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8.4 Dimensional Analysis of Pipe Flow 411<br />

y<br />

R = D/2<br />

δ s<br />

Velocity<br />

profile, u = u(y)<br />

Viscous sublayer<br />

x<br />

or<br />

∋<br />

Rough wall<br />

δ s<br />

Smooth wall<br />

∋<br />

F I G U R E 8.19 Flow in the<br />

viscous sublayer near rough and smooth<br />

walls.<br />

of the density than it is of viscosity. Second, we have introduced two additional dimensionless<br />

parameters, the Reynolds number, Re rVDm, and the relative roughness, eD, which are not<br />

present in the laminar formulation because the two parameters r and e are not important in fully<br />

developed laminar pipe flow.<br />

As was done for laminar flow, the functional representation can be simplified by imposing<br />

the reasonable assumption that the pressure drop should be proportional to the pipe length. 1Such<br />

a step is not within the realm of dimensional analysis. It is merely a logical assumption supported<br />

by experiments.2 The only way that this can be true is if the /D dependence is factored out as<br />

¢p<br />

1<br />

2rV / 2 D f aRe, e D b<br />

As was discussed in Section 8.2.3, the quantity ¢pD1/rV 2 22 is termed the friction factor, f. Thus,<br />

for a horizontal pipe<br />

where<br />

¢p f / rV 2<br />

D 2<br />

f f aRe, e D b<br />

(8.33)<br />

The major head<br />

loss in pipe flow is<br />

given in terms of<br />

the friction factor.<br />

For laminar fully developed flow, the value of f is simply f 64Re, independent of eD. For turbulent<br />

flow, the functional dependence of the friction factor on the Reynolds number and the relative<br />

roughness, f f1Re, eD2, is a rather complex one that cannot, as yet, be obtained from a theoretical<br />

analysis. The results are obtained from an exhaustive set of experiments and usually presented<br />

in terms of a curve-fitting formula or the equivalent graphical form.<br />

From Eq. 5.89 the energy equation for steady incompressible flow is<br />

p 1<br />

g a V 1 2<br />

1<br />

2g z 1 p 2<br />

g a V 2 2<br />

2<br />

2g z 2 h L<br />

where h L is the head loss between sections 112 and 122. With the assumption of a constant diameter<br />

1D 1 D 2 so that V 1 V 2 2, horizontal 1z 1 z 2 2 pipe with fully developed flow 1a 1 a 2 2, this<br />

becomes ¢p p 1 p 2 gh L , which can be combined with Eq. 8.33 to give<br />

h L major f / D<br />

V 2<br />

2g<br />

(8.34)

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