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-   -   LTSInterFoam and pressure driven flow (http://www.cfd-online.com/Forums/openfoam/97410-ltsinterfoam-pressure-driven-flow.html)

Andrea_85 February 16, 2012 10:01

LTSInterFoam and pressure driven flow
 
Hi,
I have successfully simulated a pressure driven flow using interFoam. My domain is 2D and it has an inlet and an outlet, the rest are walls. The BC i set for this case were:

inlet
p_rgh fixedValue uniform 100
U pressureInletUniformVelocity
alpha1 fixedValue uniform 1

outlet
p_rgh fixedValue uniform 0;
U pressureInletOutletVelocity;
alpha1 zeroGradient;

walls
p_rgh fixedFluxPressure; adjoint no;
U fixedValue (0 0 0);
alpha constantAlphaContactAngle;

The simulation works fine with this setting. Now i would like to compare the results with the new multiphase steady state solver: LTSInterFoam.
I set up the case using exactly the same BC as before and i copied fvSolution from the wigleyHull test case. I get a floating point error immediately after the first iteration:

Code:

15] #1  Foam::sigFpe::sigHandler(int) in "/home/aferrari/OpenFOAM/OpenFOAM-2.1.0/platforms/linux64GccDPOpt/lib/libOpenFOAM.so"
[15] #2  ?? in "/lib64/libc.so.6"
[15] #3  Foam::GaussSeidelSmoother::smooth(Foam::word const&, Foam::Field<double>&, Foam::lduMatrix const&, Foam::Field<double> const&, Foam::FieldField<Foam::Field, double> const&, Foam::UPtrList<Foam::lduInterfaceField const> const&, unsigned char, int) in "/home/aferrari/OpenFOAM/OpenFOAM-2.1.0/platforms/linux64GccDPOpt/lib/libOpenFOAM.so"
[15] #4  Foam::GaussSeidelSmoother::smooth(Foam::Field<double>&, Foam::Field<double> const&, unsigned char, int) const in "/home/aferrari/OpenFOAM/OpenFOAM-2.1.0/platforms/linux64GccDPOpt/lib/libOpenFOAM.so"
[15] #5  Foam::smoothSolver::solve(Foam::Field<double>&, Foam::Field<double> const&, unsigned char) const in "/home/aferrari/OpenFOAM/OpenFOAM-2.1.0/platforms/linux64GccDPOpt/lib/libOpenFOAM.so"
[15] #6  Foam::fvMatrix<Foam::Vector<double> >::solve(Foam::dictionary const&) in "/home/aferrari/OpenFOAM/OpenFOAM-2.1.0/platforms/linux64GccDPOpt/bin/LTSInterFoam"
[15] #7  Foam::fvMatrix<Foam::Vector<double> >::solve() in "/home/aferrari/OpenFOAM/OpenFOAM-2.1.0/platforms/linux64GccDPOpt/bin/LTSInterFoam"
[15] #8  main in "/home/aferrari/OpenFOAM/OpenFOAM-2.1.0/platforms/linux64GccDPOpt/bin/LTSInterFoam"
[15] #9  __libc_start_main in "/lib64/libc.so.6"
[15] #10  Foam::regIOobject::writeObject(Foam::IOstream::streamFormat, Foam::IOstream::versionNumber, Foam::IOstream::compressionType) const in "/home/aferrari/OpenFOAM/OpenFOAM-2.1.0/platforms/linux64GccDPOpt/bin/LTSInterFoam"
[node11:27114] *** Process received signal ***
[node11:27114] Signal: Floating point exception (8)
[node11:27114] Signal code:  (-6)
[node11:27114] Failing at address: 0x3f5000069ea
[node11:27114] [ 0] /lib64/libc.so.6 [0x2b730bb0a2d0]
[node11:27114] [ 1] /lib64/libc.so.6(gsignal+0x35) [0x2b730bb0a265]
[node11:27114] [ 2] /lib64/libc.so.6 [0x2b730bb0a2d0]
[node11:27114] [ 3] /home/aferrari/OpenFOAM/OpenFOAM-2.1.0/platforms/linux64GccDPOpt/lib/libOpenFOAM.so(_ZN4Foam19GaussSeidelSmoother6smoothERKNS_4wordERNS_5FieldIdEERKNS_9lduMatrixERKS5_RKNS_10FieldFieldIS4_dEERKNS_8UPtrListIKNS_17lduInterfaceFieldEEEhi+0x62e) [0x2b730ac3e6de]
[node11:27114] [ 4] /home/aferrari/OpenFOAM/OpenFOAM-2.1.0/platforms/linux64GccDPOpt/lib/libOpenFOAM.so(_ZNK4Foam19GaussSeidelSmoother6smoothERNS_5FieldIdEERKS2_hi+0x2d) [0x2b730ac3e9cd]
[node11:27114] [ 5] /home/aferrari/OpenFOAM/OpenFOAM-2.1.0/platforms/linux64GccDPOpt/lib/libOpenFOAM.so(_ZNK4Foam12smoothSolver5solveERNS_5FieldIdEERKS2_h+0x336) [0x2b730ac36c36]
[node11:27114] [ 6] LTSInterFoam [0x4a1309]
[node11:27114] [ 7] LTSInterFoam [0x4a22c3]
[node11:27114] [ 8] LTSInterFoam [0x431274]
[node11:27114] [ 9] /lib64/libc.so.6(__libc_start_main+0xf4) [0x2b730baf7994]
[node11:27114] [10] LTSInterFoam(_ZNK4Foam11regIOobject11writeObjectENS_8IOstream12streamFormatENS1_13versionNumberENS1_15compressionTypeE+0x121) [0x425949]
[node11:27114] *** End of error message ***

The problem is that alpha1 is not bounded between 0 and 1 and it assumes ridiculous values. See the log file below

Code:

Flow time scale min/max = 1, 1
Smoothed flow time scale min/max = 1, 1
MULES: Solving for alpha1
Liquid phase volume fraction = 0.0444861  Min(alpha1) = 0  Max(alpha1) = 1
MULES: Solving for alpha1
Liquid phase volume fraction = 0.0444861  Min(alpha1) = 0  Max(alpha1) = 1
MULES: Solving for alpha1
Liquid phase volume fraction = 0.0444861  Min(alpha1) = 0  Max(alpha1) = 1

smoothSolver:  Solving for Ux, Initial residual = 0.998308, Final residual = 1.15882e-05, No Iterations 1000
smoothSolver:  Solving for Uy, Initial residual = 1, Final residual = 0.000162056, No Iterations 1000
GAMG:  Solving for p_rgh, Initial residual = 1, Final residual = 0.00986187, No Iterations 9
GAMG:  Solving for p_rgh, Initial residual = 0.0015966, Final residual = 1.29717e-05, No Iterations 13
time step continuity errors : sum local = 0.00770126, global = -0.000948279, cumulative = -0.000948279
GAMG:  Solving for p_rgh, Initial residual = 0.0400645, Final residual = 0.000289038, No Iterations 11
GAMG:  Solving for p_rgh, Initial residual = 0.0323362, Final residual = 0.000266529, No Iterations 11
time step continuity errors : sum local = 0.00667514, global = 0.000862335, cumulative = -8.59436e-05
GAMG:  Solving for p_rgh, Initial residual = 0.110602, Final residual = 0.000707688, No Iterations 7
GAMG:  Solving for p_rgh, Initial residual = 0.0013311, Final residual = 8.2218e-08, No Iterations 31
time step continuity errors : sum local = 1.97485e-06, global = 2.71952e-07, cumulative = -8.56717e-05
ExecutionTime = 0.92 s  ClockTime = 1 s

 MassFlows:  top = -4.91653e-09  bottom = 4.91654e-09
 Averages of p_rgh :  top = 100  bottom = 0
Time = 2

Flow time scale min/max = 1, 1
Smoothed flow time scale min/max = 1, 1
MULES: Solving for alpha1
Liquid phase volume fraction = 0.0899103  Min(alpha1) = -170.294  Max(alpha1) = 64.7941
MULES: Solving for alpha1
Liquid phase volume fraction = 0.135334  Min(alpha1) = -32767.5  Max(alpha1) = 29184.1
MULES: Solving for alpha1
Liquid phase volume fraction = 0.180754  Min(alpha1) = -7.28461e+06  Max(alpha1) = 1.19618e+07

Here my fvSolution

Code:

pcorr
    {
        solver          PCG;

    preconditioner
        {
            preconditioner  GAMG;
   
            smoother        DICGaussSeidel;
            agglomerator    faceAreaPair;
            mergeLevels    1;
            nCellsInCoarsestLevel 10;
            cacheAgglomeration true;

            tolerance      1e-6;
            relTol          0;
        };
   
        tolerance      1e-6;
        relTol          0;
    };
       
    p_rgh
    {
        solver          GAMG;
       
        smoother        GaussSeidel;
        agglomerator    faceAreaPair;
        mergeLevels    1;
        nCellsInCoarsestLevel 10;
        cacheAgglomeration true;

        tolerance    1e-7;
        relTol          0.01;
    };
       
    p_rghFinal
    {
        $p_rgh;
        tolerance    1e-7;
        relTol          0;
    }
   
    "U.*"
    {
        solver          smoothSolver;
       
        smoother        GaussSeidel;
        nSweeps        1;
   
        tolerance    1e-8;
        relTol          0;
    };

I got the same error using PCG for both pressure and velocity.
What am I doing wrong? How can i fix it?

Best Regards

andrea

Ralph M August 17, 2012 02:20

Hi Andrea,

Maybe a stupid question but did you change the MULES-files?

Ralph

Andrea_85 August 20, 2012 03:55

Hi Ralph,
what you mean exactly? I used the tutorial case of LTSInterFoam as a starting point for my simulation, chianging just the geometry and the physical properties.

best

andrea

Ralph M August 21, 2012 08:44

Hi Andrea,

In that case you please don't mind. I was looking for methods to influence/limit maxAlpha to 1, through Google I found your post but apparently you have other problems to solve.

Because of the quick blow-up of your computations your boundary conditions might be inappropiate? And how looks the rest of your FvSolutions file?

Regards,

Ralph


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