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Shock Waves in 3D Flow

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Old   October 16, 2013, 22:49
Default Shock Waves in 3D Flow
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For supersonic flow going over a 3D wedge in Fluent, what is the recommended procedure to view the shock waves?

For 2D flow, the shock wave angle is easily found by plotting the pressure coefficient; however, my Cp data is not reliable.
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