Relationship Between Upstream Turbulent Boundary-Layer Velocity Fluctuations and Separation Shock Unsteadiness
Author:
Affiliation:
1. University of Texas at Austin, Austin, Texas 78712-1085
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1609
Reference29 articles.
1. Some new aspects of the shock-wave/boundary-layer interaction in compression-ramp flows
2. Separation shock motion in fin, cylinder, and compression ramp - Induced turbulent interactions
3. Detection of turbulent boundary-layer separation using fluctuating wall pressure signals
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