Development and Testing of an Experimental Aeroelastic Model with Micro-Trailing Edge Effectors
Author:
Affiliation:
1. Stanford University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2003-220
Reference17 articles.
1. Nae, C. "Synthetic Jet Influence on NACA 0012 Airfoil at High Angles of Attack," AIAA Paper 98-4523.
2. Delay of airfoil stall by periodic excitation
3. Conference, July18-23, 1999,SanFrancisco, CA.
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