NO PLIF Study of Hypersonic Transition over a Discrete Hemispherical Roughness Element
Author:
Affiliation:
1. NASA Langley Research Center
2. University of Virginia
3. John Hopkins University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-394
Reference17 articles.
1. On the evolution of a turbulent boundary layer induced by a three-dimensional roughness element
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