-. Find the required air-fuel rating in a gas turbine whose turbine and compressor efficiency are
85% and 80%, respectively. Maximum cycle temperature is 875°C. The working fluid can be
taken as air (Cp=1.0kJ/kg.K,y=1.4) which enters the compressor at 1 bar and 27°C. The
pressure ratio is 4. The fuel used has calorific value of 42000kJ/kg. There is a loss of 10% of
calorific value in the combustion chamber.
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