Effects of Leading- and Trailing-Edge Gurney Flaps on a Delta Wing
Author:
Affiliation:
1. Texas A&M University, College Station, Texas 77843-3143
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2507
Reference26 articles.
1. Predictions of vortex-lift characteristics by a leading-edge suctionanalogy
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