Dynamic LEX/forebody vortex interaction effects
Author:
Affiliation:
1. Lockheed Missiles and Space Co., Inc., Sunnyvale, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1992-2732
Reference16 articles.
1. Effects of transition on wind tunnel simulation of vehicel dynamics
2. Experimental study of effects of forebody geometry on high angle-of-attack stability
3. Wing rock generated by forebody vortices
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