Page 101 - Design and Operation of Heat Exchangers and their Networks
P. 101

Steady-state characteristics of heat exchangers  89


              all of those solutions were mathematically equivalent and all of the expres-
              sions obtained required a numerical evaluation.
                 The energy equations for the crossflow with both fluids unmixed can be
              expressed as follows:

                                      _  ∂t h  kA
                                     C h   ¼    ð t c  t h Þ             (3.97)
                                        ∂x   L x
                                             kA
                                      _  ∂t c
                                     C c   ¼    ð t h  t c Þ             (3.98)
                                        ∂y   L y
                 Normalizing the temperature of each fluid and the length of the
              exchanger in its flow direction,


                                        _
                                x ¼ kA=C h x=L x ¼ NTU h x=L x           (3.99)

                              _
                     y ¼ kA=C c y=L y ¼ NTU c y=L y ¼ R h NTU h y=L y   (3.100)
                                             t  t 0
                                          t ¼    c                      (3.101)
                                             t  t 0
                                             0
                                             h   c
              we can present the energy equations in the dimensionless form as
                                         ∂t h
                                            ¼ t c  t h                  (3.102)
                                         ∂x
                                         ∂t c
                                            ¼ t h  t c                  (3.103)
                                         ∂y
              with the boundary condition
                                 x ¼ 0 : t h ¼ 1; y ¼ 0 : t c ¼ 0       (3.104)
                 We will solve this equation system by means of the Laplace transform.
              Applying the Laplace transform respecting to y, we obtain the ordinary dif-
              ferential equation:

                                        de t h  s
                                           ¼      e t h                 (3.105)
                                        dx    s +1
              with the boundary condition

                                       x ¼ 0 : e t h ¼ 1=s              (3.106)
                 The solution in the Laplace domain is derived as

                                             1   sx

                                         e t h ¼ e s +1                 (3.107)
                                             s
   96   97   98   99   100   101   102   103   104   105   106