Page 184 - Bird R.B. Transport phenomena
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168   Chapter 5  Velocity  Distributions in Turbulent Flow

                           This result may be solved  for  /лЯ/д and the result  can be expressed  in terms  of  dimensionless
                           variables:


                                                           A  dvjdy
                                                           I  т [1 -  (y/R)]  - 1
                                                             о
                                                           f-   dvjdy
                                                           [1  -

                           where  y +  = yv+p/fi  and v +  = vjv*.  When  у  = R/2, the value of y +  is


                                                                                                ( 5 5 9 )
                           For  this value  of y , the logarithmic distribution in the caption of  Fig. 5.5-3 gives
                                         +
                                                        TT  = Ш  =  0-0052                     (5.5-10)
                                                            =
                                                              Ш
                                                              4o5
                                                        dy
                           Substituting this into Eq. 5.5-8 gives


                           This result  emphasizes  that, far  from  the tube wall, molecular momentum transport is  negli-
                           gible in comparison with eddy transport.



     §5.6  TURBULENT      FLOW IN   JETS
                           In the previous  section we  discussed  the flow in ducts, such as circular tubes; such  flows
                           are  examples  of  wall turbulence. Another  main  class  of  turbulent  flows  is free turbulence,
                           and  the main examples  of  these flows are jets and wakes.  The time-smoothed velocity  in
                           these  types  of  flows  can be  described  adequately  by  using  Prandtl's  expression  for  the
                           eddy  viscosity  in  Fig. 5.4-3, or by  using  Prandtl's mixing  length  theory with  the empiri-
                           cism given  in Eq. 5.4-6. The former  method is simpler, and hence we  use  it in the follow-
                           ing illustrative  example.

       EXAMPLE 5.6-1       A jet  of  fluid  emerges  from  a circular hole into a semi-infinite  reservoir  of  the same  fluid  as
                           depicted  in  Fig. 5.6-1. In the same  figure  we  show  roughly  what  we  expect  the profiles  of
      Time-Smoothed        tn  z-component of  the velocity  to look  like.  We  would  expect  that  for  various  values  of  z
      Velocity  Distribution  in fa e  profiles  will be similar  in shape, differing  only  by  a scale  factor  for  distance and  veloc-
                             e
      a Circular Wall  Jer  ity.  We  also  can imagine  that as  the jet  moves  outward, it will  create a net radial  inflow  so
                           that  some  of  the  surrounding  fluid  will  be  dragged  along.  We  want  to  find  the  time-
                           smoothed velocity  distribution in the jet and also the amount of  fluid  crossing  each plane of
                           constant z. Before  working  through the solution, it may  be useful  to review the information
                           on jets  in Table 5.1-1.




                               1
                                H. Schlichting, Boundary-Layer Theory, McGraw-Hill, New York, 7th edition  (1979), pp. 747-750.
                               2
                                A. A. Townsend,  The Structure of Turbulent Shear Flow, Cambridge  University  Press, 2nd edition
                           (1976), Chapter 6.
                               3
                                J. O. Hinze, Turbulence, McGraw-Hill, New York, 2nd edition  (1975), Chapter 6.
                                S. Goldstein, Modern Developments in Fluid Dynamics, Oxford  University  Press  (1938), and Dover
                               4
                           reprint  (1965), pp. 592-597.
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