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Modern Engineering Thermodynamics

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264 CHAPTER 8: Second Law Closed System Applications<br />

EXAMPLE 8.10 (Continued )<br />

Similarly,<br />

Z<br />

dQ<br />

2ðS P Þ 3 = ms ð 3 − s 2 Þ−<br />

Σ T b<br />

In this process, we are given that dQ = KdT b , where K = 5.00 Btu/R. Therefore, 2 Q 3 = K(T b3 – T b2 )+C = –9.31 Btu, where C is<br />

an integration constant. Then,<br />

Therefore,<br />

Z<br />

Σ<br />

Z<br />

dQ<br />

Tb3<br />

= K<br />

T b T b2<br />

<br />

dT <br />

b<br />

T b<br />

= K ln T b3<br />

T b2<br />

where T b2 = T 2 and T b3 = T 3 .<br />

2ðS P Þ 3<br />

= ms ð 3 − s 2 Þ− K ln T b3<br />

T b2<br />

Now, s 3 = s f 3 + x 3 s fg3 , and from Table C.7b in Thermodynamic Tables to accompany <strong>Modern</strong> <strong>Engineering</strong> <strong>Thermodynamics</strong>, at30.0psia,<br />

we get<br />

Then,<br />

and<br />

s f 3 = 0:0364 Btu/ ðlbm⋅RÞ<br />

s fg3 = 0:2209 Btu/ ðlbm⋅RÞ<br />

s 3 = 0:0364 + ð0:1952Þð0:2209 − 0:0364Þ = 0:07241 Btu/ ðlbm⋅RÞ<br />

2ðS P<br />

Þ 3<br />

= ð0:100 lbm<br />

= 0:976 Btu/R<br />

Finally, the entropy production for the entire process is given by<br />

1ðS P<br />

Þ 3 = 1 ðS P<br />

Þ½0:07241 − 0:2635 Btu/ ðlbm⋅RÞŠ− ð5:00 Btu/RÞln 15:38 + 459:67<br />

120: + 459:67<br />

Þ 2 + 1 ðS P Þ 2 = 4:00 × 10 −4 + 0:976 = 0:976 Btu/R ðto 3 significant figuresÞ<br />

In this example, a special Q = Q(T b ) relation is introduced, which is similar to that used to describe convection heat transfer<br />

processes. These relations, often called thermal constitutive equations, are mathematical models developed to describe specific<br />

heat transfer mechanisms. The following exercises illustrate this concept.<br />

Exercises<br />

17. Find 2 (S P ) 3 in Example 8.10 when T b2 = T b3 = T b = 60.0°C, and 2 Q 3 = –9.31 Btu = constant. Answer: This is not possible<br />

since 2 (S P ) 3 is negative for this process and violates the second law of thermodynamics.<br />

18. Rework part d in Example 8.10 using the relation dQ = K 2 T b dT b , where K 2 = 0.001 Btu/R 2 . Note K 2 is not the same as K<br />

in Example 8.10. Keep all other variables the same as in Example 8.10. You have to reevaluate the integral ∫dQ/T b for<br />

this exercise. Answer: 1 (S P ) 3 = 0.0855 Btu/R.<br />

19. Resolve part d in Example 8.10 for radiation heat transfer where dQ = K 3 T b 3 dT b , where K 3 = 6.30 × 10 –6 . Note that K 4 is<br />

not the same as K in Example 8.10. Keep all other variables the same as in Example 8.10. You have to re-evaluate the<br />

integral ∫dQ/T b for this exercise. Answer: 1 (S P ) 3 = 184 Btu/R.<br />

EXAMPLE 8.11 A CONTINUATION OF EXAMPLE 5.7, WITH THE<br />

ADDITION SHOWN IN ITALIC TYPE<br />

A microwave antenna for a space station consists of a 0.100 m diameter rigid, hollow, steel sphere of negligible wall thickness.<br />

During its fabrication, the sphere undergoes a heat treating operation in which it is initially filled with helium at 0.140 MPa<br />

and 200.°C, then it is plunged into cold water at 15.0°C for exactly 5.00 s. The convective heat transfer coefficient of the sphere<br />

in the water is 3.50 W/(m 2 · K). Neglecting any changes in kinetic or potential energy and assuming the helium behaves as an<br />

ideal gas, determine<br />

a. The final temperature of the helium.<br />

b. The change in total internal energy of the helium.<br />

c. The total entropy production in the helium.

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