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Evaluation of Various Turbulence Models for Shock-Wave Boundary Layer Interaction Flows

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Figure

Figure 1.1: Example of CFD application [4]
Figure 1.2: Schematic of shock-wave boundary layer interaction [4]
Figure 3.1: Verification and validation of Spalart-Allmaras Model in Fluent for 2D zero pressure gradient flat plate flow
Figure 3.2: Verification and validation of SST k-ω model in Fluent for 2D zero pressure gradient flat plate flow0.002500.002550.002600.002650.002700.002750.0028000.0050.010.015 0.02 0.025 0.03 0.035 0.04Cf @ x=0.97h=(1/N)^0.5FUN3DFluent-BaselineOpenFOAM-S
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