Discrete Roughness Effects on Shuttle Orbiter at Mach 6
Author:
Affiliation:
1. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2002-2744
Reference49 articles.
1. Shuttle Orbiter Experimental Boundary-Layer Transition Results with Isolated Roughness
2. Isolated roughness induced boundary-layer transition - Shuttle Orbiter ground tests and flight experience
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