Investigation of Nonlinear Eddy-Viscosity Turbulence Models in Shock/Boundary-Layer Interaction
Author:
Affiliation:
1. UMIST, Manchester, England M60 1QD, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.983
Reference32 articles.
1. An investigation of transonic turbulent boundary layer separation generated on an axisymmetric flow model
2. Comparison Between Experiment and Prediction for a Transonic Turbulent Separated Flow
3. Transonic, turbulent boundary-layer separation generated on an axisymmetric flow model
4. Experimental investigation of turbulence properties in transonic shock/boundary-layer interactions
5. Shock wave/turbulent boundary layer interaction and its control
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