Numerical Investigation of Plasma-Based Control for Low-Reynolds-Number Airfoil Flows
Author:
Affiliation:
1. U.S. Air Force Research Laboratory, Wright-Patterson Air Force Base, Ohio 45433-7512
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J050755
Reference67 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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