Page 447 - Bird R.B. Transport phenomena
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§14.2  Analytical  Calculations of Heat Transfer  Coefficients  for  Forced Convection Through Tubes and Slits  429

























                                                    (v z )D 2  (v z )B 2
                        Fig. 14.2-1.  The Nusselt number for  fully  developed, laminar flow of Newtonian
                        fluids  with  constant physical  properties: Nu foc  = h D/k  for  circular tubes  of diameter
                                                                loc
                         D, and Nu ]oc  = 4h B/k  for slits of half-width  B. The limiting expressions  are given  in
                                       ]oc
                        Tables  14.2-1 and  14.2-2.


                            For turbulent flow in a circular  tube with  constant heat flux, the Nusselt number can
                        be obtained  from  Eq. 13.4-20  (which  in turn originated  with  Eq. (K) of Table  14.2-1): 3
                                                             RePrVf/2
                                N u  =                                                       (14.2-4)
                                   lo w c    2/3        1/3
                                       12.48Рг  -  7.853Рг  + 3.613  In Pr  + 5.8  + 2.78  ln(^ReVf/8)
                        This  is  valid  only  for  az/(v )D 2  »  1, for  fluids  with  constant physical  properties, and
                                               z
                         for  tubes  with  no roughness.  It has  been  applied  successfully  over  the Prandtl-number
                         range  0.7  <  Pr <  590. Note that, for very large  Prandtl numbers, Eq. 14.2-4 gives
                                                                    1/3
                                                   Nu  loc  = 0.0566 RePr  V/                (14.2-5)
                              1/ 3
                        The Pr  dependence agrees  exactly  with  the large  Pr limit  in  §13.6  and  Eq.  13.3-7. For
                         turbulent flow there is little difference  between Nu for constant wall temperature and  for
                         constant wall heat flux.
                            For  the turbulent  flow  of  liquid metals, for  which  the Prandtl numbers  are  generally
                         much  less  than unity,  there  are  two  results  of  importance. Notter and  Sleicher 4  solved
                         the  energy  equation  numerically,  using  a  realistic  turbulent  velocity  profile,  and  ob-
                         tained  the rates  of  heat  transfer  through  the wall. The  final  results  were  curve-fitted  to
                         simple  analytical  expressions  for  two  cases:

                         Constant wall temperature:      Nu   = 4.8  + 0.0156 Re  08 5  Pr  09 3  (14.2-6)
                                                            loc
                                                                                 0 93
                                                                            0 85
                         Constant wall heat    flux:     Nu   = 6.3  + 0.0167 Re -  Pr -     (14.2-7)
                                                            loc
                         These equations are limited  to L/D  >  60 and constant physical  properties. Equation 14.2-
                         7 is displayed  in Fig.  14.2-2.


                            3
                             О. С  Sandall, O. T. Hanna, and  P. R. Mazet, Canad. }. Chem.  Eng., 58, 443-447  (1980).
                            4
                             R. H. Notter and С  A. Sleicher, Chem.  Eng.  Sci, 27, 2073-2093  (1972).
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