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Chapter 9 Viscous flow

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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)

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