Turbulent properties of a compressible boundary layer.
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.6640
Reference18 articles.
1. A study of turbulence generation in a hypersonic boundary layer
2. On the structure of hypersonic turbulent boundary layers
3. Boundary-layer Pitot and hot-wire surveys at a free-stream Mach number of about 20
4. Hypersonic turbulent boundary-layer measurements using an electron beam.
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