Page 475 - Bird R.B. Transport phenomena
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§15.1  The Macroscopic Energy  Balance  455

                            (total) energy  balance. Next in  §15.3 we  give the simplified  versions  of  the macroscopic
                           balances  for  steady-state  systems and illustrate their use.
                               In §15.4 we  give the differential  forms  W-forms)  of the steady-state balances. In these
                            forms, the entry and exit planes  1 and 2 are taken to be only  a differential  distance apart.
                            The  "d-forms"  are  frequently  useful  for  problems  involving  flow  in  conduits  in  which
                            the velocity,  temperature, and pressure  are continually changing  in the flow direction.
                               Finally, in §15.5 we  present several illustrations  of  unsteady-state  problems  that can
                           be solved by  the macroscopic balances.
                               This chapter will make use  of  nearly  all  the topics  we  have  covered  so  far  and pro-
                            vides an excellent opportunity to review the preceding chapters. Once again we  take this
                            opportunity  to remind the reader that in using  the macroscopic balances, it may  be nec-
                            essary  to omit some terms and to estimate the values  of  others. This requires  good  intu-
                            ition or some extra  experimental data.



      315.1  THE MACROSCOPIC         ENERGY    BALANCE
                            We  consider the system  sketched  in Fig.  7.0-1 and make the same assumptions  that were
                            made in Chapter 7 with  regard  to quantities at the entrance and exit planes:

                               (i)  The time-smoothed velocity  is perpendicular to the relevant  cross  section.
                              (ii)  The density  and other physical  properties are uniform over the cross  section,
                              (iii)  The forces  associated  with  the stress tensor т are neglected,
                              (iv)  The pressure  does not vary over  the cross  section.

                            To these we  add:
                              (v)  The  energy  transport  by  conduction  q  is  small  compared  to  the  convective  en-
                                  ergy transport and can be  neglected.
                              (vi)  The work  associated  with  [т • v] can be neglected  relative  to  pv.
                            We  now  apply  the statement  of  conservation  of  energy  to the  fluid  in  the  macroscopic
                            flow  system.  In doing this, we  make use  of the concept of potential energy  to account  for
                            the  work  done  against  the  external  forces  (this  corresponds  to using  Eq.  11.1-9,  rather
                            than  Eq. 11.1-7, as the equation  of change for  energy).
                               The statement of the law  of conservation  of energy  then takes the form:

                                          |  (U  + K  + Ф )  = pAW   + \ M)  +  PA(V,))S,
                                                             (
                                              tot   tot  м              P
                                         rate of increase of  rate at which internal, kinetic, and
                                         internal, kinetic, and  potential energy enter the system
                                         potential energy in  at plane 1 by  flow
                                         the system
                                                              -  (p U (v )  + \p (v )  + pA(v ))S  (15.1-1)
                                                                            3
                                                                 2  2  2   2  2     2  2
                                                               rate at which internal, kinetic, and
                                                               potential energy leave the system
                                                               at plane 2 by  flow
                                    +  Q            +  W m                  +  (p (i^ )S  —
                                                                                    1
                                                                                1
                                                                                  1
                                    rate at which   rate at which work is done on  rate at which work is
                                    heat is added   the system by the surroundings  done on the system by the
                                    to the system   by means of the moving  surroundings at planes 1
                                    across boundary  surfaces               and 2
                                                       2
                            Here U lol  = JpUdV, K to[  = $\pv dV, and  Ф 1о1  = Jp<t>dV are the total internal, kinetic, and
                            potential energy  in the system,  the integrations being  performed  over  the entire  volume
                            of the  system.
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