Question
In an aircraft jet engine at takeoff, the combustion products expand adiabatically in the exhaust nozzle. At entrance to the nozzle, the pressure is 0.180MPa
In an aircraft jet engine at takeoff, the combustion products expand adiabatically in the exhaust nozzle. At entrance to the nozzle, the pressure is
0.180MPa
and the temperature is
1200K
. The kinetic energy of the gas entering the nozzle is very much smaller than the kinetic energy of the gas leaving the nozzle.\ The specific heat of the exhaust gas varies with temperature approximately as follows:\
c_(p)=0.959+1.16\\\\times 10^(-4)T+3.65\\\\times 10^(-8)T^(2),
\ in which the units of
c_(p)
are
k(J)/(k)g*K
and
T
is the temperature in
K
. The molecular weight of the exhaust gas is 30 .\ Supposing the expansion to be frictionless (reversible) as well as adiabatic, show how the exhaust velocity and pressure will depend on the exhaust temperature for a series of values: 1100,1000 , and
900K
. At each temperature determine also the speed of sound
\\\\sqrt(\\\\gamma RT)
.
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