Page 698 - Bird R.B. Transport phenomena
P. 698

678  Chapter 22  Interphase Transport in Nonisothermal Mixtures


                              For the creeping flow around a solid  sphere with a slightly  soluble  coating that dis-
                          solves into the approaching fluid, we may modify  the result in Eq. 12.4-34 to get
                                                     (Зтг) 2/3  Ы у   _
                                                              в х
                                                ' "  2 «Гф
                                               Ли а 8  7
                          This result may be rewritten in terms of the Sherwood  number as
                                                                   (Зтг) 2/3  Ц
                                                                  2  7 / 3  Г ф У \  ^  )\Р®лв)
                                                 =  0.991 (ReSc)  1/3                          (22.2-8)
                          As  in the preceding  subsection  we  have  ReSc to the \-power  for  the gas-liquid  system
                          and  ReSc to the \-power  for the liquid-solid  system.
                              Both  Eq.  22.2-6  and  Eq.  22.2-8  are  valid  only  for  creeping  flow.  However,  they  are
                          not valid in the limit that Re goes  to zero. As  we  know  from  Problem 10B.1 and  Eq. 14.4-
                          5, if there is no flow past  the solid  sphere  or the spherical  bubble,  Sh m  =  2.  It has been
                          found  that a satisfactory  description of the mass  transfer  all the way  down  to Re = 0 can
                          be  obtained by using  the simple  superpositions:  Sh m  = 2 + 0.6415(ReSc) 1/2  and  Sh  =
                                                                                                 w
                                        1/3
                          2  + 0.991 (ReSc)  in lieu  of Eqs. 22.2-6 and 8.
     Mass Transfer in  Steady, Nonseparated Boundary
     Layers on Arbitrarily Shaped  Objects
                          For  systems  with  a  fluid-fluid  interface  and  no  velocity  gradient at the  interface, we
                          found  the mass flux at the surface  to be given  by  Eq. 20.3-14:

                                                      w  г/       (сло0)^, Ас    л            (22.2-9)
                                                                            |ос
                                                           h h\v dx
                                                        Jo  x  s
                          The local Sherwood number is

                                                     ^     L ^        У&±                     (22.2-10)



                                                                           l
                          in which the constant, 1/VTT, is equal to 0.5642 and Re = v p//ji.
                                                                            o
                                                                             o
                              Similarly  for  systems  with  fluid-solid  interfaces  and a velocity  gradient at the inter-
                          face, the mass flux expression is given  in Eq. 20.3-26  as
                                                                          _  o) =  vo  \ r    (22 2-11)
                                                                   \ dx
                                                                   z
                          The analogous Sherwood number expression is

                                                                                              (22.2-1


                                                                                         /
                          where  the numerical coefficient  has the value  0.5384.  In these equations  and v  are a
                                                                                               0
                                                                                          0
                          characteristic length and a characteristic velocity  that can be chosen after  the shape  of
                          the body  has been defined.  Here again we  see that the \-power  on ReSc appears in the
                          fluid-fluid  system,  and  the  \-power  on ReSc  appears  in the  fluid-solid  system—
                          regardless  of the  shape.  The  radicands  of the  Sherwood  number  expressions are
                          dimensionless.
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