Recalibration of the Shear Stress Transport Model to Improve Calculation of Shock Separated Flows
Author:
Affiliation:
1. NASA Glenn Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-685
Reference35 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. Two-equation eddy-viscosity turbulence models for engineering applications
5. Reassessment of the scale-determining equation for advanced turbulence models
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