{"created":"2023-06-20T15:15:02.792130+00:00","id":45089,"links":{},"metadata":{"_buckets":{"deposit":"6cb6142f-7bcb-45fa-b2c9-efe6c665f266"},"_deposit":{"created_by":1,"id":"45089","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"45089"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00045089","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["472860","472861"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Analysis of Inviscid Transonic Flow around an Airfoil by Diagonal Form of IAF Scheme"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1984-08","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"13","bibliographicVolumeNumber":"831","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-831","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In order to analyze inviscid transonic flow around an airfoil, the program has been developed for solving two-dimensional Euler equations by the diagonal form of implicit approximate factorization scheme. Numerical results show two patterns of shocks. One is the flow from supersonic to subsonic, which exhibits nearly normal shock. The other, a flow from supersonic to supersonic, exhibits oblique shock. Numerical solutions of Euler equations are compared with those of potential flow, showing the differences in shock position, and pressure rise after shock.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTR0831000","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-831","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空気力学第二部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Second Aerodynamics Division, National Aerospace Laboratory(NAL)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"河合, 伸坦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"KAWAI, Nobuhiro","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":"naltr00831.pdf","filesize":[{"value":"828.8 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr00831.pdf","url":"https://jaxa.repo.nii.ac.jp/record/45089/files/naltr00831.pdf"},"version_id":"a98233b8-2706-4358-af44-228e2f1feba8"}]},"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":"対角化IAF解法による非粘性遷音速流翼型解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"対角化IAF解法による非粘性遷音速流翼型解析"}]},"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":"45089","relation_version_is_last":true,"title":["対角化IAF解法による非粘性遷音速流翼型解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:45:29.971591+00:00"}