Thin/Cambered/Reflexed Airfoil Development for Micro Air Vechhicle Applications at Reynolds Numbers of 60,000 to 100,000
Author:
Affiliation:
1. Rochester Institute of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-6508
Reference14 articles.
1. Lift Distributions on Low-Aspect-Ratio Wings at Low Reynolds Numbers for Micro-Air Vehicle Applications
2. Membrane wing aerodynamics for micro air vehicles
3. Optimization of a flexible low Reynolds number airfoil
4. Investigation of Tip Vortex on Aerodynamic Performance of a Micro Air Vehicle
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