Page 166 - Bird R.B. Transport phenomena
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150  Chapter 4  Velocity  Distributions with More Than One Independent Variable

                           (a)  Find the pressure  distribution, radial  flow  velocity,  and  mass  rate  of  flow  for  an incom-
                           pressible  fluid.
                           (b)  Rework  (a) for a compressible  liquid and for an ideal  gas.
                                                                   <3>           2тгкНр  ~
                           Answers:  (a) -                          2        w  =      2
                                              In (R /R,)                          /x In  (R /R )
                                                                                        2
                                                                                           x
                                                  2
                      4D.1  Flow near  an  oscillating wall. 8  Show, by  using  Laplace transforms, that the complete solu-
                           tion to the problem stated in Eqs. 4.1-44 to 47 is
                                                               - ^    <r '(sirr        —  dw   (4D.1-1)
                                                                        w
                      4D.2  Start-up of  laminar flow in  a circular tube (Fig. 4D.2). A fluid  of constant density and  viscos-
                           ity  is  contained in a very  long  pipe  of  length  L and radius  R. Initially  the fluid  is  at rest.  At
                           time t  = 0, a pressure gradient  (0>  -  2P )/L is imposed  on the system. Determine how the ve-
                                                      o
                                                           L
                           locity profiles  change with time.
                                          Tube center           Tube wall
                                                                       \











                                 1.0  0.8  0.6  0.4  0.2  0.2  0.4  0.6  0.8  1.0


                           Fig. 4D.2.  Velocity  distribution for the unsteady  flow re-
                           sulting  from a suddenly impressed  pressure gradient in a
                           circular tube [P. Szymanski, /. Math. Pures Appl., Series 9,
                           11,67-107(1932)].


                            (a)  Show that the relevant equation of motion can be put into dimensionless  form as  follows:

                                                                                               (4D.2-1)

                                                   2
                           in which £ =  r/R,  т = fit/pR , and  ф =  [&
                                                              0
                                                                              f
                            (b)  Show that the asymptotic solution for large time is ф х  = 1 - . 2  Then define  ф, by ф(£, т)  =
                           фоо(&  ~ Ф((С  т), and solve the partial differential  equation for  ф  by  the method of separation
                                                                                 {
                           of  variables.
                            (c)  Show that the final  solution is
                                                                               2
                                                ф((, г) = (1 -  f )  -  8  ехр(-а т)           (4D.2-2)
                                                           2
                           in  which  /„(£)  is  the  nth  order  Bessel  function  of  £, and  the  a n  are  the  roots  of  the  equation
                           Jota,,)  =  0. The result  is plotted  in Fig. 4D.2.


                               8
                                 H. S. Carslaw and J. C. Jaeger, Conduction of Heat in Solids, Oxford University Press, 2nd edition
                            (1959), p. 319, Eq. (8), with e =  ^
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