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8 Commits

Author SHA1 Message Date
95fe43b079 TUT: Add and update overset tutorials 2021-08-23 19:31:22 -07:00
10b7479dca COMP: Compilation of src with Allwmake 2021-08-23 19:30:43 -07:00
054e3ebc8b ENH: Update overset solvers 2021-08-23 19:29:54 -07:00
3dc63dc67c ENH: Updating tutorials 2021-08-23 12:06:18 -07:00
141b8376f3 ENh: Updating overset solvers
1) Deleting ddtCorr option
2) Deleting fluxInterpolation flux option
3) Reducing control readers files
2021-08-23 12:05:36 -07:00
72b9a002a2 ENH: adding cellTypes for use in overset to cellSetOption 2021-08-23 12:05:35 -07:00
808565a673 ENH: Delete unused ot updated files 2021-08-23 12:03:33 -07:00
5da36a3386 ENH: overset lib modifications
1) Creating static/dynamic oversetFvMesh
2) Adding helper functions for overset solvers in include
3) Changes to allow overlapping patches from the inset mesh on the
   background mesh for cellVolumeWeightCell, trackingInverseDistanc
   and inverseDistance stencils.
2021-08-23 12:03:33 -07:00
13339 changed files with 132826 additions and 250462 deletions

View File

@ -49,7 +49,7 @@
<!--
Providing details of your set-up can help us identify any issues, e.g.
OpenFOAM version : v2206|v2112|v2106|v2012|v2006 etc
OpenFOAM version : v1806|v1812|v1906 etc
Operating system : ubuntu|openSUSE|centos etc
Hardware info : any info that may help?
Compiler : gcc|intel|clang etc

View File

@ -8,7 +8,7 @@ wmake -check-dir "$WM_PROJECT_DIR" 2>/dev/null || {
}
if [ -f "$WM_PROJECT_DIR"/wmake/scripts/AllwmakeParseArguments ]
then . "$WM_PROJECT_DIR"/wmake/scripts/AllwmakeParseArguments || \
echo "Argument parse error"
echo "Argument parse error";
else
echo "Error (${0##*/}) : WM_PROJECT_DIR appears to be incorrect"
echo " Check your OpenFOAM environment and installation"
@ -23,23 +23,23 @@ else
echo "mpirun=$(command -v mpirun || true)"
fi
echo
# Report compiler information. First non-blank line from --version output
# Report compiler information
compiler="$(wmake -show-path-cxx 2>/dev/null || true)"
if [ -x "$compiler" ]
then
echo "compiler=$compiler"
"$compiler" --version 2>/dev/null | sed -e '/^$/d;q'
"$compiler" --version 2>/dev/null | sed -ne '1p'
else
echo "compiler=unknown"
fi
echo
echo ========================================
echo "========================================"
date "+%Y-%m-%d %H:%M:%S %z" 2>/dev/null || echo "date is unknown"
echo "Starting compile ${WM_PROJECT_DIR##*/} ${0##*/}"
echo " $WM_COMPILER ${WM_COMPILER_TYPE:-system} compiler [${WM_COMPILE_CONTROL}]"
echo " $WM_COMPILER ${WM_COMPILER_TYPE:-system} compiler"
echo " ${WM_OPTIONS}, with ${WM_MPLIB} ${FOAM_MPI}"
echo ========================================
echo "========================================"
echo
# Compile tools for wmake
@ -62,24 +62,26 @@ else
echo "Skip ThirdParty (no directory)"
fi
# OpenFOAM libraries
echo "========================================"
echo "Compile OpenFOAM libraries"
echo
src/Allwmake $targetType $*
# OpenFOAM applications
echo "========================================"
echo "Compile OpenFOAM applications"
echo
applications/Allwmake $targetType $*
# Additional components/modules
case "$FOAM_MODULE_PREFIX" in
(false | none)
echo ========================================
if [ "$FOAM_MODULE_PREFIX" = false ] || [ "$FOAM_MODULE_PREFIX" = none ]
then
echo "========================================"
echo "OpenFOAM modules disabled (prefix=${FOAM_MODULE_PREFIX})"
echo
;;
(*)
# Use wmake -all instead of Allwmake to allow for overrides
( cd "$WM_PROJECT_DIR/modules" 2>/dev/null && wmake -all )
esac
elif [ -d "$WM_PROJECT_DIR/modules" ]
then
(cd "$WM_PROJECT_DIR/modules" 2>/dev/null && wmake -all)
fi
# Count files in given directory. Ignore "Test-*" binaries.
_foamCountDirEntries()
@ -91,7 +93,7 @@ _foamCountDirEntries()
# Some summary information
echo
date "+%Y-%m-%d %H:%M:%S %z" 2>/dev/null || echo "date is unknown"
echo ========================================
echo "========================================"
echo " ${WM_PROJECT_DIR##*/}"
echo " $WM_COMPILER ${WM_COMPILER_TYPE:-system} compiler"
echo " ${WM_OPTIONS}, with ${WM_MPLIB} ${FOAM_MPI}"
@ -101,6 +103,6 @@ echo " patch = $(etc/openfoam -show-patch 2>/dev/null)"
echo " bin = $(_foamCountDirEntries "$FOAM_APPBIN") entries"
echo " lib = $(_foamCountDirEntries "$FOAM_LIBBIN") entries"
echo
echo ========================================
echo "========================================"
#------------------------------------------------------------------------------

View File

@ -1,2 +1,2 @@
api=2206
api=2107
patch=0

View File

@ -40,9 +40,9 @@ Violations of the Trademark are monitored, and will be duly prosecuted.
If OpenFOAM has already been compiled on your system, simply source
the appropriate `etc/bashrc` or `etc/cshrc` file and get started.
For example, for the OpenFOAM-v2206 version:
For example, for the OpenFOAM-v2106 version:
```
source /installation/path/OpenFOAM-v2206/etc/bashrc
source /installation/path/OpenFOAM-v2106/etc/bashrc
```
## Compiling OpenFOAM
@ -127,8 +127,8 @@ These 3rd-party sources are normally located in a directory parallel
to the OpenFOAM directory. For example,
```
/path/parent
|-- OpenFOAM-v2206
\-- ThirdParty-v2206
|-- OpenFOAM-v2106
\-- ThirdParty-v2106
```
There are, however, many cases where this simple convention is inadequate:
@ -136,7 +136,7 @@ There are, however, many cases where this simple convention is inadequate:
operating system or cluster installation provides it)
* When we have changed the OpenFOAM directory name to some arbitrary
directory name, e.g. openfoam-sandbox2206, etc..
directory name, e.g. openfoam-sandbox2106, etc..
* When we would like any additional 3rd party software to be located
inside of the OpenFOAM directory to ensure that the installation is
@ -156,9 +156,9 @@ when locating the ThirdParty directory with the following precedence:
2. PREFIX/ThirdParty-VERSION
* this corresponds to the traditional approach
3. PREFIX/ThirdParty-vAPI
* allows for an updated value of VERSION, *eg*, `v2206-myCustom`,
* allows for an updated value of VERSION, *eg*, `v2106-myCustom`,
without requiring a renamed ThirdParty. The API value would still
be `2206` and the original `ThirdParty-v2206/` would be found.
be `2106` and the original `ThirdParty-v2106/` would be found.
4. PREFIX/ThirdParty-API
* same as the previous example, but using an unadorned API value.
5. PREFIX/ThirdParty-common
@ -213,4 +213,4 @@ ThirdParty directory will contain either an `Allwmake` file or a
- [Governance](http://www.openfoam.com/governance/), [Governance Projects](https://www.openfoam.com/governance/projects)
- [Contacting OpenCFD](http://www.openfoam.com/contact/)
Copyright 2016-2022 OpenCFD Ltd
Copyright 2016-2021 OpenCFD Ltd

View File

@ -8,29 +8,19 @@ wmake -check-dir "$WM_PROJECT_DIR/applications" 2>/dev/null || {
}
if [ -f "$WM_PROJECT_DIR"/wmake/scripts/AllwmakeParseArguments ]
then . "$WM_PROJECT_DIR"/wmake/scripts/AllwmakeParseArguments || \
echo "Argument parse error"
echo "Argument parse error";
else
echo "Error (${0##*/}) : WM_PROJECT_DIR appears to be incorrect"
echo " Check your OpenFOAM environment and installation"
exit 1
fi
echo ========================================
echo Compile OpenFOAM applications
echo ========================================
#------------------------------------------------------------------------------
wmake -all $targetType utilities
wmake -all $targetType solvers
wmake -all $targetType utilities
# Extra tools (optional)
# Optional
## wmake -all $targetType tools
#------------------------------------------------------------------------------
echo ========================================
echo Done OpenFOAM applications
echo ========================================
#------------------------------------------------------------------------------

View File

@ -149,7 +149,7 @@ int main(int argc, char *argv[])
mesh.update();
surfaceScalarField faceMask(localMin<scalar>(mesh).interpolate(cellMask));
//surfaceScalarField faceMask(localMin<scalar>(mesh).interpolate(cellMask));
// Since solver contains no time loop it would never execute
// function objects so do it ourselves

View File

@ -25,7 +25,6 @@ EXE_LIBS = \
-lengine \
-lturbulenceModels \
-lcompressibleTurbulenceModels \
-lthermoTools \
-lcompressibleTransportModels \
-lfluidThermophysicalModels \
-lreactionThermophysicalModels \

View File

@ -6,7 +6,7 @@
\\/ M anipulation |
-------------------------------------------------------------------------------
Copyright (C) 2011-2015 OpenFOAM Foundation
Copyright (C) 2019-2021 OpenCFD Ltd.
Copyright (C) 2019 OpenCFD Ltd.
-------------------------------------------------------------------------------
License
This file is part of OpenFOAM.
@ -43,9 +43,9 @@ Foam::autoPtr<Foam::PDRDragModel> Foam::PDRDragModel::New
Info<< "Selecting drag model " << modelType << endl;
auto* ctorPtr = dictionaryConstructorTable(modelType);
auto cstrIter = dictionaryConstructorTablePtr_->cfind(modelType);
if (!ctorPtr)
if (!cstrIter.found())
{
FatalIOErrorInLookup
(
@ -57,9 +57,7 @@ Foam::autoPtr<Foam::PDRDragModel> Foam::PDRDragModel::New
}
return autoPtr<PDRDragModel>
(
ctorPtr(dict, turbulence, rho, U, phi)
);
(cstrIter()(dict, turbulence, rho, U, phi));
}

View File

@ -6,7 +6,7 @@
\\/ M anipulation |
-------------------------------------------------------------------------------
Copyright (C) 2011-2015 OpenFOAM Foundation
Copyright (C) 2019-2021 OpenCFD Ltd.
Copyright (C) 2019 OpenCFD Ltd.
-------------------------------------------------------------------------------
License
This file is part of OpenFOAM.
@ -42,9 +42,9 @@ Foam::autoPtr<Foam::XiEqModel> Foam::XiEqModel::New
Info<< "Selecting flame-wrinkling model " << modelType << endl;
auto* ctorPtr = dictionaryConstructorTable(modelType);
auto cstrIter = dictionaryConstructorTablePtr_->cfind(modelType);
if (!ctorPtr)
if (!cstrIter.found())
{
FatalIOErrorInLookup
(
@ -55,7 +55,7 @@ Foam::autoPtr<Foam::XiEqModel> Foam::XiEqModel::New
) << exit(FatalIOError);
}
return autoPtr<XiEqModel>(ctorPtr(dict, thermo, turbulence, Su));
return autoPtr<XiEqModel>(cstrIter()(dict, thermo, turbulence, Su));
}

View File

@ -6,7 +6,7 @@
\\/ M anipulation |
-------------------------------------------------------------------------------
Copyright (C) 2011-2015 OpenFOAM Foundation
Copyright (C) 2019-2021 OpenCFD Ltd.
Copyright (C) 2019 OpenCFD Ltd.
-------------------------------------------------------------------------------
License
This file is part of OpenFOAM.
@ -42,9 +42,9 @@ Foam::autoPtr<Foam::XiGModel> Foam::XiGModel::New
Info<< "Selecting flame-wrinkling model " << modelType << endl;
auto* ctorPtr = dictionaryConstructorTable(modelType);
auto cstrIter = dictionaryConstructorTablePtr_->cfind(modelType);
if (!ctorPtr)
if (!cstrIter.found())
{
FatalIOErrorInLookup
(
@ -55,7 +55,7 @@ Foam::autoPtr<Foam::XiGModel> Foam::XiGModel::New
) << exit(FatalIOError);
}
return autoPtr<XiGModel>(ctorPtr(dict, thermo, turbulence, Su));
return autoPtr<XiGModel>(cstrIter()(dict, thermo, turbulence, Su));
}

View File

@ -6,7 +6,7 @@
\\/ M anipulation |
-------------------------------------------------------------------------------
Copyright (C) 2011-2015 OpenFOAM Foundation
Copyright (C) 2019-2021 OpenCFD Ltd.
Copyright (C) 2019 OpenCFD Ltd.
-------------------------------------------------------------------------------
License
This file is part of OpenFOAM.
@ -45,9 +45,9 @@ Foam::autoPtr<Foam::XiModel> Foam::XiModel::New
Info<< "Selecting flame-wrinkling model " << modelType << endl;
auto* ctorPtr = dictionaryConstructorTable(modelType);
auto cstrIter = dictionaryConstructorTablePtr_->cfind(modelType);
if (!ctorPtr)
if (!cstrIter.found())
{
FatalIOErrorInLookup
(
@ -59,9 +59,7 @@ Foam::autoPtr<Foam::XiModel> Foam::XiModel::New
}
return autoPtr<XiModel>
(
ctorPtr(dict, thermo, turbulence, Su, rho, b, phi)
);
(cstrIter()(dict, thermo, turbulence, Su, rho, b, phi));
}

View File

@ -19,7 +19,6 @@ EXE_LIBS = \
-lengine \
-lturbulenceModels \
-lcompressibleTurbulenceModels \
-lthermoTools \
-lcompressibleTransportModels \
-lfluidThermophysicalModels \
-lreactionThermophysicalModels \

View File

@ -26,7 +26,6 @@ EXE_LIBS = \
-lengine \
-lturbulenceModels \
-lcompressibleTurbulenceModels \
-lthermoTools \
-lcompressibleTransportModels \
-lfluidThermophysicalModels \
-lreactionThermophysicalModels \

View File

@ -20,7 +20,6 @@ EXE_LIBS = \
-lengine \
-lturbulenceModels \
-lcompressibleTurbulenceModels \
-lthermoTools \
-lcompressibleTransportModels \
-lfluidThermophysicalModels \
-lreactionThermophysicalModels \

View File

@ -20,7 +20,6 @@ EXE_LIBS = \
-lengine \
-lturbulenceModels \
-lcompressibleTurbulenceModels \
-lthermoTools \
-lcompressibleTransportModels \
-lfluidThermophysicalModels \
-lspecie

View File

@ -34,7 +34,6 @@ EXE_LIBS = \
-lsampling \
-lturbulenceModels \
-lcompressibleTurbulenceModels \
-lthermoTools \
-lspecie \
-lcompressibleTransportModels \
-lfluidThermophysicalModels \

View File

@ -1,4 +1,4 @@
const volScalarField& psi = thermo.psi();
const volScalarField& T = thermo.T();
regionModels::surfaceFilmModel& surfaceFilm = tsurfaceFilm();
const label inertIndex(composition.species().find(inertSpecie));
const label inertIndex(composition.species()[inertSpecie]);

View File

@ -19,7 +19,6 @@ EXE_LIBS = \
-lsampling \
-lturbulenceModels \
-lcompressibleTurbulenceModels \
-lthermoTools \
-lreactionThermophysicalModels \
-lspecie \
-lcompressibleTransportModels \

View File

@ -1,3 +1,3 @@
const volScalarField& psi = thermo.psi();
const volScalarField& T = thermo.T();
const label inertIndex(composition.species().find(inertSpecie));
const label inertIndex(composition.species()[inertSpecie]);

View File

@ -20,7 +20,6 @@ EXE_LIBS = \
-lsampling \
-lturbulenceModels \
-lcompressibleTurbulenceModels \
-lthermoTools \
-lreactionThermophysicalModels \
-lspecie \
-lcompressibleTransportModels \

View File

@ -1,3 +1,3 @@
const volScalarField& psi = thermo.psi();
const volScalarField& T = thermo.T();
const label inertIndex(composition.species().find(inertSpecie));
const label inertIndex(composition.species()[inertSpecie]);

View File

@ -20,7 +20,6 @@ EXE_LIBS = \
-lsampling \
-lturbulenceModels \
-lcompressibleTurbulenceModels \
-lthermoTools \
-lreactionThermophysicalModels \
-lspecie \
-lcompressibleTransportModels \

View File

@ -1,3 +1,3 @@
const volScalarField& psi = thermo.psi();
const volScalarField& T = thermo.T();
const label inertIndex(composition.species().find(inertSpecie));
const label inertIndex(composition.species()[inertSpecie]);

View File

@ -4,5 +4,6 @@ cd "${0%/*}" || exit # Run from this directory
wclean libso BCs
wclean
wclean rhoCentralDyMFoam
#------------------------------------------------------------------------------

View File

@ -5,7 +5,8 @@ cd "${0%/*}" || exit # Run from this directory
(
wmake $targetType BCs \
&& wmake $targetType
&& wmake $targetType \
&& wmake $targetType rhoCentralDyMFoam \
)
#------------------------------------------------------------------------------

View File

@ -7,7 +7,7 @@ EXE_INC = \
-I$(LIB_SRC)/thermophysicalModels/specie/lnInclude \
-I$(LIB_SRC)/TurbulenceModels/turbulenceModels/lnInclude \
-I$(LIB_SRC)/TurbulenceModels/compressible/lnInclude \
-I$(LIB_SRC)/dynamicFvMesh/lnInclude
-I$(LIB_SRC)/dynamicMesh/lnInclude
EXE_LIBS = \
-lfiniteVolume \
@ -18,7 +18,4 @@ EXE_LIBS = \
-lspecie \
-lrhoCentralFoam \
-lturbulenceModels \
-lcompressibleTurbulenceModels \
-lthermoTools \
-ldynamicFvMesh \
-ltopoChangerFvMesh
-lcompressibleTurbulenceModels

View File

@ -0,0 +1,3 @@
rhoCentralDyMFoam.C
EXE = $(FOAM_APPBIN)/rhoCentralDyMFoam

View File

@ -0,0 +1,26 @@
EXE_INC = \
-I.. \
-I../BCs/lnInclude \
-I$(LIB_SRC)/finiteVolume/lnInclude \
-I$(LIB_SRC)/meshTools/lnInclude \
-I$(LIB_SRC)/transportModels/compressible/lnInclude \
-I$(LIB_SRC)/thermophysicalModels/basic/lnInclude \
-I$(LIB_SRC)/thermophysicalModels/specie/lnInclude \
-I$(LIB_SRC)/TurbulenceModels/turbulenceModels/lnInclude \
-I$(LIB_SRC)/TurbulenceModels/compressible/lnInclude \
-I$(LIB_SRC)/dynamicMesh/lnInclude \
-I$(LIB_SRC)/dynamicFvMesh/lnInclude
EXE_LIBS = \
-lfiniteVolume \
-lfvOptions \
-lmeshTools \
-lcompressibleTransportModels \
-lfluidThermophysicalModels \
-lspecie \
-lrhoCentralFoam \
-lturbulenceModels \
-lcompressibleTurbulenceModels \
-ldynamicMesh \
-ldynamicFvMesh \
-ltopoChangerFvMesh

View File

@ -0,0 +1,288 @@
/*---------------------------------------------------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | www.openfoam.com
\\/ M anipulation |
-------------------------------------------------------------------------------
Copyright (C) 2011-2016 OpenFOAM Foundation
-------------------------------------------------------------------------------
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
rhoCentralDyMFoam
Group
grpCompressibleSolvers grpMovingMeshSolvers
Description
Density-based compressible flow solver based on central-upwind
schemes of Kurganov and Tadmor
with support for mesh-motion and topology changes.
\*---------------------------------------------------------------------------*/
#include "fvCFD.H"
#include "dynamicFvMesh.H"
#include "psiThermo.H"
#include "turbulentFluidThermoModel.H"
#include "fixedRhoFvPatchScalarField.H"
#include "directionInterpolate.H"
#include "localEulerDdtScheme.H"
#include "fvcSmooth.H"
#include "motionSolver.H"
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
int main(int argc, char *argv[])
{
argList::addNote
(
"Density-based compressible flow solver based on central-upwind"
" schemes of Kurganov and Tadmor.\n"
"With support for mesh-motion and topology changes."
);
#define NO_CONTROL
#include "postProcess.H"
#include "setRootCaseLists.H"
#include "createTime.H"
#include "createDynamicFvMesh.H"
#include "createFields.H"
#include "createFieldRefs.H"
#include "createTimeControls.H"
turbulence->validate();
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
#include "readFluxScheme.H"
const dimensionedScalar v_zero(dimVolume/dimTime, Zero);
// Courant numbers used to adjust the time-step
scalar CoNum = 0.0;
scalar meanCoNum = 0.0;
Info<< "\nStarting time loop\n" << endl;
while (runTime.run())
{
#include "readTimeControls.H"
#include "setDeltaT.H"
++runTime;
Info<< "Time = " << runTime.timeName() << nl << endl;
// Do any mesh changes
mesh.update();
// --- Directed interpolation of primitive fields onto faces
surfaceScalarField rho_pos(interpolate(rho, pos));
surfaceScalarField rho_neg(interpolate(rho, neg));
surfaceVectorField rhoU_pos(interpolate(rhoU, pos, U.name()));
surfaceVectorField rhoU_neg(interpolate(rhoU, neg, U.name()));
volScalarField rPsi("rPsi", 1.0/psi);
surfaceScalarField rPsi_pos(interpolate(rPsi, pos, T.name()));
surfaceScalarField rPsi_neg(interpolate(rPsi, neg, T.name()));
surfaceScalarField e_pos(interpolate(e, pos, T.name()));
surfaceScalarField e_neg(interpolate(e, neg, T.name()));
surfaceVectorField U_pos("U_pos", rhoU_pos/rho_pos);
surfaceVectorField U_neg("U_neg", rhoU_neg/rho_neg);
surfaceScalarField p_pos("p_pos", rho_pos*rPsi_pos);
surfaceScalarField p_neg("p_neg", rho_neg*rPsi_neg);
surfaceScalarField phiv_pos("phiv_pos", U_pos & mesh.Sf());
surfaceScalarField phiv_neg("phiv_neg", U_neg & mesh.Sf());
// Make fluxes relative to mesh-motion
if (mesh.moving())
{
phiv_pos -= mesh.phi();
phiv_neg -= mesh.phi();
}
// Note: extracted out the orientation so becomes unoriented
phiv_pos.setOriented(false);
phiv_neg.setOriented(false);
volScalarField c("c", sqrt(thermo.Cp()/thermo.Cv()*rPsi));
surfaceScalarField cSf_pos
(
"cSf_pos",
interpolate(c, pos, T.name())*mesh.magSf()
);
surfaceScalarField cSf_neg
(
"cSf_neg",
interpolate(c, neg, T.name())*mesh.magSf()
);
surfaceScalarField ap
(
"ap",
max(max(phiv_pos + cSf_pos, phiv_neg + cSf_neg), v_zero)
);
surfaceScalarField am
(
"am",
min(min(phiv_pos - cSf_pos, phiv_neg - cSf_neg), v_zero)
);
surfaceScalarField a_pos("a_pos", ap/(ap - am));
surfaceScalarField amaxSf("amaxSf", max(mag(am), mag(ap)));
surfaceScalarField aSf("aSf", am*a_pos);
if (fluxScheme == "Tadmor")
{
aSf = -0.5*amaxSf;
a_pos = 0.5;
}
surfaceScalarField a_neg("a_neg", 1.0 - a_pos);
phiv_pos *= a_pos;
phiv_neg *= a_neg;
surfaceScalarField aphiv_pos("aphiv_pos", phiv_pos - aSf);
surfaceScalarField aphiv_neg("aphiv_neg", phiv_neg + aSf);
// Reuse amaxSf for the maximum positive and negative fluxes
// estimated by the central scheme
amaxSf = max(mag(aphiv_pos), mag(aphiv_neg));
#include "centralCourantNo.H"
phi = aphiv_pos*rho_pos + aphiv_neg*rho_neg;
surfaceVectorField phiU(aphiv_pos*rhoU_pos + aphiv_neg*rhoU_neg);
// Note: reassembled orientation from the pos and neg parts so becomes
// oriented
phiU.setOriented(true);
surfaceVectorField phiUp(phiU + (a_pos*p_pos + a_neg*p_neg)*mesh.Sf());
surfaceScalarField phiEp
(
"phiEp",
aphiv_pos*(rho_pos*(e_pos + 0.5*magSqr(U_pos)) + p_pos)
+ aphiv_neg*(rho_neg*(e_neg + 0.5*magSqr(U_neg)) + p_neg)
+ aSf*p_pos - aSf*p_neg
);
// Make flux for pressure-work absolute
if (mesh.moving())
{
surfaceScalarField phia(a_pos*p_pos + a_neg*p_neg);
phia.setOriented(true);
phiEp += mesh.phi()*phia;
}
volScalarField muEff("muEff", turbulence->muEff());
volTensorField tauMC("tauMC", muEff*dev2(Foam::T(fvc::grad(U))));
// --- Solve density
solve(fvm::ddt(rho) + fvc::div(phi));
// --- Solve momentum
solve(fvm::ddt(rhoU) + fvc::div(phiUp));
U.ref() =
rhoU()
/rho();
U.correctBoundaryConditions();
rhoU.boundaryFieldRef() == rho.boundaryField()*U.boundaryField();
if (!inviscid)
{
solve
(
fvm::ddt(rho, U) - fvc::ddt(rho, U)
- fvm::laplacian(muEff, U)
- fvc::div(tauMC)
);
rhoU = rho*U;
}
// --- Solve energy
surfaceScalarField sigmaDotU
(
"sigmaDotU",
(
fvc::interpolate(muEff)*mesh.magSf()*fvc::snGrad(U)
+ fvc::dotInterpolate(mesh.Sf(), tauMC)
)
& (a_pos*U_pos + a_neg*U_neg)
);
solve
(
fvm::ddt(rhoE)
+ fvc::div(phiEp)
- fvc::div(sigmaDotU)
);
e = rhoE/rho - 0.5*magSqr(U);
e.correctBoundaryConditions();
thermo.correct();
rhoE.boundaryFieldRef() ==
rho.boundaryField()*
(
e.boundaryField() + 0.5*magSqr(U.boundaryField())
);
if (!inviscid)
{
solve
(
fvm::ddt(rho, e) - fvc::ddt(rho, e)
- fvm::laplacian(turbulence->alphaEff(), e)
);
thermo.correct();
rhoE = rho*(e + 0.5*magSqr(U));
}
p.ref() =
rho()
/psi();
p.correctBoundaryConditions();
rho.boundaryFieldRef() == psi.boundaryField()*p.boundaryField();
turbulence->correct();
runTime.write();
runTime.printExecutionTime(Info);
}
Info<< "End\n" << endl;
return 0;
}
// ************************************************************************* //

View File

@ -6,7 +6,6 @@
\\/ M anipulation |
-------------------------------------------------------------------------------
Copyright (C) 2011-2016 OpenFOAM Foundation
Copyright (C) 2021 OpenCFD Ltd.
-------------------------------------------------------------------------------
License
This file is part of OpenFOAM.
@ -31,14 +30,12 @@ Group
grpCompressibleSolvers
Description
Density-based compressible flow solver based on
central-upwind schemes of Kurganov and Tadmor with
support for mesh-motion and topology changes.
Density-based compressible flow solver based on central-upwind
schemes of Kurganov and Tadmor.
\*---------------------------------------------------------------------------*/
#include "fvCFD.H"
#include "dynamicFvMesh.H"
#include "psiThermo.H"
#include "turbulentFluidThermoModel.H"
#include "fixedRhoFvPatchScalarField.H"
@ -52,9 +49,8 @@ int main(int argc, char *argv[])
{
argList::addNote
(
"Density-based compressible flow solver based on"
" central-upwind schemes of Kurganov and Tadmor with"
" support for mesh-motion and topology changes."
"Density-based compressible flow solver based on central-upwind"
" schemes of Kurganov and Tadmor."
);
#define NO_CONTROL
@ -63,7 +59,7 @@ int main(int argc, char *argv[])
#include "addCheckCaseOptions.H"
#include "setRootCaseLists.H"
#include "createTime.H"
#include "createDynamicFvMesh.H"
#include "createMesh.H"
#include "createFields.H"
#include "createFieldRefs.H"
#include "createTimeControls.H"
@ -84,18 +80,6 @@ int main(int argc, char *argv[])
while (runTime.run())
{
#include "readTimeControls.H"
if (!LTS)
{
#include "setDeltaT.H"
++runTime;
// Do any mesh changes
mesh.update();
}
// --- Directed interpolation of primitive fields onto faces
surfaceScalarField rho_pos(interpolate(rho, pos));
@ -123,15 +107,6 @@ int main(int argc, char *argv[])
surfaceScalarField phiv_neg("phiv_neg", U_neg & mesh.Sf());
phiv_neg.setOriented(false);
// Make fluxes relative to mesh-motion
if (mesh.moving())
{
surfaceScalarField meshPhi(mesh.phi());
meshPhi.setOriented(false);
phiv_pos -= meshPhi;
phiv_neg -= meshPhi;
}
volScalarField c("c", sqrt(thermo.Cp()/thermo.Cv()*rPsi));
surfaceScalarField cSf_pos
(
@ -182,13 +157,18 @@ int main(int argc, char *argv[])
amaxSf = max(mag(aphiv_pos), mag(aphiv_neg));
#include "centralCourantNo.H"
#include "readTimeControls.H"
if (LTS)
{
#include "setRDeltaT.H"
++runTime;
}
else
{
#include "setDeltaT.H"
}
++runTime;
Info<< "Time = " << runTime.timeName() << nl << endl;
@ -209,14 +189,6 @@ int main(int argc, char *argv[])
+ aSf*p_pos - aSf*p_neg
);
// Make flux for pressure-work absolute
if (mesh.moving())
{
surfaceScalarField meshPhi(mesh.phi());
meshPhi.setOriented(false);
phiEp += meshPhi*(a_pos*p_pos + a_neg*p_neg);
}
volScalarField muEff("muEff", turbulence->muEff());
volTensorField tauMC("tauMC", muEff*dev2(Foam::T(fvc::grad(U))));

View File

@ -6,7 +6,7 @@ EXE_INC = \
-I$(LIB_SRC)/transportModels/compressible/lnInclude \
-I$(LIB_SRC)/thermophysicalModels/basic/lnInclude \
-I$(LIB_SRC)/TurbulenceModels/turbulenceModels/lnInclude \
-I$(LIB_SRC)/TurbulenceModels/compressible/lnInclude
-I$(LIB_SRC)/TurbulenceModels/compressible/lnInclude \
EXE_LIBS = \
-lfiniteVolume \
@ -17,5 +17,4 @@ EXE_LIBS = \
-lfluidThermophysicalModels \
-lspecie \
-lturbulenceModels \
-lcompressibleTurbulenceModels \
-lthermoTools
-lcompressibleTurbulenceModels

View File

@ -20,7 +20,6 @@ EXE_LIBS = \
-lspecie \
-lturbulenceModels \
-lcompressibleTurbulenceModels \
-lthermoTools \
-ldynamicMesh \
-ldynamicFvMesh \
-ltopoChangerFvMesh \

View File

@ -21,7 +21,6 @@ EXE_LIBS = \
-lspecie \
-lturbulenceModels \
-lcompressibleTurbulenceModels \
-lthermoTools \
-ldynamicFvMesh \
-ltopoChangerFvMesh \
-loverset

View File

@ -1,4 +0,0 @@
bool ddtCorr
(
pimple.dict().getOrDefault("ddtCorr", true)
);

View File

@ -69,6 +69,8 @@ mesh.setFluxRequired(p.name());
// Mask field for zeroing out contributions on hole cells
#include "createCellMask.H"
// Create bool field with interpolated cells
#include "createInterpolatedCells.H"
Info<< "Creating turbulence model\n" << endl;
autoPtr<compressible::turbulenceModel> turbulence

View File

@ -43,7 +43,6 @@ Description
#include "dynamicFvMesh.H"
#include "fluidThermo.H"
#include "turbulentFluidThermoModel.H"
#include "bound.H"
#include "pimpleControl.H"
#include "pressureControl.H"
#include "CorrectPhi.H"
@ -89,10 +88,8 @@ int main(int argc, char *argv[])
while (runTime.run())
{
#include "readControls.H"
#include "readDyMControls.H"
// Store divrhoU from the previous mesh so that it can be mapped
// and used in correctPhi to ensure the corrected phi has the
// same divergence
@ -128,7 +125,6 @@ int main(int argc, char *argv[])
{
if (pimple.firstIter() || moveMeshOuterCorrectors)
{
// Do any mesh changes
mesh.update();
@ -137,52 +133,22 @@ int main(int argc, char *argv[])
MRF.update();
#include "setCellMask.H"
const surfaceScalarField faceMaskOld
(
localMin<scalar>(mesh).interpolate(cellMask.oldTime())
);
// Zero Uf on old faceMask (H-I)
rhoUf() *= faceMaskOld;
surfaceVectorField rhoUfint(fvc::interpolate(rho*U));
// Update Uf and phi on new C-I faces
rhoUf() += (1-faceMaskOld)*rhoUfint;
// Update Uf boundary
forAll(rhoUf().boundaryField(), patchI)
{
rhoUf().boundaryFieldRef()[patchI] =
rhoUfint.boundaryField()[patchI];
}
// Calculate absolute flux from the mapped surface velocity
phi = mesh.Sf() & rhoUf();
#include "setInterpolatedCells.H"
#include "correctRhoPhiFaceMask.H"
if (correctPhi)
{
// Corrects flux on separated regions
#include "correctPhi.H"
}
// Zero phi on current H-I
const surfaceScalarField faceMask
(
localMin<scalar>(mesh).interpolate(cellMask)
);
phi *= faceMask;
U *= cellMask;
// Make the fluxes relative to the mesh-motion
fvc::makeRelative(phi, rho, U);
}
if (checkMeshCourantNo)
{
#include "meshCourantNo.H"
if (checkMeshCourantNo)
{
#include "meshCourantNo.H"
}
}
}

View File

@ -25,17 +25,6 @@ surfaceScalarField phiHbyA
fvc::interpolate(rho)*fvc::flux(HbyA)
);
if (ddtCorr)
{
surfaceScalarField faceMaskOld
(
localMin<scalar>(mesh).interpolate(cellMask.oldTime())
);
phiHbyA +=
faceMaskOld*MRF.zeroFilter(rhorAUf*fvc::ddtCorr(rho, U, phi, rhoUf));
}
fvc::makeRelative(phiHbyA, rho, U);
MRF.makeRelative(fvc::interpolate(rho), phiHbyA);
@ -134,8 +123,4 @@ if (thermo.dpdt())
}
}
surfaceScalarField faceMask
(
localMin<scalar>(mesh).interpolate(cellMask)
);
phi *= faceMask;

View File

@ -1,9 +0,0 @@
#include "readTimeControls.H"
correctPhi = pimple.dict().getOrDefault("correctPhi", false);
checkMeshCourantNo =
pimple.dict().getOrDefault("checkMeshCourantNo", false);
ddtCorr = pimple.dict().getOrDefault("ddtCorr", true);

View File

@ -49,7 +49,7 @@
);
}
// Update the boundary values of the reciprocal time-step
// Update tho boundary values of the reciprocal time-step
rDeltaT.correctBoundaryConditions();
Info<< "Flow time scale min/max = "

View File

@ -19,6 +19,5 @@ EXE_LIBS = \
-lspecie \
-lturbulenceModels \
-lcompressibleTurbulenceModels \
-lthermoTools \
-latmosphericModels \
-lregionFaModels

View File

@ -21,7 +21,6 @@ EXE_LIBS = \
-lspecie \
-lturbulenceModels \
-lcompressibleTurbulenceModels \
-lthermoTools \
-ldynamicFvMesh \
-ltopoChangerFvMesh \
-lsampling \

View File

@ -1,52 +1,22 @@
/*---------------------------------------------------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | www.openfoam.com
\\/ M anipulation |
-------------------------------------------------------------------------------
Copyright (C) 2017 OpenCFD Ltd.
-------------------------------------------------------------------------------
License
This file is part of OpenFOAM, distributed under GPL-3.0-or-later.
Info<< "Create dynamic mesh for time = "
<< runTime.timeName() << nl << endl;
Description
Create a dynamicFvMesh, with init()
Required Variables
- runTime [Time]
Provided Variables
- mesh [dynamicFvMesh], meshPtr
\*---------------------------------------------------------------------------*/
Foam::autoPtr<Foam::dynamicFvMesh> meshPtr;
{
Foam::Info << "Create dynamic mesh for time = "
<< runTime.timeName() << Foam::nl;
meshPtr = dynamicFvMesh::New
autoPtr<dynamicFvMesh> meshPtr
(
IOobject
dynamicFvMesh::New
(
polyMesh::defaultRegion,
runTime.timeName(),
runTime,
IOobject::MUST_READ
IOobject
(
polyMesh::defaultRegion,
runTime.timeName(),
runTime,
IOobject::MUST_READ
)
)
);
}
dynamicFvMesh& mesh = meshPtr();
dynamicFvMesh& mesh = meshPtr();
// Calculate initial mesh-to-mesh mapping. Note that this should be
// done under the hood, e.g. as a MeshObject
mesh.update();
Foam::Info << Foam::endl;
// ************************************************************************* //
// Calculate initial mesh-to-mesh mapping. Note that this should be
// done under the hood, e.g. as a MeshObject
mesh.update();

View File

@ -18,5 +18,4 @@ EXE_LIBS = \
-lfluidThermophysicalModels \
-lspecie \
-lturbulenceModels \
-lcompressibleTurbulenceModels \
-lthermoTools
-lcompressibleTurbulenceModels

View File

@ -16,5 +16,4 @@ EXE_LIBS = \
-lfluidThermophysicalModels \
-lspecie \
-lturbulenceModels \
-lcompressibleTurbulenceModels \
-lthermoTools
-lcompressibleTurbulenceModels

View File

@ -21,7 +21,6 @@ EXE_LIBS = \
-lspecie \
-lturbulenceModels \
-lcompressibleTurbulenceModels \
-lthermoTools \
-ldynamicMesh \
-ldynamicFvMesh \
-ltopoChangerFvMesh \

View File

@ -1,11 +1,8 @@
EXE_INC = \
-I../buoyantBoussinesqSimpleFoam \
-I../../incompressible/pimpleFoam \
-I$(LIB_SRC)/sampling/lnInclude \
-I$(LIB_SRC)/finiteVolume/lnInclude \
-I$(LIB_SRC)/meshTools/lnInclude \
-I$(LIB_SRC)/dynamicMesh/lnInclude \
-I$(LIB_SRC)/dynamicFvMesh/lnInclude \
-I$(LIB_SRC)/TurbulenceModels/turbulenceModels/lnInclude \
-I$(LIB_SRC)/TurbulenceModels/incompressible/lnInclude \
-I$(LIB_SRC)/transportModels \
@ -16,8 +13,6 @@ EXE_LIBS = \
-lfiniteVolume \
-lfvOptions \
-lmeshTools \
-ldynamicMesh \
-ldynamicFvMesh \
-lsampling \
-lturbulenceModels \
-lincompressibleTurbulenceModels \

View File

@ -6,7 +6,6 @@
\\/ M anipulation |
-------------------------------------------------------------------------------
Copyright (C) 2011-2017 OpenFOAM Foundation
Copyright (C) 2021 OpenCFD Ltd.
-------------------------------------------------------------------------------
License
This file is part of OpenFOAM.
@ -31,8 +30,7 @@ Group
grpHeatTransferSolvers
Description
Transient solver for buoyant, turbulent flow of incompressible fluids,
with optional mesh motion and mesh topology changes.
Transient solver for buoyant, turbulent flow of incompressible fluids.
Uses the Boussinesq approximation:
\f[
@ -53,11 +51,9 @@ Description
\*---------------------------------------------------------------------------*/
#include "fvCFD.H"
#include "dynamicFvMesh.H"
#include "singlePhaseTransportModel.H"
#include "turbulentTransportModel.H"
#include "radiationModel.H"
#include "CorrectPhi.H"
#include "fvOptions.H"
#include "pimpleControl.H"
@ -68,8 +64,7 @@ int main(int argc, char *argv[])
argList::addNote
(
"Transient solver for buoyant, turbulent flow"
" of incompressible fluids, with optional mesh"
" motion and mesh topology changes.\n"
" of incompressible fluids.\n"
"Uses the Boussinesq approximation."
);
@ -78,10 +73,10 @@ int main(int argc, char *argv[])
#include "addCheckCaseOptions.H"
#include "setRootCaseLists.H"
#include "createTime.H"
#include "createDynamicFvMesh.H"
#include "createDyMControls.H"
#include "createMesh.H"
#include "createControl.H"
#include "createFields.H"
#include "createUfIfPresent.H"
#include "createTimeControls.H"
#include "CourantNo.H"
#include "setInitialDeltaT.H"
#include "initContinuityErrs.H"
@ -94,7 +89,7 @@ int main(int argc, char *argv[])
while (runTime.run())
{
#include "readDyMControls.H"
#include "readTimeControls.H"
#include "CourantNo.H"
#include "setDeltaT.H"
@ -105,34 +100,6 @@ int main(int argc, char *argv[])
// --- Pressure-velocity PIMPLE corrector loop
while (pimple.loop())
{
if (pimple.firstIter() || moveMeshOuterCorrectors)
{
// Do any mesh changes
mesh.controlledUpdate();
if (mesh.changing())
{
MRF.update();
if (correctPhi)
{
// Calculate absolute flux
// from the mapped surface velocity
phi = mesh.Sf() & Uf();
#include "correctPhi.H"
// Make the flux relative to the mesh motion
fvc::makeRelative(phi, U);
}
if (checkMeshCourantNo)
{
#include "meshCourantNo.H"
}
}
}
#include "UEqn.H"
#include "TEqn.H"

View File

@ -42,12 +42,6 @@
U = HbyA + rAU*fvc::reconstruct((phig - p_rghEqn.flux())/rAUf);
U.correctBoundaryConditions();
fvOptions.correct(U);
// Correct Uf if the mesh is moving
fvc::correctUf(Uf, U, phi);
// Make the fluxes relative to the mesh motion
fvc::makeRelative(phi, U);
}
}

View File

@ -1,5 +1,4 @@
EXE_INC = \
-I../../compressible/rhoPimpleFoam \
-I$(LIB_SRC)/finiteVolume/lnInclude \
-I$(LIB_SRC)/meshTools/lnInclude \
-I$(LIB_SRC)/sampling/lnInclude \
@ -8,8 +7,6 @@ EXE_INC = \
-I$(LIB_SRC)/thermophysicalModels/radiation/lnInclude \
-I$(LIB_SRC)/TurbulenceModels/turbulenceModels/lnInclude \
-I$(LIB_SRC)/TurbulenceModels/compressible/lnInclude \
-I$(LIB_SRC)/dynamicMesh/lnInclude \
-I$(LIB_SRC)/dynamicFvMesh/lnInclude \
-I$(LIB_SRC)/regionFaModels\lnInclude
EXE_LIBS = \
@ -23,9 +20,5 @@ EXE_LIBS = \
-lspecie \
-lturbulenceModels \
-lcompressibleTurbulenceModels \
-lthermoTools \
-latmosphericModels \
-ldynamicMesh \
-ldynamicFvMesh \
-ltopoChangerFvMesh \
-lregionFaModels

View File

@ -6,7 +6,6 @@
\\/ M anipulation |
-------------------------------------------------------------------------------
Copyright (C) 2011-2017 OpenFOAM Foundation
Copyright (C) 2021 OpenCFD Ltd.
-------------------------------------------------------------------------------
License
This file is part of OpenFOAM.
@ -31,9 +30,8 @@ Group
grpHeatTransferSolvers
Description
Transient solver for buoyant, turbulent flow of compressible fluids
for ventilation and heat-transfer, with optional mesh motion
and mesh topology changes.
Transient solver for buoyant, turbulent flow of compressible fluids for
ventilation and heat-transfer.
Turbulence is modelled using a run-time selectable compressible RAS or
LES model.
@ -41,16 +39,12 @@ Description
\*---------------------------------------------------------------------------*/
#include "fvCFD.H"
#include "dynamicFvMesh.H"
#include "rhoThermo.H"
#include "turbulentFluidThermoModel.H"
#include "radiationModel.H"
#include "CorrectPhi.H"
#include "fvOptions.H"
#include "pimpleControl.H"
#include "pressureControl.H"
#include "localEulerDdtScheme.H"
#include "fvcSmooth.H"
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
@ -59,8 +53,7 @@ int main(int argc, char *argv[])
argList::addNote
(
"Transient solver for buoyant, turbulent fluid flow"
" of compressible fluids, including radiation,"
" with optional mesh motion and mesh topology changes."
" of compressible fluids, including radiation."
);
#include "postProcess.H"
@ -68,105 +61,36 @@ int main(int argc, char *argv[])
#include "addCheckCaseOptions.H"
#include "setRootCaseLists.H"
#include "createTime.H"
#include "createDynamicFvMesh.H"
#include "createDyMControls.H"
#include "initContinuityErrs.H"
#include "createMesh.H"
#include "createControl.H"
#include "createFields.H"
#include "createFieldRefs.H"
#include "createRhoUfIfPresent.H"
#include "initContinuityErrs.H"
#include "createTimeControls.H"
#include "compressibleCourantNo.H"
#include "setInitialDeltaT.H"
turbulence->validate();
if (!LTS)
{
#include "compressibleCourantNo.H"
#include "setInitialDeltaT.H"
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
Info<< "\nStarting time loop\n" << endl;
while (runTime.run())
{
#include "readDyMControls.H"
// Store divrhoU from the previous mesh
// so that it can be mapped and used in correctPhi
// to ensure the corrected phi has the same divergence
autoPtr<volScalarField> divrhoU;
if (correctPhi)
{
divrhoU.reset
(
new volScalarField
(
"divrhoU",
fvc::div(fvc::absolute(phi, rho, U))
)
);
}
if (LTS)
{
#include "setRDeltaT.H"
}
else
{
#include "compressibleCourantNo.H"
#include "setDeltaT.H"
}
#include "readTimeControls.H"
#include "compressibleCourantNo.H"
#include "setDeltaT.H"
++runTime;
Info<< "Time = " << runTime.timeName() << nl << endl;
#include "rhoEqn.H"
// --- Pressure-velocity PIMPLE corrector loop
while (pimple.loop())
{
if (pimple.firstIter() || moveMeshOuterCorrectors)
{
// Store momentum to set rhoUf for introduced faces.
autoPtr<volVectorField> rhoU;
if (rhoUf.valid())
{
rhoU.reset(new volVectorField("rhoU", rho*U));
}
// Do any mesh changes
mesh.update();
if (mesh.changing())
{
gh = (g & mesh.C()) - ghRef;
ghf = (g & mesh.Cf()) - ghRef;
MRF.update();
if (correctPhi)
{
// Calculate absolute flux
// from the mapped surface velocity
phi = mesh.Sf() & rhoUf();
#include "correctPhi.H"
// Make the fluxes relative to the mesh-motion
fvc::makeRelative(phi, rho, U);
}
if (checkMeshCourantNo)
{
#include "meshCourantNo.H"
}
}
}
if (pimple.firstIter() && !pimple.SIMPLErho())
{
#include "rhoEqn.H"
}
#include "UEqn.H"
#include "EEqn.H"

View File

@ -1,5 +1,3 @@
#include "createRDeltaT.H"
Info<< "Reading thermophysical properties\n" << endl;
autoPtr<rhoThermo> pThermo(rhoThermo::New(mesh));

View File

@ -24,7 +24,6 @@ EXE_LIBS = \
-lspecie \
-lturbulenceModels \
-lcompressibleTurbulenceModels \
-lthermoTools \
-latmosphericModels \
-loverset \
-ldynamicFvMesh \

View File

@ -124,3 +124,6 @@ dimensionedScalar initialMass("initialMass", fvc::domainIntegrate(rho));
// Mask field for zeroing out contributions on hole cells
#include "createCellMask.H"
// Create bool field with interpolated cells
#include "createInterpolatedCells.H"

View File

@ -86,9 +86,6 @@ int main(int argc, char *argv[])
while (runTime.run())
{
#include "readTimeControls.H"
#include "readControls.H"
#include "readDyMControls.H"
#include "compressibleCourantNo.H"
@ -128,45 +125,14 @@ int main(int argc, char *argv[])
MRF.update();
#include "setCellMask.H"
const surfaceScalarField faceMaskOld
(
localMin<scalar>(mesh).interpolate(cellMask.oldTime())
);
// Zero Uf on old faceMask (H-I)
rhoUf() *= faceMaskOld;
//fvc::correctRhoUf(rhoUfint, rho, U, phi);
surfaceVectorField rhoUfint(fvc::interpolate(rho*U));
// Update Uf and phi on new C-I faces
rhoUf() += (1-faceMaskOld)*rhoUfint;
// Update Uf boundary
forAll(rhoUf().boundaryField(), patchI)
{
rhoUf().boundaryFieldRef()[patchI] =
rhoUfint.boundaryField()[patchI];
}
// Calculate absolute flux from the mapped surface velocity
phi = mesh.Sf() & rhoUf();
#include "setInterpolatedCells.H"
#include "correctRhoPhiFaceMask.H"
if (correctPhi)
{
#include "correctPhi.H"
}
// Zero phi on current H-I
const surfaceScalarField faceMask
(
localMin<scalar>(mesh).interpolate(cellMask)
);
phi *= faceMask;
U *= cellMask;
// Make the fluxes relative to the mesh-motion
fvc::makeRelative(phi, rho, U);
}

View File

@ -21,16 +21,6 @@ surfaceScalarField phiHbyA
fvc::flux(rho*HbyA) + phig
);
if (ddtCorr)
{
surfaceScalarField faceMaskOld
(
localMin<scalar>(mesh).interpolate(cellMask.oldTime())
);
phiHbyA +=
faceMaskOld*MRF.zeroFilter(rhorAUf*fvc::ddtCorr(rho, U, phi));
}
MRF.makeRelative(fvc::interpolate(rho), phiHbyA);
@ -122,8 +112,4 @@ if (thermo.dpdt())
}
}
surfaceScalarField faceMask
(
localMin<scalar>(mesh).interpolate(cellMask)
);
phi *= faceMask;

View File

@ -1,9 +0,0 @@
#include "readTimeControls.H"
correctPhi = pimple.dict().getOrDefault("correctPhi", false);
checkMeshCourantNo =
pimple.dict().getOrDefault("checkMeshCourantNo", false);
ddtCorr = pimple.dict().getOrDefault("ddtCorr", true);

View File

@ -28,8 +28,6 @@ MRF.makeRelative(fvc::interpolate(rho), phiHbyA);
// Update the pressure BCs to ensure flux consistency
constrainPressure(p_rgh, rho, U, phiHbyA, rhorAUf, MRF);
fvc::makeRelative(phiHbyA, rho, U);
fvScalarMatrix p_rghDDtEqn
(
fvc::ddt(rho) + psi*correction(fvm::ddt(p_rgh))
@ -106,15 +104,7 @@ else
rho = thermo.rho();
// Correct rhoUf if the mesh is moving
fvc::correctRhoUf(rhoUf, rho, U, phi);
if (thermo.dpdt())
{
dpdt = fvc::ddt(p);
if (mesh.moving())
{
dpdt -= fvc::div(fvc::meshPhi(rho, U), p);
}
}

View File

@ -20,6 +20,5 @@ EXE_LIBS = \
-lradiationModels \
-lturbulenceModels \
-lcompressibleTurbulenceModels \
-lthermoTools \
-latmosphericModels \
-lregionFaModels

View File

@ -37,7 +37,6 @@ EXE_LIBS = \
-lcombustionModels \
-lturbulenceModels \
-lcompressibleTurbulenceModels \
-lthermoTools \
-lradiationModels \
-lregionModels \
-lregionFaModels

View File

@ -6,7 +6,7 @@
\\/ M anipulation |
-------------------------------------------------------------------------------
Copyright (C) 2011-2016 OpenFOAM Foundation
Copyright (C) 2017-2019,2022 OpenCFD Ltd.
Copyright (C) 2017-2019 OpenCFD Ltd.
-------------------------------------------------------------------------------
License
This file is part of OpenFOAM.
@ -70,7 +70,6 @@ int main(int argc, char *argv[])
#define CREATE_MESH createMeshesPostProcess.H
#include "postProcess.H"
#include "addCheckCaseOptions.H"
#include "setRootCaseLists.H"
#include "createTime.H"
#include "createMeshes.H"

View File

@ -30,7 +30,6 @@ EXE_LIBS = \
-lspecie \
-lturbulenceModels \
-lcompressibleTurbulenceModels \
-lthermoTools \
-lradiationModels \
-lfvOptions \
-lfaOptions \

View File

@ -6,7 +6,7 @@
\\/ M anipulation |
-------------------------------------------------------------------------------
Copyright (C) 2011-2016 OpenFOAM Foundation
Copyright (C) 2017-2019,2022 OpenCFD Ltd.
Copyright (C) 2017-2019 OpenCFD Ltd.
-------------------------------------------------------------------------------
License
This file is part of OpenFOAM.
@ -62,7 +62,6 @@ int main(int argc, char *argv[])
#define CREATE_MESH createMeshesPostProcess.H
#include "postProcess.H"
#include "addCheckCaseOptions.H"
#include "setRootCaseLists.H"
#include "createTime.H"
#include "createMeshes.H"

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@ -4,61 +4,21 @@
forAll(fluidNames, i)
{
if (args.dryRun() || args.found("dry-run-write"))
{
Info
<< "Operating in 'dry-run' mode:"
<< " case will run for 1 time step. "
<< "All checks assumed OK on a clean exit" << endl;
Info<< "Create fluid mesh for region " << fluidNames[i]
<< " for time = " << runTime.timeName() << nl << endl;
FieldBase::allowConstructFromLargerSize = true;
// Create a simplified 1D mesh and attempt to re-create boundary
// conditions
fluidRegions.set
fluidRegions.set
(
i,
new fvMesh
(
i,
new simplifiedMeshes::columnFvMesh(runTime, fluidNames[i])
);
// Stop after 1 iteration of the simplified mesh
if (args.found("dry-run-write"))
{
// Using saWriteNow triggers function objects execute(), write()
runTime.stopAt(Time::saWriteNow);
// Make sure mesh gets output to the current time (since
// instance no longer constant)
fluidRegions[i].setInstance(runTime.timeName());
}
else
{
// Using saNoWriteNow triggers function objects execute(),
// but not write()
runTime.stopAt(Time::saNoWriteNow);
}
functionObject::outputPrefix = "postProcessing-dry-run";
}
else
{
Info<< "Create fluid mesh for region " << fluidNames[i]
<< " for time = " << runTime.timeName() << nl << endl;
fluidRegions.set
(
i,
new fvMesh
IOobject
(
IOobject
(
fluidNames[i],
runTime.timeName(),
runTime,
IOobject::MUST_READ
)
fluidNames[i],
runTime.timeName(),
runTime,
IOobject::MUST_READ
)
);
}
)
);
}

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@ -67,7 +67,6 @@ int main(int argc, char *argv[])
#define CREATE_MESH createMeshesPostProcess.H
#include "postProcess.H"
#include "addCheckCaseOptions.H"
#include "setRootCase.H"
#include "createTime.H"
#include "createMeshes.H"

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@ -4,61 +4,21 @@
forAll(fluidNames, i)
{
if (args.dryRun() || args.found("dry-run-write"))
{
Info
<< "Operating in 'dry-run' mode:"
<< " case will run for 1 time step. "
<< "All checks assumed OK on a clean exit" << endl;
Info<< "Create fluid mesh for region " << fluidNames[i]
<< " for time = " << runTime.timeName() << nl << endl;
FieldBase::allowConstructFromLargerSize = true;
// Create a simplified 1D mesh and attempt to re-create boundary
// conditions
fluidRegions.set
fluidRegions.set
(
i,
new fvMesh
(
i,
new simplifiedMeshes::columnFvMesh(runTime, fluidNames[i])
);
// Stop after 1 iteration of the simplified mesh
if (args.found("dry-run-write"))
{
// Using saWriteNow triggers function objects execute(), write()
runTime.stopAt(Time::saWriteNow);
// Make sure mesh gets output to the current time (since
// instance no longer constant)
fluidRegions[i].setInstance(runTime.timeName());
}
else
{
// Using saNoWriteNow triggers function objects execute(),
// but not write()
runTime.stopAt(Time::saNoWriteNow);
}
functionObject::outputPrefix = "postProcessing-dry-run";
}
else
{
Info<< "Create fluid mesh for region " << fluidNames[i]
<< " for time = " << runTime.timeName() << nl << endl;
fluidRegions.set
(
i,
new fvMesh
IOobject
(
IOobject
(
fluidNames[i],
runTime.timeName(),
runTime,
IOobject::MUST_READ
)
fluidNames[i],
runTime.timeName(),
runTime,
IOobject::MUST_READ
)
);
}
)
);
}

View File

@ -12,15 +12,15 @@
if (Y.size())
{
const word inertSpecie(thermo.get<word>("inertSpecie"));
inertIndex = composition.species().find(inertSpecie);
if (inertIndex < 0)
if (!composition.species().found(inertSpecie))
{
FatalIOErrorIn(args.executable().c_str(), thermo)
<< "Inert specie " << inertSpecie
<< " not found in available species "
<< flatOutput(composition.species())
<< composition.species()
<< exit(FatalIOError);
}
inertIndex = composition.species()[inertSpecie];
}
volScalarField& rho = rhoFluid[i];

View File

@ -9,7 +9,7 @@ forAll(fluidRegions, i)
const rhoThermo& thermo = refCast<const rhoThermo>(thermoFluid[i]);
const auto& bpsi = thermo.T().boundaryField();
forAll(bpsi, patchI)
forAll (bpsi, patchI)
{
if (bpsi[patchI].useImplicit())
{
@ -23,7 +23,7 @@ forAll(solidRegions, i)
solidThermo& thermo = thermos[i];
const auto& bpsi = thermo.T().boundaryField();
forAll(bpsi, patchI)
forAll (bpsi, patchI)
{
if (bpsi[patchI].useImplicit())
{
@ -37,25 +37,7 @@ forAll(fluidRegions, i)
const rhoThermo& thermo = refCast<const rhoThermo>(thermoFluid[i]);
if (coupled)
{
Info<< "Create fvMatrixAssembly." << endl;
fvMatrixAssemblyPtr.reset
(
new fvMatrix<scalar>
(
thermo.he(),
dimEnergy/dimTime
)
);
break;
}
}
if (coupled && !fvMatrixAssemblyPtr)
{
forAll(solidRegions, i)
{
solidThermo& thermo = thermos[i];
Info<< "Create fvMatrixAssembly." << endl;
Info << "Create fvMatrixAssembly." << endl;
fvMatrixAssemblyPtr.reset
(
new fvMatrix<scalar>

View File

@ -4,67 +4,26 @@
forAll(solidNames, i)
{
if (args.dryRun() || args.found("dry-run-write"))
{
Info
<< "Operating in 'dry-run' mode:"
<< " case will run for 1 time step. "
<< "All checks assumed OK on a clean exit" << endl;
Info<< "Create solid mesh for region " << solidNames[i]
<< " for time = " << runTime.timeName() << nl << endl;
FieldBase::allowConstructFromLargerSize = true;
// Create a simplified 1D mesh and attempt to re-create boundary
// conditions
solidRegions.set
solidRegions.set
(
i,
new fvMesh
(
i,
new simplifiedMeshes::columnFvMesh(runTime, solidNames[i])
);
// Stop after 1 iteration of the simplified mesh
if (args.found("dry-run-write"))
{
// Using saWriteNow triggers function objects execute(), write()
runTime.stopAt(Time::saWriteNow);
// Make sure mesh gets output to the current time (since
// instance no longer constant)
solidRegions[i].setInstance(runTime.timeName());
}
else
{
// Using saNoWriteNow triggers function objects execute(),
// but not write()
runTime.stopAt(Time::saNoWriteNow);
}
functionObject::outputPrefix = "postProcessing-dry-run";
}
else
{
Info<< "Create solid mesh for region " << solidNames[i]
<< " for time = " << runTime.timeName() << nl << endl;
solidRegions.set
(
i,
new fvMesh
IOobject
(
IOobject
(
solidNames[i],
runTime.timeName(),
runTime,
IOobject::MUST_READ
)
solidNames[i],
runTime.timeName(),
runTime,
IOobject::MUST_READ
)
);
)
);
// Force calculation of geometric properties to prevent it being
// done
// later in e.g. some boundary evaluation
//(void)solidRegions[i].weights();
//(void)solidRegions[i].deltaCoeffs();
}
// Force calculation of geometric properties to prevent it being done
// later in e.g. some boundary evaluation
//(void)solidRegions[i].weights();
//(void)solidRegions[i].deltaCoeffs();
}

View File

@ -1,4 +1,3 @@
solidRegionDiffNo.C
solidFoam.C
EXE = $(FOAM_APPBIN)/solidFoam

View File

@ -1,6 +1,4 @@
EXE_INC = \
-I../chtMultiRegionFoam/include \
-I../chtMultiRegionFoam/solid \
-I$(LIB_SRC)/finiteVolume/lnInclude \
-I$(LIB_SRC)/meshTools/lnInclude \
-I$(LIB_SRC)/dynamicMesh/lnInclude \
@ -23,5 +21,4 @@ EXE_LIBS = \
-lfluidThermophysicalModels \
-lsolidThermo \
-lradiationModels \
-lspecie \
-lthermoTools
-lspecie

View File

@ -90,24 +90,5 @@ else
);
}
// Consider mesh flux to correct for mesh deformation
bool meshFluxCorr(false);
if (mesh.solutionDict().found("SIMPLE"))
{
meshFluxCorr =
mesh.solutionDict().subDict("SIMPLE").getOrDefault<bool>
(
"meshFluxCorrection", false
);
}
else if (mesh.solutionDict().found("PIMPLE"))
{
meshFluxCorr =
mesh.solutionDict().subDict("PIMPLE").getOrDefault<bool>
(
"meshFluxCorrection", false
);
}
#include "createRadiationModel.H"
#include "createFvOptions.H"

View File

@ -1,36 +0,0 @@
/*---------------------------------------------------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | www.openfoam.com
\\/ M anipulation |
-------------------------------------------------------------------------------
Copyright (C) 2022 OpenCFD Ltd.
-------------------------------------------------------------------------------
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
CourantNo
Description
Dummy (fluid) Courant number.
\*---------------------------------------------------------------------------*/
scalar CoNum = 0.0;
// ************************************************************************* //

View File

@ -11,14 +11,14 @@
fvOptions(rho, h)
);
if (meshFluxCorr)
if (mesh.changing())
{
surfaceScalarField phihMesh
(
fvc::interpolate(betav*rho*h)*mesh.phi()
);
hEqn -= fvc::div(phihMesh);
hEqn -= fvc::div(phihMesh);
}
hEqn.relax();

View File

@ -1,31 +0,0 @@
scalar DiNum = -GREAT;
{
tmp<volScalarField> magKappa;
if (thermo.isotropic())
{
magKappa = thermo.kappa();
}
else
{
magKappa = mag(thermo.Kappa());
}
tmp<volScalarField> tcp = thermo.Cp();
const volScalarField& cp = tcp();
tmp<volScalarField> trho = thermo.rho();
const volScalarField& rho = trho();
DiNum = max
(
solidRegionDiffNo
(
mesh,
runTime,
rho*cp,
magKappa()
),
DiNum
);
}

View File

@ -41,8 +41,6 @@ Description
#include "fvOptions.H"
#include "simpleControl.H"
#include "pimpleControl.H"
#include "dummyCourantNo.H"
#include "solidRegionDiffNo.H"
#include "coordinateSystem.H"
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
@ -90,31 +88,17 @@ int main(int argc, char *argv[])
{
pimpleControl pimple(mesh);
#include "createDyMControls.H"
while (runTime.run())
{
#include "readDyMControls.H"
#include "readSolidTimeControls.H"
#include "solidDiffusionNo.H"
#include "setMultiRegionDeltaT.H"
++runTime;
Info<< "Time = " << runTime.timeName() << nl << endl;
while (pimple.loop())
{
if (pimple.firstIter() || moveMeshOuterCorrectors)
if (pimple.firstIter())
{
// Do any mesh changes
mesh.controlledUpdate();
if (mesh.changing() && checkMeshCourantNo)
{
#include "meshCourantNo.H"
}
mesh.update();
}
while (pimple.correct())

View File

@ -1 +0,0 @@
../chtMultiRegionFoam/solid/solidRegionDiffNo.C

View File

@ -1 +0,0 @@
../chtMultiRegionFoam/solid/solidRegionDiffNo.H

View File

@ -18,5 +18,4 @@ EXE_LIBS = \
-lradiationModels \
-lspecie \
-lturbulenceModels \
-lcompressibleTurbulenceModels \
-lthermoTools
-lcompressibleTurbulenceModels

View File

@ -5,8 +5,8 @@
\\ / A nd | www.openfoam.com
\\/ M anipulation |
-------------------------------------------------------------------------------
Copyright (C) 2007-2021 PCOpt/NTUA
Copyright (C) 2013-2021 FOSS GP
Copyright (C) 2007-2019 PCOpt/NTUA
Copyright (C) 2013-2019 FOSS GP
Copyright (C) 2019 OpenCFD Ltd.
-------------------------------------------------------------------------------
License
@ -71,6 +71,9 @@ int main(int argc, char *argv[])
// Solve all adjoint equations
om.solveAdjointEquations();
// Compute all sensitivities
om.computeSensitivities();
}
Info<< "End\n" << endl;

View File

@ -1,5 +1,3 @@
#include "createRDeltaT.H"
Info<< "Reading field p\n" << endl;
volScalarField p
(

View File

@ -37,7 +37,10 @@ scalar meanCoNum = 0.0;
if (mesh.nInternalFaces())
{
surfaceScalarField phiMask(localMin<scalar>(mesh).interpolate(cellMask));
surfaceScalarField phiMask
(
localMin<scalar>(mesh).interpolate(cellMask + interpolatedCells)
);
scalarField sumPhi(fvc::surfaceSum(mag(phiMask*phi))().internalField());

View File

@ -1,5 +1,4 @@
// Solve the Momentum equation
MRF.correctBoundaryVelocity(U);
tmp<fvVectorMatrix> tUEqn

View File

@ -1,26 +0,0 @@
#include "createTimeControls.H"
bool correctPhi
(
pimple.dict().getOrDefault("correctPhi", false)
);
bool checkMeshCourantNo
(
pimple.dict().getOrDefault("checkMeshCourantNo", false)
);
bool massFluxInterpolation
(
pimple.dict().getOrDefault("massFluxInterpolation", false)
);
bool adjustFringe
(
pimple.dict().getOrDefault("oversetAdjustPhi", false)
);
bool ddtCorr
(
pimple.dict().getOrDefault("ddtCorr", true)
);

View File

@ -1,273 +0,0 @@
// Interpolation used
interpolationCellPoint<vector> UInterpolator(HbyA);
// Determine faces on outside of interpolated cells
bitSet isOwnerInterpolatedFace(mesh.nInternalFaces());
bitSet isNeiInterpolatedFace(mesh.nInternalFaces());
// Determine donor cells
labelListList donorCell(mesh.nInternalFaces());
scalarListList weightCellCells(mesh.nInternalFaces());
// Interpolated HbyA faces
vectorField UIntFaces(mesh.nInternalFaces(), Zero);
// Determine receptor neighbour cells
labelList receptorNeigCell(mesh.nInternalFaces(), -1);
{
const cellCellStencilObject& overlap = Stencil::New(mesh);
const labelList& cellTypes = overlap.cellTypes();
const labelIOList& zoneID = overlap.zoneID();
label nZones = gMax(zoneID)+1;
PtrList<fvMeshSubset> meshParts(nZones);
labelList nCellsPerZone(nZones, Zero);
// A mesh subset for each zone
forAll(meshParts, zonei)
{
meshParts.set
(
zonei,
// Select cells where the zoneID == zonei
new fvMeshSubset(mesh, zonei, zoneID)
);
}
for (label faceI = 0; faceI < mesh.nInternalFaces(); faceI++)
{
label ownType = cellTypes[mesh.faceOwner()[faceI]];
label neiType = cellTypes[mesh.faceNeighbour()[faceI]];
if
(
ownType == cellCellStencil::INTERPOLATED
&& neiType == cellCellStencil::CALCULATED
)
{
isOwnerInterpolatedFace.set(faceI);
const vector& fc = mesh.faceCentres()[faceI];
for (label zoneI = 0; zoneI < nZones; zoneI++)
{
if (zoneI != zoneID[mesh.faceOwner()[faceI]])
{
const fvMesh& partMesh = meshParts[zoneI].subMesh();
const labelList& cellMap = meshParts[zoneI].cellMap();
label cellI = partMesh.findCell(fc);
if (cellI != -1)
{
// Determine weights
labelList stencil(partMesh.cellCells()[cellI]);
stencil.append(cellI);
label st = stencil.size();
donorCell[faceI].setSize(st);
weightCellCells[faceI].setSize(st);
scalarField weights(st);
forAll(stencil, i)
{
scalar d = mag
(
partMesh.cellCentres()[stencil[i]]
- fc
);
weights[i] = 1.0/d;
donorCell[faceI][i] = cellMap[stencil[i]];
}
weights /= sum(weights);
weightCellCells[faceI] = weights;
forAll(stencil, i)
{
UIntFaces[faceI] +=
weightCellCells[faceI][i]
*UInterpolator.interpolate
(
fc,
donorCell[faceI][i]
);
}
break;
}
}
}
receptorNeigCell[faceI] = mesh.faceNeighbour()[faceI];
}
else if
(
ownType == cellCellStencil::CALCULATED
&& neiType == cellCellStencil::INTERPOLATED
)
{
isNeiInterpolatedFace.set(faceI);
const vector& fc = mesh.faceCentres()[faceI];
for (label zoneI = 0; zoneI < nZones; zoneI++)
{
if (zoneI != zoneID[mesh.faceNeighbour()[faceI]])
{
const fvMesh& partMesh = meshParts[zoneI].subMesh();
const labelList& cellMap = meshParts[zoneI].cellMap();
label cellI = partMesh.findCell(fc);
if (cellI != -1)
{
// Determine weights
labelList stencil(partMesh.cellCells()[cellI]);
stencil.append(cellI);
label st = stencil.size();
donorCell[faceI].setSize(st);
weightCellCells[faceI].setSize(st);
scalarField weights(st);
forAll(stencil, i)
{
scalar d = mag
(
partMesh.cellCentres()[stencil[i]]
- fc
);
weights[i] = 1.0/d;
donorCell[faceI][i] = cellMap[stencil[i]];
}
weights /= sum(weights);
weightCellCells[faceI] = weights;
forAll(stencil, i)
{
UIntFaces[faceI] +=
weightCellCells[faceI][i]
*UInterpolator.interpolate
(
fc,
donorCell[faceI][i]
);
}
break;
}
}
}
receptorNeigCell[faceI] = mesh.faceOwner()[faceI];
}
}
}
// contravariant U
vectorField U1Contrav(mesh.nInternalFaces(), Zero);
surfaceVectorField faceNormals(mesh.Sf()/mesh.magSf());
forAll(isNeiInterpolatedFace, faceI)
{
label cellId = -1;
if (isNeiInterpolatedFace.test(faceI))
{
cellId = mesh.faceNeighbour()[faceI];
}
else if (isOwnerInterpolatedFace.test(faceI))
{
cellId = mesh.faceOwner()[faceI];
}
if (cellId != -1)
{
const vector& n = faceNormals[faceI];
vector n1(Zero);
// 2-D cases
if (mesh.nSolutionD() == 2)
{
for (direction cmpt=0; cmpt<vector::nComponents; cmpt++)
{
if (mesh.geometricD()[cmpt] == -1)
{
switch (cmpt)
{
case vector::X:
{
n1 = vector(0, n.z(), -n.y());
break;
}
case vector::Y:
{
n1 = vector(n.z(), 0, -n.x());
break;
}
case vector::Z:
{
n1 = vector(n.y(), -n.x(), 0);
break;
}
}
}
}
}
else if (mesh.nSolutionD() == 3)
{
//Determine which is the primary direction
if (mag(n.x()) > mag(n.y()) && mag(n.x()) > mag(n.z()))
{
n1 = vector(n.y(), -n.x(), 0);
}
else if (mag(n.y()) > mag(n.z()))
{
n1 = vector(0, n.z(), -n.y());
}
else
{
n1 = vector(-n.z(), 0, n.x());
}
}
n1.normalise();
const vector n2 = normalised(n ^ n1);
tensor rot =
tensor
(
n.x() ,n.y(), n.z(),
n1.x() ,n1.y(), n1.z(),
n2.x() ,n2.y(), n2.z()
);
// tensor rot =
// tensor
// (
// n & x ,n & y, n & z,
// n1 & x ,n1 & y, n1 & z,
// n2 & x ,n2 & y, n2 & z
// );
U1Contrav[faceI].x() =
2*transform(rot, UIntFaces[faceI]).x()
- transform(rot, HbyA[receptorNeigCell[faceI]]).x();
U1Contrav[faceI].y() = transform(rot, HbyA[cellId]).y();
U1Contrav[faceI].z() = transform(rot, HbyA[cellId]).z();
HbyA[cellId] = transform(inv(rot), U1Contrav[faceI]);
}
}

View File

@ -46,11 +46,7 @@ Description
#include "fvOptions.H"
#include "cellCellStencilObject.H"
#include "zeroGradientFvPatchFields.H"
#include "localMin.H"
#include "interpolationCellPoint.H"
#include "transform.H"
#include "fvMeshSubset.H"
#include "oversetAdjustPhi.H"
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
@ -68,10 +64,9 @@ int main(int argc, char *argv[])
#include "setRootCaseLists.H"
#include "createTime.H"
#include "createDynamicFvMesh.H"
#include "createDyMControls.H"
#include "initContinuityErrs.H"
pimpleControl pimple(mesh);
#include "createFields.H"
#include "createUf.H"
#include "createMRF.H"
@ -88,7 +83,7 @@ int main(int argc, char *argv[])
while (runTime.run())
{
#include "readControls.H"
#include "readDyMControls.H"
#include "CourantNo.H"
#include "setDeltaT.H"
@ -97,45 +92,26 @@ int main(int argc, char *argv[])
Info<< "Time = " << runTime.timeName() << nl << endl;
bool changed = mesh.update();
mesh.update();
if (changed)
if (mesh.changing())
{
#include "setCellMask.H"
#include "setInterpolatedCells.H"
#include "correctPhiFaceMask.H"
surfaceScalarField faceMaskOld
(
localMin<scalar>(mesh).interpolate(cellMask.oldTime())
);
if (correctPhi)
{
// Corrects flux on separated regions
#include "correctPhi.H"
}
// Zero Uf on old faceMask (H-I)
Uf *= faceMaskOld;
// Update Uf and phi on new C-I faces
Uf += (1-faceMaskOld)*fvc::interpolate(U);
phi = mesh.Sf() & Uf;
fvc::makeRelative(phi, U);
// Zero phi on current H-I
surfaceScalarField faceMask
(
localMin<scalar>(mesh).interpolate(cellMask)
);
phi *= faceMask;
}
if (mesh.changing() && correctPhi)
{
// Calculate absolute flux from the mapped surface velocity
#include "correctPhi.H"
}
// Make the flux relative to the mesh motion
fvc::makeRelative(phi, U);
if (mesh.changing() && checkMeshCourantNo)
{
#include "meshCourantNo.H"
if (checkMeshCourantNo)
{
#include "meshCourantNo.H"
}
}
// --- Pressure-velocity PIMPLE corrector loop

View File

@ -1,29 +1,11 @@
// Option 1: interpolate rAU, do not block out rAU on blocked cells
volScalarField rAU("rAU", 1.0/UEqn.A());
mesh.interpolate(rAU);
// Option 2: do not interpolate rAU but block out rAU
//surfaceScalarField rAUf("rAUf", fvc::interpolate(blockedCells*rAU));
// Option 3: do not interpolate rAU but zero out rAUf on faces on holes
// But what about:
//
// H
// H I C C C C
// H
//
surfaceScalarField rAUf("rAUf", fvc::interpolate(rAU));
volVectorField H("H", UEqn.H());
volVectorField HbyA("HbyA", U);
HbyA = constrainHbyA(rAU*H, U, p);
if (massFluxInterpolation)
{
#include "interpolatedFaces.H"
}
if (runTime.outputTime())
{
H.write();
@ -38,18 +20,14 @@ if (pimple.nCorrPISO() <= 1)
phiHbyA = fvc::flux(HbyA);
if (ddtCorr)
if (runTime.outputTime())
{
surfaceScalarField faceMaskOld
(
localMin<scalar>(mesh).interpolate(cellMask.oldTime())
);
phiHbyA += rAUf*faceMaskOld*fvc::ddtCorr(U, Uf);
volScalarField divPhiHbyA("divPhiHbyA", fvc::div(phiHbyA));
divPhiHbyA.write();
}
MRF.makeRelative(phiHbyA);
// WIP
if (p.needReference())
{
fvc::makeRelative(phiHbyA, U);
@ -57,7 +35,8 @@ if (p.needReference())
fvc::makeAbsolute(phiHbyA, U);
}
// WIP: To adjust phi on fringe faces to help mass
// conservation
if (adjustFringe)
{
fvc::makeRelative(phiHbyA, U);
@ -79,27 +58,29 @@ while (pimple.correctNonOrthogonal())
if (pimple.finalNonOrthogonalIter())
{
phi = phiHbyA - pEqn.flux();
// option 2:
// rAUf*fvc::snGrad(p)*mesh.magSf();
pEqn.relax();
U =
cellMask*
(
HbyA -
rAU*fvc::reconstruct((pEqn.flux())/rAUf)
);
U.correctBoundaryConditions();
fvOptions.correct(U);
}
}
// Excludes error in interpolated/hole cells
#include "continuityErrs.H"
// Explicitly relax pressure for momentum corrector
p.relax();
volVectorField gradP(fvc::grad(p));
if (runTime.outputTime())
{
volVectorField Ucorrected("Ucorrected", U);
Ucorrected.write();
// Option 2: zero out velocity on blocked out cells
//U = HbyA - rAU*cellMask*gradP;
// Option 3: zero out velocity on blocked out cells
// This is needed for the scalar Eq (k,epsilon, etc)
// which can use U as source term
U = cellMask*(HbyA - rAU*gradP);
U.correctBoundaryConditions();
fvOptions.correct(U);
volScalarField divPhiCon("divPhiCon", fvc::div(phi));
divPhiCon.write();
}
{
Uf = fvc::interpolate(U);
@ -109,9 +90,4 @@ fvOptions.correct(U);
// Make the fluxes relative to the mesh motion
fvc::makeRelative(phi, U);
surfaceScalarField faceMask
(
localMin<scalar>(mesh).interpolate(cellMask)
);
phi *= faceMask;

View File

@ -1,10 +0,0 @@
#include "readTimeControls.H"
correctPhi = pimple.dict().getOrDefault("correctPhi", false);
checkMeshCourantNo = pimple.dict().getOrDefault("checkMeshCourantNo", false);
massFluxInterpolation =
pimple.dict().getOrDefault("massFluxInterpolation", false);
ddtCorr = pimple.dict().getOrDefault("ddtCorr", true);

View File

@ -81,8 +81,6 @@ Note
#include "pimpleControl.H"
#include "CorrectPhi.H"
#include "fvOptions.H"
#include "localEulerDdtScheme.H"
#include "fvcSmooth.H"
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
@ -109,12 +107,6 @@ int main(int argc, char *argv[])
turbulence->validate();
if (!LTS)
{
#include "CourantNo.H"
#include "setInitialDeltaT.H"
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
Info<< "\nStarting time loop\n" << endl;
@ -122,16 +114,8 @@ int main(int argc, char *argv[])
while (runTime.run())
{
#include "readDyMControls.H"
if (LTS)
{
#include "setRDeltaT.H"
}
else
{
#include "CourantNo.H"
#include "setDeltaT.H"
}
#include "CourantNo.H"
#include "setDeltaT.H"
++runTime;

View File

@ -1,69 +0,0 @@
{
volScalarField& rDeltaT = trDeltaT.ref();
const dictionary& pimpleDict = pimple.dict();
scalar maxCo
(
pimpleDict.getOrDefault<scalar>("maxCo", 0.8)
);
scalar rDeltaTSmoothingCoeff
(
pimpleDict.getOrDefault<scalar>("rDeltaTSmoothingCoeff", 0.02)
);
scalar rDeltaTDampingCoeff
(
pimpleDict.getOrDefault<scalar>("rDeltaTDampingCoeff", 1.0)
);
scalar maxDeltaT
(
pimpleDict.getOrDefault<scalar>("maxDeltaT", GREAT)
);
volScalarField rDeltaT0("rDeltaT0", rDeltaT);
// Set the reciprocal time-step from the local Courant number
rDeltaT.ref() = max
(
1/dimensionedScalar("maxDeltaT", dimTime, maxDeltaT),
fvc::surfaceSum(mag(phi))()()
/((2*maxCo)*mesh.V())
);
// Update the boundary values of the reciprocal time-step
rDeltaT.correctBoundaryConditions();
Info<< "Flow time scale min/max = "
<< gMin(1/rDeltaT.primitiveField())
<< ", " << gMax(1/rDeltaT.primitiveField()) << endl;
if (rDeltaTSmoothingCoeff < 1.0)
{
fvc::smooth(rDeltaT, rDeltaTSmoothingCoeff);
}
Info<< "Smoothed flow time scale min/max = "
<< gMin(1/rDeltaT.primitiveField())
<< ", " << gMax(1/rDeltaT.primitiveField()) << endl;
// Limit rate of change of time scale
// - reduce as much as required
// - only increase at a fraction of old time scale
if
(
rDeltaTDampingCoeff < 1.0
&& runTime.timeIndex() > runTime.startTimeIndex() + 1
)
{
rDeltaT =
rDeltaT0
*max(rDeltaT/rDeltaT0, scalar(1) - rDeltaTDampingCoeff);
Info<< "Damped flow time scale min/max = "
<< gMin(1/rDeltaT.primitiveField())
<< ", " << gMax(1/rDeltaT.primitiveField()) << endl;
}
}

View File

@ -20,7 +20,7 @@ volScalarField h0
IOobject
(
"h0",
runTime.findInstance(polyMesh::meshSubDir, "points"),
runTime.findInstance("polyMesh", "points"),
mesh,
IOobject::READ_IF_PRESENT
),

View File

@ -24,7 +24,3 @@ bool adjustFringe
(
simple.dict().getOrDefault("oversetAdjustPhi", false)
);
bool massFluxInterpolation
(
simple.dict().getOrDefault("massFluxInterpolation", false)
);

View File

@ -1,52 +1,22 @@
/*---------------------------------------------------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | www.openfoam.com
\\/ M anipulation |
-------------------------------------------------------------------------------
Copyright (C) 2017 OpenCFD Ltd.
-------------------------------------------------------------------------------
License
This file is part of OpenFOAM, distributed under GPL-3.0-or-later.
Info<< "Create dynamic mesh for time = "
<< runTime.timeName() << nl << endl;
Description
Create a dynamicFvMesh, with init()
Required Variables
- runTime [Time]
Provided Variables
- mesh [dynamicFvMesh], meshPtr
\*---------------------------------------------------------------------------*/
Foam::autoPtr<Foam::dynamicFvMesh> meshPtr;
{
Foam::Info << "Create dynamic mesh for time = "
<< runTime.timeName() << Foam::nl;
meshPtr = dynamicFvMesh::New
autoPtr<dynamicFvMesh> meshPtr
(
IOobject
dynamicFvMesh::New
(
polyMesh::defaultRegion,
runTime.timeName(),
runTime,
IOobject::MUST_READ
IOobject
(
polyMesh::defaultRegion,
runTime.timeName(),
runTime,
IOobject::MUST_READ
)
)
);
}
dynamicFvMesh& mesh = meshPtr();
dynamicFvMesh& mesh = meshPtr();
// Calculate initial mesh-to-mesh mapping. Note that this should be
// done under the hood, e.g. as a MeshObject
mesh.update();
Foam::Info << Foam::endl;
// ************************************************************************* //
// Calculate initial mesh-to-mesh mapping. Note that this should be
// done under the hood, e.g. as a MeshObject
mesh.update();

View File

@ -1,5 +1,5 @@
{
surfaceScalarField faceMask(localMin<scalar>(mesh).interpolate(cellMask));
//surfaceScalarField faceMask(localMin<scalar>(mesh).interpolate(cellMask));
volScalarField rAU(1.0/UEqn.A());
surfaceScalarField rAUf("rAUf", faceMask*fvc::interpolate(rAU));
@ -7,12 +7,6 @@
volVectorField HbyA("HbyA", U);
HbyA = constrainHbyA(cellMask*rAU*UEqn.H(), U, p);
//mesh.interpolate(HbyA);
if (massFluxInterpolation)
{
#include "interpolatedFaces.H"
}
tUEqn.clear();
surfaceScalarField phiHbyA("phiHbyA", fvc::flux(HbyA));

View File

@ -31,7 +31,6 @@ EXE_LIBS = \
-lmeshTools \
-lturbulenceModels \
-lcompressibleTurbulenceModels \
-lthermoTools \
-llagrangian \
-llagrangianIntermediate \
-llagrangianTurbulence \

View File

@ -1,4 +1,4 @@
const volScalarField& T = thermo.T();
const volScalarField& psi = thermo.psi();
const label inertIndex(composition.species().find(inertSpecie));
const label inertIndex(composition.species()[inertSpecie]);

View File

@ -36,7 +36,6 @@ EXE_LIBS = \
-lsampling \
-lturbulenceModels \
-lcompressibleTurbulenceModels \
-lthermoTools \
-lspecie \
-lcompressibleTransportModels \
-lfluidThermophysicalModels \

View File

@ -1,4 +1,4 @@
const label inertIndex(composition.species().find(inertSpecie));
const label inertIndex(composition.species()[inertSpecie]);
const volScalarField& T = thermo.T();
const volScalarField& psi = thermo.psi();

View File

@ -1,35 +1,27 @@
#include "createMesh.H"
dictionary filmDict;
IOobject io
IOdictionary filmDict
(
"surfaceFilmProperties",
mesh.time().constant(),
mesh,
IOobject::READ_IF_PRESENT,
IOobject::NO_WRITE,
false
IOobject
(
"surfaceFilmProperties",
runTime.constant(),
runTime,
IOobject::MUST_READ,
IOobject::NO_WRITE,
false
)
);
if (io.typeHeaderOk<IOdictionary>())
{
IOdictionary propDict(io);
const word filmRegionName = filmDict.get<word>("region");
filmDict = std::move(propDict);
const word filmRegionName = filmDict.get<word>("region");
fvMesh filmMesh
fvMesh filmMesh
(
IOobject
(
IOobject
(
filmRegionName,
runTime.timeName(),
runTime,
IOobject::MUST_READ
)
);
}
filmRegionName,
runTime.timeName(),
runTime,
IOobject::MUST_READ
)
);

View File

@ -36,7 +36,6 @@ EXE_LIBS = \
-ldynamicFvMesh \
-lturbulenceModels \
-lcompressibleTurbulenceModels \
-lthermoTools \
-lspecie \
-lcompressibleTransportModels \
-lfluidThermophysicalModels \

View File

@ -31,7 +31,6 @@ EXE_LIBS = \
-lmeshTools \
-lturbulenceModels \
-lcompressibleTurbulenceModels \
-lthermoTools \
-llagrangian \
-llagrangianIntermediate \
-llagrangianTurbulence \

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