Turbulence model assessment for shock wave/turbulent boundary-layer interaction in transonic and supersonic flows.

DOI10.1016/S0045-7930(99)00010-9zbMath1047.76514MaRDI QIDQ1567006

N. Delaunay

Publication date: 2000

Published in: Computers and Fluids (Search for Journal in Brave)

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Turbulent boundary layers (76F40)

Related Items (5)

Experience of validation and tuning of turbulence models as applied to the problem of boundary layer separation on a finite-width wedge ⋮ Modeling the effect of upstream temperature fluctuations on shock/homogeneous turbulence interaction ⋮ A physically consistent and numerically robust \(k\)-\(\varepsilon\) model for computing turbulent flows with shock waves ⋮ Modeling shock unsteadiness in shock/turbulence interaction ⋮ Anisotropic SST turbulence model for shock-boundary layer interaction

Uses Software

• Spalart-Allmaras

Cites Work

• A new flux splitting scheme
• The method of space-time conservation element and solution element -- a new approach for solving the Navier-Stokes and Euler equations
• Predictions of Channel and Boundary-Layer Flows with a Low-Reynolds-Number Turbulence Model

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