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The simulations of the Rayleigh-Taylor instability at Re = 420; the interface position obtained with the standard SPH approach (Eqs. (18), (14), (15)); the black points denote the reference data computed with the Level-Set formulation (312 × 634 cells) [8]. 

The simulations of the Rayleigh-Taylor instability at Re = 420; the interface position obtained with the standard SPH approach (Eqs. (18), (14), (15)); the black points denote the reference data computed with the Level-Set formulation (312 × 634 cells) [8]. 

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Smoothed Particle Hydrodynamics (SPH) is a fully Lagrangian, particle-based technique for fluid-flow computations. The main advantage over Eulerian techniques is no requirement of the grid, therefore this is a natural approach to simulate multi-phase flows. The main purpose of this study is an overview and the critical analysis of the SPH variants...

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... due to the computational efficiency, their usefulness is limited [ 10], and, therefore, those approaches are not discussed here. To verify the usefulness of the SPH formulations for incompressible multiphase flow computations, the case of the Rayleigh-Taylor instability has been simulated. The validation case involves two immiscible fluids enclosed in a rectangular domain of width L and height 2 L . Initially, the phases are separated by the interface located at y = L [1 − 0 . 15 sin (2 πx/L )]. The lower component has density L = 0 , while the upper one U = 1 . 8 0 . The kinematic viscosity is equal in both phases ( ν = ν L = ν U ). Since the system occurs under gravity g = [0 , − g ] and the upper phase is heavier, in the absence of the surface tension an instability always arises and vorticity is generated. For such a flow, the Reynolds number may be defined as Re = L 3 g/ν = 420. The simulations were performed with 120 × 240 particles initially homogeneously distributed in the domain. To compute the hydrostatic force, we use the technique described in [21], where the hydrostatic pressure is computed on a regular mesh and later projected on the particles. Figure 1 presents the SPH simulations compared to the Level-Set reference solutions (312 × 624 cells) obtained by Grenier et al. [8]. Presented data were computed at t = 1 , 3 , 5, normalized with the convective time scale T conv = L/g , and solved using Eqs. (14), (15) and (18), called here the standard formulation. Unfortunately, for the developed flow ( t = 5) the SPH results are not in good accordance with the Level-Set data. This discrepancy is caused by the use of Eq. (14). This symmetrical (with particle swapping) SPH form is constructed with the identity (13). Since the last term of Eq. (13) contains density gradient that is very high on the interface, this is the source of some instabilities ...

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