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This paper investigates the impact in hypersonic turbulent boundary layer and shock wave interaction simulations due to the uncertainty of the closure coefficients in three commonly use turbulence models. A set of closure coefficients, for each model, are identified as being most significant to several quantities of interest and are consistent with similar studies for different flow regimes.
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This page is a summary of: Analysis of Turbulence Model Uncertainty for Shock-Wave/Boundary-Layer Interaction Simulations, Journal of Spacecraft and Rockets, November 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.a34770.
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