Separation shock motion in fin, cylinder, and compression ramp - Induced turbulent interactions
Author:
Affiliation:
1. University of Texas at Austin, Austin, Texas
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.10173
Reference17 articles.
1. Unsteadiness of the shock wave structure in attached and separated compression ramp flows
2. Characteristic frequencies of transonic diffuser flow oscillations
3. The buffeting pressure field of a high-aspect-ratio swept wing
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