Flow structure in the wake of a wishbone vortex generator
Author:
Affiliation:
1. NASA Lewis Research Center, Cleveland, Ohio 44135
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.12282
Reference18 articles.
1. Shock-boundary layer interaction control with low-profile vortex generators and passive cavity
2. Exploratory study of vortex-generating devices for turbulent flow separation control
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