{"created":"2023-06-20T14:39:04.940437+00:00","id":5754,"links":{},"metadata":{"_buckets":{"deposit":"5c975965-5599-4ef3-83f6-bd05441ce3a9"},"_deposit":{"created_by":1,"id":"5754","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"5754"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00005754","sets":["1887:1891","9:789:998:1005"]},"author_link":["476909"],"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2007-03-30","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"216","bibliographicPageStart":"204","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":"The paper describes some aspects of the development and application within UK and mainland Europe of the aerodynamic technology required for successful design by industry of the next generation of supersonic transport aircraft. The focus is on wing design, but the methods covered are equally applicable to the design of other components and their interaction. Three areas are covered. Firstly a design method for aerodynamic shapes, developed at DERA (Defense Evaluation and Research Agency) UK, is summarized and two applications are described: an investigation of dual-point transonic/supersonic aerofoil design using an Euler CFD (Computational Fluid Dynamics) code, and the dual-point design of a delta-wing/body combination using a multi-block Euler CFD code. Secondly the initial application of the wing shape optimization method to the dual-point design of a supersonic transport wing is summarized. Finally results from a European research project on the reduction of drag and the assessment of aerodynamic design methods are presented. Two linked wing-design tasks were completed: dual-point transonic/supersonic cruise design and low-speed high-lift design. Three wing configurations were tested at low-speed, transonically and supersonically. Figures showing a selection of the measured forces and pressures indicate the effectiveness of the aerodynamic design.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063609023","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":"Defence Evaluation and Research Agency Applied Aerodynamics"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Defence Evaluation and Research Agency Applied Aerodynamics"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"Lovell, D. A.","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"476909","nameIdentifierScheme":"WEKO"}]}]},"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":"63609023.pdf","filesize":[{"value":"6.3 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"63609023.pdf","url":"https://jaxa.repo.nii.ac.jp/record/5754/files/63609023.pdf"},"version_id":"868146b5-6099-433d-a153-b21b780213a4"}]},"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":"民間航空","subitem_subject_scheme":"Other"},{"subitem_subject":"計算流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"旅客機","subitem_subject_scheme":"Other"},{"subitem_subject":"翼型設計","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":"揚抗比","subitem_subject_scheme":"Other"},{"subitem_subject":"翼型","subitem_subject_scheme":"Other"},{"subitem_subject":"抗力低減","subitem_subject_scheme":"Other"},{"subitem_subject":"ヨーロッパ","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":"civil aviation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"passenger aircraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wing design","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":"lift drag ratio","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"airfoil","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"drag reduction","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Europe","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":"Progress in aerodynamic technology to support a second-generation supersonic transport","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Progress in aerodynamic technology to support a second-generation supersonic transport","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":"5754","relation_version_is_last":true,"title":["Progress in aerodynamic technology to support a second-generation supersonic transport"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:34:21.473726+00:00"}