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Basic thermal design theory for heat exchangers  45


              2.1.4 General energy equations for steady-state and dynamic
              analysis of heat exchangers

              For general flow processes, the energy equation can be expressed as
              (Whitaker, 1977)


                     ∂T                            ∂p
                                      ð
                ρc p    + V  rT ¼r λrTÞ + βT         + V  rp + μΦ + s    (2.90)
                     ∂τ                            ∂τ
              in which T is the thermodynamic temperature, s the volumetric heat source,
              Ф the dissipation function, and β the thermal expansion coefficient:

                                            1 ∂v
                                        β                                (2.91)
                                            v ∂T
                                                   p
                 Since the flow in a heat exchanger is usually a low-velocity flow (Mach
              number Ma<0.3), the pressure variation would not be very large; therefore,
              even for gases, the pressure term in Eq. (2.90) can be omitted. Furthermore,
              if the Peclet number is not very high, the viscous dissipation in low-velocity
              flow can be neglected. Although the real velocity distribution in a heat
              exchanger is three-dimensional and could be very complicated, there is a
              main flow direction for each fluid. The main assumption to be used is that
              the fluid is completely mixed in the lateral direction but the axial mixing is
              negligible. Therefore, the flow velocity and temperature over the section
              perpendicular to the main flow direction are uniform. Such a flow pattern
              is called plug flow. By integrating Eq. (2.90) over the flow passage section
              perpendicular to the main flow direction and using the average values of the
              temperature and fluid properties over the cross-sectional area, the energy
              equation can be simplified to

                                                  Z       ðð
                          ∂t   _  ∂t  ∂     ∂t
                     A c ρc p  + C  ¼    A c λ  +   qdP +     sdA c      (2.92)
                          ∂τ    ∂x   ∂x     ∂x     P        A c
                         Ð
                 The term  P qdP is the convective heat transfer from the solid wall of the
              exchanger to the fluid per unit length along the flow direction:
                                    Z       Z
                                      qdP ¼   α t w  tÞdP                (2.93)
                                               ð
                                     P       P
              in which P is the wetted perimeter of the flow channel at x. If a flow channel
              consists of N w walls and the wall temperature and convective heat transfer
              coefficient of each wall are uniformly distributed along its wetted perimeter,
              then the convective heat transfer term can be expressed as
                                  Z        N w
                                           X

                                     qdP ¼    α j P j t w, j  t          (2.94)
                                    P      j¼1
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