Effects of Leading-Edge Shape on the Flow Over 50-deg Delta Wings
Author:
Affiliation:
1. Delft University of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-7330
Reference21 articles.
1. Unsteady aerodynamics of nonslender delta wings
2. Gordnier, R.E. and Visbal, M.R. "High-Order Compact Difference Scheme applied to the Simulationofa Low Sweep Delta Wing Flow," AIAA2003-0620,January2003.
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