{"created":"2023-06-20T14:38:20.322630+00:00","id":4879,"links":{},"metadata":{"_buckets":{"deposit":"384c8532-b415-47b9-8336-36fd88906c59"},"_deposit":{"created_by":1,"id":"4879","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"4879"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00004879","sets":["1887:1891","9:789:936:942"]},"author_link":["22251","22250"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Linear Stability Analysis of Supersonic Streamwise Vortices"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2010-02-26","bibliographicIssueDateType":"Issued"},"bibliographicVolumeNumber":"JAXA-SP-09-014","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 「境界層遷移の解明と制御」研究会講演論文集（第43回・第44回)"},{"bibliographic_title":"JAXA Special Publication: Proceedings of the 43rd and 44th JAXA Workshops on \"Investigation and Control of Boundar-Layer Transition\"","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":"第43回（2008年10月2日-10月3日）「境界層遷移の解明と制御」研究会; 第44回（2009年3月26日-3月27日）「境界層遷移の解明と制御」研究会","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":"43rd JAXA Workshops on \"Investigation and Control of Boundar-Layer Transition\" (October 2-3, 2008) ; 44th JAXA Workshops on \"Investigation and Control of Boundar-Layer Transition\" (March 26-27, 2009)","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This paper describes a theoretical study on the stability of supersonic streamwise vortices. The spatial as well as temporal stability calculations are made for a single streamwise vortex in a Mach 2.45 free stream. The basic flow data necessary for the stability analysis such as the velocity and vorticity distributions are obtained by conducting numerical simulation of the flow past the so-called alternating wedge vortex generator. By describing the results for the  unstable modes the spatial stability characteristics are shown to be in good agreement with those of temporal one. It is emphasized that the streamwise vortex is demonstrated to be much more  unstable and powerful in enhancing supersonic mixing, compared with the so-called mixing layer.  Importantly this comparison is made possible by newly defining the convective Mach number for the streamwise vortex.","subitem_description_type":"Other"}]},"item_5_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: カラー図版あり","subitem_description_type":"Other"}]},"item_5_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains color illustrations","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0064575003","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: JAXA-SP-09-014","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-113X","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":"AA11984031","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"大阪府立大学工学研究科"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Depertment of Aerospace Engineering, Osaka Prefecture University"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"比江島, 俊彦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hiejima, Toshihiko","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":"2020-01-16"}],"displaytype":"detail","filename":"64575003.pdf","filesize":[{"value":"2.2 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"64575003.pdf","url":"https://jaxa.repo.nii.ac.jp/record/4879/files/64575003.pdf"},"version_id":"5db65edc-0bab-46eb-ba32-d7ef80026a2e"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Linear stability; supersonic mixing; streamwise vortex; compressible swirl flow; q-Vortex","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 paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"超音速縦渦の線型安定解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"超音速縦渦の線型安定解析"}]},"item_type_id":"5","owner":"1","path":["942","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"4879","relation_version_is_last":true,"title":["超音速縦渦の線型安定解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:30:01.163656+00:00"}