Find the speed and mach number at which aircraft is flying

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Reference no: EM131466946

Question: When an aircraft is flying at subsonic velocity, the pressure at its nose, i.e., at the stagnation point, is found to be 160 kPa. If the ambient pressure and temperature are 100 kPa and 25°C, respectively, find the speed and the Mach number at which the aircraft is flying.

Reference no: EM131466946

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