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436 Chapter 8 ■ Viscous Flow in Pipes<br />

SOLUTION<br />

The energy equation 1Eq. 8.212 can be applied between two points<br />

on the surfaces of the reservoirs 1p 1 p 2 V 1 V 2 z 2 02<br />

as follows:<br />

p 1<br />

g V 2 1<br />

2g z 1 p 2<br />

g V 2 2<br />

2g z 2 h L<br />

or<br />

where V QA 4QpD 2 4126 ft 3 s2pD 2 , or<br />

is the velocity within the pipe. 1Note that the units on V and D are<br />

fts and ft, respectively.2 The loss coefficients are obtained from<br />

Table 8.2 and Figs. 8.22 and 8.25 as K Lent 0.5, K Lelbow 0.2,<br />

and K Lexit 1. Thus, Eq. 1 can be written as<br />

or, when combined with Eq. 2 to eliminate V,<br />

To determine D we must know f, which is a function of Re and<br />

eD, where<br />

and<br />

44 ft <br />

V 2<br />

e 1700 f 3410.22 0.5 14 f<br />

2132.2 fts 2 2 D<br />

Re VD n<br />

z 1 V 2<br />

2g af / D a K Lb<br />

V 33.1<br />

D 2<br />

f 0.00152 D 5 0.00135 D<br />

<br />

3133.12 D 2 4D 2.74 106<br />

<br />

5<br />

1.21 10 D<br />

e<br />

D 0.0005<br />

D<br />

where D is in feet. Again, we have four equations 1Eqs. 3, 4, 5, and<br />

the Moody chart or the Colebrook equation2 for the four unknowns<br />

D, f, Re, and eD.<br />

Consider the solution by using the Moody chart. Although<br />

it is often easiest to assume a value of f and make calculations<br />

to determine if the assumed value is the correct one, with the<br />

inclusion of minor losses this may not be the simplest method.<br />

For example, if we assume f 0.02 and calculate D from<br />

Eq. 3, we would have to solve a fifth-order equation. With<br />

only major losses 1see Example 8.122, the term proportional to<br />

D in Eq. 3 is absent, and it is easy to solve for D if f is given.<br />

With both major and minor losses included, this solution<br />

for D 1given f 2 would require a trial-and-error or iterative<br />

technique.<br />

Thus, for this type of problem it is perhaps easier to assume<br />

a value of D, calculate the corresponding f from Eq. 3, and with<br />

the values of Re and eD determined from Eqs. 4 and 5, look up<br />

the value of f in the Moody chart 1or the Colebrook equation2.<br />

The solution is obtained when the two values of f are in agree-<br />

(1)<br />

(2)<br />

(3)<br />

(4)<br />

(5)<br />

ment. A few rounds of calculation will reveal that the solution is<br />

given by<br />

D 1.63 ft<br />

(Ans)<br />

COMMENTS Alternatively, we can use the Colebrook equation<br />

rather than the Moody chart to solve for D. This is easily<br />

done by using the Colebrook equation (Eq. 8.35a) with f as a<br />

function of D obtained from Eq. 3 and Re and eD as functions of<br />

D from Eqs. 4 and 5. The resulting single equation for D can be<br />

solved by using a root-finding technique on a computer or calculator<br />

to obtain D 1 .63 ft. This agrees with the solution obtained<br />

using the Moody chart.<br />

By repeating the calculations for various pipe lengths, /,<br />

the results shown in Fig. E8.13b are obtained. As the pipe<br />

length increases it is necessary, because of the increased friction,<br />

to increase the pipe diameter to maintain the same<br />

flowrate.<br />

It is interesting to attempt to solve this example if all losses are<br />

neglected so that Eq. 1 becomes z 1 0. Clearly from Fig. E8.13a,<br />

z 1 44 ft. Obviously something is wrong. A <strong>fluid</strong> cannot flow<br />

from one elevation, beginning with zero pressure and velocity,<br />

and end up at a lower elevation with zero pressure and velocity<br />

unless energy is removed 1i.e., a head loss or a turbine2 somewhere<br />

between the two locations. If the pipe is short 1negligible<br />

friction2 and the minor losses are negligible, there is still the kinetic<br />

energy of the <strong>fluid</strong> as it leaves the pipe and enters the reservoir.<br />

After the <strong>fluid</strong> meanders around in the reservoir for some<br />

time, this kinetic energy is lost and the <strong>fluid</strong> is stationary. No matter<br />

how small the viscosity is, the exit loss cannot be neglected.<br />

The same result can be seen if the energy equation is written from<br />

the free surface of the upstream tank to the exit plane of the pipe,<br />

at which point the kinetic energy is still available to the <strong>fluid</strong>. In<br />

either case the energy equation becomes z 1 V 2 2g in agreement<br />

with the inviscid results of Chapter 3 1the Bernoulli<br />

equation2.<br />

D, ft<br />

1.8<br />

1.6<br />

1.4<br />

1.2<br />

1.0<br />

0.8<br />

0.6<br />

0.4<br />

0.2<br />

0.0<br />

0 500 1000<br />

, ft<br />

F I G U R E E8.13b<br />

(1700 ft, 1.63 ft)<br />

1500 2000

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