Page 39 - Design and Operation of Heat Exchangers and their Networks
P. 39

26    Design and operation of heat exchangers and their networks


          temperature (H1): a 0 ¼8.235, a 1 ¼ 2.0421, a 2 ¼3.0853, a 3 ¼ 2.4765,
          a 4 ¼1.0578, and a 5 ¼ 0.1861. The maximum deviation of Eq. (2.31)
          was reported as 0.1% for Nu T and 0.03% for Nu H1 .



          2.1.1.6 Heat transfer in turbulent flow
          In the fully turbulent region, the velocity and temperature boundary layers
          are relative thin, and the form of the channel cross section has negligible
          influence on the heat transfer and pressure drop. Therefore, the correlations
          for a circular tube can be applied to other forms of channels except the ducts
          with sharp corners. A simple correlation for turbulent heat transfer is the
          Dittus-Boelter correlation (Dittus and Boelter, 1930):
                                         4
                              n
                          0:8
            Nu ¼ 0:023Re Pr      Re > 10 ,0:7 < Pr < 120, L=d h > 10  (2.32)
          where n¼0.4 for heating and n¼0.3 for cooling.
             For fine design calculation, the Gnielinski correlation is recommended
          (Gnielinski, 1975):
                                                 "          #
                                                          2=3
                               ð f =8Þ Re 1000ÞPr      d h
                                   ð
                        Nu ¼       p ffiffiffiffiffiffiffi   2=3    1+
                             1+12:7  f =8 Pr   1       L
                                            6            5
                            K 2300 < Re < 10 ,0:6 < Pr < 10           (2.33)
          where
                                                     2
                               f ¼ 1:82lg ReÞ 1:64Š                   (2.34)
                                  ½
                                         ð

                                0:11
                       ð Pr=Pr w Þ  for liquid,0:05 < Pr=Pr w < 20
                 K ¼           0:45                                   (2.35)
                       ð T b =T w Þ   for gas,0:5 < T b =T w < 1:5
             In the transition region, the heat transfer and pressure drop become very
          sensitive to the conditions of wall surface and incoming flow and have rel-
          ative large uncertainties, which yielded large deviations among different
          experiments. A commonly used method for evaluating Nu in the transition
          region is the interpolation between the laminar and turbulent regions
          (Gnielinski, 1995):
                                Re  Re cr
                              +           Nu                          (2.36)
                                  4
            Nu ¼ Nu lam,Re¼Re cr             tur,Re¼10 4  Nu lam,Re¼Re cr
                                10   Re cr
          with Re cr ¼2300.
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