Page 34 - Design and Operation of Heat Exchangers and their Networks
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Basic thermal design theory for heat exchangers  21


                                            h                      i 3
                                         3
                                   3
                       Nu 3  ¼ 3:66 +0:7 +1:077 RePrd=xÞ   1=3   0:7
                                                  ð
                          x,T
                                "                           # 3
                                              1=6
                                 1     2                 1=2
                              +                 ð RePrd=xÞ               (2.18)
                                 2 1 + 22Pr
                 In Fig. 2.3, these equations are compared with the equation of Stephan
              (Baehr, 1960)
                                                           1:33
                                           0:0677 RePrd=LÞ
                                                 ð
                              Nu T ¼ 3:66 +                              (2.19)
                                                           0:83
                                           1+0:1Pr Red=LÞ
                                                   ð
              and the equation of Churchill and Ozoe (1973b)
                          n                       o 3=8
                                               8=9
              Nu x,T ¼ 5:357 1 + π=388ð½  ÞRePrd=xŠ
               2    0                                                  1 4=3 33=8
                                       ð π=284ÞRePrd=x
               6    B                                                  C   7
                1+ @4                                                  A   5
                      n                 o 1=2 n                    o 3=4
                                      2=3                        8=9
                                                 ð
                       1+ Pr=0:0468Þ         1+ π=388ÞRePrd=xŠ
                                                ½
                           ð
                  1:7                                                    (2.20)
                                                                          6
              The maximum deviation among them is 6.5% in 0.1<RePrd/L<10 and
              0.7 Pr 10.
                         10 3
                               Nu T , Eq. (2.17) (Gnielinski, 1989, 2010a, 2013a)
                               Nu T , Eq. (2.19) (Baehr, 1960)
                               Nu x,T , Eq. (2.18) (Gnielinski, 2010a, 2013a)
                               Nu x,T , Eq. (2.20) (Churchill and Ozoe, 1973)

                         10 2                   Pr = 0.7
                       Nu T , Nu x,T         Nu T



                         10                                  Pr = 10
                                                          Nu x,T




                          1
                          0.1    1    10    10 2  10 3  10 4  10 5  10 6
                                             RePrd/x
              Fig. 2.3 Local and mean Nusselt number Nu x,T and Nu T for thermally and
              hydrodynamically developing laminar flow.
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