{"created":"2023-06-20T15:13:31.905884+00:00","id":43451,"links":{},"metadata":{"_buckets":{"deposit":"ef312736-576a-4aad-b3a4-1ee0340b26be"},"_deposit":{"created_by":1,"id":"43451","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43451"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043451","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["463712","463716","463711","463714","463715","463713"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Blended Wing-Body Configuration Design using Transonic Inverse Code"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1990-11","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"120","bibliographicPageStart":"115","bibliographicVolumeNumber":"14","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-14","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In this paper, an iterative design procedure is described for three dimensional wing-body configuration, especially blended wing-body configuration, using a three dimensional transonic inverse method with target pressure distribution. In this application, it is combined with a full potential analysis code. Some of the design results for a conventional and a blended wing-body configuration are presented. Also a finite volume Euler solver is applied to analyze the designed configurations.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALSP0014018","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-14","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":"富士重工業株式会社"},{"subitem_text_value":"富士重工業株式会社"},{"subitem_text_value":"富士重工業株式会社"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Fuji Heavy Industries Ltd."},{"subitem_text_language":"en","subitem_text_value":"Fuji Heavy Industries Ltd."},{"subitem_text_language":"en","subitem_text_value":"Fuji Heavy Industries Ltd."}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"谷, 泰寛"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"越岡, 康弘"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"廣瀬, 秀大"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tani, Yosuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Koshioka, Yasuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hirose, Hidehiro","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":"nalsp0014018.pdf","filesize":[{"value":"1.2 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0014018.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43451/files/nalsp0014018.pdf"},"version_id":"33915fac-a74d-4d3c-8070-953332b86ba2"}]},"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":"逆解法を用いた翼胴一体化設計について","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"逆解法を用いた翼胴一体化設計について"}]},"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":"43451","relation_version_is_last":true,"title":["逆解法を用いた翼胴一体化設計について"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:14:29.319571+00:00"}