04.11.2014 Views

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

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

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

SHOW MORE
SHOW LESS

You also want an ePaper? Increase the reach of your titles

YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.

neglecting the <strong>heat</strong> capaci ty <strong>of</strong> the 1"all, mus t be <strong>transfer</strong>red<br />

th..rough the wall..<br />

Thus the value <strong>of</strong> ATs-0/ki.l<br />

must equal Ll.Ts_Yl/h. hm and L/lrw are constant over the<br />

H"hole <strong>heat</strong> <strong>transfer</strong> surface and the overall driving <strong>for</strong>ce,<br />

~To' is also constant.. Thus h is greater in a well<br />

agitated portion than in a poorly-agitated portion the total<br />

resistance to <strong>heat</strong> flov! in the <strong>for</strong>mer portion l-Jill be less<br />

than in the latter, giving rise to a greater <strong>heat</strong> flQX in<br />

the well-agitated region.<br />

Since the <strong>heat</strong> flux is higher in the v.iell-agi tated<br />

regions, the ratio,6Ts-IL/ktl' in that region must be<br />

greater than in the poo:r'ly-agi tated l"egions.<br />

Thus the<br />

driving <strong>for</strong>ce across the 1Ajall in the v-rell-agi tated regions<br />

is Greater than in the poorly -agi tated regions..<br />

This phenomena<br />

(Nas manifested by the Hall s1..u"face being closer to the<br />

<strong>batch</strong> temperature in the \.Jell-agi tated regions.<br />

Experimentally it was found that by proper location <strong>of</strong><br />

the impeller the differences in wall temperature could be<br />

virtually eliminated, even at 10VI impeller speeds.<br />

These<br />

positions, surmnarized in Table 5-1, probably gave more<br />

uni<strong>for</strong>m agitation.<br />

It is interesting to note that the Optinlum<br />

posi tion <strong>for</strong> the paddles and turbines is at the level vJhere<br />

about one half <strong>of</strong> the <strong>heat</strong> <strong>transfer</strong> surface is above and one<br />

half beloH the impeller.<br />

The propeller, v-d th its large axial<br />

flow component had to be positioned somewhat higher. These

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!