Page 260 - Modelling in Transport Phenomena A Conceptual Approach
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240   CHAPTER 8.  STEADY MICROSCOPIC BALANCES WITHOUT GEN.

            total momentum flux are expressed as

                                                             dv,
                               rxz = 7,, + (pv,)vx =7,, = -p-                 (8.1-2)
                                                              dx
                               ryz = 7yz + (PVZ) q/ = 0                       (8.1.3)
                               Xzz = Tzz + (PVz) vz = PV,                     (8.1-4)
                                                       2
            For a rectangular differential volume element of thickness Ax, length Ax and width
             W, as shown in Figure 8.1, Eq. (8.1-1) is expressed as
               (~zz.1~ WAX + rxzIx WAZ) - ( rzzIz+Az WAX + rxzIs+Ax wax) = 0  (8.1-5)

             Following the notation introduced by Bird et d. (1960), “in” and ‘‘out’’ directions
             for the fluxes are taken in the direction of  positive x-  and z-axes.  Dividing Eq.
             (8.1-5) by WAX Az and taking the limit as Ax + 0 and AZ + 0 gives







                                                                              (8.1-7)
             Substitution of Eqs. (8.1-2) and (8.1-4) into Eq.  (8.1-7) and noting that dv,/dz = 0
             yields
                                           d
                                              dv,
                                          z (z)                               (8.1-8)
                                                    =O
             The solution of  Eq.  (8.1-8) is
                                          vz = Cl 2 + cz                      (8.1-9)


             where C1 and C2 are constants of integration. The use of the boundary conditions
                                       at  x=O     vz=V                      (8.1-10)

                                       at  x=B      vz=O                     (8.1-11)
             gives the velocity distribution as


                                                                             (8.1-12)

                The use of  the velocity distribution, Eq. (8.1-12), in Eq.  (8.1-2) indicates that
             the shear stress distribution is uniform across the cross-section of  the plate, i.e.,


                                                                             (8.1-13)
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