Active Flow Control for NACA 6-Series Airfoil at Re = 64,200
Author:
Affiliation:
1. University of Arizona, Tucson, Arizona 85721
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J050051
Reference22 articles.
1. 1/5 Scale Model of Aeromot 200S SuperXimango for Scaled Flight Research
2. Experimental Investigation of Separation and Separation Control on a Laminar Airfoil
3. Aerodynamic Scaling of General Aviation Airfoil for Low Reynolds Number Application
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