Analytical, Computational, and Experimental Investigations of Equivalence Between Pitch and Plunge Motions for Airfoils at Low Reynolds Numbers
Author:
Affiliation:
1. North Carolina State University
2. Air Force Research Lab
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-535
Reference19 articles.
1. Unsteady Airfoils
2. Fixed and Flapping Wing Aerodynamics for Micro Air Vehicle Applications
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