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Apply this equation to the fluid element in Figure 2.3 leads to:<br />

P <br />

2 <br />

x<br />

D<br />

2<br />

f u a<br />

14<br />

(2.3)<br />

u u<br />

Since the change in the velocity may be expressed as du dx dt which will<br />

x t<br />

du u dx u u u<br />

give an acceleration of a u . Assuming incompressible<br />

dt x dt t x t<br />

fluid simplifies the velocity and acceleration to be independent to position along the<br />

u conduit. Thus the partial differentiate 0 and acceleration becomes:<br />

x<br />

Thus Eq. (2.3) can be written as:<br />

du<br />

a (2.4)<br />

dt<br />

dP du<br />

dx D dt<br />

2<br />

2 f u (2.5)<br />

dP is the pressure drop across the controlled volume at any time. Integration of Eq. (2.5)<br />

along the conduit length gives the pressure drop on the whole conduit:<br />

2 du 2 du<br />

P (2 f u ) dx (2 f u ) L<br />

(2.6)<br />

D dt D dt<br />

L<br />

Where P is the instantaneous fluctuating pressure drop over the conduit of length L as<br />

a result of velocity fluctuation.<br />

For the model to be able to cope with positive and negative velocity i.e. reverse flow,<br />

term<br />

2<br />

u in Eq. (2.6) may be rewritten asu u , so u alone can be used to determine the<br />

sign of this item and u u together for value. Rearranging Eq. (2.6) gives:<br />

du P<br />

2 f<br />

u u<br />

dt L D<br />

(2.7)<br />

This equation is to calculate the internal flow velocity fluctuation along the changing<br />

pressure drop.

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