{"created":"2023-06-20T15:08:20.934872+00:00","id":37773,"links":{},"metadata":{"_buckets":{"deposit":"9e6bbe10-c7eb-4429-a04f-6687a65042ac"},"_deposit":{"created_by":1,"id":"37773","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37773"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037773","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["482911","482914","482909","482913","482912","482910"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Numerical analysis of wake flow behind hypersonic vehicle"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1994-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"78","bibliographicPageStart":"73","bibliographicVolumeNumber":"22","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料: 第11回航空機計算空気力学シンポジウム論文集"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory: Proceedings of the 11th NAL Symposium on aircraft computational aerodynamics","bibliographic_titleLang":"en"}]}]},"item_5_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"航空宇宙技術研究所 10-11 Jun. 1993 東京 日本","subitem_description_type":"Other"}]},"item_5_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"National Aerospace Laboratory 10-11 Jun. 1993 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"ブラントな底面をもつ物体の後流をマッハ数5.7、8.5、10.0、物体基準レイノルズ数50,000〜335,000にわたって数値シミュレーションにより調べた。一般座標系におけるVan　Leer流束分割風上差分法の有限容積定式化を用い、極超音速層流について薄層近似ナビエ・ストークス方程式を解く。高次の空間精度を得るために、陰的差分因子近似分解法と流束リミタをもつMUSCL(保存法則用単調性上流中心差分法)スキームとを組み合せた。底面圧、中心線に沿う圧力分布、後縁衝撃波、剥離点位置および再循環領域における渦流などに特に注目した。数値シミュレーション結果は、衝撃波可視化実験からの結果とよく一致した。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The flow field behind a blunt based bodies was investigated with numerical simulation at a nominal Mach number of 5.7, 8.5, 10.0 over a range of Reynolds numbers from 50,000 to 335,000 based on the body length. The finite volume formulation of Van Leer's flux vector splitting upwind scheme, in generalized coordinates, was used to solve thin-layer approximation of the Navier-Stokes equations for a hypersonic laminar flow. An implicit approximate factorization and MUSCL (Monotonic Upstream - centered Scheme for Conservation Laws) scheme with flux limiter were used to acquire high order spatial accuracy. Special attention was given to the base-pressure, static-pressure along the center-line, trailing shock wave, the location of separation point and vortical flow in the recirculation region. The result of a numerical simulation quite agreed with that of a visualization experiment of a shock wave.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004171013","subitem_description_type":"Other"}]},"item_5_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL SP-22","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0289-260X","subitem_source_identifier_type":"ISSN"}]},"item_5_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_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"神戸大学 大学院"},{"subitem_text_value":"神戸大学 工学部　機械工学科"},{"subitem_text_value":"神戸大学 大学院"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Kobe University Graduate School"},{"subitem_text_language":"en","subitem_text_value":"Kobe University Department of Mechanical Engineering, Faculty of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Kobe University Graduate School"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"Ro, D.S."}],"nameIdentifiers":[{"nameIdentifier":"482909","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"木村, 雄吉"}],"nameIdentifiers":[{"nameIdentifier":"482910","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"小川, 和彦"}],"nameIdentifiers":[{"nameIdentifier":"482911","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Ro, Dae Sung","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"482912","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Kimura, Takeyoshi","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"482913","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Ogawa, Kazuhiko","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"482914","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":"2020-02-10"}],"displaytype":"detail","filename":"nalsp0022012.pdf","filesize":[{"value":"597.0 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0022012.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37773/files/nalsp0022012.pdf"},"version_id":"6381e9b6-1be8-4bc6-bd31-a2bebc0d1a5b"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"極超音速後流","subitem_subject_scheme":"Other"},{"subitem_subject":"極超音速渦流","subitem_subject_scheme":"Other"},{"subitem_subject":"極超音速層流","subitem_subject_scheme":"Other"},{"subitem_subject":"極超音速底面圧","subitem_subject_scheme":"Other"},{"subitem_subject":"極超音速流剥離","subitem_subject_scheme":"Other"},{"subitem_subject":"極超音速飛行物体","subitem_subject_scheme":"Other"},{"subitem_subject":"再突入物体空気力学","subitem_subject_scheme":"Other"},{"subitem_subject":"流れ数値シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ・ストークス方程式数値解","subitem_subject_scheme":"Other"},{"subitem_subject":"有限容積法","subitem_subject_scheme":"Other"},{"subitem_subject":"流束ベクトル分割法","subitem_subject_scheme":"Other"},{"subitem_subject":"MUSCL法","subitem_subject_scheme":"Other"},{"subitem_subject":"保存法則用単調性上流中心差分法","subitem_subject_scheme":"Other"},{"subitem_subject":"極超音速粘性非粘性干渉","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic wake flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic vortical flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic laminar flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic base pressure","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic flow separation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic vehicle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"reentry body aerodynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical flow simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes equation numerical solution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"finite volume method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flux vector splitting","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"MUSCL scheme","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"monotone upstream centered scheme for consevation laws","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic viscous inviscid interaction","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"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":"conference 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