Burst Frequency Effect of DBD Plasma Actuator on the Control of Separated Flow over an Airfoil
Author:
Affiliation:
1. University of Tokyo
2. Japan Aerospace Exploration Agency (JAXA)
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2012-3054
Reference31 articles.
1. Separation Control on HIgh Angle of Attack Airfoil Using Plasma Actuators
2. Dielectric Barrier Discharge Plasma Actuators for Flow Control
3. Computational Study on Effect of Synthetic Jet Design Parameters
4. Flow Control by Dielectric Barrier Discharge Actuators: Jet Mixing Enhancement
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