{"created":"2023-06-20T15:08:46.436007+00:00","id":38259,"links":{},"metadata":{"_buckets":{"deposit":"209bb06b-e152-41fa-8aee-2513a9426e0a"},"_deposit":{"created_by":1,"id":"38259","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"38259"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00038259","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["432523","432524","432526","432525"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Shape optimization of supersonic business jet for low boom and low drag design"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2003-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"219","bibliographicPageStart":"214","bibliographicVolumeNumber":"57","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料: 航空宇宙数値シミュレーション技術シンポジウム2002論文集"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory: Proceedings of Aerospace Numerical Simulation Symposium 2002","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Reduction of sonic boom intensity and improvement of lift to drag ratio are important in aerodynamic design of the future supersonic transport. They are inevitable matter especially for supersonic business jet (SSBJ), for which it will be required to cruise over land with low sonic boom. Therefore its shape must be optimized to reduce its sonic boom intensity and improve its lift to drag ratio. An shape optimization of SSBJ is conducted by using CFD and the waveform parameter method for analyses, and genetic algorithm for optimization.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0045948038","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-57","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":"三菱重工業"},{"subitem_text_value":"三菱重工業"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industries Ltd."},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industries Ltd."}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"吉本, 稔"}],"nameIdentifiers":[{"nameIdentifier":"432523","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"内山, 直樹"}],"nameIdentifiers":[{"nameIdentifier":"432524","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Yoshimoto, Minoru","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"432525","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Uchiyama, Naoki","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"432526","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":"2020-01-24"}],"displaytype":"detail","filename":"nalsp0057038.pdf","filesize":[{"value":"679.7 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0057038.pdf","url":"https://jaxa.repo.nii.ac.jp/record/38259/files/nalsp0057038.pdf"},"version_id":"8dfb02bf-7bec-4f76-9829-96fdcb84330a"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"SSBJ","subitem_subject_scheme":"Other"},{"subitem_subject":"低ソニックブーム","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","subitem_subject_scheme":"Other"},{"subitem_subject":"最適化","subitem_subject_scheme":"Other"},{"subitem_subject":"SST","subitem_subject_scheme":"Other"},{"subitem_subject":"遺伝的アルゴリズム","subitem_subject_scheme":"Other"},{"subitem_subject":"Reynolds平均化","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier-Stokes方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"低抗力","subitem_subject_scheme":"Other"},{"subitem_subject":"研究開発","subitem_subject_scheme":"Other"},{"subitem_subject":"波形パラメータ法","subitem_subject_scheme":"Other"},{"subitem_subject":"Euler解析","subitem_subject_scheme":"Other"},{"subitem_subject":"カナード配置","subitem_subject_scheme":"Other"},{"subitem_subject":"SSBJ","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"low sonic boom","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"optimization","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"SST","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"genetic algorithm","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Reynolds averaging","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier-Stokes equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"low drag","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"research and development","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"waveform parameter method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Euler solver","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"canard configuration","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"jpn"}]},"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":"低ブーム低抵抗超音速ビジネスジェット機の形状最適設計","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"低ブーム低抵抗超音速ビジネスジェット機の形状最適設計"}]},"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":"38259","relation_version_is_last":true,"title":["低ブーム低抵抗超音速ビジネスジェット機の形状最適設計"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:42:43.503701+00:00"}