The Effect of Particle Lag on Supersonic Turbulent Boundary Layer Statistics
Author:
Affiliation:
1. Virginia Polytechnic Institute and State University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-0233
Reference32 articles.
1. A numerical study of compressible turbulent boundary layers
2. Turbulence in supersonic boundary layers at moderate Reynolds number
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4. Direct numerical simulation of hypersonic turbulent boundary layers. Part 1. Initialization and comparison with experiments
5. Direct numerical simulation of a supersonic turbulent boundary layer at Mach 2.5
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