Wake Instabilities behind Discrete Roughness Elements in High Speed Boundary Layers
Author:
Affiliation:
1. NASA Langley Research Center
2. North Carolina State University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-81
Reference25 articles.
1. The Effect of Controlled Three-Dimensional Roughness on Boundary-Layer Transition at Supersonic Speeds
2. Casper, K., Wheaton, B., Johnson, H., and Schneider, S. "Effect of Freestream Noise on Roughness-Induced Transition at Mach6,"AIAAPaper 2008-4291,2008.
3. Chang, C., Choudhari, M., and Li, F. "Numerical Computations of Hypersonic Boundary-Layer over Surface Irregularities,"AIAAPaper 2010-1572,2010.
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