Control of Transitional and Turbulent Flows Using Plasma-Based Actuators
Author:
Affiliation:
1. U.S. Air Force Research Laboratory
2. Kettering University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-3230
Reference33 articles.
1. Aerodynamic flow acceleration using paraelectric and peristaltic electrohydrodynamic effects of a One Atmosphere Uniform Glow Discharge Plasma
2. Application of weakly-ionized plasmas as wing flow-control devices
3. M. Post and T. Corke. Separation control using plasma actuators - dynamic stall control on an oscillating airfoil. AIAA Paper 2004-2517, June2004.
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