In this work we extend the Particle Finite Element Method (PFEM) to multifluid flow problems with the aim of exploiting the fact that Lagrangian methods are specially well suited for tracking interfaces. We develop a numerical scheme able to deal with large jumps in the physical properties, included surface tension, and able to accurately represent all types of discontinuities in the flow variables. The scheme is based on decoupling the velocity and pressure variables through a pressure segregation method which takes into account the interface conditions. The interface is defined to be aligned with the moving mesh, so that it remains sharp along time, and pressure degrees of freedom are duplicated at the interface nodes to represent the discontinuity of this variable due to surface tension and variable viscosity. Furthermore, the mesh is refined in the vicinity of the interface to improve the accuracy and the efficiency of the computations.
We apply the resulting scheme to the benchmark problem of a twodimensional bubble rising in a liquid column presented in [1], and propose two breakup and coalescence problems to assess the ability of a multifluid code to model topology changes.
Keywords: Particle Finite Element Method (PFEM); Lagrangian simulation; multifluid flows; pressure segregation; surface tension; bubble dynamics.
The simultaneous presence of multiple fluids with different properties in external or internal flows is found in daily life, environmental problems, and numerous industrial processes. Examples are fluidfuel interaction in enhanced oil recovery, blending of polymers, emulsions in food manufacturing, rain droplet formation in clouds, fuel injection in engines, and bubble column reactors, to name only a few. Although multifluid flows occur frequently in nature and engineering practice, they still pose a major research challenge from both theoretical and computational points of view.
In the case of immiscible fluids, the dynamics of the interface between fluids plays a dominant role. The success of the simulation of such flows depends on the ability of the numerical method to model accurately the interface and the phenomena taking place on it, such as the surface tension. The origin of the surface tension force lies in the different intermolecular attractive forces that act in the two fluids, and the result is an interfacial energy per area that acts to resist the creation of new interface, so that the interface behaves like a stretched membrane trying to minimize its area.
The main difference between a singlefluid flow (homogeneous) and a multifluid (heterogeneous) one is the presence of internal interfaces. In addition to the wellknown difficulties in the simulation of homogeneous flows, namely the coupling of pressure and velocity through the incompressibility constraint, the need of the discretization spaces to satisfy the infsup condition, and the nonlinearity of the governing equations, numerical methods for heterogeneous flows face the following challenges:
This paper extends the work of the authors in the study of multifluid flows with the Particle Finite Element Method [2]. The new contributions include the scheme for describing the interface, the computation of surface tension and the enhanced pressure segregation approach. We have found that these developments are essential for accurately modeling of bubble dynamics. The paper is organized as follows: In Section 2 we present the governing equations together with the interface conditions and the possible discontinuities of the flow variables. In Section 3 we briefly review the interface descriptions most used in the literature, to focus later in the Particle Finite Element Method (Section 4) and the numerical scheme we have developed (Sections 5 and 6). Finally, in Section 7 we apply the PFEM to the solution of the twodimensional bubble rise, breakup and coalescence problems.
Figure 1: Twofluid flow configuration. 
Let , , be a bounded domain containing two different fluids (see Figure 1). We denote time by , the Cartesian spatial coordinates by , and the vectorial operator of spatial derivatives by . The evolution of the velocity and the pressure is governed by the NavierStokes equations:

where is the density, the Cauchy stress tensor, the vector of gravity acceleration, and represents the total or material derivative of a function . The constitutive equation for a Newtonian and isotropic fluid takes the form

(2) 
with the identity tensor, the dynamic viscosity, the strain rate tensor, and the volumetric strain rate.
Let be the interface that cuts the domain in two open subdomains, and , which satisfy: , , and . In each subdomain, the physical properties are defined as:

(3) 
If density and viscosity are assumed to remain constant in each fluid (i.e. fluids are incompressible, immiscible, and isothermal), we have that and . Consequently, we have on the one side that , this is the mass conservation equation for incompressible flows; and on the other side, that . This latter consequence means that interfaces are material surfaces, which move with the fluid velocity , and therefore, they are naturally tracked in Lagrangian formulations.
In order for the NavierStokes problem (1) to be wellposed, suitable boundary conditions need to be specified. On the external boundary , such that , we consider the following:

is the prescribed velocity, the outer unit normal to , and the prescribed traction vector. A Neumann boundary with is called free surface.
On the internal interfaces , the coupling conditions are [3]:

with now the unit normal to , the surface tension coefficient, the interface curvature, and represents the jump of a quantity across the interface.
Equation (6) expresses the continuity of all velocity components. The normal component has to be continuous when there is no mass flow through the interface, and the tangential components have to be continuous when both fluids are viscous (), similar to a noslip condition.
Equation (7) expresses that the jump in the normal stresses is balanced with the surface tension force. This force is proportional to the interface curvature and points to the center of the osculating circle that approximates . The surface tension coefficient is assumed constant and its value depends on the two fluids at the interface.
Discontinuities at the interface can be of two types:
Differences in density at the interface cause a kink in the hydrostatic pressure profile, leading to a jump in the pressure gradient, and then to a discontinuity in the pressure field (Fig. 2a).
Differences in viscosity lead to discontinuous components of the strain rate tensor , and therefore to a discontinuity of the velocity field at the interface (Fig. 2b):

(8) 
with the tangential derivative.
Both differences in viscosity and the presence of surface tension cause a discontinuity in the pressure field (Figs. 2b and 2c), as shown in [4]:

(9) 
Notice that even in the case of , pressure is discontinuous when .
(a)  (b) 
(c)  
Figure 2: Flow discontinuities for: (a) density jump, (b) viscosity jump, and (c) surface tension. 
(a)  (b) 
Figure 3: (a) Moving mesh adapted to the interface, and (b) fixed mesh, where interface moves through the elements. 
The main classification of interface descriptions is regarding the reference frame adopted (see Figure 3). In the moving mesh methods, the mesh is deformable and adapted to the interface, which is explicitly tracked along the trajectories of the fluid particles. Examples are methods based on the Arbitrary LagrangianEulerian (ALE) formulation [9,10], the deformablespatialdomain/stabilized spacetime deformation (DSD/SST) method [11,12], or the fully Lagrangian formulation such as in [13,14] and the Particle Finite Element Method [15,16,17,18].
On the other hand, fixed mesh methods use a separate procedure to describe the position of the interface. They can be further grouped in fronttracking methods, which use massless marker points to follow the fluid interface while the NavierStokes equations are solved on a fixed mesh [19,20], and frontcapturing methods, which introduce a new variable in the model to describe the presence or not of a fluid in a position of the domain. The most extended frontcapturing methods are the VolumeOfFluid, originally developed by Hirt [21], and the Level Set method by Osher et al. [22].
The Particle Finite Element Method (PFEM) is a Lagrangian numerical technique for modeling and analysis of complex multidisciplinary problems in fluid and solid mechanics involving thermal effects, interfacial and freesurface flows, and fluidstructure interaction, among others.
PFEM is a particle method in the sense that the domain is defined by a collection of particles that move in a Lagrangian manner according to the calculated velocity field, transporting their momentum and physical properties (e.g. density, viscosity). The interacting forces between particles are evaluated with the help of a mesh. Mesh nodes coincide with the particles, so that when the particles move so does the mesh. On this moving mesh, the governing equations are discretized using the standard finite element method. The possible large distortion of the mesh is avoided through an efficient Delaunay triangulation remeshing [23] of the computational domain. Due to the fact that all the hydrodynamical information is stored in the nodes, remeshing does not introduce numerical diffusion. This gives the method excellent capabilities for modeling large displacement and large deformation problems. A more detailed explanation of the method can be found in e.g. [16,17,24].
Since in PFEM the interface is described by mesh nodes and element edges (Fig. 3a), it is a welldefined curve, with the information regarding its location and curvature readily available. The interface nodes carry the jump of properties (e.g. density, viscosity), maintaining the interface sharp without diffusion along time. Furthermore, it is straightforward to impose the boundary conditions on the interface and to treat any number of fluids.
Regarding the modeling of the jumps in the fluid properties across the interface, while in fixed mesh methods typically the interface is considered to have a finite thickness and the fluid properties change smoothly and continuously from the value on the one side of the interface to the value on the other side, PFEM treats the interface in a sharp manner, so that it is clear which property value is valid at each point.
Figure 4: Pressure profiles when using continuous and discontinuous representations. 
Regarding the modeling of the discontinuities in the flow variables across the interface (see Section 2.1), in fixed mesh methods where the physical properties have been smoothed, functions are continuous across the interface and thus not appropriate for the approximation of discontinuous variables. When the physical properties are modeled sharp, the elements cut by the interface require a special treatment in order to be able to represent the discontinuities. Gravity dominated flows will require “enrichment” of the pressure approximation, and viscosity dominated flows will require “enrichment” of the velocity approximation. On the contrary, discontinuities need no special attention when the interface is aligned with the mesh, as the kinks in the solution are automatically represented. Only discontinuities need some attention in PFEM. In particular, the pressure field has been made doublevalued at the interface, i.e. pressure degrees of freedom have been duplicated (, ) in the interface nodes [4]. The pressure discontinuity is thus optimally approximated. Figure 4 shows that the use of continuous pressure representations may introduce errors in the incompressibility condition.
The Lagrangian approach simplifies the equations by separating the problem into a geometrical part (tracking the motion of the nodes)

(10) 
and a physical part (calculating how the flow variables change in time at each node) described by the following Stokes equations:

The latter can be further split into two parts: one related to viscosity effects, and the other related to the incompressibility. According to the incremental pressure segregation scheme [25], and after implicit backward Euler time discretization, we propose the following splitting of equations (11) [26]:



(14) 
The interfacial stress jump condition has been consistently split between steps 1 and 2. Although the continuity of the pressure difference across the interface expressed in Eq. (13.d) seems to be in contradiction with the fact that pressure is discontinuous at the interface, the scheme is able to capture this discontinuity without need of enforcing it explicitly [26].
After discretization in space (Galerkin weighted residual method), and assuming to be a free surface (i.e. ), the split discrete equations read:

where , are the vectors of nodal velocities and pressure, is the intermediate velocity introduced by the fractional step, and the time step. The matrices density weighted mass matrix, gradient matrix, divergence matrix, viscosity weighted stiffness matrix and the external force vector are defined as

where and are the standard linear FE shape functions for velocity and pressure, and superscripts refer to node indices.
The accuracy in the treatment of the discontinuous density and viscosity will be determined by how well the numerical method is able to evaluate the integrals where these discontinuities are included. Unless the interface coincides with edges of elements, there is no way for standard element shape functions to capture the discontinuity of properties inside an element. This implies that one has either to increase the number of Gauss points (e.g. see discussion about numerical integration of discontinuous and singular functions in [27]) or enrich the shape function space, as e.g. in [28,29] and in the eXtended Finite Element Method (XFEM) [30,31]. The nodal interface description for immiscible fluids in PFEM allows to evaluate exactly these integrals.
Conditions (12.c) and (12.d) are naturally included in , while pressure conditions (13.c) on and (13.d) on need to be weakly imposed in order to overcome the singularity of :

Both integrals are discretized in space as , with the pressure mass matrix on the contours and , and incorporated into the pressure Poisson equation in the following way [32]:

(23) 
The penalty parameter is defined as . It has to be sufficiently large so that the system matrix becomes invertible. is a scalar factor such that for , the pressure equation is satisfied but the discrete system may continue singular, and is equivalent to apply the pressure condition strongly and then the equation may not be satisfied.
Moreover, stabilization is needed in incompressible flows when interpolation spaces for velocity and pressure do not satisfy the infsup condition. Many stabilization procedures have been proposed in the literature, such as the StreamlineUpwind/PetrovGalerkin, Galerkin LeastSquares, Finite Calculus or Orthogonal SubScale methods. Those that include a projection of the pressure gradient need to be modified when density changes at the interface to take into account the discontinuity of the hydrostatic pressure gradient. Details are explained in [2] and [33].
The surface tension force at the interface, , is naturally incorporated in the weak form of the finite element method. If it is discretized explicitly, i.e. the surface tension force is evaluated on the interface at the previous time step, the stability of the scheme imposes the following restriction on the time step size [34]:

(24) 
where , is the mesh size and the capillary time step. With this restriction the propagation of capillary waves is resolved and their unstable amplification avoided. Unfortunately, Eq. (24) can be rather limiting for fine meshes and large surface tension coefficients. An implicit [35] or semiimplicit [36] treatment of the surface tension would circumvent this constrain.
The interface representation by nodes and element edges in PFEM allows for an easy and accurate incorporation of the surface tension, avoiding the need of regularization techniques such as the Continuum Surface Force [34].
There are several ways to calculate the curvature from the information of the interface location. The one we have followed in this work is based on the osculating circle of a curve, which is defined as the circle that approaches the curve most tightly among all tangent circles at a given point. From the radius of the osculating circle, the quantity required for is calculated as:

(25) 
Figure 5: Calculation of the osculating circle at node . 
Figure 6: Static bubble initial configuration. 
We have simulated the equilibrium state of a circular bubble of a radius (constant curvature ) in a static fluid with , , , and . The simulations have been run 100 time steps with fixed to 0.01. The bubble should remain exactly stationary and the velocity of the fluid should be exactly zero. But if the pressure is approximated continuously, the pressure fluctuations near the interface generate spurious velocity currents (see Figure 7) that may deform the bubble shape, produce a significant mass loss [38] and spoil the solution.
Figure 7: Spurious velocities in static bubble for continuous pressure. 
Figure 8 shows the pressure solution for continuous approximation and different mesh sizes. The exact jump is . We observe that the pressure solution oscillates at the interface, and it improves with finer meshes. In the case of discontinuous pressure approximation shown in Figure 9, the solution is already excellent for coarse meshes. The velocity error (measured in the norm ) for both approximations is shown in Table 1. The discontinuous pressure produces velocity solutions three orders of magnitude better than the continuous one.
(a)  (b) 
Figure 8: Continuous pressure approximation: (a) profile at final time for different , and (b) pressure field for . 
(a)  (b) 
Figure 9: Discontinuous pressure approximation: (a) profile at final time for different , and (b) pressure field for . 
Continuous  Discontinuous  
1/20  
1/40  
1/80 
Finally, Figure 10 shows the influence of the parameter on the pressure solution at the interface. For the minimum value that makes the system Eq. (23) invertible, the pressure profile is flat at the interface, i.e. the jump is represented exactly and incompressibility is satisfied. The larger the value of , the more strongly the pressure continuity condition at the interface is imposed.
Figure 10: Pressure profile for discontinuous approximation and . Influence of value on the pressure jump at the interface: , , . 
The numerical scheme developed in the previous sections will be tested in the problem of a bubble rising in a liquid column.
Bubbles and bubbly flows play a significant role in a wide range of geophysical and industrial processes, such as mixing in chemical reactors, elaboration of alloys, cooling of nuclear reactors, twophase heat exchangers, aeration processes, and atmosphereocean exchanges.
The shape and rise velocity of a bubble are controlled by the physical properties of the fluids and the surrounding flow field. Grace [39] developed a wellknown graphical correlation for single gas bubbles rising in an infinite liquid using three dimensionless numbers: the Reynolds number (), the Eötvös number (), and the Morton number ().

where is an equivalent diameter of the bubble, and the rising speed of the bubble. [39] classifies the bubble shapes into three regimes: spherical, ellipsoidal, and spherical cap. Bubbles with low or low are spherical. For higher , bubbles have an ellipsoidal shape at intermediate and spherical cap shape at high . A more detailed regime diagram was given by Clift et al. [40], which included wobbling bubbles for in the ellipsoidal regime, and the spherical cap regime was subdivided into spherical cap, skirted, and dimpled ellipsoidal cap for high, intermediate, and low numbers, respectively. These diagrams were further developed by Bhaga et al. [41], who also studied the flow field around the bubble, specially the wake that forms in the rear of the bubble for intermediate and high .
Numerous experimental studies have been performed to understand the flow dynamics of a single rising bubble, e.g. by [42,39,43,40,41,44,45,46], but the fact that approximate theoretical solutions have only been derived in the limit of very small bubble deformations, together with the difficulties in experimentally measuring the flow variables of the bubble without any interference while it is rising and deforming, make numerical simulation an important tool to gain insight of the flow.
Previous numerical studies have mostly followed the fixed mesh approach: the pioneering works [47], [48], and [49] used the fronttracking method (together with finite differences), also [50] (finite differences) and [51] (finite volume method); level set is used by [27,26,1] (finite elements) and [52] (finite volumes); VolumeofFluid is used in [53] and [54]; [55] use a hybrid approach between VOF and level set (finite volumes); and interface fitting method in [56] and [45]. The LatticeBoltzmann method is used e.g. in [57] and [58]. In these numerical works, results are qualitatively compared with experimental observations of bubble shape under different regimes. Only recently, quantitative tests for twodimensional rising bubbles have been proposed by Hysing et al. [1]. In Section 7.1 we compare the PFEM results with these test solutions, and in Section 7.2 we propose two problems on bubble breakup and coalescence to assess the ability of a multifluid code to model topology changes.
Figure 11: Initial configuration. 
The problem consists in a bubble rising in a liquid column as illustrated in Figure 11. Two tests have been proposed in [1]: test 1 considers a bubble in the ellipsoidal regime which undergoes moderate shape deformation, while in the test 2 the bubble belongs to the skirted regime and experiences much larger deformation. Both fluids are Newtonian, incompressible and isothermal, and their physical properties are listed in Table 2.
Test case  g  
1  1000  100  10  1  0.98  24.5  35  10  10  10 
2  1000  1  10  0.1  0.98  1.96  35  125  1000  100 
The reference solutions presented in [1] have been run with three different numerical approaches: the TP2D [59], the FreeLIFE [60], and the MooNMD [61]. They all use the finite element method, but the two first approaches describe the interface with the level set, while the latter tracks it in an arbitrary LagrangianEulerian way. More specific details about the methods can be found in the original publication. The following bubble quantities are used to compare the results:
The computations have been performed on unstructured meshes with element size in the bulk of the fluids and wall regions, and the mesh at the interface has been refined to , , and in order to analyze the convergence in of the solution. With a refinement based on the distance to the interface (see Figure 12), we can use an arbitrarily fine mesh without increasing the total number of nodes to impractical values as would be the case with an uniform mesh.
Figure 12: Mesh is refined close to the interface with the help of a distance function. 
 
Figure 13: Test 1. Bubble evolution for mesh size . 
For test 1, Figure 13 shows the evolution of the rising bubble. At final time s we compare the PFEM bubble shapes for the meshes and , and observe that they converge to the shape of the finest mesh (Figure 14), which is in good agreement with the TP2D solution reported in [1] (Figure 15a). The plots of the bubble circularity (Figure 15b) and rise velocity (Figure 15d) show that our bubble is slightly oscillating, but the evolution of the center of mass (Figure 15c) is again in good agreement. The oscillating behavior of the PFEM results may be explained by the fact that, on the one side, PFEM does not introduce diffusivity at the interface, and on the other side, the geometrical method we use to calculate the curvature (the osculating circle) may not be accurate enough. Regarding the volume conservation, without any correction technique the bubble volume variation between the initial and final times, , is of order (Table 3).
Figure 14: Test 1. PFEM bubble shape for different mesh sizes at s. 
(a) Shape at s  (b) Circularity 
(c) Center of mass  (d) Rise velocity 
Figure 15: Test 1. Comparison of benchmark quantities: PFEM () vs. TP2D results. 
Test  Initial Volume  Final Volume  Variation  
1  1/320  0.19635  0.1965  
2  1/640  0.19635  0.19633 
Same type of results are shown for test 2 in Figures 16, 17, and 18. Although the bubbles in both test cases rise with similar velocity, the decrease in surface tension causes bubble 2 to undergo a much larger deformation and to develop thin filaments. In the TP2D and FreeLIFE solutions these filaments break up, in contrast to the moving mesh solutions of PFEM and MooNMD (Figure 18a). In the physical reality, breakup occurs due to capillary waves present on the interface, which trigger the threedimensional PlateauRayleigh instability when the filament radius is small enough. Thus, capillary waves can cause the skirt filament to fragment during flow, though this response requires very large elongations, typically greater than 20 times the initial bubble radius [62]. Figure 19 shows the mesh of the PFEM solution in the skirted region. The filament is not thin enough to break up. The volume variation is excellent again, of order .
(16) Test 2. Bubble evolution for mesh size .  

Figure 17: Test 2. PFEM bubble shape for different mesh sizes at s. 
(a) Shape at s  (b) Circularity 
(c) Center of mass  (d) Rise velocity 
Figure 18: Test 2. Benchmark quantities comparison of PFEM (black line) and TP2D (red), FreeLIFE (green) and MooNMD (blue) results. 
Figure 19: Test 2. Detail of bubble skirt at s. 
The fact of using an explicit approach when discretizing in time the surface tension force introduces the stability condition for the time step expressed in Eq. (24). If larger time steps are taken, instabilities will develop at the interface. This time step constraint is very restrictive for fine meshes (). In our case, the refined mesh close to the interface imposes rather small global time steps (for test 1 with mesh , ; and for test 2 with , ) that undoubtedly affect the computational efficiency.
Topology changes in multifluid flows can be divided into two classes [63]:
In order to test the capabilities of PFEM to handle interfaces with changing topology, and motivated by the disagreement in the solution of test 2, we have simulated two examples on a film that fragments, namely the breakup and coalescence of bubbles.
We consider the same fluid properties and configuration of test 1. In the case of the breakup, we add a flat interface at so that the upper region belongs to the same fluid than the bubble (see Figure 20a). The bubble rises, approaching the flat interface. The film of heavy fluid that separates the two regions of light fluid becomes thinner and thinner until it fragments and the regions fuse (Figure 20). Whereas in the physical reality the fragmentation of the film is caused by attractive forces at the microscopic scale (forces which are usually not included in the continuum description), in our simulations fragmentation is caused by a connectivity change at the interface, as illustrated in Figure 21.
 
Figure 20: Bubble breakup. 
One of the main difficulties we face in our Lagrangian approach is the connectivity changes introduced by the remeshing process. In general, these reconnections may alter the equilibrium at the interface, slow down convergence and affect mass conservation. Thus, in interfacial flows it is essential to avoid them. We are using an unconstrained Delaunay triangulator which does not allow to fix connectivities. Therefore, to ensure that a specific connectivity remains, we refine long interfacial edges and remove nodes too close to the interface. Unfortunately, this strategy would preclude the possibility of breakup, as the interface could elongate endlessly. In the way PFEM defines interfaces, it is possible to have fluid regions spanned by just one element layer. The breakup criterium we have implemented in PFEM is to permit connectivity changes in elements where all nodes lie at the interface. In this way, a thin fluid thread can stop elongating and fragment. Breakup is then dependent on the mesh resolution, that is, it happens when the thickness of the film is similar to the mesh resolution of the interface. This is not a drawback specific of PFEM, breakup is mesh dependent in frontcapturing methods as well. For example, in the level set method, two interfaces are described as two different zero contours of the same level set function, and these interfaces will automatically merge once they get close enough, relative to the spatial resolution of the mesh where the level set function is defined. The resolution determines the smallest distance between two zero level sets of the level set function for which they can still be distinguished as separate zero contours. Interfaces can in fact merge faster due to the diffusivity of the schemes used for advection and reinitialization of the level set function [27].
(a)  (b) 
Figure 21: Connectivity change that produces breakup at fluid films spanned by just one mesh element. 
The pressure field at and after breakup is shown in Figures 22 and 23. The different pressure values inside and outside the bubble equilibrate after breakup, what occurs at s.
(a) s  (b) s 
(c) s  (d) s 
Figure 22: Pressure field at breakup (variable scale ranges in legend). 
(a) s  (b) s 
(c) s  (d) s 
Figure 23: Pressure field after breakup (variable scale ranges in legend). 
For the simulation of bubble coalescence, we consider the same rectangular domain as before, with two circular bubbles inside. The center of the first bubble is and its radius is equal to 0.25, the center of the second bubble is and the radius 0.2. Since the small bubble is located close to the large one, this lower bubble turns out to be in the wake of the upper bubble and rises faster than that. Figure 24 shows the coalescence process. The mechanism is again the rupture of the thin film between the bubbles. This happens not during the impact of the bubbles (around s) but during the separation after impact, as corresponds to the physical reality [64].
 
Figure 24: Bubble coalescence. 
We have developed a numerical scheme for the simulation of multifluid flows with the Particle Finite Element Method able to deal with large jumps in the physical properties (included surface tension), and able to accurately represent the and discontinuities in the flow variables. Interfaces are tracked by the moving mesh, pressure degrees of freedom have been duplicated at the interface nodes to represent the discontinuity of this variable due to surface tension and variable viscosity (Eq. 9), velocity and pressure variables have been decoupled through a pressure segregation method, and the mesh has been refined in the vicinity of the interface to improve the accuracy and efficiency of the computations.
We have first tested the scheme in a simple static bubble problem and compared the results for continuous and discontinuous pressure approximations. We have then applied the method to the more complicated rising bubble problem presented in Hysing et al. [1]. We can conclude that PFEM solutions for the single rising bubble are in good agreement with those reported in [1]. For test 1, our bubble is slightly oscillating in contrast to the reference solution. A reason for this may be that PFEM does not introduce diffusion at the interface. In any case, more comparisons with other methods are needed. For test 2, although PFEM can handle interface breakup without problems (as shown in Section 7.2), the skirt filaments remain intact. Breakup happens only when the fluid region is spanned by just one element layer. This allows to model thin films of thickness , being the mesh size at the interface. In both tests, we have achieved an excellent mass conservation without any correction.
Finally, we propose two bubble breakup and coalescence problems as benchmarks for testing the capabilities of multifluid flow codes to handle topology changes of the interface.
[1] Hysing, S. and Turek, S. and D. Kuzmin and N. Parolini and E. Burman and S. Ganesan and L. Tobiska. (2009) "Quantitative benchmark computations of twodimensional bubble dynamics", Volume 60. International Journal for Numerical Methods in Fluids 12591288
[2] Idelsohn, S.R. and MierTorrecilla, M. and Oñate, E. (2009) "Multifluid flows with the Particle Finite Element Method", Volume 198. Computer Methods in Applied Mechanics and Engineering 27502767
[3] G.K. Batchelor. (1967) "An introduction to fluid dynamics". Cambridge University Press
[4] Idelsohn, S.R. and MierTorrecilla, M. and Nigro, N. and Oñate, E. (2009) "On the analysis of heterogeneous fluids with jumps in the viscosity using a discontinuous pressure field", Volume In press. Computational Mechanics
[5] Unverdi, S.O. and Tryggvason, G. (1992) "Computations of multifluid flows", Volume 60. Physica D: Nonlinear Phenomena 7083
[6] W. Shyy. (1996) "Computational Fluid Dynamics with moving boundaries". Taylor&Francis
[7] Scardovelli, R. and Zaleski, S. (1999) "Direct Numerical Simulation of freesurface and interfacial flow", Volume 31. Annual Reviews of Fluid Mechanics 567603
[8] Caboussat, A. (2005) "Numerical simulation of twophase free surface flows", Volume 12. Archives of Computational Methods in Engineering 165224
[9] Hughes, T.J.R. and Liu, W.K. and Zimmermann, T.K. (1981) "LagrangianEulerian finite element element formulation for incompressible viscous flows", Volume 29. Computer Methods in Applied Mechanics and Engineering 239349
[10] B. Ramaswamy and M. Kawahara. (1986) "Arbitrary LagrangianEulerian finite element method for the analysis of free surface fluid flows", Volume 1. Computational Mechanics 103108
[11] T.E. Tezduyar and M. Behr and J. Liou. (1992) "A new strategy for finite element computations involving moving boundaries and interfaces. The deformingspatialdomain/spacetime procedure: I. The concept and preliminary numerical tests", Volume 94. Computer Methods in Applied Mechanics and Engineering 339351
[12] T.E. Tezduyar and M. Behr and S. Mittal and J. Liou. (1992) "A new strategy for finite element computations involving moving boundaries and interfaces. The deformingspatialdomain/spacetime procedure: II. Computation of freesurface flows, twoliquid flows and flows with drifting cylinders", Volume 94. Computer Methods in Applied Mechanics and Engineering 353371
[13] Hirt, C.W. and Cook, J.L. and Butler, T.D. (1970) "A Lagrangian method for calculating the dynamics of an incompressible fluid with free surface", Volume 5. Journal of Computational Physics 103124
[14] B. Ramaswamy and M. Kawahara. (1987) "Lagrangian finite element analysis applied to viscous free surface fluid flow", Volume 7. International Journal for Numerical Methods in Fluids 953984
[15] Idelsohn, S.R. and Oñate, E. and Del Pin, F. (2003) "A Lagrangian meshless finite element method applied to fluidstructure interaction problems", Volume 81. Computers and Structures 8–11 655–671
[16] Idelsohn, S.R. and Oñate, E. and Del Pin, F. (2004) "The Particle Finite Element Method: A powerful tool to solve incompressible flows with freesurfaces and breaking waves", Volume 61. International Journal for Numerical Methods in Engineering 7 964–989
[17] Oñate, E. and Idelsohn, S.R. and Del Pin, F. and Aubry, R. (2004) "The Particle Finite Element Method: An Overview", Volume 1. International Journal of Computational Methods 2 267–307
[18] Del Pin, F. and Idelsohn, S.R. and Oñate, E. and Aubry, R. (2007) "The ALE/Lagrangian Particle Finite Element Method: A new approach to computation of freesurfaces flows and fluidobject interactions", Volume 36. Computers and Fluids 1 27–38
[19] Harlow, F.H. (1964) "The ParticleinCell computing method for fluid dynamics", Volume 3. Methods in Computational Physics 313343
[20] Unverdi, S.O. and Tryggvason, G. (1992) "A fronttracking method for viscous, incompressible, multifluid flows", Volume 100. Journal of Computational Physics 2537
[21] Hirt, C. and Nichols, B. (1981) "Volume of Fluid (VOF) method for the dynamics of free boundaries", Volume 39. Journal of Computational Physics 201225
[22] Osher, S. and Sethian, J. (1988) "Fronts propagating with curvature dependant speed: algorithms based on HamiltonJacobi formulations", Volume 79. Journal of Computational Physics 1249
[23] Idelsohn, S.R. and Calvo, N. and Oñate, E. (2003) "Polyhedrization of an arbitrary 3D point set", Volume 192. Computer Methods in Applied Mechanics and Engineering 26492667
[24] Oñate, E. and Idelsohn, S.R. and Celigueta, M.A. and Rossi, R. (2008) "Advances in the Particle Finite Element Method for the analysis of fluidmultibody interaction and bed erosion in free surface flows", Volume 197. Computer Methods in Applied Mechanics and Engineering 17771800
[25] van Kan, J. (1986) "A secondorder accurate pressure correction scheme for viscous incompressible flow", Volume 7. SIAM Journal on Scientific and Statistical Computing 870891
[26] A. Smolianski. (2001) "Numerical Modeling of Two Fluid Interfacial Flows". University of Jyväskylä
[27] A.K. Tornberg. (2000) "Interface Tracking Methods with Application to Multiphase Flows". Royal Institute of Technology, Stockholm
[28] Minev, P.D. and Chen, T. and Nandakumar, K. (2003) "A finite element technique for multifluid incompressible flow using Eulerian grids", Volume 187. Journal of Computational Physics 255273
[29] CoppolaOwen, A.H. and Codina, R. (2005) "Improving Eulerian twophase flow finite element approximation with discontinuous gradient pressure shape functions", Volume 49. International Journal for Numerical Methods in Fluids 12871304
[30] J. Chessa and T. Belytschko. (2003) "An extended finite element method for twophase fluids", Volume 70. ASME Journal of Applied Mechanics 1017
[31] S. Gross and A. Reusken. (2007) "An extended pressure finite element space for twophase incompressible flows with surface tension", Volume 224. Journal of Computational Physics 4058
[32] Juntunen, M. and Stenberg, R. (2007) "Nitsche's method for general boundary conditions". Research Reports A530, University of Technology, Institute of Mathematics
[33] MierTorrecilla, M. (2010) "Numerical simulation of multifluid flows with the Particle Finite Element Method". Technical University of Catalonia
[34] J.U. Brackbill and D.B. Kothe and C. Zemach. (1992) "A continuum method for modeling surface tension", Volume 100. Journal of Computational Physics 335354
[35] Bänsch, E. (2001) "Finite Element discretization of the NavierStokes equations with a free capillary surface", Volume 88. Numerische Mathematik 203235
[36] Hysing, S. (2006) "A new implicit surface tension implementation for interfacial flows", Volume 51. International Journal for Numerical Methods in Fluids 659672
[37] Popinet, S. and Zaleski, S. (1999) "A front tracking algorithm for accurate representation of surface tension", Volume 30. International Journal for Numerical Methods in Fluids 775793
[38] Sussman, M. and Smereka, P. and Osher, S. (1994) "A level set approach for computing solutions to incompressible twophase flows", Volume 114. Journal of Computational Physics 146159
[39] Grace, J. R. (1973) "Shapes and Velocities of Bubbles Rising in Infinite Liquids", Volume 51. Transactions of the Institution of Chemical Engineers 116120
[40] R. Clift and J.R. Grace and M.E. Weber. (1978) "Bubbles, drops and particles". Academic Press
[41] Bhaga, D. and Weber, M.E. (1981) "Bubbles in viscous liquids: shapes, wakes and velocities", Volume 105. Journal of Fluid Mechanics 6185
[42] Haberman, W. L. and Morton, R. K. (1954) "An experimental study of bubbles moving in liquids", Volume 387. Proceedings of the American Society of Civil Engineers 125
[43] Hnat, J. G. and Buckmaster, J. D. (1976) "Spherical cap bubbles and skirt formation", Volume 19. Physics of Fluids 182194
[44] Maxworthy, T. and Gnann, C. and Kuerten, M. and Durst, F. (1996) "Experiments on the rise of air bubbles in clean viscous liquids", Volume 321. Journal of Fluid Mechanics 421441
[45] F. Raymond and J.M. Rosant. (2000) "A numerical and experimental study of the terminal velocity and shape of bubbles in viscous liquids", Volume 55. Chemical Engineering Science 943955
[46] M. Wu and M. Gharib. (2002) "Experimental Studies on the Shape and Path of Small Air Bubbles Rising in Clean Water", Volume 14. Physics of Fluids 4952
[47] Esmaeeli, A. and Tryggvason, G. (1998) "Direct numerical simulations of bubbly flows. Part 1. Low Reynolds number arrays", Volume 377. Journal of Fluid Mechanics 313345
[48] Esmaeeli, A. and Tryggvason, G. (1999) "Direct numerical simulations of bubbly flows. Part 2. Moderate Reynolds number arrays", Volume 385. Journal of Fluid Mechanics 325358
[49] Bunner, B. and Tryggvason, G. (2002) "Dynamics of homogeneous bubbly flows. Part 1. Rise velocity and microstructure of the bubbles", Volume 466. Journal of Fluid Mechanics 1752
[50] F.S. de Sousa and N. Mangiavacchi and L.G. Nonato and A. Castelo and M.F. Tomé and V.G. Ferreira and J.A. Cuminato and S. McKee. (2004) "A fronttracking/frontcapturing method for the simulation of 3D multifluid flows with free surfaces", Volume 198. Journal of Computational Physics 469499
[51] Hua, J. and Lou, J. (2007) "Numerical simulation of bubble rising in viscous liquid", Volume 222. Journal of Computational Physics 769795
[52] Z. Yu and L.S. Fan. (2008) "Direct Simulation of the Buoyant Rise of Bubbles in Infinite Liquid Using Level Set Method", Volume 86. Canadian Journal of Chemical Engineering 267275
[53] L. Chen and S.V. Garimella and J.A. Reizes and E. Leonardi. (1999) "The development of a bubble rising in a viscous liquid", Volume 387. Journal of Fluid Mechanics 6196
[54] Van Sint Annaland, M. and N. G. Deen and J. A. M. Kuipers. (2005) "Numerical Simulation of Gas Bubbles Behavior Using a ThreeDimensional Volume of Fluid Method", Volume 60. Chemical Engineering Science 29993011
[55] Bonometti, T. and Magnaudet, J. (2007) "An interfacecapturing method for incompressible twophase flows. Validation and application to bubble dynamics", Volume 33. International Journal of Multiphase Flow 109133
[56] Ryskin, G. and Leal, L. G. (1984) "Numerical solution of freeboundary problems in fluid mechanics. Part 2. Buoyancydriven motion of a gas bubble through a quiescent liquid", Volume 148. Journal of Fluid Mechanics 1935
[57] X. Frank and D. Funfschilling and N. Midoux and H. Z. Li. (2006) "Bubbles in a viscous liquid: Lattice Boltzmann simulation and experimental validation", Volume 546. Journal of Fluid Mechanics 113122
[58] I. O. Kurtoglu and C. L. Lin. (2006) "Lattice Boltzmann Study of Bubble Dynamics", Volume 50. Numerical Heat Transfer B 333351
[59] S. Turek. (1998) "Efficient Solvers for Incompressible Flow Problems". Springer
[60] Parolini, N. and Burman, E. (2005) "A finite element level set method for viscous freesurface flows". 7th Conference on Applied and Industrial Mathematics in Italy 416427
[61] Ganesan, S. and Matthies, G. and Tobiska, L. (2007) "On spurious velocities in incompressible flow problem with interfaces", Volume 196. Computer Methods in Applied Mechanics and Engineering 11931202
[62] Stone, H. (1994) "Dynamics of drop deformation and breakup in viscous fluids", Volume 26. Annual Reviews of Fluid Mechanics 65102
[63] Tryggvason, G. and Bunner, B. and Esmaeeli, A. and Juric, D. and AlRawahi, N. and Tauber, W. and Han, J. and Nas, S. and Jan, Y.J. (2001) "A fronttracking method for the computations of multiphase flow", Volume 169. Journal of Computational Physics 708759
[64] N. Bremond and A. Thiam and J. Bibette. (2008) "Decompressing Emulsion Droplets Favors Coalescence", Volume 100. Physical Review Letters
Published on 01/01/2010
Licence: CC BYNCSA license
Are you one of the authors of this document?