Asymmetric Flow Control on a Delta Wing with Dielectric Barrier Discharge Actuators
Author:
Affiliation:
1. The Hong Kong Polytechnic University, Hong Kong, People’s Republic of China
2. National Cheng Kung University, Tainan 701, Taiwan, Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J054373
Reference24 articles.
1. Predictions of vortex-lift characteristics by a leading-edge suctionanalogy
2. Connection between leading-edge sweep, vortex lift, and vortex strength for delta wings
3. Unsteady flow phenomena associated with leading-edge vortices
4. Vortex breakdown control by delta wing geometry
5. Turbulent and unsteady flow characteristics of delta wing vortex systems
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