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大迎角細長物体の横力制御におけるDBDプラズマアクチュエータ設置位置の検討
https://jaxa.repo.nii.ac.jp/records/4020
https://jaxa.repo.nii.ac.jp/records/402036cfeb28-7c7f-426f-b133-283387a6ea88
名前 / ファイル | ライセンス | アクション |
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62268020.pdf (965.1 kB)
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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 | 大迎角細長物体の横力制御におけるDBDプラズマアクチュエータ設置位置の検討 | |||||
言語 | ||||||
言語 | jpn | |||||
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 | Investigation of DBD Plasma Actuator Arrangement for Control on High-Angle-of-Attack Slender-Body Side Force | |||||
著者 |
佐藤, 雅幸
× 佐藤, 雅幸× 西田, 浩之× 松原, 暁良× 野々村, 拓× Sato, Masayuki× Nishida, Hiroyuki× Matsubara, Akira× Nonomura, Taku |
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著者所属 | ||||||
東京農工大学 | ||||||
著者所属 | ||||||
東京農工大学 | ||||||
著者所属 | ||||||
東京農工大学 | ||||||
著者所属 | ||||||
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) | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo University of Agriculture and Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo University of Agriculture and Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo University of Agriculture and Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Space Flight Systems, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構(JAXA) | |||||
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: 第45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2013論文集 en : JAXA Special Publication 巻 JAXA-SP-13-011, p. 109-114, 発行日 2014-03-31 |
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会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 第45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2013 (2013年7月4日-5日. タワーホール船堀), 東京 | |||||
会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 45th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2013 (July 4-5, 2013. Tower Hall Funabori), Tokyo, Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | We have numerically analyzed the asymmetric separation flow control over a high-angle-of-attack slender body aiming to improve the controllability of high-angle-of-attack flight. In this study, Dielectric Barrier Discharge (DBD) plasma actuator is used as flow control device. The Reynolds Averaged Navier Stokes/Large-Eddy Simulation hybrid method (RANS/LES) is adopted with the high-order compact spatial difference scheme for our research purpose. At the first of the characteristics of flow field were shown for various angles of attack; the asymmetricity of the flow field becomes stronger with angle of attack. Next, the flow control using the plasma actuator was numerically analyzed. We considered two types of actuator setting; one is body-axial actuator which adds circumferential momentum into the flow field, and the other is circumferential actuator which adds body-axial momentum into the flow field. As a result, in the case of body-axial actuator, the side force can be continuously controlled against the actuator output power, and delay of the flow separation by the actuator generates the side force change. On the other hand, in the case of the circumferential actuator, the vortex filament separation from the body surface is delayed by plasma actuator, and large side force change can be obtained even with small actuator output power. Therefore, the side force control mechanism by the circumferential plasma actuator is the suppression of the vortex separation due to the enhancement of the axial flow by the plasma actuator. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
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: AA0062268020 | |||||
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-13-011 |