Numerical Investigation of Turbulence Models for Shock-Separated Boundary-Layer 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/10.2514/3.60890
Reference5 articles.
1. !Mateer, G. G., Brosh, A., and Viegas, J. R. "A Normal Shock-Wave Turbulent Boundary Layer Interaction at Transonic Speeds,*' AIAA Paper 76-161, Washington, D.C., Jan. 1976.
2. Numerical investigation of turbulence models for shock separated boundary-layer flows
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