Air flows over a plane wall at Mach 3.5, the pressure in the flow being 100 kPa. The wall turns through an angle leading to the generation of an oblique shock wave whose strength is such that the pressure downstream of the corner is 548 kPa. Find the turning angle of the corner.
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Air flows over a plane wall at Mach 3.5, the pressure in the flow being 100 kPa. The wall turns thro...
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