Native OpenFOAM v2512 dictionaries for independent public-geometry transient wake case


======== system/controlDict ========
/*--------------------------------*- C++ -*----------------------------------*\
| =========                 |                                                 |
| \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
|  \\    /   O peration     | Version:  2512                                  |
|   \\  /    A nd           | Website:  www.openfoam.com                      |
|    \\/     M anipulation  |                                                 |
\*---------------------------------------------------------------------------*/
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
FoamFile
{
    version         2;
    format          ascii;
    class           dictionary;
    object          controlDict;
}

application     pimpleFoam;

startFrom       latestTime;

startTime       0;

stopAt          endTime;

endTime         2;

deltaT          4e-05;

adjustTimeStep  yes;

maxCo           1;

maxDeltaT       0.0002;

writeControl    adjustableRunTime;

writeInterval   0.02;

purgeWrite      0;

writeFormat     binary;

writePrecision  8;

writeCompression off;

timeFormat      general;

timePrecision   9;

runTimeModifiable true;

functions
{
    force_airframe
    {
        type            forces;
        libs            ( forces );
        patches         ( "aircraft.*" );
        rho             rhoInf;
        rhoInf          1.225;
        CofR            ( -1.5 0 2.3 );
        log             false;
        writeControl    timeStep;
        writeInterval   1;
    }
    force_fuselage
    {
        type            forces;
        libs            ( forces );
        patches         ( aircraft_fuselage );
        rho             rhoInf;
        rhoInf          1.225;
        CofR            ( -1.5 0 2.3 );
        log             false;
        writeControl    timeStep;
        writeInterval   1;
    }
    force_wing
    {
        type            forces;
        libs            ( forces );
        patches         ( aircraft_wing );
        rho             rhoInf;
        rhoInf          1.225;
        CofR            ( -1.5 0 2.3 );
        log             false;
        writeControl    timeStep;
        writeInterval   1;
    }
    force_tail
    {
        type            forces;
        libs            ( forces );
        patches         ( aircraft_tail );
        rho             rhoInf;
        rhoInf          1.225;
        CofR            ( -1.5 0 2.3 );
        log             false;
        writeControl    timeStep;
        writeInterval   1;
    }
    force_booms
    {
        type            forces;
        libs            ( forces );
        patches         ( aircraft_booms );
        rho             rhoInf;
        rhoInf          1.225;
        CofR            ( -1.5 0 2.3 );
        log             false;
        writeControl    timeStep;
        writeInterval   1;
    }
    force_nacelles
    {
        type            forces;
        libs            ( forces );
        patches         ( aircraft_nacelles );
        rho             rhoInf;
        rhoInf          1.225;
        CofR            ( -1.5 0 2.3 );
        log             false;
        writeControl    timeStep;
        writeInterval   1;
    }
    force_gear
    {
        type            forces;
        libs            ( forces );
        patches         ( aircraft_gear );
        rho             rhoInf;
        rhoInf          1.225;
        CofR            ( -1.5 0 2.3 );
        log             false;
        writeControl    timeStep;
        writeInterval   1;
    }
    coefficients
    {
        type            forceCoeffs;
        libs            ( forces );
        patches         ( "aircraft.*" );
        rho             rhoInf;
        rhoInf          1.225;
        liftDir         ( -0.34202 0 0.939693 );
        dragDir         ( 0.939693 0 0.34202 );
        pitchAxis       ( 0 1 0 );
        CofR            ( -1.5 0 2.3 );
        magUInf         44.704;
        lRef            1.55949;
        Aref            22.8159;
        log             false;
        writeControl    timeStep;
        writeInterval   1;
    }
    flux_inlet
    {
        type            surfaceFieldValue;
        libs            ( fieldFunctionObjects );
        regionType      patch;
        name            inlet;
        operation       sum;
        fields          ( phi );
        writeFields     false;
        log             false;
        writeControl    timeStep;
        writeInterval   20;
    }
    flux_outlet
    {
        type            surfaceFieldValue;
        libs            ( fieldFunctionObjects );
        regionType      patch;
        name            outlet;
        operation       sum;
        fields          ( phi );
        writeFields     false;
        log             false;
        writeControl    timeStep;
        writeInterval   20;
    }
    flux_farfield
    {
        type            surfaceFieldValue;
        libs            ( fieldFunctionObjects );
        regionType      patch;
        name            farfield;
        operation       sum;
        fields          ( phi );
        writeFields     false;
        log             false;
        writeControl    timeStep;
        writeInterval   20;
    }
    yPlus
    {
        type            yPlus;
        libs            ( fieldFunctionObjects );
        executeControl  writeTime;
        writeControl    writeTime;
        log             true;
    }
    wallShearStress
    {
        type            wallShearStress;
        libs            ( fieldFunctionObjects );
        patches         ( "aircraft.*" );
        executeControl  timeStep;
        writeControl    writeTime;
    }
    residuals
    {
        type            solverInfo;
        libs            ( utilityFunctionObjects );
        fields          ( p U k omega );
        writeControl    timeStep;
        writeInterval   1;
        log             false;
    }
    Q
    {
        type            Q;
        libs            ( fieldFunctionObjects );
        executeControl  writeTime;
        writeControl    writeTime;
    }
    vorticity
    {
        type            vorticity;
        libs            ( fieldFunctionObjects );
        executeControl  writeTime;
        writeControl    writeTime;
    }
    wakeProbes
    {
        type            probes;
        libs            ( sampling );
        fields          ( U p );
        interpolationScheme cellPoint;
        writeControl    timeStep;
        writeInterval   1;
        probeLocations  ( ( 0 3 3.5 ) ( 3 3 4.5 ) ( 6 3 5.5 ) ( 9 3 6.5 ) ( 12 3 7.5 ) ( 0 -3 3.5 ) ( 3 -3 4.5 ) ( 6 -3 5.5 ) ( 9 -3 6.5 ) ( 12 -3 7.5 ) ( 5 0 4 ) ( 8 0 5 ) ( 11 0 6 ) ( 14 0 7 ) );
    }
    physicalMean
    {
        type            fieldAverage;
        libs            ( fieldFunctionObjects );
        timeStart       0.5;
        executeControl  timeStep;
        executeInterval 1;
        writeControl    writeTime;
        restartOnRestart false;
        fields          ( U { mean on ; prime2Mean on ; base time ; } p { mean on ; prime2Mean on ; base time ; } );
    }
}


// ************************************************************************* //

======== system/fvSchemes ========
FoamFile {version 2; format ascii; class dictionary; object fvSchemes;}

ddtSchemes {default backward;}
gradSchemes {default Gauss linear; grad(U) cellLimited Gauss linear 1;}
divSchemes {default none; div(phi,U) Gauss limitedLinearV 1; div(phi,k) Gauss upwind; div(phi,omega) Gauss upwind; div((nuEff*dev2(T(grad(U))))) Gauss linear;}
laplacianSchemes {default Gauss linear limited 0.5;}
interpolationSchemes {default linear;}
snGradSchemes {default limited 0.5;}
wallDist {method meshWave;}

======== system/fvSolution ========
FoamFile {version 2; format ascii; class dictionary; object fvSolution;}

solvers {
 p {solver GAMG; smoother DICGaussSeidel; tolerance 1e-7; relTol 0.01;}
 pFinal {$p; tolerance 1e-7; relTol 0;}
 "(U|k|omega)" {solver smoothSolver; smoother symGaussSeidel; tolerance 1e-7; relTol 0.01;}
 "(U|k|omega)Final" {solver smoothSolver; smoother symGaussSeidel; tolerance 1e-7; relTol 0;}
}
PIMPLE {nOuterCorrectors 2; nCorrectors 1; nNonOrthogonalCorrectors 1; momentumPredictor yes; pRefCell 0; pRefValue 0;}
relaxationFactors {equations {".*" 1;}}

======== constant/turbulenceProperties ========
FoamFile { version 2.0; format ascii; class dictionary; object turbulenceProperties; }
simulationType RAS; RAS {RASModel kOmegaSST; turbulence on; printCoeffs on;}
======== constant/transportProperties ========
FoamFile { version 2.0; format ascii; class dictionary; object transportProperties; }
transportModel Newtonian; nu 1.46e-05;