Correlation of separation shock motion with pressure fluctuations inthe incoming boundary layer
Author:
Affiliation:
1. University of Texas at Austin, Austin, Texas 78712
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference15 articles.
1. Unsteady wave structure near separation in a Mach 5 compression rampinteraction
2. Unsteadiness of the Separation Shock Wave Structure in a Supersonic Compression Ramp Flowfield
3. Structure of the wall pressure fluctuations in a shock-induced separated turbulent flow
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