Low-Reynolds-Number Aerodynamics of a Flapping Rigid Flat Plate
Author:
Affiliation:
1. University of Michigan, Ann Arbor, Michigan 48109
2. U.S. Air Force Research Laboratory, Wright-Patterson Air Force Base, Ohio 45433
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J050827
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1. Flapping-Wing Aerodynamics
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