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8.3 Fully Developed Turbulent Flow 407<br />

11<br />

10<br />

9<br />

n<br />

8<br />

7<br />

6<br />

5<br />

10 4 10 5 10 6<br />

Re = ____ ρ VD<br />

μ<br />

F I G U R E 8.17 Exponent, n, for power-law velocity profiles.<br />

(Adapted from Ref. 1.)<br />

1.0<br />

n = 10<br />

n = 6<br />

Laminar<br />

n = 8<br />

r __<br />

R<br />

0.5<br />

V8.9 Laminar/<br />

turbulent velocity<br />

profiles<br />

Turbulent<br />

0<br />

0 0.5 1.0<br />

_<br />

__ u<br />

Vc<br />

F I G U R E 8.18<br />

Typical laminar flow and<br />

turbulent flow velocity<br />

profiles.<br />

reasonable approximate results are often obtained by using the inviscid Bernoulli equation and by<br />

assuming a fictitious uniform velocity profile. Since most flows are turbulent and turbulent flows<br />

tend to have nearly uniform velocity profiles, the usefulness of the Bernoulli equation and the uniform<br />

profile assumption is not unexpected. Of course, many properties of the flow cannot be accounted<br />

for without including viscous effects.<br />

E XAMPLE 8.4<br />

Turbulent Pipe Flow Properties<br />

GIVEN Water at 20 °C 1r 998 kgm 3 and n 1.004 <br />

10 6 m 2 s2 flows through a horizontal pipe of 0.1-m diameter<br />

with a flowrate of Q 4 10 2 m 3 s and a pressure gradient of<br />

2.59 kPa m.<br />

<br />

(b) Determine the approximate centerline velocity, V c .<br />

(c) Determine the ratio of the turbulent to laminar shear stress,<br />

t turbt lam , at a point midway between the centerline and the pipe<br />

wall 1i.e., at r 0.025 m2.<br />

FIND (a) Determine the approximate thickness of the viscous<br />

sublayer.

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