/*--------------------------------*- C++ -*----------------------------------*\
| =========                 |                                                 |
| \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
|  \\    /   O peration     | Version:  v2412                                 |
|   \\  /    A nd           | Website:  www.openfoam.com                      |
|    \\/     M anipulation  |                                                 |
\*---------------------------------------------------------------------------*/

sample.lines
{
    type                sets;
    libs                (sampling);
    writeControl        writeTime;
    timeStart           $tStartAvg;

    interpolationScheme cellPoint;
    setFormat           raw;

    sets
    (
        xbyc0.68
        {
            type            face;
            axis            z;
            start           (6.753000021E-01 0.0001 7.061254978E-02);
            end             (7.216045260E-01 0.0001 3.526125550E-01);
        }
        xbyc0.73
        {
            type            face;
            axis            z;
            start           (7.307999730E-01 0.0001 6.140028313E-02);
            end             (7.803474069E-01 0.0001 3.434002697E-01);
        }
        xbyc0.79
        {
            type            face;
            axis            z;
            start           (7.863000035E-01 0.0001 5.103440955E-02);
            end             (8.403753638E-01 0.0001 3.330343962E-01);
        }
        xbyc0.84
        {
            type            face;
            axis            z;
            start           (8.417999744E-01 0.0001 3.950987384E-02);
            end             (8.998869658E-01 0.0001 3.215098679E-01);
        }
        xbyc0.90
        {
            type            face;
            axis            z;
            start           (8.973000050E-01 0.0001 2.680198476E-02);
            end             (9.618465304E-01 0.0001 3.088019788E-01);
        }
        xbyc0.95
        {
            type            face;
            axis            z;
            start           (9.527999759E-01 0.0001 1.286614314E-02);
            end             (1.022162795E+00 0.0001 2.928661406E-01);
        }
    );

    fields
    (
        columnAverage(UMean)
        columnAverage(UPrime2Mean)
    );
}

sample.aerofoil
{
    type                surfaces;
    libs                (sampling);
    writeControl        writeTime;
    timeStart           $tStartAvg;

    interpolationScheme cell;
    surfaceFormat       raw;

    fields
    (
        pMean
        wallShearStressMean
    );

    surfaces
    (
        aerofoil
        {
            type            patch;
            patches         ( "aerofoil" );
        }
    );
}

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