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A gas turbine burns natural gas assume methane where the

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Reference no: EM13628535

A gas turbine burns natural gas (assume methane) where the air is supplied to the combustor at 1000 kpa, 500 K, and the fuel is at 298K and 1000 kpa. What is the equivalence ratio and the percent theoretical air if the adiabatic flame temperature is limited to 1800 K.

Reference no: EM13628535

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