Discuss the below:
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.