Find nozzle inlet temperature and nozzle exit velocity, Mechanical Engineering

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Find nozzle inlet temperature and nozzle exit velocity

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Q: The turbine in a jet engine receives air at 2200 R, 220 lbf/in 2. It exhausts to a nozzle at 35 lbf/in 2, which in turn exhausts to the atmosphere at 14.7 lbf/in 2. The isentropic efficiency of the turbine is 85% and the nozzle efficiency is 95%. Find the nozzle inlet temperature and the nozzle exit velocity. Assume negligible kinetic energy out of the turbine.

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Mechanical Engineering: Find nozzle inlet temperature and nozzle exit velocity

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Mechanical Engineering: Find nozzle inlet temperature and nozzle exit velocity

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