Repeat Problem 9.63, but assume a turbine inlet temperature of 1200 K. Problem 9.63 Consider a gas-turbine
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Repeat Problem 9.63, but assume a turbine inlet temperature of 1200 K.
Problem 9.63
Consider a gas-turbine engine operating with 30 kg/s of air entering at 300 K and a pressure ratio of 12.5. Using an ideal air-standard cycle as a model of this engine, determine the ideal thermal efficiency and the net shaft power delivered to the load. Assume the turbine inlet temperature is 1050 K.
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Related Book For
Thermodynamics Concepts And Applications
ISBN: 9781107179714
2nd Edition
Authors: Stephen R. Turns, Laura L. Pauley
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