Flow Control over a Nonslender Delta Wing by Microsecond Dielectric Barrier Discharge Actuation
Author:
Affiliation:
1. Air Force Engineering University, Xi’an, 710038 Shaanxi, People’s Republic of China
2. Aviation Industry Corporation of China, Harbin, 150001 Heilongjiang, People’s Republic of China
Funder
National Natural Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference22 articles.
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2. Review of flow control mechanisms of leading-edge vortices
3. Lift Force of Delta Wings
4. TaylorG.GursulI. “Unsteady Vortex Flows and Buffeting of a Low Sweep Delta Wing,” AIAA Paper 2004-1066, Jan. 2004. doi:10.2514/6.2004-1066
5. Recent developments in DBD plasma flow control
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