Computation vs. Experiment for High-Frequency Low-Reynolds Number Airfoil Pitch and Plunge
Author:
Affiliation:
1. North Carolina State University
2. Air Force Research Lab
3. Air Force Institute of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-653
Reference19 articles.
1. Airfoil Theory for Non-Uniform Motion
2. McCroskey,W.J. "ThePhenomenonofDynamicStall". NASATM81264,1981.
3. Mueller,T.J. "LowReynoldsNumberVehicles". AGARDographNo.288,1985.
4. Etkin,B. DynamicsofAtmosphericFlight. DoverPublications,2000.
5. Jet Characteristics of a Plunging Airfoil
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