An investigation of the breakdown of the leading edge vortices on a delta wing at high angles of attack
Author:
Affiliation:
1. Notre Dame, University, Notre Dame, IN
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1983-2114
Reference27 articles.
1. Predictions of vortex-lift characteristics by a leading-edge suctionanalogy
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