Thermodynamics Mech3001 - Week 5 - Problem 5 (5.25)

5-25 The stators in a gas turbine are designed to increase the kinetic energy of the gas passing through them adiabatically. Air enters a set of these nozzles at 2100 kPa and 370°C with a velocity of 25 m/s and exits at 1750 kPa and 340°C. Calculate the velocity at the exit of the nozzles.