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Mechanics of Fluids

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124 The principles governing fluids in motion<br />

Fig. 3.22<br />

number <strong>of</strong> the flow, and the location <strong>of</strong> the wall pressure tappings, but, as<br />

it does not depend on what happens beyond the throat, it is little different<br />

from that for a venturi-meter.<br />

A still simpler and cheaper arrangement is a sharp-edged orifice fitted<br />

concentrically in the pipe (Fig. 3.22). Application <strong>of</strong> Bernoulli’s equation<br />

between a point 1 upstream <strong>of</strong> the orifice and the vena contracta (2) gives,<br />

for an inviscid fluid and uniform velocity distribution:<br />

u 2 2<br />

2g = p∗ 1<br />

ϱg − p∗ 2<br />

ϱg + u2 1<br />

2g = �h + u2 1<br />

2g<br />

For a real fluid we introduce a coefficient <strong>of</strong> velocity:<br />

u2 = Cv{2g(�h + u 2 1 /2g)}1/2<br />

(3.24)<br />

We now put u1 = Q/A1 and u2 = Q/Ac = Q/CcAo where Q represents<br />

the discharge, Ac the cross-sectional area <strong>of</strong> the vena contracta, Ao the area<br />

<strong>of</strong> the orifice itself and Cc the coefficient <strong>of</strong> contraction. Then<br />

Q =<br />

CvCcAoA1<br />

(A 2 1 − C2 v C2 c A2 o )1/2 (2g�h)1/2 =<br />

C dAo(2g�h) 1/2<br />

{1 − C 2<br />

d (Ao/A1) 2 } 1/2<br />

since CvCc = Cd (eqn 3.19).<br />

The discharge coefficient C may be introduced by writing<br />

�<br />

1 − (Ao/A1)<br />

C = Cd 2<br />

1 − C2 �1/2 (Ao/A1) 2<br />

d<br />

so that finally<br />

Q =<br />

CAo(2g�h) 1/2<br />

{1 − (Ao/A1) 2 } 1/2

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