PLASMA FLOW CONTROL OVER FOREBODY AT HIGH ANGLES OF ATTACK-Reference-Cited by-同舟云学术

PLASMA FLOW CONTROL OVER FOREBODY AT HIGH ANGLES OF ATTACK

Published:2010-05-30 Issue:13 Volume:24 Page:1405-1408
ISSN:0217-9849
Container-title:Modern Physics Letters B
language:en
Short-container-title:Mod. Phys. Lett. B

Author:

ZHAO ZIJIE¹,GAO CHAO¹,LIU FENG²,LUO SHIJUN²

Affiliation:

1. National key Laboratory of Aerodynamics Design and Research, Northwestern Polytechnical University, Xi'an 710072, China

2. The Department of Mechanical and Aerospace Engineering, University of California, Irvine CA 92697-3975, USA

Abstract

Forward blowing from a pair of plasma actuators on the leeward surface and near the apex is used to switch the asymmetric vortex pair over a cone of semi-apex angle 10° at high angles of attack. Wind tunnel pressure measurements show that by appropriate design of the actuators and appropriate choice of the AC voltage and frequency, side forces and yawing moments of opposite signs can be obtained at a given angle of attack by activating one of the plasma actuators. Further work is suggested.

Publisher

World Scientific Pub Co Pte Lt

Subject

Condensed Matter Physics,Statistical and Nonlinear Physics

Link

https://www.worldscientific.com/doi/pdf/10.1142/S0217984910023736

Reference2 articles.

1. Forebody vortex control

2. Asymmetric Vortices on a Slender Body of Revolution

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