Turbulence Modeling for Shock Wave/Turbulent Boundary Layer Interactions
Randolph P. Lillard
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Turbulence Modeling for Shock Wave/Turbulent Boundary Layer Interactions

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Accurate aerodynamic computational predictions are essential for the safety of space vehicles, but these computations are of limited accuracy when large pressure gradients are present in the flow. The goal of the current project is to improve the state of compressible turbulence modeling for high speed flows with shock wave / turbulent boundary layer interactions (SWTBLI). Emphasis will be placed on models that can accurately predict the separated region caused by the SWTBLI. These flows are classified as nonequilibrium boundary layers because of the very large and variable adverse pressure gr...