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7.4  Computer  Program  BLP                                           225



         VGP      K  is  the  variable-grid  parameter.  Use  K  =  1.0  for  laminar  flow  and
                  K  =  1.14  for turbulent  flow.  For  a  flow consisting  of both  laminar  and
                  turbulent  flows,  use  K  =  1.14.
         RL       Reynolds  number,  ^oL.
                  Surface  distance,  feet  or  meters,  or  dimensionless.
                  Velocity,  feet  per  second  or  meter  per  second,  or  dimensionless.
         u e

         7.4.3  Subroutine  IVPL

         At  £ =  0,  Eq.  (7.3.6)  reduces to  the  Falkner-Skan  equation,  Eq.  (7.3.11),  which
         can  be  solved  subject  to the  boundary  conditions  of Eq.  (7.3.7).  Since the  equa-
         tions  are  solved  in  linearized  form,  initial  estimates  of j , Uj and  Vj  are  needed
                                                           /
         in order  to obtain  the  solutions  of the  nonlinear  Falkner-Skan  equation.  Various
         expressions  can  be  used  for  this  purpose.  Since  Newton's  method  is  used,  how-
         ever,  it  is useful  to  provide  as good  an  estimate  as  is possible  and  an  expression
         of the  form.
                                        3rjj   1  (i)}  °
                                   u                                       (7.4.8)
                                    i  =  ~
                                               2   Ve
         usually  satisfies  this  requirement.  The  above  equation  is obtained  by  assuming
         a  third-order  polynomial  of the  form

                                     f  =  a  + br) + erf

         and  by  determining  constants  a,  6,  c  from  the  boundary  conditions  given  by
         Eq.  (7.3.7)  for  the  zero-mass  transfer  case  and  from  one  of  the  properties  of
         momentum   equation  which  requires  that  f"  — 0  at  77  =  rj e.
            The  other  profiles  / j , Vj  follow  from  Eq.  (7.4.8)  and  can  be  written  as

                                  _  rj e (ai)  2   3 -- 1 /  'V, .VI
                               h    4   UJ        2^  KVeJ                 (7.4.9)


                                       3 1
                                  Vj  =     1 -  (%   )1                  (7.4.10)
                                                \Ve, /
                                       2r] e
         7.4.4  Subroutine  G R O W T H

         For  most  laminar-boundary-layer  flows  the  transformed  boundary-layer  thick-
         ness  rj e(x)  is almost  constant.  A value  of rj e  =  8 is sufficient.  However,  for  turbu-
         lent  boundary-layers,  rj e(x)  generally  increases  with  increasing  x.  An  estimate
         of  r} e(x)  is determined  by  the  following  procedure.
                                             n l
                                     n
            We  always  require that  rj e(x )  >  rj e(x ~ ),  and  in  fact  the  calculations  start
         with  7/ e(0)  =  rj e(xi).  When  the  computations  on  x  =  x n  (for  any  n  >  1)  have
                                                      n
                                                                               - 4
                                        |
         been  completed,  we test  to  see  if ^ j |  <  e v  at  r) e(x )  where,  say  e v  =  5  x  10 .
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