diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/Allclean b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/Allclean new file mode 100755 index 0000000000..daafdf90aa --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/Allclean @@ -0,0 +1,16 @@ +#!/bin/sh +cd ${0%/*} || exit 1 # run from this directory + +# Source tutorial run functions +. $WM_PROJECT_DIR/bin/tools/CleanFunctions + +cd wingFlutter_snappyHexMesh +cleanCase + +cd ../wingFlutter2D_simpleFoam +cleanCase + +cd ../wingFlutter2D_pimpleDyMFoam +cleanCase +rm -rf 0 + diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/Allrun b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/Allrun new file mode 100755 index 0000000000..23f224782e --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/Allrun @@ -0,0 +1,29 @@ +#!/bin/sh +cd ${0%/*} || exit 1 # run from this directory + +# Source tutorial run functions +. $WM_PROJECT_DIR/bin/tools/RunFunctions + +# Make 3D mesh in slab of cells. +cd wingFlutter_snappyHexMesh +runApplication blockMesh +runApplication snappyHexMesh -overwrite + +# Make a 2D mesh by extruding a patch and solve to steady state. +cd ../wingFlutter2D_simpleFoam +runApplication extrudeMesh +runApplication createPatch -overwrite +runApplication simpleFoam + +# Copy the mesh from the steady state case and map the results to a +# mesh motion case, then solve transient. +cd ../wingFlutter2D_pimpleDyMFoam +cp -r ../wingFlutter2D_simpleFoam/constant/polyMesh/* constant/polyMesh/ +cp -r 0.org 0 +runApplication mapFields ../wingFlutter2D_simpleFoam -sourceTime latestTime -consistent +mv 0/pointDisplacement.unmapped 0/pointDisplacement +runApplication decomposePar +runParallel pimpleDyMFoam 3 +runApplication reconstructPar + +# ----------------------------------------------------------------- end-of-file diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/0.org/U b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/0.org/U new file mode 100644 index 0000000000..345f30007b --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/0.org/U @@ -0,0 +1,45 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: 1.6 | +| \\ / A nd | Web: http://www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ +FoamFile +{ + version 2.0; + format ascii; + class volVectorField; + location "0"; + object U; +} +// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // + +#include "include/initialConditions" + +dimensions [0 1 -1 0 0 0 0]; + +internalField uniform $flowVelocity; + +boundaryField +{ + #include "include/fixedInlet" + + outlet + { + type inletOutlet; + inletValue uniform (0 0 0); + value $internalField; + } + + wing + { + type movingWallVelocity; + value uniform (0 0 0); + } + + #include "include/frontBackTopBottomPatches" +} + + +// ************************************************************************* // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/0.org/include/fixedInlet b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/0.org/include/fixedInlet new file mode 100644 index 0000000000..ccf1d6e897 --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/0.org/include/fixedInlet @@ -0,0 +1,15 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: 1.6 | +| \\ / A nd | Web: http://www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ + +inlet +{ + type fixedValue; + value $internalField; +} + +// ************************************************************************* // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/0.org/include/frontBackTopBottomPatches b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/0.org/include/frontBackTopBottomPatches new file mode 100644 index 0000000000..70336f846e --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/0.org/include/frontBackTopBottomPatches @@ -0,0 +1,24 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: 1.6 | +| \\ / A nd | Web: http://www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ + +topAndBottom +{ + type slip; +} + +front +{ + type empty +} + +back +{ + type empty; +} + +// ************************************************************************* // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/0.org/include/initialConditions b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/0.org/include/initialConditions new file mode 100644 index 0000000000..e0d098096a --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/0.org/include/initialConditions @@ -0,0 +1,15 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: 1.6 | +| \\ / A nd | Web: http://www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ + +flowVelocity (100 0 0); +pressure 0; +turbulentKE 37; +turbulentOmega 32; +#inputMode merge + +// ************************************************************************* // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/0.org/k b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/0.org/k new file mode 100644 index 0000000000..8ba642effb --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/0.org/k @@ -0,0 +1,44 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: 1.6 | +| \\ / A nd | Web: http://www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ +FoamFile +{ + version 2.0; + format ascii; + class volScalarField; + object k; +} +// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // + +#include "include/initialConditions" + +dimensions [0 2 -2 0 0 0 0]; + +internalField uniform $turbulentKE; + +boundaryField +{ + #include "include/fixedInlet" + + outlet + { + type inletOutlet; + inletValue $internalField; + value $internalField; + } + + wing + { + type kqRWallFunction; + value $internalField; + } + + #include "include/frontBackTopBottomPatches" +} + + +// ************************************************************************* // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/0.org/nut b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/0.org/nut new file mode 100644 index 0000000000..27bfad4f39 --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/0.org/nut @@ -0,0 +1,38 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: 1.6 | +| \\ / A nd | Web: www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ +FoamFile +{ + version 2.0; + format ascii; + class volScalarField; + location "0"; + object nut; +} +// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // + +dimensions [0 2 -1 0 0 0 0]; + +internalField uniform 0; + +boundaryField +{ + wing + { + type nutkWallFunction; + value uniform 0; + } + + "(front|back|topAndBottom|inlet|outlet)" + { + type calculated; + value uniform 0; + } +} + + +// ************************************************************************* // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/0.org/omega b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/0.org/omega new file mode 100644 index 0000000000..2024b25ef7 --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/0.org/omega @@ -0,0 +1,44 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: 1.6 | +| \\ / A nd | Web: http://www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ +FoamFile +{ + version 2.0; + format ascii; + class volScalarField; + object epsilon; +} +// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // + +#include "include/initialConditions" + +dimensions [0 0 -1 0 0 0 0]; + +internalField uniform $turbulentOmega; + +boundaryField +{ + #include "include/fixedInlet" + + outlet + { + type inletOutlet; + inletValue $internalField; + value $internalField; + } + + wing + { + type omegaWallFunction; + value $internalField; + } + + #include "include/frontBackTopBottomPatches" +} + + +// ************************************************************************* // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/0.org/p b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/0.org/p new file mode 100644 index 0000000000..78a5d15299 --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/0.org/p @@ -0,0 +1,44 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: 1.6 | +| \\ / A nd | Web: http://www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ +FoamFile +{ + version 2.0; + format ascii; + class volScalarField; + object p; +} +// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // + +#include "include/initialConditions" + +dimensions [0 2 -2 0 0 0 0]; + +internalField uniform $pressure; + +boundaryField +{ + inlet + { + type zeroGradient; + } + + outlet + { + type fixedValue; + value $internalField; + } + + wing + { + type zeroGradient; + } + + #include "include/frontBackTopBottomPatches" +} + +// ************************************************************************* // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/0.org/pointDisplacement b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/0.org/pointDisplacement new file mode 100644 index 0000000000..f51ea94a8d --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/0.org/pointDisplacement @@ -0,0 +1,120 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: 1.6 | +| \\ / A nd | Web: www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ +FoamFile +{ + version 2.0; + format ascii; + class pointVectorField; + location "0.01"; + object pointDisplacement; +} +// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // + +dimensions [0 1 0 0 0 0 0]; + +internalField uniform (0 0 0); + +boundaryField +{ + wing + { + type sixDoFRigidBodyDisplacement; + mass 22.9; + centreOfMass (0.4974612746 -0.01671895744 0.125); + momentOfInertia (1.958864357 3.920839234 2.057121362); + orientation + ( + 0.9953705935 0.09611129781 0 + -0.09611129781 0.9953705935 0 + 0 0 1 + ); + velocity (0 0 0); + acceleration (0 0 0); + angularMomentum (0 0 -0.5); + torque (0 0 0); + rhoName rhoInf; + rhoInf 1; + g (0 -9.81 0); + report on; + constraints + { + maxIterations 500; + + fixedLine1 + { + sixDoFRigidBodyMotionConstraint fixedLine; + tolerance 1e-9; + relaxationFactor 0.7; + fixedLineCoeffs + { + refPoint (0.25 0.007 0.125); + direction (0 1 0); + } + } + + fixedAxis1 + { + sixDoFRigidBodyMotionConstraint fixedAxis; + tolerance 1e-06; + relaxationFactor 0.7; + fixedAxisCoeffs + { + axis ( 0 0 1 ); + } + } + } + restraints + { + verticalSpring + { + sixDoFRigidBodyMotionRestraint linearSpring; + + linearSpringCoeffs + { + anchor (0.25 0.007 0.125); + refAttachmentPt (0.25 0.007 0.125); + stiffness 4000; + damping 2; + restLength 0; + } + } + axialSpring + { + sixDoFRigidBodyMotionRestraint linearAxialAngularSpring; + + linearAxialAngularSpringCoeffs + { + axis (0 0 1); + stiffness 700; + damping 0.5; + referenceOrientation $orientation; + } + } + } + value uniform (0 0 0); + } + + front + { + type empty; + } + + back + { + type empty; + } + + ".*" + { + type fixedValue; + value uniform (0 0 0); + } +} + + +// ************************************************************************* // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/constant/RASProperties b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/constant/RASProperties new file mode 100644 index 0000000000..4e21ca67e4 --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/constant/RASProperties @@ -0,0 +1,25 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: 1.6 | +| \\ / A nd | Web: www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ +FoamFile +{ + version 2.0; + format ascii; + class dictionary; + location "constant"; + object RASProperties; +} +// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // + +RASModel kOmegaSST; + +turbulence on; + +printCoeffs on; + + +// ************************************************************************* // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/constant/dynamicMeshDict b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/constant/dynamicMeshDict new file mode 100644 index 0000000000..986a599c5f --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/constant/dynamicMeshDict @@ -0,0 +1,26 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: 1.6 | +| \\ / A nd | Web: http://www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ +FoamFile +{ + version 2.0; + format ascii; + class dictionary; + object motionProperties; +} +// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // + +dynamicFvMesh dynamicMotionSolverFvMesh; + +motionSolverLibs ("libfvMotionSolvers.so"); + +solver displacementLaplacian; + +diffusivity inverseDistance (wing); + + +// ************************************************************************* // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/constant/polyMesh/boundary b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/constant/polyMesh/boundary new file mode 100644 index 0000000000..87c839b5cc --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/constant/polyMesh/boundary @@ -0,0 +1,58 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: dev | +| \\ / A nd | Web: www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ +FoamFile +{ + version 2.0; + format ascii; + class polyBoundaryMesh; + location "constant/polyMesh"; + object boundary; +} +// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // + +6 +( + topAndBottom + { + type patch; + nFaces 150; + startFace 76473; + } + inlet + { + type patch; + nFaces 48; + startFace 76623; + } + outlet + { + type patch; + nFaces 48; + startFace 76671; + } + front + { + type empty; + nFaces 38129; + startFace 76719; + } + back + { + type empty; + nFaces 38129; + startFace 114848; + } + wing + { + type wall; + nFaces 778; + startFace 152977; + } +) + +// ************************************************************************* // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/constant/transportProperties b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/constant/transportProperties new file mode 100644 index 0000000000..a9d8bf659c --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/constant/transportProperties @@ -0,0 +1,22 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: 1.6 | +| \\ / A nd | Web: http://www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ +FoamFile +{ + version 2.0; + format ascii; + class dictionary; + object transportProperties; +} + +// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // + +transportModel Newtonian; + +nu nu [0 2 -1 0 0 0 0] 1e-05; + +// ************************************************************************* // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/constant/turbulenceProperties b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/constant/turbulenceProperties new file mode 100644 index 0000000000..f6753662e2 --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/constant/turbulenceProperties @@ -0,0 +1,21 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: 1.6 | +| \\ / A nd | Web: www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ +FoamFile +{ + version 2.0; + format ascii; + class dictionary; + location "constant"; + object turbulenceProperties; +} +// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // + +simulationType RASModel; + + +// ************************************************************************* // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/system/controlDict b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/system/controlDict new file mode 100644 index 0000000000..83a4748d21 --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/system/controlDict @@ -0,0 +1,72 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: 1.6 | +| \\ / A nd | Web: www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ +FoamFile +{ + version 2.0; + format ascii; + class dictionary; + location "system"; + object controlDict; +} +// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // + +application pimpleDyMFoam; + +startFrom latestTime; + +startTime 0; + +stopAt endTime; + +endTime 1; + +deltaT 1e-5; + +writeControl adjustableRunTime; + +writeInterval 5e-3; + +purgeWrite 0; + +writeFormat ascii; + +writePrecision 10; + +writeCompression off; + +timeFormat general; + +timePrecision 6; + +runTimeModifiable true; + +adjustTimeStep yes; + +maxCo 0.9; + +libs ("libforces.so"); + +functions +{ + forces + { + type forces; + functionObjectLibs ( "libforces.so" ); + outputControl timeStep; + outputInterval 10; + patches (wing); + pName p; + UName U; + rhoName rhoInf; + log true; + rhoInf 1; + CofR (0.25 0.007 0.125); + } +} + +// ************************************************************************* // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/system/decomposeParDict b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/system/decomposeParDict new file mode 100644 index 0000000000..2dc0a0a25e --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/system/decomposeParDict @@ -0,0 +1,45 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: 1.6 | +| \\ / A nd | Web: www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ +FoamFile +{ + version 2.0; + format ascii; + class dictionary; + location "system"; + object decomposeParDict; +} +// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // + +numberOfSubdomains 3; + +method simple; + +simpleCoeffs +{ + n ( 1 3 1 ); + delta 0.001; +} + +hierarchicalCoeffs +{ + n ( 3 2 1 ); + delta 0.001; + order xyz; +} + +manualCoeffs +{ + dataFile "cellDecomposition"; +} + +metisCoeffs +{ +} + + +// ************************************************************************* // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/system/fvSchemes b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/system/fvSchemes new file mode 100644 index 0000000000..2bee15799d --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/system/fvSchemes @@ -0,0 +1,59 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: 1.6 | +| \\ / A nd | Web: http://www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ +FoamFile +{ + version 2.0; + format ascii; + class dictionary; + object fvSchemes; +} +// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // + +ddtSchemes +{ + default Euler; +} + +gradSchemes +{ + default Gauss linear; + grad(p) Gauss linear; + grad(U) Gauss linear; +} + +divSchemes +{ + default none; + div(phi,U) Gauss linearUpwind grad(U); + div(phi,k) Gauss limitedLinear 1; + div(phi,omega) Gauss limitedLinear 1; + div((nuEff*dev(grad(U).T()))) Gauss linear; +} + +laplacianSchemes +{ + default Gauss linear limited 0.5; +} + +interpolationSchemes +{ + default linear; +} + +snGradSchemes +{ + default corrected; +} + +fluxRequired +{ + default no; + p; +} + +// ************************************************************************* // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/system/fvSolution b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/system/fvSolution new file mode 100644 index 0000000000..038b442397 --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_pimpleDyMFoam/system/fvSolution @@ -0,0 +1,88 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: 1.6 | +| \\ / A nd | Web: http://www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ +FoamFile +{ + version 2.0; + format ascii; + class dictionary; + object fvSolution; +} +// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // + +solvers +{ + p + { + solver GAMG; + tolerance 1e-7; + relTol 0.01; + smoother GaussSeidel; + nPreSweeps 0; + nPostSweeps 2; + cacheAgglomeration on; + agglomerator faceAreaPair; + nCellsInCoarsestLevel 10; + mergeLevels 1; + } + + pFinal + { + solver GAMG; + tolerance 1e-7; + relTol 0; + smoother GaussSeidel; + nPreSweeps 0; + nPostSweeps 2; + cacheAgglomeration on; + agglomerator faceAreaPair; + nCellsInCoarsestLevel 10; + mergeLevels 1; + } + + "(U|k|omega)" + { + solver PBiCG; + preconditioner DILU; + tolerance 1e-06; + relTol 0; + } + + cellDisplacement + { + solver GAMG; + tolerance 1e-5; + relTol 0; + smoother GaussSeidel; + cacheAgglomeration true; + nCellsInCoarsestLevel 10; + agglomerator faceAreaPair; + mergeLevels 1; + } +} + +PIMPLE +{ + nOuterCorrectors 2; + nCorrectors 1; + nNonOrthogonalCorrectors 0; +} + +relaxationFactors +{ + p 0.3; + U 0.7; + k 0.7; + omega 0.7; +} + +cache +{ + grad(U); +} + +// ************************************************************************* // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/0/U b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/0/U new file mode 100644 index 0000000000..bd35fcfb40 --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/0/U @@ -0,0 +1,45 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: 1.6 | +| \\ / A nd | Web: http://www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ +FoamFile +{ + version 2.0; + format ascii; + class volVectorField; + location "0"; + object U; +} +// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // + +#include "include/initialConditions" + +dimensions [0 1 -1 0 0 0 0]; + +internalField uniform $flowVelocity; + +boundaryField +{ + #include "include/fixedInlet" + + outlet + { + type inletOutlet; + inletValue uniform (0 0 0); + value $internalField; + } + + wing + { + type fixedValue; + value uniform (0 0 0); + } + + #include "include/frontBackTopBottomPatches" +} + + +// ************************************************************************* // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/0/include/fixedInlet b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/0/include/fixedInlet new file mode 100644 index 0000000000..ccf1d6e897 --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/0/include/fixedInlet @@ -0,0 +1,15 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: 1.6 | +| \\ / A nd | Web: http://www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ + +inlet +{ + type fixedValue; + value $internalField; +} + +// ************************************************************************* // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/0/include/frontBackTopBottomPatches b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/0/include/frontBackTopBottomPatches new file mode 100644 index 0000000000..70336f846e --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/0/include/frontBackTopBottomPatches @@ -0,0 +1,24 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: 1.6 | +| \\ / A nd | Web: http://www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ + +topAndBottom +{ + type slip; +} + +front +{ + type empty +} + +back +{ + type empty; +} + +// ************************************************************************* // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/0/include/initialConditions b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/0/include/initialConditions new file mode 100644 index 0000000000..e0d098096a --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/0/include/initialConditions @@ -0,0 +1,15 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: 1.6 | +| \\ / A nd | Web: http://www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ + +flowVelocity (100 0 0); +pressure 0; +turbulentKE 37; +turbulentOmega 32; +#inputMode merge + +// ************************************************************************* // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/0/k b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/0/k new file mode 100644 index 0000000000..8ba642effb --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/0/k @@ -0,0 +1,44 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: 1.6 | +| \\ / A nd | Web: http://www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ +FoamFile +{ + version 2.0; + format ascii; + class volScalarField; + object k; +} +// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // + +#include "include/initialConditions" + +dimensions [0 2 -2 0 0 0 0]; + +internalField uniform $turbulentKE; + +boundaryField +{ + #include "include/fixedInlet" + + outlet + { + type inletOutlet; + inletValue $internalField; + value $internalField; + } + + wing + { + type kqRWallFunction; + value $internalField; + } + + #include "include/frontBackTopBottomPatches" +} + + +// ************************************************************************* // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/0/nut b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/0/nut new file mode 100644 index 0000000000..27bfad4f39 --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/0/nut @@ -0,0 +1,38 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: 1.6 | +| \\ / A nd | Web: www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ +FoamFile +{ + version 2.0; + format ascii; + class volScalarField; + location "0"; + object nut; +} +// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // + +dimensions [0 2 -1 0 0 0 0]; + +internalField uniform 0; + +boundaryField +{ + wing + { + type nutkWallFunction; + value uniform 0; + } + + "(front|back|topAndBottom|inlet|outlet)" + { + type calculated; + value uniform 0; + } +} + + +// ************************************************************************* // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/0/omega b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/0/omega new file mode 100644 index 0000000000..2024b25ef7 --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/0/omega @@ -0,0 +1,44 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: 1.6 | +| \\ / A nd | Web: http://www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ +FoamFile +{ + version 2.0; + format ascii; + class volScalarField; + object epsilon; +} +// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // + +#include "include/initialConditions" + +dimensions [0 0 -1 0 0 0 0]; + +internalField uniform $turbulentOmega; + +boundaryField +{ + #include "include/fixedInlet" + + outlet + { + type inletOutlet; + inletValue $internalField; + value $internalField; + } + + wing + { + type omegaWallFunction; + value $internalField; + } + + #include "include/frontBackTopBottomPatches" +} + + +// ************************************************************************* // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/0/p b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/0/p new file mode 100644 index 0000000000..78a5d15299 --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/0/p @@ -0,0 +1,44 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: 1.6 | +| \\ / A nd | Web: http://www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ +FoamFile +{ + version 2.0; + format ascii; + class volScalarField; + object p; +} +// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // + +#include "include/initialConditions" + +dimensions [0 2 -2 0 0 0 0]; + +internalField uniform $pressure; + +boundaryField +{ + inlet + { + type zeroGradient; + } + + outlet + { + type fixedValue; + value $internalField; + } + + wing + { + type zeroGradient; + } + + #include "include/frontBackTopBottomPatches" +} + +// ************************************************************************* // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/constant/RASProperties b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/constant/RASProperties new file mode 100644 index 0000000000..4e21ca67e4 --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/constant/RASProperties @@ -0,0 +1,25 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: 1.6 | +| \\ / A nd | Web: www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ +FoamFile +{ + version 2.0; + format ascii; + class dictionary; + location "constant"; + object RASProperties; +} +// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // + +RASModel kOmegaSST; + +turbulence on; + +printCoeffs on; + + +// ************************************************************************* // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/constant/extrudeProperties b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/constant/extrudeProperties new file mode 100644 index 0000000000..bbb18ba9e6 --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/constant/extrudeProperties @@ -0,0 +1,47 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: 1.6 | +| \\ / A nd | Web: http://www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ +FoamFile +{ + version 2.0; + format ascii; + class dictionary; + object extrudeProperties; +} +// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // + +// What to extrude: +// patch : from patch of another case ('sourceCase') + +constructFrom patch; +sourceCase "../wingFlutter_snappyHexMesh"; +sourcePatches (front); + +// If construct from patch: patch to use for back (can be same as sourcePatch) +exposedPatchName back; + +// Flip surface normals before usage. +flipNormals false; + +//- Linear extrusion in point-normal direction +extrudeModel linearNormal; + +nLayers 1; + +expansionRatio 1.0; + +linearNormalCoeffs +{ + thickness 0.05; +} + +// Do front and back need to be merged? Usually only makes sense for 360 +// degree wedges. +mergeFaces false; + + +// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/constant/polyMesh/boundary b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/constant/polyMesh/boundary new file mode 100644 index 0000000000..87c839b5cc --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/constant/polyMesh/boundary @@ -0,0 +1,58 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: dev | +| \\ / A nd | Web: www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ +FoamFile +{ + version 2.0; + format ascii; + class polyBoundaryMesh; + location "constant/polyMesh"; + object boundary; +} +// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // + +6 +( + topAndBottom + { + type patch; + nFaces 150; + startFace 76473; + } + inlet + { + type patch; + nFaces 48; + startFace 76623; + } + outlet + { + type patch; + nFaces 48; + startFace 76671; + } + front + { + type empty; + nFaces 38129; + startFace 76719; + } + back + { + type empty; + nFaces 38129; + startFace 114848; + } + wing + { + type wall; + nFaces 778; + startFace 152977; + } +) + +// ************************************************************************* // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/constant/transportProperties b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/constant/transportProperties new file mode 100644 index 0000000000..a9d8bf659c --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/constant/transportProperties @@ -0,0 +1,22 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: 1.6 | +| \\ / A nd | Web: http://www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ +FoamFile +{ + version 2.0; + format ascii; + class dictionary; + object transportProperties; +} + +// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // + +transportModel Newtonian; + +nu nu [0 2 -1 0 0 0 0] 1e-05; + +// ************************************************************************* // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/system/controlDict b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/system/controlDict new file mode 100644 index 0000000000..7e8f0995ed --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/system/controlDict @@ -0,0 +1,67 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: 1.6 | +| \\ / A nd | Web: www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ +FoamFile +{ + version 2.0; + format ascii; + class dictionary; + location "system"; + object controlDict; +} +// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // + +application simpleFoam; + +startFrom latestTime; + +startTime 0; + +stopAt endTime; + +endTime 3000; + +deltaT 1; + +writeControl runTime; + +writeInterval 100; + +purgeWrite 0; + +writeFormat ascii; + +writePrecision 6; + +writeCompression off; + +timeFormat general; + +timePrecision 6; + +runTimeModifiable true; + +functions +{ + forces + { + type forces; + functionObjectLibs ( "libforces.so" ); + outputControl timeStep; + outputInterval 10; + patches (wing); + pName p; + UName U; + rhoName rhoInf; + log true; + rhoInf 1; + CofR (0.4974612746 -0.01671895744 0.125); + } +} + + +// ************************************************************************* // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/system/createPatchDict b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/system/createPatchDict new file mode 100644 index 0000000000..b75b8e1075 --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/system/createPatchDict @@ -0,0 +1,49 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: 1.6 | +| \\ / A nd | Web: http://www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ +FoamFile +{ + version 2.0; + format ascii; + class dictionary; + object createPatchDict; +} + +// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // + +// Tolerance used in matching faces. Absolute tolerance is span of +// face times this factor. To load incorrectly matches meshes set this +// to a higher value. +matchTolerance 1E-3; + +// Do a synchronisation of coupled points after creation of any patches. +// Note: this does not work with points that are on multiple coupled patches +// with transformations. +pointSync true; + +// Patches to create. +patches +( + { + // Name of new patch + name wing; + + // Type of new patch + patchInfo + { + type wall; + } + + // How to construct: either from 'patches' or 'set' + constructFrom patches; + + // If constructFrom = patches : names of patches. Wildcards allowed. + patches ( wing_5degrees.obj_WALL10 ); + } +); + +// ************************************************************************* // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/system/fvSchemes b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/system/fvSchemes new file mode 100644 index 0000000000..2eb6038d7f --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/system/fvSchemes @@ -0,0 +1,59 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: 1.6 | +| \\ / A nd | Web: http://www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ +FoamFile +{ + version 2.0; + format ascii; + class dictionary; + object fvSchemes; +} +// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // + +ddtSchemes +{ + default steadyState; +} + +gradSchemes +{ + default Gauss linear; + grad(p) Gauss linear; + grad(U) Gauss linear; +} + +divSchemes +{ + default none; + div(phi,U) Gauss linearUpwind grad(U); + div(phi,k) Gauss upwind; + div(phi,omega) Gauss upwind; + div((nuEff*dev(grad(U).T()))) Gauss linear; +} + +laplacianSchemes +{ + default Gauss linear corrected; +} + +interpolationSchemes +{ + default linear; +} + +snGradSchemes +{ + default corrected; +} + +fluxRequired +{ + default no; + p; +} + +// ************************************************************************* // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/system/fvSolution b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/system/fvSolution new file mode 100644 index 0000000000..e99098b5b9 --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter2D_simpleFoam/system/fvSolution @@ -0,0 +1,79 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: 1.6 | +| \\ / A nd | Web: http://www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ +FoamFile +{ + version 2.0; + format ascii; + class dictionary; + object fvSolution; +} +// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // + +solvers +{ + p + { + solver GAMG; + tolerance 1e-7; + relTol 0.1; + smoother GaussSeidel; + nPreSweeps 0; + nPostSweeps 2; + cacheAgglomeration on; + agglomerator faceAreaPair; + nCellsInCoarsestLevel 10; + mergeLevels 1; + } + + U + { + solver smoothSolver; + smoother GaussSeidel; + tolerance 1e-8; + relTol 0.1; + nSweeps 1; + } + + k + { + solver smoothSolver; + smoother GaussSeidel; + tolerance 1e-8; + relTol 0.1; + nSweeps 1; + } + + omega + { + solver smoothSolver; + smoother GaussSeidel; + tolerance 1e-8; + relTol 0.1; + nSweeps 1; + } +} + +SIMPLE +{ + nNonOrthogonalCorrectors 0; +} + +relaxationFactors +{ + p 0.3; + U 0.7; + k 0.7; + omega 0.7; +} + +cache +{ + grad(U); +} + +// ************************************************************************* // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter_snappyHexMesh/constant/polyMesh/blockMeshDict b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter_snappyHexMesh/constant/polyMesh/blockMeshDict new file mode 100644 index 0000000000..1a5ba112ca --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter_snappyHexMesh/constant/polyMesh/blockMeshDict @@ -0,0 +1,74 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: 1.6 | +| \\ / A nd | Web: http://www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ +FoamFile +{ + version 2.0; + format ascii; + class dictionary; + object blockMeshDict; +} + +// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // + +convertToMeters 1; + +vertices +( + (-2.5 -4.8 -0.1) + ( 10 -4.8 -0.1) + ( 10 4.8 -0.1) + (-2.5 4.8 -0.1) + (-2.5 -4.8 0.1) + ( 10 -4.8 0.1) + ( 10 4.8 0.1) + (-2.5 4.8 0.1) +); + +blocks +( + hex (0 1 2 3 4 5 6 7) (75 48 1) simpleGrading (1 1 1) +); + +edges +( +); + +patches +( + patch topAndBottom + ( + (3 7 6 2) + (1 5 4 0) + ) + + patch inlet + ( + (0 4 7 3) + ) + + patch outlet + ( + (2 6 5 1) + ) + + empty front + ( + (4 5 6 7) + ) + + empty back + ( + (0 3 2 1) + ) +); + +mergePatchPairs +( +); + +// ************************************************************************* // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter_snappyHexMesh/constant/polyMesh/boundary b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter_snappyHexMesh/constant/polyMesh/boundary new file mode 100644 index 0000000000..450937dc95 --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter_snappyHexMesh/constant/polyMesh/boundary @@ -0,0 +1,58 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: dev | +| \\ / A nd | Web: www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ +FoamFile +{ + version 2.0; + format ascii; + class polyBoundaryMesh; + location "constant/polyMesh"; + object boundary; +} +// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // + +6 +( + topAndBottom + { + type patch; + nFaces 150; + startFace 2098769; + } + inlet + { + type patch; + nFaces 48; + startFace 2098919; + } + outlet + { + type patch; + nFaces 48; + startFace 2098967; + } + front + { + type empty; + nFaces 38129; + startFace 2099015; + } + back + { + type empty; + nFaces 38120; + startFace 2137144; + } + wing_5degrees.obj_WALL10 + { + type wall; + nFaces 49792; + startFace 2175264; + } +) + +// ************************************************************************* // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter_snappyHexMesh/constant/triSurface/wing_5degrees.obj b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter_snappyHexMesh/constant/triSurface/wing_5degrees.obj new file mode 100644 index 0000000000..4be2aac5f2 --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter_snappyHexMesh/constant/triSurface/wing_5degrees.obj @@ -0,0 +1,1054 @@ +# Wavefront OBJ file written 2010-05-13T09:12:43 +o wing_5degrees + +# points : 520 +# faces : 520 +# zones : 1 +# 0 WALL10 (nFaces: 520) + +# +v 1.00488 -0.0890722 -0.5 +v 1.00488 -0.0890722 0.5 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a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter_snappyHexMesh/system/controlDict b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter_snappyHexMesh/system/controlDict new file mode 100644 index 0000000000..1259284a3d --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter_snappyHexMesh/system/controlDict @@ -0,0 +1,50 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: 1.6 | +| \\ / A nd | Web: www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ +FoamFile +{ + version 2.0; + format ascii; + class dictionary; + location "system"; + object controlDict; +} +// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // + +application snappyHexMesh; + +startFrom latestTime; + +startTime 0; + +stopAt endTime; + +endTime 100; + +deltaT 1; + +writeControl runTime; + +writeInterval 1; + +purgeWrite 0; + +writeFormat ascii; + +writePrecision 6; + +writeCompression off; + +timeFormat general; + +timePrecision 6; + +runTimeModifiable true; + +} + +// ************************************************************************* // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter_snappyHexMesh/system/decomposeParDict b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter_snappyHexMesh/system/decomposeParDict new file mode 100644 index 0000000000..2dc0a0a25e --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter_snappyHexMesh/system/decomposeParDict @@ -0,0 +1,45 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: 1.6 | +| \\ / A nd | Web: www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ +FoamFile +{ + version 2.0; + format ascii; + class dictionary; + location "system"; + object decomposeParDict; +} +// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // + +numberOfSubdomains 3; + +method simple; + +simpleCoeffs +{ + n ( 1 3 1 ); + delta 0.001; +} + +hierarchicalCoeffs +{ + n ( 3 2 1 ); + delta 0.001; + order xyz; +} + +manualCoeffs +{ + dataFile "cellDecomposition"; +} + +metisCoeffs +{ +} + + +// ************************************************************************* // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter_snappyHexMesh/system/fvSchemes b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter_snappyHexMesh/system/fvSchemes new file mode 100644 index 0000000000..ae2773bf84 --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter_snappyHexMesh/system/fvSchemes @@ -0,0 +1,70 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: 1.6 | +| \\ / A nd | Web: www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ +FoamFile +{ + version 2.0; + format ascii; + class dictionary; + location "system"; + object fvSchemes; +} +// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // + +ddtSchemes +{ + default Euler; +} + +gradSchemes +{ + default Gauss linear; +} + +divSchemes +{ + default none; + div(phi,U) Gauss limitedLinearV 1; + div(phi,k) Gauss upwind; + div(phi,epsilon) Gauss upwind; + div(phi,R) Gauss upwind; + div(R) Gauss linear; + div(phid,p) Gauss limitedLinear 1; + div(phiU,p) Gauss limitedLinear 1; + div(phi,e) Gauss limitedLinear 1; + div((muEff*dev2(grad(U).T()))) Gauss linear; +} + +laplacianSchemes +{ + default none; + laplacian(muEff,U) Gauss linear limited 0.5; + laplacian(DkEff,k) Gauss linear limited 0.5; + laplacian(DREff,R) Gauss linear limited 0.5; + laplacian(DepsilonEff,epsilon) Gauss linear limited 0.5; + laplacian((rho*(1|A(U))),p) Gauss linear limited 0.5; + laplacian(alphaEff,e) Gauss linear limited 0.5; +} + +interpolationSchemes +{ + default linear; +} + +snGradSchemes +{ + default corrected; +} + +fluxRequired +{ + default no; + p; +} + + +// ************************************************************************* // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter_snappyHexMesh/system/fvSolution b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter_snappyHexMesh/system/fvSolution new file mode 100644 index 0000000000..d85a6d5e98 --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter_snappyHexMesh/system/fvSolution @@ -0,0 +1,51 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: 1.6 | +| \\ / A nd | Web: www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ +FoamFile +{ + version 2.0; + format ascii; + class dictionary; + location "system"; + object fvSolution; +} +// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // + +solvers +{ + p + { + solver PBiCG; + preconditioner DILU; + tolerance 1e-12; + relTol 0; + } + + rho + { + solver PCG; + preconditioner DIC; + tolerance 1e-08; + relTol 0; + } + + "(U|e|k|epsilon|R)" + { + $p; + tolerance 1e-08; + relTol 0; + } +} + +PISO +{ + nCorrectors 2; + nNonOrthogonalCorrectors 2; +} + + +// ************************************************************************* // diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter_snappyHexMesh/system/snappyHexMeshDict b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter_snappyHexMesh/system/snappyHexMeshDict new file mode 100644 index 0000000000..2300d79207 --- /dev/null +++ b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter_snappyHexMesh/system/snappyHexMeshDict @@ -0,0 +1,326 @@ +/*--------------------------------*- C++ -*----------------------------------*\ +| ========= | | +| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | +| \\ / O peration | Version: 1.6 | +| \\ / A nd | Web: http://www.OpenFOAM.org | +| \\/ M anipulation | | +\*---------------------------------------------------------------------------*/ +FoamFile +{ + version 2.0; + format ascii; + class dictionary; + object snappyHexMeshDict; +} +// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // + +// Which of the steps to run +castellatedMesh true; +snap true; +addLayers true; + + +// Geometry. Definition of all surfaces. All surfaces are of class +// searchableSurface. +// Surfaces are used +// - to specify refinement for any mesh cell intersecting it +// - to specify refinement for any mesh cell inside/outside/near +// - to 'snap' the mesh boundary to the surface +geometry +{ + wing_5degrees.obj + { + type triSurfaceMesh; + } + + refinementBox + { + type searchableBox; + min (-1 -1 -1); + max ( 5 1 1); + } +}; + + + +// Settings for the castellatedMesh generation. +castellatedMeshControls +{ + + // Refinement parameters + // ~~~~~~~~~~~~~~~~~~~~~ + + // If local number of cells is >= maxLocalCells on any processor + // switches from from refinement followed by balancing + // (current method) to (weighted) balancing before refinement. + maxLocalCells 1000000; + + // Overall cell limit (approximately). Refinement will stop immediately + // upon reaching this number so a refinement level might not complete. + // Note that this is the number of cells before removing the part which + // is not 'visible' from the keepPoint. The final number of cells might + // actually be a lot less. + maxGlobalCells 2000000; + + // The surface refinement loop might spend lots of iterations refining just a + // few cells. This setting will cause refinement to stop if <= minimumRefine + // are selected for refinement. Note: it will at least do one iteration + // (unless the number of cells to refine is 0) + minRefinementCells 100; + + // Number of buffer layers between different levels. + // 1 means normal 2:1 refinement restriction, larger means slower + // refinement. + nCellsBetweenLevels 6; + + + + // Explicit feature edge refinement + // ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ + + // Specifies a level for any cell intersected by its edges. + // This is a featureEdgeMesh, read from constant/triSurface for now. + features (); + + + + // Surface based refinement + // ~~~~~~~~~~~~~~~~~~~~~~~~ + + // Specifies two levels for every surface. The first is the minimum level, + // every cell intersecting a surface gets refined up to the minimum level. + // The second level is the maximum level. Cells that 'see' multiple + // intersections where the intersections make an + // angle > resolveFeatureAngle get refined up to the maximum level. + + refinementSurfaces + { + wing_5degrees.obj + { + // Surface-wise min and max refinement level + level (6 6); + } + } + + // Resolve sharp angles on fridges + resolveFeatureAngle 30; + + + // Region-wise refinement + // ~~~~~~~~~~~~~~~~~~~~~~ + + // Specifies refinement level for cells in relation to a surface. One of + // three modes + // - distance. 'levels' specifies per distance to the surface the + // wanted refinement level. The distances need to be specified in + // descending order. + // - inside. 'levels' is only one entry and only the level is used. All + // cells inside the surface get refined up to the level. The surface + // needs to be closed for this to be possible. + // - outside. Same but cells outside. + + refinementRegions + { + refinementBox + { + mode inside; + levels ((1e15 3)); + } + } + + + // Mesh selection + // ~~~~~~~~~~~~~~ + + // After refinement patches get added for all refinementSurfaces and + // all cells intersecting the surfaces get put into these patches. The + // section reachable from the locationInMesh is kept. + // NOTE: This point should never be on a face, always inside a cell, even + // after refinement. + locationInMesh (-0.5 0 0); + + + // Whether any faceZones (as specified in the refinementSurfaces) + // are only on the boundary of corresponding cellZones or also allow + // free-standing zone faces. Not used if there are no faceZones. + allowFreeStandingZoneFaces true; +} + + + +// Settings for the snapping. +snapControls +{ + //- Number of patch smoothing iterations before finding correspondence + // to surface + nSmoothPatch 3; + + //- Relative distance for points to be attracted by surface feature point + // or edge. True distance is this factor times local + // maximum edge length. + tolerance 4.0; + + //- Number of mesh displacement relaxation iterations. + nSolveIter 30; + + //- Maximum number of snapping relaxation iterations. Should stop + // before upon reaching a correct mesh. + nRelaxIter 5; +} + + + +// Settings for the layer addition. +addLayersControls +{ + // Are the thickness parameters below relative to the undistorted + // size of the refined cell outside layer (true) or absolute sizes (false). + relativeSizes true; + + // Per final patch (so not geometry!) the layer information + layers + { + "wing.*" + { + nSurfaceLayers 3; + } + } + + // Expansion factor for layer mesh + expansionRatio 1.3; + + //- Wanted thickness of final added cell layer. If multiple layers + // is the + // thickness of the layer furthest away from the wall. + // Relative to undistorted size of cell outside layer. + // is the thickness of the layer furthest away from the wall. + // See relativeSizes parameter. + finalLayerThickness 0.7; + + //- Minimum thickness of cell layer. If for any reason layer + // cannot be above minThickness do not add layer. + // Relative to undistorted size of cell outside layer. + // See relativeSizes parameter. + minThickness 0.25; + + //- If points get not extruded do nGrow layers of connected faces that are + // also not grown. This helps convergence of the layer addition process + // close to features. + nGrow 0; + + + // Advanced settings + + //- When not to extrude surface. 0 is flat surface, 90 is when two faces + // make straight angle. + featureAngle 60; + + //- Maximum number of snapping relaxation iterations. Should stop + // before upon reaching a correct mesh. + nRelaxIter 5; + + // Number of smoothing iterations of surface normals + nSmoothSurfaceNormals 1; + + // Number of smoothing iterations of interior mesh movement direction + nSmoothNormals 3; + + // Smooth layer thickness over surface patches + nSmoothThickness 10; + + // Stop layer growth on highly warped cells + maxFaceThicknessRatio 0.5; + + // Reduce layer growth where ratio thickness to medial + // distance is large + maxThicknessToMedialRatio 0.3; + + // Angle used to pick up medial axis points + // Note: changed(corrected) w.r.t 16x! 90 degrees corresponds to 130 in 16x. + minMedianAxisAngle 90; + + // Create buffer region for new layer terminations + nBufferCellsNoExtrude 0; + + + // Overall max number of layer addition iterations. The mesher will exit + // if it reaches this number of iterations; possibly with an illegal + // mesh. + nLayerIter 50; +} + + + +// Generic mesh quality settings. At any undoable phase these determine +// where to undo. +meshQualityControls +{ + //- Maximum non-orthogonality allowed. Set to 180 to disable. + maxNonOrtho 65; + + //- Max skewness allowed. Set to <0 to disable. + maxBoundarySkewness 20; + maxInternalSkewness 4; + + //- Max concaveness allowed. Is angle (in degrees) below which concavity + // is allowed. 0 is straight face, <0 would be convex face. + // Set to 180 to disable. + maxConcave 80; + + //- Minimum pyramid volume. Is absolute volume of cell pyramid. + // Set to a sensible fraction of the smallest cell volume expected. + // Set to very negative number (e.g. -1E30) to disable. + minVol 1e-13; + + //- Minimum tet volume. Is absolute volume of the tet formed by the + // face-centre decomposition triangle and the cell centre. + // Set to a sensible fraction of the smallest cell volume expected. + // Set to very negative number (e.g. -1E30) to disable. + minTetVol 1e-20; + + //- Minimum face area. Set to <0 to disable. + minArea -1; + + //- Minimum face twist. Set to <-1 to disable. dot product of face normal + //- and face centre triangles normal + minTwist 0.05; + + //- minimum normalised cell determinant + //- 1 = hex, <= 0 = folded or flattened illegal cell + minDeterminant 0.001; + + //- minFaceWeight (0 -> 0.5) + minFaceWeight 0.05; + + //- minVolRatio (0 -> 1) + minVolRatio 0.01; + + //must be >0 for Fluent compatibility + minTriangleTwist -1; + + + // Advanced + + //- Number of error distribution iterations + nSmoothScale 4; + //- amount to scale back displacement at error points + errorReduction 0.75; +} + + +// Advanced + +// Flags for optional output +// 0 : only write final meshes +// 1 : write intermediate meshes +// 2 : write volScalarField with cellLevel for postprocessing +// 4 : write current intersections as .obj files +debug 0; + + +// Merge tolerance. Is fraction of overall bounding box of initial mesh. +// Note: the write tolerance needs to be higher than this. +mergeTolerance 1E-6; + + +// ************************************************************************* //