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2.3  Reynolds-Averaged  Navier-Stokes  Equations                       55



                                       »
                (3 X  =  ua xx  +  va xy xyi  +  G ^ f a  ) + Vx^-{a  )
                                    P r ( 7 - 1 )           dry
                                                                          (2.2.48)
                      Ua xy  +  VOyy  +  ^  _



         2.3  Reynolds-Averaged      Navier-Stokes     Equations


         The  Navier-Stokes  equations  of  the  previous  section  also  apply  to  turbulent
         flows  if  the  values  of  fluid  properties  and  dependent  variables  are  replaced  by
         their  instantaneous  values.  A  direct  approach  to  solving  the  equations  for  tur-
         bulent  flows  is to  solve them  for  specific  boundary  conditions  and  initial  values
         that  include  time-dependent  quantities.  Mean  values  are  needed  in  most  prac-
         tical  cases,  so an  ensemble  of solutions  of time-dependent  equations  is  required.
         Even  for  the  most  restricted  cases,  this  approach,  referred  to  as  direct  numer-
         ical  simulation  (DNS)  and  discussed  in  [6], becomes  a  difficult  and  extremely
         expensive  computing  problem  because  the  unsteady  eddy  motions  of  turbu-
         lence  appear  over  a  wide  range  of  scales. The  usual  procedure  is to  average  the
        equations  rather  than  their  solutions,  as  discussed  in  [2,3,7].
           In  this  section  and  following  sections,  we shall  consider  the  differential  form
        of  the  conservation  equations  and,  for  simplicity,  restrict  the  discussion  to  in-
        compressible  flows.  The  treatment  of compressible  flow  equations  is similar  but
        rather  lengthy. Whenever  appropriate, the  governing equations  for  compressible
         flows  will  be  given  without  derivation.
           In  order  to obtain  the  conservation  equations  for  turbulent  flows,  we  replace
        the  instantaneous  quantities  in  the  equations  by  the  sum  of  their  mean  and
        fluctuating  parts.  For  example,  the  instantaneous  values  of  the  u-,  v-  and  w-
        velocities  are  expressed  by  the  sum  of their  mean  iZ, v,  w  and  fluctuating  parts
                                                      7
         u\  v'  and  w\  and  the  temperature  T  by  T  and  T , that  is,
                 u  =  u-\-  u  ,  v  —  v  +  v  w  =  w  +  w  T  =  T  +  T'  (2.3.1)

           With  the  help  of  the  continuity  equation,  (2.2.1),  one  can  now  write  the
         left-hand  sides  of  the  momentum  and  energy  equations  in  conservation  form
         and  introduce  the  above  relations  into  the  continuity,  momentum  and  energy
        equations.  After  time  averaging  and  making  use  of  the  substantial  derivatives
        given  by  Eq.  (2.2.5),  the  Reynolds  averaged  Navier-Stokes  (RANS)  equations
         for  three-dimensional  incompressible  flow  can  be  written  in  the  following  form:
                                    du   dv    dw
                                                                           (2.3.2)
                                    dx   dy     dz

             Du      dp      72,-            ,2)                d
                        +  /iV  u  +    4<"        Q—{u'v')        U W     (2.3.3)
            }                      gf x                       Q-Q- ZK ' ')
             Di      dx                             dy
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