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Turbulence Modeling for Shock Wave/Turbulent Boundary Layer Interactions

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Figure

Figure 1.3. Flowfield cut through the bipod fitting attachment showing Mach contours of a M inf = 3.5 case.
Figure 1.4. Constant axial cut through a M inf = 3.5 case upstream of the bipod attachment fitting.
Figure 1.6. Delta C p between the original bipod design with the foam ramps and the redesigned without the ramp.
Figure 1.7. Difference between surface C p values from SA and SST pre- pre-dictions of a M inf = 2.79 case.
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