What will be the mach number in the flow behind the wave

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Reference no: EM131467072

Question: Air is flowing over a flat wall. The Mach number, pressure, and temperature in the air stream are 3, 50 kPa, and -20°C, respectively. If the wall turns "away" from the flow through an angle of 10° leading to the formation of an expansion wave, what will be the Mach number, pressure, and temperature in the flow behind the wave?

Reference no: EM131467072

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