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414  Chapter 13  Temperature Distributions in Turbulent Flow

              ю- 1








                                                           A  Deissler  & Eian  (1952)  Pr = 0.73
                                                           *  Allen  & Eckert  (1964)  Pr  = 8.0
                                                           и  Malina  & Sparrow  (1964)  3 < Pr < 75
         « J                                               A  Friend & Metzner  (1958)  55 < Pr < 590
                                                           о  Harriott & Hamilton  (1965)  452  < Sc < 97,600






            3x10  -5
               3 x  10"  5




      Fig. 13.4-2.  Comparison of the expression  in Eq. 13.4-20  for the wall heat flux in fully  developed  turbulent
      flow with  the experimental data  of  R. G. Deissler and С  S. Eian, NACA  Tech. Note #2629 (1952); R. W.  Allen
      and  E. R. G. Eckert, J. Heat Transfer, Trans. ASME, Ser. C,  86,301-310  (1964); J. A. Malina and  E. M. Sparrow,
      Chem. Eng. Sci, 19,953-962  (1964); W.  L. Friend and A.  B. Metzner, AIChE Journal  4,393-402  (1958); P. Har-
      riott and  R. M. Hamilton, Chem. Eng. Sci., 20,1073-1078  (1965). The data  of Harriott and Hamilton are for the
      analogous mass transfer  experiment, for  which  Eq. 13.4-20 also applies.




                               Extensive  calculations based  on Eq. 13.4-19  were  performed  by  Sandall, Hanna, and
                                 3
                           Mazet.  These authors took the turbulent Prandtl number  to be  unity. They  divided  the
                           region  of  integration  into  two  parts, one  near  the wall  and  the  other  for  the  turbulent
                           core. In the "wall region"  they used  the modified  van  Driest equation  of  Eq. 5.4-7  for  the
                           mixing  length,  and  in  the  "core  region"  they  used  a  logarithmic  velocity  distribution.
                           Their final  result  3  is given  as
                              q D                            Re  PrVf/2
                               0                                                               (13.4-20)
                           k(T 0  -  T )  12.48 Pr  2/ 3  -  7.853 Pr  1/ 3  + 3.613  In  Pr  + 5.8  + 2.78  In Qg
                                  b
                           In obtaining this result, Eq. 6.1-4a has been  used.
                               Equation  13.4-20  agrees  with  the available  data on heat transfer  (and mass  transfer)
                           within  3.6 and  8.1% over  the range  0.73  <  Pr  <  590, depending on the sets  of  data  stud-
                           ied. The analogous  mass  transfer  expression,  containing Sc  = ii/p% AB  instead  of  Pr,  was
                           reported  3  to  agree  with  the  mass  transfer  data  within  8%  over  the  range  452  <  Sc  <
                           97600. The agreement  of  the theory with  the heat transfer  and mass  transfer  data, shown
                           in Fig. 13.4-2, is quite convincing.






                               3
                                О. С  Sandall, O. T. Hanna, and  P. R. Mazet, Canad. J. Chem. Eng., 58,443-447 (1980). See also  О. Т.
                           Hanna and  О. С  Sandall, AIChE  journal, 18, 527-533  (1972).
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