A study is to be made using liquid ammonia as the fuel in a gas-turbine engine. Consider
Question:
a) Air enters the compressor at 100 kPa, 25C, and is compressed to 1600 kPa, where the isentropic compressor efficiency is 87%. Determine the exit temperature and the work input per kilo mole.
b) Two kilo moles of liquid ammonia at 25C and x times theoretical air from the compressor enter the combustion chamber. What is x if the adiabatic flame temperature is to be fixed at 1600 K?
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Air P 100 kPa T 25 C b W a ideal compressor process adiabatic reve...View the full answer
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Related Book For 
Fundamentals of Thermodynamics
ISBN: 978-0471152323
6th edition
Authors: Richard E. Sonntag, Claus Borgnakke, Gordon J. Van Wylen
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