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70                                                 2.  Conservation  Equations



         2.7  Boundary    Conditions

         The  nature  of  the  equations  and  their  domains  of  dependence  and  zones  of
         influence  have  implications  for  boundary  conditions.  Thus,  for  example,  the
         steady,  two-dimensional  incompressible  form  of  the  momentum  equation  for
         laminar  flow,
                                                    2
                                                            2
                            du    du  _   I  dp    (d u    d u\                 -
                            dx    dy      Q dx     I  dx 2  dy 2  J
         is elliptic,  and  boundary  conditions  are  required  on  all  sides  of the  solution  do-
         main  (see Section  4.5). The equation  is always solved together  with the  equation
         of  continuity  and  the  normal  momentum  equation  so  that  u,  v  and  p  or  their
         gradients  must  be  specified  for  a  problem  on  its  boundaries.
            In  the  case  of  steady,  two-dimensional  boundary-layer  flows,  the  equation
                                                         2
                                 du    du      1 dp     d u
                                                         2
                                 dx    dy      g dx     dy
         is  parabolic  so  that,  with  the  continuity  equation  and  with  known  pressure,
         u  and  v  or  their  gradients  are  required  on  three  sides  of  the  solution  domain.
         The  forms  of  these  equations  appropriate  to  turbulent  flows  are  presumed  to
         have  the  same  requirements.  The  boundary  conditions  vary  considerably  from
         problem  to  problem  and  there  are  two  main  types.
            In  external  flows,  the  shear  layers  flowing  in  the  x-direction  adjoin  an  effec-
         tively  "inviscid"  freestream  extending  to  y  =  oo.  On  the  lower  side  there  may
         be either  a solid  surface,  usually taken  as  y  =  0 as  in Fig.  2.5a,  in which  case  the
         viscous  region  is  called  a  "wall  shear  layer,"  or  there  may  be  another  inviscid
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