Calculate the velocity at the exit of the nozzles


The stators in a gas turbine are designed to increase the kinetic energy of the gas passing though them adiabatically. Air enters a set of these nozzles at 200 psia and 695 degrees F with a velocity of 46 ft/s and exits at 145 psia and 650 F. calculate the velocity at the exit of the nozzles.

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Mechanical Engineering: Calculate the velocity at the exit of the nozzles
Reference No:- TGS0717869

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