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Modern Engineering Thermodynamics

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286 CHAPTER 9: Second Law Open System Applications<br />

EXAMPLE 9.2 (Continued )<br />

The modified energy rate balance equation for this system is<br />

"<br />

_Q<br />

↘<br />

0<br />

− _W<br />

↘<br />

0<br />

+ _m<br />

h 1 − h 2 + ðV 2 1 − V2 2 Þ/2g c + gðZ 1 − Z 2 Þ/g c<br />

⎵<br />

Assuming liquid water is incompressible with a constant specific heat under these conditions and using the incompressible<br />

liquid auxiliary equation for enthalpy (Eq. (6.19)) allows the preceding modifies energy rate balance equation to be<br />

written as<br />

h 2 − h 1 = cT ð 2 − T 1 Þ+ vp ð 2 − p 1 Þ = V1 2 − V2 2 /2gc<br />

0<br />

#<br />

= 0<br />

or<br />

T 2 = T 1 + v ð<br />

c p 1 − p 2 Þ− V2 2 − <br />

V2 1<br />

2cg c<br />

where v = v f (at 50.0°F) = 0.01602 ft 3 /lbm (from Table C.1a of Thermodynamic Tables to accompany <strong>Modern</strong> <strong>Engineering</strong><br />

<strong>Thermodynamics</strong>). From the data given in the problem statement, we can compute V 1 and V 2 as<br />

and<br />

V 1 =<br />

_m = 4 _mv<br />

ρA 1 πD 2 =<br />

1<br />

V 2 = 4 _mv<br />

πD 2 2<br />

40:2000 ð lbm/s Þ 0:01602 ft3 /lbm 144 in: 2 /ft 2<br />

πð1:000 in: Þ 2 = 0:5874 ft/s<br />

2<br />

D<br />

= V 1<br />

1 = ð0:5874Þ<br />

D 2<br />

<br />

1:000<br />

0:2500<br />

2<br />

= 9:399 ft/s<br />

Then,<br />

"<br />

T 2 = ð50:00 + 459:67 RÞ+ 0:01602 ft 3 ð95:00 − 14:70 lbf/in:2Þ 144 in: 2 /ft 2 #<br />

/lbm<br />

½1:0 Btu/ ðlbm.RÞŠð778:17 ft.lbf/BtuÞ<br />

ð9:399Þ 2 − ð0:5874Þ 2 ft 2 /s 2<br />

−<br />

21:0 ½ Btu/ ðlbm.RÞŠ½32:174 lbm.ft/ ðlbf.s 2 ÞŠð778:17 ft.lbf/BtuÞ<br />

= 509:9 − 0:0018 R = 509:9R<br />

and Eq. (9.14) gives 3 _S P = _mc ln T 2<br />

= ð0:2000 lbm/sÞ½1:000 Btu/ ðlbm.RÞŠln 509:9<br />

T 1 509:7<br />

= ½7:846 × 10 −5 Btu/ ðs.RÞŠð778:17 ft.lbf/BtuÞ = 0:0611 ft.lbf/ ðs.RÞ<br />

Notice that the kinetic energy term in this example (0.0018 R) provides a negligible contribution to the exit temperature<br />

and the vast majority of the entropy production results from the pressure loss across the nozzle. The increase in velocity<br />

across the nozzle as converted pressure energy does decrease the entropy production rate slightly (but only by less than<br />

1% in this case). Therefore, this nozzle is quite inefficient at converting pressure energy into kinetic energy. Its efficiency<br />

could be improved, however, by making the nozzle outlet diameter smaller, so that the outlet velocity is substantially<br />

increased.<br />

Exercises<br />

4. Determine the entropy production rate in Example 9.2 if the mass flow rate is increased from 0.2000 to 0.8000 lbm/s.<br />

Recalculate the values of V 1 , V 2 ,andT 2 , then keep the values of all the remaining variables the same as they are in<br />

Example 9.2. Answer: _S P = 0:288 ft.lbf/ ðs.RÞ:<br />

5. Determine the entropy production rate in Example 9.2 if the water hose has been lying in the sun and the water<br />

temperature is 80.00°F rather than 50.00°F. Using v = v sat (80°F), recalculate V 1 , V 2 ,andT 2 , then keep the values of all<br />

the remaining variables the same as they are in Example 9.2. Answer: _S P = 0:068 ft.lbf/ ðs.RÞ:<br />

6. The exit diameter on the nozzle in Example 9.2 is reduced to 0.1250 in. Determine the new entropy production rate<br />

for this system. Keep the values of all the variables except V 2 and T 2 the same as they are in Example 9.2.<br />

Answer: _S P = 0:064 ft.lbf/ ðs.RÞ:<br />

2 To get a meaningful answer, this problem needs to be specified to four significant figures.<br />

3 Note that, without carrying four significant figures in this example, the logarithm is zero.

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