{"created":"2023-06-20T15:13:15.969011+00:00","id":43194,"links":{},"metadata":{"_buckets":{"deposit":"3dae0fff-cba4-4b6c-ac6f-e93b68230e33"},"_deposit":{"created_by":1,"id":"43194","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43194"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043194","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["462562","462563"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Developments of Navier-Stokes Code for Hypersonic Space-Flight Vehicles"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1985-11","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"112","bibliographicPageStart":"103","bibliographicVolumeNumber":"5","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-5","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A thin-layer, Compressible Navier-Stokes code has been developed for the hypersonic flow over space flight vehicles. The implicit approximate factorization algorithm proposed by Beam and Warming has been used to obtain numerical solutions. Implicit boundary conditions arc also applied to the body and shock wave surfaces, which enable the numerical scheme to be stable and robust. Grid systems orthogonal to the body surface can be generated by the fast conformal transformations. In this report, calculations have been made for the flow around bluff bodies, indented blunt bodies and rockets in order to investigate aerothermodynamic characteristics. Numerical results indicate that there exists three types of severe aerodynamic heating, which may exceed stagnation point heating on the body surface.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALSP0005014","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-5","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":"航空宇宙技術研究所"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"山本, 行光"}],"nameIdentifiers":[{"nameIdentifier":"462562","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Yamamoto, Yukimitsu","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"462563","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":"2020-01-28"}],"displaytype":"detail","filename":"nalsp0005014.pdf","filesize":[{"value":"668.7 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0005014.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43194/files/nalsp0005014.pdf"},"version_id":"09c91157-8967-47ac-9e05-786312d6aa23"}]},"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":"宇宙飛翔体極超音速粘性流解析プログラムの開発","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"宇宙飛翔体極超音速粘性流解析プログラムの開発"}]},"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":"43194","relation_version_is_last":true,"title":["宇宙飛翔体極超音速粘性流解析プログラムの開発"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:20:37.828190+00:00"}