Page 428 - Design and Operation of Heat Exchangers and their Networks
P. 428

Experimental methods for thermal performance of heat exchangers  411


                 By means of the Laplace transform, it is easy to obtain the real-time tem-
              perature response:
                                                  ð
                                     h  p ffiffiffiffiffi i     0     p ffiffiffiffiffiffi
                                 x
                                          τ
                                                            x
                                         x
                                                              0
                    θ B¼0 ^x, ^τð  Þ ¼ e  ^ ^ τ I 0 2 ^^ + e  ^ x  e  τ  I 0 2 ^τ dτ 0  (8.76)
                                                  0^ τ
                                       τ
                                     x
                                   θ ^, ^Þ ¼ θ B¼0 ^x, ^τ  B^xð  Þ       (8.77)
                                    ð
              and outlet fluid temperature variation
                                 00
                                θ ^τðÞ ¼ θ B¼0 NTU, ^τ  BNTUð  Þ         (8.78)
                 The governing equation system (8.72)–(8.75) is identical to
              Eqs. (3.102)–(3.104) for B¼0. The solution for θ B¼0 ^x, ^τ  B^xð  Þ can be
              found in Section 3.3.1 by replacing t h , x, and y in Eq. (3.118) with θ B¼0 ,
                    τ
                        x
              ^ x, and ^ B^, respectively.
              8.3.2 Extended model
              Two important improvements have been made to extend the fundamental
              model. Howard (1964) added the axial heat conduction term into the energy
              equation of the solid wall and solved the problem numerically. The other
              improvement is to add the axial heat dispersion term into the energy equa-
              tion of the fluid to take the effect of the nonuniform flow distribution into
              account (Roetzel et al., 1993; Luo, 1997, 1998; Luo et al., 2001). Besides,
              the inlet fluid temperature variation can be arbitrary. Thus, the mathematical
              model for the single-blow testing technique can be extended as

                                                2
                              C ∂t    ∂t       ∂ t  αA
                                     _
                                  + C    ¼ A c D  +    ð t w  tÞ         (8.79)
                              L ∂τ    ∂x       ∂x 2  L
                                              2
                               C w ∂t w      ∂ t w  +  αA ð t  t w Þ     (8.80)
                               L ∂τ  ¼ A c,w λ w  ∂x 2  L
                                                  ∂t
                                          _
                                                       0
                                 x ¼ 0 : Ct  A c D  ¼ t τðÞ              (8.81)
                                                  ∂x
                                           ∂t w
                                              ¼ 0                        (8.82)
                                           ∂x
                                               ∂t
                                       x ¼ L :    ¼ 0                    (8.83)
                                               ∂x
                                           ∂t w
                                              ¼ 0                        (8.84)
                                           ∂x
                                      τ ¼ 0 : t ¼ t w ¼ t 0              (8.85)
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