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For drag flow the velocity gradient is given by<br />

Equation 3.49 can now be written as<br />

If the temperature of the upper plate is T1 and that of lower plate is T0, the temperature<br />

profile of the melt is obtained by integrating Equation 3.51. The resulting expression is<br />

(3.52)<br />

As shown in Section 4.2.3, this equation can be used to calculate the temperature of the<br />

melt film in an extruder.<br />

3.4 Dimensionless Groups<br />

Dimensionless groups can be used to describe complicated processes that are influenced<br />

by a large number of variables with the advantage that the entire process can be analyzed<br />

on a sound basis by means of a few dimensionless parameters. Their use in correlating<br />

experimental data and in scaling-up of equipment is well known.<br />

Table 3.2 shows some of the dimensionless groups often used in plastics engineering.<br />

Table 3.2 Dimensionless Groups<br />

Symbol<br />

Bi<br />

Br<br />

Deb<br />

F0<br />

Gr<br />

Gz<br />

Le<br />

Na<br />

Nu<br />

Pe<br />

Pr<br />

Re<br />

Sh<br />

Sc<br />

Sk<br />

Name<br />

Biot number<br />

Brinkman number<br />

Deborah number<br />

Fourier number<br />

Grashof number<br />

Graetz number<br />

Lewis number<br />

Nahme number<br />

Nusselt number<br />

Peclet number<br />

Prandtl number<br />

Reynolds number<br />

Sherwood number<br />

Schmidt number<br />

Stokes number<br />

Definition<br />

a Xl Xx<br />

7]w 2 1 (AAT)<br />

at It<br />

g/3-ATflv<br />

l 2 l(a-tv)<br />

aid<br />

/3T W 2 T] IX<br />

all X<br />

wll a<br />

v I a<br />

pwll T]<br />

PJIS<br />

vlS<br />

P-II(T]-W)<br />

(3.50)<br />

(3.51)

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