Richardson Foam. L. Orgogozo et al.

This commit is contained in:
Hrvoje Jasak 2017-09-21 14:04:10 +01:00
commit f7b52279af
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RichardsFoam.C
EXE = $(FOAM_USER_APPBIN)/RichardsFoam

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EXE_INC = \
-I$(LIB_SRC)/finiteVolume/lnInclude
EXE_LIBS = \
-lfiniteVolume

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/*---------------------------------------------------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | Copyright (C) 1991-2010 OpenCFD Ltd.
\\/ M anipulation |
-------------------------------------------------------------------------------
License
This file is part of OpenFOAM.
OpenFOAM 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.
OpenFOAM 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 OpenFOAM. If not, see <http://www.gnu.org/licenses/>.
Application
RichardsFoam
Description
Transient solver for flow in unsaturated porous media
With chord slope formulation of the Richards equation.
van Genuchten laws for unsaturated hydraulic properties parametrisation
Global computation of the convergence criterium
Adaptative time stepping with a stabilisation procedure
NB 1: use backward scheme for time discretisation
NB 2: use only mesh with constant cell volumes
References
version 0.0 (develloped with OpenFOAM 2.0.1)
Details may be found in:
Orgogozo, L., Renon, N., Soulaine, C., Hénon, F., Tomer, S.K., Labat, D.,
Pokrovsky, O.S., Sekhar, M., Ababou, R., Quintard, M., Submitted.
Mechanistic modelling of water fluxes at the watershed scale: An open source
massively parallel solver for Richards equation.
Submitted to Computer Physics Communications.
\*---------------------------------------------------------------------------*/
#include "fvCFD.H"
#include "pimpleControl.H"
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
int main(int argc, char *argv[])
{
# include "setRootCase.H"
# include "createTime.H"
# include "createMesh.H"
// pimpleControl pimple(mesh);
# include "readPicardControls.H"
# include "createFields.H"
# include "initContinuityErrs.H"
# include "createTimeControls.H"
Info<< "\nStarting time loop\n" << endl;
// starting of the time loop.
while (runTime.loop())
{
// time step control operations.
# include "readTimeControls.H"
# include "setDeltaT.H"
// runTime++;
Info<< "Time = " << runTime.timeName() << nl << endl;
// Beginning of the stabilisation loop for the stabilised adaptive time
// step procedure.
for (int cyc = 0; cyc < nMaxCycle; cyc++)
{
// Beginning of the Picard loop.
for (int pic = 0; pic < nIterPicard; pic++)
{
# include "psiEqn.H"
}
// Exit test for the loop associated with the stabilisation cycles
// for the adaptive time step procedure.
if (crit < precPicard)
{
break;
}
else
{
Info << "Criterion not reached, restart time loop iteration"
<< "with a smaller time step / Error = " << crit
<< nl << endl;
runTime.setDeltaT((1/tFact)*runTime.deltaTValue());
Info<< "deltaT = " << runTime.deltaTValue() << endl;
}
// End of the stabilisation cycles loop.
}
// Warning test in case of convergence failure of the Picard loop.
if (crit >= precPicard)
{
Info<< "Convergence failure / Error = " << crit << nl << endl;
currentPicard = nIterPicard;
}
// Final updating of the result fields before going to the next time
// iteration.
psi_tmp = psi;
thtil_tmp = 0.5*
(
(1 + sign(psi_tmp)) + (1 - sign(psi_tmp))*
pow((1 + pow(mag(alpha*psi_tmp),n)), - (1 - (1/n)))
);
theta = (thetas - thetar)*thtil + thetar;
U = - Krel*((fvc::grad(psi)) + vuz);
// Writting of the result.
runTime.write();
Info<< "ExecutionTime = " << runTime.elapsedCpuTime() << " s"
<< " ClockTime = " << runTime.elapsedClockTime() << " s"
<< nl << endl;
// end of the time loop.
}
Info<< "End\n" << endl;
return 0;
}
// ************************************************************************* //

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Info<< "Reading transportProperties\n" << endl;
// reading of the physical constant associated with the considered problem.
// Localisation of the data within the considered case:
// constant/transportProperties
IOdictionary transportProperties
(
IOobject
(
"transportProperties",
runTime.constant(),
mesh,
IOobject::MUST_READ,
IOobject::NO_WRITE
)
);
dimensionedScalar K
(
transportProperties.lookup("K")
);
dimensionedScalar alpha
(
transportProperties.lookup("alpha")
);
dimensionedScalar thetas
(
transportProperties.lookup("thetas")
);
dimensionedScalar thetar
(
transportProperties.lookup("thetar")
);
dimensionedScalar n
(
transportProperties.lookup("n")
);
dimensionedScalar C
(
transportProperties.lookup("C")
);
dimensionedScalar S
(
transportProperties.lookup("S")
);
// declaration of the variable and results fields
// Water velocity field [m/s]
Info<< "Reading field U\n" << endl;
volVectorField U
(
IOobject
(
"U",
runTime.timeName(),
mesh,
IOobject::MUST_READ,
IOobject::AUTO_WRITE
),
mesh
);
// Water saturation field [-]
Info<< "Reading field theta\n" << endl;
volScalarField theta
(
IOobject
(
"theta",
runTime.timeName(),
mesh,
IOobject::MUST_READ,
IOobject::AUTO_WRITE
),
mesh
);
// Water pressure field [m] - field of resolution.
Info<< "Reading field psi\n" << endl;
volScalarField psi
(
IOobject
(
"psi",
runTime.timeName(),
mesh,
IOobject::MUST_READ,
IOobject::AUTO_WRITE
),
mesh
);
// Field of residuals for the Picard loop [m].
Info<< "Reading field err\n" << endl;
volScalarField err
(
IOobject
(
"err",
runTime.timeName(),
mesh,
IOobject::MUST_READ,
IOobject::AUTO_WRITE
),
mesh
);
// Dimensionned unit scalar field [m].
Info<< "Reading field vuz\n" << endl;
volVectorField vuz
(
IOobject
(
"vuz",
runTime.timeName(),
mesh,
IOobject::MUST_READ,
IOobject::AUTO_WRITE
),
mesh
);
// Dimensionless unit vertical upward vector field.
Info<< "Reading field usf\n" << endl;
volScalarField usf
(
IOobject
(
"usf",
runTime.timeName(),
mesh,
IOobject::MUST_READ,
IOobject::AUTO_WRITE
),
mesh
);
# include "createPhi.H"
// Initialisation of the scalar containing the number of mesh cells. Note the
// use of gSum instead of sum.
double nbMesh;
nbMesh = gSum(usf);
// Initialisation of the scalar containing the residual for the exit test of the
// Picard loop.
double crit;
crit=0.;
// Initialisation of the token which counts the number of Picard iteraion for
// the adaptive time step procedure.
int currentPicard;
currentPicard = nIterPicard-3;
// Initialisation of the token which counts the number of Stabilisation cycle
// for the stabilisation of the adaptive time step procedure.
int sc;
sc = 0;
// Initialisation of the field of altitudes.
volVectorField positionVector = mesh.C();
volScalarField z = positionVector.component(vector::Z);
// Initialisation of the intermediate fields for the Picard loop.
volScalarField psi_tmp = psi;
volScalarField psim1 = psi;
// Initialisation of the varying transport properties for the Picard loop.
volScalarField thtil =
0.5*
(
(1 + sign(psi)) + (1 - sign(psi))*
pow((1 + pow(mag(alpha*psi),n)), - (1 - (1/n)))
);
volScalarField thtil_tmp =
0.5*
(
(1 + sign(psi_tmp)) + (1-sign(psi_tmp))*
pow((1 + pow(mag(alpha*psi_tmp),n)), - (1 - (1/n)))
);
volScalarField Krel =
0.5*
(
(1 + sign(psi))*K + (1 - sign(psi))*K*pow(thtil,0.5)*
pow((1 - pow((1 - pow(thtil,(n/(n - 1)))),(1 - (1/n)))),2)
);
volScalarField Crel =
S + 0.5*
(
(1 - sign(psi))*((thetas - thetar)*(thtil - thtil_tmp)*
(1./((usf*pos(psi - psi_tmp)*pos(psi_tmp - psi)) + psi - psi_tmp)))
);
// Initialisation of the gravity term.
volVectorField gradk = fvc::grad(Krel);
volScalarField gradkz = gradk.component(vector::Z);
// Initialisation of the velocity field.
U = - Krel*((fvc::grad(psi)) + vuz);

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psim1 = psi;
psi = psi_tmp;
// Resolution of the linear system.
fvScalarMatrix psiEqn
(
Crel*fvm::ddt(psi)
==
fvm::laplacian(Krel, psi, "laplacian(Krel,psi)")
+ gradkz
);
psiEqn.relax();
psiEqn.solve();
// Update of the varying transport properties.
thtil = 0.5*
(
(1 + sign(psi)) + (1 - sign(psi))*
pow((1+pow(mag(alpha*psi),n)),-(1-(1/n)))
);
Krel = 0.5*
(
(1 + sign(psi))*K + (1 - sign(psi))*K*pow(thtil, 0.5)*
pow((1 - pow((1 - pow(thtil, (n/(n - 1)))),(1 - (1/n)))), 2)
);
Crel= S + 0.5*
(
(1 - sign(psi))*
(
(thetas - thetar)*(thtil - thtil_tmp)*
(
1./((usf*pos(psi - psi_tmp)*pos(psi_tmp - psi))
+ psi - psi_tmp)
)
)
);
// Update of the gravity term.
gradk = fvc::grad(Krel);
gradkz = gradk.component(2);
// Computation of the field of residuals for the exit test of
// the Picard loop.
err = psi - psim1;
// Computation of the residual for the exit test of the Picard
// loop. Note the use of gSum instead of sum.
crit = gSumMag(err)/nbMesh;
// exit test for the Picard loop.
if (crit < precPicard)
{
Info << " Erreur = " << crit
<< " Picard = " << pic
<< nl << endl;
currentPicard=pic;
break;
}

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// Reading of the controling parameters of the Picard loop and of the
// Stabilisation cycles loop for the adaptive time step procedure.
// Localisation of the data within the considered case: system/fvSolution
const dictionary& picardDict = mesh.solutionDict().subDict("Picard");
// Maximum number of Picard iterations.
const int nIterPicard =
picardDict.lookupOrDefault<int>("nIterPicard", 1);
// Maximum number of stabilisation cycles.
const int nMaxCycle =
picardDict.lookupOrDefault<int>("nMaxCycle", 1);
// Number of time iterations with low number of Picard iteration beyond which
// the time step is increased.
const int stabilisationThreshold =
picardDict.lookupOrDefault<int>("stabilisationThreshold", 1);
// Exit criterion for the Picard loop.
const double precPicard =
picardDict.lookupOrDefault<double>("precPicard", 1.);
// Factor of increase/decrease of the time step.
const double tFact =
picardDict.lookupOrDefault<double>("tFact", 1.);

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/*---------------------------------------------------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | Copyright (C) 2004-2010 OpenCFD Ltd.
\\/ M anipulation |
-------------------------------------------------------------------------------
License
This file is part of OpenFOAM.
OpenFOAM 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.
OpenFOAM 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 OpenFOAM. If not, see <http://www.gnu.org/licenses/>.
Global
setDeltaT
Description
Reset the timestep to maintain a low number of Picard iteration and a good
convergence. Reduction of time-step is immediate, but increase is damped to
avoid unstable oscillations.
\*---------------------------------------------------------------------------*/
scalar deltaTFact = 1.;
if (adjustTimeStep)
{
deltaTFact = 1.;
// If There is a too high number of Picard iteration, decrease of the time
// step.
if (currentPicard > nIterPicard-2)
{
deltaTFact = 1./tFact;
}
if (currentPicard >= 3)
{
sc = 0;
}
if ((currentPicard < 3) && (sc < stabilisationThreshold))
{
sc = sc+1;
}
// If there is more than 'stabilisationThreshold' iteration that the number
// of Picard iteration is low, increase of the time step.
if ((currentPicard < 3) && (sc == stabilisationThreshold))
{
deltaTFact = tFact;
sc = 0;
}
// Reset of the time step if needed (time step is always lower than
// 'maxDeltaT').
if (deltaTFact != 1.)
{
runTime.setDeltaT
(
min
(
deltaTFact*runTime.deltaTValue(),
maxDeltaT
)
);
}
Info<< "deltaT = " << runTime.deltaTValue() << endl;
}
// ************************************************************************* //

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spatialMeanValueRichardsonFoam.C
EXE = $(FOAM_USER_APPBIN)/spatialMeanValueRichardsonFoam

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EXE_INC = \
-I$(LIB_SRC)/finiteVolume/lnInclude
EXE_LIBS = \
-lfiniteVolume

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/*---------------------------------------------------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | Copyright (C) 1991-2010 OpenCFD Ltd.
\\/ M anipulation |
-------------------------------------------------------------------------------
License
This file is part of OpenFOAM.
OpenFOAM 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.
OpenFOAM 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 OpenFOAM. If not, see <http://www.gnu.org/licenses/>.
Application
spatialMeanValue
Description
Calculates the spatial mean of the specified volScalarField over the
whole domain (for regular grid).
\*---------------------------------------------------------------------------*/
#include "fvCFD.H"
#include "cyclicPolyPatch.H"
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
// Main program:
int main(int argc, char *argv[])
{
# include "addRegionOption.H"
timeSelector::addOptions();
argList::validArgs.append("fieldName");
# include "setRootCase.H"
# include "createTime.H"
instantList timeDirs = timeSelector::select0(runTime, args);
# include "createNamedMesh.H"
word fieldName(args.additionalArgs()[0]);
Info << "Calculating avarage pressure heads:" << endl;
forAll(timeDirs, timeI)
{
runTime.setTime(timeDirs[timeI], timeI);
IOobject fieldHeader
(
fieldName,
runTime.timeName(),
mesh,
IOobject::MUST_READ
);
// Check field exists
if (fieldHeader.headerOk())
{
mesh.readUpdate();
// Read field and calc mean, for regular grid
if (fieldHeader.headerClassName() == volScalarField::typeName)
{
volScalarField field(fieldHeader, mesh);
int nbMesh;
nbMesh = 0;
forAll(field, cellI)
{
nbMesh++;
}
Info<< runTime.timeName()<< " "
<< sum(field).value()/nbMesh<< " "
<< endl;
}
else
{
FatalError
<< "Only possible for volScalarField "<< "s "
<< nl << exit(FatalError);
}
}
else
{
Info<< " No field " << fieldName << endl;
}
}
Info<< "End\n" << endl;
return 0;
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.7.x |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volVectorField;
location "0";
object U;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform (0 0 0);
boundaryField
{
top
{
type zeroGradient;
}
bottom
{
type zeroGradient;
}
sides
{
type empty;
}
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.7.x |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object err;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 0 0 0 0 0];
internalField uniform 1;
boundaryField
{
top
{
type zeroGradient;
}
bottom
{
type zeroGradient;
}
sides
{
type empty;
}
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.7.x |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object psi;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 0 0 0 0 0];
internalField uniform -1;
boundaryField
{
top
{
type fixedValue;
value uniform 0.01;
}
bottom
{
type fixedGradient;
gradient uniform 0;
}
sides
{
type empty;
}
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.7.x |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object theta;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 0;
boundaryField
{
top
{
type zeroGradient;
}
bottom
{
type zeroGradient;
}
sides
{
type empty;
}
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.7.x |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object usf;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 0 0 0 0 0];
internalField uniform 1.;
boundaryField
{
top
{
type zeroGradient;
}
bottom
{
type zeroGradient;
}
sides
{
type empty;
}
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.7.x |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volVectorField;
location "0";
object vuz;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform (0 0 1);
boundaryField
{
top
{
type zeroGradient;
}
bottom
{
type zeroGradient;
}
sides
{
type empty;
}
}
// ************************************************************************* //

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#!/bin/sh
# Source tutorial clean functions
. $WM_PROJECT_DIR/bin/tools/CleanFunctions
cleanCase

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#!/bin/sh
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
runApplication blockMesh
runApplication RichardsFoam
runApplication spatialMeanValueRichardsonFoam psi

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.7.1 |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object blockMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
convertToMeters 1;
vertices
(
(0 0 0)
(1 0 0)
(1 1 0)
(0 1 0)
(0 0 1)
(1 0 1)
(1 1 1)
(0 1 1)
);
blocks
(
hex (0 1 2 3 4 5 6 7) (1 1 100) simpleGrading (1 1 1)
);
edges
(
);
patches
(
patch top
(
(4 5 6 7)
)
patch bottom
(
(0 1 2 3)
)
empty sides
(
(1 2 6 5)
(3 2 6 7)
(0 3 7 4)
(0 1 5 4)
)
);
mergePatchPairs
(
);
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | foam-extend: Open Source CFD |
| \\ / O peration | Version: 4.0 |
| \\ / A nd | Web: http://www.foam-extend.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class polyBoundaryMesh;
location "constant/polyMesh";
object boundary;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
3
(
top
{
type patch;
nFaces 1;
startFace 99;
}
bottom
{
type patch;
nFaces 1;
startFace 100;
}
sides
{
type empty;
nFaces 400;
startFace 101;
}
)
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.7.1 |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object transportProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
K K [ 0 1 -1 0 0 0 0 ] 0.00000288889;
alpha alpha [ 0 -1 0 0 0 0 0 ] 3.6;
n n [ 0 0 0 0 0 0 0 ] 1.56;
thetas thetas [ 0 0 0 0 0 0 0 ] 0.43;
thetar thetar [ 0 0 0 0 0 0 0 ] 0.078;
S S [ 0 -1 0 0 0 0 0 ] 0.00001;
C C [ 0 -1 0 0 0 0 0 ] 1;
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.7.1 |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
application porousUnsaturatedFoam;
startFrom startTime;
startTime 0;
stopAt endTime;
endTime 86400;
deltaT 300;
writeControl adjustableRunTime;
writeInterval 7200;
purgeWrite 0;
writeFormat ascii;
writePrecision 6;
writeCompression uncompressed;
timeFormat general;
timePrecision 6;
runTimeModifiable yes;
adjustTimeStep yes;
maxDeltaT 3600;
functions
(
probes1
{
type probes; // Type of functionObject
// Where to load it from (if not already in solver)
functionObjectLibs ("libsampling.so");
probeLocations // Locations to be probed. runTime modifiable!
(
(0.5 0.5 1.)
);
// Fields to be probed. runTime modifiable!
fields
(
U
);
outputControl timeStep;
outputInterval 1;
}
);
//libs ( "libOpenFOAM.so" );
//libs ("libuserBCs.so");
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.7.1 |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
ddtSchemes
{
default backward;
}
gradSchemes
{
default Gauss linear;
}
divSchemes
{
default none;
}
laplacianSchemes
{
default none;
laplacian(Krel,psi) Gauss linear corrected;
}
interpolationSchemes
{
default Gauss vanLeer;
}
snGradSchemes
{
default Gauss vanLeer;
}
fluxRequired
{
default yes;
U;
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.7.1 |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
psi
{
solver PCG;
preconditioner DIC;
tolerance 1e-6;
relTol 0;
}
}
Picard
{
nIterPicard 10; //must be strictly higher than 5 ; 10 should be the best value//
nMaxCycle 10;
stabilisationThreshold 10;
precPicard 1e-4;
tFact 1.3; //1 means fixed time step ; should be lower than 1.5//
}
relaxationFactor
{
// psi 0.3;
};
// ************************************************************************* //