{"created":"2023-06-20T15:13:12.986775+00:00","id":43138,"links":{},"metadata":{"_buckets":{"deposit":"b48713cb-af52-4f8c-84e3-90d437da7fe1"},"_deposit":{"created_by":1,"id":"43138","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43138"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043138","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["462362","462363"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"A numerical design method for three-dimensional transonic wings"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1983-11","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"206","bibliographicPageStart":"199","bibliographicVolumeNumber":"1","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 SP-1","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A numerical design procedure for three-dimensional transonic wings is presented. In this method, the boundary value problem is solved for the wing geometry which induces a prescribed pressure distribution subject to additional requirements on trailing-edge closure. The method is based on the transonic small disturbance theory and utilizes a type-dependent relaxation technique. Design results for large aspect ratio supercritical swept wings are also presented.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALSP0001020","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-1","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":"航空宇宙技術研究所"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"高梨, 進"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takanashi, Susumu","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":"2020-01-28"}],"displaytype":"detail","filename":"nalsp0001020.pdf","filesize":[{"value":"487.0 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0001020.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43138/files/nalsp0001020.pdf"},"version_id":"c2d376da-da12-4ecc-8372-b0d1a53870a1"}]},"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":"三次元遷音速翼の設計","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"三次元遷音速翼の設計"}]},"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":"43138","relation_version_is_last":true,"title":["三次元遷音速翼の設計"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:22:00.160512+00:00"}