A 3D Computational Study of the Flow-Structure Interaction in Flapping Flight
Author:
Affiliation:
1. Vanderbilt University
2. Purdue University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2010-556
Reference19 articles.
1. Computational aerodynamics of low Reynolds number plunging, pitching and flexible wings for MAV applications
2. Numerical and experimental study of the fluid dynamics of a flapping wing with low order flexibility
3. Influence of flexibility on the aerodynamic performance of a hovering wing
4. A two-dimensional computational study on the fluid–structure interaction cause of wing pitch changes in dipteran flapping flight
5. 1 2 3 4 5 6 -0.5
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