The calorific value of a hydrocarbon fuel used in a tubular can-type combustor is 42000 kJ/kg. The fuel is introduced and mixed with air which enters the combustor with a velocity of 75 m/s, pressure of 55 kPa and temperature of 350 K. The proportion of mass of fuel with air is 0.0345. Assuming the thermodynamic properties of the combustion gases to be the same as that of air, calculate the Mach number, pressure and temperature of the combustion products leaving the combustor. [Ans. M2 = 0.64, p2 36.913 kPa, T2 = 1614.47 K] %3D %3D

Elements Of Electromagnetics
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The calorific value of a hydrocarbon fuel used in a tubular can-type combustor is
42000 kJ/kg. The fuel is introduced and mixed with air which enters the combustor with a
velocity of 75 m/s, pressure of 55 kPa and temperature of 350 K. The proportion of mass of
fuel with air is 0.0345. Assuming the thermodynamic properties of the combustion gases to
be the same as that of air, calculate the Mach number, pressure and temperature of the
combustion products leaving the combustor.
[Ans. M2 = 0.64, p2 = 36.913 kPa, T, = 1614.47 K]
%3D
Transcribed Image Text:The calorific value of a hydrocarbon fuel used in a tubular can-type combustor is 42000 kJ/kg. The fuel is introduced and mixed with air which enters the combustor with a velocity of 75 m/s, pressure of 55 kPa and temperature of 350 K. The proportion of mass of fuel with air is 0.0345. Assuming the thermodynamic properties of the combustion gases to be the same as that of air, calculate the Mach number, pressure and temperature of the combustion products leaving the combustor. [Ans. M2 = 0.64, p2 = 36.913 kPa, T, = 1614.47 K] %3D
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