Page 114 - Basics of Fluid Mechanics and Introduction to Computational Fluid Dynamics
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Dynamics  of Inviscid  Fluids                                                                99


                 Then,  to  ensure  that  at  far  distances  (|z|  —>  oo)  the  solution  of  our

             problem  tends  to  zero,  it  is  sufficient  to  choose  the  real  constants  »  and
              k  so  that                       ,               (e)
                                      ~1          PeO@=-49  ye               sage
                                   \=  5,  |             ep               ande=o.


                 Finally  we  have  for  the  complex  velocity  the  representation


              dF  1           f?h(é)-h(g)                     |             In(é)+h(g)           /E-a


             dz  wf,                  2-€        dé  —  5 28  fee =                              be

             a  formula  given  by  L.  I.  Sedov,  but  obtained  via  other  technique  [134].
                 On  the  other  hand,  as  a  complex  potential  f(z),  at  far  field,  has  an
             expansion  under  the  form


                                                    .
                               f(2)  =  Wooz  +  5—  logz  +  49+           +  F  +:


              and  implicitly  the  complex  velocity  is


                                      df  |             ri       ay       1

                                     dz  "©"  Orig               pital)

             we  get  for  the  circulation  I’,  necessarily'*,  the  value


                                                b                       f—a
                                                               ©)
                                          =  [  h@-b [See



                 This  value  corresponds  to  that  obtained  by  the  Joukovski  condition
              (rule),  the  fluid  velocity  being,  obviously,  bounded  at  the  sharp  trailing

             edge.  Supported  by  it  we  could  also  calculate  the  general  resultant  of
             the  fluid  pressures  on  the  thin  profile,  namely  we  have! is


                                                      .     b
                                                                                    E—a
                           Ry  —  iBy  =  ipVoe*  /  [lo  (€)  —  hh  (€)]                 dé.
                                                                                    b-—€


                 Details  on  the  theory  of  a  thin  (wing)  profile  and  even  some  extensions
             such  as  the  case  of  the  thin  airfoil  with  jet,  can  be  found  in  the  book
             of  C.  Iacob  [69].  The  thin  profile  with  jet  in  the  presence  of  the  ground
             has  been  studied  in  [113].




              '4Tn  virtue  of  the  uniqueness  of  such  a  series  development.
              'SBy  applying  directly  the  Blasius-Chaplygin  formulas,
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