Page 135 - Bird R.B. Transport phenomena
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120   Chapter 4  Velocity Distributions with More Than One Independent Variable

                               Those  readers  who  are  encountering  the method  of  separation  of  variables  for  the
                            first  time  will  have  found  the  above  sequence  of  steps  rather  long  and  complicated.
                            However,  no single step  in the development  is particularly  difficult.  The final  solution  in
                            Eq.  4.1-40 looks  rather  involved  because  of  the  infinite  sum.  Actually,  except  for  very
                            small values  of the time, only the first  few  terms in the series contribute  appreciably.
                               Although  we  do  not prove  it here, the solution  to this  problem  and  that  of  the pre-
                            ceding  problem  are closely related. 2  In the limit  of  vanishingly  small  time, Eq. 4.1-40 be-
                            comes  equivalent  to  Eq.  4.1-15.  This  is  reasonable,  since,  at  very  small  time,  in  this
                            problem  the  fluid  is  in  motion  only  very  near  the  wall  at  у  =  0, and  the  fluid  cannot
                            "feel"  the presence  of the wall at у  = b. Since the solution and result  in Example  4.1-1  are
                            far  simpler  than  those  of  this  one, they  are  often  used  to  represent  the  system  if  only
                            small  times are involved.  This is, of course, an approximation, but a very useful  one. It is
                            often  used  in heat- and mass-transport  problems  as well.

       EXAMPLE 4.1-3        A  semi-infinite body  of  liquid  is bounded on one side by  a plane surface  (the xz-plane). Ini-
                            tially  the fluid and solid  are at rest. At  time t  = 0 the solid  surface  is made to oscillate sinu-
      Unsteady  Laminar     soidally  in  the  x  direction  with  amplitude  X  and  (circular)  frequency  w.  That  is,  the
                                                                   o
      Flow near an          displacement X of the plane from its rest position is
      Oscillating  Plate
                                                           X(f)  = X  sin wt                    (4.1-41)
                                                                 o
                            and the velocity  of the fluid at у  = 0 is then

                                                      V x (0,  t)  =  —r- =  X o  O)  COS O)t   (4.1-42)
                                                              at
                            We designate the amplitude of the velocity oscillation by v 0  = X io and rewrite Eq. 4.1-42 as
                                                                              0
                                                                          iu)t
                                                      ^ ( 0 ,  t) = v  cos  o>t = v dl{e }      (4.1-43)
                                                                       o
                                                              0
                            where Ш{г] means "the real part of z."
                               For oscillating systems  we are generally not interested in the complete solution, but only
                            the  "periodic steady  state" that  exists  after  the initial "transients" have disappeared. In this
                            state  all  the  fluid  particles  in  the system  will  be  executing  sinusoidal  oscillations  with  fre-
                            quency  IO, but with  phase and amplitude that  are functions  only  of  position. This "periodic
                            steady state" solution may be obtained by an elementary technique that is widely  used. Math-
                            ematically it is an asymptotic solution for  t  —>  °o.

      SOLUTION              Once again the equation of motion is given  by

                                                                                                (4.1-44)
                                                                   dy 1
                            and the initial and boundary conditions are given n by
                                                                    by
                            I.C.:               at t <  0,  v x  = 0    for all у               (4.1-45)
                            B.C.I:              aty  = 0,  v  = v       for alH > 0             (4.1-46)
                                                           x   z
                            B.C. 2:             at у  = °°,  v  = 0     for all f > 0           (4.1-47)
                                                           x
                            The initial condition will not be needed, since we  are concerned only with the fluid response
                            after  the plate has been oscillating for a long time.
                                We postulate an oscillatory solution of the form
                                                         v (y, t) =                             (4.1-48)
                                                          x

                                 See H. S. Carslaw and J. C. Jaeger, Conduction of Heat in Solids, Oxford  University Press, 2nd edition
                                2
                            (1959), pp. 308-310, for a series solution that is particularly good for short times.
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