Skin friction and velocity profile family for compressible turbulentboundary layers
Author:
Affiliation:
1. Eloret Institute, Palo Alto, California 94303
2. Stanford University, Stanford, California 94305
3. NASA Ames Research Center, Moffett Field, California 94035
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.11820
Reference13 articles.
1. Turbulent Boundary Layer in Compressible Fluids
2. The law of the wake in the turbulent boundary layer
3. On Turbulent Flow Near a Wall
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