0.00010543037,"about_ca_system_score_gemma":0.0001035068,"threshold_uncertainty_score":0.0018109083},"labels":[],"label_agreement":null},{"id":"W1973533054","doi":"10.1109/tmech.2005.844710","title":"Flexure Control Using Piezostack Actuators: Design and Implementation","year":2005,"lang":"en","type":"article","venue":"IEEE/ASME Transactions on Mechatronics","topic":"Aeroelasticity and Vibration Control","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":"Western University","funders":"","keywords":"Controllability; Control theory (sociology); Actuator; Active vibration control; Stiffness; Vibration control; Bending moment; Controller (irrigation); Vibration; Boundary value problem; Computer science; Engineering; Control engineering; Structural engineering; Control (management); Mathematics; Physics; Mathematical analysis","score_opus":0.014968577143404747,"score_gpt":0.25024431461898144,"score_spread":0.2352757374755767,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1973533054","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":[0.06467477,0.0007197075,0.9286818,0.00011588433,0.00005849463,0.00012189874,0.000028583738,0.00041485648,0.0051840227],"genre_scores_gemma":[0.83242345,0.0004634154,0.16236137,0.000035681616,0.000021575022,0.00015407911,0.000035478537,0.00001625409,0.0044887415],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998568,0.00001599766,0.000011463385,0.000027401715,0.00007796976,0.000010303542],"domain_scores_gemma":[0.9999219,0.000023036679,0.000017501146,0.000010006022,0.000019647103,0.000007866306],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018252073,0.00027389344,0.00018293175,0.00014470045,0.00016312231,0.00036442955,0.00056103605,0.00042282417,0.0016510229],"category_scores_gemma":[0.00022641926,0.00017186381,0.00010103162,0.000114760885,0.0002527107,0.00033210302,0.00024008781,0.0003107364,0.00022497853],"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":[0.00039738507,0.00016294605,0.0017078683,0.00058449793,0.000040292525,0.00032312277,0.0002242494,0.08281458,0.522614,0.023688555,0.0006963276,0.3667461],"study_design_scores_gemma":[0.000099982026,0.0010850447,0.0028292492,0.000056008346,0.000036922087,0.00049016566,0.00007447975,0.7784449,0.19700858,0.0026310072,0.017189333,0.000054205586],"about_ca_topic_score_codex":0.0007452246,"about_ca_topic_score_gemma":0.0008508154,"teacher_disagreement_score":0.0016510229,"about_ca_system_score_codex":0.00015531109,"about_ca_system_score_gemma":0.00023995027,"threshold_uncertainty_score":0.005523205},"labels":[],"label_agreement":null},{"id":"W1974251336","doi":"10.1155/2012/695475","title":"Morphing of Bistable Composite Laminates Using Distributed Piezoelectric Actuators","year":2012,"lang":"en","type":"article","venue":"Smart Materials Research","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":29,"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 Laval","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Morphing; Materials science; Curvature; Composite laminates; Composite material; Actuator; Bistability; Piezoelectricity; Finite element method; Composite number; STRIPS; Displacement (psychology); Hinge; Structural engineering; Geometry; Computer science","score_opus":0.050898859790747784,"score_gpt":0.30877781300958457,"score_spread":0.2578789532188368,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1974251336","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":[0.9842778,0.00019055641,0.014155098,0.000027443773,0.000018335446,0.000012867852,0.000019379873,0.00010595416,0.0011925938],"genre_scores_gemma":[0.99226695,0.00009476026,0.00693865,0.000015089416,0.00000395002,0.000009407884,0.000017016593,0.0000109909715,0.0006431959],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99995613,0.0000053388153,0.0000022847714,0.000008917789,0.000019403637,0.000007896128],"domain_scores_gemma":[0.99990463,0.000024308478,0.000033928984,0.000014840554,0.000011496646,0.000010813292],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00007382976,0.00018315339,0.00011091896,0.00017429322,0.00013079785,0.00017658561,0.00012340152,0.0001547889,0.00033974522],"category_scores_gemma":[0.00015889721,0.0001405904,0.00012286459,0.00008072741,0.00022625006,0.0001980512,0.00021285833,0.00015439164,0.000058529833],"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":[0.000025230269,0.0000098418805,0.00015441065,0.000023410863,0.0000034550983,0.00009489179,0.00003009683,0.0028909934,0.9915815,0.00015286735,0.000028164335,0.0050052213],"study_design_scores_gemma":[0.0000132971745,0.00023040856,0.0027761306,0.000006585259,0.0000066242737,0.00016901961,0.00003292052,0.038051065,0.95750356,0.00015199461,0.0010481239,0.000010445685],"about_ca_topic_score_codex":0.00016281883,"about_ca_topic_score_gemma":0.00049551233,"teacher_disagreement_score":0.00033974522,"about_ca_system_score_codex":0.00014834343,"about_ca_system_score_gemma":0.0000718898,"threshold_uncertainty_score":0.0011365414},"labels":[],"label_agreement":null},{"id":"W1974803801","doi":"10.2514/6.2015-1256","title":"New methodology for the controller of an electrical actuator for morphing a wing","year":2015,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"École de Technologie Supérieure","funders":"Consortium de Recherche et d’innovation en Aérospatiale au Québec","keywords":"Morphing; Actuator; Wing; Computer science; Pneumatic actuator; Control engineering; Aerospace engineering; Engineering; Artificial intelligence","score_opus":0.10793395063228003,"score_gpt":0.31327122621729786,"score_spread":0.20533727558501783,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1974803801","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":[0.0007942074,0.00024467675,0.995695,0.000029207924,0.00008616609,0.00005063454,0.0000152388375,0.00021144132,0.002873469],"genre_scores_gemma":[0.2366294,0.0013894757,0.7397182,0.00021505509,0.00021337337,0.0010109108,0.0001674172,0.00015614883,0.020499947],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997062,0.000034455534,0.000023172846,0.00007358797,0.00014400929,0.000018618732],"domain_scores_gemma":[0.99988437,0.00002713837,0.000018940758,0.000014477772,0.000049121743,0.0000059435474],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003347978,0.0008116215,0.00056351366,0.0004598051,0.00042071257,0.0007398941,0.0011680607,0.00073977455,0.0043633],"category_scores_gemma":[0.00037502742,0.00027520434,0.0006523902,0.0002102877,0.0004600057,0.0004531006,0.0006629198,0.0008384254,0.0010522607],"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":[0.00010063288,0.000144019,0.0007121766,0.0015802037,0.00013660266,0.00082102494,0.00041741095,0.33540368,0.19131759,0.12670153,0.0041313344,0.33853385],"study_design_scores_gemma":[0.000039138493,0.0004355653,0.00046632238,0.00011361327,0.00006207874,0.00051485136,0.00004596068,0.9133265,0.020274136,0.012570239,0.05210604,0.000045526493],"about_ca_topic_score_codex":0.0012994286,"about_ca_topic_score_gemma":0.0015862603,"teacher_disagreement_score":0.0043633,"about_ca_system_score_codex":0.00035573982,"about_ca_system_score_gemma":0.00057365675,"threshold_uncertainty_score":0.014596701},"labels":[],"label_agreement":null},{"id":"W1978080733","doi":"10.1088/0964-1726/24/3/037006","title":"Analysis and design of lattice materials for large cord and curvature variations in skin panels of morphing wings","year":2015,"lang":"en","type":"article","venue":"Smart Materials and Structures","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":27,"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":"Royal Society","keywords":"Morphing; Curvature; Camber (aerodynamics); Wing; Aerodynamics; Planar; Structural engineering; Homogenization (climate); Nonlinear system; Computer science; Mechanical engineering; Materials science; Engineering; Aerospace engineering; Geometry; Physics; Mathematics; Artificial intelligence","score_opus":0.018578858527950177,"score_gpt":0.23773683648241586,"score_spread":0.21915797795446568,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1978080733","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":[0.6658995,0.00085903093,0.31280813,0.00024827057,0.000058166694,0.000090738926,0.00007616262,0.00016468095,0.019795239],"genre_scores_gemma":[0.96047115,0.00024045768,0.03770424,0.000019917075,0.0000072917474,0.0000395851,0.00002083811,0.000031912376,0.0014645301],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999453,0.000014545973,0.0000017431984,0.000009517019,0.0000205162,0.000008355773],"domain_scores_gemma":[0.99989235,0.000046557965,0.000022733382,0.000010832337,0.000013725309,0.000013801833],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015097455,0.00019861778,0.00019886829,0.0002752505,0.00013759309,0.00040236322,0.00022821927,0.00037858431,0.0010042039],"category_scores_gemma":[0.00033050164,0.00019957799,0.00018152676,0.00014118473,0.00047747887,0.0002668534,0.00020410404,0.0002227727,0.00016861175],"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":[0.000074284944,0.000079441445,0.0014950727,0.00017687358,0.0000144945125,0.0002460654,0.00007933969,0.68226635,0.2677002,0.034443576,0.0004021177,0.01302229],"study_design_scores_gemma":[0.00001090785,0.00004750497,0.0004094837,0.00000757309,0.000003394184,0.00005179944,0.000023984974,0.9847195,0.011598891,0.002216036,0.00090375205,0.000007084727],"about_ca_topic_score_codex":0.0002961855,"about_ca_topic_score_gemma":0.00049453345,"teacher_disagreement_score":0.0010042039,"about_ca_system_score_codex":0.00025061387,"about_ca_system_score_gemma":0.00020732688,"threshold_uncertainty_score":0.0033593774},"labels":[],"label_agreement":null},{"id":"W198116453","doi":"10.4203/ccp.75.41","title":"Application of the Dynamic Finite Element Formulation in Flutter Analysis of Wings","year":2009,"lang":"en","type":"article","venue":"Civil-comp proceedings","topic":"Aeroelasticity and Vibration Control","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":"Flutter; Finite element method; Computer science; Wing; Structural engineering; Aerodynamics; Engineering; Aerospace engineering","score_opus":0.004525699116515713,"score_gpt":0.20593906902063092,"score_spread":0.2014133699041152,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W198116453","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":[0.010882366,0.00026008007,0.9865165,0.00006694834,0.000020938145,0.000022725171,0.000022991382,0.000060945076,0.0021464687],"genre_scores_gemma":[0.5924057,0.001076336,0.3981376,0.00010961511,0.0000478846,0.0002789984,0.00015806718,0.00013091738,0.007654952],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99981564,0.00006188678,0.0000073463593,0.00002187611,0.0000793481,0.000013891134],"domain_scores_gemma":[0.9997955,0.00011812541,0.000013026085,0.000020882591,0.000044090386,0.000008443278],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004178964,0.00042536607,0.00044063525,0.00045172987,0.0002680189,0.00038226476,0.0005556277,0.00092813984,0.0014845231],"category_scores_gemma":[0.000889528,0.0002733138,0.0005659833,0.00019831085,0.00054807554,0.0004379387,0.0005376542,0.0005523078,0.00040996022],"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":[0.000044382283,0.00006462094,0.0010709695,0.00018061274,0.000040419316,0.00030012333,0.00023039381,0.8152028,0.06248352,0.048401892,0.0005086472,0.07147168],"study_design_scores_gemma":[0.0000035268617,0.000022056029,0.00020175049,0.000013877398,0.0000029888674,0.00007506058,0.0000183039,0.99104846,0.0024998325,0.003691019,0.0024157232,0.0000073396836],"about_ca_topic_score_codex":0.0015103235,"about_ca_topic_score_gemma":0.0010582836,"teacher_disagreement_score":0.0015103235,"about_ca_system_score_codex":0.0002116899,"about_ca_system_score_gemma":0.0003706987,"threshold_uncertainty_score":0.0049661994},"labels":[],"label_agreement":null},{"id":"W1982280704","doi":"10.1121/1.2934654","title":"Decentralised active control of single - frequency panel vibrations using piezoelectric actuator - sensor pairs","year":2008,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aeroelasticity and Vibration Control","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":"Actuator; Control theory (sociology); Vibration control; Passivity; Bending; Vibration; Diagonal; Compensation (psychology); Piezoelectric sensor; Piezoelectricity; Matrix (chemical analysis); Frequency response; Active vibration control; Acoustics; Materials science; Computer science; Control (management); Structural engineering; Engineering; Physics; Mathematics","score_opus":0.022553840801620408,"score_gpt":0.21905186701596782,"score_spread":0.19649802621434742,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1982280704","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":[0.102478795,0.00014346244,0.893884,0.00007450168,0.00006163332,0.0000581997,0.000021066295,0.0004364449,0.002841918],"genre_scores_gemma":[0.97065204,0.000055799253,0.027685277,0.000022091659,0.00002234951,0.000053281456,0.000015653444,0.000014685052,0.0014787692],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9995378,0.00007245354,0.000023114982,0.00016897121,0.00014862222,0.00004902578],"domain_scores_gemma":[0.9995078,0.00019720786,0.000101869635,0.00008111817,0.00008076932,0.0000311977],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00037035253,0.0006431647,0.0006431393,0.00015256934,0.00029596756,0.0005793825,0.00084793207,0.00036965872,0.0014866982],"category_scores_gemma":[0.00067748735,0.0003412604,0.00034328445,0.0001349148,0.00051639037,0.0006612224,0.00075954356,0.00072470354,0.0002796868],"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":[0.0007262237,0.00029225368,0.0008892025,0.00030286342,0.0001361115,0.00024135396,0.0003553499,0.32740736,0.55583835,0.007891482,0.00073677587,0.105182685],"study_design_scores_gemma":[0.00011143424,0.00067735894,0.0012388316,0.000017989994,0.00004652262,0.00015053862,0.000051796193,0.8925936,0.098883316,0.00424588,0.0019447743,0.00003792972],"about_ca_topic_score_codex":0.0004667853,"about_ca_topic_score_gemma":0.001035726,"teacher_disagreement_score":0.0014866982,"about_ca_system_score_codex":0.0002466337,"about_ca_system_score_gemma":0.00028281278,"threshold_uncertainty_score":0.004973471},"labels":[],"label_agreement":null},{"id":"W1983597452","doi":"10.1177/1045389x06072400","title":"Optimization of Piezoelectric Actuator Configuration on a Flexible Fin for Vibration Control using Genetic Algorithms","year":2007,"lang":"en","type":"article","venue":"Journal of Intelligent Material Systems and Structures","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":24,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"National Research Council Canada; Carleton University","funders":"National Research Council Canada; Natural Sciences and Engineering Research Council of Canada; Ministère de la Défense Nationale","keywords":"Fin; Actuator; Fitness function; Genetic algorithm; Control theory (sociology); Vibration; Frequency response; Vibration control; Engineering; Polynomial; Function (biology); Algorithm; Computer science; Mathematical optimization; Mathematics; Acoustics; Control (management); Mechanical engineering; Physics; Artificial intelligence; Mathematical analysis","score_opus":0.014317836596544219,"score_gpt":0.2427297007276939,"score_spread":0.22841186413114967,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1983597452","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":[0.29619688,0.00019925812,0.6997615,0.000118434975,0.000027433642,0.00006656125,0.00002462689,0.0002469963,0.0033583855],"genre_scores_gemma":[0.8588211,0.00008856038,0.1397582,0.000026590622,0.00000861281,0.0000998843,0.000033231245,0.000036733258,0.0011271297],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997907,0.00005003123,0.000008648386,0.000050184964,0.00006619547,0.000034255496],"domain_scores_gemma":[0.9997179,0.0001549099,0.00004572861,0.000024043065,0.000044051198,0.000013332848],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00042346274,0.00075771805,0.00060122076,0.0004271971,0.0003018021,0.00037528615,0.0005373604,0.0006134073,0.0007709093],"category_scores_gemma":[0.0011505762,0.00035614532,0.00035844775,0.00028276208,0.00048571965,0.00037904092,0.0003829357,0.00038305143,0.00014059401],"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":[0.000029785702,0.000043154618,0.00045224442,0.00002284995,0.000017690192,0.00004528469,0.000023686162,0.9624577,0.015489086,0.00090530043,0.0000985289,0.020414656],"study_design_scores_gemma":[0.000014923814,0.00007785745,0.00030984575,0.000004245571,0.0000109829625,0.000021376867,0.000017295328,0.99431556,0.004347686,0.000655212,0.0002177091,0.000007232256],"about_ca_topic_score_codex":0.0015106207,"about_ca_topic_score_gemma":0.002073281,"teacher_disagreement_score":0.0015106207,"about_ca_system_score_codex":0.00041615515,"about_ca_system_score_gemma":0.0005913625,"threshold_uncertainty_score":0.003019452},"labels":[],"label_agreement":null},{"id":"W1984059022","doi":"10.2514/6.2014-3170","title":"New Numerical Study of Boundary Layer Behavior on A Morphing Wing-with-Aileron System","year":2014,"lang":"en","type":"article","venue":"32nd AIAA Applied Aerodynamics Conference","topic":"Aeroelasticity and Vibration Control","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":"École de Technologie Supérieure","funders":"Department of Health and Social Care; National Institute for Health and Care Research","keywords":"Morphing; Aileron; Wing; Boundary layer; Computer science; Structural engineering; Aerospace engineering; Engineering; Computer vision","score_opus":0.011210830959235599,"score_gpt":0.20191506380511057,"score_spread":0.19070423284587495,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1984059022","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":[0.81041133,0.0011757665,0.13910662,0.002116442,0.0004997436,0.00033678467,0.0011565476,0.00052939623,0.044667322],"genre_scores_gemma":[0.96909887,0.00021171097,0.024613878,0.0002511772,0.000054877186,0.00012700932,0.0003662139,0.00009085902,0.005185354],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99957687,0.00014743384,0.000025789772,0.000077789664,0.00006609899,0.000106055675],"domain_scores_gemma":[0.99795556,0.0011642445,0.0002707436,0.000111080524,0.00031132516,0.0001870128],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0007197751,0.0005482574,0.0007266748,0.0010983145,0.0011084757,0.0019368449,0.0012721289,0.0028803495,0.00639491],"category_scores_gemma":[0.004709481,0.00032717732,0.0008834553,0.00062962505,0.0013642326,0.0011673766,0.0014113548,0.0011307541,0.00053104374],"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":[0.0002433091,0.00025050857,0.027064642,0.00017815887,0.00008573964,0.00095599913,0.00052702497,0.92645866,0.0045395973,0.026105225,0.0029680037,0.010623074],"study_design_scores_gemma":[0.000011092237,0.000019203282,0.0011640983,0.000013297134,0.0000045000634,0.00003068345,0.0000990134,0.9963708,0.00014903884,0.001546892,0.0005810983,0.000010180896],"about_ca_topic_score_codex":0.022955054,"about_ca_topic_score_gemma":0.009312573,"teacher_disagreement_score":0.022955054,"about_ca_system_score_codex":0.0009963011,"about_ca_system_score_gemma":0.0010357448,"threshold_uncertainty_score":0.045642912},"labels":[],"label_agreement":null},{"id":"W1985072536","doi":"10.1115/fedsm-icnmm2010-31104","title":"Experimental and Numerical Study of a Pitching Blade","year":2010,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Aerodynamics; Mechanics; Finite volume method; Turbulence; Lift (data mining); Stall (fluid mechanics); Reynolds-averaged Navier–Stokes equations; Reynolds number; Physics; Computer simulation; Blade (archaeology); Mathematics; Structural engineering; Engineering; Computer science","score_opus":0.006835759669851959,"score_gpt":0.2264997428147769,"score_spread":0.21966398314492494,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1985072536","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":[0.9916425,0.000091518305,0.007559476,0.000012577714,0.000014991962,0.000025805577,0.000093137875,0.000054130473,0.0005058871],"genre_scores_gemma":[0.9901174,0.00009550812,0.008983734,0.000008110792,0.0000078160065,0.000022167505,0.00012529558,0.000010392159,0.0006295756],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99973565,0.000033427787,0.000017168039,0.00006142579,0.000120610086,0.000031691983],"domain_scores_gemma":[0.99922645,0.00025475165,0.00007940176,0.00020141814,0.00018446328,0.000053412958],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000351354,0.00025026023,0.00027866522,0.0002276846,0.00033007687,0.00014194769,0.00020615655,0.00030681238,0.0017188281],"category_scores_gemma":[0.0006969446,0.00016127108,0.00015935772,0.00018384101,0.0003419195,0.00019832334,0.00019789021,0.0002979752,0.00026477425],"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":[0.00014610692,0.00012123622,0.0019923158,0.000063617656,0.0000047255244,0.00013431956,0.00014850036,0.0024989846,0.98862606,0.000110509965,0.00006221951,0.006091395],"study_design_scores_gemma":[0.00006527895,0.0061370796,0.044053104,0.000015631997,0.000035117628,0.0008039368,0.00025756157,0.035051715,0.91039234,0.0002669007,0.0028727427,0.000048657337],"about_ca_topic_score_codex":0.00037128775,"about_ca_topic_score_gemma":0.0003279621,"teacher_disagreement_score":0.0017188281,"about_ca_system_score_codex":0.000092222166,"about_ca_system_score_gemma":0.000110373694,"threshold_uncertainty_score":0.0057500005},"labels":[],"label_agreement":null},{"id":"W1985502404","doi":"10.1243/09544100jaero522","title":"Adaptive neuro-fuzzy inference system-based controllers for smart material actuator modelling","year":2009,"lang":"en","type":"article","venue":"Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":72,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure","funders":"","keywords":"Actuator; Adaptive neuro fuzzy inference system; Control theory (sociology); Neuro-fuzzy; Computer science; Control engineering; Controller (irrigation); Fuzzy control system; MATLAB; Fuzzy logic; Engineering; Artificial intelligence; Control (management)","score_opus":0.012547195839843902,"score_gpt":0.196902209280934,"score_spread":0.1843550134410901,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1985502404","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":[0.008445719,0.00021615264,0.9884609,0.00005631037,0.00004461719,0.000049932016,0.00002764185,0.0005683985,0.0021302262],"genre_scores_gemma":[0.73884153,0.00027743238,0.2548905,0.00010339531,0.00004964852,0.0004995336,0.00012502723,0.00005698097,0.0051558986],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996939,0.00006605013,0.000024167888,0.000060950108,0.00012770532,0.00002725852],"domain_scores_gemma":[0.99957746,0.00019112768,0.00004729005,0.000029720488,0.00014452163,0.000009813207],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00061879004,0.0006064108,0.0006003032,0.00032081202,0.0003734868,0.00073910435,0.001034826,0.00088165986,0.0018353314],"category_scores_gemma":[0.0014460029,0.0003383063,0.0005099939,0.0002560284,0.0004563488,0.0005232086,0.0003646879,0.001090071,0.0005211026],"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":[0.00006276038,0.000036609694,0.00022408624,0.0000758143,0.00004037322,0.000060655486,0.00006772109,0.9406279,0.005802685,0.0034072818,0.00056209136,0.049031965],"study_design_scores_gemma":[0.0000044371595,0.000012690297,0.00006033832,0.0000039595957,0.000004053479,0.000005681983,0.0000023916898,0.9985216,0.0006754649,0.00037656754,0.00032926377,0.0000034994164],"about_ca_topic_score_codex":0.007906678,"about_ca_topic_score_gemma":0.008642793,"teacher_disagreement_score":0.007906678,"about_ca_system_score_codex":0.00055903674,"about_ca_system_score_gemma":0.00064741186,"threshold_uncertainty_score":0.015721321},"labels":[],"label_agreement":null},{"id":"W1987390841","doi":"10.1115/imece2002-33063","title":"An Investigation of the Aeroelastic Response of a Two-Dimensional, Structurally Nonlinear Airfoil Subject to External Excitation","year":2002,"lang":"en","type":"article","venue":"5th International Symposium on Fluid Structure Interaction, Aeroelasticity, and Flow Induced Vibration and Noise","topic":"Aeroelasticity and Vibration Control","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":"McGill University","funders":"","keywords":"Airfoil; Aeroelasticity; Nonlinear system; Fourier transform; Aerodynamics; Frequency domain; Frequency response; Fourier series; Harmonic; Physics; Mathematical analysis; Acoustics; Control theory (sociology); Mechanics; Mathematics; Computer science; Engineering","score_opus":0.013818443794668298,"score_gpt":0.24837813683962687,"score_spread":0.23455969304495858,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1987390841","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":[0.9719919,0.00009513336,0.019841531,0.00010229512,0.00001795497,0.000055017917,0.00008212843,0.00013050147,0.0076834955],"genre_scores_gemma":[0.9963813,0.000066660905,0.0018473502,0.000013808173,0.0000054608713,0.000022351616,0.000039728664,0.000015929223,0.001607442],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998202,0.000032096905,0.0000061529745,0.000023301367,0.00008623064,0.000032127347],"domain_scores_gemma":[0.9993851,0.00042098432,0.00004313182,0.000046729354,0.00007803195,0.000026016516],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024117807,0.00033738336,0.000443408,0.00025888238,0.00043011937,0.00034140275,0.00031011074,0.00057656475,0.0013307997],"category_scores_gemma":[0.0016490074,0.00012670115,0.00036546786,0.00016635541,0.000583687,0.0002682288,0.0003994971,0.00039941637,0.00018653482],"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":[0.0006358895,0.00022391004,0.005383808,0.0004075728,0.000059677262,0.0016414176,0.0006023122,0.42697555,0.5395991,0.002178421,0.00045979454,0.021832503],"study_design_scores_gemma":[0.000018322344,0.0005304022,0.007830588,0.00001832173,0.000016834563,0.000260254,0.00021231631,0.93836766,0.05167211,0.00028806584,0.00076195085,0.000023200255],"about_ca_topic_score_codex":0.002122647,"about_ca_topic_score_gemma":0.001767707,"teacher_disagreement_score":0.002122647,"about_ca_system_score_codex":0.0002718652,"about_ca_system_score_gemma":0.0003119507,"threshold_uncertainty_score":0.0044519305},"labels":[],"label_agreement":null},{"id":"W1989041713","doi":"10.1121/1.4831366","title":"Virtual mechanical impedance approach for the active structural acoustic control of panels","year":2013,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aeroelasticity and Vibration Control","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":"Actuator; Acoustics; Radiation impedance; Acoustic impedance; Piezoelectric sensor; Controller (irrigation); Electrical impedance; Sound transmission class; Transducer; Vibration control; Engineering; Vibration; Computer science; Piezoelectricity; Electrical engineering; Physics","score_opus":0.00952078717329481,"score_gpt":0.2195133651270094,"score_spread":0.2099925779537146,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1989041713","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":[0.012068391,0.000104594124,0.9845925,0.000058201018,0.0000226353,0.000016429649,0.0000054896927,0.000053755528,0.0030779385],"genre_scores_gemma":[0.9158966,0.0001969915,0.079322234,0.00006517927,0.000038104943,0.00008460791,0.0000140924185,0.000026074234,0.004356069],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997732,0.00005238343,0.00000838162,0.000034654153,0.00011299628,0.000018382249],"domain_scores_gemma":[0.9998024,0.00010608578,0.000031097385,0.000014409974,0.00003739517,0.000008551088],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00031342724,0.00043108832,0.00026989338,0.00017855267,0.00018843704,0.0006531507,0.0005332744,0.00036610427,0.0017676188],"category_scores_gemma":[0.00057425915,0.00016237354,0.00022446965,0.00011579274,0.00059238804,0.00048120687,0.0005148678,0.00045483417,0.00023805368],"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":[0.00016653899,0.000082329,0.00023600539,0.00017401647,0.0000342952,0.00010147561,0.0001624842,0.73220134,0.14394277,0.051058333,0.00043490742,0.071405515],"study_design_scores_gemma":[0.000012423934,0.00011671033,0.00009610077,0.000006377746,0.0000073745264,0.000021998303,0.000014477532,0.98697764,0.0071555246,0.0041999836,0.0013821292,0.000009242568],"about_ca_topic_score_codex":0.00042392436,"about_ca_topic_score_gemma":0.0007133459,"teacher_disagreement_score":0.0017676188,"about_ca_system_score_codex":0.00033858785,"about_ca_system_score_gemma":0.00030678167,"threshold_uncertainty_score":0.0059132576},"labels":[],"label_agreement":null},{"id":"W1991868322","doi":"10.1109/cdc.2014.7039442","title":"Comparison of stabilization of current-actuated and voltage-actuated piezoelectric beams","year":2014,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"University of Waterloo","funders":"","keywords":"Voltage; Control theory (sociology); Current (fluid); Piezoelectricity; Beam (structure); Physics; Operator (biology); Bernoulli's principle; Mechanics; Acoustics; Computer science; Control (management); Optics","score_opus":0.018936945449688988,"score_gpt":0.2666004274398089,"score_spread":0.2476634819901199,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1991868322","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":[0.7990266,0.0027205218,0.17721522,0.00031544012,0.00016873403,0.000072705996,0.000077075165,0.0003624079,0.020041361],"genre_scores_gemma":[0.99499375,0.00027314882,0.0035664623,0.00001607436,0.00000767933,0.00002105127,0.000026852364,0.000009982074,0.0010849915],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998747,0.000022771603,0.000010427091,0.000024711886,0.000050103958,0.000017300525],"domain_scores_gemma":[0.9996867,0.00014430426,0.00004795304,0.000030644846,0.000073836374,0.000016581866],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00036109763,0.00024982396,0.00031625928,0.00035677332,0.00019370808,0.00042013242,0.00041921987,0.0005160578,0.0012152195],"category_scores_gemma":[0.0007063918,0.00010683202,0.00029781644,0.00014102315,0.00043263167,0.00043317516,0.00036154955,0.00018779832,0.00011620265],"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":[0.00097292935,0.00016214483,0.0016322888,0.000701437,0.000115922354,0.00034294455,0.0004918306,0.4174568,0.4520331,0.04282809,0.000709552,0.082552984],"study_design_scores_gemma":[0.00004964742,0.00037013297,0.0013593149,0.000031272994,0.000022136,0.000042050917,0.00005668232,0.9356564,0.058045812,0.0031653221,0.0011805586,0.000020754846],"about_ca_topic_score_codex":0.0008282512,"about_ca_topic_score_gemma":0.00052020105,"teacher_disagreement_score":0.0012152195,"about_ca_system_score_codex":0.00022946688,"about_ca_system_score_gemma":0.00017805285,"threshold_uncertainty_score":0.004065335},"labels":[],"label_agreement":null},{"id":"W1992437526","doi":"10.1016/j.matdes.2009.09.011","title":"Shape morphing of aircraft wing: Status and challenges","year":2009,"lang":"en","type":"article","venue":"Materials & Design (1980-2015)","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":706,"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":"Morphing; SMA*; Shape-memory alloy; Wing; Actuator; Aerodynamics; Smart material; Shape-memory polymer; Structural engineering; Mechanical engineering; Aerospace engineering; Computer science; Work (physics); Engineering; Materials science; Artificial intelligence; Nanotechnology","score_opus":0.03130614247250663,"score_gpt":0.23297987063380735,"score_spread":0.20167372816130072,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1992437526","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":[0.3721065,0.53801745,0.010756146,0.013100325,0.00085407664,0.000045460074,0.00060476176,0.00018027642,0.06433501],"genre_scores_gemma":[0.7459018,0.23347627,0.007105257,0.0010059681,0.00070864946,0.000029764547,0.00039189233,0.000061569146,0.0113187665],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.99964607,0.0000616475,0.000029001269,0.00008815074,0.00011456067,0.000060633723],"domain_scores_gemma":[0.9989747,0.0003946759,0.00013924799,0.00010734484,0.00029862576,0.00008544037],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0013819463,0.00020960353,0.00046039606,0.0007724793,0.00050889497,0.001841431,0.0009959148,0.00076765986,0.0037931744],"category_scores_gemma":[0.0013388857,0.00020531971,0.00023081065,0.0011045934,0.0026640974,0.002655549,0.00096646376,0.0006147643,0.0005998985],"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":[0.00024378955,0.00017979018,0.01184436,0.0009895375,0.00002004382,0.00008560079,0.00040155998,0.008310508,0.0094969645,0.024909465,0.005039052,0.93847924],"study_design_scores_gemma":[0.000055888064,0.0014374831,0.11939725,0.0015493396,0.0000694005,0.0019482375,0.008149751,0.040195234,0.036794163,0.074330315,0.7158891,0.00018382682],"about_ca_topic_score_codex":0.0039699934,"about_ca_topic_score_gemma":0.0060431007,"teacher_disagreement_score":0.0039699934,"about_ca_system_score_codex":0.0011333504,"about_ca_system_score_gemma":0.0013632956,"threshold_uncertainty_score":0.012689471},"labels":[],"label_agreement":null},{"id":"W1992911590","doi":"10.1088/0964-1726/19/10/105025","title":"Repair of a delaminated plate under static loading with piezoelectric patches","year":2010,"lang":"en","type":"article","venue":"Smart Materials and Structures","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":29,"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 Manitoba","funders":"Canada Research Chairs","keywords":"Delamination (geology); Piezoelectricity; Materials science; Finite element method; Composite material; Structural engineering; Voltage; Ultimate tensile strength; Electrode; Shear (geology); Fracture (geology); Stress (linguistics); Engineering; Electrical engineering; Geology","score_opus":0.004577732448510084,"score_gpt":0.1849177695138735,"score_spread":0.18034003706536342,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1992911590","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":[0.9392522,0.00041518605,0.058435794,0.00008680318,0.000065701926,0.000026612315,0.000037898,0.00025312928,0.0014265986],"genre_scores_gemma":[0.9828295,0.00018823329,0.015313655,0.0000130441795,0.0000052971423,0.000008889132,0.000029784453,0.000013884595,0.0015977354],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99986875,0.0000068089034,0.00000860424,0.000024183577,0.00007380855,0.000017884426],"domain_scores_gemma":[0.9997484,0.0000503707,0.00005818253,0.000073747884,0.000041685205,0.000027566879],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015711309,0.0003599696,0.00036906204,0.00029473787,0.00019369442,0.00024174902,0.0004942693,0.0005909396,0.0006102226],"category_scores_gemma":[0.00036094154,0.00023150425,0.00024393748,0.00012610284,0.0004288312,0.00025251947,0.0003596005,0.0003155133,0.00018796278],"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":[0.000091241825,0.000050202652,0.0006659085,0.00014751314,0.000026658361,0.0011643566,0.00009672055,0.039494973,0.941828,0.00052267435,0.00010148123,0.015810246],"study_design_scores_gemma":[0.0000393839,0.0012806423,0.0052966108,0.000033603344,0.00006515651,0.003165518,0.00018515042,0.27031994,0.7167669,0.00052411953,0.002286683,0.000036261463],"about_ca_topic_score_codex":0.0006520881,"about_ca_topic_score_gemma":0.0005619981,"teacher_disagreement_score":0.0006520881,"about_ca_system_score_codex":0.00017447562,"about_ca_system_score_gemma":0.00026506925,"threshold_uncertainty_score":0.002041459},"labels":[],"label_agreement":null},{"id":"W1995380237","doi":"10.1115/smasis2009-1245","title":"Real-Time Optimization of a Research Morphing Laminar Wing in a Wind Tunnel","year":2009,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Bombardier (Canada); National Research Council Canada; École de Technologie Supérieure","funders":"Natural Sciences and Engineering Research Council of Canada; Thales Group","keywords":"Wind tunnel; Laminar flow; Drag; Morphing; Lift-to-drag ratio; Angle of attack; Aerodynamics; Wing; Control theory (sociology); Actuator; Computational fluid dynamics; Computer science; Aerospace engineering; Structural engineering; Engineering","score_opus":0.021453148022871436,"score_gpt":0.2713370379156056,"score_spread":0.24988388989273416,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1995380237","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":[0.43319792,0.00009427274,0.5627298,0.000054253087,0.000020541096,0.00009122008,0.000029067016,0.0004333524,0.0033495966],"genre_scores_gemma":[0.9592813,0.000028999804,0.03980741,0.000007743675,0.0000021485678,0.00004627813,0.000019493178,0.0000143961415,0.0007922437],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999341,0.000016998136,0.0000034008563,0.000012262462,0.000023785145,0.000009414706],"domain_scores_gemma":[0.9998816,0.00004261171,0.000027529537,0.000012697212,0.000022727372,0.000012776103],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00032082605,0.00038858788,0.00019569429,0.00014449115,0.00014824346,0.00034074674,0.00028598352,0.00026793254,0.00055132003],"category_scores_gemma":[0.0003111369,0.00013937522,0.0001826393,0.000058366135,0.00023822987,0.00016202804,0.00025304078,0.00021124873,0.000081662794],"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":[0.00019394231,0.000107558764,0.0013248787,0.00012642944,0.000018465531,0.000113758004,0.000079777594,0.8432594,0.12179698,0.0011102922,0.00013906362,0.031729467],"study_design_scores_gemma":[0.000014218687,0.00022921771,0.00047737116,0.0000033690696,0.0000051813377,0.00001886766,0.000011618975,0.98980904,0.0089842975,0.000101367776,0.0003403594,0.0000050223753],"about_ca_topic_score_codex":0.0009910979,"about_ca_topic_score_gemma":0.0009187786,"teacher_disagreement_score":0.0009910979,"about_ca_system_score_codex":0.00013577663,"about_ca_system_score_gemma":0.0002966891,"threshold_uncertainty_score":0.0019706488},"labels":[],"label_agreement":null},{"id":"W1997117988","doi":"10.2514/6.2014-2187","title":"Control strategies for an experimental morphing wing model","year":2014,"lang":"en","type":"article","venue":"AIAA Atmospheric Flight Mechanics Conference","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":16,"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 du Québec","funders":"","keywords":"Morphing; Wing; Computer science; Control (management); Artificial intelligence; Engineering; Aerospace engineering","score_opus":0.020406309565418883,"score_gpt":0.22809642207230113,"score_spread":0.20769011250688224,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1997117988","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":[0.62582386,0.00012301342,0.3562155,0.00016538434,0.000065683096,0.00038381165,0.00046542878,0.0015253198,0.015232077],"genre_scores_gemma":[0.98220074,0.00002643804,0.015606883,0.00001048658,0.0000029310677,0.00018173935,0.00011731189,0.000023121811,0.0018304024],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99987376,0.000020379326,0.0000095596715,0.00002969,0.00004892879,0.000017697255],"domain_scores_gemma":[0.99982774,0.000051185598,0.000025878691,0.000038069156,0.000045255863,0.000011838438],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021757078,0.0003760151,0.00026976422,0.00021232605,0.00022152407,0.00047400748,0.0004673917,0.0003728109,0.003764221],"category_scores_gemma":[0.0004370329,0.00012515741,0.0003381101,0.00008612663,0.0003520234,0.0002853473,0.00037573968,0.0003930608,0.00022673619],"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":[0.00040870556,0.00015743634,0.0012191831,0.00016518333,0.000029658415,0.00013947941,0.0001359636,0.90584856,0.06837975,0.005134088,0.00032043588,0.018061452],"study_design_scores_gemma":[0.00004101811,0.00024870472,0.0005885898,0.0000050517333,0.000012989097,0.000013912733,0.000022686247,0.98189056,0.015855215,0.00048066126,0.000831083,0.000009547611],"about_ca_topic_score_codex":0.00374623,"about_ca_topic_score_gemma":0.0019746583,"teacher_disagreement_score":0.003764221,"about_ca_system_score_codex":0.0003190153,"about_ca_system_score_gemma":0.00030496664,"threshold_uncertainty_score":0.012592554},"labels":[],"label_agreement":null},{"id":"W1999835827","doi":"10.1007/bf01170839","title":"Modelling and analysis of piezoelectric actuators in anisotropic structures","year":2002,"lang":"en","type":"article","venue":"Acta Mechanica","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":6,"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":"Actuator; Piezoelectricity; Solid mechanics; Finite element method; Materials science; Anisotropy; Mechanics; Stress (linguistics); Mechanical engineering; Structural engineering; Physics; Composite material; Engineering; Electrical engineering","score_opus":0.013827890922998444,"score_gpt":0.1935256063516382,"score_spread":0.17969771542863977,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W1999835827","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":[0.10054175,0.0014873205,0.88438195,0.00038481483,0.00008124968,0.000051668936,0.00006998931,0.00022063595,0.012780523],"genre_scores_gemma":[0.9463061,0.0012758859,0.04406897,0.000041563922,0.00003731555,0.00008916645,0.000082279155,0.00006895818,0.008029775],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998503,0.00003335589,0.000009425236,0.000018660883,0.00006993765,0.00001831442],"domain_scores_gemma":[0.999788,0.00011895929,0.00003312829,0.000018130018,0.000030912728,0.000010912763],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00027787275,0.00049297867,0.0005991463,0.00032837476,0.0003033483,0.000734329,0.00086410047,0.0016203059,0.0009810859],"category_scores_gemma":[0.00088521175,0.0005809723,0.00055111066,0.0003746929,0.0007164136,0.00056857883,0.0005115648,0.0006058265,0.00023088529],"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":[0.000009061311,0.0000091986885,0.00012304891,0.000024767392,0.000007180457,0.000046526457,0.000023985334,0.989092,0.0032580462,0.0041603735,0.00007405567,0.0031717035],"study_design_scores_gemma":[0.0000020099321,0.0000039976157,0.00009747672,0.0000018453675,0.0000020085506,0.000011115572,0.0000043115306,0.9983107,0.00031905592,0.0010033381,0.00024202249,0.0000021368942],"about_ca_topic_score_codex":0.0051971753,"about_ca_topic_score_gemma":0.0036101611,"teacher_disagreement_score":0.0051971753,"about_ca_system_score_codex":0.000372632,"about_ca_system_score_gemma":0.00054811186,"threshold_uncertainty_score":0.010333836},"labels":[],"label_agreement":null},{"id":"W2002052908","doi":"10.1177/1045389x09356607","title":"Actuation of Slender Thin-wall Anisotropic Open Cross-section Beams Based on Asymptotically Correct Vlasov Theory","year":2009,"lang":"en","type":"article","venue":"Journal of Intelligent Material Systems and Structures","topic":"Aeroelasticity and Vibration Control","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":"Carleton University","funders":"Georgia Institute of Technology; Natural Sciences and Engineering Research Council of Canada; Utah State University","keywords":"Multiphysics; Timoshenko beam theory; Finite element method; Beam (structure); Cross section (physics); Anisotropy; Mathematical analysis; Physics; Mathematics; Structural engineering; Engineering; Optics","score_opus":0.012139287215434964,"score_gpt":0.25243567459394767,"score_spread":0.2402963873785127,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2002052908","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":[0.20343189,0.000206891,0.78688985,0.00015012447,0.000039225477,0.00003879556,0.000031010084,0.000122018675,0.009090209],"genre_scores_gemma":[0.957691,0.00017445096,0.038239416,0.000031324886,0.000014446495,0.00005931213,0.000028155737,0.00003204704,0.0037297944],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998511,0.00003511963,0.0000053554995,0.000013955589,0.00007315086,0.000021213797],"domain_scores_gemma":[0.9998416,0.00006608069,0.0000274389,0.000020125697,0.00003106908,0.000013729483],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00040160122,0.0002893989,0.00037816697,0.0002802107,0.00020114107,0.00043850203,0.000478638,0.00044992493,0.0006356536],"category_scores_gemma":[0.00055058696,0.00022158449,0.00039798935,0.00013995518,0.0008948402,0.00038901452,0.0005454162,0.00033118675,0.00011313055],"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":[0.000047026842,0.000024003803,0.00058998575,0.000047228732,0.000017845683,0.00014615084,0.000101159574,0.8634307,0.056780398,0.066759095,0.00024539256,0.011811036],"study_design_scores_gemma":[0.0000025543684,0.000012412206,0.000096435295,0.0000018217177,9.823074e-7,0.000012564471,0.000005847559,0.99509025,0.0015191389,0.003102003,0.00015220644,0.0000038836115],"about_ca_topic_score_codex":0.0012954379,"about_ca_topic_score_gemma":0.0011733974,"teacher_disagreement_score":0.0012954379,"about_ca_system_score_codex":0.000536063,"about_ca_system_score_gemma":0.0004857215,"threshold_uncertainty_score":0.003889501},"labels":[],"label_agreement":null},{"id":"W2007110656","doi":"10.2140/jomms.2009.4.693","title":"Nonlinear dynamic response of an accelerating composite rotor blade using perturbations","year":2009,"lang":"en","type":"article","venue":"Journal of mechanics of materials and structures","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":26,"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":"Nonlinear system; Blade (archaeology); Composite number; Rotor (electric); Helicopter rotor; Materials science; Structural engineering; Control theory (sociology); Engineering; Computer science; Mechanical engineering; Composite material; Physics; Artificial intelligence","score_opus":0.012928482645711437,"score_gpt":0.248775504378101,"score_spread":0.23584702173238956,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2007110656","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":[0.96178997,0.000047595295,0.035714664,0.00004330469,0.000013084812,0.0000104681885,0.000017467253,0.0000917741,0.0022716853],"genre_scores_gemma":[0.9939399,0.00004047164,0.004915188,0.000008747206,0.0000021258593,0.000007385737,0.000013728832,0.00000809324,0.0010643112],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99994266,0.000008729571,0.0000023113594,0.0000084996145,0.000029109198,0.000008800555],"domain_scores_gemma":[0.9998846,0.00004675953,0.000020522117,0.0000129620485,0.000024553045,0.000010592308],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012225629,0.00020347431,0.00016453919,0.000117013034,0.00012586197,0.00016817485,0.00013235498,0.00019929805,0.0008677974],"category_scores_gemma":[0.00034524628,0.00011821169,0.0001428738,0.000070156326,0.00026943858,0.0001285904,0.00019957912,0.00015479613,0.0001421983],"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":[0.00014368819,0.000023777375,0.00082551164,0.000033030447,0.00000866992,0.0002616366,0.00010665096,0.12204828,0.8662125,0.0016093274,0.00011859618,0.008608245],"study_design_scores_gemma":[0.000016098986,0.0002536002,0.0037534283,0.0000069084876,0.00000719744,0.00015862769,0.000059328228,0.8436643,0.15090905,0.0004706422,0.00068431784,0.000016491233],"about_ca_topic_score_codex":0.0007044637,"about_ca_topic_score_gemma":0.00049591187,"teacher_disagreement_score":0.0008677974,"about_ca_system_score_codex":0.0001449287,"about_ca_system_score_gemma":0.00018034206,"threshold_uncertainty_score":0.0029030442},"labels":[],"label_agreement":null},{"id":"W2007394817","doi":"10.1115/pvp2006-icpvt-11-93930","title":"Aerodynamic Forces Approximations Calculated With a New Analytical Formulation","year":2006,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"École de Technologie Supérieure","funders":"","keywords":"Aeroelasticity; Aerodynamics; Aerodynamic force; Laplace transform; Convergence (economics); Applied mathematics; Frequency domain; State variable; Mathematics; Computer science; Mathematical analysis; Physics; Mechanics","score_opus":0.005574691074138215,"score_gpt":0.19013822411655137,"score_spread":0.18456353304241316,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2007394817","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":[0.026022224,0.00017031094,0.96697813,0.00010033685,0.00007546649,0.00002247934,0.000044030043,0.00033367117,0.0062532243],"genre_scores_gemma":[0.6216584,0.00057179114,0.36445215,0.000114254995,0.0001386235,0.0001365014,0.0002123278,0.00025322844,0.012462753],"study_design_codex":"simulation_or_modeling","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.99978656,0.000026587322,0.0000119247225,0.000021070005,0.000135356,0.000018441493],"domain_scores_gemma":[0.99965096,0.00009275718,0.00003466952,0.00003946175,0.00017179598,0.000010307896],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023632072,0.00038605367,0.0003449372,0.0007505553,0.00025071256,0.0005689478,0.00074953854,0.00046994982,0.0018779052],"category_scores_gemma":[0.0013447405,0.00018722816,0.00039244242,0.0004228873,0.00035442688,0.00066722033,0.0004089674,0.000553521,0.00048860174],"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":[0.00006128393,0.0000683804,0.0014735635,0.00015954665,0.00002990702,0.0001684035,0.00020881822,0.75512284,0.030267034,0.06252124,0.0021837482,0.14773522],"study_design_scores_gemma":[0.000004730688,0.000012486701,0.00016200647,0.0000054566854,0.0000027702577,0.000028038256,0.000009802214,0.99460876,0.0015835747,0.0017720512,0.0018058293,0.0000045015618],"about_ca_topic_score_codex":0.0043698754,"about_ca_topic_score_gemma":0.0031955892,"teacher_disagreement_score":0.0043698754,"about_ca_system_score_codex":0.00040328063,"about_ca_system_score_gemma":0.0007447074,"threshold_uncertainty_score":0.008688927},"labels":[],"label_agreement":null},{"id":"W2008615965","doi":"10.1016/s0957-4158(03)00066-7","title":"A PZT actuator control of a single-link flexible manipulator based on linear velocity feedback and actuator placement","year":2003,"lang":"en","type":"article","venue":"Mechatronics","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":118,"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; University of New Brunswick","funders":"","keywords":"Actuator; Control theory (sociology); Vibration; Engineering; Link (geometry); Linear actuator; Mechanism (biology); Lyapunov stability; Control engineering; Computer science; Control (management); Acoustics; Artificial intelligence; Physics","score_opus":0.01505021091995712,"score_gpt":0.20823143711984068,"score_spread":0.19318122619988357,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2008615965","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":[0.3048104,0.00080245116,0.678282,0.00036525208,0.00034928496,0.00015443904,0.00007053843,0.0006855407,0.014480133],"genre_scores_gemma":[0.97775626,0.000116750525,0.01963081,0.000018781491,0.000027118675,0.00003905115,0.000013863708,0.0000074291843,0.0023899246],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998969,0.000013683366,0.000004761827,0.000033511766,0.00004020461,0.000010969862],"domain_scores_gemma":[0.99991167,0.000025794252,0.000019304985,0.000009744091,0.000022268949,0.0000111842555],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018801888,0.0003168934,0.0002978985,0.00013754469,0.00041981196,0.0003471604,0.0004021065,0.00039292403,0.0015776842],"category_scores_gemma":[0.00027805852,0.00017627575,0.0002201737,0.00013311756,0.00028496777,0.00023962151,0.00023951623,0.00026834744,0.00015541137],"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":[0.00076706085,0.00009613366,0.00085179287,0.00061559083,0.000071021335,0.0007667949,0.00035436818,0.11873842,0.6821568,0.0072130137,0.0013251555,0.18704388],"study_design_scores_gemma":[0.00022386434,0.0018989474,0.0058811447,0.00004055382,0.00006961552,0.0006191632,0.00006388255,0.88568074,0.098396644,0.001751444,0.005324752,0.0000492278],"about_ca_topic_score_codex":0.0010070466,"about_ca_topic_score_gemma":0.0015451103,"teacher_disagreement_score":0.0015776842,"about_ca_system_score_codex":0.00010609803,"about_ca_system_score_gemma":0.00025457572,"threshold_uncertainty_score":0.005277872},"labels":[],"label_agreement":null},{"id":"W2010024672","doi":"10.1177/1045389x11416031","title":"Aero-Structural Optimization and Performance Evaluation of a Morphing Wing with Variable Span and Camber","year":2011,"lang":"en","type":"article","venue":"Journal of Intelligent Material Systems and Structures","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":48,"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; European Science Foundation","keywords":"Camber (aerodynamics); Airfoil; Wing; Morphing; Aerodynamics; Structural engineering; Chord (peer-to-peer); Lift-to-drag ratio; Stall (fluid mechanics); Drag; Angle of attack; Wing twist; Wing loading; Engineering; Aerospace engineering; Computer science","score_opus":0.01844842443316193,"score_gpt":0.2068710929968936,"score_spread":0.18842266856373166,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2010024672","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":[0.98064846,0.00012313652,0.016367529,0.000028459428,0.000009836187,0.000024506739,0.000039343584,0.000070976195,0.0026877157],"genre_scores_gemma":[0.99449193,0.000033820645,0.0051346333,0.0000027855428,0.00000147245,0.000007682868,0.000022813441,0.000007797853,0.0002972656],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999256,0.0000134831025,0.0000037696252,0.00001150145,0.000031237956,0.000014319575],"domain_scores_gemma":[0.99985933,0.000042982538,0.00003130316,0.000024912255,0.000026292968,0.000015032821],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002099065,0.00051513256,0.00026498563,0.00030873076,0.00015269508,0.000236012,0.00021062825,0.0002825422,0.0006396488],"category_scores_gemma":[0.0002747699,0.00013381944,0.00038000898,0.00017278132,0.00022525477,0.0001612397,0.00018917225,0.00016854794,0.00008675498],"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":[0.0004637573,0.00012336181,0.0053666476,0.00019964355,0.00005800901,0.0002969475,0.00006843363,0.66870314,0.2849326,0.00085705187,0.00023117705,0.038699277],"study_design_scores_gemma":[0.000045422705,0.0021568956,0.010563806,0.000010172137,0.000061867264,0.00012737123,0.000046145225,0.9260633,0.05983644,0.00015516939,0.0009138764,0.000019675359],"about_ca_topic_score_codex":0.0011817687,"about_ca_topic_score_gemma":0.0009540298,"teacher_disagreement_score":0.0011817687,"about_ca_system_score_codex":0.00021139742,"about_ca_system_score_gemma":0.00019066314,"threshold_uncertainty_score":0.002349794},"labels":[],"label_agreement":null},{"id":"W2010570997","doi":"10.1177/1045389x04039936","title":"The Use of PVDF Strain Sensing in Active Control of Structural Intensity in Beams","year":2004,"lang":"en","type":"article","venue":"Journal of Intelligent Material Systems and Structures","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":20,"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":"Feed forward; Intensity (physics); Shaker; Control theory (sociology); Vibration control; Accelerometer; Vibration; Controller (irrigation); Beam (structure); Measure (data warehouse); Control system; Computer science; Acoustics; Structural engineering; Engineering; Control (management); Physics; Optics; Control engineering","score_opus":0.015892641069677898,"score_gpt":0.21898086145341292,"score_spread":0.20308822038373503,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2010570997","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":[0.49487823,0.0006998596,0.5017971,0.00014032677,0.00004079195,0.000031716194,0.000023171797,0.00016363828,0.0022251876],"genre_scores_gemma":[0.95885444,0.00019536371,0.040413715,0.000021129767,0.000014577862,0.0000148222225,0.000008296447,0.000007312071,0.0004702492],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998771,0.000020434663,0.0000053012154,0.000026848978,0.00005858509,0.000011714604],"domain_scores_gemma":[0.9997085,0.00017045032,0.000042943724,0.000027639377,0.000041552285,0.00000896298],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00022417406,0.00021347661,0.00015127196,0.00014023947,0.0001075305,0.00022449793,0.00040673028,0.0002879806,0.0003153921],"category_scores_gemma":[0.00054151844,0.000110315195,0.00012292834,0.00011834556,0.0003216039,0.00035200443,0.0002017713,0.00017766363,0.00004748181],"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":[0.00018908133,0.00006934467,0.0008573224,0.000104833016,0.000011663964,0.000057536134,0.00007952968,0.018664356,0.8669582,0.0017283887,0.00008313682,0.1111966],"study_design_scores_gemma":[0.000033608,0.0006676729,0.004686088,0.000016737777,0.000026682614,0.00020825546,0.000031397733,0.23583843,0.75522894,0.0014623984,0.0017685101,0.00003135402],"about_ca_topic_score_codex":0.0002754503,"about_ca_topic_score_gemma":0.0003676782,"teacher_disagreement_score":0.00040673028,"about_ca_system_score_codex":0.0001474932,"about_ca_system_score_gemma":0.00007167384,"threshold_uncertainty_score":0.0011855364},"labels":[],"label_agreement":null},{"id":"W2012089464","doi":"10.2514/1.21367","title":"Transient and Limit Cycle Simulation of a Nonlinear Aeroelastic System","year":2007,"lang":"en","type":"article","venue":"Journal of Aircraft","topic":"Aeroelasticity and Vibration Control","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":"McGill University","funders":"","keywords":"Aeroelasticity; Transient (computer programming); Nonlinear system; Transient response; Mechanics; Limit cycle; Wing; Steady state (chemistry); Wind tunnel; Aerodynamics; Limit (mathematics); Flutter; Aerodynamic force; Physics; Degrees of freedom (physics and chemistry); Control theory (sociology); Structural engineering; Mathematics; Engineering; Computer science; Mathematical analysis","score_opus":0.006998151187611366,"score_gpt":0.21560791511527236,"score_spread":0.20860976392766098,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2012089464","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":[0.95700216,0.000039522853,0.035670538,0.00006986875,0.000010278648,0.00003533604,0.00014063972,0.00023695131,0.006794705],"genre_scores_gemma":[0.9975943,0.000013179191,0.0015447777,0.0000057127995,8.436696e-7,0.00003065382,0.00005001935,0.000008475821,0.00075203495],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998964,0.000020294565,0.0000056220697,0.000014711187,0.0000396887,0.000023288081],"domain_scores_gemma":[0.99968696,0.00018121886,0.000028412707,0.00003191268,0.000046904,0.000024662751],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00026307625,0.00018454492,0.00030320315,0.0002404046,0.00026019115,0.00033012376,0.0004698963,0.00054734724,0.0022391363],"category_scores_gemma":[0.0012287772,0.0001500533,0.00024387633,0.00017806863,0.0006467957,0.00036880965,0.00035878413,0.00031476337,0.00014242738],"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":[0.00012075031,0.00007721389,0.0016488099,0.00004407994,0.000011838773,0.00012426105,0.00013208197,0.98299825,0.009673235,0.0026507294,0.000142663,0.0023761087],"study_design_scores_gemma":[0.0000065349614,0.000026381369,0.00030343886,0.0000014797472,0.0000013071569,0.0000069436182,0.000012049498,0.9984591,0.0009136498,0.0001996022,0.00006729912,0.0000022627253],"about_ca_topic_score_codex":0.0050252443,"about_ca_topic_score_gemma":0.0018018846,"teacher_disagreement_score":0.0050252443,"about_ca_system_score_codex":0.00050477765,"about_ca_system_score_gemma":0.00036816296,"threshold_uncertainty_score":0.009992003},"labels":[],"label_agreement":null},{"id":"W2015632741","doi":"10.2514/1.c031896","title":"Performance Enhancement of Tilt-Rotor Unmanned Aerial Vehicle Using Nacelle-Fixed Auxiliary Wing","year":2012,"lang":"en","type":"article","venue":"Journal of Aircraft","topic":"Aeroelasticity and Vibration Control","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 Knowledge Economy","keywords":"Aerospace; Nacelle; Aerospace engineering; Engineering; Aeronautics; Helicopter rotor; Mechanical engineering; Rotor (electric)","score_opus":0.01673112724178273,"score_gpt":0.22915209757980215,"score_spread":0.21242097033801943,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2015632741","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":[0.95189834,0.00074160314,0.029762497,0.00012637064,0.000092873604,0.000024638552,0.00006006083,0.00035837517,0.016935388],"genre_scores_gemma":[0.99640214,0.00009917159,0.002087866,0.000010822913,0.0000047810327,0.000003879468,0.000044495773,0.000009514777,0.0013373242],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99993336,0.0000069601406,0.0000024229937,0.000009422011,0.000029775534,0.000018050614],"domain_scores_gemma":[0.99993145,0.000008304545,0.000008984546,0.000006640298,0.0000345101,0.0000100516145],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00008291903,0.0002680856,0.00017988747,0.00016429994,0.00012949666,0.00015657036,0.00012637356,0.00013639443,0.0017465184],"category_scores_gemma":[0.00010450401,0.00003989594,0.0001665554,0.00007510153,0.00008370387,0.00019473162,0.000219142,0.00011342978,0.00032242175],"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":[0.00083844835,0.00014843496,0.004915263,0.00017697782,0.000032396587,0.0002741878,0.000097712946,0.037982874,0.8322804,0.0007955678,0.0021738675,0.12028384],"study_design_scores_gemma":[0.00009247752,0.005526395,0.02675595,0.000031297026,0.00008947617,0.00027383154,0.00027911313,0.50609523,0.4512127,0.0003743205,0.009220651,0.00004856188],"about_ca_topic_score_codex":0.00068621885,"about_ca_topic_score_gemma":0.0009403116,"teacher_disagreement_score":0.0017465184,"about_ca_system_score_codex":0.00009719295,"about_ca_system_score_gemma":0.000080713326,"threshold_uncertainty_score":0.005842626},"labels":[],"label_agreement":null},{"id":"W2015647743","doi":"10.1088/0964-1726/16/6/022","title":"Active vibration suppression of smart laminated beams using layerwise theory and an optimal control strategy","year":2007,"lang":"en","type":"article","venue":"Smart Materials and Structures","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":45,"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":"Actuator; Vibration control; Linear-quadratic regulator; Active vibration control; Vibration; Beam (structure); Control theory (sociology); Smart material; Structural engineering; Finite element method; Displacement (psychology); Controller (irrigation); Natural frequency; Engineering; Coupling (piping); Materials science; Computer science; Acoustics; Physics; Mechanical engineering; Control (management)","score_opus":0.00830981992604149,"score_gpt":0.24203920638623813,"score_spread":0.23372938646019664,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2015647743","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":[0.064325035,0.00017644829,0.93349665,0.000048964434,0.000018813558,0.000017769362,0.0000050340277,0.00013582034,0.0017755217],"genre_scores_gemma":[0.94351596,0.00013811725,0.05503626,0.000029841074,0.000017213928,0.00005232839,0.000011206615,0.0000109537605,0.0011881161],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99989784,0.000025906733,0.0000052701125,0.000016644342,0.000043446147,0.000010918844],"domain_scores_gemma":[0.99985325,0.00006133133,0.0000416384,0.000011150396,0.00002595048,0.0000066030148],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021398565,0.00036045891,0.0002522656,0.00012870374,0.000109626024,0.0002346534,0.0002596061,0.00021049312,0.0005949876],"category_scores_gemma":[0.0002461364,0.00014061494,0.00021857608,0.0000800709,0.00031798956,0.00023797809,0.00025229712,0.00019017473,0.000088023546],"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":[0.00021897684,0.00011071536,0.00057595846,0.00018783101,0.000069134854,0.00011254061,0.0001785988,0.5260788,0.35131145,0.013622803,0.0004266986,0.10710649],"study_design_scores_gemma":[0.000017186336,0.00014277115,0.0001576001,0.0000042185184,0.0000083298055,0.000012306779,0.000007415496,0.98580486,0.012559837,0.00093959534,0.00034009418,0.0000057123652],"about_ca_topic_score_codex":0.0005801918,"about_ca_topic_score_gemma":0.0006631491,"teacher_disagreement_score":0.0005949876,"about_ca_system_score_codex":0.00015471851,"about_ca_system_score_gemma":0.00018707362,"threshold_uncertainty_score":0.001990378},"labels":[],"label_agreement":null},{"id":"W2015771992","doi":"10.1177/1045389x09351609","title":"Finite Element Analysis of Broken Fiber Effects on Hollow Active Fiber Composites","year":2009,"lang":"en","type":"article","venue":"Journal of Intelligent Material Systems and Structures","topic":"Aeroelasticity and Vibration Control","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":"Carleton University; National Research Council Canada","funders":"","keywords":"Materials science; Composite material; Finite element method; Fiber; Composite number; Epoxy; Fiber-reinforced composite; Electrode; Structural engineering; Engineering","score_opus":0.0062630160641807715,"score_gpt":0.21974899786730398,"score_spread":0.2134859818031232,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2015771992","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":[0.67787796,0.0003122821,0.31392896,0.00017514198,0.00007512696,0.00007475789,0.00019657948,0.00048839656,0.0068707634],"genre_scores_gemma":[0.957604,0.00011227813,0.039107457,0.000021552281,0.0000065152394,0.000058772865,0.000108058615,0.00005854061,0.00292287],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99970704,0.000052325246,0.000013590443,0.0000296621,0.00015635934,0.000040979707],"domain_scores_gemma":[0.99919564,0.0004631107,0.00008078923,0.000062127656,0.00016842468,0.000029890423],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00063937844,0.0003694804,0.00046359107,0.0004740703,0.00030031128,0.00049521984,0.00063646655,0.0011014626,0.001771334],"category_scores_gemma":[0.0013959662,0.00039334883,0.00053527136,0.00020876701,0.0006709491,0.0004459711,0.0003518907,0.00040973324,0.00027395872],"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":[0.00009969924,0.000048218528,0.0010612761,0.00008004735,0.000017149563,0.00015181498,0.000134055,0.9346783,0.055328086,0.002155541,0.0001345753,0.006111254],"study_design_scores_gemma":[0.0000047515337,0.0000316828,0.00030775557,0.000005473281,0.0000035606354,0.00001871365,0.000017519927,0.9931977,0.0059220796,0.00018362715,0.00030136845,0.000005732515],"about_ca_topic_score_codex":0.003687935,"about_ca_topic_score_gemma":0.002231373,"teacher_disagreement_score":0.003687935,"about_ca_system_score_codex":0.00050961145,"about_ca_system_score_gemma":0.0006122403,"threshold_uncertainty_score":0.0073329806},"labels":[],"label_agreement":null},{"id":"W2017657597","doi":"10.1007/s00707-008-0098-3","title":"The dynamic behavior of a surface-bonded piezoelectric actuator with a bonding layer","year":2008,"lang":"en","type":"article","venue":"Acta Mechanica","topic":"Aeroelasticity and Vibration Control","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 Alberta","funders":"","keywords":"Actuator; Materials science; Piezoelectricity; Solid mechanics; Layer (electronics); Smart material; Composite material; Piezoelectric sensor; Deformation (meteorology); Mechanics; Engineering; Electrical engineering; Physics","score_opus":0.010914697347277208,"score_gpt":0.20625629735639597,"score_spread":0.19534160000911877,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2017657597","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":[0.9941246,0.00016996592,0.0033892011,0.000110128145,0.00003515948,0.000008343784,0.00006861582,0.00007807542,0.0020158463],"genre_scores_gemma":[0.9965481,0.000097162185,0.0017658457,0.000023219814,0.000008320733,0.000008875504,0.00007060251,0.000013574063,0.0014642719],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998981,0.000007568409,0.000002910389,0.000023008028,0.00004404431,0.000024377267],"domain_scores_gemma":[0.9998386,0.000060404305,0.000021430946,0.000014790011,0.00003269556,0.000032079348],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00009886223,0.00019854696,0.000260737,0.00016893474,0.00033385406,0.00022713409,0.0004912983,0.0006263464,0.0035297256],"category_scores_gemma":[0.00034898298,0.00023022667,0.0001922132,0.00013856067,0.000432052,0.00041852868,0.00022394078,0.0003465862,0.000348176],"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":[0.00030071786,0.000054522203,0.00046125328,0.00004777508,0.00001811056,0.00022678493,0.000070574744,0.0042109163,0.9903818,0.00046717134,0.00019596974,0.0035644711],"study_design_scores_gemma":[0.00009003193,0.0014042043,0.019359233,0.00002153989,0.000053338288,0.0003838661,0.0002495662,0.20520915,0.7698975,0.00049700466,0.0027726234,0.000061906256],"about_ca_topic_score_codex":0.0011933895,"about_ca_topic_score_gemma":0.0010501401,"teacher_disagreement_score":0.0035297256,"about_ca_system_score_codex":0.00021591359,"about_ca_system_score_gemma":0.00029258235,"threshold_uncertainty_score":0.011808097},"labels":[],"label_agreement":null},{"id":"W2017959571","doi":"10.1007/s10832-007-9131-5","title":"Spatial control of a smart beam","year":2007,"lang":"en","type":"article","venue":"Journal of Electroceramics","topic":"Aeroelasticity and Vibration Control","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":"Carleton University","funders":"","keywords":"Beam (structure); Controller (irrigation); Modal; Modal analysis; Truncation (statistics); Vibration; Range (aeronautics); Computer science; Control theory (sociology); Vibration control; Physics; Acoustics; Structural engineering; Optics; Control (management); Materials science; Engineering; Aerospace engineering; Artificial intelligence","score_opus":0.004049816315036747,"score_gpt":0.19865408738991208,"score_spread":0.19460427107487532,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2017959571","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":[0.395318,0.0001879535,0.5895817,0.00026744895,0.00024939637,0.00003825513,0.000055849272,0.00052228535,0.0137790665],"genre_scores_gemma":[0.988494,0.00004040411,0.00877844,0.000038071685,0.0000142099425,0.000013365847,0.000010100969,0.000009610309,0.0026017264],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999404,0.00000873215,0.0000026745065,0.0000133221765,0.000024285526,0.000010658361],"domain_scores_gemma":[0.99987125,0.00003959984,0.000021609916,0.00001937991,0.00003220218,0.000016040696],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001263662,0.00019205823,0.00024408755,0.00013671632,0.0002519536,0.00029260578,0.00033690495,0.00025315708,0.0029844204],"category_scores_gemma":[0.0002113698,0.00013445347,0.00013009817,0.000101835394,0.00030767825,0.00018152918,0.00046987613,0.00013186305,0.00021290785],"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":[0.00067339034,0.000111697416,0.0010737212,0.00009122565,0.00005753113,0.00030553198,0.00018022605,0.24520598,0.62903374,0.022880103,0.00180543,0.098581396],"study_design_scores_gemma":[0.00003541138,0.00031811214,0.0009979552,0.00000433704,0.000013445631,0.000047920694,0.000023971534,0.9780392,0.016602205,0.002021754,0.0018837602,0.000011922557],"about_ca_topic_score_codex":0.00082396256,"about_ca_topic_score_gemma":0.0011100591,"teacher_disagreement_score":0.0029844204,"about_ca_system_score_codex":0.0001175948,"about_ca_system_score_gemma":0.00015287996,"threshold_uncertainty_score":0.009983957},"labels":[],"label_agreement":null},{"id":"W2019031048","doi":"10.1088/0964-1726/12/2/317","title":"Optimally distributed actuator placement and control for a slewing single-link flexible manipulator","year":2003,"lang":"en","type":"article","venue":"Smart Materials and Structures","topic":"Aeroelasticity and Vibration Control","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":"Western University","funders":"","keywords":"Actuator; Control theory (sociology); Simulated annealing; Controller (irrigation); Linear-quadratic regulator; Position (finance); Optimal design; Distributed parameter system; Engineering; Computer science; Control engineering; Optimal control; Mathematics; Control (management); Mathematical optimization; Algorithm","score_opus":0.013690198578410903,"score_gpt":0.20975772595959563,"score_spread":0.19606752738118471,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2019031048","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":[0.09397174,0.00010560744,0.9044532,0.00006247804,0.000014088713,0.000028287779,0.00001249084,0.0001178589,0.0012343212],"genre_scores_gemma":[0.88520414,0.00007070867,0.11336726,0.000014830308,0.000009199184,0.000077621786,0.00001579166,0.000015115167,0.0012252999],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99987876,0.000026267766,0.0000054603724,0.000038200717,0.00003793736,0.000013316555],"domain_scores_gemma":[0.9998067,0.000082063365,0.000055981192,0.000017102584,0.000027474498,0.0000106430625],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00026890347,0.00047757747,0.00036543913,0.00016622095,0.00022231205,0.00027843818,0.00046068055,0.0005355194,0.00094659347],"category_scores_gemma":[0.00050113007,0.0003380266,0.00027286494,0.00015465007,0.00039075842,0.0002585001,0.000268884,0.00037180664,0.00016211413],"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":[0.000070015274,0.00003494351,0.00024201213,0.000059801052,0.000018803283,0.000088051376,0.00005972548,0.9133457,0.05247822,0.0028124263,0.0001383724,0.03065201],"study_design_scores_gemma":[0.0000327213,0.00013443177,0.00018123876,0.000003671816,0.000006148923,0.000018357663,0.000010203098,0.99407035,0.0044051143,0.00087986875,0.00025240355,0.0000054892034],"about_ca_topic_score_codex":0.000988986,"about_ca_topic_score_gemma":0.0014299258,"teacher_disagreement_score":0.000988986,"about_ca_system_score_codex":0.00025965637,"about_ca_system_score_gemma":0.0003856647,"threshold_uncertainty_score":0.003166616},"labels":[],"label_agreement":null},{"id":"W2021851125","doi":"10.1007/s00707-002-0969-y","title":"On the elastic wave propagation induced by a network of piezoelectric actuators","year":2003,"lang":"en","type":"article","venue":"Acta Mechanica","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":4,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Alberta","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Actuator; Solid mechanics; Waveform; Piezoelectricity; Wave propagation; Acoustics; Transverse plane; Control theory (sociology); Materials science; Mechanics; Computer science; Structural engineering; Physics; Engineering; Control (management); Optics; Telecommunications","score_opus":0.011353371464635494,"score_gpt":0.18428377193519163,"score_spread":0.17293040047055613,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2021851125","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":[0.42222896,0.0019967535,0.52017325,0.0008490711,0.0004959479,0.000054594788,0.00011392429,0.00014145802,0.053946022],"genre_scores_gemma":[0.9544794,0.0030321775,0.019732704,0.000092851944,0.00026871523,0.000028888118,0.00008138378,0.000059525402,0.022224337],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999099,0.000025221903,0.000002943161,0.000012632999,0.000037829646,0.00001151233],"domain_scores_gemma":[0.999559,0.000266398,0.0000723435,0.000019956353,0.00005624245,0.000026129763],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025193175,0.0004592341,0.00021062222,0.00046118212,0.00021507079,0.0003759402,0.00040413867,0.0004029484,0.0026677449],"category_scores_gemma":[0.0011061339,0.00020224608,0.00016360504,0.0004088881,0.00069961813,0.0008055519,0.00038755516,0.00053800043,0.000267085],"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":[0.0009248521,0.00018177452,0.0014961492,0.0003936186,0.00006998504,0.0012923937,0.00043574072,0.500848,0.118018135,0.3061793,0.002683332,0.06747678],"study_design_scores_gemma":[0.00003322813,0.00009958154,0.0012803674,0.000017388384,0.000024478326,0.00021201113,0.000056007193,0.94115734,0.0073533063,0.047838554,0.0019027324,0.00002502452],"about_ca_topic_score_codex":0.0005399918,"about_ca_topic_score_gemma":0.00038090788,"teacher_disagreement_score":0.0026677449,"about_ca_system_score_codex":0.0001632991,"about_ca_system_score_gemma":0.000087696964,"threshold_uncertainty_score":0.008924544},"labels":[],"label_agreement":null},{"id":"W2022899676","doi":"10.1006/jsvi.1999.2895","title":"APPLICATION OF THE CENTRE MANIFOLD THEORY IN NON-LINEAR AEROELASTICITY","year":2000,"lang":"en","type":"article","venue":"Journal of Sound and Vibration","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":122,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"National Research Council Canada; University of Alberta","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Aeroelasticity; Mathematics; Limit cycle; Bifurcation theory; Hopf bifurcation; Ordinary differential equation; Mathematical analysis; Limit (mathematics); Center manifold; Bifurcation; Differential equation; Runge–Kutta methods; Applied mathematics; Nonlinear system; Physics; Aerodynamics; Mechanics","score_opus":0.0047451301685759745,"score_gpt":0.19631515265800648,"score_spread":0.1915700224894305,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2022899676","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":[0.02873686,0.0032875626,0.9298192,0.0012908047,0.00090422685,0.000033584052,0.000064156564,0.00016658031,0.035696883],"genre_scores_gemma":[0.8335637,0.0048764218,0.13628635,0.00031725928,0.0019481416,0.00013443266,0.00010606675,0.00026503328,0.022502642],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.99972266,0.000117827774,0.000012899023,0.00004417918,0.000081238504,0.000021221309],"domain_scores_gemma":[0.99933285,0.0003003835,0.00005583936,0.000069243804,0.00017688028,0.00006468046],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00067359034,0.0007988487,0.0009156535,0.0014595635,0.0007155914,0.0010981687,0.0008725043,0.00092011376,0.003011699],"category_scores_gemma":[0.0025894407,0.00027143967,0.0009071032,0.0008234873,0.0019234199,0.0016539405,0.001779367,0.0018209767,0.00045544005],"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":[0.000024026116,0.000025716765,0.00018397646,0.000093870236,0.000025497271,0.000088509994,0.0001450806,0.025053136,0.002303601,0.9521338,0.0012147155,0.018707963],"study_design_scores_gemma":[0.000008189577,0.000035436362,0.00034573564,0.000019686135,0.000009736871,0.000066098866,0.000047258327,0.22753438,0.0006592319,0.7654424,0.0058120564,0.000019836316],"about_ca_topic_score_codex":0.0010495996,"about_ca_topic_score_gemma":0.00079244433,"teacher_disagreement_score":0.003011699,"about_ca_system_score_codex":0.0006555123,"about_ca_system_score_gemma":0.0005448766,"threshold_uncertainty_score":0.010075152},"labels":[],"label_agreement":null},{"id":"W2023808677","doi":"10.1088/0964-1726/13/5/020","title":"Material characterization of active fiber composites for integral twist-actuated rotor blade application","year":2004,"lang":"en","type":"article","venue":"Smart Materials and Structures","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":38,"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":"Actuator; Helicopter rotor; Characterization (materials science); Structural engineering; Turbine blade; Materials science; Rotor (electric); Mechanical engineering; Composite material; Engineering; Turbine","score_opus":0.004739769452657601,"score_gpt":0.19835252916999307,"score_spread":0.19361275971733546,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2023808677","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":[0.9844639,0.00049478654,0.013638563,0.000027796688,0.000015942562,0.000048319733,0.0001177759,0.000069581474,0.0011232137],"genre_scores_gemma":[0.985254,0.00021412158,0.013616928,0.000013750942,0.0000054737393,0.00003814908,0.00018351524,0.000018297915,0.0006557587],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99970144,0.00003705384,0.000015239706,0.000047212634,0.0001771603,0.000021792075],"domain_scores_gemma":[0.99938095,0.0001557618,0.00009827296,0.000046508372,0.0002711339,0.000047275884],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004143414,0.00031191087,0.0001987758,0.0007344189,0.0004215321,0.00022571313,0.00016601171,0.0003094949,0.00065793295],"category_scores_gemma":[0.0007052416,0.00013882875,0.00015265781,0.0001901428,0.0001933595,0.00022055673,0.00010168664,0.00018217874,0.00015637073],"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":[0.000015633157,0.000009595698,0.00023526825,0.0000145753165,0.0000011897655,0.000014773618,0.000010900752,0.00020126766,0.9980925,0.000014622153,0.000008461603,0.0013813308],"study_design_scores_gemma":[0.000004571097,0.000299515,0.0058763986,0.0000047128187,0.0000085534975,0.00011731917,0.00003190561,0.0029594735,0.9899402,0.000023102197,0.000727793,0.000006431077],"about_ca_topic_score_codex":0.0005377613,"about_ca_topic_score_gemma":0.0015422837,"teacher_disagreement_score":0.0007344189,"about_ca_system_score_codex":0.00018035392,"about_ca_system_score_gemma":0.00026256056,"threshold_uncertainty_score":0.0022010207},"labels":[],"label_agreement":null},{"id":"W2024703571","doi":"10.1115/dscc2014-6337","title":"Robust Stall Flutter Suppression Using ℋ2/ℋ∞ Control","year":2014,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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 Toronto","funders":"","keywords":"Control theory (sociology); Flutter; Aeroelasticity; Aerodynamics; Nonlinear system; Stall (fluid mechanics); Robustness (evolution); Inflow; Robust control; Computer science; Control system; Frequency domain; Controller (irrigation); Engineering; Control engineering; Control (management)","score_opus":0.016609687402640773,"score_gpt":0.1916699415992756,"score_spread":0.17506025419663485,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2024703571","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":[0.080592364,0.0005794242,0.909556,0.00008622225,0.00011549646,0.000056882134,0.000043937627,0.0009941139,0.007975704],"genre_scores_gemma":[0.9841882,0.000098357246,0.014076093,0.000027309903,0.000022613667,0.00004584745,0.000039393824,0.00001443199,0.0014876308],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997614,0.000034054305,0.00001796858,0.000061269755,0.00008988781,0.00003543256],"domain_scores_gemma":[0.9998223,0.00003803698,0.000057863937,0.000011650348,0.00006190017,0.000008335494],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003735767,0.00073771813,0.00041380932,0.000245464,0.0002574933,0.0004762636,0.00056923553,0.0003147736,0.0007398165],"category_scores_gemma":[0.00043664392,0.00017689385,0.00036872653,0.000116547555,0.0002811985,0.00029934593,0.00046557173,0.00031201646,0.00017852629],"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":[0.000706473,0.000115599425,0.0009877003,0.0005053918,0.00011012641,0.00026152705,0.00021243362,0.70523685,0.14969805,0.008136687,0.0017109027,0.1323183],"study_design_scores_gemma":[0.000020710044,0.00033635137,0.0005201256,0.000010779772,0.0000149138705,0.000031071766,0.000011519382,0.98585826,0.011558133,0.00038643944,0.0012385718,0.000013061613],"about_ca_topic_score_codex":0.0025762832,"about_ca_topic_score_gemma":0.0014399915,"teacher_disagreement_score":0.0025762832,"about_ca_system_score_codex":0.00026032713,"about_ca_system_score_gemma":0.00026767314,"threshold_uncertainty_score":0.005122602},"labels":[],"label_agreement":null},{"id":"W2025768102","doi":"10.1007/s00707-006-0313-z","title":"Wave propagation generated by piezoelectric actuators attached to elastic substrates","year":2006,"lang":"en","type":"article","venue":"Acta Mechanica","topic":"Aeroelasticity and Vibration Control","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 Alberta","funders":"","keywords":"Actuator; Piezoelectricity; Electric field; Waveform; Acoustics; Solid mechanics; Field (mathematics); Wave propagation; Mechanics; Piezoelectric sensor; Control theory (sociology); Physics; Materials science; Computer science; Engineering; Mathematics; Optics; Electrical engineering; Voltage","score_opus":0.007859723861084952,"score_gpt":0.18991578485911143,"score_spread":0.18205606099802646,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2025768102","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":[0.9621131,0.00033013374,0.027505552,0.00010925471,0.00007885751,0.000019818945,0.00006847067,0.00010413829,0.009670721],"genre_scores_gemma":[0.98653877,0.00039861377,0.0047664577,0.000018334082,0.000024468522,0.000015896572,0.000089886365,0.000031048643,0.008116524],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99994016,0.000008481052,0.0000018267893,0.000007839174,0.000025871484,0.000015814152],"domain_scores_gemma":[0.9997645,0.000113148526,0.000041903066,0.000014451304,0.00003414146,0.000031810567],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000123296,0.00040411978,0.00021273029,0.00027884648,0.00021972386,0.00044399523,0.00021527123,0.00034865993,0.0024059378],"category_scores_gemma":[0.00035715752,0.00025479207,0.00014230167,0.00031446642,0.00043033305,0.00030554345,0.00024914983,0.00037969265,0.00044021857],"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":[0.00057105464,0.000042620606,0.00076284213,0.000104628685,0.000012305055,0.0004803526,0.00020244131,0.006488559,0.9730051,0.0049150004,0.00035247955,0.013062637],"study_design_scores_gemma":[0.00015695948,0.00043663644,0.011591246,0.000025020761,0.00004130572,0.0004955531,0.00022650631,0.14040916,0.8411595,0.0029441905,0.0024593968,0.000054624314],"about_ca_topic_score_codex":0.00021830284,"about_ca_topic_score_gemma":0.00019381967,"teacher_disagreement_score":0.0024059378,"about_ca_system_score_codex":0.00012885565,"about_ca_system_score_gemma":0.00014891813,"threshold_uncertainty_score":0.008048654},"labels":[],"label_agreement":null},{"id":"W2030566459","doi":"10.1115/imece2002-33614","title":"Active Control of Sound Radiation Into Enclosures Using Structural Error Sensors","year":2002,"lang":"en","type":"article","venue":"5th International Symposium on Fluid Structure Interaction, Aeroelasticity, and Flow Induced Vibration and Noise","topic":"Aeroelasticity and Vibration Control","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":"Enclosure; Acoustics; Actuator; Computer science; Acoustic radiation; Vibration control; Vibration; Sound transmission class; Genetic algorithm; Optimal control; Benchmark (surveying); Coupling (piping); Engineering; Physics; Mechanical engineering; Optics; Electrical engineering; Radiation; Mathematics","score_opus":0.01674402054809721,"score_gpt":0.2565206889142696,"score_spread":0.2397766683661724,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2030566459","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":[0.24752301,0.00028422466,0.7494407,0.000072256546,0.000042320138,0.000026416948,0.000017579836,0.00037716367,0.002216252],"genre_scores_gemma":[0.9622559,0.00008185732,0.036816586,0.00001401163,0.000008651122,0.000022102624,0.000011984462,0.000013614695,0.0007753544],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997311,0.000049062346,0.000014709064,0.00006285376,0.00012092085,0.000021293316],"domain_scores_gemma":[0.9995888,0.00018613112,0.000101942715,0.000040404248,0.000063967076,0.000018662586],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025544103,0.00040980667,0.0003742533,0.00018408657,0.00015732297,0.0004130343,0.00055936875,0.00037912276,0.0003878997],"category_scores_gemma":[0.00062682026,0.00014429618,0.00024351919,0.00013180573,0.00035328147,0.00041144958,0.00055979413,0.0003286585,0.00008771277],"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":[0.00026494203,0.00014549839,0.0014164837,0.00017844116,0.000042186173,0.00012652551,0.0001554211,0.34742585,0.5412326,0.0032685243,0.00022899649,0.10551452],"study_design_scores_gemma":[0.000023959687,0.00033108843,0.0008743328,0.000008150505,0.00001605797,0.00004142232,0.000019158922,0.89011043,0.10696782,0.00068481476,0.00090974115,0.0000130527715],"about_ca_topic_score_codex":0.0003321461,"about_ca_topic_score_gemma":0.0005229476,"teacher_disagreement_score":0.00055936875,"about_ca_system_score_codex":0.00018383663,"about_ca_system_score_gemma":0.00016854474,"threshold_uncertainty_score":0.0013508797},"labels":[],"label_agreement":null},{"id":"W2030696121","doi":"10.1121/1.429593","title":"Investigation of active structural intensity control in finite beams: Theory and experiment","year":2000,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aeroelasticity and Vibration Control","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":"Université de Sherbrooke","funders":"","keywords":"Intensity (physics); Feed forward; Control theory (sociology); Computer science; Controller (irrigation); Accelerometer; Beam (structure); Energy (signal processing); Acceleration; Process (computing); Control (management); Mathematics; Physics; Optics; Statistics","score_opus":0.007036947891591015,"score_gpt":0.21128853862038885,"score_spread":0.20425159072879784,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2030696121","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":[0.66364324,0.00030299043,0.33002916,0.00022023912,0.00004576276,0.00014655356,0.00005977435,0.000534891,0.0050173756],"genre_scores_gemma":[0.96853495,0.00013270938,0.03041375,0.000033076285,0.000008458735,0.00006995174,0.00002244153,0.000014247683,0.0007704572],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9996119,0.00005517864,0.000011504576,0.000052957406,0.00023263333,0.000035814835],"domain_scores_gemma":[0.9989242,0.0007391372,0.00008058656,0.00009290789,0.00011955691,0.00004351176],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00070151093,0.00024845623,0.00030149092,0.00019479661,0.00019441436,0.00035625196,0.00079645857,0.0006027136,0.0016591572],"category_scores_gemma":[0.0014955179,0.00018285484,0.00016095338,0.00016352441,0.0007743827,0.00062419474,0.00035054804,0.00033024434,0.00016241381],"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":[0.0005718555,0.0005606505,0.0020987603,0.0002764411,0.000028661054,0.00013790368,0.0005298942,0.06710538,0.86359936,0.015277654,0.0003575568,0.049455825],"study_design_scores_gemma":[0.00008363854,0.0014740569,0.003321378,0.00004155218,0.000019292052,0.00008352511,0.00010947092,0.7081429,0.28147036,0.0035200766,0.0016975155,0.00003620504],"about_ca_topic_score_codex":0.00046195075,"about_ca_topic_score_gemma":0.0003524981,"teacher_disagreement_score":0.0016591572,"about_ca_system_score_codex":0.00034239984,"about_ca_system_score_gemma":0.00021861319,"threshold_uncertainty_score":0.005550444},"labels":[],"label_agreement":null},{"id":"W2031067553","doi":"10.1177/1045389x04044450","title":"Dual-Stack Piezoelectric Device with Bidirectional Actuation and Improved Performance","year":2004,"lang":"en","type":"article","venue":"Journal of Intelligent Material Systems and Structures","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":29,"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":"Pennsylvania State University","keywords":"Actuator; Stack (abstract data type); Piezoelectricity; Mechanical engineering; Materials science; Engineering; Acoustics; Structural engineering; Computer science; Electrical engineering","score_opus":0.0071520812119691985,"score_gpt":0.19532549948825637,"score_spread":0.18817341827628717,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2031067553","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":[0.8087442,0.003977683,0.16932072,0.00045719146,0.0003888309,0.00011079234,0.0004981057,0.00074938935,0.015753102],"genre_scores_gemma":[0.87917227,0.0012643301,0.112663426,0.00009783771,0.00006764467,0.00008668503,0.00023289176,0.000042100546,0.006372924],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99982256,0.000008996736,0.00001246454,0.00004005043,0.00009143161,0.000024549205],"domain_scores_gemma":[0.999877,0.000022314098,0.000034216497,0.0000123777245,0.00003731666,0.00001677905],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017729693,0.00041597945,0.00028187546,0.00032278098,0.00015787326,0.00030696217,0.0006031653,0.0004313294,0.0009660089],"category_scores_gemma":[0.00020869676,0.00021126786,0.00023222827,0.00024696972,0.0001382065,0.0006449331,0.00043645856,0.000419355,0.0004230699],"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":[0.000035814526,0.000019653266,0.00021540091,0.00010039434,0.0000063604084,0.000045181372,0.00002591358,0.00026040882,0.98704034,0.00051114877,0.00024926398,0.011490263],"study_design_scores_gemma":[0.00003383119,0.00037740357,0.0021292975,0.000021638314,0.000039960858,0.0005857551,0.000049581777,0.017011171,0.968617,0.00017447078,0.010917104,0.000042800333],"about_ca_topic_score_codex":0.0003200013,"about_ca_topic_score_gemma":0.00079490495,"teacher_disagreement_score":0.0009660089,"about_ca_system_score_codex":0.00020006648,"about_ca_system_score_gemma":0.00023600076,"threshold_uncertainty_score":0.0032316446},"labels":[],"label_agreement":null},{"id":"W2033125898","doi":"10.4271/2013-01-2286","title":"Aerodynamic Cell Design for Air Load Measurements on High Aspect Ratio Airfoils","year":2013,"lang":"en","type":"article","venue":"SAE technical papers on CD-ROM/SAE technical paper series","topic":"Aeroelasticity and Vibration Control","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":"Aerodynamics; Airfoil; Aerospace engineering; Aspect ratio (aeronautics); Acoustics; Materials science; Computer science; Engineering; Physics; Composite material","score_opus":0.01730440410848314,"score_gpt":0.2179881374132506,"score_spread":0.20068373330476746,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2033125898","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":[0.67994237,0.00014458268,0.31522062,0.000064521795,0.00006404588,0.00036502842,0.00039529725,0.001062989,0.0027405163],"genre_scores_gemma":[0.940277,0.000059874652,0.058297962,0.00001788273,0.000008225823,0.00022596329,0.0001867344,0.000041660434,0.0008846892],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9990157,0.00017964675,0.000038158425,0.00012986397,0.00055997993,0.00007666711],"domain_scores_gemma":[0.9985781,0.0004007842,0.00014517421,0.00018578515,0.0006078215,0.000082327424],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00087726803,0.0006063328,0.0005642693,0.00063659216,0.0003640684,0.00066181604,0.00086565345,0.00060922484,0.0016519318],"category_scores_gemma":[0.0014881386,0.00020852132,0.0002434955,0.00033444277,0.00037606547,0.00025179656,0.00035178853,0.00030826457,0.0005281048],"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":[0.00049587415,0.00016279495,0.009171345,0.00025198216,0.000018233482,0.0002006813,0.00029287755,0.0245795,0.90704334,0.00059916085,0.0005518696,0.056632247],"study_design_scores_gemma":[0.00007802888,0.0014511958,0.02464766,0.000025237117,0.00003487844,0.000328048,0.00023853098,0.16700372,0.8014316,0.0001962239,0.0044982173,0.00006668781],"about_ca_topic_score_codex":0.0012577472,"about_ca_topic_score_gemma":0.0015242659,"teacher_disagreement_score":0.0016519318,"about_ca_system_score_codex":0.0004331219,"about_ca_system_score_gemma":0.0005134441,"threshold_uncertainty_score":0.0055263042},"labels":[],"label_agreement":null},{"id":"W2033631567","doi":"10.1177/1045389x13491639","title":"Development of robust control law for active buffeting load alleviation of smart fin structures","year":2013,"lang":"en","type":"article","venue":"Journal of Intelligent Material Systems and Structures","topic":"Aeroelasticity and Vibration Control","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":"National Research Council Canada","funders":"","keywords":"Aeroelasticity; Aerodynamics; Wind tunnel; Engineering; Parametric statistics; Robustness (evolution); Fin; Control theory (sociology); Robust control; Vibration control; Structural engineering; Vibration; Control system; Computer science; Aerospace engineering; Control (management); Mathematics; Acoustics","score_opus":0.013648460732422743,"score_gpt":0.21327749576984734,"score_spread":0.1996290350374246,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2033631567","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":[0.024555707,0.00013850264,0.9725495,0.00005706014,0.00004602505,0.00006709057,0.000014514308,0.00045020878,0.002121415],"genre_scores_gemma":[0.95106316,0.00013015431,0.04679703,0.000047808404,0.000025243378,0.00011802872,0.000038388323,0.000020200423,0.0017599458],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996773,0.000034056604,0.000023334771,0.00008681635,0.00014064148,0.00003785491],"domain_scores_gemma":[0.9995441,0.00012434518,0.00010057553,0.000032962336,0.00018340418,0.000014673236],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005915826,0.0006540025,0.0004052969,0.00028464192,0.00023140448,0.0004693537,0.00067544816,0.00052002334,0.0008748373],"category_scores_gemma":[0.0010203915,0.00020675715,0.0003563858,0.000105911626,0.00042109995,0.00037300895,0.000440917,0.0005700043,0.00017544352],"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":[0.00019466833,0.000100753445,0.0005812047,0.00030279785,0.000057048306,0.00030242745,0.00022849787,0.71274436,0.12650806,0.010250653,0.0011494966,0.14758007],"study_design_scores_gemma":[0.000019784422,0.00024989145,0.00020983713,0.000008412653,0.0000103309385,0.000026168787,0.00000874997,0.9886026,0.009679093,0.00047803455,0.0006991657,0.0000079215415],"about_ca_topic_score_codex":0.0020547602,"about_ca_topic_score_gemma":0.0014428605,"teacher_disagreement_score":0.0020547602,"about_ca_system_score_codex":0.00025709564,"about_ca_system_score_gemma":0.00057356333,"threshold_uncertainty_score":0.0040856004},"labels":[],"label_agreement":null},{"id":"W2036185572","doi":"10.4028/www.scientific.net/amr.585.332","title":"On the Actuation Authority of Adaptive Sandwich Beam with Composite Actuators: Coupled Finite Element Analysis","year":2012,"lang":"en","type":"article","venue":"Advanced materials research","topic":"Aeroelasticity and Vibration Control","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":"Canadian Society of Intestinal Research","funders":"","keywords":"Materials science; Actuator; Volume fraction; Composite number; Finite element method; Composite material; Beam (structure); Timoshenko beam theory; Shear (geology); Structural engineering; Fiber; Engineering; Electrical engineering","score_opus":0.03613015298742386,"score_gpt":0.307402973280112,"score_spread":0.2712728202926882,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2036185572","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":[0.2505612,0.00019969422,0.7401446,0.000102284874,0.000019511044,0.00005255582,0.000043212982,0.00007953596,0.008797379],"genre_scores_gemma":[0.94194627,0.00015156313,0.055674143,0.000024344708,0.0000060888074,0.00007570929,0.000030202424,0.000025214069,0.002066571],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998398,0.0000505379,0.000006648725,0.00002023135,0.00006720593,0.000015514071],"domain_scores_gemma":[0.99958485,0.00026382782,0.000056212,0.000022664597,0.000053945867,0.000018415698],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00063203985,0.00036459963,0.00030444056,0.00031769046,0.00019646362,0.00040674946,0.0004497405,0.000744091,0.0010795534],"category_scores_gemma":[0.0009937813,0.0002930849,0.00045427887,0.00016497183,0.00062835147,0.00034741985,0.0004326993,0.0003959466,0.00016846182],"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":[0.000047984835,0.000020947895,0.0005934976,0.000057815825,0.000014599155,0.00005204866,0.00006094211,0.9612188,0.027134392,0.00504535,0.00005962948,0.005694049],"study_design_scores_gemma":[0.0000017965524,0.000013234314,0.00008419565,0.0000027994781,0.0000020304983,0.0000062800937,0.0000052411383,0.9982449,0.001329612,0.00022269612,0.00008522794,0.0000020712455],"about_ca_topic_score_codex":0.0011466072,"about_ca_topic_score_gemma":0.001177801,"teacher_disagreement_score":0.0011466072,"about_ca_system_score_codex":0.00024296514,"about_ca_system_score_gemma":0.00044173165,"threshold_uncertainty_score":0.003611505},"labels":[],"label_agreement":null},{"id":"W2037022935","doi":"10.2514/1.5089","title":"Closed-Loop Aeroservoelastic Analysis Validation Method","year":2004,"lang":"en","type":"article","venue":"Journal of Aircraft","topic":"Aeroelasticity and Vibration Control","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":"École de Technologie Supérieure","funders":"National Aeronautics and Space Administration","keywords":"Loop (graph theory); Aeroelasticity; Control theory (sociology); Computer science; Engineering; Aerospace engineering; Aerodynamics; Mathematics; Control (management)","score_opus":0.008565356543908494,"score_gpt":0.2431025079979353,"score_spread":0.23453715145402682,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2037022935","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":[0.009032521,0.00023949107,0.98298025,0.00007819292,0.00007188056,0.00008134547,0.00008382622,0.0010097544,0.006422838],"genre_scores_gemma":[0.816954,0.00024638034,0.1699986,0.0001371317,0.00005711291,0.0005078182,0.00061417295,0.00030797045,0.011176766],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994161,0.00010874224,0.000031006555,0.00011715755,0.00025611778,0.00007088894],"domain_scores_gemma":[0.99889153,0.0003416622,0.000086672946,0.00009078829,0.00055774127,0.000031621585],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0011350174,0.0009594136,0.00078288314,0.00066531793,0.00071019947,0.0011220397,0.0010028897,0.0009983853,0.00782217],"category_scores_gemma":[0.0026384185,0.0003738364,0.00076709903,0.00018456922,0.0004962724,0.00052946765,0.0016937711,0.0011741593,0.0017036307],"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":[0.00013681909,0.000033560984,0.0011921483,0.00023314497,0.00004981243,0.00015866934,0.000109674176,0.8880417,0.009262328,0.0081863515,0.0020441615,0.09055158],"study_design_scores_gemma":[0.000008232353,0.000029949135,0.00015774976,0.000023923416,0.000005499159,0.000021779255,0.000008753305,0.99522483,0.0018421537,0.00093399617,0.0017374482,0.000005646451],"about_ca_topic_score_codex":0.00667769,"about_ca_topic_score_gemma":0.0032480408,"teacher_disagreement_score":0.00782217,"about_ca_system_score_codex":0.00054650666,"about_ca_system_score_gemma":0.001683683,"threshold_uncertainty_score":0.02616769},"labels":[],"label_agreement":null},{"id":"W2037599563","doi":"10.1115/dscc2014-6294","title":"Linear Parameter-Varying Control of a Wing-Section Stall Flutter","year":2014,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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 Toronto","funders":"","keywords":"Control theory (sociology); Flutter; Wing; Stall (fluid mechanics); Nonlinear system; Linearization; Lyapunov function; Jacobian matrix and determinant; Engineering; Computer science; Mathematics; Aerodynamics; Structural engineering; Physics; Control (management); Applied mathematics","score_opus":0.008183972953641027,"score_gpt":0.1964363523141425,"score_spread":0.18825237936050146,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2037599563","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":[0.14262629,0.00027179593,0.8500383,0.0000693675,0.000044615565,0.00004442027,0.000020706733,0.0003784936,0.006506048],"genre_scores_gemma":[0.9933936,0.000054170858,0.0056287544,0.0000125165925,0.000007247144,0.000021413396,0.000009276622,0.000008685971,0.0008643696],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999207,0.000016737637,0.000003282486,0.000020823036,0.0000244116,0.00001394428],"domain_scores_gemma":[0.9999081,0.000031011405,0.000027032847,0.000007322647,0.000020667825,0.000005837906],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00019255164,0.00047819127,0.0002725862,0.00015739125,0.00023823328,0.0003640316,0.00040992312,0.0002601056,0.00074544235],"category_scores_gemma":[0.00028462702,0.0001508367,0.00022195603,0.00008243716,0.00031938258,0.00023154772,0.00031662703,0.00029653838,0.00011940612],"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":[0.00015488084,0.00006107343,0.00057393947,0.00016679366,0.00003632359,0.00017819944,0.00017029015,0.84819895,0.099851124,0.0048054513,0.0004388958,0.04536411],"study_design_scores_gemma":[0.000009030484,0.0001614879,0.0002185375,0.0000046112996,0.000007116678,0.000017425631,0.00001140943,0.99403244,0.0045955414,0.0003038732,0.00063399173,0.0000045009233],"about_ca_topic_score_codex":0.0017519856,"about_ca_topic_score_gemma":0.0015126927,"teacher_disagreement_score":0.0017519856,"about_ca_system_score_codex":0.00018700959,"about_ca_system_score_gemma":0.00022727229,"threshold_uncertainty_score":0.0034835339},"labels":[],"label_agreement":null},{"id":"W2037958515","doi":"10.1007/s00466-003-0525-1","title":"Optimal shape control of functionally graded smart plates using genetic algorithms","year":2004,"lang":"en","type":"article","venue":"Computational Mechanics","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":38,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Canada Research Chairs; University of Toronto","funders":"","keywords":"Genetic algorithm; Voltage; Displacement (psychology); Optimal control; Volume fraction; Actuator; Smart material; Control theory (sociology); Piezoelectricity; Materials science; Algorithm; Mathematics; Computer science; Engineering; Mathematical optimization; Control (management); Composite material","score_opus":0.016455221569425114,"score_gpt":0.21378015867233627,"score_spread":0.19732493710291116,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2037958515","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":[0.2250144,0.0002109496,0.76445496,0.00019492426,0.00008988121,0.000078420075,0.00003120147,0.0003308633,0.009594417],"genre_scores_gemma":[0.94853574,0.00006905806,0.04917748,0.000043543405,0.000012596115,0.00006757184,0.00002308809,0.000036815578,0.0020341834],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99987566,0.000033070206,0.0000049354853,0.000021201942,0.000038694783,0.00002638214],"domain_scores_gemma":[0.99963474,0.00015800979,0.00006418824,0.000027041107,0.00008932783,0.000026572994],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000455396,0.0006637729,0.0007116008,0.0006140434,0.00035322216,0.00066909153,0.0009163208,0.000830121,0.0012352742],"category_scores_gemma":[0.0010690117,0.00044399124,0.0004549506,0.00032862218,0.0010288351,0.0003628077,0.000638365,0.00043288397,0.00016961798],"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":[0.000022859625,0.000014172128,0.00009579822,0.000009064005,0.0000064408046,0.000018354094,0.00001665284,0.9885731,0.0018910596,0.0021277138,0.00008484266,0.007139858],"study_design_scores_gemma":[0.0000105023855,0.000019247296,0.000034287677,0.000001907362,0.0000028236502,0.0000027571516,0.0000052542355,0.9984097,0.00034910665,0.0010939311,0.00006808509,0.0000025232803],"about_ca_topic_score_codex":0.0048380666,"about_ca_topic_score_gemma":0.0053177136,"teacher_disagreement_score":0.0048380666,"about_ca_system_score_codex":0.000693241,"about_ca_system_score_gemma":0.0006834721,"threshold_uncertainty_score":0.009619832},"labels":[],"label_agreement":null},{"id":"W2040538794","doi":"10.4028/www.scientific.net/amr.143-144.424","title":"Electromagnetic Material Based Semi-Passive Switching Shunt Damper","year":2010,"lang":"en","type":"article","venue":"Advanced materials research","topic":"Aeroelasticity and Vibration Control","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":"Kootenay Association for Science & Technology","funders":"","keywords":"Damper; Electromagnetic coil; Electronic circuit; Vibration; Magnet; Engineering; Shunt (medical); RLC circuit; Electronic engineering; Electrical engineering; Voltage; Structural engineering; Acoustics; Physics; Capacitor","score_opus":0.012296309003480603,"score_gpt":0.2862827041751754,"score_spread":0.27398639517169476,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2040538794","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":[0.27096844,0.0007669462,0.71663195,0.00018506667,0.00024039701,0.00011243256,0.00008230474,0.0021283135,0.008884209],"genre_scores_gemma":[0.9346249,0.00015443325,0.06137004,0.000046247427,0.0000402796,0.00004085044,0.00002758983,0.000024474513,0.0036711667],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99989426,0.000015798913,0.000005785483,0.000022073911,0.000055323973,0.0000067197698],"domain_scores_gemma":[0.9998555,0.000056846624,0.000033461012,0.000021088386,0.000022736405,0.000010235501],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012524158,0.00020478769,0.00014794988,0.00019019286,0.00012496852,0.00020611842,0.0006384392,0.0002666479,0.0018107273],"category_scores_gemma":[0.00024161488,0.00010645191,0.00012531361,0.000078315315,0.00021102447,0.00029407602,0.00018301183,0.00019231532,0.00025179822],"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":[0.00019499549,0.000064101245,0.00032047599,0.00021605924,0.000013688403,0.000114197996,0.00007853451,0.0062803235,0.903727,0.0038642979,0.0004252646,0.084701076],"study_design_scores_gemma":[0.000114321454,0.0012095954,0.0027661494,0.00003493317,0.000064202206,0.00081164646,0.000037624366,0.22881913,0.73876286,0.002018063,0.025319112,0.000042343218],"about_ca_topic_score_codex":0.00008408692,"about_ca_topic_score_gemma":0.00016434662,"teacher_disagreement_score":0.0018107273,"about_ca_system_score_codex":0.00011513367,"about_ca_system_score_gemma":0.000091575785,"threshold_uncertainty_score":0.006057501},"labels":[],"label_agreement":null},{"id":"W2040823482","doi":"10.2514/1.40657","title":"Promising Benefits of an Active-Extrados Morphing Laminar Wing","year":2009,"lang":"en","type":"article","venue":"Journal of Aircraft","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":35,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure","funders":"","keywords":"Morphing; Wing; Laminar flow; Swept wing; Materials science; Structural engineering; Aerospace engineering; Computer science; Engineering; Computer graphics (images)","score_opus":0.010649028868195973,"score_gpt":0.2215181777381759,"score_spread":0.21086914886997993,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2040823482","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":[0.9441508,0.0004337,0.048962254,0.00012455683,0.00011633003,0.000018822888,0.000053635635,0.0003670618,0.0057727927],"genre_scores_gemma":[0.9917025,0.00006976659,0.006476506,0.000024287556,0.000020564301,0.000004241907,0.000028579989,0.000015610827,0.0016579111],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99996305,0.0000065578943,0.0000026178184,0.000008263875,0.000010895703,0.000008674991],"domain_scores_gemma":[0.9998901,0.00001833121,0.000021573112,0.000030219913,0.000017494098,0.000022210823],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00011483576,0.00031960921,0.00014899667,0.00014014055,0.000185597,0.0003474402,0.0003319634,0.00023207709,0.0018113763],"category_scores_gemma":[0.000112582034,0.00007046911,0.00021436898,0.00005790919,0.00019199596,0.00038518556,0.00032728398,0.00021383556,0.00028442545],"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":[0.0019522714,0.00040523105,0.0069357688,0.00012607512,0.000039515948,0.00018605187,0.000051054794,0.014496031,0.84686357,0.0035645629,0.0002746623,0.1251052],"study_design_scores_gemma":[0.0004113997,0.0113508925,0.04390471,0.00005622285,0.00024116882,0.0012091082,0.00017448892,0.22788899,0.70037246,0.002490955,0.011795267,0.00010436373],"about_ca_topic_score_codex":0.00009855885,"about_ca_topic_score_gemma":0.00022133828,"teacher_disagreement_score":0.0018113763,"about_ca_system_score_codex":0.00006242226,"about_ca_system_score_gemma":0.00006903975,"threshold_uncertainty_score":0.006059706},"labels":[],"label_agreement":null},{"id":"W2042010175","doi":"10.2514/1.19954","title":"Method Based on Chebyshev Polynomials for Aerservoelastic Interactions on an F/A-18 Aircraft","year":2007,"lang":"en","type":"article","venue":"Journal of Aircraft","topic":"Aeroelasticity and Vibration Control","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":"Université du Québec à Montréal","funders":"National Aeronautics and Space Administration","keywords":"Chebyshev polynomials; Chebyshev filter; Mathematics; Applied mathematics; Computer science; Mathematical analysis","score_opus":0.02445395827528705,"score_gpt":0.3136800344265471,"score_spread":0.28922607615126006,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2042010175","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":[0.009433155,0.00014875717,0.98728895,0.00008101057,0.00013170071,0.00005628965,0.000043175074,0.00015959026,0.0026574],"genre_scores_gemma":[0.2949306,0.0007393584,0.6835152,0.00023144064,0.0002517668,0.00037017363,0.00017896852,0.00039599094,0.01938647],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99975437,0.00009013732,0.000008903857,0.00002681559,0.000087432854,0.00003221058],"domain_scores_gemma":[0.9994081,0.00030370583,0.0000347612,0.00004936588,0.0001654475,0.000038548875],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00058509,0.00072746334,0.00085237785,0.0006162746,0.00081191,0.0006564839,0.001162555,0.0015320086,0.0058221756],"category_scores_gemma":[0.0012727143,0.00036425603,0.00067655015,0.0006104905,0.0005720347,0.00089773146,0.00074186845,0.0016069999,0.0011971286],"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":[0.0003357201,0.00033127514,0.00089474785,0.00031589987,0.000112433976,0.0002809827,0.00018997613,0.7384115,0.02614655,0.058972266,0.004155145,0.1698534],"study_design_scores_gemma":[0.000011699664,0.000020872627,0.00006010127,0.0000041652,0.00000403399,0.000017836846,0.000011133628,0.9973495,0.00051334343,0.001166228,0.0008337104,0.0000073514366],"about_ca_topic_score_codex":0.0072283824,"about_ca_topic_score_gemma":0.0076072514,"teacher_disagreement_score":0.0072283824,"about_ca_system_score_codex":0.00042878685,"about_ca_system_score_gemma":0.0013926001,"threshold_uncertainty_score":0.019477129},"labels":[],"label_agreement":null},{"id":"W2047201894","doi":"10.5139/ijass.2011.12.2.93","title":"Review of Active Rotor Control Research in Canada","year":2011,"lang":"en","type":"article","venue":"International Journal of Aeronautical and Space Sciences","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":13,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"Carleton University","funders":"Natural Sciences and Engineering Research Council of Canada; Mitacs; Ontario Centres of Excellence","keywords":"Engineering; Wind tunnel; Context (archaeology); Control (management); Rotor (electric); Tower; Stiffness; Systems engineering; Aerospace engineering; Mechanical engineering; Computer science; Structural engineering; Geography","score_opus":0.059063389686181675,"score_gpt":0.30722699691124405,"score_spread":0.24816360722506237,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2047201894","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":[0.0010138091,0.9651222,0.0025788946,0.0017983456,0.0011554668,0.000025958472,0.00015644799,0.00006853583,0.028080348],"genre_scores_gemma":[0.01453177,0.9663105,0.0022194828,0.0007596185,0.0005015842,0.000017844899,0.00026298393,0.000038414593,0.015357737],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9987068,0.000064475564,0.000101691556,0.0001297347,0.0008922138,0.00010504394],"domain_scores_gemma":[0.9961599,0.00058487174,0.00015416543,0.00007949853,0.002863174,0.00015837634],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0014714166,0.00089872343,0.0008456208,0.004420713,0.0013282842,0.0027859332,0.0015074328,0.0011681292,0.012193507],"category_scores_gemma":[0.0027028273,0.0005070231,0.0004592781,0.006657254,0.0012087425,0.0016559085,0.0007693615,0.00090533955,0.0028436019],"study_design_candidate":"not_applicable","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":[0.00010362571,0.000055452616,0.0005156087,0.008337387,0.000037163252,0.00016798374,0.00019853971,0.0017453284,0.0020218245,0.012733309,0.054736793,0.919347],"study_design_scores_gemma":[0.0000073774645,0.000060778533,0.0018126328,0.0033086198,0.000037929625,0.00016332732,0.00015755222,0.0003749533,0.00079703564,0.00087933213,0.9923741,0.000026341073],"about_ca_topic_score_codex":0.42596123,"about_ca_topic_score_gemma":0.45293266,"teacher_disagreement_score":0.57403874,"about_ca_system_score_codex":0.010165976,"about_ca_system_score_gemma":0.023146445,"threshold_uncertainty_score":0.8469637},"labels":[],"label_agreement":null},{"id":"W2047574649","doi":"10.1115/imece2010-38851","title":"Novel Morphing Wing Design Using Antagonistic Shape Memory Alloy Actuation","year":2010,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"University of Toronto","funders":"","keywords":"Morphing; Wing; Shape-memory alloy; Parallelogram; Structural engineering; Computer science; FLEX; Wing twist; Engineering; Aerospace engineering; Mechanical engineering; Aerodynamics; Computer graphics (images); Artificial intelligence; Angle of attack; Hinge","score_opus":0.03310814000892818,"score_gpt":0.23424063896032551,"score_spread":0.20113249895139734,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2047574649","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":[0.3557359,0.00061994983,0.62474936,0.00015808363,0.00015606813,0.00007223688,0.00007814506,0.00055782526,0.017872369],"genre_scores_gemma":[0.78700507,0.00032187015,0.20564249,0.000061708895,0.000035504498,0.0000528418,0.00009277359,0.00004561064,0.006742121],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99995196,0.0000040071377,0.0000036163374,0.000010563544,0.000022418371,0.000007435749],"domain_scores_gemma":[0.99996555,0.000003802213,0.000010313943,0.0000051779875,0.000009397742,0.000005625693],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00006635385,0.00028663265,0.00016831346,0.00014189167,0.00012272946,0.00019930053,0.00036299592,0.00020227152,0.0006248168],"category_scores_gemma":[0.00005512827,0.00012390275,0.00016035016,0.00008068131,0.00016264053,0.00020545542,0.00020367657,0.00016698985,0.00030706488],"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":[0.00004754889,0.000016453123,0.000250312,0.00005912037,0.000008765547,0.000105138686,0.00002321918,0.0075828647,0.96342963,0.0038819506,0.00022774891,0.024367228],"study_design_scores_gemma":[0.00005804429,0.00061411125,0.002060285,0.000014498223,0.000044616078,0.0014149062,0.000031941527,0.3223826,0.64899254,0.0021055075,0.022249233,0.00003170777],"about_ca_topic_score_codex":0.00010338725,"about_ca_topic_score_gemma":0.0002496468,"teacher_disagreement_score":0.0006248168,"about_ca_system_score_codex":0.00010515808,"about_ca_system_score_gemma":0.00013255366,"threshold_uncertainty_score":0.002090156},"labels":[],"label_agreement":null},{"id":"W2050935084","doi":"10.2514/1.c032295","title":"Nature of Freeplay-Induced Aeroelastic Oscillations","year":2014,"lang":"en","type":"article","venue":"Journal of Aircraft","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":28,"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":"Aeroelasticity; Aerodynamics; Control theory (sociology); Stiffness; Nonlinear system; Preload; Aerodynamic force; Bifurcation; Mechanics; Structural engineering; Mathematics; Engineering; Physics; Control (management); Computer science","score_opus":0.005159401277545323,"score_gpt":0.20569810701528407,"score_spread":0.20053870573773874,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2050935084","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":[0.9369433,0.00017511514,0.05500842,0.00006357559,0.000028606206,0.00003087136,0.00007459106,0.0001737325,0.007501867],"genre_scores_gemma":[0.9985904,0.00002187839,0.0007404117,0.0000042571637,0.0000032166433,0.000007972985,0.000020616666,0.000009235753,0.0006020197],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999255,0.00000916207,0.000002763569,0.000015487285,0.00003442873,0.000012646624],"domain_scores_gemma":[0.9996425,0.00019326285,0.000057572226,0.000037484333,0.0000429027,0.000026351725],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001025099,0.00022408024,0.00013872486,0.00033526318,0.00015124009,0.00025154388,0.00019385849,0.00020023271,0.0018421797],"category_scores_gemma":[0.00076045713,0.00009942038,0.00015191855,0.00007871678,0.000413633,0.00023187602,0.0002418246,0.00023711249,0.00014360218],"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":[0.00082501955,0.00014587033,0.010209028,0.00032311186,0.000044464145,0.0017539422,0.000935162,0.056192193,0.871576,0.020169439,0.0004957087,0.037329957],"study_design_scores_gemma":[0.000053888685,0.00052018295,0.06401056,0.00006018377,0.000030746047,0.0013099317,0.00038841946,0.78318584,0.13627099,0.011628712,0.0024893852,0.000051080962],"about_ca_topic_score_codex":0.00027744946,"about_ca_topic_score_gemma":0.00018634548,"teacher_disagreement_score":0.0018421797,"about_ca_system_score_codex":0.00012507987,"about_ca_system_score_gemma":0.00009362056,"threshold_uncertainty_score":0.006162703},"labels":[],"label_agreement":null},{"id":"W2053563376","doi":"10.1177/0954410014538244","title":"Active control of aeroelastic oscillations of a cantilever structure using piezoelectric strips","year":2014,"lang":"en","type":"article","venue":"Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering","topic":"Aeroelasticity and Vibration Control","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":"McGill University","funders":"","keywords":"Aeroelasticity; Cantilever; Aerodynamics; Vibration control; Controller (irrigation); Finite element method; Vibration; Actuator; Control theory (sociology); Aerodynamic force; Piezoelectricity; Piezoelectric sensor; Structural engineering; Engineering; Acoustics; Computer science; Physics; Control (management); Aerospace engineering","score_opus":0.006163996586688285,"score_gpt":0.18261414283994923,"score_spread":0.17645014625326094,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2053563376","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":[0.5487756,0.0003666582,0.44555166,0.000094411684,0.00007074407,0.000032494776,0.000028026518,0.0003247447,0.004755579],"genre_scores_gemma":[0.9854924,0.00012062476,0.013439203,0.0000106431835,0.000008737028,0.00001842372,0.000010318197,0.000006731977,0.0008929251],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999666,0.0000062093736,0.0000018411833,0.000008097338,0.000013374043,0.0000039742827],"domain_scores_gemma":[0.9999001,0.0000598503,0.000014807575,0.000007357245,0.000011729429,0.000006203628],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00009033593,0.00021527348,0.00010156153,0.00008072394,0.00010743058,0.00018445538,0.00026773108,0.0001679811,0.00071698497],"category_scores_gemma":[0.00019173966,0.000113775764,0.00012633525,0.000060065515,0.00020050687,0.00013949155,0.00022163775,0.00019951692,0.00007382251],"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":[0.0001694319,0.00007895081,0.00043217992,0.00013066089,0.00002883639,0.00014747673,0.00010506469,0.08735414,0.8552363,0.0032269058,0.00023992005,0.05285011],"study_design_scores_gemma":[0.00006360665,0.0005314722,0.0013072384,0.0000121911,0.000028247605,0.0000875648,0.000031692223,0.89574194,0.09912044,0.0013335954,0.0017280296,0.000014035363],"about_ca_topic_score_codex":0.00027739658,"about_ca_topic_score_gemma":0.00041390597,"teacher_disagreement_score":0.00071698497,"about_ca_system_score_codex":0.000063877975,"about_ca_system_score_gemma":0.00010017762,"threshold_uncertainty_score":0.0023985505},"labels":[],"label_agreement":null},{"id":"W2056256778","doi":"10.2514/1.c032451","title":"Optimal Configuration Design for the Variable Geometry Wing-Box","year":2014,"lang":"en","type":"article","venue":"Journal of Aircraft","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":16,"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":"Kinematics; Configuration design; Wing; Configuration space; Morphing; Optimal design; Rigidity (electromagnetism); Aeroelasticity; Stiffness; Mechanism (biology); Reconfigurability; Computer science; Control theory (sociology); Engineering; Structural engineering; Aerospace engineering; Aerodynamics","score_opus":0.012911078903533315,"score_gpt":0.21666379427640925,"score_spread":0.20375271537287593,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2056256778","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":[0.089406125,0.00033810906,0.8989657,0.000101854195,0.000039961644,0.000083914034,0.000065287655,0.00017440801,0.01082466],"genre_scores_gemma":[0.8419888,0.00019572192,0.15475336,0.0000378546,0.000011721597,0.00014393419,0.00008391693,0.00005251492,0.0027321193],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997867,0.000060157312,0.000008870377,0.000049207527,0.00006603686,0.000029093002],"domain_scores_gemma":[0.99982136,0.00006175289,0.000046742218,0.000019416551,0.000036086636,0.0000146103985],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00032523423,0.00045798384,0.00042219405,0.00034507978,0.00022304582,0.00046757932,0.0004468511,0.0004862561,0.002865278],"category_scores_gemma":[0.0005478225,0.00026054762,0.00027318147,0.00019056554,0.0005749541,0.00040742513,0.00052497874,0.00035698203,0.00036031325],"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":[0.00010320877,0.000031387477,0.00062399963,0.0001142917,0.000016571283,0.00016265473,0.000060312334,0.9157126,0.024683703,0.02589508,0.00055135094,0.032044787],"study_design_scores_gemma":[0.000036898753,0.00028575634,0.00059567246,0.00003128908,0.00001759459,0.00016322886,0.000044118537,0.97814274,0.0061944057,0.010439473,0.0040270616,0.000021755734],"about_ca_topic_score_codex":0.00042049424,"about_ca_topic_score_gemma":0.00046302445,"teacher_disagreement_score":0.002865278,"about_ca_system_score_codex":0.00024058874,"about_ca_system_score_gemma":0.0003996468,"threshold_uncertainty_score":0.009585321},"labels":[],"label_agreement":null},{"id":"W2056582127","doi":"10.2514/1.17646","title":"New Mixed Method for Unsteady Aerodynamic Force Approximations for Aeroservoelasticity Studies","year":2006,"lang":"en","type":"article","venue":"Journal of Aircraft","topic":"Aeroelasticity and Vibration Control","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":"Bombardier (Canada); École de Technologie Supérieure","funders":"","keywords":"Aerodynamics; Aerodynamic force; Aerospace engineering; Aeroelasticity; Computational fluid dynamics; Computer science; Mechanics; Applied mathematics; Physics; Mathematics; Engineering","score_opus":0.017077113922196206,"score_gpt":0.2798639302832571,"score_spread":0.26278681636106094,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2056582127","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":[0.00392198,0.00019621704,0.9938554,0.000054189062,0.000060443737,0.00004080248,0.000060981976,0.0002498809,0.0015599933],"genre_scores_gemma":[0.08499167,0.0003034759,0.9068526,0.000114701405,0.000085760206,0.00044162732,0.00035136405,0.0004694929,0.006389336],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99951375,0.00017951122,0.000024970306,0.00004120163,0.00021148282,0.000028977362],"domain_scores_gemma":[0.9988788,0.0005781967,0.00008342625,0.000090318994,0.00031126058,0.00005794611],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00086550624,0.0009687468,0.0007447419,0.0011194822,0.00055144564,0.000834533,0.0016805578,0.0013132166,0.005361981],"category_scores_gemma":[0.0028992335,0.00051548524,0.0010541225,0.0007303043,0.0005279809,0.0012020791,0.0011168327,0.0016686909,0.0019312412],"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":[0.00043197165,0.00034878612,0.0031148177,0.0007312719,0.00025504027,0.00035764728,0.00032338916,0.5479589,0.035235424,0.09946715,0.006820531,0.304955],"study_design_scores_gemma":[0.0000064559,0.000015611029,0.000058084373,0.000008497174,0.0000030235897,0.000019150579,0.000007788854,0.99587786,0.0006284025,0.0014697871,0.001899067,0.0000063051766],"about_ca_topic_score_codex":0.004088666,"about_ca_topic_score_gemma":0.0045622378,"teacher_disagreement_score":0.005361981,"about_ca_system_score_codex":0.00050007744,"about_ca_system_score_gemma":0.0011597903,"threshold_uncertainty_score":0.0179376},"labels":[],"label_agreement":null},{"id":"W2057020885","doi":"10.2514/2.4566","title":"Minimization of Vibration of Spacecraft Appendages During Shape Control Using Smart Structures","year":2000,"lang":"en","type":"article","venue":"Journal of Guidance Control and Dynamics","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":20,"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 Space Agency","funders":"","keywords":"Spacecraft; Appendage; Control theory (sociology); Vibration; Computer science; Aerospace engineering; Minification; Trajectory; Vibration control; Control (management); Engineering; Control engineering; Geology; Acoustics; Physics; Artificial intelligence","score_opus":0.004593893093402211,"score_gpt":0.19965364825134174,"score_spread":0.19505975515793952,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2057020885","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":[0.81702393,0.00009530483,0.178392,0.000058969028,0.000014276411,0.00002528006,0.000011268376,0.00018002752,0.004198827],"genre_scores_gemma":[0.99174315,0.000012875783,0.007806516,0.000004138221,0.0000018374473,0.0000073833635,0.00000566679,0.000010467139,0.00040788227],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999471,0.000010154356,0.000001954907,0.000007425785,0.000019819472,0.0000136634235],"domain_scores_gemma":[0.9998468,0.000049758382,0.000036333604,0.00002061986,0.000024186505,0.000022208675],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017497058,0.0002193289,0.00022276526,0.00019002029,0.00018105605,0.00016906188,0.00021040885,0.00019059768,0.00092874584],"category_scores_gemma":[0.00041922688,0.0001436115,0.00012483833,0.00008046572,0.00028400574,0.00019855492,0.00026100088,0.00009675749,0.000108594744],"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":[0.00071904843,0.000105079744,0.0029572782,0.00010047378,0.000028785507,0.000105865125,0.00017038795,0.6447136,0.23763523,0.0028892495,0.00037003786,0.11020496],"study_design_scores_gemma":[0.000037296377,0.000484101,0.0029497675,0.000008526237,0.000013546825,0.00003801987,0.00006319634,0.97087896,0.024001831,0.0010175037,0.00049918273,0.000008076128],"about_ca_topic_score_codex":0.0006648356,"about_ca_topic_score_gemma":0.0014285103,"teacher_disagreement_score":0.00092874584,"about_ca_system_score_codex":0.00015479908,"about_ca_system_score_gemma":0.00016739829,"threshold_uncertainty_score":0.0031070113},"labels":[],"label_agreement":null},{"id":"W2057070352","doi":"10.2514/1.21564","title":"Sensitivity Analysis and Optimal Design of Smart Peizolaminated Composite Beams","year":2006,"lang":"en","type":"article","venue":"AIAA Journal","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":9,"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":"Natural Sciences and Engineering Research Council of Canada","keywords":"Finite element method; Actuator; Sensitivity (control systems); Beam (structure); Bending moment; Piezoelectricity; Optimal design; Structural engineering; Bending; Control theory (sociology); Moment (physics); Optimization problem; Materials science; Computer science; Engineering; Physics; Algorithm; Composite material; Electronic engineering","score_opus":0.0059763015105981435,"score_gpt":0.1895426365008577,"score_spread":0.18356633499025957,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2057070352","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":[0.31152752,0.00051524566,0.6786135,0.00023690745,0.000026770616,0.00009721234,0.00008335497,0.00016695376,0.008732602],"genre_scores_gemma":[0.98022836,0.00014230567,0.018658208,0.00002118843,0.0000029870348,0.00005634729,0.000023151471,0.0000125779725,0.0008547268],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997328,0.000096815376,0.000007949159,0.00003800558,0.000084439765,0.00003992458],"domain_scores_gemma":[0.9992723,0.0005293701,0.00007496217,0.000022022303,0.000081110345,0.000020334266],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0011232283,0.0006123068,0.00052469387,0.00043450706,0.00021167757,0.0006284548,0.00033519193,0.0006364389,0.00090931496],"category_scores_gemma":[0.0017693496,0.00056511327,0.00046269264,0.00016711664,0.00061229104,0.0003227305,0.00061075593,0.00036031342,0.00008914755],"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":[0.00004410448,0.000012734195,0.00017663222,0.00004093069,0.000015224187,0.000031402225,0.00001585156,0.98999447,0.0058179647,0.0012450406,0.000036219444,0.0025694421],"study_design_scores_gemma":[0.0000063806165,0.000049452017,0.00016827938,0.000004874013,0.000006321135,0.0000065462164,0.000007731297,0.9961558,0.0028579927,0.00059782877,0.00013396074,0.0000048211305],"about_ca_topic_score_codex":0.0021465009,"about_ca_topic_score_gemma":0.0013774184,"teacher_disagreement_score":0.0021465009,"about_ca_system_score_codex":0.00074360863,"about_ca_system_score_gemma":0.0006054568,"threshold_uncertainty_score":0.005940318},"labels":[],"label_agreement":null},{"id":"W2057721396","doi":"10.1115/smasis2012-8005","title":"Study of Aerospace Structures With Bonded Piezoelectric Strips Subjected to Unsteady Aerodynamic Loads for Structural Health Monitoring","year":2012,"lang":"en","type":"article","venue":"Volume 1: Development and Characterization of Multifunctional Materials; Modeling, Simulation and Control of Adaptive Systems; Structural Health Monitoring","topic":"Aeroelasticity and Vibration Control","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":"McGill University","funders":"","keywords":"Aeroelasticity; Piezoelectricity; Structural engineering; Aerodynamics; Aerodynamic force; Acoustics; Actuator; Structural health monitoring; Torsion (gastropod); STRIPS; Materials science; Piezoelectric sensor; Wing; Finite element method; Mechanics; Engineering; Physics; Composite material","score_opus":0.03141638893543802,"score_gpt":0.2695948427685962,"score_spread":0.23817845383315817,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2057721396","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":[0.9893684,0.00014048084,0.009829331,0.000036672,0.0000073061683,0.000011826803,0.000022415947,0.000018661865,0.0005648592],"genre_scores_gemma":[0.99687696,0.000107326494,0.0025073518,0.000008043531,0.000005093891,0.000010581275,0.000026232448,0.000004155139,0.00045414182],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99986863,0.000020592366,0.0000036428612,0.000021469843,0.000071068636,0.000014507757],"domain_scores_gemma":[0.9997758,0.0001135906,0.000041275056,0.00002222782,0.000033265824,0.0000139093645],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017361532,0.00028662226,0.00029683425,0.00029548767,0.00020193354,0.00023628287,0.00023403202,0.0005734764,0.00062066625],"category_scores_gemma":[0.00045130184,0.00017492705,0.00024472675,0.00012934844,0.00043875017,0.00023065445,0.00021607443,0.00026332668,0.00012922393],"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":[0.00018867225,0.00015411277,0.006250914,0.0001484943,0.0000595359,0.00086802564,0.00035431946,0.1984049,0.7730869,0.0007453704,0.00011912717,0.019619606],"study_design_scores_gemma":[0.000018812878,0.0009568599,0.028353991,0.000019339923,0.000034142155,0.00028361328,0.00031071893,0.85329807,0.1156024,0.0004474461,0.00065388565,0.00002058787],"about_ca_topic_score_codex":0.0005311655,"about_ca_topic_score_gemma":0.00049143675,"teacher_disagreement_score":0.00062066625,"about_ca_system_score_codex":0.00010125103,"about_ca_system_score_gemma":0.000121322686,"threshold_uncertainty_score":0.0020763278},"labels":[],"label_agreement":null},{"id":"W2058730537","doi":"10.1115/imece2003-41085","title":"Adaptive Vibration Control of Flexible Plate Structures With Actuator Placement Optimization","year":2003,"lang":"en","type":"article","venue":"Aerospace","topic":"Aeroelasticity and Vibration Control","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 Space Agency","funders":"","keywords":"Controllability; Vibration control; Actuator; Control theory (sociology); Vibration; Finite element method; Active vibration control; Reduction (mathematics); Genetic algorithm; Computer science; Engineering; Structural engineering; Acoustics; Control (management); Mathematics","score_opus":0.007202348408146643,"score_gpt":0.18885712686186765,"score_spread":0.181654778453721,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2058730537","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":[0.15087943,0.00017566481,0.84595436,0.00007606921,0.000026707261,0.000019019479,0.000008987097,0.00020153442,0.0026582154],"genre_scores_gemma":[0.96574944,0.00006467023,0.032627434,0.000013533141,0.000009944133,0.000021571703,0.000007724539,0.000010791856,0.0014949425],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999331,0.000014751205,0.0000024235894,0.000015852213,0.000025796111,0.0000081687085],"domain_scores_gemma":[0.99991786,0.00003764403,0.000021008482,0.000004994289,0.0000139243075,0.0000046011874],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00013464913,0.00034740343,0.0001592649,0.00010122284,0.00012620521,0.00015340961,0.00028831686,0.00024329178,0.00055853237],"category_scores_gemma":[0.00026875176,0.00014925376,0.0001297227,0.00009086181,0.00027669896,0.00015250155,0.00016958093,0.00017772005,0.00010028485],"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":[0.000098456556,0.000037759877,0.00032155114,0.000060881484,0.000018251005,0.000103937105,0.000056109235,0.7920161,0.14227381,0.0028793123,0.00023182404,0.061902087],"study_design_scores_gemma":[0.000009759621,0.00007686016,0.00021463346,0.0000018912871,0.0000041940475,0.000015109366,0.0000060136686,0.9898337,0.009258214,0.0003579004,0.00021877198,0.0000029550997],"about_ca_topic_score_codex":0.0007673801,"about_ca_topic_score_gemma":0.0009393311,"teacher_disagreement_score":0.0007673801,"about_ca_system_score_codex":0.00014661544,"about_ca_system_score_gemma":0.00015992108,"threshold_uncertainty_score":0.0018684268},"labels":[],"label_agreement":null},{"id":"W2059009499","doi":"10.2514/6.2013-5164","title":"Unmanned Aerial System Hydra Technologies Éhecatl wing optimization using a morphing approach","year":2013,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Université du Québec","funders":"","keywords":"Morphing; Lernaean Hydra; Computer science; Wing; Computer graphics (images); Aeronautics; Aerospace engineering; Engineering; Geography","score_opus":0.01113539176909741,"score_gpt":0.17715566421980347,"score_spread":0.16602027245070605,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2059009499","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":[0.15583658,0.0005160839,0.7954255,0.0004104427,0.00018208752,0.00028942572,0.0002638611,0.0028346756,0.0442413],"genre_scores_gemma":[0.8104832,0.00024269166,0.17568985,0.00015177266,0.000020300391,0.00021465373,0.00022901715,0.00014922454,0.012819353],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999074,0.000015321239,0.000003850663,0.000018002662,0.000038017035,0.000017480626],"domain_scores_gemma":[0.9999236,0.000025589237,0.000012398408,0.000013095568,0.000017323891,0.0000080064265],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001804021,0.00043762737,0.00026262566,0.00026607295,0.00023319655,0.00043816795,0.00038588312,0.00040800736,0.00674383],"category_scores_gemma":[0.00033540078,0.00014286018,0.00042664586,0.00013950246,0.00026301504,0.00031764625,0.00075326307,0.00037173153,0.001117814],"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":[0.00033591627,0.00019351149,0.004234412,0.0003022585,0.00006619973,0.00044154035,0.00021606365,0.5210175,0.09161926,0.008121789,0.0052993256,0.36815223],"study_design_scores_gemma":[0.00005509047,0.00060588453,0.0026089968,0.00004302669,0.000043409003,0.0001899439,0.00017296073,0.9611736,0.01398067,0.002650756,0.018438667,0.000036983172],"about_ca_topic_score_codex":0.0019059605,"about_ca_topic_score_gemma":0.0021372684,"teacher_disagreement_score":0.00674383,"about_ca_system_score_codex":0.00015416554,"about_ca_system_score_gemma":0.00029176424,"threshold_uncertainty_score":0.022560298},"labels":[],"label_agreement":null},{"id":"W2061354452","doi":"10.1115/smasis2012-7999","title":"Control of Oscillations of a Wing Subjected to 3D Unsteady Subsonic Aerodynamic Loads Using Piezoelectric Actuators","year":2012,"lang":"en","type":"article","venue":"Volume 1: Development and Characterization of Multifunctional Materials; Modeling, Simulation and Control of Adaptive Systems; Structural Health Monitoring","topic":"Aeroelasticity and Vibration Control","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":"McGill University","funders":"","keywords":"Aeroelasticity; Aerodynamics; Cantilever; Actuator; Wing; Aerodynamic force; Vibration control; Vibration; Finite element method; Acoustics; Control theory (sociology); Piezoelectricity; Structural engineering; Mechanics; Engineering; Computer science; Physics; Control (management)","score_opus":0.02692543366885948,"score_gpt":0.2537588532722187,"score_spread":0.22683341960335923,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2061354452","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":[0.962629,0.000050007915,0.03638582,0.00003123741,0.000009497426,0.0000060500315,0.000012173104,0.00007123545,0.00080503133],"genre_scores_gemma":[0.9970471,0.000025706599,0.0027363528,0.0000033398815,0.0000011193221,0.000004614772,0.000005854127,0.0000033181059,0.00017265519],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99997234,0.0000045637657,0.0000016917608,0.00000507681,0.000012250179,0.0000040502464],"domain_scores_gemma":[0.99991584,0.000037141825,0.000020648127,0.000008759107,0.000010545136,0.0000071805835],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00008500885,0.0001658241,0.00010454298,0.00008331255,0.00010731549,0.00016413114,0.00012521293,0.00013149202,0.00031515403],"category_scores_gemma":[0.00017466754,0.000067997666,0.000089511545,0.000040963547,0.00022582142,0.00007976918,0.00014765954,0.000111810354,0.000037053534],"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":[0.0001795165,0.000046684938,0.0016839572,0.000057671026,0.000014341482,0.00015706793,0.00022197962,0.11708666,0.85373735,0.00084876193,0.00010873699,0.025857288],"study_design_scores_gemma":[0.000012565485,0.00018100624,0.0036321713,0.000004845082,0.0000075976573,0.000034390527,0.00005334124,0.89369917,0.10161331,0.0002504116,0.0005012466,0.000009969851],"about_ca_topic_score_codex":0.00039529242,"about_ca_topic_score_gemma":0.00061747455,"teacher_disagreement_score":0.00039529242,"about_ca_system_score_codex":0.00007727849,"about_ca_system_score_gemma":0.000095006086,"threshold_uncertainty_score":0.001054287},"labels":[],"label_agreement":null},{"id":"W2061637191","doi":"10.1006/jsvi.2001.4064","title":"NON-LINEAR AEROELASTIC ANALYSIS USING THE POINT TRANSFORMATION METHOD, PART 1: FREEPLAY MODEL","year":2002,"lang":"en","type":"article","venue":"Journal of Sound and Vibration","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":65,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"National Research Council Canada; University of Alberta","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Aeroelasticity; Transformation (genetics); Harmonics; Limit cycle; Limit (mathematics); Point (geometry); Amplitude; Mathematics; Chaotic; Control theory (sociology); Computer science; Mathematical analysis; Applied mathematics; Engineering; Aerodynamics; Physics; Geometry; Aerospace engineering","score_opus":0.03016138071434434,"score_gpt":0.25604052410142697,"score_spread":0.22587914338708262,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2061637191","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":[0.021726685,0.00017462636,0.9734292,0.000058272188,0.000037645674,0.000037249585,0.000089582536,0.00018381127,0.004262971],"genre_scores_gemma":[0.8832266,0.0008651885,0.073645964,0.000043719123,0.000066420274,0.00024874668,0.00042271407,0.00026109483,0.04121953],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998883,0.00002615114,0.000004117745,0.000023753999,0.000046198544,0.000011383346],"domain_scores_gemma":[0.99988973,0.000047044516,0.000012925293,0.000014221457,0.00003023922,0.0000058590713],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00013466377,0.0006831058,0.0006179243,0.0002545039,0.00025009684,0.00060947106,0.0008514699,0.00065284263,0.0042054737],"category_scores_gemma":[0.00043351162,0.00025467816,0.0005981372,0.00029309132,0.00040262088,0.0008598435,0.0004596784,0.00063297607,0.0010672137],"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":[0.00007481848,0.00008856592,0.00039990604,0.00018138869,0.00004429012,0.00018246577,0.00010609266,0.9064296,0.026111294,0.028257322,0.0014112171,0.03671311],"study_design_scores_gemma":[0.0000036058007,0.000014592942,0.00013258184,0.000001867467,0.0000042782676,0.00001447877,0.0000061742867,0.9970385,0.0008318813,0.0013191586,0.0006289708,0.0000039929023],"about_ca_topic_score_codex":0.0045852675,"about_ca_topic_score_gemma":0.003171534,"teacher_disagreement_score":0.0045852675,"about_ca_system_score_codex":0.00020988751,"about_ca_system_score_gemma":0.0004781368,"threshold_uncertainty_score":0.014068663},"labels":[],"label_agreement":null},{"id":"W2063498684","doi":"10.1109/acc.2012.6314992","title":"LQ optimal actuator location in structures","year":2012,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"University of Waterloo","funders":"","keywords":"Actuator; Control theory (sociology); Linear-quadratic regulator; Subgradient method; Convex optimization; Quadratic equation; Computer science; Optimization problem; Regular polygon; Optimal control; Mathematical optimization; Mathematics; Control (management)","score_opus":0.008125685706612195,"score_gpt":0.208283353894902,"score_spread":0.20015766818828978,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2063498684","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":[0.018866356,0.00039798918,0.977887,0.00025953917,0.000025336829,0.000030484853,0.00002163164,0.00017813338,0.0023334862],"genre_scores_gemma":[0.9251028,0.00047240852,0.070738025,0.00015642827,0.00007315854,0.00018149942,0.00008370575,0.00008769009,0.003104373],"study_design_codex":"simulation_or_modeling","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.99933225,0.00033813564,0.000022170081,0.000120710865,0.00013309105,0.000053706404],"domain_scores_gemma":[0.9989827,0.000628657,0.00015534197,0.000034257857,0.0001586919,0.000040250834],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0011858011,0.000791271,0.0010691371,0.00031514053,0.0002328384,0.0008002517,0.00047552647,0.0008056375,0.0013748477],"category_scores_gemma":[0.0031931188,0.00049598346,0.00027630935,0.00031575133,0.0013136718,0.00069603825,0.0007201168,0.000651429,0.0002652121],"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":[0.00009135912,0.00003363232,0.00033582852,0.00016973562,0.000033462344,0.00008643638,0.00008735974,0.95350826,0.0053019803,0.022436695,0.0010106396,0.01690467],"study_design_scores_gemma":[0.000026878213,0.000068403555,0.00013249202,0.000008218535,0.0000049320547,0.000009847722,0.000010371947,0.99083394,0.00051855826,0.008116855,0.00026391787,0.000005685526],"about_ca_topic_score_codex":0.0033161067,"about_ca_topic_score_gemma":0.0014628085,"teacher_disagreement_score":0.0033161067,"about_ca_system_score_codex":0.00071034906,"about_ca_system_score_gemma":0.000997218,"threshold_uncertainty_score":0.006593585},"labels":[],"label_agreement":null},{"id":"W2063836297","doi":"10.1109/tuffc.2009.1106","title":"Fabrication and performance of high-frequency composite transducers with triangular-pillar geometry","year":2009,"lang":"en","type":"article","venue":"IEEE Transactions on Ultrasonics Ferroelectrics and Frequency Control","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":26,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Health Sciences Centre; University of Toronto; Sunnybrook Health Science Centre; Dalhousie University","funders":"","keywords":"Fabrication; Transducer; Pillar; Materials science; Composite number; Acoustics; Geometry; Structural engineering; Engineering; Physics; Composite material; Mathematics","score_opus":0.004934598638756155,"score_gpt":0.17944573053307988,"score_spread":0.17451113189432374,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2063836297","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":[0.90054065,0.0009690562,0.094598316,0.00015938329,0.00012698009,0.00013186575,0.00020494241,0.00055749196,0.00271125],"genre_scores_gemma":[0.8494467,0.00031423022,0.1486031,0.00005237667,0.000024178536,0.000082960454,0.00012041908,0.000036264035,0.0013197768],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9994367,0.000039481216,0.00003589663,0.0001282996,0.00030798494,0.000051700616],"domain_scores_gemma":[0.99899834,0.00032952527,0.0001596125,0.00012062704,0.00028826116,0.000103573104],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004669186,0.0003379264,0.00033673554,0.00028131006,0.00019895042,0.00047396024,0.0005543293,0.0006871452,0.0008123561],"category_scores_gemma":[0.0013604985,0.0003873319,0.00019662835,0.00031321187,0.00037838204,0.0004313703,0.00038367455,0.00029036755,0.00039312805],"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":[0.000051513005,0.000010943846,0.00015874737,0.000031966396,0.0000036070048,0.000029158771,0.000029770026,0.00055154087,0.99575764,0.00004882635,0.00003120467,0.0032951632],"study_design_scores_gemma":[0.000020728545,0.00031884166,0.0019706055,0.000003483846,0.000015540503,0.0001620904,0.000030918625,0.0075957133,0.98894334,0.000038714497,0.00088230503,0.000017669803],"about_ca_topic_score_codex":0.00091912446,"about_ca_topic_score_gemma":0.0015189145,"teacher_disagreement_score":0.00091912446,"about_ca_system_score_codex":0.00035607335,"about_ca_system_score_gemma":0.00038302402,"threshold_uncertainty_score":0.0027176142},"labels":[],"label_agreement":null},{"id":"W2065818713","doi":"10.1177/1045389x07082381","title":"Optimizing the Thickness of Piezoceramic Actuators for Bending Vibration of Planar Structures","year":2007,"lang":"en","type":"article","venue":"Journal of Intelligent Material Systems and Structures","topic":"Aeroelasticity and Vibration Control","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":"Université de Sherbrooke","funders":"","keywords":"Actuator; Planar; Materials science; Bending; Finite element method; Vibration; Coupling (piping); Square (algebra); Substrate (aquarium); Noise (video); Structural engineering; Vibration control; Acoustics; Composite material; Engineering; Geometry; Electrical engineering; Computer science","score_opus":0.012472872640132823,"score_gpt":0.23706267448978774,"score_spread":0.2245898018496549,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2065818713","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":[0.6219629,0.0016299575,0.37038097,0.00019798272,0.000046928653,0.000046556346,0.00007182387,0.00022842479,0.0054343445],"genre_scores_gemma":[0.9534095,0.00044334418,0.045545842,0.000016191756,0.000010677122,0.00002752268,0.00003207118,0.000029834671,0.0004849287],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99988234,0.000015655127,0.000007113134,0.000023879144,0.00004753883,0.000023392906],"domain_scores_gemma":[0.9997758,0.00007323833,0.000075371434,0.000014813871,0.00004798257,0.000012759057],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020751772,0.0007044798,0.00025375665,0.0003096425,0.00017329214,0.00035766963,0.00038720178,0.00034751176,0.00037185272],"category_scores_gemma":[0.0006936593,0.00031440737,0.000155966,0.00016483864,0.00028125616,0.00039332465,0.000276464,0.00021103371,0.00017117399],"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":[0.00007962799,0.000042659816,0.000739525,0.00018964811,0.000022490458,0.0001262571,0.00004549111,0.18418615,0.79081917,0.0014831945,0.00015039802,0.022115415],"study_design_scores_gemma":[0.00004624459,0.00043843105,0.0021737542,0.00003990626,0.00007355496,0.00029415335,0.000119330136,0.5421127,0.4512895,0.0017292771,0.0016445077,0.000038615668],"about_ca_topic_score_codex":0.0003092961,"about_ca_topic_score_gemma":0.0007106622,"teacher_disagreement_score":0.0007044798,"about_ca_system_score_codex":0.00028839547,"about_ca_system_score_gemma":0.00042915504,"threshold_uncertainty_score":0.0020924807},"labels":[],"label_agreement":null},{"id":"W2067786857","doi":"10.1177/1077546306064268","title":"A Discrete Optimal Control Method for a Flexible Cantilever Beam with Time Delay","year":2006,"lang":"en","type":"article","venue":"Journal of Vibration and Control","topic":"Aeroelasticity and Vibration Control","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":false,"ca_institutions":"University of Guelph","funders":"","keywords":"Control theory (sociology); Discretization; Cantilever; Modal; Controller (irrigation); Stability (learning theory); Vibration control; Vibration; Control system; Instability; Beam (structure); Computer science; Control (management); Mathematics; Engineering; Physics","score_opus":0.003536917045848326,"score_gpt":0.2095834541941109,"score_spread":0.20604653714826257,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2067786857","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":[0.0038273963,0.00011229342,0.99467975,0.00006359717,0.00003897235,0.000019785517,0.000007089768,0.000046293306,0.0012047044],"genre_scores_gemma":[0.6766483,0.0004791736,0.31625643,0.000096403055,0.00008969262,0.00028425344,0.000050819835,0.000031271175,0.0060636685],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99983215,0.00003362638,0.000008341023,0.00004986444,0.00006189831,0.000014090822],"domain_scores_gemma":[0.9998596,0.000067645866,0.00001862793,0.00000964963,0.000037083493,0.0000074114805],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00036428397,0.00047001388,0.00036496253,0.00020668244,0.00028817094,0.0005146337,0.0005228018,0.00052298995,0.0021200064],"category_scores_gemma":[0.0005249873,0.00021718984,0.00031798315,0.00019800967,0.00056767755,0.00041970293,0.0004033979,0.00070851826,0.00017936816],"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":[0.00012560723,0.00009096619,0.00036314788,0.00032672368,0.000039231043,0.00012902322,0.00019859787,0.74927735,0.030813392,0.07732366,0.0015195947,0.13979268],"study_design_scores_gemma":[0.000016550954,0.000057189267,0.000047030047,0.000004756253,0.0000049503637,0.0000143640655,0.0000063642424,0.9958144,0.001103567,0.001919948,0.0010061492,0.0000047471813],"about_ca_topic_score_codex":0.0034432425,"about_ca_topic_score_gemma":0.0025549098,"teacher_disagreement_score":0.0034432425,"about_ca_system_score_codex":0.0005239018,"about_ca_system_score_gemma":0.00089569506,"threshold_uncertainty_score":0.007092178},"labels":[],"label_agreement":null},{"id":"W2069929960","doi":"10.1106/vyjr-2ugx-ud2f-dahx","title":"Active Cabin Noise and Vibration Control for Turboprop Aircraft Using Multiple Piezoelectric Actuators","year":2000,"lang":"en","type":"article","venue":"Journal of Intelligent Material Systems and Structures","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":26,"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); National Research Council Canada","funders":"","keywords":"Fuselage; Turboprop; Acoustics; Accelerometer; Propeller; Vibration; Engineering; Active noise control; Actuator; Loudspeaker; Noise (video); Noise reduction; Structural engineering; Aerospace engineering; Computer science; Physics; Electrical engineering; Marine engineering","score_opus":0.009000704594883207,"score_gpt":0.2134875782363977,"score_spread":0.2044868736415145,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2069929960","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":[0.84393257,0.00034239033,0.15396005,0.00007165394,0.00002522723,0.000022615654,0.000015266907,0.00024942015,0.0013806833],"genre_scores_gemma":[0.98905075,0.00008416375,0.009897168,0.0000098850305,0.000008365333,0.000011404476,0.000014046273,0.0000064704086,0.0009177399],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.999887,0.000014336224,0.0000035991375,0.000017841005,0.00006543132,0.000011811532],"domain_scores_gemma":[0.9998615,0.000048761467,0.00003125064,0.000006798576,0.000040841907,0.000010799923],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012722549,0.00038328045,0.00015275711,0.0001968925,0.00018938993,0.00019526093,0.00034409936,0.00018045386,0.0004693439],"category_scores_gemma":[0.00023198726,0.00012815169,0.0001155201,0.00008398626,0.00021722958,0.00013390675,0.0001880515,0.0001396643,0.00007925254],"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":[0.00038515928,0.00006181437,0.0008827333,0.00010139146,0.0000104619085,0.00010472525,0.00011049846,0.011706882,0.9237849,0.00038243172,0.00009205133,0.0623769],"study_design_scores_gemma":[0.00011431378,0.00313754,0.010251591,0.000020741312,0.00008229967,0.0003889714,0.000097230244,0.3709233,0.61104494,0.00041516506,0.0034944655,0.000029357056],"about_ca_topic_score_codex":0.0014975914,"about_ca_topic_score_gemma":0.003061757,"teacher_disagreement_score":0.0014975914,"about_ca_system_score_codex":0.00016395611,"about_ca_system_score_gemma":0.00023001451,"threshold_uncertainty_score":0.0029777288},"labels":[],"label_agreement":null},{"id":"W2070539590","doi":"10.1016/j.jsv.2014.10.028","title":"Time-domain modeling and control of a wing-section stall flutter","year":2014,"lang":"en","type":"article","venue":"Journal of Sound and Vibration","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":23,"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":"Flutter; Stall (fluid mechanics); Wing; Section (typography); Structural engineering; Engineering; Computer science; Aeronautics; Control theory (sociology); Aerospace engineering; Aerodynamics; Control (management); Artificial intelligence","score_opus":0.006201137391971381,"score_gpt":0.18917652578645597,"score_spread":0.18297538839448457,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2070539590","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":[0.3448188,0.00039111325,0.6387676,0.00031312116,0.00015225956,0.0000827813,0.00012504766,0.00057874137,0.014770527],"genre_scores_gemma":[0.99360305,0.000070112335,0.0039803307,0.000019492267,0.000007963287,0.00002212263,0.000025690222,0.0000123267955,0.0022589937],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999187,0.000017546898,0.0000039957245,0.000017378778,0.00002292374,0.00001945186],"domain_scores_gemma":[0.9998503,0.00006386048,0.000026293108,0.000010021903,0.000039451927,0.000009999679],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00028284593,0.0003905577,0.00056350423,0.0002118789,0.0004174439,0.0005780818,0.0004927616,0.00068357337,0.0017647687],"category_scores_gemma":[0.0004602467,0.00025656403,0.00033870953,0.000116709816,0.00036532574,0.0002638114,0.00040489715,0.00033928853,0.00019234813],"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":[0.00008000317,0.00003481852,0.00032964806,0.000036324156,0.000015538146,0.0000679256,0.00004558956,0.98219115,0.008895449,0.0013576396,0.00018405143,0.006761872],"study_design_scores_gemma":[0.0000027692156,0.000017799752,0.00010400278,0.0000011480722,0.0000024903802,0.0000030108292,0.0000035149005,0.9993375,0.00037171497,0.00006637206,0.0000883236,0.0000013910341],"about_ca_topic_score_codex":0.010700702,"about_ca_topic_score_gemma":0.006189742,"teacher_disagreement_score":0.010700702,"about_ca_system_score_codex":0.0003167481,"about_ca_system_score_gemma":0.00048310295,"threshold_uncertainty_score":0.021276832},"labels":[],"label_agreement":null},{"id":"W2071012667","doi":"10.1177/1077546308097269","title":"Optimization of Mechatronic Design Quotient Using Genetic Algorithm in Vibration Controllers for Flexible Beams","year":2009,"lang":"en","type":"article","venue":"Journal of Vibration and Control","topic":"Aeroelasticity and Vibration Control","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":"University of British Columbia","funders":"","keywords":"Control theory (sociology); Genetic algorithm; Optimal design; Damper; Vibration control; Controller (irrigation); Mechatronics; Vibration; Benchmark (surveying); Active vibration control; Control engineering; Linear-quadratic regulator; Engineering; Optimal control; Computer science; Mathematical optimization; Mathematics; Control (management); Artificial intelligence","score_opus":0.013197605360484624,"score_gpt":0.22596365182413047,"score_spread":0.21276604646364586,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2071012667","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":[0.09069604,0.0003580445,0.9067006,0.00010689229,0.000014807294,0.000052831514,0.000008967205,0.00014099707,0.0019208235],"genre_scores_gemma":[0.8442789,0.00018610206,0.15449782,0.00004284815,0.000006956802,0.00011921167,0.00002313264,0.00002705109,0.0008180583],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996556,0.00014532062,0.000015926067,0.00004724488,0.00010560177,0.000030319537],"domain_scores_gemma":[0.9995683,0.00029480652,0.00004462848,0.000016903396,0.00006575212,0.000009591905],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0012125156,0.00058928016,0.0004122808,0.00043963606,0.0002091019,0.0004915253,0.00039293678,0.00059180957,0.00057118014],"category_scores_gemma":[0.0023260708,0.00026090932,0.0003096909,0.0003347426,0.0005946182,0.00038384978,0.00039586885,0.0003459499,0.000076964025],"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":[0.000033658675,0.0000303267,0.0004032127,0.000041121653,0.000015555577,0.000025985928,0.000038626054,0.95683426,0.0047099586,0.0031394153,0.00009894675,0.034628905],"study_design_scores_gemma":[0.000011359284,0.000040681527,0.00012353227,0.0000037873108,0.0000049685273,0.000007154474,0.000005536854,0.9980374,0.0009137418,0.0007186755,0.00013078602,0.0000024106325],"about_ca_topic_score_codex":0.002338264,"about_ca_topic_score_gemma":0.001502463,"teacher_disagreement_score":0.002338264,"about_ca_system_score_codex":0.0005436823,"about_ca_system_score_gemma":0.0007084376,"threshold_uncertainty_score":0.006412506},"labels":[],"label_agreement":null},{"id":"W2072485654","doi":"10.1117/12.813090","title":"Layout optimization of a multi-zoned, multi-layered composite wing under free vibration","year":2009,"lang":"en","type":"article","venue":"Proceedings of SPIE, the International Society for Optical Engineering/Proceedings of SPIE","topic":"Aeroelasticity and Vibration Control","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":"Okanagan University College; University of British Columbia","funders":"","keywords":"Vibration; Wing; Composite number; Finite element method; Computer science; Natural frequency; Materials science; Acoustics; Structural engineering; Composite material; Engineering","score_opus":0.014308948370518566,"score_gpt":0.22474849874467748,"score_spread":0.2104395503741589,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2072485654","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":[0.5658637,0.00022393532,0.4244104,0.00013255271,0.00003523224,0.00007542564,0.000101213845,0.000495443,0.008661992],"genre_scores_gemma":[0.9306284,0.000056417903,0.06792484,0.000014651584,0.000003297995,0.00005695167,0.000038058664,0.00004197295,0.0012354733],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999026,0.000024994913,0.0000026917642,0.000015473524,0.00003259504,0.000021623993],"domain_scores_gemma":[0.9998166,0.000078394136,0.000031833104,0.000017495347,0.000037010886,0.00001863756],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024734723,0.00044929143,0.00036284197,0.00034041976,0.0002683815,0.00039299706,0.00038462508,0.0005188514,0.001328071],"category_scores_gemma":[0.00046583716,0.00037619294,0.0003093734,0.00015581556,0.00027153414,0.00026748178,0.00031751848,0.00022725863,0.0001900424],"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":[0.00006125554,0.000027787411,0.00038604342,0.000035130433,0.000012602529,0.000046758207,0.000019656067,0.9697948,0.022265092,0.00052175514,0.00009959125,0.00672944],"study_design_scores_gemma":[0.00001574122,0.0000909299,0.0003308324,0.0000026014845,0.000007617294,0.000018751296,0.000012724065,0.9952669,0.0037651332,0.0001872318,0.0002962566,0.0000052467954],"about_ca_topic_score_codex":0.0015495952,"about_ca_topic_score_gemma":0.0021717162,"teacher_disagreement_score":0.0015495952,"about_ca_system_score_codex":0.00046457248,"about_ca_system_score_gemma":0.000577905,"threshold_uncertainty_score":0.0044428706},"labels":[],"label_agreement":null},{"id":"W2073486560","doi":"10.4028/www.scientific.net/amr.569.207","title":"Modelling of Electroelastic Behaviour of Embedded Piezoelectric Actuators in Smart Structures: 2D and 3D Effects","year":2012,"lang":"en","type":"article","venue":"Advanced materials research","topic":"Aeroelasticity and Vibration Control","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 Alberta","funders":"","keywords":"Actuator; Piezoelectricity; Materials science; Finite element method; Stress (linguistics); Structural engineering; Shear (geology); Smart material; Acoustics; Mechanical engineering; Composite material; Engineering; Physics; Electrical engineering","score_opus":0.02367165218848718,"score_gpt":0.28912211568666724,"score_spread":0.2654504634981801,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2073486560","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":[0.51648176,0.0005842714,0.4682019,0.00026499262,0.000058934293,0.000082225095,0.00016068597,0.00030327216,0.013861939],"genre_scores_gemma":[0.96648693,0.0005141367,0.02827922,0.00004165359,0.000011028328,0.00010566704,0.00006467803,0.000039146238,0.004457486],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999155,0.00001882354,0.0000049497294,0.0000144808455,0.000035866735,0.000010315383],"domain_scores_gemma":[0.9999056,0.00003997373,0.000016807027,0.00001627218,0.000013230856,0.000008091672],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016096137,0.00044082495,0.00033357885,0.0002000066,0.00017525427,0.00053054065,0.00057957275,0.001267362,0.0009438062],"category_scores_gemma":[0.0004073884,0.000455015,0.0004111324,0.00017280735,0.0005320363,0.00068298046,0.0003445612,0.0003393681,0.00021836154],"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":[0.000013943446,0.000030308733,0.00038282617,0.000030970605,0.000009034896,0.00015554675,0.000056927816,0.95896786,0.035290793,0.0023179636,0.000056889825,0.0026869108],"study_design_scores_gemma":[0.0000032098276,0.000011560698,0.00028871608,0.0000022832503,0.000002285867,0.000030853615,0.000007812302,0.9975546,0.0016397487,0.0002592164,0.00019500307,0.0000047515286],"about_ca_topic_score_codex":0.0014788229,"about_ca_topic_score_gemma":0.0015844279,"teacher_disagreement_score":0.0014788229,"about_ca_system_score_codex":0.0002270624,"about_ca_system_score_gemma":0.00039537612,"threshold_uncertainty_score":0.0031573772},"labels":[],"label_agreement":null},{"id":"W2079795690","doi":"10.1121/1.4783133","title":"Harmonic control of vibration and sound radiation of a plate using a virtual impedance approach.","year":2008,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aeroelasticity and Vibration Control","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":"Acoustics; Electrical impedance; Harmonic; Vibration; Radiation impedance; Structural acoustics; Computer science; Impedance control; Shaker; Audio frequency; Engineering; Physics; Sound pressure; Electrical engineering","score_opus":0.013882112752934524,"score_gpt":0.21493457002971464,"score_spread":0.20105245727678012,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2079795690","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":[0.09810822,0.00026108808,0.89612967,0.00006871944,0.000044826626,0.00003307427,0.00001034799,0.000128388,0.0052156197],"genre_scores_gemma":[0.9458892,0.0001242186,0.05119682,0.000021721467,0.000023720902,0.000025284144,0.000010253178,0.00001158434,0.002697297],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99990904,0.00001758095,0.0000028293418,0.000019512463,0.000044699245,0.0000063225416],"domain_scores_gemma":[0.99990916,0.000040051837,0.00001800012,0.000012544544,0.00001382516,0.0000064095284],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0000945229,0.00028874874,0.00012954569,0.0001014866,0.000086697015,0.00022524061,0.00030791888,0.00018522699,0.0011142052],"category_scores_gemma":[0.00022203985,0.00008033874,0.00016359413,0.00006462683,0.0003228536,0.0002206358,0.00026204163,0.00020681096,0.00016860227],"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":[0.00018646824,0.000049621944,0.00031415647,0.00015946143,0.000033999186,0.00008149566,0.00009949279,0.09479368,0.8116867,0.0081769,0.00026371327,0.0841544],"study_design_scores_gemma":[0.00007907582,0.0008072922,0.0013204567,0.00001787655,0.00006158831,0.00019440809,0.000049751547,0.7673055,0.22064485,0.0035704544,0.005917775,0.00003095201],"about_ca_topic_score_codex":0.0001819076,"about_ca_topic_score_gemma":0.00029485844,"teacher_disagreement_score":0.0011142052,"about_ca_system_score_codex":0.00012310805,"about_ca_system_score_gemma":0.00009167399,"threshold_uncertainty_score":0.003727436},"labels":[],"label_agreement":null},{"id":"W2080456176","doi":"10.2514/1.c032127","title":"Design and Motion Control of Fully Variable Morphing Wings","year":2013,"lang":"en","type":"article","venue":"Journal of Aircraft","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":73,"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":"Morphing; Wing; Kinematics; Computer science; Actuator; Modular design; Mechanism (biology); Aerodynamics; Motion control; Control theory (sociology); Engineering; Aerospace engineering; Control (management); Artificial intelligence; Robot","score_opus":0.006612545694617306,"score_gpt":0.17674826469116414,"score_spread":0.17013571899654684,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2080456176","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":[0.29622203,0.00030863096,0.6988588,0.00005415472,0.00004718425,0.00006432369,0.000031909964,0.0002985688,0.004114381],"genre_scores_gemma":[0.9594018,0.0000907119,0.03950279,0.000010065547,0.000007229725,0.000049571157,0.000013740677,0.000009983722,0.0009141243],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99993706,0.000010530274,0.0000046286236,0.000016491573,0.000020548516,0.00001072501],"domain_scores_gemma":[0.9999069,0.000018393228,0.00003683443,0.000013830231,0.000014841578,0.000009109112],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017959063,0.00023677046,0.00018773277,0.000113925904,0.00012494266,0.0002785701,0.00039562795,0.00019120329,0.00050015014],"category_scores_gemma":[0.00019646288,0.00017442953,0.00016543936,0.00006584009,0.00025477944,0.0001714484,0.00028381762,0.00014986056,0.0000624506],"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":[0.00022360224,0.000045658526,0.000872491,0.00016749126,0.00003532864,0.00019396705,0.000108528024,0.5002954,0.3997624,0.009588945,0.00028317262,0.08842301],"study_design_scores_gemma":[0.000046280216,0.0004612549,0.0011572074,0.000008701883,0.000014099116,0.000078734454,0.000014108666,0.9723226,0.022304183,0.0011944604,0.0023840754,0.000014264414],"about_ca_topic_score_codex":0.0002836734,"about_ca_topic_score_gemma":0.00027342772,"teacher_disagreement_score":0.00050015014,"about_ca_system_score_codex":0.00010282221,"about_ca_system_score_gemma":0.0001797539,"threshold_uncertainty_score":0.001673162},"labels":[],"label_agreement":null},{"id":"W2081436025","doi":"10.2514/6.2012-4639","title":"Design and Experimental Validation of a Control System for a Morphing Wing","year":2012,"lang":"en","type":"article","venue":"AIAA Atmospheric Flight Mechanics Conference","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":29,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure","funders":"Consortium de Recherche et d’innovation en Aérospatiale au Québec","keywords":"Morphing; Wing; Computer science; Aerospace engineering; Computer graphics (images); Engineering","score_opus":0.01827543334343302,"score_gpt":0.21133023118606453,"score_spread":0.19305479784263152,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2081436025","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":[0.5666258,0.0001955473,0.4192459,0.0004014743,0.00042990976,0.0031805257,0.0005267797,0.004178335,0.005215719],"genre_scores_gemma":[0.9466145,0.00003931081,0.050127905,0.00007377627,0.000020702071,0.0006423832,0.00015652807,0.000066076136,0.002258972],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99919814,0.000115959956,0.000073078554,0.00021250195,0.0002988983,0.000101386504],"domain_scores_gemma":[0.9983595,0.00040751047,0.0001746683,0.0002986987,0.00063660735,0.0001229239],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0012828356,0.00074705237,0.00040353695,0.00057042117,0.00089060643,0.00062597817,0.0013214974,0.001081636,0.005423984],"category_scores_gemma":[0.0018881893,0.0003989664,0.00031092338,0.00014936423,0.00065999536,0.0005544392,0.0006438522,0.00050196674,0.0008229402],"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":[0.0016666547,0.0010072713,0.0033113998,0.0006730645,0.000105735795,0.00024084306,0.00046159807,0.019202046,0.87629646,0.0015152317,0.0011241812,0.09439546],"study_design_scores_gemma":[0.0012834745,0.010105904,0.014932913,0.000058229652,0.00021944522,0.00031539507,0.00014885142,0.19382904,0.76671207,0.00044277692,0.01185626,0.00009563255],"about_ca_topic_score_codex":0.0019905742,"about_ca_topic_score_gemma":0.0013044514,"teacher_disagreement_score":0.005423984,"about_ca_system_score_codex":0.0004047179,"about_ca_system_score_gemma":0.0009733356,"threshold_uncertainty_score":0.018145084},"labels":[],"label_agreement":null},{"id":"W2081440725","doi":"10.1115/detc2014-34010","title":"Elastodynamic Modeling and Simulation of the AIRBUS A380 Wing","year":2014,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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 Alberta","funders":"","keywords":"Fuselage; Wing; Vibration; Equations of motion; Aerodynamics; Structural engineering; Finite element method; Natural frequency; Euler equations; Modal analysis; Euler's formula; Cantilever; Modal; Acoustics; Engineering; Physics; Mechanics; Classical mechanics; Mathematics; Mathematical analysis; Materials science","score_opus":0.005950921527190667,"score_gpt":0.188721590449589,"score_spread":0.18277066892239832,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2081440725","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":[0.72060597,0.00032834263,0.22981161,0.000336474,0.00006680206,0.0001238357,0.0008040188,0.0006538092,0.047269158],"genre_scores_gemma":[0.9831339,0.00013985224,0.0095648635,0.000024543348,0.000009721363,0.000082944076,0.00022332711,0.000029469635,0.0067912643],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999101,0.000024948018,0.000003677644,0.000012199869,0.000030616255,0.00001838543],"domain_scores_gemma":[0.99992895,0.00003000945,0.000013269099,0.000007378178,0.0000121488265,0.000008212049],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00014134799,0.00037595775,0.00034227697,0.0003247038,0.00034629056,0.0004570723,0.00044295657,0.00078916707,0.0029109546],"category_scores_gemma":[0.00031193107,0.00020886677,0.00030808977,0.00027937788,0.000367503,0.00037573272,0.0004099327,0.00033320696,0.0003216999],"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":[0.00002303096,0.00001906457,0.00040123583,0.00001514885,0.000004645206,0.000080179765,0.00003093237,0.99239,0.0035135208,0.0014782575,0.00010844732,0.0019355664],"study_design_scores_gemma":[0.0000045833253,0.00001770105,0.00029403862,0.0000014373726,0.0000013529575,0.00001426846,0.0000115525045,0.99856704,0.00043315455,0.00019856147,0.00045400378,0.000002286924],"about_ca_topic_score_codex":0.0057397657,"about_ca_topic_score_gemma":0.0029100967,"teacher_disagreement_score":0.0057397657,"about_ca_system_score_codex":0.0002914445,"about_ca_system_score_gemma":0.00047872512,"threshold_uncertainty_score":0.01141274},"labels":[],"label_agreement":null},{"id":"W2081715187","doi":"10.2514/6.2006-444","title":"Approximations of unsteady aerodynamic forces for closed loop flutter aeroservoelasticity studies","year":2006,"lang":"en","type":"article","venue":"44th AIAA Aerospace Sciences Meeting and Exhibit","topic":"Aeroelasticity and Vibration Control","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":"École de Technologie Supérieure","funders":"Natural Sciences and Engineering Research Council of Canada; Langley Research Center","keywords":"Flutter; Aerodynamics; Aerodynamic force; Aeroelasticity; Mechanics; Loop (graph theory); Control theory (sociology); Aerospace engineering; Closed loop; Computer science; Physics; Engineering; Mathematics; Control engineering; Artificial intelligence; Control (management)","score_opus":0.018667674393346625,"score_gpt":0.2531594230433034,"score_spread":0.23449174864995678,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2081715187","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":[0.07046522,0.00021216617,0.9269262,0.00003600867,0.000034632994,0.000030341691,0.000028837114,0.00019470483,0.002071869],"genre_scores_gemma":[0.8371089,0.00044093162,0.15882558,0.000029950053,0.000033031636,0.000114059236,0.000108649,0.00012625086,0.0032126482],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99980336,0.000056697045,0.000007235467,0.000012180803,0.00010214553,0.000018363842],"domain_scores_gemma":[0.99926656,0.00049211516,0.000055322733,0.000063608764,0.00010154237,0.000020988671],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00051247573,0.00040736742,0.00036641187,0.0004371058,0.00027324245,0.00052016316,0.00044488517,0.00055431505,0.0009693635],"category_scores_gemma":[0.0027595297,0.00021139641,0.00036214548,0.00023696331,0.00044297244,0.00059587735,0.00032810032,0.0008438701,0.0002812481],"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":[0.00009610794,0.00008653927,0.0012732877,0.00009196521,0.000021423362,0.00014606545,0.00020498471,0.91487074,0.017767908,0.01626073,0.0003631977,0.048817188],"study_design_scores_gemma":[0.0000021648445,0.000011956861,0.00009293263,0.0000030975473,8.3479625e-7,0.000010176052,0.000007849955,0.9984243,0.00079035,0.0003967565,0.00025713292,0.0000025307788],"about_ca_topic_score_codex":0.0038354723,"about_ca_topic_score_gemma":0.0026988497,"teacher_disagreement_score":0.0038354723,"about_ca_system_score_codex":0.00029634053,"about_ca_system_score_gemma":0.00037423402,"threshold_uncertainty_score":0.007626295},"labels":[],"label_agreement":null},{"id":"W2083330600","doi":"10.1177/1077546305055772","title":"Development and Application of an Active Control System for Smart Structures Using the Wave Method","year":2005,"lang":"en","type":"article","venue":"Journal of Vibration and Control","topic":"Aeroelasticity and Vibration Control","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":"Canadian Space Agency","funders":"","keywords":"Controller (irrigation); Control theory (sociology); Parametric statistics; Actuator; Control engineering; Vibration control; Engineering; Control system; Open-loop controller; Simple (philosophy); Vibration; Computer science; Control (management); Mathematics; Acoustics; Physics","score_opus":0.012364905601296128,"score_gpt":0.2513174831078521,"score_spread":0.238952577506556,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2083330600","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":[0.0162483,0.000109448396,0.98081243,0.00005743714,0.000052013896,0.000053981807,0.000006948619,0.00037586258,0.0022835755],"genre_scores_gemma":[0.5735871,0.00034929955,0.41831928,0.00010626379,0.00006852771,0.00029206648,0.000046017332,0.000040291972,0.0071912273],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99985373,0.000014142771,0.0000073597384,0.000026826237,0.00008830597,0.0000095606565],"domain_scores_gemma":[0.9998511,0.000040850988,0.000019675712,0.000023448234,0.000051423805,0.0000135305045],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00022340038,0.00026798365,0.00023158571,0.0002019135,0.00020760935,0.00034319772,0.0005985478,0.00046831157,0.0014930377],"category_scores_gemma":[0.00030905943,0.00014117772,0.00017643734,0.00010447034,0.0003640215,0.0004907849,0.00028960782,0.00037568063,0.00038450884],"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":[0.0001071699,0.00014706732,0.00067647384,0.00020952594,0.000027675009,0.00022254797,0.00021086479,0.04954812,0.48954168,0.038432285,0.001503957,0.4193727],"study_design_scores_gemma":[0.000075886805,0.0007604883,0.0008355601,0.000027864078,0.000038352042,0.00026633707,0.000042245705,0.8192553,0.15036666,0.004905652,0.023393136,0.00003257094],"about_ca_topic_score_codex":0.00030877255,"about_ca_topic_score_gemma":0.00040846597,"teacher_disagreement_score":0.0014930377,"about_ca_system_score_codex":0.0001371285,"about_ca_system_score_gemma":0.0002565792,"threshold_uncertainty_score":0.0049946904},"labels":[],"label_agreement":null},{"id":"W2084439657","doi":"10.1016/s0263-8231(00)00034-3","title":"Simulations and experiments on active vibration control of a plate with integrated piezoceramics","year":2000,"lang":"en","type":"article","venue":"Thin-Walled Structures","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":24,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Université Laval","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Active vibration control; Vibration; Vibration control; Acoustics; Structural engineering; Computer science; Materials science; Engineering; Physics","score_opus":0.006488909789261741,"score_gpt":0.2113477336293847,"score_spread":0.20485882384012294,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2084439657","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":[0.97727716,0.00009271071,0.015686005,0.00009785528,0.000031998283,0.00003595023,0.000097409655,0.00015286126,0.006528095],"genre_scores_gemma":[0.99811137,0.000019314846,0.0012874808,0.0000060021544,0.0000021428586,0.00001565434,0.000019431798,0.000008066298,0.0005305207],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99984705,0.000026697377,0.000007131283,0.000019508314,0.000060042807,0.000039524894],"domain_scores_gemma":[0.9991352,0.00055355177,0.000074165335,0.00006250543,0.00011519555,0.000059430236],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00030851303,0.0005754113,0.00053066807,0.0002878428,0.00042933327,0.0004658916,0.0008255249,0.0011181643,0.0021629876],"category_scores_gemma":[0.001161899,0.00032410506,0.00033167397,0.00025302052,0.0008742935,0.00048221843,0.0003693464,0.0005528042,0.00013116955],"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":[0.00021559355,0.00012480465,0.0006339136,0.000057265202,0.00001421138,0.000077511955,0.00005909015,0.9870358,0.008040729,0.0007487004,0.00012060565,0.0028718705],"study_design_scores_gemma":[0.000041808897,0.000114880815,0.00042311833,0.0000035578726,0.000007115233,0.0000071250925,0.000017234794,0.99550205,0.0036562446,0.00014245592,0.00007897601,0.0000054350608],"about_ca_topic_score_codex":0.0054857275,"about_ca_topic_score_gemma":0.0031587624,"teacher_disagreement_score":0.0054857275,"about_ca_system_score_codex":0.00043944293,"about_ca_system_score_gemma":0.00042110978,"threshold_uncertainty_score":0.01090759},"labels":[],"label_agreement":null},{"id":"W2084660559","doi":"10.1177/1077546306071407","title":"Design of Vibration Controllers for Flexible Beams Using the Mechatronic Design Quotient (MDQ) Approach","year":2007,"lang":"en","type":"article","venue":"Journal of Vibration and Control","topic":"Aeroelasticity and Vibration Control","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":"Control theory (sociology); Optimal design; Damper; Vibration; Mechatronics; Linear-quadratic regulator; Settling time; Vibration control; Optimal control; Controller (irrigation); Engineering; Control engineering; Computer science; Mathematical optimization; Mathematics; Control (management); Step response","score_opus":0.0303989863737632,"score_gpt":0.24201655423968088,"score_spread":0.21161756786591768,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2084660559","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":[0.010925432,0.00023556486,0.98774856,0.000043398366,0.00001634056,0.000058261485,0.0000056025697,0.0000673336,0.0008993989],"genre_scores_gemma":[0.6894898,0.0004370648,0.30843958,0.0000834932,0.000028524786,0.0004441377,0.000036547346,0.000049196435,0.0009916415],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9992506,0.00021178454,0.000064581145,0.00013219396,0.0002818291,0.000059028516],"domain_scores_gemma":[0.99932003,0.00036480973,0.00012242988,0.00003451193,0.000140881,0.000017295299],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0018014644,0.0011350899,0.00064067956,0.00045963746,0.00027118847,0.0007166765,0.0006014113,0.00069045956,0.0010032046],"category_scores_gemma":[0.0021764133,0.00041683626,0.00071111275,0.0002498547,0.0006100156,0.00058394653,0.00088284013,0.00064575445,0.00019536728],"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":[0.00010526692,0.0000761483,0.0006303787,0.00042029613,0.00007388265,0.00010525919,0.00018202183,0.8376332,0.049436085,0.012741939,0.0002336647,0.09836191],"study_design_scores_gemma":[0.000029704188,0.00031826168,0.0002461964,0.000024133657,0.00002296886,0.000038798622,0.000026175085,0.9897462,0.0053060767,0.0030947148,0.0011338218,0.000012867295],"about_ca_topic_score_codex":0.0010270644,"about_ca_topic_score_gemma":0.00072414015,"teacher_disagreement_score":0.0018014644,"about_ca_system_score_codex":0.0004653086,"about_ca_system_score_gemma":0.00087175146,"threshold_uncertainty_score":0.009527147},"labels":[],"label_agreement":null},{"id":"W2086192304","doi":"10.1088/0964-1726/20/12/125007","title":"Design and verification of a smart wing for an extreme-agility micro-air-vehicle","year":2011,"lang":"en","type":"article","venue":"Smart Materials and Structures","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":33,"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; National Research Council Canada","funders":"Japan Society for the Promotion of Science; Ministry of Education, Culture, Sports, Science and Technology","keywords":"Aileron; Deflection (physics); Actuator; Wing; Airfoil; Finite element method; Engineering; Bimorph; Aerodynamics; Smart material; Structural engineering; Aerospace engineering; Computer science; Materials science; Physics; Electrical engineering; Optics","score_opus":0.04181961462839049,"score_gpt":0.22082192108545745,"score_spread":0.17900230645706697,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2086192304","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":[0.8193466,0.00029464098,0.17310965,0.00026059346,0.00015138884,0.0003639677,0.00015055492,0.0005694784,0.005753201],"genre_scores_gemma":[0.9514572,0.00006754901,0.04631537,0.000025774996,0.0000054494913,0.00009273846,0.000057281537,0.000017218075,0.0019613614],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99976295,0.000021910828,0.000009219346,0.000029325913,0.00014619977,0.000030376974],"domain_scores_gemma":[0.9997291,0.000030051675,0.000056912173,0.0000525728,0.0000847225,0.00004655134],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00032758212,0.00021137444,0.00020577577,0.00014242236,0.00016016005,0.000261029,0.0004462603,0.00047109602,0.00070305995],"category_scores_gemma":[0.00034486665,0.00010757316,0.00016042523,0.000038080696,0.0002938983,0.0002078938,0.0003261496,0.00021486908,0.00025732812],"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":[0.00015332483,0.00008347709,0.0026453538,0.00020338756,0.000023950664,0.00053065264,0.00011329338,0.053895812,0.9142166,0.0028672086,0.00045136674,0.024815591],"study_design_scores_gemma":[0.00009909459,0.0021259452,0.0069983723,0.000034076114,0.00003097704,0.00045304885,0.00010221562,0.33425578,0.64138883,0.0005874742,0.013887265,0.000036894922],"about_ca_topic_score_codex":0.00046079932,"about_ca_topic_score_gemma":0.00047922827,"teacher_disagreement_score":0.00070305995,"about_ca_system_score_codex":0.0002313597,"about_ca_system_score_gemma":0.0004685862,"threshold_uncertainty_score":0.0023519993},"labels":[],"label_agreement":null},{"id":"W2087044687","doi":"10.1088/0964-1726/18/2/025007","title":"Active shape control of composite structures under thermal loading","year":2009,"lang":"en","type":"article","venue":"Smart Materials and Structures","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":22,"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":"Composite number; Materials science; Thermal; Composite material; Structural engineering; Engineering; Physics; Thermodynamics","score_opus":0.006532730668267736,"score_gpt":0.20571313024101723,"score_spread":0.1991803995727495,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2087044687","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":[0.9856757,0.00011382465,0.012566715,0.000027415841,0.000015496553,0.0000059478084,0.000007809937,0.00007540698,0.001511607],"genre_scores_gemma":[0.9966009,0.000042935797,0.0029331238,0.000008041435,0.0000034211967,0.0000039575234,0.0000062269187,0.0000073862834,0.0003939622],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999081,0.000008113142,0.000003242678,0.000016847076,0.000048970614,0.000014698765],"domain_scores_gemma":[0.9998331,0.00004334856,0.00005430567,0.000023157934,0.000028814718,0.000017137078],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000104341016,0.00018088143,0.0001247423,0.00012307108,0.00013235473,0.0001769961,0.0001869028,0.00016433284,0.00031725765],"category_scores_gemma":[0.000252757,0.000122040925,0.00008610701,0.00006830761,0.00035324288,0.00017569229,0.00018688606,0.00011912192,0.00007812064],"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":[0.000043279262,0.000009136283,0.00014526484,0.000013472761,0.0000015157159,0.000032402553,0.000032903215,0.003316014,0.99229866,0.00014643375,0.000025839776,0.0039349957],"study_design_scores_gemma":[0.000012743102,0.00015697328,0.0020261006,0.000002714364,0.0000053351955,0.000078982775,0.000029356059,0.03894518,0.9579238,0.00013616165,0.0006721506,0.000010409588],"about_ca_topic_score_codex":0.00018426079,"about_ca_topic_score_gemma":0.00038789542,"teacher_disagreement_score":0.00031725765,"about_ca_system_score_codex":0.00014648729,"about_ca_system_score_gemma":0.00009520742,"threshold_uncertainty_score":0.00106287},"labels":[],"label_agreement":null},{"id":"W2087568287","doi":"10.1177/1077546311430104","title":"On the methodology for evaluation of dynamic effects of a surface bonded piezoelectric patch for active vibration control","year":2012,"lang":"en","type":"article","venue":"Journal of Vibration and Control","topic":"Aeroelasticity and Vibration Control","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 Victoria","funders":"","keywords":"Vibration; Actuator; Piezoelectricity; Beam (structure); Control theory (sociology); Transfer matrix; Active vibration control; Vibration control; Smart material; Transfer-matrix method (optics); Piezoelectric sensor; Materials science; Work (physics); Normal mode; Voltage; Acoustics; Structural engineering; Engineering; Computer science; Mechanical engineering; Physics; Control (management)","score_opus":0.022978909750064874,"score_gpt":0.28663438355962667,"score_spread":0.2636554738095618,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2087568287","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":[0.0016004321,0.00004006622,0.9971967,0.00000612061,0.0000053709796,0.000025634314,0.0000066982416,0.0001162988,0.00100273],"genre_scores_gemma":[0.16620053,0.00034095198,0.8298103,0.000025911197,0.000019450224,0.00024541063,0.000045154906,0.00019583969,0.0031164496],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99973136,0.000069929454,0.000010478447,0.000026044898,0.00014910505,0.000013115069],"domain_scores_gemma":[0.9996433,0.00019765717,0.000026425056,0.000052223506,0.00007508117,0.000005255132],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00061504,0.0005073072,0.0004168045,0.0005049945,0.00023134271,0.0004923362,0.0007840299,0.00040590717,0.0035070996],"category_scores_gemma":[0.001409281,0.0002504932,0.00047118333,0.0003257062,0.0005253637,0.0004716844,0.0003410233,0.00053745514,0.0009712777],"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":[0.000046586083,0.000089243134,0.00039621932,0.0005410395,0.000046010155,0.00018555403,0.00018214212,0.47376162,0.15449741,0.11360255,0.0009950565,0.2556565],"study_design_scores_gemma":[0.0000048666543,0.000070354334,0.0001732501,0.000019276813,0.000007872292,0.000075018186,0.000012457351,0.9722549,0.017313711,0.0066675264,0.003390185,0.000010680853],"about_ca_topic_score_codex":0.0007904815,"about_ca_topic_score_gemma":0.0005336733,"teacher_disagreement_score":0.0035070996,"about_ca_system_score_codex":0.00025663254,"about_ca_system_score_gemma":0.00045571863,"threshold_uncertainty_score":0.011732459},"labels":[],"label_agreement":null},{"id":"W2090229922","doi":"10.1121/1.4904550","title":"Optimal virtual mechanical impedances for the vibroacoustic active control of a thin plate","year":2015,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":6,"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":"Natural Sciences and Engineering Research Council of Canada","keywords":"Actuator; Mechanical impedance; Electrical impedance; Acoustics; Controller (irrigation); Computer science; Harmonic; Sound power; Reduction (mathematics); Vibration; Control theory (sociology); Acoustic impedance; Maximum power transfer theorem; Power (physics); Engineering; Physics; Control (management); Mathematics; Electrical engineering; Sound (geography)","score_opus":0.014171053628891041,"score_gpt":0.2382880154508284,"score_spread":0.22411696182193735,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2090229922","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":[0.039802946,0.0001150712,0.9580274,0.00004859567,0.000021793141,0.000039263923,0.00000925233,0.0001513601,0.0017843265],"genre_scores_gemma":[0.8948803,0.00007035827,0.10373377,0.000022555878,0.00001001824,0.00007447938,0.000015153861,0.0000258218,0.0011676246],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99966323,0.000070032,0.000016568136,0.000046807752,0.0001779648,0.000025453814],"domain_scores_gemma":[0.9997168,0.00013497133,0.00006799528,0.000019176645,0.00004670917,0.00001421703],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00037361644,0.0006576104,0.0003793876,0.0003200367,0.00020341921,0.0007708579,0.00058700057,0.00040220885,0.001337838],"category_scores_gemma":[0.0009159767,0.00029228153,0.00026508645,0.00019194033,0.0005625643,0.00035023087,0.00046553087,0.0004842092,0.00020174647],"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":[0.00046501646,0.00023788393,0.0004225665,0.000322421,0.000060137587,0.00016110006,0.00020012166,0.5536892,0.2878365,0.020488385,0.00051621284,0.13560046],"study_design_scores_gemma":[0.00004632647,0.00018201798,0.00020335261,0.000009708723,0.000014574976,0.000032020078,0.00001730102,0.98238474,0.014595432,0.0018436019,0.00065649004,0.000014360869],"about_ca_topic_score_codex":0.000724261,"about_ca_topic_score_gemma":0.0010856636,"teacher_disagreement_score":0.001337838,"about_ca_system_score_codex":0.00039737084,"about_ca_system_score_gemma":0.00038565107,"threshold_uncertainty_score":0.0044754744},"labels":[],"label_agreement":null},{"id":"W2091055591","doi":"10.1115/imece2014-37611","title":"Active Vibration Control of a Composite Sandwich Plate","year":2014,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":29,"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":"Vibration; Active vibration control; Finite element method; Modal; Vibration control; Modal analysis; Natural frequency; Modal testing; Composite plate; Actuator; Structural engineering; Materials science; Controller (irrigation); Piezoelectric sensor; Acoustics; Control theory (sociology); Composite number; Piezoelectricity; Engineering; Computer science; Composite material; Physics","score_opus":0.004403351362608709,"score_gpt":0.18369789242129111,"score_spread":0.1792945410586824,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2091055591","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":[0.92712444,0.00032154965,0.06854223,0.00005373844,0.000056373392,0.00003120749,0.000033849446,0.0003445391,0.0034921882],"genre_scores_gemma":[0.99565566,0.00003713573,0.0037931188,0.0000073232413,0.000004563699,0.000009517146,0.0000068981212,0.000003687502,0.00048208458],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998976,0.000012887349,0.000004119598,0.000023968512,0.00004861543,0.000012719169],"domain_scores_gemma":[0.9998487,0.000055769386,0.000030470226,0.000016377744,0.000031665564,0.000016856457],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016965113,0.00040840078,0.00017635897,0.00019706941,0.000118959244,0.00022262259,0.00048026082,0.00026041476,0.001252394],"category_scores_gemma":[0.00023393432,0.000090185575,0.00012227878,0.000075158634,0.0003272503,0.00011659424,0.00031570287,0.00021013098,0.00014300506],"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":[0.00019006124,0.000047136553,0.00023726701,0.00013124917,0.000011355652,0.0001426963,0.00004928119,0.012357348,0.96974427,0.00034873068,0.00008354153,0.016657166],"study_design_scores_gemma":[0.000076607925,0.0023903076,0.0045254515,0.00002709412,0.000040753344,0.00020478989,0.00005549521,0.21567963,0.775333,0.00034900245,0.0012868576,0.000031055708],"about_ca_topic_score_codex":0.00025570588,"about_ca_topic_score_gemma":0.00026524294,"teacher_disagreement_score":0.001252394,"about_ca_system_score_codex":0.00010387938,"about_ca_system_score_gemma":0.00009137499,"threshold_uncertainty_score":0.0041896105},"labels":[],"label_agreement":null},{"id":"W2091778354","doi":"10.1142/s0219455414500849","title":"Analytical and Experimental Aeroelastic Wing Flutter Analysis and Suppression","year":2015,"lang":"en","type":"article","venue":"International Journal of Structural Stability and Dynamics","topic":"Aeroelasticity and Vibration Control","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":"Université de Sherbrooke","funders":"","keywords":"Aeroelasticity; Flutter; Airfoil; Control theory (sociology); Aerodynamics; Wing; Aerodynamic force; Engineering; Structural engineering; Nonlinear system; Wind tunnel; Controller (irrigation); Computer science; Aerospace engineering; Physics; Control (management)","score_opus":0.012169862511544245,"score_gpt":0.2528685429956917,"score_spread":0.24069868048414747,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2091778354","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":[0.9912509,0.00014344507,0.0053068073,0.000034020344,0.000019359322,0.000045293,0.00018498191,0.000113455775,0.0029018305],"genre_scores_gemma":[0.9976343,0.000084207495,0.0013383243,0.000004008478,0.0000041017993,0.00002931523,0.0000744531,0.000010605383,0.0008208674],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997814,0.000019816,0.000009099653,0.00002797816,0.000111969544,0.00004981386],"domain_scores_gemma":[0.99963844,0.00013788432,0.000050749815,0.00005681033,0.00008895716,0.000027224278],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00028225276,0.00039405556,0.0003245259,0.00030462726,0.0003685222,0.000209072,0.00039689572,0.0004166206,0.0022913008],"category_scores_gemma":[0.0006288838,0.0001448117,0.00026282578,0.00023179181,0.0005096063,0.00021276236,0.00031218666,0.0002731945,0.0002248447],"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":[0.0002640327,0.00021593517,0.00083046564,0.00016328083,0.000007768334,0.00018381825,0.00023501477,0.014012739,0.9788078,0.00036504105,0.00023714913,0.004676861],"study_design_scores_gemma":[0.00009369378,0.0025360354,0.012051039,0.000026913747,0.000019931347,0.00026241434,0.0002903756,0.16073598,0.8217791,0.00033515517,0.001828189,0.00004133216],"about_ca_topic_score_codex":0.00092432485,"about_ca_topic_score_gemma":0.0007902161,"teacher_disagreement_score":0.0022913008,"about_ca_system_score_codex":0.00021684341,"about_ca_system_score_gemma":0.00015200187,"threshold_uncertainty_score":0.0076651573},"labels":[],"label_agreement":null},{"id":"W2093982091","doi":"10.1121/1.3106124","title":"Decentralized harmonic control of sound radiation and transmission by a plate using a virtual impedance approach","year":2009,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":18,"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":"Acoustics; Sound transmission class; Radiation impedance; Sound power; Materials science; Electrical impedance; Actuator; Lead zirconate titanate; Polyvinylidene fluoride; Acoustic impedance; Soundproofing; Harmonic; Transmission (telecommunications); Piezoelectricity; Radiation; Transmission loss; Power (physics); Optics; Sound (geography); Computer science; Physics; Electrical engineering; Optoelectronics; Ferroelectricity; Engineering; Telecommunications; Dielectric","score_opus":0.008399196258565904,"score_gpt":0.22186740879054456,"score_spread":0.21346821253197865,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2093982091","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":[0.066053234,0.00011510109,0.9256646,0.000106104366,0.000028298693,0.000034658467,0.00001563391,0.00019958573,0.00778275],"genre_scores_gemma":[0.9701025,0.00008084764,0.02606351,0.000025121572,0.000022071865,0.00004636884,0.000010203081,0.000022115986,0.0036272192],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997353,0.00006029102,0.000009165545,0.00006555435,0.000091985974,0.00003768058],"domain_scores_gemma":[0.9997569,0.00011103424,0.00004325251,0.00002681878,0.00004334476,0.000018589053],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00031670192,0.00041333897,0.0004435879,0.00020382926,0.0002485664,0.00078364485,0.0007095886,0.00032800648,0.0016176676],"category_scores_gemma":[0.00042720544,0.00022888958,0.0003211321,0.00013768088,0.00090410764,0.0005137782,0.0006579047,0.00038994852,0.00025032944],"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":[0.00027541115,0.00009642703,0.00030294532,0.0001675979,0.000058039437,0.00014769389,0.00020071835,0.76722485,0.13353303,0.04076268,0.0005309302,0.056699652],"study_design_scores_gemma":[0.000036420388,0.00018357763,0.00015599107,0.000004309825,0.000016365091,0.000027565717,0.000018563152,0.9858607,0.007211334,0.0056122416,0.0008587642,0.000014153261],"about_ca_topic_score_codex":0.00090262684,"about_ca_topic_score_gemma":0.0008309971,"teacher_disagreement_score":0.0016176676,"about_ca_system_score_codex":0.00043831274,"about_ca_system_score_gemma":0.00038772443,"threshold_uncertainty_score":0.005411625},"labels":[],"label_agreement":null},{"id":"W2095539708","doi":"10.1016/j.jfluidstructs.2004.03.002","title":"Equivalent linear modal parameter estimation for a nonlinear aeroelastic system","year":2004,"lang":"en","type":"article","venue":"Journal of Fluids and Structures","topic":"Aeroelasticity and Vibration Control","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":"McGill University","funders":"","keywords":"Aeroelasticity; Modal; Nonlinear system; Structural engineering; Mathematics; Control theory (sociology); Engineering; Physics; Computer science; Materials science; Mechanics; Aerodynamics; Composite material","score_opus":0.011146062652337717,"score_gpt":0.2370544462320982,"score_spread":0.22590838357976048,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2095539708","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":[0.046237167,0.00006292225,0.95167845,0.000064564476,0.000012702192,0.000022220449,0.000047514328,0.00025976615,0.001614643],"genre_scores_gemma":[0.95801276,0.000066820256,0.03882255,0.000039775125,0.000014853995,0.00004473326,0.00009677923,0.000037414626,0.002864249],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999742,0.000066994086,0.000013927104,0.00006168295,0.000092740505,0.00002264083],"domain_scores_gemma":[0.99961996,0.0002348915,0.00003384343,0.00003373853,0.00006798649,0.00000953958],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00031300023,0.00040603123,0.00045467573,0.00024529744,0.0002916655,0.00045040596,0.00045206863,0.0007613683,0.0021438794],"category_scores_gemma":[0.0013981909,0.00023503987,0.0002655767,0.00012720996,0.00032106717,0.0006697592,0.0005638811,0.00044227557,0.00032752997],"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":[0.00039818502,0.000112683905,0.0012723044,0.00017267615,0.000070310445,0.00015597671,0.00016990959,0.788558,0.061433077,0.0030539325,0.0006902852,0.14391266],"study_design_scores_gemma":[0.000005339295,0.000019221106,0.0004112092,0.0000021027702,0.000005875001,0.000014295837,0.00000751961,0.99714714,0.0017904273,0.00044795676,0.00014452254,0.0000044671124],"about_ca_topic_score_codex":0.004020244,"about_ca_topic_score_gemma":0.003781426,"teacher_disagreement_score":0.004020244,"about_ca_system_score_codex":0.00026139186,"about_ca_system_score_gemma":0.0002779239,"threshold_uncertainty_score":0.007993698},"labels":[],"label_agreement":null},{"id":"W2096155237","doi":"10.1177/1045389x09343478","title":"Finite Element Modeling of a Slewing Non-linear Flexible Beam for Active Vibration Control with Arrays of Sensors and Actuators","year":2009,"lang":"en","type":"article","venue":"Journal of Intelligent Material Systems and Structures","topic":"Aeroelasticity and Vibration Control","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":"Simon Fraser University; University of Victoria","funders":"","keywords":"Finite element method; Galerkin method; Discretization; Beam (structure); Equations of motion; Vibration; Mathematical analysis; Actuator; Singularity; Control theory (sociology); Physics; Mathematics; Structural engineering; Classical mechanics; Engineering; Computer science; Acoustics","score_opus":0.011383967679556468,"score_gpt":0.22582303433033793,"score_spread":0.21443906665078147,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2096155237","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":[0.034918636,0.00013906989,0.95915836,0.00011208435,0.000029448578,0.000040602623,0.000055642202,0.00016248206,0.0053836205],"genre_scores_gemma":[0.7531109,0.0003990184,0.23139364,0.000077410215,0.000016434735,0.00041545276,0.00014185075,0.000056830544,0.01438847],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99986064,0.000031013544,0.000006212607,0.000022604163,0.00006931778,0.0000101014775],"domain_scores_gemma":[0.99990153,0.000047185036,0.000014331881,0.0000121949715,0.000019431873,0.000005398229],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002936689,0.0003416722,0.00033634462,0.0002416854,0.00026356603,0.0004261169,0.00082980306,0.0010738387,0.0019127832],"category_scores_gemma":[0.0003422073,0.0002530999,0.00043021183,0.00019854945,0.00043932378,0.00046027824,0.0003439288,0.00046068162,0.00041813886],"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":[0.000021737014,0.000022167978,0.00031255494,0.00003879168,0.000010552896,0.000085137945,0.00008650647,0.9616504,0.021226933,0.0060072714,0.0001309168,0.010407114],"study_design_scores_gemma":[0.0000019291665,0.00001598432,0.00009802897,0.0000038057037,0.0000017691046,0.000012412515,0.000009371665,0.99786806,0.0010579509,0.00030899316,0.00061922346,0.0000024921762],"about_ca_topic_score_codex":0.001584326,"about_ca_topic_score_gemma":0.0019246077,"teacher_disagreement_score":0.0019127832,"about_ca_system_score_codex":0.00026654496,"about_ca_system_score_gemma":0.00046586097,"threshold_uncertainty_score":0.0063988566},"labels":[],"label_agreement":null},{"id":"W2096860513","doi":"10.1016/j.ijsolstr.2005.04.020","title":"A smart single-lap adhesive joint integrated with partially distributed piezoelectric patches","year":2005,"lang":"en","type":"article","venue":"International Journal of Solids and Structures","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":26,"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":"Piezoelectricity; Materials science; Joint (building); Adhesive; Finite element method; Stress (linguistics); Composite material; Bending; Piezoelectric sensor; Piezoelectric coefficient; Lap joint; Structural engineering; Layer (electronics); Engineering","score_opus":0.009596621844516297,"score_gpt":0.20582856472730884,"score_spread":0.19623194288279255,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2096860513","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":[0.83872676,0.0015994735,0.15310563,0.00018016597,0.00032138248,0.000035267836,0.00009649036,0.0011202026,0.004814606],"genre_scores_gemma":[0.94875455,0.00020453049,0.047625236,0.00004993823,0.00004875936,0.000015634641,0.000035591864,0.00002118104,0.003244653],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998678,0.0000125708875,0.0000065223994,0.000037956266,0.000054524528,0.000020670106],"domain_scores_gemma":[0.99984586,0.000020591426,0.00003091605,0.000033527765,0.00003274791,0.000036316695],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00011476571,0.0002712477,0.00046854353,0.00018595305,0.00016631339,0.00026191448,0.0007230789,0.00050737825,0.000995277],"category_scores_gemma":[0.00013924543,0.0002366612,0.00023340608,0.0001821117,0.0001786988,0.00034310107,0.00035453032,0.00019788719,0.00043908824],"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":[0.00008895489,0.0000321606,0.00045706047,0.00008253056,0.000018053022,0.0002570541,0.000025845116,0.0011261017,0.9792378,0.00032458757,0.0002917122,0.018058062],"study_design_scores_gemma":[0.00013844173,0.003014216,0.00999642,0.000023860606,0.00021636966,0.0038357181,0.0000867809,0.1201398,0.84964967,0.0005384242,0.012275461,0.00008480482],"about_ca_topic_score_codex":0.00013462962,"about_ca_topic_score_gemma":0.00033818104,"teacher_disagreement_score":0.000995277,"about_ca_system_score_codex":0.00008763093,"about_ca_system_score_gemma":0.00014006413,"threshold_uncertainty_score":0.0033295155},"labels":[],"label_agreement":null},{"id":"W2097074848","doi":"10.1115/1.1891816","title":"Damping Characteristics of Beams with Enhanced Self-Sensing Active Constrained Layer Treatments Under Various Boundary Conditions","year":2004,"lang":"en","type":"article","venue":"Journal of vibration and acoustics","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":6,"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":"Atomic Energy of Canada Limited; Chinese University of Hong Kong","keywords":"Constrained-layer damping; Cantilever; Beam (structure); Stiffness; Vibration control; Enhanced Data Rates for GSM Evolution; Vibration; Boundary value problem; Structural engineering; Materials science; Boundary (topology); Modal; Acoustics; Control theory (sociology); Physics; Engineering; Computer science; Mathematics; Mathematical analysis; Control (management); Composite material","score_opus":0.007485919665676937,"score_gpt":0.22245514135808944,"score_spread":0.2149692216924125,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2097074848","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":[0.96833193,0.00024221536,0.03060458,0.000020469332,0.000008499523,0.000011992148,0.000041154766,0.000048110207,0.000691095],"genre_scores_gemma":[0.98959804,0.0000986207,0.009698471,0.000012383742,0.000002374499,0.000024665784,0.000046930396,0.000010131674,0.0005083783],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99980766,0.000020475614,0.000008998353,0.000037761118,0.00010063755,0.00002454385],"domain_scores_gemma":[0.9996424,0.00015148947,0.00008212519,0.000042156986,0.000067503584,0.000014467561],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025850575,0.00028524015,0.00025464903,0.0002630918,0.00012392686,0.0002173398,0.00032206753,0.00031544894,0.000828379],"category_scores_gemma":[0.00047753804,0.00014260852,0.00018048364,0.00015147866,0.00037197856,0.00040784501,0.00024712682,0.00019670524,0.00014191087],"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":[0.0001443764,0.000024322522,0.0011109483,0.00006024407,0.000012895438,0.000040340634,0.00014249202,0.005637623,0.98481905,0.00042018795,0.00003903514,0.007548478],"study_design_scores_gemma":[0.000020961019,0.00038621222,0.006566193,0.000012479828,0.00002208642,0.00006315317,0.00013924917,0.08479805,0.906819,0.00024849927,0.0009013878,0.000022693594],"about_ca_topic_score_codex":0.00033868468,"about_ca_topic_score_gemma":0.00073609984,"teacher_disagreement_score":0.000828379,"about_ca_system_score_codex":0.00014393368,"about_ca_system_score_gemma":0.00008685026,"threshold_uncertainty_score":0.0027711987},"labels":[],"label_agreement":null},{"id":"W2099210588","doi":"10.1109/imtc.1997.610244","title":"Experimental validation of analytical models of flexible structures with bonded piezoelectric film actuators and sensors","year":2002,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"McMaster University","funders":"Canadian Space Agency","keywords":"Piezoelectricity; Cantilever; Poling; Materials science; Polyvinylidene fluoride; Actuator; Beam (structure); Finite element method; Vibration; Piezoelectric sensor; Structural engineering; Composite material; Acoustics; Ferroelectricity; Computer science; Optoelectronics; Physics; Engineering; Polymer","score_opus":0.01735806826328038,"score_gpt":0.21388248864302511,"score_spread":0.19652442037974474,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2099210588","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":[0.75246805,0.00035988903,0.2405348,0.0003089156,0.0001486418,0.00027855244,0.00038936967,0.000873428,0.00463839],"genre_scores_gemma":[0.9429792,0.00022234471,0.05418899,0.000034604975,0.000009247679,0.0003502311,0.00023474853,0.00006508792,0.0019156175],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99823546,0.00017541324,0.0000803314,0.0002198862,0.0011647843,0.00012413348],"domain_scores_gemma":[0.9975689,0.0009491677,0.00026633614,0.00054201164,0.00060184277,0.0000716901],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0016540666,0.000829709,0.0004075875,0.00040352406,0.000605333,0.00056671957,0.0021745616,0.001419935,0.0025982463],"category_scores_gemma":[0.005219608,0.00055877573,0.0004384767,0.00030611144,0.0010420182,0.0011079151,0.00086690154,0.001015569,0.0007523409],"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":[0.00028279354,0.00052405096,0.002212016,0.00034719254,0.000060053782,0.00054091203,0.00055688404,0.2641942,0.701517,0.0055069225,0.00066184363,0.023596212],"study_design_scores_gemma":[0.000057788653,0.0007670797,0.0016039811,0.000033953733,0.000023940569,0.00011147843,0.00010644825,0.5805004,0.4139271,0.0009986588,0.0018344332,0.000034685247],"about_ca_topic_score_codex":0.0014901529,"about_ca_topic_score_gemma":0.0015704101,"teacher_disagreement_score":0.0025982463,"about_ca_system_score_codex":0.00083204266,"about_ca_system_score_gemma":0.0005303308,"threshold_uncertainty_score":0.008747697},"labels":[],"label_agreement":null},{"id":"W2101269677","doi":"10.2514/1.12198","title":"Chebyshev Polynomials for Unsteady Aerodynamic Calculations in Aeroservoelasticity","year":2006,"lang":"en","type":"article","venue":"Journal of Aircraft","topic":"Aeroelasticity and Vibration Control","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":"Université du Québec à Montréal","funders":"National Aeronautics and Space Administration","keywords":"Aerodynamics; Chebyshev polynomials; Chebyshev filter; Mathematics; Applied mathematics; Computer science; Mathematical analysis; Physics; Mechanics","score_opus":0.005203104224118423,"score_gpt":0.20271760323257837,"score_spread":0.19751449900845994,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2101269677","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":[0.028676653,0.0010627366,0.9647404,0.00013224114,0.0000713008,0.00002689159,0.000036784924,0.00022929595,0.0050236345],"genre_scores_gemma":[0.5100022,0.0036031958,0.47276834,0.000080392216,0.00017730857,0.00021038762,0.00012946693,0.0004825468,0.012546137],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997414,0.00010316328,0.000009121548,0.000011137883,0.00011213689,0.000023021956],"domain_scores_gemma":[0.9993057,0.00046418273,0.00003583765,0.00006768969,0.00010215098,0.00002444498],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0007436792,0.00048135367,0.00045504427,0.0004894685,0.00034120103,0.000692096,0.00044154745,0.0005346745,0.0016686925],"category_scores_gemma":[0.002759724,0.00027403526,0.0003700201,0.00081470114,0.0005697202,0.00081271003,0.0004978589,0.0010802756,0.00091349974],"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":[0.000117548225,0.00008438202,0.00057389867,0.00018992256,0.000034149518,0.00023946277,0.00029976125,0.66594887,0.014454544,0.21800965,0.0018468073,0.09820109],"study_design_scores_gemma":[0.0000071014106,0.0000164491,0.00012366309,0.00001058945,0.000003102187,0.000022672108,0.000025150193,0.98471236,0.0011834477,0.011774082,0.0021141595,0.0000071972036],"about_ca_topic_score_codex":0.004249907,"about_ca_topic_score_gemma":0.0031107336,"teacher_disagreement_score":0.004249907,"about_ca_system_score_codex":0.00036742454,"about_ca_system_score_gemma":0.0006245248,"threshold_uncertainty_score":0.008450329},"labels":[],"label_agreement":null},{"id":"W2103090039","doi":"10.1109/iros.1998.724695","title":"Combined PD feedback and distributed piezoelectric-polymer vibration control of a single-link flexible manipulator","year":2002,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":16,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto","funders":"","keywords":"Control theory (sociology); Actuator; Vibration; Vibration control; SIGNAL (programming language); Angular velocity; Lyapunov stability; Computer science; Beam (structure); Engineering; Physics; Acoustics; Control (management); Structural engineering","score_opus":0.014585209309105136,"score_gpt":0.1836307745826992,"score_spread":0.16904556527359405,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2103090039","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":[0.25792167,0.0005941953,0.73614484,0.00018659545,0.00008214042,0.000047186546,0.000018496856,0.00039685966,0.0046080467],"genre_scores_gemma":[0.9579224,0.00012362492,0.039576493,0.000021448706,0.00002120994,0.000036372083,0.000007578305,0.000006328566,0.002284549],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99989617,0.000011675478,0.000005285017,0.000026753232,0.000050151117,0.000010004449],"domain_scores_gemma":[0.999902,0.00003747894,0.000023137896,0.000008691751,0.000019245463,0.000009501897],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015907062,0.0002903745,0.00020629085,0.00014015459,0.0001849238,0.00019863389,0.0003803705,0.00026920848,0.00076142704],"category_scores_gemma":[0.00025319523,0.00014148593,0.0001591125,0.00008055431,0.00027039976,0.0002778084,0.00030430534,0.00022618235,0.00010019232],"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":[0.000297587,0.00011685491,0.0007280581,0.00030224028,0.00004782289,0.00043335455,0.00015814902,0.20287897,0.5838461,0.006908071,0.00044808738,0.20383482],"study_design_scores_gemma":[0.00013618417,0.00103475,0.0010361795,0.000021723716,0.000033639226,0.00024667627,0.000023091123,0.9049332,0.086853914,0.0024737606,0.0031800133,0.00002682792],"about_ca_topic_score_codex":0.00038849973,"about_ca_topic_score_gemma":0.00070095225,"teacher_disagreement_score":0.00076142704,"about_ca_system_score_codex":0.00013688643,"about_ca_system_score_gemma":0.00020580577,"threshold_uncertainty_score":0.0025472045},"labels":[],"label_agreement":null},{"id":"W2103568751","doi":"10.1177/1045389x15572011","title":"Aeroelastic control of non-rotating and rotating wings using the dynamic stiffness modulation principle via piezoelectric actuators","year":2015,"lang":"en","type":"article","venue":"Journal of Intelligent Material Systems and Structures","topic":"Aeroelasticity and Vibration Control","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":"Carleton University","funders":"Conselho Nacional de Desenvolvimento Científico e Tecnológico","keywords":"Aeroelasticity; Helicopter rotor; Rotor (electric); Flutter; Control theory (sociology); Engineering; Stiffness; Vibration control; Actuator; Aerodynamics; Vibration; Structural engineering; Computer science; Physics; Acoustics; Aerospace engineering; Mechanical engineering; Control (management)","score_opus":0.012075874492750879,"score_gpt":0.243021998936501,"score_spread":0.23094612444375012,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2103568751","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":[0.8047905,0.0004348861,0.19086453,0.00007825838,0.000048750007,0.00004221232,0.000022236543,0.0001603268,0.0035583628],"genre_scores_gemma":[0.9851382,0.000102885075,0.013539249,0.000008188946,0.00000457824,0.000010992498,0.000008559888,0.0000051058373,0.0011822755],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99995863,0.0000046236237,0.0000024367203,0.000007066643,0.000022310387,0.000004953711],"domain_scores_gemma":[0.99992454,0.000034196368,0.000015346068,0.000009640654,0.0000117738045,0.000004468023],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00009261867,0.00015013789,0.000077543504,0.00009949284,0.00010029069,0.00014870896,0.00019119598,0.00010314962,0.0005058453],"category_scores_gemma":[0.00014888603,0.000089301895,0.000107441316,0.00005117384,0.00016599827,0.00014672367,0.00014476711,0.00011380614,0.000065193075],"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":[0.0000631002,0.00002946976,0.000316389,0.00004926458,0.0000050145413,0.000045287594,0.00003936944,0.0052287667,0.9575617,0.00056662294,0.0000601949,0.03603476],"study_design_scores_gemma":[0.00006403053,0.0008866116,0.0083009135,0.000016103146,0.000025506191,0.000297108,0.000056595352,0.24003713,0.7450801,0.0007027608,0.004512354,0.000020806352],"about_ca_topic_score_codex":0.00030373113,"about_ca_topic_score_gemma":0.00067648175,"teacher_disagreement_score":0.0005058453,"about_ca_system_score_codex":0.00007305177,"about_ca_system_score_gemma":0.00008644819,"threshold_uncertainty_score":0.0016921759},"labels":[],"label_agreement":null},{"id":"W2104954869","doi":"10.1109/robot.2005.1570124","title":"A High Authority Piezoelectric Stack Actuator for Structurally Flexible Mechanisms","year":2006,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Western University","funders":"","keywords":"Actuator; Control theory (sociology); Stack (abstract data type); Stiffness; Bending moment; Piezoelectricity; Vibration control; Vibration; Computer science; Bending; Engineering; Control engineering; Structural engineering; Control (management); Physics; Acoustics; Electrical engineering","score_opus":0.006389797846571767,"score_gpt":0.19738755454222287,"score_spread":0.1909977566956511,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2104954869","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":[0.37416932,0.0028912623,0.60600895,0.00030007525,0.00016164087,0.000090059155,0.00008840564,0.00044265387,0.01584762],"genre_scores_gemma":[0.943435,0.0005606315,0.05129883,0.000032501754,0.000027587907,0.00003174198,0.000032573033,0.000008808766,0.004572426],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999106,0.000009244983,0.0000037889733,0.000012143402,0.00005559557,0.000008601671],"domain_scores_gemma":[0.99994016,0.000014366318,0.000016146094,0.000007709283,0.000013747515,0.000008014414],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000119678094,0.00021713473,0.00013337244,0.00015117507,0.00020162013,0.00021720723,0.0003484134,0.0003103799,0.0011623629],"category_scores_gemma":[0.0001423755,0.000090814865,0.0001403556,0.00011212146,0.00022943581,0.00030697562,0.00026109745,0.00025242945,0.00024192424],"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":[0.00006331751,0.000025061634,0.0005081757,0.00022102066,0.000016475557,0.0002975049,0.00007401691,0.011971441,0.9140097,0.01298262,0.0003121801,0.059518564],"study_design_scores_gemma":[0.00011190715,0.002224257,0.00934932,0.00008058019,0.000099883066,0.0027323875,0.00014281238,0.27709913,0.63482046,0.00970745,0.06351138,0.00012042994],"about_ca_topic_score_codex":0.00021351,"about_ca_topic_score_gemma":0.00037900137,"teacher_disagreement_score":0.0011623629,"about_ca_system_score_codex":0.00008397746,"about_ca_system_score_gemma":0.0001759159,"threshold_uncertainty_score":0.0038884282},"labels":[],"label_agreement":null},{"id":"W2105742696","doi":"10.1017/s0001924000006977","title":"A hybrid fuzzy logic proportional-integral-derivative and conventional on-off controller for morphing wing actuation using shape memory alloy Part 1: Morphing system mechanisms and controller architecture design","year":2012,"lang":"en","type":"article","venue":"The Aeronautical Journal","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":68,"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; École de Technologie Supérieure","funders":"","keywords":"Morphing; Control theory (sociology); Controller (irrigation); Shape-memory alloy; Actuator; Fuzzy logic; Open-loop controller; Computer science; SMA*; Pneumatic actuator; Control engineering; Engineering; Artificial intelligence; Control (management)","score_opus":0.03784893466985908,"score_gpt":0.2440884487583815,"score_spread":0.20623951408852242,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2105742696","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":[0.08110816,0.0005515659,0.9002102,0.00012775397,0.0001915142,0.00021071627,0.00003997333,0.0012708139,0.016289284],"genre_scores_gemma":[0.92667484,0.00012947283,0.06686756,0.00011804858,0.00003712194,0.000120914185,0.000035279565,0.000019971543,0.0059967944],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997199,0.000025286226,0.00001628959,0.000065176326,0.00014731594,0.000025957514],"domain_scores_gemma":[0.9998838,0.000023639272,0.000013387853,0.00001339623,0.00005736933,0.000008534219],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025896536,0.0003715464,0.00028378514,0.00028419343,0.0003084348,0.0006718404,0.00096409227,0.0005131789,0.0016870695],"category_scores_gemma":[0.00028130764,0.00016164903,0.0003128448,0.00013242783,0.00025742408,0.00030449775,0.00027712932,0.0003621099,0.00027391015],"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":[0.0006940629,0.0003428367,0.0014863351,0.00045057404,0.00016213807,0.00047995866,0.00032894526,0.15650074,0.4184307,0.015238051,0.0024551617,0.40343046],"study_design_scores_gemma":[0.00009494995,0.0005505805,0.001297549,0.000035608406,0.00007691056,0.00024648113,0.00003291738,0.916524,0.07057268,0.0015044764,0.009026045,0.00003784297],"about_ca_topic_score_codex":0.002245501,"about_ca_topic_score_gemma":0.0023349994,"teacher_disagreement_score":0.002245501,"about_ca_system_score_codex":0.00039264225,"about_ca_system_score_gemma":0.00035531833,"threshold_uncertainty_score":0.0056438446},"labels":[],"label_agreement":null},{"id":"W2105940130","doi":"10.1177/1077546307081315","title":"Aeroservoelasticity Analysis Method Based on an Error Analytical Form Applied on a Business Aircraft","year":2008,"lang":"en","type":"article","venue":"Journal of Vibration and Control","topic":"Aeroelasticity and Vibration Control","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":"Bombardier (Canada); École de Technologie Supérieure","funders":"","keywords":"Aeroelasticity; Aerodynamics; Aerodynamic force; Flutter; Laplace transform; Mathematics; Control theory (sociology); Structural engineering; Computer science; Physics; Mechanics; Mathematical analysis; Engineering","score_opus":0.015066811751803867,"score_gpt":0.24879897911844964,"score_spread":0.2337321673666458,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2105940130","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":[0.011580437,0.00007004635,0.9866785,0.000041845655,0.000031052215,0.000017131972,0.000014972969,0.00019014387,0.0013758485],"genre_scores_gemma":[0.5009908,0.0002901455,0.49106407,0.000067105975,0.000052377945,0.0001297569,0.00010613137,0.00016521304,0.0071343025],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995646,0.00006455544,0.000016326032,0.00006155225,0.0002746356,0.000018252667],"domain_scores_gemma":[0.99936134,0.0002520546,0.00006375211,0.000062873914,0.00024371281,0.000016301541],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00040293092,0.000391481,0.00043452095,0.00057774415,0.0003525406,0.000498882,0.0004976599,0.0004847035,0.001543548],"category_scores_gemma":[0.0015622184,0.00015503913,0.0003764573,0.00038924653,0.00033697305,0.0004993784,0.00039383888,0.00065844704,0.00040847628],"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":[0.00021179201,0.00012107834,0.0038202542,0.0003540681,0.00007621444,0.0003180694,0.00040805372,0.39501727,0.11754542,0.047885098,0.0025705982,0.4316721],"study_design_scores_gemma":[0.000007962551,0.00004266473,0.00052264525,0.000007738455,0.0000061434243,0.00009993436,0.00002011662,0.9853359,0.010205147,0.0014581803,0.0022817203,0.000011821654],"about_ca_topic_score_codex":0.0025137006,"about_ca_topic_score_gemma":0.0015158195,"teacher_disagreement_score":0.0025137006,"about_ca_system_score_codex":0.00025294526,"about_ca_system_score_gemma":0.0005614073,"threshold_uncertainty_score":0.0051636696},"labels":[],"label_agreement":null},{"id":"W2109612976","doi":"10.1007/s00419-009-0344-8","title":"Modelling and dynamic stability of a hingeless active fibre composite blade","year":2009,"lang":"en","type":"article","venue":"Archive of Applied Mechanics","topic":"Aeroelasticity and Vibration Control","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":"Blade (archaeology); Smart material; Rotor (electric); Composite number; Helicopter rotor; Structural engineering; Vibration; Parametric statistics; Engineering; Turbine blade; Materials science; Mechanical engineering; Composite material; Acoustics; Physics; Turbine","score_opus":0.007630577487861772,"score_gpt":0.19049852464215267,"score_spread":0.1828679471542909,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2109612976","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":[0.7036094,0.00033143992,0.28175083,0.00019395415,0.00007539337,0.00004964906,0.000107941865,0.00028667136,0.0135946395],"genre_scores_gemma":[0.99398226,0.000049777773,0.0032802112,0.000005534103,0.0000055028104,0.000009185044,0.000021403335,0.000015009003,0.002631094],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99992585,0.000016868999,0.0000033496876,0.000014282971,0.000028222978,0.000011382329],"domain_scores_gemma":[0.99981016,0.00008158375,0.000033367687,0.000021006259,0.00003768293,0.000016295942],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00022247747,0.0004127194,0.00045071004,0.0003183053,0.00048419973,0.00060193025,0.00070505746,0.0013923715,0.0014025471],"category_scores_gemma":[0.0005550928,0.0003393107,0.00051248696,0.00016250892,0.0006538261,0.00044747515,0.00037885635,0.00036066826,0.00030156737],"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":[0.00005896666,0.000014839669,0.00029904014,0.000019968387,0.0000071027816,0.00012813283,0.000032953903,0.98739666,0.00869301,0.0014361116,0.00006054616,0.001852769],"study_design_scores_gemma":[0.0000024207543,0.000015837262,0.00019482255,0.0000013023606,0.0000015963385,0.000010779041,0.0000051091406,0.9991416,0.00039319563,0.00015983479,0.000071410046,0.000002195018],"about_ca_topic_score_codex":0.008539852,"about_ca_topic_score_gemma":0.00439858,"teacher_disagreement_score":0.008539852,"about_ca_system_score_codex":0.00043267253,"about_ca_system_score_gemma":0.0004535403,"threshold_uncertainty_score":0.01698029},"labels":[],"label_agreement":null},{"id":"W2111546371","doi":"10.2514/6.2004-1631","title":"Vibration Control of Box Structures Using Multiple Piezo-Actuators and Sensors","year":2004,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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; Institute for Christian Studies; University of Toronto","funders":"","keywords":"Actuator; Vibration; Vibration control; Acoustics; Active vibration control; Computer science; Control (management); Engineering; Control theory (sociology); Electrical engineering; Physics; Artificial intelligence","score_opus":0.00878987884059098,"score_gpt":0.20084958690347338,"score_spread":0.1920597080628824,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2111546371","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":[0.31795165,0.00034637138,0.6785165,0.00009691549,0.000065616594,0.00001834551,0.000032916403,0.00031924993,0.002652474],"genre_scores_gemma":[0.9672616,0.00013418969,0.030561332,0.000014279343,0.000017889672,0.000029117362,0.000020879232,0.000010281426,0.001950539],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99991834,0.000019025114,0.000004331942,0.000022240321,0.000026389354,0.000009775886],"domain_scores_gemma":[0.9998852,0.00005963302,0.000022843928,0.000008600952,0.000013954228,0.000009779199],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020482227,0.00036431281,0.00035191822,0.00009363136,0.00013716656,0.00022603833,0.00031933235,0.00031786892,0.00081516634],"category_scores_gemma":[0.0002608317,0.00021039542,0.00016322733,0.00008871734,0.00029166663,0.00038303263,0.0003762403,0.0002239914,0.00011674377],"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":[0.0005741661,0.0000760628,0.0011249509,0.00017590597,0.000056258057,0.00022765694,0.00013013165,0.5811274,0.32524034,0.010997446,0.0005500421,0.07971954],"study_design_scores_gemma":[0.000026876456,0.00019259106,0.0005769512,0.0000063524353,0.0000107658025,0.000027832748,0.00001061423,0.9834387,0.01313714,0.001930228,0.00063381577,0.000008164852],"about_ca_topic_score_codex":0.00054326095,"about_ca_topic_score_gemma":0.00086262135,"teacher_disagreement_score":0.00081516634,"about_ca_system_score_codex":0.00012737284,"about_ca_system_score_gemma":0.0001539264,"threshold_uncertainty_score":0.002726972},"labels":[],"label_agreement":null},{"id":"W2115264385","doi":"10.1177/1077546029202","title":"Enhanced Active Constrained Layer Damping Treatment for Broadband Vibration Suppression","year":2002,"lang":"en","type":"article","venue":"Journal of Vibration and Control","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":12,"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 Office; Atomic Energy of Canada Limited","keywords":"Constrained-layer damping; Vibration; Damping torque; Vibration control; Control theory (sociology); Broadband; Magnetic damping; Stiffness; Active vibration control; Noise (video); Enhanced Data Rates for GSM Evolution; Damping ratio; Engineering; Structural engineering; Acoustics; Physics; Computer science; Voltage; Control (management); Telecommunications","score_opus":0.017959559997804075,"score_gpt":0.23786008232735312,"score_spread":0.21990052232954904,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2115264385","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":[0.3281233,0.0008282785,0.65967554,0.0001399853,0.00007593628,0.000055019416,0.00005040648,0.0006755398,0.010375964],"genre_scores_gemma":[0.9195132,0.00018848029,0.077011056,0.00005905533,0.000015743532,0.000042371175,0.00003908411,0.000060049133,0.0030708045],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99990404,0.000015796624,0.0000039048855,0.000018255716,0.000040790783,0.000017202878],"domain_scores_gemma":[0.9998939,0.000031105217,0.000026669057,0.00001616681,0.000022544935,0.0000096122485],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00010372664,0.0004485678,0.00021698738,0.00023022667,0.00015528029,0.00024356077,0.00038758124,0.00032370051,0.0026689821],"category_scores_gemma":[0.00025528498,0.00012676133,0.00016650047,0.000111331385,0.00022869783,0.00048351134,0.00040621514,0.00023192754,0.00041519228],"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":[0.00012311303,0.000038899758,0.00020486901,0.00012281998,0.000013754274,0.00010497148,0.00005653257,0.009327106,0.9450161,0.004221905,0.00025327058,0.0405166],"study_design_scores_gemma":[0.000071331684,0.00064680685,0.00087312225,0.000033910237,0.00005019509,0.0003654565,0.00006418966,0.21334662,0.76981866,0.0022656852,0.012434518,0.000029434312],"about_ca_topic_score_codex":0.00013871852,"about_ca_topic_score_gemma":0.0003436566,"teacher_disagreement_score":0.0026689821,"about_ca_system_score_codex":0.000111455345,"about_ca_system_score_gemma":0.00010157684,"threshold_uncertainty_score":0.008928597},"labels":[],"label_agreement":null},{"id":"W2117761179","doi":"10.1177/0954410011408226","title":"On–off and proportional–integral controller for a morphing wing. Part 1: Actuation mechanism and control design","year":2011,"lang":"en","type":"article","venue":"Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":51,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"National Research Council Canada; École de Technologie Supérieure","funders":"Consortium de Recherche et d’innovation en Aérospatiale au Québec","keywords":"Control theory (sociology); Controller (irrigation); Actuator; Morphing; Open-loop controller; Engineering; Computer science; Control engineering; Electrical engineering","score_opus":0.01818589749089428,"score_gpt":0.18940955778549554,"score_spread":0.17122366029460126,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2117761179","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":[0.03319013,0.0007400934,0.9508288,0.0001701585,0.00020824728,0.00019592485,0.000038393577,0.0009690805,0.013659086],"genre_scores_gemma":[0.84508604,0.00040581182,0.14180742,0.00016560154,0.000110022964,0.0002298391,0.000079378544,0.000049213475,0.012066656],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.999801,0.000016982573,0.00000906183,0.000049515445,0.000111041576,0.000012344402],"domain_scores_gemma":[0.9999198,0.000017136554,0.000015169336,0.000010526628,0.00003204132,0.0000053860163],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001920802,0.00044225855,0.00018627923,0.00016912718,0.00019887113,0.00045668907,0.00054272346,0.000368276,0.0023407415],"category_scores_gemma":[0.00021754009,0.00014001633,0.00022482112,0.00008919254,0.00026273585,0.00025132284,0.0002075652,0.00043052327,0.00038888602],"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":[0.0003180138,0.00015081161,0.0007649517,0.0005356494,0.00007085575,0.00038035685,0.00023778029,0.091132544,0.56609464,0.014827446,0.002968189,0.32251877],"study_design_scores_gemma":[0.00009713275,0.0009182222,0.0022595827,0.000050211245,0.000076981356,0.0005169602,0.00003951008,0.84007233,0.11517798,0.0033166348,0.03743467,0.000039705214],"about_ca_topic_score_codex":0.0007643776,"about_ca_topic_score_gemma":0.0007709464,"teacher_disagreement_score":0.0023407415,"about_ca_system_score_codex":0.00027538964,"about_ca_system_score_gemma":0.00024769155,"threshold_uncertainty_score":0.00783056},"labels":[],"label_agreement":null},{"id":"W2124937491","doi":"10.1016/s0263-8231(00)00013-6","title":"Dynamic analysis of piezoceramic actuation effects on plate vibrations","year":2000,"lang":"en","type":"article","venue":"Thin-Walled Structures","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":16,"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 Laval","funders":"","keywords":"Vibration; Acoustics; Structural engineering; Materials science; Control theory (sociology); Physics; Computer science; Engineering; Control (management)","score_opus":0.003939057133834289,"score_gpt":0.2127114484615294,"score_spread":0.2087723913276951,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2124937491","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":[0.8841455,0.0005567427,0.09025056,0.00011255947,0.000036900343,0.000024678591,0.00006111564,0.00012718234,0.024684833],"genre_scores_gemma":[0.9962896,0.00011402749,0.0011451347,0.0000072411844,0.000005457474,0.0000065814393,0.000014665253,0.0000081034495,0.0024091497],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99995995,0.000004542658,0.0000010930061,0.0000057935267,0.000019542771,0.00000910139],"domain_scores_gemma":[0.99993575,0.000037243153,0.000007721867,0.000004568402,0.000010353173,0.000004336783],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000052693264,0.00021288167,0.00018801403,0.00019716905,0.00015089856,0.00022513798,0.00019498279,0.00020678021,0.002184067],"category_scores_gemma":[0.00029332694,0.00012576072,0.00014603333,0.000120557175,0.00030841626,0.00014234564,0.00017673148,0.00017922148,0.0001694274],"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":[0.00020547955,0.000053336895,0.0007354678,0.0001142476,0.000026309595,0.00046654625,0.000078641664,0.5254055,0.43287605,0.009002277,0.00023842628,0.030797554],"study_design_scores_gemma":[0.000007574308,0.00004246013,0.0031462284,0.00000540651,0.00000764142,0.00005888235,0.00002759539,0.96363884,0.03200072,0.0005873179,0.00046936303,0.000007934514],"about_ca_topic_score_codex":0.0011966913,"about_ca_topic_score_gemma":0.0008905746,"teacher_disagreement_score":0.002184067,"about_ca_system_score_codex":0.00017953927,"about_ca_system_score_gemma":0.00013843786,"threshold_uncertainty_score":0.007306397},"labels":[],"label_agreement":null},{"id":"W2124995604","doi":"10.1051/meca/2014078","title":"Bending nearfield compensation in the context of vibroacoustic active control","year":2014,"lang":"en","type":"article","venue":"Mechanics & Industry","topic":"Aeroelasticity and Vibration Control","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":"Université de Sherbrooke","funders":"","keywords":"Acoustics; Actuator; Context (archaeology); Bending; Compensation (psychology); Transfer function; Vibration; Acoustic radiation; Transducer; Noise (video); Infrasound; Stiffness; Radiation; Engineering; Physics; Structural engineering; Computer science; Optics; Electrical engineering","score_opus":0.011009004142351893,"score_gpt":0.2083779330215752,"score_spread":0.1973689288792233,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2124995604","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":[0.049271915,0.0011005925,0.9455072,0.00011374328,0.000070396374,0.000016321892,0.00001072082,0.00014555147,0.0037635344],"genre_scores_gemma":[0.919946,0.0005235134,0.07570481,0.0000521279,0.00007633058,0.000016539494,0.000031622145,0.0000288005,0.0036202436],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997837,0.000040505463,0.000007923897,0.00004992845,0.000098941244,0.000019056577],"domain_scores_gemma":[0.9998424,0.000068057154,0.000020396206,0.000019865462,0.000041373572,0.000007927598],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00019906466,0.00029261722,0.0002464527,0.00019461653,0.00014427734,0.0003580275,0.0003629738,0.0003557161,0.00078260194],"category_scores_gemma":[0.00047353056,0.0001057298,0.00012088895,0.00022008092,0.00037794223,0.00033820458,0.00031850048,0.0003169487,0.00014752528],"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":[0.00035360464,0.000075436976,0.00054418243,0.0002779453,0.00003334607,0.00020954937,0.00016040666,0.13280123,0.5786526,0.023080315,0.00061135925,0.26320004],"study_design_scores_gemma":[0.000012952777,0.00024959358,0.0016208398,0.000025494015,0.00003133665,0.00024011124,0.000035334022,0.8782567,0.10967892,0.0057326676,0.0040854835,0.000030496401],"about_ca_topic_score_codex":0.00045202728,"about_ca_topic_score_gemma":0.0005292981,"teacher_disagreement_score":0.00078260194,"about_ca_system_score_codex":0.0001594857,"about_ca_system_score_gemma":0.0001525001,"threshold_uncertainty_score":0.0026180744},"labels":[],"label_agreement":null},{"id":"W2125001838","doi":"10.2514/6.2002-5405","title":"Integrated Wing Design with Three Disciplines","year":2002,"lang":"en","type":"article","venue":"9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization","topic":"Aeroelasticity and Vibration Control","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":"National Research Council Canada","funders":"U.S. Department of Defense","keywords":"Wing; Computer science; Aerospace engineering; Engineering","score_opus":0.015503317566761887,"score_gpt":0.20803016827165882,"score_spread":0.19252685070489695,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2125001838","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":[0.021126764,0.00008074403,0.97200036,0.000028650866,0.00002129239,0.00007563306,0.000021392,0.00032942733,0.0063156467],"genre_scores_gemma":[0.34744385,0.00017016463,0.6460663,0.000056200624,0.000021173422,0.0003402587,0.00011686079,0.00012903598,0.0056561115],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99928457,0.000096995565,0.000027120588,0.00010029323,0.00040590303,0.00008517803],"domain_scores_gemma":[0.99974996,0.00005381239,0.00002246081,0.000057475663,0.000093255636,0.00002319221],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006566798,0.0005485767,0.0005414165,0.00047669417,0.00031774165,0.0008436598,0.00079899025,0.0006537249,0.0029357446],"category_scores_gemma":[0.0009225299,0.00040500256,0.0007739246,0.0003791293,0.00039858432,0.00065673323,0.0017895637,0.0009970085,0.0008535481],"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":[0.000249786,0.00027571525,0.0015455969,0.00026421927,0.00010858698,0.00014061906,0.00027807878,0.53180826,0.08635723,0.05186656,0.0008709451,0.3262344],"study_design_scores_gemma":[0.00008632653,0.0004843461,0.0007964549,0.000044636374,0.00006923816,0.000114133414,0.00005996013,0.92073613,0.038828544,0.018793954,0.019959416,0.000026843436],"about_ca_topic_score_codex":0.0006669918,"about_ca_topic_score_gemma":0.0008120218,"teacher_disagreement_score":0.0029357446,"about_ca_system_score_codex":0.0003714169,"about_ca_system_score_gemma":0.0010092552,"threshold_uncertainty_score":0.009820998},"labels":[],"label_agreement":null},{"id":"W2125813587","doi":"10.1017/s0001924000006989","title":"A hybrid fuzzy logic proportional-integral-derivative and conventional on-off controller for morphing wing actuation using shape memory alloy Part 2: Controller implementation and validation","year":2012,"lang":"en","type":"article","venue":"The Aeronautical Journal","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":56,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"National Research Council Canada; École de Technologie Supérieure","funders":"Consortium de Recherche et d’innovation en Aérospatiale au Québec","keywords":"PID controller; Actuator; Control theory (sociology); Computer science; Fuzzy logic; Test bench; Data acquisition; Controller (irrigation); Wind tunnel; Shape-memory alloy; MATLAB; Control engineering; Engineering; Temperature control; Embedded system","score_opus":0.04186361858211562,"score_gpt":0.2942646546717574,"score_spread":0.25240103608964176,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2125813587","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":[0.37021607,0.00032502515,0.61554074,0.00010775417,0.00020748115,0.0003421102,0.000098444005,0.0028680838,0.010294205],"genre_scores_gemma":[0.95032597,0.00004113955,0.0471366,0.000032575113,0.00000622426,0.0000992403,0.000027001237,0.000017123679,0.0023141142],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997049,0.000029813165,0.000016010705,0.000049257964,0.00017530144,0.000024785402],"domain_scores_gemma":[0.9997347,0.00008019459,0.000027655133,0.00004243906,0.00010263337,0.000012380862],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00043121164,0.00031678827,0.00027497538,0.00023914724,0.00021004306,0.0005309661,0.00090371975,0.00045159555,0.0017621834],"category_scores_gemma":[0.0005594747,0.00016271623,0.00025546757,0.00009078456,0.0002560416,0.00021955674,0.00025354503,0.0003005046,0.00022055903],"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":[0.001035895,0.00042192242,0.00203579,0.00063656457,0.00010978514,0.000419965,0.00028771293,0.22731052,0.530179,0.0040276786,0.0011297186,0.23240541],"study_design_scores_gemma":[0.00014930543,0.0008924865,0.0020806824,0.000027183743,0.00005085639,0.00014971208,0.000027006356,0.8300881,0.16164315,0.0004007997,0.004454284,0.000036495334],"about_ca_topic_score_codex":0.0018947275,"about_ca_topic_score_gemma":0.0016028305,"teacher_disagreement_score":0.0018947275,"about_ca_system_score_codex":0.0003189931,"about_ca_system_score_gemma":0.00030493698,"threshold_uncertainty_score":0.005895078},"labels":[],"label_agreement":null},{"id":"W2126723600","doi":"10.1243/09544100jaero63","title":"Aerodynamic forces based on an error analytical formulation for aeroservoelasticity studies on an F/A-18 aircraft","year":2006,"lang":"en","type":"article","venue":"Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering","topic":"Aeroelasticity and Vibration Control","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":"École de Technologie Supérieure","funders":"","keywords":"Laplace transform; Aerodynamic force; Convergence (economics); Aerodynamics; Applied mathematics; Mathematics; Function (biology); Domain (mathematical analysis); Frequency domain; Approximation error; Variable (mathematics); State variable; Mathematical analysis; Computer science; Physics; Mechanics","score_opus":0.020868780246358572,"score_gpt":0.25704579057230675,"score_spread":0.23617701032594818,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2126723600","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":[0.03393262,0.00021662106,0.96366894,0.00007968488,0.00005131554,0.000021006177,0.00002108435,0.00009526651,0.0019134763],"genre_scores_gemma":[0.7056315,0.0006698388,0.2868545,0.000054538817,0.000079502584,0.00011133104,0.00009623484,0.00010958934,0.006392921],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997992,0.000045194447,0.000008994107,0.000015811967,0.00012165934,0.000009138201],"domain_scores_gemma":[0.9997229,0.00011742027,0.000043878965,0.000022372958,0.00008715405,0.0000062678187],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003781536,0.00038483043,0.00029145452,0.0005234712,0.00023790481,0.0004218782,0.00035374248,0.00041797152,0.001153659],"category_scores_gemma":[0.0014323995,0.00013822825,0.00028674633,0.00030385508,0.00034520696,0.00046761657,0.00031465178,0.000566017,0.00020177648],"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":[0.00011183164,0.0000860067,0.002766687,0.00022226298,0.00003194703,0.00023293184,0.00021529716,0.7496497,0.039680142,0.052284177,0.0014163518,0.15330262],"study_design_scores_gemma":[0.000004635367,0.000037909715,0.0004610775,0.000010060404,0.000003487582,0.000045215227,0.000016788148,0.9934029,0.002737034,0.0016664416,0.0016071507,0.000007219171],"about_ca_topic_score_codex":0.002403788,"about_ca_topic_score_gemma":0.002024468,"teacher_disagreement_score":0.002403788,"about_ca_system_score_codex":0.00020295658,"about_ca_system_score_gemma":0.00040668395,"threshold_uncertainty_score":0.004779637},"labels":[],"label_agreement":null},{"id":"W2129074762","doi":"10.2514/2.2748","title":"Feedforward Piezoelectric Structural Control: An Application to Aircraft Cabin Noise Reduction","year":2001,"lang":"en","type":"article","venue":"Journal of Aircraft","topic":"Aeroelasticity and Vibration Control","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":false,"ca_institutions":"Bombardier (Canada); National Research Council Canada","funders":"","keywords":"Acoustics; Noise (video); Vibration; Actuator; Reduction (mathematics); Feed forward; Noise control; Noise reduction; Active noise control; Vibration control; Propeller; Controller (irrigation); Engineering; Piezoelectric sensor; Piezoelectricity; Control theory (sociology); Computer science; Physics; Control engineering; Electrical engineering; Control (management)","score_opus":0.005805182006945693,"score_gpt":0.22405051413342675,"score_spread":0.21824533212648106,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2129074762","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":[0.071310334,0.00033018357,0.92448,0.0001771863,0.0000548638,0.000043418433,0.000009099887,0.00040561252,0.0031892168],"genre_scores_gemma":[0.9161777,0.00025513844,0.08150945,0.000047294907,0.000026970141,0.000045082183,0.000009480076,0.000009479552,0.0019193239],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998965,0.00001816295,0.0000041475782,0.000015284542,0.00005460483,0.000011200695],"domain_scores_gemma":[0.999821,0.00010236675,0.000016522936,0.000009903702,0.000043757613,0.0000063942625],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00028245413,0.00038947575,0.00018813777,0.000117524956,0.00017895339,0.00019677183,0.00034792066,0.00038877816,0.0009385291],"category_scores_gemma":[0.0006068144,0.000119042874,0.00013893667,0.00008347662,0.00028762472,0.00015568784,0.00026514308,0.00027487444,0.000079613994],"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":[0.00022529849,0.00016505722,0.00067974936,0.00031497353,0.000026971424,0.00032291622,0.0001775008,0.3624349,0.27734894,0.0072883647,0.0004819116,0.3505334],"study_design_scores_gemma":[0.00003515844,0.0005787163,0.00070436485,0.00001782904,0.000020343894,0.00010358701,0.000020918556,0.9503841,0.044292286,0.002139749,0.0016909479,0.000011970124],"about_ca_topic_score_codex":0.0010018111,"about_ca_topic_score_gemma":0.0015219323,"teacher_disagreement_score":0.0010018111,"about_ca_system_score_codex":0.00014267856,"about_ca_system_score_gemma":0.00025813634,"threshold_uncertainty_score":0.0031397343},"labels":[],"label_agreement":null},{"id":"W2129544168","doi":"10.1109/robot.2004.1302548","title":"Active vibration control in a macro-manipulator using strengthened piezoelectric actuators","year":2004,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Western University","funders":"","keywords":"Actuator; Cantilever; Active vibration control; Vibration control; Vibration; Stiffness; Mechanism (biology); Bending moment; Beam (structure); Control theory (sociology); Bending; Piezoelectricity; Computer science; Engineering; Control (management); Structural engineering; Acoustics; Physics; Artificial intelligence; Electrical engineering","score_opus":0.009291931913097082,"score_gpt":0.20827091209728069,"score_spread":0.1989789801841836,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2129544168","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":[0.5310365,0.00037803428,0.46451405,0.000084715124,0.000040641098,0.000017080698,0.000011232219,0.00015882964,0.0037589187],"genre_scores_gemma":[0.98160326,0.00010251932,0.01695476,0.000008887445,0.0000072654566,0.00000955386,0.000004054474,0.0000033152016,0.0013063219],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999641,0.0000049268174,0.0000011924036,0.000008583735,0.000016478985,0.000004699732],"domain_scores_gemma":[0.99995685,0.000017892333,0.000009816033,0.000004421699,0.0000062229888,0.0000048269803],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0000770822,0.0001522528,0.00008354032,0.000060710485,0.00010977257,0.00013139927,0.0001720404,0.0001535394,0.0007401775],"category_scores_gemma":[0.00010231253,0.000067048946,0.00008916608,0.00003648915,0.00023300784,0.0001738333,0.00016284801,0.00014080894,0.000085639665],"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":[0.00012229645,0.000031325017,0.0005877111,0.00008249518,0.00001880244,0.0002598066,0.00009563413,0.06982613,0.8724471,0.008104773,0.00014897315,0.048274912],"study_design_scores_gemma":[0.000045631597,0.001126272,0.003732891,0.000016682267,0.00003003968,0.00021000225,0.00005823749,0.8844779,0.10222207,0.0034752667,0.0045814374,0.0000234836],"about_ca_topic_score_codex":0.00032429176,"about_ca_topic_score_gemma":0.0005788371,"teacher_disagreement_score":0.0007401775,"about_ca_system_score_codex":0.0000698354,"about_ca_system_score_gemma":0.000101003585,"threshold_uncertainty_score":0.0024760962},"labels":[],"label_agreement":null},{"id":"W2133896643","doi":"10.1177/1045389x06074679","title":"Compensation of Thermally Induced Distortion in Composite Structures using Macro-fiber Composites","year":2007,"lang":"en","type":"article","venue":"Journal of Intelligent Material Systems and Structures","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":33,"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 Laval","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Materials science; Composite number; Actuator; Finite element method; Composite material; Distortion (music); Piezoelectricity; Thermal; Composite plate; Deformation (meteorology); Voltage; Compensation (psychology); Fiber; Structural engineering; Engineering; Electrical engineering","score_opus":0.016091640119161775,"score_gpt":0.24259287748301414,"score_spread":0.22650123736385236,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2133896643","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":[0.9692462,0.00028503351,0.029147493,0.000039520877,0.000026332807,0.000008728681,0.000010712263,0.00012441662,0.0011115724],"genre_scores_gemma":[0.9897425,0.000082850784,0.009692244,0.000008459318,0.0000058645073,0.0000037652658,0.000010391058,0.000009109611,0.00044484242],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99991333,0.0000069427915,0.0000025616678,0.0000147081255,0.00004911633,0.000013423304],"domain_scores_gemma":[0.99984443,0.000038007827,0.00004955227,0.000018360639,0.000037144164,0.000012454867],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000097822616,0.00027620423,0.00013073126,0.00012717466,0.00015938249,0.000104803396,0.00015743761,0.00016571218,0.0003516816],"category_scores_gemma":[0.00028185316,0.00012899605,0.00012260032,0.00004928399,0.0001678266,0.0001648432,0.00011012915,0.00014179334,0.000108443666],"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":[0.00004613769,0.000009426474,0.00044038435,0.000018868497,0.0000034793738,0.000039585066,0.00002109308,0.0036497188,0.98850495,0.000104143386,0.000023427045,0.0071387053],"study_design_scores_gemma":[0.000011585602,0.00034624702,0.0058462494,0.00000609348,0.0000120326295,0.00022387797,0.000028796863,0.042733986,0.9494013,0.00010472975,0.0012729629,0.000012149645],"about_ca_topic_score_codex":0.0004172555,"about_ca_topic_score_gemma":0.001143248,"teacher_disagreement_score":0.0004172555,"about_ca_system_score_codex":0.00012554468,"about_ca_system_score_gemma":0.00014068816,"threshold_uncertainty_score":0.0011764169},"labels":[],"label_agreement":null},{"id":"W2136059142","doi":"10.2514/6.2007-1773","title":"Intelligent Identification System with Applications to Transient Aeroelastic Data","year":2007,"lang":"en","type":"article","venue":"48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference","topic":"Aeroelasticity and Vibration Control","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 Alberta","funders":"McGill University; Texas A and M University","keywords":"Aeroelasticity; Transient (computer programming); Identification (biology); Computer science; System identification; Control engineering; Aerodynamics; Aerospace engineering; Engineering; Data modeling; Database","score_opus":0.016516100496846393,"score_gpt":0.23984256045846214,"score_spread":0.22332645996161574,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2136059142","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":[0.01367016,0.00031843007,0.97979194,0.0002030617,0.00009271157,0.000067859255,0.00006303848,0.002894202,0.0028985278],"genre_scores_gemma":[0.63060665,0.00063399394,0.35850644,0.00025428087,0.00014488831,0.00029784066,0.00036821226,0.00013732344,0.009050371],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99956864,0.00008130837,0.000046787125,0.00012073597,0.00014377885,0.00003859785],"domain_scores_gemma":[0.9993593,0.0001900484,0.00007525838,0.000094599556,0.00025743977,0.000023272065],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00058724097,0.00055125676,0.00064338074,0.0007096258,0.0005888004,0.00080101157,0.0006060896,0.001146047,0.0021304484],"category_scores_gemma":[0.0018863704,0.00025929813,0.00033958608,0.0006771836,0.00037110585,0.00083058665,0.00066651014,0.0007002655,0.0008624101],"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":[0.00024547937,0.00016106594,0.003122065,0.00025179208,0.000055350374,0.0006039823,0.0005038721,0.30374178,0.037244067,0.01571185,0.0045394856,0.6338193],"study_design_scores_gemma":[0.000011595628,0.000055332788,0.00077063567,0.000012146135,0.000013022366,0.000093284594,0.000030243165,0.9860771,0.005687627,0.0024178224,0.004807396,0.00002381457],"about_ca_topic_score_codex":0.002720055,"about_ca_topic_score_gemma":0.0015415861,"teacher_disagreement_score":0.002720055,"about_ca_system_score_codex":0.00036544018,"about_ca_system_score_gemma":0.0006058369,"threshold_uncertainty_score":0.0071270466},"labels":[],"label_agreement":null},{"id":"W2137248862","doi":"10.1177/1045389x11409079","title":"Active sound control with smart foams using piezoelectric sensoriactuator","year":2011,"lang":"en","type":"article","venue":"Journal of Intelligent Material Systems and Structures","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":16,"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":"Natural Sciences and Engineering Research Council of Canada","keywords":"Active noise control; Actuator; Microphone; Noise control; Noise (video); Piezoelectricity; Smart material; Engineering; Electronic engineering; Computer science; Noise reduction; Materials science; Loudspeaker; Filter (signal processing); Electrical engineering","score_opus":0.017815326631526802,"score_gpt":0.2059620342030914,"score_spread":0.1881467075715646,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2137248862","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":[0.5335928,0.0007199827,0.4609891,0.00017427721,0.00009591991,0.00004723782,0.000034549284,0.0006575748,0.0036885815],"genre_scores_gemma":[0.958491,0.00009974762,0.040688884,0.000031343192,0.000010703455,0.00001777689,0.0000121879475,0.000009070374,0.00063927093],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99984515,0.00002358607,0.000009705085,0.000025202478,0.000082758146,0.00001366581],"domain_scores_gemma":[0.9998018,0.000078059864,0.000046009623,0.00001953912,0.00004221976,0.000012452508],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016941868,0.0002094479,0.00020257224,0.000157093,0.00011484003,0.0002166312,0.0004224702,0.00028504033,0.0005688136],"category_scores_gemma":[0.00040717737,0.00009555668,0.00012978604,0.00011832886,0.00028931722,0.00039593584,0.00031239178,0.00013626067,0.00007807164],"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":[0.00034411438,0.00005964934,0.0007062472,0.0001777914,0.000017749146,0.0001598127,0.00014236243,0.016368372,0.90743697,0.002794389,0.00023792183,0.071554594],"study_design_scores_gemma":[0.000101962745,0.001108764,0.0014547419,0.000031964224,0.00004618625,0.00036164382,0.0000607317,0.37106603,0.6187924,0.0014577819,0.00547732,0.000040484825],"about_ca_topic_score_codex":0.00024055224,"about_ca_topic_score_gemma":0.00033841,"teacher_disagreement_score":0.0005688136,"about_ca_system_score_codex":0.00012930232,"about_ca_system_score_gemma":0.00012200787,"threshold_uncertainty_score":0.0019028783},"labels":[],"label_agreement":null},{"id":"W2137726208","doi":"10.1088/0964-1726/14/5/035","title":"A novel smart adhesively bonded joint system","year":2005,"lang":"en","type":"article","venue":"Smart Materials and Structures","topic":"Aeroelasticity and Vibration Control","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":"Dalhousie University","funders":"","keywords":"Joint (building); Structural engineering; Materials science; Composite material; Smart material; Engineering; Computer science; Forensic engineering","score_opus":0.011019949496161897,"score_gpt":0.19096732582977113,"score_spread":0.17994737633360924,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2137726208","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":[0.11796152,0.0013106739,0.86645883,0.00016632857,0.0004063464,0.00014479169,0.00014128014,0.0034749343,0.009935253],"genre_scores_gemma":[0.62382865,0.0005350714,0.3625871,0.00018467238,0.00015926844,0.00019648748,0.00017531346,0.000088746565,0.012244626],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99957365,0.000038256203,0.000023359624,0.00012507186,0.00020561303,0.00003400579],"domain_scores_gemma":[0.9997849,0.000020168613,0.000034365374,0.00005514773,0.00007017391,0.00003527661],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021100172,0.00046536294,0.0005664776,0.00034126756,0.00035431643,0.00050737336,0.0011795195,0.0009453479,0.0033004766],"category_scores_gemma":[0.00039037436,0.0003540753,0.0002227077,0.00031732811,0.00028931943,0.00079977757,0.00087843987,0.00036327547,0.001971768],"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":[0.00010743112,0.000076979326,0.0006021637,0.0002316762,0.00004278775,0.00039085533,0.00014980823,0.016794732,0.8245645,0.010125523,0.0026815257,0.14423206],"study_design_scores_gemma":[0.00013547823,0.0018392709,0.0025878751,0.000050810057,0.00019179372,0.002767971,0.00008588105,0.5726049,0.3287754,0.005006487,0.08577353,0.00018061516],"about_ca_topic_score_codex":0.00036630695,"about_ca_topic_score_gemma":0.00047890877,"teacher_disagreement_score":0.0033004766,"about_ca_system_score_codex":0.0001655664,"about_ca_system_score_gemma":0.00036278836,"threshold_uncertainty_score":0.011041224},"labels":[],"label_agreement":null},{"id":"W2139223235","doi":"10.1109/robot.2002.1013587","title":"Optimizing the performance of piezoelectric actuators for active vibration control","year":2003,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Western University","funders":"","keywords":"Actuator; Controllability; Piezoelectricity; Cantilever; Materials science; Vibration; Beam (structure); Vibration control; Controllability Gramian; Acoustics; Piezoelectric accelerometer; Active vibration control; Control theory (sociology); PMUT; Structural engineering; Computer science; Engineering; Control (management); Composite material; Electrical engineering; Physics; Mathematics","score_opus":0.0067701801953779835,"score_gpt":0.1928385534995134,"score_spread":0.18606837330413542,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2139223235","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":[0.6007203,0.0017402915,0.39080983,0.00018355058,0.000047144953,0.00003595489,0.00003503014,0.00038963417,0.006038342],"genre_scores_gemma":[0.97520214,0.00027276523,0.02376865,0.000011695778,0.000011719382,0.000011877457,0.00001723602,0.00002469429,0.00067927176],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.999798,0.000028792474,0.000009528939,0.000033218403,0.00010609502,0.000024353869],"domain_scores_gemma":[0.9997621,0.00012809949,0.000044153,0.00001682917,0.00003977078,0.000009040365],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003110977,0.000424195,0.0001925375,0.00015408015,0.00013814551,0.00036477103,0.00025431637,0.0002814976,0.00081277854],"category_scores_gemma":[0.0009786652,0.00014004705,0.00009068471,0.000120476965,0.00017027995,0.00041864702,0.0001942174,0.00018189859,0.00024854697],"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":[0.000115387156,0.000042450913,0.0005117806,0.000104710314,0.000011526481,0.000050801373,0.000034856654,0.041577224,0.89198416,0.0010813716,0.00014208085,0.0643437],"study_design_scores_gemma":[0.000044641536,0.0008198961,0.0027412684,0.000019396419,0.000037618407,0.00018000888,0.000058978774,0.3968307,0.59462005,0.0013417371,0.003283418,0.00002231416],"about_ca_topic_score_codex":0.00016564346,"about_ca_topic_score_gemma":0.00025314357,"teacher_disagreement_score":0.00081277854,"about_ca_system_score_codex":0.0001149108,"about_ca_system_score_gemma":0.00015575317,"threshold_uncertainty_score":0.002718985},"labels":[],"label_agreement":null},{"id":"W2140180594","doi":"10.1007/s00707-009-0231-y","title":"The dynamic behaviour of surface-bonded piezoelectric actuators with debonded adhesive layers","year":2009,"lang":"en","type":"article","venue":"Acta Mechanica","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":27,"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 Alberta","funders":"","keywords":"Materials science; Actuator; Piezoelectricity; Adhesive; Solid mechanics; Composite material; Smart material; Stress (linguistics); Shear stress; Layer (electronics); Structural engineering; Computer science; Engineering","score_opus":0.004120586084469366,"score_gpt":0.19301898370028187,"score_spread":0.1888983976158125,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2140180594","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":[0.99707437,0.0004334822,0.0014304647,0.000035328165,0.000019430556,0.000004732616,0.000033069675,0.000020815629,0.00094837736],"genre_scores_gemma":[0.99768186,0.00022821376,0.0007821716,0.000018746241,0.0000071777536,0.000006669189,0.000055790664,0.0000104669225,0.0012088573],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99982256,0.000014786474,0.00000658322,0.000033548222,0.00008344967,0.000039184535],"domain_scores_gemma":[0.99966156,0.00016600935,0.00004166545,0.00002402773,0.00007082106,0.000035918925],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001710004,0.00026214935,0.00026282854,0.00020683245,0.00024996122,0.0003229161,0.00043246636,0.00045484476,0.0024364302],"category_scores_gemma":[0.00071411615,0.0003050853,0.0001605671,0.00016369009,0.0003848589,0.00041361054,0.00028257078,0.0003307803,0.00032159165],"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":[0.00018204267,0.000023339313,0.00025939915,0.00004428474,0.000011098958,0.000094224066,0.00007544808,0.0017141895,0.9941043,0.00015683153,0.000065396074,0.0032695169],"study_design_scores_gemma":[0.0000354343,0.00066443847,0.014272904,0.00002207244,0.000032204214,0.000224858,0.00020426884,0.053132106,0.92923146,0.00022104406,0.001924496,0.000034640478],"about_ca_topic_score_codex":0.0005805807,"about_ca_topic_score_gemma":0.0008193518,"teacher_disagreement_score":0.0024364302,"about_ca_system_score_codex":0.00022790614,"about_ca_system_score_gemma":0.00017692421,"threshold_uncertainty_score":0.008150697},"labels":[],"label_agreement":null},{"id":"W2141232744","doi":"10.1121/1.4781276","title":"Stability conditions in decentralized active vibration control of a flexible plate","year":2005,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aeroelasticity and Vibration Control","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":"Control theory (sociology); Convergence (economics); Actuator; Dissipative system; Stability (learning theory); Controller (irrigation); Transfer function; Decentralised system; Diagonal; Vibration; Transfer matrix; Vibration control; Computer science; Matrix (chemical analysis); Active vibration control; Harmonic; Linear-quadratic regulator; Mathematics; Control (management); Optimal control; Mathematical optimization; Physics; Engineering; Materials science; Acoustics","score_opus":0.01036266983371721,"score_gpt":0.23810713535079853,"score_spread":0.22774446551708133,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2141232744","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":[0.15510227,0.00024145393,0.83904296,0.00013034372,0.000027121425,0.000032728414,0.000031236224,0.0001937646,0.0051980927],"genre_scores_gemma":[0.9929597,0.0000651963,0.005817643,0.000010124313,0.000010241242,0.000038415303,0.000015568981,0.000014280934,0.0010689276],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996953,0.000072114875,0.000010297849,0.00006844011,0.0001230657,0.000030832194],"domain_scores_gemma":[0.9991597,0.0004388866,0.00013377743,0.000043494096,0.00020660405,0.000017496779],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006174669,0.00041693743,0.00035894528,0.00024287759,0.00028023717,0.0005330779,0.00034361993,0.00037736134,0.0014371504],"category_scores_gemma":[0.0018195923,0.0002185396,0.00028209752,0.00010777924,0.0008597919,0.0004681181,0.00047258724,0.0004324179,0.00023797447],"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":[0.00024976005,0.000040822557,0.00080303545,0.00020520126,0.000047418263,0.00029580676,0.00025351497,0.8332633,0.09856876,0.03331262,0.0005457332,0.032414068],"study_design_scores_gemma":[0.000019188843,0.00009307377,0.00048434385,0.0000068394743,0.000006241837,0.000032882584,0.000020315332,0.9899059,0.0052254116,0.0039436235,0.00025507066,0.0000072362254],"about_ca_topic_score_codex":0.0011520337,"about_ca_topic_score_gemma":0.00068895624,"teacher_disagreement_score":0.0014371504,"about_ca_system_score_codex":0.0003419961,"about_ca_system_score_gemma":0.0003235614,"threshold_uncertainty_score":0.0048077703},"labels":[],"label_agreement":null},{"id":"W2142902668","doi":"10.1121/1.2139624","title":"Decentralized harmonic active vibration control of a flexible plate using piezoelectric actuator-sensor pairs","year":2006,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":27,"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":"Control theory (sociology); Actuator; Decentralised system; Diagonal; Vibration; Stability (learning theory); Active vibration control; Weighting; Dissipative system; Vibration control; Computer science; Harmonic; Control (management); Mathematics; Physics; Acoustics","score_opus":0.010143559064893242,"score_gpt":0.22056753029198586,"score_spread":0.2104239712270926,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2142902668","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":[0.5970542,0.00010131138,0.40092024,0.00007782517,0.000035574154,0.000026941943,0.000013633969,0.000178731,0.0015915475],"genre_scores_gemma":[0.9908698,0.000016631451,0.008700017,0.0000046311206,0.000004882718,0.000009976202,0.0000041289854,0.0000025428312,0.00038747196],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998647,0.000025092173,0.0000043796117,0.00003731257,0.000051540967,0.000016958405],"domain_scores_gemma":[0.9997702,0.00008691041,0.000053473224,0.000029780105,0.000041997042,0.000017678369],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021857608,0.00038823573,0.00031655427,0.000100393445,0.00016368229,0.00020947226,0.00047200217,0.00019863104,0.00056056544],"category_scores_gemma":[0.00031986312,0.00015547556,0.00019564765,0.00008977569,0.00036478424,0.00029567452,0.00039481246,0.00028787545,0.00008674763],"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":[0.00035606822,0.0001531837,0.0012403161,0.00011603653,0.00005115606,0.00016276754,0.0001343125,0.33669648,0.5918976,0.0019085833,0.00020978643,0.06707373],"study_design_scores_gemma":[0.0000640767,0.00071056024,0.0019186877,0.0000046918367,0.000021879523,0.00005754957,0.000031260013,0.9071096,0.08860985,0.00096687314,0.00048684288,0.00001809405],"about_ca_topic_score_codex":0.00044923407,"about_ca_topic_score_gemma":0.0007021169,"teacher_disagreement_score":0.00056056544,"about_ca_system_score_codex":0.00012847042,"about_ca_system_score_gemma":0.00014672172,"threshold_uncertainty_score":0.0018752217},"labels":[],"label_agreement":null},{"id":"W2144033295","doi":"10.2514/6.2004-5373","title":"Aerodynamic Forces Formulation for Aircraft Aeroservoelasticity Studies","year":2004,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"École de Technologie Supérieure","funders":"National Aeronautics and Space Administration","keywords":"Aerodynamics; Aerospace engineering; Aerodynamic force; Aeronautics; Computer science; Engineering","score_opus":0.020481625196999892,"score_gpt":0.25871874536242306,"score_spread":0.23823712016542317,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2144033295","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":[0.007146645,0.003914371,0.91042,0.00075284654,0.0009175555,0.00017129749,0.00075467426,0.00023865432,0.07568387],"genre_scores_gemma":[0.27303746,0.009871351,0.52941525,0.0012324295,0.0029848753,0.0013811911,0.0021411004,0.0011143198,0.17882217],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99966395,0.00006269562,0.000022951976,0.00004223238,0.00019102028,0.000017147879],"domain_scores_gemma":[0.9997402,0.00005442567,0.000031684664,0.000029059873,0.00013284566,0.000011770803],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00046713382,0.0011692012,0.00049339473,0.0008929635,0.00057273544,0.00083799334,0.0008790793,0.00062089553,0.009358259],"category_scores_gemma":[0.00071376987,0.00019768614,0.0005248444,0.00050219573,0.00044328457,0.0009394013,0.0007081291,0.0012140324,0.0036314395],"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":[0.000024197381,0.00006796589,0.00042976355,0.00034786836,0.000030435469,0.0003862875,0.00028945217,0.08092775,0.024474278,0.7837979,0.019321663,0.08990248],"study_design_scores_gemma":[0.000021123577,0.00015889954,0.0014370847,0.00017242896,0.000025285397,0.00048211243,0.0001923664,0.40384537,0.005434934,0.27281108,0.3153743,0.000044913377],"about_ca_topic_score_codex":0.0019928226,"about_ca_topic_score_gemma":0.0019634098,"teacher_disagreement_score":0.009358259,"about_ca_system_score_codex":0.0004689662,"about_ca_system_score_gemma":0.00046524766,"threshold_uncertainty_score":0.031306505},"labels":[],"label_agreement":null},{"id":"W2146754038","doi":"10.1177/1045389x11411222","title":"Distributed Actuation Requirements of Piezoelectric Structures Under Servoconstraints","year":2011,"lang":"en","type":"article","venue":"Journal of Intelligent Material Systems and Structures","topic":"Aeroelasticity and Vibration Control","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":"University of Waterloo","funders":"","keywords":"Piezoelectricity; Actuator; Displacement (psychology); Control theory (sociology); Field (mathematics); Control engineering; Computer science; Engineering; Topology (electrical circuits); Mechanical engineering; Control (management); Mathematics; Electrical engineering; Pure mathematics","score_opus":0.028840135490898994,"score_gpt":0.23130236307231183,"score_spread":0.20246222758141283,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2146754038","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":[0.45081106,0.0003061209,0.53693455,0.00026553898,0.000023148652,0.000056957055,0.0001110757,0.00020234611,0.011289238],"genre_scores_gemma":[0.98962736,0.0000697601,0.009138783,0.000022096672,0.000011468019,0.000051506304,0.00007396106,0.000022513223,0.0009825787],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99925643,0.0000729261,0.000035725596,0.00010843866,0.00045513007,0.000071237846],"domain_scores_gemma":[0.9985998,0.0008328877,0.00019771689,0.000098047174,0.00022566802,0.000045781177],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005714894,0.00033111288,0.00032935326,0.00022215334,0.0003099201,0.0005027125,0.0005724587,0.00047341388,0.001349433],"category_scores_gemma":[0.0028151765,0.000194348,0.00023886329,0.00015665818,0.0005196121,0.0006924078,0.00053061853,0.00054587045,0.00016417669],"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":[0.000248019,0.000099885634,0.0014972824,0.00026088054,0.000020167245,0.00073291076,0.0004408968,0.37967953,0.5049461,0.066425234,0.0005597148,0.04508947],"study_design_scores_gemma":[0.000067517125,0.00037193167,0.0028854986,0.000020350846,0.000012061216,0.00034279886,0.00013147522,0.8963457,0.07061644,0.027269503,0.0019170891,0.000019694417],"about_ca_topic_score_codex":0.00041919408,"about_ca_topic_score_gemma":0.0004344986,"teacher_disagreement_score":0.001349433,"about_ca_system_score_codex":0.00038908108,"about_ca_system_score_gemma":0.00040389717,"threshold_uncertainty_score":0.004514277},"labels":[],"label_agreement":null},{"id":"W2149766359","doi":"10.1016/j.engfracmech.2011.06.014","title":"Analytical modelling of the electromechanical behaviour of surface-bonded piezoelectric actuators including the adhesive layer","year":2011,"lang":"en","type":"article","venue":"Engineering Fracture Mechanics","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":62,"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 Alberta","funders":"","keywords":"Materials science; Actuator; Adhesive; Piezoelectricity; Composite material; Layer (electronics); Stress (linguistics); Adhesive bonding; Shear stress; Deformation (meteorology); Shear (geology); Structural engineering; Computer science; Engineering","score_opus":0.03161466313298796,"score_gpt":0.20542270625215692,"score_spread":0.17380804311916895,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2149766359","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":[0.28318086,0.0014928324,0.66007346,0.0004457227,0.00013370074,0.00010913284,0.00025033843,0.00045797508,0.053856064],"genre_scores_gemma":[0.9702609,0.00059868395,0.014874175,0.00004364441,0.000026045369,0.00006926514,0.0000707757,0.000048453505,0.014008091],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999861,0.000022014776,0.00000513911,0.000019714824,0.0000735492,0.000018579167],"domain_scores_gemma":[0.9998412,0.00006898432,0.000019404757,0.000019795278,0.000043577504,0.0000069596585],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00019004094,0.0004275817,0.00046149918,0.0002548584,0.00025779865,0.00058042543,0.0010631988,0.0012797957,0.0020366092],"category_scores_gemma":[0.0007350028,0.00038836792,0.0004542161,0.0002842788,0.000535683,0.00050385523,0.00032228004,0.00042227795,0.000551835],"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":[0.00002977932,0.00003104697,0.00021926934,0.0000955539,0.000016854367,0.00018207301,0.000084845684,0.954328,0.031320762,0.005613632,0.0002495402,0.0078286305],"study_design_scores_gemma":[0.000002033265,0.000010994567,0.00012986019,0.0000034527645,0.0000031499033,0.000016932752,0.000006650988,0.9980533,0.0010624366,0.00042395477,0.0002843354,0.0000028006175],"about_ca_topic_score_codex":0.0034223527,"about_ca_topic_score_gemma":0.0028290313,"teacher_disagreement_score":0.0034223527,"about_ca_system_score_codex":0.00034188302,"about_ca_system_score_gemma":0.00049913215,"threshold_uncertainty_score":0.006813109},"labels":[],"label_agreement":null},{"id":"W2151834378","doi":"10.1007/s10999-011-9176-0","title":"Bio-inspired wing morphing for unmanned aerial vehicles using intelligent materials","year":2011,"lang":"en","type":"article","venue":"International Journal of Mechanics and Materials in Design","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":40,"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":"Biomimetics; Morphing; Actuator; Wing; Aerodynamics; Computer science; Servomotor; Adaptability; Mechanical engineering; Drone; Systems engineering; Engineering; Control engineering; Aerospace engineering; Simulation; Artificial intelligence","score_opus":0.06408526438484916,"score_gpt":0.2593776044744593,"score_spread":0.19529234008961013,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2151834378","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":[0.5484998,0.001813031,0.42524603,0.0004011951,0.000291064,0.000058450114,0.000048162172,0.0004840394,0.023158263],"genre_scores_gemma":[0.95094776,0.00021993727,0.04542655,0.00003419447,0.000011262876,0.000021511787,0.000016263892,0.000022201502,0.0033004675],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99997926,0.0000027496287,8.300298e-7,0.0000039523356,0.000010342432,0.0000028862291],"domain_scores_gemma":[0.9999732,0.000008514511,0.00000595087,0.0000046806394,0.0000048745082,0.000002720358],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00004865358,0.00015303062,0.0001304853,0.00015334437,0.00013990996,0.00023466571,0.00019348436,0.00027130486,0.0007665535],"category_scores_gemma":[0.00008165587,0.000099766454,0.00015629039,0.00008029516,0.00022398627,0.00025425942,0.00018488379,0.00013929032,0.000110927],"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":[0.00008385584,0.00009490338,0.00076507847,0.00014535492,0.000029779743,0.00021355583,0.000086230226,0.2993385,0.5894597,0.013113849,0.0008238028,0.09584544],"study_design_scores_gemma":[0.000016595675,0.00015753333,0.0009518836,0.000009319207,0.000012832657,0.000115436334,0.000038260634,0.9290144,0.061814863,0.003321646,0.0045312024,0.000016025106],"about_ca_topic_score_codex":0.00020929717,"about_ca_topic_score_gemma":0.00045056743,"teacher_disagreement_score":0.0007665535,"about_ca_system_score_codex":0.00012376637,"about_ca_system_score_gemma":0.000087614215,"threshold_uncertainty_score":0.0025643706},"labels":[],"label_agreement":null},{"id":"W2155630502","doi":"10.1017/s0001924000001962","title":"Method for aerodynamic unsteady forces time calculations on an F/A-18 aircraft","year":2008,"lang":"en","type":"article","venue":"The Aeronautical Journal","topic":"Aeroelasticity and Vibration Control","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":"École de Technologie Supérieure","funders":"National Aeronautics and Space Administration","keywords":"Laplace transform; Aerodynamic force; Aerodynamics; Flutter; Mach number; Mathematics; Aeroelasticity; Time domain; Frequency domain; Function (biology); Mathematical analysis; Applied mathematics; Mechanics; Computer science; Physics","score_opus":0.026004375277271716,"score_gpt":0.2836609364487432,"score_spread":0.25765656117147145,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2155630502","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":[0.0053229663,0.000036331316,0.9932181,0.00001849116,0.00003239659,0.000022605038,0.00003146892,0.00069502374,0.00062257244],"genre_scores_gemma":[0.08955494,0.00012541366,0.9041767,0.00003150574,0.000031303818,0.00017778375,0.00015472052,0.00037250912,0.0053751846],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99965525,0.00008107777,0.0000149064335,0.000030199853,0.00020306968,0.000015490958],"domain_scores_gemma":[0.999295,0.00029760544,0.000037623344,0.000068748486,0.00027982623,0.000021204589],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000408012,0.00047645342,0.00036378094,0.0005737588,0.00027446199,0.0003291988,0.00058112823,0.00039615823,0.0061400062],"category_scores_gemma":[0.0015311328,0.00022692974,0.00035430223,0.00027549808,0.00022462424,0.00035424583,0.00034592152,0.00071424275,0.0019715426],"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":[0.0003228805,0.0002345035,0.0015508215,0.0003735591,0.00016391197,0.0002121897,0.00026059535,0.17841165,0.091038465,0.0128369145,0.006455535,0.70813906],"study_design_scores_gemma":[0.00003323476,0.00009208217,0.00047895516,0.00001017146,0.000011947559,0.00012999892,0.000025597717,0.9716769,0.01682896,0.0012219776,0.009467198,0.00002291678],"about_ca_topic_score_codex":0.0020756985,"about_ca_topic_score_gemma":0.0021507402,"teacher_disagreement_score":0.0061400062,"about_ca_system_score_codex":0.00016716444,"about_ca_system_score_gemma":0.0006924846,"threshold_uncertainty_score":0.020540297},"labels":[],"label_agreement":null},{"id":"W2155968507","doi":"10.1177/1045389x04040901","title":"Vibration Control of Spacecraft Box Structures Using a Collocated Piezo-Actuator/Sensor","year":2004,"lang":"en","type":"article","venue":"Journal of Intelligent Material Systems and Structures","topic":"Aeroelasticity and Vibration Control","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":"Toronto Metropolitan University; University of Toronto","funders":"","keywords":"Actuator; Vibration; Vibration control; Active vibration control; Spacecraft; Engineering; Control theory (sociology); Bending; Smart material; Structural engineering; Control system; Acoustics; Computer science; Aerospace engineering; Physics; Materials science; Control (management); Electrical engineering","score_opus":0.01159679278856423,"score_gpt":0.2230159432293469,"score_spread":0.21141915044078266,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2155968507","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":[0.43558034,0.000177156,0.56089807,0.00011552535,0.000053998057,0.000018556646,0.000030841635,0.00025650763,0.00286909],"genre_scores_gemma":[0.9902395,0.00003246676,0.008979908,0.000008963551,0.0000063469274,0.000010386029,0.000010403854,0.000004754962,0.00070724386],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999361,0.000015601836,0.0000031049308,0.000017859911,0.000019891932,0.000007397572],"domain_scores_gemma":[0.99991107,0.000033988603,0.00002213282,0.000010850333,0.000014206036,0.000007736544],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017592985,0.0002856203,0.00020544895,0.00006925458,0.00014135122,0.00021462502,0.00024361305,0.0002772094,0.0007189473],"category_scores_gemma":[0.0002055432,0.00016368993,0.000139266,0.00006422564,0.00027070026,0.0001912516,0.00029454488,0.00021050277,0.000099339355],"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":[0.00048535396,0.00006880055,0.0010637066,0.00011931704,0.00004722562,0.00021271981,0.00017786663,0.67345834,0.26334667,0.0069696116,0.00066103565,0.053389423],"study_design_scores_gemma":[0.000022577544,0.0001693936,0.0005469438,0.0000035638473,0.0000084146905,0.000018838715,0.0000098897535,0.99011034,0.007998887,0.00070999097,0.00039611128,0.0000050742706],"about_ca_topic_score_codex":0.0010002533,"about_ca_topic_score_gemma":0.001214387,"teacher_disagreement_score":0.0010002533,"about_ca_system_score_codex":0.00014400025,"about_ca_system_score_gemma":0.00013988557,"threshold_uncertainty_score":0.002405107},"labels":[],"label_agreement":null},{"id":"W2163851121","doi":"10.1243/09544100jaero487","title":"Adaptive neuro-fuzzy controllers for an open-loop morphing wing system","year":2009,"lang":"en","type":"article","venue":"Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":31,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure","funders":"Natural Sciences and Engineering Research Council of Canada; Consortium de Recherche et d’innovation en Aérospatiale au Québec","keywords":"Airfoil; Morphing; Control theory (sociology); Adaptive neuro fuzzy inference system; Computer science; Wing; Controller (irrigation); Angle of attack; Lift (data mining); Control engineering; Fuzzy control system; Fuzzy logic; Engineering; Aerodynamics; Artificial intelligence; Aerospace engineering","score_opus":0.01827247253774382,"score_gpt":0.22023506704186827,"score_spread":0.20196259450412446,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2163851121","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":[0.07651001,0.00016515062,0.91564256,0.00011248531,0.00010470745,0.00014211505,0.00004080644,0.0010406867,0.0062414003],"genre_scores_gemma":[0.9129608,0.00003549437,0.08372012,0.00004729038,0.000018605178,0.00015015101,0.000030716557,0.000014588533,0.0030223115],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99976355,0.00004191078,0.000016314867,0.000049408263,0.00010573552,0.000023098142],"domain_scores_gemma":[0.99973434,0.00010044504,0.000032967324,0.000025243728,0.00009456901,0.000012311883],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00048627463,0.00040966607,0.0003369348,0.0002325234,0.00032088725,0.0005665851,0.0005887044,0.00048977893,0.0019714828],"category_scores_gemma":[0.0009176723,0.00015631021,0.0002704861,0.00013119896,0.00040598342,0.00024720412,0.0003323564,0.0005362332,0.0002608887],"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":[0.00036923966,0.00014231926,0.00089438056,0.00017088461,0.00006888887,0.0003173898,0.00024691893,0.7644016,0.056429535,0.008801912,0.00092479656,0.1672321],"study_design_scores_gemma":[0.000025001067,0.00008499913,0.0002547729,0.0000051742463,0.000008205484,0.000021519181,0.000006639683,0.9944318,0.0039426805,0.0004841031,0.0007291334,0.0000059334793],"about_ca_topic_score_codex":0.0041570864,"about_ca_topic_score_gemma":0.0034287733,"teacher_disagreement_score":0.0041570864,"about_ca_system_score_codex":0.00044252735,"about_ca_system_score_gemma":0.00042388088,"threshold_uncertainty_score":0.008265793},"labels":[],"label_agreement":null},{"id":"W2172238820","doi":"10.1177/0954410011408271","title":"On–off and proportional–integral controller for a morphing wing. Part 2: Control validation – numerical simulations and experimental tests","year":2011,"lang":"en","type":"article","venue":"Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":39,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"National Research Council Canada; École de Technologie Supérieure","funders":"Consortium de Recherche et d’innovation en Aérospatiale au Québec; École de technologie supérieure","keywords":"Airfoil; Actuator; Wind tunnel; Test bench; Data acquisition; Computer science; Control theory (sociology); Morphing; Controller (irrigation); Linear variable differential transformer; Simulation; Engineering; Transformer; Structural engineering; Mechanical engineering; Electrical engineering","score_opus":0.014874736958819006,"score_gpt":0.21417086088052595,"score_spread":0.19929612392170695,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2172238820","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":[0.6594201,0.000437583,0.31820166,0.00016249066,0.00023705115,0.0008076181,0.00038462266,0.0037284938,0.016620371],"genre_scores_gemma":[0.97612154,0.0000411119,0.021506594,0.00002722934,0.000005769789,0.00015595132,0.00009654248,0.000030862713,0.002014401],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997179,0.000030423034,0.000018619341,0.000042938842,0.00016206017,0.000027997788],"domain_scores_gemma":[0.99970144,0.000080339196,0.000038207385,0.00006767588,0.00009763411,0.000014684002],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00036098764,0.00044285337,0.00022168444,0.00023612996,0.00023637505,0.0003132071,0.0004838101,0.00035299812,0.0031221788],"category_scores_gemma":[0.0005980312,0.00012327085,0.00026353565,0.00009617373,0.0002681945,0.00022938945,0.00023088395,0.0003195757,0.0003188836],"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":[0.0011558558,0.0006022153,0.0036956659,0.0011633199,0.00008468423,0.0004112313,0.00034923002,0.24297671,0.58898085,0.0024198398,0.002301923,0.15585856],"study_design_scores_gemma":[0.00019989144,0.0018616898,0.0067840545,0.000039243343,0.00004902832,0.00016300855,0.00006206739,0.69171363,0.290509,0.0005214294,0.008055499,0.000041445597],"about_ca_topic_score_codex":0.0018245686,"about_ca_topic_score_gemma":0.0012496279,"teacher_disagreement_score":0.0031221788,"about_ca_system_score_codex":0.00027743756,"about_ca_system_score_gemma":0.00031256577,"threshold_uncertainty_score":0.01044476},"labels":[],"label_agreement":null},{"id":"W2174168317","doi":"10.1016/j.ultras.2015.11.004","title":"Coupled circuit based representation of piezoelectric structures modeled using the finite volume method","year":2015,"lang":"en","type":"article","venue":"Ultrasonics","topic":"Aeroelasticity and Vibration Control","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 Toronto","funders":"","keywords":"Finite volume method; Finite element method; Representation (politics); Volume (thermodynamics); Circuit extraction; Equivalent circuit; Computer science; Electronic circuit; RC circuit; Algorithm; Short circuit; Voltage; Mechanics; Electrical engineering; Physics; Engineering; Structural engineering","score_opus":0.04743040988959015,"score_gpt":0.2767712873258895,"score_spread":0.22934087743629936,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2174168317","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":[0.010886608,0.00015196514,0.9750279,0.00008844635,0.000049630475,0.000031880612,0.000095845506,0.00024753096,0.013420089],"genre_scores_gemma":[0.75760174,0.0006816562,0.20339024,0.00020737122,0.00008917641,0.00030160425,0.00038495194,0.00027848542,0.037064787],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99986637,0.00003300644,0.000004590865,0.000017870898,0.00006564121,0.000012425006],"domain_scores_gemma":[0.99985504,0.00006508228,0.000018645851,0.00001559297,0.00003563787,0.000010053598],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001846472,0.00040100404,0.00047903985,0.00043381608,0.00019985752,0.00070990884,0.0012428765,0.001410351,0.0053358357],"category_scores_gemma":[0.00047845067,0.0003637827,0.00047053277,0.00038025557,0.00040398785,0.0006750121,0.00041378877,0.00061780243,0.0009285812],"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":[0.000024763423,0.000038626673,0.0001430052,0.00006729022,0.000027418768,0.00013035483,0.00008143662,0.9128694,0.01116618,0.059102852,0.00074561476,0.015603053],"study_design_scores_gemma":[0.0000036897684,0.0000072071985,0.000028766997,0.0000032675323,0.000003097109,0.000018003988,0.000006475128,0.994964,0.00045849307,0.0034411848,0.0010625708,0.0000032544333],"about_ca_topic_score_codex":0.0022047877,"about_ca_topic_score_gemma":0.0024926034,"teacher_disagreement_score":0.0053358357,"about_ca_system_score_codex":0.00033516347,"about_ca_system_score_gemma":0.0005039244,"threshold_uncertainty_score":0.01785016},"labels":[],"label_agreement":null},{"id":"W2203988482","doi":"10.1017/s0001924000011131","title":"Design, numerical simulation and experimental testing of a controlled electrical actuation system in a real aircraft morphing wing model","year":2015,"lang":"en","type":"article","venue":"The Aeronautical Journal","topic":"Aeroelasticity and Vibration Control","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":"École de Technologie Supérieure","funders":"Consortium de Recherche et d’innovation en Aérospatiale au Québec; Università degli Studi di Napoli Federico II","keywords":"Morphing; Actuator; Wing; Aileron; Flight control surfaces; Rigidity (electromagnetism); Torque; Engineering; Structural engineering; Wind tunnel; Mechanism (biology); Mechanical engineering; Aerospace engineering; Computer science; Aerodynamics; Electrical engineering; Physics","score_opus":0.0617546517549101,"score_gpt":0.28153384202266213,"score_spread":0.21977919026775203,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2203988482","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":[0.7794796,0.00017806239,0.19966152,0.00020950186,0.000099461235,0.0004697578,0.00051949563,0.0014257393,0.01795683],"genre_scores_gemma":[0.9797847,0.000042850053,0.017529853,0.000015367199,0.0000025218958,0.00018690378,0.00009391644,0.000022095193,0.0023217213],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998627,0.00002256374,0.000008262912,0.00002553254,0.00005946188,0.000021536242],"domain_scores_gemma":[0.9997677,0.00008308014,0.00003388916,0.00004180429,0.000054187476,0.00001935718],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00027645848,0.00039771042,0.00033846972,0.00023825098,0.00030392432,0.00049541576,0.00066046795,0.0007353468,0.0035905407],"category_scores_gemma":[0.0004014701,0.00017271511,0.0003487045,0.000101172765,0.00046473416,0.00024108036,0.0002623256,0.00031272465,0.00033147197],"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":[0.00014420645,0.00009711728,0.0011297476,0.000154758,0.000018335857,0.00018273859,0.00009240098,0.9428187,0.047934886,0.0010499996,0.00020390337,0.00617315],"study_design_scores_gemma":[0.000039348488,0.00026587534,0.00073573773,0.000007953523,0.000011105261,0.00002198431,0.000026033993,0.9829692,0.0148383,0.00011584359,0.0009595253,0.000009153297],"about_ca_topic_score_codex":0.0028206273,"about_ca_topic_score_gemma":0.0018902798,"teacher_disagreement_score":0.0035905407,"about_ca_system_score_codex":0.00037531694,"about_ca_system_score_gemma":0.00049202197,"threshold_uncertainty_score":0.012011588},"labels":[],"label_agreement":null},{"id":"W2207015500","doi":"10.5589/q15-008","title":"Module discretization and consolidation of a modular morphing wing","year":2015,"lang":"en","type":"article","venue":"Canadian aeronautics and space journal","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":0,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Wing; Morphing; Discretization; Climb; Drag; Lift-to-drag ratio; Computer science; Engineering; Mathematics; Aerospace engineering; Control theory (sociology); Mathematical analysis; Artificial intelligence","score_opus":0.013241784610798323,"score_gpt":0.19197913591196097,"score_spread":0.17873735130116264,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2207015500","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":[0.32355773,0.00009423456,0.6702221,0.000039883616,0.00003207576,0.000078670164,0.000049894905,0.0003472236,0.005578202],"genre_scores_gemma":[0.8619885,0.0000436744,0.13669893,0.000015696027,0.000003659513,0.000045361947,0.000049485476,0.000034356657,0.0011202799],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999068,0.000016640366,0.000006540874,0.0000186487,0.000033116492,0.000018256653],"domain_scores_gemma":[0.9998776,0.000028368111,0.00002373685,0.00003624992,0.000024891098,0.000009110323],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024652132,0.0002527888,0.000228959,0.00023013602,0.00013632578,0.00033787166,0.000351384,0.00024673695,0.0008700129],"category_scores_gemma":[0.00035917276,0.00017515788,0.00033369398,0.00015573001,0.00027776125,0.00026933145,0.00042918455,0.0003215665,0.00014470264],"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":[0.000081209444,0.000058245812,0.0031999277,0.000086750675,0.000029946028,0.00016842673,0.00010628155,0.7309329,0.19710739,0.006814817,0.00031302404,0.061101142],"study_design_scores_gemma":[0.000014321047,0.00025625073,0.0019103384,0.000012585515,0.000017401848,0.000109170374,0.000030975883,0.9472821,0.04579377,0.0014829687,0.003077293,0.000012980961],"about_ca_topic_score_codex":0.0005981794,"about_ca_topic_score_gemma":0.0007137304,"teacher_disagreement_score":0.0008700129,"about_ca_system_score_codex":0.0001965397,"about_ca_system_score_gemma":0.00023193374,"threshold_uncertainty_score":0.0029104948},"labels":[],"label_agreement":null},{"id":"W2217865710","doi":"10.2514/1.c033252","title":"Design Segmented Stiff Skin for a Morphing Wing","year":2015,"lang":"en","type":"article","venue":"Journal of Aircraft","topic":"Aeroelasticity and Vibration Control","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":"Toronto Metropolitan University","funders":"","keywords":"Morphing; Wing; Airfoil; Wingspan; Chord (peer-to-peer); Segmentation; Computer science; Wing configuration; Wing twist; Angle of attack; Structural engineering; Aerodynamics; Artificial intelligence; Engineering; Aerospace engineering","score_opus":0.038037208299726885,"score_gpt":0.24321159122697408,"score_spread":0.2051743829272472,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2217865710","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":[0.026932765,0.00014940316,0.96825916,0.00004338974,0.00004185524,0.0000678444,0.00002196858,0.00036586882,0.0041177464],"genre_scores_gemma":[0.60526615,0.00018813345,0.390807,0.00005922586,0.000024047733,0.00012776241,0.00010020079,0.000094677685,0.0033328168],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99986553,0.000013482859,0.000008182167,0.000043479642,0.00004999439,0.00001934523],"domain_scores_gemma":[0.9999176,0.000012379397,0.000015554542,0.000013599595,0.000029780576,0.000011066066],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015012843,0.0006223002,0.00026972333,0.00042948945,0.0002646208,0.00040206395,0.00044429587,0.0004130918,0.0019601935],"category_scores_gemma":[0.00024162549,0.00019027918,0.00044830705,0.0001952883,0.00028975777,0.0004194887,0.00046336357,0.00025567348,0.0004617762],"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":[0.00011436101,0.000053448937,0.0016795022,0.00038013098,0.000048025224,0.000318918,0.00027944893,0.20034267,0.53596157,0.020110203,0.0018932106,0.23881851],"study_design_scores_gemma":[0.000026416705,0.00032280068,0.0010601192,0.000022600103,0.000040500923,0.00041816637,0.000069340706,0.9067146,0.0753994,0.004008525,0.011880866,0.00003666722],"about_ca_topic_score_codex":0.00072006497,"about_ca_topic_score_gemma":0.00057985703,"teacher_disagreement_score":0.0019601935,"about_ca_system_score_codex":0.00029574163,"about_ca_system_score_gemma":0.00031294202,"threshold_uncertainty_score":0.0065574646},"labels":[],"label_agreement":null},{"id":"W2233302968","doi":"10.82308/54738","title":"Active vibration and buckling control of piezoelectric smart structures","year":2013,"lang":"en","type":"article","venue":"eScholarship@McGill (McGill)","topic":"Aeroelasticity and Vibration Control","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":"McGill University","keywords":"Finite element method; Vibration; Active vibration control; Vibration control; Structural engineering; Beam (structure); Piezoelectric sensor; Timoshenko beam theory; Piezoelectricity; Shell (structure); Buckling; Hamilton's principle; Materials science; Cantilever; Engineering; Composite material; Acoustics; Physics","score_opus":0.006618045364533679,"score_gpt":0.18313310278329978,"score_spread":0.1765150574187661,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2233302968","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":[0.58761257,0.00064649736,0.38932082,0.00026066505,0.00010623932,0.000062711515,0.000063392676,0.00040359198,0.021523561],"genre_scores_gemma":[0.9848199,0.0001160876,0.0077782753,0.00003055706,0.000011354067,0.00002012615,0.000015814156,0.000010763746,0.007197232],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99996126,0.000004031373,0.0000016866177,0.000008289047,0.000019707797,0.0000051383554],"domain_scores_gemma":[0.9999441,0.0000225174,0.000010542598,0.000004639936,0.000012029019,0.0000061824135],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00009980109,0.00018257939,0.00015866087,0.00011141178,0.00012288908,0.00024855646,0.00024605426,0.00017672323,0.0021171838],"category_scores_gemma":[0.0001481242,0.00007470447,0.000107030864,0.00004574711,0.0002073759,0.00020091143,0.00024865623,0.00011042317,0.00018957256],"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":[0.00032372907,0.000091932845,0.0007673732,0.00022203385,0.000025424668,0.00015251717,0.00025705938,0.27830207,0.53602743,0.0106274,0.00077368977,0.17242934],"study_design_scores_gemma":[0.00002320818,0.00026011383,0.0010363881,0.000013494443,0.00000821889,0.000032539247,0.00003884523,0.9629962,0.030872282,0.0022987037,0.0024087382,0.00001135368],"about_ca_topic_score_codex":0.0004891598,"about_ca_topic_score_gemma":0.0010091268,"teacher_disagreement_score":0.0021171838,"about_ca_system_score_codex":0.00016060997,"about_ca_system_score_gemma":0.000116344585,"threshold_uncertainty_score":0.0070827007},"labels":[],"label_agreement":null},{"id":"W2240817763","doi":"10.4028/www.scientific.net/amm.798.582","title":"Actuation System Design for a Morphing Aileron","year":2015,"lang":"en","type":"article","venue":"Applied Mechanics and Materials","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":8,"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":"Consortium de Recherche et d’innovation en Aérospatiale au Québec","keywords":"Aileron; Morphing; Trailing edge; Engineering; Actuator; Aerodynamics; Mechanism (biology); Hinge; Mechanical engineering; Aerospace engineering; Computer science; Structural engineering","score_opus":0.0331741814673858,"score_gpt":0.20726288731741793,"score_spread":0.17408870585003214,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2240817763","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":[0.13052511,0.000525811,0.8455741,0.00015812035,0.00011694721,0.00022105001,0.00012186114,0.0010967661,0.021660186],"genre_scores_gemma":[0.88536096,0.00023346381,0.10152344,0.00007429486,0.000025757727,0.00018610357,0.00011870508,0.000043473858,0.012433852],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99990594,0.000010303615,0.000003972147,0.000033609114,0.000035938774,0.0000102504355],"domain_scores_gemma":[0.99996805,0.0000071434324,0.000007611777,0.0000038414546,0.000009789424,0.0000035120706],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00008212535,0.00027822505,0.00019855076,0.00013985434,0.00022453301,0.00034875184,0.00036597796,0.00035645408,0.0029244048],"category_scores_gemma":[0.00008985285,0.00010163119,0.00018066047,0.00007251588,0.00016842071,0.00020501217,0.00021305244,0.00019812449,0.00049396715],"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":[0.00018736695,0.000054434564,0.0009090087,0.00031839017,0.000037679016,0.0005726369,0.00021620891,0.16286653,0.71677,0.014493534,0.0011673261,0.10240691],"study_design_scores_gemma":[0.00005619751,0.0010703444,0.002558239,0.000036326357,0.000047184432,0.00070041686,0.000068110494,0.8526205,0.10182096,0.0018959228,0.039083682,0.00004214912],"about_ca_topic_score_codex":0.0005780044,"about_ca_topic_score_gemma":0.00078531634,"teacher_disagreement_score":0.0029244048,"about_ca_system_score_codex":0.00026310733,"about_ca_system_score_gemma":0.00028459093,"threshold_uncertainty_score":0.009783149},"labels":[],"label_agreement":null},{"id":"W2265412228","doi":"10.1017/s0001924000013300","title":"‘Smart spring’ identification for hovering rotor aeroelastic-stability augmentation","year":2003,"lang":"en","type":"article","venue":"The Aeronautical Journal","topic":"Aeroelasticity and Vibration Control","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":"Carleton University","funders":"","keywords":"Aeroelasticity; Control theory (sociology); Spring (device); Helicopter rotor; Modal; Structural engineering; Stiffness; Rotor (electric); Smart material; Controller (irrigation); Aerodynamics; Cantilever; Computer science; Engineering; Mechanical engineering; Aerospace engineering; Materials science; Artificial intelligence","score_opus":0.019788136532122858,"score_gpt":0.2314772449558309,"score_spread":0.21168910842370806,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2265412228","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":[0.027366001,0.00008593017,0.97006845,0.000038069877,0.000022260687,0.000032506265,0.0000217512,0.00025328185,0.0021117353],"genre_scores_gemma":[0.92863643,0.00008813659,0.0674382,0.000039270264,0.000018113582,0.000084620566,0.000059554022,0.000033056425,0.00360262],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.999835,0.000045446235,0.000008924859,0.00004275117,0.000050770643,0.000016996435],"domain_scores_gemma":[0.9997389,0.00010211079,0.00004747203,0.000039931485,0.00006120332,0.000010337421],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00033843194,0.00062890176,0.0004674902,0.0002753508,0.0001693778,0.0004489881,0.00037917504,0.000618528,0.0018653787],"category_scores_gemma":[0.0005375156,0.00021533754,0.00035265472,0.00012478657,0.0004249794,0.0003465733,0.0005363963,0.00040412572,0.000473501],"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":[0.0002688172,0.000102066246,0.0010472471,0.00036768123,0.000096245705,0.00021766427,0.00018489089,0.6611895,0.16424643,0.015728164,0.0012575879,0.15529364],"study_design_scores_gemma":[0.000005068785,0.000063940024,0.0002323026,0.0000057815396,0.00000499712,0.00001350801,0.000006212449,0.99490815,0.0031447078,0.0008730589,0.0007376509,0.0000046397045],"about_ca_topic_score_codex":0.00078258256,"about_ca_topic_score_gemma":0.0009572219,"teacher_disagreement_score":0.0018653787,"about_ca_system_score_codex":0.00017995335,"about_ca_system_score_gemma":0.00024031935,"threshold_uncertainty_score":0.006240368},"labels":[],"label_agreement":null},{"id":"W2267999761","doi":"10.1177/0954410015588573","title":"Design and wind tunnel experimental validation of a controlled new rotary actuation system for a morphing wing application","year":2015,"lang":"en","type":"article","venue":"Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":29,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure","funders":"Beijing Institute of Technology; Technische Universiteit Delft; Canada Research Chairs; National University of Singapore; University of Notre Dame","keywords":"Airfoil; Morphing; Wing; Wind tunnel; Actuator; Controller (irrigation); Angle of attack; Control theory (sociology); Flow (mathematics); Position (finance); Computer science; Flow control (data); Aerodynamics; Computational fluid dynamics; Simulation; Engineering; Structural engineering; Aerospace engineering; Mechanics; Control (management); Physics; Artificial intelligence","score_opus":0.01942749760644243,"score_gpt":0.2136392248933855,"score_spread":0.19421172728694305,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2267999761","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":[0.90377325,0.00020055269,0.09089043,0.00014468584,0.00015447415,0.0010406522,0.00035847127,0.0008957933,0.0025416776],"genre_scores_gemma":[0.9665155,0.00007847926,0.031165715,0.000029861973,0.000013292215,0.0003689208,0.00013446496,0.000034100514,0.0016597756],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9995484,0.000058689056,0.00003837282,0.000086717206,0.00021365851,0.000054219112],"domain_scores_gemma":[0.99917585,0.00018880382,0.00013854173,0.00015450569,0.00026724182,0.00007499848],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0008557991,0.00051552604,0.00030037572,0.00031232266,0.00031022134,0.00037133959,0.0006828233,0.00062352646,0.0018805079],"category_scores_gemma":[0.0009176715,0.00021550473,0.00024443617,0.00011524945,0.0004888573,0.00033225375,0.00036052492,0.00043277748,0.00030945655],"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":[0.00036321877,0.00042210694,0.0013705348,0.00046612247,0.000024555164,0.00020743677,0.00022233481,0.0070360084,0.97068685,0.0003961017,0.00037942533,0.018425299],"study_design_scores_gemma":[0.00032699492,0.008352051,0.012224497,0.000045858586,0.000043119162,0.00029612044,0.00009672683,0.052208785,0.9195721,0.000095954696,0.00668194,0.00005590415],"about_ca_topic_score_codex":0.0005575707,"about_ca_topic_score_gemma":0.00048460418,"teacher_disagreement_score":0.0018805079,"about_ca_system_score_codex":0.00022650628,"about_ca_system_score_gemma":0.00041701132,"threshold_uncertainty_score":0.0062909126},"labels":[],"label_agreement":null},{"id":"W2274237557","doi":"","title":"Experimental Studies on Active Noise Control Using Smart Structures","year":2003,"lang":"ko","type":"article","venue":"PolyU Institutional Research Archive (Hong Kong Polytechnic University)","topic":"Aeroelasticity and Vibration Control","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 British Columbia","funders":"","keywords":"Loudspeaker; Acoustics; Vibration; Actuator; Noise (video); Active noise control; Vibration control; Engineering; Piezoelectricity; Noise control; Active vibration control; Control system; Noise floor; Smart material; Computer science; Noise measurement; Noise reduction; Materials science; Electrical engineering; Physics","score_opus":0.06530157642961952,"score_gpt":0.31650172651449027,"score_spread":0.25120015008487073,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2274237557","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":[0.9720908,0.00013209642,0.025720742,0.000052849326,0.00004650515,0.00007395945,0.000063428626,0.000100488585,0.0017192825],"genre_scores_gemma":[0.992576,0.00008311096,0.006460675,0.000009688355,0.000007008332,0.000057690737,0.0000380904,0.0000074406134,0.0007603687],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99943084,0.00008499613,0.000046752484,0.000099329416,0.00026222004,0.00007587802],"domain_scores_gemma":[0.99880755,0.0004924239,0.00017517147,0.00015919395,0.00030111158,0.00006457623],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006270237,0.00043006832,0.00038316209,0.00035448215,0.00036291443,0.00028423595,0.0004758548,0.00046873785,0.0013617176],"category_scores_gemma":[0.0014768007,0.00017664018,0.00025096702,0.00016686443,0.0006654248,0.00037192556,0.00037322554,0.00023450846,0.00014691225],"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":[0.0008331128,0.00095257774,0.0012777314,0.00039186617,0.000032223074,0.00015996893,0.0003223972,0.036820333,0.9400351,0.0011682819,0.00017744931,0.017828932],"study_design_scores_gemma":[0.00022144434,0.010185197,0.005818576,0.00004755754,0.00006964368,0.00014410868,0.000258188,0.09983043,0.88011605,0.0007786378,0.0024719208,0.000058140937],"about_ca_topic_score_codex":0.00071690296,"about_ca_topic_score_gemma":0.00069349376,"teacher_disagreement_score":0.0013617176,"about_ca_system_score_codex":0.00019348768,"about_ca_system_score_gemma":0.00019073076,"threshold_uncertainty_score":0.004555404},"labels":[],"label_agreement":null},{"id":"W2306296840","doi":"10.1017/aer.2016.6","title":"Drag optimisation of a wing equipped with a morphing upper surface","year":2016,"lang":"en","type":"article","venue":"The Aeronautical Journal","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":42,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure; Université du Québec à Montréal","funders":"","keywords":"Airfoil; Drag coefficient; Morphing; Aerodynamics; Wing; Drag; Lift-to-drag ratio; Swept wing; Solver; Zero-lift drag coefficient; Aerospace engineering; Lift coefficient; Angle of attack; Structural engineering; Reynolds number; Mechanics; Lift-induced drag; Computer science; Mathematics; Turbulence; Physics; Engineering; Mathematical optimization; Artificial intelligence","score_opus":0.010223762633470202,"score_gpt":0.20181495983575815,"score_spread":0.19159119720228796,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2306296840","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":[0.97214895,0.000058352434,0.024542734,0.00003725648,0.00002022027,0.00002179943,0.0000640438,0.00019650308,0.0029102007],"genre_scores_gemma":[0.99289906,0.000018884284,0.006344374,0.0000049238542,0.0000010474257,0.000009387296,0.000041413434,0.00001855502,0.0006623522],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.999933,0.000010006774,0.0000027942174,0.000010219107,0.000025514886,0.000018478771],"domain_scores_gemma":[0.99989617,0.000031591568,0.000013390189,0.000024066532,0.000020821652,0.000013899991],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000162056,0.00030396925,0.00040012083,0.0002449179,0.00018278354,0.00042737045,0.00030032502,0.00045006818,0.0011395388],"category_scores_gemma":[0.00026953028,0.00017573668,0.0004340159,0.00013718512,0.00025534167,0.00016656207,0.00030436218,0.00025094024,0.00014854045],"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":[0.0002671972,0.000105185994,0.0017743066,0.000088320594,0.000030407466,0.00020565647,0.00007318655,0.7961954,0.18719372,0.00061162375,0.000210895,0.013244079],"study_design_scores_gemma":[0.000026621767,0.00037195333,0.0019796256,0.000006362173,0.000016816692,0.000027255503,0.000020938314,0.95647967,0.04034497,0.0000820167,0.0006305647,0.000013241167],"about_ca_topic_score_codex":0.0025646666,"about_ca_topic_score_gemma":0.0015078872,"teacher_disagreement_score":0.0025646666,"about_ca_system_score_codex":0.00023965945,"about_ca_system_score_gemma":0.0002604011,"threshold_uncertainty_score":0.0050994754},"labels":[],"label_agreement":null},{"id":"W2312663217","doi":"10.2514/6.2001-1361","title":"Design and testing of an adaptive RPV aeroelastic demonstrator","year":2001,"lang":"en","type":"article","venue":"19th AIAA Applied Aerodynamics Conference","topic":"Aeroelasticity and Vibration Control","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 Victoria","funders":"","keywords":"Aeroelasticity; Computer science; Aerospace engineering; Engineering; Aerodynamics","score_opus":0.024947201235374483,"score_gpt":0.2032510557310564,"score_spread":0.17830385449568192,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2312663217","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":[0.6758837,0.0002519077,0.30700734,0.0005152472,0.0001972773,0.00057295803,0.0003406855,0.0034153392,0.011815666],"genre_scores_gemma":[0.9401082,0.000055640096,0.050806195,0.00008149422,0.000019485165,0.0002757713,0.00018574594,0.000112276306,0.0083552245],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9993813,0.0001055434,0.000029430126,0.00013224556,0.0002715921,0.000079805824],"domain_scores_gemma":[0.99899465,0.00019147091,0.00013382257,0.00021739247,0.0003019301,0.00016074491],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0009382028,0.00043772417,0.00051488914,0.00020213041,0.0004968579,0.00051288254,0.002098233,0.0014458604,0.0038202768],"category_scores_gemma":[0.0012175477,0.00027689055,0.00025498332,0.000097909324,0.00039683824,0.00075327203,0.00085057947,0.0006601501,0.0013392402],"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":[0.00094928296,0.00036768612,0.00289988,0.00047619347,0.00009282776,0.00068924716,0.00041786677,0.024453755,0.90221804,0.0015267406,0.0013049063,0.06460362],"study_design_scores_gemma":[0.0005160283,0.011154831,0.010051682,0.000054910684,0.000109918874,0.001338103,0.00028116305,0.1389606,0.80140007,0.00058134715,0.035461728,0.0000896144],"about_ca_topic_score_codex":0.00033000513,"about_ca_topic_score_gemma":0.00029253773,"teacher_disagreement_score":0.0038202768,"about_ca_system_score_codex":0.00018392131,"about_ca_system_score_gemma":0.00040217437,"threshold_uncertainty_score":0.01278007},"labels":[],"label_agreement":null},{"id":"W2315346151","doi":"10.2514/6.2003-1722","title":"Active Robust Shape Control of Flexible Structures","year":2003,"lang":"en","type":"article","venue":"44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference","topic":"Aeroelasticity and Vibration Control","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":"Canadian Space Agency","funders":"","keywords":"Computer science; Control (management); Artificial intelligence","score_opus":0.01126674467590601,"score_gpt":0.20756789443393503,"score_spread":0.196301149758029,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2315346151","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":[0.03760297,0.000418231,0.9570087,0.00009790663,0.000050445044,0.000014975828,0.000019042907,0.0005482731,0.004239521],"genre_scores_gemma":[0.9581218,0.00029750977,0.038178578,0.00005069253,0.000039003546,0.000039046423,0.00004690278,0.00004434344,0.0031821507],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99971884,0.000032135766,0.000010095278,0.00005112953,0.00016545111,0.0000222825],"domain_scores_gemma":[0.9996902,0.000095603835,0.000070905335,0.000055578865,0.00007302729,0.000014685447],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00031549105,0.00044151867,0.0003049329,0.00029998933,0.00018390536,0.00050827785,0.00064249075,0.00049747946,0.0010160112],"category_scores_gemma":[0.0007277736,0.00018724457,0.0003902633,0.00017717575,0.0007273552,0.0005724516,0.00065964286,0.00046226548,0.0002486112],"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":[0.00018889239,0.000038483817,0.00023148235,0.00012107549,0.00004897643,0.00015471001,0.000113780916,0.628104,0.15774076,0.03944257,0.00078894576,0.17302638],"study_design_scores_gemma":[0.000020913996,0.00014404011,0.00018817984,0.0000061265955,0.000007967849,0.000047828165,0.000011174893,0.9636785,0.023463938,0.009586922,0.0028306958,0.000013746165],"about_ca_topic_score_codex":0.00063938973,"about_ca_topic_score_gemma":0.0005473462,"teacher_disagreement_score":0.0010160112,"about_ca_system_score_codex":0.00029000707,"about_ca_system_score_gemma":0.00017957215,"threshold_uncertainty_score":0.0033989549},"labels":[],"label_agreement":null},{"id":"W2315654202","doi":"10.2514/6.2002-1481","title":"Method Validation for Aeroservoelastic Analysis","year":2002,"lang":"en","type":"article","venue":"43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference","topic":"Aeroelasticity and Vibration Control","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":"École de Technologie Supérieure","funders":"Langley Research Center","keywords":"Computer science","score_opus":0.0160034353066242,"score_gpt":0.23557569065794184,"score_spread":0.21957225535131764,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2315654202","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":[0.01427084,0.00018796057,0.98149157,0.00007060288,0.00007055434,0.00015922732,0.00013803242,0.001458879,0.002152295],"genre_scores_gemma":[0.36671767,0.00023922005,0.6278353,0.00009449816,0.000021369613,0.0008764257,0.0005061681,0.0009098266,0.002799581],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9967319,0.0012737759,0.00017929419,0.0002712474,0.0014374586,0.000106370724],"domain_scores_gemma":[0.9882578,0.0063743275,0.00042276003,0.0017117667,0.0031452219,0.0000879673],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0050145388,0.0008963665,0.0006465153,0.0010507245,0.00083285564,0.0010844122,0.0014237019,0.0013973789,0.008201381],"category_scores_gemma":[0.023978684,0.0003843049,0.0005687987,0.0003997914,0.00067299616,0.0009504284,0.0014952893,0.00095567276,0.001402517],"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":[0.0010685517,0.00048738404,0.007595224,0.0019017264,0.0003676718,0.0007145021,0.00092568784,0.4102965,0.09488959,0.030913288,0.0056103105,0.44522953],"study_design_scores_gemma":[0.00011923718,0.00022115478,0.0014228362,0.00018058169,0.000031544547,0.00025010272,0.00016013152,0.93043846,0.04941723,0.0059155035,0.0117998505,0.000043469827],"about_ca_topic_score_codex":0.002694428,"about_ca_topic_score_gemma":0.0013930477,"teacher_disagreement_score":0.008201381,"about_ca_system_score_codex":0.00040556275,"about_ca_system_score_gemma":0.0012367659,"threshold_uncertainty_score":0.027436376},"labels":[],"label_agreement":null},{"id":"W2316923778","doi":"10.2514/6.2016-0082","title":"The Influence of Control Surface Faults on Flexible Aircraft","year":2016,"lang":"en","type":"article","venue":"AIAA Guidance, Navigation, and Control Conference","topic":"Aeroelasticity and Vibration Control","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":"University of Toronto","funders":"","keywords":"Control (management); Surface (topology); Aerospace engineering; Computer science; Materials science; Automotive engineering; Engineering; Artificial intelligence","score_opus":0.006287469769828964,"score_gpt":0.20703821758433055,"score_spread":0.20075074781450158,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2316923778","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":[0.99416006,0.000110211084,0.0024378079,0.00009182943,0.00003768766,0.0000039137517,0.000045337118,0.000042278716,0.0030709063],"genre_scores_gemma":[0.99977,0.000015499978,0.00004434125,0.000002314668,0.0000034605018,3.9464146e-7,0.000010360957,0.000003873575,0.0001498528],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99978906,0.000041630767,0.0000064651977,0.000023210154,0.000053868716,0.000085803535],"domain_scores_gemma":[0.9971929,0.0019827113,0.00018890432,0.00012355256,0.00036009468,0.00015184419],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00027108533,0.00034251346,0.00032406088,0.000422317,0.000401482,0.00061383774,0.00023942307,0.0006598652,0.002240188],"category_scores_gemma":[0.0047869617,0.00014224564,0.00025926996,0.00022336651,0.0007119132,0.0004247366,0.00027530064,0.00035788963,0.00014894779],"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":[0.0036158005,0.00025149135,0.019400429,0.00011263115,0.000089833185,0.0021222671,0.00014610178,0.9057577,0.036350872,0.0026023563,0.0011341319,0.028416393],"study_design_scores_gemma":[0.000064303276,0.00048281788,0.06179829,0.000009969469,0.00006536769,0.00022946426,0.0002398576,0.9255021,0.009968818,0.0013256287,0.00028700574,0.000026336784],"about_ca_topic_score_codex":0.010415262,"about_ca_topic_score_gemma":0.0051852195,"teacher_disagreement_score":0.010415262,"about_ca_system_score_codex":0.0004930092,"about_ca_system_score_gemma":0.00023843597,"threshold_uncertainty_score":0.020709276},"labels":[],"label_agreement":null},{"id":"W2318164419","doi":"10.2514/6.2015-2497","title":"A New Method for Tuning PI Gains for Position Control of BLDC Motor Based Wing Morphing Actuators","year":2015,"lang":"en","type":"article","venue":"AIAA Modeling and Simulation Technologies Conference","topic":"Aeroelasticity and Vibration Control","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":"Université du Québec","funders":"National Research Council Canada; Deutsches Zentrum für Luft- und Raumfahrt; Natural Sciences and Engineering Research Council of Canada; Consortium de Recherche et d’innovation en Aérospatiale au Québec","keywords":"Morphing; Actuator; Control theory (sociology); Wing; Position (finance); Computer science; DC motor; Control engineering; Control (management); Engineering; Aerospace engineering; Electrical engineering; Artificial intelligence","score_opus":0.06276308924209548,"score_gpt":0.30358472205221415,"score_spread":0.24082163281011867,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2318164419","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":[0.0021964852,0.00006615801,0.99592763,0.00001498332,0.00003439372,0.000030572264,0.000008379981,0.0003307443,0.0013905382],"genre_scores_gemma":[0.38992584,0.00022774562,0.60271657,0.00008075227,0.000059163747,0.0002622395,0.00007767366,0.00012346375,0.006526563],"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997086,0.00003424517,0.000018576937,0.000080710626,0.00014026332,0.000017560369],"domain_scores_gemma":[0.99979216,0.000051073825,0.000031818912,0.00003471882,0.000082392864,0.000007855375],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00029077037,0.0006469073,0.000416198,0.00034626748,0.0004328464,0.0005734712,0.0006376809,0.00041611155,0.0032403343],"category_scores_gemma":[0.0006840918,0.00024088206,0.0002779843,0.0002552134,0.00027887625,0.0003686856,0.0003330539,0.00067453017,0.0007550828],"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":[0.00019209873,0.00011607424,0.00051422406,0.00068218866,0.00007145434,0.00019111673,0.00034753978,0.05949769,0.25706455,0.014694093,0.0024754466,0.6641536],"study_design_scores_gemma":[0.00008939825,0.00047000454,0.0011795602,0.00005721652,0.0000745633,0.0004727107,0.00005799911,0.86893797,0.09459112,0.0032469819,0.030773487,0.000049004564],"about_ca_topic_score_codex":0.0010434168,"about_ca_topic_score_gemma":0.0013857498,"teacher_disagreement_score":0.0032403343,"about_ca_system_score_codex":0.00025998012,"about_ca_system_score_gemma":0.00031007853,"threshold_uncertainty_score":0.010840058},"labels":[],"label_agreement":null},{"id":"W2318925169","doi":"10.2514/6.2002-1625","title":"Active Robust Vibration Control of a Circular Plate Structure Using Piezoelectric Actuators","year":2002,"lang":"en","type":"article","venue":"43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference","topic":"Aeroelasticity and Vibration Control","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 Space Agency","funders":"","keywords":"Vibration control; Actuator; Piezoelectricity; Vibration; Active vibration control; Control theory (sociology); Robust control; Piezoelectric sensor; Acoustics; Materials science; Computer science; Structural engineering; Engineering; Physics; Control (management); Control system; Electrical engineering; Artificial intelligence","score_opus":0.01310603224851672,"score_gpt":0.19409886500160584,"score_spread":0.1809928327530891,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2318925169","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":[0.21177405,0.00027916027,0.78223455,0.00016456279,0.0000600449,0.000031680658,0.000025561336,0.00039723283,0.005033183],"genre_scores_gemma":[0.9802799,0.00007936624,0.01798671,0.000018504,0.000011141448,0.00002466392,0.000016692422,0.0000074928157,0.0015755236],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99989283,0.000012643606,0.000004728636,0.000029046298,0.000049915427,0.0000107327205],"domain_scores_gemma":[0.9998754,0.000047183083,0.000030299725,0.000014349833,0.000024984607,0.0000076983215],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018742676,0.0004119437,0.00018002835,0.00012969796,0.00015256366,0.00027173435,0.00051553367,0.00035251188,0.0006954727],"category_scores_gemma":[0.00032439225,0.00015934632,0.00021264007,0.00008631631,0.00048378264,0.00025779472,0.00031926233,0.00025627727,0.00012515693],"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":[0.00028016872,0.00009224633,0.00047989763,0.00014211304,0.00006089939,0.0002871874,0.00012470505,0.39704427,0.5104749,0.01013293,0.00049268355,0.08038791],"study_design_scores_gemma":[0.000028796265,0.00023015722,0.00039358344,0.000005871993,0.000015650661,0.00004408394,0.000012499732,0.9597622,0.037785176,0.0009732073,0.0007382055,0.00001050443],"about_ca_topic_score_codex":0.0010074591,"about_ca_topic_score_gemma":0.0009461868,"teacher_disagreement_score":0.0010074591,"about_ca_system_score_codex":0.0001805611,"about_ca_system_score_gemma":0.00025451917,"threshold_uncertainty_score":0.002326548},"labels":[],"label_agreement":null},{"id":"W2319322669","doi":"10.2514/6.2015-0904","title":"Systemic modeling and design approach for morphing wing aileron controller using Matlab/Simulink","year":2015,"lang":"en","type":"article","venue":"AIAA Modeling and Simulation Technologies Conference","topic":"Aeroelasticity and Vibration Control","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":"École de Technologie Supérieure","funders":"","keywords":"Aileron; Morphing; MATLAB; Computer science; Wing; Elevator; Controller (irrigation); Control engineering; Simulation; Engineering; Aerospace engineering; Computer graphics (images)","score_opus":0.12751498247957604,"score_gpt":0.26737440020812087,"score_spread":0.13985941772854482,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2319322669","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":[0.0059953607,0.00009805374,0.9797609,0.000055067198,0.000036833997,0.00008686086,0.000037599402,0.00072118465,0.01320814],"genre_scores_gemma":[0.7833597,0.0003589446,0.190933,0.00011846879,0.00003888606,0.000524548,0.00020861595,0.0001821765,0.024275787],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998031,0.0000319146,0.000010549368,0.000038608636,0.00010101065,0.000014682891],"domain_scores_gemma":[0.9998914,0.000017130478,0.00001547471,0.000011820193,0.00006013183,0.000004108171],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025091344,0.00056361087,0.00042657572,0.00029224085,0.00044779753,0.0006239016,0.0006506999,0.0004549404,0.005098628],"category_scores_gemma":[0.00023594631,0.00023562956,0.0004664822,0.00012476681,0.00018780532,0.00035267574,0.0005301046,0.00054058706,0.0009537665],"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":[0.000093057584,0.000068704496,0.0007923621,0.00037814621,0.00005724785,0.00025590532,0.00023527893,0.82421356,0.043138698,0.021404471,0.0022024545,0.10716017],"study_design_scores_gemma":[0.000015356838,0.000108834574,0.00025033348,0.000014048443,0.000020592763,0.000056984005,0.000021403326,0.9854945,0.0065822885,0.0012421655,0.0061855493,0.000007975195],"about_ca_topic_score_codex":0.0032653396,"about_ca_topic_score_gemma":0.0034870629,"teacher_disagreement_score":0.005098628,"about_ca_system_score_codex":0.00027966118,"about_ca_system_score_gemma":0.0006102799,"threshold_uncertainty_score":0.017056644},"labels":[],"label_agreement":null},{"id":"W2320448628","doi":"10.2514/6.2016-1082","title":"Self-adaptive morphing wing model, smart actuated and controlled by using a multiloop controller based on a laminar flow real time optimizer","year":2016,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Université du Québec","funders":"Consortium de Recherche et d’innovation en Aérospatiale au Québec","keywords":"Morphing; Computer science; Laminar flow; Control theory (sociology); Controller (irrigation); Flow (mathematics); Wing; Control engineering; Engineering; Aerospace engineering; Artificial intelligence; Control (management); Mathematics","score_opus":0.01023696561733592,"score_gpt":0.19792789711911984,"score_spread":0.18769093150178393,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2320448628","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":[0.30818263,0.00013312987,0.68047476,0.00008016222,0.000046107634,0.0001852052,0.00025036436,0.0023023179,0.0083452575],"genre_scores_gemma":[0.95051646,0.000041514053,0.046239633,0.000015253388,0.0000048768757,0.0001301425,0.00012999553,0.00002951177,0.002892598],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999403,0.000005980235,0.0000026148768,0.000017468266,0.00002684197,0.000006823731],"domain_scores_gemma":[0.9999467,0.000010596169,0.000012038094,0.000011640801,0.000013034293,0.000005992297],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00009486024,0.00023332487,0.00019855113,0.00017153965,0.00017925943,0.00030084373,0.00047839322,0.0002565594,0.0013748228],"category_scores_gemma":[0.00010873961,0.000111639994,0.0002489302,0.00007492821,0.0002266668,0.00017622701,0.0002542429,0.00020705977,0.00017750429],"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":[0.00026687566,0.00011432055,0.0017827072,0.00014963916,0.00003944443,0.00015767709,0.00011790629,0.77944404,0.17382754,0.0038146104,0.0006319643,0.039653286],"study_design_scores_gemma":[0.000018437186,0.00012416157,0.0007502269,0.0000026861417,0.000009067544,0.00003427065,0.000008277363,0.9849118,0.012324482,0.0002991331,0.0015094187,0.00000806358],"about_ca_topic_score_codex":0.0018474408,"about_ca_topic_score_gemma":0.0015609463,"teacher_disagreement_score":0.0018474408,"about_ca_system_score_codex":0.00018320161,"about_ca_system_score_gemma":0.0003091434,"threshold_uncertainty_score":0.0045992136},"labels":[],"label_agreement":null},{"id":"W2321672834","doi":"10.2514/6.2011-1884","title":"Wing Line Discretization for the Development of a Modular Morphing Wing","year":2011,"lang":"en","type":"article","venue":"52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference","topic":"Aeroelasticity and Vibration Control","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":"Wing; Morphing; Modular design; Discretization; Computer science; Line (geometry); Wing twist; Structural engineering; Aerospace engineering; Engineering; Computer graphics (images); Mathematics; Geometry; Aerodynamics","score_opus":0.023872139598021265,"score_gpt":0.22022065207033525,"score_spread":0.196348512472314,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2321672834","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":[0.007085806,0.000034033088,0.99108803,0.000015048365,0.000012132822,0.000025553274,0.000020851065,0.00018170594,0.001536778],"genre_scores_gemma":[0.17916295,0.00007407733,0.81911504,0.000025502895,0.000009424946,0.00009932202,0.00008080601,0.000088390574,0.0013444262],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99982905,0.00003913445,0.000011274516,0.00003075494,0.00007518677,0.00001444853],"domain_scores_gemma":[0.99968565,0.00014614275,0.000035915404,0.000054822765,0.00006486475,0.000012760607],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003682321,0.00033106047,0.0002914384,0.0002879103,0.00020596164,0.00033354165,0.0006080588,0.0003865311,0.002371948],"category_scores_gemma":[0.0008816948,0.00019218792,0.0004281001,0.00020237376,0.0002703,0.00033020592,0.00043268778,0.00062680413,0.00064134214],"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":[0.000098818105,0.00006411002,0.0019300724,0.00017504212,0.000034860434,0.00018655648,0.00025159234,0.7053671,0.06627845,0.02585043,0.0013799428,0.19838296],"study_design_scores_gemma":[0.00000970815,0.000040577706,0.00014414941,0.000009020145,0.0000043299397,0.000053429416,0.000014579776,0.98811275,0.0059312433,0.0016872754,0.0039868895,0.0000060694606],"about_ca_topic_score_codex":0.001016186,"about_ca_topic_score_gemma":0.0012354249,"teacher_disagreement_score":0.002371948,"about_ca_system_score_codex":0.00031106034,"about_ca_system_score_gemma":0.0003107746,"threshold_uncertainty_score":0.007934928},"labels":[],"label_agreement":null},{"id":"W2322552448","doi":"10.2514/6.2015-2499","title":"Control validation of a morphing wing in an open loop architecture","year":2015,"lang":"en","type":"article","venue":"AIAA Modeling and Simulation Technologies Conference","topic":"Aeroelasticity and Vibration Control","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":"Université du Québec","funders":"Consortium de Recherche et d’innovation en Aérospatiale au Québec","keywords":"Morphing; Computer science; Architecture; Wing; Loop (graph theory); Artificial intelligence; Engineering; Aerospace engineering; Mathematics; Geography","score_opus":0.06578387083850014,"score_gpt":0.2829340845677288,"score_spread":0.21715021372922866,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2322552448","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":[0.8414343,0.00004282642,0.15393963,0.00007077832,0.000056029527,0.00011155337,0.000052087624,0.0006109995,0.0036817864],"genre_scores_gemma":[0.99389666,0.0000053311405,0.0055774455,0.000006335881,0.0000012047095,0.00001905726,0.000012708571,0.0000046774694,0.00047657193],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997328,0.000049456426,0.000013706783,0.000058312216,0.000111455396,0.00003426658],"domain_scores_gemma":[0.9995034,0.00015200062,0.00007031953,0.00009792974,0.00014553341,0.00003092586],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005706172,0.00024899596,0.00015423671,0.0001857466,0.00018747913,0.00032972023,0.00039215374,0.0003013995,0.0012163132],"category_scores_gemma":[0.0008573152,0.00008191027,0.0002028374,0.00004842995,0.0003953812,0.00020523259,0.000306913,0.00020558121,0.00009351706],"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":[0.0008227007,0.00031718134,0.004259314,0.00025860922,0.000055516382,0.00040641316,0.00032974704,0.49816617,0.4349163,0.0035783176,0.0003987292,0.05649103],"study_design_scores_gemma":[0.000058855934,0.0010463697,0.002406565,0.000009100163,0.000016163416,0.00004412408,0.000035688292,0.91769063,0.07746759,0.00040740077,0.0008054067,0.000012068423],"about_ca_topic_score_codex":0.0018612888,"about_ca_topic_score_gemma":0.0010485396,"teacher_disagreement_score":0.0018612888,"about_ca_system_score_codex":0.00023477111,"about_ca_system_score_gemma":0.0002517147,"threshold_uncertainty_score":0.0040690303},"labels":[],"label_agreement":null},{"id":"W2322912110","doi":"10.2514/6.2004-1890","title":"Design and Development of Piezoelectric Inchworm Actuator","year":2004,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Concordia University","funders":"","keywords":"Actuator; Piezoelectricity; Computer science; Materials science; Acoustics; Physics; Artificial intelligence","score_opus":0.012916352981114633,"score_gpt":0.19244430133215604,"score_spread":0.1795279483510414,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2322912110","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":[0.08205322,0.0014647851,0.9015429,0.00030388703,0.00022921518,0.00033848936,0.00015452942,0.0009321828,0.012980798],"genre_scores_gemma":[0.36894742,0.0017153876,0.612172,0.00013677396,0.00008347886,0.00045542303,0.00022387192,0.0000520065,0.016213572],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99973816,0.000014311403,0.000014278807,0.000044110733,0.00016932384,0.00001977165],"domain_scores_gemma":[0.9998621,0.00002218482,0.000026749663,0.000010589767,0.00006419549,0.000014164297],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002213805,0.00025763328,0.00024315956,0.0001504556,0.00014673446,0.00017885973,0.0005980671,0.00039661716,0.0015475905],"category_scores_gemma":[0.00019755689,0.00019757326,0.00017265946,0.00009879993,0.00015776265,0.0003545891,0.00022581495,0.000326344,0.00045632874],"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":[0.000038036258,0.000031567164,0.00036871893,0.00044214426,0.0000087735125,0.00024802494,0.000097131204,0.004603382,0.9291053,0.003716754,0.00061414635,0.06072612],"study_design_scores_gemma":[0.00006753798,0.0011144778,0.003993209,0.000074215444,0.00003206067,0.0023863935,0.00008108856,0.093316995,0.822536,0.0008541167,0.07548775,0.000056082336],"about_ca_topic_score_codex":0.00035289468,"about_ca_topic_score_gemma":0.00043078847,"teacher_disagreement_score":0.0015475905,"about_ca_system_score_codex":0.00017835818,"about_ca_system_score_gemma":0.00052462734,"threshold_uncertainty_score":0.0051772594},"labels":[],"label_agreement":null},{"id":"W2325636143","doi":"10.2514/6.2010-3072","title":"Modulation Control of Bi-State Adaptive Impedance Device for Active Vibration Suppression","year":2010,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Electrical impedance; Modulation (music); Vibration; Active vibration control; State (computer science); Control theory (sociology); Vibration control; Frequency modulation; Computer science; Control (management); Acoustics; Materials science; Physics; Engineering; Electrical engineering; Telecommunications; Radio frequency","score_opus":0.010408196601347576,"score_gpt":0.22910570529907967,"score_spread":0.2186975086977321,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2325636143","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":[0.42109892,0.0004463982,0.56777424,0.00018822898,0.00014586715,0.000065954846,0.000040136543,0.00057208014,0.009668217],"genre_scores_gemma":[0.99115115,0.000043694923,0.00776682,0.000012776167,0.000006334971,0.000017129269,0.000008392649,0.0000037508844,0.0009897265],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99990845,0.000016813456,0.000006840709,0.000014185651,0.00004488461,0.0000087668395],"domain_scores_gemma":[0.9998939,0.00003596738,0.000026272572,0.000012124223,0.000023635812,0.0000081305],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00011820976,0.00016672604,0.00012259424,0.00010863162,0.00013246054,0.00024056579,0.00031359252,0.00014672423,0.0011059106],"category_scores_gemma":[0.000288393,0.000070030925,0.0000890247,0.00007479572,0.00017130199,0.00020853942,0.00027982946,0.00019048867,0.00016089124],"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":[0.00035552974,0.00013096345,0.000717831,0.00019368106,0.000021847027,0.00010953912,0.0002118972,0.030102614,0.86039615,0.007367665,0.00052419136,0.09986817],"study_design_scores_gemma":[0.00011812196,0.00085835386,0.0026134264,0.000022043383,0.000027656295,0.00014680678,0.000041401603,0.8523373,0.13680638,0.0017419353,0.0052610016,0.000025638019],"about_ca_topic_score_codex":0.0002381045,"about_ca_topic_score_gemma":0.00048513178,"teacher_disagreement_score":0.0011059106,"about_ca_system_score_codex":0.00009861036,"about_ca_system_score_gemma":0.00008050201,"threshold_uncertainty_score":0.0036996007},"labels":[],"label_agreement":null},{"id":"W2327947413","doi":"10.2514/6.2007-1068","title":"Time Base Aeroservoelasticity Wind Tunnel Testing","year":2007,"lang":"en","type":"article","venue":"45th AIAA Aerospace Sciences Meeting and Exhibit","topic":"Aeroelasticity and Vibration Control","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":"Bombardier (Canada)","funders":"McGill University","keywords":"Wind tunnel; Base (topology); Computer science; Marine engineering; Aerospace engineering; Engineering; Mathematics","score_opus":0.01760529466341955,"score_gpt":0.21843306103083251,"score_spread":0.20082776636741295,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2327947413","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":[0.9884709,0.000035096087,0.009482317,0.000015241343,0.000016915448,0.00009532293,0.00024137789,0.00015475448,0.0014880075],"genre_scores_gemma":[0.99530727,0.000030785162,0.0028112116,0.000017809254,0.0000026636662,0.000058276135,0.0002795569,0.000016659762,0.001475831],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99971896,0.000025588124,0.000017669052,0.0000334162,0.00014987876,0.000054485954],"domain_scores_gemma":[0.9990308,0.00016918003,0.00007481495,0.00010189009,0.0005302051,0.00009315693],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003855577,0.00038311406,0.00021919802,0.00029162128,0.00027910314,0.00019812827,0.0004898153,0.0005513358,0.003541854],"category_scores_gemma":[0.00090598455,0.00015344456,0.0001445311,0.00017860564,0.00023805707,0.00042613538,0.00025676322,0.0002321831,0.00036405015],"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":[0.0013175845,0.00037332697,0.005184363,0.0002148118,0.000025456395,0.00066571264,0.00022551963,0.011997704,0.9567892,0.00045487063,0.0006242947,0.0221272],"study_design_scores_gemma":[0.0002249029,0.018100966,0.04730808,0.000080400125,0.000039168568,0.0008209451,0.0004963455,0.04364074,0.8838653,0.00049553416,0.0048379144,0.00008964595],"about_ca_topic_score_codex":0.00070939143,"about_ca_topic_score_gemma":0.0011579803,"teacher_disagreement_score":0.003541854,"about_ca_system_score_codex":0.00009573691,"about_ca_system_score_gemma":0.00019820612,"threshold_uncertainty_score":0.011848688},"labels":[],"label_agreement":null},{"id":"W2331250327","doi":"10.1115/detc2005-84530","title":"Analytical Formulation and Damping Analysis of Beams With Enhanced Active Constrained Layer Treatments Under Various Boundary Conditions","year":2005,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Atomic Energy of Canada Limited","keywords":"Constrained-layer damping; Materials science; Boundary (topology); Boundary layer; Boundary value problem; Active layer; Modal; Layer (electronics); Structural engineering; Mechanics; Control theory (sociology); Computer science; Physics; Acoustics; Engineering; Mathematical analysis; Mathematics; Composite material; Vibration control; Vibration","score_opus":0.011133951661043352,"score_gpt":0.25099043355855727,"score_spread":0.2398564818975139,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2331250327","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":[0.18451457,0.00046427592,0.8090321,0.00008263705,0.000022669476,0.00004305859,0.00005493214,0.000098647295,0.0056870445],"genre_scores_gemma":[0.9369916,0.00040975836,0.058970682,0.00003531142,0.000012638483,0.00007889476,0.00006146123,0.000032518154,0.0034072723],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999877,0.000019245568,0.0000037679179,0.00002082995,0.000064601365,0.000014574693],"domain_scores_gemma":[0.9998579,0.000061194616,0.000026546551,0.000013508316,0.000035502042,0.0000053345548],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00026445687,0.00042857596,0.00022413753,0.00025692093,0.00014332791,0.00033953367,0.00042863193,0.00043277172,0.0011264676],"category_scores_gemma":[0.0005467286,0.00017546577,0.000319868,0.00012085783,0.0003952851,0.0006360345,0.0003094899,0.00026340352,0.00017330008],"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":[0.00012277062,0.000061829574,0.0013355705,0.00030268278,0.000042346895,0.00022928425,0.00032727048,0.45944518,0.45867014,0.04143953,0.0004591391,0.0375643],"study_design_scores_gemma":[0.0000059113017,0.000038558002,0.00041120884,0.000008323632,0.0000061499236,0.000036447887,0.000040231516,0.97857714,0.01858792,0.001459436,0.0008215221,0.0000071252175],"about_ca_topic_score_codex":0.0006822827,"about_ca_topic_score_gemma":0.0010503673,"teacher_disagreement_score":0.0011264676,"about_ca_system_score_codex":0.00021009753,"about_ca_system_score_gemma":0.00020664107,"threshold_uncertainty_score":0.0037683845},"labels":[],"label_agreement":null},{"id":"W2332683070","doi":"10.3166/jesa.37.501-526","title":"Contrôle actif des structures appliqué à une structure souple","year":2003,"lang":"fr","type":"article","venue":"Journal Européen des Systèmes Automatisés","topic":"Aeroelasticity and Vibration Control","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":"Physics; Humanities; Philosophy","score_opus":0.01307296918586679,"score_gpt":0.23275399430711122,"score_spread":0.21968102512124443,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2332683070","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":[0.4386294,0.0005528863,0.52428395,0.0008350501,0.00083462964,0.00025841544,0.00008380293,0.000967759,0.03355415],"genre_scores_gemma":[0.9437923,0.0002970639,0.016966814,0.00012175885,0.0001836119,0.00013252933,0.000053255088,0.000057179936,0.03839539],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99935764,0.00015109792,0.0000142967365,0.000108798224,0.00030796177,0.00006025744],"domain_scores_gemma":[0.99906975,0.00055570016,0.000048556005,0.000056008208,0.00021537486,0.00005462423],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006367502,0.00089484744,0.0006159698,0.0004643668,0.0006766807,0.0012911784,0.00047082553,0.0015446078,0.005755033],"category_scores_gemma":[0.0017006674,0.00023148987,0.00060606183,0.00014989314,0.0009955083,0.00036325678,0.00033863756,0.0011406554,0.0007215257],"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":[0.0012472965,0.00043779987,0.0017962791,0.0002524102,0.00009974284,0.00093318993,0.0006765749,0.17440136,0.63923585,0.010726538,0.0025396408,0.16765332],"study_design_scores_gemma":[0.00029437075,0.0019539895,0.013159948,0.000043774635,0.00004568184,0.0007783616,0.00021405393,0.8043131,0.16366184,0.0021680577,0.013295746,0.00007096623],"about_ca_topic_score_codex":0.00996946,"about_ca_topic_score_gemma":0.0052438485,"teacher_disagreement_score":0.00996946,"about_ca_system_score_codex":0.00076540746,"about_ca_system_score_gemma":0.00042542384,"threshold_uncertainty_score":0.019822896},"labels":[],"label_agreement":null},{"id":"W2333505503","doi":"10.2514/6.2013-1715","title":"Blade Sailing Phenomenon Modeling for Feedback Control","year":2013,"lang":"en","type":"article","venue":"54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference","topic":"Aeroelasticity and Vibration Control","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":"Control theory (sociology); Aeroelasticity; Nonlinear system; Rotor (electric); Aerodynamics; Helicopter rotor; Discretization; Blade (archaeology); Galerkin method; Flapping; Computer science; Blade element theory; Controller (irrigation); Elevator; Actuator; Engineering; Physics; Aerospace engineering; Structural engineering; Mathematics; Mechanical engineering; Mathematical analysis; Control (management)","score_opus":0.009321421201920421,"score_gpt":0.1972072194385199,"score_spread":0.18788579823659948,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2333505503","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":[0.020601477,0.00017789332,0.9639986,0.0001412489,0.00008355961,0.00005149215,0.00010882628,0.0004410458,0.014395824],"genre_scores_gemma":[0.94505554,0.00041157292,0.041467972,0.000084084306,0.00006028394,0.00020947104,0.00025653595,0.000080789316,0.012373688],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999052,0.000017789851,0.0000041123676,0.000019983496,0.000041957912,0.000010908527],"domain_scores_gemma":[0.99991643,0.000017082453,0.000016391385,0.000012757761,0.00003252624,0.0000047313188],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012676472,0.00045550583,0.00042379528,0.00015835541,0.00024432456,0.0005533279,0.0007443931,0.0004500173,0.0029491014],"category_scores_gemma":[0.00028473855,0.00015973148,0.00046444323,0.00011071713,0.0003063073,0.00044694016,0.00040520378,0.0006620034,0.0006194887],"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":[0.000030590436,0.00003270708,0.00032591267,0.00007851439,0.00001280962,0.00009720879,0.00008531488,0.95050836,0.014467405,0.020419382,0.0009590184,0.0129828155],"study_design_scores_gemma":[0.0000017802108,0.000014360869,0.000059888847,0.0000023158664,0.0000017802228,0.000006162253,0.0000053132935,0.99745446,0.00044808286,0.00093765714,0.0010666099,0.0000016604297],"about_ca_topic_score_codex":0.0046346053,"about_ca_topic_score_gemma":0.0029031027,"teacher_disagreement_score":0.0046346053,"about_ca_system_score_codex":0.0003242763,"about_ca_system_score_gemma":0.00043648414,"threshold_uncertainty_score":0.009865701},"labels":[],"label_agreement":null},{"id":"W2412903919","doi":"10.1177/1045389x15620036","title":"Real-time monitoring of a variable-camber aileron rib by original strain-angle transducer","year":2015,"lang":"en","type":"article","venue":"Journal of Intelligent Material Systems and Structures","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":8,"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":"Consortium de Recherche et d’innovation en Aérospatiale au Québec","keywords":"Hinge; Fiber Bragg grating; Transducer; Rotation (mathematics); Structural engineering; Optics; Grating; Buckling; Displacement (psychology); Acoustics; Materials science; Engineering; Wavelength; Computer science; Physics","score_opus":0.014729974663153034,"score_gpt":0.2310373666827165,"score_spread":0.21630739201956345,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2412903919","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":[0.77061766,0.0011365428,0.2208511,0.00015323191,0.000116049145,0.00008261166,0.00026149157,0.0016599107,0.005121459],"genre_scores_gemma":[0.95773715,0.00021702814,0.039411634,0.000037894206,0.000014878979,0.000026257636,0.00007947706,0.000028558774,0.002447188],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997075,0.000032463082,0.0000075855137,0.00007230425,0.00016164203,0.000018509487],"domain_scores_gemma":[0.99980694,0.00006150087,0.000044170774,0.00002303135,0.000050620936,0.000013720291],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002400427,0.00032711867,0.00023207729,0.00026178168,0.00010529454,0.00039438964,0.0005291137,0.00056526816,0.0009899843],"category_scores_gemma":[0.00032245403,0.00012949962,0.00012873886,0.00019425963,0.00027530457,0.0003978048,0.00019170802,0.00018732314,0.00029048414],"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":[0.00012530881,0.000023183491,0.0009858285,0.00008907701,0.000005478977,0.00011535812,0.00010724263,0.0031798985,0.97760254,0.00049274205,0.00013681386,0.017136589],"study_design_scores_gemma":[0.000016131964,0.0005856728,0.010511606,0.00002318194,0.000027771435,0.00041359453,0.00009269531,0.12951535,0.85294825,0.00024575836,0.0055713565,0.000048590617],"about_ca_topic_score_codex":0.00043820826,"about_ca_topic_score_gemma":0.0008490365,"teacher_disagreement_score":0.0009899843,"about_ca_system_score_codex":0.00028627543,"about_ca_system_score_gemma":0.00014683536,"threshold_uncertainty_score":0.0033118129},"labels":[],"label_agreement":null},{"id":"W2415649882","doi":"10.1017/aer.2016.64","title":"Distributed actuation concepts for a morphing aileron device","year":2016,"lang":"en","type":"article","venue":"The Aeronautical Journal","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":42,"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":"Consortium de Recherche et d’innovation en Aérospatiale au Québec","keywords":"Morphing; Aileron; Actuator; Camber (aerodynamics); Airfoil; Aerodynamics; Computer science; Engineering; Kinematics; Aerospace engineering; Electrical engineering; Physics","score_opus":0.021261138933606216,"score_gpt":0.2665230049904933,"score_spread":0.2452618660568871,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2415649882","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":[0.41881394,0.0013900126,0.5450493,0.00041877964,0.00021448347,0.00014267133,0.00008040591,0.0005812339,0.03330919],"genre_scores_gemma":[0.91481644,0.0001735114,0.07736804,0.000061731786,0.000021072963,0.000058789497,0.00002577962,0.000014751155,0.0074600107],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999418,0.0000071910017,0.0000026616453,0.000016399774,0.000025180074,0.000006858686],"domain_scores_gemma":[0.9999645,0.00001001913,0.000009558717,0.0000054398724,0.000005669653,0.0000048065895],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00007458425,0.00018746806,0.00013037375,0.00015438354,0.0001528597,0.00029184853,0.0003612851,0.0003247933,0.0017114508],"category_scores_gemma":[0.00007281315,0.000076828364,0.000101215606,0.00005371451,0.0002816039,0.00027435343,0.0002818795,0.0002249292,0.00020067288],"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":[0.00006779915,0.000041039442,0.00018600022,0.00009133803,0.000008013036,0.000310916,0.000102990096,0.021221805,0.92575425,0.021644812,0.0004477241,0.030123347],"study_design_scores_gemma":[0.00009249174,0.0013448276,0.0027040544,0.00004004936,0.000023305978,0.0012574247,0.00013451964,0.6348051,0.30286312,0.012141948,0.044535637,0.000057485533],"about_ca_topic_score_codex":0.00013707385,"about_ca_topic_score_gemma":0.00023380501,"teacher_disagreement_score":0.0017114508,"about_ca_system_score_codex":0.00019489731,"about_ca_system_score_gemma":0.00007830441,"threshold_uncertainty_score":0.0057253838},"labels":[],"label_agreement":null},{"id":"W2418326639","doi":"10.2514/6.2016-4368","title":"Open loop morphing wing architecture based ANFIS controller","year":2016,"lang":"en","type":"article","venue":"16th AIAA Aviation Technology, Integration, and Operations Conference","topic":"Aeroelasticity and Vibration Control","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":"Université du Québec","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Morphing; Computer science; Architecture; Wing; Open-loop controller; Loop (graph theory); Controller (irrigation); Control engineering; Control theory (sociology); Closed loop; Aerospace engineering; Engineering; Artificial intelligence; Control (management); Mathematics","score_opus":0.012733470437127681,"score_gpt":0.2277681216987026,"score_spread":0.21503465126157492,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2418326639","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":[0.10225111,0.00025339876,0.881707,0.00016354928,0.00023225784,0.0000945541,0.000050823448,0.0013137575,0.01393343],"genre_scores_gemma":[0.9546764,0.000084115636,0.04001401,0.00005267217,0.0000237952,0.0000863721,0.00005187515,0.000017592663,0.004993223],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99988985,0.000017543949,0.000008034871,0.000028605658,0.00004265016,0.000013381284],"domain_scores_gemma":[0.9998505,0.00004529679,0.000020241581,0.000010765397,0.00006710283,0.000006031347],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025311753,0.0004509507,0.00036443837,0.00017197692,0.00032597457,0.00044353143,0.0004832455,0.00061186636,0.0022389893],"category_scores_gemma":[0.00044672503,0.00015879437,0.00024164186,0.0000934748,0.0002590367,0.00027525576,0.00034113953,0.00046136454,0.0003114114],"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":[0.00024016673,0.00008533131,0.00078023865,0.0001295239,0.00005450059,0.00018090637,0.00013877267,0.8356316,0.035314783,0.002679569,0.0010650917,0.12369954],"study_design_scores_gemma":[0.000010026956,0.000071357215,0.00021160759,0.0000042511574,0.000009949048,0.000016673823,0.000007373219,0.9968706,0.0021724938,0.0001557729,0.00046670405,0.0000030645563],"about_ca_topic_score_codex":0.0034292163,"about_ca_topic_score_gemma":0.0033494332,"teacher_disagreement_score":0.0034292163,"about_ca_system_score_codex":0.0001878628,"about_ca_system_score_gemma":0.00026856374,"threshold_uncertainty_score":0.007490158},"labels":[],"label_agreement":null},{"id":"W2418489673","doi":"10.13111/2066-8201.2016.8.2.6","title":"A Neural Network Controller New Methodology for the ATR-42 Morphing Wing Actuation","year":2016,"lang":"en","type":"article","venue":"INCAS BULLETIN","topic":"Aeroelasticity and Vibration Control","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":"École de Technologie Supérieure; Université du Québec à Montréal","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Morphing; Controller (irrigation); Control theory (sociology); Actuator; Wind tunnel; Airfoil; PID controller; Position (finance); Artificial neural network; Wing; Engineering; Computer science; Control engineering; Structural engineering; Aerospace engineering; Artificial intelligence; Control (management); Temperature control","score_opus":0.0486698388637987,"score_gpt":0.2563753269860189,"score_spread":0.2077054881222202,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2418489673","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":[0.0058279275,0.00034779057,0.98778206,0.000043715703,0.00008832744,0.00007818828,0.000022601831,0.0004950172,0.0053142607],"genre_scores_gemma":[0.5179619,0.00070968014,0.4620322,0.00012203865,0.00008821968,0.00048898766,0.0001335987,0.00008119469,0.018382099],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99985623,0.000016148726,0.000008525426,0.000037261616,0.0000700018,0.000011831247],"domain_scores_gemma":[0.99993,0.000017140439,0.000009699756,0.0000067358324,0.00003258337,0.000003846059],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00022608187,0.00041958492,0.0003017586,0.00022433636,0.00021521376,0.00036149408,0.0005796957,0.00040018148,0.0022708077],"category_scores_gemma":[0.00027462744,0.00015155725,0.0002887201,0.00016136828,0.0002285799,0.0002774016,0.00027161054,0.00061907526,0.00036940223],"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":[0.000113137925,0.000112004134,0.00040214558,0.00036259159,0.00008416015,0.00019936736,0.000097389886,0.42516837,0.11121851,0.013841135,0.0019688136,0.44643238],"study_design_scores_gemma":[0.000014753131,0.00012692071,0.00032296547,0.000014370092,0.000016922017,0.00006942283,0.000006690736,0.9826736,0.010774749,0.0008120892,0.0051562632,0.000011180995],"about_ca_topic_score_codex":0.003458937,"about_ca_topic_score_gemma":0.004125114,"teacher_disagreement_score":0.003458937,"about_ca_system_score_codex":0.00034042727,"about_ca_system_score_gemma":0.0003941574,"threshold_uncertainty_score":0.0075966716},"labels":[],"label_agreement":null},{"id":"W2433017098","doi":"10.1017/aer.2016.62","title":"Design and optimisation of an aerofoil with active continuous trailing-edge flap","year":2016,"lang":"en","type":"article","venue":"The Aeronautical Journal","topic":"Aeroelasticity and Vibration Control","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":"SFU Community Trust Endowment Fund; University of Michigan; National Aeronautics and Space Administration","keywords":"Airfoil; Aerodynamics; Trailing edge; Aeroelasticity; Structural engineering; Computational fluid dynamics; Stack (abstract data type); Transonic; Engineering; Mechanics; Mechanical engineering; Computer science; Aerospace engineering; Physics","score_opus":0.013044240139943668,"score_gpt":0.21028889625964922,"score_spread":0.19724465611970554,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2433017098","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":[0.6081422,0.00028193995,0.38109925,0.00006893939,0.00003344365,0.00016152817,0.0001207994,0.00038725062,0.009704525],"genre_scores_gemma":[0.9681265,0.000043772372,0.030721098,0.0000058267055,0.000002889974,0.00005328817,0.000030331195,0.000019370133,0.0009969589],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998578,0.00001842178,0.000005254425,0.00003049463,0.000058944468,0.000029059744],"domain_scores_gemma":[0.9998622,0.00004106796,0.000033230677,0.0000160131,0.00003054757,0.00001695083],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00026381292,0.00039487306,0.00027675202,0.00031394343,0.00019707921,0.0004883808,0.00046048232,0.00045718948,0.0011928316],"category_scores_gemma":[0.00029351885,0.00020475118,0.00034869966,0.00010389512,0.0003034125,0.0002408313,0.0002975735,0.00025220212,0.00018562283],"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":[0.000296819,0.00010480457,0.0021736224,0.00020394468,0.00003718734,0.00022326155,0.00005562886,0.7320825,0.2118142,0.0018383646,0.00024744237,0.05092227],"study_design_scores_gemma":[0.000052627554,0.0007004828,0.0022673567,0.000015147588,0.000023175951,0.00008716519,0.00003223399,0.958299,0.03536742,0.0002689836,0.0028707183,0.000015764988],"about_ca_topic_score_codex":0.0009967587,"about_ca_topic_score_gemma":0.0011194721,"teacher_disagreement_score":0.0011928316,"about_ca_system_score_codex":0.0002607052,"about_ca_system_score_gemma":0.00041787408,"threshold_uncertainty_score":0.0039904118},"labels":[],"label_agreement":null},{"id":"W2466918884","doi":"10.1017/s000192400001318x","title":"Active Control of a hybrid actuation system for aircraft vertical fin buffet load alleviation","year":2006,"lang":"en","type":"article","venue":"The Aeronautical Journal","topic":"Aeroelasticity and Vibration Control","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":"National Research Council Canada","funders":"Air Force Research Laboratory; Langley Research Center; Boeing","keywords":"Rudder; Linear-quadratic-Gaussian control; Structural engineering; Aileron; Control theory (sociology); Fin; Actuator; Engineering; Flight control surfaces; Aeroelasticity; Wing; Optimal control; Aerodynamics; Computer science; Marine engineering; Aerospace engineering","score_opus":0.007479613763417855,"score_gpt":0.20541819860911326,"score_spread":0.1979385848456954,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2466918884","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":[0.5992834,0.00017134412,0.3925893,0.00012208497,0.00008878973,0.00013025568,0.00008185625,0.0010266687,0.0065063434],"genre_scores_gemma":[0.9931272,0.000012533862,0.005992845,0.000014842826,0.000005139155,0.000027372242,0.000011881408,0.000003950671,0.0008042132],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999093,0.000012897286,0.000006809959,0.000023842787,0.000031630992,0.000015553194],"domain_scores_gemma":[0.9998129,0.000054620883,0.00005058046,0.0000149232355,0.00005348688,0.000013575741],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024773713,0.00030664334,0.00017830989,0.0001673236,0.00023032856,0.00030752076,0.0003683657,0.00018690423,0.0013157806],"category_scores_gemma":[0.00025809844,0.00009792949,0.00012845903,0.000061435276,0.00018910391,0.00013218055,0.0003108173,0.00016627263,0.00013042249],"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":[0.0008516178,0.00034692942,0.002259392,0.00033195,0.000075552794,0.00041583893,0.00034296425,0.2418773,0.59266466,0.0021300346,0.0012120303,0.15749177],"study_design_scores_gemma":[0.000084220934,0.0011324981,0.0023545285,0.000020372838,0.000027427832,0.00005855976,0.000037714024,0.9547326,0.039437797,0.00027144956,0.0018243766,0.000018439587],"about_ca_topic_score_codex":0.0015920762,"about_ca_topic_score_gemma":0.0016334023,"teacher_disagreement_score":0.0015920762,"about_ca_system_score_codex":0.00016686664,"about_ca_system_score_gemma":0.00018305599,"threshold_uncertainty_score":0.004401684},"labels":[],"label_agreement":null},{"id":"W2469868570","doi":"10.1017/s0001924000004978","title":"Control laws for an active tunable vibration absorber designed for rotor blade damping augmentation","year":2004,"lang":"en","type":"article","venue":"The Aeronautical Journal","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":36,"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; Carleton University","funders":"","keywords":"Helicopter rotor; Vibration; Aerodynamics; Spring (device); Actuator; Rotor (electric); Stiffness; Vibration control; Smart material; Blade (archaeology); Engineering; Active vibration control; Structural engineering; Control theory (sociology); Computer science; Acoustics; Mechanical engineering; Aerospace engineering; Materials science; Control (management); Physics; Electrical engineering","score_opus":0.02336283819835352,"score_gpt":0.2666612921493038,"score_spread":0.24329845395095026,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2469868570","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":[0.025308637,0.00017199431,0.96386737,0.0002524156,0.00011739814,0.000074912576,0.00004000698,0.0004577657,0.009709435],"genre_scores_gemma":[0.94428873,0.0002056851,0.047453523,0.0001052737,0.000037907386,0.00020967965,0.00003155164,0.000024395687,0.00764316],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99991405,0.000012994723,0.00000469765,0.000024224837,0.00003425025,0.000009888956],"domain_scores_gemma":[0.99984276,0.000060349506,0.000039344093,0.000010437493,0.00004134448,0.000005714902],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024549046,0.0003155846,0.0002154813,0.00015496921,0.00019863331,0.0005063144,0.000498533,0.0005366118,0.002435772],"category_scores_gemma":[0.0004319499,0.00013980448,0.00020718656,0.00010260124,0.00041313353,0.00024327089,0.00025758267,0.00052339316,0.0003617726],"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":[0.00024587323,0.00011077917,0.0007646504,0.0003751197,0.000052238473,0.00039431461,0.00035818727,0.6297445,0.20349582,0.06949975,0.0034072325,0.09155155],"study_design_scores_gemma":[0.000032236458,0.00015304827,0.0002114795,0.000012284815,0.000013202314,0.000039647133,0.000013450951,0.98846895,0.0061810096,0.0024094896,0.0024577647,0.0000075297867],"about_ca_topic_score_codex":0.0014397962,"about_ca_topic_score_gemma":0.0014328061,"teacher_disagreement_score":0.002435772,"about_ca_system_score_codex":0.00023958863,"about_ca_system_score_gemma":0.00026420332,"threshold_uncertainty_score":0.008148491},"labels":[],"label_agreement":null},{"id":"W2477359657","doi":"10.1017/s0001924000012045","title":"Laplace-domain approximation to the transfer functions of a rotor blade in forward flight","year":2001,"lang":"en","type":"article","venue":"The Aeronautical Journal","topic":"Aeroelasticity and Vibration Control","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":"Carleton University","funders":"","keywords":"Helicopter rotor; Laplace transform; Aerodynamics; Aeroelasticity; Mathematics; Mathematical analysis; Airfoil; Control theory (sociology); Physics; Rotor (electric); Computer science; Mechanics","score_opus":0.009900275419170062,"score_gpt":0.21052909653161853,"score_spread":0.20062882111244845,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2477359657","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":[0.138264,0.0001095757,0.8533506,0.00011878778,0.000038778133,0.000030378842,0.00003288221,0.00028650675,0.0077685146],"genre_scores_gemma":[0.96407115,0.00013198642,0.030935237,0.000034260458,0.000017656372,0.000029089622,0.000036159487,0.000024539595,0.0047198683],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999548,0.0000132328705,0.0000013097043,0.0000051060924,0.000019624718,0.000005855654],"domain_scores_gemma":[0.9998505,0.00008395337,0.000011679522,0.000012893146,0.000034983957,0.000005865293],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002753757,0.00024177277,0.00013425566,0.0002129899,0.00010709396,0.00024802994,0.00024642755,0.0004593022,0.0018028112],"category_scores_gemma":[0.0007160334,0.00010965007,0.0002234624,0.000108336986,0.00040081338,0.0002692493,0.00019030279,0.00034433237,0.00036063456],"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":[0.00014933973,0.00008034523,0.000876763,0.00009584579,0.000014739696,0.00038881402,0.00025842653,0.86950594,0.05845686,0.030703343,0.00091950904,0.038550038],"study_design_scores_gemma":[0.0000054130223,0.000018234487,0.00015334762,0.0000026050304,0.0000010568828,0.000027451768,0.000013931847,0.9966415,0.0018128391,0.0010540298,0.00026680614,0.000002799885],"about_ca_topic_score_codex":0.0013004835,"about_ca_topic_score_gemma":0.0006604613,"teacher_disagreement_score":0.0018028112,"about_ca_system_score_codex":0.00014591696,"about_ca_system_score_gemma":0.00022285874,"threshold_uncertainty_score":0.006030977},"labels":[],"label_agreement":null},{"id":"W2480545482","doi":"10.1016/j.compstruct.2016.07.019","title":"Time to flutter theory for viscoelastic composite aircraft wings","year":2016,"lang":"en","type":"article","venue":"Composite Structures","topic":"Aeroelasticity and Vibration Control","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":"Carleton University","funders":"","keywords":"Flutter; Viscoelasticity; Wing; Structural engineering; Aeroelasticity; Materials science; Aerodynamics; Engineering; Aerospace engineering; Composite material","score_opus":0.004885456595290076,"score_gpt":0.20465795506659637,"score_spread":0.1997724984713063,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2480545482","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":[0.0694472,0.0026595795,0.86596096,0.00087282213,0.00073267205,0.000057282985,0.00007217214,0.00012778996,0.0600696],"genre_scores_gemma":[0.8952782,0.0023633041,0.02634015,0.0004283807,0.0004570438,0.00011339651,0.000098694385,0.00016259652,0.07475819],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99991095,0.00002061269,0.00000356648,0.000013883333,0.00003483306,0.00001615115],"domain_scores_gemma":[0.99972874,0.000120042496,0.000027865754,0.000019522904,0.000070116526,0.000033670007],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003389591,0.0007000336,0.0004205592,0.0008861463,0.00047244268,0.00073277706,0.0009657702,0.0011157278,0.0051557473],"category_scores_gemma":[0.0012016327,0.00022263234,0.00053638424,0.00024726894,0.0010379056,0.0013590733,0.00076191843,0.0011977222,0.00036487816],"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":[0.00007399598,0.000054144464,0.00024580088,0.00014232947,0.000033110602,0.00031300302,0.00024200416,0.21267314,0.011559255,0.75744116,0.0026323837,0.014589626],"study_design_scores_gemma":[0.0000067072438,0.000026769501,0.00021591975,0.000012757874,0.0000073672245,0.00006127974,0.00003900887,0.8893765,0.00050500955,0.10821187,0.0015240589,0.000012744509],"about_ca_topic_score_codex":0.0018926268,"about_ca_topic_score_gemma":0.001171288,"teacher_disagreement_score":0.0051557473,"about_ca_system_score_codex":0.00056680146,"about_ca_system_score_gemma":0.00029616794,"threshold_uncertainty_score":0.017247677},"labels":[],"label_agreement":null},{"id":"W2496049786","doi":"10.1017/s0001924000005182","title":"Dynamic modelling and stability of hingeless helicopter blades with a smart spring","year":2004,"lang":"en","type":"article","venue":"The Aeronautical Journal","topic":"Aeroelasticity and Vibration Control","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":"Carleton University","funders":"","keywords":"Helicopter rotor; Floquet theory; Galerkin method; Blade (archaeology); Smart material; Spring (device); Aeroelasticity; Blade element momentum theory; Stiffness; Equations of motion; Structural engineering; Parametric statistics; Stability (learning theory); Modal; Rotor (electric); Control theory (sociology); Computer science; Turbine blade; Aerodynamics; Engineering; Mechanical engineering; Aerospace engineering; Mathematics; Physics; Nonlinear system; Materials science; Turbine; Classical mechanics; Finite element method","score_opus":0.012306939820225826,"score_gpt":0.20174709747910322,"score_spread":0.1894401576588774,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2496049786","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":[0.9243644,0.00009231485,0.07269548,0.000044932778,0.00001270982,0.00002093821,0.000030273995,0.000071192524,0.0026678187],"genre_scores_gemma":[0.9981724,0.0000235662,0.0012843569,0.0000025945437,0.0000015753596,0.0000047537683,0.000007414939,0.0000032079492,0.0005000797],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99994385,0.000013390342,0.0000028512457,0.0000102939375,0.00002022491,0.000009296491],"domain_scores_gemma":[0.9998896,0.000033900793,0.000028876868,0.000017613987,0.000018450253,0.000011566858],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015926323,0.00029164855,0.00024841502,0.00027524735,0.00022435968,0.00040772933,0.00033356738,0.0005485582,0.00069101184],"category_scores_gemma":[0.00029975548,0.00021141193,0.00027764315,0.00010464572,0.00070049945,0.00028174516,0.00025204298,0.00017023236,0.00014629465],"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":[0.0001060354,0.000024927756,0.0013833904,0.000025298034,0.000014187312,0.0003152106,0.000095389325,0.94276047,0.04945372,0.0020453092,0.000083446146,0.0036925783],"study_design_scores_gemma":[0.0000041235494,0.00003535527,0.00050587876,0.0000013683099,0.0000017748379,0.000014986647,0.000010930503,0.9982324,0.0008536277,0.00023462632,0.00010236447,0.000002535713],"about_ca_topic_score_codex":0.0017573342,"about_ca_topic_score_gemma":0.0008881658,"teacher_disagreement_score":0.0017573342,"about_ca_system_score_codex":0.0002222919,"about_ca_system_score_gemma":0.00017491503,"threshold_uncertainty_score":0.003494203},"labels":[],"label_agreement":null},{"id":"W2509902617","doi":"10.3390/aerospace3030025","title":"Effect of the Backward-Facing Step Location on the Aerodynamics of a Morphing Wing","year":2016,"lang":"en","type":"article","venue":"Aerospace","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":22,"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":"Airfoil; Morphing; Lift coefficient; Aerodynamics; Aerospace engineering; NACA airfoil; Angle of attack; Trailing edge; Lift-to-drag ratio; Wing; Pressure coefficient; Chord (peer-to-peer); Drag coefficient; Reynolds number; Structural engineering; Computer science; Drag; Engineering; Mechanics; Physics; Artificial intelligence","score_opus":0.004285905692221155,"score_gpt":0.18602014417344584,"score_spread":0.1817342384812247,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2509902617","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":[0.9976191,0.00008362824,0.0011080744,0.000029756186,0.00002167806,0.0000069885573,0.000029469064,0.00003115978,0.0010701572],"genre_scores_gemma":[0.99912566,0.000031271753,0.00065701077,0.000007978217,0.0000014748847,0.000002063538,0.000012955978,0.0000041292196,0.00015740906],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99991214,0.000011290096,0.0000066134244,0.000014477594,0.000027144948,0.000028296434],"domain_scores_gemma":[0.99965334,0.0001552088,0.00007072909,0.000029499908,0.000047997604,0.000043149732],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00013033336,0.00031553948,0.00025663056,0.00018438257,0.00027678075,0.00042106904,0.00020503074,0.000363653,0.001723152],"category_scores_gemma":[0.00059559976,0.00015100997,0.00021495453,0.000097268516,0.00032547087,0.00023804005,0.0003321676,0.00032424228,0.00016976474],"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":[0.0010661734,0.00018107642,0.013078679,0.00024097296,0.00004808409,0.0020739054,0.00015063878,0.13443275,0.83508927,0.00064712705,0.00030719367,0.012684121],"study_design_scores_gemma":[0.00016009809,0.0046602017,0.053755306,0.00008695795,0.00017781628,0.0010464562,0.0008110982,0.3522932,0.5839763,0.000292603,0.002626583,0.00011337971],"about_ca_topic_score_codex":0.0007628669,"about_ca_topic_score_gemma":0.0009474421,"teacher_disagreement_score":0.001723152,"about_ca_system_score_codex":0.00013875158,"about_ca_system_score_gemma":0.0002271449,"threshold_uncertainty_score":0.0057644844},"labels":[],"label_agreement":null},{"id":"W2523450473","doi":"10.1017/aer.2016.94","title":"Non-linear aeroelastic analysis in the time domain of high-aspect-ratio wings: Effect of chord and taper-ratio variation","year":2016,"lang":"en","type":"article","venue":"The Aeronautical Journal","topic":"Aeroelasticity and Vibration Control","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":"University of Victoria","funders":"","keywords":"Aeroelasticity; Aspect ratio (aeronautics); Wing; Flutter; Chord (peer-to-peer); Structural engineering; Stall (fluid mechanics); Lift-to-drag ratio; Drag; Aerodynamics; Mathematics; Mechanics; Engineering; Materials science; Computer science; Physics; Composite material","score_opus":0.004151401839048733,"score_gpt":0.20720811827867194,"score_spread":0.2030567164396232,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2523450473","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":[0.98727787,0.0001298517,0.010592596,0.000035968773,0.000009501581,0.000013710934,0.000036877096,0.00006106713,0.0018425648],"genre_scores_gemma":[0.99812037,0.00005209066,0.0014065471,0.0000047121757,0.000002449137,0.0000050638714,0.00002015496,0.000010196089,0.00037822602],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999329,0.00001584134,0.0000037756608,0.000007737643,0.000025993393,0.000013682893],"domain_scores_gemma":[0.999721,0.00015895888,0.000043292144,0.000022531493,0.00003454089,0.000019645311],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018348306,0.00033217965,0.00028838805,0.00030620658,0.0002100775,0.00036103494,0.00030367065,0.000407143,0.0008667611],"category_scores_gemma":[0.000563987,0.00013257047,0.00041324896,0.00018875822,0.00042123484,0.00020500689,0.00023068019,0.00030485823,0.00010928409],"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":[0.00032545291,0.00020232727,0.005607802,0.00015369407,0.000045352226,0.0008138274,0.00018198472,0.7947149,0.18497565,0.0007933249,0.00015116646,0.012034486],"study_design_scores_gemma":[0.000012224145,0.00012697888,0.00362132,0.000006735149,0.0000072391413,0.000049234844,0.000044781704,0.98006755,0.015820934,0.00008668973,0.00014892186,0.000007402788],"about_ca_topic_score_codex":0.0037193827,"about_ca_topic_score_gemma":0.0021706994,"teacher_disagreement_score":0.0037193827,"about_ca_system_score_codex":0.00015196622,"about_ca_system_score_gemma":0.00020447084,"threshold_uncertainty_score":0.007395506},"labels":[],"label_agreement":null},{"id":"W2547685126","doi":"10.1177/1045389x16672565","title":"Development of a morphing wing extrados made of composite materials and actuated by shape memory alloys","year":2016,"lang":"en","type":"article","venue":"Journal of Intelligent Material Systems and Structures","topic":"Aeroelasticity and Vibration Control","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":"École de Technologie Supérieure","funders":"","keywords":"Morphing; Finite element method; Materials science; Shape-memory alloy; Complex geometry; Parametric statistics; Actuator; Structural engineering; Wing; Composite number; Displacement (psychology); Geometry; Aerodynamics; Mechanical engineering; Engineering; Composite material; Computer science; Mathematics; Aerospace engineering","score_opus":0.011652582289133847,"score_gpt":0.2103940424844442,"score_spread":0.19874146019531036,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2547685126","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":[0.8428961,0.00059772463,0.14695448,0.000069077854,0.00011938975,0.00009539155,0.00010251797,0.0004254702,0.008739824],"genre_scores_gemma":[0.87984985,0.0003027307,0.11583399,0.000021476313,0.000007540634,0.000027478629,0.00007778298,0.000049629845,0.0038295053],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99991953,0.0000045863603,0.000004280678,0.000017730164,0.000043144024,0.00001064733],"domain_scores_gemma":[0.9999199,0.000009439547,0.000019378043,0.000018869725,0.000015313923,0.00001709679],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00009173451,0.0001880784,0.00015305587,0.00018382419,0.00008930623,0.00017952028,0.00026705855,0.00022031102,0.0005363641],"category_scores_gemma":[0.00012078859,0.0001403999,0.0002268404,0.00008573911,0.00015492874,0.00018868946,0.00026662476,0.0002615073,0.0002270581],"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":[0.000015138811,0.000011559442,0.00021460388,0.00004514393,0.0000041244257,0.00011422619,0.000023352073,0.0030734858,0.9867286,0.0005244333,0.00004344088,0.009201944],"study_design_scores_gemma":[0.000010272961,0.00043357973,0.0031922073,0.000012019349,0.000013905149,0.000801478,0.000022210705,0.023433337,0.96227145,0.00015227005,0.009643365,0.0000139135855],"about_ca_topic_score_codex":0.00012180026,"about_ca_topic_score_gemma":0.00022494551,"teacher_disagreement_score":0.0005363641,"about_ca_system_score_codex":0.000098458055,"about_ca_system_score_gemma":0.00012745195,"threshold_uncertainty_score":0.0017942786},"labels":[],"label_agreement":null},{"id":"W2555095606","doi":"10.1177/0954410016675893","title":"The effect of stiffness and geometric parameters on the nonlinear aeroelastic performance of high aspect ratio wings","year":2016,"lang":"en","type":"article","venue":"Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering","topic":"Aeroelasticity and Vibration Control","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":"University of Victoria","funders":"","keywords":"Flutter; Aeroelasticity; Stiffness; Wing; Bending stiffness; Inertia; Aspect ratio (aeronautics); Structural engineering; Torsion (gastropod); Swept wing; Nonlinear system; Lift (data mining); Mechanics; Materials science; Aerodynamics; Engineering; Physics; Classical mechanics; Computer science; Composite material","score_opus":0.005353454749602329,"score_gpt":0.175843822696405,"score_spread":0.17049036794680267,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2555095606","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":[0.99436957,0.00014362409,0.0043709446,0.000012222224,0.000005136435,0.000006639198,0.000018337376,0.000021165772,0.0010524538],"genre_scores_gemma":[0.99920386,0.000042802567,0.00058537297,0.0000018254511,6.771616e-7,0.0000022131944,0.000008119336,0.0000040293066,0.00015103201],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99986815,0.000031049112,0.000010081555,0.000017059798,0.000045299057,0.000028248976],"domain_scores_gemma":[0.99938834,0.00036566262,0.000120768425,0.00005000628,0.000053614436,0.000021606276],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002621406,0.00039088377,0.00021162532,0.00028575733,0.00014843045,0.00029001787,0.00016205122,0.0002704838,0.0007443332],"category_scores_gemma":[0.0009813075,0.00017866015,0.00023960255,0.00014318243,0.0002786017,0.00026667307,0.00022551567,0.00017746266,0.00014471852],"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":[0.00061855675,0.00017808488,0.014476234,0.00025441393,0.00005453241,0.0006426221,0.00014528364,0.36598262,0.59513295,0.00034015445,0.0000839592,0.022090552],"study_design_scores_gemma":[0.00006699287,0.0034706923,0.06185709,0.00003741196,0.00016792033,0.00071362354,0.00031264243,0.5614552,0.3704575,0.00031518046,0.0010668277,0.000078996236],"about_ca_topic_score_codex":0.0004926935,"about_ca_topic_score_gemma":0.0009344572,"teacher_disagreement_score":0.0007443332,"about_ca_system_score_codex":0.00010720615,"about_ca_system_score_gemma":0.00013097434,"threshold_uncertainty_score":0.0024901032},"labels":[],"label_agreement":null},{"id":"W2557714052","doi":"10.1139/tcsme-2011-0021","title":"A FAILURE CONTROL METHOD FOR SMART COMPOSITE MORPHING AIRFOIL BY PIEZOELECTRIC ACTUATOR","year":2011,"lang":"en","type":"article","venue":"Transactions of the Canadian Society for Mechanical Engineering","topic":"Aeroelasticity and Vibration Control","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":"Morphing; Airfoil; Actuator; Structural engineering; Finite element method; Displacement (psychology); Piezoelectricity; Composite number; Materials science; Smart material; Failure mechanism; Buckling; Nonlinear system; Flight control surfaces; Computer science; Engineering; Composite material; Aerodynamics; Aerospace engineering; Electrical engineering","score_opus":0.009042553798347683,"score_gpt":0.18862147172924734,"score_spread":0.17957891793089967,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2557714052","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":[0.023139926,0.000091704875,0.97564065,0.000039149952,0.000035363166,0.000022231387,0.0000057414345,0.00016402725,0.0008611947],"genre_scores_gemma":[0.8699712,0.00014033841,0.12685679,0.000038982795,0.000038928632,0.00009236159,0.000019785894,0.000028391705,0.0028132894],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999093,0.000010663885,0.000004836736,0.000026137326,0.000041838888,0.000007149085],"domain_scores_gemma":[0.99985826,0.0000394909,0.000021822281,0.000011201333,0.000058289454,0.000010937881],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021762057,0.00041255716,0.0003057171,0.00023683411,0.00032122608,0.00020256315,0.000541852,0.00037605557,0.0012276904],"category_scores_gemma":[0.0002921325,0.00015916834,0.0002191489,0.00007054839,0.00034310942,0.00035643912,0.00027218807,0.0003319017,0.00010912654],"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":[0.00019380852,0.000071932925,0.0010210678,0.00034449322,0.00004617689,0.00037028655,0.00046929068,0.3198664,0.3131384,0.015329462,0.001848684,0.34730002],"study_design_scores_gemma":[0.000010108058,0.00007978478,0.00021507182,0.0000038714475,0.000007500117,0.000052522017,0.000011939805,0.99153554,0.0067498456,0.0006059484,0.00072028255,0.000007634308],"about_ca_topic_score_codex":0.002042864,"about_ca_topic_score_gemma":0.0016465152,"teacher_disagreement_score":0.002042864,"about_ca_system_score_codex":0.00018996686,"about_ca_system_score_gemma":0.00021559352,"threshold_uncertainty_score":0.0041069984},"labels":[],"label_agreement":null},{"id":"W2560347813","doi":"","title":"Optimal virtual mechanical impedances approach for the vibroacoustic active control of a panel","year":2014,"lang":"en","type":"article","venue":"HAL (Le Centre pour la Communication Scientifique Directe)","topic":"Aeroelasticity and Vibration Control","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":"Electrical impedance; Computer science; Mechanical impedance; Control (management); Acoustics; Engineering; Electrical engineering; Physics; Artificial intelligence","score_opus":0.011464682872096236,"score_gpt":0.19798038908122512,"score_spread":0.18651570620912888,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2560347813","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":[0.009293034,0.00011113472,0.9857756,0.00009355234,0.00004659156,0.0000184982,0.000010662133,0.000068938294,0.0045819213],"genre_scores_gemma":[0.9174452,0.00022183725,0.07385982,0.000082610415,0.0000660247,0.00010688635,0.000032204363,0.000059906768,0.008125381],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997212,0.00009545811,0.0000106791595,0.000045966623,0.0000962079,0.000030371422],"domain_scores_gemma":[0.99974257,0.00013233903,0.000024528263,0.000015409882,0.00006932975,0.00001571975],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00045770974,0.0006268423,0.00060191395,0.00026282904,0.0003088703,0.0010206033,0.00061852473,0.000911603,0.0043567466],"category_scores_gemma":[0.00089653855,0.0002743686,0.00047962056,0.00023246575,0.0005949926,0.0004889293,0.0006706716,0.0006737887,0.0004334164],"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":[0.00016955618,0.0000752208,0.00015826772,0.0001678751,0.000047044192,0.000089507,0.00013596081,0.8868445,0.020391596,0.027655605,0.0010728397,0.06319195],"study_design_scores_gemma":[0.000006199895,0.000029153434,0.00004691359,0.000003826279,0.0000057314396,0.000009812956,0.000008404985,0.99726677,0.00056563853,0.0016543384,0.0003996804,0.000003503826],"about_ca_topic_score_codex":0.00210802,"about_ca_topic_score_gemma":0.0019473111,"teacher_disagreement_score":0.0043567466,"about_ca_system_score_codex":0.00042581517,"about_ca_system_score_gemma":0.0005077982,"threshold_uncertainty_score":0.014574766},"labels":[],"label_agreement":null},{"id":"W2568866629","doi":"10.2514/6.2017-1425","title":"Numerical and Experimental Testing of a Morphing Upper Surface Wing Equipped with Conventional and Morphing Ailerons","year":2017,"lang":"en","type":"article","venue":"55th AIAA Aerospace Sciences Meeting","topic":"Aeroelasticity and Vibration Control","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":"National Research Council Canada; Université du Québec","funders":"","keywords":"Morphing; Aileron; Computer science; Wing; Structural engineering; Computer graphics (images); Engineering","score_opus":0.0259881109624222,"score_gpt":0.25648629111490967,"score_spread":0.23049818015248746,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2568866629","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":[0.95152074,0.00022648158,0.035750847,0.00022127693,0.0004908794,0.00069316814,0.00044614845,0.0002992387,0.010351225],"genre_scores_gemma":[0.9668501,0.00019232379,0.027065184,0.00010279684,0.000029916388,0.00059550646,0.00024508414,0.000074221425,0.0048448998],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9983523,0.0003204063,0.00016727607,0.0003204323,0.0005930616,0.00024651035],"domain_scores_gemma":[0.9956226,0.002393,0.00030300216,0.0006324766,0.00070102944,0.00034784424],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0019501407,0.0008270615,0.0004682089,0.0010455546,0.0004871197,0.0011717912,0.0014357187,0.0014626266,0.014011332],"category_scores_gemma":[0.011095773,0.00036174885,0.0009556103,0.00045895073,0.0015881737,0.0010398661,0.0015217505,0.00092952355,0.001767713],"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":[0.019691072,0.010046965,0.030277247,0.002446342,0.00022604711,0.0020810482,0.005781304,0.087186016,0.50448525,0.016192747,0.0046809493,0.31690493],"study_design_scores_gemma":[0.0013889566,0.115669794,0.106546946,0.0014432371,0.0008539545,0.0014887224,0.009015562,0.46272296,0.23799805,0.016642971,0.045663778,0.00056512747],"about_ca_topic_score_codex":0.0015346725,"about_ca_topic_score_gemma":0.0011864337,"teacher_disagreement_score":0.014011332,"about_ca_system_score_codex":0.000424101,"about_ca_system_score_gemma":0.00061315595,"threshold_uncertainty_score":0.046872556},"labels":[],"label_agreement":null},{"id":"W2568984447","doi":"10.2514/6.2017-1735","title":"Flutter Suppression for a Two Degree of Freedom Aeroelastic Wing Section: a Structured H-infinity-Based Gain-Scheduling Approach with Explicit Hidden Coupling Terms Handling","year":2017,"lang":"en","type":"article","venue":"AIAA Guidance, Navigation, and Control Conference","topic":"Aeroelasticity and Vibration Control","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":"Polytechnique Montréal","funders":"","keywords":"Aeroelasticity; Flutter; Wing; Section (typography); Control theory (sociology); Infinity; Computer science; Degree (music); Structural engineering; Aerodynamics; Mathematics; Engineering; Mathematical analysis; Physics; Aerospace engineering; Artificial intelligence; Acoustics","score_opus":0.022993462838732253,"score_gpt":0.24159646083338795,"score_spread":0.2186029979946557,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2568984447","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":[0.014032849,0.000058114576,0.982698,0.00003549283,0.00003394015,0.000015806892,0.000010312063,0.00011391061,0.0030016159],"genre_scores_gemma":[0.7997124,0.00018807054,0.1940675,0.000083440675,0.000077205645,0.00007353691,0.00006061697,0.00013297249,0.005604224],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998833,0.000029870058,0.000003989148,0.000016983693,0.00004847326,0.00001736776],"domain_scores_gemma":[0.99977463,0.000102116974,0.000025813086,0.000021572454,0.00005526157,0.000020494239],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00034919314,0.00067857193,0.00048855564,0.00023939864,0.00031950593,0.00036922251,0.0007659329,0.00061465875,0.002747447],"category_scores_gemma":[0.0006017972,0.00023822214,0.00048666113,0.00019224637,0.0004362001,0.00043019277,0.00055909035,0.0006189311,0.0005652035],"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":[0.00025871617,0.00010489127,0.0002800939,0.00012781828,0.000037419544,0.00013170084,0.00014573644,0.8496333,0.05714399,0.012640345,0.0012369206,0.078259096],"study_design_scores_gemma":[0.00000648747,0.000031790758,0.00003007745,0.0000024846076,0.0000029006953,0.000008268823,0.000005048045,0.99777645,0.0012031491,0.00076106586,0.00016979076,0.0000025103402],"about_ca_topic_score_codex":0.0013309035,"about_ca_topic_score_gemma":0.001594218,"teacher_disagreement_score":0.002747447,"about_ca_system_score_codex":0.00022714512,"about_ca_system_score_gemma":0.00041039896,"threshold_uncertainty_score":0.009191096},"labels":[],"label_agreement":null},{"id":"W2570207712","doi":"10.2514/6.2017-0267","title":"Effects of Speed on Coupled Sweep and Camber in Morphing Wings","year":2017,"lang":"en","type":"article","venue":"55th AIAA Aerospace Sciences Meeting","topic":"Aeroelasticity and Vibration Control","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":false,"ca_institutions":"","funders":"Air Force Office of Scientific Research; Natural Sciences and Engineering Research Council of Canada; U.S. Air Force","keywords":"Morphing; Camber (aerodynamics); Computer science; Aerospace engineering; Engineering; Computer graphics (images)","score_opus":0.00983558498725836,"score_gpt":0.2351978842209249,"score_spread":0.22536229923366655,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2570207712","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":[0.99700004,0.00006828026,0.0012010052,0.000027581222,0.000027179938,0.0000073515025,0.000018333742,0.000029755933,0.0016204541],"genre_scores_gemma":[0.99860173,0.000030040814,0.00034941733,0.0000050939966,0.0000050861036,0.0000019084168,0.00001543575,0.000029463425,0.0009617476],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997037,0.00006382123,0.000012861855,0.000044084485,0.000116945856,0.000058617064],"domain_scores_gemma":[0.9966061,0.0018352768,0.00024656169,0.00016552261,0.0008763005,0.00027031818],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00039354464,0.00018590163,0.00030732702,0.00045648147,0.00046402277,0.0007035462,0.00023825304,0.0005021955,0.006069316],"category_scores_gemma":[0.004220535,0.00022030936,0.00016978222,0.0001631206,0.0002763175,0.00048015942,0.0004948586,0.00021447835,0.0008077271],"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":[0.0043286765,0.00030133358,0.044306245,0.0002699002,0.00011382132,0.0012956595,0.0005984641,0.043765556,0.7912172,0.0009720815,0.0011730384,0.111658156],"study_design_scores_gemma":[0.00014972122,0.0022459116,0.34636566,0.00005972642,0.00016352833,0.001023894,0.0012816287,0.27834794,0.3650509,0.00081481907,0.0043721753,0.00012406598],"about_ca_topic_score_codex":0.00052667834,"about_ca_topic_score_gemma":0.0009892521,"teacher_disagreement_score":0.006069316,"about_ca_system_score_codex":0.00013703178,"about_ca_system_score_gemma":0.00022849493,"threshold_uncertainty_score":0.020303845},"labels":[],"label_agreement":null},{"id":"W2570476262","doi":"10.2514/6.2017-1721","title":"Gust Load Alleviation Control for a Flexible Aircraft with Loss of Control Effectiveness","year":2017,"lang":"en","type":"article","venue":"AIAA Guidance, Navigation, and Control Conference","topic":"Aeroelasticity and Vibration Control","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 Toronto","funders":"China Scholarship Council; University of Toronto","keywords":"Control (management); Computer science; Control theory (sociology); Automotive engineering; Environmental science; Engineering; Artificial intelligence","score_opus":0.010358696703092371,"score_gpt":0.2353993585895532,"score_spread":0.22504066188646082,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2570476262","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":[0.5966361,0.00021142117,0.39565334,0.0003496838,0.00011711527,0.00004937534,0.000034482004,0.00032243103,0.006625971],"genre_scores_gemma":[0.9983139,0.000011540736,0.0012187158,0.0000098449145,0.0000065632707,0.000005172793,0.0000043337727,0.0000028108436,0.0004270934],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999149,0.0000106343105,0.000005097641,0.000013638899,0.000024079976,0.000031669384],"domain_scores_gemma":[0.99984396,0.000046587687,0.000034492106,0.000013353886,0.0000450759,0.000016555936],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00018225466,0.0004438178,0.0003108048,0.00015870505,0.0005065307,0.000432414,0.00041316345,0.00037050227,0.00085710693],"category_scores_gemma":[0.0003636587,0.00013078563,0.00021017487,0.000118532706,0.00047653745,0.0002831808,0.00045855762,0.00032540545,0.00009121923],"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":[0.0013835506,0.00015994864,0.0020676274,0.00014369337,0.00006489232,0.0007799933,0.00031364482,0.7941848,0.1261696,0.004382631,0.0013842196,0.06896532],"study_design_scores_gemma":[0.000021563561,0.00020514072,0.0007431395,0.0000029287016,0.00000911936,0.000028526323,0.000020883303,0.99580246,0.0027506654,0.0002727984,0.00013758555,0.0000052234204],"about_ca_topic_score_codex":0.0042121126,"about_ca_topic_score_gemma":0.003686523,"teacher_disagreement_score":0.0042121126,"about_ca_system_score_codex":0.00023666323,"about_ca_system_score_gemma":0.0002614437,"threshold_uncertainty_score":0.008375168},"labels":[],"label_agreement":null},{"id":"W2571369867","doi":"10.1016/j.cja.2016.12.013","title":"Optimization and design of an aircraft’s morphing wing-tip demonstrator for drag reduction at low speed, Part I – Aerodynamic optimization using genetic, bee colony and gradient descent algorithms","year":2017,"lang":"en","type":"article","venue":"Chinese Journal of Aeronautics","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":56,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"National Research Council Canada; École de Technologie Supérieure","funders":"Natural Sciences and Engineering Research Council of Canada; Consortium de Recherche et d’innovation en Aérospatiale au Québec","keywords":"Morphing; Aerodynamics; Wing; Genetic algorithm; Reduction (mathematics); Convergence (economics); Drag; Descent (aeronautics); Wind tunnel; Engineering; Computer science; Aerospace engineering; Control theory (sociology); Mathematical optimization; Mathematics; Artificial intelligence","score_opus":0.019324257275566088,"score_gpt":0.24420123959042267,"score_spread":0.2248769823148566,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2571369867","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":[0.32643452,0.00034578537,0.66644454,0.0001455647,0.000032213993,0.00013419516,0.000047481644,0.0004028136,0.0060129194],"genre_scores_gemma":[0.8548493,0.00013477373,0.1430955,0.000022244334,0.0000065487284,0.00012043629,0.000049985174,0.000036672474,0.0016844757],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99991703,0.000017415765,0.0000034566203,0.000016927946,0.000032043798,0.000013106326],"domain_scores_gemma":[0.9998971,0.000037244277,0.000019880612,0.000011709008,0.000024932402,0.000009151987],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002744939,0.00043833253,0.00032369466,0.00026872384,0.00023604532,0.00035666244,0.00036390044,0.0005783574,0.00065760413],"category_scores_gemma":[0.00031026037,0.00020628847,0.00030516848,0.00013520455,0.00025685798,0.00021636699,0.00023628716,0.0002751571,0.00014279604],"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":[0.00006406123,0.000071218215,0.001055541,0.00014201642,0.000031450996,0.00016392449,0.00005731764,0.85733384,0.09655637,0.001623639,0.0003278482,0.042572733],"study_design_scores_gemma":[0.000013713827,0.00018423382,0.00073803845,0.0000043050363,0.000010892059,0.00005179509,0.000015132946,0.988384,0.009653544,0.00018527656,0.0007530516,0.0000059159715],"about_ca_topic_score_codex":0.00092760543,"about_ca_topic_score_gemma":0.0009334365,"teacher_disagreement_score":0.00092760543,"about_ca_system_score_codex":0.00021564736,"about_ca_system_score_gemma":0.00036695285,"threshold_uncertainty_score":0.0021999478},"labels":[],"label_agreement":null},{"id":"W2571372758","doi":"10.1016/j.cja.2016.12.018","title":"Optimization and design of an aircraft's morphing wing-tip demonstrator for drag reduction at low speeds, Part II - Experimental validation using Infra-Red transition measurement from Wind Tunnel tests","year":2017,"lang":"en","type":"article","venue":"Chinese Journal of Aeronautics","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":58,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"National Research Council Canada; École de Technologie Supérieure","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Aileron; Wing; Morphing; Airfoil; Wind tunnel; Aerodynamics; Angle of attack; Aerospace engineering; Engineering; Lift coefficient; Genetic algorithm; Drag; Reduction (mathematics); Swept wing; Simulation; Structural engineering; Computer science; Mechanics; Turbulence; Physics; Mathematics; Artificial intelligence","score_opus":0.04026882417990416,"score_gpt":0.25935484882795373,"score_spread":0.21908602464804958,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2571372758","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":[0.9663439,0.00024922699,0.030275017,0.00006574643,0.000034323348,0.00049358484,0.000351987,0.00038633976,0.0017998168],"genre_scores_gemma":[0.9652039,0.00019541246,0.0319709,0.000019107725,0.0000056448944,0.00031569347,0.000322134,0.000050122842,0.0019172044],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99980706,0.000026029315,0.00001154437,0.00004584894,0.00007432995,0.0000351905],"domain_scores_gemma":[0.99970883,0.00003570263,0.00006336924,0.000038252005,0.00008220658,0.00007158195],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005053764,0.00061638793,0.000485731,0.00050742325,0.0003124889,0.00039939772,0.00085039635,0.0005186877,0.0017276123],"category_scores_gemma":[0.00047874858,0.00023759269,0.00034910563,0.00016314937,0.00019134536,0.000277322,0.00031677255,0.00033897103,0.0005359971],"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":[0.0004105866,0.0004506211,0.0028622837,0.0003747793,0.000029637577,0.00019228084,0.000054543878,0.016605748,0.95880544,0.0002255223,0.00024415235,0.019744512],"study_design_scores_gemma":[0.00032733433,0.01711839,0.0328111,0.000045051824,0.00021943013,0.00032735805,0.00017035847,0.081532,0.85820436,0.00015499427,0.009006688,0.000082826955],"about_ca_topic_score_codex":0.001171828,"about_ca_topic_score_gemma":0.0016811073,"teacher_disagreement_score":0.0017276123,"about_ca_system_score_codex":0.00031221315,"about_ca_system_score_gemma":0.00039812675,"threshold_uncertainty_score":0.005779445},"labels":[],"label_agreement":null},{"id":"W2587443300","doi":"","title":"Numerical and experimental validation of the optimization methodologies for a wing-tip structure equipped with conventional and morphing ailerons","year":2016,"lang":"en","type":"article","venue":"Espace École de technologie supérieure (École de technologie supérieure)","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":2,"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":"Natural Sciences and Engineering Research Council of Canada; Consortium de Recherche et d’innovation en Aérospatiale au Québec; McGill University","keywords":"Morphing; Wing; Aerodynamics; Aileron; Airfoil; Wind tunnel; Aerospace engineering; Airplane; Engineering; Multidisciplinary design optimization; Computer science; Artificial intelligence","score_opus":0.015144829942009058,"score_gpt":0.2488922616030085,"score_spread":0.23374743166099946,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2587443300","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":[0.82899755,0.00020788507,0.15475596,0.00014517312,0.00007222566,0.00018989318,0.00029409182,0.00033122,0.015005951],"genre_scores_gemma":[0.9173544,0.00007802781,0.08029896,0.000015480471,0.000004043741,0.00010132324,0.00013059513,0.000032808868,0.0019843322],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99975246,0.00004052367,0.000014489964,0.000040963205,0.000120725475,0.000030782863],"domain_scores_gemma":[0.9995055,0.00019252782,0.00006865184,0.00010774257,0.000103445986,0.00002213604],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00067317224,0.0004312854,0.00027491953,0.0002418585,0.00024139983,0.0003659867,0.00051542046,0.00061726297,0.0021739418],"category_scores_gemma":[0.0008089164,0.0001642052,0.00029204754,0.00017415117,0.0004307086,0.0002606776,0.00029675133,0.0004279848,0.0002612329],"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":[0.00031919053,0.00033076853,0.002847878,0.00033788558,0.000029176832,0.00021343732,0.0002037933,0.6819774,0.27357662,0.0036941993,0.00045434004,0.036015406],"study_design_scores_gemma":[0.000042913096,0.0010865179,0.0031937785,0.000020912295,0.000016963548,0.000068529815,0.000082436636,0.87429255,0.11845999,0.00028357483,0.0024261477,0.000025648587],"about_ca_topic_score_codex":0.00088265055,"about_ca_topic_score_gemma":0.0012914294,"teacher_disagreement_score":0.0021739418,"about_ca_system_score_codex":0.000265314,"about_ca_system_score_gemma":0.00027821446,"threshold_uncertainty_score":0.0072725415},"labels":[],"label_agreement":null},{"id":"W2598607014","doi":"10.1177/0954410017699003","title":"New control methodology for a morphing wing demonstrator","year":2017,"lang":"en","type":"article","venue":"Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":13,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"National Research Council Canada; École de Technologie Supérieure","funders":"Consortium de Recherche et d’innovation en Aérospatiale au Québec","keywords":"Wing; Morphing; Airfoil; Actuator; Wind tunnel; Aerodynamics; Aerospace engineering; Pressure sensor; Acoustics; Engineering; Computer science; Mechanical engineering; Computer vision; Physics; Electrical engineering","score_opus":0.025890098846417357,"score_gpt":0.24257313598384736,"score_spread":0.21668303713743,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2598607014","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":[0.034504686,0.00010412083,0.960693,0.000062604275,0.00005869825,0.00014254477,0.000027556089,0.0008456705,0.0035610206],"genre_scores_gemma":[0.76668364,0.00011472177,0.22708952,0.000085060856,0.000047654514,0.00023853792,0.00008101021,0.00008001862,0.0055799307],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99962914,0.00003115088,0.000024318311,0.00009697,0.00019254298,0.000025854019],"domain_scores_gemma":[0.9997818,0.00003782545,0.00004735058,0.0000389865,0.00007993577,0.000014137546],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00032504887,0.0003321923,0.0001657019,0.000286202,0.00020314573,0.0003937921,0.00060498406,0.00030617855,0.0014967852],"category_scores_gemma":[0.0003281538,0.00011213921,0.00021970815,0.00008098524,0.00030679425,0.0002794661,0.0004015394,0.0003471715,0.00020462881],"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":[0.00010720598,0.000058130732,0.00036057943,0.00020836105,0.000019641297,0.00021119222,0.00019923593,0.01642834,0.84584326,0.005727438,0.00041201583,0.13042459],"study_design_scores_gemma":[0.000078471574,0.0023076916,0.0037360564,0.00004806382,0.00006530622,0.0006336246,0.0000862233,0.41280833,0.54253036,0.0025009653,0.035133917,0.00007093009],"about_ca_topic_score_codex":0.0004201002,"about_ca_topic_score_gemma":0.00038544319,"teacher_disagreement_score":0.0014967852,"about_ca_system_score_codex":0.00017920388,"about_ca_system_score_gemma":0.00018842357,"threshold_uncertainty_score":0.005007267},"labels":[],"label_agreement":null},{"id":"W25994713","doi":"10.1121/1.4919346","title":"Experimental Investigations of Generalized Predictive Control for Tiltrotor Stability Augmentation","year":2001,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aeroelasticity and Vibration Control","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":"Model predictive control; Stability (learning theory); Engineering; Wind tunnel; Control theory (sociology); Aeronautics; Control (management); Computer science; Aerospace engineering; Artificial intelligence; Machine learning","score_opus":0.017183935674697278,"score_gpt":0.25110177579670095,"score_spread":0.23391784012200367,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W25994713","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":[0.952024,0.00020775814,0.042693425,0.00011289896,0.00007014269,0.00018182043,0.0001233301,0.00035680286,0.0042298855],"genre_scores_gemma":[0.9951697,0.000048163565,0.0039970907,0.000012307274,0.0000047782896,0.00004503364,0.00003702314,0.000013969289,0.00067194126],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997265,0.0000451492,0.000018201263,0.00006675458,0.000085104344,0.000058255264],"domain_scores_gemma":[0.99934965,0.0003062866,0.00009767779,0.00009004912,0.00012087113,0.000035432768],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004806045,0.0004948426,0.00030482074,0.00020317247,0.00036414614,0.00047284566,0.00052723114,0.00025239648,0.0032792562],"category_scores_gemma":[0.002467456,0.00015751914,0.00015514871,0.00015717227,0.0005117857,0.000335953,0.0005086743,0.00025712972,0.0002478893],"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":[0.006458674,0.00082478125,0.00311591,0.00052880775,0.00006172918,0.00024799546,0.00072744914,0.046558198,0.7830048,0.004099321,0.0006443232,0.153728],"study_design_scores_gemma":[0.000535693,0.0067722076,0.018684868,0.000060155096,0.00009944456,0.00014916102,0.00033730856,0.6348619,0.3309681,0.0023731696,0.005061255,0.000096739976],"about_ca_topic_score_codex":0.005853811,"about_ca_topic_score_gemma":0.0039125467,"teacher_disagreement_score":0.005853811,"about_ca_system_score_codex":0.00038576341,"about_ca_system_score_gemma":0.0003769484,"threshold_uncertainty_score":0.011639476},"labels":[],"label_agreement":null},{"id":"W2602827044","doi":"10.13111/2066-8201.2016.8.1.10","title":"Flutter Analysis of a Morphing Wing Technology Demonstrator: Numerical Simulation and Wind Tunnel Testinga","year":2016,"lang":"en","type":"article","venue":"INCAS BULLETIN","topic":"Aeroelasticity and Vibration Control","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":"École de Technologie Supérieure","funders":"","keywords":"Aileron; Flutter; Morphing; Aeroelasticity; Wing; Structural engineering; Wind tunnel; Finite element method; Engineering; Aerospace engineering; Aerodynamics; Computer science","score_opus":0.009838961470555855,"score_gpt":0.21871223023805217,"score_spread":0.20887326876749632,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2602827044","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":[0.99184155,0.000022461203,0.0072976137,0.000018089459,0.000004534617,0.000029156772,0.00006697285,0.000083818886,0.00063583633],"genre_scores_gemma":[0.994958,0.00001712397,0.0043963343,0.0000035730677,7.7110025e-7,0.000019479648,0.000057390316,0.000007007385,0.00054029335],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998547,0.00002791374,0.0000087296685,0.000020577434,0.000063688225,0.000024427685],"domain_scores_gemma":[0.9996866,0.00013821786,0.000038535316,0.00006319257,0.0000486859,0.00002472661],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005111899,0.00036923675,0.0003763298,0.00030874577,0.00025091274,0.00023801507,0.0005023638,0.00073523435,0.0010514861],"category_scores_gemma":[0.00047714813,0.0001731392,0.0004048763,0.00012035709,0.0003865895,0.00025219633,0.00023671561,0.00026465664,0.00013706864],"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":[0.00062045996,0.00035646078,0.011200017,0.00020170047,0.00003658639,0.0008883739,0.000527564,0.3404116,0.62454957,0.0006379603,0.00027908987,0.020290643],"study_design_scores_gemma":[0.000056838573,0.0023488023,0.015767233,0.000017299675,0.00002564159,0.00029767855,0.00015642324,0.8389519,0.14135763,0.000107115025,0.00087882695,0.000034589735],"about_ca_topic_score_codex":0.0014705706,"about_ca_topic_score_gemma":0.0013834712,"teacher_disagreement_score":0.0014705706,"about_ca_system_score_codex":0.00021679237,"about_ca_system_score_gemma":0.00018020267,"threshold_uncertainty_score":0.003517568},"labels":[],"label_agreement":null},{"id":"W2604306466","doi":"10.1117/12.2260008","title":"Preliminary aeroelastic assessment of a large aeroplane equipped with a camber-morphing aileron","year":2017,"lang":"en","type":"article","venue":"Proceedings of SPIE, the International Society for Optical Engineering/Proceedings of SPIE","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":8,"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":"Aileron; Morphing; Computer science; Aeroelasticity; Robustness (evolution); Camber (aerodynamics); Flight envelope; Parametric statistics; Aerospace engineering; Wing; Engineering; Aerodynamics; Mathematics","score_opus":0.010813967626490893,"score_gpt":0.24032803134755218,"score_spread":0.22951406372106128,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2604306466","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":[0.9967443,0.000076397075,0.0012044626,0.000028659617,0.000012053607,0.00002803157,0.00027991622,0.000058082704,0.0015680956],"genre_scores_gemma":[0.9982085,0.000044197794,0.0005407097,0.0000116948995,0.0000031679003,0.00001246612,0.00025917665,0.000010279495,0.00090971234],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998834,0.000016208414,0.0000049778596,0.00003169437,0.000040284438,0.000023325028],"domain_scores_gemma":[0.99984336,0.00005750192,0.00001050183,0.000020782898,0.000033945744,0.000033927103],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023356036,0.00048769696,0.0003732092,0.00039199283,0.00040615644,0.0003999551,0.00029146924,0.0009618977,0.0017763528],"category_scores_gemma":[0.00027346995,0.00012005975,0.00036321036,0.00015844619,0.00029912314,0.00038590888,0.00038720196,0.0004018961,0.00046257532],"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":[0.0035247412,0.00052542257,0.046252117,0.00060568925,0.000091891685,0.0057315133,0.0014435328,0.046811406,0.85877496,0.0004275584,0.0012833732,0.034527823],"study_design_scores_gemma":[0.00020365245,0.014090216,0.632845,0.0001364763,0.00018748286,0.0024294464,0.0035823998,0.1482525,0.18745697,0.00045311634,0.010202613,0.0001601048],"about_ca_topic_score_codex":0.0011496887,"about_ca_topic_score_gemma":0.00197293,"teacher_disagreement_score":0.0017763528,"about_ca_system_score_codex":0.00013963023,"about_ca_system_score_gemma":0.00009817801,"threshold_uncertainty_score":0.0059425235},"labels":[],"label_agreement":null},{"id":"W2615546480","doi":"10.1016/s1474-6670(17)33953-8","title":"Optimal Placement/Control of Distributed Actuators for a Slewing Flexible Manipulator","year":2002,"lang":"en","type":"article","venue":"IFAC Proceedings Volumes","topic":"Aeroelasticity and Vibration Control","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":"Western University","funders":"","keywords":"Actuator; Simulated annealing; Control theory (sociology); Manipulator (device); Control engineering; Engineering; Controller (irrigation); Vibration; Computer science; Control (management); Robot; Algorithm; Artificial intelligence","score_opus":0.015812246065919005,"score_gpt":0.20766455893417585,"score_spread":0.19185231286825685,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2615546480","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":[0.14942788,0.00019081446,0.8460376,0.00015141365,0.00007038475,0.00003271029,0.000019567238,0.00013829522,0.0039312686],"genre_scores_gemma":[0.968991,0.00007815326,0.028489929,0.000021455366,0.000020924164,0.000036643636,0.000012256897,0.000013055987,0.0023366257],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998826,0.000023982167,0.000005640444,0.000031748496,0.000038037528,0.000018069917],"domain_scores_gemma":[0.99982387,0.00006580119,0.000046379555,0.000015670463,0.00003321774,0.000015095568],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00034671093,0.0005136756,0.00040921292,0.00022097792,0.0003300158,0.00047469002,0.00046710268,0.0005669416,0.0011123266],"category_scores_gemma":[0.0006118888,0.00035345813,0.00028395402,0.0002473286,0.00058588997,0.00029370782,0.0004883026,0.0003741944,0.00014858154],"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":[0.00026831817,0.00007683104,0.0003001698,0.000096080585,0.000025143121,0.00016320714,0.00010584327,0.8910222,0.051648382,0.0050858464,0.00039517245,0.050812755],"study_design_scores_gemma":[0.000040105002,0.00017167721,0.00030606112,0.0000045675574,0.000008296128,0.000020913765,0.000018121758,0.9937831,0.003053939,0.002267819,0.00031861066,0.000006703689],"about_ca_topic_score_codex":0.002412499,"about_ca_topic_score_gemma":0.0030778474,"teacher_disagreement_score":0.002412499,"about_ca_system_score_codex":0.0003346673,"about_ca_system_score_gemma":0.00036275273,"threshold_uncertainty_score":0.004796922},"labels":[],"label_agreement":null},{"id":"W2731837221","doi":"10.1109/cec.2017.7969359","title":"Optimal vibration control and innovization for rectangular plate","year":2017,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Ontario Tech University","funders":"","keywords":"Actuator; Cantilever; Control theory (sociology); GRASP; Vibration control; Observability; Genetic algorithm; Active vibration control; Controller (irrigation); Piezoelectric sensor; Vibration; Computer science; Maximization; Piezoelectricity; Engineering; Control (management); Mathematical optimization; Mathematics; Acoustics; Structural engineering; Artificial intelligence","score_opus":0.009004075617110774,"score_gpt":0.2190117257370545,"score_spread":0.2100076501199437,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2731837221","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":[0.08235908,0.00044579254,0.90884596,0.000094243274,0.0000343521,0.000043198277,0.000017516348,0.0001497879,0.00801001],"genre_scores_gemma":[0.9393501,0.00023745038,0.058041304,0.000030799027,0.000011451648,0.000058929734,0.000018009203,0.000021070198,0.002230903],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998356,0.00003440125,0.000007100745,0.000047911773,0.000052933297,0.000021960663],"domain_scores_gemma":[0.9998628,0.000058648144,0.000029440233,0.000009252452,0.000034456,0.0000053956624],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00038033805,0.00034338003,0.00027976252,0.00024198307,0.00016844623,0.00035233615,0.00038142115,0.0003155419,0.0010832745],"category_scores_gemma":[0.00056767074,0.00016155781,0.00034096153,0.00017521683,0.00050603313,0.00023612544,0.00033430313,0.00032028393,0.0000958575],"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":[0.00013686674,0.00004533874,0.0005274513,0.00018249135,0.00002671047,0.00013650113,0.00013105919,0.8728828,0.055205867,0.019136608,0.0004142398,0.051174004],"study_design_scores_gemma":[0.000009704051,0.00010821124,0.00024831982,0.0000068604304,0.000007104003,0.000021542808,0.0000136154795,0.9944666,0.0033940389,0.0012719261,0.00044498898,0.000006958366],"about_ca_topic_score_codex":0.001679435,"about_ca_topic_score_gemma":0.0011575177,"teacher_disagreement_score":0.001679435,"about_ca_system_score_codex":0.00025767306,"about_ca_system_score_gemma":0.0003511412,"threshold_uncertainty_score":0.0036239624},"labels":[],"label_agreement":null},{"id":"W2768245768","doi":"10.1177/1045389x17740978","title":"Harmonic active vibration control using piezoelectric self-sensing actuation with complete digital compensation","year":2017,"lang":"en","type":"article","venue":"Journal of Intelligent Material Systems and Structures","topic":"Aeroelasticity and Vibration Control","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":"Natural Sciences and Engineering Research Council of Canada","keywords":"Actuator; Compensation (psychology); Lead zirconate titanate; Vibration; Piezoelectricity; Active vibration control; Harmonic; Accelerometer; Acoustics; Vibration control; Piezoelectric sensor; Control theory (sociology); Piezoelectric accelerometer; Electronic engineering; Engineering; Computer science; Electrical engineering; Physics; Control (management)","score_opus":0.016580385287837715,"score_gpt":0.22212580720895603,"score_spread":0.2055454219211183,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2768245768","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":[0.2527658,0.00072737626,0.7393331,0.00016078213,0.0001859956,0.00009776344,0.000047370042,0.0009481402,0.005733692],"genre_scores_gemma":[0.9167588,0.00016017581,0.07956998,0.00006181815,0.000047798938,0.000037783342,0.00003385456,0.000022922484,0.0033069267],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99984205,0.000009665716,0.000008872882,0.00003456706,0.0000932316,0.000011636342],"domain_scores_gemma":[0.99987113,0.000034180714,0.00002772789,0.000022358401,0.00003796016,0.0000066226708],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00011526538,0.00023150712,0.00015162521,0.00016942013,0.000114505536,0.0002619417,0.0006416252,0.00019566574,0.0008846805],"category_scores_gemma":[0.00020624581,0.000120838806,0.00013863706,0.00010759081,0.00023657907,0.0002948936,0.00022687478,0.00022332564,0.0001447747],"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":[0.00012406798,0.0000678899,0.00038292113,0.00014664512,0.000018892912,0.000048833874,0.00007721481,0.0055751186,0.8908536,0.0020954502,0.0002531583,0.100356184],"study_design_scores_gemma":[0.000077486286,0.00081617513,0.0029055323,0.000023061972,0.000054955337,0.0003572128,0.00003713531,0.2131554,0.77367866,0.00084006594,0.008017797,0.000036521735],"about_ca_topic_score_codex":0.00034969472,"about_ca_topic_score_gemma":0.0007319015,"teacher_disagreement_score":0.0008846805,"about_ca_system_score_codex":0.00018976591,"about_ca_system_score_gemma":0.00016184259,"threshold_uncertainty_score":0.0029595494},"labels":[],"label_agreement":null},{"id":"W2769589218","doi":"10.1016/b978-0-08-100964-2.00008-3","title":"The Design of Skin Panels for Morphing Wings in Lattice Materials","year":2017,"lang":"en","type":"book-chapter","venue":"Elsevier eBooks","topic":"Aeroelasticity and Vibration Control","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":"McGill University","funders":"","keywords":"Morphing; Homogenization (climate); Microarchitecture; Wing; Materials science; Nonlinear system; Anisotropy; Structural engineering; Lattice (music); Computer science; Composite material; Engineering; Physics; Acoustics; Optics; Parallel computing; Artificial intelligence","score_opus":0.026908320591202933,"score_gpt":0.23406676262380519,"score_spread":0.20715844203260225,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2769589218","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":[0.04640347,0.0070099384,0.76492155,0.00033398956,0.0005377203,0.0000994839,0.00021671064,0.00076463004,0.17971244],"genre_scores_gemma":[0.53395545,0.005091672,0.37335154,0.00014620299,0.00011221923,0.00014249703,0.0002210378,0.00036013004,0.08661935],"study_design_codex":"design_other","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999255,0.000015879525,0.000002426242,0.000008855919,0.000036885947,0.00001052686],"domain_scores_gemma":[0.9999652,0.000012249274,0.0000038254493,0.000005130815,0.00000817969,0.0000054040224],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012756392,0.0004115112,0.00023590785,0.00023773318,0.00015875636,0.00059559266,0.00045076825,0.00046700984,0.00628125],"category_scores_gemma":[0.00016148221,0.00024454432,0.000293405,0.00017985591,0.00022265442,0.0003279971,0.00036691243,0.00045160713,0.0013482383],"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":[0.000077877085,0.00010401575,0.0004931963,0.0006247466,0.000032238866,0.00043640155,0.00014487485,0.2555973,0.28250152,0.11818386,0.01163148,0.33017248],"study_design_scores_gemma":[0.000038575483,0.0002563905,0.0014469613,0.00027595024,0.000025899166,0.001179915,0.0001393894,0.6711888,0.09303568,0.065012194,0.16734779,0.000052462397],"about_ca_topic_score_codex":0.00014035935,"about_ca_topic_score_gemma":0.00037075594,"teacher_disagreement_score":0.00628125,"about_ca_system_score_codex":0.00016539915,"about_ca_system_score_gemma":0.00015140862,"threshold_uncertainty_score":0.021012902},"labels":[],"label_agreement":null},{"id":"W2782008044","doi":"10.2514/6.2018-0337","title":"Semi-Active Sound Transmission Control of Sandwich Panels Treated with MR Fluid Core Layer","year":2018,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Concordia University","funders":"","keywords":"Layer (electronics); Sound transmission class; Core (optical fiber); Transmission (telecommunications); Materials science; Sound (geography); Acoustics; Computer science; Composite material; Physics; Telecommunications","score_opus":0.01755100987377754,"score_gpt":0.22603054542527742,"score_spread":0.2084795355514999,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2782008044","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":[0.9852764,0.00011679619,0.013468062,0.000020101732,0.00002798341,0.0000047746435,0.000016568476,0.00005590027,0.001013444],"genre_scores_gemma":[0.9987809,0.0000214621,0.00086329057,0.0000026785456,0.0000017709441,0.0000024905457,0.0000052377645,0.000004242727,0.00031786258],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999435,0.000008941026,0.000002381609,0.000012886625,0.000017804501,0.0000144795395],"domain_scores_gemma":[0.99988914,0.000031000705,0.000025933945,0.000011410549,0.000026783933,0.000015593161],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00010073753,0.00024849508,0.00020465496,0.00009138379,0.00013202033,0.00022609868,0.00025466408,0.0002603115,0.0011342755],"category_scores_gemma":[0.00014953125,0.00007676019,0.00017907833,0.000054524604,0.00024275188,0.00015248076,0.00012665633,0.00019087485,0.00013570856],"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":[0.0003431841,0.00004060224,0.00008654289,0.000044715183,0.0000063005646,0.000031260082,0.000036359117,0.005222451,0.9908236,0.00014769197,0.00004654679,0.0031707801],"study_design_scores_gemma":[0.000029740468,0.0004315031,0.0017648689,0.000007310212,0.000023655877,0.000028234022,0.00005973666,0.1295925,0.8676215,0.0000970272,0.00033166708,0.0000121826815],"about_ca_topic_score_codex":0.0002614432,"about_ca_topic_score_gemma":0.0003454193,"teacher_disagreement_score":0.0011342755,"about_ca_system_score_codex":0.00007192306,"about_ca_system_score_gemma":0.00009137638,"threshold_uncertainty_score":0.003794551},"labels":[],"label_agreement":null},{"id":"W2782139169","doi":"10.2514/6.2018-1910","title":"Morphing Wings: A Study Using Aerodynamic Shape Optimization","year":2018,"lang":"en","type":"article","venue":"2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":7,"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":"Morphing; Aerodynamics; Computer science; Aerospace engineering; Aeronautics; Computer graphics (images); Engineering","score_opus":0.014765683332036731,"score_gpt":0.23224975159229722,"score_spread":0.21748406826026048,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2782139169","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":[0.92592126,0.000719086,0.062079187,0.00008666874,0.000041029154,0.000091803755,0.00011561339,0.00013285626,0.010812445],"genre_scores_gemma":[0.97924703,0.00028203774,0.018324949,0.000018253357,0.000012227197,0.000019365812,0.00012170942,0.000067043715,0.0019073293],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99991035,0.000025117786,0.0000048384804,0.000017633918,0.000027655296,0.000014290871],"domain_scores_gemma":[0.99966395,0.00020400064,0.00003265632,0.00004735263,0.0000362267,0.000015782502],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00023760357,0.00037560417,0.00039636088,0.00040850256,0.00030931053,0.0004684303,0.0004076116,0.00067161216,0.0014366898],"category_scores_gemma":[0.0009272683,0.00025645643,0.0005203067,0.0003738327,0.00032682222,0.00046421879,0.00023902027,0.0002975684,0.00016910315],"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":[0.00035341608,0.00036022958,0.008817726,0.00021745673,0.000111630856,0.00029010396,0.00013829247,0.8625425,0.034113556,0.0044524223,0.0005503069,0.088052325],"study_design_scores_gemma":[0.0000122031315,0.00013907967,0.002521801,0.0000067634637,0.000018504985,0.000060246173,0.00004019841,0.9937768,0.0025768185,0.00023959966,0.0006004212,0.0000075868584],"about_ca_topic_score_codex":0.0023298995,"about_ca_topic_score_gemma":0.0017266851,"teacher_disagreement_score":0.0023298995,"about_ca_system_score_codex":0.00015652737,"about_ca_system_score_gemma":0.00016917556,"threshold_uncertainty_score":0.004806161},"labels":[],"label_agreement":null},{"id":"W2784110549","doi":"10.2514/6.2018-2066","title":"An Efficient Model for Aeroelastic Tailoring of Aircraft Wings Under Gust Loads","year":2018,"lang":"en","type":"article","venue":"2018  AIAA Aerospace Sciences Meeting","topic":"Aeroelasticity and Vibration Control","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":"Aeroelasticity; Aerospace engineering; Wing; Aerodynamics; Computer science; Structural engineering; Aeronautics; Engineering; Automotive engineering","score_opus":0.025269369357605376,"score_gpt":0.26463050224747536,"score_spread":0.23936113288987,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2784110549","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":[0.109670706,0.000502286,0.85853004,0.00044494282,0.00020317303,0.00016482524,0.00065965246,0.0007570054,0.029067427],"genre_scores_gemma":[0.9494281,0.00034547178,0.030289289,0.00011442341,0.00006795319,0.0002517074,0.0005346502,0.000250662,0.018717822],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99987006,0.000029589713,0.000008386055,0.00002110797,0.00004473409,0.000026234393],"domain_scores_gemma":[0.9997789,0.000084052306,0.000021643971,0.000024167317,0.000066633416,0.000024494368],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00030590312,0.0007897192,0.0009681345,0.00042697563,0.0006997522,0.0009941917,0.0012741297,0.0023459787,0.0030990057],"category_scores_gemma":[0.00093954813,0.00048498219,0.00088008156,0.00040276215,0.00059404696,0.000841054,0.0009199226,0.0010921546,0.0006682761],"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":[0.000012847474,0.000012621868,0.00016112262,0.000017458271,0.000006830834,0.000039965624,0.000013368411,0.9955166,0.00088051043,0.0015096829,0.00014082101,0.0016883067],"study_design_scores_gemma":[0.0000037282077,0.000004054971,0.000039869472,0.0000012209545,0.0000017855821,0.0000030861804,0.000003114957,0.9993512,0.00008479926,0.00034062986,0.00016488617,0.0000016059583],"about_ca_topic_score_codex":0.02036112,"about_ca_topic_score_gemma":0.0124475425,"teacher_disagreement_score":0.02036112,"about_ca_system_score_codex":0.00058619777,"about_ca_system_score_gemma":0.0012630528,"threshold_uncertainty_score":0.040485203},"labels":[],"label_agreement":null},{"id":"W2793913129","doi":"","title":"Conception et validation expérimentale de la structure d’une aile déformable et de son système d’actionnement","year":2017,"lang":"fr","type":"article","venue":"Espace École de technologie supérieure (École de technologie supérieure)","topic":"Aeroelasticity and Vibration Control","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":"Humanities; Physics; Art","score_opus":0.011529074129616968,"score_gpt":0.2892545237318503,"score_spread":0.27772544960223333,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2793913129","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":[0.5370487,0.0011754379,0.4139724,0.00090531976,0.0009503694,0.0010811937,0.002041463,0.0051655145,0.037659563],"genre_scores_gemma":[0.84772897,0.00042626585,0.13120121,0.00017957478,0.000036146273,0.00073745893,0.0010151652,0.00045214506,0.018222963],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9984255,0.00013929266,0.000062712796,0.00031963142,0.00092571357,0.00012711511],"domain_scores_gemma":[0.99792707,0.00040875765,0.00012570531,0.0005064765,0.0009267457,0.00010519873],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0017515261,0.00075775856,0.00060348475,0.0006636319,0.00086354656,0.0016456031,0.0012787629,0.0015097233,0.013623835],"category_scores_gemma":[0.0024300967,0.0005788212,0.0007560473,0.00037715904,0.0012497945,0.0014757076,0.001037601,0.0009668616,0.0024487565],"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":[0.0005391912,0.00035750205,0.0033902873,0.00076998724,0.000080212245,0.00034296638,0.001189887,0.06334824,0.8251881,0.007876507,0.0038530456,0.09306413],"study_design_scores_gemma":[0.00011710232,0.0022676524,0.01127551,0.00013414623,0.000104189516,0.00026311888,0.0007410011,0.13818249,0.7890452,0.0014729344,0.056237925,0.00015865413],"about_ca_topic_score_codex":0.0051137875,"about_ca_topic_score_gemma":0.0061937734,"teacher_disagreement_score":0.013623835,"about_ca_system_score_codex":0.0014633866,"about_ca_system_score_gemma":0.0015865585,"threshold_uncertainty_score":0.045576274},"labels":[],"label_agreement":null},{"id":"W2797698811","doi":"10.1017/aer.2018.15","title":"Numerical and experimental transition results evaluation for a morphing wing and aileron system","year":2018,"lang":"en","type":"article","venue":"The Aeronautical Journal","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":45,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure","funders":"Natural Sciences and Engineering Research Council of Canada; Consortium de Recherche et d’innovation en Aérospatiale au Québec","keywords":"Aileron; Morphing; Wing; Wind tunnel; Angle of attack; Lift coefficient; Structural engineering; Aerodynamics; Aerospace engineering; Computer science; Engineering; Mechanics; Physics; Turbulence; Artificial intelligence","score_opus":0.021236927542926873,"score_gpt":0.2597708019944338,"score_spread":0.23853387445150692,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2797698811","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":[0.9678384,0.00012902818,0.025727458,0.00007156353,0.00006757888,0.000081974475,0.0001690029,0.0006200024,0.0052948664],"genre_scores_gemma":[0.99398804,0.000021005619,0.004803264,0.000005695271,0.0000024796323,0.00002556782,0.00007156245,0.000019247844,0.0010631267],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997199,0.00004272669,0.000020612091,0.00004566686,0.00012174997,0.000049208465],"domain_scores_gemma":[0.9994035,0.0001946112,0.000048154263,0.000116721574,0.00019124264,0.000045812165],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00058765104,0.0003605347,0.00038707777,0.00040029956,0.00045287196,0.0004816153,0.0004745975,0.0005660796,0.004586552],"category_scores_gemma":[0.00093335606,0.00012789728,0.00029584905,0.00020574672,0.0005012041,0.00039236408,0.0003740444,0.00027527308,0.0005171448],"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":[0.0029275033,0.0006489863,0.006055391,0.00057663716,0.000045803394,0.0005857243,0.0010174306,0.10140115,0.82054555,0.001507927,0.0011251533,0.06356275],"study_design_scores_gemma":[0.00019241447,0.0056624,0.01698616,0.000040087456,0.000082789586,0.00027142555,0.00054820155,0.3342017,0.63587385,0.00035498643,0.005693351,0.00009264932],"about_ca_topic_score_codex":0.0010354685,"about_ca_topic_score_gemma":0.00090297044,"teacher_disagreement_score":0.004586552,"about_ca_system_score_codex":0.00028152633,"about_ca_system_score_gemma":0.00015715774,"threshold_uncertainty_score":0.015343547},"labels":[],"label_agreement":null},{"id":"W2801525744","doi":"10.1139/tcsme-2001-0018","title":"A FINITE ELEMENT FORMULATION FOR LAMINATED ELASTIC - PIEZOELECTRIC PLATES USING A DISCRETE LAYER","year":2001,"lang":"en","type":"article","venue":"Transactions of the Canadian Society for Mechanical Engineering","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":true,"route_about_ca":false,"ca_institutions":"Université de Sherbrooke","funders":"","keywords":"Piezoelectricity; Materials science; Discretization; Vibration; Piezoelectric sensor; Finite element method; Displacement (psychology); Piezoelectric coefficient; Layer (electronics); Acoustics; Composite material; Mechanics; Structural engineering; Mathematical analysis; Physics; Mathematics; Engineering","score_opus":0.015293662428966267,"score_gpt":0.21534388780675864,"score_spread":0.20005022537779238,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2801525744","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":[0.010960288,0.00019519473,0.98334485,0.00015208016,0.000051158582,0.000052612162,0.00013407225,0.00010376418,0.005005991],"genre_scores_gemma":[0.34587124,0.00088182295,0.63137126,0.00017938092,0.00008041668,0.00061246933,0.00043754178,0.00015856736,0.020407323],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99979347,0.00005197193,0.00001154908,0.000031226857,0.00009631327,0.000015446803],"domain_scores_gemma":[0.9997055,0.00017702371,0.000031034528,0.000023707791,0.000046616522,0.000016213879],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000532957,0.0007446833,0.00069455797,0.00044324086,0.00041144,0.0009362123,0.0012573658,0.0019497669,0.0035660078],"category_scores_gemma":[0.0009139891,0.0006685819,0.00072191807,0.0004673737,0.000817616,0.0007563211,0.00078711746,0.0011001021,0.00086984923],"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":[0.0000244831,0.00003230229,0.00030311308,0.00012057144,0.000017640774,0.00013103693,0.00009729233,0.95749533,0.008572956,0.022981562,0.0004279866,0.009795805],"study_design_scores_gemma":[0.0000074110544,0.0000137178295,0.000043203796,0.0000128669735,0.000003332097,0.000027343282,0.000019312833,0.9957361,0.0009252932,0.0017219548,0.001484674,0.0000047311073],"about_ca_topic_score_codex":0.0023231006,"about_ca_topic_score_gemma":0.002759678,"teacher_disagreement_score":0.0035660078,"about_ca_system_score_codex":0.00045182096,"about_ca_system_score_gemma":0.0008423139,"threshold_uncertainty_score":0.011929452},"labels":[],"label_agreement":null},{"id":"W2884800990","doi":"10.1088/1361-665x/aad649","title":"Robust fluid-structure interaction analysis of an adaptive airfoil using shape memory alloy actuators","year":2018,"lang":"en","type":"article","venue":"Smart Materials and Structures","topic":"Aeroelasticity and Vibration Control","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":"Polytechnique Montréal","funders":"FP7 Energy","keywords":"Airfoil; Shape-memory alloy; Actuator; Fluid–structure interaction; Materials science; Alloy; Mechanical engineering; Structural engineering; Computer science; Mechanics; Composite material; Engineering; Physics; Finite element method; Artificial intelligence","score_opus":0.019683274872659858,"score_gpt":0.23365148299251629,"score_spread":0.21396820811985642,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2884800990","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":[0.5257095,0.00021526124,0.46465275,0.00013226003,0.000047490896,0.000069787064,0.00005514228,0.00038376445,0.008733992],"genre_scores_gemma":[0.9911179,0.000031400014,0.0074830293,0.000009204713,0.0000044862713,0.00003061755,0.000015444732,0.00001597444,0.0012919796],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999168,0.00002178777,0.0000030657498,0.0000121941575,0.000033643086,0.000012473504],"domain_scores_gemma":[0.9998771,0.00005100106,0.000025727202,0.000012335668,0.000021511712,0.000012318434],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00019385664,0.00039645194,0.00037889354,0.0002759105,0.00031233666,0.00042582367,0.0004967518,0.0005959149,0.0007873399],"category_scores_gemma":[0.0003207548,0.00016569148,0.00039591172,0.00010047984,0.0005226152,0.00025475468,0.00036746115,0.00029122815,0.00010064334],"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":[0.000035179193,0.000024035216,0.0005673889,0.000020270067,0.000014204071,0.000100022364,0.00002696426,0.97910863,0.015209207,0.0021309075,0.000056399356,0.0027067834],"study_design_scores_gemma":[0.0000012506811,0.00000981151,0.000075150056,4.9178266e-7,8.8668725e-7,0.0000036733068,0.0000018973628,0.99933404,0.00047060294,0.000048462112,0.0000527651,9.682725e-7],"about_ca_topic_score_codex":0.0041745002,"about_ca_topic_score_gemma":0.0016824869,"teacher_disagreement_score":0.0041745002,"about_ca_system_score_codex":0.00034708082,"about_ca_system_score_gemma":0.0004643394,"threshold_uncertainty_score":0.008300424},"labels":[],"label_agreement":null},{"id":"W2886925008","doi":"10.5539/jsd.v11n4p78","title":"Innovative Controller Design for a 5MW Wind Turbine Blade","year":2018,"lang":"en","type":"article","venue":"Journal of Sustainable Development","topic":"Aeroelasticity and Vibration Control","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":"Blade pitch; Pitch angle; Pitch control; PID controller; Turbine; Control theory (sociology); Actuator; Controller (irrigation); Trajectory; Turbine blade; Computer science; Engineering; Control engineering; Aerospace engineering; Physics; Control (management)","score_opus":0.014619996142800226,"score_gpt":0.22609656637669762,"score_spread":0.21147657023389738,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2886925008","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":[0.02605806,0.00038597596,0.96468526,0.00012262893,0.00020501805,0.00019627917,0.000049752398,0.00065490283,0.0076420372],"genre_scores_gemma":[0.7487402,0.00035806405,0.23963243,0.00011764303,0.00006903034,0.00032626488,0.00012425093,0.00003859767,0.01059365],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99980754,0.000017851518,0.000012192919,0.000043195545,0.00010624396,0.000013040573],"domain_scores_gemma":[0.9998487,0.000018507055,0.000020410771,0.000010771776,0.000094067276,0.0000075579806],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00029754173,0.0003938428,0.00028501722,0.00019678383,0.00031166265,0.00056838465,0.0006830865,0.0006139272,0.001908395],"category_scores_gemma":[0.0002940163,0.00016010905,0.0002768478,0.000118439384,0.00016153841,0.0002494434,0.00024602728,0.00046677285,0.00053687196],"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":[0.00028609298,0.00015081288,0.0010539844,0.0008819888,0.000089022215,0.0005200914,0.00022784837,0.23139729,0.4572789,0.01004812,0.0026529455,0.2954128],"study_design_scores_gemma":[0.000068026275,0.0007637881,0.001372964,0.000039945604,0.00004729122,0.00029557524,0.000037484504,0.92280203,0.056616627,0.0008138818,0.017112592,0.000029906863],"about_ca_topic_score_codex":0.0014292961,"about_ca_topic_score_gemma":0.0020725145,"teacher_disagreement_score":0.001908395,"about_ca_system_score_codex":0.00032919348,"about_ca_system_score_gemma":0.00063350325,"threshold_uncertainty_score":0.006384194},"labels":[],"label_agreement":null},{"id":"W2886927931","doi":"10.1088/1361-665x/aad7d9","title":"Numerical and experimental validation of a full scale servo-actuated morphing aileron model","year":2018,"lang":"en","type":"article","venue":"Smart Materials and Structures","topic":"Aeroelasticity and Vibration Control","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":true,"ca_institutions":"","funders":"Consortium de Recherche et d’innovation en Aérospatiale au Québec","keywords":"Aileron; Morphing; Actuator; Aeroelasticity; Camber (aerodynamics); Engineering; Context (archaeology); Aerodynamics; Computer science; Aerospace engineering; Control engineering","score_opus":0.009439844109370588,"score_gpt":0.219300010050994,"score_spread":0.2098601659416234,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2886927931","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":[0.8757384,0.0002532049,0.08820752,0.00027516708,0.00010693279,0.00026663675,0.0010156255,0.0010069313,0.033129625],"genre_scores_gemma":[0.99050623,0.00005354888,0.006120463,0.000016782931,0.0000030383162,0.00010176688,0.00017807138,0.000018866316,0.0030012573],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99985826,0.000023190742,0.000009148646,0.00002968133,0.000056807326,0.000022823058],"domain_scores_gemma":[0.99970764,0.00011478876,0.000040880434,0.000056495377,0.000055828878,0.000024361703],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00027185195,0.00045867066,0.00042233092,0.00034419054,0.00038363415,0.00074965757,0.0008924596,0.0015430526,0.004376702],"category_scores_gemma":[0.0005320999,0.00016526876,0.00038517473,0.00017742865,0.0006026117,0.00034017762,0.0005753313,0.0005388437,0.00052786246],"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":[0.00011559269,0.00010311849,0.0013340886,0.00014328059,0.000013443051,0.0002292134,0.00010189662,0.97028244,0.021127738,0.00160402,0.00031760914,0.004627539],"study_design_scores_gemma":[0.000016013646,0.00013107623,0.0006554681,0.00001009138,0.000006109657,0.000021987058,0.000030116411,0.9932823,0.0046762377,0.0001625842,0.0009992812,0.000008638195],"about_ca_topic_score_codex":0.005726553,"about_ca_topic_score_gemma":0.003262406,"teacher_disagreement_score":0.005726553,"about_ca_system_score_codex":0.00039279257,"about_ca_system_score_gemma":0.00044639345,"threshold_uncertainty_score":0.014641523},"labels":[],"label_agreement":null},{"id":"W2900739591","doi":"10.25071/10315/35296","title":"Dynamics Of A Free Pitching Flexible Cantilever Naca0012 Airfoil At Transitional Reynolds Numbers","year":2018,"lang":"en","type":"article","venue":"Progress in Canadian Mechanical Engineering","topic":"Aeroelasticity and Vibration Control","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":"Royal Military College of Canada","funders":"","keywords":"Airfoil; Reynolds number; Dynamics (music); Cantilever; Mechanics; Physics; Control theory (sociology); Computer science; Aerospace engineering; Acoustics; Engineering; Turbulence; Artificial intelligence","score_opus":0.005792903016579783,"score_gpt":0.2037836420173323,"score_spread":0.1979907390007525,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2900739591","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":[0.99760324,0.000017575185,0.001196577,0.000017714448,0.0000026329876,0.000004557376,0.000015739248,0.000016999595,0.0011249722],"genre_scores_gemma":[0.9992797,0.000009867502,0.0003456467,0.0000041650105,5.0958e-7,0.000003429385,0.00001589347,0.0000029988005,0.00033787594],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99995255,0.000004520963,0.0000018752236,0.0000073882807,0.000014772834,0.000018855428],"domain_scores_gemma":[0.9998858,0.000024443174,0.000020079733,0.000009248943,0.000019362751,0.000041167867],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00008364482,0.00019104345,0.00021354949,0.0002610748,0.00041079216,0.00035661025,0.00027593024,0.00046992698,0.00083644013],"category_scores_gemma":[0.00031161212,0.00013979674,0.0002132329,0.00009435746,0.00060231076,0.0003004473,0.0004063278,0.00031355157,0.00009742075],"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":[0.0011208084,0.00029183476,0.04238206,0.00014803592,0.000087895605,0.0032397648,0.0017398114,0.3675242,0.55663615,0.0058085374,0.0006577181,0.02036309],"study_design_scores_gemma":[0.000056497196,0.0007278919,0.061732017,0.000021791291,0.000025685136,0.0004036893,0.00070582214,0.9113558,0.02346189,0.0007447573,0.00070274057,0.00006141211],"about_ca_topic_score_codex":0.004375917,"about_ca_topic_score_gemma":0.0030022599,"teacher_disagreement_score":0.004375917,"about_ca_system_score_codex":0.00030090052,"about_ca_system_score_gemma":0.00035369038,"threshold_uncertainty_score":0.008700848},"labels":[],"label_agreement":null},{"id":"W2909338288","doi":"10.2514/6.2019-1857","title":"Stretchable Structure for a Benchtop-Scale Morphed Leading Edge Demonstration","year":2019,"lang":"en","type":"article","venue":"AIAA Scitech 2019 Forum","topic":"Aeroelasticity and Vibration Control","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":"National Research Council Canada","funders":"","keywords":"Enhanced Data Rates for GSM Evolution; Scale (ratio); Computer science; Materials science; Artificial intelligence; Physics","score_opus":0.004433744533971285,"score_gpt":0.19927106635091696,"score_spread":0.19483732181694569,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2909338288","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":[0.9467565,0.00035689888,0.04179305,0.00039761557,0.000189904,0.000114216724,0.0003054867,0.0012702903,0.0088160075],"genre_scores_gemma":[0.9443504,0.00020076228,0.04800929,0.00012136352,0.000023193425,0.00008978919,0.000196537,0.00014580715,0.006862963],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99987483,0.000007576263,0.000003488258,0.000020237036,0.00007317723,0.000020697533],"domain_scores_gemma":[0.99986017,0.00003697003,0.000021342645,0.000024801217,0.000021434556,0.00003520002],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015424332,0.00026546835,0.000121516154,0.00010121619,0.00022916406,0.00023142874,0.00033422408,0.0005271276,0.0026238607],"category_scores_gemma":[0.00019047197,0.00012612027,0.00016922623,0.000058974183,0.00021082454,0.00031743856,0.0003935889,0.00092468323,0.0006137228],"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":[0.000018304218,0.000033163407,0.00006971108,0.000018178253,0.0000013239782,0.00012557284,0.0000282263,0.00023736252,0.99684036,0.00020763,0.00020123363,0.0022188865],"study_design_scores_gemma":[0.000016101803,0.0006652606,0.0017829711,0.0000047744998,0.000003732991,0.00027030136,0.000032943357,0.0048815776,0.9852872,0.00012292479,0.0069221966,0.000009981945],"about_ca_topic_score_codex":0.00022974887,"about_ca_topic_score_gemma":0.00045334277,"teacher_disagreement_score":0.0026238607,"about_ca_system_score_codex":0.00015276339,"about_ca_system_score_gemma":0.00009672382,"threshold_uncertainty_score":0.008777678},"labels":[],"label_agreement":null},{"id":"W2911975575","doi":"10.1051/cocv/2019004","title":"Modeling and stabilization of current-controlled piezo-electric beams with dynamic electromagnetic field","year":2019,"lang":"en","type":"article","venue":"ESAIM Control Optimisation and Calculus of Variations","topic":"Aeroelasticity and Vibration Control","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":"University of Waterloo","funders":"","keywords":"Piezoelectricity; Beam (structure); Cantilever; Boundary value problem; Mathematical analysis; Inertia; Constrained-layer damping; Classical mechanics; Boundary layer; Mechanics; Magnetic field; Physics; Viscoelasticity; Field (mathematics); Mathematics; Acoustics; Vibration; Optics; Vibration control; Structural engineering; Engineering","score_opus":0.004115210389548799,"score_gpt":0.20070597278585398,"score_spread":0.19659076239630519,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2911975575","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":[0.054922186,0.0005058619,0.9275499,0.00034934626,0.000077991914,0.00006728795,0.00008670518,0.00027567465,0.016165067],"genre_scores_gemma":[0.94693124,0.0006607909,0.03505077,0.00009317099,0.000045771383,0.00030624616,0.000098051256,0.000039973067,0.016774114],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99982566,0.00003388841,0.000009722999,0.000044067503,0.00006921706,0.000017357916],"domain_scores_gemma":[0.99988186,0.0000431843,0.000028879425,0.000011632877,0.000026744685,0.000007728841],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00035517712,0.0004974844,0.0004410168,0.00031116002,0.00027525236,0.00068823906,0.0010536741,0.0008960351,0.0014989753],"category_scores_gemma":[0.00036541684,0.00027006507,0.0005230902,0.0002207745,0.0007288689,0.0006743714,0.00078024593,0.0005569267,0.00024950856],"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":[0.000046434092,0.000058366895,0.0004179491,0.000096092816,0.000028925884,0.0001582545,0.00015686266,0.8834144,0.03918387,0.06471389,0.00041005443,0.011314918],"study_design_scores_gemma":[0.000006938713,0.000025781208,0.00010220956,0.0000040317213,0.0000038315557,0.000011318331,0.000010434885,0.9944811,0.001275255,0.0034804286,0.0005942753,0.0000043477876],"about_ca_topic_score_codex":0.0022597504,"about_ca_topic_score_gemma":0.0015111947,"teacher_disagreement_score":0.0022597504,"about_ca_system_score_codex":0.00048567916,"about_ca_system_score_gemma":0.0005168035,"threshold_uncertainty_score":0.0050145388},"labels":[],"label_agreement":null},{"id":"W2915861369","doi":"10.29252/jafm.73.245.27620","title":"Experimental Evaluation of the Critical Flutter Speed on Wings of Different Aspect Ratio","year":2017,"lang":"en","type":"article","venue":"Journal of Applied Fluid Mechanics","topic":"Aeroelasticity and Vibration Control","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":"Université de Sherbrooke","funders":"","keywords":"Flutter; Chord (peer-to-peer); Wing; Wind tunnel; Propeller; Angle of attack; Reynolds number; Aeroelasticity; Wind speed; Aerodynamics; Critical speed; Mechanics; Structural engineering; Physics; Acoustics; Vibration; Meteorology; Marine engineering; Engineering; Turbulence; Computer science","score_opus":0.026188924643323286,"score_gpt":0.27244890815294953,"score_spread":0.24625998350962625,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2915861369","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":[0.99815315,0.00007325647,0.0014555361,0.00000520768,0.000010612902,0.000019338584,0.00005237317,0.000013354055,0.00021710829],"genre_scores_gemma":[0.9971258,0.00007878778,0.0023334345,0.0000068091595,0.0000036463841,0.000028659322,0.00006983267,0.0000069671914,0.00034602432],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99981827,0.00002030965,0.000015178432,0.00003114899,0.00006339945,0.00005174004],"domain_scores_gemma":[0.9992704,0.00022459193,0.00010997352,0.00006886503,0.0002568048,0.0000694458],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00045885888,0.00038472572,0.00026597048,0.000252111,0.00025596665,0.00015678175,0.00020627156,0.00032291148,0.001166204],"category_scores_gemma":[0.00072004163,0.00011371546,0.00019888309,0.000112289876,0.00030492974,0.00024297257,0.00022529901,0.00031138377,0.00009480861],"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":[0.0003299615,0.00014573328,0.0011051724,0.00009312557,0.0000048360507,0.000072210656,0.00011045255,0.001029453,0.9944482,0.000060599476,0.000038816557,0.0025613883],"study_design_scores_gemma":[0.00003727445,0.0064343116,0.014470196,0.000023831133,0.000025485911,0.00012369285,0.00018295828,0.0068090986,0.9712914,0.000060880648,0.00051868765,0.000022248783],"about_ca_topic_score_codex":0.0002308078,"about_ca_topic_score_gemma":0.00034482297,"teacher_disagreement_score":0.001166204,"about_ca_system_score_codex":0.00008493585,"about_ca_system_score_gemma":0.00010810397,"threshold_uncertainty_score":0.0039013028},"labels":[],"label_agreement":null},{"id":"W2921395671","doi":"10.1088/1361-665x/ab0fab","title":"A review of manufacturing techniques of smart composite structures with embedded bulk piezoelectric transducers","year":2019,"lang":"en","type":"review","venue":"Smart Materials and Structures","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":48,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Royal Military College of Canada","funders":"","keywords":"Actuator; Smart material; Piezoelectricity; Embedding; Structural health monitoring; Piezoelectric sensor; Process (computing); Transducer; Energy harvesting; Composite number; Mechanical engineering; Computer science; Engineering; Materials science; Energy (signal processing); Electrical engineering; Nanotechnology; Artificial intelligence","score_opus":0.014357072323805358,"score_gpt":0.25086528278685954,"score_spread":0.23650821046305417,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2921395671","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":[0.0004966495,0.995928,0.0009630551,0.00013186893,0.00019123846,0.000011619121,0.00003534878,0.000013465672,0.0022287227],"genre_scores_gemma":[0.001953602,0.99562436,0.0011579203,0.000094107774,0.000111542904,0.000013294626,0.000048689628,0.000003016148,0.0009935498],"study_design_codex":"design_other","study_design_gemma":"systematic_review","domain_scores_codex":[0.9997446,0.000030196015,0.000043011718,0.000059454236,0.00010308444,0.000019631241],"domain_scores_gemma":[0.9996954,0.00014874038,0.000048800026,0.000012475643,0.00008076076,0.000013890165],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00047657764,0.0009222584,0.0010267474,0.002954642,0.00028953355,0.000762856,0.0006556479,0.00074244104,0.002766451],"category_scores_gemma":[0.00056220917,0.00045799842,0.0005660351,0.0027336292,0.00028339634,0.0012263984,0.00045664288,0.0008688714,0.0014650535],"study_design_candidate":"systematic_review","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":[0.000048695932,0.00014589113,0.00021966493,0.055625513,0.00010951633,0.00034291108,0.0001241725,0.0009883192,0.016252464,0.007622768,0.013212107,0.9053079],"study_design_scores_gemma":[0.000006185373,0.00015957125,0.0007862477,0.0038390455,0.00012371819,0.0012054682,0.000073176976,0.0002758385,0.006054176,0.0015028587,0.9859407,0.00003285877],"about_ca_topic_score_codex":0.000800875,"about_ca_topic_score_gemma":0.0010873227,"teacher_disagreement_score":0.002954642,"about_ca_system_score_codex":0.0003360664,"about_ca_system_score_gemma":0.0007856637,"threshold_uncertainty_score":0.009254754},"labels":[],"label_agreement":null},{"id":"W2946534939","doi":"10.1017/aer.2019.35","title":"A linear guide-based actuation concept for a novel morphing aileron","year":2019,"lang":"en","type":"article","venue":"The Aeronautical Journal","topic":"Aeroelasticity and Vibration Control","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":"U.S. Air Force; Consortium de Recherche et d’innovation en Aérospatiale au Québec; National Aeronautics and Space Administration","keywords":"Aileron; Morphing; Hinge; Actuator; Camber (aerodynamics); Deflection (physics); Engineering; Impulse (physics); Structural engineering; Aeroelasticity; Control theory (sociology); Computer science; Wing; Aerodynamics; Aerospace engineering; Physics","score_opus":0.014831893787589529,"score_gpt":0.24094234879951626,"score_spread":0.22611045501192673,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2946534939","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":[0.31474972,0.0013587333,0.64714193,0.00027035773,0.00029191634,0.0003331164,0.00019259012,0.0028693175,0.032792263],"genre_scores_gemma":[0.7756765,0.00032682056,0.20618506,0.00013784383,0.00004353748,0.00016799007,0.000102315884,0.00007482049,0.017285086],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998971,0.000010824066,0.00000429134,0.000027714494,0.000044520333,0.000015442602],"domain_scores_gemma":[0.99994385,0.0000074752847,0.000014791089,0.000010783398,0.0000118340095,0.00001125017],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00010079595,0.00031746732,0.00013754443,0.00023410055,0.00014514306,0.00024817305,0.00063114386,0.00037615045,0.0018992326],"category_scores_gemma":[0.00007663672,0.0001319423,0.00017174619,0.00008167783,0.00028759043,0.00027209235,0.00035729172,0.00023591594,0.0005816585],"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":[0.000066277906,0.000030306235,0.00033673033,0.00019732188,0.000011967063,0.00031117335,0.0000929284,0.0050747977,0.9347256,0.0065000476,0.0008172495,0.051835686],"study_design_scores_gemma":[0.00011356282,0.0031425646,0.0065450626,0.000099379766,0.00006562885,0.0037405,0.00014405552,0.16329838,0.63821924,0.0022660792,0.18221529,0.00015021446],"about_ca_topic_score_codex":0.00026216582,"about_ca_topic_score_gemma":0.00047973645,"teacher_disagreement_score":0.0018992326,"about_ca_system_score_codex":0.00017168971,"about_ca_system_score_gemma":0.00016168527,"threshold_uncertainty_score":0.0063536167},"labels":[],"label_agreement":null},{"id":"W2952068287","doi":"10.48550/arxiv.1008.5111","title":"Optimal piezo-electro-mechanical coupling to control plate vibrations","year":2010,"lang":"en","type":"preprint","venue":"arXiv (Cornell University)","topic":"Aeroelasticity and Vibration Control","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 Asian Studies Association","funders":"","keywords":"Dissipative system; Dissipation; Piezoelectricity; Actuator; Coupling (piping); Mechanical energy; Vibration; Vibration control; Modal; Electric potential energy; Energy exchange; Acoustics; Energy (signal processing); Physics; Control theory (sociology); Engineering; Materials science; Computer science; Mechanical engineering; Electrical engineering; Control (management)","score_opus":0.027728472494262663,"score_gpt":0.17103150425811256,"score_spread":0.1433030317638499,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2952068287","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":[0.17521042,0.00046947037,0.8127406,0.00011591861,0.000067133275,0.000041822328,0.000012856233,0.00016428318,0.01117749],"genre_scores_gemma":[0.9720219,0.000116324,0.025424546,0.000023731329,0.000010432044,0.000032902153,0.000005781917,0.000015873706,0.002348537],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999175,0.000015713431,0.0000038789194,0.000018988156,0.000036021473,0.00000789166],"domain_scores_gemma":[0.9999299,0.000031517673,0.00001439051,0.0000073792758,0.00000859845,0.000008132383],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012454276,0.00033279174,0.00016660639,0.00014509034,0.00013517658,0.00027455046,0.00031692119,0.00018723529,0.001316971],"category_scores_gemma":[0.00028577883,0.00014846484,0.00010195433,0.00010068779,0.00036417544,0.00028849504,0.00043082662,0.0003145738,0.0001100352],"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":[0.00018029229,0.00015752151,0.00053509546,0.00022083714,0.00005452412,0.00016100102,0.00014614126,0.4034765,0.45783406,0.07615389,0.00046057935,0.060619585],"study_design_scores_gemma":[0.000029462495,0.00019315742,0.00040529235,0.000010196096,0.000022434415,0.000074676835,0.000027736618,0.93427026,0.052253008,0.010289652,0.0024101497,0.000013968744],"about_ca_topic_score_codex":0.00012313035,"about_ca_topic_score_gemma":0.00026347258,"teacher_disagreement_score":0.001316971,"about_ca_system_score_codex":0.00018154546,"about_ca_system_score_gemma":0.00012427157,"threshold_uncertainty_score":0.0044056773},"labels":[],"label_agreement":null},{"id":"W2971340222","doi":"10.1017/aer.2019.106","title":"A new hybrid control methodology for a morphing aircraft wing-tip actuation mechanism","year":2019,"lang":"en","type":"article","venue":"The Aeronautical Journal","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":18,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure","funders":"","keywords":"Actuator; Control theory (sociology); Morphing; Engineering; Flight control surfaces; Control system; Torque; Linear variable differential transformer; Computer science; Transformer; Voltage; Aerodynamics; Control (management); Physics","score_opus":0.02668384024693603,"score_gpt":0.2518845722237182,"score_spread":0.22520073197678214,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2971340222","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":[0.007550712,0.00018207953,0.9896209,0.000019534773,0.00004094631,0.000052377927,0.000011535349,0.0002000031,0.002321885],"genre_scores_gemma":[0.6108587,0.00034204827,0.3791819,0.00006983639,0.00007629829,0.0003448326,0.0000683133,0.00008337264,0.008974614],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997497,0.00004132333,0.000016260634,0.0000655441,0.00010880458,0.000018391285],"domain_scores_gemma":[0.9999138,0.00002168061,0.00001567878,0.000015564898,0.000026503842,0.000006728918],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003975567,0.0005402811,0.0003970802,0.00049307523,0.00023241808,0.00058458664,0.00084977585,0.0004956198,0.0028340546],"category_scores_gemma":[0.00020979447,0.00021218944,0.0005521115,0.00020496467,0.00047729848,0.00039900956,0.00073902693,0.00041321188,0.00037319725],"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":[0.00010767895,0.000112402435,0.00045919622,0.00067386305,0.00013928446,0.00036324735,0.00027183018,0.31341454,0.36082697,0.10047501,0.0009910149,0.22216488],"study_design_scores_gemma":[0.000029030356,0.00034186177,0.00026410582,0.000022408438,0.000030088126,0.00011677575,0.000014624007,0.97119194,0.012285841,0.0057419925,0.009941457,0.000019828063],"about_ca_topic_score_codex":0.0007460606,"about_ca_topic_score_gemma":0.0006993342,"teacher_disagreement_score":0.0028340546,"about_ca_system_score_codex":0.00025903448,"about_ca_system_score_gemma":0.0002186941,"threshold_uncertainty_score":0.009480834},"labels":[],"label_agreement":null},{"id":"W2974918968","doi":"10.3390/biomimetics4040065","title":"Fuzzy Logic-Based Control for a Morphing Wing Tip Actuation System: Design, Numerical Simulation, and Wind Tunnel Experimental Testing","year":2019,"lang":"en","type":"article","venue":"Biomimetics","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":9,"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; École de Technologie Supérieure","funders":"Natural Sciences and Engineering Research Council of Canada; Consortium de Recherche et d’innovation en Aérospatiale au Québec","keywords":"Aileron; Morphing; Wind tunnel; Wing; Aerospace engineering; Airfoil; Fuel efficiency; Flight envelope; Engineering; Computer science; Automotive engineering; Aerodynamics","score_opus":0.04106222995749191,"score_gpt":0.25426525108194564,"score_spread":0.21320302112445372,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2974918968","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":[0.52602446,0.00043264366,0.46070838,0.00033968338,0.00016179561,0.00078198034,0.00013272311,0.0008691757,0.010549066],"genre_scores_gemma":[0.96580905,0.00007113541,0.03250175,0.000028921453,0.0000055833884,0.00013801943,0.00003057127,0.000008100697,0.0014069728],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99974734,0.000034324385,0.000017917917,0.000039843722,0.00013534797,0.000025238975],"domain_scores_gemma":[0.99967766,0.000112026595,0.00005247202,0.000030507577,0.000103780134,0.000023646482],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00050651137,0.0003369128,0.0002255322,0.00023681107,0.00034083822,0.00046246732,0.0005479682,0.00049682974,0.0015054604],"category_scores_gemma":[0.00058251875,0.00014450024,0.00023980184,0.00009030459,0.00037934678,0.00021870658,0.00017413507,0.00032920105,0.00013702734],"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":[0.0009207899,0.00047982237,0.0031489949,0.00089226017,0.00008149282,0.00037117975,0.00044328964,0.46086025,0.4093453,0.0042950194,0.0008400378,0.11832152],"study_design_scores_gemma":[0.0001388824,0.0014701306,0.002096118,0.000030538136,0.00004206834,0.00009860313,0.000059803886,0.9101377,0.08268474,0.00023941662,0.002975479,0.000026631544],"about_ca_topic_score_codex":0.004147382,"about_ca_topic_score_gemma":0.0027447897,"teacher_disagreement_score":0.004147382,"about_ca_system_score_codex":0.00044169882,"about_ca_system_score_gemma":0.0005190169,"threshold_uncertainty_score":0.008246481},"labels":[],"label_agreement":null},{"id":"W2975928344","doi":"10.1017/aer.2019.114","title":"Novel morphing wing actuator control-based Particle Swarm Optimisation","year":2019,"lang":"en","type":"article","venue":"The Aeronautical Journal","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":22,"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; École de Technologie Supérieure","funders":"","keywords":"Morphing; Actuator; Particle swarm optimization; Wing; Wind tunnel; Control system; Computer science; Engineering; Flight control surfaces; MATLAB; Control engineering; Control theory (sociology); Simulation; Aerodynamics; Control (management); Aerospace engineering; Artificial intelligence","score_opus":0.01219636136373295,"score_gpt":0.20957756399158722,"score_spread":0.19738120262785427,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2975928344","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":[0.082787275,0.00027670347,0.9071483,0.00009962997,0.00008322189,0.00015516375,0.000034177752,0.00060200586,0.00881352],"genre_scores_gemma":[0.8616029,0.00010351625,0.1339941,0.00004235858,0.000019382225,0.00023497976,0.000056798763,0.000050409675,0.0038955589],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99986446,0.000032180964,0.00000760485,0.00002703293,0.000054977198,0.0000137686875],"domain_scores_gemma":[0.9998301,0.00007525098,0.000025432872,0.000019990839,0.000039803574,0.000009383862],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00036238687,0.00051774574,0.00046821605,0.00024677176,0.00020046653,0.0005457792,0.000544502,0.0005681336,0.0012826199],"category_scores_gemma":[0.00041954088,0.0001811082,0.00034764447,0.0001734234,0.0003506045,0.00020815244,0.00036652945,0.00036840327,0.00021223779],"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":[0.00013465056,0.00008576395,0.0006608325,0.00018404127,0.000052800413,0.000110316825,0.000110804904,0.8999352,0.038056493,0.004042039,0.0005383213,0.056088757],"study_design_scores_gemma":[0.000008899591,0.000033981283,0.00013960124,0.000002932924,0.0000027788658,0.0000057054144,0.000003077218,0.99788505,0.0014319248,0.00013938585,0.00034453516,0.0000021748692],"about_ca_topic_score_codex":0.0015820641,"about_ca_topic_score_gemma":0.0009250097,"teacher_disagreement_score":0.0015820641,"about_ca_system_score_codex":0.00022322345,"about_ca_system_score_gemma":0.00023994248,"threshold_uncertainty_score":0.004290819},"labels":[],"label_agreement":null},{"id":"W2977585544","doi":"10.2514/6.2018-1154","title":"Multifunctional skin materials based on tailorable, carbon-nanotube-polyurethane composite sheets","year":2018,"lang":"en","type":"article","venue":"2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference","topic":"Aeroelasticity and Vibration Control","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":"National Research Council Canada","funders":"","keywords":"Polyurethane; Carbon nanotube; Materials science; Composite number; Composite material; Nanotechnology","score_opus":0.008389774944095802,"score_gpt":0.2051453730790343,"score_spread":0.1967555981349385,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2977585544","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":[0.9790871,0.0015562526,0.0093198875,0.00015026165,0.00025787632,0.00006830293,0.00014699546,0.00034980054,0.009063619],"genre_scores_gemma":[0.98496985,0.00059989584,0.0064416565,0.000088503875,0.000029734785,0.000024464955,0.00008112469,0.000039296025,0.0077254917],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99991786,0.000010841687,0.0000043381983,0.000022683547,0.000025924304,0.000018483815],"domain_scores_gemma":[0.99985945,0.000026694446,0.000028911489,0.00001557923,0.00004140653,0.000027944478],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00014466526,0.00029562914,0.00013127967,0.00026180412,0.00014802508,0.00028742623,0.00013144201,0.0003540527,0.0030860926],"category_scores_gemma":[0.00018641211,0.00014413543,0.0001632787,0.00010923606,0.00012036627,0.0004441627,0.00014189573,0.00022676797,0.0006994464],"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":[0.000045212724,0.000013451576,0.00007828839,0.000053533804,0.0000033580484,0.00007415024,0.000010751055,0.000112995425,0.9962071,0.000105594365,0.00014037882,0.003155159],"study_design_scores_gemma":[0.0000065134464,0.00013306102,0.0011602392,0.0000071576746,0.000010586855,0.00014229666,0.00001817389,0.000995527,0.995187,0.000035050372,0.0022988843,0.0000055821215],"about_ca_topic_score_codex":0.000050018927,"about_ca_topic_score_gemma":0.00019063769,"teacher_disagreement_score":0.0030860926,"about_ca_system_score_codex":0.00007898853,"about_ca_system_score_gemma":0.000080875274,"threshold_uncertainty_score":0.010324001},"labels":[],"label_agreement":null},{"id":"W2998012945","doi":"","title":"Bending nearfield compensation in the context of vibroacoustic active control","year":2013,"lang":"fr","type":"article","venue":"HAL (Le Centre pour la Communication Scientifique Directe)","topic":"Aeroelasticity and Vibration Control","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":"Compensation (psychology); Bending; Context (archaeology); Acoustics; Computer science; Structural engineering; Physics; Engineering; Geology; Psychology","score_opus":0.00962357532283285,"score_gpt":0.19989450836511763,"score_spread":0.1902709330422848,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2998012945","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":[0.29274783,0.0012434884,0.66773885,0.0008935856,0.00034824063,0.00003421813,0.000027967391,0.00030478602,0.036661122],"genre_scores_gemma":[0.9779829,0.00018856522,0.015551522,0.000046766596,0.00007342039,0.0000054193083,0.00001597716,0.00001838739,0.0061169434],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99983585,0.00003341303,0.0000037342943,0.000030774718,0.00007002627,0.000026143656],"domain_scores_gemma":[0.9997447,0.00012622008,0.00002089157,0.000019566198,0.00006845321,0.0000202444],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020966427,0.00023298652,0.0002288012,0.00013946748,0.0002596987,0.00046729104,0.00029668203,0.0005182143,0.0026710338],"category_scores_gemma":[0.0005736486,0.00006486986,0.000099598874,0.00018810765,0.00036667922,0.00039037957,0.00031572994,0.00037680147,0.00022699531],"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":[0.0010190103,0.00016077413,0.0010383783,0.00020535477,0.000026327203,0.0006309539,0.00020000192,0.14741977,0.6273429,0.036781207,0.0016786745,0.18349667],"study_design_scores_gemma":[0.000026134332,0.0002996363,0.0031400945,0.000035934743,0.000029937626,0.00043921985,0.00010470585,0.87906206,0.102380596,0.0094296625,0.0050228788,0.000029125888],"about_ca_topic_score_codex":0.0007730832,"about_ca_topic_score_gemma":0.0016177779,"teacher_disagreement_score":0.0026710338,"about_ca_system_score_codex":0.00019787719,"about_ca_system_score_gemma":0.00021030055,"threshold_uncertainty_score":0.008935511},"labels":[],"label_agreement":null},{"id":"W3000022936","doi":"10.1016/j.mechmachtheory.2019.103767","title":"Design and analysis of a configuration-based lengthwise morphing structure","year":2020,"lang":"en","type":"article","venue":"Mechanism and Machine Theory","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":35,"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; Shanghai University","keywords":"Morphing; Statics; Truss; Actuator; Wing; Structural engineering; Statically indeterminate; Computer science; Mechanism (biology); Planar; Airfoil; Engineering; Artificial intelligence","score_opus":0.011067051661997687,"score_gpt":0.18867396460609628,"score_spread":0.17760691294409858,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3000022936","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":[0.07436238,0.0001570991,0.91474545,0.00010184693,0.00003815299,0.00010741925,0.000043604716,0.0004477023,0.009996432],"genre_scores_gemma":[0.85602087,0.000101634134,0.14060941,0.00003848843,0.000012306606,0.00010228318,0.0000533788,0.000037022015,0.0030246314],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99991906,0.000011517291,0.00000314131,0.00001695315,0.00004072217,0.000008612612],"domain_scores_gemma":[0.9999118,0.000015868616,0.000022829769,0.00001809381,0.000022017488,0.000009342052],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012888883,0.00024687388,0.00031853173,0.00029016775,0.00023905718,0.00032891775,0.00084352435,0.00046901227,0.0021934896],"category_scores_gemma":[0.00019918976,0.00017302878,0.00026226058,0.000163748,0.00032887948,0.00022699445,0.00040290656,0.0002627341,0.00032002083],"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":[0.00010776713,0.00008625992,0.0011795512,0.00016784584,0.000050421648,0.00022656046,0.00007461629,0.6326115,0.21436423,0.0311526,0.00067188236,0.11930673],"study_design_scores_gemma":[0.000015401774,0.00026730934,0.0009104952,0.000007313718,0.000017426803,0.00012866387,0.000011842242,0.98576593,0.008769493,0.001436762,0.002659421,0.00000995158],"about_ca_topic_score_codex":0.00051882793,"about_ca_topic_score_gemma":0.0005552156,"teacher_disagreement_score":0.0021934896,"about_ca_system_score_codex":0.00024286509,"about_ca_system_score_gemma":0.00039202103,"threshold_uncertainty_score":0.007337928},"labels":[],"label_agreement":null},{"id":"W3009338800","doi":"10.1017/aer.2020.19","title":"Comparison and analyses of a variable span-morphing of the tapered wing with a varying sweep angle","year":2020,"lang":"en","type":"article","venue":"The Aeronautical Journal","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":28,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure","funders":"","keywords":"Chord (peer-to-peer); Wing; Wing twist; Airfoil; Swept wing; Angle of attack; Morphing; Camber (aerodynamics); Aerodynamics; Wing configuration; Lift-to-drag ratio; Span (engineering); Structural engineering; Stall (fluid mechanics); Lift coefficient; Wingspan; Wing loading; Aircraft flight mechanics; Aerospace engineering; Computer science; Engineering; Physics; Mechanics; Reynolds number","score_opus":0.05050215976025912,"score_gpt":0.2749531818509068,"score_spread":0.22445102209064766,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3009338800","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":[0.9817493,0.00017915788,0.015572953,0.000013079618,0.000010222521,0.000024787776,0.000061024733,0.000076891585,0.0023126577],"genre_scores_gemma":[0.9961671,0.000037770405,0.0032819742,0.0000025007714,0.0000011823154,0.000006064072,0.000036499394,0.0000071652435,0.00045966712],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998697,0.000019299077,0.000007894106,0.000019480423,0.000064871914,0.000018827131],"domain_scores_gemma":[0.999785,0.000056682224,0.00005249768,0.000039537445,0.000052866853,0.000013388369],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015497024,0.00022328028,0.00013149642,0.0003464324,0.00009704403,0.00020631858,0.00016890751,0.00014991057,0.000943266],"category_scores_gemma":[0.00029180234,0.00007455103,0.00028574697,0.0001390085,0.00011721672,0.00013141143,0.00012381488,0.000094342344,0.000107016574],"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":[0.0007137599,0.00012308331,0.013630367,0.00047764974,0.000091174086,0.00046198064,0.00016064929,0.2257041,0.6409005,0.0007392715,0.00032245647,0.11667507],"study_design_scores_gemma":[0.000054531374,0.005509163,0.08160443,0.000051974785,0.00018057518,0.00059324555,0.00026259155,0.52191657,0.38234305,0.00033053398,0.007103979,0.000049418013],"about_ca_topic_score_codex":0.00039401706,"about_ca_topic_score_gemma":0.0004477717,"teacher_disagreement_score":0.000943266,"about_ca_system_score_codex":0.000109052366,"about_ca_system_score_gemma":0.00009305733,"threshold_uncertainty_score":0.003155589},"labels":[],"label_agreement":null},{"id":"W3009620080","doi":"10.22215/etd/2009-06676","title":"Dynamics of elastic nonlinear rotating composite beams with embedded actuators","year":2009,"lang":"en","type":"dissertation","venue":"","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":14,"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; Library and Archives Canada","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Dynamics (music); Actuator; Nonlinear system; Physics; Humanities; Engineering; Mechanical engineering; Electrical engineering; Art; Acoustics; Quantum mechanics","score_opus":0.0037300289273209395,"score_gpt":0.20999604004965558,"score_spread":0.20626601112233464,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3009620080","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":[0.8803627,0.00038789146,0.088110715,0.00052106776,0.00015357792,0.000038486054,0.00010260912,0.000134042,0.030188916],"genre_scores_gemma":[0.9766948,0.00021218373,0.005620074,0.00004219019,0.00002153274,0.000024497998,0.000044008466,0.00002198065,0.0173186],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999528,0.0000075416738,0.0000015484244,0.000007995787,0.00002154749,0.000008597089],"domain_scores_gemma":[0.9998797,0.00002877067,0.00002993754,0.0000094876505,0.000025016925,0.00002703079],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015071263,0.00023773771,0.00020026937,0.00024465186,0.00026696434,0.0004251561,0.00030107153,0.00034461802,0.0034979645],"category_scores_gemma":[0.00034803644,0.00018283531,0.00017618181,0.00014222122,0.00043112694,0.0004452806,0.0005341962,0.00032061388,0.00037388026],"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":[0.0004362462,0.00013480577,0.0027271796,0.000095118994,0.00006429699,0.0005287229,0.00031963192,0.7872576,0.1286483,0.04832085,0.001886843,0.029580353],"study_design_scores_gemma":[0.000019888006,0.00009531734,0.002553454,0.0000056258605,0.0000049502564,0.00004566895,0.000055726625,0.99012333,0.0034769839,0.0025367732,0.0010665043,0.00001573442],"about_ca_topic_score_codex":0.0016044229,"about_ca_topic_score_gemma":0.0015077471,"teacher_disagreement_score":0.0034979645,"about_ca_system_score_codex":0.0002261567,"about_ca_system_score_gemma":0.00025842592,"threshold_uncertainty_score":0.011701822},"labels":[],"label_agreement":null},{"id":"W3009827646","doi":"10.22215/etd/2012-06728","title":"Control-centric modelling and nonlinear control of the blade sailing phenomenon","year":2012,"lang":"en","type":"dissertation","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Carleton University; Canadian Heritage; Library and Archives Canada","funders":"","keywords":"Phenomenon; Control (management); Blade (archaeology); Humanities; Engineering; Telecommunications; Computer science; Art; Mechanical engineering; Philosophy; Artificial intelligence; Epistemology","score_opus":0.007608936918416129,"score_gpt":0.19147591164719133,"score_spread":0.1838669747287752,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3009827646","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":[0.14733866,0.0006830205,0.8283911,0.0004222073,0.00016343649,0.000053975004,0.00006216017,0.00022796473,0.02265754],"genre_scores_gemma":[0.9886227,0.00023933577,0.0056036105,0.0000143579955,0.000019409646,0.00002593602,0.000025941785,0.000018501341,0.005430133],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999182,0.000026229101,0.0000039873244,0.000013879594,0.00002610032,0.000011676693],"domain_scores_gemma":[0.9998878,0.000039131224,0.000020488938,0.000010699545,0.00003411345,0.000007785124],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024499756,0.0004641294,0.0004145261,0.00019023857,0.00030474487,0.00078338874,0.000439992,0.0004435369,0.0012483353],"category_scores_gemma":[0.00051097316,0.00022971336,0.00041923946,0.00016076794,0.000533976,0.0004617209,0.00045603001,0.000476198,0.00020167454],"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":[0.00005167179,0.000016481561,0.0002167501,0.000042879434,0.000012237291,0.000054905595,0.00007632299,0.97616196,0.0075781643,0.009496024,0.0002257917,0.0060668057],"study_design_scores_gemma":[0.0000021750413,0.000012451909,0.000110478315,0.0000015161808,0.000001481228,0.000003848826,0.000005318756,0.9986475,0.00029463888,0.0007337861,0.00018464742,0.0000022065856],"about_ca_topic_score_codex":0.007572625,"about_ca_topic_score_gemma":0.005077117,"teacher_disagreement_score":0.007572625,"about_ca_system_score_codex":0.00045386903,"about_ca_system_score_gemma":0.0004440287,"threshold_uncertainty_score":0.015057087},"labels":[],"label_agreement":null},{"id":"W3028272442","doi":"","title":"Contrôle actif de la forme de structures soumises à un chargement thermique à l'aide de piézocomposites","year":2007,"lang":"fr","type":"article","venue":"HAL (Le Centre pour la Communication Scientifique Directe)","topic":"Aeroelasticity and Vibration Control","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 Laval","funders":"","keywords":"Physics; Humanities; Philosophy","score_opus":0.007981866314615171,"score_gpt":0.21628628706467595,"score_spread":0.20830442075006078,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3028272442","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":[0.8314538,0.0002505809,0.16054364,0.00024548525,0.00016610473,0.00005231764,0.00003451425,0.00036938008,0.006884311],"genre_scores_gemma":[0.9883349,0.00008438829,0.0061302725,0.00002376944,0.000018367075,0.00003020829,0.000015146084,0.00002102978,0.0053418726],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997656,0.000037676185,0.0000056044087,0.00005080625,0.00011095507,0.00002934143],"domain_scores_gemma":[0.9994123,0.00035621546,0.0000584203,0.000038432343,0.00010225974,0.000032459313],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00035505238,0.0005230448,0.00028607133,0.00018589401,0.00029395995,0.00069649145,0.00030005944,0.0005669894,0.002161243],"category_scores_gemma":[0.00083841593,0.0001585609,0.00023960049,0.00007706706,0.00052406755,0.00028497292,0.00021529463,0.00041858235,0.00018265026],"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":[0.0007134747,0.00014663843,0.00051855674,0.00008211343,0.000022514083,0.00010019899,0.0001832601,0.044974037,0.9145926,0.0015092627,0.0002810874,0.036876235],"study_design_scores_gemma":[0.00012647382,0.0007683435,0.0072332695,0.000008857114,0.000020370942,0.000117384756,0.00006546787,0.4546617,0.5339828,0.00056461355,0.0024170638,0.000033706845],"about_ca_topic_score_codex":0.0027374248,"about_ca_topic_score_gemma":0.0022147254,"teacher_disagreement_score":0.0027374248,"about_ca_system_score_codex":0.00043991735,"about_ca_system_score_gemma":0.00021490618,"threshold_uncertainty_score":0.0072300434},"labels":[],"label_agreement":null},{"id":"W3046589153","doi":"10.22215/etd/2009-06257","title":"Modelling and attenuation feasibility of the aeroelastic response of active helicopter rotor systems during the engagement/disengagement phase of maritime operation","year":2009,"lang":"en","type":"dissertation","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Canadian Heritage; Library and Archives Canada","funders":"","keywords":"Disengagement theory; Aeroelasticity; Rotor (electric); Aeronautics; Engineering; Aerospace engineering; Attenuation; Helicopter rotor; Aerodynamics; Physics; Electrical engineering; Optics","score_opus":0.026482842301344,"score_gpt":0.27063844369765067,"score_spread":0.24415560139630665,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3046589153","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":[0.8837959,0.0001891354,0.1050757,0.00022336407,0.00004090847,0.0000593216,0.00016138837,0.0002553305,0.010198912],"genre_scores_gemma":[0.99743795,0.000037903916,0.0010797929,0.0000038114822,0.000003128854,0.000012710395,0.00004758534,0.000012134151,0.0013650121],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99992514,0.000017878323,0.000003898296,0.000016758378,0.000018629096,0.000017661407],"domain_scores_gemma":[0.9997092,0.00016714998,0.000026587699,0.000018026167,0.00006153146,0.000017537717],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00022372419,0.0005143826,0.0002507458,0.00022729482,0.00031094058,0.0006487531,0.00035066635,0.00082142773,0.0018050926],"category_scores_gemma":[0.0010184917,0.000256365,0.00043304492,0.00010962936,0.00029108187,0.00045854234,0.0002733696,0.000554625,0.0003322357],"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":[0.00022126798,0.00008062703,0.0017184964,0.000052810585,0.00001627856,0.00008948326,0.0001159478,0.971141,0.017896904,0.0005265208,0.00021061071,0.007930141],"study_design_scores_gemma":[0.0000051090706,0.000038791535,0.0007006223,0.000002618677,0.0000036936733,0.0000058290357,0.000020020627,0.9975931,0.0014566123,0.00007804335,0.00009267002,0.0000029837374],"about_ca_topic_score_codex":0.017106414,"about_ca_topic_score_gemma":0.007447167,"teacher_disagreement_score":0.017106414,"about_ca_system_score_codex":0.0002834366,"about_ca_system_score_gemma":0.0004273983,"threshold_uncertainty_score":0.03401369},"labels":[],"label_agreement":null},{"id":"W3084409283","doi":"10.32393/csme.2020.1215","title":"Experimental Testing, Modeling, and Simulation of 3D Printed Composite Material for Morphing Wing Application","year":2020,"lang":"en","type":"article","venue":"Progress in Canadian Mechanical Engineering. Volume 3","topic":"Aeroelasticity and Vibration Control","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":"National Research Council Canada; Concordia University","funders":"National Research Council Canada","keywords":"Morphing; 3d printed; Wing; Composite number; Computer science; Engineering drawing; Mechanical engineering; Structural engineering; Computer graphics (images); Engineering; Manufacturing engineering","score_opus":0.015798842049679292,"score_gpt":0.23168238096515797,"score_spread":0.21588353891547868,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3084409283","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":[0.91078573,0.0001778493,0.07724877,0.000070348375,0.000045535046,0.000112852926,0.00050761865,0.00060068176,0.010450652],"genre_scores_gemma":[0.9756429,0.000105899155,0.022561517,0.000010232016,0.0000035216428,0.00006762231,0.0001233942,0.00002393119,0.0014609179],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99983203,0.000020143096,0.000007311017,0.000020937397,0.000105027284,0.00001455226],"domain_scores_gemma":[0.9997768,0.00008860875,0.000029379673,0.000049511975,0.000045792407,0.000009961709],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00026350425,0.00031171643,0.0001678026,0.0002320178,0.00017123618,0.000336003,0.0005001592,0.0005599201,0.0018849372],"category_scores_gemma":[0.00038509854,0.00017413672,0.00030295664,0.00017900458,0.00032034406,0.00023253358,0.00017170346,0.0002299119,0.00027111042],"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":[0.00013810373,0.00013739475,0.0025365774,0.0001934054,0.000015289395,0.00028626568,0.00011533828,0.712756,0.26158053,0.0009150194,0.0003151604,0.021010995],"study_design_scores_gemma":[0.000014695692,0.00036141954,0.0039044835,0.000010211339,0.000011335955,0.000073796655,0.000034423163,0.8702499,0.123785324,0.00017066066,0.001367916,0.000015848607],"about_ca_topic_score_codex":0.0013854073,"about_ca_topic_score_gemma":0.0018470945,"teacher_disagreement_score":0.0018849372,"about_ca_system_score_codex":0.00032563755,"about_ca_system_score_gemma":0.00026556203,"threshold_uncertainty_score":0.006305754},"labels":[],"label_agreement":null},{"id":"W3085266538","doi":"10.1177/1045389x20953907","title":"Development of a hybrid (rigid-flexible) morphing leading edge equipped with bending and extending capabilities","year":2020,"lang":"en","type":"article","venue":"Journal of Intelligent Material Systems and Structures","topic":"Aeroelasticity and Vibration Control","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":"National Research Council Canada","funders":"","keywords":"Morphing; Camber (aerodynamics); Finite element method; Airfoil; Wing; Aerodynamics; Engineering; Structural engineering; Chord (peer-to-peer); Computer science; Mechanical engineering; Aerospace engineering; Artificial intelligence","score_opus":0.020413121133600477,"score_gpt":0.22438469597796337,"score_spread":0.2039715748443629,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3085266538","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":[0.14663711,0.00024766047,0.822404,0.00015741837,0.00014181407,0.00023237518,0.00032946107,0.001905064,0.027945036],"genre_scores_gemma":[0.70395845,0.00032494904,0.27676997,0.0000823942,0.00001497325,0.00027040712,0.0004973344,0.00017448426,0.017907012],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99992716,0.000005324403,0.0000028358388,0.0000110304745,0.000040919836,0.000012741265],"domain_scores_gemma":[0.9999336,0.000012369705,0.00000911384,0.000018855379,0.000014624836,0.000011415084],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012387287,0.00024130478,0.00023481587,0.00015917973,0.00020298618,0.00047268588,0.0008768887,0.0006094554,0.003809619],"category_scores_gemma":[0.00014504069,0.00017668735,0.0004272857,0.000089808986,0.00027063317,0.0003921511,0.0004576247,0.00042773274,0.0011699493],"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":[0.00014939354,0.00018245957,0.0017832293,0.00032638284,0.00004130381,0.00077681174,0.00013053285,0.60376066,0.28670675,0.027854359,0.001818383,0.07646978],"study_design_scores_gemma":[0.00004007862,0.0007214086,0.0009767223,0.000026815853,0.000023917113,0.00046116198,0.000040885705,0.8960888,0.07190872,0.0019149665,0.02775372,0.000042807376],"about_ca_topic_score_codex":0.0005233732,"about_ca_topic_score_gemma":0.00055713375,"teacher_disagreement_score":0.003809619,"about_ca_system_score_codex":0.000155337,"about_ca_system_score_gemma":0.0003990029,"threshold_uncertainty_score":0.012744486},"labels":[],"label_agreement":null},{"id":"W3099257955","doi":"10.3390/aerospace7110166","title":"On the Design of Aeroelastically Scaled Models of High Aspect-Ratio Wings","year":2020,"lang":"en","type":"article","venue":"Aerospace","topic":"Aeroelasticity and Vibration Control","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":"University of Victoria","funders":"","keywords":"Aeroelasticity; Flight envelope; Aerodynamics; Flutter; Wind tunnel; Aerospace engineering; Envelope (radar); Structural engineering; Wing; Engineering; Scaling; Drag; Aerodynamic force; Aspect ratio (aeronautics); Computer science; Physics; Mathematics","score_opus":0.022220227783274402,"score_gpt":0.1904168723755557,"score_spread":0.1681966445922813,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3099257955","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":[0.10241208,0.00063053105,0.8833616,0.00022102482,0.00007580814,0.00023532052,0.00027550748,0.00035854476,0.0124296835],"genre_scores_gemma":[0.8351467,0.00095971767,0.15758151,0.00007985837,0.00003825936,0.00058378384,0.0004998918,0.00014696078,0.004963281],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998838,0.00003946499,0.000006303538,0.000018372537,0.00004046658,0.000011701428],"domain_scores_gemma":[0.99973935,0.000116445764,0.000052396048,0.000032977394,0.000042318097,0.000016528522],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00034544762,0.00074743904,0.0006676033,0.0003488714,0.00026095807,0.0006954282,0.0006789474,0.0008691293,0.0017845469],"category_scores_gemma":[0.0008339413,0.00038703994,0.0008520043,0.0002167936,0.0005860464,0.00041527502,0.00041542563,0.0006030213,0.0003669275],"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":[0.00001006942,0.000014758281,0.00015968994,0.000047912967,0.000007764788,0.00003582726,0.000019523766,0.99014854,0.003910345,0.002600376,0.00009042164,0.0029548293],"study_design_scores_gemma":[0.0000044904627,0.00001787404,0.00006096953,0.0000060257235,0.0000027143076,0.000008206793,0.000004521373,0.9985392,0.00040481114,0.00042083065,0.00052781194,0.0000025364295],"about_ca_topic_score_codex":0.0028281342,"about_ca_topic_score_gemma":0.002934656,"teacher_disagreement_score":0.0028281342,"about_ca_system_score_codex":0.00037341416,"about_ca_system_score_gemma":0.00064449984,"threshold_uncertainty_score":0.005969882},"labels":[],"label_agreement":null},{"id":"W3109470644","doi":"10.1201/9781003076155-141","title":"Modelling and Development of Procedures for Embedment of Piezoelectric Components into Composite","year":2020,"lang":"en","type":"book-chapter","venue":"","topic":"Aeroelasticity and Vibration Control","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":"National Research Council Canada; Université de Sherbrooke","funders":"","keywords":"Embedment; Composite number; Materials science; Piezoelectricity; Composite material","score_opus":0.025484315890237176,"score_gpt":0.21001240506126626,"score_spread":0.18452808917102909,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3109470644","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":[0.001754872,0.00007161602,0.9963946,0.000012194738,0.0000072246467,0.000033993623,0.000030486191,0.00024369317,0.001451314],"genre_scores_gemma":[0.054060027,0.00041819757,0.9394344,0.000011990494,0.0000071944714,0.00024335695,0.0001645116,0.00025615303,0.0054041273],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9997539,0.000035153476,0.000011712088,0.000038410955,0.00014522557,0.000015569713],"domain_scores_gemma":[0.99973375,0.00013232879,0.000026465681,0.000044937497,0.000055419692,0.000007050233],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005788741,0.0005896717,0.00048654308,0.0005073693,0.00034031091,0.00073947076,0.0015616303,0.0008684769,0.0027313617],"category_scores_gemma":[0.0010884928,0.0006531713,0.0007267112,0.0003554259,0.00053284987,0.00081922923,0.000585807,0.00089644035,0.0011683317],"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":[0.00001921274,0.000051016712,0.00031827512,0.00038707326,0.000021643946,0.00010523954,0.0001885921,0.8070175,0.032937467,0.07378453,0.00077299675,0.08439657],"study_design_scores_gemma":[0.000005369735,0.000029582308,0.000091903545,0.00003716339,0.000009447052,0.00008998933,0.000022640224,0.96091443,0.015082563,0.011408354,0.012294244,0.000014297188],"about_ca_topic_score_codex":0.0020599528,"about_ca_topic_score_gemma":0.0021075176,"teacher_disagreement_score":0.0027313617,"about_ca_system_score_codex":0.00053277897,"about_ca_system_score_gemma":0.0009039338,"threshold_uncertainty_score":0.009137273},"labels":[],"label_agreement":null},{"id":"W3109938030","doi":"10.1201/9781003076155-139","title":"Electromechanical Analysis of a Piezoelectric Instrumented Composite Bonded Repair Patch","year":2020,"lang":"en","type":"book-chapter","venue":"","topic":"Aeroelasticity and Vibration Control","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":"National Research Council Canada; Martec (Canada); Université de Sherbrooke","funders":"","keywords":"Piezoelectricity; Materials science; Composite number; Composite material; Structural engineering; Piezoelectric sensor; Engineering","score_opus":0.009278008834354189,"score_gpt":0.1899561661100393,"score_spread":0.1806781572756851,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3109938030","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":[0.881645,0.0006035991,0.11052767,0.00013529007,0.000054501492,0.000059129678,0.00010944116,0.00021750756,0.006647932],"genre_scores_gemma":[0.9700969,0.00026535956,0.022899885,0.000029979112,0.000011580894,0.000029442417,0.00007183616,0.000019810164,0.0065752235],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998958,0.000011219951,0.0000021579913,0.000021742417,0.00006323179,0.000005871581],"domain_scores_gemma":[0.99991727,0.000030436302,0.0000113795295,0.000017002927,0.000017014263,0.00000697317],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00013493189,0.00015946502,0.00025619738,0.00018780243,0.00012458884,0.00023669167,0.00049041025,0.00038474423,0.0012959667],"category_scores_gemma":[0.0002136281,0.00009827974,0.00014497085,0.000107193264,0.0003532715,0.00018810136,0.00020377272,0.00023626619,0.00034494014],"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":[0.00009241631,0.000069194044,0.0006803546,0.00010304084,0.000009036985,0.00039346438,0.0000753489,0.030165873,0.9523089,0.001003323,0.00019120035,0.014907792],"study_design_scores_gemma":[0.000031727915,0.0016767165,0.017020656,0.000025217418,0.000030076624,0.001174605,0.00029679667,0.57625574,0.39630216,0.0013225905,0.0058281124,0.000035532288],"about_ca_topic_score_codex":0.00022037173,"about_ca_topic_score_gemma":0.00021751726,"teacher_disagreement_score":0.0012959667,"about_ca_system_score_codex":0.00013158999,"about_ca_system_score_gemma":0.000111809066,"threshold_uncertainty_score":0.0043354034},"labels":[],"label_agreement":null},{"id":"W3111572758","doi":"10.13111/2066-8201.2020.12.4.2","title":"Artificial Neural Networks-Extended Great Deluge Model to predict Actuators Displacements for a Morphing Wing Tip System","year":2020,"lang":"en","type":"article","venue":"INCAS BULLETIN","topic":"Aeroelasticity and Vibration Control","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":"Université de Montréal; École de Technologie Supérieure; Polytechnique Montréal; Université du Québec à Montréal","funders":"Natural Sciences and Engineering Research Council of Canada; Consortium de Recherche et d’innovation en Aérospatiale au Québec","keywords":"Morphing; Actuator; Wing; Engineering; Structural engineering; Wing twist; Aerodynamics; Mechanical engineering; Acoustics; Angle of attack; Computer science; Aerospace engineering; Artificial intelligence","score_opus":0.02308531378960834,"score_gpt":0.22329714038234164,"score_spread":0.2002118265927333,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3111572758","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":[0.303328,0.0028709322,0.6725958,0.0012749195,0.00044606984,0.00021001193,0.000560941,0.0012727322,0.017440608],"genre_scores_gemma":[0.9744071,0.00034786967,0.01809913,0.0001240888,0.00003011481,0.00026046706,0.00029598217,0.000026437143,0.006408928],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99981624,0.000046137007,0.000016325064,0.00004992227,0.000035172234,0.000036214802],"domain_scores_gemma":[0.9994733,0.00031708498,0.000040619594,0.000010479119,0.00014082427,0.000017762963],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006403744,0.00087985897,0.0007382217,0.00050669705,0.00041269584,0.00086604664,0.00094721693,0.0016816949,0.002512809],"category_scores_gemma":[0.0012139804,0.00050198584,0.0006611894,0.0003278464,0.00051848707,0.00040667562,0.0006130344,0.001197684,0.00033493637],"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":[0.000025059464,0.000015000038,0.00038984357,0.000017724464,0.000014107341,0.000033778488,0.000010113745,0.99498427,0.00023484648,0.00026222612,0.0001295194,0.003883463],"study_design_scores_gemma":[0.0000010925454,0.0000044683084,0.000041506566,0.00000131455,0.0000012679841,9.1907003e-7,0.0000014013342,0.9998387,0.000031391453,0.00004628339,0.00003057996,8.9204457e-7],"about_ca_topic_score_codex":0.028745215,"about_ca_topic_score_gemma":0.0156368,"teacher_disagreement_score":0.028745215,"about_ca_system_score_codex":0.00093405356,"about_ca_system_score_gemma":0.00088594336,"threshold_uncertainty_score":0.057155788},"labels":[],"label_agreement":null},{"id":"W3115937263","doi":"10.18280/jesa.530608","title":"Proxy-Based Sliding Mode Vibration Control with an Adaptive Approximation Compensator for Euler-Bernoulli Smart Beams","year":2020,"lang":"en","type":"article","venue":"Journal Européen des Systèmes Automatisés","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":4,"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":"Control theory (sociology); PID controller; Timoshenko beam theory; Sliding mode control; Lyapunov stability; Vibration; Vibration control; Modal; Computer science; Beam (structure); Controller (irrigation); Mathematics; Control engineering; Engineering; Physics; Control (management); Acoustics; Nonlinear system; Structural engineering","score_opus":0.022389130502147497,"score_gpt":0.23118529654230455,"score_spread":0.20879616604015705,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3115937263","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":[0.040329818,0.00034469872,0.9566091,0.00006046084,0.00009347913,0.000031311436,0.000012851609,0.00031767527,0.0022006286],"genre_scores_gemma":[0.95289403,0.00018402084,0.044481587,0.000034905486,0.000022749527,0.000050738483,0.000023441766,0.000010678365,0.002297885],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99986637,0.000022957456,0.000009423788,0.000028051501,0.000059558242,0.00001355114],"domain_scores_gemma":[0.99989295,0.00002842561,0.000020975167,0.000016899181,0.00003270501,0.000008097613],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00027238147,0.00026357736,0.00023718053,0.00018852025,0.00015108573,0.00027642027,0.0004798058,0.0003115156,0.0009941582],"category_scores_gemma":[0.00030920442,0.00011670915,0.00023822056,0.00014217038,0.00028736432,0.0002268296,0.00035384318,0.00032040733,0.00011845034],"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":[0.0005439565,0.00011029727,0.0014572729,0.00031432204,0.00007415517,0.00025740516,0.00018346072,0.4690841,0.21659943,0.017444884,0.001593607,0.29233712],"study_design_scores_gemma":[0.000018721312,0.00018921275,0.00049186876,0.000008278846,0.000010753318,0.000033349654,0.000005257293,0.98736995,0.009780683,0.0005620329,0.0015209321,0.000009028075],"about_ca_topic_score_codex":0.0010114927,"about_ca_topic_score_gemma":0.0008687219,"teacher_disagreement_score":0.0010114927,"about_ca_system_score_codex":0.00020042562,"about_ca_system_score_gemma":0.0002312865,"threshold_uncertainty_score":0.0033257604},"labels":[],"label_agreement":null},{"id":"W3133197453","doi":"10.3390/app11041664","title":"Aerodynamic Design Optimization of a Morphing Leading Edge and Trailing Edge Airfoil–Application on the UAS-S45","year":2021,"lang":"en","type":"article","venue":"Applied Sciences","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":43,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure; Université du Québec à Montréal","funders":"","keywords":"Airfoil; Aerodynamics; Trailing edge; Lift coefficient; Aerospace engineering; Computer science; Leading edge; Solver; Engineering; Mathematics; Mathematical optimization; Turbulence; Structural engineering; Physics; Mechanics","score_opus":0.023181921198107285,"score_gpt":0.21977414338116122,"score_spread":0.19659222218305394,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3133197453","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":[0.5076621,0.00033154053,0.48182282,0.00011903993,0.000049682556,0.000111978996,0.00008840781,0.00027478844,0.009539713],"genre_scores_gemma":[0.93174183,0.00008741824,0.06650817,0.000017907292,0.0000068602576,0.000058501515,0.00005980568,0.00002888855,0.0014905414],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999255,0.000013272674,0.0000035860337,0.000013989061,0.000029570112,0.000014062254],"domain_scores_gemma":[0.9999399,0.000017068296,0.000009612122,0.0000059287395,0.000019770097,0.000007611345],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020071688,0.00037346652,0.0003109198,0.00022048272,0.0002341077,0.00032884438,0.00030732204,0.00039792582,0.0007798177],"category_scores_gemma":[0.00022266206,0.00015592526,0.00040454726,0.00011597993,0.00021955738,0.00017358584,0.0002586416,0.0002654104,0.00011644014],"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":[0.00007542025,0.00004591165,0.001486866,0.00010175168,0.000018195324,0.000114902505,0.00004310196,0.9208434,0.04182665,0.0018951098,0.00025371573,0.033294972],"study_design_scores_gemma":[0.000012635629,0.000105632396,0.0006376308,0.0000042893507,0.0000064389183,0.000034281133,0.000016032176,0.9929126,0.005190439,0.00016866604,0.0009061545,0.0000051895304],"about_ca_topic_score_codex":0.002673713,"about_ca_topic_score_gemma":0.0024795437,"teacher_disagreement_score":0.002673713,"about_ca_system_score_codex":0.00024052084,"about_ca_system_score_gemma":0.0005620503,"threshold_uncertainty_score":0.0053162575},"labels":[],"label_agreement":null},{"id":"W3149158800","doi":"","title":"ACTIVE VIBRATION SUPPRESSION VIA LINEARIZING HYSTERESIS OF PIEZOCERAMIC ACTUATORS","year":2007,"lang":"en","type":"article","venue":"机械工程学报(英文版)","topic":"Aeroelasticity and Vibration Control","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 Toronto","funders":"","keywords":"Cantilever; Control theory (sociology); Active vibration control; Actuator; Vibration; Hysteresis; Controller (irrigation); Vibration control; Beam (structure); Lyapunov function; Compensation (psychology); Engineering; Structural engineering; Physics; Acoustics; Computer science; Nonlinear system; Control (management)","score_opus":0.006681706589095959,"score_gpt":0.21297320013897153,"score_spread":0.20629149354987558,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3149158800","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":[0.25565028,0.0009375519,0.73883986,0.0001133557,0.000053379077,0.00003352169,0.000025693467,0.00081785215,0.003528505],"genre_scores_gemma":[0.95960766,0.00018222588,0.03878476,0.000022593313,0.000018639208,0.000023329294,0.000016645876,0.00001571301,0.0013284509],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999268,0.000009252639,0.0000037786351,0.000017496543,0.000032244472,0.000010322045],"domain_scores_gemma":[0.99988186,0.000058677906,0.000020279103,0.000014038755,0.000018990087,0.0000062287213],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0000911024,0.00020963069,0.00014731906,0.000109512344,0.000104968625,0.0001648781,0.00039683652,0.0001430502,0.000751504],"category_scores_gemma":[0.00021879065,0.00009612184,0.00008745853,0.00007749368,0.000246546,0.00024280213,0.00026014526,0.00023273076,0.00011152008],"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":[0.00010236619,0.000033519587,0.00024691847,0.000096913456,0.000008100053,0.00006633101,0.00010544697,0.007191235,0.9114439,0.0028417597,0.00017595214,0.077687554],"study_design_scores_gemma":[0.000057604833,0.00059937866,0.0015083012,0.000021291868,0.0000250106,0.00035276063,0.0000617533,0.2944794,0.6946682,0.0024272522,0.005774856,0.000024151479],"about_ca_topic_score_codex":0.00023999557,"about_ca_topic_score_gemma":0.00029858522,"teacher_disagreement_score":0.000751504,"about_ca_system_score_codex":0.00008903413,"about_ca_system_score_gemma":0.00009556908,"threshold_uncertainty_score":0.0025140047},"labels":[],"label_agreement":null},{"id":"W3163944649","doi":"10.1007/s10443-021-09886-y","title":"Applied Finite Element Procedure for Morphing Wing Design","year":2021,"lang":"en","type":"article","venue":"Applied Composite Materials","topic":"Aeroelasticity and Vibration Control","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":"Memorial University of Newfoundland","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Finite element method; Buckling; Morphing; Structural engineering; Bifurcation; Bistability; Nonlinear system; Wing; Computer science; Mathematics; Materials science; Engineering","score_opus":0.016085180458160965,"score_gpt":0.2082372200533522,"score_spread":0.19215203959519125,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3163944649","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":[0.0020705725,0.000016933856,0.9931126,0.000031269225,0.00003654551,0.00004381886,0.000053884913,0.00015273457,0.004481695],"genre_scores_gemma":[0.09256616,0.00010126739,0.88980216,0.000109406385,0.000028438424,0.0005038927,0.00022996395,0.00034780806,0.016310817],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99983835,0.00004092752,0.000007327613,0.000017453849,0.000083145926,0.000012749565],"domain_scores_gemma":[0.9997842,0.00006501681,0.000010363772,0.000030185347,0.000103591534,0.000006711716],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004092406,0.00039779174,0.00037784624,0.00058275694,0.00034713608,0.0003787942,0.0009129212,0.0005939685,0.0121143535],"category_scores_gemma":[0.00085974234,0.00023632748,0.0004418744,0.00039279167,0.0003247868,0.00027359018,0.00056738895,0.0008703716,0.0024215311],"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":[0.00009818294,0.00015684399,0.00062899705,0.00036238748,0.000061282786,0.00020214567,0.00021479616,0.49637035,0.04640356,0.12931621,0.005782809,0.32040238],"study_design_scores_gemma":[0.00001992089,0.00004234392,0.0001812221,0.000022093924,0.0000119853685,0.000070388596,0.000026321442,0.9579992,0.0073703267,0.014907991,0.019338705,0.0000095465875],"about_ca_topic_score_codex":0.0014153422,"about_ca_topic_score_gemma":0.0021551976,"teacher_disagreement_score":0.0121143535,"about_ca_system_score_codex":0.00020519481,"about_ca_system_score_gemma":0.00073949195,"threshold_uncertainty_score":0.04052651},"labels":[],"label_agreement":null},{"id":"W3199049970","doi":"10.2514/1.j060089","title":"Aeroservoelasticity of an Airfoil with Parametric Uncertainty and Subjected to Atmospheric Gusts","year":2021,"lang":"en","type":"article","venue":"AIAA Journal","topic":"Aeroelasticity and Vibration Control","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":"Concordia University","funders":"","keywords":"Airfoil; Flutter; Control theory (sociology); Controller (irrigation); Stiffness; Nonlinear system; Parametric statistics; Aerodynamics; Mathematics; Engineering; Physics; Mechanics; Structural engineering; Computer science","score_opus":0.004603551724389759,"score_gpt":0.19118306494666162,"score_spread":0.18657951322227187,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3199049970","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":[0.9101285,0.00019152221,0.085911244,0.00019055243,0.000033811026,0.000016670432,0.00003369579,0.00010297684,0.0033910281],"genre_scores_gemma":[0.9995059,0.000015817795,0.0002913929,0.0000039521115,0.0000022042275,0.0000030100991,0.0000043402097,9.768671e-7,0.00017251422],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998996,0.000017515233,0.000004182869,0.00001907017,0.00003155747,0.000028049546],"domain_scores_gemma":[0.99985135,0.000054906683,0.000046284327,0.00000972629,0.00002538926,0.000012361187],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001661246,0.00041075674,0.0003253468,0.00015502154,0.0004222176,0.00031053944,0.00022524319,0.0005156145,0.0002771729],"category_scores_gemma":[0.0004387667,0.00013964991,0.00029352782,0.00007880586,0.00051669887,0.0002494653,0.0005665446,0.0002967253,0.000023184823],"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":[0.0001538675,0.000024216582,0.0038197462,0.000068040135,0.0000381442,0.0008920541,0.00019842328,0.95336294,0.032522317,0.0015634618,0.00017307926,0.0071837297],"study_design_scores_gemma":[0.0000042302,0.00005902769,0.0020132053,0.0000020640643,0.0000067727524,0.00003496388,0.00003312875,0.99645317,0.0011011924,0.00020183668,0.000085819935,0.0000046659156],"about_ca_topic_score_codex":0.008435837,"about_ca_topic_score_gemma":0.003437186,"teacher_disagreement_score":0.008435837,"about_ca_system_score_codex":0.00020545229,"about_ca_system_score_gemma":0.000250681,"threshold_uncertainty_score":0.016773462},"labels":[],"label_agreement":null},{"id":"W3210866300","doi":"10.32920/ryerson.14645931.v1","title":"Aerodynamic aspects in the development of morphing winglet for a regional aircraft","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Toronto Metropolitan University","funders":"","keywords":"Wingtip device; Morphing; Stall (fluid mechanics); Wing; Bending moment; Lift-induced drag; Drag; Aerodynamics; Structural engineering; Pitching moment; Camber (aerodynamics); Lift-to-drag ratio; Aerospace engineering; Engineering; Computer science; Angle of attack","score_opus":0.028047171475281286,"score_gpt":0.23929731517533837,"score_spread":0.21125014370005707,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3210866300","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":[0.93502486,0.00037698785,0.05746852,0.000070634174,0.00002777483,0.00003745629,0.000056643894,0.00012488598,0.0068123075],"genre_scores_gemma":[0.9848466,0.00011586744,0.0138659105,0.00000963321,0.0000055352216,0.0000060133166,0.000038715796,0.000014094813,0.0010977607],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99993503,0.000010476784,0.0000031530833,0.00001211997,0.000024700723,0.000014583464],"domain_scores_gemma":[0.99992955,0.000013466168,0.000016936263,0.000013362788,0.000017978904,0.000008650404],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012749959,0.00018353818,0.000104225655,0.00013667552,0.00010244521,0.00019745709,0.00016979566,0.00013097409,0.0008570612],"category_scores_gemma":[0.00015825851,0.00006614392,0.00027599733,0.000077565244,0.000109304005,0.00013432968,0.00016273826,0.00014841602,0.00016478647],"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":[0.00016947495,0.00004281252,0.009787994,0.00012767411,0.000027599934,0.00063861045,0.000094752926,0.11206213,0.8088542,0.0029951276,0.00028805024,0.064911574],"study_design_scores_gemma":[0.000027156622,0.003135504,0.09073865,0.000031167307,0.00012770847,0.0018673457,0.00023252795,0.607298,0.2828395,0.00090041134,0.0127562955,0.000045750625],"about_ca_topic_score_codex":0.0004994322,"about_ca_topic_score_gemma":0.0008396883,"teacher_disagreement_score":0.0008570612,"about_ca_system_score_codex":0.00011881108,"about_ca_system_score_gemma":0.0000834997,"threshold_uncertainty_score":0.0028671622},"labels":[],"label_agreement":null},{"id":"W3212643166","doi":"10.3390/app112210631","title":"Experimental Validation and Evaluation of a Coupled Twist-Camber Morphing Wing Concept","year":2021,"lang":"en","type":"article","venue":"Applied Sciences","topic":"Aeroelasticity and Vibration Control","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 Victoria","funders":"","keywords":"Camber (aerodynamics); Airfoil; Wing; Wing twist; Morphing; Lift-to-drag ratio; Lift-induced drag; Drag; Structural engineering; Wing loading; Lift (data mining); Aerodynamics; Aerospace engineering; Lift coefficient; Angle of attack; Engineering; Computer science; Mechanics; Physics","score_opus":0.03362233106322447,"score_gpt":0.2772199569730331,"score_spread":0.2435976259098086,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3212643166","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":[0.9620304,0.00020937299,0.034491744,0.00005830597,0.000106488864,0.00027997332,0.00017483879,0.00020928815,0.0024394917],"genre_scores_gemma":[0.9741219,0.00012219937,0.024146205,0.000017608936,0.000008652272,0.00011222962,0.000090146445,0.000019533669,0.0013614156],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.999754,0.000023796561,0.000013359792,0.000043645945,0.00012665847,0.00003847461],"domain_scores_gemma":[0.99953496,0.00007494927,0.00007950426,0.00012595035,0.00011965238,0.00006506857],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00060921843,0.00044401368,0.00022758216,0.00031205005,0.0001983345,0.0002652313,0.0005604783,0.00052315946,0.001690145],"category_scores_gemma":[0.00059476413,0.00010954807,0.00021127754,0.00013538722,0.00042844587,0.00033909484,0.0003767905,0.0003033124,0.00024719493],"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":[0.0001895441,0.00024639937,0.0007636446,0.00022685241,0.000009531107,0.00017996096,0.0001203341,0.0055992967,0.97750014,0.00072575326,0.00019989435,0.014238629],"study_design_scores_gemma":[0.00012646205,0.014699182,0.0120545635,0.00005531714,0.000042275664,0.0005287263,0.00018437236,0.044741027,0.9183035,0.00035999584,0.008850051,0.000054549713],"about_ca_topic_score_codex":0.00016657794,"about_ca_topic_score_gemma":0.00017831143,"teacher_disagreement_score":0.001690145,"about_ca_system_score_codex":0.00012240023,"about_ca_system_score_gemma":0.00018941809,"threshold_uncertainty_score":0.0056540966},"labels":[],"label_agreement":null},{"id":"W3214540259","doi":"10.1115/imece2000-1711","title":"Wind-Tunnel Determination of Aeroelastic Response of Piezoelectric and Aileron Controlled 3-D Wing","year":2000,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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 Victoria","funders":"","keywords":"Aileron; Aeroelasticity; Wing; Wind tunnel; Structural engineering; Aerodynamics; Actuator; Vibration; Flight control surfaces; Elevator; Vibration control; Engineering; Wing configuration; Aerospace engineering; Acoustics; Physics","score_opus":0.006325275029498996,"score_gpt":0.1979177000483595,"score_spread":0.1915924250188605,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W3214540259","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":[0.9980253,0.00000686928,0.0017999677,0.000002666433,0.0000016967413,0.0000051554325,0.000018101213,0.000020175497,0.00012019265],"genre_scores_gemma":[0.9990631,0.0000057100365,0.00074708665,0.0000026198734,3.843551e-7,0.000005502392,0.000015063942,0.0000027877957,0.00015776017],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998847,0.00002104396,0.000006572024,0.000015109883,0.000047319656,0.00002528586],"domain_scores_gemma":[0.99966896,0.0001270806,0.00003711244,0.000035807043,0.00007794209,0.00005322498],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002496304,0.0002543906,0.0001306281,0.00014958202,0.00012657097,0.00014726457,0.00016865597,0.0002715546,0.0009648752],"category_scores_gemma":[0.00042452125,0.00009756625,0.00011649534,0.000055235887,0.0002509785,0.00013278896,0.00018210996,0.00017482799,0.0001008421],"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":[0.0003129737,0.00009141417,0.002255313,0.000031534186,0.0000067324117,0.000098659024,0.00007655544,0.006336267,0.9876109,0.000041652096,0.000026700158,0.0031113843],"study_design_scores_gemma":[0.00011024022,0.0049127527,0.052907247,0.000015210473,0.000017667051,0.00023146367,0.00024081224,0.08792957,0.8529517,0.000074556054,0.00057448656,0.000034337496],"about_ca_topic_score_codex":0.0004778516,"about_ca_topic_score_gemma":0.0005220148,"teacher_disagreement_score":0.0009648752,"about_ca_system_score_codex":0.00006719802,"about_ca_system_score_gemma":0.00008198646,"threshold_uncertainty_score":0.00322783},"labels":[],"label_agreement":null},{"id":"W4200018421","doi":"10.13111/2066-8201.2021.13.4.10","title":"Morphing Winglet Design for Aerodynamic Performance Optimization of the CRJ-700 Aircraft. Part 1 – Structural Design","year":2021,"lang":"en","type":"article","venue":"INCAS BULLETIN","topic":"Aeroelasticity and Vibration Control","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":"Carleton University; École de Technologie Supérieure","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Morphing; Wingtip device; Aerodynamics; Aerospace engineering; Software; Structural engineering; Wing; Computer science; Engineering; Simulation; Computer graphics (images)","score_opus":0.017309973476170904,"score_gpt":0.19582175839975033,"score_spread":0.17851178492357941,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4200018421","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":[0.19106337,0.00041558626,0.7866597,0.00009884534,0.000054590284,0.0001677447,0.00014838159,0.00038517494,0.021006577],"genre_scores_gemma":[0.7937233,0.00033765595,0.19975609,0.000037587983,0.000020380763,0.0001630549,0.00022397653,0.0001065602,0.005631465],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99990094,0.000017483379,0.0000031119127,0.000012914717,0.000054605327,0.0000109453285],"domain_scores_gemma":[0.99994004,0.0000124057215,0.000011955251,0.000009055073,0.000021443977,0.000005171859],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002055132,0.0003463074,0.00023503136,0.0003283322,0.00013371868,0.00030910538,0.00034434893,0.00029877,0.001948748],"category_scores_gemma":[0.0002098733,0.000143574,0.0003505166,0.00014668338,0.00017392333,0.00014796595,0.00021622531,0.0002393708,0.00036894085],"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":[0.00012553296,0.00008350559,0.0017302067,0.0002476058,0.000029469315,0.00018953065,0.0001179859,0.67096525,0.18775602,0.0070443666,0.0011891054,0.13052143],"study_design_scores_gemma":[0.000018855068,0.00049837,0.0021154985,0.000020265996,0.000026812975,0.00020073882,0.000041559808,0.9613441,0.02395637,0.0011371648,0.010627436,0.000012874285],"about_ca_topic_score_codex":0.0005710059,"about_ca_topic_score_gemma":0.00087411486,"teacher_disagreement_score":0.001948748,"about_ca_system_score_codex":0.00020051603,"about_ca_system_score_gemma":0.00028207386,"threshold_uncertainty_score":0.0065191984},"labels":[],"label_agreement":null},{"id":"W4200036809","doi":"10.13111/2066-8201.2021.13.4.11","title":"Structural Design and Control of a Morphing Winglet to optimize the Aerodynamic Performance of the CRJ-700 Aircraft. Part 2 – Control","year":2021,"lang":"en","type":"article","venue":"INCAS BULLETIN","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":2,"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; École de Technologie Supérieure","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Wingtip device; Morphing; Aerodynamics; Computer science; Wing; Aerospace engineering; Simulation; Engineering; Computer graphics (images)","score_opus":0.007356538329208504,"score_gpt":0.1757379186152094,"score_spread":0.1683813802860009,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4200036809","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":[0.28473365,0.00042124427,0.70376086,0.00008136067,0.0001030905,0.00016434303,0.00004558925,0.00034096275,0.010348896],"genre_scores_gemma":[0.96907973,0.000083722756,0.02947203,0.000016244534,0.000010843528,0.000043148393,0.000030919924,0.000009559473,0.001253773],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99992096,0.000008908907,0.0000038685894,0.000019994906,0.00003712158,0.000009289879],"domain_scores_gemma":[0.9999298,0.000011520006,0.000019232439,0.00000797619,0.00002438569,0.000007130826],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015747169,0.00024974442,0.0001287822,0.00016935504,0.00010536395,0.0002676254,0.000322234,0.00020228329,0.0007906232],"category_scores_gemma":[0.00013787151,0.00008004181,0.00017057179,0.000062204774,0.00013986901,0.000114733,0.00015030705,0.00017195102,0.00012303013],"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":[0.00028773118,0.00013745377,0.0014702487,0.00029161273,0.000035127323,0.00016697639,0.0000971573,0.19524433,0.67342055,0.004845461,0.0006270934,0.123376295],"study_design_scores_gemma":[0.000038500497,0.0012764342,0.0044071977,0.000017233175,0.000039264007,0.00014179052,0.000034153592,0.9138731,0.07449777,0.00046240538,0.005197394,0.000014786975],"about_ca_topic_score_codex":0.0005584706,"about_ca_topic_score_gemma":0.00058894657,"teacher_disagreement_score":0.0007906232,"about_ca_system_score_codex":0.00011942057,"about_ca_system_score_gemma":0.00016422146,"threshold_uncertainty_score":0.0026448965},"labels":[],"label_agreement":null},{"id":"W4205148641","doi":"10.2514/6.2022-2573","title":"Dynamic Loading of an Aircraft Morphing Winglet","year":2022,"lang":"en","type":"article","venue":"AIAA SCITECH 2022 Forum","topic":"Aeroelasticity and Vibration Control","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":"Wingtip device; Morphing; Aerospace engineering; Computer science; Aeronautics; Engineering; Wing; Computer graphics (images)","score_opus":0.005005165261035873,"score_gpt":0.20281565888441425,"score_spread":0.19781049362337838,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4205148641","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":[0.88224244,0.00013379812,0.09821974,0.00015766399,0.00015014032,0.00014715196,0.0003124386,0.0013188083,0.017317865],"genre_scores_gemma":[0.97794205,0.00004498453,0.01650344,0.000041559713,0.00000963216,0.000036917398,0.00017614238,0.000042252042,0.0052030687],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99992037,0.000006846801,0.000004114078,0.000016267924,0.000037559497,0.000014838636],"domain_scores_gemma":[0.99993575,0.000011929186,0.000008637392,0.000018459588,0.0000124704575,0.000012743987],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00010663266,0.00022516867,0.00016616707,0.00022054074,0.00023703155,0.00021244246,0.00034829136,0.00025689375,0.003901964],"category_scores_gemma":[0.00012632235,0.00009301617,0.00017888038,0.00005708886,0.00020725728,0.00021609772,0.00040162745,0.00016141738,0.00053704984],"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":[0.00026166413,0.00006563155,0.0016547209,0.00008979842,0.000011653067,0.00081243063,0.00013701872,0.013469212,0.92393243,0.0021060933,0.00129387,0.05616542],"study_design_scores_gemma":[0.000077110526,0.0019898014,0.01982899,0.000051693587,0.000035551024,0.0009491557,0.00025270504,0.38085145,0.56938493,0.0014519057,0.025056843,0.00006990254],"about_ca_topic_score_codex":0.00039600662,"about_ca_topic_score_gemma":0.0004186907,"teacher_disagreement_score":0.003901964,"about_ca_system_score_codex":0.00015504459,"about_ca_system_score_gemma":0.000110778274,"threshold_uncertainty_score":0.013053358},"labels":[],"label_agreement":null},{"id":"W4205272101","doi":"10.2514/6.2022-1041","title":"Aerodynamic Design and Performance Optimization of Camber Adaptive Winglet for the UAS-S45","year":2022,"lang":"en","type":"article","venue":"AIAA SCITECH 2022 Forum","topic":"Aeroelasticity and Vibration Control","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":"École de Technologie Supérieure","funders":"","keywords":"Wingtip device; Aileron; Lift-to-drag ratio; Camber (aerodynamics); Drag; Climb; Aerospace engineering; Aerodynamics; Lift-induced drag; NACA airfoil; Engineering; Computer science; Structural engineering; Physics; Mechanics; Turbulence; Reynolds number","score_opus":0.00967183357963023,"score_gpt":0.18593457537954214,"score_spread":0.17626274179991192,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4205272101","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":[0.7406935,0.00054595934,0.23557766,0.00020288215,0.00008713811,0.0001858638,0.00019626803,0.00034799628,0.022162661],"genre_scores_gemma":[0.94813627,0.00013899266,0.048354063,0.000023796969,0.0000072519842,0.000077364835,0.0000973058,0.000032976932,0.0031319212],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99990666,0.000016257742,0.0000039463916,0.000015005729,0.0000435799,0.000014528885],"domain_scores_gemma":[0.99989486,0.000027892987,0.000022102362,0.000011470098,0.000030476223,0.0000131905],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003331536,0.00037601189,0.00029028673,0.0003165078,0.00022836009,0.00047411435,0.00035277847,0.0004934124,0.0015643083],"category_scores_gemma":[0.00023854079,0.00016230792,0.00039537347,0.00016043228,0.00018028481,0.0001912062,0.0002495647,0.00023663526,0.00031599918],"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":[0.00031040327,0.000214313,0.0044706403,0.000293285,0.00004248469,0.0003714619,0.0001249209,0.7541413,0.16627431,0.0029721472,0.0013315345,0.06945325],"study_design_scores_gemma":[0.000022406848,0.00067249767,0.0023979272,0.000014210749,0.000012931053,0.00007689955,0.000042952666,0.97139174,0.022169858,0.00027041705,0.0029134105,0.000014749415],"about_ca_topic_score_codex":0.00084454217,"about_ca_topic_score_gemma":0.0009421832,"teacher_disagreement_score":0.0015643083,"about_ca_system_score_codex":0.000291524,"about_ca_system_score_gemma":0.00039564588,"threshold_uncertainty_score":0.005233109},"labels":[],"label_agreement":null},{"id":"W4206155864","doi":"10.2514/6.2021-2567","title":"Withdrawn: Numerical Study of the Boundary Layer Behavior on Morphing Trailing Edge Wing using intermittency Transition model","year":2021,"lang":"en","type":"article","venue":"AIAA AVIATION 2021 FORUM","topic":"Aeroelasticity and Vibration Control","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","funders":"","keywords":"Trailing edge; Morphing; Intermittency; Boundary layer; Wing; Leading edge; Mechanics; Aerospace engineering; Materials science; Computer science; Physics; Turbulence; Engineering; Computer graphics (images)","score_opus":0.02094061938598146,"score_gpt":0.24677171516028099,"score_spread":0.22583109577429952,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4206155864","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":[0.57650864,0.010754719,0.05315259,0.038510323,0.12200723,0.0009052034,0.04504455,0.0029907087,0.15012608],"genre_scores_gemma":[0.79255176,0.0035339457,0.019324066,0.0032364177,0.006110028,0.00023379359,0.026557261,0.00088685204,0.14756589],"study_design_codex":"not_applicable","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998342,0.00001831741,0.000018375833,0.000022561417,0.00008796509,0.000018546183],"domain_scores_gemma":[0.99847156,0.0003759184,0.00008894878,0.00009676252,0.0008205415,0.0001462583],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00032871962,0.0002634437,0.00036733257,0.00052856473,0.00052356184,0.00060040166,0.0009320408,0.00090564496,0.029300809],"category_scores_gemma":[0.0026926463,0.00009238342,0.00037245036,0.00072063203,0.00030998542,0.0005928241,0.00035667434,0.0005716463,0.0035660013],"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":[0.0037190004,0.00033272745,0.009151943,0.0026647937,0.00022717702,0.004472647,0.00034679807,0.04450948,0.085715696,0.025012512,0.665048,0.15879926],"study_design_scores_gemma":[0.0022118092,0.0014139689,0.11204587,0.00059834024,0.00036863412,0.0022322559,0.0008533922,0.39310524,0.066940464,0.022104278,0.39785278,0.0002729994],"about_ca_topic_score_codex":0.006631494,"about_ca_topic_score_gemma":0.003775876,"teacher_disagreement_score":0.029300809,"about_ca_system_score_codex":0.0003467149,"about_ca_system_score_gemma":0.0007715605,"threshold_uncertainty_score":0.09802097},"labels":[],"label_agreement":null},{"id":"W4210582370","doi":"10.1007/s00707-021-03138-7","title":"Aeroelastic behaviour of a flexible morphing wing design for unmanned aerial vehicle","year":2022,"lang":"en","type":"article","venue":"Acta Mechanica","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":7,"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":"Fonds de recherche du Québec – Nature et technologies; Natural Sciences and Engineering Research Council of Canada","keywords":"Aeroelasticity; Wing; Morphing; Aerodynamics; Aileron; Flight envelope; Aerospace engineering; Flight control surfaces; Flight dynamics; Aircraft flight mechanics; Stiffness; Aerodynamic force; Computer science; Rigid body dynamics; Structural engineering; Control theory (sociology); Engineering; Rigid body; Physics; Classical mechanics","score_opus":0.024952696482827726,"score_gpt":0.22515360664396872,"score_spread":0.200200910161141,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4210582370","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":[0.9670718,0.000086230124,0.029256668,0.000040573268,0.000009317775,0.000015059172,0.000021623398,0.00003459861,0.0034641067],"genre_scores_gemma":[0.9984384,0.000013608659,0.0010495759,0.0000026840007,9.213407e-7,0.0000032948255,0.00000780792,0.0000031843704,0.0004804997],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999471,0.0000124804865,0.0000018483463,0.00000717811,0.00002143041,0.000009851161],"domain_scores_gemma":[0.9999087,0.000031882402,0.000018809738,0.000008697598,0.00002284346,0.000009056429],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000100652935,0.00020191062,0.00014219356,0.00018716336,0.00016327917,0.00017390194,0.00014157945,0.00029145842,0.0010128254],"category_scores_gemma":[0.00023174407,0.00008849613,0.00022516567,0.00006833119,0.00014328172,0.0000939271,0.00012592848,0.00010129535,0.000095817275],"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":[0.00028833182,0.00006378095,0.0040069376,0.00010391782,0.00004216717,0.0003776805,0.00017669567,0.6887546,0.28112423,0.0007008553,0.0001869096,0.02417388],"study_design_scores_gemma":[0.000010874786,0.0005205358,0.008730545,0.000008477584,0.000026968595,0.000084764964,0.000088075656,0.9763417,0.0135261435,0.00014856581,0.0005047951,0.0000085343345],"about_ca_topic_score_codex":0.0018029904,"about_ca_topic_score_gemma":0.0014465407,"teacher_disagreement_score":0.0018029904,"about_ca_system_score_codex":0.00010307342,"about_ca_system_score_gemma":0.00011408279,"threshold_uncertainty_score":0.003584981},"labels":[],"label_agreement":null},{"id":"W4210621059","doi":"10.3390/designs6010010","title":"Optimization and Design of a Flexible Droop-Nose Leading-Edge Morphing Wing Based on a Novel Black Widow Optimization Algorithm—Part I","year":2022,"lang":"en","type":"article","venue":"Designs","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":19,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure; Université du Québec à Montréal","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Airfoil; Aerodynamics; Leading edge; Morphing; Wing; Computer science; Aerospace engineering; Solver; Engineering; Control theory (sociology); Mathematical optimization; Mathematics; Artificial intelligence","score_opus":0.0367619492630068,"score_gpt":0.22552029348425068,"score_spread":0.18875834422124388,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4210621059","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":[0.12295488,0.00026783333,0.87071764,0.00008440466,0.00004764536,0.0001288942,0.000054606924,0.00024863903,0.0054953923],"genre_scores_gemma":[0.7698654,0.00015722259,0.22676411,0.00004683727,0.000013331153,0.00022105472,0.000100786194,0.000060312384,0.002771075],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999267,0.000011720996,0.00000366249,0.000016774764,0.00002648046,0.000014653607],"domain_scores_gemma":[0.999946,0.0000145253825,0.000011271954,0.000006055514,0.00001477371,0.000007269784],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017793472,0.0003902313,0.00035685577,0.00025348194,0.0001920097,0.00042808804,0.0004086751,0.0004480761,0.0010230702],"category_scores_gemma":[0.00023716786,0.00020165608,0.0003742276,0.00016457605,0.00025845377,0.00021953184,0.00035760403,0.000268023,0.00015822108],"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":[0.00010014754,0.00005230661,0.0010667047,0.00009360246,0.000032805827,0.00010002623,0.00004374951,0.8957919,0.040600006,0.003943238,0.0004874543,0.057688005],"study_design_scores_gemma":[0.00000876635,0.00006545402,0.00023625272,0.0000035504986,0.000004405224,0.000019647707,0.000007702971,0.99621767,0.0026213003,0.00018542113,0.00062560965,0.0000042004885],"about_ca_topic_score_codex":0.0014104372,"about_ca_topic_score_gemma":0.0011752566,"teacher_disagreement_score":0.0014104372,"about_ca_system_score_codex":0.00019710626,"about_ca_system_score_gemma":0.00048085817,"threshold_uncertainty_score":0.0034225583},"labels":[],"label_agreement":null},{"id":"W4226410280","doi":"10.2514/1.c036710","title":"Flutter Predictions for Very Flexible Wing Wind Tunnel Test","year":2022,"lang":"en","type":"article","venue":"Journal of Aircraft","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":38,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Kensington Health","funders":"Engineering and Physical Sciences Research Council; PAZY Foundation","keywords":"Flutter; Aeroelasticity; Wing; Wind tunnel; Freestream; Aerodynamics; Structural engineering; Angle of attack; Nonlinear system; Engineering; Longitudinal static stability; Aerospace engineering; Mechanics; Physics; Reynolds number; Turbulence","score_opus":0.011955221345883558,"score_gpt":0.21546962379216233,"score_spread":0.20351440244627877,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4226410280","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":[0.92637926,0.00015699542,0.06538361,0.000104184706,0.000030202857,0.00010892909,0.00048541176,0.00029825926,0.0070533],"genre_scores_gemma":[0.9967417,0.000027513343,0.0023696395,0.000009734463,0.0000015969132,0.000032244552,0.00012473001,0.00001380898,0.00067903474],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998529,0.000024066409,0.000006953278,0.000015796599,0.00006434623,0.000035955],"domain_scores_gemma":[0.9994777,0.0002541025,0.000054418233,0.000042921078,0.00012977987,0.0000411451],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00053989707,0.00040916647,0.00028990343,0.00039687759,0.00026761138,0.0003744317,0.00058631063,0.0008195415,0.0020849302],"category_scores_gemma":[0.0015714773,0.00013905144,0.0003955882,0.000119767705,0.0003804307,0.00038843695,0.00034618314,0.00041797367,0.00030752516],"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":[0.00015187434,0.00007677974,0.0044415924,0.000058157148,0.000007003316,0.00019659923,0.00005303638,0.9598302,0.028561277,0.00096672354,0.00033308446,0.0053235637],"study_design_scores_gemma":[0.00000765091,0.00012129501,0.0014485657,0.000008977201,0.0000018737976,0.000022488628,0.000015747262,0.99428636,0.0037575911,0.00018365952,0.0001373893,0.000008313971],"about_ca_topic_score_codex":0.0037594244,"about_ca_topic_score_gemma":0.0025791505,"teacher_disagreement_score":0.0037594244,"about_ca_system_score_codex":0.00026634402,"about_ca_system_score_gemma":0.00035306512,"threshold_uncertainty_score":0.007475078},"labels":[],"label_agreement":null},{"id":"W4226487946","doi":"10.1007/978-3-030-99826-4_1","title":"Design, Synthesis, and Implementation of a Dynamic Loading Mechanism for Morphing Winglets","year":2022,"lang":"en","type":"book-chapter","venue":"Mechanisms and machine science","topic":"Aeroelasticity and Vibration Control","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":"Toronto Metropolitan University","funders":"","keywords":"Wingtip device; Morphing; Structural engineering; Mechanism (biology); Linkage (software); Wing; Engineering; Aerodynamics; Computer science; Aerospace engineering; Physics","score_opus":0.014555923928720373,"score_gpt":0.23337766784287237,"score_spread":0.218821743914152,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4226487946","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":[0.025957113,0.00016708742,0.96312743,0.00006204484,0.00007455954,0.00013605114,0.00006152802,0.001398623,0.0090155555],"genre_scores_gemma":[0.32545024,0.00023565834,0.6623479,0.000057748854,0.000025683592,0.00024141022,0.00017416089,0.00029036566,0.011176704],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998524,0.000011193814,0.0000090588055,0.000026955453,0.00008094162,0.000019398332],"domain_scores_gemma":[0.99986684,0.000030650688,0.000022676333,0.00003506583,0.000034727975,0.000010061833],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021991982,0.00043451306,0.00032788207,0.0003471275,0.0002868754,0.00048747894,0.0012403451,0.00065931986,0.0042826002],"category_scores_gemma":[0.00030197648,0.0003493993,0.000372962,0.00017688541,0.0003162617,0.00030288647,0.00052650366,0.0003968051,0.0010270879],"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":[0.00012435664,0.00012037861,0.0006018689,0.00040979832,0.00005391618,0.00030271956,0.00020076893,0.12272306,0.5720944,0.041605953,0.0023614783,0.25940135],"study_design_scores_gemma":[0.000115245006,0.0007819288,0.001615268,0.00007539364,0.00007709724,0.0006878638,0.00006921968,0.6967243,0.23560211,0.008404614,0.055797525,0.00004935183],"about_ca_topic_score_codex":0.00038153116,"about_ca_topic_score_gemma":0.0005213254,"teacher_disagreement_score":0.0042826002,"about_ca_system_score_codex":0.00019099137,"about_ca_system_score_gemma":0.00036476232,"threshold_uncertainty_score":0.014326692},"labels":[],"label_agreement":null},{"id":"W4226505870","doi":"10.3390/designs6020036","title":"Optimized Active Control of a Smart Cantilever Beam Using Genetic Algorithm","year":2022,"lang":"en","type":"article","venue":"Designs","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":19,"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 du Québec à Rimouski","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Cantilever; Actuator; Active vibration control; Genetic algorithm; Vibration; Control theory (sociology); Vibration control; PID controller; Beam (structure); Position (finance); Computer science; Engineering; Acoustics; Control engineering; Control (management); Structural engineering; Temperature control; Physics; Artificial intelligence","score_opus":0.021472555826633953,"score_gpt":0.21980658801466946,"score_spread":0.1983340321880355,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4226505870","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":[0.14147153,0.00039372212,0.8485746,0.00022995062,0.00006831257,0.00011075848,0.00004342435,0.00037096668,0.008736824],"genre_scores_gemma":[0.9119654,0.00012274865,0.08445791,0.000079928475,0.00001194413,0.0001896811,0.000041626856,0.000024882002,0.00310591],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99986565,0.000029425355,0.000004302499,0.00003063683,0.000038272596,0.00003176689],"domain_scores_gemma":[0.9997198,0.00014809925,0.000039205443,0.000010058279,0.000070279384,0.00001247947],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0004491206,0.00058700115,0.00053504645,0.00040258534,0.000253365,0.0005709932,0.0005778967,0.00094181066,0.0014712106],"category_scores_gemma":[0.00083248276,0.0003116145,0.00039938878,0.00023554444,0.0004980996,0.00022540452,0.00032843425,0.0003762071,0.00014566007],"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":[0.00002010402,0.000018071933,0.00017915716,0.000019723597,0.000012239142,0.000027667478,0.000019953392,0.9876993,0.002914463,0.0012156566,0.0001282538,0.0077454196],"study_design_scores_gemma":[0.000007590244,0.000020879812,0.00006147937,0.000002143597,0.000002964046,0.0000024697697,0.0000035988096,0.9993488,0.0002534466,0.0001946089,0.00010036771,0.0000015911716],"about_ca_topic_score_codex":0.0053775134,"about_ca_topic_score_gemma":0.0043466617,"teacher_disagreement_score":0.0053775134,"about_ca_system_score_codex":0.0005118806,"about_ca_system_score_gemma":0.00068338873,"threshold_uncertainty_score":0.010692418},"labels":[],"label_agreement":null},{"id":"W4230151429","doi":"10.32920/ryerson.14656272.v1","title":"Flutter Suppression of an Airfoil Using Neuro-Fuzzy Control","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Flutter; Airfoil; Aeroelasticity; Control theory (sociology); Controller (irrigation); Computer science; Fuzzy logic; Aerodynamics; Critical speed; Vibration; Engineering; Structural engineering; Control (management); Artificial intelligence; Physics; Acoustics; Aerospace engineering","score_opus":0.01572576447439938,"score_gpt":0.23336843570686178,"score_spread":0.2176426712324624,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4230151429","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":[0.24322982,0.00059850165,0.746859,0.00016943166,0.000068224756,0.00007584748,0.000027381599,0.00042999134,0.008541725],"genre_scores_gemma":[0.9780808,0.00008447783,0.021067532,0.000015232347,0.000006482668,0.000023958108,0.000008883365,0.000003729911,0.0007088082],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99989176,0.000020977863,0.00000646728,0.000021183527,0.00004704892,0.000012539385],"domain_scores_gemma":[0.99985003,0.000053441192,0.000027395074,0.000012750029,0.00004819467,0.000008133014],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025414742,0.00037724338,0.00023505042,0.0002083367,0.00028582517,0.0004211192,0.00034033298,0.00044288774,0.00033433214],"category_scores_gemma":[0.00055644196,0.000114793394,0.00027670505,0.00011491387,0.00034335666,0.00022723437,0.00021838362,0.00027021288,0.00005908823],"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":[0.000177312,0.00007812096,0.00085684744,0.00012182165,0.00004257201,0.00017000067,0.00012075702,0.8529996,0.06782356,0.003140914,0.00040261037,0.074065916],"study_design_scores_gemma":[0.000007131911,0.000056980494,0.00031371356,0.000006338554,0.000007751782,0.000022661212,0.0000062714203,0.99345917,0.005446389,0.0003275029,0.00034134477,0.0000047922913],"about_ca_topic_score_codex":0.005057512,"about_ca_topic_score_gemma":0.0040390766,"teacher_disagreement_score":0.005057512,"about_ca_system_score_codex":0.00035440899,"about_ca_system_score_gemma":0.00036587767,"threshold_uncertainty_score":0.010056138},"labels":[],"label_agreement":null},{"id":"W4232582803","doi":"10.32920/ryerson.14643981.v1","title":"Aerodynamic analysis for module discretization and consolidation of a morphing wing","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Wing; Morphing; Aerodynamics; Discretization; Climb; Computer science; Aerospace engineering; Engineering; Mathematics; Artificial intelligence; Mathematical analysis","score_opus":0.01149761575108512,"score_gpt":0.22441267578508856,"score_spread":0.21291506003400343,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4232582803","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":[0.9414171,0.000067711044,0.056633204,0.000018656568,0.000009544904,0.000023517001,0.000054972093,0.000105354586,0.001669916],"genre_scores_gemma":[0.99139845,0.00001832156,0.008244993,0.000003400794,8.538704e-7,0.000009842785,0.000043156982,0.000011352121,0.0002696409],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999211,0.000010609982,0.0000051554803,0.000010639489,0.00003461954,0.000018008612],"domain_scores_gemma":[0.9998337,0.000056562236,0.000026546011,0.0000370279,0.00003401486,0.000012144323],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021152645,0.00015869552,0.00020104442,0.00018076367,0.00014961469,0.00029174835,0.00019309181,0.00021598236,0.00060651806],"category_scores_gemma":[0.00044379386,0.000104081846,0.0002397568,0.00019911285,0.00023035907,0.00015299924,0.00017077407,0.00019447572,0.00007951218],"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":[0.0002569309,0.00010375255,0.01142408,0.00009498098,0.00003907111,0.00025154065,0.000159162,0.51960635,0.42161077,0.0025008444,0.00028899117,0.043663573],"study_design_scores_gemma":[0.0000128610545,0.00030913108,0.012487155,0.000008991419,0.000014433524,0.00010118714,0.000047183876,0.91838,0.06740789,0.00030255667,0.0009150345,0.0000135735045],"about_ca_topic_score_codex":0.0009227268,"about_ca_topic_score_gemma":0.0008045462,"teacher_disagreement_score":0.0009227268,"about_ca_system_score_codex":0.00017854638,"about_ca_system_score_gemma":0.00019237785,"threshold_uncertainty_score":0.002028942},"labels":[],"label_agreement":null},{"id":"W4234260691","doi":"10.32920/ryerson.14643981","title":"Aerodynamic analysis for module discretization and consolidation of a morphing wing","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Wing; Morphing; Aerodynamics; Discretization; Climb; Computer science; Aerospace engineering; Engineering; Mathematics; Artificial intelligence; Mathematical analysis","score_opus":0.01149761575108512,"score_gpt":0.22441267578508856,"score_spread":0.21291506003400343,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4234260691","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":[0.9414171,0.000067711044,0.056633204,0.000018656568,0.000009544904,0.000023517001,0.000054972093,0.000105354586,0.001669916],"genre_scores_gemma":[0.99139845,0.00001832156,0.008244993,0.000003400794,8.538704e-7,0.000009842785,0.000043156982,0.000011352121,0.0002696409],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999211,0.000010609982,0.0000051554803,0.000010639489,0.00003461954,0.000018008612],"domain_scores_gemma":[0.9998337,0.000056562236,0.000026546011,0.0000370279,0.00003401486,0.000012144323],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021152645,0.00015869552,0.00020104442,0.00018076367,0.00014961469,0.00029174835,0.00019309181,0.00021598236,0.00060651806],"category_scores_gemma":[0.00044379386,0.000104081846,0.0002397568,0.00019911285,0.00023035907,0.00015299924,0.00017077407,0.00019447572,0.00007951218],"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":[0.0002569309,0.00010375255,0.01142408,0.00009498098,0.00003907111,0.00025154065,0.000159162,0.51960635,0.42161077,0.0025008444,0.00028899117,0.043663573],"study_design_scores_gemma":[0.0000128610545,0.00030913108,0.012487155,0.000008991419,0.000014433524,0.00010118714,0.000047183876,0.91838,0.06740789,0.00030255667,0.0009150345,0.0000135735045],"about_ca_topic_score_codex":0.0009227268,"about_ca_topic_score_gemma":0.0008045462,"teacher_disagreement_score":0.0009227268,"about_ca_system_score_codex":0.00017854638,"about_ca_system_score_gemma":0.00019237785,"threshold_uncertainty_score":0.002028942},"labels":[],"label_agreement":null},{"id":"W4237252076","doi":"10.32920/ryerson.14645931","title":"Aerodynamic aspects in the development of morphing winglet for a regional aircraft","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Wingtip device; Morphing; Stall (fluid mechanics); Wing; Bending moment; Drag; Lift-induced drag; Aerodynamics; Structural engineering; Pitching moment; Lift-to-drag ratio; Camber (aerodynamics); Aerospace engineering; Engineering; Angle of attack; Computer science","score_opus":0.028047171475281286,"score_gpt":0.23929731517533837,"score_spread":0.21125014370005707,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4237252076","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":[0.93502486,0.00037698785,0.05746852,0.000070634174,0.00002777483,0.00003745629,0.000056643894,0.00012488598,0.0068123075],"genre_scores_gemma":[0.9848466,0.00011586744,0.0138659105,0.00000963321,0.0000055352216,0.0000060133166,0.000038715796,0.000014094813,0.0010977607],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99993503,0.000010476784,0.0000031530833,0.00001211997,0.000024700723,0.000014583464],"domain_scores_gemma":[0.99992955,0.000013466168,0.000016936263,0.000013362788,0.000017978904,0.000008650404],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012749959,0.00018353818,0.000104225655,0.00013667552,0.00010244521,0.00019745709,0.00016979566,0.00013097409,0.0008570612],"category_scores_gemma":[0.00015825851,0.00006614392,0.00027599733,0.000077565244,0.000109304005,0.00013432968,0.00016273826,0.00014841602,0.00016478647],"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":[0.00016947495,0.00004281252,0.009787994,0.00012767411,0.000027599934,0.00063861045,0.000094752926,0.11206213,0.8088542,0.0029951276,0.00028805024,0.064911574],"study_design_scores_gemma":[0.000027156622,0.003135504,0.09073865,0.000031167307,0.00012770847,0.0018673457,0.00023252795,0.607298,0.2828395,0.00090041134,0.0127562955,0.000045750625],"about_ca_topic_score_codex":0.0004994322,"about_ca_topic_score_gemma":0.0008396883,"teacher_disagreement_score":0.0008570612,"about_ca_system_score_codex":0.00011881108,"about_ca_system_score_gemma":0.0000834997,"threshold_uncertainty_score":0.0028671622},"labels":[],"label_agreement":null},{"id":"W4242336168","doi":"10.32920/ryerson.14646720.v1","title":"Modeling of Gust Energy Extractions through Aeroelastic Tailoring","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Aeroelasticity; Aerodynamics; Robustness (evolution); Computer science; Drag; Wing; Structural engineering; Efficient energy use; Control theory (sociology); Engineering; Aerospace engineering","score_opus":0.028566949604349412,"score_gpt":0.23233847760116721,"score_spread":0.2037715279968178,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4242336168","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":[0.8005342,0.00015014752,0.18824564,0.00009942703,0.00002068919,0.00006243193,0.00017186678,0.00034553217,0.010370119],"genre_scores_gemma":[0.99555594,0.000054710545,0.0026235403,0.00000663375,0.0000016317235,0.000019017192,0.000033647928,0.000013701698,0.0016910451],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999157,0.000012609023,0.0000047405565,0.000012212369,0.000030344843,0.000024298643],"domain_scores_gemma":[0.9999056,0.000042841,0.000016812668,0.000010580457,0.000013311794,0.000010848132],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001486548,0.0004317241,0.00038101614,0.00023768832,0.0002818322,0.00054609403,0.0004387533,0.00064927235,0.0007962173],"category_scores_gemma":[0.0003597162,0.00018790545,0.00036849728,0.00020629872,0.00040175612,0.000418639,0.00054450927,0.00033487345,0.00013173977],"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":[0.000033755518,0.000016431917,0.00058726023,0.000012636886,0.000005757204,0.000060373113,0.000022155595,0.99010545,0.0066707875,0.00051232986,0.000036262634,0.0019368272],"study_design_scores_gemma":[0.0000029844466,0.000022648257,0.00037336603,0.000001506322,0.000002341688,0.00000884049,0.00000690106,0.99814904,0.0011813615,0.00015263981,0.00009572464,0.0000027524707],"about_ca_topic_score_codex":0.004825896,"about_ca_topic_score_gemma":0.0026281655,"teacher_disagreement_score":0.004825896,"about_ca_system_score_codex":0.00026833313,"about_ca_system_score_gemma":0.00037199756,"threshold_uncertainty_score":0.009595573},"labels":[],"label_agreement":null},{"id":"W4242505847","doi":"10.32920/14636265.v2","title":"Effect of the Backward-Facing Step Location on the Aerodynamics of a Morphing Wing","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Airfoil; Morphing; Lift coefficient; Aerospace engineering; Aerodynamics; Angle of attack; NACA airfoil; Trailing edge; Chord (peer-to-peer); Pressure coefficient; Drag coefficient; Wing; Lift-to-drag ratio; Reynolds number; Structural engineering; Marine engineering; Computer science; Drag; Mechanics; Engineering; Physics; Computer graphics (images)","score_opus":0.006915303188539129,"score_gpt":0.202719342762873,"score_spread":0.19580403957433387,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4242505847","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":[0.9976191,0.00008362824,0.0011080744,0.000029756186,0.00002167806,0.0000069885573,0.000029469064,0.00003115978,0.0010701572],"genre_scores_gemma":[0.99912566,0.000031271753,0.00065701077,0.000007978217,0.0000014748847,0.000002063538,0.000012955978,0.0000041292196,0.00015740906],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99991214,0.000011290096,0.0000066134244,0.000014477594,0.000027144948,0.000028296434],"domain_scores_gemma":[0.99965334,0.0001552088,0.00007072909,0.000029499908,0.000047997604,0.000043149732],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00013033336,0.00031553948,0.00025663056,0.00018438257,0.00027678075,0.00042106904,0.00020503074,0.000363653,0.001723152],"category_scores_gemma":[0.00059559976,0.00015100997,0.00021495453,0.000097268516,0.00032547087,0.00023804005,0.0003321676,0.00032424228,0.00016976474],"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":[0.0010661734,0.00018107642,0.013078679,0.00024097296,0.00004808409,0.0020739054,0.00015063878,0.13443275,0.83508927,0.00064712705,0.00030719367,0.012684121],"study_design_scores_gemma":[0.00016009809,0.0046602017,0.053755306,0.00008695795,0.00017781628,0.0010464562,0.0008110982,0.3522932,0.5839763,0.000292603,0.002626583,0.00011337971],"about_ca_topic_score_codex":0.0007628669,"about_ca_topic_score_gemma":0.0009474421,"teacher_disagreement_score":0.001723152,"about_ca_system_score_codex":0.00013875158,"about_ca_system_score_gemma":0.0002271449,"threshold_uncertainty_score":0.0057644844},"labels":[],"label_agreement":null},{"id":"W4243603407","doi":"10.22215/etd/2019-13506","title":"Effects of Geometric Nonlinearities on the Fidelity of Aeroelasticity Loads Analyses of Very Flexible Airframes","year":2019,"lang":"en","type":"dissertation","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Airframe; Aeroelasticity; Finite element method; Nonlinear system; Structural engineering; Stiffness; Engineering; Aerospace engineering; Aerodynamics; Physics","score_opus":0.017860645578113652,"score_gpt":0.26989471664271397,"score_spread":0.2520340710646003,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4243603407","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":[0.8476029,0.00041642442,0.13641427,0.00018814018,0.000029541088,0.000044096767,0.00015467357,0.00026997863,0.014879985],"genre_scores_gemma":[0.9860833,0.00019850796,0.0122463405,0.000014333741,0.000007229776,0.000012977112,0.00007487352,0.00006186212,0.0013004343],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999595,0.00012143154,0.00002310363,0.00005222337,0.00016317681,0.00004515915],"domain_scores_gemma":[0.9975044,0.0017847181,0.00018706218,0.0003009698,0.00018898532,0.00003392957],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0008602697,0.00037835265,0.00030011064,0.00029307063,0.0003118826,0.00069471553,0.0003512398,0.00049870485,0.0024969736],"category_scores_gemma":[0.005317338,0.00019062495,0.0003108715,0.00027296774,0.0005626946,0.00045863978,0.000604525,0.0006351897,0.00041190875],"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":[0.00016178282,0.000061099796,0.005505906,0.00015066304,0.000017859145,0.00016267721,0.00027668764,0.912736,0.031773094,0.003313435,0.000246799,0.045594044],"study_design_scores_gemma":[0.000007476759,0.00016597877,0.005422028,0.000048349353,0.000010734709,0.0001038523,0.00013881474,0.9717524,0.019746304,0.0014771915,0.0011109085,0.000015909414],"about_ca_topic_score_codex":0.0018528054,"about_ca_topic_score_gemma":0.0019771277,"teacher_disagreement_score":0.0024969736,"about_ca_system_score_codex":0.0002846593,"about_ca_system_score_gemma":0.00031837326,"threshold_uncertainty_score":0.008353233},"labels":[],"label_agreement":null},{"id":"W4244787548","doi":"10.32920/ryerson.14646720","title":"Modeling of Gust Energy Extractions through Aeroelastic Tailoring","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Aeroelasticity; Aerodynamics; Robustness (evolution); Computer science; Drag; Efficient energy use; Structural engineering; Control theory (sociology); Aerospace engineering; Engineering","score_opus":0.028566949604349412,"score_gpt":0.23233847760116721,"score_spread":0.2037715279968178,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4244787548","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":[0.8005342,0.00015014752,0.18824564,0.00009942703,0.00002068919,0.00006243193,0.00017186678,0.00034553217,0.010370119],"genre_scores_gemma":[0.99555594,0.000054710545,0.0026235403,0.00000663375,0.0000016317235,0.000019017192,0.000033647928,0.000013701698,0.0016910451],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999157,0.000012609023,0.0000047405565,0.000012212369,0.000030344843,0.000024298643],"domain_scores_gemma":[0.9999056,0.000042841,0.000016812668,0.000010580457,0.000013311794,0.000010848132],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001486548,0.0004317241,0.00038101614,0.00023768832,0.0002818322,0.00054609403,0.0004387533,0.00064927235,0.0007962173],"category_scores_gemma":[0.0003597162,0.00018790545,0.00036849728,0.00020629872,0.00040175612,0.000418639,0.00054450927,0.00033487345,0.00013173977],"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":[0.000033755518,0.000016431917,0.00058726023,0.000012636886,0.000005757204,0.000060373113,0.000022155595,0.99010545,0.0066707875,0.00051232986,0.000036262634,0.0019368272],"study_design_scores_gemma":[0.0000029844466,0.000022648257,0.00037336603,0.000001506322,0.000002341688,0.00000884049,0.00000690106,0.99814904,0.0011813615,0.00015263981,0.00009572464,0.0000027524707],"about_ca_topic_score_codex":0.004825896,"about_ca_topic_score_gemma":0.0026281655,"teacher_disagreement_score":0.004825896,"about_ca_system_score_codex":0.00026833313,"about_ca_system_score_gemma":0.00037199756,"threshold_uncertainty_score":0.009595573},"labels":[],"label_agreement":null},{"id":"W4248928927","doi":"10.32920/ryerson.14656272","title":"Flutter Suppression of an Airfoil Using Neuro-Fuzzy Control","year":2021,"lang":"en","type":"preprint","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Flutter; Airfoil; Aeroelasticity; Control theory (sociology); Controller (irrigation); Fuzzy logic; Computer science; Aerodynamics; Engineering; Structural engineering; Control (management); Artificial intelligence; Aerospace engineering","score_opus":0.01572576447439938,"score_gpt":0.23336843570686178,"score_spread":0.2176426712324624,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4248928927","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":[0.24322982,0.00059850165,0.746859,0.00016943166,0.000068224756,0.00007584748,0.000027381599,0.00042999134,0.008541725],"genre_scores_gemma":[0.9780808,0.00008447783,0.021067532,0.000015232347,0.000006482668,0.000023958108,0.000008883365,0.000003729911,0.0007088082],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99989176,0.000020977863,0.00000646728,0.000021183527,0.00004704892,0.000012539385],"domain_scores_gemma":[0.99985003,0.000053441192,0.000027395074,0.000012750029,0.00004819467,0.000008133014],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025414742,0.00037724338,0.00023505042,0.0002083367,0.00028582517,0.0004211192,0.00034033298,0.00044288774,0.00033433214],"category_scores_gemma":[0.00055644196,0.000114793394,0.00027670505,0.00011491387,0.00034335666,0.00022723437,0.00021838362,0.00027021288,0.00005908823],"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":[0.000177312,0.00007812096,0.00085684744,0.00012182165,0.00004257201,0.00017000067,0.00012075702,0.8529996,0.06782356,0.003140914,0.00040261037,0.074065916],"study_design_scores_gemma":[0.000007131911,0.000056980494,0.00031371356,0.000006338554,0.000007751782,0.000022661212,0.0000062714203,0.99345917,0.005446389,0.0003275029,0.00034134477,0.0000047922913],"about_ca_topic_score_codex":0.005057512,"about_ca_topic_score_gemma":0.0040390766,"teacher_disagreement_score":0.005057512,"about_ca_system_score_codex":0.00035440899,"about_ca_system_score_gemma":0.00036587767,"threshold_uncertainty_score":0.010056138},"labels":[],"label_agreement":null},{"id":"W4251126057","doi":"10.1106/mhd5-0n62-24eh-8b9t","title":"Wave Propagation in Electromechanical Structures: Induced by Surface-Bonded Piezoelectric Actuators","year":2001,"lang":"en","type":"article","venue":"Journal of Intelligent Material Systems and Structures","topic":"Aeroelasticity and Vibration Control","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 Alberta","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Actuator; Piezoelectricity; Waveform; Acoustics; Wave propagation; Surface wave; Materials science; Surface acoustic wave; Surface (topology); Piezoelectric sensor; Physics; Engineering; Optics; Geometry; Mathematics; Electrical engineering; Voltage","score_opus":0.012245960264191958,"score_gpt":0.21651790542484983,"score_spread":0.2042719451606579,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4251126057","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":[0.95562696,0.00009084672,0.042233925,0.000061841456,0.000022121549,0.00001769432,0.000018423938,0.000089606714,0.0018386894],"genre_scores_gemma":[0.9923253,0.00009271,0.006734901,0.0000096932445,0.000003924003,0.000010023064,0.000013976814,0.000009527052,0.0007999037],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998691,0.000019993717,0.0000033473675,0.00001349796,0.000076993194,0.000017001003],"domain_scores_gemma":[0.9998155,0.000093919116,0.000037882393,0.000017611374,0.000025136971,0.000009863514],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00017258013,0.00029061988,0.00020550127,0.0001656463,0.00017562999,0.0002993525,0.0003485109,0.0005901755,0.00055486057],"category_scores_gemma":[0.00061719713,0.00024174925,0.00021250772,0.00013901856,0.0005970536,0.00042946878,0.00033993038,0.00032504267,0.00009943413],"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":[0.00020546424,0.000098501805,0.001686082,0.00011427783,0.000026603037,0.0009941891,0.00043103518,0.45354515,0.5221942,0.0042371405,0.00017879564,0.016288579],"study_design_scores_gemma":[0.000024913877,0.0001312677,0.0014386575,0.0000075861544,0.00000823382,0.0001315266,0.00006576828,0.9201182,0.07700431,0.0007627959,0.0002942101,0.0000125930055],"about_ca_topic_score_codex":0.00042983535,"about_ca_topic_score_gemma":0.0003765833,"teacher_disagreement_score":0.0005901755,"about_ca_system_score_codex":0.00019920232,"about_ca_system_score_gemma":0.00018219436,"threshold_uncertainty_score":0.0018562078},"labels":[],"label_agreement":null},{"id":"W4281866781","doi":"10.2514/1.c036846","title":"Aircraft Flutter and Aerodynamic Work","year":2022,"lang":"en","type":"article","venue":"Journal of Aircraft","topic":"Aeroelasticity and Vibration Control","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":"Transport Canada","funders":"","keywords":"Flutter; Aeroelasticity; Airspeed; Aerodynamics; Aerodynamic force; Aerospace engineering; Control theory (sociology); Engineering; Work (physics); Computer science; Structural engineering; Mechanical engineering","score_opus":0.004921243277216424,"score_gpt":0.18116988776957824,"score_spread":0.1762486444923618,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4281866781","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":[0.4546557,0.006338358,0.38742164,0.00067677785,0.00044911666,0.00008167825,0.00048550396,0.00047626396,0.14941496],"genre_scores_gemma":[0.9514601,0.0023452612,0.021422729,0.00008443918,0.00016232628,0.00006414,0.00024290057,0.00021537885,0.024002787],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.9996469,0.000060431325,0.000016711287,0.00007393828,0.00015631328,0.000045684825],"domain_scores_gemma":[0.99978465,0.00009229843,0.00003147351,0.00004126507,0.00003437166,0.000016067079],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002035463,0.00043252244,0.00025377647,0.0011273264,0.00041008962,0.00133301,0.0003628387,0.00051258126,0.0041940766],"category_scores_gemma":[0.0009458822,0.00016721146,0.00042293908,0.0005965471,0.0009107487,0.001012971,0.0013521127,0.0005015014,0.0008718598],"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":[0.0001835957,0.00008099745,0.008115401,0.00041409337,0.000076054515,0.0008271161,0.0012846458,0.35529643,0.06789187,0.37941974,0.0025508148,0.18385912],"study_design_scores_gemma":[0.000029501121,0.00044935086,0.03960934,0.00029256666,0.00004611041,0.0022186623,0.0010698455,0.58671284,0.025149947,0.24760582,0.09662512,0.00019084512],"about_ca_topic_score_codex":0.00076301955,"about_ca_topic_score_gemma":0.0005152419,"teacher_disagreement_score":0.0041940766,"about_ca_system_score_codex":0.00030218356,"about_ca_system_score_gemma":0.00015986923,"threshold_uncertainty_score":0.014030576},"labels":[],"label_agreement":null},{"id":"W4293155122","doi":"10.1061/(asce)as.1943-5525.0001465","title":"Dynamic Aeroelastic Performance Optimization of Adaptive Aerospace Structures Using Structural Geometric Nonlinearities","year":2022,"lang":"en","type":"article","venue":"Journal of Aerospace Engineering","topic":"Aeroelasticity and Vibration Control","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":"Carleton University","funders":"","keywords":"Aeroelasticity; Aerodynamics; Truss; Actuator; Structural engineering; Control theory (sociology); Stiffness; Engineering; Modal; Computer science; Aerospace engineering","score_opus":0.0076011404282444045,"score_gpt":0.19681221057843518,"score_spread":0.18921107015019079,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4293155122","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":[0.2790355,0.00025319852,0.71318907,0.00008787411,0.000019834746,0.000041620893,0.000023709623,0.0001408241,0.0072083436],"genre_scores_gemma":[0.9716153,0.00008771803,0.02705638,0.000016277596,0.0000062517743,0.000039797196,0.000016627955,0.000018848448,0.0011428266],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99987197,0.00002697614,0.000004320601,0.000023220138,0.000057548164,0.00001589834],"domain_scores_gemma":[0.9998522,0.00006169333,0.00003893775,0.000013228635,0.000026887768,0.0000069594294],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00029279612,0.0005591726,0.00032396824,0.00025631514,0.00013905423,0.00038375903,0.00039643972,0.00042547227,0.0005678399],"category_scores_gemma":[0.00044899838,0.00020378883,0.00027626482,0.00011422276,0.00043156074,0.0002917965,0.0003468865,0.00028421133,0.00012362281],"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":[0.000013847161,0.000017474229,0.00020305066,0.000019893605,0.000007381421,0.000017842513,0.00001428496,0.9773971,0.014696538,0.00062785414,0.000025150988,0.006959551],"study_design_scores_gemma":[0.0000030195426,0.000064470405,0.0001886634,0.0000021804483,0.0000030457743,0.000007167916,0.0000066446314,0.99746096,0.0018593693,0.00022455712,0.00017734614,0.0000025526763],"about_ca_topic_score_codex":0.00078158756,"about_ca_topic_score_gemma":0.0010949089,"teacher_disagreement_score":0.00078158756,"about_ca_system_score_codex":0.00027697504,"about_ca_system_score_gemma":0.00025216822,"threshold_uncertainty_score":0.0020095706},"labels":[],"label_agreement":null},{"id":"W4295951724","doi":"10.4050/f-0078-2022-1130","title":"Design and Test of an Active Pneumatic Trailing Edge Flap for High-Speed Rotorcraft","year":2022,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Trailing edge; Airfoil; Aerodynamics; Actuator; Helicopter rotor; Rotor (electric); Finite element method; Structural engineering; Mechanical engineering; Enhanced Data Rates for GSM Evolution; Leading edge; Engineering; Aerospace engineering; Computer science; Acoustics; Physics; Electrical engineering","score_opus":0.016281922340432065,"score_gpt":0.2170055360106441,"score_spread":0.20072361367021202,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4295951724","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":[0.9200948,0.00011652547,0.07410646,0.00011902913,0.000094483614,0.00033388066,0.00015999196,0.00048392106,0.0044908742],"genre_scores_gemma":[0.9582587,0.000047030473,0.03976918,0.000025702195,0.0000074421678,0.000077248966,0.00007545726,0.000022990747,0.0017163425],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997242,0.00004351572,0.000012278517,0.00003884805,0.0001444424,0.00003665244],"domain_scores_gemma":[0.9995277,0.000073670955,0.00009874833,0.00011894567,0.00010686806,0.0000740372],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005713421,0.00038013107,0.00019006288,0.00019698602,0.00021037094,0.0002689589,0.0005732155,0.0005399022,0.0011448665],"category_scores_gemma":[0.000506891,0.00014862859,0.0002016457,0.000070768314,0.00038891088,0.00036523363,0.00027604366,0.0003014935,0.0002438519],"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":[0.00040854738,0.000465734,0.0046317494,0.00038696761,0.000040618514,0.0008100495,0.00015713216,0.039390713,0.8972167,0.0020912967,0.0009385641,0.053461928],"study_design_scores_gemma":[0.0004849446,0.021844186,0.021512702,0.00006193909,0.000065543245,0.0014014859,0.00012631911,0.18659185,0.7535627,0.00057479355,0.013713824,0.000059758553],"about_ca_topic_score_codex":0.0002047998,"about_ca_topic_score_gemma":0.0002947755,"teacher_disagreement_score":0.0011448665,"about_ca_system_score_codex":0.00021529317,"about_ca_system_score_gemma":0.0004019714,"threshold_uncertainty_score":0.0038298965},"labels":[],"label_agreement":null},{"id":"W4296745147","doi":"10.3390/aerospace9100532","title":"Free Vibration Analysis of a Reconfigurable Modular Morphing Wing","year":2022,"lang":"en","type":"article","venue":"Aerospace","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":6,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"Toronto Metropolitan University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Morphing; Modular design; Structural engineering; Wing; Finite element method; Computer science; Vibration; Bending stiffness; Aeroelasticity; Bending; Engineering; Topology (electrical circuits); Aerospace engineering; Aerodynamics; Acoustics; Artificial intelligence; Physics","score_opus":0.008756923527353471,"score_gpt":0.19149429304330293,"score_spread":0.18273736951594946,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4296745147","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":[0.96923,0.00007295235,0.028850246,0.000028549299,0.000005822321,0.000009342755,0.00003668915,0.000045854045,0.0017206318],"genre_scores_gemma":[0.9986052,0.000012630491,0.0010613377,0.000002076256,5.088496e-7,0.0000030091453,0.000012992994,0.000002142672,0.00030005802],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99996376,0.000005710733,0.0000016272841,0.000008968989,0.000013343009,0.0000065469508],"domain_scores_gemma":[0.99994874,0.000020889118,0.000009960344,0.000007989253,0.0000075430603,0.0000048552656],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00008616055,0.00014417611,0.0000888234,0.00020043175,0.000104279345,0.00010833937,0.00014150064,0.00019750604,0.0006531137],"category_scores_gemma":[0.00012331482,0.000056896733,0.00015570922,0.000075433636,0.00024151149,0.00010390057,0.00013159074,0.000096693664,0.00006484661],"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":[0.00037252269,0.000059221144,0.00981126,0.00011266056,0.00004015274,0.00065543456,0.00042304254,0.27089474,0.680422,0.0027883262,0.00028466067,0.034136],"study_design_scores_gemma":[0.000007707476,0.00021287003,0.016916603,0.0000072482835,0.000010501829,0.00010476935,0.00008792804,0.95760477,0.024185883,0.00042761938,0.00042216657,0.000012022644],"about_ca_topic_score_codex":0.00076557236,"about_ca_topic_score_gemma":0.0005075761,"teacher_disagreement_score":0.00076557236,"about_ca_system_score_codex":0.00009635181,"about_ca_system_score_gemma":0.00006821341,"threshold_uncertainty_score":0.0021848679},"labels":[],"label_agreement":null},{"id":"W4297994210","doi":"","title":"Optimal piezo-electro-mechanical coupling to control plate vibrations","year":2001,"lang":"en","type":"article","venue":"HAL (Le Centre pour la Communication Scientifique Directe)","topic":"Aeroelasticity and Vibration Control","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 Asian Studies Association","funders":"","keywords":"Coupling (piping); Vibration; Vibration control; Acoustics; Control theory (sociology); Control (management); Materials science; Structural engineering; Physics; Mechanical engineering; Engineering; Computer science; Artificial intelligence","score_opus":0.008239349006429307,"score_gpt":0.2014004847335763,"score_spread":0.193161135727147,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4297994210","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":[0.17545913,0.0004642584,0.81452364,0.000098534976,0.00005727801,0.000042544343,0.000011592306,0.00019038995,0.009152717],"genre_scores_gemma":[0.96680015,0.000120711884,0.030796355,0.000022992217,0.000009530223,0.000034926856,0.0000061973665,0.000017309583,0.0021917329],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99991655,0.0000151181775,0.000003860206,0.000018031593,0.000038311213,0.000008175564],"domain_scores_gemma":[0.99991906,0.00003633415,0.00001806775,0.000007996044,0.000009864187,0.000008585213],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000119649456,0.0003225404,0.00015891508,0.00013591952,0.00012640681,0.00024668942,0.0003176726,0.00017084916,0.0012012521],"category_scores_gemma":[0.00027508184,0.0001547799,0.00009048405,0.00009198354,0.0003427403,0.0003045773,0.0003546525,0.0002879479,0.000116501],"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":[0.00017267716,0.00014478329,0.00042428033,0.00021479224,0.00004498899,0.00015720665,0.00012248522,0.32247427,0.5613937,0.053730637,0.0003816417,0.06073862],"study_design_scores_gemma":[0.00004111059,0.00025161705,0.00047636553,0.000011488946,0.000028808297,0.000106064894,0.00002790343,0.88930506,0.09729465,0.009136162,0.0033034186,0.000017424625],"about_ca_topic_score_codex":0.000108527245,"about_ca_topic_score_gemma":0.0002818322,"teacher_disagreement_score":0.0012012521,"about_ca_system_score_codex":0.00016453619,"about_ca_system_score_gemma":0.000114334456,"threshold_uncertainty_score":0.004018545},"labels":[],"label_agreement":null},{"id":"W4299552437","doi":"","title":"A novel passive electric network analog to Kirchhoff-Love plate designed to efficiently damp forced vibrations by distributed piezoelectric transducers","year":2013,"lang":"en","type":"preprint","venue":"HAL (Le Centre pour la Communication Scientifique Directe)","topic":"Aeroelasticity and Vibration Control","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 Asian Studies Association","funders":"","keywords":"Damp; Piezoelectricity; Vibration; Acoustics; Transducer; Physics","score_opus":0.007901076179368449,"score_gpt":0.19819040902891236,"score_spread":0.1902893328495439,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4299552437","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":[0.11841615,0.00071478455,0.85682595,0.00019486976,0.00018419395,0.00006994482,0.00009132308,0.00048243033,0.0230203],"genre_scores_gemma":[0.83046216,0.00041433386,0.15489742,0.00008217603,0.00003622419,0.00006108674,0.00008375407,0.000032762113,0.013930081],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99994314,0.000009652884,0.0000018787896,0.000016655928,0.000023776789,0.0000049011555],"domain_scores_gemma":[0.99995995,0.00001038377,0.00000781036,0.0000062970958,0.000010324178,0.0000050805634],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000070937975,0.00029328614,0.00013880187,0.00012790143,0.00012854909,0.0002819233,0.0006298252,0.00025691162,0.0014283668],"category_scores_gemma":[0.00010831799,0.00010915578,0.000115814386,0.00012784546,0.00027080506,0.00043430313,0.0002018011,0.00021084666,0.0002854763],"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":[0.00013485772,0.000078644574,0.0003623499,0.00028332908,0.00002699092,0.00035947814,0.00009909195,0.042832643,0.828943,0.040162865,0.0011851488,0.085531615],"study_design_scores_gemma":[0.00005482221,0.00072086457,0.0012272204,0.000035079753,0.000045947334,0.00089673523,0.000051567535,0.5346215,0.42261124,0.0076144827,0.032082967,0.000037586877],"about_ca_topic_score_codex":0.00016717306,"about_ca_topic_score_gemma":0.0003758094,"teacher_disagreement_score":0.0014283668,"about_ca_system_score_codex":0.00016536302,"about_ca_system_score_gemma":0.0001276564,"threshold_uncertainty_score":0.004778385},"labels":[],"label_agreement":null},{"id":"W4308124840","doi":"10.3390/designs6060102","title":"Optimization and Design of a Flexible Droop Nose Leading Edge Morphing Wing Based on a Novel Black Widow Optimization (B.W.O.) Algorithm—Part II","year":2022,"lang":"en","type":"article","venue":"Designs","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":6,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure; Université du Québec à Montréal","funders":"Canada Research Chairs","keywords":"Airfoil; Stall (fluid mechanics); Leading edge; Wing; Morphing; Drag; Lift coefficient; Trailing edge; Fitness function; Angle of attack; Engineering; Mathematics; Aerodynamics; Control theory (sociology); Algorithm; Genetic algorithm; Structural engineering; Computer science; Mathematical optimization; Aerospace engineering; Mechanics; Reynolds number; Physics; Artificial intelligence","score_opus":0.03743736356590247,"score_gpt":0.22590735513479784,"score_spread":0.18846999156889538,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4308124840","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":[0.25646937,0.00027575638,0.73724246,0.0001254028,0.00004592281,0.00018549652,0.00006663721,0.00028270364,0.0053062895],"genre_scores_gemma":[0.78917426,0.00011773942,0.20812379,0.000055903696,0.000010131955,0.00024403693,0.00009450926,0.00004005871,0.002139523],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99992704,0.000014261347,0.000003294886,0.000017078743,0.00002247411,0.000015778707],"domain_scores_gemma":[0.99993634,0.000021266856,0.000012397539,0.0000045949228,0.000018271494,0.0000072119983],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002121253,0.00042024476,0.00040210728,0.00027862377,0.00021119192,0.0004218975,0.00040421245,0.0005594272,0.00091875717],"category_scores_gemma":[0.00030879994,0.00022195475,0.00039775192,0.0001616734,0.00025304971,0.00021209476,0.00034540924,0.00025029745,0.00013783642],"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":[0.00010367228,0.00005149928,0.001213919,0.000069294634,0.000029403353,0.00007950832,0.0000379312,0.9338595,0.019616012,0.0017661329,0.00033866655,0.042834345],"study_design_scores_gemma":[0.000011788324,0.000057420017,0.00025533675,0.0000029968041,0.0000047738044,0.000010447561,0.000007696917,0.9978205,0.0014880359,0.000095930794,0.00024218344,0.000002952347],"about_ca_topic_score_codex":0.002811383,"about_ca_topic_score_gemma":0.002321861,"teacher_disagreement_score":0.002811383,"about_ca_system_score_codex":0.00020567336,"about_ca_system_score_gemma":0.0006232199,"threshold_uncertainty_score":0.0055900216},"labels":[],"label_agreement":null},{"id":"W4312690758","doi":"10.1121/10.0015667","title":"Active structural acoustic control using the weighted sum of spatial gradients method","year":2022,"lang":"en","type":"article","venue":"The Journal of the Acoustical Society of America","topic":"Aeroelasticity and Vibration Control","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":"Health Canada","funders":"","keywords":"Attenuation; Acoustic radiation; Structural acoustics; Computer science; Acoustics; Acoustic attenuation; Vibration; Metric (unit); Field (mathematics); Radiation; Physics; Optics; Mathematics; Engineering","score_opus":0.009876094570155515,"score_gpt":0.24711952761203396,"score_spread":0.23724343304187845,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4312690758","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":[0.0039464766,0.0001129206,0.9934049,0.000045317636,0.00002873529,0.000024684303,0.000008401399,0.00013174777,0.0022967898],"genre_scores_gemma":[0.5597199,0.00044775067,0.4293393,0.000100942976,0.00009233034,0.00022204415,0.00007332707,0.00020244805,0.009801907],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998011,0.000051019757,0.000007925834,0.000025777434,0.000099223325,0.0000149852685],"domain_scores_gemma":[0.99986434,0.000056378274,0.000018975526,0.000011284445,0.00003883253,0.000010197728],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003769874,0.00067406584,0.0004533795,0.00035719495,0.00017796525,0.0005806471,0.00072693557,0.00043881353,0.0018714978],"category_scores_gemma":[0.0004670902,0.00022491011,0.00033109108,0.000301222,0.000525197,0.0006482812,0.00054450455,0.0004977792,0.0002921105],"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":[0.00010857832,0.000054493874,0.00028077283,0.00015898336,0.00004471831,0.00007458495,0.00007670912,0.76548,0.033329334,0.057836972,0.0015901746,0.1409647],"study_design_scores_gemma":[0.0000053039735,0.000023372853,0.000030859435,0.000003037198,0.000002341041,0.0000076012443,0.0000025632985,0.99587387,0.0014133931,0.0017627587,0.000871261,0.0000037631255],"about_ca_topic_score_codex":0.0018268296,"about_ca_topic_score_gemma":0.0017027111,"teacher_disagreement_score":0.0018714978,"about_ca_system_score_codex":0.0003334329,"about_ca_system_score_gemma":0.0005126401,"threshold_uncertainty_score":0.0062607527},"labels":[],"label_agreement":null},{"id":"W4317632706","doi":"10.2514/6.2023-1582","title":"Aerodynamic Optimization of a Novel Synthetic Trailing Edge and Chord Elongation Morphing: Application to the UAS-S45 Airfoil","year":2023,"lang":"en","type":"article","venue":"AIAA SCITECH 2023 Forum","topic":"Aeroelasticity and Vibration Control","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":"École de Technologie Supérieure","funders":"","keywords":"Airfoil; Trailing edge; Chord (peer-to-peer); Morphing; Aerodynamics; Angle of attack; Leading edge; Lift coefficient; Deflection (physics); Aerospace engineering; Stall (fluid mechanics); Wing; Transonic; Computer science; Structural engineering; Acoustics; Physics; Mechanics; Engineering; Turbulence; Artificial intelligence; Classical mechanics","score_opus":0.008618972315355392,"score_gpt":0.21336166341967555,"score_spread":0.20474269110432017,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4317632706","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":[0.765349,0.0003012493,0.22524281,0.00011096005,0.00004303043,0.000100689394,0.00009465978,0.00019264444,0.008564968],"genre_scores_gemma":[0.96177495,0.000051206036,0.037290778,0.000009853683,0.0000034304107,0.000029894007,0.00003523396,0.000012245121,0.0007923292],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99996316,0.0000070817805,0.000001784884,0.000006900751,0.000014256138,0.000006812209],"domain_scores_gemma":[0.9999471,0.000016253887,0.000012928266,0.0000050280846,0.000012516281,0.0000062121603],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012812958,0.00032059706,0.00016701451,0.00016612874,0.000105350286,0.00022529002,0.00018575687,0.00026447375,0.00069324696],"category_scores_gemma":[0.00019760813,0.00009043307,0.00021275159,0.000083940715,0.00014900774,0.00012171934,0.00016435728,0.000145491,0.000057659625],"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":[0.00019097242,0.00011140098,0.0022302233,0.00019872066,0.000027174032,0.00016576487,0.00004974042,0.8300487,0.1103322,0.0019670974,0.00041125057,0.05426674],"study_design_scores_gemma":[0.000020209616,0.00034854855,0.0010865843,0.0000051813417,0.000009228007,0.000050290342,0.00001670874,0.98786527,0.009539617,0.00013602694,0.0009148457,0.0000075354437],"about_ca_topic_score_codex":0.00082295545,"about_ca_topic_score_gemma":0.0010617943,"teacher_disagreement_score":0.00082295545,"about_ca_system_score_codex":0.0001484814,"about_ca_system_score_gemma":0.00022645293,"threshold_uncertainty_score":0.0023192167},"labels":[],"label_agreement":null},{"id":"W4317632928","doi":"10.2514/6.2023-1583","title":"A Pareto Multi-Objective Optimization of a Camber Morphing Airfoil using Non-Dominated Sorting Genetic Algorithm","year":2023,"lang":"en","type":"article","venue":"AIAA SCITECH 2023 Forum","topic":"Aeroelasticity and Vibration Control","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":"École de Technologie Supérieure","funders":"","keywords":"Airfoil; Aerodynamics; Angle of attack; Lift-to-drag ratio; Genetic algorithm; Computer science; Camber (aerodynamics); Multi-objective optimization; Stall (fluid mechanics); Algorithm; Mathematics; Mathematical optimization; Engineering; Aerospace engineering","score_opus":0.012957813106410908,"score_gpt":0.23946387168054664,"score_spread":0.22650605857413572,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4317632928","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":[0.2439378,0.00051090476,0.73266876,0.00028794273,0.00010913867,0.00029751656,0.00016867222,0.0005963849,0.021422919],"genre_scores_gemma":[0.73894095,0.00018362835,0.2524493,0.0001418664,0.000016452155,0.00046068945,0.0002561183,0.000076855205,0.007474149],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99980015,0.000061680235,0.0000062478916,0.000027580138,0.0000666206,0.000037795493],"domain_scores_gemma":[0.99968743,0.0001585885,0.000033929642,0.000014286173,0.000083491155,0.000022255826],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00077468756,0.0009406234,0.0007026946,0.0009598246,0.00042351338,0.0007341355,0.000734993,0.0011558584,0.002119141],"category_scores_gemma":[0.0010392249,0.00028288775,0.00082706305,0.00050249306,0.0004419334,0.00021916688,0.0004921,0.00050964253,0.00022643826],"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":[0.00003567938,0.000045207213,0.0003986465,0.000046853835,0.00001801207,0.00005044023,0.000029066914,0.98034555,0.0018755677,0.0014832612,0.0003603108,0.015311456],"study_design_scores_gemma":[0.000008854206,0.000044959277,0.0001265183,0.000008215765,0.0000052221935,0.000007213344,0.000010037704,0.99861705,0.0006404968,0.0002457189,0.00028284578,0.0000028564],"about_ca_topic_score_codex":0.006998395,"about_ca_topic_score_gemma":0.0046794056,"teacher_disagreement_score":0.006998395,"about_ca_system_score_codex":0.00082674046,"about_ca_system_score_gemma":0.0013303953,"threshold_uncertainty_score":0.0139153},"labels":[],"label_agreement":null},{"id":"W4317633488","doi":"10.2514/6.2023-1584","title":"Design of a Variable Camber Morphing Winglet with Composite Lamination Structural Analysis and Failure Analysis – Application to the UAS-S45","year":2023,"lang":"en","type":"article","venue":"AIAA SCITECH 2023 Forum","topic":"Aeroelasticity and Vibration Control","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":"École de Technologie Supérieure","funders":"","keywords":"Morphing; Camber (aerodynamics); Wingtip device; Structural engineering; Materials science; Wing; Composite material; Computer science; Engineering","score_opus":0.004580930683928202,"score_gpt":0.19799406440659342,"score_spread":0.19341313372266522,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4317633488","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":[0.63245654,0.00019791773,0.361285,0.000066941335,0.000029909506,0.0001358183,0.00009577249,0.0004982903,0.005233831],"genre_scores_gemma":[0.880159,0.000083544066,0.11774413,0.00001929518,0.000004749348,0.00006002757,0.000068870795,0.00003691933,0.0018234255],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99989057,0.000011860891,0.0000052499186,0.000023154607,0.000055364933,0.000013863666],"domain_scores_gemma":[0.9998611,0.000022974638,0.000037955724,0.000021582799,0.00003958441,0.00001678906],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024611127,0.00029085824,0.00022077828,0.00036018685,0.00016142707,0.00032323212,0.00046763953,0.0003655196,0.0011499888],"category_scores_gemma":[0.00016704446,0.00016762142,0.00041157962,0.00009575462,0.00016243332,0.00015842836,0.0002269131,0.00015953605,0.00029587813],"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":[0.00019776312,0.00011309944,0.0056606107,0.00028755658,0.000048550868,0.00051510154,0.00014654311,0.17007834,0.7278847,0.0018064323,0.00044667773,0.092814565],"study_design_scores_gemma":[0.00003106078,0.0012350978,0.008865624,0.00003108564,0.000050525883,0.00040709673,0.00007372198,0.8224471,0.16126448,0.0003630625,0.005200311,0.000030821357],"about_ca_topic_score_codex":0.00041453398,"about_ca_topic_score_gemma":0.000660721,"teacher_disagreement_score":0.0011499888,"about_ca_system_score_codex":0.00018393077,"about_ca_system_score_gemma":0.00024466048,"threshold_uncertainty_score":0.0038470626},"labels":[],"label_agreement":null},{"id":"W4327741231","doi":"10.3390/aerospace10030300","title":"Functional Hazard Assessment of a Modular Re-Configurable Morphing Wing Using Taguchi and Finite Element Methodologies","year":2023,"lang":"en","type":"article","venue":"Aerospace","topic":"Aeroelasticity and Vibration Control","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":true,"ca_institutions":"Toronto Metropolitan University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Morphing; Finite element method; Wing; Structural engineering; Modular design; Engineering; Computer science; Artificial intelligence","score_opus":0.07741881782234643,"score_gpt":0.30560406055000083,"score_spread":0.2281852427276544,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4327741231","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":[0.73628205,0.00027156353,0.2612268,0.000043807446,0.000017115042,0.0000804968,0.000047556794,0.00012932654,0.0019012245],"genre_scores_gemma":[0.9636355,0.000077925484,0.03575968,0.0000067407414,0.0000021980784,0.000022645907,0.000018504532,0.00000712263,0.00046970622],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998497,0.000039046525,0.000007697125,0.000024473686,0.00006334512,0.000015702644],"domain_scores_gemma":[0.999642,0.00017733165,0.0000664323,0.000045649238,0.00005324878,0.000015354995],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00054695224,0.0004443092,0.0002627138,0.00065371714,0.00011166789,0.0003826295,0.000307524,0.00044592074,0.00046128937],"category_scores_gemma":[0.00054206996,0.0001754626,0.00044555936,0.00019310598,0.00031679068,0.00025208888,0.00026538814,0.00017990325,0.00007953485],"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":[0.00016176648,0.00010185839,0.007395513,0.00016984197,0.000032368323,0.00027876682,0.0001775744,0.5892882,0.3354092,0.0010353711,0.0001100662,0.06583951],"study_design_scores_gemma":[0.0000052655937,0.00042357756,0.0047789575,0.000010158809,0.00002409729,0.00008120257,0.00006082859,0.95380664,0.040087283,0.00032901566,0.00037586098,0.000017099144],"about_ca_topic_score_codex":0.00060170685,"about_ca_topic_score_gemma":0.00094099,"teacher_disagreement_score":0.00065371714,"about_ca_system_score_codex":0.00026723047,"about_ca_system_score_gemma":0.00018900188,"threshold_uncertainty_score":0.0028925538},"labels":[],"label_agreement":null},{"id":"W4365455613","doi":"10.1016/j.jsv.2023.117723","title":"Particle swarm optimization of a non-collocated MIMO PPF active vibration control of a composite sandwich plate","year":2023,"lang":"en","type":"article","venue":"Journal of Sound and Vibration","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":35,"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":"Natural Sciences and Engineering Research Council of Canada","keywords":"Particle swarm optimization; Control theory (sociology); Vibration; MIMO; Boundary value problem; Actuator; Vibration control; Position (finance); Engineering; Mathematics; Computer science; Algorithm; Acoustics; Physics; Mathematical analysis; Electronic engineering","score_opus":0.00964306440203838,"score_gpt":0.22384629207525972,"score_spread":0.21420322767322134,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4365455613","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":[0.22282809,0.0003736079,0.7675997,0.00032815489,0.00024056959,0.00007111658,0.000034264347,0.0001598921,0.008364647],"genre_scores_gemma":[0.98469156,0.00006036986,0.012778486,0.000033093525,0.00002143706,0.000042869557,0.0000151910945,0.000009303947,0.002347614],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999806,0.00006256511,0.000008862211,0.00004217691,0.000052053776,0.00002844738],"domain_scores_gemma":[0.99962366,0.00017803194,0.000044682227,0.000019482986,0.00011074989,0.000023436083],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0006009758,0.0006486631,0.0007897553,0.00022815421,0.00038949578,0.0007559396,0.0006197105,0.0012594884,0.0014553055],"category_scores_gemma":[0.00075536815,0.00036085158,0.0005370503,0.00014951044,0.0006248894,0.00029096645,0.00049555366,0.0005127884,0.00013375745],"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":[0.00013763706,0.00004601734,0.00023953816,0.000055769895,0.000040821586,0.000074640324,0.000039570732,0.98386097,0.0058354004,0.00078415876,0.00019517915,0.008690262],"study_design_scores_gemma":[0.0000054342804,0.000038604834,0.000078616766,0.0000013207771,0.0000035518665,0.0000024958229,0.0000034911855,0.99949884,0.00028910502,0.00004550375,0.00003159615,0.000001417656],"about_ca_topic_score_codex":0.006185731,"about_ca_topic_score_gemma":0.0033748366,"teacher_disagreement_score":0.006185731,"about_ca_system_score_codex":0.0003017664,"about_ca_system_score_gemma":0.00052217924,"threshold_uncertainty_score":0.012299478},"labels":[],"label_agreement":null},{"id":"W4366090424","doi":"10.3390/aerospace10040376","title":"Structural Dynamic Characterization of a Modular Morphing Wing Exploiting Finite Elements and Taguchi Methodology","year":2023,"lang":"en","type":"article","venue":"Aerospace","topic":"Aeroelasticity and Vibration Control","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":true,"ca_institutions":"Toronto Metropolitan University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Morphing; Wing; Modular design; Aeroelasticity; Finite element method; Aerodynamics; Structural engineering; Computer science; Engineering; Aerospace engineering; Artificial intelligence","score_opus":0.031117974163572388,"score_gpt":0.2553008254884908,"score_spread":0.22418285132491841,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4366090424","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":[0.83404624,0.00019772875,0.16396715,0.000028894592,0.000015877264,0.000037779213,0.00007766591,0.00012743776,0.0015011842],"genre_scores_gemma":[0.96395993,0.000069817324,0.035272088,0.0000058559717,0.0000018371798,0.000016018017,0.000044372497,0.00000888466,0.00062118703],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99990225,0.00001185982,0.0000053940075,0.000020497362,0.00004762136,0.000012303234],"domain_scores_gemma":[0.99979657,0.00008451025,0.00003716719,0.000033297907,0.000037192083,0.000011228203],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020444141,0.00027295548,0.0001815053,0.0005120128,0.00009265223,0.00018739371,0.00023395885,0.00031363947,0.0004897331],"category_scores_gemma":[0.0002951954,0.00011762788,0.00023140383,0.00022294672,0.00028156978,0.00015618074,0.00012154235,0.0001510307,0.00009729978],"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":[0.000068206005,0.000033046123,0.0027015763,0.000065922184,0.000008048608,0.00010347947,0.00010434847,0.04598849,0.9188353,0.00046520866,0.00004822492,0.031578183],"study_design_scores_gemma":[0.000011064862,0.00088891113,0.023707327,0.000020985344,0.0000423638,0.00029835847,0.00014657072,0.5510763,0.42152765,0.00040434633,0.0018434798,0.00003268096],"about_ca_topic_score_codex":0.00050484913,"about_ca_topic_score_gemma":0.0011426166,"teacher_disagreement_score":0.0005120128,"about_ca_system_score_codex":0.00014578637,"about_ca_system_score_gemma":0.00012712968,"threshold_uncertainty_score":0.0016383529},"labels":[],"label_agreement":null},{"id":"W4377249382","doi":"10.1063/5.0113342","title":"Aerodynamic characteristics of two stage morphing wing of UAV","year":2023,"lang":"en","type":"article","venue":"AIP conference proceedings","topic":"Aeroelasticity and Vibration Control","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 Waterloo","funders":"","keywords":"Morphing; Aerodynamics; Wing; Computer science; Aerospace engineering; Aeronautics; Stage (stratigraphy); Engineering; Artificial intelligence; Geology","score_opus":0.01957425526632279,"score_gpt":0.23797451487628216,"score_spread":0.21840025960995937,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4377249382","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":[0.9953365,0.000053742824,0.0014976084,0.000030984116,0.000018295072,0.000007362286,0.00010301764,0.000027598242,0.0029248786],"genre_scores_gemma":[0.9984938,0.000018030678,0.00021004517,0.000005574873,0.000003079624,0.0000028055917,0.000111446956,0.000004540118,0.0011506941],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999534,0.000004461365,0.0000018033381,0.0000080610025,0.00001713543,0.000015085061],"domain_scores_gemma":[0.99987316,0.00004425812,0.00001826302,0.000009965292,0.000032232136,0.00002212871],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00005002184,0.00019763771,0.00014309945,0.0002678286,0.00021393466,0.000178504,0.00014475275,0.0003469882,0.0019710108],"category_scores_gemma":[0.0001744129,0.00008753872,0.0002452018,0.00012550544,0.00013797711,0.0001192401,0.000111405185,0.00019539522,0.0001716046],"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":[0.0017340076,0.00022925592,0.04631626,0.00023547656,0.00009529723,0.0037885194,0.0006293488,0.17773701,0.7267679,0.0018354096,0.0027389715,0.037892535],"study_design_scores_gemma":[0.00004687214,0.0017371728,0.4703291,0.000027170181,0.000039696795,0.0012809414,0.0007634461,0.47343323,0.049370028,0.00040655216,0.0024986842,0.00006703822],"about_ca_topic_score_codex":0.0016887302,"about_ca_topic_score_gemma":0.0010881393,"teacher_disagreement_score":0.0019710108,"about_ca_system_score_codex":0.00010517453,"about_ca_system_score_gemma":0.000074686235,"threshold_uncertainty_score":0.0065936446},"labels":[],"label_agreement":null},{"id":"W4377249642","doi":"10.1063/5.0113351","title":"Design and analysis of a chord wise morphing wing using NACA0015 airfoil","year":2023,"lang":"en","type":"article","venue":"AIP conference proceedings","topic":"Aeroelasticity and Vibration Control","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 Waterloo","funders":"","keywords":"Morphing; Airfoil; Chord (peer-to-peer); Computer science; Wing; Computer graphics (images); Structural engineering; Engineering; Computer network","score_opus":0.04341137577324193,"score_gpt":0.24907104407338687,"score_spread":0.20565966830014493,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4377249642","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":[0.44760644,0.0004090804,0.5281608,0.00023523235,0.0000875963,0.00023434855,0.00009369192,0.00092304434,0.022249708],"genre_scores_gemma":[0.96070766,0.00007935726,0.036119197,0.000028728442,0.000008414518,0.00005300433,0.000035464338,0.000043734264,0.002924571],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999198,0.000014069995,0.000003201137,0.0000092389955,0.000040156097,0.000013468348],"domain_scores_gemma":[0.9999236,0.000014502854,0.000017581086,0.000010113006,0.000024344992,0.000009969483],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015733497,0.00032517657,0.00032183426,0.00020721184,0.00031462446,0.0003359304,0.00053763855,0.0004367826,0.0015494609],"category_scores_gemma":[0.00017292157,0.00016295441,0.00033044713,0.00008572202,0.00020348828,0.00015288666,0.0002632245,0.00021968782,0.00020481854],"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":[0.00017017363,0.00006185385,0.0022450692,0.00020707255,0.000059754057,0.00031442996,0.00007728937,0.77545583,0.1648732,0.0031620795,0.00057863607,0.052794687],"study_design_scores_gemma":[0.000023612585,0.00029495853,0.001633205,0.0000083213645,0.000026823143,0.000086548025,0.000026906102,0.98122865,0.014187643,0.00019223837,0.002281801,0.000009322634],"about_ca_topic_score_codex":0.0022024687,"about_ca_topic_score_gemma":0.001562838,"teacher_disagreement_score":0.0022024687,"about_ca_system_score_codex":0.0002611983,"about_ca_system_score_gemma":0.000422716,"threshold_uncertainty_score":0.0051834583},"labels":[],"label_agreement":null},{"id":"W4379743266","doi":"10.32920/23328482.v1","title":"Frequency Analysis of Wing with Morphing Winglets","year":2023,"lang":"en","type":"preprint","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Morphing; Wing; Aeroelasticity; Structural engineering; Flutter; Swept wing; Wingtip device; Aerospace; Extrapolation; Natural frequency; MATLAB; Computer science; Engineering; Vibration; Aerospace engineering; Aerodynamics; Acoustics; Physics; Computer graphics (images); Mathematics","score_opus":0.02419805949690963,"score_gpt":0.22387235557688234,"score_spread":0.19967429607997272,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4379743266","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":[0.9813401,0.000040670813,0.017155482,0.000033377426,0.000019330566,0.000019567813,0.00006976949,0.000084410465,0.0012373552],"genre_scores_gemma":[0.9932069,0.000035457877,0.005610901,0.000011895581,0.0000036999681,0.000012546924,0.00010167124,0.000018051138,0.0009989543],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998311,0.000016138038,0.000007260178,0.000038297672,0.00008441425,0.00002273997],"domain_scores_gemma":[0.9997985,0.000057376365,0.000028502101,0.000047743102,0.00005486515,0.0000131424185],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021069976,0.00023227476,0.0002175241,0.00026422145,0.00024682024,0.0002199385,0.00028411567,0.00029372517,0.0011696361],"category_scores_gemma":[0.0003830129,0.00012326897,0.00032890175,0.0001449591,0.00032582233,0.00024339453,0.0002781065,0.00022891577,0.00020061395],"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":[0.00018275414,0.00007534204,0.0047431537,0.00007788874,0.000013752271,0.00032845687,0.00037854057,0.020377811,0.9508772,0.00083089643,0.0002740212,0.021840293],"study_design_scores_gemma":[0.000023037792,0.0012610637,0.033350207,0.00001760016,0.000035712437,0.00038818966,0.0004546176,0.27774465,0.68199587,0.0005527441,0.0041301255,0.000046274825],"about_ca_topic_score_codex":0.0006205551,"about_ca_topic_score_gemma":0.00045810084,"teacher_disagreement_score":0.0011696361,"about_ca_system_score_codex":0.00018345963,"about_ca_system_score_gemma":0.000091300426,"threshold_uncertainty_score":0.003912747},"labels":[],"label_agreement":null},{"id":"W4379745706","doi":"10.32920/23328482","title":"Frequency Analysis of Wing with Morphing Winglets","year":2023,"lang":"en","type":"preprint","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Morphing; Wing; Aeroelasticity; Structural engineering; Flutter; Swept wing; Wingtip device; Aerospace; Extrapolation; Natural frequency; MATLAB; Engineering; Computer science; Vibration; Aerospace engineering; Aerodynamics; Acoustics; Physics; Mathematics; Computer graphics (images)","score_opus":0.02419805949690963,"score_gpt":0.22387235557688234,"score_spread":0.19967429607997272,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4379745706","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":[0.9813401,0.000040670813,0.017155482,0.000033377426,0.000019330566,0.000019567813,0.00006976949,0.000084410465,0.0012373552],"genre_scores_gemma":[0.9932069,0.000035457877,0.005610901,0.000011895581,0.0000036999681,0.000012546924,0.00010167124,0.000018051138,0.0009989543],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998311,0.000016138038,0.000007260178,0.000038297672,0.00008441425,0.00002273997],"domain_scores_gemma":[0.9997985,0.000057376365,0.000028502101,0.000047743102,0.00005486515,0.0000131424185],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00021069976,0.00023227476,0.0002175241,0.00026422145,0.00024682024,0.0002199385,0.00028411567,0.00029372517,0.0011696361],"category_scores_gemma":[0.0003830129,0.00012326897,0.00032890175,0.0001449591,0.00032582233,0.00024339453,0.0002781065,0.00022891577,0.00020061395],"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":[0.00018275414,0.00007534204,0.0047431537,0.00007788874,0.000013752271,0.00032845687,0.00037854057,0.020377811,0.9508772,0.00083089643,0.0002740212,0.021840293],"study_design_scores_gemma":[0.000023037792,0.0012610637,0.033350207,0.00001760016,0.000035712437,0.00038818966,0.0004546176,0.27774465,0.68199587,0.0005527441,0.0041301255,0.000046274825],"about_ca_topic_score_codex":0.0006205551,"about_ca_topic_score_gemma":0.00045810084,"teacher_disagreement_score":0.0011696361,"about_ca_system_score_codex":0.00018345963,"about_ca_system_score_gemma":0.000091300426,"threshold_uncertainty_score":0.003912747},"labels":[],"label_agreement":null},{"id":"W4381432163","doi":"10.1061/jaeeez.aseng-4769","title":"Aeroelastic Design-Space Exploration for Gust-Energy Harvesting","year":2023,"lang":"en","type":"article","venue":"Journal of Aerospace Engineering","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto","funders":"","keywords":"Aeroelasticity; Parametric statistics; Torsion (gastropod); Structural engineering; Stiffness; Wing; Work (physics); Energy (signal processing); Energy harvesting; Computer science; Aerospace engineering; Engineering; Mathematics; Aerodynamics; Mechanical engineering","score_opus":0.02749325232340314,"score_gpt":0.21422238249447728,"score_spread":0.18672913017107415,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4381432163","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":[0.6733391,0.0006133725,0.3146151,0.00013869473,0.000024230332,0.00023370063,0.0001269965,0.00031196076,0.010596857],"genre_scores_gemma":[0.94491374,0.00015763141,0.053749688,0.000020538035,0.000002832561,0.000099735495,0.00005624666,0.000023146786,0.0009763789],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99980503,0.000052775726,0.000008165271,0.00002693927,0.000076494696,0.000030502446],"domain_scores_gemma":[0.99975973,0.00010906415,0.000055849523,0.000029002465,0.00003587028,0.000010386691],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00063840335,0.0005705258,0.00030550122,0.00041349305,0.0001673295,0.00044050778,0.00029543642,0.0003360438,0.001440054],"category_scores_gemma":[0.0006817527,0.00019183347,0.00036060705,0.00021182558,0.00030770054,0.00033448293,0.00034593043,0.00029918074,0.00017927172],"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":[0.00030345167,0.0003349638,0.003084394,0.00030957515,0.00006154286,0.000117088486,0.00012761696,0.7537471,0.16244052,0.004219133,0.0002734775,0.07498109],"study_design_scores_gemma":[0.000074434276,0.0028441192,0.0053313784,0.00004200506,0.00007121981,0.0001319469,0.00014973916,0.91739637,0.06575147,0.0038501837,0.00431679,0.000040316667],"about_ca_topic_score_codex":0.00037877978,"about_ca_topic_score_gemma":0.0009565932,"teacher_disagreement_score":0.001440054,"about_ca_system_score_codex":0.00026256003,"about_ca_system_score_gemma":0.0003693371,"threshold_uncertainty_score":0.004817426},"labels":[],"label_agreement":null},{"id":"W4382243047","doi":"10.1007/978-3-031-29933-9_30","title":"Aerodynamic Shape Optimization of the Morphing Leading Edge for the UAS-S45 Winglet","year":2023,"lang":"en","type":"book-chapter","venue":"Sustainable aviation","topic":"Aeroelasticity and Vibration Control","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":"École de Technologie Supérieure","funders":"","keywords":"Wingtip device; Airfoil; Aerodynamics; Leading edge; Lift-induced drag; Aerospace engineering; Morphing; Engineering; Lift-to-drag ratio; Drag; Structural engineering; Computer science; Artificial intelligence","score_opus":0.011810507927769411,"score_gpt":0.2015419730883647,"score_spread":0.18973146516059528,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4382243047","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":[0.11206641,0.0009399386,0.81183445,0.00029191506,0.00019807457,0.00008393951,0.00018489646,0.00043708825,0.07396331],"genre_scores_gemma":[0.75166196,0.0008117947,0.1966555,0.00012546199,0.00006873156,0.00010619679,0.0003546046,0.00043777886,0.04977793],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999484,0.000007736465,0.0000014424913,0.0000075565863,0.000026736443,0.000008175941],"domain_scores_gemma":[0.99996316,0.000012383997,0.00000304441,0.0000049227783,0.000011899085,0.000004538429],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00013284152,0.00036372355,0.00033074594,0.0001589016,0.00019461116,0.00040999346,0.0003498264,0.00046442347,0.0038889218],"category_scores_gemma":[0.0002229514,0.00019612206,0.00044997575,0.00012556852,0.00020362025,0.00023086875,0.0004110446,0.00044006732,0.00081687694],"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":[0.00010650814,0.0000591079,0.0005864742,0.0001230374,0.000019376715,0.000108543485,0.000079635,0.7814376,0.03750144,0.014742066,0.0040183603,0.16121796],"study_design_scores_gemma":[0.0000063171506,0.00007222049,0.00038837342,0.000013429399,0.0000052090086,0.00005701399,0.00002516212,0.9884525,0.0031854592,0.0026837098,0.0051041134,0.000006437023],"about_ca_topic_score_codex":0.0010591733,"about_ca_topic_score_gemma":0.0014250957,"teacher_disagreement_score":0.0038889218,"about_ca_system_score_codex":0.00020309248,"about_ca_system_score_gemma":0.00028885694,"threshold_uncertainty_score":0.013009787},"labels":[],"label_agreement":null},{"id":"W4386285244","doi":"10.18280/mmep.100414","title":"Advanced Hybrid Nonlinear Control for Morphing Quadrotors","year":2023,"lang":"en","type":"article","venue":"Mathematical Modelling and Engineering Problems","topic":"Aeroelasticity and Vibration Control","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":"Morphing; Nonlinear system; Computer science; Control theory (sociology); Control (management); Nonlinear control; Control engineering; Artificial intelligence; Engineering; Physics","score_opus":0.017248818729704424,"score_gpt":0.20561681205619883,"score_spread":0.1883679933264944,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4386285244","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":[0.08947068,0.0004350863,0.904626,0.00008329592,0.00009147718,0.00003179869,0.000021867094,0.0002428433,0.0049968194],"genre_scores_gemma":[0.9454077,0.00016286412,0.050809383,0.000044571345,0.00001788841,0.00004135764,0.00002795163,0.000017652861,0.0034706278],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99994004,0.000009807802,0.0000029058822,0.000017063254,0.00002291,0.0000073760298],"domain_scores_gemma":[0.9999285,0.000021536302,0.00001986418,0.000008057004,0.00001658711,0.000005473783],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001382707,0.0003558258,0.0002032796,0.00013104867,0.000129995,0.00024613988,0.00029651262,0.00017951205,0.0007409638],"category_scores_gemma":[0.00019524083,0.000096546886,0.00014765517,0.00008680397,0.00028858965,0.00019604502,0.00032661352,0.00021515139,0.00012499915],"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":[0.00013494314,0.00004855688,0.00068303896,0.00015688426,0.000031543455,0.00017546944,0.0000990583,0.69028527,0.18059573,0.0075683827,0.00065928337,0.119561866],"study_design_scores_gemma":[0.000007585261,0.00013183986,0.00032783396,0.00000341108,0.000002884677,0.000034885576,0.0000070705773,0.99232614,0.0051581105,0.0005875646,0.0014069191,0.0000058153387],"about_ca_topic_score_codex":0.0011148518,"about_ca_topic_score_gemma":0.001355767,"teacher_disagreement_score":0.0011148518,"about_ca_system_score_codex":0.00021023098,"about_ca_system_score_gemma":0.00012064538,"threshold_uncertainty_score":0.002478838},"labels":[],"label_agreement":null},{"id":"W4386371884","doi":"10.3390/act12090350","title":"A Self–Tuning Intelligent Controller for a Smart Actuation Mechanism of a Morphing Wing Based on Shape Memory Alloys","year":2023,"lang":"en","type":"article","venue":"Actuators","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":14,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"École de Technologie Supérieure","funders":"Natural Sciences and Engineering Research Council of Canada; Consortium de Recherche et d’innovation en Aérospatiale au Québec","keywords":"Morphing; Actuator; Smart material; Wing; Shape-memory alloy; Flutter; Flight envelope; Engineering; Mechanical engineering; Controller (irrigation); Aerospace engineering; Aeroelasticity; Mechanism (biology); Pneumatic actuator; Aerodynamics; Computer science; Materials science; Artificial intelligence; Electrical engineering","score_opus":0.017974136906025763,"score_gpt":0.2273469169711576,"score_spread":0.20937278006513185,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4386371884","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":[0.34884393,0.0011508253,0.6298211,0.00019850137,0.00033344692,0.0002316264,0.000072303665,0.0034189066,0.01592939],"genre_scores_gemma":[0.9496857,0.00013469641,0.045858506,0.00006583563,0.000024609379,0.00006429547,0.000027082247,0.000038665294,0.0041006543],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.999908,0.0000085905085,0.0000069666175,0.00002510233,0.000041113457,0.000010346943],"domain_scores_gemma":[0.99990654,0.000018987223,0.000021843014,0.000017103346,0.000026595228,0.000008913878],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00014446305,0.00029000128,0.0001874752,0.00023563945,0.0001682132,0.0003129704,0.0007052933,0.00029182457,0.0014037223],"category_scores_gemma":[0.00017698984,0.00012195262,0.00024788218,0.00006831542,0.00019175922,0.00020121741,0.00016498944,0.00018772097,0.00028043654],"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":[0.00021383193,0.00005295226,0.00045565979,0.00019853111,0.0000388127,0.0002320316,0.0001237713,0.010892186,0.9171014,0.0029189715,0.00049438904,0.06727749],"study_design_scores_gemma":[0.00013557884,0.0011399905,0.0049562994,0.000047493086,0.00011547101,0.0008980281,0.000059020706,0.4097832,0.5551928,0.0009953735,0.02660738,0.00006930491],"about_ca_topic_score_codex":0.00032947387,"about_ca_topic_score_gemma":0.00040832814,"teacher_disagreement_score":0.0014037223,"about_ca_system_score_codex":0.00012827932,"about_ca_system_score_gemma":0.00012991793,"threshold_uncertainty_score":0.0046958923},"labels":[],"label_agreement":null},{"id":"W4388089548","doi":"10.1016/j.cja.2023.10.024","title":"Seamless morphing trailing edge flaps for UAS-S45 using high-fidelity aerodynamic optimization","year":2023,"lang":"en","type":"article","venue":"Chinese Journal of Aeronautics","topic":"Aeroelasticity and Vibration Control","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":"École de Technologie Supérieure; Université du Québec à Montréal","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Morphing; Trailing edge; Aerodynamics; Aerospace engineering; Computer science; Enhanced Data Rates for GSM Evolution; Fidelity; Engineering; Physics; Structural engineering; Computer vision","score_opus":0.018337921072760034,"score_gpt":0.2605425205243306,"score_spread":0.24220459945157055,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4388089548","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":[0.54441106,0.00030901187,0.44642645,0.00009171777,0.00003678424,0.000096491094,0.00007923815,0.00032525492,0.008223987],"genre_scores_gemma":[0.94076693,0.00006522034,0.05838533,0.000010610153,0.0000033246338,0.000053708787,0.000035920468,0.0000133746835,0.00066565425],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99994254,0.00001129393,0.0000028243737,0.000010153767,0.000021657983,0.000011496952],"domain_scores_gemma":[0.9999249,0.000030419296,0.0000141032215,0.000012254364,0.000012209221,0.000006250352],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00022541807,0.00036519868,0.00026106634,0.00018401604,0.00019852616,0.00028897953,0.00023736445,0.00031954644,0.00083095947],"category_scores_gemma":[0.00026119928,0.00015610243,0.00038344602,0.00010553418,0.00020855134,0.00023463214,0.00032915865,0.00026555546,0.00010517473],"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":[0.00007109801,0.000050802104,0.0020087936,0.000088860645,0.000016954824,0.00013464152,0.000041759748,0.9095388,0.049670245,0.0017266012,0.00018700487,0.036464427],"study_design_scores_gemma":[0.000007826422,0.00012984723,0.00062071154,0.0000041633966,0.000005619286,0.00003773767,0.000012934611,0.99500954,0.0034837232,0.00027850666,0.00040394897,0.0000054530615],"about_ca_topic_score_codex":0.0009268576,"about_ca_topic_score_gemma":0.0011386832,"teacher_disagreement_score":0.0009268576,"about_ca_system_score_codex":0.00014645139,"about_ca_system_score_gemma":0.00029896403,"threshold_uncertainty_score":0.0027797818},"labels":[],"label_agreement":null},{"id":"W4388552075","doi":"10.1016/j.jfluidstructs.2023.104016","title":"Electroactive morphing effects on the aerodynamic performance through wobulation around an A320 wing with vibrating trailing edge at high Reynolds number","year":2023,"lang":"en","type":"article","venue":"Journal of Fluids and Structures","topic":"Aeroelasticity and Vibration Control","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":"Ontario Tech University","funders":"Office National d'études et de Recherches Aérospatiales; European Commission; Natural Sciences and Engineering Research Council of Canada; Horizon 2020 Framework Programme; Partnership for Advanced Computing in Europe AISBL; University of Ontario Institute of Technology","keywords":"Morphing; Trailing edge; Reynolds number; Drag; Aerodynamics; Lift-to-drag ratio; Wing; Vortex shedding; Physics; Wake; Mechanics; Lift-induced drag; Aerospace engineering; Acoustics; Turbulence; Engineering; Computer science","score_opus":0.008178009043150901,"score_gpt":0.2124705181433689,"score_spread":0.20429250910021798,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4388552075","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":[0.99908733,0.000021136691,0.0004479511,0.000010498314,0.0000044635835,0.0000013146172,0.0000056287286,0.000012472479,0.00040939546],"genre_scores_gemma":[0.9997161,0.000009896649,0.00010271371,0.0000022433878,7.4095794e-7,5.6980394e-7,0.0000029783705,0.0000025679763,0.00016214137],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999583,0.0000063058715,0.000002205019,0.000007025214,0.000013349734,0.000012887873],"domain_scores_gemma":[0.99986744,0.000057007182,0.00001887228,0.000013818375,0.00002054346,0.000022358212],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000081349805,0.00018681944,0.00016331326,0.00011059493,0.00020055028,0.00021140628,0.00016324477,0.0002258789,0.001532288],"category_scores_gemma":[0.00029106354,0.00010171321,0.000124038,0.00007537259,0.00029060713,0.0001804334,0.0002442489,0.00013353507,0.000118195014],"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":[0.000704411,0.00007712963,0.001704296,0.000042486427,0.000011247007,0.00043285923,0.00013379336,0.009618155,0.978956,0.00026916934,0.00008475647,0.007965796],"study_design_scores_gemma":[0.000120385586,0.003151482,0.089189336,0.000024606563,0.00008972032,0.0007523217,0.0005821844,0.24881935,0.6555547,0.00046023293,0.0011691808,0.00008648898],"about_ca_topic_score_codex":0.00028993574,"about_ca_topic_score_gemma":0.00037257854,"teacher_disagreement_score":0.001532288,"about_ca_system_score_codex":0.00007166933,"about_ca_system_score_gemma":0.000064771455,"threshold_uncertainty_score":0.0051259995},"labels":[],"label_agreement":null},{"id":"W4388775518","doi":"10.1007/978-3-031-45321-2_7","title":"Aerodynamic Shape Optimization and the Effect of Morphing Winglet-Induced Tip Vortex Structure on the UAS-S45","year":2023,"lang":"en","type":"book-chapter","venue":"Sustainable aviation","topic":"Aeroelasticity and Vibration Control","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":"École de Technologie Supérieure","funders":"","keywords":"Wingtip device; Morphing; Camber (aerodynamics); Aerospace engineering; Fuel efficiency; Aerodynamics; Engineering; Drag; Wing; Trim; Elevator; Lift-to-drag ratio; Automotive engineering; Aeronautics; Computer science; Structural engineering","score_opus":0.004431787597191634,"score_gpt":0.17414039155637626,"score_spread":0.16970860395918463,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4388775518","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":[0.7261866,0.0025034205,0.12775968,0.00050005276,0.0002959662,0.000038356487,0.00014310489,0.00030823096,0.14226459],"genre_scores_gemma":[0.9715547,0.0005967287,0.012066023,0.00004146627,0.000027785007,0.000009671905,0.000049789287,0.00011165367,0.015542272],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999634,0.000010449291,0.000001067676,0.0000051415136,0.000013471158,0.0000064943706],"domain_scores_gemma":[0.999933,0.000038662034,0.0000068165855,0.0000063223915,0.000009261313,0.0000059181007],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000096607495,0.00024039771,0.0002675045,0.00010239246,0.00018974871,0.00041382667,0.00015422757,0.00027693599,0.004048554],"category_scores_gemma":[0.00030544004,0.00012056385,0.00023993151,0.00012778952,0.00025852697,0.00023329016,0.0002501319,0.00024316978,0.00044404183],"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":[0.00040918347,0.00013042332,0.00090029504,0.00011464802,0.000027385102,0.00018716214,0.00005996455,0.7389186,0.12057528,0.026059574,0.002244223,0.110373266],"study_design_scores_gemma":[0.000015110855,0.00016825617,0.0018475952,0.000010147503,0.00000883113,0.00006481299,0.000033666995,0.97481245,0.014925606,0.0055352133,0.0025671374,0.000011186615],"about_ca_topic_score_codex":0.00051578163,"about_ca_topic_score_gemma":0.0006648949,"teacher_disagreement_score":0.004048554,"about_ca_system_score_codex":0.0001574163,"about_ca_system_score_gemma":0.00011425937,"threshold_uncertainty_score":0.013543785},"labels":[],"label_agreement":null},{"id":"W4389584805","doi":"10.17118/11143/20918","title":"Finite element analysis of bimorph piezoelectric actuators consideringthermopiezoelectricity","year":2023,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"York University","funders":"","keywords":"Bimorph; Finite element method; Actuator; Piezoelectricity; Computer science; Structural engineering; Acoustics; Materials science; Engineering; Physics; Artificial intelligence","score_opus":0.013977832192956334,"score_gpt":0.2216717640147916,"score_spread":0.20769393182183526,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4389584805","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":[0.52037245,0.00038593533,0.4499431,0.00041199423,0.00010743228,0.00020200151,0.00032558385,0.00050795666,0.027743561],"genre_scores_gemma":[0.9604972,0.00012979782,0.033083286,0.00005343351,0.00001168607,0.00016809728,0.00012262938,0.00006234179,0.0058714957],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99972326,0.00005830443,0.000011767865,0.000036742767,0.0001295748,0.000040313036],"domain_scores_gemma":[0.9993457,0.0003985293,0.00007193521,0.00004503123,0.00010352498,0.00003524743],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005728774,0.00052570686,0.00068527384,0.0006413901,0.0005146335,0.0008354572,0.0009807149,0.001948252,0.003975686],"category_scores_gemma":[0.0012975588,0.00051615224,0.00069516286,0.00033612104,0.0008314058,0.00043434885,0.0006685281,0.0005746788,0.00044913107],"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":[0.000035038272,0.0000556025,0.000603331,0.00005050075,0.000016028784,0.000076685654,0.00005583471,0.9890832,0.005187307,0.0013777398,0.00009442558,0.0033644026],"study_design_scores_gemma":[0.0000027529238,0.000014499108,0.00013615075,0.0000044037474,0.0000023414996,0.00000638928,0.00001169306,0.999,0.00055897096,0.00011373076,0.00014621031,0.000002852638],"about_ca_topic_score_codex":0.00583936,"about_ca_topic_score_gemma":0.0040277215,"teacher_disagreement_score":0.00583936,"about_ca_system_score_codex":0.0006543909,"about_ca_system_score_gemma":0.0011262804,"threshold_uncertainty_score":0.013300002},"labels":[],"label_agreement":null},{"id":"W4390229016","doi":"10.1177/10775463231223778","title":"Nonlinear flap for passive flutter control of bidimensional wing","year":2023,"lang":"en","type":"article","venue":"Journal of Vibration and Control","topic":"Aeroelasticity and Vibration Control","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","keywords":"Aeroelasticity; Control theory (sociology); Nonlinear system; Flutter; Wing; Tuned mass damper; Damper; Aerodynamics; Stiffness; Engineering; Flight control surfaces; Structural engineering; Aerodynamic force; Computer science; Physics; Aerospace engineering; Control (management)","score_opus":0.008318834430395071,"score_gpt":0.2190346489122921,"score_spread":0.21071581448189702,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4390229016","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":[0.42928004,0.000468966,0.5619465,0.00015957012,0.0001337559,0.00011543903,0.000062947016,0.0003601133,0.0074725426],"genre_scores_gemma":[0.9495249,0.00009838304,0.047975097,0.000026784923,0.000008210569,0.000062352636,0.000021480173,0.000012813499,0.0022699607],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999348,0.000011898452,0.0000035294872,0.000014464453,0.000029832936,0.000005455489],"domain_scores_gemma":[0.9999175,0.000028711156,0.000015736541,0.000015152184,0.000016996315,0.000005830461],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015330577,0.00028830007,0.00016423462,0.00008040519,0.0001294105,0.00020877199,0.00026667662,0.00024267321,0.0010839863],"category_scores_gemma":[0.00020277436,0.00006340139,0.0001245683,0.000040602667,0.000241966,0.00019300806,0.00023169062,0.00023329038,0.00015681883],"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":[0.00025130817,0.0000833246,0.00074443466,0.00034284499,0.000015994752,0.00019212942,0.00018107887,0.056367148,0.86713743,0.0055442085,0.00036368944,0.06877633],"study_design_scores_gemma":[0.0000849119,0.0013616646,0.0021124014,0.000040470415,0.000021811278,0.00026937714,0.000039405768,0.7960504,0.19039614,0.0016049244,0.00798584,0.000032595675],"about_ca_topic_score_codex":0.00016667439,"about_ca_topic_score_gemma":0.00023799694,"teacher_disagreement_score":0.0010839863,"about_ca_system_score_codex":0.00010343773,"about_ca_system_score_gemma":0.0000894565,"threshold_uncertainty_score":0.0036263466},"labels":[],"label_agreement":null},{"id":"W4391300876","doi":"10.2514/6.2024-2150","title":"Design and Optimization of Droop Nose Leading Edge (DNLE) Morphing Wing Skin for the UAS-S45","year":2024,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"École de Technologie Supérieure","funders":"","keywords":"Voltage droop; Morphing; Wing; Computer science; Enhanced Data Rates for GSM Evolution; Engineering; Computer vision; Aerospace engineering; Electrical engineering","score_opus":0.019578793117450914,"score_gpt":0.23237467720639812,"score_spread":0.2127958840889472,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4391300876","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":[0.66818357,0.0003189729,0.32121852,0.00007352801,0.000037097623,0.000101963575,0.00006332644,0.00023441736,0.009768514],"genre_scores_gemma":[0.9615785,0.000091165864,0.037057612,0.000012682736,0.0000025340278,0.000033238226,0.000032502747,0.000022398372,0.0011694792],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999261,0.000011606685,0.0000029463401,0.000015931457,0.000027115104,0.00001636471],"domain_scores_gemma":[0.99994946,0.000011078498,0.0000126920795,0.0000055500755,0.000012456983,0.000008733327],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012951123,0.00034581867,0.00021685501,0.000252396,0.00016478474,0.00028818383,0.000219937,0.00029521962,0.000816828],"category_scores_gemma":[0.00016909766,0.0001659204,0.0003589922,0.000094518655,0.00017381822,0.00019408653,0.00027907014,0.00019233438,0.00014076881],"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":[0.0001435826,0.000061656014,0.0030710737,0.00020891923,0.000034901524,0.00043305403,0.000096312906,0.6223568,0.31466776,0.001971876,0.00030877776,0.05664524],"study_design_scores_gemma":[0.000019893025,0.0005039203,0.0035865447,0.000014036981,0.000026464591,0.00020758226,0.00009882237,0.9540853,0.03859214,0.00044696583,0.0024006935,0.000017556453],"about_ca_topic_score_codex":0.00060222036,"about_ca_topic_score_gemma":0.0009831697,"teacher_disagreement_score":0.000816828,"about_ca_system_score_codex":0.00017330999,"about_ca_system_score_gemma":0.0002599556,"threshold_uncertainty_score":0.0027325153},"labels":[],"label_agreement":null},{"id":"W4391824889","doi":"10.1016/j.ast.2024.108993","title":"Optimal design and analysis of a deformable mechanism for a redundantly driven variable swept wing","year":2024,"lang":"en","type":"article","venue":"Aerospace Science and Technology","topic":"Aeroelasticity and Vibration Control","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":"National Natural Science Foundation of China","keywords":"Actuator; Mechanism (biology); Slider; Control theory (sociology); Morphing; MATLAB; Wing; Compliant mechanism; Computer science; Variable (mathematics); Simulation; Engineering; Mechanical engineering; Aerospace engineering; Structural engineering; Physics; Mathematics; Finite element method","score_opus":0.008119421260021704,"score_gpt":0.22032536035274716,"score_spread":0.21220593909272545,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4391824889","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":[0.12793854,0.0004159634,0.86112124,0.0003286985,0.00008149844,0.00013438179,0.00007480629,0.00016534177,0.009739521],"genre_scores_gemma":[0.9545916,0.00018264126,0.040934555,0.000045138855,0.00002019241,0.00013099433,0.000039375805,0.0000355451,0.0040201223],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99978274,0.000047029436,0.000009261281,0.000035552668,0.0000917711,0.000033577424],"domain_scores_gemma":[0.9996984,0.00011896791,0.00007908611,0.000025126501,0.000053642427,0.0000248305],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00064559013,0.00064176373,0.0008224608,0.0004818306,0.00042784202,0.0006932982,0.0007337452,0.00169554,0.002919673],"category_scores_gemma":[0.0010175399,0.00072032126,0.0006914374,0.00021153937,0.0007894852,0.00036913945,0.00084410043,0.00050742226,0.00033492138],"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":[0.00008039652,0.000027148155,0.00022408702,0.00007083651,0.000025941934,0.00013389516,0.000034231503,0.97662896,0.010905873,0.0051642773,0.00011352821,0.0065907678],"study_design_scores_gemma":[0.000014724198,0.00007451291,0.00018107267,0.0000042594243,0.000008250867,0.000014830882,0.000009451622,0.9985442,0.00042290732,0.0005011554,0.00021958344,0.000005008806],"about_ca_topic_score_codex":0.0036378962,"about_ca_topic_score_gemma":0.0024140417,"teacher_disagreement_score":0.0036378962,"about_ca_system_score_codex":0.0004754467,"about_ca_system_score_gemma":0.0011801937,"threshold_uncertainty_score":0.009767294},"labels":[],"label_agreement":null},{"id":"W4392382873","doi":"10.32920/25336306","title":"Rib Design for a Flexible Trailing Edge of Aircraft","year":2024,"lang":"en","type":"preprint","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Morphing; Trailing edge; Software; Wing; Finite element method; Computer science; CAD; Structural engineering; Engineering; Engineering drawing; Mechanical engineering; Aerospace engineering; Computer graphics (images)","score_opus":0.04126937081254387,"score_gpt":0.2621284575370391,"score_spread":0.22085908672449525,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4392382873","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":[0.051818345,0.000642436,0.87447286,0.00016825563,0.00021100945,0.00018393694,0.00029302522,0.001560856,0.07064932],"genre_scores_gemma":[0.58062375,0.00052512705,0.3854403,0.0001746929,0.000046382203,0.00018643177,0.00042935822,0.00034665165,0.032227352],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.999731,0.00003744838,0.000015438414,0.000037411795,0.00014641891,0.000032211483],"domain_scores_gemma":[0.9998386,0.000021970027,0.000027065998,0.000036092762,0.000063287654,0.000012929242],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00026179466,0.00038650312,0.00021942177,0.00035601226,0.00029023306,0.0006599171,0.000558846,0.00061393715,0.009031813],"category_scores_gemma":[0.0003061952,0.00018324074,0.00047210298,0.00019133587,0.0002725789,0.0002884205,0.0004070346,0.0003801722,0.0028379462],"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":[0.00035015258,0.00011907309,0.0021688805,0.000998335,0.000057427966,0.00082658627,0.00027666823,0.26815337,0.29877764,0.07051726,0.008939344,0.3488153],"study_design_scores_gemma":[0.000086552835,0.0019529804,0.0049772793,0.0002304084,0.00012044288,0.0020864606,0.00018591259,0.6019386,0.13979599,0.0115096755,0.23700513,0.00011060146],"about_ca_topic_score_codex":0.00042078155,"about_ca_topic_score_gemma":0.00069755764,"teacher_disagreement_score":0.009031813,"about_ca_system_score_codex":0.00025929665,"about_ca_system_score_gemma":0.00032870268,"threshold_uncertainty_score":0.03021437},"labels":[],"label_agreement":null},{"id":"W4392383102","doi":"10.32920/25336306.v1","title":"Rib Design for a Flexible Trailing Edge of Aircraft","year":2024,"lang":"en","type":"preprint","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Morphing; Trailing edge; Software; Wing; Finite element method; CAD; Computer science; Engineering; Section (typography); Engineering drawing; Structural engineering; Mechanical engineering; Computer graphics (images)","score_opus":0.04126937081254387,"score_gpt":0.2621284575370391,"score_spread":0.22085908672449525,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4392383102","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":[0.051818345,0.000642436,0.87447286,0.00016825563,0.00021100945,0.00018393694,0.00029302522,0.001560856,0.07064932],"genre_scores_gemma":[0.58062375,0.00052512705,0.3854403,0.0001746929,0.000046382203,0.00018643177,0.00042935822,0.00034665165,0.032227352],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.999731,0.00003744838,0.000015438414,0.000037411795,0.00014641891,0.000032211483],"domain_scores_gemma":[0.9998386,0.000021970027,0.000027065998,0.000036092762,0.000063287654,0.000012929242],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00026179466,0.00038650312,0.00021942177,0.00035601226,0.00029023306,0.0006599171,0.000558846,0.00061393715,0.009031813],"category_scores_gemma":[0.0003061952,0.00018324074,0.00047210298,0.00019133587,0.0002725789,0.0002884205,0.0004070346,0.0003801722,0.0028379462],"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":[0.00035015258,0.00011907309,0.0021688805,0.000998335,0.000057427966,0.00082658627,0.00027666823,0.26815337,0.29877764,0.07051726,0.008939344,0.3488153],"study_design_scores_gemma":[0.000086552835,0.0019529804,0.0049772793,0.0002304084,0.00012044288,0.0020864606,0.00018591259,0.6019386,0.13979599,0.0115096755,0.23700513,0.00011060146],"about_ca_topic_score_codex":0.00042078155,"about_ca_topic_score_gemma":0.00069755764,"teacher_disagreement_score":0.009031813,"about_ca_system_score_codex":0.00025929665,"about_ca_system_score_gemma":0.00032870268,"threshold_uncertainty_score":0.03021437},"labels":[],"label_agreement":null},{"id":"W4392696443","doi":"10.3390/app14062384","title":"A Study on the Surrogate-Based Optimization of Flexible Wings Considering a Flutter Constraint","year":2024,"lang":"en","type":"article","venue":"Applied Sciences","topic":"Aeroelasticity and Vibration Control","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 Victoria","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Flutter; Constraint (computer-aided design); Computer science; Mathematical optimization; Structural engineering; Engineering; Mathematics; Mechanical engineering; Aerospace engineering; Aerodynamics","score_opus":0.03468813933784622,"score_gpt":0.24762347650828748,"score_spread":0.21293533717044125,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4392696443","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":[0.11026302,0.0010640016,0.878753,0.00036327585,0.00012964058,0.00008035669,0.00014636085,0.00021524099,0.008985051],"genre_scores_gemma":[0.87971604,0.00057361013,0.116217814,0.00010096309,0.000050960778,0.00015885996,0.00033251557,0.000106501066,0.0027426702],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99968696,0.00014297757,0.00001298984,0.000039942362,0.00008017937,0.00003689804],"domain_scores_gemma":[0.99870396,0.0009398046,0.00008482989,0.00008315795,0.0001355098,0.000052693376],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0011646516,0.00074269966,0.0008555406,0.00034015393,0.00024126384,0.00084239664,0.00045309114,0.00090713985,0.0012115926],"category_scores_gemma":[0.0029438147,0.00028305256,0.0008716938,0.00033916126,0.00045394775,0.0004373611,0.00055071845,0.0009676872,0.00019188249],"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":[0.000023388959,0.000026162112,0.0003512986,0.000045103356,0.000014973687,0.000029244009,0.0000102457,0.9905688,0.0010977223,0.001832997,0.00013888557,0.0058611976],"study_design_scores_gemma":[0.0000031448242,0.000033318865,0.00011347677,0.0000070799783,0.0000029426644,0.0000107408,0.0000039406877,0.99882156,0.00031369104,0.0003963086,0.00029148237,0.0000022795168],"about_ca_topic_score_codex":0.0017547098,"about_ca_topic_score_gemma":0.0010335768,"teacher_disagreement_score":0.0017547098,"about_ca_system_score_codex":0.0002264441,"about_ca_system_score_gemma":0.0006582663,"threshold_uncertainty_score":0.0061593056},"labels":[],"label_agreement":null},{"id":"W4396684783","doi":"10.1016/j.ymssp.2024.111496","title":"An experimental approach to multi-input multi-output nonlinear active vibration control of a clamped sandwich beam","year":2024,"lang":"en","type":"article","venue":"Mechanical Systems and Signal Processing","topic":"Aeroelasticity and Vibration Control","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":"McGill University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Nonlinear system; Beam (structure); Vibration; Active vibration control; Vibration control; Control theory (sociology); Structural engineering; Engineering; Computer science; Control (management); Physics; Acoustics","score_opus":0.022137766538741367,"score_gpt":0.2592217539774392,"score_spread":0.23708398743869782,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4396684783","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":[0.7903935,0.00027292542,0.20399667,0.00013180844,0.00013636338,0.00024944238,0.00011906037,0.00029309012,0.0044071507],"genre_scores_gemma":[0.97020155,0.0000883546,0.028200053,0.000023455912,0.000008499819,0.00012710995,0.000037491092,0.0000070137194,0.0013065232],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997235,0.00004113607,0.000017002745,0.00006489436,0.00012439278,0.000028990326],"domain_scores_gemma":[0.9996964,0.00009571006,0.00004879421,0.00005630262,0.000081577266,0.000021219823],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00038992972,0.00037393713,0.00026519338,0.0001973033,0.00025237363,0.00034687956,0.0005460828,0.00048442525,0.002012332],"category_scores_gemma":[0.00051177037,0.0001383208,0.00024725127,0.00010542756,0.0004179402,0.00029842442,0.00055444054,0.00047602877,0.00018002577],"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":[0.00017159597,0.00021247834,0.0004489698,0.00021747604,0.000012287895,0.00007039638,0.00010088742,0.0065558166,0.97874886,0.0006100893,0.000056147004,0.01279498],"study_design_scores_gemma":[0.000065836175,0.004331132,0.004763205,0.000028443019,0.000032642005,0.00010160437,0.00013872237,0.09054093,0.8975574,0.00052403926,0.0018827195,0.00003332348],"about_ca_topic_score_codex":0.0004146818,"about_ca_topic_score_gemma":0.00067004777,"teacher_disagreement_score":0.002012332,"about_ca_system_score_codex":0.00018491833,"about_ca_system_score_gemma":0.0002504789,"threshold_uncertainty_score":0.0067319274},"labels":[],"label_agreement":null},{"id":"W4399306704","doi":"10.1088/1742-6596/2762/1/011001","title":"Preface","year":2024,"lang":"en","type":"article","venue":"Journal of Physics Conference Series","topic":"Aeroelasticity and Vibration Control","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":"Computer science","score_opus":0.014415954075567351,"score_gpt":0.21823896083849617,"score_spread":0.20382300676292883,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4399306704","genre_codex":"other","genre_gemma":"editorial","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"editorial","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.001462799,0.013480192,0.0060864957,0.02522293,0.18803279,0.0006452997,0.009837618,0.002012904,0.75321907],"genre_scores_gemma":[0.0042827027,0.006444874,0.0022575015,0.004545236,0.018462501,0.0002427325,0.007449325,0.00075277034,0.9555624],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.99896383,0.00012607423,0.000070169335,0.00018965713,0.0005496308,0.00010074863],"domain_scores_gemma":[0.99627966,0.00048174814,0.00012513294,0.00028800822,0.0021839882,0.0006414273],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0013711858,0.001124315,0.0008936483,0.002385434,0.0022174593,0.0045977947,0.0014903545,0.0014721929,0.50824374],"category_scores_gemma":[0.0074859248,0.00038021477,0.00069178734,0.0018667707,0.0006332509,0.0033929278,0.0022298098,0.0030678557,0.3789015],"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":[0.000024388013,0.000017741457,0.000071934075,0.00009036884,0.0000017470855,0.000036050882,0.000062350424,0.000058672318,0.00011584118,0.0028695054,0.9580046,0.03864687],"study_design_scores_gemma":[0.0000029812477,0.000014681228,0.00017505206,0.00008725762,0.000001083987,0.00005408125,0.0000674272,0.000024022771,0.00004882024,0.0011362889,0.9983846,0.000003653502],"about_ca_topic_score_codex":0.0023869458,"about_ca_topic_score_gemma":0.0027979307,"teacher_disagreement_score":0.50824374,"about_ca_system_score_codex":0.0017248612,"about_ca_system_score_gemma":0.0021588812,"threshold_uncertainty_score":0},"labels":[],"label_agreement":null},{"id":"W4400275862","doi":"10.4050/f-0080-2024-1289","title":"Aerodynamic Optimization and Experimental Analysis of Shrouded Rotor Blades","year":2024,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Thrust; Airfoil; Aerodynamics; Chord (peer-to-peer); Aerospace engineering; Blade element theory; Rotor (electric); Payload (computing); Engineering; Blade element momentum theory; Lift (data mining); Computer science; Mechanical engineering; Automotive engineering","score_opus":0.004516869240271374,"score_gpt":0.21513251562181468,"score_spread":0.21061564638154331,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4400275862","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":[0.9752873,0.00017551686,0.021862412,0.000025879679,0.000028689115,0.000039410195,0.00013050635,0.000120931494,0.0023293134],"genre_scores_gemma":[0.9889981,0.0000811714,0.010003787,0.000004965456,0.0000049158793,0.000025511941,0.00010113724,0.000019314128,0.00076097687],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997807,0.000038051683,0.000013371736,0.000039991697,0.000098001576,0.000029966226],"domain_scores_gemma":[0.9995789,0.0001040919,0.000091708825,0.000077097655,0.00012941431,0.000018799483],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00034756275,0.00032693724,0.00028621047,0.00028203972,0.00024082648,0.00021542337,0.00021136216,0.00027944316,0.00094658625],"category_scores_gemma":[0.00055730186,0.00012233313,0.00022530567,0.00016387452,0.0002707715,0.0001989601,0.00018046197,0.00020060745,0.00021161401],"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":[0.000349265,0.00036762073,0.0037460055,0.00025745673,0.000023253275,0.0001906713,0.0001383373,0.094334066,0.87090975,0.00101953,0.00034432297,0.028319659],"study_design_scores_gemma":[0.00005588265,0.004021336,0.016993368,0.000025929026,0.000027178361,0.00014440496,0.0001407388,0.31420562,0.6613221,0.00038867607,0.0026355453,0.000039188235],"about_ca_topic_score_codex":0.0002531554,"about_ca_topic_score_gemma":0.00038795994,"teacher_disagreement_score":0.00094658625,"about_ca_system_score_codex":0.00015040096,"about_ca_system_score_gemma":0.000116282026,"threshold_uncertainty_score":0.003166616},"labels":[],"label_agreement":null},{"id":"W4400638600","doi":"","title":"Wake flow dynamics of an A320 morphing wing prototype through Time-Resolved PIV and Hi-Fi simulations","year":2024,"lang":"en","type":"article","venue":"HAL (Le Centre pour la Communication Scientifique Directe)","topic":"Aeroelasticity and Vibration Control","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":"Ontario Tech University","funders":"","keywords":"Morphing; Wake; Wing; Aerospace engineering; Flow (mathematics); Computer science; Dynamics (music); Computational fluid dynamics; Simulation; Mechanics; Physics; Computer graphics (images); Acoustics; Engineering","score_opus":0.008750811275697887,"score_gpt":0.21117191551155515,"score_spread":0.20242110423585727,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4400638600","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":[0.99115753,0.000030622916,0.0068264036,0.000035537298,0.000011537118,0.00002276948,0.000098045115,0.00009220506,0.0017253341],"genre_scores_gemma":[0.9965243,0.00001756291,0.0027953861,0.000005057862,0.0000013883807,0.000015430174,0.000057830144,0.000007030877,0.0005760076],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999627,0.000004824813,0.0000018384566,0.0000056772988,0.0000146131315,0.000010405498],"domain_scores_gemma":[0.9999261,0.000024405468,0.000011351112,0.000011182795,0.000013829428,0.000013218843],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000110050736,0.00024246528,0.00021654363,0.00018554977,0.00019800346,0.00026281277,0.00032541502,0.0004257557,0.0009455168],"category_scores_gemma":[0.00018740265,0.000097767595,0.00022353398,0.00008947817,0.00035742234,0.00018224998,0.00021084145,0.00019320486,0.000101917394],"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":[0.00041146,0.00025027647,0.006784605,0.00017224149,0.000035036457,0.00058698,0.0002468022,0.74689376,0.22826134,0.0014421334,0.00052608264,0.014389234],"study_design_scores_gemma":[0.000028806642,0.00029391376,0.0071643717,0.000005760416,0.000007269865,0.00005461079,0.000071199276,0.98001695,0.011737971,0.00017248811,0.00043247995,0.000014103072],"about_ca_topic_score_codex":0.0014588089,"about_ca_topic_score_gemma":0.0009930785,"teacher_disagreement_score":0.0014588089,"about_ca_system_score_codex":0.00015145815,"about_ca_system_score_gemma":0.00019197656,"threshold_uncertainty_score":0.0031630397},"labels":[],"label_agreement":null},{"id":"W4401534127","doi":"10.3390/drones8080392","title":"Novel Twist Morphing Aileron and Winglet Design for UAS Control and Performance","year":2024,"lang":"en","type":"article","venue":"Drones","topic":"Aeroelasticity and Vibration Control","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":"École de Technologie Supérieure; Université du Québec à Montréal","funders":"Canada Research Chairs","keywords":"Aileron; Morphing; Drag; Wingtip device; Twist; Lift-induced drag; Lift-to-drag ratio; Airfoil; Wing; Elevator; Actuator; Computer science; Aerospace engineering; Engineering; Structural engineering; Mathematics; Geometry; Artificial intelligence","score_opus":0.016679267752585485,"score_gpt":0.20250525809252756,"score_spread":0.18582599033994207,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4401534127","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":[0.18074645,0.00034942865,0.8077169,0.000079703,0.00007844458,0.00009956863,0.00006979388,0.00035147372,0.010508198],"genre_scores_gemma":[0.84203494,0.00020211042,0.15341309,0.000046776542,0.000024494491,0.00009788084,0.00009796227,0.00005214629,0.0040306197],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999236,0.000011402284,0.000003643374,0.000015386633,0.00003597147,0.000009941493],"domain_scores_gemma":[0.99993944,0.0000101613305,0.000017380482,0.000008747809,0.000016586786,0.00000767158],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000112220616,0.00039371554,0.0001946258,0.00021983472,0.00012448576,0.00025489216,0.00029053344,0.00028059137,0.0011750814],"category_scores_gemma":[0.00013145141,0.000108797896,0.00019424612,0.000086900465,0.00014080465,0.00028140823,0.00021268082,0.00025773892,0.00026331915],"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":[0.00023951867,0.000093045186,0.0018454117,0.00024025282,0.000030814976,0.00021401678,0.00007149748,0.2406982,0.5846218,0.008554984,0.0008089312,0.16258162],"study_design_scores_gemma":[0.000031332766,0.0012790291,0.002922336,0.000021399635,0.000029910738,0.00036859774,0.0000390538,0.8930048,0.085688,0.0016601672,0.014920496,0.000035071193],"about_ca_topic_score_codex":0.00027069327,"about_ca_topic_score_gemma":0.00044661755,"teacher_disagreement_score":0.0011750814,"about_ca_system_score_codex":0.00015851858,"about_ca_system_score_gemma":0.00016125203,"threshold_uncertainty_score":0.0039310455},"labels":[],"label_agreement":null},{"id":"W4401742261","doi":"10.1088/1742-6596/2820/1/011001","title":"Preface","year":2024,"lang":"en","type":"article","venue":"Journal of Physics Conference Series","topic":"Aeroelasticity and Vibration Control","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":"Computer science","score_opus":0.014415954075567351,"score_gpt":0.21823896083849617,"score_spread":0.20382300676292883,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4401742261","genre_codex":"other","genre_gemma":"editorial","domain_codex":null,"domain_gemma":null,"model_version":"metacan-v3-hybrid-931329e0061c","genre_candidate":"editorial","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0019564815,0.010006286,0.007791183,0.027587984,0.14574526,0.0007203753,0.015445658,0.0025071914,0.78823966],"genre_scores_gemma":[0.012728714,0.008647955,0.004819152,0.008077845,0.032280233,0.00064011995,0.021380402,0.0017178537,0.90970767],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.9987513,0.00017842636,0.000109911874,0.00023714693,0.0006127969,0.00011044365],"domain_scores_gemma":[0.9948655,0.0008618492,0.00021987992,0.0004845884,0.0029327713,0.0006354826],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.001525516,0.001150968,0.0008557698,0.002562328,0.002732679,0.004421324,0.0017198053,0.0016229338,0.49859342],"category_scores_gemma":[0.012071366,0.00036118852,0.00068369583,0.0022082007,0.00079116237,0.003737756,0.002230788,0.003267965,0.3328418],"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":[0.000030897834,0.000017983179,0.00011251993,0.0001518562,0.0000026959044,0.00006795479,0.00015743152,0.00006507405,0.000118849144,0.0045533646,0.9513984,0.043322988],"study_design_scores_gemma":[0.0000038349726,0.000016385698,0.00022255846,0.00013116881,0.0000014825463,0.00007734068,0.000118079464,0.000025201181,0.000055556,0.0014531865,0.9978904,0.0000047293493],"about_ca_topic_score_codex":0.0032052991,"about_ca_topic_score_gemma":0.0026894775,"teacher_disagreement_score":0.49859342,"about_ca_system_score_codex":0.0020058556,"about_ca_system_score_gemma":0.0023908766,"threshold_uncertainty_score":0},"labels":[],"label_agreement":null},{"id":"W4401751422","doi":"10.1109/aim55361.2024.10637077","title":"An Examination of the Thermopiezoelectric Effect in Multilayer Stack Actuators","year":2024,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"York University","funders":"","keywords":"Stack (abstract data type); Actuator; Computer science; Materials science; Artificial intelligence; Operating system","score_opus":0.004046219781584253,"score_gpt":0.21244478488867197,"score_spread":0.2083985651070877,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4401751422","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":[0.9832395,0.0009024299,0.010642079,0.000091049835,0.000030655927,0.000012105767,0.000063351516,0.00010947863,0.0049094385],"genre_scores_gemma":[0.99646384,0.00035469962,0.0025225093,0.000013144285,0.000005311693,0.0000054564302,0.00001733461,0.000016556694,0.0006011414],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99991095,0.0000066953885,0.000003872965,0.0000123131185,0.000047625545,0.000018511208],"domain_scores_gemma":[0.9997949,0.00011957283,0.00003229438,0.000014313825,0.000027980137,0.0000109499715],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016097487,0.00018764581,0.00024314126,0.00017890596,0.00017432828,0.00031293905,0.00019391857,0.00025343965,0.0015196841],"category_scores_gemma":[0.00057244836,0.00014616316,0.00017965469,0.00016004586,0.0002478836,0.0003492436,0.0002936132,0.00022022787,0.00014473274],"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":[0.000093249386,0.000022881162,0.0009202806,0.00013716043,0.000017915907,0.00017659565,0.00009696255,0.011295795,0.9792783,0.0005642463,0.00007048687,0.0073260376],"study_design_scores_gemma":[0.000014797536,0.00044150854,0.01700347,0.000059789647,0.00005779778,0.00031414072,0.00018336103,0.16286243,0.8155025,0.0004570775,0.003069061,0.00003395544],"about_ca_topic_score_codex":0.0005061354,"about_ca_topic_score_gemma":0.0006806043,"teacher_disagreement_score":0.0015196841,"about_ca_system_score_codex":0.0001062268,"about_ca_system_score_gemma":0.00014768446,"threshold_uncertainty_score":0.005083859},"labels":[],"label_agreement":null},{"id":"W4402824879","doi":"10.1007/s00707-024-04074-y","title":"Finite element analysis of thermopiezoelectric bimorph actuators considering temperature-dependent piezoelectric strain coefficients","year":2024,"lang":"en","type":"article","venue":"Acta Mechanica","topic":"Aeroelasticity and Vibration Control","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":"York University","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Bimorph; Solid mechanics; Finite element method; Piezoelectricity; Materials science; Actuator; Strain (injury); Mechanics; Mathematical analysis; Structural engineering; Mathematics; Physics; Composite material; Engineering; Electrical engineering","score_opus":0.009156522693719537,"score_gpt":0.21852480080729866,"score_spread":0.20936827811357914,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4402824879","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":[0.46386287,0.00047695357,0.50506085,0.0003918344,0.00007242344,0.00007792067,0.00013010102,0.00027195117,0.02965499],"genre_scores_gemma":[0.96777713,0.00017629967,0.024072548,0.000039646264,0.000011068978,0.000074336676,0.000054318025,0.000049540773,0.007744956],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99985826,0.000031951746,0.0000047579388,0.00001726683,0.00007083499,0.000016966482],"domain_scores_gemma":[0.9997305,0.00017227563,0.000026376021,0.000021353519,0.000038504277,0.000011055474],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00031856183,0.00030093122,0.0005513156,0.00033391136,0.00030130727,0.0004706305,0.0006308303,0.00097167195,0.0025504017],"category_scores_gemma":[0.00069020427,0.0003753808,0.00037306815,0.00023850237,0.00051795307,0.00047627088,0.0003532944,0.00037207897,0.0003094501],"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":[0.00007943307,0.00006930635,0.00037553688,0.00009376728,0.000020934105,0.00009588578,0.00007535253,0.95871353,0.025908472,0.005777708,0.00014893047,0.008641086],"study_design_scores_gemma":[0.0000022616266,0.0000136306935,0.00018261668,0.0000031649045,0.0000024207825,0.000010598591,0.000010739335,0.9980028,0.0013306942,0.0002785326,0.00015962141,0.000002878097],"about_ca_topic_score_codex":0.0013061627,"about_ca_topic_score_gemma":0.001576398,"teacher_disagreement_score":0.0025504017,"about_ca_system_score_codex":0.00030881938,"about_ca_system_score_gemma":0.00047853464,"threshold_uncertainty_score":0.008531928},"labels":[],"label_agreement":null},{"id":"W4404085617","doi":"10.18280/rcma.340503","title":"Active Vibration Control of Piezoelectric Composite Plates Using Gain Scheduling Method","year":2024,"lang":"fr","type":"article","venue":"Revue des composites et des matériaux avancés","topic":"Aeroelasticity and Vibration Control","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":"Composite number; Piezoelectricity; Vibration; Vibration control; Active vibration control; Materials science; Structural engineering; Computer science; Acoustics; Composite material; Engineering; Physics","score_opus":0.04536105679915554,"score_gpt":0.3009849253521594,"score_spread":0.2556238685530039,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4404085617","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":[0.047454707,0.00029461095,0.9490341,0.000040032694,0.000054488035,0.00003513586,0.0000086743885,0.0002687305,0.0028094915],"genre_scores_gemma":[0.9506513,0.00016017037,0.047340926,0.00001763778,0.000020541574,0.0000432995,0.000011376528,0.000012029527,0.0017426859],"study_design_codex":"simulation_or_modeling","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99989307,0.000015318477,0.000004480589,0.000025793897,0.000051587474,0.000009659777],"domain_scores_gemma":[0.99988484,0.000049608938,0.000022059392,0.0000065999875,0.000029644863,0.0000072022112],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00019572806,0.00040449575,0.0002277734,0.00018976752,0.00020679126,0.00027266418,0.00046648015,0.00021033084,0.0008469603],"category_scores_gemma":[0.0002735383,0.00013433455,0.0002134589,0.000114602095,0.0003087387,0.00019436283,0.00024444176,0.0003034958,0.000121744175],"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":[0.0003546923,0.00015039157,0.00051328633,0.00030606732,0.000054230462,0.00018784618,0.00018397186,0.4959029,0.31096587,0.007929134,0.0005605875,0.18289115],"study_design_scores_gemma":[0.000026781348,0.00026727116,0.00028073584,0.000007142322,0.000012076273,0.000038892005,0.000012425109,0.977458,0.020283226,0.0006684723,0.00093587145,0.000009144122],"about_ca_topic_score_codex":0.0011439458,"about_ca_topic_score_gemma":0.0011988904,"teacher_disagreement_score":0.0011439458,"about_ca_system_score_codex":0.00021542893,"about_ca_system_score_gemma":0.0002677714,"threshold_uncertainty_score":0.0028333664},"labels":[],"label_agreement":null},{"id":"W4406784319","doi":"10.1007/978-981-96-0771-6_11","title":"Design of Multi-Mode Morphing Wings Based on Multi-Stable Beam-Type Metastructures","year":2025,"lang":"en","type":"book-chapter","venue":"Lecture notes in computer science","topic":"Aeroelasticity and Vibration Control","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":"Morphing; Computer science; Mode (computer interface); Beam (structure); Type (biology); Computer vision; Optics; Human–computer interaction; Physics; Geology","score_opus":0.023739425408842343,"score_gpt":0.24554200697907633,"score_spread":0.22180258157023397,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4406784319","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":[0.20545356,0.0003373894,0.78592324,0.00005630737,0.000059242047,0.00006695574,0.00005613376,0.00040135763,0.00764586],"genre_scores_gemma":[0.8813391,0.00012382565,0.11577281,0.000023199567,0.0000103108205,0.00006946797,0.000056374607,0.00003575577,0.0025692503],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999504,0.0000054092943,0.0000032763564,0.000014219689,0.00001727198,0.000009491841],"domain_scores_gemma":[0.99992466,0.000012408501,0.00002300719,0.00001095834,0.000019099733,0.000009873851],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00009682182,0.00030066678,0.00027118385,0.00021805757,0.00019777419,0.00026970764,0.00064489775,0.0004148455,0.0013033393],"category_scores_gemma":[0.00012520672,0.00018125626,0.00030702096,0.00013329704,0.00015016594,0.00025823087,0.00030264028,0.00019732589,0.0002648962],"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":[0.00019040961,0.00007764208,0.0013963898,0.00019450946,0.000053757918,0.00021054364,0.00007883033,0.14423852,0.7408675,0.0116933845,0.0006167954,0.10038168],"study_design_scores_gemma":[0.00002600564,0.0005213454,0.0021839943,0.000018508981,0.000031623866,0.0002808572,0.00003110972,0.9423927,0.049930036,0.0013464249,0.0032155004,0.000021766939],"about_ca_topic_score_codex":0.00021086779,"about_ca_topic_score_gemma":0.0004454984,"teacher_disagreement_score":0.0013033393,"about_ca_system_score_codex":0.00014394025,"about_ca_system_score_gemma":0.00015744676,"threshold_uncertainty_score":0},"labels":[],"label_agreement":null},{"id":"W4407597914","doi":"10.1016/j.ymssp.2025.112447","title":"An adaptive active vibration control for flexible beam systems under unknown deterministic disturbances","year":2025,"lang":"en","type":"article","venue":"Mechanical Systems and Signal Processing","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":10,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Canadian Institute for Theoretical Astrophysics; University of Toronto","funders":"Ministry of Science and Technology of the People's Republic of China; National Natural Science Foundation of China","keywords":"Control theory (sociology); Vibration; Vibration control; Active vibration control; Beam (structure); Adaptive control; Control (management); Computer science; Input shaping; Control engineering; Engineering; Structural engineering; Physics; Acoustics; Artificial intelligence","score_opus":0.015223033178686039,"score_gpt":0.2474910536736306,"score_spread":0.23226802049494458,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4407597914","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":[0.0414455,0.00035954054,0.95415163,0.00013237962,0.00012256922,0.000036462738,0.000022208384,0.00013691449,0.0035928483],"genre_scores_gemma":[0.9768063,0.00016941394,0.019645194,0.00003897632,0.00006201365,0.00006179704,0.000020896669,0.000013050576,0.0031824259],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998374,0.000031666987,0.000008589902,0.000042311916,0.00006213164,0.000017924229],"domain_scores_gemma":[0.9998229,0.000094112314,0.00001907209,0.000011347809,0.000044654793,0.000007938807],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00027954788,0.00044869503,0.00041721595,0.00018068889,0.00024747886,0.00044851264,0.00052554405,0.0005650454,0.0015093969],"category_scores_gemma":[0.0006810562,0.00020168915,0.00026892938,0.00020025561,0.00042850795,0.0003605488,0.0005469131,0.00039886596,0.00013666054],"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":[0.0003723231,0.000081463375,0.00037975522,0.0003077772,0.00009622331,0.00017767615,0.00016568457,0.7559372,0.06321968,0.01474832,0.0010889663,0.1634249],"study_design_scores_gemma":[0.000015312044,0.000088769404,0.0001961673,0.0000037528428,0.000007945814,0.000011620494,0.0000036994834,0.99795294,0.00092692266,0.00050946063,0.00027979337,0.0000035679177],"about_ca_topic_score_codex":0.002063911,"about_ca_topic_score_gemma":0.0020618003,"teacher_disagreement_score":0.002063911,"about_ca_system_score_codex":0.00017080778,"about_ca_system_score_gemma":0.00025965736,"threshold_uncertainty_score":0.005049467},"labels":[],"label_agreement":null},{"id":"W4409250282","doi":"10.1016/j.rser.2025.115618","title":"Morphing structural materials used in wind turbine blades","year":2025,"lang":"en","type":"article","venue":"Renewable and Sustainable Energy Reviews","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":16,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto","funders":"Engineering and Physical Sciences Research Council; National Natural Science Foundation of China; University of Liverpool; Newcastle University","keywords":"Morphing; Turbine blade; Turbine; Marine engineering; Engineering; Structural engineering; Forensic engineering; Computer science; Aerospace engineering; Computer graphics (images)","score_opus":0.007511874358524201,"score_gpt":0.22176861834501388,"score_spread":0.21425674398648967,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4409250282","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":[0.08243887,0.8628777,0.024786908,0.00048337263,0.0010119642,0.00007841491,0.00017219779,0.00010931225,0.028041307],"genre_scores_gemma":[0.47560588,0.48477715,0.024098353,0.00062023924,0.0005445619,0.000098091135,0.00023345028,0.000055643126,0.013966607],"study_design_codex":"bench_or_experimental","study_design_gemma":"not_applicable","domain_scores_codex":[0.9998697,0.000019844229,0.000013714689,0.000028082644,0.000059035916,0.000009605903],"domain_scores_gemma":[0.99993396,0.000024722282,0.000022786227,0.0000044811736,0.000011114306,0.0000030229005],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00013016096,0.0003011588,0.00023116833,0.00067720393,0.00015990339,0.0003689869,0.000240636,0.000605121,0.0011722322],"category_scores_gemma":[0.0002038139,0.00018902242,0.00020800126,0.0005532675,0.00023307829,0.00045483158,0.00019861646,0.00042129427,0.00048347886],"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":[0.00009867862,0.0000987126,0.0006403049,0.015324127,0.000051656854,0.0009629378,0.00027526042,0.0045135515,0.5660664,0.032090906,0.0039315107,0.37594602],"study_design_scores_gemma":[0.000015658115,0.0007524427,0.0046994765,0.0025484539,0.0001340371,0.004402878,0.00023907985,0.0052560987,0.29875922,0.011358907,0.671769,0.000064751664],"about_ca_topic_score_codex":0.00017093714,"about_ca_topic_score_gemma":0.00040633985,"teacher_disagreement_score":0.0011722322,"about_ca_system_score_codex":0.00013785482,"about_ca_system_score_gemma":0.000117926174,"threshold_uncertainty_score":0.0039215684},"labels":[],"label_agreement":null},{"id":"W4409947492","doi":"10.3390/aerospace12050381","title":"Structural and Topological Optimization of a Novel Elephant Trunk Mechanism for Morphing Wing Applications","year":2025,"lang":"en","type":"article","venue":"Aerospace","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure; Université du Québec à Montréal","funders":"Natural Sciences and Engineering Research Council of Canada; Canada Research Chairs","keywords":"Morphing; Wing; Mechanism (biology); Elephant trunks; Computer science; Topology (electrical circuits); Engineering; Aerospace engineering; Physics; Computer graphics (images); Medicine; Electrical engineering","score_opus":0.012420221426537939,"score_gpt":0.23775719222988706,"score_spread":0.22533697080334913,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4409947492","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":[0.7749348,0.0004825766,0.21443143,0.00010388331,0.0000550284,0.00007411903,0.00010477848,0.00024948487,0.009563911],"genre_scores_gemma":[0.9594463,0.00012335708,0.03884725,0.000008739385,0.0000038891526,0.00004994269,0.000047460075,0.000013892199,0.001459153],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99994504,0.0000055695214,0.0000025736692,0.000010332516,0.000026784308,0.000009565014],"domain_scores_gemma":[0.999949,0.000007574744,0.000016707712,0.000011403802,0.000009718431,0.000005550433],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00011704082,0.00025618417,0.00019278881,0.00034578965,0.00014680107,0.00021761454,0.00034044395,0.0003271957,0.0015448013],"category_scores_gemma":[0.00014977227,0.00012351418,0.0002740878,0.00014395316,0.00020159342,0.00020403926,0.0002429408,0.00013046304,0.00015267413],"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":[0.00010433083,0.00007145916,0.0023134903,0.00025208018,0.00004012948,0.000561428,0.00004709668,0.23508997,0.7051197,0.00601113,0.00039926835,0.049989983],"study_design_scores_gemma":[0.000076381795,0.0011115791,0.007580959,0.00003483586,0.000060447645,0.0009755197,0.000105022074,0.8725423,0.10718595,0.0015804686,0.008708363,0.000038164373],"about_ca_topic_score_codex":0.0001514648,"about_ca_topic_score_gemma":0.0002322442,"teacher_disagreement_score":0.0015448013,"about_ca_system_score_codex":0.00011300829,"about_ca_system_score_gemma":0.00017139707,"threshold_uncertainty_score":0.0051679015},"labels":[],"label_agreement":null},{"id":"W4410255886","doi":"10.1016/j.compstruct.2025.119271","title":"Active vibration control of a curved sandwich beam using a nonlinear PPF algorithm","year":2025,"lang":"en","type":"article","venue":"Composite Structures","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":6,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"McGill University","funders":"Canada Foundation for Innovation; Natural Sciences and Engineering Research Council of Canada; École de technologie supérieure","keywords":"Nonlinear system; Beam (structure); Vibration; Structural engineering; Active vibration control; Vibration control; Control theory (sociology); Materials science; Computer science; Control (management); Engineering; Physics; Acoustics; Artificial intelligence","score_opus":0.006463464423723098,"score_gpt":0.23522645601448394,"score_spread":0.22876299159076086,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4410255886","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":[0.24648689,0.00016585595,0.74785596,0.000107086795,0.00004518476,0.00007481354,0.000030315918,0.00030167747,0.0049321926],"genre_scores_gemma":[0.9651782,0.00003536579,0.03369073,0.000019598387,0.000003837007,0.00005121619,0.000010920844,0.000005608877,0.0010044976],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.999926,0.00001438882,0.0000056700833,0.000017920689,0.000025886813,0.000010090766],"domain_scores_gemma":[0.99978644,0.000087187764,0.000034903274,0.000016483522,0.00006531078,0.000009687077],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00028905226,0.00034429296,0.00020378573,0.00013850493,0.00016913298,0.0002690281,0.00032325985,0.00034407803,0.0011463381],"category_scores_gemma":[0.00037500774,0.00010367195,0.0001699484,0.00008118156,0.00031279112,0.00014079982,0.00024060617,0.00024151172,0.000114968],"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":[0.00050492625,0.0001165551,0.0010482223,0.00026840082,0.000049316444,0.00017010841,0.00023582215,0.5890205,0.2948405,0.00467642,0.0004483294,0.10862098],"study_design_scores_gemma":[0.00002618883,0.00021074638,0.00040220236,0.0000065899744,0.000007217303,0.00002004709,0.000011330461,0.9852217,0.0135522885,0.0002547423,0.00028079413,0.0000061666256],"about_ca_topic_score_codex":0.0015927796,"about_ca_topic_score_gemma":0.0015285455,"teacher_disagreement_score":0.0015927796,"about_ca_system_score_codex":0.00014567145,"about_ca_system_score_gemma":0.0002601197,"threshold_uncertainty_score":0.0038349032},"labels":[],"label_agreement":null},{"id":"W4410446126","doi":"10.3390/app15105570","title":"Development and Experimental Study of a Seamless Morphing Trailing Edge Flap Equipped with an Elephant Trunk Actuation Mechanism","year":2025,"lang":"en","type":"article","venue":"Applied Sciences","topic":"Aeroelasticity and Vibration Control","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":"École de Technologie Supérieure; Université du Québec à Montréal","funders":"","keywords":"Morphing; Mechanism (biology); Trailing edge; Computer science; Engineering; Structural engineering; Physics; Computer graphics (images)","score_opus":0.021021943090154198,"score_gpt":0.25531285506872403,"score_spread":0.23429091197856983,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4410446126","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":[0.9908504,0.00004286261,0.00824816,0.00001459053,0.000022775495,0.000040803403,0.000043608823,0.000054601198,0.00068211317],"genre_scores_gemma":[0.9891684,0.00004192646,0.010068287,0.0000064331266,0.0000031151496,0.00003208867,0.000031170588,0.0000061310666,0.00064257754],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997931,0.00001777768,0.00001227626,0.000043698714,0.00009556508,0.000037514696],"domain_scores_gemma":[0.9996766,0.00005283481,0.00007743886,0.00009436697,0.000052875745,0.000045900964],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003534814,0.0002845318,0.00018543816,0.00020425221,0.00016590631,0.00017171507,0.00034144867,0.0003571725,0.0011681318],"category_scores_gemma":[0.0003931983,0.00013486308,0.00023242939,0.00010291059,0.00036024523,0.00027638336,0.00031994394,0.00024553845,0.00014982682],"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":[0.00012286668,0.00014146266,0.0022922428,0.00011055022,0.0000074595896,0.00040156613,0.00010666987,0.0045254496,0.98344654,0.00044696222,0.00010042633,0.008297758],"study_design_scores_gemma":[0.000094047355,0.008703754,0.031975962,0.000037274054,0.00004505011,0.000978121,0.00024390352,0.05055257,0.902408,0.00020736495,0.0047037425,0.000050213628],"about_ca_topic_score_codex":0.00019232613,"about_ca_topic_score_gemma":0.0002192877,"teacher_disagreement_score":0.0011681318,"about_ca_system_score_codex":0.00009870162,"about_ca_system_score_gemma":0.00019540584,"threshold_uncertainty_score":0.0039077997},"labels":[],"label_agreement":null},{"id":"W4411037466","doi":"10.18280/jesa.580415","title":"Vibration Performance on the 3D-Printed UAV Wing","year":2025,"lang":"fr","type":"article","venue":"Journal Européen des Systèmes Automatisés","topic":"Aeroelasticity and Vibration Control","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; 3d printed; Vibration; Aeronautics; Computer science; Aerospace engineering; Engineering; Acoustics; Physics; Biomedical engineering","score_opus":0.015187922837910253,"score_gpt":0.23269337166992057,"score_spread":0.2175054488320103,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4411037466","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":[0.99383175,0.00014669119,0.0044624093,0.000024185785,0.000032663378,0.0000050013873,0.000050086255,0.00009030163,0.001356941],"genre_scores_gemma":[0.9972826,0.00005947979,0.0013616293,0.000008554546,0.000002538016,0.0000040417485,0.000046075515,0.000009140408,0.0012259954],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998573,0.000011759795,0.000008686747,0.000026536714,0.00007835105,0.000017339853],"domain_scores_gemma":[0.9996655,0.0001171117,0.000054044667,0.000050902083,0.000088843495,0.000023505714],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012629188,0.00019785002,0.00015586015,0.00021934895,0.00011640861,0.00022001567,0.00019547628,0.00041135703,0.0014023221],"category_scores_gemma":[0.00044078566,0.00010094081,0.0002372606,0.0001270726,0.00016651506,0.00015016051,0.00012646758,0.00014247859,0.00032497512],"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":[0.00023850998,0.000044924156,0.002003515,0.00011567174,0.000016316197,0.00034388763,0.000172379,0.014684018,0.96085036,0.00011575385,0.00020189601,0.021212893],"study_design_scores_gemma":[0.000026698252,0.002115271,0.03639553,0.000025071837,0.00004106524,0.00040910117,0.00023651254,0.056448255,0.9019827,0.0001044133,0.0021674952,0.0000478569],"about_ca_topic_score_codex":0.00051265163,"about_ca_topic_score_gemma":0.0005974424,"teacher_disagreement_score":0.0014023221,"about_ca_system_score_codex":0.00011480719,"about_ca_system_score_gemma":0.000052738254,"threshold_uncertainty_score":0.004691243},"labels":[],"label_agreement":null},{"id":"W4411061174","doi":"10.13111/2066-8201.2025.17.2.5","title":"Comparison of Aerodynamic Characteristics of Morphing and Conventional Wings","year":2025,"lang":"en","type":"article","venue":"INCAS BULLETIN","topic":"Aeroelasticity and Vibration Control","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":"École de Technologie Supérieure; Université du Québec à Montréal","funders":"","keywords":"Morphing; Aerodynamics; Wing; Aerospace engineering; Computer science; Structural engineering; Aeronautics; Engineering; Computer graphics (images)","score_opus":0.007618360741140128,"score_gpt":0.24519922339691028,"score_spread":0.23758086265577014,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4411061174","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":[0.9869409,0.00014088216,0.010671852,0.000015440426,0.000011222612,0.000013522538,0.000060381353,0.000039817183,0.0021059925],"genre_scores_gemma":[0.99667466,0.000043678643,0.0028584304,0.000004621515,0.0000025986456,0.0000052053592,0.000063196916,0.000003947706,0.00034365122],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999417,0.000005973802,0.000004743312,0.0000110764895,0.0000271086,0.000009465409],"domain_scores_gemma":[0.9999083,0.000030180776,0.000016155514,0.000019174393,0.00001718149,0.000008931696],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001149166,0.00016963479,0.00010763113,0.00019143404,0.000077041565,0.0001888412,0.00014592712,0.00015586209,0.00094294973],"category_scores_gemma":[0.00023587658,0.000054388394,0.00018965393,0.00011486785,0.00013018592,0.00020588233,0.00014326423,0.00009193855,0.00007757205],"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":[0.0006845716,0.000117247815,0.021314107,0.00026977493,0.000053334094,0.00041300667,0.000100088626,0.105532505,0.7771946,0.0014708885,0.00032996916,0.092519954],"study_design_scores_gemma":[0.00009214953,0.0027552845,0.21977891,0.00003630679,0.00012269855,0.0013081486,0.00025941638,0.56570643,0.20277782,0.00093354017,0.0061513227,0.000077934616],"about_ca_topic_score_codex":0.00023011805,"about_ca_topic_score_gemma":0.0002635163,"teacher_disagreement_score":0.00094294973,"about_ca_system_score_codex":0.00008392078,"about_ca_system_score_gemma":0.00005499128,"threshold_uncertainty_score":0.0031544566},"labels":[],"label_agreement":null},{"id":"W4411572179","doi":"10.1017/aer.2025.10028","title":"Aeroelastic stability of imperfectly supported high-aspect-ratio wings","year":2025,"lang":"en","type":"article","venue":"The Aeronautical Journal","topic":"Aeroelasticity and Vibration Control","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":"Natural Sciences and Engineering Research Council of Canada; Concordia University","keywords":"Aeroelasticity; Wing; Aspect ratio (aeronautics); Stability (learning theory); Structural engineering; Aerospace engineering; Engineering; Computer science; Materials science; Aerodynamics; Composite material","score_opus":0.008181477115154354,"score_gpt":0.21873449973923517,"score_spread":0.21055302262408082,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4411572179","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":[0.9919647,0.000107369204,0.0063876165,0.000017925151,0.000008434786,0.0000037358204,0.000021033571,0.00001909067,0.0014701377],"genre_scores_gemma":[0.99932766,0.000016789865,0.00048017973,0.0000017729277,0.0000010749137,0.0000013925177,0.000009457026,0.0000020542936,0.00015967045],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998983,0.000014367032,0.0000062498275,0.000014068741,0.000046583602,0.000020465934],"domain_scores_gemma":[0.9996125,0.00014026712,0.000109546854,0.00005098494,0.00004490309,0.000041840714],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002066332,0.00023512887,0.00027355392,0.00032318773,0.00020147217,0.0005522254,0.00028974176,0.00034941593,0.00049332133],"category_scores_gemma":[0.0009089395,0.00010247501,0.00018274381,0.00014194431,0.0007903599,0.0002950173,0.0003780006,0.0002353168,0.00007274382],"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":[0.00036245777,0.00007122183,0.009634605,0.000086986125,0.000047651058,0.00094852835,0.00012175646,0.7978416,0.17920855,0.00514074,0.00014108072,0.006394829],"study_design_scores_gemma":[0.000013350094,0.00014153398,0.007902435,0.000012688287,0.000007921967,0.00011076746,0.00007112466,0.97481245,0.015599636,0.0010960193,0.00021717102,0.000014848973],"about_ca_topic_score_codex":0.0008460137,"about_ca_topic_score_gemma":0.0004213662,"teacher_disagreement_score":0.0008460137,"about_ca_system_score_codex":0.00018125834,"about_ca_system_score_gemma":0.00013774102,"threshold_uncertainty_score":0.0016822219},"labels":[],"label_agreement":null},{"id":"W4412671571","doi":"10.1007/s11071-025-11607-0","title":"Experimental study of nonlinear PPF-based active vibration controllers for a carbon fiber beam subject to mass changes","year":2025,"lang":"en","type":"article","venue":"Nonlinear Dynamics","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":0,"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":"Natural Sciences and Engineering Research Council of Canada","keywords":"Nonlinear system; Beam (structure); Vibration; Control theory (sociology); Materials science; Structural engineering; Physics; Computer science; Engineering; Acoustics; Control (management); Artificial intelligence","score_opus":0.009048570067530315,"score_gpt":0.25173650449228935,"score_spread":0.24268793442475903,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4412671571","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":[0.9925122,0.00006315292,0.0061320947,0.000041525695,0.000035527275,0.000041375322,0.000058220263,0.000081351674,0.001034567],"genre_scores_gemma":[0.9979145,0.00002882024,0.0013786163,0.00000719061,0.000004293746,0.000018925359,0.000023816197,0.0000055455885,0.00061839324],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99977535,0.000025872549,0.0000142849085,0.000046990535,0.000092920745,0.00004451287],"domain_scores_gemma":[0.9991456,0.00034287552,0.00007990961,0.000084860934,0.00029923537,0.000047489215],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00038242602,0.00038311206,0.0002624314,0.00026471014,0.0005268164,0.00020285347,0.00053012057,0.00055770256,0.0028684048],"category_scores_gemma":[0.00083790877,0.00016223628,0.00017665804,0.00015702892,0.00046872153,0.00033915046,0.000248343,0.00029976064,0.00020072264],"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":[0.0014776367,0.00034475932,0.0005455004,0.00017045994,0.000011338982,0.00007730056,0.00014173886,0.0025508895,0.9842152,0.0001661903,0.00010569866,0.0101932725],"study_design_scores_gemma":[0.00019560817,0.006217755,0.0138518335,0.000026290383,0.000043326876,0.000121133606,0.0001542164,0.058809027,0.9193749,0.000120094,0.0010536376,0.000032212018],"about_ca_topic_score_codex":0.0016986867,"about_ca_topic_score_gemma":0.001356449,"teacher_disagreement_score":0.0028684048,"about_ca_system_score_codex":0.00018565648,"about_ca_system_score_gemma":0.00024321594,"threshold_uncertainty_score":0.009595811},"labels":[],"label_agreement":null},{"id":"W4413963459","doi":"10.1016/j.mechrescom.2025.104509","title":"Nonlinear electromechanical behaviour of piezoelectric thin sheet actuators under large deformation","year":2025,"lang":"en","type":"article","venue":"Mechanics Research Communications","topic":"Aeroelasticity and Vibration Control","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":"Natural Sciences and Engineering Research Council of Canada","keywords":"Piezoelectricity; Actuator; Nonlinear system; Materials science; Deformation (meteorology); Acoustics; Structural engineering; Mechanics; Composite material; Mechanical engineering; Engineering; Physics; Electrical engineering","score_opus":0.0391339372503653,"score_gpt":0.33982671870810116,"score_spread":0.30069278145773587,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4413963459","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":[0.9553699,0.0004209827,0.03612902,0.00021393338,0.00003318045,0.000017215254,0.000035535293,0.00005777416,0.007722633],"genre_scores_gemma":[0.9957651,0.00020099395,0.0024068253,0.000021724678,0.000006213911,0.000010192752,0.000016903472,0.0000064355118,0.0015657687],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99991906,0.000015368452,0.0000035012272,0.000012595173,0.000039173032,0.0000103196035],"domain_scores_gemma":[0.9998772,0.000053280208,0.000023412134,0.000019471245,0.000017000055,0.0000096360245],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00016501415,0.00023109472,0.00023231041,0.00014930159,0.00017650818,0.0002650205,0.00024039565,0.000495931,0.00068280706],"category_scores_gemma":[0.0003551267,0.0001337563,0.00018680053,0.00012331211,0.0005962583,0.000339246,0.0002957808,0.00025726485,0.00014036136],"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":[0.00010772704,0.00005702323,0.0015859634,0.00012842665,0.000034809997,0.001005526,0.00030517986,0.18841216,0.7886119,0.008616096,0.00030855555,0.010826621],"study_design_scores_gemma":[0.00000687081,0.00007586594,0.0027284974,0.0000115931825,0.0000066050734,0.00019374726,0.000072969226,0.9563795,0.037272293,0.0026443247,0.0005870323,0.000020703143],"about_ca_topic_score_codex":0.0003546402,"about_ca_topic_score_gemma":0.00035063643,"teacher_disagreement_score":0.00068280706,"about_ca_system_score_codex":0.0001291015,"about_ca_system_score_gemma":0.00015109063,"threshold_uncertainty_score":0.0022841692},"labels":[],"label_agreement":null},{"id":"W4414406564","doi":"10.3390/drones9090663","title":"Mechanisms and Control Strategies for Morphing Structures in Quadrotors: A Review and Future Prospects","year":2025,"lang":"en","type":"review","venue":"Drones","topic":"Aeroelasticity and Vibration Control","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":"Hôpital Notre-Dame; Université du Québec à Montréal","funders":"","keywords":"Morphing; Scalability; Key (lock); Aerodynamics; Control (management); Drone; Flexibility (engineering); Robot","score_opus":0.010471579715046364,"score_gpt":0.26421659276087595,"score_spread":0.2537450130458296,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4414406564","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":[0.00043040086,0.996739,0.0012602218,0.00012553901,0.00015281512,0.000007920406,0.000020928195,0.000016891678,0.0012462693],"genre_scores_gemma":[0.0030941614,0.99449545,0.0012349972,0.000121895755,0.00014535504,0.000014489256,0.00005339175,0.000004700219,0.0008356145],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.99985147,0.00001504099,0.000024307883,0.000040892475,0.000052694588,0.00001560233],"domain_scores_gemma":[0.9997056,0.0001598651,0.000056156794,0.000012010091,0.000050953862,0.000015303342],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00037701847,0.0010128369,0.0012227666,0.001609515,0.0002492936,0.000844712,0.0007716803,0.0011258031,0.0030989822],"category_scores_gemma":[0.0005295075,0.00045180865,0.00078055786,0.001307911,0.00039812826,0.0014255213,0.0004914824,0.0009613923,0.0013806584],"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":[0.000055864293,0.0001282244,0.00023806933,0.03378142,0.00012709436,0.00018557433,0.000081750535,0.0034724516,0.007760448,0.008401743,0.009561102,0.9362062],"study_design_scores_gemma":[0.00001833125,0.00035765124,0.0009138002,0.0050354176,0.00023806676,0.0010740057,0.000097598844,0.0016580501,0.0029100114,0.0038551204,0.9837804,0.00006148013],"about_ca_topic_score_codex":0.0007507281,"about_ca_topic_score_gemma":0.00088421704,"teacher_disagreement_score":0.0030989822,"about_ca_system_score_codex":0.00027578033,"about_ca_system_score_gemma":0.0005421529,"threshold_uncertainty_score":0.010367155},"labels":[],"label_agreement":null},{"id":"W4414518460","doi":"10.1016/j.ast.2025.111004","title":"Tuning and miniaturization of active vibration controllers of a fixed-wing composite aircraft drone using the experiment-on-the-loop system","year":2025,"lang":"en","type":"article","venue":"Aerospace Science and Technology","topic":"Aeroelasticity and Vibration Control","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":"McGill University","funders":"","keywords":"Drone; Payload (computing); Controller (irrigation); Active vibration control; Miniaturization; Vibration; Control theory (sociology); Reduction (mathematics)","score_opus":0.006733519539462277,"score_gpt":0.21965438777199428,"score_spread":0.212920868232532,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4414518460","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":[0.84565973,0.00023889769,0.1492833,0.000096005984,0.00008325901,0.00012300895,0.000063532076,0.0007224544,0.0037297911],"genre_scores_gemma":[0.9832722,0.000020509444,0.015670503,0.000016555112,0.0000069757975,0.000033468536,0.000024110735,0.000015442263,0.0009401552],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9998807,0.0000142768795,0.000006084762,0.000040685085,0.00004480724,0.00001350172],"domain_scores_gemma":[0.9997155,0.00009124396,0.000034523022,0.00006305402,0.000071569186,0.000023972583],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00019490752,0.0002844903,0.00025102613,0.00018759715,0.00026581003,0.00028050796,0.0004392044,0.00027599972,0.0013518648],"category_scores_gemma":[0.00036848793,0.00012988212,0.00013803516,0.00005518681,0.0002013719,0.00021318371,0.0002429619,0.00021029073,0.00020806593],"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":[0.0003170306,0.00009774542,0.00086009945,0.000096116746,0.000020092344,0.00007634028,0.00010262053,0.0069640987,0.961627,0.00036513965,0.00016135148,0.029312283],"study_design_scores_gemma":[0.00020199956,0.0020676667,0.014923513,0.00002399105,0.00007531311,0.00035316203,0.00008015869,0.23205589,0.74316746,0.00024345242,0.00675895,0.000048500795],"about_ca_topic_score_codex":0.00041816916,"about_ca_topic_score_gemma":0.00087398663,"teacher_disagreement_score":0.0013518648,"about_ca_system_score_codex":0.00012215386,"about_ca_system_score_gemma":0.00018383346,"threshold_uncertainty_score":0.004522443},"labels":[],"label_agreement":null},{"id":"W4414828759","doi":"10.1016/j.compstruct.2025.119719","title":"Controlled morphing of structures using smart piezoelectric patches subject to thermo-electro-mechanical loading","year":2025,"lang":"en","type":"article","venue":"Composite Structures","topic":"Aeroelasticity and Vibration Control","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":"University of Toronto","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Morphing; Piezoelectricity; Nonlinear system; Stiffness; Finite element method; Smart material; Deformation (meteorology); Piezoelectric sensor","score_opus":0.009590849711268116,"score_gpt":0.23868430870054252,"score_spread":0.2290934589892744,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4414828759","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":[0.9922463,0.0001135147,0.0057683573,0.000040588246,0.000033548004,0.000008599431,0.000014360985,0.000056234276,0.0017184918],"genre_scores_gemma":[0.9974414,0.00004585082,0.0017842252,0.000013595499,0.00000534768,0.000004766687,0.000007660884,0.000012239047,0.00068485265],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99996126,0.0000030255123,0.0000015090093,0.000009503167,0.000013436936,0.000011163336],"domain_scores_gemma":[0.99994576,0.0000134685315,0.000020289994,0.000009231528,0.000004268935,0.0000069839643],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00004921162,0.00017320128,0.00014819526,0.00010287703,0.00010506837,0.00020110366,0.00016047312,0.00018728671,0.0010065323],"category_scores_gemma":[0.00011356885,0.00014370603,0.00009098493,0.00006797439,0.00030362257,0.00016740036,0.00020761945,0.00021057083,0.000093995644],"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":[0.000053815358,0.000016864293,0.00010434429,0.000029016177,0.0000039701076,0.00005688997,0.00003758584,0.0020515576,0.9942286,0.00034651053,0.000068836205,0.0030020536],"study_design_scores_gemma":[0.000040163788,0.00026610226,0.003310058,0.000005704232,0.000009478289,0.00012525744,0.000043514014,0.040858626,0.9539907,0.0002501266,0.0010886813,0.000011610672],"about_ca_topic_score_codex":0.00011081515,"about_ca_topic_score_gemma":0.00035222716,"teacher_disagreement_score":0.0010065323,"about_ca_system_score_codex":0.00010058693,"about_ca_system_score_gemma":0.00006952443,"threshold_uncertainty_score":0.0033672452},"labels":[],"label_agreement":null},{"id":"W4415474597","doi":"10.1016/j.ymssp.2025.113529","title":"Adaptive modeling and parameter identification of piezoelectric structures under system uncertainty and nonlinear effects","year":2025,"lang":"en","type":"article","venue":"Mechanical Systems and Signal Processing","topic":"Aeroelasticity and Vibration Control","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":"Northern Ontario Academic Medicine Association","funders":"Istanbul Teknik Üniversitesi","keywords":"Nonlinear system; Sensitivity (control systems); Identification (biology); Structural health monitoring; Noise (video); System identification; Control theory (sociology); Control reconfiguration","score_opus":0.009624574421537944,"score_gpt":0.21778871707764894,"score_spread":0.208164142656111,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4415474597","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":[0.10762975,0.00027025002,0.88840175,0.00025126946,0.000032501877,0.000024689225,0.000050562372,0.00015588543,0.0031834734],"genre_scores_gemma":[0.9886425,0.00012218808,0.009372291,0.000021288739,0.000010736826,0.000036178262,0.000033845503,0.000013569798,0.0017473449],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99986553,0.000036352652,0.000006732534,0.000032688553,0.00004331988,0.000015504918],"domain_scores_gemma":[0.9996792,0.0001985081,0.000048095808,0.000023213648,0.000043098946,0.000007746488],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00032209148,0.00030348598,0.00044298466,0.00022587483,0.0002251706,0.00043667643,0.00056943734,0.0007592685,0.0006560389],"category_scores_gemma":[0.0015739151,0.00031358236,0.00028836002,0.0002397568,0.0004925137,0.000560238,0.0005769325,0.00057557586,0.00010000887],"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":[0.000016462505,0.0000085505535,0.00017328946,0.000015276306,0.000009194688,0.000027443044,0.000028276994,0.98902965,0.0018746898,0.0018469442,0.00007062581,0.0068996414],"study_design_scores_gemma":[9.518537e-7,0.0000041459643,0.00010334118,6.977106e-7,0.0000010747033,0.0000032787116,0.0000020461182,0.9991787,0.00015567712,0.0005120775,0.000036814065,0.0000011869013],"about_ca_topic_score_codex":0.00662256,"about_ca_topic_score_gemma":0.0043889764,"teacher_disagreement_score":0.00662256,"about_ca_system_score_codex":0.0003370733,"about_ca_system_score_gemma":0.000523944,"threshold_uncertainty_score":0.013168037},"labels":[],"label_agreement":null},{"id":"W4415946679","doi":"","title":"Investigation of novel electroactive morphing concepts for aerodynamic performance increase of an A320 wing through High-Fidelity numerical simulation","year":2025,"lang":"fr","type":"article","venue":"theses.fr (ABES)","topic":"Aeroelasticity and Vibration Control","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":"Morphing; Swept wing; Aerodynamics; Wing; Flight control surfaces","score_opus":0.025686845179141028,"score_gpt":0.28940701268617147,"score_spread":0.2637201675070304,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4415946679","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":[0.9057602,0.00053340226,0.07152331,0.00033000254,0.00008716526,0.00010764109,0.00030722943,0.00039578218,0.02095529],"genre_scores_gemma":[0.98143643,0.00014796495,0.016420808,0.000018630559,0.0000033306624,0.000045507546,0.00008578078,0.000041907326,0.0017997718],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999186,0.000012942861,0.0000040728264,0.000009698193,0.000040345105,0.000014419346],"domain_scores_gemma":[0.99980134,0.00009414431,0.000023374709,0.000027198375,0.000037079215,0.000016859516],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025469344,0.00030671878,0.0002615791,0.00023382885,0.00028028284,0.0005442187,0.00039860446,0.00062699174,0.0022560637],"category_scores_gemma":[0.00057693775,0.0001533236,0.00034675095,0.00014693789,0.00039214717,0.00037269935,0.00032328974,0.00033200835,0.00019388528],"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":[0.00021990169,0.00017369082,0.0033869422,0.00025664258,0.000025443138,0.00027704966,0.00025142604,0.85309607,0.11688861,0.0052660266,0.00082114735,0.019337052],"study_design_scores_gemma":[0.00001250774,0.00007781776,0.00077911624,0.000013595422,0.000004546944,0.000027493119,0.000040614377,0.98957086,0.008114394,0.0002489634,0.0011018628,0.000008203652],"about_ca_topic_score_codex":0.0015590851,"about_ca_topic_score_gemma":0.001319526,"teacher_disagreement_score":0.0022560637,"about_ca_system_score_codex":0.00024036791,"about_ca_system_score_gemma":0.00032308238,"threshold_uncertainty_score":0.007547319},"labels":[],"label_agreement":null},{"id":"W4416129079","doi":"10.1038/s41378-025-01065-4","title":"Machine learning-driven metastructure design for sensor-free linearization of MEMS electrothermal actuators","year":2025,"lang":"en","type":"article","venue":"Microsystems & Nanoengineering","topic":"Aeroelasticity and Vibration Control","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 Toronto; McGill University","funders":"Natural Sciences and Engineering Research Council of Canada; Government of Canada; Hitachi America","keywords":"Actuator; Microelectromechanical systems; Nonlinear system; Linearization; Finite element method; Displacement (psychology); Stiffness; Voltage","score_opus":0.005634966538122666,"score_gpt":0.19301664833700616,"score_spread":0.18738168179888348,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4416129079","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":[0.039170608,0.00020166396,0.95745873,0.000101174075,0.000018905745,0.000041828545,0.000035504127,0.0003910346,0.002580479],"genre_scores_gemma":[0.8416485,0.000114984185,0.15622552,0.00006043722,0.000011166602,0.00013012925,0.00006989218,0.00005376726,0.0016856567],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998678,0.000017727554,0.0000071697623,0.000031223997,0.00006284353,0.000013231667],"domain_scores_gemma":[0.99987686,0.000043389045,0.000033374974,0.00001458857,0.000025689733,0.00000604821],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0002366585,0.0003716502,0.00029853708,0.0001732614,0.0001519807,0.0002855076,0.0005456913,0.00034742264,0.0009291693],"category_scores_gemma":[0.00042834927,0.0002734019,0.00026389418,0.00013558296,0.00032183825,0.00044638367,0.00033662433,0.00037023533,0.00022856791],"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":[0.000079094185,0.00006163004,0.00040559276,0.00019076289,0.000032147676,0.00009901284,0.00007518089,0.75806916,0.17509277,0.008916967,0.0005707797,0.05640688],"study_design_scores_gemma":[0.000004296465,0.000053598535,0.000089997404,0.0000043692585,0.000003173881,0.000014767823,0.0000037355182,0.98520225,0.013175304,0.0007312151,0.0007123418,0.000004903704],"about_ca_topic_score_codex":0.00058483746,"about_ca_topic_score_gemma":0.0015386107,"teacher_disagreement_score":0.0009291693,"about_ca_system_score_codex":0.00043324125,"about_ca_system_score_gemma":0.00045526252,"threshold_uncertainty_score":0.0031433702},"labels":[],"label_agreement":null},{"id":"W60841607","doi":"","title":"Method based on Chebyshev polynomials theories for aeroservoelastic interactions studies on a F/A-18 aircraft","year":2006,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"École de Technologie Supérieure; Université du Québec à Montréal","funders":"","keywords":"Chebyshev polynomials; Mathematics; Orthogonality; Flutter; Padé approximant; Laplace transform; Mathematical analysis; Applied mathematics; Square (algebra); Aerodynamics; Frequency domain; Domain (mathematical analysis); Geometry; Physics","score_opus":0.02760330826265343,"score_gpt":0.31016895418954005,"score_spread":0.2825656459268866,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W60841607","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":[0.011972862,0.00017521715,0.98539746,0.000053374493,0.000046995854,0.000034516157,0.000024018247,0.00021099696,0.0020845467],"genre_scores_gemma":[0.3333925,0.0009091387,0.6555996,0.00008668459,0.0000775532,0.00029822576,0.00010155033,0.00013750927,0.009397323],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99981123,0.00005097485,0.0000052262644,0.000016598837,0.00010279327,0.000013177126],"domain_scores_gemma":[0.99973935,0.0001397849,0.000018280842,0.000026706417,0.00006759421,0.000008321642],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0003400782,0.00032718104,0.00039674403,0.00049316057,0.00026244944,0.00030150128,0.00042657024,0.00045579445,0.0029260349],"category_scores_gemma":[0.0008309848,0.0001445271,0.0003435711,0.00040273086,0.00026141977,0.00044772602,0.0002884576,0.0006368491,0.0005719736],"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":[0.00023173333,0.00022779193,0.001569623,0.00039489774,0.00005796713,0.00029895888,0.00023630139,0.43213674,0.07572105,0.06935018,0.003747929,0.41602686],"study_design_scores_gemma":[0.000014010704,0.000046138575,0.00033173268,0.000007755804,0.0000054801026,0.000069653484,0.000017070282,0.9903092,0.0043088663,0.0021022782,0.0027750218,0.000012793807],"about_ca_topic_score_codex":0.001972041,"about_ca_topic_score_gemma":0.0016347193,"teacher_disagreement_score":0.0029260349,"about_ca_system_score_codex":0.00018610293,"about_ca_system_score_gemma":0.0006670821,"threshold_uncertainty_score":0.009788513},"labels":[],"label_agreement":null},{"id":"W61021522","doi":"10.1007/1-4020-4131-4_17","title":"Electric Charge Loading of a Piezoelectric Solid Cylinder","year":2006,"lang":"en","type":"book-chapter","venue":"Solid mechanics and its applications","topic":"Aeroelasticity and Vibration Control","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 British Columbia","funders":"","keywords":"Bessel function; Piezoelectricity; Cylinder; Fourier series; Transverse isotropy; Electric field; Hankel transform; RADIUS; Piezoelectric coefficient; Boundary value problem; Materials science; Isotropy; Physics; Mechanics; Acoustics; Mathematical analysis; Mathematics; Geometry; Optics; Computer science","score_opus":0.010178884443626683,"score_gpt":0.2147501941830701,"score_spread":0.2045713097394434,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W61021522","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":[0.9170661,0.00035516822,0.018571889,0.00035721602,0.00027162879,0.000050522176,0.00006447376,0.0001439634,0.06311901],"genre_scores_gemma":[0.986979,0.00008518316,0.0007113489,0.00003590881,0.000026105216,0.0000065542463,0.000024940742,0.000017565519,0.012113425],"study_design_codex":"bench_or_experimental","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.9998834,0.000008609504,0.0000034817804,0.000012098651,0.00006568904,0.000026755033],"domain_scores_gemma":[0.9999205,0.000026778487,0.0000073549395,0.00001568961,0.000012160328,0.000017543249],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00008956208,0.000260241,0.0003569851,0.00028045633,0.0003863353,0.00048841664,0.0004024584,0.0004735935,0.005172006],"category_scores_gemma":[0.0003001713,0.00015211554,0.0001638489,0.00018127561,0.0009782256,0.00039781752,0.0006869504,0.00023921883,0.0003396612],"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":[0.0015020772,0.0002008413,0.00088957243,0.00027702254,0.00004117419,0.0037679356,0.00064969464,0.050367706,0.8147774,0.054085292,0.00204466,0.07139663],"study_design_scores_gemma":[0.00031673937,0.002028499,0.025181146,0.000083259765,0.00006456213,0.0031361717,0.001222271,0.4774108,0.4195118,0.043977782,0.026872084,0.00019489067],"about_ca_topic_score_codex":0.00043647396,"about_ca_topic_score_gemma":0.00034668052,"teacher_disagreement_score":0.005172006,"about_ca_system_score_codex":0.00019671387,"about_ca_system_score_gemma":0.0001926385,"threshold_uncertainty_score":0.017302096},"labels":[],"label_agreement":null},{"id":"W6892179053","doi":"10.5066/p9rmsu2r","title":"Geologic Provinces of the World, 2000 World Petroleum Assessment, all defined provinces","year":2000,"lang":"en","type":"dataset","venue":"USGS DOI Tool Production Environment","topic":"Aeroelasticity and Vibration Control","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":"Petroleum; Geological survey; Submarine pipeline; Bathymetry; Mineral resource classification; Bathymetric chart; Shapefile","score_opus":0.008716655287055503,"score_gpt":0.2067683510075766,"score_spread":0.1980516957205211,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6892179053","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":[0.001990771,0.00023157985,0.00061382394,0.00008376171,0.000034024175,0.00009425228,0.9621793,0.00049089856,0.034281548],"genre_scores_gemma":[0.0114218,0.00061807164,0.0030932568,0.00005969669,0.000009077886,0.0002470162,0.9661126,0.0002979891,0.01814048],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.99973613,0.000023251241,0.00002549335,0.00004090468,0.00012491098,0.000049309183],"domain_scores_gemma":[0.9991115,0.00007044666,0.00008434441,0.00010086341,0.00057124323,0.000061681676],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00025168326,0.00092494814,0.00031139504,0.0049132677,0.0006479158,0.0013426124,0.00083695236,0.00027910445,0.050651226],"category_scores_gemma":[0.0017634413,0.00054668536,0.00029628235,0.014578132,0.00017886978,0.001264958,0.0006161372,0.0005648454,0.0275303],"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":[0.000069001064,0.000024862587,0.006863773,0.0002884599,0.000008948389,0.00005013657,0.0001612057,0.0013284361,0.00020904666,0.0034639,0.9519224,0.035609864],"study_design_scores_gemma":[0.000032655636,0.000008235406,0.022008011,0.00010815666,0.0000056072977,0.000062370724,0.00024270745,0.00063851604,0.00019670671,0.00067667506,0.97600776,0.00001252544],"about_ca_topic_score_codex":0.37638593,"about_ca_topic_score_gemma":0.3489603,"teacher_disagreement_score":0.37638593,"about_ca_system_score_codex":0.0026285243,"about_ca_system_score_gemma":0.0057413415,"threshold_uncertainty_score":0.7483902},"labels":[],"label_agreement":null},{"id":"W6907005458","doi":"10.1899/0887-3593(2005)024&lt;0148:bmcisl&gt;2.0.co;2","title":"Benthic macroinvertebrate communities in southwestern Lake Ontario following invasion of Dreissena and Echinogammarus: 1983 to 2000","year":2005,"lang":"en","type":"article","venue":"BioOne Complete (BioOne)","topic":"Aeroelasticity and Vibration Control","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":"Dreissena; Cobble; Benthic zone; Neogobius; Round goby; Abundance (ecology); Invertebrate; Mollusca; Biomass (ecology)","score_opus":0.14013603858421067,"score_gpt":0.21475137287039803,"score_spread":0.07461533428618736,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6907005458","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":[0.99900925,0.000059890517,0.000015525153,0.000033418695,0.0000012063457,0.0000060576635,0.00034771726,0.000002950817,0.00052397576],"genre_scores_gemma":[0.9979463,0.00010117463,0.00006400208,0.00003613377,0.000001841516,0.0000128463,0.00057249214,0.0000013864507,0.0012638606],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.9998611,0.0000066480297,0.000007651915,0.000022985836,0.000056620454,0.000044974266],"domain_scores_gemma":[0.9993668,0.000022554163,0.00019899187,0.0000127998965,0.00023793099,0.00016093382],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012484417,0.00017624194,0.00017969546,0.0005032526,0.0012906509,0.00059066905,0.00033930503,0.00032151438,0.000991418],"category_scores_gemma":[0.00044409558,0.0002496844,0.00015591084,0.0007380574,0.00036800138,0.0002891573,0.0004919654,0.00022110964,0.00018416243],"study_design_candidate":"observational","study_design_consensus":"observational","about_ca_topic_candidate":true,"about_ca_topic_consensus":true,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000088993555,0.000027332886,0.9907596,0.000031236934,0.000026870406,0.00015273817,0.0018203375,0.00008273811,0.003300858,0.00001890912,0.00042748303,0.0032628544],"study_design_scores_gemma":[0.0000016806438,0.0000074305613,0.9992124,0.0000033767308,0.0000034575958,0.000011055836,0.00030489903,0.00004917143,0.000066151246,0.0000017019408,0.00033733965,0.000001411147],"about_ca_topic_score_codex":0.8901518,"about_ca_topic_score_gemma":0.9812145,"teacher_disagreement_score":0.1098482,"about_ca_system_score_codex":0.00747355,"about_ca_system_score_gemma":0.0030184775,"threshold_uncertainty_score":0.22099018},"labels":[],"label_agreement":null},{"id":"W6910504814","doi":"10.4050/f-0071-2015-10136","title":"Assessment of CFD/CSD Analytical Tools for Improved Rotor Loads","year":2015,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Bell Helicopter Textron (Canada)","funders":"","keywords":"Torsion (gastropod); Lift (data mining); Wind tunnel; Helicopter rotor; Rotor (electric); Bending","score_opus":0.04526292548027371,"score_gpt":0.2986963339474346,"score_spread":0.2534334084671609,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6910504814","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":[0.2938228,0.0009062381,0.64004976,0.0014516496,0.00040494607,0.00054391194,0.0018127892,0.010994026,0.050013863],"genre_scores_gemma":[0.7025029,0.00045992082,0.29096135,0.00016092874,0.00006175702,0.00030986892,0.00084318744,0.0009415375,0.003758572],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99779034,0.0004021842,0.00011272141,0.00013858415,0.0014146871,0.00014139553],"domain_scores_gemma":[0.99271363,0.0030018075,0.00029235485,0.0009760473,0.0028239146,0.00019223377],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.003439578,0.0014474674,0.0007557966,0.0026977756,0.0007757798,0.0018275533,0.0029875026,0.0012093597,0.0058615413],"category_scores_gemma":[0.009716814,0.0006278519,0.0009350917,0.0012761841,0.000690476,0.0017964877,0.001993903,0.0012909406,0.0014031436],"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":[0.00079203513,0.0009894965,0.012982651,0.00064397464,0.00008939104,0.00036749267,0.00055572006,0.63043153,0.0460393,0.029502044,0.006409776,0.27119666],"study_design_scores_gemma":[0.000046856563,0.00008668886,0.0010699619,0.000053237356,0.000013762252,0.00003587779,0.000060869465,0.9842839,0.0103792325,0.0011622582,0.0027795732,0.000027742142],"about_ca_topic_score_codex":0.006015741,"about_ca_topic_score_gemma":0.0046911533,"teacher_disagreement_score":0.006015741,"about_ca_system_score_codex":0.0014010211,"about_ca_system_score_gemma":0.0022230886,"threshold_uncertainty_score":0.019608855},"labels":[],"label_agreement":null},{"id":"W6944428183","doi":"10.17638/03174751","title":"Rotorcraft flight control for improved handling, loads reduction and envelope protection","year":2023,"lang":"en","type":"article","venue":"OpenGrey (Institut de l'Information Scientifique et Technique)","topic":"Aeroelasticity and Vibration Control","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":"Flight envelope; Envelope (radar); Control system; Nonlinear system; Fly-by-wire; Flight control surfaces; Range (aeronautics); Nonlinear control; Aircraft flight mechanics","score_opus":0.015343300985108978,"score_gpt":0.24236568545197132,"score_spread":0.22702238446686235,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6944428183","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":[0.177496,0.0014517924,0.777258,0.0004970173,0.00014525783,0.00010798754,0.00019693776,0.001231904,0.041615155],"genre_scores_gemma":[0.94073695,0.00092540635,0.041958757,0.00009662932,0.000041247775,0.00004078115,0.00014214554,0.00003882368,0.016019315],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999256,0.0000090472595,0.0000026742525,0.000016887552,0.00003733428,0.000008479116],"domain_scores_gemma":[0.9999577,0.000009193499,0.000011653825,0.000007709417,0.000011009823,0.0000027137448],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000096547075,0.00027342382,0.00012116742,0.00007806464,0.00014828997,0.00037019138,0.00017955521,0.00021394323,0.0033213384],"category_scores_gemma":[0.0001462955,0.00007432623,0.00016876374,0.0000784251,0.00018823412,0.00028977793,0.00021993661,0.00026025466,0.00046995722],"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":[0.00022664087,0.00013793912,0.0021009909,0.00046772332,0.000047616184,0.00017116385,0.00030908492,0.3122816,0.32935783,0.08424695,0.008084915,0.26256755],"study_design_scores_gemma":[0.00006201641,0.0005414357,0.003119922,0.00006191748,0.000024746181,0.00014696941,0.00006454987,0.89728445,0.04182758,0.0075341756,0.049308807,0.000023426688],"about_ca_topic_score_codex":0.0015596449,"about_ca_topic_score_gemma":0.0019734784,"teacher_disagreement_score":0.0033213384,"about_ca_system_score_codex":0.00022851603,"about_ca_system_score_gemma":0.00032865946,"threshold_uncertainty_score":0.011111021},"labels":[],"label_agreement":null},{"id":"W6967865531","doi":"10.5281/zenodo.13386075","title":"Supplementary information of the paper: Impact of a block structure on the Lotka-Volterra model.","year":2024,"lang":"en","type":"article","venue":"Zenodo (CERN European Organization for Nuclear Research)","topic":"Aeroelasticity and Vibration Control","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":"Block (permutation group theory); Block structure; Information structure; Data structure","score_opus":0.01372806296926033,"score_gpt":0.21345092940284727,"score_spread":0.19972286643358694,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6967865531","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":[0.0115007525,0.006659442,0.36026102,0.007458786,0.029397972,0.0003687836,0.43872422,0.011167048,0.13446191],"genre_scores_gemma":[0.19454889,0.005559627,0.11149356,0.0050934195,0.01091223,0.0010666662,0.47488463,0.013144529,0.18329649],"study_design_codex":"not_applicable","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995789,0.000088439265,0.00004249607,0.000078771365,0.00017635444,0.00003498513],"domain_scores_gemma":[0.9952055,0.0026251194,0.00029420585,0.0005029574,0.0011678512,0.0002043517],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0006609956,0.0011056478,0.0011752269,0.0013126677,0.00033333278,0.0009836901,0.0016285984,0.0015757888,0.6239592],"category_scores_gemma":[0.011122574,0.00039015154,0.00075433525,0.0012825973,0.00020346577,0.0016502292,0.0009997208,0.0010344796,0.12128284],"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":[0.00025928408,0.00014129172,0.0007143888,0.0017776982,0.000108268396,0.00035045287,0.00004593584,0.011196934,0.0030612657,0.053888284,0.88438356,0.044072714],"study_design_scores_gemma":[0.00035199433,0.00024072405,0.0039371187,0.00044660908,0.00009921423,0.0015431049,0.00006735436,0.0995621,0.005037143,0.19549112,0.69305265,0.00017089925],"about_ca_topic_score_codex":0.0016890689,"about_ca_topic_score_gemma":0.0016425718,"teacher_disagreement_score":0.6239592,"about_ca_system_score_codex":0.0006127242,"about_ca_system_score_gemma":0.0009299491,"threshold_uncertainty_score":0.5363766},"labels":[],"label_agreement":null},{"id":"W6980314263","doi":"","title":"Boundary layer behaviour on a morphing airfoil: simulation and wind tunnel tests","year":2009,"lang":"en","type":"article","venue":"NPARC","topic":"Aeroelasticity and Vibration Control","field":"Engineering","cited_by":4,"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":"Natural Sciences and Engineering Research Council of Canada; Consortium de Recherche et d’innovation en Aérospatiale au Québec","keywords":"Airfoil; Morphing; Swept wing; Laminar flow; Aerodynamics; Wing; Drag; NACA airfoil; Angle of attack; Wind tunnel","score_opus":0.016887773505834786,"score_gpt":0.24774632135863994,"score_spread":0.23085854785280516,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6980314263","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":[0.99850476,0.000023135859,0.0009054234,0.000014293801,0.0000058838577,0.000012785831,0.000058466307,0.00004282417,0.00043248298],"genre_scores_gemma":[0.99888486,0.000013542795,0.00083272986,0.000004261353,8.431763e-7,0.000008964988,0.00006260806,0.0000064744977,0.00018578002],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998123,0.00003364172,0.000012113214,0.000021220258,0.00006333605,0.000057368565],"domain_scores_gemma":[0.9993981,0.00027672292,0.000064472886,0.00008573351,0.000089029716,0.00008600687],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0005571083,0.00045287653,0.000553708,0.00042668817,0.00042113787,0.0003576292,0.0005459647,0.0007024729,0.0013350016],"category_scores_gemma":[0.0008504599,0.00020072341,0.00038456512,0.00020285037,0.00054233253,0.0003405803,0.0003236811,0.00053096964,0.000101573736],"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":[0.0021975883,0.001688807,0.022188803,0.00044743155,0.00010522581,0.0014286785,0.00075305806,0.6417688,0.307083,0.0013282477,0.00074687717,0.020263426],"study_design_scores_gemma":[0.0001661814,0.004098465,0.013414675,0.000034818735,0.00003703354,0.00017781745,0.00028744337,0.8883971,0.092549846,0.0002371425,0.0005561199,0.00004333865],"about_ca_topic_score_codex":0.0021893815,"about_ca_topic_score_gemma":0.0016405712,"teacher_disagreement_score":0.0021893815,"about_ca_system_score_codex":0.00023807252,"about_ca_system_score_gemma":0.00020984148,"threshold_uncertainty_score":0.004465997},"labels":[],"label_agreement":null},{"id":"W6987087053","doi":"","title":"The SHARCS Project: Smart Hybrid Active Rotor Control System for Noise and Vibration Attenuation of Helicopter Blades","year":2005,"lang":"en","type":"article","venue":"IRIS Research product catalog (Sapienza University of Rome)","topic":"Aeroelasticity and Vibration Control","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":"Helicopter rotor; Vibration; Rotor (electric); Active vibration control; Wind tunnel; Vibration control; Wind power; Trailing edge; Noise (video)","score_opus":0.02668676550950512,"score_gpt":0.26673568713132795,"score_spread":0.24004892162182284,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6987087053","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":[0.36780727,0.00089544436,0.585532,0.00050268933,0.00033013042,0.0008324757,0.0010601354,0.015641239,0.02739861],"genre_scores_gemma":[0.78900194,0.0003395188,0.16405044,0.00020190029,0.00014757372,0.00046552374,0.0031545765,0.0003434646,0.042295124],"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9997004,0.000055063876,0.000010044244,0.000050430237,0.00015271342,0.000031440108],"domain_scores_gemma":[0.9997706,0.000030232182,0.000022163335,0.000033550383,0.00010273851,0.000040734107],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0007181112,0.0005165371,0.0004936142,0.00043624145,0.00022821469,0.00040237437,0.00050894497,0.0004397509,0.004147236],"category_scores_gemma":[0.00028948358,0.00015499671,0.00019788134,0.00017332386,0.00044441383,0.00038173195,0.00042107765,0.00029804796,0.00094725343],"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":[0.0019903232,0.0007024784,0.0031888627,0.0005000361,0.000083321785,0.00027067075,0.0002650418,0.049745057,0.32393208,0.00928854,0.033241324,0.5767923],"study_design_scores_gemma":[0.0020115764,0.006488307,0.01389758,0.0000620137,0.00011195314,0.00051412516,0.00015935986,0.5731668,0.29439232,0.0022540453,0.10686155,0.00008030835],"about_ca_topic_score_codex":0.0014233523,"about_ca_topic_score_gemma":0.0012702274,"teacher_disagreement_score":0.004147236,"about_ca_system_score_codex":0.0002817336,"about_ca_system_score_gemma":0.00047718154,"threshold_uncertainty_score":0.013873875},"labels":[],"label_agreement":null},{"id":"W6987891558","doi":"","title":"Vibration Analysis of an Electric UAV Wing Model","year":2022,"lang":"en","type":"article","venue":"Canadian acoustics","topic":"Aeroelasticity and Vibration Control","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":"","score_opus":0.008161514907329526,"score_gpt":0.18965592399214512,"score_spread":0.1814944090848156,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6987891558","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":[0.619208,0.0006517816,0.30320644,0.0006804119,0.000116751915,0.000082758874,0.0004834006,0.00042799523,0.075142466],"genre_scores_gemma":[0.9875794,0.00008614098,0.001930061,0.000034281773,0.000009433576,0.000021718974,0.00009103804,0.00002195243,0.010225989],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99994445,0.000012570904,0.0000023015446,0.000012772849,0.000015206631,0.000012697064],"domain_scores_gemma":[0.99991417,0.000036427024,0.000013920286,0.000006557305,0.000022304564,0.0000066018933],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00011620432,0.00038879577,0.00041915072,0.00021258614,0.0003581702,0.00040611465,0.00035800363,0.00089283544,0.0032307934],"category_scores_gemma":[0.0003343892,0.00019035106,0.00034698192,0.00015226065,0.0003525749,0.00023084521,0.0003332883,0.00033371276,0.00028503733],"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":[0.000047698682,0.000017993116,0.00059042184,0.0000294791,0.000018069877,0.00016577782,0.00005367901,0.98754185,0.004654771,0.0031989457,0.0003137126,0.0033676662],"study_design_scores_gemma":[0.0000074887093,0.00002015183,0.00041532548,0.0000035072508,0.0000048550028,0.000016532758,0.000017521359,0.9985891,0.00029163389,0.0003474605,0.00028285323,0.000003490437],"about_ca_topic_score_codex":0.0198596,"about_ca_topic_score_gemma":0.00882951,"teacher_disagreement_score":0.0198596,"about_ca_system_score_codex":0.00036686155,"about_ca_system_score_gemma":0.00038365042,"threshold_uncertainty_score":0.039488018},"labels":[],"label_agreement":null},{"id":"W6989361380","doi":"","title":"An approach to fatigue damage estimation of helicopter rotating components using computational intelligence techniques","year":2013,"lang":"en","type":"article","venue":"NPARC","topic":"Aeroelasticity and Vibration Control","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 intelligence; Rotor (electric); Computational model; State (computer science); Control (management); Helicopter rotor; SIGNAL (programming language); Component (thermodynamics)","score_opus":0.03690768974008835,"score_gpt":0.27509394460567416,"score_spread":0.2381862548655858,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6989361380","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":[0.0106353145,0.00011838713,0.9882131,0.000078477344,0.000009608292,0.000018387787,0.000027835333,0.00016543236,0.00073348405],"genre_scores_gemma":[0.5775008,0.00039077236,0.41992784,0.0000939438,0.000078853875,0.00013806106,0.0002037822,0.00005925244,0.0016067663],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99969816,0.000058968515,0.000021090858,0.0000685881,0.00012602464,0.000027196527],"domain_scores_gemma":[0.99927324,0.00029245444,0.00014719815,0.000099627556,0.00016709046,0.00002031411],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00043337568,0.0009159649,0.0006450084,0.001161489,0.00032836632,0.0008156375,0.0007977913,0.00060777116,0.0006140709],"category_scores_gemma":[0.0020226394,0.00040145862,0.000609429,0.0006019862,0.0005258226,0.00075319165,0.00057499716,0.00083893054,0.00022755374],"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":[0.00003755996,0.00007905329,0.0015570087,0.000067072084,0.000062133484,0.000046420457,0.00007091205,0.87134796,0.008196973,0.0056798966,0.0004978345,0.11235726],"study_design_scores_gemma":[0.0000013156249,0.00001291367,0.00040768564,0.0000031943491,0.0000044403614,0.000008812541,0.000006293464,0.99624485,0.0010212287,0.0020272043,0.00025723755,0.00000486529],"about_ca_topic_score_codex":0.0039838497,"about_ca_topic_score_gemma":0.0027520955,"teacher_disagreement_score":0.0039838497,"about_ca_system_score_codex":0.0004367913,"about_ca_system_score_gemma":0.0004776967,"threshold_uncertainty_score":0.007921338},"labels":[],"label_agreement":null},{"id":"W6991617442","doi":"","title":"Impact des activités du pharmacien sur la qualité de la pharmacothérapie des patients ayant des besoins complexes suivis en GMF-UMF","year":2018,"lang":"fr","type":"other","venue":"Corpus Université Laval (Université Laval)","topic":"Aeroelasticity and Vibration Control","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":true,"ca_institutions":"","funders":"Université Laval","keywords":"Urban environment; Poison control; Life style; Health services","score_opus":0.010832726181111453,"score_gpt":0.23047199891372955,"score_spread":0.2196392727326181,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6991617442","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":[0.9681169,0.010985432,0.0006468299,0.0044619944,0.00011365135,0.00038772778,0.0016707947,0.000047264653,0.0135694165],"genre_scores_gemma":[0.98638874,0.0034952757,0.001433583,0.0010073928,0.000042963522,0.000253772,0.0006849976,0.0000127854,0.0066805845],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.99749124,0.0008852511,0.00016165267,0.0002066481,0.00074601016,0.00050925266],"domain_scores_gemma":[0.9923792,0.0015614979,0.0016374919,0.00019619631,0.0024667473,0.0017589668],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0031591165,0.00029311396,0.00081980356,0.0004990422,0.0011244377,0.0015439793,0.0005395848,0.0006031248,0.007763221],"category_scores_gemma":[0.010494878,0.00017240315,0.0010901864,0.00081261166,0.0005250068,0.0006210213,0.00083116814,0.0010000517,0.000683319],"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":[0.008748548,0.0022013697,0.61155355,0.0025238576,0.0014494228,0.00030993542,0.0046935645,0.0012814995,0.0038105207,0.0008606198,0.0075582843,0.35500878],"study_design_scores_gemma":[0.00024649838,0.0029000142,0.9826738,0.00072827504,0.00052302977,0.00008127281,0.001713796,0.0005968428,0.0006980904,0.00010781263,0.00969228,0.000038351845],"about_ca_topic_score_codex":0.4991514,"about_ca_topic_score_gemma":0.74459624,"teacher_disagreement_score":0.4991514,"about_ca_system_score_codex":0.009668075,"about_ca_system_score_gemma":0.017895147,"threshold_uncertainty_score":0.992492},"labels":[],"label_agreement":null},{"id":"W6994250043","doi":"","title":"The inner cover","year":2015,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Middle East; Middle Eastern studies; Cover (algebra); Geologist; Turkish","score_opus":0.014499911047507488,"score_gpt":0.19730690375087417,"score_spread":0.1828069927033667,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6994250043","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":[0.001519891,0.025678411,0.0034960625,0.02477326,0.058363564,0.00030528783,0.0029224337,0.003029147,0.87991196],"genre_scores_gemma":[0.0060444362,0.012821926,0.0012336948,0.0062992787,0.008067549,0.00011258341,0.0016497392,0.00092964317,0.9628413],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.9988092,0.00015954957,0.000058637044,0.00025036576,0.0005700801,0.00015224036],"domain_scores_gemma":[0.9959831,0.00058667274,0.00021444999,0.00038231997,0.0016549499,0.0011784506],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.0010021782,0.0013126576,0.0008579869,0.0017601236,0.0018975991,0.0065825055,0.0013487256,0.0028540848,0.6574258],"category_scores_gemma":[0.0069401697,0.0004659005,0.000746926,0.0011355382,0.0007471079,0.0035894085,0.0033665744,0.0026225434,0.55444825],"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":[0.000027985408,0.000019250017,0.00015934941,0.00012883617,0.0000031079749,0.00013831268,0.00004903524,0.0000328502,0.0002644081,0.0013487372,0.9249118,0.07291633],"study_design_scores_gemma":[0.00000268994,0.000008887793,0.000171098,0.00009415251,0.000001982214,0.0003537797,0.00006413324,0.000025399137,0.00009204026,0.00036528727,0.9988172,0.0000033205713],"about_ca_topic_score_codex":0.0015297062,"about_ca_topic_score_gemma":0.0028807262,"teacher_disagreement_score":0.6574258,"about_ca_system_score_codex":0.0012741819,"about_ca_system_score_gemma":0.0024447842,"threshold_uncertainty_score":0.4886405},"labels":[],"label_agreement":null},{"id":"W6999455344","doi":"","title":"Convergence acceleration to a periodic steady state for aeroelastic simulations","year":2006,"lang":"en","type":"dissertation","venue":"eScholarship@McGill (McGill)","topic":"Aeroelasticity and Vibration Control","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":"McGill University; Library and Archives Canada","funders":"McGill University","keywords":"Transonic; Aeroelasticity; Flutter; Solver; Frequency domain; Nonlinear system; Convergence (economics); Time domain; Supersonic speed","score_opus":0.015551498921272687,"score_gpt":0.2380010104519411,"score_spread":0.22244951153066841,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W6999455344","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":[0.17934847,0.0004899411,0.7734616,0.0004624074,0.00017789671,0.00016252333,0.00019881617,0.0017235,0.043974806],"genre_scores_gemma":[0.79344773,0.00044569606,0.19663453,0.00006497025,0.000027046977,0.0002796719,0.00029916226,0.0004256893,0.008375504],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998709,0.000030579373,0.000005574762,0.000011845883,0.000064521235,0.000016555212],"domain_scores_gemma":[0.9995369,0.00022703128,0.000032948967,0.00006410164,0.00011528902,0.000023702709],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00044437186,0.0004439955,0.0003624826,0.00042003434,0.0005072506,0.00047435978,0.0004236842,0.00057142926,0.003260806],"category_scores_gemma":[0.0024958444,0.00027155588,0.00039532525,0.00026094762,0.00047434398,0.00047301626,0.00066790334,0.0006567183,0.00082046236],"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":[0.00008411763,0.00009804288,0.0018289058,0.0001418318,0.000016115613,0.00015277679,0.0001902691,0.9074926,0.01583705,0.0304764,0.0018132738,0.041868653],"study_design_scores_gemma":[0.0000033769713,0.000014797655,0.00013728844,0.000008571399,0.0000010849818,0.000010094252,0.000010075084,0.9972691,0.00080332096,0.0011396523,0.0006004252,0.0000021215783],"about_ca_topic_score_codex":0.0043098642,"about_ca_topic_score_gemma":0.0041401545,"teacher_disagreement_score":0.0043098642,"about_ca_system_score_codex":0.0003950163,"about_ca_system_score_gemma":0.00065871346,"threshold_uncertainty_score":0.010908425},"labels":[],"label_agreement":null},{"id":"W7009726253","doi":"","title":"Exploration de la réalité des femmes non-monogames consensuelles au Québec : vécu relationnel et expérience des services de santé et services sociaux","year":2023,"lang":"fr","type":"other","venue":"Knowledge UdeS (Institutional Deposit of the University of Sherbrooke)","topic":"Aeroelasticity and Vibration Control","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":"Social impact; Gender relations; Paid work","score_opus":0.016530431736169988,"score_gpt":0.2370272912066167,"score_spread":0.2204968594704467,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7009726253","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":[0.9829571,0.0012804298,0.00050844956,0.0033672312,0.00004915223,0.00004531468,0.0002917356,0.000006823795,0.011493778],"genre_scores_gemma":[0.99155116,0.0008113769,0.0003905263,0.0007603816,0.000005897611,0.000048783302,0.00010141283,0.0000066168577,0.006323796],"study_design_codex":"qualitative","study_design_gemma":"qualitative","domain_scores_codex":[0.9986739,0.000582686,0.000025782749,0.00014515659,0.00021784496,0.00035461207],"domain_scores_gemma":[0.9982407,0.00044553078,0.00015503279,0.00006429912,0.0006781813,0.00041623035],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0020544836,0.00027204305,0.00044122958,0.000887517,0.009818519,0.0029082322,0.0008499394,0.00070097396,0.009748866],"category_scores_gemma":[0.002977455,0.0002600302,0.00023392252,0.0014413162,0.0039061108,0.0016389162,0.001831281,0.001511363,0.0003592164],"study_design_candidate":"qualitative","study_design_consensus":"qualitative","about_ca_topic_candidate":true,"about_ca_topic_consensus":true,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00010765676,0.00011190006,0.13139434,0.00020347725,0.0000414287,0.00065376196,0.82261515,0.00010000913,0.0011985248,0.006535874,0.004757542,0.032280426],"study_design_scores_gemma":[0.000007918584,0.00007257065,0.14609818,0.00033922814,0.00003313012,0.00014426396,0.8305704,0.00021600236,0.00017754521,0.0005905677,0.021711955,0.000038276597],"about_ca_topic_score_codex":0.949112,"about_ca_topic_score_gemma":0.9823454,"teacher_disagreement_score":0.050888002,"about_ca_system_score_codex":0.020310188,"about_ca_system_score_gemma":0.026770325,"threshold_uncertainty_score":0.1473614},"labels":[],"label_agreement":null},{"id":"W7021071529","doi":"","title":"A new morphing wing mechanism using smart actuators controlled by a self-tuning fuzzy logic controller","year":2011,"lang":"en","type":"article","venue":"NPARC","topic":"Aeroelasticity and Vibration Control","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":"Fuzzy logic; Morphing; Actuator; Airfoil; Controller (irrigation); Fuzzy control system; Adaptive neuro fuzzy inference system; Wind tunnel","score_opus":0.021966488121293665,"score_gpt":0.2066048717810403,"score_spread":0.18463838365974664,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7021071529","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":[0.12239519,0.0005152232,0.87013286,0.00011691775,0.00017046106,0.00009405148,0.000039937204,0.0010349783,0.0055004153],"genre_scores_gemma":[0.8153994,0.00020593738,0.18020304,0.00007915914,0.0000334703,0.00007229095,0.000039043705,0.0000212348,0.003946433],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.9999118,0.0000064583,0.0000061020596,0.00002103295,0.00004556356,0.000009068548],"domain_scores_gemma":[0.9999368,0.000010809969,0.000015374295,0.000012005299,0.000017519591,0.00000743858],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00014204408,0.00021354623,0.00018810746,0.00022431176,0.0001519762,0.00022076503,0.00050039194,0.00032047115,0.00073301484],"category_scores_gemma":[0.00011968163,0.00012173455,0.00025917258,0.00007890422,0.00021514257,0.00024380331,0.00023454381,0.00018949975,0.0001581223],"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":[0.00016995915,0.00005951216,0.0009768984,0.0002623159,0.00006121454,0.0003550698,0.00011012428,0.041808605,0.78765666,0.008940141,0.00078717404,0.15881239],"study_design_scores_gemma":[0.0001159706,0.00063629093,0.0046376893,0.000044514003,0.00010989911,0.0011377119,0.000038014834,0.74846137,0.21915123,0.002636529,0.022956572,0.00007434572],"about_ca_topic_score_codex":0.0002828176,"about_ca_topic_score_gemma":0.00037422116,"teacher_disagreement_score":0.00073301484,"about_ca_system_score_codex":0.000102644306,"about_ca_system_score_gemma":0.00013723,"threshold_uncertainty_score":0.0024521947},"labels":[],"label_agreement":null},{"id":"W7037226167","doi":"","title":"Development of thermoplastic composite cones for helicopter tail boom application","year":2014,"lang":"en","type":"article","venue":"NPARC","topic":"Aeroelasticity and Vibration Control","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":"Thermoplastic composites; Thermoplastic; Bending; Compression molding; Composite number; Buckling; Compaction; Molding (decorative); Compression (physics)","score_opus":0.008387481948878348,"score_gpt":0.20155480807308782,"score_spread":0.19316732612420948,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7037226167","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":[0.9320854,0.001950908,0.048370454,0.000056906083,0.00007709092,0.00045701332,0.00036899347,0.00041696028,0.016216207],"genre_scores_gemma":[0.88499993,0.0019530995,0.10020694,0.00003651279,0.000010177366,0.00016107263,0.00046216548,0.0000898101,0.01208031],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99985003,0.000008453585,0.0000054638253,0.000021338235,0.00009521109,0.00001944572],"domain_scores_gemma":[0.9997508,0.000017582259,0.000046803503,0.000017187254,0.0001199417,0.000047682857],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00020037613,0.00036616132,0.00019046543,0.00039547583,0.00020351175,0.00024149998,0.0002444497,0.00024060479,0.0010857127],"category_scores_gemma":[0.00017109778,0.00014796638,0.0002447811,0.00021242343,0.00010174629,0.00021624386,0.00013800568,0.00034711906,0.00040540253],"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":[0.00003942452,0.000048902,0.0003297668,0.00008106354,0.0000021797416,0.00019779846,0.000026977728,0.000690214,0.9901529,0.00017061607,0.00007909325,0.00818116],"study_design_scores_gemma":[0.0000081935195,0.0010808363,0.0042720395,0.00002315793,0.0000083438545,0.0004140705,0.000031949137,0.0039302534,0.984608,0.000041699146,0.0055702864,0.000011222884],"about_ca_topic_score_codex":0.00089458196,"about_ca_topic_score_gemma":0.0029218476,"teacher_disagreement_score":0.0010857127,"about_ca_system_score_codex":0.00017080292,"about_ca_system_score_gemma":0.00045778198,"threshold_uncertainty_score":0.003632009},"labels":[],"label_agreement":null},{"id":"W7042667762","doi":"","title":"Passive Aeroelastic Control of Aircraft Wings Via Nonlinear Oscillators","year":2021,"lang":"en","type":"article","venue":"theses.fr (ABES)","topic":"Aeroelasticity and Vibration Control","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":"Natural Sciences and Engineering Research Council of Canada; Université de Toulouse; Polytechnique Montréal","keywords":"Work (physics); Derating; Manipulator (device)","score_opus":0.005912374888979317,"score_gpt":0.1934826919408716,"score_spread":0.18757031705189228,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7042667762","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":[0.35678715,0.000557172,0.6273832,0.00035277227,0.000106275584,0.00004539595,0.00004528647,0.00031554385,0.014407146],"genre_scores_gemma":[0.980496,0.00025140122,0.013207616,0.00001968169,0.000016460155,0.00003078739,0.000015022816,0.000015297232,0.005947632],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9999436,0.000012969255,0.0000021968217,0.000014921558,0.000020576339,0.0000057668626],"domain_scores_gemma":[0.9999174,0.000035825335,0.000018289626,0.000008575781,0.0000147503115,0.000005231532],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00013843943,0.00023903575,0.00015779125,0.00007605931,0.0001508029,0.0003673529,0.00034540266,0.00024724772,0.0009311692],"category_scores_gemma":[0.000360908,0.000111866124,0.00018353293,0.00006784021,0.00028039163,0.000285995,0.00029947984,0.0002228802,0.00016550168],"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":[0.00033525404,0.000091193826,0.0008785616,0.0002109801,0.00004328892,0.00015027738,0.0003460052,0.554005,0.362916,0.025592571,0.00054904027,0.05488168],"study_design_scores_gemma":[0.00002341049,0.00011671437,0.00029997938,0.00000707408,0.0000089162895,0.000019126666,0.000018335193,0.9858838,0.010019994,0.0019004717,0.001694435,0.0000077999075],"about_ca_topic_score_codex":0.0006928916,"about_ca_topic_score_gemma":0.00077015406,"teacher_disagreement_score":0.0009311692,"about_ca_system_score_codex":0.00016668759,"about_ca_system_score_gemma":0.00018611198,"threshold_uncertainty_score":0.003115058},"labels":[],"label_agreement":null},{"id":"W7066711592","doi":"","title":"Influences and Transformations: Mohsin Hamid’s Mongrelization of the West and the East in <i>The Reluctant Fundamentalist</i>","year":2023,"lang":"fr","type":"article","venue":"Project Muse (Johns Hopkins University)","topic":"Aeroelasticity and Vibration Control","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":"Criticism; Government (linguistics); Work (physics); Subject (documents)","score_opus":0.013634513362767692,"score_gpt":0.1991010336170166,"score_spread":0.1854665202542489,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7066711592","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":[0.33311418,0.23402742,0.0016432456,0.13939713,0.002279248,0.00001499674,0.00021549861,0.000012618686,0.2892956],"genre_scores_gemma":[0.9678614,0.023473274,0.00030923716,0.0035292695,0.0002225619,0.000005112033,0.0000272396,0.000009251329,0.004562666],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"qualitative","domain_scores_codex":[0.9985514,0.0008516059,0.000057497164,0.00013043424,0.0001866461,0.00022236315],"domain_scores_gemma":[0.9986326,0.0007655258,0.00026127129,0.00011322227,0.00015141266,0.000075902564],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0028972065,0.00017991955,0.00032542468,0.00095297676,0.0051312693,0.002768026,0.00040063282,0.0009558262,0.003318467],"category_scores_gemma":[0.003234799,0.00016677217,0.00012547694,0.0029531408,0.016146585,0.0028635862,0.0023220011,0.0018309087,0.00017545173],"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":[0.00008640635,0.00001845,0.0039453767,0.00024884517,0.000033277498,0.00025202232,0.11950528,0.00009560864,0.00019305538,0.8418755,0.0071525183,0.026593724],"study_design_scores_gemma":[0.000041502797,0.00006622704,0.033038538,0.0015092165,0.000067047535,0.00069376326,0.18199192,0.00009954085,0.000414106,0.120695,0.6613365,0.00004657726],"about_ca_topic_score_codex":0.085621424,"about_ca_topic_score_gemma":0.1253189,"teacher_disagreement_score":0.085621424,"about_ca_system_score_codex":0.0043923133,"about_ca_system_score_gemma":0.005181696,"threshold_uncertainty_score":0.17024606},"labels":[],"label_agreement":null},{"id":"W7083852630","doi":"","title":"News Espresso: Texas burial for Bush, China demands Canada release Huawei executive, Paris riots","year":2018,"lang":"en","type":"other","venue":"Internet Archive (Internet Archive)","topic":"Aeroelasticity and Vibration Control","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":"George (robot); China; Thursday; Newspaper; Presidential system; Parliament; Coffin; Spanish Civil War; CONTEST","score_opus":0.006645626754413964,"score_gpt":0.20626303938669147,"score_spread":0.1996174126322775,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7083852630","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":[0.0023436584,0.003422303,0.00018872581,0.03880798,0.028430102,0.00026916186,0.012991542,0.0014978421,0.9120487],"genre_scores_gemma":[0.0032835582,0.0013558462,0.00008924997,0.009301157,0.0023846866,0.000054659333,0.003306302,0.0002501085,0.9799745],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.99954456,0.000013867317,0.000011144882,0.000034873934,0.0002706742,0.00012478324],"domain_scores_gemma":[0.9986376,0.00008006726,0.00005057712,0.00006591419,0.00070702215,0.00045874977],"candidate_categories":["insufficient_payload"],"consensus_categories":[],"category_scores_codex":[0.00037491802,0.0011296459,0.0005774199,0.0010041039,0.005204144,0.0058382056,0.00079533155,0.0038015186,0.39862755],"category_scores_gemma":[0.0015438874,0.00049047126,0.00041381462,0.001464462,0.00074326823,0.001872495,0.0014094951,0.0046165874,0.22003077],"study_design_candidate":"not_applicable","study_design_consensus":"not_applicable","about_ca_topic_candidate":true,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000009317377,0.0000050809476,0.0000763297,0.00001336641,9.08388e-7,0.000039596,0.000019370344,0.000005687169,0.000034903183,0.00011556731,0.9977189,0.0019610305],"study_design_scores_gemma":[0.000006936215,0.0000057145385,0.0009852471,0.000035941724,0.0000017450194,0.000017814804,0.00018428356,0.000020206946,0.00004911063,0.000029428029,0.99865854,0.000005029019],"about_ca_topic_score_codex":0.2721944,"about_ca_topic_score_gemma":0.5445826,"teacher_disagreement_score":0.7278056,"about_ca_system_score_codex":0.0043833,"about_ca_system_score_gemma":0.0057069655,"threshold_uncertainty_score":0.8577848},"labels":[],"label_agreement":null},{"id":"W7097756564","doi":"","title":"DOI:10.5139/IJASS.2011.12.2.93 Review of Active Rotor Control Research in Canada","year":2016,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Tower; Control (management); Rotor (electric); Key (lock); Wind tunnel; Control system","score_opus":0.02737485332549496,"score_gpt":0.2601215140025644,"score_spread":0.23274666067706942,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7097756564","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":[0.0037118276,0.52925867,0.0034580703,0.00583091,0.0031344213,0.00008773595,0.0009226143,0.00035975885,0.45323595],"genre_scores_gemma":[0.034685794,0.57667804,0.0036137863,0.0015205701,0.0008562345,0.000033012147,0.00093609997,0.0001906504,0.38148582],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9989611,0.00004108236,0.000047298494,0.00009430626,0.0007221929,0.00013408609],"domain_scores_gemma":[0.99790096,0.00013932135,0.0000856281,0.000070401235,0.001620248,0.00018340224],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0010026686,0.0006246986,0.00056512724,0.0037573876,0.0016578828,0.0038808284,0.0011635498,0.0013254313,0.1514742],"category_scores_gemma":[0.0016318089,0.0003771434,0.00029443117,0.0062434925,0.0017592894,0.0015472664,0.00097564276,0.0006017513,0.057066344],"study_design_candidate":"not_applicable","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":[0.00008827963,0.00005800324,0.0013085888,0.001981936,0.0000189475,0.00018862772,0.00016355938,0.00049992,0.0014893992,0.008367359,0.106914856,0.8789205],"study_design_scores_gemma":[0.000004461658,0.000029720386,0.0031944355,0.0010312983,0.000016877526,0.00026328934,0.00019772584,0.00012796123,0.0004948008,0.00051538023,0.9941087,0.000015484235],"about_ca_topic_score_codex":0.47089535,"about_ca_topic_score_gemma":0.5499957,"teacher_disagreement_score":0.52910465,"about_ca_system_score_codex":0.009421192,"about_ca_system_score_gemma":0.01745307,"threshold_uncertainty_score":0.93630886},"labels":[],"label_agreement":null},{"id":"W7098028659","doi":"","title":"On a Finite Element Approach to Modeling of Piezoelectric Element Driven Compliant Mechanisms","year":2009,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Copying; Work (physics); Permission; Element (criminal law); Finite element method; Head (geology)","score_opus":0.018503117007929743,"score_gpt":0.21636614055632733,"score_spread":0.19786302354839758,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7098028659","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":[0.004520795,0.00019852287,0.988485,0.00014911362,0.000046606674,0.00006127746,0.000057871883,0.00015241235,0.00632833],"genre_scores_gemma":[0.29977953,0.0016896399,0.66281986,0.00020191788,0.000063426094,0.0006852736,0.0003269097,0.0002239922,0.03420941],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9998202,0.000049804392,0.00001306465,0.000021725271,0.00008237451,0.000012846105],"domain_scores_gemma":[0.9997993,0.00011444959,0.000016081232,0.000021178093,0.000039311293,0.000009664133],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00054948754,0.0004699306,0.00054363545,0.0006562377,0.0005291008,0.00092513626,0.0015501612,0.0017954167,0.0054043774],"category_scores_gemma":[0.0008898964,0.00062904565,0.0011208027,0.0005392483,0.0007208236,0.00090159883,0.0008281379,0.0012316281,0.0012547827],"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":[0.00002399999,0.00004225294,0.00019437593,0.000074689306,0.00001853324,0.000112054266,0.00011728591,0.9127585,0.008042054,0.056434855,0.000567218,0.021614078],"study_design_scores_gemma":[0.0000038480043,0.000017143697,0.000048412236,0.000020094782,0.0000042665406,0.000024899391,0.000014674384,0.98883504,0.0006011207,0.0066067143,0.0038172933,0.0000064028386],"about_ca_topic_score_codex":0.00390854,"about_ca_topic_score_gemma":0.003936699,"teacher_disagreement_score":0.0054043774,"about_ca_system_score_codex":0.00043910227,"about_ca_system_score_gemma":0.00064605894,"threshold_uncertainty_score":0.01807946},"labels":[],"label_agreement":null},{"id":"W7100824638","doi":"","title":"Psychological Impact of Cyber-Bullying: Implications for School Counsellors L’effet psychologique de cyber-intimidation: Implications pour les conseillers scolaires","year":2016,"lang":"en","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Poison control; Psychological distress; Inclusion (mineral); Qualitative research; Socialization","score_opus":0.035714988299519725,"score_gpt":0.3255776731009761,"score_spread":0.2898626848014563,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7100824638","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":[0.9948803,0.00085671083,0.0000595236,0.0025231102,0.000014134239,0.00002817104,0.000114222814,0.000005803607,0.0015181081],"genre_scores_gemma":[0.99571615,0.0021147828,0.00026502332,0.000571507,0.000014816293,0.000041225863,0.00007459801,0.0000033042347,0.0011986551],"study_design_codex":"observational","study_design_gemma":"observational","domain_scores_codex":[0.9989502,0.00027623458,0.00006689616,0.00007223135,0.00033263452,0.0003018994],"domain_scores_gemma":[0.9973826,0.0005099339,0.0006182706,0.00007316768,0.0006568918,0.000759171],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0012286883,0.00022030136,0.00041137743,0.00071940373,0.0037513713,0.0014652279,0.0005897018,0.00052013685,0.002748235],"category_scores_gemma":[0.0031514047,0.00022878093,0.00030504778,0.0011455384,0.0011506162,0.00065629213,0.0009520416,0.0009102911,0.00019454824],"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":[0.000041786727,0.00017990948,0.9257805,0.00016974266,0.00002723926,0.0007050068,0.03473481,0.000043406093,0.00067304436,0.00015555056,0.0016417472,0.035847276],"study_design_scores_gemma":[0.0000066338944,0.00016966816,0.8884506,0.00031304086,0.00003504661,0.00034175112,0.106781654,0.000053004413,0.00029906852,0.00009863122,0.003436139,0.000014763653],"about_ca_topic_score_codex":0.4113287,"about_ca_topic_score_gemma":0.62372357,"teacher_disagreement_score":0.4113287,"about_ca_system_score_codex":0.004121576,"about_ca_system_score_gemma":0.009123175,"threshold_uncertainty_score":0.817869},"labels":[],"label_agreement":null},{"id":"W7115036076","doi":"","title":"Positive position feedback-based methods for active vibration control of carbon fibre structures (aka Killing the vibes)","year":2025,"lang":"en","type":"dissertation","venue":"eScholarship@McGill (McGill)","topic":"Aeroelasticity and Vibration Control","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; Natural Sciences and Engineering Research Council of Canada; Westlake University; McGill University","keywords":"Position (finance); Vibration; Vibration control; Carbon fibers; Active vibration control; Control theory (sociology)","score_opus":0.009634871818850399,"score_gpt":0.25779284780591877,"score_spread":0.24815797598706837,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7115036076","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":[0.016508188,0.005232198,0.95773375,0.00030743962,0.00044918217,0.00006379077,0.000024408362,0.000395963,0.019284949],"genre_scores_gemma":[0.78224546,0.005163984,0.17012691,0.00020120274,0.00036274394,0.00017888466,0.00005785864,0.00007834189,0.041584574],"study_design_codex":"design_other","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99989593,0.000013214524,0.000003705778,0.000020216417,0.000057965466,0.000009005019],"domain_scores_gemma":[0.99994516,0.000023087272,0.0000069042667,0.000004671527,0.000016743203,0.000003498972],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0001718425,0.0003364567,0.00019891761,0.00020526296,0.00018643257,0.00033574185,0.0003402613,0.00042156785,0.002570516],"category_scores_gemma":[0.00027735054,0.00010881989,0.00023135419,0.00012450843,0.00024775034,0.00024341728,0.000311352,0.00055893126,0.000396947],"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":[0.00012722956,0.00008928954,0.00023686385,0.0004598564,0.000033714572,0.00014150438,0.00023790376,0.17450684,0.13469256,0.0633779,0.006518159,0.6195781],"study_design_scores_gemma":[0.000026939166,0.0003672025,0.00071835174,0.00007044656,0.000017970253,0.0001773105,0.00004007353,0.9296146,0.02091139,0.015199243,0.032825425,0.000030967545],"about_ca_topic_score_codex":0.0008399352,"about_ca_topic_score_gemma":0.00094072823,"teacher_disagreement_score":0.002570516,"about_ca_system_score_codex":0.00020769725,"about_ca_system_score_gemma":0.000162018,"threshold_uncertainty_score":0.008599222},"labels":[],"label_agreement":null},{"id":"W7125246713","doi":"10.18280/rcma.350619","title":"Experimental Evaluation of Morphing Wing Technologies: A Systematic Review","year":2025,"lang":"","type":"article","venue":"Revue des composites et des matériaux avancés","topic":"Aeroelasticity and Vibration Control","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":"Morphing; Wing; Field (mathematics); Displacement (psychology)","score_opus":0.06350386906890289,"score_gpt":0.32052829648180914,"score_spread":0.25702442741290626,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7125246713","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":[0.004090675,0.9908125,0.0010842575,0.00025291843,0.00019863728,0.0020384188,0.0009058282,0.000019564675,0.00059721124],"genre_scores_gemma":[0.044520453,0.9460408,0.004720773,0.0010031274,0.00012479427,0.0025833005,0.0006590394,0.000028904331,0.00031891486],"study_design_codex":"systematic_review","study_design_gemma":"systematic_review","domain_scores_codex":[0.9805124,0.006919781,0.007454938,0.0016151828,0.003159812,0.00033795185],"domain_scores_gemma":[0.93927175,0.043025203,0.0106826145,0.0016766081,0.0048171277,0.00052666984],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.020240558,0.0019877856,0.011315626,0.0080961995,0.00082144304,0.0038632953,0.0033299287,0.0024841605,0.0063362583],"category_scores_gemma":[0.07005821,0.0012278138,0.010640045,0.0061280704,0.0021125337,0.002647345,0.0023163434,0.0013904487,0.0005400837],"study_design_candidate":"systematic_review","study_design_consensus":"systematic_review","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0008267409,0.00006796057,0.00064445595,0.93860495,0.01591341,0.00009261581,0.00028326816,0.00012807654,0.0003720526,0.00023987409,0.00070794154,0.042118546],"study_design_scores_gemma":[0.0015023904,0.001216956,0.0053738444,0.78726286,0.17575033,0.00035087476,0.0008119503,0.00015334476,0.0007080548,0.00059201394,0.026164923,0.00011245046],"about_ca_topic_score_codex":0.0066227983,"about_ca_topic_score_gemma":0.020318657,"teacher_disagreement_score":0.020240558,"about_ca_system_score_codex":0.0035979692,"about_ca_system_score_gemma":0.0138452705,"threshold_uncertainty_score":0.107043564},"labels":[],"label_agreement":null},{"id":"W7132439579","doi":"","title":"Conceptual design for the actuation and skin integration of a morphing leading edge","year":2019,"lang":"en","type":"article","venue":"NPARC","topic":"Aeroelasticity and Vibration Control","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":true,"ca_institutions":"","funders":"","keywords":"Morphing; Wing; Trailing edge; Takeoff; Leading edge; Camber (aerodynamics); Airfoil; Airplane; Lift (data mining)","score_opus":0.027267463543161986,"score_gpt":0.2321426269427827,"score_spread":0.20487516339962072,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7132439579","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":[0.039983593,0.0011194819,0.8901471,0.00087625615,0.00078211667,0.0007776393,0.0004206868,0.0024134303,0.06347973],"genre_scores_gemma":[0.41623878,0.0010383909,0.5511872,0.00045243892,0.00011335583,0.000667148,0.00032979462,0.00025457144,0.02971832],"study_design_codex":"bench_or_experimental","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9996824,0.000023182085,0.000015258553,0.000043216634,0.00018827422,0.000047692236],"domain_scores_gemma":[0.99980813,0.000013043753,0.000033456556,0.000029973393,0.00008178386,0.000033605727],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00033890415,0.00061718916,0.00029776138,0.0003448006,0.00036623672,0.0010916527,0.0014970824,0.0010252901,0.004800404],"category_scores_gemma":[0.0003243496,0.00042557353,0.0005487823,0.00016483488,0.00040985903,0.00080531894,0.0006126118,0.00090618705,0.0020543076],"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":[0.00015779166,0.00015686876,0.00072515424,0.00095202663,0.000042355634,0.0012856461,0.00029849962,0.036646277,0.7489485,0.10101154,0.007112493,0.10266302],"study_design_scores_gemma":[0.00014041422,0.0023043936,0.0023161334,0.0002491679,0.00011142192,0.002705915,0.00021308761,0.26018423,0.33891377,0.0126007255,0.3800921,0.00016858515],"about_ca_topic_score_codex":0.0005763367,"about_ca_topic_score_gemma":0.0007191964,"teacher_disagreement_score":0.004800404,"about_ca_system_score_codex":0.0004997689,"about_ca_system_score_gemma":0.0007210431,"threshold_uncertainty_score":0.016058981},"labels":[],"label_agreement":null},{"id":"W7132946000","doi":"","title":"A hierarchical theory for layered beams with piezoelectric actuation","year":2004,"lang":"","type":"dissertation","venue":"TSpace","topic":"Aeroelasticity and Vibration Control","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":"University of Toronto","keywords":"Piezoelectricity; Superposition principle; Composite number; Finite element method; Displacement (psychology); Timoshenko beam theory; Stress (linguistics); Beam (structure)","score_opus":0.010538337326342689,"score_gpt":0.2699978234744535,"score_spread":0.2594594861481108,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7132946000","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":[0.015702548,0.00039343562,0.9683193,0.0001707172,0.000053017473,0.000036351743,0.00008565767,0.00014518776,0.015093785],"genre_scores_gemma":[0.6482955,0.0013700299,0.33177376,0.00035855215,0.00010935964,0.00034936095,0.00022484832,0.00008502216,0.017433533],"study_design_codex":"theoretical_or_conceptual","study_design_gemma":"theoretical_or_conceptual","domain_scores_codex":[0.9997614,0.00003032269,0.000011006191,0.000031009786,0.00013281264,0.0000335737],"domain_scores_gemma":[0.99985456,0.000038106424,0.000019669495,0.000028414788,0.00004229937,0.000016937644],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00041363577,0.0003374115,0.00025201248,0.00054647593,0.00038231723,0.0005341842,0.00086085725,0.0005701654,0.0028821977],"category_scores_gemma":[0.00046740603,0.00032189378,0.00061475666,0.00033301645,0.0007559666,0.0010137627,0.0006629239,0.0007036907,0.00065798406],"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":[0.000010064435,0.000017374517,0.00023197503,0.0000531314,0.000011371754,0.00006510031,0.00014902577,0.113522775,0.014580276,0.8570818,0.0008478856,0.013429221],"study_design_scores_gemma":[0.000008261207,0.000041906365,0.0003556089,0.000016448874,0.000007861,0.000050163148,0.00003418977,0.76471305,0.0020827742,0.22771913,0.004953055,0.0000175812],"about_ca_topic_score_codex":0.0018342277,"about_ca_topic_score_gemma":0.0018273141,"teacher_disagreement_score":0.0028821977,"about_ca_system_score_codex":0.00075384293,"about_ca_system_score_gemma":0.0005759589,"threshold_uncertainty_score":0.009641945},"labels":[],"label_agreement":null},{"id":"W7138412816","doi":"10.1109/aset66891.2025.11428017","title":"Optimized Finite Time Lyapunov Control for the Stabilization of a Blended Wing Body UAV","year":2025,"lang":"","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Carleton University","funders":"","keywords":"Control theory (sociology); Lyapunov function; Wing; Stability (learning theory); Control (management); Trajectory","score_opus":0.0074452211084744205,"score_gpt":0.22397723529303323,"score_spread":0.2165320141845588,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7138412816","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":[0.30056798,0.00025088261,0.6900334,0.00022744284,0.00010533969,0.000044836535,0.000056298788,0.00028004294,0.008433865],"genre_scores_gemma":[0.9941083,0.000022558594,0.0045779175,0.000014404011,0.0000056244808,0.000019479987,0.000014784893,0.0000091161655,0.0012278402],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99989045,0.000027538788,0.000005229406,0.000017167522,0.00003697996,0.000022678598],"domain_scores_gemma":[0.9998097,0.000056886965,0.000038798502,0.0000117084755,0.000065679385,0.000017273584],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00031288387,0.0005451958,0.00041468718,0.00024414482,0.0002887102,0.0005806911,0.0003952608,0.0004661748,0.0013349736],"category_scores_gemma":[0.00058577885,0.00019614356,0.0002101352,0.0001449374,0.00039050556,0.00024473583,0.0005719188,0.0003885362,0.00015680568],"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":[0.00025511996,0.00004077297,0.00036847382,0.000060178543,0.000032282478,0.000100044184,0.00007455456,0.9641953,0.01434374,0.0049453825,0.0004011553,0.015182913],"study_design_scores_gemma":[0.00001056636,0.0000610557,0.00009897087,0.000002162141,0.0000027282701,0.0000037012474,0.000005917211,0.99871445,0.0006099882,0.0003903403,0.00009778313,0.000002277738],"about_ca_topic_score_codex":0.004404236,"about_ca_topic_score_gemma":0.0034112872,"teacher_disagreement_score":0.004404236,"about_ca_system_score_codex":0.00045323712,"about_ca_system_score_gemma":0.0005132214,"threshold_uncertainty_score":0.008757234},"labels":[],"label_agreement":null},{"id":"W7152634890","doi":"10.70675/eb558d08zed33z4b4bzbce3ze3b29a83561d","title":"Investigation of novel electroactive morphing concepts for aerodynamic performance increase of an A320 wing through High-Fidelity numerical simulation","year":2025,"lang":"","type":"dissertation","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Morphing; Swept wing; Wing; Aerodynamics; Numerical modeling","score_opus":0.023093662055659717,"score_gpt":0.2902859220296846,"score_spread":0.2671922599740249,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7152634890","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":[0.8525804,0.0006355131,0.11498557,0.00038643298,0.00009357772,0.00016448324,0.00031134085,0.00038224537,0.030460378],"genre_scores_gemma":[0.9768337,0.00018581077,0.02046915,0.000022483737,0.0000035311032,0.00006206562,0.00007571723,0.000033561366,0.0023140905],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99991536,0.00001374129,0.000004484019,0.000010615146,0.000040987507,0.000014712112],"domain_scores_gemma":[0.99981374,0.00008843727,0.000023576042,0.000023968993,0.000034934594,0.00001530552],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00028278178,0.00031090292,0.00027108457,0.0002480633,0.00027773026,0.0006006715,0.0004049821,0.0006590277,0.002082813],"category_scores_gemma":[0.000593975,0.00015535211,0.0003819546,0.0001539198,0.00043748517,0.00038676642,0.0003850774,0.00037957865,0.00018436745],"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":[0.00017461834,0.00014631056,0.0026891555,0.00021408545,0.000022328117,0.00023861787,0.0002124004,0.8721553,0.101504445,0.0064492356,0.00053682853,0.015656548],"study_design_scores_gemma":[0.000011174983,0.00006482086,0.00058170105,0.00001308966,0.0000039176134,0.000024245983,0.00003432401,0.99170965,0.006360804,0.00028185028,0.00090742996,0.000006960954],"about_ca_topic_score_codex":0.0018751204,"about_ca_topic_score_gemma":0.0013734663,"teacher_disagreement_score":0.002082813,"about_ca_system_score_codex":0.0002764482,"about_ca_system_score_gemma":0.0003650187,"threshold_uncertainty_score":0.0069677234},"labels":[],"label_agreement":null},{"id":"W7164156074","doi":"10.4050/f-0079-2023-0132","title":"Full-Aircraft CH-53K Hover Simulations with HELIOS","year":2023,"lang":"","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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); Power (physics); Propulsion; Carry (investment); Lift coefficient","score_opus":0.01285729112213172,"score_gpt":0.22206047271460144,"score_spread":0.20920318159246973,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7164156074","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":[0.884081,0.0003227143,0.021600368,0.0005033756,0.00013385822,0.00022716001,0.01039022,0.0017875733,0.0809537],"genre_scores_gemma":[0.97043407,0.00018121622,0.014639978,0.00012822059,0.000039012582,0.00035996488,0.0056633637,0.00065231364,0.007901895],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99984455,0.000025460955,0.000005620674,0.00001835028,0.00005687962,0.000049210565],"domain_scores_gemma":[0.99947315,0.00024607757,0.000031859825,0.000046046993,0.00013544952,0.00006743059],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00035561266,0.0008573601,0.00087330193,0.0004290571,0.00072667416,0.0006798413,0.001478682,0.00096824573,0.011715182],"category_scores_gemma":[0.0012004755,0.00046196926,0.000756626,0.0007153562,0.0004480693,0.0006088806,0.0007285067,0.0010798023,0.0010065022],"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":[0.00014523852,0.00010203168,0.0019908878,0.00008372758,0.00004143109,0.00015575533,0.00009851662,0.98701525,0.0017867311,0.0023696227,0.00346406,0.0027467727],"study_design_scores_gemma":[0.00009549609,0.000052630134,0.0015026926,0.000013682022,0.000010397573,0.000020074955,0.000072223374,0.99497706,0.000699325,0.00079928094,0.0017425598,0.00001459955],"about_ca_topic_score_codex":0.02139814,"about_ca_topic_score_gemma":0.017353753,"teacher_disagreement_score":0.02139814,"about_ca_system_score_codex":0.000752618,"about_ca_system_score_gemma":0.001091661,"threshold_uncertainty_score":0.042547166},"labels":[],"label_agreement":null},{"id":"W7164516150","doi":"10.4050/sm_2023_prop-1002","title":"VFS Future Advanced Rotorcraft Drive System (FARDS) Review","year":2023,"lang":"","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Presentation (obstetrics); Control system; Airframe; Propulsion; Work (physics)","score_opus":0.006597442428634635,"score_gpt":0.22410032307276215,"score_spread":0.2175028806441275,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7164516150","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":[0.00053764624,0.9796601,0.0011103939,0.0011982429,0.0028096342,0.000036594614,0.00020558234,0.00006783505,0.014373972],"genre_scores_gemma":[0.005120441,0.97331256,0.0012591688,0.0012667044,0.0012818394,0.000037013157,0.00072520797,0.000018541248,0.016978504],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9996486,0.000026550666,0.000038284288,0.000045577155,0.00020528106,0.000035667497],"domain_scores_gemma":[0.9991736,0.0001515402,0.00007700746,0.000016360098,0.00052487245,0.000056505272],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00063944614,0.0005552825,0.0005228145,0.0016891903,0.00022212623,0.0007920336,0.00073185127,0.0010318451,0.01356629],"category_scores_gemma":[0.00095341454,0.00023317832,0.00041315737,0.0012272116,0.00019510182,0.0014428474,0.00049966364,0.0007637965,0.0058724633],"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":[0.00006762912,0.000037143498,0.00015675684,0.008089935,0.000047210076,0.000077191355,0.000016835005,0.0005457997,0.002153079,0.002388184,0.12294948,0.86347073],"study_design_scores_gemma":[0.000008488731,0.00011056499,0.0004892951,0.001694634,0.000035843128,0.0002577926,0.000015291756,0.00010924435,0.00049392413,0.00038948446,0.9963846,0.000010747967],"about_ca_topic_score_codex":0.002153709,"about_ca_topic_score_gemma":0.0032754024,"teacher_disagreement_score":0.01356629,"about_ca_system_score_codex":0.0006303687,"about_ca_system_score_gemma":0.0024206948,"threshold_uncertainty_score":0.04538375},"labels":[],"label_agreement":null},{"id":"W7164576450","doi":"10.4050/sm_prop_2003-1483","title":"Advanced Rotorcraft Transmission II (ART II)","year":2003,"lang":"","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"","score_opus":0.006449216587451768,"score_gpt":0.20629916138222607,"score_spread":0.1998499447947743,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7164576450","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":[0.01953773,0.0072782347,0.048449732,0.0019004697,0.006825662,0.00072167447,0.005416191,0.0029604416,0.90691],"genre_scores_gemma":[0.14433847,0.0053011314,0.023719762,0.00077027915,0.0016979815,0.00025695798,0.0119138025,0.0006123702,0.81138927],"study_design_codex":"not_applicable","study_design_gemma":"not_applicable","domain_scores_codex":[0.9995012,0.000043086508,0.00002021717,0.000049362712,0.000304079,0.00008195813],"domain_scores_gemma":[0.99945754,0.000025508689,0.000037055437,0.00007537194,0.00032326998,0.00008132779],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00054510986,0.0007157234,0.0002541879,0.0010559633,0.0007047444,0.0012097377,0.0005163744,0.0009750387,0.06897879],"category_scores_gemma":[0.0005820512,0.00030661235,0.00024052862,0.0007882253,0.00027065355,0.0010385667,0.0007949568,0.0013393583,0.039398085],"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":[0.0004464652,0.000130267,0.0010429369,0.00046724454,0.000025724072,0.00038643758,0.00013173657,0.0020355007,0.02640721,0.015110502,0.58089584,0.3729202],"study_design_scores_gemma":[0.000049831822,0.00030362263,0.0025915913,0.000108793836,0.000013241458,0.0004599428,0.000045248373,0.001304989,0.00715003,0.0015629758,0.9863919,0.00001779425],"about_ca_topic_score_codex":0.0018582129,"about_ca_topic_score_gemma":0.0026875865,"teacher_disagreement_score":0.06897879,"about_ca_system_score_codex":0.0004581526,"about_ca_system_score_gemma":0.00082804717,"threshold_uncertainty_score":0.23075706},"labels":[],"label_agreement":null},{"id":"W7164819878","doi":"10.4050/sm_struct_2009-1784","title":"Application of Rotorcraft Damage Tolerance to Rotorcraft Drive System Components","year":2009,"lang":"","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Control system; Component (thermodynamics); Reliability (semiconductor); Field (mathematics)","score_opus":0.006940035510392714,"score_gpt":0.2151613397226254,"score_spread":0.2082213042122327,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7164819878","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":[0.6282693,0.0027185297,0.34760073,0.0003217807,0.00014110465,0.00010293061,0.00017472773,0.00086139276,0.019809434],"genre_scores_gemma":[0.98735017,0.00023961907,0.011207438,0.000015176169,0.000007772858,0.00000628176,0.000039291863,0.000016565233,0.0011177141],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.999729,0.000029565457,0.000015295484,0.000035439254,0.00016028911,0.00003051374],"domain_scores_gemma":[0.9993531,0.00012598379,0.000113045244,0.00012579914,0.00025311697,0.000028854301],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00024963563,0.00026274385,0.00017369445,0.00055877626,0.00018165316,0.0002086872,0.000256624,0.00029580508,0.00084493624],"category_scores_gemma":[0.0011600185,0.000117009906,0.00015013988,0.00027566098,0.00018807536,0.00023081331,0.0003593125,0.00021769422,0.00015524164],"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":[0.00025066378,0.00012284429,0.009366429,0.00033784134,0.000054328415,0.000407345,0.00017962664,0.111836076,0.56128633,0.003827846,0.000978356,0.31135243],"study_design_scores_gemma":[0.000025690337,0.0011411842,0.032155063,0.000069712274,0.00006994342,0.0018774071,0.00012615486,0.26224068,0.687967,0.003321026,0.010953471,0.0000526519],"about_ca_topic_score_codex":0.00052765745,"about_ca_topic_score_gemma":0.00074523216,"teacher_disagreement_score":0.00084493624,"about_ca_system_score_codex":0.00018348549,"about_ca_system_score_gemma":0.00020276239,"threshold_uncertainty_score":0.0028265715},"labels":[],"label_agreement":null},{"id":"W7164851644","doi":"10.4050/sm_struct_2021-1015","title":"Development and Demonstration of An Intelligent Fastenerless Composite Structure","year":2021,"lang":"","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Composite number; Development (topology); Process (computing); Field (mathematics)","score_opus":0.012471342241674283,"score_gpt":0.21608325439570134,"score_spread":0.20361191215402705,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7164851644","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":[0.6064891,0.00055031694,0.36351046,0.00052166596,0.0003551617,0.00042221977,0.0003138835,0.0027963393,0.025040919],"genre_scores_gemma":[0.7915236,0.00020559122,0.1962897,0.000060163577,0.000015356267,0.00011410999,0.0003041594,0.00008396133,0.011403352],"study_design_codex":"bench_or_experimental","study_design_gemma":"bench_or_experimental","domain_scores_codex":[0.99966586,0.000018254117,0.0000102624,0.000030810508,0.00024319286,0.00003161919],"domain_scores_gemma":[0.99970716,0.000027972827,0.000035494963,0.00003884465,0.00011555404,0.00007488816],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00047819814,0.00032849656,0.00019288645,0.00037467203,0.00035565978,0.00028406992,0.00075918384,0.00094022823,0.0016059199],"category_scores_gemma":[0.00035510058,0.00016523394,0.00025781165,0.00011421405,0.0002621943,0.00045153763,0.00047804153,0.00059312925,0.00052968645],"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":[0.000093461786,0.00011503004,0.00039471372,0.00009499754,0.0000090985195,0.00040137945,0.000098431985,0.0063213245,0.9681211,0.00200704,0.0006373878,0.021705985],"study_design_scores_gemma":[0.00011936655,0.0018245464,0.00358924,0.000021700402,0.00003171332,0.0010283988,0.00004772643,0.047033623,0.9263551,0.0006285429,0.019281672,0.000038292546],"about_ca_topic_score_codex":0.00043300158,"about_ca_topic_score_gemma":0.0004939992,"teacher_disagreement_score":0.0016059199,"about_ca_system_score_codex":0.00017582938,"about_ca_system_score_gemma":0.00043989893,"threshold_uncertainty_score":0.0053723454},"labels":[],"label_agreement":null},{"id":"W7164860609","doi":"10.4050/sm_struct_2001-4447","title":"Technology For Rotorcraft Integrated Analysis And Design (TRIAD)","year":2001,"lang":"","type":"article","venue":"","topic":"Aeroelasticity and Vibration Control","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":"Process (computing); Process design; Design process; Integrated design; System integration; Design technology; Engineering design process","score_opus":0.016283790026128692,"score_gpt":0.23325795100464666,"score_spread":0.21697416097851796,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W7164860609","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":[0.0023267108,0.002265073,0.93698895,0.0006519476,0.00050328637,0.00020520946,0.0005727069,0.01163202,0.044854145],"genre_scores_gemma":[0.03830601,0.002538248,0.9238042,0.00032796987,0.00015615822,0.0006373707,0.0020498843,0.0016807549,0.030499408],"study_design_codex":"design_other","study_design_gemma":"not_applicable","domain_scores_codex":[0.9967945,0.00048260103,0.00015016377,0.0002484505,0.0021531456,0.00017109037],"domain_scores_gemma":[0.99797875,0.00036135322,0.00019259044,0.00054532196,0.00077480165,0.00014718226],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.0028850494,0.0010868857,0.00081442954,0.0020147131,0.0006199592,0.0027327635,0.00108292,0.0011256175,0.019780915],"category_scores_gemma":[0.0033171582,0.0008294339,0.0010619067,0.001134585,0.0006581076,0.0017462956,0.0022345209,0.0018156447,0.010534339],"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":[0.00021263871,0.000106697364,0.0011576551,0.00064576877,0.000113023474,0.00017866505,0.00040459287,0.02468286,0.03711,0.12417961,0.10678834,0.7044201],"study_design_scores_gemma":[0.00014833608,0.00029160528,0.0006703343,0.00023160811,0.00006653896,0.00046921446,0.000062793035,0.0650986,0.024491008,0.037256286,0.87114364,0.000070013695],"about_ca_topic_score_codex":0.0008616651,"about_ca_topic_score_gemma":0.0011488124,"teacher_disagreement_score":0.019780915,"about_ca_system_score_codex":0.00079636974,"about_ca_system_score_gemma":0.0023234887,"threshold_uncertainty_score":0.06617373},"labels":[],"label_agreement":null}]}