Unsteady Flow Simulation of a High Lift Trapezoidal Wing Using Lattice Boltzmann Method
Author:
Affiliation:
1. Exa Corporation
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-4145
Reference35 articles.
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4. Johnson .P.L., Jones K.M., Madson M.D. "Experimental Investigation of a Simplified 3DHighLift Configuration in support ofCFD Validation"AIAA Paper2000-4217,August2000.
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