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Prediction of batch heat transfer coefficients for pseudoplastic fluids ...

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.3S<br />

The effect <strong>of</strong> using a 10"1 (0,,1.4-) exponent <strong>for</strong> the<br />

viscosi ty ratio also increases the error 1"hen comparing the<br />

eight inch by one inch paddle data (geometrically similar<br />

to Chilton) with Chilton's (39) correlation. Comparing the<br />

date to Chilton's equation there is an average error <strong>of</strong>l:<br />

16.3 percent. Uhl recalculated Chiltonts data and claLms<br />

that the exponent <strong>of</strong> the viscosity ratio should be 0 .. 2.4-<br />

instead <strong>of</strong> 0.14.<br />

Using l;'hl! s modification <strong>of</strong> Chilton I s<br />

equation there is an average deviation <strong>of</strong>± 11.1 percent<br />

between the predicted and measured Nusselt numbers.<br />

The<br />

results are plotted in Figure 6-2.<br />

The points are fairly<br />

evenly distributed along the line <strong>of</strong> perfect agreement.<br />

It ,,,ould be expected that the meaS1.U'ed values vJOuld be<br />

about 10 to 20 percent above the predicted values since Chilton<br />

did not use baffles. However, Chilton measL~ed<br />

the<br />

wall temperature at only one position, just opposite the<br />

impeller. This '--Tould lead to a measured driving <strong>for</strong>ce l--Thich<br />

lIms less than the actual value, causing the calculated<br />

Husselt nu.mbers to be greater than they should be.<br />

Naturally<br />

the correlation based on this data would predict Nusselt<br />

numbers which are too high.<br />

The propeller data were compared w~th Brown's (32)<br />

correlation and are plotted in FigLU'e 6-3. The average<br />

deviation is 26 .. 9 percent and thus the fit is not very good.<br />

ROV-lever, Brown t s correlation is only based on limited data,

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