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46                                                 2.  Conservation  Equations


                 -j£  +  V  •  EtV  =  q h  -  V  • q +  V  • {Ilij  • V)  +  gf  •  V  (2.2.15a)

         or  in  terms  of  internal  energy  per  unit  mass,  e,  as

                             DP                            C)U '
                           Q^+P{V-Y)       =  q h-V-q  + Oij^            (2.2.15b)

         In  the  above  equations,  IIij  represents  the  stress  tensor  given  by

                                     Ilij  =  —pSij  +  (Tij              (2.2.16a)
         and  (T{j (dui/dxj)  represents  the  dissipation  function  ^  given  by


           $  =  fj, \(—\ 2  l(—\  2    2^—V       (—     — V      (—     —V
                    Vdx)       \dyj       \dz  J   \dx    dy)     \dy      dzj

                            2
                                                 dtvV
                H   du   9w\ _2/du 3  \dx  dv_  dz  J                    (2.2.16b)
                            J
                                           dy
                    dz
                          dx
         Finally,  we  need  an  equation  of  state  for  the  fluid  to  relate  p,  g  and  e.  The
        commonest  example  is the  perfect  gas  law
                                     p =  (7  -  l)c vgT

        where
                                  e  =  c vT,  7  =  c p/c v

        with  c v  and  c p  representing  the  specific  heats  in  constant  volume  and  pressure,
        respectively.
           The terms  on the  left-hand  side  of the  energy equation  given  by Eq.  (2.2.15a)
        represent  the  rate  of  increase  of  total  energy  in  the  control  volume  (per  unit
        volume)  and  the  rate  of  total  energy  lost  by  convection  through  the  control
        volume  (per  unit  volume),  respectively.  The  first  term  on the  right-hand  side  of
        the equation  represents the heat  produced  per  unit  volume  by external  agencies,
        the  second  term  represents  the  rate  of  heat  lost  by  conduction  through  the
        control  volume  (per  unit  volume),  and  the  third  and  fourth  terms  represent
        the  work  done  on  the  control  volume  by  the  surface  forces  and  body  forces,
        respectively  (per  unit  volume).
           In the  numerical  solution  of the  conservation  equations,  it  is often  preferable
        to express them  in  "divergence  form"  or  "conservation  form"  to  avoid  numerical
        difficulties  that  may  arise  in  some  flows,  such  as  flows  containing  shock  waves,
        when  the  nondivergence  form  or  the  nonconservation  form  of  the  equations  is
        used.  In  conservation  form  the  coefficients  of  the  derivative  terms  can  be  con-
        stant  or variable;  if variable, their  derivatives  do not  appear  in the equation.  For
        example, the continuity  equation  (2.2.12a)  is in the  conservation  form.  However,
        if  it  is written  as
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