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Miscellaneous notes on mass transfer coefficient models

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P.C. Chau (UCSD, 1999)<br />

_____________<br />

Appendix<br />

Derivati<strong>on</strong> 1. Turbulent flow in a tube<br />

In a fully developed turbulent flow, the velocity profile is "flat," and at steady state, we have<br />

U – = U – (z), and C A = C A (z). A steady state differential <strong>mass</strong> balance would lead to the step<br />

0= (UC A ) z –(UC A ) z+dz πR 2 +k(C s –C A )2πRdz (A1)<br />

where the first two terms are the c<strong>on</strong>vective transport in and out of the differential volume, and the<br />

last term is the <strong>mass</strong> transport from the wall with some local <strong>mass</strong> <strong>transfer</strong> <strong>coefficient</strong> k. Recall<br />

that the laminar boundary layer "grows" with distance and hence k = k(z).<br />

We next do a Taylor expansi<strong>on</strong> <strong>on</strong> the z+dz term and if we further assume that U – = c<strong>on</strong>stant,<br />

the <strong>mass</strong> balance becomes<br />

U dC A<br />

dz = 2k<br />

R (C s –C A )<br />

(A2)<br />

We now integrate this equati<strong>on</strong> between the two boundaries C A (0) = C Ao , and C A (L) = C AL :<br />

C L dC A<br />

= 2<br />

(C s –C A ) UR<br />

C o<br />

0<br />

L<br />

k dz<br />

(A3)<br />

The result is<br />

ln C s –C AL<br />

C s –C Ao<br />

=– 2kL<br />

UR<br />

(A4)<br />

where we have introduced the definiti<strong>on</strong><br />

k = 1 L<br />

0<br />

L<br />

k dz<br />

(A5)<br />

as the average (or overall) <strong>mass</strong> <strong>transfer</strong> <strong>coefficient</strong>.<br />

With this result, we could have written Eq. (A2) with the overall <strong>mass</strong> <strong>transfer</strong> <strong>coefficient</strong> as<br />

in Eq. (1), and the integrati<strong>on</strong> would still lead to (A4) since k – is a c<strong>on</strong>stant. Because we could get<br />

away with this sloppiness in the final result, it is <strong>on</strong>e reas<strong>on</strong> why we see people write Eq. (1) even<br />

in research papers. In other words, Eq. (1) is really wr<strong>on</strong>g; (A2) is the proper form. This comment<br />

applies to derivati<strong>on</strong>s below and we will not repeat it.<br />

Derivati<strong>on</strong> 2. Laminar flow in a tube<br />

The derivati<strong>on</strong> for the case of laminar flow is not as straightforward. Now, the axial velocity<br />

and c<strong>on</strong>centrati<strong>on</strong> of species A are functi<strong>on</strong>s of radial positi<strong>on</strong>, u z = u z (z) and C A = C A (r, z). At<br />

steady state, an exercise of differential <strong>mass</strong> balance leads to<br />

0= u z (r)C A (r,z) z –u z (r)C A (r,z) z+dz πR 2 +n A,w (z) 2πRdz (A6)<br />

In c<strong>on</strong>trast to Eq. (A1), we have written the radial and axial dependence explicitly. We also have<br />

used the notati<strong>on</strong> n A,w (z) to denote the local wall flux; the introducti<strong>on</strong> of the <strong>mass</strong> <strong>transfer</strong> model<br />

will be delayed. As analogous to (A2), the next step after (A6) is<br />

d<br />

dz u z(r)C A (r,z) = 2 R n A,w(z)<br />

(A7)<br />

2

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