Page 216 - Bird R.B. Transport phenomena
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200  Chapter 7  Macroscopic Balances for Isothermal Flow  Systems
                           which can be obtained by using  integral  calculus. Since no  fluid  crosses  plane 1 we know  that
                           w x  — 0. The outlet mass  flow  rate w , as determined from the Hagen-Poiseuille  formula, is
                                                       2
                                                                              A
                                                                          pgl)D p
                                                        128/>tL                                  (7.1-5)
                           The  Hagen-Poiseuille  formula  was derived  for steady-state  flow, but we use it here since the
                           volume  of  liquid  in the tank  is  changing  slowly  with  time; this  is an example  of  a  "quasi-
                           steady-state"  approximation. When  these  expressions  for m  and w  are substituted  into Eq.
                                                                           tot
                                                                                  2
                           7.1-2, we get, after  some rearrangement,
                                                         (2R  -  h)h dh _ ,-p-
                                                          h + L  dt  128/xL                     U    ;
                           We  now abbreviate  the constant on the right side  of  the equation as A. The equation is  easier
                           to integrate if we make the change of variable H = h + L so that
                                                    [H -  (2R + L)](H -L)dH_  A                  ( п л п  ,
                                                            H          df
                           We  now  integrate this equation between  t  = 0 (when h  = 2R or H  = 2R + L), and  £ =  f efflux
                           (when h =  0 or H = L). This gives  for the  efflux  time

                                                                                                 (7.1-8)
                           in which  Л is given  by the right side  of  Eq. 7.1-6. Note that we  have obtained this result with-
                           out  any detailed analysis  of the fluid motion within the sphere.


      §7.2  THE MACROSCOPIC MOMENTUM              BALANCE

                           We  now apply the law  of conservation  of momentum to the system  in Fig. 7.0-1, using the
                           same  two  assumptions  mentioned in  the previous  section, plus  two  additional assump-
                           tions:  (iii)  the  forces  associated  with  the stress  tensor  т  are  neglected  at  planes  1 and  2,
                           since they are generally  small compared to the pressure  forces  at the entry and exit planes,
                           and  (iv) the pressure does not vary  over the cross section at the entry and exit planes.
                               Since momentum is a vector quantity, each term in the balance must be a vector.  We
                           use unit vectors  щ  and u  to represent the direction of flow at planes  1 and  2. The law  of
                                                2
                           conservation  of momentum then reads
                                      j  t  P tot  = р№)Ь\Щ  ~ P ^2>S u  + PiSiUt -  p S u  +  F ^  + m g  (7.2-1)
                                                              2
                                                         2
                                                               2
                                                                            2 2
                                                                          2
                                                                                        tot
                                     rate of  rate of   rate of   pressure  pressure  force of force of
                                     increase of momentum  momentum  force on  force on  solid  gravity
                                     momentum in at plane 1  out at plane 2 fluid at  fluid at  surface on fluid
                                                                  plane 1  plane 2  on fluid
                           Here P  tot  = JpvdV  is the total momentum in the system. The equation states that the total
                           momentum within the system  changes because  of the convection of momentum into and
                           out  of  the system,  and because  of  the various  forces  acting  on the system:  the  pressure
                           forces  at the ends  of  the system, the force  of  the solid  surfaces  acting on the  fluid  in the
                           system,  and  the force  of  gravity  acting on the  fluid  within  the walls  of  the system.  The
                           subscript  "s  —> f"  serves as a reminder of the direction of the force.
                               By introducing the symbols  for the mass rate of flow and the A symbol we  finally  get
                           for the unsteady-state macroscopic momentum balance

                                               |  Ptot = -  д ( | ^  w  + pSju  +  F ^  + m |   (7.2-2)
                                                                                tot
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