The Dassault Falcon aircraft is powered by two TF37 turbofan jet engines. At a cruise condition, each
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The Dassault Falcon aircraft is powered by two TF37 turbofan jet engines. At a cruise condition, each engine consumes fuel at a rate of 0.232 kg/s with a concomitant air consumption of 16.4 kg/s. The fuel blend can be approximated as C12H22, and the air composition can be assumed to be 21% O2 and 79% N2.
A. Determine the equivalence ratio for the combustion process.
B. Determine the composition of the combustion products exiting the combustor assuming complete combustion with no dissociation. Express your results as mole fractions.
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To determine the equivalence ratio we need to compare the actual fueltoair ratio to the stoichiometr...View the full answer
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Related Book For 
Thermodynamics Concepts And Applications
ISBN: 9781107179714
2nd Edition
Authors: Stephen R. Turns, Laura L. Pauley
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