Aerodynamic Performance of a Corrugated Dragonfly Airfoil Compared with Smooth Airfoils at Low Reynolds Numbers
Author:
Affiliation:
1. Iowa State University
2. Institute of Mechanics, Chinese Academy of Sciences
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2007-483
Reference14 articles.
1. Mueller, T. J. (ed.), Fixed and Flapping Wing Aerodynamics for Micro Air Vehicle Applications (Progress in AstronauticsandAeronautics),ISBN1-56347-517-0.2001.
2. Form and function in corrugated insect wings
3. Biomechanical aspects of the insect wing: an analysis using the finite element method
4. Aerodynamic properties of an insect wing section and a smooth aerofoil compared
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