An aircraft is cruising at a velocity of 1000 km/h at an altitude of 10 km, where

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An aircraft is cruising at a velocity of 1000 km/h at an altitude of 10 km, where the static temperature and pressure are -50oC and 26.5 kPa, respectively. Determine (a) the Mach number of the aircraft. Also determine (b) the pressure (p) and (c) temperature (T) of the air brought to rest is entropically by a diffuser.
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