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302                   Thermal Hydraulics Aspects of Liquid Metal Cooled Nuclear Reactors

         centrifugal fluid force becomes more important). At a given velocity, the tube will
         buckle in a ground mode shape and show small-amplitude vibrations around this buck-
         led state due to turbulence. The amplitude of the buckling increases with increasing
         flow velocity. The onset of buckling is also marked by a vanishing ground mode fre-
         quency. At even higher flow velocities, the tube starts to flutter around its initial
         straight position. Eventually, there is a small regime of restabilization in between
         the divergence (buckling) and flutter regime. Note that the maximal displacement
         in Fig. 6.2.2.7 consists of the sum of steady and unsteady contributions.



         6.2.2.3.2 Methodology
         The modal characteristics of a tube in the unstable region are determined with the
         methodology published earlier in De Ridder et al. (2013). Briefly summarized, this
         methodology consists of four steps:
         1. Compute in-vacuum eigenmodes of the structure.
         2. Deform solid and fluid domain with scaled eigenmodes.
         3. Compute the free vibration decay (w(z,t)) using a coupled CFD-CSM computation with a
            partitioned but fully coupled approach (Degroote et al., 2009).
                                                     P       c i t
         4. Fit a modal expression to the computed decay (w(z,t)   a i (z)e  sin(ω i t+φ i (z))).
         Note that the initially imposed in-vacuum mode of the structure alone does not nec-
         essarily agree with the modes of the fluid and structure together.
            The numerical settings are identical to those in the previous section. As turbulent
         eddies are not explicitly resolved, it is impossible to predict the turbulence-induced
         vibration part in Fig. 6.2.2.7 with the present computations. As inlet conditions, a very
         low inlet turbulence level is applied, so that turbulence in the flow is generated by the
         developing boundary layer on the tube. The grids used for the simulations are plotted
         in Fig. 6.2.2.8.


















         Fig. 6.2.2.8 Cross-sectional view of the meshes, with the fluid mesh in blue and the solid mesh
         in gray.
         Adapted from De Ridder, J., Doar  e, O., Degroote, J., Van Tichelen, K., Schuurmans, P.,
         Vierendeels, J., 2015. Simulating the fluid forces and fluid-elastic instabilities of a clamped-
         clamped beam in turbulent axial flow. J. Fluids Struct. 55, 139–154.
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