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Basic thermal design theory for heat exchangers  27


              2.1.1.7 Heat transfer in concentric annular ducts
              For heat transfer in concentric annular ducts, three boundary conditions
              have often been met: (1) heat transfer through the inner tube, with the insu-
              lated outer tube; (2) heat transfer through the outer tube, with the insulated
              inner tube; and (3) heat transfer through both the inner and outer tubes hav-
              ing the same wall temperature. A typical example is double-pipe heat
              exchangers, which are usually treated as boundary condition (1).
                 Stephan (1962) developed a set of correlations. For boundary conditions
                                                                       6
              (1) and (2), the Nusselt number for turbulent flow (2300 Re 10 ) can be
              evaluated by the following equations, respectively:
                                   h            i
                                 0:45         2=3     0:75      0:42     0:14
                          ð
                Nu i ¼ 0:033 d o =d i Þ  1+ d h =LÞ  Re   180 Pr   ð μ=μ Þ
                                        ð
                                                                       w
                                                                         (2.37)
                                     h            i
                                               2=3     0:75       0:42     0:14
                         ð
              Nu o ¼ 0:037 1 0:1d i =d o Þ 1+ d h =Lð  Þ  Re   180 Pr  ð μ=μ Þ
                                                                         w
                                                                         (2.38)
                 For boundary condition (3), Stephan suggested the following relation:
                                          Nu i d i =d o +Nu o
                                    Nu ¼                                 (2.39)
                                             d i =d o +1
                 For hydrodynamically developed laminar flow in the thermal entrance
              region, Stephan expressed the Nusselt number as follows:

                                                              0:8
                                               0:19 RePrd h =LÞ
                                                   ð
                         Nu ¼ Nu ∞ + fd i =d o Þ                         (2.40)
                                      ð
                                                               0:467
                                            1+0:117 RePrd h =LÞ
                                                    ð
              in which Nu ∞ is the Nusselt number for fully developed laminar flow under
              the corresponding boundary condition, and the function f (d i /d o ) was given as
                            8
                                            1=2
                                     ð
                              1+0:14 d i =d o Þ  , heat transfer inner tube
                            <
                                           1=3
                   ð
                  fd i =d o Þ ¼  1+0:14 d i =d o Þ  ,  heat transfer outer tube  (2.41)
                                     ð
                            :              0:1
                              1+0:14 d i =d o Þ ,  heat transfer both tubes
                                     ð
                 Martin’s expressions (Gnielinski, 2010b, 2013b) can be used for Nu ∞ :
                       8
                                         0:8
                         3:66 + 1:2 d i =d o Þ  ,      heat transfer inner tube
                                  ð
                       >
                       >
                       <                0:5
                         3:66 + 1:2 d i =d o Þ ,       heat transfer outer tube
                                  ð
                Nu ∞ ¼
                       > 3:66 + 4 0:102= 0:02 + d i =d o Þ½  ð  Š heat transfer both tubes
                       >
                       :                          0:04
                                            ð d i =d o Þ  ,
                                                                         (2.42)
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