Wall cooling effects on hypersonic transitional/turbulent boundary layers at high Reynolds numbers
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Va.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.7440
Reference34 articles.
1. Equilibrium layers and wall turbulence
2. A note on von Kármán's constant in low Reynolds number turbulent flows
3. Kinematic eddy viscosity at low Reynolds numbers.
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