/*---------------------------------------------------------------------------*\
| =========                 |                                                 |
| \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
|  \\    /   O peration     | Version:  2406                                  |
|   \\  /    A nd           | Website:  www.openfoam.com                      |
|    \\/     M anipulation  |                                                 |
\*---------------------------------------------------------------------------*/
Build  : _1653fa08-20260127 OPENFOAM=2406 patch=260127 version=2406
Arch   : "LSB;label=32;scalar=64"
Exec   : rhoSimpleFoam -postProcess -func wallShearStress -noZero -noFunctionObjects
Date   : Aug 31 2026
Time   : 08:19:45
Host   : maxime
PID    : 410
I/O    : uncollated
Case   : /home/maxime/Images/RobustMesh/case_2d/naca0012_trans/naca0012
nProcs : 1
trapFpe: Floating point exception trapping enabled (FOAM_SIGFPE).
fileModificationChecking : Monitoring run-time modified files using timeStampMaster (fileModificationSkew 5, maxFileModificationPolls 20)
allowSystemOperations : Allowing user-supplied system call operations

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

Create mesh for time = 25000


SIMPLE: no convergence criteria found. Calculations will run for 0 steps.

wallShearStress wallShearStress:
    processing all (1) wall patches

Time = 25000
Reading thermophysical properties

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

Reading field U

Reading/calculating face flux field phi

Creating turbulence model

Selecting turbulence model type RAS
Selecting RAS turbulence model kOmegaSST
Selecting patchDistMethod meshWave
RAS
{
    RASModel        kOmegaSST;
    turbulence      on;
    printCoeffs     on;
    alphaK1         0.85;
    alphaK2         1;
    alphaOmega1     0.5;
    alphaOmega2     0.856;
    gamma1          0.55555556;
    gamma2          0.44;
    beta1           0.075;
    beta2           0.0828;
    betaStar        0.09;
    a1              0.31;
    b1              1;
    c1              10;
    F3              false;
    decayControl    false;
    kInf            0;
    omegaInf        0;
}

No MRF models present

Creating finite volume options from "system/fvOptions"

Selecting finite volume options type limitTemperature
    Source: limitT
    - selecting all cells
    - selected 305801 cell(s) with volume 705.60541
wallShearStress wallShearStress write:
    writing field wallShearStress
    min/max(aerofoil) = (-124.93457 -97.815208 -8.8702575e-13), (-1.8480886 52.836599 6.8388251e-13)

End

