Aerospace Engineering > GATE 2023 > Combustion
A gas turbine combustor is burning methane and air at an equivalence ratio φ = (F/A)/(F/A)stoich, where φ = 0.5 and (F/A)stoich is the ratio of the mass flow rate of fuel to the mass flow rate of air at stoichiometry. If the air flow rate is ṁair = 20 kg/s, then the mass flow rate of methane is _______ kg/s. (round off to two decimal places)
Correct : 1
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