/*--------------------------------*- C++ -*----------------------------------*\
| =========                 |                                                 |
| \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
|  \\    /   O peration     | Version:  v2006                                 |
|   \\  /    A nd           | Web:      www.OpenFOAM.com                      |
|    \\/     M anipulation  |                                                 |
\*---------------------------------------------------------------------------*/
FoamFile
{
    version     2.0;
    format      ascii;
    class       dictionary;
    location    "system";
    object      controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

application     pimpleFoam;

startFrom       startTime;

startTime       0;

stopAt          endTime;

endTime         0.2; // 5;

deltaT          1e-3;

writeControl    adjustableRunTime;

writeInterval   0.1;

purgeWrite      0;

writeFormat     ascii;

writePrecision  6;

writeCompression off;

timeFormat      general;

timePrecision   6;

runTimeModifiable true;

adjustTimeStep  yes;

maxCo           0.5;

functions
{
    AMI1
    {
        type            surfaceFieldValue;
        functionObjectLibs ("libfieldFunctionObjects.so");
	log		true;
 	executeControl      timeStep;
        executeInterval     1;
	writeFields	true;
	regionType	patch;
	name		AMI1;
	operation	sum;
	surfaceFormat	none;
	fields		(phi);
    }
    AMI2
    {
         type            surfaceFieldValue;
        functionObjectLibs ("libfieldFunctionObjects.so");
	log		true;
 	executeControl      timeStep;
        executeInterval     1;
	writeFields	true;
	regionType	patch;
	name		AMI2;
	operation	sum;
	surfaceFormat	none;
	fields		(phi);
    }

forces
{
    type        forces;

    functionObjectLibs ( "libforces.so" );

    outputControl   timeStep;
    timeInterval    1;

    log         yes;

    patches     ( "rotor" );
    pName       p;
    UName       U;
    rho     rhoInf;     // Indicates incompressible
    log         true;
    rhoInf      997;        // Redundant for incompressible

    CofR        (0 0 0);    // Rotation around centre line of propeller
    pitchAxis   (0 0 1);
}


}

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