Numerical simulation of the interaction between a leading-edge vortex and a vertical tail
Author:
Affiliation:
1. USAF, Wright Lab., Wright-Patterson AFB, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1996-2012
Reference58 articles.
1. Some subsonic and transonic buffet characteristics of the twin-vertical-tails of a fighter airplane configuration
2. Shah, G. H. "Wind-Tunnel Investigation of Aerodynamic and Tail Buffet Characteristics of Leading-Edge Extension Modifications to the F/A18," AIAA Paper 91-2889, Aug.1991.
3. Wind-tunnel studies of F/A-18 tail buffet
4. Full-scale high angle-of-attack tests of an F/A-18
5. Washburn, A. E., Jenkins, L. N., and Ferman, M. A. "Experimental Investigation of Vortex-Fin Interaction," AIAA Paper 93-0050, Jan.1993.
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