forces
{
    type            forceCoeffs;
    libs            (forces);
    writeControl    timeStep;
    writeInterval   1;

    patches         (Airfoil airfoil airfoil_slat airfoil_main airfoil_flap);

    rho             rhoInf;
    rhoInf          0.1524;

    log             false;

    liftDir         (0 1 0);
    dragDir         (1 0 0);
    CofR            (0.25 0 0);
    pitchAxis       (0 0 1);

    magUInf         238.174;
    lRef            1;
    Aref            1;
}
