Physics, 01.07.2019 22:30 kellygaytan
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 300 psia and 700°f with a velocity of 82 ft/s and exits at 250 psia and 645°f. calculate the velocity at the exit of the nozzles. the specific heat of air at the average temperature of 672.5°f is cp = 0.253 btu/lbm·r.
Answers: 1
Physics, 22.06.2019 12:30
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