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Mechanics of Fluids

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262 Flow and losses in pipes and fittings<br />

Exit loss<br />

Fig. 7.9<br />

From the energy equation for a constant density fluid we have<br />

p1<br />

ϱg + u2 1<br />

2g + z − hl = p2<br />

ϱg + u2 2<br />

+ z<br />

2g<br />

where h l represents the loss <strong>of</strong> total head between sections 1 and 2.<br />

and substitution from eqn 7.13 gives<br />

∴ hl = p1 − p2<br />

ϱg + u2 1 − u2 2<br />

2g<br />

h l = u2(u2 − u1)<br />

g<br />

+ u2 1 − u2 2<br />

2g<br />

= (u1 − u2) 2<br />

2g<br />

Since by continuity A1u1 = A2u2 eqn 7.14 may be alternatively written<br />

hl = u2 �<br />

1<br />

1 −<br />

2g<br />

A1<br />

A2<br />

� 2<br />

= u2 �<br />

2 A2<br />

2g A1<br />

− 1<br />

� 2<br />

(7.14)<br />

(7.15)<br />

This result was first obtained by J.-C. Borda (1733–99) and<br />

L. M. N. Carnot (1753–1823) and is sometimes known as the Borda–Carnot<br />

head loss. In view <strong>of</strong> the assumptions made, eqns 7.14 and 7.15 are subject<br />

to some inaccuracy, but experiments show that for coaxial pipes they are<br />

within only a few per cent <strong>of</strong>f the truth.<br />

If A2 →∞, then eqn 7.15 shows that the head loss at an abrupt enlargement<br />

tends to u2 1 /2g. This happens at the submerged outlet <strong>of</strong> a pipe discharging<br />

into a large reservoir, for example (Fig. 7.9), or for a duct discharging<br />

to atmosphere. The velocity head in the pipe, corresponding to the kinetic<br />

energy <strong>of</strong> the fluid divided by weight, is thus lost in turbulence in the<br />

reservoir. In such circumstances the loss is usually termed the exit loss for<br />

the pipe.<br />

7.6.2 Loss at abrupt contraction<br />

Although an abrupt contraction (Fig. 7.10) is geometrically the reverse <strong>of</strong> an<br />

abrupt enlargement it is not possible to apply the momentum equation to a<br />

control volume between sections 1 and 2. This is because, just upstream <strong>of</strong>

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