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5.4 Second Law of Thermodynamics—Irreversible Flow 239<br />

shaft work. This application of both Eqs. 5.54 and 5.82 allows us to ascertain the amount of loss that<br />

occurs in incompressible turbomachine flows as is demonstrated in Example 5.28.<br />

E XAMPLE 5.28<br />

Energy—Fan Performance<br />

GIVEN Consider the fan of Example 5.19.<br />

FIND Show that only some of the shaft power into the air<br />

is converted into useful effects. Develop a meaningful efficiency<br />

equation and a practical means for estimating lost shaft<br />

energy.<br />

SOLUTION<br />

We use the same control volume used in Example 5.19. Application<br />

of Eq. 5.82 to the contents of this control volume yields<br />

p 2<br />

r V 2 2<br />

2 gz 2 p 1<br />

r V 2 1<br />

2 gz 1 w shaft loss<br />

net in<br />

As in Example 5.26, we can see with Eq. 1 that a “useful effect”<br />

in this fan can be defined as<br />

useful effect w shaft loss<br />

net in<br />

a p 2<br />

r V 2 2<br />

2 gz 2b a p 1<br />

r V 1 2<br />

2 gz 1b<br />

(1)<br />

(2) (Ans)<br />

In other words, only a portion of the shaft work delivered to the<br />

air by the fan blades is used to increase the available energy of the<br />

air; the rest is lost because of <strong>fluid</strong> friction.<br />

A meaningful efficiency equation involves the ratio of shaft<br />

work converted into a useful effect 1Eq. 22 to shaft work into the<br />

air, w shaft net in . Thus, we can express efficiency, h, as<br />

h <br />

w shaft<br />

net in loss<br />

w shaft<br />

net in<br />

(3)<br />

However, when Eq. 5.54, which was developed from the momentof-momentum<br />

equation 1Eq. 5.422, is applied to the contents of<br />

the control volume of Fig. E5.19, we obtain<br />

w shaft U 2 V u2<br />

net in<br />

Combining Eqs. 2, 3, and 4, we obtain<br />

h 531p 2r2 1V 2 222 gz 2 4<br />

31p 1r2 1V 2 122 gz 1 46U 2 V u2<br />

(4)<br />

(5) (Ans)<br />

Equation 5 provides us with a practical means to evaluate the efficiency<br />

of the fan of Example 5.19.<br />

Combining Eqs. 2 and 4, we obtain<br />

loss U 2 V u2 ca p 2<br />

r V 2 2<br />

2 gz 2b<br />

a p 1<br />

r V 2 1<br />

2 gz 1bd<br />

(6) (Ans)<br />

COMMENT Equation 6 provides us with a useful method of<br />

evaluating the loss due to <strong>fluid</strong> friction in the fan of Example<br />

5.19 in terms of <strong>fluid</strong> mechanical variables that can be measured.<br />

5.4 Second Law of Thermodynamics—Irreversible Flow 5<br />

The second law of<br />

thermodynamics<br />

formalizes the notion<br />

of loss.<br />

The second law of thermodynamics affords us with a means to formalize the inequality<br />

ǔ 2 ǔ 1 q net 0<br />

(5.90)<br />

in<br />

for steady, incompressible, one-dimensional flow with friction 1see Eq. 5.732. In this section we<br />

continue to develop the notion of loss of useful or available energy for flow with friction. Minimization<br />

of loss of available energy in any flow situation is of obvious engineering importance.<br />

5.4.1 Semi-infinitesimal Control Volume Statement<br />

of the Energy Equation<br />

If we apply the one-dimensional, steady flow energy equation, Eq. 5.70, to the contents of a control<br />

volume that is infinitesimally thin as illustrated in Fig 5.8, the result is<br />

m # c dǔ d a p r b d aV2 2 b g 1dz2d dQ# net<br />

in<br />

(5.91)<br />

5 This entire section may be omitted without loss of continuity in the text material.

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