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Highly unstable buoyantPimpleFoam simulation

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Old   September 27, 2019, 03:25
Default Highly unstable buoyantPimpleFoam simulation
  #1
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Piotr Ładyński
Join Date: Apr 2017
Posts: 55
Rep Power: 9
piotr.mecht is on a distinguished road
Simulation background
========================
I'm trying to perform a buoyantPimpleFoam simulation, but it quickly goes unstable in the first timesteps. The goal is to estimate inlet water jet deviation in domestic hot water tank possibly with different initial conditions and dimensions.

Flow conditions:
initial water temperature (internalField) 42°C
inlet water temperature 20°C
inlet/outlet connector diameter 0.023 m
tank diameter 0.45 m
connectors distance 1.0 m
water flow 3 l/min -> ~0.12 m/s on average (~0.15 m/s max with distributed profile)

Problem solution history
========================
I've tried do reduce timestep, but my Courant number didn't get any smaller.
I also thought my mesh might be bad, because of some concave cells or some single cells with low determinant (checkMesh results), but concave cells are often hard to avoid with snappyHexMesh and they seem to be acceptable in many cases.
I tried to run the same case with fine tetmesh + layers addition + several nOrthogonalCorrectors, but the tendency was the same, so i think now that some other settings might be wrong or they require more tuning.
I blindly played with some fvSolution and fvSchemes, but with similiar results.

Residuals
========================
Enthaply residual in each timestep starts with 1, when static pressure isn't initialized so i helped it with funkySetFields, its initial value reduced significantly but it starts with ~0.7 initial value in second iteration
p_rgh initial residual is >0.4 it seems to be high but it goes serveral orders of magnitude lower in piso and pimple loop (I don't think I understand this output clearly)
Second iteration starts with low max Courant number e.g. ~0.2 , but third or fourth instantly goes to ~100
Omega goes wild in the second iteration with minimum negative value and maximum value of >4.5E+4
Solver crashes whith being unable to converge correct

Output example:
Code:
Starting time loop

Courant Number mean: 1.49349e-08 max: 0.02674
Time = 0.0001

diagonal:  Solving for rho, Initial residual = 0, Final residual = 0, No Iterations 0
DILUPBiCG:  Solving for Ux, Initial residual = 1, Final residual = 5.48763e-08, No Iterations 3
DILUPBiCG:  Solving for Uy, Initial residual = 1, Final residual = 1.80726e-08, No Iterations 3
DILUPBiCG:  Solving for Uz, Initial residual = 1, Final residual = 2.18823e-08, No Iterations 3
DILUPBiCG:  Solving for h, Initial residual = 0.000321462, Final residual = 1.67432e-07, No Iterations 1
DICPCG:  Solving for p_rgh, Initial residual = 0.996965, Final residual = 0.00952103, No Iterations 479
DICPCG:  Solving for p_rgh, Initial residual = 0.000555127, Final residual = 5.38467e-06, No Iterations 86
DICPCG:  Solving for p_rgh, Initial residual = 5.38737e-06, Final residual = 5.28314e-08, No Iterations 167
DICPCG:  Solving for p_rgh, Initial residual = 5.28319e-08, Final residual = 9.66085e-09, No Iterations 392
[...char limit]
diagonal:  Solving for rho, Initial residual = 0, Final residual = 0, No Iterations 0
time step continuity errors : sum local = 1.32918e-13, global = -9.31681e-17, cumulative = 3.77663e-16
DICPCG:  Solving for p_rgh, Initial residual = 0.0396398, Final residual = 0.000376473, No Iterations 479
DICPCG:  Solving for p_rgh, Initial residual = 0.000235303, Final residual = 2.23339e-06, No Iterations 85
DICPCG:  Solving for p_rgh, Initial residual = 2.23373e-06, Final residual = 2.03148e-08, No Iterations 170
DICPCG:  Solving for p_rgh, Initial residual = 2.0315e-08, Final residual = 9.81896e-09, No Iterations 378
diagonal:  Solving for rho, Initial residual = 0, Final residual = 0, No Iterations 0
time step continuity errors : sum local = 1.35542e-13, global = -1.49899e-17, cumulative = 3.62673e-16
DILUPBiCG:  Solving for omega, Initial residual = 1.47021e-05, Final residual = 4.75973e-09, No Iterations 1
bounding omega, min: -52.5363 max: 95779.9 average: 224.474
DILUPBiCG:  Solving for k, Initial residual = 1, Final residual = 2.35803e-08, No Iterations 3
ExecutionTime = 215.67 s  ClockTime = 216 s

Courant Number mean: 1.90016e-05 max: 0.239056
Time = 0.0002

diagonal:  Solving for rho, Initial residual = 0, Final residual = 0, No Iterations 0
DILUPBiCG:  Solving for Ux, Initial residual = 0.0965107, Final residual = 1.40458e-09, No Iterations 2
DILUPBiCG:  Solving for Uy, Initial residual = 0.233133, Final residual = 3.71724e-09, No Iterations 2
DILUPBiCG:  Solving for Uz, Initial residual = 0.238017, Final residual = 1.34334e-09, No Iterations 2
DILUPBiCG:  Solving for h, Initial residual = 0.608475, Final residual = 9.47492e-10, No Iterations 2
DICPCG:  Solving for p_rgh, Initial residual = 0.488246, Final residual = 0.00484784, No Iterations 461
DICPCG:  Solving for p_rgh, Initial residual = 2.29527e-05, Final residual = 2.23269e-07, No Iterations 87
DICPCG:  Solving for p_rgh, Initial residual = 2.23269e-07, Final residual = 9.84747e-09, No Iterations 85
DICPCG:  Solving for p_rgh, Initial residual = 9.84746e-09, Final residual = 9.84746e-09, No Iterations 0
diagonal:  Solving for rho, Initial residual = 0, Final residual = 0, No Iterations 0
time step continuity errors : sum local = 3.94984e-11, global = -1.08582e-13, cumulative = -1.08219e-13
[...skipped some for character limit]]
DILUPBiCG:  Solving for omega, Initial residual = 9.8383e-06, Final residual = 2.19925e-07, No Iterations 1
bounding omega, min: -328.374 max: 95813.5 average: 225.052
DILUPBiCG:  Solving for k, Initial residual = 0.0024148, Final residual = 3.30216e-07, No Iterations 4
ExecutionTime = 335.97 s  ClockTime = 336 s

Courant Number mean: 0.00278018 max: 77.708
Time = 0.0003

diagonal:  Solving for rho, Initial residual = 0, Final residual = 0, No Iterations 0
DILUPBiCG:  Solving for Ux, Initial residual = 0.00294713, Final residual = 5.09134e-07, No Iterations 5
DILUPBiCG:  Solving for Uy, Initial residual = 0.0498396, Final residual = 1.30056e-07, No Iterations 9
DILUPBiCG:  Solving for Uz, Initial residual = 0.245217, Final residual = 8.18823e-07, No Iterations 8
DILUPBiCG:  Solving for h, Initial residual = 0.999938, Final residual = 5.25371e-07, No Iterations 3
DICPCG:  Solving for p_rgh, Initial residual = 0.869755, Final residual = 0.00846313, No Iterations 487
DICPCG:  Solving for p_rgh, Initial residual = 5.09343e-05, Final residual = 4.87965e-07, No Iterations 88
DICPCG:  Solving for p_rgh, Initial residual = 4.87965e-07, Final residual = 9.50119e-09, No Iterations 78
DICPCG:  Solving for p_rgh, Initial residual = 9.50298e-09, Final residual = 9.50298e-09, No Iterations 0
diagonal:  Solving for rho, Initial residual = 0, Final residual = 0, No Iterations 0
[...]
time step continuity errors : sum local = 1.18932e-09, global = 4.01695e-11, cumulative = 4.48692e-11
DICPCG:  Solving for p_rgh, Initial residual = 0.0262778, Final residual = 0.000244534, No Iterations 513
DICPCG:  Solving for p_rgh, Initial residual = 0.000155778, Final residual = 1.50242e-06, No Iterations 79
DICPCG:  Solving for p_rgh, Initial residual = 1.50243e-06, Final residual = 1.48662e-08, No Iterations 215
DICPCG:  Solving for p_rgh, Initial residual = 1.48865e-08, Final residual = 9.91452e-09, No Iterations 4
diagonal:  Solving for rho, Initial residual = 0, Final residual = 0, No Iterations 0
time step continuity errors : sum local = 1.14702e-09, global = 1.97249e-11, cumulative = 6.45941e-11
DILUPBiCG:  Solving for omega, Initial residual = 0.999996, Final residual = 4.51237e-08, No Iterations 8
bounding omega, min: -154.316 max: 1.68053e+13 average: 4.75822e+08
DILUPBiCG:  Solving for k, Initial residual = 0.965169, Final residual = 5.95112e-07, No Iterations 7
ExecutionTime = 508.91 s  ClockTime = 510 s

Courant Number mean: 0.3024 max: 2550.14
Time = 0.0004

diagonal:  Solving for rho, Initial residual = 0, Final residual = 0, No Iterations 0
DILUPBiCG:  Solving for Ux, Initial residual = 0.0150419, Final residual = 5.99711e-07, No Iterations 11
DILUPBiCG:  Solving for Uy, Initial residual = 0.236398, Final residual = 4.35313e-07, No Iterations 15
DILUPBiCG:  Solving for Uz, Initial residual = 0.312253, Final residual = 2.32705e-07, No Iterations 15
DILUPBiCG:  Solving for h, Initial residual = 0.99989, Final residual = 6.77965e-07, No Iterations 6

    From function Foam::scalar Foam::species::thermo<Thermo, Type>::T(Foam::scalar, Foam::scalar, Foam::scalar, Foam::scalar (Foam::species::thermo<Thermo, Type>::*)(Foam::scalar, Foam::scalar) const, Foam::scalar (Foam::species::thermo<Thermo, Type>::*)(Foam::scalar, Foam::scalar) const, Foam::scalar (Foam::species::thermo<Thermo, Type>::*)(Foam::scalar) const, bool) const [with Thermo = Foam::hPolynomialThermo<Foam::icoPolynomial<Foam::specie> >; Type = Foam::sensibleEnthalpy; Foam::scalar = double; Foam::species::thermo<Thermo, Type> = Foam::species::thermo<Foam::hPolynomialThermo<Foam::icoPolynomial<Foam::specie> >, Foam::sensibleEnthalpy>]
    in file /home/ubuntu/OpenFOAM/OpenFOAM-dev/src/thermophysicalModels/specie/lnInclude/thermoI.H at line 70
    Energy -> temperature conversion failed to converge:
          [0] iter          Test           e/h          Cv/p          Tnew
          [0] 0       316.267   2.73901e+06          4200      -341.927
          [0] 1      -341.927  -3.12693e+06          4200        396.53
          [0] 2        396.53   3.20771e+06          4200       -373.26
          [0] 3       -373.26  -3.19648e+06          4200       381.757
          [0] 4       381.757   3.11801e+06          4200      -366.676
          [0] 5      -366.676  -3.18078e+06          4200       384.601
          [0] 6       384.601   3.13528e+06          4200      -367.945
          [0] 7      -367.945  -3.18376e+06          4200       384.043
          [char limit saving]
          [0] 100       384.135   3.13245e+06          4200      -367.737
          [0] 101      -367.737  -3.18327e+06          4200       384.135
          [1] iter          Test           e/h          Cv/p          Tnew
          [1] 0       317.791   1.11566e+07          4200      -1245.64
          [1] 1      -1245.64  -6.61605e+06          4200       1422.51
          [1] 2       1422.51   5.20461e+06          4200       1276.22
          [1] 3       1276.22   4.85664e+06          4200       1212.77
          [...]
          [1] 98       1104.47    4.7527e+06          4200       1065.77
          [1] 99       1065.77   4.81153e+06          4200       1013.06
          [1] 100       1013.06   4.96851e+06          4200       922.981
          [1] 101       922.981   5.52505e+06          4200        700.39
--------------------------------------------------------------------------
MPI_ABORT was invoked on rank 0 in communicator MPI COMMUNICATOR 3 SPLIT FROM 0
with errorcode 1.
Problem
========================
No clue on how to make anything work. Are my BCs ok? Is my thermophysicalProperties entry any wrong? Should i change anything in fv* dictionaries? Is my mesh to coarse maybe? It's already several milion cells!

========================
Thermophysical
Code:
thermoType
{
    type            heRhoThermo;
    mixture         pureMixture;
    transport       polynomial;
    thermo          hPolynomial;
    equationOfState icoPolynomial;
    specie          specie;
    energy          sensibleEnthalpy;
}

pRef            100000;
//dpdt off;

mixture
{
    specie
    {
        molWeight       18;
    }
    equationOfState
    {
        rhoCoeffs<8> (117.045534 7.913913 -0.02254739 1.97987E-05 0 0 0 0);
    }
    thermodynamics
    {
        Hf              0;
        Sf                0;
        CpCoeffs<8> (4200 0 0 0 0 0 0 0);
        
    }
    transport
    {
        muCoeffs<8> (0.1368992 -0.0012040579 3.5597468E-06 -3.526231E-09 0 0 0 0);
        kappaCoeffs<8> (-2.4283206 0.0233779 -5.9953665E-05 5.2602452E-08 0 0 0 0);
    }
}


// ************************************************************************* //
p_rgh
Code:
internalField   uniform 1E+5;

boundaryField
{
    Inlet
    {
        type            fixedFluxPressure;
        gradient        uniform 0;
        value           $internalField;
    }
    Outlet
    {
        type            fixedValue;
        value           $internalField;
    }
    Mantle
    {
        type            fixedFluxPressure;
        gradient        uniform 0;
        value           $internalField;
    }
    Connectors
    {
        type            fixedFluxPressure;
        gradient        uniform 0;
        value           $internalField;
    }
    SymmetryY
    {
        type            symmetry;
    }
    
}
p
Code:
internalField   uniform 1E+5; // initialize with funkySetFields

boundaryField
{
    Inlet
    {
        type            calculated;
        value            $internalField;
    }
    Outlet
    {
        type            calculated;
        value            $internalField;
    }
    Mantle
    {
        type            calculated;
        value            $internalField;
    }
    Connectors
    {
        type            calculated;
        value            $internalField;
    }
    SymmetryY
    {
        type            symmetry;
    }
    
}
velocity
Code:
internalField   uniform (0 0 0);

boundaryField
{
    Inlet
    {
        type            groovyBC;
        //valueExpression "vector(0.015*pow((1-(sqrt(pow(pos().z,2)+pow(pos().y,2))/0.0115)),0.14),0,0)";
        valueExpression "vector(0.15*pow((1-(sqrt(pow(pos().z,2)+pow(pos().y,2))/0.0115)),0.14),0,0)";
        value           uniform (0.12 0 0);
    }
    Outlet
    {
        type            zeroGradient;
    }
    Mantle
    {
        type            noSlip;
    }
    Connectors
    {
        type            noSlip;
    }
    SymmetryY
    {
        type            symmetry;
    }

}
omega
Code:
internalField   uniform 0.937;

boundaryField
{
    Inlet
    {
        type            fixedValue;
        value           uniform 0.937;
    }
    Outlet
    {
        type            zeroGradient;
    }
    Mantle
    {
        type            omegaWallFunction;
        value           uniform 0.937;
        
    }
    Connectors
    {
        type            omegaWallFunction;
        value           uniform 0.937;
    }
    SymmetryY
    {
        type            symmetry;
    }
    
}
k
Code:
internalField   uniform 8.44E-5;

boundaryField
{
    Inlet
    {
        type            fixedValue;        
        value           $internalField;
        
    }
    Outlet
    {
        type            zeroGradient;
    }
    Mantle
    {
        type            kLowReWallFunction;// kqRWallFunction;
        value           $internalField;
        
    }
    Connectors
    {
        type            kLowReWallFunction;// kqRWallFunction;
        value           $internalField;
        
    }
    SymmetryY
    {
        type            symmetry;
    }
    
}
nut
Code:
internalField   uniform 0;

boundaryField
{
    Inlet
    {
        type            calculated;        
        value           $internalField;
    }
    Outlet
    {
        type            calculated;
        value           $internalField;
    }
    Mantle
    {
        type            nutLowReWallFunction; // nutkWallFunction; // nutLowReWallFunction
        value           uniform 0;
        
    }
    Connectors
    {
        type            nutLowReWallFunction; // nutkWallFunction;
        value           uniform 0;
    }
    SymmetryY
    {
        type            symmetry;
    }
    
}
T
Code:
internalField   uniform 315.15;

boundaryField
{
    Inlet
    {
        type            fixedValue;
        value           uniform 293.15;
        
    }
    Outlet
    {
        type            zeroGradient; //inletOutlet;
        //inletValue      315.15 ;//$internalField;
        //value           $internalField;
    }
    Mantle
    {
        type            zeroGradient;
    }
    Connectors
    {
        type            zeroGradient;
    }
    SymmetryY
    {
        type            symmetry;
    }
    
}
alphat
Code:
internalField   uniform 0;

boundaryField
{
    Inlet
    {
        type            calculated;
        value           uniform 0;
    }
    Outlet
    {
        type            calculated;
        value           uniform 0;
    }
    Mantle
    {
        type            compressible::alphatJayatillekeWallFunction;
        Prt             0.85;
        value           uniform 0;
    }
    Connectors
    {
        type            compressible::alphatJayatillekeWallFunction;
        Prt             0.85;
        value           uniform 0;
    }
    SymmetryY
    {
        type            symmetry;  
    }
    
}
fvSolution
Code:
solvers
{
    cellDisplacement // OpenFOAM+ only
    {
        solver          GAMG;
        smoother        GaussSeidel;
        tolerance       1E-07;
        relTol          0.01;
    }
    
    
    "rho.*"
    {
        solver          PCG;
        preconditioner  DIC;
        tolerance       0;
        relTol          0;
    }

    p_rgh
    {
        solver          PCG;
        preconditioner  DIC;
        tolerance       1e-8;
        relTol          0.01;
        maxIter            2000;    // non-default
    }

    p_rghFinal
    {
        $p_rgh;
        relTol          0;
    }

    omega
    {
        solver          PBiCGStab; // PBiCGStab;
        preconditioner  DILU;
        tolerance       1e-7;
        relTol          0.1;
    }
    
    h
    {
        solver          PBiCGStab; // PBiCGStab;
        preconditioner  DILU;
        tolerance       1e-7;
        relTol          0.01;
    }

    "(U|h|e|k|R)"
    {
        solver          PBiCG; // PBiCGStab;
        preconditioner  DILU;
        tolerance       1e-6;
        relTol          0.1;
        maxIter         1500;
    }

    "(U|h|e|k|omega|R)Final"
    {
        $U;
        relTol          0;
    }
}


PIMPLE
{
    momentumPredictor yes;
    nOuterCorrectors 1; //3;
    nCorrectors     4; //3
    nNonOrthogonalCorrectors 1; // 0;
    pRefCell        0;
    pRefValue       1e5;
}

relaxationFactors
{
    fields
    {
        p_rgh 0.6;
        p 0.6;
        rho 0.6;
    }
equations
    {
        "U.*" 0.7;
        "rho.*" 0.7;
        "p_rgh.*" 0.7;
        "epsilon" 0.3;
        "omega" 0.3;
        "h" 0.5;
        "k" 0.6;
    }
}
fvSchemes
Code:
ddtSchemes
{
    default         Euler;
}

gradSchemes
{
    default         Gauss linear;
}

divSchemes
{
    default         none;
    
    div(phi,U)      Gauss linearUpwindV grad(U);
    div(phi,h)      Gauss linearUpwind grad(U);
    div(phi,e)      Gauss linearUpwind grad(U);
    div(phi,k)      Gauss linearUpwind grad(omega);
    div(phi,omega)  Gauss linearUpwind grad(omega);
    div(phi,R)      Gauss linearUpwind grad(U);
    div(phi,K)      Gauss linearUpwind grad(U);
    div(phi,Ekp)    Gauss linearUpwind grad(U);
    div(R)          Gauss linearUpwind grad(U);
    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;   
}

laplacianSchemes
{
    default            Gauss linear uncorrected;
    laplacian(1,p)     Gauss linear corrected;
}

interpolationSchemes
{
    default         linear;
}

snGradSchemes
{
    default         corrected;
}

wallDist
{
    method meshWave;
}

fluxRequired
{
    default no;
    p_rgh;
}

// ************************************************************************* //
Attached Images
File Type: png meshExample.png (93.5 KB, 56 views)
File Type: png connectorShape.png (50.1 KB, 46 views)
File Type: png Omega03.png (157.8 KB, 58 views)
Attached Files
File Type: zip tankDHW01.zip (25.7 KB, 6 views)
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Old   May 20, 2020, 07:38
Default
  #2
New Member
 
Khaled Yassin
Join Date: Aug 2019
Location: Jülich-Germany
Posts: 12
Rep Power: 6
Yassin-K is on a distinguished road
Hi piotr.mecht,

Have you found the soultion of this problem??
__________________
--
Best Regards,

Khaled Yassin,
Research Assistant
Institute for Energy and Environmental Research (IEK-14)
Forschungszentrum Jülich
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Old   May 23, 2020, 09:15
Default
  #3
Member
 
Piotr Ładyński
Join Date: Apr 2017
Posts: 55
Rep Power: 9
piotr.mecht is on a distinguished road
Yes!

As the fluid i tried to simulate (water) was changing its density only due to temperature changes, the solver was having hard time trying to calculate pressure-work term.


From OpenFOAM-v1906 source code energy equation looks like:

Code:
fvScalarMatrix EEqn
    (
        fvm::ddt(rho, he) + fvm::div(phi, he)
      + fvc::ddt(rho, K) + fvc::div(phi, K)
      + (
            he.name() == "e"
          ? fvc::div
            (
                fvc::absolute(phi/fvc::interpolate(rho), U),
                p,
                "div(phiv,p)"
            )
          : -dpdt
        )
      - fvm::laplacian(turbulence->alphaEff(), he)
     ==
        rho*(U&g)
      + radiation->Sh(thermo, he)
      + fvOptions(rho, he)
    );
You can disable dpdt calculation, by adding
Code:
dpdt off;
line to your thermophysicalProperties dictionary. It's available, when you use sensibleEnthalpy energy equation.
I remember, that buoyantPimpleFoam worked somehow differently in openfoam 7 and OpenFOAM-v1906, and that particular case was crashing in OF7.


My thermophysicalProperties dictionary looked like this:
Code:
/*--------------------------------*- C++ -*----------------------------------*\
| =========                 |                                                 |
| \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
|  \\    /   O peration     | Version:  v1906                                 |
|   \\  /    A nd           | Web:      www.OpenFOAM.com                      |
|    \\/     M anipulation  |                                                 |
\*---------------------------------------------------------------------------*/
FoamFile
{
    version     2.0;
    format      ascii;
    class       dictionary;
    location    "constant";
    object      thermophysicalProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

thermoType
{
    type            heRhoThermo;
    mixture         pureMixture;
    transport       polynomial;
    thermo          hPolynomial;
    equationOfState icoPolynomial;
    specie          specie;
    energy          sensibleEnthalpy;
}

pRef            1E+5;
dpdt off;

mixture
{
    specie
    {
        nMoles            1;
        molWeight       18;
    }
    equationOfState
    {
        rhoCoeffs<8> (117.045534 7.913913 -0.02254739 1.97987E-05 0 0 0 0);
    }
    thermodynamics
    {
        Hf              0;
        Sf                0;
        CpCoeffs<8> (4200 0 0 0 0 0 0 0);
        
    }
    transport
    {
        muCoeffs<8> (0.1368992 -0.0012040579 3.5597468E-06 -3.526231E-09 0 0 0 0);
        kappaCoeffs<8> (-2.4283206 0.0233779 -5.9953665E-05 5.2602452E-08 0 0 0 0);
    }
}
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Old   May 23, 2020, 09:33
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Khaled Yassin
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Thank you very much for your answer....I will try that
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