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 ...

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54 The es tima ted accuracy is ± 17% fu"'1d ± 2076 for the jacket and coil respectively. There are five criticisms or limitations to this 1-1ork. 1. The Hall velocity term t.!aS chosen on an unsound basis. 2. The viscosity term in the Reynolds and Prandtl numbers does not take into account changes of apparent viscosity with changes in agitation rate. 3. Only one impeller was used. ~-. The viscosity range covered is limited. 5. The viscosity ratio term does not revert to the one generally accepted for Newtonian fluids as fLoo approaches fLo ltJork of Salamone et al (165) The second Hork on this subject, dealing with jacketed vessels only, was done by J. J. Salamone, A. Cristaldi, and A. Korn. Salamone et ale studied the heat transfer characteristics of power-law pseudoplastics, Hith flow behavior indexes varying from 0.33 to 0.77, in a 12 inch diffi~eter stainless steel vessel, using a four inch flat bladed turbine with six blades. The heat transfer runs Here of the unsteady state variety and the Hilson plot method was used to calculate the batch heat transfer coefficient. The results were cross plotted

ss to (2-46 where ill is the consistency index factor used for flow in pipes (118) .. (2-L~ 7 The generalized Reynolds number range covered was 83 to 1286 and the fluid consistency index, evaluated at the average bulk temperature, ranged from o.ol~_6 to 0.609 Ibfsec~/ft2. Equating the generalized Reynolds number to the NeHtonian Reynolds number Sh01-JS that the apparent viscosity used in the above correlation is 1:Jhich is very similar to the apparent viscosi ty in pipes if N is substituted by V/D. As reported earlier in this chapter, Netzner and his co-workers have experimentally determined that the apparent viscosity in agitated vessels could best be represented by fL ( c' 1\T) n-l a.= K II.:.; l~ (2-25 and that the Reynolds num.ber be expressed as {2-26 The Sal~10ne (165) correlation is an improvement over

54<br />

The es tima ted accuracy is ± 17% fu"'1d ± 2076 <strong>for</strong> the jacket<br />

and coil respectively.<br />

There are five criticisms or limitations to this<br />

1-1ork.<br />

1. The Hall velocity term t.!aS chosen on an unsound<br />

basis.<br />

2. The viscosity term in the Reynolds and Prandtl<br />

numbers does not take into account changes <strong>of</strong> apparent<br />

viscosity with changes in agitation rate.<br />

3. Only one impeller was used.<br />

~-. The viscosity range covered is limited.<br />

5. The viscosity ratio term does not revert to the<br />

one generally accepted <strong>for</strong> Newtonian <strong>fluids</strong> as<br />

fLoo approaches fLo<br />

ltJork <strong>of</strong> Salamone et al (165)<br />

The second Hork on this subject, dealing with jacketed<br />

vessels only, was done by J. J. Salamone, A. Cristaldi, and<br />

A. Korn.<br />

Salamone et ale studied the <strong>heat</strong> <strong>transfer</strong> characteristics<br />

<strong>of</strong> power-law <strong>pseudoplastic</strong>s, Hith flow behavior indexes varying<br />

from 0.33 to 0.77, in a 12 inch diffi~eter<br />

stainless steel<br />

vessel, using a four inch flat bladed turbine with six blades.<br />

The <strong>heat</strong> <strong>transfer</strong> runs Here <strong>of</strong> the unsteady state variety<br />

and the Hilson plot method was used to calculate the <strong>batch</strong><br />

<strong>heat</strong> <strong>transfer</strong> coefficient. The results were cross plotted

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