Interactions Between Wholly Laminar or Wholly Turbulent Boundary Layers and Shock Waves Strong Enough to Cause Separation
Author:
Affiliation:
1. National Physical Laboratory, Teddington, England
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.2826
Reference13 articles.
1. The measurement of skin friction in a turbulent boundary layer at a Mach number of 2.5, including the effect of a shock-wave
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