Prediction of hypersonic shock wave turbulent boundary layer interactions with the k-l two equation turbulence model-Reference-Cited by-同舟云学术

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Prediction of hypersonic shock wave turbulent boundary layer interactions with the k-l two equation turbulence model

Published:1995-01-09 Issue: Volume: Page:
ISSN:
Container-title:33rd Aerospace Sciences Meeting and Exhibit
language:
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Author:

Smith Brian

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1995-232

Reference13 articles.

1. Smith, B. R. "A Near Wall Model for the k - I TwoEquationTurbulenceModel,AIMPaper 94-2386.

2. Van Driest transformation and compressible wall-bounded flows

3. Turbulence models for compressible boundary layers

4. Kussoy,M. I.andHorstman, K. C. "Intersecting Shock-WavemurbulentBoundaq-Layer Interactions at Mach 8.3,NASATM 103909,Feb. 1992.

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