{"created":"2023-06-20T15:13:35.672122+00:00","id":43517,"links":{},"metadata":{"_buckets":{"deposit":"84014723-0b92-49dd-9025-4da619fc71c6"},"_deposit":{"created_by":1,"id":"43517","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43517"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043517","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["464028","464029","464030","464027"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"The Role of Computational Fluid Dynamics in Aeronautical Engineering (9)-Analysis of Hypersonic Equilibrium Air Flow-"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1991-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"140","bibliographicPageStart":"135","bibliographicVolumeNumber":"16","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-16","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Numerical simulation of hypersonic flow around a 2-D cylinder and a 3-D complete reentry vehicle have been carried out by solving Euler/Navier-Stokes equations which incorporate the equation of state for an equilibrium air. The governing equations are solved by an implicit finite volume TVD upwind scheme using a two-equation turbulence model for a viscous flow. Curve-fits for the thermodynamic and transport properties of an equilibrium air adopted in order to estimate real gas effects. Convective fluxes are calculated by the roe's approximate Riemann solver generalized for an equilibrium air. The results of hypersonic flow analysis using this code suggest us that the real gas effects, such as chemical reaction, are not negligible to predict the hypersonic flow characteristics accurately.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALSP0016021","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-16","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":"川崎重工業株式会社岐阜技術研究所"},{"subitem_text_value":"川崎重工業株式会社航空宇宙事業本部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Gifu Technical Institute Kawasaki Heavy Industries, Ltd."},{"subitem_text_language":"en","subitem_text_value":"Aerospace Group  Kawasaki Heavy Industries, Ltd."}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"岸本, 琢司"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"花光, 明"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kishimoto, Takuji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hanamitsu, Akira","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":"nalsp0016021.pdf","filesize":[{"value":"471.9 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0016021.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43517/files/nalsp0016021.pdf"},"version_id":"689f70f5-a3da-46da-ac45-da00e6f9d356"}]},"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":"設計における数値計算の活用について(その9): 極超音速平衡流の解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"設計における数値計算の活用について(その9): 極超音速平衡流の解析"}]},"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":"43517","relation_version_is_last":true,"title":["設計における数値計算の活用について(その9): 極超音速平衡流の解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:12:53.388620+00:00"}