{"created":"2023-06-20T15:15:06.126268+00:00","id":45154,"links":{},"metadata":{"_buckets":{"deposit":"0bdab0fd-dfb3-4315-9262-a1996401f9e9"},"_deposit":{"created_by":1,"id":"45154","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"45154"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00045154","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["473167","473165","473166","473170","473169","473168"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Numerical Analysis of Inviscid Flows about Wing-Fuselage Combinations III. Calculation Based on the Euler Equations"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1985-12","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"10","bibliographicVolumeNumber":"896","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-896","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The main purpose of this paper is to numerically analyse inviscid flows about wing-fuselage combinations. In the third series we present a numerical procedure for calculating flows based on the Euler equations by the finite volume method using the Runge-Kutta type scheme and the local time stepping technique. The grids, which have already been generated by the code YOKUDO-G in the first series, are used in the calculations. Many examples are presented to show the utility of this numerical procedure for flows about several wing-fuselage combinations. Numerical results obtained by this procedure are compared with experimental results and the numerical results obtained using the full potential equation in the second series.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTR0896000","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 TR-896","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":"0389-4010","subitem_source_identifier_type":"ISSN"}]},"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計算センター"},{"subitem_text_value":"航空宇宙技術研究所計算センター"},{"subitem_text_value":"航空宇宙技術研究所計算センター"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Computer Center, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Computer Center, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Computer Center, National Aerospace Laboratory(NAL)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"石黒, 登美子"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小川, 哲"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小口, 慶子"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"ISHIGURO, Tomiko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"OGAWA, Satoru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"OGUCHI, Keiko","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":"2020-01-29"}],"displaytype":"detail","filename":"naltr00896.pdf","filesize":[{"value":"2.5 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr00896.pdf","url":"https://jaxa.repo.nii.ac.jp/record/45154/files/naltr00896.pdf"},"version_id":"c66a51d2-568a-4d9b-a54c-a75271c0d22f"}]},"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":"翼胴結合体まわり非粘性圧縮流の数値解析 Ⅲ.Euler方程式による計算","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"翼胴結合体まわり非粘性圧縮流の数値解析 Ⅲ.Euler方程式による計算"}]},"item_type_id":"3","owner":"1","path":["1893","1917"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"45154","relation_version_is_last":true,"title":["翼胴結合体まわり非粘性圧縮流の数値解析 Ⅲ.Euler方程式による計算"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:44:23.239989+00:00"}