Evaluation of turbulence models for three primary types of shock-separated boundary layers
Author:
Affiliation:
1. NASA, Ames Research Center, Moffett Field, Calif.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1977-692
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1. Turbulence stress measurements in a nonadiabatic hypersonic boundarylayer
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1. Turbulence Modeling for Computational Areodynamics;Journal of Spacecraft and Rockets;2003-09
2. An experimental/computational study of heat transfer in sharp fin induced turbulent interactions at Mach 5;22nd Fluid Dynamics, Plasma Dynamics and Lasers Conference;1991-06-24
3. Effect of short regions of surface curvature on compressible turbulent boundary layers;AIAA Journal;1990-01
4. Turbulence structure in a shock wave/turbulent boundary-layer interaction;AIAA Journal;1989-07
5. Response of a compressible, turbulent boundary layer to a short region of surface curvature;AIAA Journal;1989-01
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