Question: Air flowing steadily in a nozzle experiences a normal shock at a Mach number of 2.5. If the pressure and temperature of air are 60

Air flowing steadily in a nozzle experiences a normal shock at a Mach number of 2.5. If the pressure and temperature of air are 60 kPa and 273 K, respectively, upstream of the shock, determine
(a) The pressure (p), temperature (T),
(b) Velocity (V),
(c) Mach number and
(d) The total pressure downstream of the shock.

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