A comparison of solvers and approaches - Montanuniversität Leoben
A comparison of solvers and approaches - Montanuniversität Leoben
A comparison of solvers and approaches - Montanuniversität Leoben
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Introduction<br />
VoF-approach<br />
FAM-approach<br />
Conclusion<br />
References<br />
5th OpenFOAM TM Workshop, Chalmers, Gothenburg<br />
bgschaid,pvita,dprieling,hsteiner<br />
June 21-24,<br />
RoWaFloSim<br />
2010<br />
1/33<br />
Liquid coverage <strong>of</strong> rotating discs<br />
A <strong>comparison</strong> <strong>of</strong> <strong>solvers</strong> <strong>and</strong> <strong>approaches</strong><br />
Bernhard F.W. Gschaider 1 Petr Vita 2 Doris Prieling 3<br />
Helfried Steiner 3<br />
1 ICE Strömungsforschung<br />
<strong>Leoben</strong>, Austria<br />
2 Department Mineral Resources <strong>and</strong> Petroleum Engineering, Montanuniversität<br />
<strong>Leoben</strong>, Austria<br />
3 Institute <strong>of</strong> Fluid Mechanics <strong>and</strong> Heat Transfer, Graz University <strong>of</strong> Technology,<br />
Austria
Outline<br />
Introduction<br />
VoF-approach<br />
FAM-approach<br />
Conclusion<br />
References<br />
1 Introduction<br />
Problem description<br />
Approximate solution<br />
Published benchmark cases<br />
2 VoF-approach<br />
Overview<br />
Exploiting rotational symmetry<br />
Dynamic meshing<br />
Summary VoF<br />
3 FAM-approach<br />
Overview<br />
Implementation<br />
Results<br />
Summary<br />
4 Conclusion<br />
Results summary<br />
Acknowledgements<br />
bgschaid,pvita,dprieling,hsteiner RoWaFloSim 2/33
Wafer cleaning<br />
Introduction<br />
VoF-approach<br />
FAM-approach<br />
Conclusion<br />
References<br />
Problem description<br />
Approximate solution<br />
Published benchmark cases<br />
• Important step during the<br />
production <strong>of</strong> semiconductor<br />
silicon-wafers<br />
• But the same happens<br />
during etching etc<br />
• Two contradicting goals:<br />
• Wafer should be fully wetted<br />
• Minimum amount <strong>of</strong> liquid<br />
• Goal <strong>of</strong> this project is to<br />
develop a simulation tool that<br />
helps with the planing <strong>of</strong> this<br />
process<br />
bgschaid,pvita,dprieling,hsteiner RoWaFloSim 3/33
Simulation features<br />
Introduction<br />
VoF-approach<br />
FAM-approach<br />
Conclusion<br />
References<br />
Problem description<br />
Approximate solution<br />
Published benchmark cases<br />
• Liquid film<br />
• Thin (compared to the size <strong>of</strong> the geometry)<br />
• On a rotating surface<br />
• Liquid jet impinges on the surface<br />
• Not necessarily on the center<br />
• Position <strong>and</strong> strength change during time<br />
• Transport <strong>of</strong> reactants in the liquid<br />
• All this should be achieved in a reasonable time-frame<br />
bgschaid,pvita,dprieling,hsteiner RoWaFloSim 4/33
Asymptotic solutions<br />
Introduction<br />
VoF-approach<br />
FAM-approach<br />
Conclusion<br />
References<br />
Problem description<br />
Approximate solution<br />
Published benchmark cases<br />
Nusselt solution<br />
Ro 2 ≪ 1, Ro 2 = ( ) ū 2<br />
ωr<br />
ν ∂2 v r<br />
∂z 2 = −rω2<br />
Film thickness<br />
( ) 1<br />
3 Qν 3<br />
δ =<br />
2π ω 2 r 2<br />
Asymptotic solution<br />
Rauscher et al. (1973) [RKC73]:<br />
(<br />
δ<br />
62<br />
= r ∗−2/3 +<br />
h 0 315 − 2 )<br />
9 F −1 r ∗−10/3 +O(r −4 )<br />
with F −1 = 2πgν<br />
3ω 2 Q , r ∗ = r/l<br />
characteristic lengths: l =<br />
(<br />
9Q 2<br />
4π 2 νω<br />
) 1<br />
4<br />
<strong>and</strong> h 0 = ( ν<br />
ω<br />
) 1<br />
2<br />
Viscous−<br />
Resistance<br />
Inertial−<br />
Force<br />
Gravitational−<br />
Force<br />
Centrifugal−<br />
Force<br />
Coriolis−<br />
Force<br />
leading order balance<br />
higher order correction<br />
bgschaid,pvita,dprieling,hsteiner RoWaFloSim 5/33
Ozar et el<br />
Introduction<br />
VoF-approach<br />
FAM-approach<br />
Conclusion<br />
References<br />
Problem description<br />
Approximate solution<br />
Published benchmark cases<br />
• Rotating disc<br />
• Inlet at the center<br />
• Not by a jet, but through a<br />
collar<br />
• This allows a good control<br />
over the flow properties<br />
• Lots <strong>of</strong> experimental data<br />
bgschaid,pvita,dprieling,hsteiner RoWaFloSim 6/33
Charwat et al<br />
Introduction<br />
VoF-approach<br />
FAM-approach<br />
Conclusion<br />
References<br />
Problem description<br />
Approximate solution<br />
Published benchmark cases<br />
• Impinging jet on the center <strong>of</strong><br />
the disc<br />
• Closer to the actual<br />
application<br />
• Still axi-symmetric<br />
• Described in [CKG72]<br />
• Analytical solution in [KK09]<br />
bgschaid,pvita,dprieling,hsteiner RoWaFloSim 7/33
Introduction<br />
VoF-approach<br />
FAM-approach<br />
Conclusion<br />
References<br />
The Volume <strong>of</strong> Fluid Method<br />
Overview<br />
Exploiting rotational symmetry<br />
Dynamic meshing<br />
Summary VoF<br />
• Multiphase solver for 2 liquids with a high density difference<br />
• Volume fraction <strong>of</strong> one liquid is solved for<br />
• Implemented in OpenFOAM TM in the interFoam-family <strong>of</strong><br />
<strong>solvers</strong><br />
• For details look elsewhere<br />
bgschaid,pvita,dprieling,hsteiner RoWaFloSim 8/33
Introduction<br />
VoF-approach<br />
FAM-approach<br />
Conclusion<br />
References<br />
Different implementations<br />
Overview<br />
Exploiting rotational symmetry<br />
Dynamic meshing<br />
Summary VoF<br />
• There are 3 schemes to calculate VoF in Fluent:<br />
HRIC High resolution interface capturing<br />
QUICK Quick Upwind Interpolation for Convective<br />
Kinematics<br />
PLIC Geometric reconstruction<br />
• “only” one implementation in OpenFOAM TM<br />
γ-differencing scheme Implementation in interFoam <strong>and</strong><br />
others<br />
• If not otherwise noted the same grid was used in Fluent <strong>and</strong><br />
OpenFOAM TM for all calculations<br />
bgschaid,pvita,dprieling,hsteiner RoWaFloSim 9/33
Motivation<br />
Introduction<br />
VoF-approach<br />
FAM-approach<br />
Conclusion<br />
References<br />
Overview<br />
Exploiting rotational symmetry<br />
Dynamic meshing<br />
Summary VoF<br />
• Both sets <strong>of</strong> experiments were set up in an axially symmetric<br />
fashion<br />
• Minimizes amount <strong>of</strong> computational time<br />
• More calculations possible<br />
• Of course assumes that all the effects are symmetric<br />
• Slightly different implementation:<br />
OpenFOAM Needs a modified mesh <strong>and</strong> special boundary<br />
conditions<br />
Fluent Modifies all the differential operators but uses a<br />
2D-mesh<br />
bgschaid,pvita,dprieling,hsteiner RoWaFloSim 10/33
Introduction<br />
VoF-approach<br />
FAM-approach<br />
Conclusion<br />
References<br />
Overview<br />
Exploiting rotational symmetry<br />
Dynamic meshing<br />
Summary VoF<br />
Comparing a case (200 rpm, 7 l/min)<br />
0.4<br />
Instantaneous film thickness after t=2s<br />
Testcase 1b<br />
ω=200rpm, Q=7lpm, ν L<br />
=1x10 −6 m 2 /s, θ=10deg<br />
0.4<br />
Instantaneous film thickness after t=2s<br />
0.35<br />
0.35<br />
0.3<br />
0.3<br />
δ [mm]<br />
0.25<br />
0.2<br />
0.15<br />
0.1<br />
0.05<br />
FLUENT PLIC, α=0.5<br />
Nusselt solution<br />
Asympt. Rauscher 1973<br />
Exp. Thomas 1991<br />
0<br />
50 100 150 200<br />
r [mm]<br />
δ [mm]<br />
0.25<br />
0.2<br />
0.15<br />
0.1<br />
0.05<br />
FLUENT HRIC, α=0.5<br />
Nusselt solution<br />
Asympt. Rauscher 1973<br />
Exp. Thomas 1991<br />
0<br />
50 100 150 200<br />
r [mm]<br />
δ [mm]<br />
0.4<br />
0.35<br />
0.3<br />
0.25<br />
0.2<br />
0.15<br />
0.1<br />
0.05<br />
FLUENT QUICK, α=0.5<br />
OpenFOAM Inter−γ<br />
Nusselt solution<br />
Asympt. Rauscher 1973<br />
Exp. Thomas 1991<br />
Instantaneous film thickness after t=2s<br />
0<br />
50 100 150 200<br />
r [mm]<br />
δ [mm]<br />
0.4<br />
0.35<br />
0.3<br />
0.25<br />
0.2<br />
0.15<br />
0.1<br />
0.05<br />
Temporal film thickness variation, monitor at r=180mm<br />
FLUENT PLIC<br />
FLUENT HRIC<br />
FLUENT QUICK<br />
OpenFOAM Inter−γ<br />
0<br />
1.85 1.9 1.95 2<br />
t [s]<br />
bgschaid,pvita,dprieling,hsteiner RoWaFloSim 11/33
Introduction<br />
VoF-approach<br />
FAM-approach<br />
Conclusion<br />
References<br />
Overview<br />
Exploiting rotational symmetry<br />
Dynamic meshing<br />
Summary VoF<br />
Comparing a case (200 rpm, 7 l/min) - time average<br />
0.4<br />
0.35<br />
0.3<br />
Test case 1b<br />
ω=200rpm, Q=7lpm, ν L<br />
=1x10 −6 m 2 /s, θ=10deg<br />
FLUENT PLIC<br />
FLUENT HRIC<br />
FLUENT QUICK<br />
OpenFOAM Inter−γ<br />
Nusselt solution<br />
Asympt. Rauscher 1973<br />
Exp. Thomas 1991<br />
0.25<br />
δ [mm]<br />
0.2<br />
0.15<br />
0.1<br />
0.05<br />
Temporal averages<br />
• good agreement with experimental<br />
data<br />
• QUICK ≈ Inter-γ (smooth)<br />
• approach asymptotic solution in outer<br />
region<br />
0<br />
50 60 80 100 120 140 160 180 200<br />
r [mm]<br />
bgschaid,pvita,dprieling,hsteiner RoWaFloSim 12/33
Introduction<br />
VoF-approach<br />
FAM-approach<br />
Conclusion<br />
References<br />
Overview<br />
Exploiting rotational symmetry<br />
Dynamic meshing<br />
Summary VoF<br />
Comparing another case (300 rpm, 3 l/min)<br />
Test case 1f<br />
ω=300rpm, Q=3lpm, ν L<br />
=0.66x10 −6 m 2 /s, θ=10deg<br />
δ [mm]<br />
0.4<br />
0.35<br />
0.3<br />
0.25<br />
0.2<br />
0.15<br />
Instantaneous film thickness after t=2s<br />
FLUENT PLIC, α=0.5<br />
Nusselt solution<br />
Asympt. Rauscher 1973<br />
Exp. Ozar 2003<br />
δ [mm]<br />
0.4<br />
0.35<br />
0.3<br />
0.25<br />
0.2<br />
0.15<br />
Instantaneous film thickness after t=2s<br />
FLUENT HRIC, α=0.5<br />
Nusselt solution<br />
Asympt. Rauscher 1973<br />
Exp. Ozar 2003<br />
0.1<br />
0.1<br />
0.05<br />
0.05<br />
0<br />
50 60 80 100 120 140 160 180 200<br />
r [mm]<br />
0<br />
50 100 150 200<br />
r [mm]<br />
δ [mm]<br />
0.4<br />
0.35<br />
0.3<br />
0.25<br />
0.2<br />
0.15<br />
Instantaneous film thickness after t=2s<br />
FLUENT QUICK, α=0.5<br />
OpenFOAM Inter−γ<br />
Nusselt solution<br />
Asympt. Rauscher 1973<br />
Exp. Ozar 2003<br />
δ [mm]<br />
0.4<br />
0.35<br />
0.3<br />
0.25<br />
0.2<br />
0.15<br />
Temporal film thickness variation, monitor at r=180mm<br />
FLUENT PLIC<br />
FLUENT HRIC<br />
FLUENT QUICK<br />
OpenFOAM Inter−γ<br />
0.1<br />
0.1<br />
0.05<br />
0.05<br />
0<br />
50 100 150 200<br />
r [mm]<br />
0<br />
1.85 1.9 1.95 2<br />
t [s]<br />
bgschaid,pvita,dprieling,hsteiner RoWaFloSim 13/33
Introduction<br />
VoF-approach<br />
FAM-approach<br />
Conclusion<br />
References<br />
Overview<br />
Exploiting rotational symmetry<br />
Dynamic meshing<br />
Summary VoF<br />
Comparing anothert case (300 rpm, 3 l/min) - time<br />
average<br />
0,4<br />
0,35<br />
0,3<br />
0,25<br />
• Exp. data<br />
overpredicted<br />
• HRIC, Inter-γ:<br />
enhanced waviness<br />
• Smaller Ro 2 (ω ↑,<br />
Q ↓)<br />
Test case 1f<br />
ω=300rpm, Q=3lpm, ν L<br />
=0.66x10 −6 m 2 /s, θ=10deg<br />
FLUENT PLIC<br />
FLUENT HRIC<br />
FLUENT QUICK<br />
OpenFOAM Inter−γ<br />
Nusselt solution<br />
Asympt. Rauscher 1973<br />
Exp. Ozar 2003<br />
δ [mm]<br />
0,2<br />
0,15<br />
0,1<br />
0,05<br />
0<br />
50 60 80 100 120 140 160 180 200<br />
r [mm]<br />
bgschaid,pvita,dprieling,hsteiner RoWaFloSim 14/33
Introduction<br />
VoF-approach<br />
FAM-approach<br />
Conclusion<br />
References<br />
Overview<br />
Exploiting rotational symmetry<br />
Dynamic meshing<br />
Summary VoF<br />
Hydraulic jump on stationary disc (7 l/min)<br />
bgschaid,pvita,dprieling,hsteiner RoWaFloSim 15/33
Introduction<br />
VoF-approach<br />
FAM-approach<br />
Conclusion<br />
References<br />
Overview<br />
Exploiting rotational symmetry<br />
Dynamic meshing<br />
Summary VoF<br />
Comparison impinging jet (Charwat 1)<br />
0.6<br />
0.5<br />
0.4<br />
Film thickness − test case C1<br />
Q=0.3lpm, ω=60rpm, Re=1156<br />
FLUENT PLIC, α−mean<br />
FLUENT HRIC, α−mean<br />
FLUENT QUICK, α−mean<br />
OpenFOAM Inter−γ<br />
Kim & Kim 2009<br />
Exp. Charwat (data fit)<br />
δ [mm]<br />
0.3<br />
0.2<br />
0.1<br />
0<br />
mesh: 71160 cells<br />
nozzle inflow included<br />
20 40 60 80 100 120 140 160 180<br />
r [mm]<br />
bgschaid,pvita,dprieling,hsteiner RoWaFloSim 16/33
Introduction<br />
VoF-approach<br />
FAM-approach<br />
Conclusion<br />
References<br />
Overview<br />
Exploiting rotational symmetry<br />
Dynamic meshing<br />
Summary VoF<br />
Comparison impinging jet (Charwat 2)<br />
0.35<br />
0.3<br />
0.25<br />
Film thickness − test case C2<br />
Q=0.18lpm, ω=180rpm, Re=694<br />
FLUENT PLIC<br />
FLUENT HRIC<br />
FLUENT QUICK<br />
OpenFOAM Inter−γ<br />
Kim & Kim 2009<br />
Exp. Charwat (data fit)<br />
δ [mm]<br />
0.2<br />
0.15<br />
0.1<br />
0.05<br />
0<br />
mesh: 71160 cells<br />
nozzle inflow included<br />
20 40 60 80 100 120 140 160 180<br />
r [mm]<br />
bgschaid,pvita,dprieling,hsteiner RoWaFloSim 17/33
Introduction<br />
VoF-approach<br />
FAM-approach<br />
Conclusion<br />
References<br />
MOVIE: Impinging jet<br />
Overview<br />
Exploiting rotational symmetry<br />
Dynamic meshing<br />
Summary VoF<br />
bgschaid,pvita,dprieling,hsteiner RoWaFloSim 18/33
Introduction<br />
VoF-approach<br />
FAM-approach<br />
Conclusion<br />
References<br />
Motivation <strong>and</strong> model setup<br />
Overview<br />
Exploiting rotational symmetry<br />
Dynamic meshing<br />
Summary VoF<br />
• Full 3D was considered<br />
• Large meshes due to different length-scales (wafer diameter vs.<br />
film thickness)<br />
• Grid near the wafer determines the resolution <strong>of</strong> the film<br />
• The solution: interDyMFoam<br />
• Finer grid resolution at the surface <strong>of</strong> the liquid<br />
• The Ozar case was calculated<br />
• Coarse blockMesh<br />
bgschaid,pvita,dprieling,hsteiner RoWaFloSim 19/33
Introduction<br />
VoF-approach<br />
FAM-approach<br />
Conclusion<br />
References<br />
Overview<br />
Exploiting rotational symmetry<br />
Dynamic meshing<br />
Summary VoF<br />
MOVIE: Dynamically meshed case<br />
bgschaid,pvita,dprieling,hsteiner RoWaFloSim 20/33
Introduction<br />
VoF-approach<br />
FAM-approach<br />
Conclusion<br />
References<br />
Overview<br />
Exploiting rotational symmetry<br />
Dynamic meshing<br />
Summary VoF<br />
Comparison <strong>of</strong> the VoF-<strong>approaches</strong><br />
• All <strong>approaches</strong> <strong>and</strong> <strong>solvers</strong> give similar time averaged results<br />
which are consistent with the experimental data<br />
• Results are mesh-independent, except for PLIC<br />
• Instantaneous values differ significantly<br />
• Axial-symmetric solution fast, but limited in physical<br />
phenomena it can tackle<br />
• 3D with mesh refinement takes a long time<br />
• Even then the surface film is only 3–5 computational cells<br />
“thick”<br />
bgschaid,pvita,dprieling,hsteiner RoWaFloSim 21/33
Motivation<br />
Introduction<br />
VoF-approach<br />
FAM-approach<br />
Conclusion<br />
References<br />
Overview<br />
Implementation<br />
Results<br />
• Disadvantages <strong>of</strong> the VoF-approach:<br />
Axial-symmetric Can not simulate a jet that does not<br />
impinge on the center <strong>of</strong> the disc<br />
3D-dynamic Takes too long for reasonable grid resolutions<br />
• The simulation should be able to<br />
• Simulate arbitrary processes<br />
• Computational times <strong>of</strong> months for processes that last in the<br />
order <strong>of</strong> a minute are unacceptable<br />
bgschaid,pvita,dprieling,hsteiner RoWaFloSim 22/33
Introduction<br />
VoF-approach<br />
FAM-approach<br />
Conclusion<br />
References<br />
The FiniteAreaMethod<br />
Overview<br />
Implementation<br />
Results<br />
• Specialisation <strong>of</strong> the FVM to flows on surfaces<br />
• Possible applications: wall-films<br />
• Implementation by H.Jasak <strong>and</strong> Z.Tukovic in OpenFOAM TM<br />
• Not in the “<strong>of</strong>ficial” version. Only in 1.5-dev<br />
• Only a demo-solver that models the transport-equation on a<br />
prescribed velocity field available<br />
• Equations are solved on a boundary-patch <strong>of</strong> the volume mesh<br />
• Solution <strong>of</strong> the volume (impinging jet) can be used as a source<br />
term<br />
bgschaid,pvita,dprieling,hsteiner RoWaFloSim 23/33
Introduction<br />
VoF-approach<br />
FAM-approach<br />
Conclusion<br />
References<br />
The simplified wafer model<br />
Overview<br />
Implementation<br />
Results<br />
• Based on the shallow-water equations<br />
• The height <strong>of</strong> the fluid-film takes a dual role as “Density” <strong>of</strong><br />
the fluid <strong>and</strong> Pressure<br />
• Equations are solved using an adapted PISO-approach<br />
• Implemented using the finiteArea-approach<br />
bgschaid,pvita,dprieling,hsteiner RoWaFloSim 24/33
Introduction<br />
VoF-approach<br />
FAM-approach<br />
Conclusion<br />
References<br />
Overview<br />
Implementation<br />
Results<br />
The modified shallow water equations<br />
• Liquid velocity:<br />
∂⃗u<br />
∂t + ⃗u∇⃗u + g∇h − σ ρ ∇∇2 h = ν∇ 2 ⃗u + ν h 2 (⃗u wafer − ⃗u)<br />
• With added surface tension<br />
• <strong>and</strong> motion <strong>of</strong> the wafer<br />
• Liquid height<br />
∂h<br />
∂t<br />
+ h∇⃗u + ⃗u∇h = 0<br />
bgschaid,pvita,dprieling,hsteiner RoWaFloSim 25/33
Introduction<br />
VoF-approach<br />
FAM-approach<br />
Conclusion<br />
References<br />
Replaying the Ozar case<br />
Overview<br />
Implementation<br />
Results<br />
• Need for validation <strong>of</strong> the solver:<br />
• Significantly differs from the VoF-approach<br />
• Ozar case chosen for validation because:<br />
• It is easy to set up <strong>and</strong> well defined<br />
• Especially the inner boundary condition<br />
• For the Charwat case (<strong>and</strong> application) the impinging jet is<br />
modelled by a source term in the continuity equation<br />
• Experimental <strong>and</strong> computational data exists<br />
bgschaid,pvita,dprieling,hsteiner RoWaFloSim 26/33
Introduction<br />
VoF-approach<br />
FAM-approach<br />
Conclusion<br />
References<br />
Overview<br />
Implementation<br />
Results<br />
Film height <strong>and</strong> liquid velocity with FAM<br />
bgschaid,pvita,dprieling,hsteiner RoWaFloSim 27/33
Introduction<br />
VoF-approach<br />
FAM-approach<br />
Conclusion<br />
References<br />
Overview<br />
Implementation<br />
Results<br />
Quantative <strong>comparison</strong> <strong>of</strong> the <strong>approaches</strong><br />
bgschaid,pvita,dprieling,hsteiner RoWaFloSim 28/33
Introduction<br />
VoF-approach<br />
FAM-approach<br />
Conclusion<br />
References<br />
Overview<br />
Implementation<br />
Results<br />
MOVIE: Transient covering <strong>of</strong> a wafer<br />
bgschaid,pvita,dprieling,hsteiner RoWaFloSim 29/33
Introduction<br />
VoF-approach<br />
FAM-approach<br />
Conclusion<br />
References<br />
Summary <strong>of</strong> the results<br />
Results summary<br />
Acknowledgements<br />
• Two different <strong>solvers</strong> were compared<br />
• Two well-documented experimental cases were investigated<br />
• A variety <strong>of</strong> different solutions to the cases were taken<br />
• Asymptotic solution<br />
• Axial-symmetric solution using VoF<br />
• Full 3D-solution <strong>of</strong> the VoF<br />
• A special solver using the FAM<br />
• All <strong>approaches</strong> give similar results<br />
• Potentially best results (not surprisingly) would be given by<br />
the full 3D-solution<br />
• Usable for the actual application is the FAM-approach<br />
bgschaid,pvita,dprieling,hsteiner RoWaFloSim 30/33
Acknowledgements<br />
Introduction<br />
VoF-approach<br />
FAM-approach<br />
Conclusion<br />
References<br />
Results summary<br />
Acknowledgements<br />
• This work is part <strong>of</strong> the project RoWaFloSim which is<br />
funded by Austrian Research Promotion Fund within the<br />
ModSim-programme<br />
• The industrial sponsor <strong>and</strong> user <strong>of</strong> this work is the Lam<br />
Research AG (http://www.lamrc.com/)<br />
• This work would not have been possible without the people<br />
who brought us OpenFOAM TM , especially Henry Weller <strong>and</strong><br />
Hrvoje Jasak<br />
• No dams were hurt during the making <strong>of</strong> this study<br />
bgschaid,pvita,dprieling,hsteiner RoWaFloSim 31/33
The End<br />
Introduction<br />
VoF-approach<br />
FAM-approach<br />
Conclusion<br />
References<br />
Results summary<br />
Acknowledgements<br />
Thanks for listening!<br />
Questions<br />
bgschaid,pvita,dprieling,hsteiner RoWaFloSim 32/33
Previous work<br />
Introduction<br />
VoF-approach<br />
FAM-approach<br />
Conclusion<br />
References<br />
[CKG72] A F Charwat, R E Kelly, <strong>and</strong> C Gazley. The flow <strong>and</strong> stability <strong>of</strong> thin<br />
liquid films on a rotating disk. Journal <strong>of</strong> Fluid Mechanics,<br />
53:2:227–255, 1972.<br />
[KK09] Tae-Sung Kim <strong>and</strong> Moon-Uhn Kim. The flow <strong>and</strong> hydrodynamic<br />
stability <strong>of</strong> a liquid film on a rotating disc. Fluid Dynamics Research,<br />
41(3):035504 (28pp), Juni 2009.<br />
[OCF03] B. Ozar, B. Cetegen, <strong>and</strong> A. Faghri. Experiments on the flow <strong>of</strong> a<br />
thin liquid film over a horizontal stationary <strong>and</strong> rotating disk surface.<br />
Experiments in Fluids, 34:556–565, 2003.<br />
[RKC73] J. Rauscher, R. Kelly, <strong>and</strong> J. Cole. An asymptotic solution for the<br />
laminar flow <strong>of</strong> thin films on a rotating disk. Appl. Mechanics,<br />
40:45–47, 1973.<br />
[TFH91] S. Thomas, A. Faghri, <strong>and</strong> W. Hankey. Experimental analysis <strong>and</strong><br />
flow visualization <strong>of</strong> a thin liquid film on a stationary <strong>and</strong> rotating<br />
disk. Journal <strong>of</strong> Fluids Engineering, 113:73–80, 1991.<br />
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