Page 493 - Bird R.B. Transport phenomena
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§15.5  Use of the Macroscopic Balances to Solve  Unsteady-State Problems  473
                            Insulation                         Fig. 15.5-6.  Free batch expansion  of
                                                               a compressible  fluid.  The sketch
                                                    Convergent  shows  the locations of surfaces  1
                                                      nozzle   and 2.
                          Tank volume = V


                        Ambient pressure  = p a




                  For the same region, the energy  balance  of  Eq. (E) of Table  15.5-1 becomes

                                                                                     (15.5-36)

                  in which  V is the total volume in the system  being  considered, and w x  is the mass  rate of flow
                  of  gas  leaving  the system.  In writing  this  equation, we  have  neglected  the kinetic energy  of
                  the fluid.
                     Substituting the mass balance into both sides  of the energy  equation gives

                                               (dU,
                                                            Pi  dt                   (15.5-37)

                  For a stationary  system  under the influence  of no external  forces  other than gravity, йФ^ /dt =
                  0, so that Eq. 15.5-37 becomes

                                                                                     (15.5-38)
                                                         p\
                  This equation may be combined with the thermal and caloric equations  of state for the fluid in
                  order  to obtain p (p^) and  T^).  We  find,  thus, that the condition of  the fluid in the tank de-
                               x
                  pends  only  on  the  degree  to  which  the  tank  has  been  emptied  and  not  on  the  rate  of  dis-
                  charge.  For the special  case  of  an ideal  gas  with  constant C ,  for  which  dll  = C dT  and p  =
                                                                                  v
                                                                  v
                  pRT/M, we  may integrate Eq. 15.5-38 to obtain
                                                  Р\Р\  У  = PoPo                    (15.5-39)
                  in which  у  = C /C . This result also follows  from  Eq. 11.4-57.
                              p  v
                  (b)  Discharge of  the gas  through the  nozzle.  For the sake  of  simplicity  we  assume  here that
                  the flow between  surfaces  1 and 2 is both frictionless  and  adiabatic. Also, since w }  is  not  far
                  different  from  w ,  it is  also  appropriate  to consider  at any  one instant that the flow is  quasi-
                               2
                  steady-state.  Then we  can use  the macroscopic mechanical energy  balance in the form  of Eq.
                  15.2-2 with  the second, fourth, and  fifth  terms omitted. That is,

                                                \v\    ±dp  =  O                     (15.5-40)

                  Since we  are dealing  with  an ideal gas, we  may use the result  in Eq. 15.5-34  to get the instan-
                  taneous  discharge  rate. Since  in  this  problem  the ratio  S /S }  is  very  small  and  its  square  is
                                                                2
                  even  smaller,  we  can replace  the denominator under  the square  root  sign  in  Eq.  15.5-34  by
                  unity. Then the p  outside the square root sign  is moved  inside and use is made of  Eq. 15.5-39.
                               2
                  This gives

                                                       -  1)][(р /ро) 2/у  -         (15.5-41)
                                                             2
                  in which  S  is the cross-sectional  area  of the nozzle opening.
                          2
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