|
[Sponsors] |
ReactingFoam EDC v2016, calculation not converging |
|
LinkBack | Thread Tools | Search this Thread | Display Modes |
March 15, 2022, 05:13 |
ReactingFoam EDC v2016, calculation not converging
|
#1 |
New Member
Chris
Join Date: Nov 2021
Posts: 12
Rep Power: 5 |
Hey guys,
when I try to switch from EDC v2005 to v2016 in the DLR_A_LTS case, the pressure flucuates in the flame zone and the calculation doesn't converge. I'm using the Jones-Lindsted mechanism and these are my settings: chemistryProperties: Code:
chemistryType { solver EulerImplicit; method standard; } EulerImplicitCoeffs { cTauChem 1; equilibriumRateLimiter on; } Code:
combustionModel EDC; EDCCoeffs { version v2016; } Code:
solvers { "rho.*" { solver diagonal; } p { solver PCG; preconditioner DIC; tolerance 1e-6; relTol 0.01; } pFinal { $p; relTol 0; } "(U|h|k|epsilon)" { solver PBiCGStab; preconditioner DILU; tolerance 1e-6; relTol 0.1; } "(U|h|k|epsilon)Final" { $U; relTol 0; } "Yi.*" { solver PBiCG; preconditioner DILU; tolerance 1e-8; relTol 0; } } PIMPLE { momentumPredictor yes; nOuterCorrectors 1; nCorrectors 2; nNonOrthogonalCorrectors 0; maxDeltaT 1e-7; maxCo 0.025; alphaTemp 0.005; alphaY 0.005; Yref { O2 0.1; CH4 0.1; } rDeltaTSmoothingCoeff 0.05; rDeltaTDampingCoeff 0.2; } relaxationFactors { equations { ".*" 1.0; } } Code:
ddtSchemes { default localEuler; } gradSchemes { default Gauss linear; } divSchemes { default none; div(phi,U) Gauss limitedLinearV 1; div(phi,Yi) Gauss limitedLinear01 1; div(phi,h) Gauss limitedLinear 1; div(phi,K) Gauss limitedLinear 1; div(phid,p) Gauss limitedLinear 1; div(phi,epsilon) Gauss limitedLinear 1; div(phi,Yi_h) Gauss limitedLinear01 1; div(phi,k) Gauss limitedLinear 1; div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear; } laplacianSchemes { default Gauss linear orthogonal; } interpolationSchemes { default linear; } snGradSchemes { default orthogonal; } Code:
ELEMENTS H O C N END SPECIES CH4 O2 CO2 CO H2O H2 N2 H O OH END REACTIONS CAL/MOLE CH4 + 0.5O2 => CO+2H2 7.82E+13 0.0 30000 !1 FORD/CH4 0.5/ FORD/O2 1.25/ CH4 + H2O => CO+3H2 3.0E11 0.0 30000 !2 CO + H2O <=> CO2+H2 2.75E+12 0.0 20000 !3 H2 + 0.5O2 <=> H2O 1.209E+18 -1.0 40000 !4 FORD/H2 0.25/ FORD/O2 1.5/ O2 <=> 2O 1.5E+09 0.0 113000 !5 H2O <=> H + OH 2.3E+22 -3.0 120000 !6 END Does anyone have an Idea what could lead to this instability? |
|
March 15, 2022, 07:46 |
|
#2 |
Senior Member
Uwe Pilz
Join Date: Feb 2017
Location: Leipzig, Germany
Posts: 744
Rep Power: 15 |
1) Check your boundary conditions. Are they physical correct?
2) check your mesh 3) During the run: check maxCo and time step continuity error If all above is ok: 4) start with a more stable simulation: - first order schemes - underrelaxation If even that does not help: 5) start with a more stable physics - start with low Reynolds number (small velocity or high viscosity) - start with steady state calculation (simpleFoam) - start with laminar or even potential flow If you set runTimeModifialble you may change most of it during the run.
__________________
Uwe Pilz -- Die der Hauptbewegung überlagerte Schwankungsbewegung ist in ihren Einzelheiten so hoffnungslos kompliziert, daß ihre theoretische Berechnung aussichtslos erscheint. (Hermann Schlichting, 1950) |
|
March 15, 2022, 08:22 |
|
#3 |
New Member
Chris
Join Date: Nov 2021
Posts: 12
Rep Power: 5 |
Hello Uwe,
thank you very much for your fast reply. The case is part of the tutorials, why I assume that the BC's and mesh shouldn't be any problem. I tried to obey the other steps you suggested above and this is the result for the residual of the static pressure p. Despite getting smaller, the residual is still oscillating and doesn't converge. |
|
March 15, 2022, 12:37 |
|
#4 |
Senior Member
Uwe Pilz
Join Date: Feb 2017
Location: Leipzig, Germany
Posts: 744
Rep Power: 15 |
I only can repeat my advices. You switched to another model and this means you have a different case. Please increase complexity step by step.
__________________
Uwe Pilz -- Die der Hauptbewegung überlagerte Schwankungsbewegung ist in ihren Einzelheiten so hoffnungslos kompliziert, daß ihre theoretische Berechnung aussichtslos erscheint. (Hermann Schlichting, 1950) |
|
Tags |
edc, reactingfoam, v2016 |
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
calculation of thermal conductivity in reactingFoam | sto16 | OpenFOAM Running, Solving & CFD | 11 | April 25, 2017 00:46 |
Question about temperature calculation in reactingFoam?? | lfgmarc | OpenFOAM Programming & Development | 0 | December 27, 2011 22:55 |
Modeling the Sandia flame D with EDC | Christoph_84 | FLUENT | 1 | September 18, 2011 21:24 |
MRF and Heat transfer calculation | Susan YU | FLUENT | 0 | June 2, 2010 09:46 |
Warning 097- | AB | Siemens | 6 | November 15, 2004 05:41 |