Effect of Surface Roughness on Unseparated Shock-Wave/Turbulent Boundary-Layer Interactions
Author:
Affiliation:
1. University of Cambridge, Cambridge, England CB2 1PZ, United Kingdom
2. Iowa State University, Ames, Iowa 50011-3231
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1825
Reference13 articles.
1. Wedge-induced turbulent boundary-layer separation on a roughened surface at Mach 6.0
2. Supersonic shock/turbulent boundary-layer interaction on a roughened surface
3. Large-Scale Roughness Influence on Turbulent Hypersonic Boundary Layers Approaching Compression Corners
4. An experimental study of transonic shock/turbulent boundary layer interaction on a roughened surface
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