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5.3 First Law of Thermodynamics—The Energy Equation 225<br />

Section (1) Control volume Section (2) Pipe<br />

R<br />

r<br />

u max<br />

u max<br />

u 1 = u max 1 -<br />

R<br />

_ r 2<br />

u<br />

[ ( ) ] 2 = u max 1 -<br />

[ ( R<br />

_ r )<br />

2<br />

]<br />

F I G U R E 5.6<br />

developed pipe flow.<br />

Simple, fully<br />

p<br />

Work is transferred<br />

by rotating shafts,<br />

normal stresses,<br />

and tangential<br />

stresses.<br />

τ<br />

^<br />

n<br />

δ W• tangential stress = 0<br />

V<br />

Note that the value of W # normal stress for particles on the wetted inside surface of the pipe is zero because<br />

V nˆ is zero there. Thus, W # normal stress can be nonzero only where <strong>fluid</strong> enters and leaves the<br />

control volume. Although only a simple pipe flow was considered, Eq. 5.62 is quite general and<br />

the control volume used in this example can serve as a general model for other cases.<br />

Work transfer can also occur at the control surface because of tangential stress forces. Rotating<br />

shaft work is transferred by tangential stresses in the shaft material. For a <strong>fluid</strong> particle, shear<br />

stress force power, dW # tangential stress, can be evaluated as the dot product of tangential stress force,<br />

dF tangential stress , and the <strong>fluid</strong> particle velocity, V. That is,<br />

dW # tangential stress dF tangential stress V<br />

For the control volume of Fig. 5.6, the <strong>fluid</strong> particle velocity is zero everywhere on the wetted inside<br />

surface of the pipe. Thus, no tangential stress work is transferred across that portion of the<br />

control surface. Furthermore, if we select the control surface so that it is perpendicular to the <strong>fluid</strong><br />

particle velocity, then the tangential stress force is also perpendicular to the velocity. Therefore,<br />

the tangential stress work transfer is zero on that part of the control surface. This is illustrated in<br />

the figure in the margin. Thus, in general, we select control volumes like the one of Fig. 5.6 and<br />

consider <strong>fluid</strong> tangential stress power transfer to be negligibly small.<br />

Using the information we have developed about power, we can express the first law of thermodynamics<br />

for the contents of a control volume by combining Eqs. 5.59, 5.60, and 5.62 to obtain<br />

0<br />

0t er dV cs<br />

erV nˆ dA Q # net W # shaft cs<br />

pV nˆ dA<br />

cv in net in<br />

(5.63)<br />

When the equation for total stored energy 1Eq. 5.562 is considered with Eq. 5.63, we obtain the<br />

energy equation:<br />

0<br />

0t er dV cs<br />

aǔ p<br />

cv<br />

r V 2<br />

2 gzb rV nˆ dA Q# net W # shaft<br />

in net in<br />

(5.64)<br />

5.3.2 Application of the Energy Equation<br />

In Eq. 5.64, the term 00t cv<br />

er dV represents the time rate of change of the total stored energy,<br />

e, of the contents of the control volume. This term is zero when the flow is steady. This term is<br />

also zero in the mean when the flow is steady in the mean 1cyclical2.<br />

In Eq. 5.64, the integrand of<br />

aǔ p<br />

cs<br />

r V 2<br />

gzb rV nˆ dA<br />

2<br />

can be nonzero only where <strong>fluid</strong> crosses the control surface 1V nˆ 02. Otherwise, V nˆ is zero<br />

and the integrand is zero for that portion of the control surface. If the properties within parentheses,<br />

ǔ, pr, V 2 2, and gz, are all assumed to be uniformly distributed over the flow cross-sectional<br />

areas involved, the integration becomes simple and gives<br />

aǔ p<br />

cs<br />

r V 2<br />

2 gzb rV nˆ dA a aǔ p<br />

flow<br />

r V 2<br />

gzb m#<br />

2<br />

out<br />

aflow<br />

aǔ p (5.65)<br />

r V 2<br />

gzb m#<br />

2<br />

in

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