Numerical Investigation of Plasma-Based Control for Low-Reynolds Number Airfoil Flows
Author:
Affiliation:
1. U. S. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2010-4255
Reference71 articles.
1. PIV application in advanced low reynolds number facility
2. An Investigation of Low-Reynolds-Number Flows Past Airfoils
3. Comparison of Laminar Separation Bubble Measurements on a Low Reynolds Number Airfoil in Three Facilities
4. Numerical and Experimental Flow Analysis of Moving Airfoils with Laminar Separation Bubbles
5. Scanning PIV measurements of a laminar separation bubble
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3. Comparative Study of Implicit and Subgrid-Scale Model LES Techniques for Low-Reynolds Number Airfoil Applications;20th AIAA Computational Fluid Dynamics Conference;2011-06-14
4. Adaptive Variationally-Optimized Computing of Flow Dynamics, Separation, and Control;20th AIAA Computational Fluid Dynamics Conference;2011-06-14
5. Numerical Investigation of Serpentine Plasma Actuators for Separation Control at Low Reynolds Number;41st AIAA Fluid Dynamics Conference and Exhibit;2011-06-14
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