Turbulence Model for Nonequilibrium Adverse Pressure Gradient Flows
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/10.2514/3.60611
Reference9 articles.
1. !Zwarts, F.J. "The Compressible Turbulent Boundary Layer in a Pressure Gradient," Ph.D. thesis,1970, Dept of Mechanical Engineering, McGill University, Montreal, Canada.
2. An experiment on the adiabatic compressible turbulent boundary layer in adverse and favourable pressure gradients
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