Previous: Modifications for practice Up: Modifications for practice Next: When the options are This is an automatically generated documentation by LaTeX2HTML utility. In case of any issue, please, contact us at info@cfdsupport.com. Finer mesh In file blockMeshDict we can change computational mesh to 50×50 cells3.1.# mcedit system/blockMeshDict blocks ( hex (0 1 2 3 4 5 6 7) (50 50 1) simpleGrading (1 1 1) ); Run blockMesh:# blockMesh For transient simulations the Courant number should by always checked. Let us change time step to 0.0005s and computation time to 1.5s. Solution will be saved in times 0.1, 0.2, 0.3, …, 1.5s Let us modify controlDict, e.g.:# gedit system/controlDict stopAt endTime; endTime 1.5; deltaT 0.0005; writeControl runTime; writeInterval 0.1; Run icoFoam on background and forward output into the text file log:# icoFoam > log & It is useful to watch the log file how the computation goes:# tail -f log Pressing ctrl+c one can jump back to the console Results can be viewed during computation in paraview (button Refresh Times always rereads the time layers):# paraFoam Figure: OpenFOAM cavity tutorial. Velocity vector field. Figure: OpenFOAM cavity tutorial. Velocity magnitude. Previous: Modifications for practice Up: Modifications for practice Next: When the options are OpenFOAM Training by CFD Support, CFD SUPPORT, info@cfdsupport.com +420 212 243 883 © CFD support, s.r.o., Sokolovská 270/201, 190 00 Praha 9, Czech Republic
Next: SIMPLE Algorithm Up: TCFDSRTSolver – compressible, transient, Previous: Under-Relaxation Contents Index System of Linear Equations Finite Volume Method converts the system of differential equations to the system of linear equations: Such a linear algebra problem can be solved with following methods implemented in OpenFOAM: Linear system solver method: GAMG (Geometric-Algebraic Multi-Grid) for both symmetric and asymmetric matricesPBiCG (Preconditioned Biconjugate Gradient ) for asymmetric matricesPCG (Preconditioned Conjugate Gradient) for symmetric matricessmoothSolver (solver using a smoother for both symmetric and asymmetric matrices )ICCG (Incomplete Cholesky preconditioned PCG solver, i.e. PBiCG with DIC )3.1BICCG (Diagonal Incomplete LU preconditioned PBiCG solver, i.e. PCG with DILU)3.2 Method preconditioner: DILU (Diagonal Incomplete LU decomposition)DIC (Diagonal incomplete-Cholesky) for symmetric matricesFDIC (Faster diagonal incomplete-Cholesky) for symmetric matricesdiagonal (Diagonal)GAMG (Geometric-Algebraic Multi-Grid)none (No preconditioning)DICGaussSeidel, GaussSeidel, nonBlockingGaussSeidel, symGaussSeidel (for symmetric matrices)For more details see e.g. [10]. Next: SIMPLE Algorithm Up: TCFDSRTSolver – compressible, transient, Previous: Under-Relaxation Contents Index OpenFOAM Training by CFD Support, CFD SUPPORT, info@cfdsupport.com +420 212 243 883 © CFD support, s.r.o., Sokolovská 270/201, 190 00 Praha 9, Czech Republic
Previous: TCFD- Running in Up: TCFD- Running in Next: CFD Processor command mode This is an automatically generated documentation by LaTeX2HTML utility. In case of any issue, please, contact us at info@cfdsupport.com. TCFD – CFD Theory & Formulas SubsectionsFormulas for the Efficiency EvaluationHydro Turbine EfficiencyPump EfficiencyCompressor EfficiencyTurbine EfficiencyFan EfficiencyWind Turbine EfficiencyPropeller EfficiencyStator EfficiencyVirtual Tunnel EfficiencyTCFD SolversblueSolver – steady state, incompressibleblueDyMSolver – transient, incompressibleredSolver – steady state, compressibleredDyMSolver – transient, compressiblegreenSolver – steady state, cavitationgreenDyMSolver – transient, cavitationCompressible Mathematical ModelIncompressible Mathematical ModelUnstructured GridFinite Volume MethodThree DimensionalSteady-StateSegregated SolverCell Centered ApproachUnder-RelaxationSystem of Linear EquationsSIMPLE AlgorithmSpatial Integration Numerical SchemeTemporal Integration Numerical SchemeNon-Orthogonal CorrectorsNumber of Iterations on Rotor and Stator PartMinimal and Maximal Values OptionsTurbulent FlowMRFMessage Passing Interface (MPI)Notes on gravitational potential and hydrostatic pressurePotential of a homogeneous gravitational fieldHydrostatic pressureCenter of mass of a surfaceWater turbines – notes on calculationsAlternative formulationModel settingModel setting without an explicit use of in the momentum equationConclusionInterface between rotor and stator partFrozen Rotor vs. Mixing PlaneCavitation Modeling in TCFDCavitation Risk and Cavitation IndexMultiphase cavitationKeywords in .tcfd file OpenFOAM Training by CFD Support, CFD SUPPORT, info@cfdsupport.com +420 212 243 883 © CFD support, s.r.o., Sokolovská 270/201, 190 00 Praha 9, Czech Republic