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reactingFoam diverging nozzle convergence issues |
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#1 |
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New Member
Join Date: Nov 2024
Posts: 3
Rep Power: 2 ![]() |
Dear Foamers,
I'm new to OpenFOAM and trying to simulate a diverging nozzle with reactingFoam in OF v2312. After a month of testing different BC setups, I got a case running for Re=2000—only possible by mapping fields from a rhoPimpleFoam case with simpler geometry. This allowed me to work up to Re=5000, but issues arise at Re=7000. Regarding the geometry: the oxidizer inlet has a diameter of 2.5 mm, the outlet 9 mm, and the height is about 41 mm. At Re=7000, the inlet velocity is around 122 m/s. I read that for such speeds, enabling the Transonic option in the Pimple section is recommended. However, with this setting, I get floating point exceptions after about 100 iterations. I also noticed that my cumulative continuity error grows rapidly, although residuals seem to be on the right track. The main task is to achieve a homogenous mixing of H2 and Air at the outlet by changing the Fuel pipes (angle, height etc.) Best Luca |
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#2 |
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New Member
Join Date: Nov 2024
Posts: 3
Rep Power: 2 ![]() |
velocity
Code:
internalField uniform (0 122.994 0);
boundaryField
{
wall
{
type noSlip;
}
inlet
{
type fixedValue;
value uniform (0 122.994 0);
}
outlet
{
type pressureInletOutletVelocity;
value uniform (0 9.49 0);
inletValue uniform (0 0 0);
}
}
Code:
internalField uniform 101325;
boundaryField
{
wall
{
type zeroGradient;
}
inlet
{
type totalPressure;
p0 $internalField;
value $internalField;
}
outlet
{
type totalPressure;
p0 $internalField;
value $internalField;
}
}
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#3 |
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New Member
Join Date: Nov 2024
Posts: 3
Rep Power: 2 ![]() |
fvSchemes
Code:
ddtSchemes
{
default localEuler;
}
gradSchemes
{
default Gauss linear;
grad(U) cellLimited Gauss linear 0.333;
}
divSchemes
{
default none;
div(phi,U) bounded Gauss upwind;
div(U) bounded Gauss upwind;
div(phid,p) bounded Gauss upwind;
div(phi,K) bounded Gauss upwind;
div(phi,h) bounded Gauss upwind;
div(phi,(p|rho)) bounded Gauss upwind;
turbulence bounded Gauss upwind;
div(phi,k) $turbulence;
div(phi,epsilon) $turbulence;
div(phi,omega) $turbulence;
div(phi,R) $turbulence;
div((rho*R)) bounded Gauss linear;
div(R) bounded Gauss linear;
div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;
}
laplacianSchemes
{
default Gauss linear corrected;
}
interpolationSchemes
{
default linear;
}
snGradSchemes
{
default corrected;
}
Code:
solvers
{
p
{
solver GAMG;
tolerance 1e-06;
relTol 0.1;
smoother GaussSeidel;
nPreSweeps 0;
nPostSweeps 2;
cacheAgglomeration on;
agglomerator faceAreaPair;
nCellsInCoarsestLevel 1000;
mergeLevels 1;
}
pFinal
{
$p;
tolerance 1e-06;
relTol 0.01;
}
"(U|h|k|epsilon)"
{
solver smoothSolver;
smoother symGaussSeidel;
tolerance 1e-07;
relTol 0.01;
}
"(U|h|k|epsilon)Final"
{
$U;
tolerance 1e-07;
relTol 0.001;
}
rho
{
solver diagonal;
}
rhoFinal
{
solver diagonal;
}
}
PIMPLE
{
momentumPredictor yes;
nOuterCorrectors 2;
nCorrectors 3;
nNonOrthogonalCorrectors 1;
transonic yes;
pMaxFactor 1.5;
pMinFactor 0.9;
maxCo 0.2;
rDeltaTSmoothingCoeff 0.1;
rDeltaTDampingCoeff 1;
maxDeltaT 1;
}
relaxationFactors
{
fields
{
".*" 0.8;
"(U|h|p|k|epsilon).*" table ((0 0.85) (1000 0.9) (5000 0.7));
}
equation
{
".*" 0.8;
"(U|h|p|k|epsilon).*" table ((0 0.85) (1000 0.9) (5000 0.7));
}
}
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| Tags |
| convergence issues, nozzle simulation, reactingfoam, setup |
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