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26 CHAPTER 9. VISCOUS FLOW<br />
At this point, the radial pressure gradient is not yet specified, and we have<br />
not used the mass conservation equation so far. So the mass conservation<br />
equation can be used to obtain the radial pressure gradient. It is convenient<br />
to integrate the mass conservation equation over the width of the channel to<br />
get<br />
∫ h(r ∗ )<br />
0<br />
dz ∗ 1 r ∗ ∂<br />
∂r ∗r∗∂u∗ r<br />
This can be simplified to provide<br />
1<br />
r ∗<br />
1<br />
∂<br />
r ∗ ∂r ∗r∗<br />
∂<br />
∂r ∗r∗<br />
∂ (<br />
∂r ∗<br />
∫ h(r ∗<br />
∂r + )<br />
∗ 0<br />
∂ ∫ h(r ∗ )<br />
∂r ∗ 0<br />
− h(r∗ ) 3<br />
12<br />
dz ∗∂u∗ z<br />
∂z ∗ = 0 (9.103)<br />
dz ∗ u ∗ r − 1 = 0<br />
∂p ∗ )<br />
− 1 = 0 (9.104)<br />
∂r ∗<br />
This equation can be integrated to provide the radial pressure gradient,<br />
∂p ∗<br />
∂r ∗ = − 6r∗<br />
h(r ∗ ) 3 − C 1<br />
r ∗ h(r ∗ ) 3 (9.105)<br />
The condition that the pressure is finite throughout the channel requires<br />
that the constant C 1 is zero. A second integration with respect to the radial<br />
coordinate provides the pressure.<br />
p ∗ =<br />
3<br />
(1 + (r ∗2 /2)) 2 + C 2 (9.106)<br />
The pressure C 2 is obtained from the condition that the dimensional pressure<br />
scales as (µU/R) in the limit r ∗ → 0, and therefore the scaled pressure is<br />
proportional to ǫ 3 in this limit.<br />
p ∗ =<br />
3<br />
(1 + (r ∗2 /2)) 2 (9.107)<br />
The scaled force in the z ∗ direction is obtained by integrating the axial<br />
component of the product of the stress tensor and the unit normal,<br />
∫<br />
F z = 2π<br />
r dr(T zz n z + T zr n r ) (9.108)