Page 159 - Aerodynamics for Engineering Students
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142  Aerodynamics for Engineering Students

                    If  this source-sink  pair  is placed  in a  uniform stream -U in the z direction it
                  generates the flow around a body of revolution known as a Rankine body. The shape
                  is very similar to the two-dimensional Rankine oval shown in Fig. 3.18 and described
                  in Section 3.3.7.

                  3.4.5  The point doublet and the potential flow around
                          a sphere
                  A point doublet is produced when the source-sink pair in Fig. 3.30 become infinitely
                  close together. This is closely analogous to line doublet described in Section 3.3.8.
                  Mathematically the expressions for the velocity potential and stream function for a
                  point doublet can be derived from Eqns (3.70) and (3.71) respectively by  allowing
                  a + 0 keeping p = 2Qa fixed. The latter quantity is known as the strength of the
                  doublet.
                    If a is very small a2 may be neglected compared to 2Ra  cos cp in Eqn (3.70) then it
                  can be written as
                                                     1
                                     { R2 cos2 cp + R2 sin2 cp + 2aR cos cp} 'I2
                                                     1
                                   -                                 1
                                     { R2 cos2 cp + R2 sin2 cp - 2aR cos cp}lI2

                                               1                    1        1       (3.72)
                                       { 1 + 2(a/R) cos cp}'I2 - { 1 - 2(a/R) cos cp}l/'
                  On expanding
                                               1
                                            --           1
                                            &E     - lTF-X+  **.
                                                         2
                  Therefore as a --t 0 Eqn (3.72) reduces to
                                           Q
                                      ~=-(l--coscp-1--coscp
                                                   a
                                          4sR     R            R
                                             Qa
                                        -
                                        -  --    coscp = --    coscp                 (3.73)
                                            2rR2          4sR2
                    In a similar way write


                                                       a  a
                                              =coscp~-~-cos2cp
                                                      R   R
                  Thus as a + 0 Eqn (3.71) reduces to
                                       $=- Qa  (1 - cos  cp)  = - cp                 (3.74)
                                                                  2
                                                             P
                                                      2
                                                                sin
                                           21rR             41rR
                    The streamline patterns corresponding to  the point doublet are similar to those
                  depicted in Fig. 3.20.  It is apparent from this streamline pattern and from the form
                  of  Eqn  (3.74)  that,  unlike the  point  source, the  flow  field  for  the  doublet is  not
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