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The liquid octane in a gas turbine is burned with 400% excess air that enters the combustion

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The liquid octane in a gas turbine is burned with 400% excess air that enters the combustion chamber at 7 8C. The products of combustion leave the constant-pressure combustion chamber at 707 8C. The fuel flow rate is 0.5 kg/s. Calculate the heat flow rate from the combustion chamber.
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With 400 theoretical air the combustion equation is C 8 H 18 l 50O 2 376N 2 8CO ...View the full answer


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Thermodynamics for Engineers

Thermodynamics for Engineers

ISBN: ?978-1133112860

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Authors: Kenneth A. Kroos, Merle C. Potter

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