Combustion gases enter a gas turbine at 900C, 800 kPa, and 100 m/s and leave at 650C,
Question:
(a) The exergy of the combustion gases at the turbine inlet and
(b) The work output of the turbine under reversible conditions.
Assume the surroundings to be at 25°C and 100 kPa. Can this turbine be adiabatic?
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Related Book For
Thermodynamics An Engineering Approach
ISBN: 978-0073398174
8th edition
Authors: Yunus A. Cengel, Michael A. Boles
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