{"created":"2023-06-20T15:07:46.662055+00:00","id":37140,"links":{},"metadata":{"_buckets":{"deposit":"4a623b7e-48ce-4379-8eee-b72b1855a6c7"},"_deposit":{"created_by":1,"id":"37140","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37140"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037140","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["479097","479101","479105","479104","479100","479098","479096","479102","479099","479103"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"超音速輸送機翼の逆設計法"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1998-02","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"92","bibliographicPageStart":"87","bibliographicVolumeNumber":"37","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_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":"航空宇宙技術研究所 12-13 Jun. 1997 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":"National Aerospace Laboratory 12-13 Jun. 1997 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"SST(超音速輸送機)の逆設計法を開発した。本手法では高梨の亜音速逆問題で用いる残差修正の概念を用いる。LSP(小動揺線形化)方程式の積分微分形式を解くことにより、与えられた翼の計算圧力分布と規定目標圧力分布との差を反復減少する。オイラー/ナビエ・ストークス方程式により、圧力分布を計算した。数値結果はSST設計に本手法を用いることが出来ることを示した。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The inverse design method for Supersonic Transport (SST) is developed. This method utilizes Takanishi's residual-correction concept, which is used in the transonic inverse problem. The difference between the computed pressure distribution of given wing and the prescribed target pressure distribution is iteratively reduced by solving the integrodifferential form of Linearized Small Perturbation (LSP) equation. The pressure distribution is computed by Euler/Navier-Stokes equation. The numerical results show the possibility of using this method to the design of SST.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001433014","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: NAL SP-37","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0289-260X","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":"AN10097345","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"東北大学 大学院"},{"subitem_text_value":"東北大学 工学部"},{"subitem_text_value":"東北大学 工学部"},{"subitem_text_value":"富士通 HPCシステム部"},{"subitem_text_value":"航空宇宙技術研究所 数理解析部　応用解析研究室"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Tohoku University Graduate School"},{"subitem_text_language":"en","subitem_text_value":"Tohoku University Faculty of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Tohoku University Faculty of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Fujitsu Ltd Supercomputer Systems Engineering Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Applied Mathematics Laboratory, Computational Science Division"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"Jeong, Shinkyu"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"大林, 茂"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中橋, 和博"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"松島, 紀佐"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"岩宮, 敏幸"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Jeong, Shinkyu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Obayashi, Shigeru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakahashi, Kazuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsushima, Kisa","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Iwamiya, Toshiyuki","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":"nalsp0037014.pdf","filesize":[{"value":"349.9 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0037014.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37140/files/nalsp0037014.pdf"},"version_id":"7875c235-cdcd-421b-8937-708a72d82b24"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"SST","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速輸送機","subitem_subject_scheme":"Other"},{"subitem_subject":"逆設計法","subitem_subject_scheme":"Other"},{"subitem_subject":"主翼設計","subitem_subject_scheme":"Other"},{"subitem_subject":"残差修正","subitem_subject_scheme":"Other"},{"subitem_subject":"小動揺線形化方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"LSP方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"線形化方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"積分微分形式","subitem_subject_scheme":"Other"},{"subitem_subject":"圧力分布","subitem_subject_scheme":"Other"},{"subitem_subject":"反復減少処理","subitem_subject_scheme":"Other"},{"subitem_subject":"オイラー方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ・ストークス方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"設計ツール","subitem_subject_scheme":"Other"},{"subitem_subject":"SST","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic transport","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"inverse design method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"main wing design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"residual correction","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"linearized small perturbation equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"LSP equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"linearized equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"integrodifferential form","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pressure distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"iterative reduction treatment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Euler equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"design tool","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":"Inverse design method for wing of supersonic transport","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Inverse design method for wing of supersonic transport","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1891","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"37140","relation_version_is_last":true,"title":["Inverse design method for wing of supersonic transport"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:25:05.137436+00:00"}