Page 79 - Bird R.B. Transport phenomena
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64  Chapter 2  Shell Momentum Balances and Velocity  Distributions in Laminar Flow
                      2B.4 Laminar slit flow with  a moving wall  ("plane  Couette flow").  Extend  Problem  2B.3 by  al-
                           lowing  the wall at x  = В to move in the positive  z direction at a steady  speed  %  Obtain (a) the
                           shear-stress  distribution  and  (b) the velocity  distribution.  Draw  carefully  labeled  sketches  of
                           these  functions.

                                                              -  <3> L )B :
                           Answers:  T  =      ]Х       =           НУН            1
                                   XZ           ~Ж'^         2/xL
                      2B.5 Interrelation  of  slit  and  annulus formulas.  When  an annulus is  very  thin, it may, to a  good
                           approximation, be considered as a thin slit. Then the results  of Problem 2B.3 can be taken over
                           with  suitable  modifications.  For example, the mass  rate  of  flow  in an annulus with  outer wall
                           of radius R and inner wall  of radius  (1 -  e)R, where e is small, may be obtained from Problem
                           2B.3 by replacing 2B by sR, and  Wby  2тг(1 -  \e)R. In this way  we get  for  the mass rate of  flow:
                                                                  Vp
                                                    IV  =                                      (2B.5-1)

                           Show that this same result  may be obtained from  Eq. 2.4-17 by setting к equal to 1 -  e every-
                           where  in the formula  and  then expanding  the expression  for  w  in powers  of  s.  This  requires
                           using the Taylor series  (see §C2)
                                                 In (\-e)=  -e-  \e 2  -  \е ъ  -  \e A        (2B.5-2)

                           and then performing  a long division.  The first term in the resulting  series  will be Eq. 2B.5-1. Cau-
                           tion: In the derivation it is necessary  to use the first four terms of the Taylor series  in Eq. 2B.5-2.
                      2B.6 Flow  of  a film  on  the  outside  of  a circular tube  (see  Fig.  2B.6).  In a gas  absorption  experi-
                           ment a viscous  fluid  flows upward  through a small circular tube and then downward  in lami-
                           nar flow on the outside. Set up a momentum balance over  a shell  of  thickness  Ar in the  film,









                            Velocity
                           distribution
                           inside tube            Velocity
                                                 distribution
                                                   outside
                                                   in film


                                                 Ar


                                z-Momentum       z-Momentum
                                  into shell      out of shell
                                 of thickness     of thickness
                                    Ar               Ar


                                             T   Gravity force
                                                   acting on
                                                  the volume
                                                   2тгтАгЬ



                                                             Fig. 2B.6  Velocity  distribution and z-momentum
                                                             balance for the flow of a falling  film  on the outside
                                                             of a circular tube.
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