In a gas turbine natural gas methane and stoichiometric air

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Reference no: EM13631619

In a gas turbine, natural gas (methane) and stoichiometric air flow into the combustion chamber at 1000kpa, 500K. Secondary air is also at 1000kpa, 500Kpa, is added right after the combustion to result in a product mixture temperature of 1500K. Find the air-fuel ratio mass basis for the primary reactant flow and the ratio of the secondary air to the primary air.

Reference no: EM13631619

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