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Computational Modelling

Smoothed Particle Hydrodynamics - Application

Validation study of HPDC in a plate die

Contact personnel:  J. Ha, P.W. Cleary

High pressure die casting (HPDC) is an important industrial process by which very complex shaped castings with excellent surface finishes can be produced in high volumes and at low cost. Smoothed particle hydrodynamics (SPH), being a Lagrangrian method, is well suited to modelling momentum-dominated flows involving droplet formation, splashing and free surfaces, such as occur in HPDC. A preliminary validation of the application of SPH to HPDC has been undertaken by comparing SPH predictions with those obtained both from an independent numerical simulation and from a water-analogue experiment for a relatively simple plate die.

The geometry considered is a thin flat plate, 150 mm high, 100 mm wide and 2 mm thick. Water flows through a gate of width 45 mm at the bottom of the plate. The Reynolds number for the flow is Re = 1.29x106, based on the gate velocity of 8.6 m/s and the height of the plate.

The SPH predictions are compared with the corresponding numerical and experimental results of Schmid & Klein [1]. The numerical simulations of Schmid & Klein were performed using RIPPLE, a computer program developed by Kothe and co-workers at Los Alamos National Laboratory. RIPPLE uses the volume of fluid (VOF) method. It is capable of simulating transient, two-dimensional flows of incompressible fluid involving free surfaces with or without surface tension. Surface tension is modelled as a volume force derived from the continuum-surface-force model so that surface tension effects at the free surface as well as wall-adhesion effects are modelled. RIPPLE uses finite difference discretization on an Eulerian, rectilinear mesh in Cartesian or cylindrical geometry. A two-step projection method is used to solve for the incompressible flow. The Poisson pressure equation is solved via an incomplete Cholesky conjugate gradient technique. The method of partial-cell treatment is used to handle obstacles and curved interior boundaries interior to the mesh.

As seen in the plots below, the SPH simulations and the VOF simulations of Schmid and Klein generally compare well with the experimental results. Both capture the essential nature of the flow. However, there are several smaller scale flow features that our SPH simulations are better able to capture than could be done with the VOF technique employed by Schmid and Klein.

VOF Experiment SPH
plate_vof_1.gif (2504 bytes) plate_exp_1.gif (26282 bytes) plate_sph_1.gif (3738 bytes)
t = 12.43 ms

 

plate_vof_2.gif (3072 bytes) plate_exp_2.gif (33863 bytes) plate_sph_2.gif (5334 bytes)
t = 23.08 ms

 

plate_vof_3.gif (3293 bytes) plate_exp_3.gif (38974 bytes) plate_sph_3.gif (6299 bytes)
t = 26.63 ms

 

plate_vof_4.gif (3697 bytes) plate_exp_4.gif (38056 bytes) plate_sph_4.gif (5494 bytes)
t = 33.73 ms

At the first time shown above, the shape of the SPH jet is much closer to the experiment. The front of the jet is curved in a similar way and is broader than the jet behind. The sides of the jet are also not straight. These differences do not result from the choice of method but rather from the choice of initial conditions. In our SPH solution, we include a reasonable length of tube to the mould and we start the simulation with the fluid several jet diameters from the entrance to the mould. Viscous interaction with the walls produces a velocity distribution within the jet that is neither constant (as used by Schmid and Klein) nor parabolic, but rather somewhere in between. This is particularly important for predicting the shape of the initial material in the jet. The interaction of the jet front with the walls creates a pair of oppositely rotating eddies at the front. Once the jet has entered the cavity, recirculating fluid in these eddies distorts the front of the jet giving it a rounded shape that increases as the jet moves further into the cavity. This demonstrates how critical it is to use correct initial conditions for the fluid velocity. In die casting simulations this essentially means that a reasonable amount of the die casting machine before the entry to the die cavity must be simulated in order to correctly prescribe the initial velocity distribution. Some small differences still remain in the shape of the early jet, but to obtain a closer result requires more knowledge about the inlet geometry and the way in which the fluid was accelerated.

The experimental results at 26.63 ms show that the fluid travelling down along the left side walls of the cavity is of fairly uniform thickness, except near the tip where there appears to be a reasonable amount of fragmented fluid. The jet on the right is more fragmented. The SPH results demonstrate both these features (constant thickness of the jet and fragmentation) while the simulations of Schmid and Klein show tapered side jets that narrow towards there tip. In both the SPH case and the experiment there are hints of the main jet narrowing marginally half way up the die cavity. The curvature of the U-shaped free surface is closer to the experiment in the SPH solution than for the VOF. In particular there should be more curvature as the fluid turns and enters the downward side jet and less curvature where the fluid in the main jet starts to broaden out. The VOF solutions have the curvatures the opposite way around. Both numerical schemes underpredict the distance that the U-shaped free surfaces have moved from the top wall of the cavity. Similarly, the SPH solution does not capture the structure of the side jets as they start at around 23 ms. We suspect that this is due to some three dimensionality of the flow, where the fluid flows preferentially along the upper and lower horizontal surfaces of the die.

The largest differences between the SPH and VOF solutions occurs late in the filling process. At 33.73 ms, the upward jet in the experiment has become pinched and is narrower than the gate width. The VOF simulations predict very long narrow voids on either side of the upward jet with little sign of this pinching. The SPH solution does predict the narrowing of the jet by about the correct amount and better captures the rounded shape of the voids.

Overall, both numerical solutions are very good, but the SPH solution captures a range of the fine detail better than does the VOF, particularly at later times in the filling process.

More details concerning this validation study can be found in [2].

Download QuickTime animation (0.76 MB)

References

[1] M. Schmid and F. Klein, Fluid flow in die cavities - experimental and numerical simulation, NADCA 18. International Die Casting Congress and Exposition (Indianapolis, 1995) pp. 93-99. (See also Markus Schmid's Homepage.)

[2] J. Ha and P.W. Cleary, Comparison of SPH simulations of high pressure die casting with the experiments and VOF simulations of Schmid and Klein, submitted to International Journal of Cast Metals Research (1999).

 

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last updated July 18, 2007 05:20 PM

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