Parametric Study of Vortices Shed from Airfoil Vortex Generators
Author:
Affiliation:
1. Modern Technologies Corporation, Middleburg Heights, Ohio 44130-6557
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.3672
Reference28 articles.
1. Improving diffusing S-duct performance by secondary flow control
2. Development of Vortex Generator Use for a Transitioning High-Speed Inlet
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