Page 257 - Thermal Hydraulics Aspects of Liquid Metal Cooled Nuclear Reactors
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228                   Thermal Hydraulics Aspects of Liquid Metal Cooled Nuclear Reactors

            As outflow BCs have to represent the continuation of the physical domain beyond
         the edge of the computational domain, transport equations extrapolated from the
         domain interior are often enforced in the form of

             ∂Φ     ∂Φ
                + U c  ¼ 0                                           (6.1.1.12)
              ∂t     ∂x
         InmanycasesauniformvalueforU c ensuring massconservationisused.Anexpression
         for the convective velocity U c can be imposed in Eq. (6.1.1.12) also based on the spe-
         cific flow configuration. For example, Craske and van Reeuwijk (2013), which deal
         with turbulent jets and plumes, suggest the use of an exponential function for U c (y).
            In the review on open outflow conditions by Hattori et al. (2013), the method by
         Stevens (1990) is described as a promising approach for buoyant, turbulent plumes.
         The method proposed by Stevens (1990) is based on a one-dimensional advection-
         diffusion equation at the outflow, where a diffusion term is added to Eq. (6.1.1.12)
         and a phase velocity is introduced in addition to U c .



         6.1.1.3.4 Boundary conditions for the thermal field

         Turbulent channel geometry is also the most frequently used geometry for studies of
         the near-wall heat transfer. The most accurate approach is conjugate heat transfer,
         where heat conduction inside the realistic heated walls is taken into account.
         A relevant study for liquid metal applications is the DNS of Tiselj and Cizelj
         (2012), who performed a conjugate heat transfer DNS at a low Prandtl number,
         Pr ¼ 0.01. Most of the DNS heat transfer studies (Kasagi et al., 1992; Kawamura
         et al., 1998; Na and Hanratty, 2000) were performed with simplified thermal BCs
         without solid walls and the dimensionless temperature at the fluid-solid contact plane
         that was fixed to zero:


             θðy ¼ hÞ¼ 0 ðnonfluctuating thermal BCÞ                 (6.1.1.13)

         This type of thermal BC is a very good approximation of reality when the thermal activ-
                   q ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi                 +
         ityratioK ¼  ðλρc p Þ =ðλρc p Þ goestozero,whiletheheatedwallthicknessd ,andthe
                          f      w
         parameter G ¼ α f /α w remains finite (α ¼ λ/ρc p ). In that case, temperature fluctuations
         generated in the fluid do not penetrate into the solid wall. This type of ideal thermal BC
         was denoted as “nonfluctuating BC” by Tiselj and Cizelj (2012). An example of such
         systemisair/metalcombinationoffluidand solid.Forwater/steelcombinationthether-
         mal BC is still close to nonfluctuating BC if the heated wall is thick enough; however,
         the approximation fails when the metal wall thickness is small.
            The thermal BC, which permits maximum penetration of the turbulent temperature
         fluctuations from the fluid into the solid, is defined as:

                                  !
                                ∂θ 0
             hθðy ¼ hÞi   ¼ 0           ¼ 0 ðfluctuating thermal BCÞ  (6.1.1.14)
                       x,z,t
                                ∂y
                                    y¼ h
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