Revisiting Turbulence Model Validation for High-Mach Number Axisymmetric Compression Corner Flows
Author:
Affiliation:
1. NASA Glenn Research Center
2. NASA Langley Research Center
3. Wright State University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-0316
Reference21 articles.
1. Overview of the 2010 AIAA Shock Boundary Layer Interaction Workshop
2. Lessons Learned from the 2010 AIAA Shock Boundary Layer Interaction Prediction Workshop
3. Assessment of Computational Fluid Dynamics and Experimental Data for Shock Boundary-Layer Interactions
4. Description of a Website Resource for Turbulence Modeling Verification and Validation
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