Liquid octane (C8H18) enters the combustion chamber of a gas turbine steadily at 1 atm and 25°C, and it is burned with air that enters the combustion chamber at the same state. Determine the adiabatic flame temperature for (a) complete combustion with 100% theoretical air, (b) complete combustion with 400% theoretical air, and (c) incomplete combustion with 90% theoretical air.

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