Nanosecond Dielectric Barrier Discharge Plasma Actuator Flow Control of Compressible Dynamic Stall
Author:
Affiliation:
1. Ohio State University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-2341
Reference18 articles.
1. Dynamic Stall Experiments on Oscillating Airfoils
2. Design and development of a compressible dynamic stall facility
3. Airfoil dynamic stall at constant pitch rate and high Reynolds number
4. Experimental investigation of the flow field of an oscillating airfoil and estimation of lift from wake surveys
5. The control of flow separation by periodic excitation
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