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256                                                8.  Stability  and  Transition



         8.4  C o m p u t e r  P r o g r a m  S T P

         We  now  describe  a  stability-transition  program  (STP)  for  calculating  the  neu-
         tral  stability  curves  and  transition  of  two-dimensional  flows  based  on  spatial
         amplification  theory  and  the  numerical  method  discussed  in  Sections  8.2  and
         8.3.  The  program  (Appendix  B)  requires  that  the  boundary-layer  velocity  pro-
         files  be  calculated  with  the  boundary-layer  program  of  Chapter  7  so  that  u
         and  u"  can  be  used  at  each  ^-station  as  a  function  of  r\. For  convenience,  the
         velocity  uo  and  length  L  scales  in  the  Orr-Sommerfeld  equation  are  chosen  to
         correspond  to
                                               / i/x    x
                                  =  u e,  L  =  J—  =  - =                 (8.4.1)
                                u 0
                                                 u
                                              V e      VRx
         with  Reynolds  number  R  now  given  by

                                     R = ^    =  y/1£                       (8.4.2)

         With  this  choice,  the  boundary-layer  grid  of  the  velocity  profiles  can  be  used
         in  the  solution  of  the  Orr-Sommerfeld  equation.  This  means,  that  u  and  u"  in
         the  stability-transition  program  are  related  to the output  of the  boundary-layer
         program  by
                                     u  =  f,  u"  =  f"                    (8.4.3)

         and that  the output  of the  boundary-layer  program  can  be arranged  to  calculate
         u"  once the solutions  of the boundary-layer  equations  are known. The  parameter
         f"  can  be  obtained  either  by  differentiating  f"  with  respect  to  r\ or  from  the
         finite-differenced  momentum  equation,  Eq.  (7.3.18),  which  for  laminar  flow  can
         be  written  as

                                       2 n        l                    1
           v'j  =  U"T  =  -*i(fv)]  +  a 2(u j)  -  a n(v?- f?  -  f^v?)  +  R]'  (8.4.4)

         where  i?™ _1  is  given  by  Eq.  (7.3.20a).
            With  boundary-layer  profiles  known  at  each  x-station,  the  stability  calcula-
         tions  can  be  started  at  any  x-station  where  the  critical  Reynolds  number  i? cr
         is  less than  the  local  Reynolds  number  used  in the  boundary-layer  calculations.
         For  external  flows,  an  estimate  of  R$*  can  be  obtained  from  Fig.  8.2  with  R$*
         known  from  the  boundary-layer  calculations  and  included  in  the  output  sub-
         routine.
            The  calculations  for  transition  are  first  performed  for  a  neutral  stability
         curve  at  the  specified  x-location  where  R  (~  yfR^)  is  known.  The  calculation
         of  uo  and  a  requires  initial  estimates.  A  convenient  procedure  to  achieve  this  is
         the  continuation  method  discussed  in  [3] but  to  retain  a  comparatively  simple
         program,  this  is  not  part  of the  present  description.  The  initial  estimates  of  UJ
         and  a  for  a  given  R  can  be  obtained  for  Blasius  flow.
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