Page 179 - Bird R.B. Transport phenomena
P. 179

§5.4  Empirical Expressions  for  the Turbulent Momentum Flux  163

                                      U)
                           in  which  /JL  is  the  turbulent  viscosity  (often  called  the  eddy  viscosity, and  given  the
                           symbol  E). AS one  can  see  from  Table  5.1-1,  for  at  least  one  of  the  flows  given  there,
                           the  circular  jet,  one  might  expect  Eq.  5.4-1  to  be  useful.  Usually,  however,  /x (0  is  a
                           strong  function  of  position  and  the intensity  of  turbulence.  In fact,  for  some  systems  2
                           /x (0  may  even  be  negative  in some  regions.  It must be emphasized  that the viscosity  JJL
                           is  a  property  of  the fluid, whereas  the  eddy  viscosity  /л и)  is  primarily  a  property  of
                           the flow.
                               For  two  kinds  of  turbulent  flows  (i.e., flows  along  surfaces  and  flows  in  jets  and
                                                       U)
                           wakes), special  expressions  for  /JL  are  available:

                           (i)  Wall turbulence:  /x (0  = J  у^Л   0 < Щ- < 5                  (5.4-2)

                           This  expression,  derivable  from  Eq. 5.3-13,  is  valid  only  very  near  the wall.  It is  of  con-
                           siderable  importance  in  the  theory  of  turbulent  heat  and  mass  transfer  at  fluid-solid
                           interfaces. 3
                           (ii)  Free turbulence:     /x  = pK b(v  -  v )                      (5.4-3)
                                                        (0
                                                             0  zmax  z>min
                           in  which  K 0  is  a  dimensionless  coefficient  to  be  determined  experimentally,  b  is  the
                           width  of  the mixing  zone  at a downstream  distance  z, and  the quantity in  parentheses
                           represents  the maximum  difference  in  the z-component  of  the  time-smoothed  veloci-
                                                     4
                           ties  at  that distance  z. Prandtl  found  Eq.  5.4-3  to be  a  useful  empiricism  for  jets  and
                           wakes.

      The  Mixing  Length of  Prandtl

                           By  assuming  that eddies  move  around  in a  fluid  very  much as  molecules  move  around
                                                                         5
                           in a low-density  gas  (not a very good  analogy) Prandtl  developed  an expression  for mo-
                           mentum  transfer  in a turbulent  fluid.  The "mixing  length"  / plays  roughly  the same  role
                           as  the mean  free  path in  kinetic theory  (see  §1.4). This kind  of  reasoning  led  Prandtl to
                           the following  relation:

                                                                      dv r
                                                                                                * ~
                                                                     IT                        (5 4  4)
                           If the mixing  length were  a universal  constant, Eq. 5.4-4  would  be very  attractive, but in
                           fact  / has been found  to be a function  of position. Prandtl proposed  the following  expres-
                           sions  for  /:
                           (i)  Wall turbulence:  / = к^у  (у  = distance from  wall)           (5.4-5)
                           (ii)  Free turbulence:  / = к Ь  (b = width  of mixing  zone)        (5.4-6)
                                                    2
                           in which  K] and  к  are constants. A  result  similar  to Eq. 5.4-4  was  obtained by  Taylor 6  by
                                          2
                           his  "vorticity  transport theory" some years  prior to Prandtl's proposal.




                               2
                                J. O. Hinze, Appl. Sci. Res., 22,163-175  (1970); V. Kruka and S. Eskinazi, /. Fluid. Mech., 20,  555-579
                            (1964).
                               3
                                С  S. Lin, R. W. Moulton, and G. L. Putnam, Ind. Eng.  Chem., 45, 636-640  (1953).
                                L. Prandtl, Zeits.  f. crngew. Math.  u. Mech., 22, 241-243  (1942).
                               4
                                L. Prandtl, Zeits.  f. angew. Math.  u. Mech., 5,136-139 (1925).
                               5
                                G. I. Taylor, Phil. Trans. A215,1-26 (1915), and Proc. Roy. Soc. (London), A135,  685-701  (1932).
                               6
   174   175   176   177   178   179   180   181   182   183   184