Effect of Camber on the Aerodynamics of Adaptive-Wing Micro Air Vehicles
- 1 November 2005
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 42 (6) , 1537-1542
- https://doi.org/10.2514/1.12401
Abstract
No abstract availableKeywords
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- Aerodynamic lift at Reynolds numbers below 7 x 10 exp 4AIAA Journal, 1996
- Catalog of low-Reynolds-number airfoil data for wind-turbine applicationsPublished by Office of Scientific and Technical Information (OSTI) ,1982