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Transport Phenomena.pdf

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§1.2 Generalization of Newton's Law of Viscosity 17<br />

any instant of time we can slice the volume element in such a way as to remove half the<br />

fluid within it. As shown in the figure, we can cut the volume perpendicular to each of<br />

the three coordinate directions in turn. We can then ask what force has to be applied on<br />

the free (shaded) surface in order to replace the force that had been exerted on that surface<br />

by the fluid that was removed. There will be two contributions to the force: that associated<br />

with the pressure, and that associated with the viscous forces.<br />

The pressure force will always be perpendicular to the exposed surface. Hence in (a)<br />

the force per unit area on the shaded surface will be a vector pb x<br />

—that is, the pressure (a<br />

scalar) multiplied by the unit vector 8 r<br />

in the x direction. Similarly, the force on the<br />

shaded surface in (b) will be pb y<br />

, and in (c) the force will be pb z<br />

. The pressure forces will<br />

be exerted when the fluid is stationary as well as when it is in motion.<br />

The viscous forces come into play only when there are velocity gradients within the<br />

fluid. In general they are neither perpendicular to the surface element nor parallel to it,<br />

but rather at some angle to the surface (see Fig. 1.2-1). In (a) we see a force per unit area<br />

т г<br />

exerted on the shaded area, and in (b) and (c) we see forces per unit area т у<br />

and T Z<br />

.<br />

Each of these forces (which are vectors) has components (scalars); for example, т х<br />

has<br />

components T rt<br />

, i xy<br />

, and T XZ<br />

. Hence we can now summarize the forces acting on the three<br />

shaded areas in Fig. 1.2-1 in Table 1.2-1. This tabulation is a summary of the forces per<br />

unit area (stresses) exerted within a fluid, both by the thermodynamic pressure and the<br />

viscous stresses. Sometimes we will find it convenient to have a symbol that includes both<br />

types of stresses, and so we define the molecular stresses as follows:<br />

TTjj = p8jj + Tjj where i and / may be x, y, or z (1.2-2)<br />

Here 8ц is the Kronecker delta, which is 1 if i = j and zero if i Ф j.<br />

Just as in the previous section, the т {]<br />

(and also the тг ()<br />

) may be interpreted in two ways:<br />

ттц = pdij + Ту = force in the; direction on a unit area perpendicular to the i direction,<br />

where it is understood that the fluid in the region of lesser x, is exerting<br />

the force on the fluid of greater x {<br />

iTjj = p8jj + Tjj = flux of y-momentum in the positive i direction—that is, from the region<br />

of lesser x x<br />

to that of greater x- x<br />

Both interpretations are used in this book; the first one is particularly useful in describing<br />

the forces exerted by the fluid on solid surfaces. The stresses ir xx<br />

= p + r XXf<br />

тг уу<br />

= p +<br />

T<br />

yy/ ^zz — V + T zz a r e called normal stresses, whereas the remaining quantities, тг ху<br />

= т ху<br />

,<br />

n yz<br />

= r yzf<br />

... are called shear stresses. These quantities, which have two subscripts associated<br />

with the coordinate directions, are referred to as "tensors," just as quantities (such<br />

as velocity) that have one subscript associated with the coordinate directions are called<br />

Table 1.2-1 Summary of the Components of the Molecular Stress Tensor (or Molecular<br />

Momentum-Flux Tensor)"<br />

Direction<br />

Components of the forces (per unit area)<br />

normal Vector force<br />

acting o n the s h a d e d face ( c o m p o n e n t s of the<br />

to the per unit area on the momentum flux through the shaded face)<br />

shaded shaded face (momentum<br />

face flux through shaded face) x-component y-component z-component<br />

a<br />

These are referred to as components of the "molecular momentum flux tensor" because they are<br />

associated with the molecular motions, as discussed in §1.4 and Appendix D. The additional "convective<br />

momentum flux tensor" components, associated with bulk movement of the fluid, are discussed in §1.7.

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