Consider air entering a heated duct at P1 = 1 atm and T1 = 288 K. Ignore the effect of friction. Calculate the amount of heat per unit mass (in joules per kilogram) necessary to choke the flow at the exit of the duct, as well as the pressure and temperature at the duct exit, for an inlet Mach number of

(a) M1 = 2.0
(b) M1 = 0.2.

The solution for the given problem is done below.

Explanation:

M1 = 2.0

= 0.3636

= 0.5289

= 0.7934

Isentropic Flow Chart:  M1 = 2.0 , = 1.8

T1 = (1.8)(288K) = 653.4 K.

In order to choke the flow at the exit (M2=1), the above T0* must be stagnation temperature at the exit.

At the inlet,

T02= = (1.8)(288K) = 518.4 K.

Q= Cp(T02-T01) = = 135.7* J/Kg.

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