{"created":"2023-06-20T14:53:28.963847+00:00","id":21663,"links":{},"metadata":{"_buckets":{"deposit":"5c7226a0-6b49-4738-8526-7cc47013fa48"},"_deposit":{"created_by":1,"id":"21663","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"21663"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00021663","sets":["1887:1888"]},"author_link":["203262","203264","203260","203263","203261","203265"],"item_7_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Boundary Layer Transition Control for Highly Swept Wing using DBD Plasma Actuator"}]},"item_7_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2015-12-05","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"6","bibliographicPageEnd":"240(8)","bibliographicPageStart":"233(1)","bibliographicVolumeNumber":"63","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":"The boundary layer transition caused by the cross flow instability over a highly swept wing was controlled by using a DBD plasma actuator. The plasma actuator installed near the leading edge, and induced the flow to suppress the cross flow velocity that causes the transition on the highly swept wing. A low-speed wind tunnel tests were performed to understand the effects of the plasma actuator for a 60 degrees swept wing on Re=487000. The results were shown that when plasma actuator is activated the transition location delayed to downstream than no actuation of the plasma actuator. It means that the plasma actuator contributes to reduce the cross flow velocity component hence the boundary layer transition can be delayed to downstream. With increasing the voltage of the plasma actuator, the displacements of the transition locations are also increased. This trend was also observed at different free-stream velocities.","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: DS1540389001","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":"郭, 東潤"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"上田, 良稲"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"野口, 正芳"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kwak, Dongyoun","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ueda, Yoshine","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Noguchi, Masayoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Aerodynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Boundary Layer","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Transition","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Plasma Actuator","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":"プラズマアクチュエータによる大きな後退角を持つ翼の境界層制御","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"プラズマアクチュエータによる大きな後退角を持つ翼の境界層制御"}]},"item_type_id":"7","owner":"1","path":["1888"],"pubdate":{"attribute_name":"公開日","attribute_value":"2016-02-17"},"publish_date":"2016-02-17","publish_status":"0","recid":"21663","relation_version_is_last":true,"title":["プラズマアクチュエータによる大きな後退角を持つ翼の境界層制御"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T03:32:05.191123+00:00"}