Momentum Transfer for an Aerodynamic Plasma Actuator with an Imposed Boundary Layer
Author:
Affiliation:
1. University of California, Davis
2. U.S. Air Force Academy
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-168
Reference19 articles.
1. Using Plasma Actuators Flaps to Control Laminar Separation on Turbine Blades in a Linear Cascade
2. Plasma Actuators for Separation Control of Low Pressure Turbine Blades
3. Phased plasma arrays for unsteady flow control
4. Separation Control on High Angle of Attack Airfoil Using Plasma Actuators
5. Application of weakly-ionized plasmas as wing flow-control devices
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