The products of combustion enter a convergent nozzle of a jet engine at a total pressure of 125 kPa, and a total temperature of 650 61616 C The atmospheric pressure is 45 kPa and the flow is adiabatic with a rate of 25 kg s Determine the exit area of the nozzle ...

The critical pressure Perit P 125 05 ...

The products of combustion enter a convergent nozzle of a jet engine at a total pressure of

Question:

The products of combustion enter a convergent nozzle of a jet engine at a total pressure of 125 kPa, and a total temperature of 650C. The atmospheric pressure is 45 kPa and the flow is adiabatic with a rate of 25 kg/s. Determine the exit area of the nozzle.