{"created":"2023-06-20T14:54:23.732605+00:00","id":22740,"links":{},"metadata":{"_buckets":{"deposit":"8aa613d9-6e06-4a7f-b0e9-2e85d218553f"},"_deposit":{"created_by":1,"id":"22740","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"22740"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00022740","sets":["1887:1888"]},"author_link":["213361","213366","213362","213368","213363","213364","213367","213365"],"item_7_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2016-01-29","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"1","bibliographicPageEnd":"48","bibliographicPageStart":"38","bibliographicVolumeNumber":"4","bibliographic_titles":[{},{"bibliographic_title":"Journal of Flow Control, Measurement & Visualization","bibliographic_titleLang":"en"}]}]},"item_7_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In this study, the wing design problem for different planforms for supersonic transport (SST) under supersonic and transonic cruise conditions is discussed to obtain knowledge of the supersonic air-foil from the viewpoint of wing planform dependency. Two types of planforms were considered-a cranked arrow wing with a high sweep-back angle and a tapered wing with a low sweep- back angle. The optimum airfoils of these planforms were designed by efficient global optimization, which combined the evolutionary algorithm with the Kriging surrogate model. To acquire design knowledge, the functional analysis of variance was applied to the solution space and the design space. The design results show that the optimum airfoil and the contribution ratios of design variables for the airfoils of the two planform are different.","subitem_description_type":"Other"}]},"item_7_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: カラー図版あり","subitem_description_type":"Other"}]},"item_7_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains color illustrations","subitem_description_type":"Other"}]},"item_7_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: PA1620055000","subitem_description_type":"Other"}]},"item_7_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Scientific Research Publishing"}]},"item_7_relation_25":{"attribute_name":"DOI","attribute_value_mlt":[{"subitem_relation_name":[{"subitem_relation_name_text":"info:doi/10.4236/jfcmv.2016.41004"}],"subitem_relation_type_id":{"subitem_relation_type_id_text":"http://dx.doi.org/10.4236/jfcmv.2016.41004","subitem_relation_type_select":"DOI"}}]},"item_7_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"2329-3322","subitem_source_identifier_type":"ISSN"}]},"item_7_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"首都大学東京"},{"subitem_text_value":"首都大学東京"},{"subitem_text_value":"宇宙航空研究開発機構航空技術部門 (JAXA)"},{"subitem_text_value":"富山大学"}]},"item_7_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Tokyo Metropolitan University"},{"subitem_text_language":"en","subitem_text_value":"Tokyo Metropolitan University"},{"subitem_text_language":"en","subitem_text_value":"Aeronautical Technology Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"University of Toyama"}]},"item_access_right":{"attribute_name":"アクセス権","attribute_value_mlt":[{"subitem_access_right":"metadata only access","subitem_access_right_uri":"http://purl.org/coar/access_right/c_14cb"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"岸, 祐希"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"金崎, 雅博"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"牧野, 好和"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"松島, 紀佐"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kishi, Yuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kanazaki, Masahiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Makino, Yoshikazu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsushima, Kisa","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Supersonic Wing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Multi-Point Design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Airfoil Design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Knowledge Discovery","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"journal article","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"Planform Dependency on Airfoil Design Results for Supersonic Wing in Supersonic and Transonic","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Planform Dependency on Airfoil Design Results for Supersonic Wing in Supersonic and Transonic","subitem_title_language":"en"}]},"item_type_id":"7","owner":"1","path":["1888"],"pubdate":{"attribute_name":"公開日","attribute_value":"2016-05-31"},"publish_date":"2016-05-31","publish_status":"0","recid":"22740","relation_version_is_last":true,"title":["Planform Dependency on Airfoil Design Results for Supersonic Wing in Supersonic and Transonic"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T03:16:08.823084+00:00"}