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release on 2013-05-16_16-27-58

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goniva
2013-05-16 16:27:59 +02:00
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81
README
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@ -1,81 +0,0 @@
/*---------------------------------------------------------------------------*\
CFDEMcoupling - Open Source CFD-DEM coupling
CFDEMcoupling is part of the CFDEMproject
www.cfdem.com
Christoph Goniva, christoph.goniva@cfdem.com
Copyright 2009-2012 JKU Linz
Copyright 2012- DCS Computing GmbH, Linz
-------------------------------------------------------------------------------
License
This file is part of CFDEMcoupling.
CFDEMcoupling is free software; you can redistribute it and/or modify it
under the terms of the GNU General Public License as published by the
Free Software Foundation; either version 3 of the License, or (at your
option) any later version.
CFDEMcoupling is distributed in the hope that it will be useful, but WITHOUT
ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or
FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License
for more details.
You should have received a copy of the GNU General Public License
along with CFDEMcoupling; if not, write to the Free Software Foundation,
Inc., 51 Franklin St, Fifth Floor, Boston, MA 02110-1301 USA
Description
This code is designed to realize coupled CFD-DEM simulations using LIGGGHTS
and OpenFOAM. Note: this code is not part of OpenFOAM (see DISCLAIMER).
\*---------------------------------------------------------------------------*/
CFDEM coupling provides an open source parallel coupled CFD-DEM framework
combining the strengths of LIGGGHTS DEM code and the Open Source
CFD package OpenFOAM(R)(*). The CFDEMcoupling toolbox allows to expand
standard CFD solvers of OpenFOAM(R)(*) to include a coupling to the DEM
code LIGGGHTS. In this toolbox the particle representation within the
CFD solver is organized by "cloud" classes. Key functionalities are organised
in sub-models (e.g. force models, data exchange models, etc.) which can easily
be selected and combined by dictionary settings.
The coupled solvers run fully parallel on distributed-memory clusters.
Features are:
- its modular approach allows users to easily implement new models
- its MPI parallelization enables to use it for large scale problems
- the "forum"_lws on CFD-DEM gives the possibility to exchange with other
users / developers
- the use of GIT allows to easily update to the latest version
- basic documentation is provided
The file structure:
- "src" directory including the source files of the coupling toolbox and models
- "applications" directory including the solver files for coupled CFD-DEM simulations
- "doc" directory including the documentation of CFDEMcoupling
- "tutorials" directory including basic tutorial cases showing the functionality
Details on installation are given on the "www.cfdem.com"
The functionality of this CFD-DEM framwork is described via "tutorial cases" showing
how to use different solvers and models.
CFDEMcoupling stands for Computational Fluid Dynamics (CFD) -
Discrete Element Method (DEM) coupling.
CFDEMcoupling is an open-source code, distributed freely under the terms of the
GNU Public License (GPL).
Core development of CFDEMcoupling is done by
Christoph Goniva and Christoph Kloss, both at DCS Computing GmbH, 2012
\*---------------------------------------------------------------------------*/
(*) "OpenFOAM(R)"_of is a registered trade mark of the ESI Group.
This offering is not affiliated, approved or endorsed by ESI Group,
the producer of the OpenFOAM® software and owner of the OpenFOAM® trade mark.
\*---------------------------------------------------------------------------*/

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doc/CFDEMcoupling_Manual.pdf
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doc/githubAccess_public.pdf
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27
src/lagrangian/cfdemParticle/Make/files
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@ -6,7 +6,6 @@ voidFractionModels = subModels/voidFractionModel
locateModels = subModels/locateModel locateModels = subModels/locateModel
meshMotionModels = subModels/meshMotionModel meshMotionModels = subModels/meshMotionModel
momCoupleModels = subModels/momCoupleModel momCoupleModels = subModels/momCoupleModel
regionModels = subModels/regionModel
dataExchangeModels = subModels/dataExchangeModel dataExchangeModels = subModels/dataExchangeModel
averagingModels = subModels/averagingModel averagingModels = subModels/averagingModel
clockModels = subModels/clockModel clockModels = subModels/clockModel
@ -22,20 +21,33 @@ $(forceModels)/forceModel/newForceModel.C
$(forceModels)/noDrag/noDrag.C $(forceModels)/noDrag/noDrag.C
$(forceModels)/checkCouplingInterval/checkCouplingInterval.C $(forceModels)/checkCouplingInterval/checkCouplingInterval.C
$(forceModels)/DiFeliceDrag/DiFeliceDrag.C $(forceModels)/DiFeliceDrag/DiFeliceDrag.C
$(forceModels)/DiFeliceDragNLift/DiFeliceDragNLift.C
$(forceModels)/GidaspowDrag/GidaspowDrag.C $(forceModels)/GidaspowDrag/GidaspowDrag.C
$(forceModels)/SchillerNaumannDrag/SchillerNaumannDrag.C $(forceModels)/SchillerNaumannDrag/SchillerNaumannDrag.C
$(forceModels)/Archimedes/Archimedes.C $(forceModels)/Archimedes/Archimedes.C
$(forceModels)/ArchimedesIB/ArchimedesIB.C $(forceModels)/ArchimedesIB/ArchimedesIB.C
$(forceModels)/interface/interface.C $(forceModels)/interface/interface.C
$(forceModels)/ShirgaonkarIB/ShirgaonkarIB.C $(forceModels)/ShirgaonkarIB/ShirgaonkarIB.C
$(forceModels)/fieldTimeAverage/fieldTimeAverage.C
$(forceModels)/fieldBound/fieldBound.C
$(forceModels)/volWeightedAverage/volWeightedAverage.C
$(forceModels)/totalMomentumExchange/totalMomentumExchange.C
$(forceModels)/KochHillDrag/KochHillDrag.C $(forceModels)/KochHillDrag/KochHillDrag.C
$(forceModels)/BeetstraDrag/multiphaseFlowBasic/multiphaseFlowBasic.C
$(forceModels)/BeetstraDrag/BeetstraDrag.C
$(forceModels)/LaEuScalarLiquid/LaEuScalarLiquid.C
$(forceModels)/LaEuScalarTemp/LaEuScalarTemp.C $(forceModels)/LaEuScalarTemp/LaEuScalarTemp.C
$(forceModels)/LaEuScalarDust/LaEuScalarDust.C
$(forceModels)/virtualMassForce/virtualMassForce.C $(forceModels)/virtualMassForce/virtualMassForce.C
$(forceModels)/gradPForce/gradPForce.C $(forceModels)/gradPForce/gradPForce.C
$(forceModels)/gradULiftForce/gradULiftForce.C
$(forceModels)/viscForce/viscForce.C $(forceModels)/viscForce/viscForce.C
$(forceModels)/MeiLift/MeiLift.C $(forceModels)/MeiLift/MeiLift.C
$(forceModels)/fieldTimeAverage/fieldTimeAverage.C $(forceModels)/KochHillDragNLift/KochHillDragNLift.C
$(forceModels)/volWeightedAverage/volWeightedAverage.C $(forceModels)/solidsPressureForce/solidsPressureForce.C
$(forceModels)/periodicPressure/periodicPressure.C
$(forceModels)/periodicPressureControl/periodicPressureControl.C
$(forceModels)/averageSlipVel/averageSlipVel.C
$(forceModelsMS)/forceModelMS/forceModelMS.C $(forceModelsMS)/forceModelMS/forceModelMS.C
$(forceModelsMS)/forceModelMS/newForceModelMS.C $(forceModelsMS)/forceModelMS/newForceModelMS.C
@ -65,21 +77,18 @@ $(locateModels)/turboEngineSearch/turboEngineSearch.C
$(locateModels)/turboEngineSearchM2M/turboEngineSearchM2M.C $(locateModels)/turboEngineSearchM2M/turboEngineSearchM2M.C
$(locateModels)/engineSearchIB/engineSearchIB.C $(locateModels)/engineSearchIB/engineSearchIB.C
$(meshMotionModels)/meshMotionModel/meshMotionModel.C $(meshMotionModels)/meshMotionModel/meshMotionModel.C
$(meshMotionModels)/meshMotionModel/newMeshMotionModel.C $(meshMotionModels)/meshMotionModel/newMeshMotionModel.C
$(meshMotionModels)/noMeshMotion/noMeshMotion.C $(meshMotionModels)/noMeshMotion/noMeshMotion.C
$(meshMotionModels)/DEMdrivenMeshMotion/DEMdrivenMeshMotion.C
$(momCoupleModels)/momCoupleModel/momCoupleModel.C $(momCoupleModels)/momCoupleModel/momCoupleModel.C
$(momCoupleModels)/momCoupleModel/newMomCoupleModel.C $(momCoupleModels)/momCoupleModel/newMomCoupleModel.C
$(momCoupleModels)/explicitCouple/explicitCouple.C $(momCoupleModels)/explicitCouple/explicitCouple.C
$(momCoupleModels)/explicitCoupleSource/explicitCoupleSource.C
$(momCoupleModels)/implicitCouple/implicitCouple.C $(momCoupleModels)/implicitCouple/implicitCouple.C
$(momCoupleModels)/noCouple/noCouple.C $(momCoupleModels)/noCouple/noCouple.C
$(regionModels)/regionModel/regionModel.C
$(regionModels)/regionModel/newRegionModel.C
$(regionModels)/allRegion/allRegion.C
$(dataExchangeModels)/dataExchangeModel/dataExchangeModel.C $(dataExchangeModels)/dataExchangeModel/dataExchangeModel.C
$(dataExchangeModels)/dataExchangeModel/newDataExchangeModel.C $(dataExchangeModels)/dataExchangeModel/newDataExchangeModel.C
$(dataExchangeModels)/oneWayVTK/oneWayVTK.C $(dataExchangeModels)/oneWayVTK/oneWayVTK.C
@ -110,4 +119,4 @@ $(smoothingModels)/smoothingModel/newSmoothingModel.C
$(smoothingModels)/noSmoothing/noSmoothing.C $(smoothingModels)/noSmoothing/noSmoothing.C
$(smoothingModels)/constDiffSmoothing/constDiffSmoothing.C $(smoothingModels)/constDiffSmoothing/constDiffSmoothing.C
LIB = $(FOAM_USER_LIBBIN)/lib$(CFDEM_LIB_NAME) LIB = $(CFDEM_LIB_DIR)/lib$(CFDEM_LIB_NAME)

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tutorials/cfdemSolverPiso/ErgunTestCG/Allrun.sh Executable file
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#!/bin/bash
#===================================================================#
# allrun script for testcase as part of test routine
# run settlingTest
# Christoph Goniva - Sept. 2010
#===================================================================#
#- define variables
casePath="$(dirname "$(readlink -f ${BASH_SOURCE[0]})")"
# check if mesh was built
if [ -d "$casePath/CFD/constant/polyMesh/boundary" ]; then
echo "mesh was built before - using old mesh"
else
echo "mesh needs to be built"
cd $casePath/CFD
blockMesh
fi
#- run parallel CFD-DEM in new terminal
gnome-terminal --title='cfdemSolverPiso ErgunTestCG CFD' -e "bash $casePath/parCFDDEMrun.sh"

41
tutorials/cfdemSolverPiso/ErgunTestCG/CFD/0/Ksl Normal file
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@ -0,0 +1,41 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.6 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object Ksl;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -3 -1 0 0 0 0];
internalField uniform 0;
boundaryField
{
wall
{
type zeroGradient;
//type fixedValue;
//value uniform 0;
}
inlet
{
type zeroGradient;
}
outlet
{
type zeroGradient;
}
}
// ************************************************************************* //

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tutorials/cfdemSolverPiso/ErgunTestCG/CFD/0/U Normal file
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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.6 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volVectorField;
object U;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform (0 0 0);
boundaryField
{
wall
{
//type fixedValue;
//value uniform (0 0 0);
type slip;
}
inlet
{
/*type flowRateInletVelocity;
flowRate 0.001;
value uniform (0 0 0);*/
/*type fixedValue;
value uniform (0 0 0.0001);*/
//type zeroGradient;
/* type groovyBC;
variables "Uend=vector(0,0,0.02);tEnd=0.1;";
valueExpression "((time() < tEnd) ? Uend/tEnd*time():Uend)";
value uniform (0 0 0);*/
/*// 2.0.x, 1.6,ext
type timeVaryingUniformFixedValue;
fileName "steps_0p1s";
outOfBounds clamp;
value uniform (0 0 0);*/
// 2.1.x
type uniformFixedValueVoidfraction;
uniformValue table
(
(0.000 (0 0 0.002))
(0.020 (0 0 0.002))
(0.021 (0 0 0.004))
(0.040 (0 0 0.004))
(0.041 (0 0 0.006))
(0.060 (0 0 0.006))
(0.061 (0 0 0.008))
(0.080 (0 0 0.008))
(0.081 (0 0 0.010))
(0.100 (0 0 0.010))
(0.101 (0 0 0.012))
(0.120 (0 0 0.012))
(0.121 (0 0 0.014))
(0.140 (0 0 0.014))
(0.141 (0 0 0.016))
(0.160 (0 0 0.016))
(0.161 (0 0 0.018))
(0.180 (0 0 0.018))
(0.181 (0 0 0.020))
(0.200 (0 0 0.020))
);
}
outlet
{
/*type fluxCorrectedVelocity; //inletOutlet;
value uniform (0 0 0);
inletValue uniform (0 0 0);*/
type zeroGradient;
}
}
// ************************************************************************* //

45
tutorials/cfdemSolverPiso/ErgunTestCG/CFD/0/Us Normal file
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@ -0,0 +1,45 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.6 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volVectorField;
location "0";
object Us;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform (0 0 0);
boundaryField
{
wall
{
type zeroGradient;
//type fixedValue;
//value uniform (1 0 0);
}
inlet
{
type zeroGradient;
//type fixedValue;
//value uniform (1 0 0);;
}
outlet
{
type zeroGradient;
//type fixedValue;
//value uniform (1 0 0);
}
}
// ************************************************************************* //

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tutorials/cfdemSolverPiso/ErgunTestCG/CFD/0/epsilon Normal file
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@ -0,0 +1,48 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.6 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object epsilon;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -3 0 0 0 0];
internalField uniform 0.003;
boundaryField
{
wall
{
type epsilonWallFunction;
Cmu 0.09;
kappa 0.41;
E 9.8;
value uniform 0.003;
}
outlet
{
type inletOutlet;
inletValue uniform 0.003;
value uniform 0.003;
}
inlet
{
/*type turbulentMixingLengthDissipationRateInlet;
mixingLength 0.005;
value uniform 0.003;*/
type zeroGradient;
}
}
// ************************************************************************* //

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tutorials/cfdemSolverPiso/ErgunTestCG/CFD/0/k Normal file
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@ -0,0 +1,45 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.6 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object k;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -2 0 0 0 0];
internalField uniform 0.001;
boundaryField
{
wall
{
type kqRWallFunction;
value uniform 0.001;
}
outlet
{
type inletOutlet;
inletValue uniform 0.001;
value uniform 0.001;
}
inlet
{
/*type turbulentIntensityKineticEnergyInlet;
intensity 0.05;
value uniform 0.001;*/
type zeroGradient;
}
}
// ************************************************************************* //

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tutorials/cfdemSolverPiso/ErgunTestCG/CFD/0/nut Normal file
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@ -0,0 +1,45 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.6 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object nut;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -1 0 0 0 0];
internalField uniform 0;
boundaryField
{
wall
{
type nutWallFunction;
Cmu 0.09;
kappa 0.41;
E 9.8;
value uniform 0;
}
outlet
{
type calculated;
value uniform 0;
}
inlet
{
type calculated;
value uniform 0;
}
}
// ************************************************************************* //

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tutorials/cfdemSolverPiso/ErgunTestCG/CFD/0/p Normal file
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@ -0,0 +1,43 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.6 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object p;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -2 0 0 0 0];
internalField uniform 1.0e5;
boundaryField
{
wall
{
type zeroGradient;
}
inlet
{
type zeroGradient;
//type fixedValue;
//value uniform 100000;
}
outlet
{
//type zeroGradient;
type fixedValue;
value uniform 100000;
}
}
// ************************************************************************* //

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tutorials/cfdemSolverPiso/ErgunTestCG/CFD/0/rho Normal file
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@ -0,0 +1,39 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.6 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object rho;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -3 0 0 0 0 0];
internalField uniform 30;
boundaryField
{
wall
{
type zeroGradient;
}
inlet
{
type zeroGradient;
}
outlet
{
type zeroGradient;
}
}
// ************************************************************************* //

39
tutorials/cfdemSolverPiso/ErgunTestCG/CFD/0/voidfraction Normal file
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@ -0,0 +1,39 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.6 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object voidfraction;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 1;
boundaryField
{
wall
{
type zeroGradient;
}
outlet
{
type zeroGradient;
}
inlet
{
type zeroGradient;
}
}
// ************************************************************************* //

25
tutorials/cfdemSolverPiso/ErgunTestCG/CFD/constant/RASProperties Normal file
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@ -0,0 +1,25 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.6 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object RASProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
RASModel laminar;
turbulence off;
printCoeffs on;
// ************************************************************************* //

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tutorials/cfdemSolverPiso/ErgunTestCG/CFD/constant/couplingProperties Normal file
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@ -0,0 +1,177 @@
/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "";
case "";
instance "";
local "";
class dictionary;
object couplingProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
//===========================================================================//
// sub-models & settings
modelType "A"; // A or B
couplingInterval 100;
voidFractionModel divided;
locateModel engine;
meshMotionModel noMeshMotion;
regionModel allRegion;
IOModel "basicIO";
dataExchangeModel twoWayMPI;//twoWayFiles;//oneWayVTK;//
averagingModel dense;//dilute;//
clockModel off;//standardClock;//
forceModels
(
//GidaspowDrag
//DiFeliceDrag
KochHillDrag
gradPForce
viscForce
//Archimedes
//volWeightedAverage
//totalMomentumExchange
);
momCoupleModels
(
implicitCouple
);
turbulenceModelType "RASProperties";//"LESProperties";//
//===========================================================================//
// sub-model properties
implicitCoupleProps
{
velFieldName "U";
granVelFieldName "Us";
voidfractionFieldName "voidfraction";
}
ArchimedesProps
{
densityFieldName "rho";
gravityFieldName "g";
}
gradPForceProps
{
pFieldName "p";
densityFieldName "rho";
voidfractionFieldName "voidfraction";
velocityFieldName "U";
//interpolation;
}
viscForceProps
{
velocityFieldName "U";
densityFieldName "rho";
interpolation;
}
volWeightedAverageProps
{
scalarFieldNames
(
voidfraction
);
vectorFieldNames
(
);
upperThreshold 0.999;
lowerThreshold 0;
verbose;
}
totalMomentumExchangeProps
{
implicitMomExFieldName "Ksl";
explicitMomExFieldName "none";
fluidVelFieldName "U";
granVelFieldName "Us";
densityFieldName "rho";
}
GidaspowDragProps
{
velFieldName "U";
densityFieldName "rho";
}
DiFeliceDragProps
{
velFieldName "U";
densityFieldName "rho";
voidfractionFieldName "voidfraction";
}
KochHillDragProps
{
velFieldName "U";
densityFieldName "rho";
voidfractionFieldName "voidfraction";
//verbose;
}
virtualMassForceProps
{
velFieldName "U";
densityFieldName "rho";
}
oneWayVTKProps
{
couplingFilename "vtk_out%4.4d.vtk";
maxNumberOfParticles 30000;
}
twoWayFilesProps
{
maxNumberOfParticles 10100;
}
centreProps
{
alphaMin 0.10;
}
engineProps
{
treeSearch true;
}
dividedProps
{
alphaMin 0.1;
scaleUpVol 1.0;
}
twoWayMPIProps
{
maxNumberOfParticles 10100;
liggghtsPath "../DEM/in.liggghts_resume";
}
// ************************************************************************* //

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tutorials/cfdemSolverPiso/ErgunTestCG/CFD/constant/g Normal file
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@ -0,0 +1,22 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.6 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class uniformDimensionedVectorField;
location "constant";
object g;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -2 0 0 0 0];
value ( 0 0 -9.81 );
// ************************************************************************* //

30
tutorials/cfdemSolverPiso/ErgunTestCG/CFD/constant/liggghtsCommands Normal file
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/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "";
case "";
instance "";
local "";
class dictionary;
object liggghtsCommands;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
liggghtsCommandModels
(
runLiggghts
);
// ************************************************************************* //

154
tutorials/cfdemSolverPiso/ErgunTestCG/CFD/constant/polyMesh/blockMeshDict Normal file
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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.0 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object blockMeshDict;
}
// ************************************
meshGenApp blockMesh;
convertToMeters 1;
//64 mm column diameter
//15 cm length
//Width of middle square section
//how many cells in the square section
//how many cells from square section to perimeter
// how many cells from top to bottom
vertices
(
( 0.0069 0.0069 0.0 ) // Vertex fiveoclocksqb = 0
(-0.0069 0.0069 0.0 ) // Vertex sevenoclocksqb = 1
(-0.0069 -0.0069 0.0 ) // Vertex elevenoclocksqb = 2
( 0.0069 -0.0069 0.0 ) // Vertex oneoclocksqb = 3
( 0.00975807358913172 0.00975807357161699 0.0 ) // Vertex fiveoclockcb = 4
(-0.00975807358913172 0.00975807357161699 0.0) // Vertex sevenoclockcb = 5
(-0.00975807358913172 -0.00975807357161699 0.0) // Vertex elevenoclockcb = 6
( 0.00975807358913172 -0.00975807357161699 0.0) // Vertex oneoclockcb = 7
( 0.0069 0.0069 0.0553) // Vertex fiveoclocksqt = 8
(-0.0069 0.0069 0.0553) // Vertex sevenoclocksqt = 9
(-0.0069 -0.0069 0.0553) // Vertex elevenoclocksqt = 10
( 0.0069 -0.0069 0.0553) // Vertex oneoclocksqt = 11
( 0.00975807358913172 0.00975807357161699 0.0553) // Vertex fiveoclockct = 12
(-0.00975807358913172 0.00975807357161699 0.0553) // Vertex sevenoclockct = 13
(-0.00975807358913172 -0.00975807357161699 0.0553) // Vertex elevenoclockct = 14
( 0.00975807358913172 -0.00975807357161699 0.0553) // Vertex oneoclockct = 15
);
blocks
(
//square block
hex (
2 3 0 1
10 11 8 9
)
(8 8 24)
simpleGrading (1 1 1)
//slice1
hex (
1 0 4 5
9 8 12 13
)
(8 4 24)
simpleGrading (1 1 1)
//slice2
hex (
6 2 1 5
14 10 9 13
)
( 4 8 24)
simpleGrading (1 1 1)
//slice3
hex (
6 7 3 2
14 15 11 10
)
(8 4 24)
simpleGrading (1 1 1)
//slice4
hex (
3 7 4 0
11 15 12 8
)
(4 8 24)
simpleGrading (1 1 1)
);
//create the quarter circles
edges
(
arc 4 5 (0.0 0.0138 0.0 )
arc 5 6 (-0.0138 0.0 0.0)
arc 6 7 (0.0 -0.0138 0.0 )
arc 7 4 (0.0138 0.0 0.0)
arc 12 13 (0.0 0.0138 0.0553 )
arc 13 14 (-0.0138 0.0 0.0553 )
arc 14 15 (0.0 -0.0138 0.0553 )
arc 15 12 (0.0138 0.0 0.0553 )
);
patches
(
patch inlet
(
(0 3 2 1)
(0 4 7 3)
(4 0 1 5)
(1 2 6 5)
(3 7 6 2)
)
patch outlet
(
(8 11 10 9)
(8 12 15 11)
(12 8 9 13)
(9 10 14 13)
(11 15 14 10)
)
wall wall
(
(5 4 12 13)
(5 13 14 6)
(6 14 15 7)
(7 15 12 4)
)
);
mergePatchPairs
(
);

38
tutorials/cfdemSolverPiso/ErgunTestCG/CFD/constant/transportProperties Normal file
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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.6 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object transportProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
transportModel Newtonian;
nu nu [ 0 2 -1 0 0 0 0 ] 1.5e-04;
CrossPowerLawCoeffs
{
nu0 nu0 [ 0 2 -1 0 0 0 0 ] 1e-06;
nuInf nuInf [ 0 2 -1 0 0 0 0 ] 1e-06;
m m [ 0 0 1 0 0 0 0 ] 1;
n n [ 0 0 0 0 0 0 0 ] 1;
}
BirdCarreauCoeffs
{
nu0 nu0 [ 0 2 -1 0 0 0 0 ] 1e-06;
nuInf nuInf [ 0 2 -1 0 0 0 0 ] 1e-06;
k k [ 0 0 1 0 0 0 0 ] 0;
n n [ 0 0 0 0 0 0 0 ] 1;
}
// ************************************************************************* //

21
tutorials/cfdemSolverPiso/ErgunTestCG/CFD/constant/turbulenceProperties Normal file
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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.6 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object turbulenceProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
simulationType RASModel;
// ************************************************************************* //

69
tutorials/cfdemSolverPiso/ErgunTestCG/CFD/octave/loaddata.m Normal file
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function [data,colname]=loaddata(filename,columns,headerlines)
% data = loaddata(filename,columns,headerlines)
% data = loaddata(filename,0,headerlines): automatc detection of
% columns by word count in first headerline or first data line
% (if headerline==0), separated by blanks or tabs
% columns=-1: write colum assignment code lines
% works only if headerline>0 and colnames separated by
% not more than 1 blank!
% columns=-2: columns separated by 2 blanks (fluent/scheme auswertung-instat.scm)
% [data, colname] = loaddata(filename,0,headerlines)
% colname = cell string array of column names from headerline
fprintf(1,'loading %s ... ', filename);
f=fopen(filename,'r');
if f==-1
fprintf(1,'\n*** error: could not open "%s" ...\n', filename);
data=[];
else
for i=1:headerlines
if i==1 s=fgets(f); else fgets(f); end
end
if headerlines==0
s=fgets(f); frewind(f);
end
if columns<=0 % & headerlines>=1
fprintf(1,'\n');
fprintf(1,' %s',s);
pos = findstr(sprintf('\t'),s); % trennzeichenpositionen in zeile suchen
if length(pos)>0
endpos=length(s);
%if isspace(s(endpos-1)) endpos=endpos-1; end
pos = [0 pos(1,:) endpos]; % anfangs- und endposition hinzuf<EFBFBD>gen
elseif columns==-2 % spalteneintr<EFBFBD>ge durch 2 blanks getrennt (fluent/scheme)
pos=[0];
for i=1:length(s)-1
if isspace(s(i)) & isspace(s(i+1))
pos(end+1)=i+1;
end
end
pos(end+1)=length(s);
else % spalteneintr<EFBFBD>ge durch blanks getrennt
%pos = findstr(' ',s); % trennzeichenpositionen in zeile suchen
pos=[];
word=0;
for i=1:length(s)
if isspace(s(i))
word=0;
elseif ~word
word=1;
pos(end+1)=i-1;
end
end
pos(end+1)=length(s);
end
if headerlines>=1
for i=1:length(pos)-1 % alle spalten
colname{i}=s(pos(i)+1:pos(i+1)-1);
if columns==-1 fprintf(' = data(strmatch(''%s'',colname),:); %% column %d\n', colname{i},i); end
if columns==-2 fprintf('%% column %d: %s\n', i, colname{i}); end
end
end
columns = length(pos)-1;
fprintf(1,' total: %d columns ',columns);
end
data=fscanf(f,'%f',[columns,inf]);
fclose(f);
fprintf(1,'done.\n');
end

22
tutorials/cfdemSolverPiso/ErgunTestCG/CFD/octave/scaling.m Normal file
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close all;
clear;
clc;
%====================================%
% setting up the scaling factor
%====================================%
%-constants
g=9.81
%- particle props
dp=0.0008
rhoP=200
Vp=dp^3*pi/6
np=19531
%- scaling
dParcel=dp*2
VParcel=dParcel^3*pi/6
nParcel=np*Vp/VParcel
dragForceScale=dParcel/dp

96
tutorials/cfdemSolverPiso/ErgunTestCG/CFD/octave/totalPressureDrop.m Normal file
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close all;
clear;
clc;
%====================================%
% simulation data 1
%====================================%
rhoG = 30 % density in kg/m3
%path = '../probes/0/p';
path = '../probes/0/p';
columns=22;
headerlines=4;
data = loaddata(path,columns,headerlines);
data=transpose(data);
[x,y]=size(data)
dp_sim = (data(:,2)-data(:,y))*rhoG;
t_sim = data(:,1);
%fprintf('final pressureDrop of sim = %f Pa\n',dp_sim(length(dp_sim)) )
%====================================%
% analytical calculation
%====================================%
%===================
% Ergun Equation
%===================
fprintf('\ncalc Ergun eqn:\n')
dp = 0.0008 % particle diameter
phip = 1 % sphericity
epsilon = 0.451335 % void fraction
Ustart = 0.002
Uend = 0.02
timeStepSize = 0.001; % time interval of pressure data
Tstart = 0;
Tend = t_sim(length(t_sim));
deltaU=(Uend-Ustart)/((Tend-Tstart)/timeStepSize);
U = Ustart+deltaU:deltaU:Uend; % velocity over time
Ua = U / epsilon; % physical velocity
L = 0.0156 % length of bed
nuG = 1.5*10^-4 % kinemat Visk in m2/s
muG = nuG*rhoG % dynam visc in Pa s
dpErgun= L * (
150*((1-epsilon)^2/epsilon^3)*((muG.*U)/(phip*dp)^2)
+1.75*((1-epsilon)/epsilon^3)*((rhoG.*U.^2)/(phip*dp))
);
fprintf('NOTE: this pressure is divided by density (according to CFD solver)\n')
fprintf('so the result does not depend on density\n')
%fprintf('final pressure drop (Ergun eqn)= %f Pa\n',dpErgun)
%==================================
% min fluidization velocity in m/s
%==================================
rhoP = 7000 % particle density in kg/m3
g = 9.81 % gravity m/s2
Umf = dp^2*(rhoP-rhoG)*g/(150*muG)*(epsilon^3*phip^2)/(1-epsilon)
ReMF = Umf*dp*rhoG/muG % must be <20 !!!
%Umf = sqrt(phip*dp^2/1.75*(rhoP-rhoG)/rhoG*g*epsilon^3) % Re>1000
dpUmf= L * (
150*((1-epsilon)^2/epsilon^3)*((muG.*Umf)/(phip*dp)^2)
+1.75*((1-epsilon)/epsilon^3)*((rhoG.*Umf.^2)/(phip*dp))
);
%====================================%
% plot data
%====================================%
length(U)
length(dp_sim)
figure(2)
plot(U,dp_sim)
title("Ergun pressure drop vs. simulation")
a=strcat("analytical (Ergun), Umf=",num2str(Umf),", dpUmf=",num2str(dpUmf));
legend(a,"simulation")
xlabel("velocity in [m/s]")
ylabel("pressure drop [Pa]")
axis([0,Uend,0,dpErgun(length(dpErgun))])
figure(1)
plot(U,dpErgun,U,dp_sim,[Umf,Uend],dpUmf*ones(1,2))
title("Ergun pressure drop vs. simulation")
a=strcat("analytical (Ergun), Umf=",num2str(Umf),", dpUmf=",num2str(dpUmf));
legend(a,"simulation")
xlabel("velocity in [m/s]")
ylabel("pressure drop [Pa]")
axis([0,Uend,0,dpErgun(length(dpErgun))])
%print('cfdemSolverPiso_settlingTest.eps','-deps2')
print -color "cfdemSolverPiso_ErgunTestMPI.eps"
replot;

22
tutorials/cfdemSolverPiso/ErgunTestCG/CFD/steps_0p1s Normal file
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(
(0.000 (0 0 0.002))
(0.010 (0 0 0.002))
(0.011 (0 0 0.004))
(0.020 (0 0 0.004))
(0.021 (0 0 0.006))
(0.030 (0 0 0.006))
(0.031 (0 0 0.008))
(0.040 (0 0 0.008))
(0.041 (0 0 0.010))
(0.050 (0 0 0.010))
(0.051 (0 0 0.012))
(0.060 (0 0 0.012))
(0.061 (0 0 0.014))
(0.070 (0 0 0.014))
(0.071 (0 0 0.016))
(0.080 (0 0 0.016))
(0.081 (0 0 0.018))
(0.090 (0 0 0.018))
(0.091 (0 0 0.020))
(0.100 (0 0 0.020))
)

168
tutorials/cfdemSolverPiso/ErgunTestCG/CFD/system/controlDict Normal file
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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.6 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
application pisoFoam;
startFrom startTime;
startTime 0;
stopAt endTime;
endTime 0.2;//0.01;
deltaT 0.001;
writeControl adjustableRunTime;
writeInterval 0.005;//0.01;
purgeWrite 0;
writeFormat ascii;
writePrecision 6;
writeCompression uncompressed;
timeFormat general;
timePrecision 6;
runTimeModifiable yes;
adjustTimeStep no;
maxCo 0.1;
//libs ( "libgroovyBC.so" );
libs ( "libfiniteVolumeCFDEM.so" );
functions
(
probes
{
type probes;
// Where to load it from
functionObjectLibs ( "libsampling.so" );
// Name of the directory for probe data
name probes;
probeLocations
(
(0 0 0.0001)
(0 0 0.0026)
(0 0 0.0051)
(0 0 0.0076)
(0 0 0.0101)
(0 0 0.0126)
(0 0 0.0151)
(0 0 0.0176)
(0 0 0.0201)
(0 0 0.0226)
(0 0 0.0251)
(0 0 0.0276)
(0 0 0.0301)
(0 0 0.0326)
(0 0 0.0351)
(0 0 0.0375)
(0 0 0.0401)
(0 0 0.0426)
(0 0 0.0451)
(0 0 0.0476)
(0 0 0.0529)
);
// Fields to be probed
fields ( p U voidfraction volAverage_voidfraction);
// Write at same frequency as fields
outputControl timeStep;//outputTime;
outputInterval 1;
}
probes_inletFlux
{
type faceSource;
functionObjectLibs ("libfieldFunctionObjects.so");
enabled true;
outputControl timeStep; //outputTime;
log true; // log to screen?
valueOutput true; // Write values at run-time output times?
source patch; // Type of face source:
sourceName inlet; // faceZone name, see below
operation sum;
fields
(
phi
);
}
probes_outletFlux
{
type faceSource;
functionObjectLibs ("libfieldFunctionObjects.so");
enabled true;
outputControl timeStep; //outputTime;
log true; // log to screen?
valueOutput true; // Write values at run-time output times?
source patch; // Type of face source:
sourceName outlet; // faceZone name, see below
operation sum;
fields
(
phi
);
}
probes_wallFlux
{
type faceSource;
functionObjectLibs ("libfieldFunctionObjects.so");
enabled true;
outputControl timeStep; //outputTime;
log true; // log to screen?
valueOutput true; // Write values at run-time output times?
source patch; // Type of face source:
sourceName wall; // faceZone name, see below
operation sum;
fields
(
phi
);
}
/*pressureDrop
{
type patchAverage;
functionObjectLibs
(
"libsimpleFunctionObjects.so"
);
verbose true;
patches
(
inlet
outlet
);
fields
(
p
);
factor 1;
}*/
);
// ************************************************************************* //

117
tutorials/cfdemSolverPiso/ErgunTestCG/CFD/system/controlDict.foam Normal file
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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.6 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
application pisoFoam;
startFrom startTime;
startTime 0;
stopAt endTime;
endTime 0.1;//0.01;
deltaT 0.001;
writeControl adjustableRunTime;
writeInterval 0.001;//0.01;
purgeWrite 0;
writeFormat ascii;
writePrecision 6;
writeCompression uncompressed;
timeFormat general;
timePrecision 6;
runTimeModifiable yes;
adjustTimeStep no;
maxCo 0.1;
libs ("libOpenFOAM.so" "libgroovyBC.so");
functions
(
probes
{
type probes;
// Where to load it from
functionObjectLibs ( "libsampling.so" );
// Name of the directory for probe data
name probes;
probeLocations
(
(0 0 0.0001)
(0 0 0.0026)
(0 0 0.0051)
(0 0 0.0076)
(0 0 0.0101)
(0 0 0.0126)
(0 0 0.0151)
(0 0 0.0176)
(0 0 0.0201)
(0 0 0.0226)
(0 0 0.0251)
(0 0 0.0276)
(0 0 0.0301)
(0 0 0.0326)
(0 0 0.0351)
(0 0 0.0375)
(0 0 0.0401)
(0 0 0.0426)
(0 0 0.0451)
(0 0 0.0476)
(0 0 0.0529)
);
// Fields to be probed
fields ( p U voidfraction volAverage_voidfraction);
// Write at same frequency as fields
outputControl timeStep;//outputTime;
outputInterval 1;
}
/*pressureDrop
{
type patchAverage;
functionObjectLibs
(
"libsimpleFunctionObjects.so"
);
verbose true;
patches
(
inlet
outlet
);
fields
(
p
);
factor 1;
}*/
);
// ************************************************************************* //

86
tutorials/cfdemSolverPiso/ErgunTestCG/CFD/system/decomposeParDict Normal file
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/*-------------------------------*- C++ -*---------------------------------*\
| ========= |
| \\ / OpenFOAM |
| \\ / |
| \\ / The Open Source CFD Toolbox |
| \\/ http://www.OpenFOAM.org |
\*-------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
note "mesh decomposition control dictionary";
location "system";
object decomposeParDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
numberOfSubdomains 4;
//- Keep owner and neighbour on same processor for faces in zones:
// preserveFaceZones (heater solid1 solid3);
//method scotch;
// method hierarchical;
method simple;
// method metis;
// method manual;
simpleCoeffs
{
n (1 2 2);
delta 0.001;
}
hierarchicalCoeffs
{
n (2 2 1);
delta 0.001;
order xyz;
}
metisCoeffs
{
/*
processorWeights
(
1
1
1
1
);
*/
}
scotchCoeffs
{
//processorWeights
//(
// 1
// 1
// 1
// 1
//);
//writeGraph true;
//strategy "b";
}
manualCoeffs
{
dataFile "decompositionData";
}
//// Is the case distributed
//distributed yes;
//// Per slave (so nProcs-1 entries) the directory above the case.
//roots
//(
// "/tmp"
// "/tmp"
//);
// ************************************************************************* //

33
tutorials/cfdemSolverPiso/ErgunTestCG/CFD/system/funkySetFieldsDict Executable file
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FoamFile
{
version 2.0;
format ascii;
root "/.automount/werner/Werner/bgschaid/bgschaid-foamStuff/DepositionTests";
case "neutralTest";
instance "system";
local "";
class dictionary;
object funkySetFieldsDict;
}
expressions
(
init
{
field voidfraction;
expression "1";
valuePatches 2(inlet outlet); // set value 1 at those patches
}
setGamma
{
field voidfraction;
expression "0.43";
//condition "pow(pow(pos().x-0.2,2) + pow(pos().y-0,2)+ pow(pos().z-0,2),0.5) < 0.04";
condition "pos().z < 0.01467 && pos().z > 0.0";
keepPatches true;
//valuePatches 1(inlet); // set value 1 at those patches
}
);

76
tutorials/cfdemSolverPiso/ErgunTestCG/CFD/system/fvSchemes Normal file
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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.6 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
ddtSchemes
{
default Euler;
}
gradSchemes
{
default Gauss linear;
grad(p) Gauss linear;
grad(U) Gauss linear;
}
divSchemes
{
default Gauss linear;
div(phi,U) Gauss limitedLinearV 1;
div(phi,k) Gauss limitedLinear 1;
div(phi,epsilon) Gauss limitedLinear 1;
div(phi,R) Gauss limitedLinear 1;
div(R) Gauss linear;
div(phi,nuTilda) Gauss limitedLinear 1;
div((viscousTerm*dev(grad(U).T()))) Gauss linear;
div((nu*dev(grad(U).T()))) Gauss linear;
div((nuEff*dev(grad(U).T()))) Gauss linear;
}
laplacianSchemes
{
default Gauss linear corrected;
laplacian(viscousTerm,U) Gauss linear corrected;
laplacian(nu,U) Gauss linear corrected;
laplacian(nuEff,U) Gauss linear corrected;
laplacian((1|A(U)),p) Gauss linear corrected;
laplacian((voidfraction2|A(U)),p) Gauss linear corrected;
laplacian(DkEff,k) Gauss linear corrected;
laplacian(DepsilonEff,epsilon) Gauss linear corrected;
laplacian(DREff,R) Gauss linear corrected;
laplacian(DnuTildaEff,nuTilda) Gauss linear corrected;
}
interpolationSchemes
{
default linear;
interpolate(U) linear;
}
snGradSchemes
{
default corrected;
}
fluxRequired
{
default no;
p ;
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.6 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
p
{
solver PCG;
preconditioner DIC;
tolerance 1e-06;
relTol 0.1;
}
pFinal
{
solver PCG;
preconditioner DIC;
tolerance 1e-06;
relTol 0;
}
U
{
solver PBiCG;
preconditioner DILU;
tolerance 1e-05;
relTol 0;
}
k
{
solver PBiCG;
preconditioner DILU;
tolerance 1e-05;
relTol 0;
}
epsilon
{
solver PBiCG;
preconditioner DILU;
tolerance 1e-05;
relTol 0;
}
R
{
solver PBiCG;
preconditioner DILU;
tolerance 1e-05;
relTol 0;
}
nuTilda
{
solver PBiCG;
preconditioner DILU;
tolerance 1e-05;
relTol 0;
}
}
PISO
{
nCorrectors 4;
nNonOrthogonalCorrectors 1;
pRefCell 0;
pRefValue 0;
}
// ************************************************************************* //

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#######################################################
# tutorial case showing coarse graining functionality #
# Christoph Goniva 08.02.2013 #
#######################################################
echo both
#######################################################
# variables #
#######################################################
variable cg equal 2
variable nPorg equal 19531
variable nPscal equal ${nPorg}/(${cg}*${cg}*${cg})
#######################################################
atom_style granular
atom_modify map array
communicate single vel yes
coarsegraining ${cg}
boundary m m m
newton off
units si
region reg block -0.015 0.015 -0.015 0.015 -0.001 0.0554 units box
create_box 1 reg
neighbor 0.001 bin
neigh_modify delay 0
#Material properties required for new pair styles
fix m1 all property/global youngsModulus peratomtype 5.e6
fix m2 all property/global poissonsRatio peratomtype 0.45
fix m3 all property/global coefficientRestitution peratomtypepair 1 0.3
fix m4 all property/global coefficientFriction peratomtypepair 1 0.5
fix m5 all property/global characteristicVelocity scalar 1.
#pair style
pair_style gran/hooke/history
pair_coeff * *
#timestep, gravity
timestep 0.000005
fix gravi all gravity 9.81 vector 0.0 0.0 -1.0
#walls
fix zwalls1 all wall/gran/hooke/history primitive type 1 zplane 0.0
fix zwalls2 all wall/gran/hooke/history primitive type 1 zplane 0.0553
fix cylwalls all wall/gran/hooke/history primitive type 1 zcylinder 0.01385 0. 0. tangential_damping off
#particle distributions and insertion
region bc cylinder z 0.0 0.0 0.012 0. 0.055 units box
fix pts1 all particletemplate/sphere 1 atom_type 1 density constant 200 radius constant 0.0004
fix pdd1 all particledistribution/discrete 1. 1 pts1 1.0
fix ins all insert/pack seed 100001 distributiontemplate pdd1 vel constant 0. 0. -1. insert_every once overlapcheck yes all_in yes particles_in_region ${nPscal} region bc
#apply nve integration to all particles that are inserted as single particles
fix integr all nve/sphere
#screen output
compute 1 all erotate/sphere
thermo_style custom step atoms ke c_1 vol
thermo 1000
thermo_modify lost ignore norm no
compute_modify thermo_temp dynamic yes
#insert the first particles so that dump is not empty
run 1
dump dmp all custom 5000 post/dump.liggghts_init id type type x y z ix iy iz vx vy vz fx fy fz omegax omegay omegaz radius
#force : f_couple_cfd[0] f_couple_cfd[1] f_couple_cfd[2]
#node : f_couple_cfd[6]
#cell id : f_couple_cfd[7]
run 10000 upto
write_restart liggghts.restart_coarseGraining_${cg}

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#######################################################
# tutorial case showing coarse graining functionality #
# Christoph Goniva 08.02.2013 #
#######################################################
echo both
#######################################################
# variables #
#######################################################
variable cg equal 2
variable nPorg equal 19531
variable nPscal equal ${nPorg}/(${cg}*${cg}*${cg})
#######################################################
atom_style granular
atom_modify map array
communicate single vel yes
coarsegraining ${cg}
boundary m m m
newton off
units si
processors 1 2 2
#read the restart file
read_restart ../DEM/liggghts.restart_coarseGraining_${cg}
#do not do this here, the simulation box is in the restart file!
#region reg block -0.015 0.015 -0.015 0.015 -0.001 0.0554 units box
#create_box 1 reg
neighbor 0.0005 bin
neigh_modify delay 0
#Material properties required for new pair styles
fix m1 all property/global youngsModulus peratomtype 5.e6
fix m2 all property/global poissonsRatio peratomtype 0.45
fix m3 all property/global coefficientRestitution peratomtypepair 1 0.3
fix m4 all property/global coefficientFriction peratomtypepair 1 0.5
fix m5 all property/global characteristicVelocity scalar 1.
#pair style
pair_style gran/hooke/history #Hertzian without cohesion
pair_coeff * *
#timestep, gravity
timestep 0.00001
fix gravi all gravity 9.81 vector 0.0 0.0 -1.0
#walls
fix zwalls1 all wall/gran/hooke/history primitive type 1 zplane 0.0
fix zwalls2 all wall/gran/hooke/history primitive type 1 zplane 0.0553
fix cylwalls all wall/gran/hooke/history primitive type 1 zcylinder 0.01385 0. 0. tangential_damping off
# change the particles density
set group all density 7000
#cfd coupling
fix cfd all couple/cfd couple_every 100 mpi
fix cfd2 all couple/cfd/force
#apply nve integration to all particles that are inserted as single particles
fix integr all nve/sphere
#center of mass
compute centerOfMass all com
#compute total dragforce
#compute dragtotal all reduce sum f_dragforce[1] f_dragforce[2] f_dragforce[3]
#screen output
compute 1 all erotate/sphere
thermo_style custom step atoms ke c_1 vol c_centerOfMass[3] #c_dragtotal[1] c_dragtotal[2] c_dragtotal[3]
thermo 10
thermo_modify lost ignore norm no
compute_modify thermo_temp dynamic yes
#insert the first particles so that dump is not empty
dump myDump all stl 1 post/dump_*.stl
#run 1
dump dmp all custom 5000 ../DEM/post/dump*.liggghts_restart id type type x y z ix iy iz vx vy vz fx fy fz omegax omegay omegaz radius
undump myDump
run 1

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dummyfile

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#!/bin/bash
#===================================================================#
# allrun script for testcase as part of test routine
# run settlingTest CFD part
# Christoph Goniva - Feb. 2011
#===================================================================#
#- source CFDEM env vars
. ~/.bashrc
#- include functions
source $CFDEM_SRC_DIR/etc/functions.sh
#--------------------------------------------------------------------------------#
#- define variables
casePath="$(dirname "$(readlink -f ${BASH_SOURCE[0]})")"
logpath=$casePath
headerText="run_parallel_cfdemSolverPiso_ErgunTestMPI_CFDDEM"
logfileName="log_$headerText"
solverName="cfdemSolverPiso"
nrProcs="4"
machineFileName="none" # yourMachinefileName | none
debugMode="off" # on | off | strict
testHarnessPath="$CFDEM_TEST_HARNESS_PATH"
runOctave="true"
postproc="false"
#--------------------------------------------------------------------------------#
#- call function to run a parallel CFD-DEM case
parCFDDEMrun $logpath $logfileName $casePath $headerText $solverName $nrProcs $machineFileName $debugMode
if [ $runOctave == "true" ]
then
#------------------------------#
# octave
#- change path
cd octave
#- rmove old graph
rm cfdemSolverPiso_ErgunTestMPI.eps
#- run octave
octave totalPressureDrop.m
#- show plot
evince cfdemSolverPiso_ErgunTestMPI.eps
#- copy log file to test harness
cp ../../$logfileName $testHarnessPath
cp cfdemSolverPiso_ErgunTestMPI.eps $testHarnessPath
fi
if [ $postproc == "true" ]
then
#- keep terminal open (if started in new terminal)
echo "simulation finisehd? ...press enter to proceed"
read
#- get VTK data from liggghts dump file
cd $casePath/DEM/post
python -i $CFDEM_LPP_DIR/lpp.py dump*.liggghts_restart
#- get VTK data from CFD sim
cd $casePath/CFD
foamToVTK #- serial run of foamToVTK
#source $CFDEM_SRC_DIR/etc/functions.sh #- include functions
#pseudoParallelRun "foamToVTK" $nrPostProcProcessors #- pseudo parallel run of foamToVTK
#- start paraview
paraview
#- keep terminal open (if started in new terminal)
echo "...press enter to clean up case"
echo "press Ctr+C to keep data"
read
fi
#- clean up case
echo "deleting data at: $casePath :\n"
rm -r $casePath/CFD/0.*
rm -r $casePath/CFD/log.*
rm -r $casePath/CFD/octave/octave-core
rm -r $casePath/CFD/VTK
rm -r $casePath/CFD/processor*
rm -r $casePath/CFD/couplingFiles/*
rm -r $casePath/DEM/post/*
rm -r $casePath/DEM/log.*
rm -r $casePath/DEM/liggghts.restartCFDEM*
rm -r $casePath/CFD/probes*
rm -r $casePath/CFD/particles
rm -r $casePath/CFD/lagrangian
rm -r $casePath/CFD/clockData
echo "done"
#- preserve post directory
echo "dummyfile" >> $casePath/DEM/post/dummy