Reynolds Number Effects on Airfoils in Reverse Flow
Author:
Affiliation:
1. University of Maryland, College Park
2. U.S. Naval Academy
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-1973
Reference26 articles.
1. Time-Averaged Aerodynamics of Sharp and Blunt Trailing-Edge Static Airfoils in Reverse Flow
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