CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > Software User Forums > OpenFOAM > OpenFOAM Meshing & Mesh Conversion

[snappyHexMesh] Error: Cannot find face 165412 in any of the patches 1(rocket_scaled)

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   November 16, 2019, 14:24
Default Error: Cannot find face 165412 in any of the patches 1(rocket_scaled)
  #1
New Member
 
Kjersti Bragstad
Join Date: Nov 2019
Posts: 1
Rep Power: 0
Xaxte is on a distinguished road
Hello,



We tried to generate a mesh around an imported geometry (stl.file) with snappyHexMesh. It says that it generated a mesh that was ok, and it looks ok in paraview. But when we run the rhoPimpleFoam solver we get the following error message:


Code:
/*---------------------------------------------------------------------------*\
  =========                 |
  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox
   \\    /   O peration     | Website:  https://openfoam.org
    \\  /    A nd           | Version:  7
     \\/     M anipulation  |
\*---------------------------------------------------------------------------*/
Build  : 7-6ef561967074
Exec   : rhoPimpleFoam
Date   : Nov 16 2019
Time   : 18:33:36
Host   : "kjersti-VirtualBox"
PID    : 3426
I/O    : uncollated
Case   : /home/kjersti/OpenFOAM/kjersti-7/run/prism
nProcs : 1
sigFpe : Enabling floating point exception trapping (FOAM_SIGFPE).
fileModificationChecking : Monitoring run-time modified files using timeStampMaster (fileModificationSkew 10)
allowSystemOperations : Allowing user-supplied system call operations

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

Create mesh for time = 0


PIMPLE: No convergence criteria found


PIMPLE: No corrector convergence criteria found
        Calculations will do 2 corrections


PIMPLE: Operating solver in transient mode with 2 outer correctors


Reading thermophysical properties

Selecting thermodynamics package 
{
    type            hePsiThermo;
    mixture         pureMixture;
    transport       const;
    thermo          hConst;
    equationOfState perfectGas;
    specie          specie;
    energy          sensibleInternalEnergy;
}

Reading field U

Reading/calculating face flux field phi

Creating turbulence model

Selecting turbulence model type RAS
Selecting RAS turbulence model kEpsilon
RAS
{
    RASModel        kEpsilon;
    turbulence      on;
    printCoeffs     on;
    Cmu             0.09;
    C1              1.44;
    C2              1.92;
    C3              0;
    sigmak          1;
    sigmaEps        1.3;
}

Creating field dpdt

Creating field kinetic energy K

No MRF models present

No finite volume options present
Courant Number mean: 0.000372342 max: 0.0298496

Starting time loop

Courant Number mean: 0.000372342 max: 0.0298496
Time = 5e-09

PIMPLE: Iteration 1
diagonal:  Solving for rho, Initial residual = 0, Final residual = 0, No Iterations 0
smoothSolver:  Solving for Ux, Initial residual = 1, Final residual = 1.87371e-07, No Iterations 2
smoothSolver:  Solving for Uy, Initial residual = 1, Final residual = 7.07998e-08, No Iterations 2
smoothSolver:  Solving for Uz, Initial residual = 1, Final residual = 4.96554e-07, No Iterations 1
smoothSolver:  Solving for e, Initial residual = 1, Final residual = 2.6378e-07, No Iterations 2
smoothSolver:  Solving for p, Initial residual = 1, Final residual = 7.11171e-07, No Iterations 1
diagonal:  Solving for rho, Initial residual = 0, Final residual = 0, No Iterations 0
time step continuity errors : sum local = 8.63045e-12, global = -2.41024e-12, cumulative = -2.41024e-12
PIMPLE: Iteration 2
smoothSolver:  Solving for Ux, Initial residual = 2.91336e-05, Final residual = 1.51895e-08, No Iterations 1
smoothSolver:  Solving for Uy, Initial residual = 0.00102276, Final residual = 6.36141e-07, No Iterations 1
smoothSolver:  Solving for Uz, Initial residual = 1.53354e-05, Final residual = 5.23964e-09, No Iterations 1
smoothSolver:  Solving for e, Initial residual = 0.00015063, Final residual = 1.26379e-07, No Iterations 1
smoothSolver:  Solving for p, Initial residual = 2.38202e-05, Final residual = 1.62645e-10, No Iterations 1
diagonal:  Solving for rho, Initial residual = 0, Final residual = 0, No Iterations 0
time step continuity errors : sum local = 1.61197e-13, global = 1.98876e-14, cumulative = -2.39035e-12


--> FOAM FATAL ERROR: 
Cannot find face 165412 in any of the patches 1(rocket_scaled)
It seems your patches are not consistent with the mesh : internalFaces:158590  total number of faces:191060

    From function Foam::label Foam::polyBoundaryMesh::whichPatch(Foam::label) const
    in file meshes/polyMesh/polyBoundaryMesh/polyBoundaryMesh.C at line 747.

FOAM aborting

#0  Foam::error::printStack(Foam::Ostream&) at ??:?
#1  Foam::error::abort() at ??:?
#2  Foam::polyBoundaryMesh::whichPatch(int) const at ??:?
#3  void Foam::fvMatrix<double>::setValuesFromList<Foam::UList>(Foam::UList<int> const&, Foam::UList<double> const&) at ??:?
#4  Foam::epsilonWallFunctionFvPatchScalarField::manipulateMatrix(Foam::fvMatrix<double>&) at ??:?
#5  Foam::fvMatrix<double>::boundaryManipulate(Foam::GeometricField<double, Foam::fvPatchField, Foam::volMesh>::Boundary&) at ??:?
#6  Foam::RASModels::kEpsilon<Foam::EddyDiffusivity<Foam::ThermalDiffusivity<Foam::CompressibleTurbulenceModel<Foam::fluidThermo> > > >::correct() at ??:?
#7  ? in "/opt/openfoam7/platforms/linux64GccDPInt32Opt/bin/rhoPimpleFoam"
#8  __libc_start_main in "/lib/x86_64-linux-gnu/libc.so.6"
#9  ? in "/opt/openfoam7/platforms/linux64GccDPInt32Opt/bin/rhoPimpleFoam"
Aborted (core dumped)
The constant/polyMesh/boundary file is this



Code:
/*--------------------------------*- C++ -*----------------------------------*\
  =========                 |
  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox
   \\    /   O peration     | Website:  https://openfoam.org
    \\  /    A nd           | Version:  7
     \\/     M anipulation  |
\*---------------------------------------------------------------------------*/
FoamFile
{
    version     2.0;
    format      ascii;
    class       polyBoundaryMesh;
    location    "1.5e-08/polyMesh";
    object      boundary;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

1
(
    
    rocket_scaled
    {
        type            wall;
        inGroups        1(wall);
        nFaces          20066;
        startFace       170994;
    }
)

// ************************************************************************* //
Have any of you experienced something similar or know what could be wrong? Attached is a picture of the mesh. If you need any more files, just tell me!


Thank you so much for your help, it would be highly appreciated!
Attached Images
File Type: jpg mesh_ask.jpg (129.4 KB, 1 views)
Xaxte is offline   Reply With Quote

Reply

Tags
fatalerror, openfoam, openfoam7, rhopimplefoam, snappyhexmesh


Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

BB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Trackbacks are Off
Pingbacks are On
Refbacks are On


Similar Threads
Thread Thread Starter Forum Replies Last Post
[Other] mesh airfoil NACA0012 anand_30 OpenFOAM Meshing & Mesh Conversion 13 March 7, 2022 18:22
how to set periodic boundary conditions Ganesh FLUENT 15 November 18, 2020 07:09
[Netgen] Import netgen mesh to OpenFOAM hsieh OpenFOAM Meshing & Mesh Conversion 32 September 13, 2011 06:50
channelFoam for a 3D pipe AlmostSurelyRob OpenFOAM 3 June 24, 2011 14:06
Errors running allwmake in OpenFOAM141dev with WM_COMPILE_OPTION%3ddebug unoder OpenFOAM Installation 11 January 30, 2008 21:30


All times are GMT -4. The time now is 14:53.