Page 499 - Modelling in Transport Phenomena A Conceptual Approach
P. 499

11.1.  UNSTEADY LAMINAR FLOWIN A TUBE                               479

           Substitution of e. (11.1-51) into Eq. (11.1-52) gives



                                                                          (11.1-53)


           Note  that  when  r  --f  00,  Q --$ ..(Po - PL)@/S~L which  is  identical  with
           Eq. (9.1-83).

           11.1.2  Approximate Solution by the Area Averaging
                    Technique1

           It should be kept in mind that the purpose of  obtaining the velocity distribution
           is to get a relationship between the volumetric flow rate and the pressure drop in
           order to estimate the power  required to pump the fluid.
              The  area  averaging technique enables one  to  calculate the  average velocity,
           and hence the volumetric flow rate, without determining the velocity distribution.
           Multiplication of  &.  (11.1-13) by  T drde and integration over the cross-sectional
           area of  the pipe gives




                                                        5
                                            +I I Rpa ; (r2)rdrdQ  (11.1-54)
                                                2=

           The term on the left side of Eq. (11.1-54) can be rearranged in the form
                                         -



               p J"^ IR % r drde = p [ $I2= Jd" w, r dr d 0)  = pR2 - (11.1-55)
                                                                   dt
                                                                  d(wz)
                 0   0
                                              nRa (v,  )
           Therefore, IZq.  (11.1-54) becomes


                                                                          (11.1-56)


           Note that the area averaging technique transforms a partial differential equation
           to an ordinary differential equation.  However, one has to pay the price for this
           simplification. That is, to proceed further, it is necessary to express the velocity
           gradient at the wall,  (awZ/ar),=R, in terms of  the average velocity, (w,).  If  it is

             'This  development is taken from  Slattery (1972).
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