13.02.2013 Views

Mechanics of Fluids

Mechanics of Fluids

Mechanics of Fluids

SHOW MORE
SHOW LESS

You also want an ePaper? Increase the reach of your titles

YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.

where the hs represent vertical depths <strong>of</strong> liquid in the channel, and the zs<br />

the heights <strong>of</strong> the channel bed above datum level. To take account <strong>of</strong> nonuniformity<br />

<strong>of</strong> velocity over the cross-section, we may write<br />

h1 + z1 + α1u 2 1 /2g − hf = h2 + z2 + α2u 2 2 /2g (10.3)<br />

The rate at which mechanical energy is lost to friction may be expressed<br />

by h f/l, where l represents the length <strong>of</strong> channel over which the head loss<br />

h f takes place. This quantity h f/l may be termed the energy gradient since it<br />

corresponds to the slope <strong>of</strong> a graph <strong>of</strong> the total mechanical energy divided<br />

by weight plotted against distance along the channel. In the special case<br />

<strong>of</strong> uniform flow, u1 = u2, α1 = α2 and h1 = h2 in eqn 10.3. Therefore<br />

h f = z1 − z2. The energy gradient is thus the same as the actual, geometrical,<br />

gradient <strong>of</strong> the channel bed and <strong>of</strong> the liquid surface. This, it must be<br />

emphasized, is true only for uniform flow in open channels. In discussing<br />

non-uniform flow it is important to take note <strong>of</strong> the differences between the<br />

energy gradient, the slope <strong>of</strong> the free surface and the slope <strong>of</strong> the bed.<br />

10.4 STEADY UNIFORM FLOW – THE CHÉZY EQUATION<br />

Steady uniform flow is the simplest type <strong>of</strong> open channel flow to analyse,<br />

although in practice it is not <strong>of</strong> such frequent occurrence as might at first be<br />

supposed. Uniform conditions over a length <strong>of</strong> the channel are achieved only<br />

if there are no influences to cause a change <strong>of</strong> depth, there is no alteration <strong>of</strong><br />

the cross-section <strong>of</strong> the stream, and there is no variation in the roughness <strong>of</strong><br />

the solid boundaries. Indeed, strictly uniform flow is scarcely ever achieved in<br />

practice, and even approximately uniform conditions are more the exception<br />

than the rule. Nevertheless, when uniform flow is obtained the free surface<br />

is parallel to the bed <strong>of</strong> the channel (sometimes termed the invert) and the<br />

depth from the surface to the bed is then termed the normal depth.<br />

The basic formula describing uniform flow is due to the French engineer<br />

Antoine de Chézy (1718–98). He deduced the equation from the results <strong>of</strong><br />

experiments conducted on canals and on the River Seine in 1769. Here,<br />

however, we shall derive the expression analytically.<br />

In steady uniform (or normal) flow there is no change <strong>of</strong> momentum, and<br />

thus the net force on the liquid is zero. Figure 10.5 represents a stretch <strong>of</strong><br />

a channel in which these conditions are found. The slope <strong>of</strong> the channel<br />

is constant, the length <strong>of</strong> channel between the planes 1 and 2 is l and the<br />

(constant) cross-sectional area is A. It is assumed that the stretch <strong>of</strong> the<br />

channel considered is sufficiently far from the inlet (or from a change <strong>of</strong><br />

slope or <strong>of</strong> other conditions) for the flow pattern to be fully developed.<br />

Now the control volume <strong>of</strong> liquid between sections 1 and 2 is acted on by<br />

hydrostatic forces F1 and F2 at the ends. However, since the cross-sections<br />

at 1 and 2 are identical, F1 and F2 are equal in magnitude and have the<br />

same line <strong>of</strong> action; they thus balance and have no effect on the motion <strong>of</strong><br />

the liquid. Hydrostatic forces acting on the sides and bottom <strong>of</strong> the control<br />

volume are perpendicular to the motion, and so they too have no effect.<br />

The only forces we need consider are those due to gravity and the resistance<br />

Steady uniform flow – the Chézy equation 419

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!