Effect of Camber on the Aerodynamics of Adaptive-Wing Micro Air Vehicles
Author:
Affiliation:
1. University of Arizona, Tucson, Arizona 85721
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.12401
Reference18 articles.
1. Catalog of low-Reynolds-number airfoil data for wind-turbine applications
2. Fixed and Flapping Wing Aerodynamics for Micro Air Vehicle Applications
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