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10.3 Heat transfer to liquid coolant  113




                     The nodal internal power generation, P c , the fuel temperature, T f , and the inlet
                  coolant temperature, θ in , are defined by other subsystem equations. That leaves
                  two variables, but the coolant equation provides only one. An assumption is required
                  to eliminate θ out . θ avg must be retained because it appears in the equation for heat
                  transfer from fuel to coolant. The average temperature is given by the following:
                                            θ avg ¼ θ in + θ out Þ=2            (10.3)
                                                 ð
                  or
                                                                                (10.4)
                                             θ out ¼ 2 θ avg   θ in
                  There is a problem with this formulation. Note in Eq. (10.4) that a sudden increase in
                  inlet temperature would cause a sudden decrease in outlet temperature. This is an
                  unphysical feature, causing consideration of an alternate formulation.
                     Another possibility is the “well-stirred-tank” formulation. That is, the outlet tem-
                  perature from the node is set equal to the average node temperature. This solves the
                  problem in the previous formulation, but equating average and outlet temperatures
                  does not represent actual behavior very well.
                     Ray Mann of Oak Ridge National Laboratory addressed the problem [2]. Mann’s
                  formulation uses two coolant nodes adjacent to a single fuel node; Fig. 10.2 shows
                  this arrangement. Well-stirred-tank models represent each pair of coolant nodes. The
                  outlet temperature of the first coolant node (assumed equal to the average tempera-
                  ture of that node) serves as the coolant temperature that provides the driving force for
                  heat transfer from the fuel. Each coolant node receives half of the heat transfer from
                  the fuel node. Therefore, the model equations for Mann’s formulation are as follows:
                                      dθ 1             UA
                                              ð
                                 M c C c  ¼ WC c θ in  θ 1 Þ +  T f  θ 1 + P c1  (10.5)
                                       dt               2
                                      dθ 2             UA
                                               ð
                                  M c C c  ¼ WC c θ 1  θ 2 Þ +  T f  θ 1 + P c2  (10.6)
                                       dt               2
                                                            ∼
                                                            Θ 2
                                                          ∼
                                                          Θ 2

                                                            ∼
                                           T f              Θ 1

                                                          ∼
                                                          Θ 1



                                                          Q in
                  FIG. 10.2
                  Schematic of Mann’s model with one fuel node and two coolant nodes.
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