{"created":"2023-06-20T15:07:51.896871+00:00","id":37226,"links":{},"metadata":{"_buckets":{"deposit":"2e72bf26-f12c-466f-8a80-0b693181c8d5"},"_deposit":{"created_by":1,"id":"37226","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37226"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037226","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["479734","479735"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"渦・衝撃波干渉の数値計算"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1999-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"14","bibliographicPageStart":"11","bibliographicVolumeNumber":"40","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","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":"30 Sep.-1 Oct. 1997 (21st). 26-27 Mar. 1998 (22nd)","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":"30 Sep.-1 Oct. 1997 (21st). 26-27 Mar. 1998 (22nd)","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"垂直衝撃波と縦渦との干渉を、圧縮性オイラー方程式を解くことによって数値的に調べた。軸対称3次元流を仮定した。その支配方程式を、有限差分法を用いて不連続化した。衝撃波歪と流れ構造に及ぼす上層流マッハ数、還流強度および縦渦の軸方向速度分布の影響を調べた。その結果として生じる流れの量(密度、圧力および速度など)を広範囲にわたって可視化した。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"An interaction between a normal shock wave and a streamwise vortex is numerically investigated by solving the compressible Euler equations. Axisymmetric three dimensional flow is assumed. The governing equations are made discrete by using a finite difference scheme. The influences of the upstream Mach number, strength of circulation and axial velocity profiles of the streamwise vortex on the distortion of shock wave and flow configuration are examined. The resulting flow quantities such as density, pressure and velocity are extensively visualized.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001655003","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-40","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":"計算流体力学研究所"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Institute of Computational Fluid Dynamics"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"橋口, 真宜"}],"nameIdentifiers":[{"nameIdentifier":"479734","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Hashiguchi, Masanori","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"479735","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":"nalsp0040003.pdf","filesize":[{"value":"1.7 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0040003.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37226/files/nalsp0040003.pdf"},"version_id":"8e0e4536-35e8-4ce6-b762-a2c23619a2ca"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"渦衝撃波干渉","subitem_subject_scheme":"Other"},{"subitem_subject":"計算流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"圧縮性流","subitem_subject_scheme":"Other"},{"subitem_subject":"軸対称3次元流","subitem_subject_scheme":"Other"},{"subitem_subject":"垂直衝撃波","subitem_subject_scheme":"Other"},{"subitem_subject":"縦渦","subitem_subject_scheme":"Other"},{"subitem_subject":"圧縮性オイラー方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"流れの可視化","subitem_subject_scheme":"Other"},{"subitem_subject":"衝撃波歪","subitem_subject_scheme":"Other"},{"subitem_subject":"上層流マッハ数","subitem_subject_scheme":"Other"},{"subitem_subject":"還流強度","subitem_subject_scheme":"Other"},{"subitem_subject":"流れ構造","subitem_subject_scheme":"Other"},{"subitem_subject":"shock wave vortex interaction","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"compressible flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"axisymmetric three dimensional flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"normal shock wave","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"streamwise vortex","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"compressible Euler equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flow visualization","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"shock wave distortion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"upstream Mach number","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"circulation strength","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flow configuration","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"Computational study of shock/vortex interaction","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Computational study of shock/vortex interaction","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1891","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"37226","relation_version_is_last":true,"title":["Computational study of shock/vortex interaction"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:23:11.665179+00:00"}