Modified Shear-Stress Transport Turbulence Model for Supersonic Flows
Author:
Affiliation:
1. Yeungnam University, Gyeongsangbuk-do, 712-749, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.10223
Reference19 articles.
1. Detailed Study of Attached and Separated Compression Corner Flowfields in High Reynolds Number Supersonic Flow
2. The Baldwin-Lomax Turbulence Model for Two-Dimensional Shock-Wave/Boundary-Layer Interactions
3. Comparison of two-equation turbulence models for boundary layers with pressure gradient
4. An assessment of several turbulence models for supersonic compression ramp flow
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