The Lattice Boltzmann Method for Flapping Wing Aerodynamics
Author:
Affiliation:
1. University of Michigan
2. Western Michigan University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2010-4867
Reference35 articles.
1. Aerodynamics of Low Reynolds Number Flyers
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3. Muller, T. J., Fixed and Flapping Wing Aerodynamics for Micro Air Vehicle Applications. AIAA Prog Astronaut Aeronaut 2001: 195.
4. Fixed membrane wings for micro air vehicles: Experimental characterization, numerical modeling, and tailoring
5. Can Tip Vortices Enhance Lift of a Flapping Wing?
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