Nonlinear Aeroelastic Analysis of Highly Flexible Flapping Wings Using an ALE Formulation of Embedded Boundary Method
Author:
Affiliation:
1. Stanford University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-0221
Reference40 articles.
1. 1Ramasamy M, Lee, T E and Leishman, J G. Flowfield of a rotating-wing micro air vehicle. Journal of aircraft 2007; 44:1236-1244.
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3. Effect of flexibility on flapping wing characteristics in hover and forward flight;Computers & Fluids;2018-09
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