Page 202 - Bird R.B. Transport phenomena
P. 202

186   Chapter 6  Interphase Transport in Isothermal Systems

                            When  these expressions  are substituted  into Eqs.  6.3-5  and  6, it is  then evident  that the
                            friction  factor  in  Eq.  6.3-4  must  have  the  form  f(t)  =  /(Re, t), which,  when  time  aver-
                            aged  over  the turbulent fluctuations,  simplifies  to
                                                             /  = /(Re)                         (6.3-13)
                            by using  arguments similar  to those in §6.2. Hence from  the definition  of the friction  fac-
                            tor  and the dimensionless  form  of the equations  of change and the boundary conditions,
                            we  find  that / must be a function  of  Re alone.
                               Many  experimental  measurements  of  the drag  force  on  spheres  are  available,  and
                            when  these are plotted  in dimensionless  form,  Fig.  6.3-1  results.  For this  system  there  is
                            no  sharp transition from  an unstable laminar flow  curve  to a stable  turbulent flow  curve
                            as  for  long  tubes  at a Reynolds  number  of  about  2100  (see Fig. 6.2-2). Instead, as  the ap-
                            proach  velocity  increases, / varies  smoothly  and moderately up  to Reynolds  numbers  of
                                                                             5
                                        5
                            the  order  of  10 . The kink in the curve at about Re = 2  X 10  is associated  with the shift  of
                            the  boundary  layer  separation zone from  in front  of  the equator to in back  of the equator
                            of the sphere.  1
                               We  have  juxtaposed  the discussions  of  tube  flow  and  flow  around  a sphere  to em-
                            phasize  the fact  that various  flow  systems  behave  quite differently.  Several  points  of  dif-
                            ference between  the two  systems  are:
                                        Flow in  Tubes                     Flow Around Spheres
                            •  Rather well defined  laminar-turbulent  • No well defined  laminar-turbulent
                              transition at about Re = 2100         transition
                            •  The only contribution to / is the friction  • Contributions to / from  both  friction
                              drag                                  and form  drag
                            •  No boundary  layer  separation      • There is a kink  in the/vs.  Re curve
                                                                    associated  with  a shift  in the separation
                                                                    zone
                            The  general  shape  of the curves  in Figs.  6.1-2 and  6.3-1 should be carefully  remembered.
                               For  the creeping flow region, we  already  know  that the drag  force  is  given  by Stokes'
                            law, which  is  a  consequence  of  solving  the  continuity equation  and  the  Navier-Stokes
                            equation  of  motion  without  the pDv/Dt  term.  Stokes'  law  can  be  rearranged  into  the
                            form  of  Eq. 6.1-5  to get

                                                               2
                                                                  2
                                                      F  = T T K ) ( > J L  2 4  )              (6.3-14)
                                                          (
                                                       k                7
                            Hence for  creeping flow around a sphere
                                                       /  = Ц    for  Re <  0.1                 (6.3-15)
                            and  this is the straight-line asymptote as Re —> 0 of the friction  factor  curve  in Fig. 6.3-1.
                               For  higher values  of  the Reynolds number, Eq. 4.2-21  can describe / accurately up to
                            about Re =  1. However, the empirical  expression 2

                                                /  = f  / Ц  + 0.5407 Г  for  Re <  6000        (6.3-16)





                                1
                                 R. K. Adair,  The Physics of Baseball, Harper and Row, New  York  (1990).
                               2
                                F. F. Abraham,  Physics of Fluids, 13,2194  (1970); M. Van  Dyke, Physics of Fluids, 14,1038-1039  (1971).
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