High Fidelity Computational Simulation of a Membrane Wing Airfoil
Author:
Affiliation:
1. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-614
Reference21 articles.
1. Computation of unsteady laminar flow over a flexible two‐dimensional membrane wing
2. A study of flexible airfoil aerodynamics with application to Micro Aerial Vehicles
3. Unsteady Aerodynamics of Membrane Airfoils
4. Dynamics of a Compliant Membrane as Related to Mammalian Flight
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