Engineering, 12.03.2021 21:50 tannerroland
Air flows along a flat wall at a Mach number of 3.5 and a pressure of 100 kPa. The wall turns towards the flow through an angle of 25o leading to the formation of an oblique shock wave. A short distance downstream of this, the wall turns away from the flow through an angle of 25o leading to the generation of an expansion wave causing the flow to be parallel to its original direction. Find the Mach number and pressure downstream of the expansion wave.
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Air flows along a flat wall at a Mach number of 3.5 and a pressure of 100 kPa. The wall turns toward...
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