Modelling of Levitation Melting using a Fixed Mesh Method

Similar documents
The Level Set Method THE LEVEL SET METHOD THE LEVEL SET METHOD 203

EOF Library: Open-Source Elmer and OpenFOAM Coupler for Simulation of MHD With Free Surface

Induction furnaces that ensure contact less control of electromagnetic

This tutorial illustrates how to set up and solve a problem involving solidification. This tutorial will demonstrate how to do the following:

Using of open source code library OpenFOAM for 3D magnetohydrodynamic calculations in semiconductor crystal growth technologies

Navier-Stokes & Flow Simulation

MATHEMATICAL MODELING OF SILICON SINGLE CRYSTAL INDUSTRIAL GROWTH

Simulation of Droplet Impingement on a Solid Surface by the Level Set Method

Solved with COMSOL Multiphysics 4.2

Modeling and Simulation of Single Phase Fluid Flow and Heat Transfer in Packed Beds

Possibility of Implicit LES for Two-Dimensional Incompressible Lid-Driven Cavity Flow Based on COMSOL Multiphysics

Arbitrary Lagrangian-Eulerian method for coupled Navier-Stokes and convection-diffusion equations with moving boundaries

Turbulent Premixed Combustion with Flamelet Generated Manifolds in COMSOL Multiphysics

Numerical Investigation of Non-Newtonian Laminar Flow in Curved Tube with Insert

Free Convection in a Water Glass

LS-DYNA 980 : Recent Developments, Application Areas and Validation Process of the Incompressible fluid solver (ICFD) in LS-DYNA.

Strömningslära Fluid Dynamics. Computer laboratories using COMSOL v4.4

Comparison Between 2D and 3D Modelling of HF Electromagnetic Field in FZ Silicon Crystal Growth Process

Smoothing the Path to Simulation-Led Device Design

Phase-field simulation of two-phase micro-flows in a Hele-Shaw cell

Microwell Mixing with Surface Tension

Simulating Sinkage & Trim for Planing Boat Hulls. A Fluent Dynamic Mesh 6DOF Tutorial

CS 231. Fluid simulation

Navier-Stokes & Flow Simulation

Investigation of cross flow over a circular cylinder at low Re using the Immersed Boundary Method (IBM)

CFD in COMSOL Multiphysics

Design Modification and Analysis of Two Wheeler Engine Cooling Fins by CFD

Outline. COMSOL Multyphysics: Overview of software package and capabilities

Lab 9: FLUENT: Transient Natural Convection Between Concentric Cylinders

Terminal Falling Velocity of a Sand Grain

A 3D VOF model in cylindrical coordinates

A Coupled 3D/2D Axisymmetric Method for Simulating Magnetic Metal Forming Processes in LS-DYNA

Estimation of Flow Field & Drag for Aerofoil Wing

QUASI-3D SOLVER OF MEANDERING RIVER FLOWS BY CIP-SOROBAN SCHEME IN CYLINDRICAL COORDINATES WITH SUPPORT OF BOUNDARY FITTED COORDINATE METHOD

Recent applications of overset mesh technology in SC/Tetra

Modeling Void Drainage with Thin Film Dynamics

Optimisation of liquid flow in cavitation tunnel using CFD method

Steady Flow: Lid-Driven Cavity Flow

An Overview of Computational Fluid Dynamics

Axial Channel Water Jacket Cooling

Direct numerical simulations of flow and heat transfer over a circular cylinder at Re = 2000

Ashwin Shridhar et al. Int. Journal of Engineering Research and Applications ISSN : , Vol. 5, Issue 6, ( Part - 5) June 2015, pp.

midas NFX 2017R1 Release Note

FEMLAB Exercise 1 for ChE366

Coupled Analysis of FSI

Keywords: flows past a cylinder; detached-eddy-simulations; Spalart-Allmaras model; flow visualizations

Particle-based Magnetohydrodynamics Modeling and Visualization: Part II - Numerical Simulation

COMPUTER MODELING METHODOLOGY FOR LASER CUTTING PROCESS SUPPORTED WITH EXPERIMENT ON STAINLESS STEEL PLATE

Convection Cooling of Circuit Boards 3D Natural Convection

Rotating Moving Boundary Analysis Using ANSYS 5.7

Homogenization and numerical Upscaling. Unsaturated flow and two-phase flow

CGT 581 G Fluids. Overview. Some terms. Some terms

Overview of Traditional Surface Tracking Methods

Auto Injector Syringe. A Fluent Dynamic Mesh 1DOF Tutorial

Using ANSYS and CFX to Model Aluminum Reduction Cell since1984 and Beyond. Dr. Marc Dupuis

FLOWVISION CFD FREQUENTLY ASKED QUESTIONS

CFD Analysis of 2-D Unsteady Flow Past a Square Cylinder at an Angle of Incidence

The viscous forces on the cylinder are proportional to the gradient of the velocity field at the

A STUDY ON THE UNSTEADY AERODYNAMICS OF PROJECTILES IN OVERTAKING BLAST FLOWFIELDS

Middle East Technical University Mechanical Engineering Department ME 413 Introduction to Finite Element Analysis Spring 2015 (Dr.

Modeling a Nozzle in a Borehole

STUDY OF FLOW PERFORMANCE OF A GLOBE VALVE AND DESIGN OPTIMISATION

Shape optimisation using breakthrough technologies

Connecting through the Cloud

NUMERICAL VISCOSITY. Convergent Science White Paper. COPYRIGHT 2017 CONVERGENT SCIENCE. All rights reserved.

Animation of Fluids. Animating Fluid is Hard

MESHLESS SOLUTION OF INCOMPRESSIBLE FLOW OVER BACKWARD-FACING STEP

Final drive lubrication modeling

The Transient Modeling of Bubble Pinch-Off Using an ALE Moving Mesh

The Level Set Method. Lecture Notes, MIT J / 2.097J / 6.339J Numerical Methods for Partial Differential Equations

Navier-Stokes & Flow Simulation

Computational Fluid Dynamics using OpenCL a Practical Introduction

Computational Fluid Dynamics (CFD) Simulation in Air Duct Channels Using STAR CCM+

Computation of Velocity, Pressure and Temperature Distributions near a Stagnation Point in Planar Laminar Viscous Incompressible Flow

Optimization of under-relaxation factors. and Courant numbers for the simulation of. sloshing in the oil pan of an automobile

Coupling of STAR-CCM+ to Other Theoretical or Numerical Solutions. Milovan Perić

Numerical Simulation of Multi-Phase Core-Shell Molten Metal Drop Oscillations

Recent Approaches of CAD / CAE Product Development. Tools, Innovations, Collaborative Engineering.

CIBSE Application Manual AM11 Building Performance Modelling Chapter 6: Ventilation Modelling

Flow Structures Extracted from Visualization Images: Vector Fields and Topology

Speed and Accuracy of CFD: Achieving Both Successfully ANSYS UK S.A.Silvester

Topology optimization of heat conduction problems

Best Practices: Electronics Cooling. Ruben Bons - CD-adapco

Introduction To FLUENT. David H. Porter Minnesota Supercomputer Institute University of Minnesota

Design, Modification and Analysis of Two Wheeler Cooling Sinusoidal Wavy Fins

Coupled Simulation of the Fluid Flow and Conjugate Heat Transfer in Press Hardening Processes

Continued Investigation of Small-Scale Air-Sea Coupled Dynamics Using CBLAST Data

Solving Partial Differential Equations on Overlapping Grids

An Example Eddy Currents

IMAGE ANALYSIS DEDICATED TO POLYMER INJECTION MOLDING

Numerical Study of Turbulent Flow over Backward-Facing Step with Different Turbulence Models

Flow and Heat Transfer in a Mixing Elbow

real world design & problems fluid flow engineering solving Computational Fluid Dynamics System

Preliminary Spray Cooling Simulations Using a Full-Cone Water Spray

Preliminary investigation into two-way fluid structure interaction of heliostat wind loads Josh Wolmarans

An Introduction to SolidWorks Flow Simulation 2010

Temperature Analysis of Intel Server by using CFD and Experimentation

FIDAP Fidap 8.5 Page 1 of 6

Ab initio NMR Chemical Shift Calculations for Biomolecular Systems Using Fragment Molecular Orbital Method

Figure 2: Water Into Kerosene, Volume Fraction (Left) And Total Density Of Mixture (Right)

Transcription:

International Scientific Colloquium Modelling for Electromagnetic Processing Hannover, October 27-29, 2008 Modelling of Levitation Melting using a Fixed Mesh Method D. Hectors, E. Toorman, K. Van Reusel Abstract Numerical modelling is indispensable in the design of levitation melting equipment. The shape and the position of the levitated molten metal are very important for the power transfer from the coil towards the molten metal. This paper verifies whether the shape and position of this molten metal can be determined using the level set method. Introduction Levitation melting is a technique based on the induction of eddy currents in a metallic sample by an alternating electromagnetic flux. These eddy currents heat the sample by Joule effect. The induced currents give cause to Lorentz forces at the same time. When the magnetic field is generated by a suitably shaped coil, the forces may attain a sufficient magnitude to levitate the specimen. Simultaneously, the molten metal droplet deforms, due to the magnetic pressure. The shape and the position of the liquid metal-air interface are very important for the coupling between the inductor and the levitated load. The rotational component of the levitation force, together with the thermal gradients in the liquid metal (causing convection flows), produce a stirring effect in the droplet. The main advantage of levitation melting is that the metal is molten without contact. The applications of this technique are based on this main advantage: measurement of thermophysical properties of liquid metals [1,2], elaboration of materials that require a high degree of purity [3], processing of strongly reactive metals or alloys, and investigation of solidification of undercooled melts [4]. Numerical modelling is indispensable in the design of levitation melting equipment. The shape and the position of the molten metal is very important for the power transfer from a coil or inductor towards the molten metal. Results from numerical models tracking the position and the shape of the interface have recently been published [5]. In this publication [5] the tracking of the interface is based on a moving mesh method (ALE). This paper describes another technique for tracking the interface, using a fixed mesh method (level set). The first section explains the level set method generally. Section two shows some results obtained by using this method for levitation melting and compares it with the ALE method. Finally, some conclusions are given. 1. General description of the level set method The level set method is a technique to represent moving interfaces or boundaries using a fixed mesh. The level set method is very similar to the volume of fluid (VOF) technique [6]. The level set method however has a higher order of accuracy in comparison to VOF [7]. The major drawback of the level set method used to be that it was not conservative, but this problem has been solved [7]. 157

Fig.1. Surface plot of a level set function [8] The level set method is useful for problems where the computational domain can be divided into two domains separated by an interface [8] (Fig.1). The interface is represented by a certain level set or isocontour of a globally defined function, the level set function ( ). This function is a smooth step function equal to zero in one domain and equal to one in the other domain. Across the interface, there is a smooth transition from zero to one. The interface is defined by the 0.5 isocontour, or the level set, of. By using the level set method, the following equation is solved in combination with the incompressible Navier-Stokes equations: d u (1 ) dt (1) The terms on the left hand side gives the correct motion of the interface, while the right hand side terms are necessary for numerical stability. Stabilization is necessary because (1) is a hyperbolic equation [6]. In (1), u is the velocity field, is a parameter that determines the thickness of the region where goes smoothly from zero to one. The parameter determines the amount of reinitialization or stabilization of the level set function. A more general description of the level set method can be found in [9] and [10]. 2. Application of level set in levitation melting The level set method is available in the commercial finite element software Comsol [11]. This software has been used for modelling levitation melting, tracking the liquid metalair interface of a molten droplet at constant temperature, levitated by a current conducting coil. In our situation, we are interested in the deformation and movement of a liquid metal droplet, levitated by a conical coil with one winding. The 2D axisymmetric geometrical set-up of the model can be seen on Fig.2. The initial shape of the metal is a sphere. The surrounding airbox is defined bigger than shown on the figure, which is a zoom. The electromagnetic model uses the time-harmonic axisymmetric electromagnetic diffusion equation of the scalar variable Az. This equation is solved for the whole geometry of the model. The impedance boundary condition is used on the coil, since we are not interested in the internal magnetic fields within the coil, and this way is much easier to mesh at the high frequency of 550 khz. The impedance boundary condition is not used on the metal though. Otherwise, we would not be able to simulate the stirring of the liquid metal. 158

surrounding airbox small airbox metal conical coil Fig.2. Geometrical set-up The electromagnetic module is coupled with the level set module, in which there are 4 unknowns: velocity components u and v, pressure p, and level set function. The level set module is solved for the metal domain, and a small part of the airbox (small airbox on Fig.2). Last part is kept as small as possible, to avoid to solve the Navier-Stokes equations for too much nodes, but is made sufficiently large to surely contain the liquid deformation. The metal and the small airbox need to be meshed finely, in order to track the interface well. This fine mesh (Fig.3) allows the level set interface to be small. Fig.3. Mesh The Lorentz force and gravity are entered as volume forces. The surface tension force is entered as a force on the metal-air boundary. The turbulent viscosity is taken a factor 500 larger than the laminar viscosity, like it is standard practice in laminar flow modelling. The level set equation (1) is solved transiently together with the Navier-Stokes equations. At every time step, the electromagnetic diffusion equation is solved time-harmonically. 159

The result of the steady-state liquid metal-air interface shape obtained by the level set method is given in Fig.4. The shape looks very realistic. initial droplet shape deformed droplet shape Fig.4. Regime deformed droplet shape initial droplet shape deformed droplet shape Fig.5. Regime deformed droplet shape with other surface tension The model allows to investigate the variation of different parameters (inductor geometry, metal characteristics ). On Fig.5, the surface tension coefficient is reduced with a factor of 4, which can clearly be seen on the steady state shape. 160

The regime droplet shape is obtained after a transient solve. Fig.6 shows the average movement of the lower part of the droplet. It can clearly be seen that the droplet has a damped oscillation movement towards a steady-state position, which is described in literature [1]. After about 1 s, the steady-state is reached. Fig.6. Transient behaviour of droplet The stirring in the liquid metal due to Lorentz forces can be seen on Fig.7. The twophase flow can be seen on the figure. Fig.7. Streamlines of the velocity field of the two phase flow Compared to the ALE-method, the level set method has several advantages and disadvantages: Advantages: It is much easier to implement the surface tension force, and thus easier to obtain a result. 161

Fewer unknowns need to be solved for each triangle. Disadvantages: The Navier-Stokes equations also need to be solved for a part of the airbox. The mesh needs to be finer. The viscosity and density vary smoothly from one fluid to the other. This is not the case in reality. Conclusions and future work It is possible to track the liquid metal air interface in levitation melting, using the level set method. The results look very realistic. The models allow to investigate the behaviour of the levitated molten droplet. A next step is to compare the achieved results with position and shape measurements. References [1] Egry, I.: Physical property measurement of liquid metals at high temperatures under microgravity. Materials Transactions, Vol. 45, 2004, pp. 3235-3240. [2] Lohöfer, G.: Electrical resistivity measurement of liquid metals. Measurements Science and Technology, Vol. 16, 2005, pp. 417-425. [3] Gillo, P.: Cold crucible induction melting: theory and applications. Int. Symposium on Heating by Internal Sources, Padua, 2001. [4] Yasuda, H., Ohnaka, I., Fujita, S., Tamura, Y., Mizuguchi, T., Nagira, T.: Dynamics and solidification behavior of the metallic melt levitated by simultaneous imposition of alternating and static magnetic fields. Joint 15 th Riga and 6 th PAMIR Int. Conference on Fundamental and Applied MHD, Riga, 2005. [5] Ernst, R., Garnier, C., Petitpas, P., Trassy, C.: 2D and 3D numerical modelling of a cold crucible for optimising of industrial processes. Int. Symposium on Heating by Electromagnetic Sources, Padua, 2007. [6] Coppola-Owen, A., Codina, R.: A finite element model for free surface flows on fixed meshes. Int. J. Numer. Meth. Fluids, Vol. 54, 2007, pp. 1151-1171. [7] Olsson, E., Kreiss, G.: A conservative level set method for two phase flow. J. Comp. Phys., Vol. 210, 2005, pp. 225-246. [8] Chemical Engineering user s guide, Comsol Multiphysics. [9] Osher, S., Fedkiw, R.: Level Set Methods and Dynamic Implicit Surfaces. Springer-Verlag, Berlin, 2003. [10] Sussman, M., Almgren, A., Colella, J., Howell, L., Welcome, M.: An adaptive level set approach for incompressible two phase flows. Journal of Computational Physics, Vol. 148, 1999, pp. 81 124. [11] www.comsol.com Authors Ir. Ing. Hectors, Dietrich Prof. Dr. Ir. Toorman, Erik Research group Electrical Energy (ELECTA) Hydraulics Laboratory Department Electrical Engineering (ESAT) Department of Civil Engineering K.U.Leuven K.U.Leuven Kasteelpark Arenberg 10 Kasteelpark Arenberg 40 3001 Heverlee, Belgium 3001 Heverlee, Belgium E-mail: dietrich.hectors@esat.kuleuven.be E-mail: erik.toorman@bwk.kuleuven.be Prof. Ir. Van Reusel, Koen Research group Electrical Energy (ELECTA) Department Electrical Engineering (ESAT) K.U.Leuven Kasteelpark Arenberg 10 3001 Heverlee, Belgium E-mail: koen.vanreusel@esat.kuleuven.be 162