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Dynamic analysis of heat exchangers and their networks  343


              is usually adopted in solving the differential equations. By this technique, the
              differential equations are substituted by the finite-difference equations.
                 The first step of this method is to discretize the solution space, that is, to
              divide the spatial and time spaces into M and N intervals, x 0 <x 1 <…<x M ,
              τ 0 <τ 1 <…<τ N , with the grid steps Δx i ¼x i  x i 1 and Δτ j ¼τ j  τ j 1 .
              According to the finite-difference forms of the spatial derivatives, the
              finite-difference method is further divided into the explicit and implicit rep-
              resentations  and  other  combinations  of  these  two  preliminary
              representations.
                 For a parallel-flow heat exchanger, if a forward finite-difference scheme
              is applied to the time derivative, the differential equations (7.21)–(7.23) can
              be discretized into following explicit finite-difference equations:

                       Δτ            Δτ
                  n       n 1                       n 1           n 1
                  t ¼    t    +1         NTU 1 Δτ t    + NTU 1 Δτt       (7.99)
                  1,i     1,i 1                     1,i           w,i
                      Δx             Δx
                      Δτ              Δτ   NTU 2 Δτ       NTU 2 Δτ
                t n  ¼   t n 1  +1                   t n 1  +      t n 1  (7.100)
                2,i       2,i 1                      2,i           w,i
                    R τ Δx          R τ Δx    R τ            R τ

               n       NTU 1 Δτ  R 2 NTU 2 Δτ  n 1  NTU 1 Δτ  n 1  R 2 NTU 2 Δτ  n 1
               t  ¼ 1                     t   +       t   +          t   (7.101)
               w,i                         w,i         1,i           2,i
                         R w       R w            R w          R w
              in which the dimensionless variables and parameters are defined as follows:
                              _
                                                                         _
                                                     _
                x ¼ x=L, τ ¼ τC 1 =C 1 , NTU 1 ¼ αAÞ =C 1 , NTU 2 ¼ αAÞ =C 2 ,
                                              ð
                                                                  ð
                                                   1                  2
                           _   _          _  _
                                                 ð
                     R 2 ¼ C 2 =C 1 , R τ ¼ C 1 =C 2 = C 1 =C 2 Þ, R w ¼ C w =C 1
              To maintain numerical stability, Δx and Δτ should be chosen according to
              the following constraints:
                         Δτ                             Δx
                      1      NTU 1 Δτ   0or Δτ                          (7.102)
                         Δx                         1 + NTU 1 Δx
                         Δτ    NTU 2 Δτ                 R τ Δx
                     1                    0or Δτ                        (7.103)
                        R τ Δx     R τ               1 + NTU 2 Δx
                   NTU 1 Δτ   R 2 NTU 2 Δτ                  R w
                1                          0or Δτ                       (7.104)
                      R w         R w                NTU 1 + R 2 NTU 2

              With the given initial and boundary conditions, Eqs. (7.99)–(7.101)
              can be used to calculate and analyze the dynamic temperature responses
              of the exchanger subject to arbitrary inlet temperature and/or flow
              disturbances.
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