Page 647 - Bird R.B. Transport phenomena
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§20.2  Steady-State Transport in Binary Boundary Layers  627


                              When  a fast reaction  occurs (or when x is very  large), a series solution in 1 /f  is more ap-
                           propriate. For large f,  we assume that the dominant term is of the form Д = const. • £"' where
                           m < 0. Substitution  of this trial function  into Eq. 20.2-13 then shows that

                                                     A =  (Scf)  -1/2  for large f            (20.2-19)
                           Combination  of  Eqs. 20.2-12 and  19 shows  that,  at  large  distances  from  the  leading  edge,
                           the concentration boundary  layer thickness 8 C = 5Д becomes a constant independent  of  v x
                           and  v.
                              Once  A(£, Sc) is known,  then  the  concentration  profiles  and  the  mass  transfer  rate  at
                           the  surface  may be found.  A more  refined  treatment  of  this problem  has been  given  else-
                           where. 7


       EXAMPLE 20.2-2      The laminar boundary layer on a flat plate (see Fig. 20.2-2) has been a popular system for heat
                           and  mass transfer  studies. In this example, we give an analysis  of subsonic  forced  convection
     Forced Convection  from  in this geometry at high mass-transfer  rates, and discuss the analogies that hold  in this situa-
     a Flat Plate  at High  tion. This example is an extension  of Example 4.4-2.
     Mass-Transfer  Rates
                           SOLUTION
                           Consider  the nonisothermal, steady, two-dimensional flow  of a binary fluid  in the system  of
                           Fig. 20.2-2. The fluid properties p, /л, С , k, and ЯЬ  are considered constant, viscous dissipa-
                                                          р
                                                                   АВ
                           tion  is  neglected, and there are no homogeneous chemical reactions. The Prandtl boundary
                           layer equations for the laminar region are
                           Continuity:                                                         (20.2-20)
                                                     ~дХ  ~ду  ~~
                                                       Sv     Sv
                           Motion:                       x  x   x                              (20.2-21)
                                                                    V
                                                       ST     ST
                           Energy:                               =                             (20.2-22)
                                                       Sx    <Sy
                           Continuity  of A:                  Sa) A  VAB~                     (20.2-23)




                                 Outer flow:  II, = 1  Transition
                                            r
                                   — +    II =1      region
                                            T
                                          II. = 1
                           Line of constant  II -
                                                         Turbulent
                                                         boundary
                                   /    Laminar            layer*
                           У 4   /      boundary                       Fig. 20.2-2. Tangential flow along a
                                /        layer*
                                   Vun                                 sharp-edged semi-infinite flat plate
                                                                       with mass transfer into the stream.
                                                                       The  laminar-turbulent transition
                                                                       usually occurs at a length Reynolds
                             Leading edge                   = 0        number (xv /v)  on the order of
                                                                         5
                                                                             6
                            * The boundary layer below  the plate is omitted here.  10 tol0 .  x  crit


                                P. L. Chambre and J. D. Young,  Physics  of Fluids, 1,48-54 (1958). Catalytic surface  reactions in
                               7
                           boundary  layers  have  been studied by P. L. Chambre and A. Acrivos,  /. Appl.  Phys., 27,1322-1328  (1956).
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