Modeling and Experiment of Leading Edge Separation Control Using SDBD Plasma Actuators
Author:
Affiliation:
1. United States Air Force Academy Space Physics and Atmospheric Research Center Department of Physics
2. University of Notre Dame
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2007-877
Reference40 articles.
1. 1Matlis, E. H., Controlled experiments on instabilities and transition to turbulence on a sharp cone at Mach 3.5, Ph.D. thesis,University of Notre Dame, 2004.
2. Simulation of Plasma Actuators Using the Wind-US Code
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