An experimental study of static and dynamic vortex breakdown on slender delta wing planforms
Author:
Affiliation:
1. Notre Dame, Univ., IN
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1994-1879
Reference15 articles.
1. Flow studies of slender wing vortices
2. Prediction of leading-edge vortex breakdown on a delta wing oscillating in roll
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