Calculate the exit temperature

Reference no: EM13277969

Air flows through the supersonic nozzle. The inlet conditions are 7 KPa and 420 degree C. The nozzle exit diameter is adjusted such that the exiting velocity is 700m/s. Calculate:

A) the exit temperature

B) mass flow rate

C) the exit diameter Assume an adiabatic quasiequilibrium flow.

Reference no: EM13277969

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