{"created":"2023-06-20T14:53:30.700220+00:00","id":21690,"links":{},"metadata":{"_buckets":{"deposit":"be1ee760-1704-4218-aaa9-9dd4a730304a"},"_deposit":{"created_by":1,"id":"21690","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"21690"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00021690","sets":["1887:1888"]},"author_link":["203652","203658","203654","203656","203653","203659","203657","203655"],"item_7_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Experimental Investigation of Vortex Generators for Flow Separation Control on the Hinge Line of Leading-Edge Flap"}]},"item_7_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2016-02-05","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"1","bibliographicPageEnd":"40(40)","bibliographicPageStart":"35(35)","bibliographicVolumeNumber":"64","bibliographic_titles":[{"bibliographic_title":"日本航空宇宙学会論文集"},{"bibliographic_title":"Journal of the Japan Society for Aeronautical and Space Sciences","bibliographic_titleLang":"en"}]}]},"item_7_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Experiments were conducted to investigate effects of vortex generators on flow separation for a cranked-arrow wing at a low speed wind tunnel. A kind of delta-shaped vortex generator was applied to control the boundary layer separation flow near the hinge line of the deflected leading-edge flap. Effects on aerodynamic performance were estimated according to the force measurement data and flow patterns were observed by oilflow visualization technique. It was found that the drag coefficient was reduced and the lift-to-drag ratio was improved as the vortex generator was suitably equipped on the hinge line of the leading-edge flap. It was observed that swirling longitude vortices were generated from the leading-edge of the vortex generator, and thus suppressed the boundary layer flow separation.","subitem_description_type":"Other"}]},"item_7_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: 図版あり","subitem_description_type":"Other"}]},"item_7_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains illustrations","subitem_description_type":"Other"}]},"item_7_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: DS1540529006","subitem_description_type":"Other"}]},"item_7_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"Japan Society for Aeronautical and Space Sciences"}]},"item_7_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"日本航空宇宙学会"}]},"item_7_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1344-6460","subitem_source_identifier_type":"ISSN"}]},"item_7_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA11307372","subitem_source_identifier_type":"NCID"}]},"item_access_right":{"attribute_name":"アクセス権","attribute_value_mlt":[{"subitem_access_right":"metadata only access","subitem_access_right_uri":"http://purl.org/coar/access_right/c_14cb"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"雷, 忠"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"滝沢, 啓介"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"郭, 東潤"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"野口, 正芳"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Lei, Zhong","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takizawa, Keisuke","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kwak, Dongyoun","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Noguchi, Masayoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Vortex Generator","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Boundary Layer Separation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Flow Control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"High-Lift Device","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Aerodynamic Performance","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":"journal article","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"ボルテックス・ジェネレーターによる翼前縁フラップ ヒンジラインの剥離制御に関する実験研究","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"ボルテックス・ジェネレーターによる翼前縁フラップ ヒンジラインの剥離制御に関する実験研究"}]},"item_type_id":"7","owner":"1","path":["1888"],"pubdate":{"attribute_name":"公開日","attribute_value":"2016-03-28"},"publish_date":"2016-03-28","publish_status":"0","recid":"21690","relation_version_is_last":true,"title":["ボルテックス・ジェネレーターによる翼前縁フラップ ヒンジラインの剥離制御に関する実験研究"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T03:31:52.548289+00:00"}