Page 156 - Bird R.B. Transport phenomena
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140   Chapter 4  Velocity  Distributions with  More Than One Independent Variable

                              1.0                                            Fig.  4.4-4.  Velocity  profile for
                                                                             wedge flow  with included
                              0.8                                            angle  /Зтг. Negative values of
                                                                             /3 correspond to the flow
                              0.6                                            around an "external corner"
                                                                             [see Fig. 4.3-4Ш)] with  slip at
                              0.4                                            the wall upstream of the
                                                                             corner.
                              0.2






     SOLUTION              We  now have  to solve  Eq. 4.4-11, using  Eq.  4.4-31  for v (x). When  we introduce the stream
                                                                        e
                           function  from  the first row of Table 4.2-1, we obtain the following  differential  equation for ф:
                                                 г
                                             дф  д ф  дф д ф _  I  с р  ^  1    д ф
                                                                2
                                                                                 3
                                                         2
                                                                                               (4.4-32)
                                             ~fry~dx~dy~~dx~rf~\2-p
                           which  corresponds to Eq. 4.4-20 with the term v (dv /dx)  added. It was discovered 9  that this
                                                                  e
                                                                     e
                           equation  can be reduced  to a single  ordinary  differential  equation by introducing a dimen-
                           sionless  stream function f(rj) by
                                                    ф(х,у) =                                   (4.4-33)
                           in which the independent variable is
                                                                      У
                                                                                               (4.4-34)
                           Then Eq. 4.4-32 becomes the Falkner-Skan equation 9
                                                                     2
                                                      f'"-ff"-p(\  -/' ) =                     (4.4-35)
                           This  equation has been  solved  numerically  with  the appropriate boundary  conditions,  and
                           the results are shown in Fig. 4.4-4.
                              It can be seen  that for positive  values  of /3, which  corresponds to the systems  shown in
                           Fig.  4.3-4(a)  and Fig. 4.3-5, the fluid  is accelerating  and the velocity  profiles  are stable. For
                           negative  values  of j3, down to /3 = -0.199,  the flows are decelerating but stable, and no sepa-
                           ration  occurs.  However,  if  /3 >  -0.199,  the velocity  gradient  at the wall  becomes  zero,  and
                           separation  of the flow  occurs. Therefore,  for the interior  corner  flows  and for wedge  flows,
                           there is no separation, but for the exterior corner flows, separation may occur.


                           QUESTIONS FOR DISCUSSION

                           1.  For what  types  of  problems  is the method  of combination  of variables  useful? The
                             method  of separation of  variables?
                           2.  Can the flow  near  a cylindrical  rod of  infinite  length  suddenly  set in motion in the
                             axial  direction be described by the method in Example 4.1-1?


                              9
                                V. M. Falkner and S. W. Skan, Phil. Mag., 12, 865-896  (1931); D. R. Hartree, Proc. Camb. Phil. Soc,
                           33, Part  II, 223-239  (1937); H. Rouse (ed.), Advanced  Mechanics of Fluids, Wiley, New York  (1959), Chapter
                           VII, Sec. D; H. Schlichting and K. Gersten, Boundary-Layer Theory, Springer-Verlag,  Berlin (2000), pp.
                           169-173 (isothermal), 220-221  (nonisothermal); W. E. Stewart and R. Prober, Int. J. Heat Mass  Transfer, 5,
                           1149-1163  (1962); 6, 221-229, 872 (1963), include wedge  flow  with heat and mass  transfer.
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