{"created":"2023-06-20T14:39:05.448341+00:00","id":5764,"links":{},"metadata":{"_buckets":{"deposit":"cf986362-8bc6-45c1-a6e0-27f391ecb129"},"_deposit":{"created_by":1,"id":"5764","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"5764"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00005764","sets":["1887:1891","9:789:998:1005"]},"author_link":["476949","476945","476948","476947","476950","476946"],"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2007-03-30","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"303","bibliographicPageStart":"292","bibliographicVolumeNumber":"JAXA-SP-06-029E","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料"},{"bibliographic_title":"JAXA Special Publication: Proceedings of International Workshops on Numerical Simulation Technology for Design of Next Generation Supersonic Civil Transport (SST-CFD Workshop)","bibliographic_titleLang":"en"}]}]},"item_5_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"SST-CFDワークショップ.次世代超音速機の数値シミュレーション利用技術に関する国際ワークショップ 航空宇宙技術研究所 20000117-20000119 東京 日本","subitem_description_type":"Other"}]},"item_5_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"SST-CFD Workshop. International Workshops on Numerical Simulation Technology for Design of Next Generation Supersonic Civil Transport National Aerospace Laboratory 20000117-20000119 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"preliminary SST (SuperSonic Transport) wing planform design program was developed using the simplex downhill method for numerical optimization and lifting surface, theory for aerodynamic analysis. The wing planform was restricted to an arrow wing with a constant planform area, and the geometry was represented by at most seven independent design variables. The objective function of the optimization was the inviscid drag at design condition (M = 2, C(sub L) = 0.1) with penalty functions for the violation of geometry constraints. Because the program only performs aerodynamic analysis, variables were bound or held constant based on multidisciplinary considerations such as structural and manufacturing restrictions, in order to avoid unrealistic planforms. The results showed the design variables could be grouped into a set of primary variables (aspect ratio, slenderness ratio, sweep angle of inner leading edge) which played key roles to the optimization, and a set of secondary variables, primarily used to satisfy the geometry constraints. Finally, as a preparation for the multi-point design, the optimization was performed at several design Mach numbers and corresponding design lift coefficients while keeping the flight altitude and the weight of the aircraft the same. The resulting optimum geometry changed to the trade off the induced drag from the high aspect ratio with the wave drag from the high leading edge sweep.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063609033","subitem_description_type":"Other"}]},"item_5_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: JAXA-SP-06-029E","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-113X","subitem_source_identifier_type":"ISSN"}]},"item_5_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA11984031","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"Purdue University School of Aeronautics and Astronautics"},{"subitem_text_value":"Purdue University School of Aeronautics and Astronautics"},{"subitem_text_value":"航空宇宙技術研究所 次世代航空機プロジェクト推進センター"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Purdue University School of Aeronautics and Astronautics"},{"subitem_text_language":"en","subitem_text_value":"Purdue University School of Aeronautics and Astronautics"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Advanced Technology Aircraft Project Center"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"Matsumura, Shin"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sullivan, John P."}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"真保, 雄一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsumura, Shin","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sullivan, John P.","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shinbo, Yuichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-02-10"}],"displaytype":"detail","filename":"63609033.pdf","filesize":[{"value":"4.5 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"63609033.pdf","url":"https://jaxa.repo.nii.ac.jp/record/5764/files/63609033.pdf"},"version_id":"b0c6f717-e5ac-4da3-8637-de7044d8a60a"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"超音速機","subitem_subject_scheme":"Other"},{"subitem_subject":"航空機設計","subitem_subject_scheme":"Other"},{"subitem_subject":"旅客機","subitem_subject_scheme":"Other"},{"subitem_subject":"計算流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"空力解析","subitem_subject_scheme":"Other"},{"subitem_subject":"設計最適化","subitem_subject_scheme":"Other"},{"subitem_subject":"翼平面形","subitem_subject_scheme":"Other"},{"subitem_subject":"空力特性","subitem_subject_scheme":"Other"},{"subitem_subject":"空力抵抗","subitem_subject_scheme":"Other"},{"subitem_subject":"揚抗比","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic aircraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aircraft design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"passenger aircraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"design optimization","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wing planform","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic drag","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"lift drag ratio","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":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"Development of a preliminary SST planform design tool using a numerical optimization routine","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Development of a preliminary SST planform design tool using a numerical optimization routine","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1005","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"5764","relation_version_is_last":true,"title":["Development of a preliminary SST planform design tool using a numerical optimization routine"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:34:10.751322+00:00"}