Limitations of the DBD effects on the external flow
Author:
Affiliation:
1. Tech-X
2. Princeton University
3. Lockheed Martin Corporation
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2010-470
Reference21 articles.
1. Electrohydrodynamic Flow Control with a Glow-Discharge Surface Plasma
2. J.R. Roth,"Aerodynamicflowacceleration using paraelectricandperistalticelectrohydrodynamiceffects ofa OneAtmosphereUniform GlowDischargePlasma", Phys. Plasmas 10,2117(2003)
3. Separation Control on HIgh Angle of Attack Airfoil Using Plasma Actuators
4. DBD Plasma Actuators Driven by a Combination of Low Frequency Bias Voltage and Nanosecond Pulses
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