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Finite wing theoly  21 9

                To find the velocity at P due to the length AB the sum of induced velocities due to
              all such elements is required. Before integrating, however, all the variables must be
              quoted in terms of a single variable. A convenient variable is $ (see Fig. 5.10) and the
              limits of the integration are
                                                           (;  1
                                                 to  OB=+--@
                                 $,4  = -(;-a)
              since $ passes through zero when integrating from A to B.

                                     sin 6’  = cos 4,  r2 = h2 sec’  $
                                     ds = d(h tan 4) = h sec’  $d $

              The integration of Eqn (5.8) is thus





                         -
                         --  (cosa+cosp)
                           47rh                                                  (5.9)
              This result is of the utmost importance in what follows and is so often required that it
              is best committed to memory. All the values for induced velocity now to be used in
              this chapter are derived from this Eqn (5.9), that is limited to a straight line vortex of
              length AB.
              The influence of a semi-infinite vortex (Fig. 5.11~) If one end of the vortex stretches
              to infinity, e.g. end By then p = 0 and cos p = 1, so that Eqn (5.9) becomes
                                              r
                                         v = - (cos0 + 1)                       (5.10)
                                             47rh
              When  the  point  P  is  opposite  the  end  of  the  vortex  (Fig.  5.11b),  so  that
              CY = 7r/2,  COSQ  = 0, Eqn (5.9) becomes
                                                   r
                                              )I=-                              (5.11)
                                                  47rh
              The influence of an infinite vortex (Fig. 5.11~)  When a = ,8 = 0, Eqn (5.9)  gives
                                                   r
                                              v=-                               (5.12)
                                                  27rh
              and this will be recognized as the familiar expression for velocity due to the line
              vortex of Section 3.3.2. Note that this is twice the velocity induced by a semi-infinite
              vortex, a result that can be seen intuitively.
                In nature, a vortex is a core of fluid rotating as though it were solid, and around
             which  air  flows in  concentric circles. The  vorticity  associated with  the  vortex is
              confined to its core, so although an element of outside air is flowing in circles the
              element itself does not rotate. This is not easy to visualize, but a good analogy is with
              a car on a fairground big wheel. Although the car circulates round the axis of the
             wheel, the car does not rotate about its own axis. The top of the car is always at the
              top and the passengers are never upside down. The elements of air in the flow outside
              a vortex core behave in a very similar way.
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