/*--------------------------------*- C++ -*----------------------------------*\ | ========= | | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / O peration | Version: v2012 | | \\ / A nd | Website: www.openfoam.com | | \\/ M anipulation | | \*---------------------------------------------------------------------------*/ FoamFile { version 2.0; format ascii; class dictionary; object fvOptions; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // disk { type rotorDisk; 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) ); } } } // ************************************************************************* //