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60       BASICS  OF  FLUID  MECHANICS  AND  INTRODUCTION  TO  CFD


              so  that  ®,(P)  >  ®,(M),  which  means  v?(P)  >  v?(M).  In  other  words

              the  unique  possibility  for  the  velocity  to  get  a  maximum  value  is  only
              on  the  boundary.       Concerning  the  minimum  value  of  the  velocity  this
             could  be  reached  inside  the  domain,  namely  in  the  so-called  stagnation
             points  (with  zero  velocity).  If  the  fluid  flow  is  steady  and  the  external
             forces  can  be  neglected,  from  the  second  Bernoulli  theorem  (integral)

              it  comes  that,  at  a  such  stagnation  point,  the  pressure  has  a  maximum
             while  at  boundary  points  of  maximum  velocity,  the  pressure  should  have
              a  minimum.
                 Let  us  now  consider  the  case  of  an  incompressible  irrotational  plane
              (2-dimensional)  fluid  flow.
                 Let  Oxy  be  the  plane  where  we  study  the  considered  fluid  flow,  u

              and  v  being  the  velocity  vector  components  on  Oz  and  Oy  respectively,
              and  gq  the  magnitude  of  this  vector.  The  fluid  being  incompressible,  the
             equation  of  continuity  can  be  written  gu  +  oe  =  0,  such  that  udx  —  vdy
              is,  for  every  fixed  t,  an  exact  total differential  in  «  and  y.  Consequently,
              there  is  a  function  w  (z,y,t)  ,  defined  to  within  an  additive  function  of
              time  by  the  equality  udy  —vudz  =  dy,  where  ¢  is  seen  as  a  parameter  and
             not  as  an  independent  variable.

                 This  function  w(z,y,t)  is  the  stream  function  of  the  flow  since  the
              curves  ~  =  constant,  at  any  fixed  moment  t,  define  the  streamlines
              of  the  flow  that  has  been  shown.          On  the  other  side,  the  flow  being
              irrotational,  we  also  have  Su  —  ge  =  0  which  proves  the  existence  of  a

              second  function  ®  (z,y,t),  the  velocity  potential,  defined  also  to  within
              an  additive  function  of  time,  such  that  udz  +  vdy  =  d®  where  again  t  is
              considered  a  parameter  and  not  an  independent  variable.  Hence


                                      ya  22  _                     Oh  _  OY
                                             Ox  =  Oy’             Oy         Ox

              or,  under  vectorial  form

                                           v  =  grad®  =  —k  x  grady,

             k  being  the  unit  vector  of  the  axis  directly  perpendicular  on  the  plane

              Oxy.
                 But  these  equalities  show  that  the  two  functions  ®  and  w  satisfy
             the  classical  Cauchy-Riemann  system  and,  consequently,  the  function
              f  =  &@+  ty  is  a  monogenic  (analytic)  function  of  the  complex  variable
              z=  2+ty  which  could  depend,  eventually,  on  the  parameter  t.  This
             function  is  called  the  complex  potential  of  the  flow  and  it  is  obviously
             defined  to  within  an  additive  function  of  time.  The  real  and  imaginary

             part  of  f(z),  which  means  the  velocity  potential  and  the  stream  function
              of  the  flow,  are  two  conjugate  harmonic  functions;  the  equipotential  lines
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