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titleDBDプラズマアクチュエータを用いた低レイノルズ数領域におけるNACA0012 翼の空力特性の改善
Other TitleEnhancement of Aerodynamic Characteristics of NACA 0012 Airfoil with a DBD Plasma Actuator at Low Reynolds Numbers
Author(jpn)簗瀬, 祐太; 木田, 大穂; 大竹, 智久; 村松, 旦典; 本橋, 龍郎
Author(eng)Yanase, Yuta; Kida, Oho; Otake, Tomohisa; Muramatsu, Akinori; Motohashi, Tatsuo
Author Affiliation(jpn)日本大学; 日本大学; 日本大学; 日本大学理工学部; 日本大学理工学部
Author Affiliation(eng)Nihon University; Nihon University; Nihon University; College of Science and Technology, Nihon University; College of Science and Technology, Nihon University
Issue Date2011-02-28
PublisherJapan Aerospace Exploration Agency (JAXA)
宇宙航空研究開発機構
Publication titleJAXA special publication: Proceedings of 42nd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2010
宇宙航空研究開発機構特別資料: 第42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2010 論文集
VolumeJAXA-SP-10-012
Publication date2011-02-28
Languagejpn
eng
AbstractThe effects of a DBD plasma actuator applied to a NACA0012 airfoil were examined at a Reynolds number of 10,000 using three approaches, namely, aerodynamic force measurements using a wind tunnel balance, velocity profiles of the wake obtained using a hot-wire anemometer, and smoke-wire visualization around the airfoil. As a result, the magnitude of lift approximately doubled and the drag was reduced by about 30 percents. The lift curve changed from nonlinear to linear at the lower angles of attack below 6 degrees with actuator operation. These phenomena are occurred by suppression of flow separation near the leading edge. This separation was suppressed by a downwash induced by the actuator operation. Though there might be some limitation in the performance of the plasma actuator against the angle of attack, the plasma actuator enhanced the aerodynamic performance of the airfoil under our experimental conditions.
DescriptionOriginal contains color illustrations
Meeting Information: 42nd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2010 (June 24-25, 2010. Yonago Convention Center BiG SHiP), Yonago, Tottori Japan
形態: カラー図版あり
会議情報: 第42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2010 (2010年6月24日-25日. 米子コンベンションセンター BiG SHiP)
Document TypeConference Paper
JAXA Category特別資料
ISSN1349-113X
NCIDAA11984031
SHI-NOAA0064967046
Report NoJAXA-SP-10-012
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/16058


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