Separation Control on HIgh Angle of Attack Airfoil Using Plasma Actuators
- 1 November 2004
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 42 (11), 2177-2184
- https://doi.org/10.2514/1.2929
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
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- Mechanisms and Responses of a Single Dielectric Barrier Plasma Actuator: Plasma MorphologyAIAA Journal, 2004
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