Sidewall Interaction of a Supersonic Flow over a Compression Ramp
Author:
Affiliation:
1. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-1976
Reference59 articles.
1. Thermoacoustic loads and fatigue of hypersonic vehicle skin panels
2. Direct simulation of the turbulent boundary layer along a compression ramp at M = 3 and Reθ = 1685
3. Direct numerical simulation and analysis of a spatially evolving supersonic turbulent boundary layer at M=2.25
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