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Extrusion Introduction An extruder is a common machine in industry ...

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Figure 6. Standard cyl<strong>in</strong>drical coord<strong>in</strong>ate<br />

Govern<strong>in</strong>g Equations<br />

Under the assumptions ((a)~(d)), the govern<strong>in</strong>g equations, cont<strong>in</strong>uity equation and the r-<br />

and z-directional momentum equation, for the flow <strong>in</strong> the draw-down region are as<br />

follows:<br />

1 <br />

r r ru<br />

p<br />

r<br />

p<br />

z<br />

<br />

<br />

( ) + w<br />

<br />

z = 0 (1)<br />

1<br />

<br />

<br />

2<br />

u <br />

ru<br />

<br />

<br />

(2)<br />

r<br />

<br />

r r<br />

1<br />

<br />

r<br />

<br />

<br />

2<br />

z <br />

2<br />

w w <br />

r <br />

r r 2<br />

z <br />

(3)<br />

As <strong>in</strong>dicated <strong>in</strong> Figure 5, u and w are the r- and z-directional component of the velocity<br />

vector u. R o (z) and R i (z) are the position of the outer and the <strong>in</strong>ner surface of the tube<br />

that should be also determ<strong>in</strong>ed as the solution along with u, w and p for th<strong>is</strong> free surface<br />

problem.<br />

The boundary conditions at the two free surfaces are follows,<br />

At r = R o (z),<br />

u<br />

<br />

<br />

<br />

<br />

R o<br />

z<br />

<br />

<br />

<br />

w<br />

<br />

0<br />

(4)

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