Page 332 - Bird R.B. Transport phenomena
P. 332

316  Chapter  10  Shell Energy Balances and Temperature Distributions in Solids and Laminar Flow

                               Now let us evaluate the local heat transfer driving force, T o  — T , which is the  differ-
                                                                                    b
                            ence between the wall and bulk temperatures at a distance z down the tube:
                                                      rji  rj-i  1 1  / U  1 1                 (10.8-34)
                                                      io  b
                                                       ~ ~24X~48 к
                            where D is the tube diameter. We may now rearrange this result in the form  of a dimen-
                            sionless wall heat flux
                                                             q D     48
                                                              0
                                                          k(T  - T )  И                        (10.8-35)
                                                             0
                                                                 b
                            which, in Chapter  14, will be identified as a Nusselt number.
                               Before leaving this section, we point out that the dimensionless axial coordinate £ in-
                            troduced  above may be rewritten  in the following  way:

                                                                                               (10.8-36)
                                                  D{v z)p          RePrlUJ    Pe \R
                            Here D is the tube diameter, Re is the Reynolds number used  in Part I, and Pr and Pe are
                            the Prandtl and  Peclet numbers introduced  in Chapter  9. We shall find  in Chapter  11 that
                            the Reynolds and Prandtl numbers can be expected  to appear in forced  convection  prob-
                            lems. This point will be reinforced  in Chapter  14 in connection with correlations  for  heat
                            transfer  coefficients.


      §10.9  FREE CONVECTION
                            In  §10.8 we gave  an example  of  forced  convection.  In this  section we turn  our  attention
                            to an elementary  free  convection problem—namely,  the flow between two parallel  walls
                            maintained  at different  temperatures  (see Fig. 10.9-1).
                               A  fluid  with  density  p and  viscosity  /л is  located between two  vertical walls a dis-
                            tance  2B apart. The heated wall  at у =  —В is maintained at  temperature T , and the
                                                                                             2
                            cooled  wall  at у =  +B is maintained at temperature T .  It is assumed that  the tempera-
                                                                          }
                                                                              1 2
                            ture difference is sufficiently  small that terms containing (AT)  can be neglected.
                               Because  of the temperature gradient in the system, the fluid near the hot wall  rises
                            and  that near the cold wall descends. The system is closed at the top and bottom, so that
                            the  fluid  is  continuously circulating between the plates. The mass  rate  of  flow  of  the




                            Temperature
                            distribution

                             Velocity
                            distribution
                               v z {y)







                                                           Fig. 10.9-1. Laminar free convection flow between
                                                           two vertical plates at two different temperatures. The
                                                           velocity is a cubic function of the coordinate y.
   327   328   329   330   331   332   333   334   335   336   337