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Mechanics of Fluids

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The steady-flow energy equation for open channels 417<br />

the mechanical energy divided by weight is represented by the sum <strong>of</strong> three<br />

terms:<br />

p u2<br />

+ + z<br />

ϱg 2g<br />

Now if the streamlines are sensibly straight and parallel – and even in gradually<br />

varied flow the curvature <strong>of</strong> streamlines is usually very slight – there is a<br />

hydrostatic variation <strong>of</strong> pressure over the cross-section. In other words, the<br />

pressure at any point in the stream is governed only by its depth below the<br />

free surface. (Where there is appreciable curvature <strong>of</strong> the streamlines – as<br />

in rapidly varied flow – there are accelerations perpendicular to them, and<br />

consequently differences <strong>of</strong> pressure additional to the hydrostatic variation.<br />

Also, if the slope <strong>of</strong> the channel is exceptionally large, say greater than 1 in<br />

10, there is a modification <strong>of</strong> the hydrostatic pressure variation even when<br />

the streamlines are straight and parallel. This is because lines perpendicular<br />

to the streamlines – along which the piezometric pressure is constant<br />

(Section 3.6) – cannot then be considered vertical.)<br />

When the pressure variation is hydrostatic, a point at which the (gauge)<br />

pressure is p is at a depth p/ϱg below the surface, and so the sum (p/ϱg) + z<br />

(see Fig. 10.2) represents the height <strong>of</strong> the surface above datum level. The<br />

expression for the mechanical energy divided by weight is thus simplified to<br />

Height <strong>of</strong> surface above datum + u 2 /2g (10.1)<br />

We see that the height <strong>of</strong> the individual streamline above datum has no place<br />

in the expression. If it be further assumed that at the section considered the<br />

velocity is the same along all streamlines, then the expression 10.1 has the<br />

same value for the entire stream.<br />

In practice, however, a uniform distribution <strong>of</strong> velocity over a section is<br />

never achieved. The actual velocity distribution in an open channel is influenced<br />

both by the solid boundaries (as in closed conduits such as pipes) and<br />

by the free surface. Bends in the channel and irregularities in the boundaries<br />

also have an effect. The irregularities in the boundaries <strong>of</strong> open channels<br />

are usually so large, and occur in such a random manner, that each channel<br />

has its own peculiar pattern <strong>of</strong> velocity distribution. Nevertheless, it may in<br />

general be said that the maximum velocity usually occurs at a point slightly<br />

below the free surface (at from 0.05 to 0.25 times the full depth) and that<br />

the average velocity, which is usually <strong>of</strong> the order <strong>of</strong> 85% <strong>of</strong> the velocity at<br />

Fig. 10.2

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