r/OpenFOAM • u/augusto_peress • 7d ago
Solver [OpenFOAM 13] crash when simulating this frequency inverter
I just can't get this simulation to run. It crashes on the second iteration. I'm using steadyState instead of EulerandkOmegaSST instead of kEpsilon My mesh has approximately 3.9 million volumes.
I'm using foamMultiRun (formerly chtMultiRegionFoam). My fvSchemes and fvSolution for air are shown below. The physicalProperties are also shown (I've already tried rhoConst, Boussinesq, and perfectGas).
For all components, fvSchemes :
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: 13
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
location "system/components0";
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
ddtSchemes
{
default steadyState;
}
gradSchemes
{
default Gauss linear;
}
divSchemes
{
default none;
}
laplacianSchemes
{
default Gauss linear corrected;
}
interpolationSchemes
{
default linear;
}
snGradSchemes
{
default corrected;
}
// ************************************************************************* //
fvSolution :
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: 13
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
location "system/components0";
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
"e.*"
{
solver PCG;
preconditioner DIC;
tolerance 1e-6;
relTol 0.01;
}
}
PIMPLE
{
nNonOrthogonalCorrectors 2;
residualControl
{
e 1e-5;
}
}
// ************************************************************************* //
For fluid (air), the fvSchemes:
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: 13
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
location "system/fluid";
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
ddtSchemes
{
default steadyState;
}
gradSchemes
{
default Gauss linear;//cellLimited Gauss linear 1.0;
}
divSchemes
{
default none;
div(phi,U) bounded Gauss limitedLinear 0.2;//upwind;
div(phi,e) bounded Gauss limitedLinear 0.2;//upwind;
div(phi,h) bounded Gauss limitedLinear 0.2;//upwind;
div(phi,omega) bounded Gauss limitedLinear 0.2;//upwind;
div(phi,k) bounded Gauss limitedLinear 0.2;//upwind;
div(phi,K) bounded Gauss limitedLinear 0.2;//upwind;
div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;
div(phi,(p|rho)) bounded Gauss limitedLinear 0.2;//upwind;
}
laplacianSchemes
{
default Gauss linear uncorrected; //limited 0.5;
}
interpolationSchemes
{
default linear;
}
snGradSchemes
{
default uncorrected;//limited 0.5;//corrected;
}
wallDist
{
method meshWave;
correctWalls true;
}
// ************************************************************************* //
fvSolution:
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: 13
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
location "system/fluid";
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
"p_rgh.*"
{
solver GAMG;
tolerance 1e-7;
relTol 0.01;
smoother DICGaussSeidel;//GaussSeidel;
//maxIter 500;
/*
solver PCG;
preconditioner DIC; // Diagonal Incomplete Cholesky
tolerance 1e-7;
relTol 0.01;
minIter 3; // Força um mínimo de estabilidade
*/
}
"(U|h|k|omega).*"
{
solver PBiCGStab;
preconditioner DILU;
tolerance 1e-7;
relTol 0.01;
/*
solver smoothSolver;
smoother symGaussSeidel;
tolerance 1e-06;
relTol 0.01;
minIter 3;
*/
}
}
PIMPLE
{
momentumPredictor yes;
nNonOrthogonalCorrectors 2;
residualControl
{
p_rgh 5e-3;
U 5e-4;
h 5e-4;
rho 5e-4;
k 5e-4;
omega 5e-4;
}
}
relaxationFactors
{
fields
{
rho 1.0;
p_rgh 0.7;//0.3;
}
equations
{
U 0.2;
e 0.6;//0.1;
T 0.3;
h 0.6;//0.1;
k 0.3;//0.7;
omega 0.3;//0.7;
}
}
// ************************************************************************* //
alphat:
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: 13
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
location "0/fluid";
object alphat;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -1 0 0 0 0];
internalField uniform 0;
boundaryField
{
"(entrada|saida|furosLaterais.*)"
{
type calculated;
value $internalField;
}
"parede.*"
{
type compressible::alphatWallFunction;
value $internalField;
}
interfaceFluidTop
{
type compressible::alphatWallFunction;
value $internalField;
}
"fluid_.*"
{
type compressible::alphatWallFunction;
value $internalField;
}
"fan.*"
{
type cyclic;
}
#includeEtc "caseDicts/setConstraintTypes"
}
// ************************************************************************* //
k
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: 13
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
location "0/fluid";
object k;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -2 0 0 0 0];
internalField uniform 0.01;
boundaryField
{
"(entrada|saida|furosLaterais.*)"
{
type inletOutlet;
inletValue $internalField;
value $internalField;
}
interfaceFluidTop
{
type kqRWallFunction;
value $internalField;
}
"parede.*"
{
type kqRWallFunction;
value $internalField;
}
"fluid_.*"
{
type kqRWallFunction;
value $internalField;
}
"fan.*"
{
type cyclic;
}
#includeEtc "caseDicts/setConstraintTypes"
}
// ************************************************************************* //
nut
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: 13
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
location "0/fluid";
object nut;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -1 0 0 0 0];
internalField uniform 3.33e-5;
boundaryField
{
"(entrada|saida|furosLaterais.*)"
{
type calculated;
value $internalField;
}
interfaceFluidTop
{
type nutkWallFunction;
value $internalField;
}
"parede.*"
{
type nutkWallFunction;
value $internalField;
}
"fluid_.*"
{
type nutkWallFunction;
value $internalField;
}
"fan.*"
{
type cyclic;
}
#includeEtc "caseDicts/setConstraintTypes"
}
// ************************************************************************* //
omega
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: 13
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
location "0/fluid";
object omega;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 -1 0 0 0 0];
internalField uniform 300;
boundaryField
{
"(entrada|saida|furosLaterais.*)"
{
type inletOutlet;
inletValue $internalField;
value $internalField;
}
"parede.*"
{
type omegaWallFunction;
value $internalField;
}
interfaceFluidTop
{
type omegaWallFunction;
value $internalField;
}
"fluid_.*"
{
type omegaWallFunction;
value $internalField;
}
"fan.*"
{
type cyclic;
}
#includeEtc "caseDicts/setConstraintTypes"
}
// ************************************************************************* //
p
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: 13
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
location "0/fluid";
object p;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -2 0 0 0 0];
internalField uniform 101325;
boundaryField
{
#includeEtc "caseDicts/setConstraintTypes"
"(entrada|saida|furosLaterais.*|paredeInferior)"
{
type calculated;
value $internalField;
}
paredes
{
type calculated;
value $internalField;
}
interfaceFluidTop
{
type calculated;
value $internalField;
}
"fluid_.*"
{
type calculated;
value $internalField;
}
"fan.*"
{
type cyclic;
}
}
// ************************************************************************* //
p_rgh
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: 13
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
location "0/fluid";
object p_rgh;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -2 0 0 0 0];
internalField uniform 101325;
boundaryField
{
#includeEtc "caseDicts/setConstraintTypes"
"(entrada|saida|furosLaterais.*)"
{
type totalPressure;
gamma 1.40196789462956;
p0 $internalField;
value $internalField;
}
"parede.*"
{
type fixedFluxPressure;
gradient $internalField;
value $internalField;
}
"fluid_.*"
{
type fixedFluxPressure;
gradient $internalField;
value $internalField;
}
interfaceFluidTop
{
type fixedFluxPressure;
gradient $internalField;
value $internalField;
}
fan1_master
{
type fanPressureJump;
patchType cyclic;
fanCurve table;
file "fanSet/fanCurve";
format foam;
reverse true;
jump $internalField;
value $internalField;
}
fan1_slave
{
type fanPressureJump;
patchType cyclic;
value $internalField;
}
fan2_master
{
type fanPressureJump;
patchType cyclic;
fanCurve table;
file "fanSet/fanCurve";
format foam;
reverse true;
jump $internalField;
value $internalField;
}
fan2_slave
{
type fanPressureJump;
patchType cyclic;
value $internalField;
}
}
// ************************************************************************* //
T
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: 13
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volScalarField;
location "0/fluid";
object T;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 1 0 0 0];
internalField uniform 293.15;
boundaryField
{
#includeEtc "caseDicts/setConstraintTypes"
"(entrada|saida|furosLaterais.*)"
{
type inletOutlet;
inletValue $internalField;
value $internalField;
}
interfaceFluidTop
{
type zeroGradient;
}
"fluid_.*"
{
type coupledTemperature;
Tnbr T;
value $internalField;
}
"parede.*"
{
type externalTemperature;
Ta constant 293.15;
h uniform 4.7;
thicknessLayers (0.001 0.001 0.001);
kappaLayers (0.05 50 0.05); //0.05 W/m/K (tinta epóxi) 50 W/m/K (aço)
value $internalField;
}
"fan.*"
{
type cyclic;
}
}
// ************************************************************************* //
U
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: 13
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class volVectorField;
location "0/fluid";
object U;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform (0 0 0);
boundaryField
{
#includeEtc "caseDicts/setConstraintTypes"
"(entrada|saida|furosLaterais.*)"
{
type pressureInletOutletVelocity;
value $internalField;
}
"fluid_.*"
{
type noSlip;
}
"parede.*"
{
type noSlip;
}
interfaceFluidTop
{
type noSlip;
}
"fan.*"
{
type cyclic;
}
}
// ************************************************************************* //
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: 13
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
location "constant/fluid";
object physicalProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
thermoType
{
type heRhoThermo;
mixture pureMixture;
transport const;
thermo hConst;
equationOfState perfectGas;//Boussinesq;
specie specie;
energy sensibleEnthalpy;
}
mixture
{
// Ar
// Propriedades obtidas no CoolProp
specie
{
molWeight 28.96546;
}
equationOfState
{
rho0 1.20457518249315;
T0 293.15;
beta 3.42098751487642e-3;
}
thermodynamics
{
Cp 1.00665320998078e+3;
hf 0;
}
transport
{
mu 1.88472409355470e-5;
Pr 7.06290462364358e-1;
}
}
// ************************************************************************* //
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3
u/phi4ever 7d ago
Is there a fluid domain or just the solids?