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Old   February 12, 2011, 22:24
Exclamation Stagnation Temperature at Wall
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I am trying to model a hypersonic flow with a laminar flow at the wall (adiabatic) to visualize the boundary layer. When I run the case everything seems fine and I can get a converged solution however the temperature at the wall is significantly higher than the stagnation temperature for the flow and I cant seem to get rid of this, does anyone have any ideas?
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