|
[Sponsors] |
Using rotorDisk(or any other blade simulator) for mixing purpose by applying fvOption |
|
LinkBack | Thread Tools | Search this Thread | Display Modes |
January 18, 2021, 16:47 |
Using rotorDisk(or any other blade simulator) for mixing purpose by applying fvOption
|
#1 |
Senior Member
Farzad Faraji
Join Date: Nov 2019
Posts: 206
Rep Power: 8 |
Dear Friends
I want to use rotorDisk example in my case which is a lagrangian solver(I have already added fvOptions and I can add external momentum sources). according to the code; https://github.com/OpenFOAM/OpenFOAM...stem/fvOptions which I copied here; Code:
/*--------------------------------*- C++ -*----------------------------------*\ ========= | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox \\ / O peration | Website: https://openfoam.org \\ / A nd | Version: 6 \\/ 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) ); } } } // ************************************************************************* // Thanks, Farzad |
|
Tags |
fvoptions, lagrangian, rotordisksource |
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
How to split air blade in CFX Post without loosing accuracy | JonasII | CFX | 7 | May 18, 2021 17:54 |
Gaps between Turbine Blade Rows | cdelorenzo | CFX | 1 | November 26, 2019 02:22 |
[TurboGrid] Slotted rotor Blade using Turbogrid | drcsm | ANSYS Meshing & Geometry | 0 | March 15, 2016 01:26 |
Problem in conducting CFD of analysis of wind turbine blade | atulpat | CFX | 16 | August 17, 2013 05:09 |
Compressor Blade Analysis in Ansys CFX | LynchMobster47 | Main CFD Forum | 0 | April 10, 2012 23:43 |