Expansion in a gas turbine can be approximated with a
Chapter 7, Problem 81HP(choose chapter or problem)
Problem 81HP
Expansion in a gas turbine can be approximated with a polytropic process with exponent n = 1.25. The inlet air is at 1200 K, 800 kPa and the exit pressure is 125 kPa with a mass flow rate of 0.75 kg/s. Find the turbine heat transfer and power output.
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