Aeroelastic Dynamics of a NACA 0012 Airfoil at Transitional Reynolds Numbers
Author:
Affiliation:
1. Laval University
2. Royal Military College of Canada
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-4034
Reference13 articles.
1. Self-sustained aeroelastic oscillations of a NACA0012 airfoil at low-to-moderate Reynolds numbers
2. Coherent structures in an airfoil boundary layer and wake at low Reynolds numbers
3. 3Poirel, D. Wing LCO at Transitional Re Numbers NATO RTO-AVT-152, (2008).
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