LLaminar-Turbulent Transition behind Discrete Roughness Elements in a High-Speed Boundary Layer
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/10.2514/6.2010-1575
Reference47 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 atMach 6,"AIAAPaper2008-4291,2008.
3. Reda, D.C., Wilder, M. C., and Prabhu, D. K. "Transition Experiments on Blunt Bodies with Isolated Roughness ElementsinHypersonicFreeFlight," AIAA-2010-1367.
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