Page 102 - Basics of Fluid Mechanics and Introduction to Computational Fluid Dynamics
P. 102

Dynamics  of Inviscid  Fluids                                                                87


              of  the  vortex  panels.  References  can  be  found,  for  instance,  in  the  book

              of  Chow  [22].


              6.3        Example
                 Let  us  consider,  for  instance,  a  source  panel  of  length  2,  lying  sym-

              metrically  on  the  Oy  axis  [22].  Assume  that  on  it,  sources  of  the  strength
              A  per  unit  length  are  distributed.  The  velocity  potential  induced  at  every
             point  (z,y)  by  the  source  contained  in  the  infinitesimal  panel  element
                                       !                         1
              dy’  at  (0,y’)  is  Au  In  [x?  +  (y  —  y’)?]?  (this  expression  is  obtained  by
             taking  the  real  part  of  the  source  complex  potential).
                 The  potential  induced  by  the  entire  panel  is


                                                 Xd     L
                                   ®(x,y)  =  z/  In  {a?  +  (y  —  y')"]  dy’
                                                  TS-L

              and  the  velocity  components  can  be  obtained  by  derivation  with  respect
              to  xz,  respectively  y,


                                 u(z,y)  =  +  [arctg  (#22)  —  arctg  (44)



                                                     x?  +  (y+L)?
                                          —    A
                                 v(z,y)  =  7  In  PE lyo  Lye


                 Considering  a  point  (z,y)  such  that  z  >  0  and  y  €  (~-L,L),if  c> 0

              from  the  right  of  the  panel  we  obtain  the  limit  u(+0,y)  =  3.             On  the
              other  hand,  by  a  similar  approach  from  the  left,  we  obtain  the  limit
              u(—0,y)  =  —3.         Thus  the  panel  generates  a  flow  having  an  outward
              normal  velocity  of  magnitude  A,  The  tangential  velocity  v  is  the  same
              on  both  sides  of  the  panel  and  it  is  zero  at  the  midpoint  and  infinite  at

              the  edges  of  the  panel.
                 If  such  a  panel  with  sources  of  strength  4  =  2U  is  placed  normal
              to  a  uniform  flow  of  speed  U,  the  induced  normal  velocity  cancels  the
              oncoming  flow  on  the  left  side  and  thus  the  resultant  flow  is  tangent  to
              the  surface.  So,  the  panel  becomes  coincident  with  one  of  the  streamlines
              of  the  flow.

                 If  the  panel  makes  an  angle  @  with  the  uniform  stream,  the  generated
              flow  cancels  the  normal  induced  flow  if  its  strength  is  A  =  2U  sin  @.
                 Let  now  m  be  the  number  of  the  panels.  On  each  panel  are  distributed
              uniform  sources  of  strength  A1,...,Am  (strength  per  unit  length)  respec-
              tively.  The  velocity  potential  of  the  resultant  flow  at  every  point  (z;,  y;)
              from  the  flow  field,  generated  by  the  sources  from  the  7-th  panel  is,  as
              above,  Au  J,  Inrijds;  where  J  is  the  panel  and  A,;ds;  is  the  strength  of
   97   98   99   100   101   102   103   104   105   106   107