Closed-Loop Flow Control of a Forebody at a High Incidence Angle
Author:
Affiliation:
1. Department of Aeronautics, U.S. Air Force Academy, USAF Academy, Colorado 80840
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J052563
Reference34 articles.
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5. The Asymmetric Vortex Wake Problem - Asking the Right Question
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