High Fidelity Computational Aeroelastic Analysis of a Plunging Membrane Airfoil
Author:
Affiliation:
1. University of Oklahoma
2. U.S. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-2472
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1. Quick Estimates of Flight Fitness in Hovering Animals, Including Novel Mechanisms for Lift Production
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3. Numerical Study on the Unsteady-Force-Generation Mechanism of Insect Flapping Motion
4. Effects of Dynamic Stall on Propulsive Efficiency and Thrust of Flapping Airfoil
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