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396 Chapter 8 ■ Viscous Flow in Pipes D V (1) (2) μ Δp = p 1 – p 2 = F(V, , D, ) Dimensional analysis can be used to put pipe flow parameters into dimensionless form. 8.2.3 From Dimensional Analysis Although fully developed laminar pipe flow is simple enough to allow the rather straightforward solutions discussed in the previous two sections, it may be worthwhile to consider this flow from a dimensional analysis standpoint. Thus, we assume that the pressure drop in the horizontal pipe, ¢p, is a function of the average velocity of the fluid in the pipe, V, the length of the pipe, /, the pipe diameter, D, and the viscosity of the fluid, m, as shown by the figure in the margin. We have not included the density or the specific weight of the fluid as parameters because for such flows they are not important parameters. There is neither mass 1density2 times acceleration nor a component of weight 1specific weight times volume2 in the flow direction involved. Thus, There are five variables that can be described in terms of three reference dimensions 1M, L, T2. According to the results of dimensional analysis 1Chapter 72, this flow can be described in terms of k r 5 3 2 dimensionless groups. One such representation is (8.17) where f1/D2 is an unknown function of the length to diameter ratio of the pipe. Although this is as far as dimensional analysis can take us, it seems reasonable to impose a further assumption that the pressure drop is directly proportional to the pipe length. That is, it takes twice the pressure drop to force fluid through a pipe if its length is doubled. The only way that this can be true is if f1/D2 C/D, where C is a constant. Thus, Eq. 8.17 becomes which can be rewritten as or (8.18) The basic functional dependence for laminar pipe flow given by Eq. 8.18 is the same as that obtained by the analysis of the two previous sections. The value of C must be determined by theory 1as done in the previous two sections2 or experiment. For a round pipe, C 32. For ducts of other cross-sectional shapes, the value of C is different 1see Section 8.4.32. It is usually advantageous to describe a process in terms of dimensionless quantities. To this end we rewrite the pressure drop equation for laminar horizontal pipe flow, Eq. 8.8, as ¢p 32m/VD 2 and divide both sides by the dynamic pressure, rV 2 2, to obtain the dimensionless form as This is often written as where the dimensionless quantity ¢p F1V, /, D, m2 D ¢p mV f a / D b D ¢p mV C/ D ¢p / Cm V D 2 Q AV 1p 4C2 ¢pD 4 m/ ¢p 1 2 rV 132m/V D 2 2 64 a m 2 1 2 rV 2 rVD b a / D b 64 Re a / D b ¢p f / rV 2 D 2 f ¢p1D/21rV 2 22 is termed the friction factor, or sometimes the Darcy friction factor [H. P. G. Darcy (1803–1858)]. 1This parameter should not be confused with the less-used Fanning friction

8.2 Fully Developed Laminar Flow 397 f 10 1 0.1 0.01 10 100 Laminar flow Re 1000 factor, which is defined to be f4. In this text we will use only the Darcy friction factor.2 Thus, the friction factor for laminar fully developed pipe flow is simply f 64 Re (8.19) as shown by the figure in the margin. By substituting the pressure drop in terms of the wall shear stress 1Eq. 8.52, we obtain an alternate expression for the friction factor as a dimensionless wall shear stress f 8t w rV 2 (8.20) Knowledge of the friction factor will allow us to obtain a variety of information regarding pipe flow. For turbulent flow the dependence of the friction factor on the Reynolds number is much more complex than that given by Eq. 8.19 for laminar flow. This is discussed in detail in Section 8.4. 8.2.4 Energy Considerations In the previous three sections we derived the basic laminar flow results from application of F ma or dimensional analysis considerations. It is equally important to understand the implications of energy considerations of such flows. To this end we consider the energy equation for incompressible, steady flow between two locations as is given in Eq. 5.89 p 1 g a 1 V 1 2 2g z 1 p 2 g a 2 V 2 2 2g z 2 h L (8.21) p 1 h L z 1 (1) p 2 (2) z 2 Recall that the kinetic energy coefficients, a 1 and a 2 , compensate for the fact that the velocity profile across the pipe is not uniform. For uniform velocity profiles, a 1, whereas for any nonuniform profile, a 7 1. The head loss term, h L , accounts for any energy loss associated with the flow. This loss is a direct consequence of the viscous dissipation that occurs throughout the fluid in the pipe. For the ideal 1inviscid2 cases discussed in previous chapters, a 1 a 2 1, h L 0, and the energy equation reduces to the familiar Bernoulli equation discussed in Chapter 3 1Eq. 3.72. Even though the velocity profile in viscous pipe flow is not uniform, for fully developed flow it does not change from section 112 to section 122 so that a 1 a 2 . Thus, the kinetic energy is the same at any section 1a 1 V 12 2 a 2 V 22 22 and the energy equation becomes a p 1 g z 1b a p 2 g z 2b h L (8.22) The energy dissipated by the viscous forces within the fluid is supplied by the excess work done by the pressure and gravity forces as shown by the figure in the margin. A comparison of Eqs. 8.22 and 8.10 shows that the head loss is given by h L 2t/ gr 1recall p 1 p 2 ¢p and z 2 z 1 / sin u2, which, by use of Eq. 8.4, can be rewritten in the form The head loss in a pipe is a result of the viscous shear stress on the wall. h L 4/t w gD (8.23) It is the shear stress at the wall 1which is directly related to the viscosity and the shear stress throughout the fluid2 that is responsible for the head loss. A closer consideration of the assumptions involved in the derivation of Eq. 8.23 will show that it is valid for both laminar and turbulent flow.

8.2 Fully Developed Laminar Flow 397<br />

f<br />

10<br />

1<br />

0.1<br />

0.01<br />

10 100<br />

Laminar flow<br />

Re<br />

1000<br />

factor, which is defined to be f4. In this text we will use only the Darcy friction factor.2 Thus,<br />

the friction factor for laminar fully developed pipe flow is simply<br />

f 64<br />

Re<br />

(8.19)<br />

as shown by the figure in the margin.<br />

By substituting the pressure drop in terms of the wall shear stress 1Eq. 8.52, we obtain an alternate<br />

expression for the friction factor as a dimensionless wall shear stress<br />

f 8t w<br />

rV 2<br />

(8.20)<br />

Knowledge of the friction factor will allow us to obtain a variety of information regarding pipe<br />

flow. For turbulent flow the dependence of the friction factor on the Reynolds number is much<br />

more complex than that given by Eq. 8.19 for laminar flow. This is discussed in detail in<br />

Section 8.4.<br />

8.2.4 Energy Considerations<br />

In the previous three sections we derived the basic laminar flow results from application of F ma<br />

or dimensional analysis considerations. It is equally important to understand the implications of<br />

energy considerations of such flows. To this end we consider the energy equation for incompressible,<br />

steady flow between two locations as is given in Eq. 5.89<br />

p 1<br />

g a 1 V 1 2<br />

2g z 1 p 2<br />

g a 2 V 2 2<br />

2g z 2 h L<br />

(8.21)<br />

p 1<br />

<br />

h L<br />

z 1<br />

(1)<br />

p 2 <br />

(2)<br />

z 2<br />

Recall that the kinetic energy coefficients, a 1 and a 2 , compensate for the fact that the velocity<br />

profile across the pipe is not uniform. For uniform velocity profiles, a 1, whereas for any<br />

nonuniform profile, a 7 1. The head loss term, h L , accounts for any energy loss associated with<br />

the flow. This loss is a direct consequence of the viscous dissipation that occurs throughout the<br />

<strong>fluid</strong> in the pipe. For the ideal 1inviscid2 cases discussed in previous chapters, a 1 a 2 1, h L 0,<br />

and the energy equation reduces to the familiar Bernoulli equation discussed in Chapter 3<br />

1Eq. 3.72.<br />

Even though the velocity profile in viscous pipe flow is not uniform, for fully developed<br />

flow it does not change from section 112 to section 122 so that a 1 a 2 . Thus, the kinetic energy<br />

is the same at any section 1a 1 V 12 2 a 2 V 22 22 and the energy equation becomes<br />

a p 1<br />

g z 1b a p 2<br />

g z 2b h L<br />

(8.22)<br />

The energy dissipated by the viscous forces within the <strong>fluid</strong> is supplied by the excess work done<br />

by the pressure and gravity forces as shown by the figure in the margin.<br />

A comparison of Eqs. 8.22 and 8.10 shows that the head loss is given by<br />

h L 2t/<br />

gr<br />

1recall p 1 p 2 ¢p and z 2 z 1 / sin u2, which, by use of Eq. 8.4, can be rewritten in the form<br />

The head loss in a<br />

pipe is a result of<br />

the viscous shear<br />

stress on the wall.<br />

h L 4/t w<br />

gD<br />

(8.23)<br />

It is the shear stress at the wall 1which is directly related to the viscosity and the shear stress<br />

throughout the <strong>fluid</strong>2 that is responsible for the head loss. A closer consideration of the assumptions<br />

involved in the derivation of Eq. 8.23 will show that it is valid for both laminar and turbulent<br />

flow.

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