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This is a well known verification model for shock wave capture. A supersonic flow over a 15° ramp is modeled, and because of the ramp, an oblique shock wave is formed. The Inlet Mach number is about 2.5, density is 1.22 kg/m3 and temperature is 289 K.


[1] “ANSY Fluid Dynamics verification Manual”, 2019 R3.