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|
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 4.x |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object fvOptions;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
disk
{
type rotorDisk;
active on;
rotorDiskCoeffs
{
selectionMode cellZone;
cellZone rotatingZone;
fields (U); // Names of fields on which to apply source
nBlades 3; // Number of blades
tipEffect 0.96; // Normalised radius above which lift = 0
inletFlowType local; // Inlet flow type specification
inletVelocity (0 1 0);
geometryMode specified;
origin (0 0 0);
axis (0 1 0);
refDirection (0 0 1); // Reference direction
// - used as reference for psi angle
rpm 1000;
//pointAbove (0 0 0.25);
trimModel fixedTrim; // fixed || targetForce
rhoRef 1000;
rhoInf 1;
fixedTrimCoeffs
{
theta0 0;
theta1c 0;
theta1s 0;
}
flapCoeffs
{
beta0 0; // Coning angle [deg]
beta1c 0; // Lateral flapping coeff (cos coeff)
beta2s 0; // Longitudinal flapping coeff (sin coeff)
}
blade
{
data
(
(profile1 (0.1 -6 0.02))
(profile1 (0.25 -6 0.02))
);
}
profiles
{
profile1
{
type lookup;
data
(
(-90 0.21 1.45)
(-18 0.21 1.45)
(-16 0.165 1.3)
(-14 0.125 1.1)
(-12 0.092 0.95)
(-10 0.07 0.8)
(-8 0.05 0.64)
(-6 0.04 0.5)
(-4 0.028 0.32)
(-2 0.022 0.18)
(0 0.02 0)
(2 0.022 0.18)
(4 0.028 0.32)
(6 0.04 0.5)
(8 0.05 0.64)
(10 0.07 0.8)
(12 0.092 0.95)
(14 0.125 1.1)
(16 0.165 1.3)
(18 0.21 1.45)
(90 0.21 1.45)
);
}
}
}
}
// ************************************************************************* //
|
