Lift Augmentation of a Low-Aspect-Ratio Thick Wing in Ground Effect
Author:
Affiliation:
1. University of New South Wales, Sydney, New South Wales 2052, Australia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2940
Reference6 articles.
1. An analytic solution for two- and three-dimensional wings in ground effect
2. Simulation of Hydrodynamic Effects of 2-Dimensional WIG Moving near the Free Surface
3. Numerical simulation of unsteady flow induced by a flat plate movingnear ground
4. Rae, W. A., Jr., and Pope, Alan, Low-Speed Wind Tunnel Testing, 2nd ed.Wiley, New York, 1984, pp.371and 421.
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