Twin tail/delta wing configuration buffet due to unsteady vortex breakdown flow
Author:
Affiliation:
1. Old Dominion Univ., Norfolk, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1996-2517
Reference23 articles.
1. Vortex-fin interaction on a fighter aircraft
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