Determine the air velocity at the exit when inlet velocity

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Reference no: EM13718978

The exhaust nozzle of a jet engine expands air at 388 kPa and 174 C adiabatically to 95 kPa. Determine the air velocity at the exit when the inlet velocity is low and the nozzle isentropic efficiency is 96 percent.

Reference no: EM13718978

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