{"created":"2023-06-20T15:13:18.333988+00:00","id":43229,"links":{},"metadata":{"_buckets":{"deposit":"82cbf463-0653-4d97-a35b-8e9cbf2bfa60"},"_deposit":{"created_by":1,"id":"43229","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43229"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043229","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["462726","462724","462729","462725","462727","462728"],"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 Supersonic Flows Using Panel Method"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1986-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"106","bibliographicPageStart":"99","bibliographicVolumeNumber":"7","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-7","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Steady supersonic linearized potential flows about two types of wings and a wing-body configuration were simulated using the panel method program MARCAP. Linearly varying doublet distribution is adopted to ensure the continuity of the strength on panel edges, while constant distribution on each panel is used for source. Morino's scheme is employed for most cases. The velocity boundary condition scheme is also applied to some cases. The results show good agreement with analytical solutions and wind tunnel testings. The computation time is within a reasonable limit, and the program size is comparable to those of panel methods for incompressible or subsonic flows.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALSP0007013","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-7","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":"三菱電機株式会社"},{"subitem_text_value":"三菱電機株式会社"},{"subitem_text_value":"三菱スペースソフトウェア株式会社"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Electric Corporation"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Electric Corporation"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Space Software Corporation"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"丸山, 祐一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"秋下, 貞夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中村, 昭人"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Maruyama, Yuichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Akishita, Sadao","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakamura, Akihito","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":"nalsp0007013.pdf","filesize":[{"value":"451.6 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0007013.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43229/files/nalsp0007013.pdf"},"version_id":"568ac67c-c8bd-4836-90ad-4f17772c83e8"}]},"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":"パネル法による超音速流の数値解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"パネル法による超音速流の数値解析"}]},"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":"43229","relation_version_is_last":true,"title":["パネル法による超音速流の数値解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:19:47.187785+00:00"}