{"created":"2023-06-20T14:35:37.436151+00:00","id":1878,"links":{},"metadata":{"_buckets":{"deposit":"603420b3-0a62-450c-8ad6-c35d0b8c7c5d"},"_deposit":{"created_by":1,"id":"1878","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"1878"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00001878","sets":["1887:1893","9:10:39:53"]},"author_link":["476621","476614","476616","476615","476620","476618","476619","476617"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Natural Laminar Flow Wing Design for a Small Supersonic Transport QSST"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2016-11-18","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"60","bibliographicPageStart":"1","bibliographicVolumeNumber":"JAXA-RR-16-001","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構研究開発報告"},{"bibliographic_title":"JAXA Research and Development Report","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"摩擦抵抗を低減するため自然層流翼設計が小型超音速旅客機QSSTに対して適用された。設計対象は, マッハ数1.6, 50人乗りを想定したJAXAの概念設計の参照機体である。自然層流設計システムのいくつかの部分が, 高い空力性能を達成するために改善された。下面の目標圧力分布を修正した結果, 全抵抗, すなわち摩擦抵抗だけでなく圧力抵抗も改善された。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Natural laminar flow wing design was applied to the small supersonic transport QSST by using a computational fluid dynamics based supersonic inverse design method, aimed to reduce friction drag. The design target is a small supersonic passenger aircraft (Mach 1.6, 36-50 passengers), which is a reference airframe for JAXA's conceptual design. In this study, some parts of the natural laminar flow design system were improved in order to achieve high aerodynamic performance. The total drag, i.e. not only the friction drag but also the pressure drag, was improved by this modification of the target pressure distribution of the lower surface.","subitem_description_type":"Other"}]},"item_3_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: カラー図版あり","subitem_description_type":"Other"}]},"item_3_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains color illustrations","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA1630029000","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: JAXA-RR-16-001","subitem_description_type":"Other"}]},"item_3_identifier_registration":{"attribute_name":"ID登録","attribute_value_mlt":[{"subitem_identifier_reg_text":"10.20637/JAXA-RR-16-001/0001","subitem_identifier_reg_type":"JaLC"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構(JAXA)"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-1113","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":"AA1192675X","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"学習院大学"},{"subitem_text_value":"株式会社エイ・エス・アイ総研"},{"subitem_text_value":"宇宙航空研究開発機構航空技術部門次世代航空イノベーションハブ(JAXA)"},{"subitem_text_value":"学習院大学"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Gakushuin University"},{"subitem_text_language":"en","subitem_text_value":"Advanced Science & Intelligence Research Institute"},{"subitem_text_language":"en","subitem_text_value":"Next Generation Aeronautical Innovation Hub Center, Aeronautical Technology Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Gakushuin University"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"牛山, 剣吾"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"石川, 敬掲"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"徳川, 直子"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小池, 寿宜"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ushiyama, Kengo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ishikawa, Hiroaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tokugawa, Naoko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Koike, Kazunori","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":"2020-01-31"}],"displaytype":"detail","filename":"AA1630029000.pdf","filesize":[{"value":"4.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"AA1630029000.pdf","url":"https://jaxa.repo.nii.ac.jp/record/1878/files/AA1630029000.pdf"},"version_id":"316d216f-799b-4796-89e2-b025b7c016e4"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Drag Reduction","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Inverse Design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Computational Fluid Dynamics","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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"小型超音速旅客機の自然層流翼設計","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"小型超音速旅客機の自然層流翼設計"}]},"item_type_id":"3","owner":"1","path":["53","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2016-11-18"},"publish_date":"2016-11-18","publish_status":"0","recid":"1878","relation_version_is_last":true,"title":["小型超音速旅客機の自然層流翼設計"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:37:34.008310+00:00"}