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Mechanics of Fluids

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compensate for the reduction in velocity experienced by the fluid near the<br />

walls, that near the centre must be accelerated. Not until the position C<br />

is reached, however, is the full parabolic distribution established. It is this<br />

final, fully developed form to which the equations we have derived apply.<br />

The parabolic velocity pr<strong>of</strong>ile is theoretically reached only after an infinite<br />

distance; but it is usual to regard the so-called entry length as the distance<br />

along the pipe to the point at which the maximum velocity is only 1% different<br />

from the final value. The way in which the flow thus settles down in the<br />

entry length is discussed in greater detail in Section 7.9. It may, however, be<br />

said here that except in short pipes (i.e. with a length up to about 200 times<br />

the diameter) the different conditions at the inlet to the pipe do not significantly<br />

affect the change <strong>of</strong> pressure over the whole length. No significant<br />

deviation from the parabolic pr<strong>of</strong>ile occurs at the outlet end.<br />

From eqn 6.6 the mean velocity <strong>of</strong> the fluid may be calculated.<br />

Mean velocity = Q<br />

Area =−πR4<br />

8µ<br />

dp∗ �<br />

πR<br />

dx<br />

2 =− R2 dp<br />

8µ<br />

∗<br />

dx<br />

Steady laminar flow in circular pipes 195<br />

(6.9)<br />

From eqn 6.4 we see that the maximum velocity occurs in the centre <strong>of</strong> the<br />

pipe, where r = 0.<br />

∴ umax =− dp∗<br />

�<br />

R<br />

dx<br />

2<br />

�<br />

(6.10)<br />

4µ<br />

Thus, for fully developed laminar flow, the mean velocity is 1<br />

2 umax.<br />

The Hagen–Poiseuille formula has been amply verified by experiment and<br />

it is interesting to note that this agreement between theory and experimental<br />

results is perhaps the principal justification for the assumption that a fluid<br />

continuum does not slip past a solid boundary. The integration constant in<br />

eqn 6.3 had to be determined from the conditions at the wall: if a velocity<br />

other than zero had been assumed, say u0, the value <strong>of</strong> Q given by eqn 6.6<br />

would be increased by an amount πR 2 u0. It is only when u0 is zero that<br />

agreement between theory and experiment is obtained. Newton’s hypothesis<br />

(eqn 6.1) is also <strong>of</strong> course vindicated by the agreement with experimental<br />

results.<br />

Another result which the Hagen–Poiseuille formula verifies is that in laminar<br />

flow the drop in piezometric pressure is proportional directly to the<br />

mean velocity. Moreover, the formula is completely determined by our analysis<br />

and does not involve any additional coefficients that have to be obtained<br />

experimentally – or estimated – for a particular pipe. Thus we should expect<br />

moderate roughness <strong>of</strong> the walls <strong>of</strong> the pipe not to affect laminar flow, and<br />

this conclusion too is confirmed by experiment.<br />

The Hagen–Poiseuille formula was developed on the assumption that<br />

the centre-line <strong>of</strong> the pipe was straight. Slight curvature <strong>of</strong> the centre-line,<br />

in other words, a radius <strong>of</strong> curvature large compared with the radius <strong>of</strong><br />

the pipe, does not appreciably affect the flow through the pipe. For smaller<br />

radii <strong>of</strong> curvature, however, the flow is not accurately described by the<br />

Hagen–Poiseuille formula.

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