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09: the mass analysis of exhaust gases of the gas turbine engine as: yCO2=0.06264, yH20=0.05125, y02=0.13667 and yNz=0.7494. calculation: (a) the molars weight of burnt
09: the mass analysis of exhaust gases of the gas turbine engine as:
yCO2=0.06264, yH20=0.05125, y02=0.13667 and yNz=0.7494.
calculation: (a) the molars weight of burnt gases (b) the equivalence ratio
(c) the type of fuel (d) adiabatic flame temperature (e) adiabatic flame
temperature if the initial temperature of fresh gases is 323K.
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Elementary Principles of Chemical Processes
Authors: Richard M. Felder, Ronald W. Rousseau
3rd Edition
978-0471687573, 9788126515820, 978-0-471-4152, 0471720631, 047168757X, 8126515821, 978-0471720638
