{"created":"2023-06-20T15:11:43.292743+00:00","id":41435,"links":{},"metadata":{"_buckets":{"deposit":"12b43da1-43cc-43a4-853e-99bce3a15e0e"},"_deposit":{"created_by":1,"id":"41435","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41435"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041435","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["490020"],"item_3_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"協調的最適化法を用いた超音速民間輸送機の設計"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2000-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"160","bibliographicPageStart":"153","bibliographicVolumeNumber":"49T","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_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":"航空宇宙技術研究所 17-19 Jan. 2000 東京 日本","subitem_description_type":"Other"}]},"item_3_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":"National Aerospace Laboratory 17-19 Jan. 2000 Tokyo Japan","subitem_description_type":"Other"}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"協調的最適化法すなわち分散設計のための戦略を2種の超音速民間機概念の最適化へ応用したことについて述べた。この設計手法では、作業を特定分野のサブ問題に分解し、最適システムを達成するよう調整する。高信頼度モデリングの必要な大規模問題に対して、過去数年間にStanford大、NASAおよびボーイング社の研究者が開発し方法の適用を進めている。本報はこれらの応用のひとつである超音速輸送機の初期設計について述べ、従来設計および新しい自然層流翼概念についての初期成果を示した。この考え方のフィージビリティーを示したいくつかの初期飛行試験結果で、層流設計概念の概要を補足した。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This paper describes the application of collaborative optimization, a strategy for distributed design, to the optimization of two supersonic civil aircraft concepts. This design approach permits tasks to be decomposed into domain-specific subproblems, and coordinated to achieve an optimal system. Developed over the past few years by researchers at Stanford, NASA, and Boeing, the methodology is now being applied to large-scale problems requiring high-fidelity modeling. The paper describes one of these applications, the preliminary design of supersonic transports, and provides preliminary results for both a conventional design and a novel natural laminar flow concept. A summary of the laminar flow design concept is complemented by some initial flight test results demonstrating the feasibility of the idea.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0028638019","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL SP-49T","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0289-260X","subitem_source_identifier_type":"ISSN"}]},"item_3_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN10097345","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"Stanford University"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Stanford University"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"Kroo, Ilan","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"490020","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":"nalsp0049019.pdf","filesize":[{"value":"3.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0049019.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41435/files/nalsp0049019.pdf"},"version_id":"452c6016-23aa-4bd3-8b4a-4745cec2a347"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"協調的最適化法","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速民間輸送機","subitem_subject_scheme":"Other"},{"subitem_subject":"サブ問題","subitem_subject_scheme":"Other"},{"subitem_subject":"空気力学","subitem_subject_scheme":"Other"},{"subitem_subject":"構造解析","subitem_subject_scheme":"Other"},{"subitem_subject":"ミッション解析","subitem_subject_scheme":"Other"},{"subitem_subject":"最適システム","subitem_subject_scheme":"Other"},{"subitem_subject":"高信頼度モデリング","subitem_subject_scheme":"Other"},{"subitem_subject":"層流デザイン","subitem_subject_scheme":"Other"},{"subitem_subject":"collaborative optimization","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic civil transport","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"subproblem","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"structure analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"mission analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"optimal system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high fidelity modeling","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"laminar flow design","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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"Supersonic civil transport design using collaborative optimization","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Supersonic civil transport design using collaborative optimization","subitem_title_language":"en"}]},"item_type_id":"3","owner":"1","path":["1893","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"41435","relation_version_is_last":true,"title":["Supersonic civil transport design using collaborative optimization"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:00:17.649363+00:00"}