[Marie_Dal]

Hello everyone,
I am new to OpenFoam. I am currently running a simulation of an airfoil using SimpleFoam with the turbulence model KomegaSST LM. After just a few iterations (4), the value of bounding omega (max) starts to be very high, which I believe is the reason why a warning appears a couple iterations after:

--> FOAM Warning :
From function Foam::tmp<Foam::DimensionedField<double, Foam::volMesh> > Foam::RASModels::kOmegaSSTLM<BasicMomentumTranspor tModel>::ReThetat0(const Internal&, const Internal&, const Internal&) const [with BasicMomentumTransportModel = Foam::IncompressibleMomentumTransportModel<Foam::k inematicTransportModel>; Foam::GeometricField<double, Foam::fvPatchField, Foam::volMesh>::Internal = Foam::DimensionedField<double, Foam::volMesh>]
in file ../momentumTransportModels/lnInclude/kOmegaSSTLM.C at line 300
Number of lambda iterations exceeds maxLambdaIter(10)

Now in my very little experience with this turbulence model, I believe this to be a boundary condition problem. I tried different values for omega, using wall functions for k, omega and nut, and also removing them, but nothing seems to work.

I tried turning my turbulence model back to the K omega SST, and the simulation runs without inconvenience, for which I assume the mesh is not the problem.

This is what an itertion with this warning looks like:

Time = 6

smoothSolver: Solving for Ux, Initial residual = 0.0493299, Final residual = 0.00422165, No Iterations 5
smoothSolver: Solving for Uy, Initial residual = 0.249744, Final residual = 0.0204515, No Iterations 4
GAMG: Solving for p, Initial residual = 0.107384, Final residual = 0.00826549, No Iterations 3
time step continuity errors : sum local = 0.000609625, global = -6.2441e-06, cumulative = -1.32525e-05
--> FOAM Warning :
From function Foam::tmp<Foam::DimensionedField<double, Foam::volMesh> > Foam::RASModels::kOmegaSSTLM<BasicMomentumTranspor tModel>::ReThetat0(const Internal&, const Internal&, const Internal&) const [with BasicMomentumTransportModel = Foam::IncompressibleMomentumTransportModel<Foam::k inematicTransportModel>; Foam::GeometricField<double, Foam::fvPatchField, Foam::volMesh>::Internal = Foam::DimensionedField<double, Foam::volMesh>]
in file ../momentumTransportModels/lnInclude/kOmegaSSTLM.C at line 300
Number of lambda iterations exceeds maxLambdaIter(10)
smoothSolver: Solving for ReThetat, Initial residual = 0.0628862, Final residual = 0.00492529, No Iterations 5
smoothSolver: Solving for gammaInt, Initial residual = 0.00826379, Final residual = 0.000491998, No Iterations 4
bounding gammaInt, min: -0.0724182 max: 1.11402 average: 0.963246
smoothSolver: Solving for omega, Initial residual = 0.0155426, Final residual = 0.00154728, No Iterations 6
bounding omega, min: -112.337 max: 2.47547e+10 average: 1.1801e+06
smoothSolver: Solving for k, Initial residual = 0.998501, Final residual = 7.2704e-05, No Iterations 1
ExecutionTime = 6.61 s ClockTime = 7 s



An error finally comes up after 18 iterations, when everything has already diverged:

Time = 18

smoothSolver: Solving for Ux, Initial residual = 0.730684, Final residual = 3.77352e+08, No Iterations 10
smoothSolver: Solving for Uy, Initial residual = 0.658047, Final residual = 3.8716e+08, No Iterations 10
#0 Foam::error::printStack(Foam::Ostream&) at ??:?
#1 Foam::sigFpe::sigHandler(int) at ??:?
#2 ? in "/lib/x86_64-linux-gnu/libc.so.6"
#3 Foam::GAMGSolver::scale(Foam::Field<double>&, Foam::Field<double>&, Foam::lduMatrix const&, Foam::FieldField<Foam::Field, double> const&, Foam::UPtrList<Foam::lduInterfaceField const> const&, Foam::Field<double> const&, unsigned char) const at ??:?
#4 Foam::GAMGSolver::Vcycle(Foam::PtrList<Foam::lduMa trix::smoother> const&, Foam::Field<double>&, Foam::Field<double> const&, Foam::Field<double>&, Foam::Field<double>&, Foam::Field<double>&, Foam::Field<double>&, Foam::Field<double>&, Foam::PtrList<Foam::Field<double> >&, Foam::PtrList<Foam::Field<double> >&, unsigned char) const at ??:?
#5 Foam::GAMGSolver::solve(Foam::Field<double>&, Foam::Field<double> const&, unsigned char) const at ??:?
#6 Foam::fvMatrix<double>::solveSegregated(Foam::dict ionary const&) at ??:?
#7 Foam::fvMatrix<double>::solve(Foam::dictionary const&) in "/opt/openfoam9/platforms/linux64GccDPInt32Opt/bin/simpleFoam"
#8 Foam::fvMatrix<double>::solve() in "/opt/openfoam9/platforms/linux64GccDPInt32Opt/bin/simpleFoam"
#9 ? in "/opt/openfoam9/platforms/linux64GccDPInt32Opt/bin/simpleFoam"
#10 __libc_start_main in "/lib/x86_64-linux-gnu/libc.so.6"
#11 ? in "/opt/openfoam9/platforms/linux64GccDPInt32Opt/bin/simpleFoam"



I have faced very similar problems with other simulations, but changing boundary conditions (usually rising the value for omega) has always seemed to fix them. Yet, no matter what I try with this simulation, I can't seem to fix it.

I very much appreciate anyone's advice. I attach below boundary conditions and gradient schemes.

Thank you. :)

BOUNDARY CONDITIONS:

GammaInt:

internalField uniform 1;
boundaryField
{ inlet { type fixedValue;
value $internalField; }
outlet
{ type zeroGradient; }
walls
{ type zeroGradient; }
airfoil
{ type zeroGradient; }
frontAndBackPlanes
{ type empty; } }


K:
internalField uniform 0.00135;

boundaryField
{ inlet
{ type fixedValue;
value uniform 0.00135; }
outlet
{ type zeroGradient; }
airfoil
{ type fixedValue;
value uniform 1e-6; }
walls
{ type zeroGradient; }
frontAndBackPlanes
{ type empty; }}

nut
internalField uniform 0.0020125;

boundaryField
{ inlet { type freestream;
freestreamValue uniform 0.0020125; }

outlet { type freestream;
freestreamValue uniform 0.0020125; }

airfoil { type nutkWallFunction;
value uniform 0.00000020125; }

walls { type zeroGradient; }

frontAndBackPlanes { type empty; }}


OMEGA:
dimensions [0 0 -1 0 0 0 0];

internalField uniform 2.6708;

boundaryField
{ inlet { type fixedValue;
value $internalField; }

outlet { type zeroGradient; }

airfoil { type omegaWallFunction;
value $internalField; }

walls { type zeroGradient; }

frontAndBackPlanes { type empty; }}



ReThetaT
internalField uniform 1170.563958;
boundaryField
{ inlet { type fixedValue;
value $internalField; }

outlet { type zeroGradient; }

walls { type zeroGradient; }

airfoil { type zeroGradient; }

frontAndBackPlanes { type empty; }}

For U and P I use freeStream and no slip conditions on the airfoil, altough those boundary conditions are vastly tested and I am certain those are not the problem.

[akamal1099]

Hello my friend
did you find a solution?? I am experiencing this problem now.
Thanks

[em17]

Hi, I am also having the exact same error. Has anyone managed to fix it?

Thanks, Em

[akamal1099]

Hello,
I did manage to fix it.

1. Don't take y+ to be 1. Instead, take it to be >30 so you can use wall function for turbulence quantities
2. I setted the inlet and outlet in one group and called it freestream
3. Make sure you have the right boundary conditions for ReTheta and Gamma. You can check in openfoam wiki

I will upload my boundary files. But again I tried a lot to do the analysis with y+ = 1 but I couldn't. Some experts told me it a mesh problem even thought my mesh was fine per checkMesh. But there point was that if you are solving a 2D problem (only one cell in z direction throughout the whole mesh), the solver will experience such issues. So, I worked with y+>30 and I used wall fucntions

Hope it help.
Thanks

[akamal1099]

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