Application of an Integrated Flow and Plasma Actuation Model to an Airfoil
Author:
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J054478
Reference44 articles.
1. Separation Control
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5. Simulation of Plasma Actuators Using the Wind-US Code
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