{"meta":{"query_hash":"3f121e49a020","filters":{"venue":"9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization"},"cohort_total":6,"direct_labels_cover":0,"predictions_cover":6,"exported":6,"export_cap":100000,"truncated":false,"label_status":"direct model label, unvalidated","prediction_status":"machine_predicted_unvalidated (Codex and Gemma teacher distillation)","score_status":"score_only:v0-immature-baseline","snapshot":{"source":"OpenAlex, pinned release, all 482 partitions","release":"2026-06-24","frame_built":"2026-07-12"},"permalink":"https://metacan.xera.ac/q/3f121e49a020","api":"https://metacan.xera.ac/api/v1/cohort?venue=9th+AIAA%2FISSMO+Symposium+on+Multidisciplinary+Analysis+and+Optimization"},"results":[{"id":"W2085910326","doi":"10.2514/6.2002-5656","title":"A Preliminary Study of Wing Aerodynamic, Structural and Aeroelastic Design and Optimization","year":2002,"lang":"en","type":"article","venue":"9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization","topic":"Computational Fluid Dynamics and Aerodynamics","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":"Aeroelasticity; Aerodynamics; Wing; Computer science; Finite element method; Computational fluid dynamics; Aerospace engineering; Design methods; Wing configuration; Engineering; Structural engineering; Mechanical engineering","score_opus":0.008587318536714154,"score_gpt":0.21713448939967844,"score_spread":0.2085471708629643,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2085910326","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.5176229,0.000181942,0.4816792,0.000036098714,0.00006301923,0.00032566517,0.000011620029,0.00005782222,0.000021769925],"genre_scores_gemma":[0.93237394,0.000558845,0.0668185,0.000005431647,0.000024043253,0.000021633898,0.000115232244,0.00004070098,0.000041685173],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9983657,0.00011700517,0.0005366912,0.00049711723,0.0002551353,0.00022837557],"domain_scores_gemma":[0.99916244,0.00023725604,0.0001377863,0.00022607837,0.00010557117,0.00013087953],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00018630867,0.00033640422,0.00046657442,0.0005433357,0.000313668,0.00010710594,0.00009495073,0.000109628214,0.000025271896],"category_scores_gemma":[0.000018861972,0.0003293217,0.00006793521,0.0007449655,0.000073561285,0.0003163282,0.0001089669,0.00014956483,4.5247054e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00007053706,0.00013430261,0.0071936115,0.00006631254,0.00035290638,0.000005595179,0.001394487,0.9900198,0.0001666304,0.00005364149,0.0000023233663,0.00053987134],"study_design_scores_gemma":[0.0008738747,0.000673471,0.026886065,0.000041011044,0.00074978883,0.000007614822,0.00032017333,0.97010523,0.0000063900393,0.00002115841,1.7750469e-7,0.00031505237],"about_ca_topic_score_codex":0.000014799909,"about_ca_topic_score_gemma":0.0000183172,"teacher_disagreement_score":0.4148607,"about_ca_system_score_codex":0.000050514238,"about_ca_system_score_gemma":0.0000058190944,"threshold_uncertainty_score":0.9999159},"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":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.02383179,0.00013614283,0.97418183,0.00041629528,0.000108738095,0.0003187072,0.000017760793,0.0003225542,0.00066617853],"genre_scores_gemma":[0.9398882,0.00026451092,0.05914103,0.00003099653,0.00010041167,0.000058266134,0.00013957768,0.000052096817,0.00032493158],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99851155,0.00007739274,0.00040591756,0.00043808675,0.00025388517,0.00031318655],"domain_scores_gemma":[0.99916726,0.00016619713,0.00009757543,0.00030093844,0.00010673385,0.00016127157],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00016206143,0.00036324415,0.0004390075,0.00044654726,0.00043648007,0.00017528146,0.00013963284,0.00013801873,0.0002744409],"category_scores_gemma":[0.000017772893,0.00028315157,0.000118132964,0.0013167682,0.000080760285,0.00049709575,0.00003823933,0.00020957993,0.000019458681],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00008410719,0.00008938839,0.0044219047,0.000023877106,0.00046737993,0.000007616476,0.000454874,0.9930666,0.0005233778,0.00007390935,0.00006439721,0.00072254695],"study_design_scores_gemma":[0.00071556994,0.000245272,0.0025397204,0.000055369434,0.00074781454,0.0000027621184,0.00012975396,0.99468786,0.000457947,0.000016961661,0.000024279425,0.000376678],"about_ca_topic_score_codex":0.000008582423,"about_ca_topic_score_gemma":0.000077809666,"teacher_disagreement_score":0.9160564,"about_ca_system_score_codex":0.000054028533,"about_ca_system_score_gemma":0.000009284713,"threshold_uncertainty_score":0.9999621},"labels":[],"label_agreement":null},{"id":"W2317622940","doi":"10.2514/6.2002-5624","title":"Designing and Optimizing Missiles in an Interactive Environment","year":2002,"lang":"en","type":"article","venue":"9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization","topic":"Aerospace and Aviation Technology","field":"Engineering","cited_by":2,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Lockheed Martin (Canada)","funders":"","keywords":"Computer science; Human–computer interaction","score_opus":0.009532920055399938,"score_gpt":0.2188528044326598,"score_spread":0.20931988437725987,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2317622940","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.42836705,0.00043806486,0.56977797,0.00042815175,0.00006193498,0.00026175048,0.000009179382,0.0002282602,0.00042766996],"genre_scores_gemma":[0.94163513,0.0019945502,0.056116074,0.000017740702,0.000021236847,0.000030172398,0.00005584097,0.000027184486,0.00010204801],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9989241,0.0000592526,0.0002929851,0.0003894121,0.000112506,0.00022178575],"domain_scores_gemma":[0.9995429,0.00005763127,0.000076754586,0.00020774371,0.000015967877,0.00009902951],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.000112302114,0.0002251356,0.0003025154,0.00053531973,0.00016548297,0.00007118309,0.00008028137,0.00014268013,0.00011481022],"category_scores_gemma":[0.000006351752,0.00022586732,0.00005248925,0.0004291962,0.000056455672,0.00044600354,0.00005328101,0.00018470516,0.000005444442],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000014607172,0.00008273949,0.013592652,0.000014170072,0.00008941902,0.000006958344,0.0016700154,0.97959894,0.0033464755,0.000020815552,0.0000073964106,0.001555836],"study_design_scores_gemma":[0.00039815012,0.00013846264,0.004234208,0.00003172282,0.00015720066,0.0000017770952,0.00087004085,0.9902662,0.0036235934,0.000014326552,0.000011055364,0.0002532636],"about_ca_topic_score_codex":0.00000727311,"about_ca_topic_score_gemma":0.000014652429,"teacher_disagreement_score":0.51366186,"about_ca_system_score_codex":0.000070332564,"about_ca_system_score_gemma":0.0000018742059,"threshold_uncertainty_score":0.9210602},"labels":[],"label_agreement":null},{"id":"W2319273161","doi":"10.2514/6.2002-5595","title":"Optimization Using Variable Fidelity Solvers: Exploration of an Approximation Management Framework for Aerodynamic Shape Optimization","year":2002,"lang":"en","type":"article","venue":"9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization","topic":"Advanced Numerical Analysis Techniques","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":"Polytechnique Montréal","funders":"","keywords":"Aerodynamics; Computer science; Variable (mathematics); Fidelity; High fidelity; Mathematical optimization; Aerospace engineering; Engineering; Mathematics","score_opus":0.021654708117916276,"score_gpt":0.27321464887377367,"score_spread":0.2515599407558574,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2319273161","genre_codex":"methods","genre_gemma":"methods","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0044063283,0.00007200284,0.9938673,0.00006261439,0.00009550573,0.0008846232,0.000048227244,0.0003707785,0.00019264557],"genre_scores_gemma":[0.17209588,0.0008378895,0.8255935,0.000016395,0.00005112307,0.0001438074,0.0011665539,0.00006515623,0.000029736946],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9975246,0.00012236561,0.00094072137,0.0006972405,0.00037586264,0.00033918084],"domain_scores_gemma":[0.9984633,0.00011590197,0.0004307034,0.00055416743,0.00029665817,0.00013932207],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00037158272,0.00041891352,0.0006286926,0.0008807728,0.00037938802,0.000118371,0.00020294207,0.000269885,0.00020399694],"category_scores_gemma":[0.000043703552,0.0004408492,0.0002132861,0.0022791915,0.00006945893,0.0019340435,0.00006808761,0.00015912173,9.555879e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00007046466,0.00027662853,0.00010944308,0.00019299645,0.00042220068,7.212736e-7,0.00029966352,0.99601245,0.00031182411,0.0007386697,0.000004882503,0.0015600533],"study_design_scores_gemma":[0.00045290546,0.00019379337,0.00004603585,0.000098261604,0.0013956152,6.250756e-7,0.00022369772,0.9959587,0.0004990072,0.0006804005,0.000004178562,0.00044677072],"about_ca_topic_score_codex":0.000010708597,"about_ca_topic_score_gemma":0.000003477695,"teacher_disagreement_score":0.16827382,"about_ca_system_score_codex":0.00020737147,"about_ca_system_score_gemma":0.0000066908274,"threshold_uncertainty_score":0.9998043},"labels":[],"label_agreement":null},{"id":"W2320453204","doi":"10.2514/6.2002-5400","title":"Constraints Specifications on NURBS Surfaces for Wing Geometric Representation","year":2002,"lang":"en","type":"article","venue":"9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization","topic":"Manufacturing Process and Optimization","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":"Polytechnique Montréal","funders":"","keywords":"Representation (politics); Wing; Computer science; Computational geometry; Computer graphics (images); Geometric modeling; Engineering drawing; Artificial intelligence; Geometry; Mathematics; Engineering; Structural engineering","score_opus":0.03235669986547847,"score_gpt":0.2550808575944513,"score_spread":0.22272415772897286,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2320453204","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.04543514,0.00022882843,0.9479689,0.0004960275,0.00031567243,0.00070802734,0.00009136124,0.0003433922,0.0044126287],"genre_scores_gemma":[0.9668288,0.001739743,0.029802782,0.000027027623,0.000103168066,0.00010221858,0.00058785453,0.00005146265,0.00075692596],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99832785,0.000048546113,0.00049484737,0.00056043646,0.00026721624,0.00030108314],"domain_scores_gemma":[0.9989671,0.00024684242,0.00016025617,0.00035989485,0.0001319674,0.00013390144],"candidate_categories":["metaepi_narrow"],"consensus_categories":[],"category_scores_codex":[0.00019974791,0.00030619424,0.00037174835,0.0010592203,0.00048419723,0.00018567644,0.00013980568,0.00014745077,0.00041808607],"category_scores_gemma":[0.000051860177,0.00030111056,0.00017197392,0.0016417208,0.00007274221,0.00035178728,0.000025243527,0.00013917808,0.000015634983],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000029062849,0.000121526486,0.001863375,0.00007159427,0.00023164896,0.0000011259757,0.000396249,0.99407077,0.00014993483,0.00014817104,0.00019734002,0.002719219],"study_design_scores_gemma":[0.00057570246,0.00012465134,0.0063795294,0.0000419203,0.0003946396,0.0000010051984,0.00015053696,0.98933274,0.002529989,0.000022848011,0.00010607058,0.0003403995],"about_ca_topic_score_codex":0.0000065848008,"about_ca_topic_score_gemma":0.000006366242,"teacher_disagreement_score":0.9213937,"about_ca_system_score_codex":0.00008081557,"about_ca_system_score_gemma":0.000005679998,"threshold_uncertainty_score":0.9999441},"labels":[],"label_agreement":null},{"id":"W2323402416","doi":"10.2514/6.2002-5464","title":"Effective Multi-Mission Aircraft Conceptual Design Optimization Using a Hybrid Multi-Objective Evolutionary Method","year":2002,"lang":"en","type":"article","venue":"9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization","topic":"Advanced Multi-Objective Optimization Algorithms","field":"Computer Science","cited_by":9,"is_retracted":false,"has_abstract":false,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Toronto Metropolitan University","funders":"","keywords":"Conceptual design; Computer science; Evolutionary algorithm; Evolutionary computation; Multi-objective optimization; Systems engineering; Engineering; Artificial intelligence; Human–computer interaction; Machine learning","score_opus":0.03141683009952633,"score_gpt":0.3019477032560249,"score_spread":0.27053087315649854,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2323402416","genre_codex":"methods","genre_gemma":"methods","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"methods","genre_consensus":"methods","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.0003000136,0.00041841884,0.99577713,0.00029283523,0.00044348065,0.0020757355,0.000067202425,0.00053209707,0.00009309166],"genre_scores_gemma":[0.03681435,0.00047591448,0.9613757,0.00013346504,0.0001114646,0.0001657906,0.00022559005,0.00010394954,0.0005937325],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9929239,0.0017972735,0.0011245562,0.002430148,0.0008480746,0.0008760568],"domain_scores_gemma":[0.9955597,0.0008658519,0.0009190891,0.001098739,0.001015256,0.00054136425],"candidate_categories":["metaepi_narrow","sts"],"consensus_categories":[],"category_scores_codex":[0.00089981296,0.000996781,0.0011230654,0.0017853706,0.0017552585,0.0003420613,0.0007512726,0.00036554376,0.00016811964],"category_scores_gemma":[0.00032670095,0.00097585545,0.00047964594,0.003980775,0.00034973264,0.002605198,0.000617196,0.00055906165,0.000024247465],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00012936897,0.0010842262,0.0009217304,0.000021744485,0.00057418254,0.00004430668,0.0023656262,0.9920941,0.0005773096,0.0001270766,0.000026153406,0.0020341945],"study_design_scores_gemma":[0.003414129,0.0005259104,0.0010350675,0.00009637609,0.00072071794,0.000048492315,0.00035758398,0.99085903,0.0017886182,0.0000270869,0.000013078516,0.0011139336],"about_ca_topic_score_codex":0.00005418061,"about_ca_topic_score_gemma":0.000004134924,"teacher_disagreement_score":0.036514338,"about_ca_system_score_codex":0.00073131593,"about_ca_system_score_gemma":0.000101496575,"threshold_uncertainty_score":0.9995443},"labels":[],"label_agreement":null}]}