Page 110 - Basics of Fluid Mechanics and Introduction to Computational Fluid Dynamics
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Dynamics  of Inviscid  Fluids                                                               95



                                           Adj  =  —w;  =  —150  (r  —  75)
                                          dy;        _                            ’
                                            dn   lon  —  0

              that  is,  equivalently,  to  choose  w,  (r)  =  -lj;Gn (r,  r;)  ,  where  Gy (r,  r;)
              is  the  Green’s  function  for  the  Neumann  problem  associated  with  the

              Laplace  operator  (Laplacian)  in  the  domain  D.
                 Retaking  again  the  Euler  system  in  the  form



                                  Aw  =  —-W,uU=  Oy,  v  =  —Oz'p,  sie          = 0,

              we  can  write



                                        b=-s  for r’)  In|r  —r'| dr’,


              and  then  we  set  u  =  dyy,  v  =  —Ozy.  But  these  equations  seem  to  be
             just  the  equations  established  for  a  system  of  point  vortices,  the  integral

             representation  for  ~  being  replaced  by  the  formula  y%  =  >  w;  (r),  valid


              in  the  conditions  of  a  point  vortices  system  analogously  a as  a  Riemann
              integral  is  approximated  by  a  Riemann  sum.                 This  suggests  that  an
              inviscid  incompressible  flow  can  be  approximated  by  the  flow  induced
             by  a  discrete  system  of  vortices,  The  convergence  of  solutions  of  the
             discrete  vortex  equations  to  solutions  of  Euler’s  equations  as  N  —  oo  is

              studied  in  [38]  and  in  [61].
                 Vortex  systems  provide  both  a  useful  tool  in  the  study  of  general
             properties  of  Euler’s  equations  and  a  good  starting  point  for  setting  up
              effective  algorithms  for  solving  these  equations  in  specific  situations.


             8.        Thin  Profile  Theory

                 The  theory  of  a  wing  with  an  infinite  span  (i.e.,  the  theory  of  profiles)
             requires  knowledge  of  the  conformal  mapping  of the  profile  outside,  from
              the  physical  plane  (z)  onto  the  outside  of  a  disk  from  the  plane  (Z).
              However,  for  an  arbitrary  (wing)  profile,  it  is  difficult  to  get  effectively

              this  mapping;  that  is  why,  many  times,  one  prefers  the  reverse  procedure,
              that  is  to  construct  (wing)  profiles  as  images  of  some  circumferences
              through  given  conformal  mappings.  The  Joukovski,  Karman—Trefftz,
              von  Mises,  etc.  profiles  belong  to  this  category  [69].
                 In  the  particular  case  of  the  thin  profiles  with  weak  curvature,  the
             problem  of  a  flow  past  such  a  profile  can  be  directly  solved  in  a  quite
              simple  approximative  manner.  More  precisely,  this  time  it  will  not  be

              necessary  to  determine  the  above  mentioned  conformal  mapping  but
              only  the  solving,  in  the  physical  plane,  of  a  boundary  value  problem  of
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