Determine the ratio of the inlet to exit area, Mechanical Engineering

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Determine the ratio of the inlet to exit area

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Q: At 700 kPa and 120°C enters an adiabatic nozzle steadily with a velocity of 20 m/s and leaves at 400 kPa and 30°C. Determine

(a) The exit velocity and

(b) The ratio of the inlet to exit area A1/A2.

You should solve the given problem step by step.You should include all the units which are needed to solve the given problem.Your steps and calculation should be clear and understanadable.

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Mechanical Engineering: Determine the ratio of the inlet to exit area

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Mechanical Engineering: Determine the ratio of the inlet to exit area

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