An expansion in a gas turbine can be approximated with a

Chapter 7, Problem 204EUP

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Problem 204EUP

An expansion in a gas turbine can be approximated with a polytropic process with exponent n = 1.25. The inlet air is at 2100 R, 120 psia, and the exit pressure is 18 psia with a mass flow rate of 2 lbm/s. Find the turbine heat transfer and power output.

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