Page 78 - Bird R.B. Transport phenomena
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Problems  63

              2В.1 Different  choice  of  coordinates  for  the  falling  film  problem.  Rederive  the velocity  profile
                   and  the average  velocity  in  §2.2, by  replacing  x  by  a coordinate x  measured  away  from  the
                   wall; that is, x  = 0 is  the wall surface,  and x  = 8 is the liquid-gas  interface. Show  that the ve-
                   locity distribution  is then given  by

                                                 2
                                                                2
                                          v  =  (pg8 /fjL)[(x/8)  -  \(x/8) \  cos /3  (2B.1-1)
                                          z
                   and  then use this to get the average  velocity.  Show how one can get  Eq. 2B.1-1  from  Eq. 2.2-18
                   by  making a change  of  variable.
              2B.2  Alternate procedure  for  solving flow problems.  In this chapter we  have  used  the  following
                   procedure: (i) derive  an equation for the momentum flux, (ii) integrate this equation, (iii) insert
                   Newton's  law  to get  a first-order  differential  equation for  the velocity,  (iv) integrate the latter
                   to get  the velocity  distribution. Another  method is:  (i) derive  an equation  for  the momentum
                   flux, (ii) insert Newton's law  to get a second-order differential  equation for  the velocity  profile,
                   (iii) integrate the latter to get the velocity  distribution. Apply  this second method to the  falling
                   film  problem by  substituting  Eq. 2.2-14 into Eq. 2.2-10 and continuing as directed until the ve-
                   locity distribution has been obtained and the integration constants evaluated.

              2B.3  Laminar flow in  a narrow slit (see Fig. 2B.3).

                          Fluid in



















                              Fluid out   Fig. 2B.3  Flow through a slit, with  В «  W «  L

                   (a)  A Newtonian fluid  is  in laminar flow  in a narrow slit formed  by  two  parallel  walls a dis-
                   tance  2B apart. It is understood that В «  W, so  that "edge  effects"  are unimportant. Make a
                   differential  momentum balance, and obtain the following  expressions  for  the momentum-flux
                   and  velocity  distributions:

                                                                                       (2B.3-1)



                                             V-  =                                     (2B.3-2)
                   In these expressions  & = p  + pgh  = p  -  pgz.
                   (b)  What  is the ratio  of the average  velocity  to the maximum velocity  for  this  flow?
                   (c)  Obtain the slit analog  of the Hagen-Poiseuille equation.
                   (d)  Draw a meaningful  sketch  to show  why  the above  analysis  is inapplicable  if  В = W.
                   (e)  How can the result  in  (b) be obtained  from  the results  of  §2.5?
                   Answers:  (b) (v )/v  = I
                              z  Zfmax
                                           3
                                2  (9>o ~  ® )B W
                                        L    P
                                3      fiL
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