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Calculation diverges, Liquid behavior around a rotating object

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Old   December 1, 2016, 10:54
Default Calculation diverges, Liquid behavior around a rotating object
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Toru Kizaki
Join Date: Nov 2016
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Hi,
I am trying to simulate liquid behavior around a rotating object using the solver "interFoam".
The problem is that a calculation always diverges. I suspect the reason is a very small gap in the model (though the small gap is necessary for my task.).
The small gap induces a large difference of a mesh size in the model. I ended up with no solutions for this problem though I have repeated the calculation with many different conditions including different mesh sizes.
I would really appreciate if you give me some advice or hints.
  1. Model description

    Model type: 2D

    <Calculation area>
    Shape: rectangular
    Size: 1000 mm * 1600 mm

    <Rotating object>
    Shape and size of the rotating object: circle (cylinder in 3D), 400 mm in diameter
    Circumferential speed: 30 m/s
    Position: the rotating object is placed at the position where the distance between its circumference and the bottom edge of the calculation area becomes 0.1 mm.
    • the model picture
      1.jpg
    • the detail pictures showing the position where the gap is 0.1 mm
      2.jpg
      3.jpg

    <Liquid>
    Type: water
    Initial condition: Initially no liquid exist in the area. It is supplied through a nozzle placed near the rotating object. The initial speed is 20 m/s.

    <Solver, Turbulence model>
    interFoam, k-epsilon

  2. Problematic results
    • Last snaps before the calculation has diverged (3 msec after an initial state).
      4.jpg
      5.jpg

  3. Some codes
    • controlDict
      Code:
      /*--------------------------------*- C++ -*----------------------------------*\
      | =========                 |                                                 |
      | \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
      |  \\    /   O peration     | Version:  v1606+                                |
      |   \\  /    A nd           | Web:      www.OpenFOAM.com                      |
      |    \\/     M anipulation  |                                                 |
      \*---------------------------------------------------------------------------*/
      FoamFile
      {
          version     2.0;
          format      ascii;
          class       dictionary;
          location    "system";
          object      controlDict;
      }
      // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
      
      application     interFoam;
      
      startFrom       latestTime;
      
      startTime       0;
      
      stopAt          endTime;
      
      endTime         1;
      
      deltaT          0.000001;
      
      writeControl    adjustableRunTime;
      
      writeInterval   0.001;
      
      purgeWrite      0;
      
      writeFormat     ascii;
      
      writePrecision  6;
      
      writeCompression uncompressed;
      
      timeFormat      general;
      
      timePrecision   6;
      
      runTimeModifiable yes;
      
      adjustTimeStep  on;
      
      maxCo           1;
      maxAlphaCo      1;
      
      maxDeltaT       1;
      
      
      // ************************************************************************* //
    • fvSchemes
      Code:
      /*--------------------------------*- C++ -*----------------------------------*\
      | =========                 |                                                 |
      | \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
      |  \\    /   O peration     | Version:  v1606+                                |
      |   \\  /    A nd           | Web:      www.OpenFOAM.com                      |
      |    \\/     M anipulation  |                                                 |
      \*---------------------------------------------------------------------------*/
      FoamFile
      {
          version     2.0;
          format      ascii;
          class       dictionary;
          location    "system";
          object      fvSchemes;
      }
      // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
      
      ddtSchemes
      {
          default         Euler;
      }
      
      gradSchemes
      {
          default         Gauss linear;
      }
      
      divSchemes
      {
          div(rhoPhi,U)   Gauss linearUpwind grad(U);
          div(phi,alpha)  Gauss vanLeer;
          div(phirb,alpha) Gauss linear;
          div(phi,k)      Gauss upwind;
          div(phi,epsilon) Gauss upwind;
          div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;
      }
      
      laplacianSchemes
      {
          default         Gauss linear corrected;
      }
      
      interpolationSchemes
      {
          default         linear;
      }
      
      snGradSchemes
      {
          default         corrected;
      }
      
      
      // ************************************************************************* //
    • fvSolution
      Code:
      /*--------------------------------*- C++ -*----------------------------------*\
      | =========                 |                                                 |
      | \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
      |  \\    /   O peration     | Version:  v1606+                                |
      |   \\  /    A nd           | Web:      www.OpenFOAM.com                      |
      |    \\/     M anipulation  |                                                 |
      \*---------------------------------------------------------------------------*/
      FoamFile
      {
          version     2.0;
          format      ascii;
          class       dictionary;
          location    "system";
          object      fvSolution;
      }
      // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
      
      solvers
      {
          "alpha.water.*"
          {
              nAlphaCorr      2;
              nAlphaSubCycles 1;
              cAlpha          1;
      
              MULESCorr       yes;
              nLimiterIter    2;
      
              solver          smoothSolver;
              smoother        symGaussSeidel;
              tolerance       1e-8;
              relTol          0;
          }
      
          pcorr
          {
              solver          PCG;
              preconditioner  DIC;
              tolerance       1e-5;
              relTol          0;
          }
      
          p_rgh
          {
              solver          PCG;
              preconditioner  DIC;
              tolerance       1e-07;
              relTol          0.05;
          }
      
          p_rghFinal
          {
              $p_rgh;
              relTol          0;
          }
      
          "(U|k|epsilon).*"
          {
              solver          smoothSolver;
              smoother        symGaussSeidel;
              tolerance       1e-06;
              relTol          0;
              minIter         1;
          }
      }
      
      PIMPLE
      {
          momentumPredictor   yes;
          nOuterCorrectors    200;
          nCorrectors         1;
          nNonOrthogonalCorrectors 0;
          turbOnFinalIterOnly false;
          residualControl
          {
              U
              {
                  tolerance 1e-5;
                  relTol    0;
              }
              p_rgh
              {
                  tolerance 5e-4;
                  relTol    0;
              }
              alpha.water
              {
                  tolerance 1e-2;
                  relTol    0;
              }
          }
      }
      
      relaxationFactors
      {
          fields
          {
              p_rgh      0.3;
              p_rghFinal 1;
          }
          equations
          {
              "U|k|epsilon"     0.3;
              "(U|k|epsilon)Final"   1;
          }
      }
      
      // ************************************************************************* //

Last edited by toru; December 1, 2016 at 13:10.
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