Numerical Investigation of UCAV 1303 Configuration with and without Simple Deployable Vortex Flaps
Author:
Affiliation:
1. Naval Air Systems Command
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-2989
Reference8 articles.
1. Ghee, T. "A deployable serrated flap for Air Vehicle Control of a Representative UCAV Configuration",AIAAPaper 2002-3276
2. Recent Enhancements to USM3D Unstructured Flow Solver for Unsteady Flows
3. Spalart P., and Allmaras S. A. "One-equation turbulence model for aerodynamic flows," AIAAPaper 92-0439,January1992.
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