Page 215 - Bird R.B. Transport phenomena
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§7.1  The Macroscopic Mass Balance  199

                           ity is perpendicular to the  relevant  cross  section,  and  (ii) at planes 1 and 2 the  density
                           and other physical properties are uniform  over the cross section.
                               The law  of conservation  of mass for this system is then
                                                     d
                                                               v
                                                                       v
                                                     T  m tot  =  P\( \)$\  ~ Pi( i)^2          (7.1-1)
                                                     at
                                                     rate of  rate of  rate of
                                                     increase  mass in  mass out
                                                     of mass  at plane 1  at plane 2
                           Here m tot = JpdV  is the total mass of fluid contained  in the system between planes  1 and
                           2. We now  introduce  the  symbol w = p(v)S  for  the mass  rate of flow, and  the  notation
                           Aw = w 2 -  w x (exit value minus entrance value). Then the unsteady-state macroscopic mass
                           balance becomes


                                                          ^-m inl=-bw                           (7.1-2)

                           If the  total  mass of fluid does  not  change  with  time, then  we  get  the  steady-state  macro-
                           scopic mass balance
                                                             Aw  = 0                            (7.1-3)
                           which is just the statement that the rate of mass entering equals the rate of mass leaving.
                               For the macroscopic  mass balance we use the term  "steady  state"  to mean  that  the
                           time derivative on the left side  of Eq. 7.1-2 is zero. Within the system, because  of the pos-
                           sibility  for moving parts, flow instabilities, and  turbulence, there may well be regions of
                           unsteady  flow.


       EXAMPLE   7.1-1     A spherical  tank  of radius R and  its  drainpipe  of length L and  diameter  D are  completely
                           filled  with a heavy oil. At time t = 0 the valve at the bottom  of the drainpipe is opened. How
      Draining of a Spherical  long will it take to drain the tank? There is an air vent at the very top of the spherical tank. Ig-
      Tank                 nore the amount  of oil that clings to the inner surface  of the tank, and assume that the flow in
                           the drainpipe is laminar.

      SOLUTION             We label three planes as in Fig. 7.1-1, and  we let the instantaneous liquid  level above plane 2
                           be h(t). Then, at any time t the total mass of liquid in the sphere is

                                                                     | | j p                    (7.1-4)

                            Airvent

                                              Plane 1






                                              Plane 2








                                              Plane 3  Fig. 7.1-1.  Spherical tank with drainpipe.
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