Page 621 - Bird R.B. Transport phenomena
        P. 621
     §19.5  Dimensional Analysis  of the Equations of Change for Nonreacting Binary Mixtures  601
      EXAMPLE   19.5-1     We  wish  to  predict  the  concentration  distribution  about  a  long  isothermal  cylinder  of  a
                           volatile  solid  Л, immersed  in a gaseous  stream  of  a species  B, which  is  insoluble  in solid  A.
     Concentration         The system  is similar  to that pictured  in Fig. 11.5-1, except that here we  consider the  transfer
     Distribution  about  a  of  mass rather than heat. The vapor  pressure  of the solid  is small  compared to the total pres-
     Long Cylinder         sure in the gas, so that the mass  transfer  system  is virtually  isothermal.
                              Can the results  of Example  11.5-1 be used to make the desired prediction?
     SOLUTION              The results  of  Example  11.5-1  are applicable  if  it can be shown  that suitably  defined  dimen-
                           sionless  concentration profiles  in  the mass  transfer  system  are  identical  to  the temperature
                           profiles  in the heat transfer  system:
                                                       a> (x, y, z) = f(x, y, z)              (19.5-14)
                                                         A
                           This  equality  will  be  realized  if  the  differential  equations  and  boundary  conditions  for  the
                           two systems  can be put into identical form.
                              We  therefore  begin  by  choosing  the same  reference  length, velocity,  and  pressure  as  in
                           Example  11.5-1, and  an analogous  composition function: w  = (w  -  о) )/(со  -  a) ). Here
                                                                          A    A    А0   Ах   A0
                           o)  is the mass  fraction  of A  in the gas  adjacent  to the interface, and o)  is the value  far  from
                            A0                                                     Ax
                           the cylinder.  We  also  specify  that ш А  = со  so  that OJ  = 0. The equations  of  change needed
                                                             А0
                                                                      A
                           here are then Eqs. 19.5-8, 9, and 11. Thus the differential  equations here and in Problem  11.5-1
                           are analogous except for  the viscous  heating term in Eq. 11.5-3.
                              As  for the boundary conditions, we have here:
                           B.C. 1:  as x 2  + у 2  -> °°,   v->8                              (19.5-15)
                                                                x
                           B.C2:   atx-    =               V  = R^1T^^)     -Vu.              (19.5-16)
                                       +  r   5 /
                           B.C. 3:  at*  2  + f  =  oo and у  = 0,  SJ> = 0                   (19.5-17)
                           The boundary condition on v, obtained with the help of Fick's first law, states that there is an
                           interfacial  radial velocity  resulting  from  the sublimation  of  A.
                              If we compare the above description with that for  heat transfer  in Example 11.5-1, we  see
                           that there is no mass  transfer  counterpart of the viscous  dissipation  term in the energy  equa-
                           tion  and  no  heat  transfer  counterpart  to  the  interfacial  radial  velocity  component  in  the
                           boundary  condition of  Eq. 19.5-16.  The descriptions  are otherwise  analogous, however,  with
                           o) , Sc, and Gr  taking the places  of  f,  Pr, and Gr.
                            A         w
                              When  the Brinkman  number  is  sufficiently  small,  viscous  dissipation  will be unimpor-
                           tant, and that term in the energy  equation can be neglected. Neglecting the Brinkman number
                           term is appropriate, except  for  flows  of very viscous  fluids  with large  velocity  gradients, or in
                           hypersonic boundary  layers  (§10.4). Similarly, when (l/ReSc)[(^  -  a) )/(l  -  co )]  is very
                                                                                0
                                                                                             A0
                                                                                    Aoo
                           small, it may be set equal to zero without introducing appreciable error. If these limiting con-
                           ditions  are met, analogous  behavior  will  be  obtained  for  heat and  mass  transfer.  More pre-
                           cisely, the dimensionless  concentration <b  will have the same dependence on x, y, z, t, Re, Pr,
                                                             A
                           and Gr  as the dimensionless temperature T will have on x, y, z, t, Re, Pr, and Gr. The concen-
                                 w
                           tration  and  temperature profiles  will  then be  identical  at a given  Re whenever  Sc  = Pr and
                           Gr w  = Gr.
                              The thermal Grashof number can, at least in principle, be varied  at will be changing  T o  -
                           Т .  Hence it  is  likely  that the desired  Grashof  numbers  can be obtained. However,  it  can be
                            ж
                           seen from  Tables  9.1-1 and  17.1-1 that Schmidt numbers for gases can vary over a considerably
                           wide  range  than can the Prandtl numbers. Hence it  may  be  difficult  to obtain a  satisfactory
                           thermal model of the mass transfer  process, except in a limited range  of the Schmidt number.
                              Another possibly  serious obstacle to achieving  similar heat and mass transfer behavior  is
                           the possible  nonuniformity  of  the surface  temperature. The heat  of  sublimation  must be ob-
                           tained  from  the surrounding gas, and this in turn will cause the solid  temperature to become
                           lower  than that  of  the gas.  Hence it  is  necessary  to consider both heat and mass  transfer  si-
                           multaneously. A very  simple analysis  of simultaneous heat and mass  transfer  is discussed  in
                           the next example.
     	
