{"created":"2023-06-20T14:38:53.589510+00:00","id":5530,"links":{},"metadata":{"_buckets":{"deposit":"c9c97bab-9440-467d-81fb-1ddde02e2fbd"},"_deposit":{"created_by":1,"id":"5530","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"5530"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00005530","sets":["1887:1891","9:789:972:976"]},"author_link":["26905","26901","26902","26904","26906","26903"],"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2008-02-29","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"30","bibliographicPageStart":"27","bibliographicVolumeNumber":"JAXA-SP-07-026E","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40回"},{"bibliographic_title":"JAXA Special Publication: Proceedings of the 40th JAXA Workshop on Investigation and Control of Boundary-Layer Transition","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Flows around a leading-edge slat are investigated experimentally at Reynolds numbers Re less than or equal to 5.2 x 10(exp 5). When the slat operates to suppress the leading-edge stall, a periodic vortex shedding occurs due to the instability of laminar wake of the slat at Reynolds numbers less than 2.1 x 10(exp 5). The Reynolds number variation of the shedding frequency is not unlike that of the circular-cylinder wake at low Reynolds numbers. For Re greater than or equal to 2.3 x 10(exp 5), prominent spectral peaks appear both in the velocity fluctuations and sound-pressure and the frequency of such distinguished noise is found to be proportional to U(sub infinity)(exp 0.84) as reported in the experiment on the sound generation in a single-element airfoil at small angles of attack, suggesting a possibility of feedback loop between the shear layer instability immediately upstream the slat trailing-edge and the generated sound.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063908009","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-07-026E","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":"首都大学東京 大学院システムデザイン研究科"},{"subitem_text_value":"首都大学東京 大学院システムデザイン研究科"},{"subitem_text_value":"首都大学東京 大学院システムデザイン研究科"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Tokyo Metropolitan University Graduate School of System Design"},{"subitem_text_language":"en","subitem_text_value":"Tokyo Metropolitan University Graduate School of System Design"},{"subitem_text_language":"en","subitem_text_value":"Tokyo Metropolitan University Graduate School of System Design"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"真喜屋, 実寛"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"稲澤, 歩"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"浅井, 雅人"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Makiya, Sanehiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Inasawa, Ayumu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Asai, Masahito","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":"63908009.pdf","filesize":[{"value":"987.4 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"63908009.pdf","url":"https://jaxa.repo.nii.ac.jp/record/5530/files/63908009.pdf"},"version_id":"f2bc0511-fb12-4e63-b219-d09ec716e309"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"流れの分布","subitem_subject_scheme":"Other"},{"subitem_subject":"前縁スラット","subitem_subject_scheme":"Other"},{"subitem_subject":"低レイノルズ数","subitem_subject_scheme":"Other"},{"subitem_subject":"高揚力装置","subitem_subject_scheme":"Other"},{"subitem_subject":"層流域後流","subitem_subject_scheme":"Other"},{"subitem_subject":"渦","subitem_subject_scheme":"Other"},{"subitem_subject":"音圧","subitem_subject_scheme":"Other"},{"subitem_subject":"空力特性","subitem_subject_scheme":"Other"},{"subitem_subject":"空力騒音","subitem_subject_scheme":"Other"},{"subitem_subject":"翼型","subitem_subject_scheme":"Other"},{"subitem_subject":"流れの可視化","subitem_subject_scheme":"Other"},{"subitem_subject":"パワースペクトル","subitem_subject_scheme":"Other"},{"subitem_subject":"flow distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"leading edge slat","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"low Reynolds number","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high-lift device","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"laminar wake","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"vortex","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"sound pressure","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic noise","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"airfoil","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flow visualization","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"power spectrum","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":"Detailed flow field around a leading-edge slat at low Reynolds numbers","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Detailed flow field around a leading-edge slat at low Reynolds numbers","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["976","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"5530","relation_version_is_last":true,"title":["Detailed flow field around a leading-edge slat at low Reynolds numbers"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:12:49.333706+00:00"}