CONTACT SURFACE TAILORING IN A CHEMICAL SHOCK TUBE
Author:
Affiliation:
1. University of Toronto, Toronto, Ontario, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.2019
Reference6 articles.
1. The turbulent boundary layer with variable Prandtl number
2. Turbulent Boundary Layer in Compressible Fluids
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