Page 688 - Bird R.B. Transport phenomena
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668  Chapter 21  Concentration Distributions in Turbulent Flow


      PROBLEMS       21A.1.  Determination  of  eddy  diffusivity  (Figs.  18C.1  and  21A.1).  In Problem  18C.1  we  gave  the
                           formula  for  the concentration profiles  in diffusion  from  a point source in a moving  stream. In
                           isotropic  highly  turbulent  flow,  Eq.  18C.1-2  may  be  modified  by  replacing  ЯЬ АВ  by  the  eddy
                           diffusivity  4b%. This  equation  has  been  found  to  be  useful  for  determining  the  eddy
                           diffusivity.
                           (a)  Show  that if one plots sc A  versus  s  -  z the slope is  —v /24b %.
                                                                             A
                                                                         Q
                           (b)  Use the data  on the diffusion  of CO  from  a point source in a turbulent air stream  shown
                                                           2
                           in Fig. 21 A.I  to get ЯЬ%  for  these conditions: pipe diameter, 15.24 cm; v 0  = 1512 cm/s.
                           (c)  Compare the value  of %b% with  the molecular diffusivity  %b AB  for  the system  CO -air.
                                                                                               2
                           (d)  List all assumptions made in the calculations.
                                                2
                           Answer:  (b) <&%  =  19 cm /s
                     21A.2.  Heat  and  mass transfer analogy.  Write  the mass  transfer  analog  of  Eq. 13.4-19. What  are the
                           limitations  of the resulting  equation?
                     21B.1.  Wall mass flux for  turbulent flow with no  chemical reactions.  Use the diffusional  analog  of
                           Eq.  13.3-7  for  turbulent  flow  in circular  tubes, and  the Blasius  formula  for  the friction  factor,
                           to obtain the following  expression  for  the Sherwood  number,

                                                                    7/8
                                                        Sh = 0.0160 Re Sc 1/3                  (21B.1-1)
                           valid  for  large Schmidt numbers. 1
                     21В.2.  Alternate  expressions  for  the  turbulent  mass flux.  Seek  an  asymptotic  expression  for  the
                           turbulent  mass  flux  for  long  circular  tubes  with  a boundary  condition  of  constant wall  mass
                           flux. Assume  that the net mass  transfer  across the wall is  small.
                           (a)  Parallel the approach to laminar flow  heat transfer  in §10.8 to write

                                                                    Cd  + 11,(0  + C           (21B.2-1)
                                                                                 2
                           in which f  = r/D,^  = (z/D)/ReSc, а>  is the inlet mass  fraction  of A, and  j  is the interfacial
                                                          л]
                                                                                       A 0
                           mass  flux  of A  into the  fluid.


                              1.2

                                                 О
                              1.0
                                                  о
                              0.8           о
                                               4- +  с
                                          с  +    +
                              0.6           +      +              Fig.  21A.1.  Concentration traverse  data  for
                            I            °+          + о          CO  injected  into a turbulent air stream with
                                                                     2
                            "o 0.4      +                         Re = 119,000 in a tube of diameter  15.24 cm.
                                       о               +о
                                      +                           The circles are concentrations at a distance
                                                          +       z = 112.5 cm downstream  from the injection
                              0.2
                                                          о       point, and the crosses  are concentrations at
                                                                  z = 152.7 cm. [Experimental data are taken
                                0
                               -0.6  -0.4  -0.2  0  0.2  0.4  0.6  from  W.  L. Towle and T. K. Sherwood, Ind.
                                            r/R  —                Eng. Chem., 31,457-462  (1939).]



                                 O. T. Hanna, О. С  Sandall, and  C. L. Wilson,  Ind. Eng.  Chem.  Res., 28, 2286-2290  (1987).
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