{"created":"2023-06-20T14:37:49.298422+00:00","id":4265,"links":{},"metadata":{"_buckets":{"deposit":"7039d241-785e-45b8-91a6-b91cf26a5f0c"},"_deposit":{"created_by":1,"id":"4265","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"4265"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00004265","sets":["1398:1530:1537","1543:1874:1881","1887:1891","9:789:888:896"]},"author_link":["18692","18693","18696","18698","18697","18699","18695","18701","18694","18700"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Numerical Study on Effect of Circumferential Driving Position of DBD Plasma Actuator on Asymmetric Separation Vortex Control for High-Angle-of-Attack Slender-Body"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2013-03-29","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"156","bibliographicPageStart":"151","bibliographicVolumeNumber":"JAXA-SP-12-010","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料"},{"bibliographic_title":"JAXA Special Publication: Proceedings of 44th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2012","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44回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2012 (2012年7月5日-6日. 富山国際会議場大手町フォーラム), 富山市, 富山県","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":"44th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2012 (July 5-6, 2012. Toyama International Conference Center), Toyama Japan","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"We have analyzed the asymmetric separation flow over a slender body at high angle of attack by numerical simulation aiming a control of the asymmetric vortices using a dielectric barrier discharge (DBD) plasma actuator. Reynolds Averaged Navier Stokes/Large-Eddy Simulation hybrid method (RANS/LES) is adopted with high-order compact spatial difference scheme. First, the characteristics of the asymmetric separation flow were explained for various angles of attack. When the angle of attack becomes higher, the asymmetricity of the flow field becomes stronger. The side force has nonlinearity in the relation with the angle of attack. We estimated the circumferential flow separation point using circumferential pressure distribution. Separation point is changed with the angle of attack, axial position and body side (right or left hand side). Next, numerical simulations of the flow field over the slender body with the plasma actuator actuation were con\"\"\" ducted. Plasma actuators are located circumferential position of plus or minus 80degs, plus or minus 100degs or plus or minus 120degs. We investigated the influence of the positional relation between the flow separation point and the actuator location on the side force control effect. As a result, the flow control effect can be improved by installing the actuator near to the flow separation point. The flow can be controlled by the plasma actuator located not only before the flow separation point but also after that; this result indicates the flow control is due to the Coanda effect.","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: AA0061958025","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-12-010","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(JAXA)"}]},"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":"東京農工大学"},{"subitem_text_value":"東京農工大学"},{"subitem_text_value":"東京農工大学"},{"subitem_text_value":"宇宙航空研究開発機構宇宙科学研究所宇宙飛翔工学研究系(JAXA)（ISAS)"},{"subitem_text_value":"宇宙航空研究開発機構宇宙科学研究所宇宙飛翔工学研究系(JAXA)（ISAS)"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Tokyo University of Agriculture and Technology"},{"subitem_text_language":"en","subitem_text_value":"Tokyo University of Agriculture and Technology"},{"subitem_text_language":"en","subitem_text_value":"Tokyo University of Agriculture and Technology"},{"subitem_text_language":"en","subitem_text_value":"Department of Space Flight Systeｍs, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"},{"subitem_text_language":"en","subitem_text_value":"Department of Space Flight Systeｍs, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"佐藤, 雅幸"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"稲葉, 亮司"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"西田, 浩之"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"野々村, 拓"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"藤井, 孝蔵"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sato, Masayuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Inaba, Ryoji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nishida, Hiroyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nonomura, Taku","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fujii, Kozo","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":"61958025.pdf","filesize":[{"value":"1.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"61958025.pdf","url":"https://jaxa.repo.nii.ac.jp/record/4265/files/61958025.pdf"},"version_id":"0eaf59ff-03ca-4c5a-8a74-f4df727ca30e"}]},"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":"DBDプラズマアクチュエータを用いた大迎角細長物体の非対称剥離渦制御における周方向駆動位置の影響の数値解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"DBDプラズマアクチュエータを用いた大迎角細長物体の非対称剥離渦制御における周方向駆動位置の影響の数値解析"}]},"item_type_id":"5","owner":"1","path":["896","1537","1881","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"4265","relation_version_is_last":true,"title":["DBDプラズマアクチュエータを用いた大迎角細長物体の非対称剥離渦制御における周方向駆動位置の影響の数値解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:43:39.862267+00:00"}