{"created":"2023-06-20T15:08:35.356792+00:00","id":38076,"links":{},"metadata":{"_buckets":{"deposit":"3fb1af1f-8cab-4eea-8248-4a8aafb4612b"},"_deposit":{"created_by":1,"id":"38076","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"38076"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00038076","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["431576","431578","431579","431577"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"地域輸送用の全翼機コンセプト"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2002-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"238","bibliographicPageStart":"233","bibliographicVolumeNumber":"53","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2001論文集"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory: Proceedings of Aerospace Numerical Simulation Symposium 2001","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The flying wing is regarded as an alternate configuration to reduce drag and structural weight. This paper presents the design process of a medium size Blended-Wing-Body airplane, which in essence is a flying wing configuration. Because of the rapid changing of thickness and chord distribution, it requires special design tools. In the present study the wing surface is generated using RAPID method. Takanashi's inverse design method is utilized to obtain the airfoil shape. The required target pressure distribution is specified using constrained target pressure specification techniques. The present study shows that the design difficulties can be overcome by using the proposed design tools.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0032819040","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-53","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 大学院工学研究科"},{"subitem_text_value":"東北大学 大学院工学研究科"}]},"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 of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Tohoku University Graduate School of Engineering"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"Pambagjo, Tjoetjoek Eko"}],"nameIdentifiers":[{"nameIdentifier":"431576","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"中橋, 和博"}],"nameIdentifiers":[{"nameIdentifier":"431577","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Pambagjo, Tjoetjoek Eko","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"431578","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Nakahashi, Kazuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"431579","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":"nalsp0053039.pdf","filesize":[{"value":"2.7 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0053039.pdf","url":"https://jaxa.repo.nii.ac.jp/record/38076/files/nalsp0053039.pdf"},"version_id":"4eff854a-7bd8-46e6-92f3-4f0b02505f37"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"全翼機","subitem_subject_scheme":"Other"},{"subitem_subject":"地域輸送","subitem_subject_scheme":"Other"},{"subitem_subject":"航空機設計","subitem_subject_scheme":"Other"},{"subitem_subject":"航空機配置","subitem_subject_scheme":"Other"},{"subitem_subject":"アスペクト比","subitem_subject_scheme":"Other"},{"subitem_subject":"ペイロード","subitem_subject_scheme":"Other"},{"subitem_subject":"空力係数","subitem_subject_scheme":"Other"},{"subitem_subject":"flying wing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"regional transport","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aircraft design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aircraft configuration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aspect ratio","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"payload","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic coefficient","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":"Flying wing concept for regional transport","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Flying wing concept for regional 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":"38076","relation_version_is_last":true,"title":["Flying wing concept for regional transport"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:45:32.879449+00:00"}