Proper Orthogonal Decomposition for Three-Dimensional Membrane Wing Aerodynamics
Author:
Affiliation:
1. University of Florida
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2003-3917
Reference24 articles.
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3. 3Farhat, C., Pierson, K., and Degand, C. "CFD Based Simulation of the Unsteady Aeroelastic Response of a Maneuvering Vehicle," AIAA Paper 2000-0899.
4. 4Liu, F., Cai, J., Zhu,Y., Wong, A.S.F., and Tsai, H. M. "Calculations of Wing Flutter by a Coupled CFD-CSD Method," AIAAPaper 2000-0907.
5. 5Hartwich, P. M., Dobbs, S. K., Arslan, A. E., and Kim, S. C. "Navier-Stokes Computations of Limit Cycle Oscillations for a B-1-like Configuration," AIAA Paper2000-2338.
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