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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168 TABLE A-4. SLOPE OF "LOG SHEAR STRESS VERSUS ROTATIONAL SPEED II FLUID TEMPERATURE SLOPE 0 .. 15% Carbopo1 18.5 0.656 25.0 0 .. 651 41 .. 3 0 .. 681. 63 .. 0 0 .. 720 82 .. 0 0 .. 717 0 .. 20% Carbcpol 17.5 0 .. 433 25 .. 0 0 .. 436 ~.2.7 0 .. 422 61.7 0.427 83 .. 8 0.457 18.6 0 .. 370 25 .. 0 0 .. 366 41.8 0 .. 363 59 .. 5 0.374 83.5 0.341

The results are tabulated ~ Table A-5. The flow behavior index~ ~, am~ fluid 00nsisteRey logarithm of the shear stress and Shear rate. T~e results are listed ~ Table A-b. Since the fluid properties were needed as functions of temperature, the fluid eonsistency index was p10tted versus the temperature on semrllogarithmie eeordinates; as suggested by Ferment (63). The poi~ts deseribed a straight line vJhiel3. CaE. be expressed as IGg K :: A + B (T) (A-IO The constamts~ 'A ~d BI were calculated using a linear regression. The flew behavior index was mot very temperature dependent but eould be expressed as m :: C + D (T) (A-II vrhere C and D Here evaluated using a linear regression. The results are given in Table A-7. TABLE A-7 CONSTANTS FOR EQUATIONS A-IO ~d A-il A~;' Fluid B C D C"C- l ) (oC-l) 0.15% Capbopol 0 .. 702 -0 .. 00947 0.631 0.00117 0 .. 20% Carbo])ol 1 .. 607 -0.00bl0 0.423 0.00027 0 .. 24$& CarbQPol 1.906 -0.00308 0.378 -0.00034 ,:. Tke use of tl'il.ese e0l1lsta:mts gives K in. d'J1llles see. Ja jelii1. 2

168<br />

TABLE A-4.<br />

SLOPE OF "LOG SHEAR STRESS VERSUS ROTATIONAL<br />

SPEED II<br />

FLUID TEMPERATURE SLOPE<br />

0 .. 15% Carbopo1 18.5 0.656<br />

25.0 0 .. 651<br />

41 .. 3 0 .. 681.<br />

63 .. 0 0 .. 720<br />

82 .. 0 0 .. 717<br />

0 .. 20% Carbcpol 17.5 0 .. 433<br />

25 .. 0 0 .. 436<br />

~.2.7 0 .. 422<br />

61.7 0.427<br />

83 .. 8 0.457<br />

18.6 0 .. 370<br />

25 .. 0 0 .. 366<br />

41.8 0 .. 363<br />

59 .. 5 0.374<br />

83.5 0.341

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