Page 45 - Mechanical Engineers Reference Book
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1/34  Mechanical engineering principles
         Stream functions may be superposed so that if   Tangential velocity vg = -
                                                                         a*
           = fn(x,y) describes flow pattern A,                           ar                  (1.126)
         and
                                                       1.5.9.2  The velocity potential
         $2  = fn(x,y) describes flow pattern B,
                                                       In a gravitational field there is a property the change in which
         then   = $1  + $2  describes the flow pattern produced by the   is independent of the path of the change: potential energy. In a
         combination of A and B.                       continuous, irrotational  flow field there is also a property the
          The x and y components of  the flow velocity v are given by   change in which is independent of the path of the change. This
              a*        a*                             property  is the velocity potential (4). It can be shown that
         v,  = - -;  and v  = -                (1.124)
               ay       ax
                                                                                             (1.127)
         or
                        a*                             or
         v,  = -,   and vy = - -
                                                                         a4
             aY         ax                                   a4   and v, = - -               (1.128)
         depending on sign convention.  In polar coordinates the com-   "a=--'   ra0'   ar
         ponents are                                   Lines of  constant 4 are known as velocity potential lines with
                           -a*                         an equation
         Radial velocity v,   = -              (1.125)
                           ra0                          v,dx  + vydy = 0                      (1.129)




                           -
                           -
                        V
                           -
                        Parallel flow
                      J, = Vy = Vr cos 0
                      @  = Vx=Vrsin0



                                                42





                                     44-




                     I
                    $6                          46
            Source   +=-d                Vortex   J, = mr
                         2n                          2n
                         m
                    @  =-  -lnr                                    -+2
                         271
                                                                          Doublet in parallel flow






         Figure 1.48  Simple flow patterns
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