432 ENGINEERING THERMODYNAMICS
dharm
\M-therm\Th9-2.pm5
For an isothermal process 1-A :
SA – S 1 = mR loge
V
V
A
1
or SA – S 1 = nR 0 loge
V
V
A
1
= 0.536 × 8.314 × loge
54
18
.
.
= 4.896 kJ/K
For constant volume process A-2 :
SA – S 2 = mcv dT
T
A
z 2
= mcv loge
T
T
1
2
i.e., SA – S 2 = nCv loge
T
T
1
2
= 0.536 × 21.07 × loge
323
316 7.
= 0.222 kJ/K
∴ S 2 – S 1 = (SA – S 1 ) – (SA – S 2 )
= 4.896 – 0.222 = 4.674 kJ/K
Referring to Fig. 9.8, the change of entropy of CO can be found in a similar way to the above,
i.e., S 2 – S 1 = (SB – S 1 ) + (S 2 – SB)
∴ S 2 – S 1 = nR 0 loge
V
V
B
1
+ nCv loge
T
T
2
1
= 0.1478 × 8.314 × loge
54
36
.
. + 0.1478 × 20.86 loge^
316 7
293
.
= 0.498 + 0.239 = 0.737 kJ/K
Hence the change of entropy of the whole system is given by
(S 2 – S 1 )system = ()SS 21 − O 2 + ()SS 21 − CO
i.e., Change of entropy of system = 4.674 + 0.737 = 5.411 kJ/K. (Ans.)
+Example 9.12. Two vessels, A and B, both containing nitrogen, are connected by a
valve which is opened to allow the contents to mix and achieve an equilibrium temperature of
30 °C. Before mixing the following information is known about the gases in the two vessels.
Vessel Pressure (p) Tem. (t) Contents
A 16 bar 55°C 0.6 kg mole
B 6.4 bar 25°C 3.6 kg
(a) Calculate : (i) The final equilibrium pressure ;
(ii) The amount of heat transferred to the surroundings ;
(b) If the vessel had been perfectly insulated, calculate :
(i) The final temperature ;
(ii) The final pressure.
Assume γ = 1.4.
Solution. Refer Fig. 9.9.
Vessel A :
pAVA = nAR 0 TA (where VA = volume of vessel A)