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Old   January 18, 2013, 04:02
Default Questions on dynamicTopoFvMesh
  #1
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Daniele Vicario
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Hi,
I'm trying to understand how to use dynamicTopoFvMesh library to simulate a free moving (6DoF) object into a fluid.

I'm following the circCylinder3d tutorial just to understand how to setup my case that will use pimpleDyMFoam and I've got lots of questions...
just a couple to start:

1. What is tetFemSolution ?

2. In dynamicMeshDict there are position constrains:

Code:
//- Constrain surface mesh-motion on a specified cylinder
    cylindricalConstraints
    {
        //- Specify options per slip patch
        sideWall
        {
            axisPoint      (0.0 0.0 0.0);
            axisVector     (0.0 0.0 1.0);
            radius          1.0;
        }
    }

    //- Specify fixedValue patches for the motionSolver
    fixedValuePatches
    {
        topWall
        {
            type          angularOscillatingDisplacement;
            amplitude     -0.0125;
            //type          oscillatingDisplacement;
            //amplitude     (0 0 -0.01);
            axis          (1 0 0);
            origin        (0 0 3);
            angle0        0.0;
            omega         0.15;
            value         uniform (0 0 0);
        }
    }
but what is then motionU file for ?

Code:
boundaryField
{
    bottomWall
    {
        type            fixedValue;
        value           uniform (0 0 0);
    }

    sideWall
    {
        type            slip;
    }

    topWall
    {
        type            oscillatingFixedValue;
        refValue        uniform (0 0 0);
        amplitude       uniform (0 0 0.5);
        frequency       0.1;
        //type            fixedValue;
        //value           uniform (0 0 0.1);
    }

    outlet
    {
        type            fixedValue;
        value           uniform (0 0 0);
    }
}
3. The only type of motion constrain I found (in mesquiteOptions) are:
// angularOscillatingDisplacement
// angularOscillatingVelocity
// oscillatingDisplacement
// oscillatingVelocity
// surfaceDisplacement
// surfaceSlipDisplacement

Is there something similar to the following type ?
Code:
oggetto
    {
        type            sixDoFRigidBodyDisplacement;
        centreOfMass    (0 0 0.2);
        momentOfInertia (0.000001 0.000001 0.000001);
        mass            0.01;
        rhoName         rhoInf;
        rhoInf          1000;  // needed only for solvers solving for kinematic pressure
        report          on;
        value           uniform (0 0 0);
    }
I'm sorry if these question seems I little confused but I definitely need a starting point.

Thanks.
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Old   January 18, 2013, 10:14
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Sandeep Menon
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Daniele,

Sorry if the whole thing was confusing to you. I'll briefly explain:

1. The tetFemSolution file is for the tetDecompositionMotionSolvers in OpenFOAM-1.6-ext. If you don't use that library, then this file has no effect, since the mesquiteMotionSolver does not use it any way.

2. The motionU file is a way for motionSolvers to input boundary conditions, and again, is not used by the mesquiteMotionSolver, and is input using dynamicMeshDict instead. However, it appears that the fixedValuePatches approach is too simplistic, and using more complicated patch fields like sixDoFRigidBodyDisplacement may not work this way (this particular patch writes the initial position to disk, which is required for solution restarts). I've attached a diff patch which I've tested only briefly with the Port-2.1.x branch of the github repository - for some reason, it doesn't work with OF-1.6-ext. This patch basically points the mesquiteMotionSolver to use the pointDisplacement field (which the fvMotionSolver uses) to calculate 6-DoF properties.

3. Remember to add a libs entry in your controlDict that loads libforces.so (located at $FOAM_SRC/postProcessing/functionObjects/forces, if you're curious), so that the 6DoF stuff is picked up, and those patches become available for run time selection.

Hope this helps.
Attached Files
File Type: patch mesquite.diff.patch (2.7 KB, 61 views)
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Old   January 18, 2013, 12:09
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Daniele Vicario
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Hi Sandeep,
many thanks for the clarifications !

I'll try the patch and let you know.
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Old   January 18, 2013, 13:59
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Daniele Vicario
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It give me a strange error:

Code:
/*---------------------------------------------------------------------------*\
| =========                 |                                                 |
| \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
|  \\    /   O peration     | Version:  2.1                                   |
|   \\  /    A nd           | Web:      www.OpenFOAM.org                      |
|    \\/     M anipulation  |                                                 |
\*---------------------------------------------------------------------------*/
/*   Windows 32 and 64 bit porting by blueCAPE: http://www.bluecape.com.pt   *\
|  Based on Windows porting (2.0.x v4) by Symscape: http://www.symscape.com   |
\*---------------------------------------------------------------------------*/
Build  : 2.1-fb1015c3f1b5
Exec   : C:\PROGRA~2\BLUECF~1.1\OpenFOAM-2.1\platforms\linuxmingw-w64DPOpt\bin\pimpleDyMFoam.exe
Date   : Jan 18 2013
Time   : 18:50:58
Host   : "UFFTECNICO7"
PID    : 5668
Case   : f:/taps/cfd/valvmov-topo
nProcs : 1
SigFpe : Enabling floating point exception trapping (FOAM_SIGFPE).
fileModificationChecking : Monitoring run-time modified files using timeStampMaster
allowSystemOperations : Disallowing user-supplied system call operations

// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
Create time

Create mesh for time = 0

Selecting dynamicFvMesh dynamicTopoFvMesh
Selecting metric Knupp
Selecting motion solver: mesquiteMotionSolver
Selecting quality metric: AspectRatioGamma
Selecting objective function: LPtoP
Selecting optimization algorithm: FeasibleNewton
Outer termination criterion (tcOuter) was not found. Using default values.
Reading field p

Reading field U

Reading/calculating face flux field phi

Selecting incompressible transport model Newtonian
Selecting turbulence model type laminar
Reading field rAU if present

No field sources present


PIMPLE: no residual control data found. Calculations will employ 2 corrector loops


Starting time loop

Courant Number mean: 0.001961305481 max: 0.207096507
deltaT = 0.001111111111
Time = 0.00111111


************** QualityAssessor(free only) Summary **************

  Evaluating quality for 72062 free elements of 72220 total elements.
  There were no inverted elements detected.
  No entities had undefined values for any computed metric.

          metric     minimum     average         rms     maximum    std.dev.
AspectRatioGamma 1.001149442 1.201508832 1.208379622 3.0127907370.1286772598

************** QualityAssessor(free only) Summary **************

  Evaluating quality for 72062 free elements of 72220 total elements.
  There were no inverted elements detected.
  No entities had undefined values for any computed metric.

          metric     minimum     average         rms     maximum    std.dev.
AspectRatioGamma 1.001124721 1.201507976 1.208379044 3.0144733790.1286798298

 ~~~ Mesh Quality Statistics ~~~
 Min: 0.4792098079
 Max: 0.9992508882
 Mean: 0.8898675635
 Cells: 72220
 ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~

 Topo modifier time: 0.648 s
 Bisections :: Total: 0, Surface: 0
 Collapses  :: Total: 0, Surface: 0
 Swaps      :: Total: 441, Surface: 0


--> FOAM FATAL ERROR:
attempted to assign to a const reference to constant object

    From function Foam::tmp<T>::operator=(const tmp<T>&)
    in file C:/PROGRA~2/BLUECF~1.1/OpenFOAM-2.1/src/OpenFOAM/lnInclude/tmpI.H at line 270.

FOAM aborting



Backtrace:
        ZN10StackTraceC1Ev [0x6c5815de+62]
                 module: C:\PROGRA~2\BLUECF~1.1\OpenFOAM-2.1\platforms\linuxmingw-w64DPOpt\lib\libstack_trace.dll
        (No symbol) [0x44ed1a0]
        RtlCaptureContext [0x775eb6f0+0]
                 module: C:\Windows\system32\kernel32.dll
        (No symbol) [0x76cc10]
        (No symbol) [0x590270]
        (No symbol) [0x5904a0]
        (No symbol) [0x1b]
        (No symbol) [0x7602a8]
        RtlAllocateHeap [0x77cd3488+232]
                 module: C:\Windows\SYSTEM32\ntdll.dll

This application has requested the Runtime to terminate it in an unusual way.
Please contact the application's support team for more information.
Actually I've got this error even before the patch.

Here you can find the case: https://www.box.com/s/9pg0lcuhu20th8cnccfh

Thanks for any help.
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Old   January 18, 2013, 15:27
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Sandeep Menon
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Anyway you could give me a more meaningful stack trace? I you compile with debug symbols, that would be helpful.

I think I might have seen this error before. Perhaps the attached diff would help. Not sure if this is the same problem though.
Attached Files
File Type: patch topoMapperTemplates.patch (1.1 KB, 30 views)
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Old   January 18, 2013, 18:07
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  #6
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Bruno Santos
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wyldckat is just really nicewyldckat is just really nicewyldckat is just really nicewyldckat is just really nice
Greetings to all!

@Sandeep: Your latest patch "topoMapperTemplates.patch" fixed the problem!

Sorry about the nearly meaningless stack trace. I'm the guy responsible for this OpenFOAM port named blueCFD, and this particular version Daniele is using is still a preview version, for which the stack trace is still very flaky.

Although it's not necessary but as future reference, on Linux (Ubuntu 12.04 x86_64), the respective stack trace was this (although not using debug symbols):
Code:
#0  Foam::error::printStack(Foam::Ostream&) in "/home/user/OpenFOAM/OpenFOAM-2.1.x/platforms/linux64GccDPOpt/lib/libOpenFOAM.so"
#1  Foam::error::abort() in "/home/user/OpenFOAM/OpenFOAM-2.1.x/platforms/linux64GccDPOpt/lib/libOpenFOAM.so"
#2  void Foam::topoMapper::storeGradients<Foam::Vector<double>, Foam::GeometricField<Foam::Tensor<double>, Foam::fvPatchField, Foam::volMesh> >(Foam::HashTable<Foam::autoPtr<Foam::GeometricField<Foam::Tensor<double>, Foam::fvPatchField, Foam::volMesh> >, Foam::word, Foam::string::hash>&) const in "/home/user/OpenFOAM/user-2.1.x/platforms/linux64GccDPOpt/lib/libdynamicTopoFvMesh.so"
#3  Foam::topoMapper::storeGradients() const in "/home/user/OpenFOAM/user-2.1.x/platforms/linux64GccDPOpt/lib/libdynamicTopoFvMesh.so"
#4  Foam::topoMapper::storeMeshInformation() const in "/home/user/OpenFOAM/user-2.1.x/platforms/linux64GccDPOpt/lib/libdynamicTopoFvMesh.so"
#5  Foam::dynamicTopoFvMesh::resetMesh() in "/home/user/OpenFOAM/user-2.1.x/platforms/linux64GccDPOpt/lib/libdynamicTopoFvMesh.so"
#6  Foam::dynamicTopoFvMesh::update() in "/home/user/OpenFOAM/user-2.1.x/platforms/linux64GccDPOpt/lib/libdynamicTopoFvMesh.so"
#7  
 in "/home/user/OpenFOAM/OpenFOAM-2.1.x/platforms/linux64GccDPOpt/bin/pimpleDyMFoam"
#8  __libc_start_main in "/lib/x86_64-linux-gnu/libc.so.6"
#9  
 in "/home/user/OpenFOAM/OpenFOAM-2.1.x/platforms/linux64GccDPOpt/bin/pimpleDyMFoam"
Aborted (core dumped)
Best regards,
Bruno
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Old   January 19, 2013, 04:01
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Daniele Vicario
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Thanks to both Bruno and Sandeep!

But I still have problems:

I cleared all the position BC from dynamicMeshDict and I used the following pointDisplacement dict:

Code:
dimensions      [0 1 0 0 0 0 0];

internalField   uniform (0 0 0);

boundaryField
{
    wall
    {
        type            fixedValue;
        value           uniform (0 0 0);
    }
    inlet
    {
        type            fixedValue;
        value           uniform (0 0 0);
    }
    outlet
    {
        type            fixedValue;
        value           uniform (0 0 0);
    }
    oggetto
    {
        type            sixDoFRigidBodyDisplacement;
        centreOfMass    (0 0 0.2);
        momentOfInertia (0.000001 0.000001 0.000001);
        mass            0.01;
        rhoName         rhoInf;
        rhoInf          1000;  // needed only for solvers solving for kinematic pressure
        report          on;
        value           uniform (0 0 0);
    }
}
dynamicMeshDict is:

Code:
//- Select the type of dynamicFvMesh
dynamicFvMesh           dynamicTopoFvMesh;

//- Select the type of motionSolver
motionSolverLibs ("libmesquiteMotionSolver.so" "libfvMotionSolvers.so");
solver                  mesquiteMotionSolver;

mesquiteOptions
{
    //- Optimization metric
    optMetric               AspectRatioGamma;

    //- Objective function
    objFunction             LPtoP;

    //- Optimization algorithm
    optAlgorithm            FeasibleNewton;

   
    tcInner
    {
        absGradL2            1e-4;
        cpuTime              0.5;
    }

     //- Power value for the LPtoP objective function
    pValue                  2;
    power                   2;

    //- Specify a tolerance for the surface-smoothing CG solver
    tolerance               1e-2;

    //- Specify number of CG sweeps for surface-smoothing
    nSweeps                 2;

    //- Specify slip patches for the motionSolver
    slipPatches
    {
      
    }

    //- Constrain surface mesh-motion on a specified cylinder
    cylindricalConstraints
    {
       
    }

    //- Specify fixedValue patches for the motionSolver
    fixedValuePatches
    {
         
        
    
    
    }
     

    //- Specify interval for surface smoothing
    surfInterval            1;
}

//- Options for dynamicTopoFvMesh
dynamicTopoFvMesh
{
    
    allOptionsMandatory no;

    
    //debug               2;

    //- Specify the number of threads
    threads             1;

    //- Specify re-meshing interval
    //- Negative value implies no re-meshing
    interval            1;

    //- Specify whether the length-scale field
    //- should be dumped to disk
    dumpLengthScale     false;

    //- sliverThreshold specifies the
    //- quality criteria for sliver removal.
    sliverThreshold     0.35;

    //- Should the tool attempt to remove slivers
    //- that fall below the sliverThreshold value?
    removeSlivers       false;

    //- Skip mapping step. Useful while using
    //- this tool as a pre-processor
    // skipMapping         true;

    // Toggle edgeRefinement on/off
    edgeRefinement      off;

  
    refinementOptions
    {
        collapseRatio   0.5;
        bisectionRatio  1.5;
        growthFactor    1.0;

        fixedLengthScalePatches
        {
            oggetto     0.2;
        }

        //- Avoid refinement on certain patches, if necessary
        noModificationPatches
        {
            inlet;
            outlet;
            wall;
            oggetto;
        }

        //- Set floating length-scale values on certain patches
        freeLengthScalePatches
        {
            inlet;
            outlet;
            wall;
        }

       
    }

     //- Tetrahedral mesh quality metric
    tetMetric          Knupp;

    //- Avoid 2-2 swapping on certain patches
    noSwapPatches
    {}
}
This setup results in a not moving object ("oggetto" in the case I posted before).

If I then modified dynamicMeshDict adding the same position BC:

Code:
fixedValuePatches
    {
        oggetto
    {
        type            sixDoFRigidBodyDisplacement;
        centreOfMass    (0 0 0.2);
        momentOfInertia (0.000001 0.000001 0.000001);
        mass            0.01;
        rhoName         rhoInf;
        rhoInf          1000;  // needed only for solvers solving for kinematic pressure
        report          on;
        value           uniform (0 0 0);
    } 
    }
Then the solver displays some information regarding centre of mass / linear velocity and angular velocity but the centre of mass is fixed. See the output below:

Code:
Create time

Create mesh for time = 0

Selecting dynamicFvMesh dynamicTopoFvMesh
Selecting metric Knupp
Selecting motion solver: mesquiteMotionSolver
Selecting quality metric: AspectRatioGamma
Selecting objective function: LPtoP
Selecting optimization algorithm: FeasibleNewton
Outer termination criterion (tcOuter) was not found. Using default values.
Reading field p

Reading field U

Reading/calculating face flux field phi

Selecting incompressible transport model Newtonian
Selecting turbulence model type laminar
Reading field rAU if present

No field sources present


PIMPLE: no residual control data found. Calculations will employ 2 corrector loops


Starting time loop

Courant Number mean: 0.001961305481 max: 0.207096507
deltaT = 0.001
Time = 0.001

Centre of mass: (0 0 0.2)
Linear velocity: (0 0 0)
Angular velocity: (0 0 0)

************** QualityAssessor(free only) Summary **************

  Evaluating quality for 72062 free elements of 72220 total elements.
  There were no inverted elements detected.
  No entities had undefined values for any computed metric.

          metric     minimum     average         rms     maximum    std.dev.
AspectRatioGamma 1.001149442 1.201508832 1.208379622 3.0127907370.1286772598

************** QualityAssessor(free only) Summary **************

  Evaluating quality for 72062 free elements of 72220 total elements.
  There were no inverted elements detected.
  No entities had undefined values for any computed metric.

          metric     minimum     average         rms     maximum    std.dev.
AspectRatioGamma 1.001124721 1.201507976 1.208379044 3.0144733790.1286798298

 ~~~ Mesh Quality Statistics ~~~
 Min: 0.4792098079
 Max: 0.9992508882
 Mean: 0.8898675635
 Cells: 72220
 ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~

 Topo modifier time: 0.441044 s
 Bisections :: Total: 0, Surface: 0
 Collapses  :: Total: 0, Surface: 0
 Swaps      :: Total: 441, Surface: 0
 Mapping time: 0.051005 s
 Reordering time: 0.135013 s
 ~~~ No flux correction ~~~

 ~~~ Mesh Quality Statistics ~~~
 Min: 0.4792098079
 Max: 0.9992508882
 Mean: 0.8888376015
 Cells: 72226
 ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~

GAMG:  Solving for pcorr, Initial residual = 1, Final residual = 0.009784238691, No Iterations 14
GAMG:  Solving for pcorr, Initial residual = 0.1318015667, Final residual = 0.005524330453, No Iterations 1
GAMG:  Solving for pcorr, Initial residual = 0.0274078549, Final residual = 0.001671230422, No Iterations 1
time step continuity errors : sum local = 0.003519238986, global = 2.951992158e-005, cumulative = 2.951992158e-005
PIMPLE: iteration 1
DILUPBiCG:  Solving for Ux, Initial residual = 0.2099944886, Final residual = 0.001067176115, No Iterations 1
DILUPBiCG:  Solving for Uy, Initial residual = 0.2176037194, Final residual = 0.001119524463, No Iterations 1
DILUPBiCG:  Solving for Uz, Initial residual = 0.9144495281, Final residual = 0.006921714113, No Iterations 1
GAMG:  Solving for p, Initial residual = 1, Final residual = 0.006135893841, No Iterations 16
GAMG:  Solving for p, Initial residual = 0.2245647768, Final residual = 0.001579813968, No Iterations 2
GAMG:  Solving for p, Initial residual = 0.04407841501, Final residual = 0.0004149844197, No Iterations 2
time step continuity errors : sum local = 0.0005491589084, global = 1.44487661e-005, cumulative = 4.396868768e-005
PIMPLE: iteration 2
DILUPBiCG:  Solving for Ux, Initial residual = 0.4474193232, Final residual = 9.817080748e-007, No Iterations 64
DILUPBiCG:  Solving for Uy, Initial residual = 0.4486384426, Final residual = 7.49347033e-007, No Iterations 61
DILUPBiCG:  Solving for Uz, Initial residual = 0.6700159044, Final residual = 8.998574123e-007, No Iterations 61
GAMG:  Solving for p, Initial residual = 0.2749979373, Final residual = 0.001482151148, No Iterations 14
GAMG:  Solving for p, Initial residual = 0.1748427853, Final residual = 0.001382902354, No Iterations 2
GAMG:  Solving for p, Initial residual = 0.03707025143, Final residual = 4.711430883e-008, No Iterations 22
time step continuity errors : sum local = 5.367153172e-007, global = -5.911960027e-008, cumulative = 4.390956808e-005
ExecutionTime = 8.398 s  ClockTime = 9 s

Courant Number mean: 1.488762178 max: 300.8061065
deltaT = 1.639344262e-005
Time = 0.00101639

Centre of mass: (0 0 0.2)
Linear velocity: (4.896733259e-005 2.424161936e-005 0.006302055408)
Angular velocity: (2.485263244e-005 -0.0001594212928 -4.137107884e-005)

************** QualityAssessor(free only) Summary **************

  Evaluating quality for 72068 free elements of 72226 total elements.
  There were no inverted elements detected.
  No entities had undefined values for any computed metric.

          metric     minimum     average         rms     maximum    std.dev.
AspectRatioGamma 1.001124721 1.203706166  1.21061955 3.0144733790.1291942728
BTW: I left the solver running for a while and even with a not-zero velocity the center of mass remained fixed. Why ?

Last question / problem:

I made the tests with:

edgeRefinement off;

I think I don't need it so far. However when I enable the refinement it returns an error (see enclosed file).


Any idea or comment ?
Attached Files
File Type: txt referr.txt (12.1 KB, 10 views)
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Last edited by danvica; January 19, 2013 at 06:07.
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Old   January 19, 2013, 06:23
Default
  #8
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Daniele Vicario
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A small update:

@Sandeep: in the first patch you sent me there was an additional flag called "usePointDisplacement".

Code:
if (optionsDict.found("usePointDisplacement"))
+    {
+        boundaryConditions_.reset
+        (
+            new pointVectorField
+            (
+                IOobject
+                (
+                    "pointDisplacement",
+                    Mesh_.time().timeName(),
+                    Mesh_,
+                    IOobject::MUST_READ,
+                    IOobject::AUTO_WRITE
+                ),
+                pointMesh::New(Mesh_)
+            )
+        );
+    }
From what I can understand it seems that you have to enable it in order to use the pointDisplacement file.

I tried but it returns more or less the same error:

Code:
/*---------------------------------------------------------------------------*\
| =========                 |                                                 |
| \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
|  \\    /   O peration     | Version:  2.1                                   |
|   \\  /    A nd           | Web:      www.OpenFOAM.org                      |
|    \\/     M anipulation  |                                                 |
\*---------------------------------------------------------------------------*/
/*   Windows 32 and 64 bit porting by blueCAPE: http://www.bluecape.com.pt   *\
|  Based on Windows porting (2.0.x v4) by Symscape: http://www.symscape.com   |
\*---------------------------------------------------------------------------*/
Build  : 2.1-fb1015c3f1b5
Exec   : C:\PROGRA~2\BLUECF~1.1\OpenFOAM-2.1\platforms\linuxmingw-w64DPOpt\bin\pimpleDyMFoam.exe
Date   : Jan 19 2013
Time   : 11:16:40
Host   : "UFFTECNICO7"
PID    : 5212
Case   : f:/taps/cfd/valvmov-topo
nProcs : 1
SigFpe : Enabling floating point exception trapping (FOAM_SIGFPE).
fileModificationChecking : Monitoring run-time modified files using timeStampMaster
allowSystemOperations : Disallowing user-supplied system call operations

// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
Create time

Create mesh for time = 0

Selecting dynamicFvMesh dynamicTopoFvMesh
Selecting metric Knupp
Selecting motion solver: mesquiteMotionSolver
Selecting quality metric: AspectRatioGamma
Selecting objective function: LPtoP
Selecting optimization algorithm: FeasibleNewton
Outer termination criterion (tcOuter) was not found. Using default values.
Reading field p

Reading field U

Reading/calculating face flux field phi

Selecting incompressible transport model Newtonian
Selecting turbulence model type laminar
Reading field rAU if present

No field sources present


PIMPLE: no residual control data found. Calculations will employ 2 corrector loops


Starting time loop

Courant Number mean: 1.961305481e-005 max: 0.00207096507
deltaT = 1.19047619e-005
Time = 1.19048e-005

Centre of mass: (0 0 0.2)
Linear velocity: (0 0 0)
Angular velocity: (0 0 0)
Solving for point motion:  Initial residual: 1 Final residual: 0.007879279805 No Iterations: 12
Solving for point motion:  Initial residual: 1 Final residual: 0.005761454167 No Iterations: 18

************** QualityAssessor(free only) Summary **************

  Evaluating quality for 72062 free elements of 72220 total elements.
  There were no inverted elements detected.
  No entities had undefined values for any computed metric.

          metric     minimum     average         rms     maximum    std.dev.
AspectRatioGamma 1.000929751 1.202198694  1.20924222 3.0127907370.1303266922

************** QualityAssessor(free only) Summary **************

  Evaluating quality for 72062 free elements of 72220 total elements.
  There were no inverted elements detected.
  No entities had undefined values for any computed metric.

          metric     minimum     average         rms     maximum    std.dev.
AspectRatioGamma 1.001152746 1.202272074 1.209234895 3.0212553940.1295796677

 ~~~ Mesh Quality Statistics ~~~
 Min: 0.4784923963
 Max: 0.9992322401
 Mean: 0.8895440621
 Cells: 72220
 ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~

 Topo modifier time: 0.443 s
 Bisections :: Total: 0, Surface: 0
 Collapses  :: Total: 0, Surface: 0
 Swaps      :: Total: 472, Surface: 0
 Mapping time: 0.058 s
 Reordering time: 0.139 s
 ~~~ No flux correction ~~~

 ~~~ Mesh Quality Statistics ~~~
 Min: 0.4784923963
 Max: 0.9992322401
 Mean: 0.8884998041
 Cells: 72226
 ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~

GAMG:  Solving for pcorr, Initial residual = 1, Final residual = 0.008812231801, No Iterations 14
GAMG:  Solving for pcorr, Initial residual = 0.131029343, Final residual = 0.00548001763, No Iterations 1
GAMG:  Solving for pcorr, Initial residual = 0.02724234412, Final residual = 0.001672274306, No Iterations 1
time step continuity errors : sum local = 4.373115074e-005, global = 4.508582388e-007, cumulative = 4.508582388e-007
PIMPLE: iteration 1
DILUPBiCG:  Solving for Ux, Initial residual = 0.8981178464, Final residual = 0.02090304535, No Iterations 1
DILUPBiCG:  Solving for Uy, Initial residual = 0.8276717749, Final residual = 0.01968424129, No Iterations 1
DILUPBiCG:  Solving for Uz, Initial residual = 0.7550246921, Final residual = 0.01660081128, No Iterations 1
GAMG:  Solving for p, Initial residual = 1, Final residual = 0.007054332566, No Iterations 14
GAMG:  Solving for p, Initial residual = 0.1219790556, Final residual = 0.000873474047, No Iterations 2
GAMG:  Solving for p, Initial residual = 0.02592907917, Final residual = 0.0002061318523, No Iterations 2
time step continuity errors : sum local = 5.656009101e-006, global = 2.517583376e-007, cumulative = 7.026165764e-007
PIMPLE: iteration 2
DILUPBiCG:  Solving for Ux, Initial residual = 0.2348991934, Final residual = 8.590299483e-007, No Iterations 4
DILUPBiCG:  Solving for Uy, Initial residual = 0.233874458, Final residual = 8.983213027e-008, No Iterations 5
DILUPBiCG:  Solving for Uz, Initial residual = 0.089038337, Final residual = 5.353018298e-008, No Iterations 5
GAMG:  Solving for p, Initial residual = 0.0406207147, Final residual = 0.000269779655, No Iterations 8
GAMG:  Solving for p, Initial residual = 0.06275711829, Final residual = 0.0005373520539, No Iterations 2
GAMG:  Solving for p, Initial residual = 0.01329922478, Final residual = 5.808675466e-008, No Iterations 17
time step continuity errors : sum local = 1.18446448e-009, global = -2.537820206e-010, cumulative = 7.023627944e-007
ExecutionTime = 6.299 s  ClockTime = 6 s

Courant Number mean: 0.1408376737 max: 2.181599535
deltaT = 1.411564626e-005
Time = 2.60204e-005



Backtrace:
        ZN10StackTraceC1Ev [0x6c5815de+62]
                 module: C:\PROGRA~2\BLUECF~1.1\OpenFOAM-2.1\platforms\linuxmingw-w64DPOpt\lib\libstack_trace.dll
        (No symbol) [0x4148d40]
        RtlCaptureContext [0x775eb6f0+0]
                 module: C:\Windows\system32\kernel32.dll
        (No symbol) [0x22ff30]
        (No symbol) [0x68e0000]
        (No symbol) [0x3342c10]
        (No symbol) [0x5d12f0]
        (No symbol) [0x5e0080]
        (No symbol) [0x48923b0]
        (No symbol) [0x6bee310]
        (No symbol) [0x48923c0]
        (No symbol) [0x19200010000f]
        (No symbol) [0x53002b002b0033]
        (No symbol) [0x206002b002b]
        (No symbol) [0x3f1]
        (No symbol) [0x100000300]
        (No symbol) [0x7e]
Any idea ?
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Old   January 19, 2013, 15:05
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Hi!

First note: I don't know how to help Daniele any further on how to set-up this case for having the loose object float away with the flow. I'm only able so far to diagnose why things were crashing.


Second note: Just to inform readers that I've already sent an email to Daniele informing about the problems that were happening with this case in particular, at least about the error itself.
In summary:
  1. The case with these latest settings did not crash on Linux.
  2. Doing a full check mesh:
    Code:
    checkMesh -allTopology -allGeometry
    revealed that there were around 70 something cells with very small or null determinant.
  3. The conclusion coincides with an older diagnoses I've done in the past: on Linux it is possible to stretch a bit more the boundaries of memory access, such as accessing a negative location in an array (e.g array[-1]), while on Windows this simply leads to a crash.
  4. Full debug build for Windows didn't provide much more information, although it might have been because I mistakenly left the "symbol strip" option turned on... either way, the current implementation of stack tracing on blueCFD is still a bit flaky
    edit: nope, without stripping symbols it still doesn't give a decent stack trace... going to have to revamp the system...
Best regards,
Bruno

Last edited by wyldckat; January 20, 2013 at 10:30. Reason: see "edit:"
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Old   January 20, 2013, 11:35
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Hi,
first I want to thank Bruno for the support.

Then, just to complete the thread, I enclose some pictures of the mesh.

It's a simple two diameter pipe, with a sphere inside of the bigger diameter part.

In order to mesh it using just tet elements I used Netgen. Everything was fine for checkmesh (skew and not-orto) but I hadn't check the small-determinant cells.

I don't know why normally these faulty cells are not so important...or maybe they are and they are the hidden cause of lots of crashes... or maybe it's just me that I'm stick to Windows.

However the main problem is that I don't know how to refine the mesh in order to avoid them.

You can see their position in the last picture (white coloured). I neither don't know what caused them. The geometry is quite simple and I cannot understand how Netgen can create such cells in those (simple) position.


I googled a little but there's not so many information avaible on the topic.

BTW I tried:
Netgen itself: mesh resolution seems to have no correlation with the number of null-determinant cells.
GMsh, Engrid: Windows version are too instables.
MeshLab: Still studying it. Help needed
Salome: I wanted to locally refine the edges but it crash immediately.


Anyway I'll leave this thread,for now, and I'll create another in the right meshing forum to try to solve this problem. I'll come back asap.

But if you have any idea post it wherever you want !!
Attached Images
File Type: jpg pict1.jpg (17.6 KB, 50 views)
File Type: jpg pict2.jpg (15.6 KB, 55 views)
File Type: jpg pict3.jpg (19.7 KB, 55 views)
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Old   January 21, 2013, 10:01
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Daniele,

If I vaguely recall, I remember having trouble with objects falling under gravity using pimpleDyMFoam as well, and that using interDyMFoam (with a bogus alpha field of all fluid) seemed to fix the problem. Again, this is a little weird since gravity is supposed to be picked up from the boundary condition in pimpleDyMFoam, and there's some funky settings where a registered gravity field is sometimes used instead. You may want to also check if pressure is being dealt with in a consistent manner for both situations.

Your 'cells with small determinants' seems okay to me from a visual observation, and if checkMesh gives you a decent non-orthogonality, you should be good on that front. I've run meshes with far worse and still succeeded.
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Old   January 21, 2013, 10:47
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Thanks for your support Sandeep.

I will definitely try interDyMFoam but so far the main problem seems caused by the 0-det cells.

Bruno made a deep analysis of the issue that, I want to confirm, happens just on this Windows porting.

In few words, it brings to an out-of-range array access. Linux manages better than Windows this kind of problems.

I'm still looking for a way to get rid of this cells but, as you said, normally OF can manage worse meshes without problems: I don't know if I'm going to find the right tool.

Thanks.
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Old   January 28, 2013, 18:02
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Greetings to all!

I've finally managed to figure out what's wrong! And I don't have enough experience to fix this .
It's not a problem with cell determinant being null or very small...
It's the first patch on this thread that's broken!

The problem is this part of the patch:
Code:
@@ -3583,6 +3604,14 @@ void mesquiteMotionSolver::applyFixedValuePatches()
     // Fetch the sub-dictionary
     const dictionary& optionsDict = subDict("mesquiteOptions");
 
+    if (boundaryConditions_.valid())
+    {
+        //boundaryConditions_().boundaryField().updateCoeffs();
+        boundaryConditions_().correctBoundaryConditions();
+
+        refPoints_ += boundaryConditions_().internalField();
+    }
+    else
The call to "boundaryConditions_().correctBoundaryConditions() " leads to a crash on Linux as well and gives this stack trace:
Code:
#0  Foam::error::printStack(Foam::Ostream&) in "/home/user/OpenFOAM/OpenFOAM-2.1.x/platforms/linux64GccDPOpt/lib/libOpenFOAM.so"
#1  Foam::sigSegv::sigHandler(int) in "/home/user/OpenFOAM/OpenFOAM-2.1.x/platforms/linux64GccDPOpt/lib/libOpenFOAM.so"
#2   in "/lib/x86_64-linux-gnu/libc.so.6"
#3  Foam::valuePointPatchField<Foam::Vector<double> >::evaluate(Foam::UPstream::commsTypes) in "/home/user/OpenFOAM/OpenFOAM-2.1.x/platforms/linux64GccDPOpt/lib/libOpenFOAM.so"
#4  Foam::GeometricField<Foam::Vector<double>, Foam::pointPatchField, Foam::pointMesh>::GeometricBoundaryField::evaluate() in "/home/user/OpenFOAM/OpenFOAM-2.1.x/platforms/linux64GccDPOpt/lib/libfiniteVolume.so"
#5  Foam::mesquiteMotionSolver::applyFixedValuePatches() in "/home/user/OpenFOAM/user-2.1.x/platforms/linux64GccDPOpt/lib/libmesquiteMotionSolver.so"
#6  Foam::mesquiteMotionSolver::solve() in "/home/user/OpenFOAM/user-2.1.x/platforms/linux64GccDPOpt/lib/libmesquiteMotionSolver.so"
#7  Foam::motionSolver::newPoints() in "/home/user/OpenFOAM/OpenFOAM-2.1.x/platforms/linux64GccDPOpt/lib/libdynamicMesh.so"
#8  Foam::dynamicTopoFvMesh::update() in "/home/user/OpenFOAM/user-2.1.x/platforms/linux64GccDPOpt/lib/libdynamicTopoFvMesh.so"
#9  
 in "/home/user/OpenFOAM/OpenFOAM-2.1.x/platforms/linux64GccDPOpt/bin/pimpleDyMFoam"
#10  __libc_start_main in "/lib/x86_64-linux-gnu/libc.so.6"
#11  
 in "/home/user/OpenFOAM/OpenFOAM-2.1.x/platforms/linux64GccDPOpt/bin/pimpleDyMFoam"
Segmentation fault (core dumped)
The case ready to be tested is available here: https://www.dropbox.com/s/bs3ehwn6xq...topo_v2.tar.gz
Simply run:
Code:
pimpleDyMFoam
edit: I'm using the (almost) latest version of OpenFOAM 2.1.x. As far as I can understand, the problem is due to the "boundaryConditions_" variable not being updated along with the remaining mesh, which leads to this weird crash...

Best regards,
Bruno

Last edited by wyldckat; January 28, 2013 at 18:08. Reason: see "edit:"
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Old   January 28, 2013, 22:42
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Bruno,

Is this after a topology change? If so, could you check if the patch field is being mapped after topo-changes? If not, perhaps the pointMesh mapper is being incorrectly called (or maybe not at all).

Thanks
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Old   January 29, 2013, 05:25
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Hi Sandeep,

I think there are topology changes and some mapping seems to occur... but not for the second iteration, if I understand it correctly. I've used the following debug flags to turn on some more reports on what OpenFOAM does (placed inside the file "~/.OpenFOAM/2.1.x/controlDict"):
Code:
DebugSwitches
{
    primitiveMesh       1;
    mesquiteMotionSolver 1;
    polyMesh         1;
}
The respective output from running pimpleDyMFoam:
Code:
Create time

Create mesh for time = 0

Selecting dynamicFvMesh dynamicTopoFvMesh
void polyMesh::initMesh() : initialising primitiveMesh
primitiveMesh::clearGeom() : clearing geometric data
primitiveMesh::clearAddressing() : clearing topology
primitiveMesh::reset : mesh reset to nInternalPoints:-1 nPoints:14143 nEdges:-1 nInternalFaces:140933 nFaces:147947 nCells:72220
primitiveMesh::calcCells() : calculating cells
Selecting metric Knupp
primitiveMesh::calcEdges(const bool) : calculating edges, pointEdges and optionally faceEdges
primitiveMesh::faceEdges() : calculating faceEdges
primitiveMesh::edgeFaces() : calculating edgeFaces
Selecting motion solver: mesquiteMotionSolver
Reading options for mesquiteMotionSolver
Selecting quality metric: AspectRatioGamma
Selecting objective function: LPtoP
Selecting optimization algorithm: FeasibleNewton
Outer termination criterion (tcOuter) was not found. Using default values.
Reading field p

Reading field U

Reading/calculating face flux field phi

primitiveMesh::calcFaceCentresAndAreas() : Calculating face centres and face areas
primitiveMesh::calcFaceCentresAndAreas() : Finished calculating face centres and face areas
polyMesh::globalData() const : Constructing parallelData from processor topology
This needs the patch faces to be correctly matched
primitiveMesh::calcCellCentresAndVols() : Calculating cell centres and cell volumes
primitiveMesh::calcCellCentresAndVols() : Finished calculating cell centres and cell volumes
Selecting incompressible transport model Newtonian
Selecting turbulence model type laminar
Reading field rAU if present

No field sources present


PIMPLE: no residual control data found. Calculations will employ 2 corrector loops


Starting time loop

Courant Number mean: 1.961305481e-008 max: 2.07096507e-006
deltaT = 0.001111111111
Time = 0.00111111

nTet       = 72220
nHex       = 0
nPyr       = 0
nPrism     = 0
nPolyhedra = 0
Applying fixed-value patches, if any
Centre of mass: (0 0 0.2)
Linear velocity: (0 0 0)
Angular velocity: (0 0 0)

************** QualityAssessor(free only) Summary **************

  Evaluating quality for 72062 free elements of 72220 total elements.
  There were no inverted elements detected. 
  No entities had undefined values for any computed metric.

          metric     minimum     average         rms     maximum    std.dev.
AspectRatioGamma 1.001149442 1.201508832 1.208379622 3.0127907370.1286772598

************** QualityAssessor(free only) Summary **************

  Evaluating quality for 72062 free elements of 72220 total elements.
  There were no inverted elements detected. 
  No entities had undefined values for any computed metric.

          metric     minimum     average         rms     maximum    std.dev.
AspectRatioGamma 1.001124721 1.201507976 1.208379044 3.0144733790.1286798298

 ~~~ Mesh Quality Statistics ~~~ 
 Min: 0.4792098079
 Max: 0.9992508882
 Mean: 0.8898675635
 Cells: 72220
 ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ 

 Topo modifier time: 0.365021 s
 Bisections :: Total: 0, Surface: 0
 Collapses  :: Total: 0, Surface: 0
 Swaps      :: Total: 441, Surface: 0
primitiveMesh::calcCellCells() : calculating cellCells
 Mapping time: 0.042002 s
 Reordering time: 0.103006 s
void polyMesh::clearAddressing() : clearing topology
primitiveMesh::clearAddressing() : clearing topology
void polyMesh::setInstance(const fileName& inst) : Resetting file instance to "0.00111111"
void polyMesh::initMesh() : initialising primitiveMesh
primitiveMesh::clearGeom() : clearing geometric data
primitiveMesh::clearAddressing() : clearing topology
primitiveMesh::reset : mesh reset to nInternalPoints:-1 nPoints:14143 nEdges:-1 nInternalFaces:140945 nFaces:147959 nCells:72226
void polyMesh::clearGeom() : clearing geometric data
primitiveMesh::clearGeom() : clearing geometric data
void polyMesh::clearAddressing() : clearing topology
primitiveMesh::clearAddressing() : clearing topology
void polyMesh::updateMesh(const mapPolyMesh&) : updating addressing and (optional) pointMesh/pointFields
void polyMesh::setInstance(const fileName& inst) : Resetting file instance to "0.00111111"
Mapping volTensorField grad(U)
primitiveMesh::calcCellCentresAndVols() : Calculating cell centres and cell volumes
primitiveMesh::calcFaceCentresAndAreas() : Calculating face centres and face areas
primitiveMesh::calcFaceCentresAndAreas() : Finished calculating face centres and face areas
primitiveMesh::calcCellCentresAndVols() : Finished calculating cell centres and cell volumes
tmp<scalarField> polyMesh::movePoints(const pointField&) :  Moving points for time 0.001111111111 index 1
bool primitiveMesh::checkMeshMotion(const pointField& newPoints, const bool report) const: checking mesh motion
Min volume = 3.690509017e-010.  Total volume = 0.001987458117.  Cell volumes OK.
Min area = 8.235135209e-007.  Face areas OK.
Pyramid volumes OK.
Non-orthogonality check OK.
Mesh motion check OK.
primitiveMesh::clearGeom() : clearing geometric data
primitiveMesh::calcCellCentresAndVols() : Calculating cell centres and cell volumes
primitiveMesh::calcFaceCentresAndAreas() : Calculating face centres and face areas
primitiveMesh::calcFaceCentresAndAreas() : Finished calculating face centres and face areas
primitiveMesh::calcCellCentresAndVols() : Finished calculating cell centres and cell volumes
 ~~~ No flux correction ~~~ 
tmp<scalarField> polyMesh::movePoints(const pointField&) :  Moving points for time 0.001111111111 index 1
bool primitiveMesh::checkMeshMotion(const pointField& newPoints, const bool report) const: checking mesh motion
Min volume = 3.698076689e-010.  Total volume = 0.001987458117.  Cell volumes OK.
Min area = 8.244142416e-007.  Face areas OK.
Pyramid volumes OK.
Non-orthogonality check OK.
Mesh motion check OK.
primitiveMesh::clearGeom() : clearing geometric data
primitiveMesh::calcCellCentresAndVols() : Calculating cell centres and cell volumes
primitiveMesh::calcFaceCentresAndAreas() : Calculating face centres and face areas
primitiveMesh::calcFaceCentresAndAreas() : Finished calculating face centres and face areas
primitiveMesh::calcCellCentresAndVols() : Finished calculating cell centres and cell volumes
Clearing out mesquiteMotionSolver for topo-changes

 ~~~ Mesh Quality Statistics ~~~ 
 Min: 0.4792098079
 Max: 0.9992508882
 Mean: 0.8888376015
 Cells: 72226
 ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ 

polyMesh::globalData() const : Constructing parallelData from processor topology
This needs the patch faces to be correctly matched
GAMG:  Solving for pcorr, Initial residual = 1, Final residual = 0.009784238691, No Iterations 14
GAMG:  Solving for pcorr, Initial residual = 0.1318015667, Final residual = 0.005524330453, No Iterations 1
GAMG:  Solving for pcorr, Initial residual = 0.0274078549, Final residual = 0.001671230422, No Iterations 1
time step continuity errors : sum local = 3.91026554e-008, global = 3.279991287e-010, cumulative = 3.279991287e-010
PIMPLE: iteration 1
DILUPBiCG:  Solving for Ux, Initial residual = 0.001776048218, Final residual = 9.263663799e-011, No Iterations 1
DILUPBiCG:  Solving for Uy, Initial residual = 0.001404779735, Final residual = 7.728408671e-011, No Iterations 1
DILUPBiCG:  Solving for Uz, Initial residual = 0.00987428103, Final residual = 8.50084699e-010, No Iterations 1
GAMG:  Solving for p, Initial residual = 1, Final residual = 0.009588103798, No Iterations 14
GAMG:  Solving for p, Initial residual = 0.1302883199, Final residual = 0.0009036470934, No Iterations 2
GAMG:  Solving for p, Initial residual = 0.02737724854, Final residual = 0.0002262485978, No Iterations 2
time step continuity errors : sum local = 5.294873174e-009, global = 1.106183578e-010, cumulative = 4.386174865e-010
PIMPLE: iteration 2
DILUPBiCG:  Solving for Ux, Initial residual = 0.1834820032, Final residual = 5.636594204e-007, No Iterations 2
DILUPBiCG:  Solving for Uy, Initial residual = 0.1830492352, Final residual = 5.109273914e-007, No Iterations 2
DILUPBiCG:  Solving for Uz, Initial residual = 0.05322444189, Final residual = 1.831625782e-007, No Iterations 2
GAMG:  Solving for p, Initial residual = 0.01625682761, Final residual = 0.0001395819713, No Iterations 10
GAMG:  Solving for p, Initial residual = 0.07015457008, Final residual = 0.0004928326396, No Iterations 2
GAMG:  Solving for p, Initial residual = 0.01514164752, Final residual = 7.103417641e-008, No Iterations 14
time step continuity errors : sum local = 1.648956177e-012, global = 4.143241703e-013, cumulative = 4.390318106e-010
ExecutionTime = 4.949 s  ClockTime = 5 s

Courant Number mean: 0.02715254901 max: 0.4297419588
deltaT = 0.00126984127
Time = 0.00238095

primitiveMesh::calcCells() : calculating cells
nTet       = 72226
nHex       = 0
nPyr       = 0
nPrism     = 0
nPolyhedra = 0
Applying fixed-value patches, if any
Best regards,
Bruno
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Old   February 3, 2013, 14:53
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Greetings to all!

@Sandeep: any chance you can (help us) figure out what's missing here?

Because after roughly 5h of studying dynamic meshing, studying the "mesquiteMotionSolver" and doing several trial-and-errors... I haven't managed to fix this problem.

Attached is a patch with the code where I stopped trying to fix this.

In essence, my findings are as follows:
  • "mesquiteMotionSolver" doesn't do things the same way that OpenFOAM 2.1.x does things. From what I could understand:
    • 2.1.x relies on already existing code for moving/mapping points and fields.
    • "mesquiteMotionSolver" does things directly.
  • Since "mesquiteMotionSolver" does things directly, "boundaryConditions_()" is just junk when "mesquiteMotionSolver::update()" is completed (well, somewhere in the middle...).
  • Given this situation, the only hack I can figure out that might work is to backup the last displacement on the boundaries and reconstruct the field when necessary.
  • Attached is an attempt at this, but is fails miserably, probably because using the method "boundaryConditions_().boundaryField().set(" is a very bad idea...
  • The only other way I can imagine is to write out the boundaries onto file and then recreate them, the same way that the fixed patches are made.
Best regards,
Bruno
Attached Files
File Type: patch mesquiteMotionSolver_attempting_fix.patch (5.1 KB, 8 views)
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Old   February 4, 2013, 00:02
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Sandeep Menon
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I think I might know why things are not being mapped. The boundaryConditions_ member is instantiated using a pointMesh::New function, which may not be registering itself correctly for all subsequent pointField mapping.

I say this because the only field that is currently being mapped (from your logs) is the volTensorField grad(U). It would be helpful to ensure that the pointMesh exists during the mapping process (in MapGeometricFields.H), so that all pointFields associated with it are mapped accordingly as well.

Another possibility is to have the boundaryConditions_ pointVectorField mapped during the mesquiteMotionSolver::update(const mapPolyMesh& mpm) call. I think a pointMapper will need to be instantiated for this, but I can't remember off the top of my head - perhaps you could take a cue from other parts of OpenFOAM, like the fvMotionSolver::updateMesh() functions.
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Old   February 4, 2013, 06:19
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Bruno Santos
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Hi Sandeep,

Many thanks! I'll look into this further.

Best regards,
Bruno
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Old   February 18, 2013, 19:09
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Hi Sandeep,

Unfortunately, I'm unable to figure out how to do the point mapping. All of my tests seem to indicate that "boundaryConditions_()" no longer has enough information when it is working inside "void mesquiteMotionSolver::update(const mapPolyMesh& mpm)".

Attached is a hack that seems to work, although it has to resort to the file system for storing the "pointDisplacement" field. It's applied on top of your two patches, if I'm not mistaken.
It's a (very) sub-optimal solution, but it gets the job done... or at least I hope so.

edit: after several iterations, it looks like the sphere is starting to get deformed... I can only guess that it's because there are points that are being erased/added, which are not mapped out with this hack...

Best regards,
Bruno
Attached Files
File Type: patch suboptimal_hack.patch (2.4 KB, 5 views)

Last edited by wyldckat; February 18, 2013 at 19:28. Reason: see "edit:"
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Old   February 19, 2013, 10:25
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Bruno,

I'm willing to bet that the points on the sphere correspond to un-mapped points. Can you add a noModificationPatches / noSwapPatches entry in dynamicMeshDict with your "sphere" patch, and see if the deformations still happen?

If you look at the Foam:: polyMesh::updateMesh(const mapPolyMesh& mpm) function in polyMeshUpdate.C, you'll see this bit:

Code:
    if (thisDb().foundObject<pointMesh>(pointMesh::typeName))
    {
        const_cast<pointMesh&>
        (
            thisDb().lookupObject<pointMesh>
            (
                pointMesh::typeName
            )
        ).updateMesh(mpm);
    }
As Mattijs put it, this is indeed a bit of a hack, and a proper callback mechanism needs to be put into place for MeshObject (like the way it's done in 1.6-ext). You may need to add this to the mesquiteMotionSolver::updateMesh member function as well, and see if the boundary conditions get mapped.
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