CHARACTERISTICS OF FORE-BODY SEPARATE FLOW AT HIGH ANGLE OF ATTACK UNDER PLASMA CONTROL

被引:1
作者
Wang, Jianlei [1 ]
Li, Huaxing [1 ]
Liu, Feng [2 ]
Luo, Shijun [2 ]
机构
[1] NW Polytech Univ, Natl Key Lab Aerodynam Design & Res, Xian 710072, Peoples R China
[2] Univ Calif Irvine, Dept Mech & Aerosp Engn, Irvine, CA 92697 USA
来源
MODERN PHYSICS LETTERS B | 2010年 / 24卷 / 13期
关键词
Single-dielectric barrier discharge (SDBD); plasma actuator; active flow control; high angles of attack; slender body;
D O I
10.1142/S0217984910023724
中图分类号
O59 [应用物理学];
学科分类号
摘要
A pair of plasma actuators with horseshoe shape is proposed for dynamic manipulation of forebody aerodynamic load at high angles of attack. Preliminary wind tunnel pressure measurements show that asymmetric force over a conical forebody with semi-apex angle 10 degrees can be manipulated by activating the plasma actuator mounted on one side of the cone tip. Further work is suggested.
引用
收藏
页码:1401 / 1404
页数:4
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