Compute the exit area of the nozzle, Mechanical Engineering

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Compute the exit area of the nozzle

Solve the below problem:

Q: 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.

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Mechanical Engineering: Compute the exit area of the nozzle

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Mechanical Engineering: Compute the exit area of the nozzle

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