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Mechanics of Fluids

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344 Boundary layers, wakes and other shear layers<br />

the idea <strong>of</strong> mixing length permitted useful progress in the investigation <strong>of</strong><br />

turbulent flow. Similar results are, however, obtainable by more rigorous<br />

methods, and the concept is now largely outmoded.<br />

8.12 VELOCITY DISTRIBUTION IN TURBULENT FLOW<br />

It was Prandtl who first deduced an acceptable expression for the variation<br />

<strong>of</strong> velocity in turbulent flow past a flat plate and in a circular pipe. He<br />

used his mixing length concept (Section 8.11) together with some intuitive<br />

assumptions about its variation with distance from the boundary. Using<br />

somewhat different assumptions, von Kármán and others obtained the same<br />

basic result. The expressions are all semi-empirical in that the values <strong>of</strong><br />

the constant terms have to be determined by experiment but the forms <strong>of</strong><br />

the expressions are derived theoretically.<br />

However, the same results may be obtained from dimensional analysis<br />

without the hypothesis <strong>of</strong> mixing length and in fact with less far-reaching<br />

assumptions. We shall here use this more general method based on dimensional<br />

analysis.<br />

For fully developed turbulent flow in a circular pipe we require primarily<br />

to know the way in which the time-average value <strong>of</strong> the velocity varies<br />

with position in the cross-section. If the flow is steady – in the sense that the<br />

time-average value at a given point does not change with time – then considerations<br />

<strong>of</strong> symmetry indicate that this velocity u is the same at all points at<br />

the same distance from the pipe axis. The independent variables that affect<br />

the value <strong>of</strong> u are the density ϱ and dynamic viscosity µ <strong>of</strong> the fluid, the<br />

radius R <strong>of</strong> the pipe, the position <strong>of</strong> the point (distance y from the pipe wall,<br />

or radius r = R − y from the axis), the roughness <strong>of</strong> the pipe wall – which<br />

may be represented by some characteristic height k <strong>of</strong> the surface bumps (as<br />

in Section 7.3), and the shear stress τ0 at the wall. (The pressure drop divided<br />

by length could be used as a variable in place <strong>of</strong> τ0, as it is simply related<br />

to τ0, but τ0 – here taken as positive – is more convenient for our purpose.)<br />

Application <strong>of</strong> the principles <strong>of</strong> dimensional analysis suggests the following<br />

relation:<br />

�<br />

u<br />

R<br />

= φ1<br />

(τ0/ϱ) 1/2 ν<br />

� �1/2 τ0<br />

ϱ<br />

, y<br />

�<br />

k<br />

,<br />

R R<br />

(8.41)<br />

where ν = µ/ϱ and φ{}means ‘some function <strong>of</strong>’. (Suffixes on the φ symbols<br />

will be used to distinguish one function from another, but in general the form<br />

<strong>of</strong> the function will not be known.)<br />

Noting that (τ0/ϱ) 1/2 has the same dimensions as velocity, it is convenient<br />

to make the substitution<br />

uτ =<br />

� �1/2 τ0<br />

ϱ<br />

where uτ is known as the friction velocity. Its introduction allows velocity<br />

distribution equations to be expressed in simpler and more compact forms.

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