Suppression of Tonal Trailing-Edge Noise From an Airfoil Using a Plasma Actuator
Author:
Affiliation:
1. Department of Aerospace Engineering, Tokyo Metropolitan University, Tokyo 191, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J052203
Reference24 articles.
1. Dielectric Barrier Discharge Plasma Actuators for Flow Control
2. Separation Control on HIgh Angle of Attack Airfoil Using Plasma Actuators
3. Unsteady Plasma Actuators for Separation Control of Low-Pressure Turbine Blades
4. Plasma Actuators for Cylinder Flow Control and Noise Reduction
5. Plasma Flow Control of Cylinders in a Tandem Configuration
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