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プラズマアクチュエータを用いた翼周り流れの制御
https://jaxa.repo.nii.ac.jp/records/5961
https://jaxa.repo.nii.ac.jp/records/596162542a83-44e3-4122-85d9-a37cf9548eeb
名前 / ファイル | ライセンス | アクション |
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63154017.pdf (2.2 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | プラズマアクチュエータを用いた翼周り流れの制御 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | プラズマアクチュエータ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 翼 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 迎角 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | アクチュエータ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 剥離流 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 速度分布 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 流れの分布 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ナビエ・ストークス方程式 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 数値解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | レイノルズ数 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 流れの制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 剥離制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | NACA0012翼 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | plasma actuator | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wing | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | angle of attack | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | actuator | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | separated flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | velocity distribution | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flow distribution | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Navier-Stokes equation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | numerical analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Reynolds number | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flow control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | separation control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | NACA 0012 wing | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Simulation of flow control with a plasma actuator applied to a wing section | |||||
著者 |
椿野, 大輔
× 椿野, 大輔× 田中, 義輝× 藤井, 孝藏× Tsubakino, Daisuke× Tanaka, Yoshiteru× Fujii, Kozo |
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著者所属 | ||||||
東京大学 大学院 | ||||||
著者所属 | ||||||
東京大学 大学院 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 | ||||||
著者所属(英) | ||||||
en | ||||||
University of Tokyo Graduate School | ||||||
著者所属(英) | ||||||
en | ||||||
University of Tokyo Graduate School | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構 | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構特別資料: 航空宇宙数値シミュレーション技術シンポジウム2006論文集 en : JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2006 巻 JAXA-SP-06-010, p. 89-94, 発行日 2006-12-01 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This paper investigates effective layout of a dielectric barrier discharge plasma actuator for a flow separation control on the NACA0012 wing using computational simulations. The flow condition of low speed and low Reynolds number, M(sub infinity) = 0.1 and Re = 1.0 x 10(exp 5) is considered. Three cases of locations of the actuators are simulated. The actuator is placed at the 5 percent, 10 percent and 20 percent chord from the leading edge for each case. When the low velocity is induced by the actuator, the location has little effect on the capability to suppress the flow separation. However, if the higher velocity is induced, the actuator placed near the separation point can provide the better capability. Further increasing the angles of attack, another separation occurs from the trailing edge. Then the actuator placed near the leading edge can not suppress such separation. This is the control limitation of the single actuator. The result motivates use of the multiple plasma actuators for effective separation control. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-113X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11984031 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063154017 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-SP-06-010 |