Page 194 - Thermal Hydraulics Aspects of Liquid Metal Cooled Nuclear Reactors
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System thermal hydraulics for liquid metals                       165

           when there is a relative acceleration between the two phases. This contribute is impor-
           tant only when the velocity is close to the sound speed in the fluid:
              Thermal energy equations


                                                       k
               ∂ α k ρ u k Þ  +  1 ∂ α k ρ u k w k AÞ ¼ p  ∂α k  p ∂ α k u A
                ð
                            ð
                                                      k
                               k
                    k
                  ∂t     A      ∂z          ∂t     A  ∂z
                                                   1    f k,w
                                                             2
                                        + q k,w + q k,i + α k ρ k  w w k j k ¼ f, gð  Þ
                                                             j
                                                   2     D   k
           where u k represents the internal energy for the phase k.
              In the previous energy equations, q k,w and q k,i are, respectively, the phasic wall heat
           transfer rate and the phasic interface heat transfer rate that take also into account for
           the energy associated with the interface mass transfer.
              Non-condensable gas
              If the gas includes also a noncondensable gas, the mass balance equation for the
           noncondensable gas must be added:
               ∂         1 ∂
                  α g ρ  +   α g ρ w g A ¼ 0
               ∂t    nc  A∂z    nc
           in which the noncondensable gas is assumed to move with the same velocity and hav-
           ing the same temperature of the vapor phase. For what concerns the energy and
           momentum balance equations, the noncondensable gas is accounted together with
           the vapor phase as a Daltonian gas mixture.
              In the previous equations, the calculation of the mass transfer through the interface
           Γ i , wall friction term F w , interfacial friction term F i , wall heat transfer q w , interfacial
           heat transfer q i , and virtual mass term F k,vm requires the use of empirical correlations:
           constitutive laws.



           4.3   Thermodynamic properties for the liquid metals
                 to be implemented in a STH code

           In STH codes, developed to cover a wide amount of working fluids, the thermody-
           namic property data functions are in general required as a function of both temperature
           and pressure. Frequently in the literature, the thermodynamic properties of a liquid
           metal are instead given at atmospheric pressure as temperature functions only, due
           to the very limited pressure dependence in common applications and the fact that fre-
           quently only liquid phase is considered. So, the reconstruction of the functional depen-
           dence from both temperature and pressure of these properties is needed to be
           implemented in the STH code.
              Moreover, a strategy for the reconstruction of the thermodynamic properties in
           vapor phase should be also accounted. This is mainly required to take into account
           the presence of noncondensable gases that may be used as cover gas and that can
           be mixed with the vapor phase of the used liquid-metal coolant.
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