openfoam-propeller-server

mahmood@cluster:~$ of230
mahmood@cluster:~$ cd of-test/propeller/
mahmood@cluster:propeller$ cat submit.tor
#!/bin/bash
#PBS -l nodes=1:ppn=4
#
#PBS -q default
#PBS -N myJobName
#PBS -A MyProjectName
#PBS -o outputFileName
#PBS -j oe

module load openmpi-x86_64
source /export/apps/mechanics/OpenFOAM/OpenFOAM-2.3.0/etc/bashrc WM_NCOMPPROCS=4 foamCompiler=ThirdParty WM_COMPILER=Gcc48 WM_MPLIB=SYSTEMOPENMPI

mpirun -np 4 pimpleDyMFoam -parallel | tee log
mahmood@cluster:propeller$ mpirun -np 4 pimpleDyMFoam -parallel | tee log
/*---------------------------------------------------------------------------*\
| =========                 |                                                 |
| \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
|  \\    /   O peration     | Version:  2.3.0                                 |
|   \\  /    A nd           | Web:      www.OpenFOAM.org                      |
|    \\/     M anipulation  |                                                 |
\*---------------------------------------------------------------------------*/
Build  : 2.3.0-f5222ca19ce6
Exec   : pimpleDyMFoam -parallel
Date   : Mar 25 2016
Time   : 20:18:29
Host   : "cluster.scu"
PID    : 16497
Case   : /home/mahmood/of-test/propeller
nProcs : 4
Slaves :
3
(
"cluster.scu.16498"
"cluster.scu.16499"
"cluster.scu.16500"
)

Pstream initialized with:
    floatTransfer      : 0
    nProcsSimpleSum    : 0
    commsType          : nonBlocking
    polling iterations : 0
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 solidBodyMotionFvMesh
Selecting solid-body motion function rotatingMotion
Applying solid body motion to cellZone innerCylinderSmall

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

Reading field p

Reading field U

Reading/calculating face flux field phi

AMI: Creating addressing and weights between 18496 source faces and 18720 target faces
AMI: Patch source sum(weights) min/max/average = 0.984261, 1.01509, 1.00007
AMI: Patch target sum(weights) min/max/average = 0.969379, 1.00121, 0.999945
Selecting incompressible transport model Newtonian
Selecting turbulence model type RASModel
Selecting RAS turbulence model kEpsilon
kEpsilonCoeffs
{
    Cmu             0.09;
    C1              1.44;
    C2              1.92;
    sigmaEps        1.3;
}

Reading/calculating face velocity Uf

No finite volume options present

Courant Number mean: 2.49591e-05 max: 0.0531646
Reading surface description:
    zNormal
    isoQ
    propeller

forces forces:
    Not including porosity effects


Starting time loop

Courant Number mean: 2.4712e-05 max: 0.0526382
deltaT = 1.17647e-05
Time = 1.17647e-05

solidBodyMotionFunctions::rotatingMotion::transformation(): Time = 1.17647e-05 transformation: ((0 0 0) (1 (0 0.000929412 0)))
AMI: Creating addressing and weights between 18496 source faces and 18720 target faces
AMI: Patch source sum(weights) min/max/average = 0.98423, 1.01595, 1.00007
AMI: Patch target sum(weights) min/max/average = 0.962631, 1.00123, 0.999931
PIMPLE: iteration 1
smoothSolver:  Solving for Ux, Initial residual = 1, Final residual = 0.0287315, No Iterations 1
smoothSolver:  Solving for Uy, Initial residual = 1, Final residual = 2.28778e-05, No Iterations 1
smoothSolver:  Solving for Uz, Initial residual = 1, Final residual = 0.0287384, No Iterations 1
GAMG:  Solving for p, Initial residual = 1, Final residual = 0.00911793, No Iterations 7
time step continuity errors : sum local = 6.56636e-07, global = -1.21501e-07, cumulative = -1.21501e-07
PIMPLE: iteration 2
smoothSolver:  Solving for Ux, Initial residual = 0.00534773, Final residual = 8.90939e-07, No Iterations 2
smoothSolver:  Solving for Uy, Initial residual = 0.0695713, Final residual = 4.76815e-07, No Iterations 3
smoothSolver:  Solving for Uz, Initial residual = 0.00541302, Final residual = 8.91135e-07, No Iterations 2
GAMG:  Solving for p, Initial residual = 0.0385816, Final residual = 9.15203e-07, No Iterations 10
time step continuity errors : sum local = 3.61992e-09, global = -4.91902e-10, cumulative = -1.21993e-07
smoothSolver:  Solving for epsilon, Initial residual = 0.000513198, Final residual = 8.99462e-08, No Iterations 2
smoothSolver:  Solving for k, Initial residual = 1, Final residual = 6.75339e-08, No Iterations 5
ExecutionTime = 9.56 s  ClockTime = 9 s

forces forces output:
    sum of forces:
        pressure : (-0.0383127 714.841 -0.0288737)
        viscous  : (-2.95581e-07 -0.00328577 8.35609e-07)
        porous   : (0 0 0)
    sum of moments:
        pressure : (-0.000313981 -3.82599 -0.00178011)
        viscous  : (2.65066e-08 -0.000409938 -8.4531e-09)
        porous   : (0 0 0)


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