{"created":"2023-06-20T15:13:31.768696+00:00","id":43449,"links":{},"metadata":{"_buckets":{"deposit":"2c72bc87-3614-43d2-84a5-960211deabc7"},"_deposit":{"created_by":1,"id":"43449","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43449"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043449","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["463701","463703","463702","463705","463704","463706"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Aerodynamic Design of Non-Planar Wing by Inverse Method with Navier-Stokes Equation"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1990-11","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"108","bibliographicPageStart":"103","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":"As various airplanes are increasing recently, aerodynamic design method with high accuracy has been requested about non-planar wings which are tip-fin configuration of HOPE and winglet of civil transport, etc. On non-planar wing design, it is indispensable to using Navier-Stokes code for viscous effect of corner flow and this induced separation It is presented that non-planar wing was designed using inverse method with Navier-Stokes code instead of usual full-potential code. We have applied tip-fin of HOPE to design configuration through the courtesy of NASDA.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALSP0014016","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":"三菱重工業株式会社"},{"subitem_text_value":"三菱重工業株式会社"},{"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":"Mitsubishi Heavy Industries Co.Ltd."},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industries Co.Ltd."},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"海田, 武司"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"荻野, 純"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"高梨, 進"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kaiden, Takashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ogino, Jun","creatorNameLang":"en"}],"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":"nalsp0014016.pdf","filesize":[{"value":"1.2 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0014016.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43449/files/nalsp0014016.pdf"},"version_id":"1a0cbc29-a7ba-40af-8334-1d511121d2f6"}]},"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":"ナビエ・ストークス逆解法による非平面主翼の空力設計","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"ナビエ・ストークス逆解法による非平面主翼の空力設計"}]},"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":"43449","relation_version_is_last":true,"title":["ナビエ・ストークス逆解法による非平面主翼の空力設計"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:14:31.077473+00:00"}