LES on Turbulent Separated Flow around NACA0015 at Reynolds Number 1,600,000 toward Active Flow Control
Author:
Affiliation:
1. University of Tokyo
2. Japan Aerospace Exploration Agency (JAXA)
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-2687
Reference30 articles.
1. SDBD plasma enhanced aerodynamics: concepts, optimization and applications
2. Separation Control on HIgh Angle of Attack Airfoil Using Plasma Actuators
3. Dielectric Barrier Discharge Plasma Actuators for Flow Control
4. SYNTHETIC JETS
5. Computational Study on Effect of Synthetic Jet Design Parameters
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