{"created":"2023-06-20T15:11:41.822412+00:00","id":41403,"links":{},"metadata":{"_buckets":{"deposit":"55736bc0-cfc6-4abe-9835-e94fc701d015"},"_deposit":{"created_by":1,"id":"41403","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41403"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041403","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["489887","489884","489886","489885"],"item_3_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"超音速前縁受容性の数値シミュレーション"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2000-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"46","bibliographicPageStart":"43","bibliographicVolumeNumber":"48T","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_3_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 27-29 Sept.2000 東京 日本","subitem_description_type":"Other"}]},"item_3_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 27-29 Sept.2000 Tokyo Japan","subitem_description_type":"Other"}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"前縁上に入射する時間周期性マッハ波に対する超音速境界層の受容性を主流マッハ数2.2および4.5の条件で数値的に調べた。マッハ波が境界層プレートの下から来る場合には、励起流は上側境界層内のT-S(Tollmien-Schlichting)波により、および、1±1/Mで進行する圧力波が優勢な強制場のため、下側境界層内の強制波動により支配されることが分かった。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The receptivity of supersonic boundary layer to time periodic Mach wave incident onto leading-edge is examined numerically at a freestream Mach number 2.2 and 4.5. When the Mach wave is coming from below the boundary layer plate, the excited flow is found to be governed by the T-S (Tollmien-Schlichting) wave in the upper side boundary layer and by the forced waves in the lower side boundary layer that are due to the forcing field dominated by pressure waves traveling at 1 +/- 1/M.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0028637017","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-48T","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":"大阪府立大学"},{"subitem_text_value":"大阪府立大学"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Osaka Prefecture University"},{"subitem_text_language":"en","subitem_text_value":"Osaka Prefecture University"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"坂上, 昇史"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"西岡, 通男"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sakaue, Shoji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nishioka, Michio","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":"2020-02-10"}],"displaytype":"detail","filename":"nalsp0048018.pdf","filesize":[{"value":"351.7 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0048018.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41403/files/nalsp0048018.pdf"},"version_id":"d5588456-bc0a-4d6b-812e-8675e25ba4a9"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"超音速前縁受容性","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速境界層","subitem_subject_scheme":"Other"},{"subitem_subject":"時間周期マッハ波","subitem_subject_scheme":"Other"},{"subitem_subject":"T-S波","subitem_subject_scheme":"Other"},{"subitem_subject":"Tollmien-Schlichting","subitem_subject_scheme":"Other"},{"subitem_subject":"強制波","subitem_subject_scheme":"Other"},{"subitem_subject":"励起流","subitem_subject_scheme":"Other"},{"subitem_subject":"層流制御","subitem_subject_scheme":"Other"},{"subitem_subject":"外部擾乱","subitem_subject_scheme":"Other"},{"subitem_subject":"主流マッハ数","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic leading edge receptivity","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic boundary layer","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"time periodic Mach wave","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"T S wave","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Tollmien Schlichting","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"forced wave","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"excited flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"laminar control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"external disturbance","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"free stream Mach number","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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"Numerical simulations of supersonic leading-edge receptivity","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Numerical simulations of supersonic leading-edge receptivity","subitem_title_language":"en"}]},"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":"41403","relation_version_is_last":true,"title":["Numerical simulations of supersonic leading-edge receptivity"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:01:06.622045+00:00"}