Flapping Wing CFD/CSD Aeroelastic Formulation Based on a Co-rotational Shell Finite Element
Author:
Affiliation:
1. University of Michigan
2. University of Florida
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-2412
Reference68 articles.
1. Aerodynamics of Low Reynolds Number Flyers
2. Flapping and flexible wings for biological and micro air vehicles
3. Mueller, T., ed. Fixed and Flapping Wing Aerodynamics for Micro Air Vehicle Applications. Progress in AeronauticsandAstronautics.Vol.195.2001,AIAA:NewYork.
4. Challenges Facing Future Micro-Air-Vehicle Development
5. Support and deformability in insect wings
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