diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/Allclean b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/Allclean
new file mode 100755
index 0000000000000000000000000000000000000000..daafdf90aa2acf7e70397901afba87ecc7b9017e
--- /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 0000000000000000000000000000000000000000..23f224782ea73e3b0ac7b33a52420e25660e9175
--- /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 0000000000000000000000000000000000000000..345f30007b004214f5e2d9dbe032e1e5313412b4
--- /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 0000000000000000000000000000000000000000..ccf1d6e897baf617a75af14cdf49e136cb168f4d
--- /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 0000000000000000000000000000000000000000..70336f846e6428ba9578120138cf680fb4fc4b05
--- /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 0000000000000000000000000000000000000000..e0d098096aea7dcb37f78c607bd48210b3860f16
--- /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 0000000000000000000000000000000000000000..8ba642effb82407c85cd573a4003cf5b64fc6c51
--- /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 0000000000000000000000000000000000000000..27bfad4f3909450b4e2e115c1e20da313e5e0502
--- /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 0000000000000000000000000000000000000000..2024b25ef7a61172628ed36c60ce313ccc428081
--- /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 0000000000000000000000000000000000000000..78a5d1529945bb82c0ce7bd21e0e39bca8196f32
--- /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 0000000000000000000000000000000000000000..f51ea94a8d0b46e410b580d3d0d9f4c0804ee0e7
--- /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 0000000000000000000000000000000000000000..4e21ca67e4664818ae61d6e2810f816ea3613943
--- /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 0000000000000000000000000000000000000000..986a599c5f6fb54ca9ce0f46162ad9217b1e213d
--- /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 0000000000000000000000000000000000000000..87c839b5cc87ad27afc6454cadeabdf17a56cac9
--- /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 0000000000000000000000000000000000000000..a9d8bf659c481e6b65403d6814dbbf361361b5ba
--- /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 0000000000000000000000000000000000000000..f6753662e27e414f4bfb666745b7888fef8510bb
--- /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 0000000000000000000000000000000000000000..83a4748d219e7d56dfc4d510e565ab8b2321eb2f
--- /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 0000000000000000000000000000000000000000..2dc0a0a25e2f99ce5eb53af57cf68543bf23eff6
--- /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 0000000000000000000000000000000000000000..2bee15799dbc02b91812c538ff4bb95babbc39d4
--- /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 0000000000000000000000000000000000000000..038b442397ebdf55f778c1d22f15909c56b38397
--- /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 0000000000000000000000000000000000000000..bd35fcfb40cc0394b19a543f3f1607549e463108
--- /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 0000000000000000000000000000000000000000..ccf1d6e897baf617a75af14cdf49e136cb168f4d
--- /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 0000000000000000000000000000000000000000..70336f846e6428ba9578120138cf680fb4fc4b05
--- /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 0000000000000000000000000000000000000000..e0d098096aea7dcb37f78c607bd48210b3860f16
--- /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 0000000000000000000000000000000000000000..8ba642effb82407c85cd573a4003cf5b64fc6c51
--- /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 0000000000000000000000000000000000000000..27bfad4f3909450b4e2e115c1e20da313e5e0502
--- /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 0000000000000000000000000000000000000000..2024b25ef7a61172628ed36c60ce313ccc428081
--- /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 0000000000000000000000000000000000000000..78a5d1529945bb82c0ce7bd21e0e39bca8196f32
--- /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 0000000000000000000000000000000000000000..4e21ca67e4664818ae61d6e2810f816ea3613943
--- /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 0000000000000000000000000000000000000000..bbb18ba9e66e35d9fad161d83d6564c048f9c3ec
--- /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 0000000000000000000000000000000000000000..87c839b5cc87ad27afc6454cadeabdf17a56cac9
--- /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 0000000000000000000000000000000000000000..a9d8bf659c481e6b65403d6814dbbf361361b5ba
--- /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 0000000000000000000000000000000000000000..7e8f0995ededc5071af3fc81aed256f026a31c52
--- /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 0000000000000000000000000000000000000000..b75b8e1075f5c2f01de1948ea2acfebffe48f939
--- /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 0000000000000000000000000000000000000000..2eb6038d7f1eb31b8cb71726f352f8c9f69a026c
--- /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 0000000000000000000000000000000000000000..e99098b5b9c395c01a65884467579249c4e1dfa4
--- /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 0000000000000000000000000000000000000000..1a5ba112ca6198044972c6f28b652185a097c227
--- /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 0000000000000000000000000000000000000000..450937dc95904651824be979ddd0b1e709f31f21
--- /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 0000000000000000000000000000000000000000..4be2aac5f2f0b963d2ec6208458908df4fd04c50
--- /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)
+
+# <points count="520">
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+f 396 395 397
+f 397 398 396
+f 398 397 399
+f 399 400 398
+f 400 399 401
+f 401 402 400
+f 402 401 403
+f 403 404 402
+f 404 403 405
+f 405 406 404
+f 406 405 407
+f 407 408 406
+f 408 407 409
+f 409 410 408
+f 410 409 411
+f 411 412 410
+f 412 411 413
+f 413 414 412
+f 414 413 415
+f 415 416 414
+f 416 415 417
+f 417 418 416
+f 418 417 419
+f 419 420 418
+f 420 419 421
+f 421 422 420
+f 422 421 423
+f 423 424 422
+f 424 423 425
+f 425 426 424
+f 426 425 427
+f 427 428 426
+f 428 427 429
+f 429 430 428
+f 430 429 431
+f 431 432 430
+f 432 431 433
+f 433 434 432
+f 434 433 435
+f 435 436 434
+f 436 435 437
+f 437 438 436
+f 438 437 439
+f 439 440 438
+f 440 439 441
+f 441 442 440
+f 442 441 443
+f 443 444 442
+f 444 443 445
+f 445 446 444
+f 446 445 447
+f 447 448 446
+f 448 447 449
+f 449 450 448
+f 450 449 451
+f 451 452 450
+f 452 451 453
+f 453 454 452
+f 454 453 455
+f 455 456 454
+f 456 455 457
+f 457 458 456
+f 458 457 459
+f 459 460 458
+f 460 459 461
+f 461 462 460
+f 462 461 463
+f 463 464 462
+f 464 463 465
+f 465 466 464
+f 466 465 467
+f 467 468 466
+f 468 467 469
+f 469 470 468
+f 470 469 471
+f 471 472 470
+f 472 471 473
+f 473 474 472
+f 474 473 475
+f 475 476 474
+f 476 475 477
+f 477 478 476
+f 478 477 479
+f 479 480 478
+f 480 479 481
+f 481 482 480
+f 482 481 483
+f 483 484 482
+f 484 483 485
+f 485 486 484
+f 486 485 487
+f 487 488 486
+f 488 487 489
+f 489 490 488
+f 490 489 491
+f 491 492 490
+f 492 491 493
+f 493 494 492
+f 494 493 495
+f 495 496 494
+f 496 495 497
+f 497 498 496
+f 498 497 499
+f 499 500 498
+f 500 499 501
+f 501 502 500
+f 502 501 503
+f 503 504 502
+f 504 503 505
+f 505 506 504
+f 506 505 507
+f 507 508 506
+f 508 507 509
+f 509 510 508
+f 510 509 511
+f 511 512 510
+f 512 511 513
+f 513 514 512
+f 514 513 515
+f 515 516 514
+f 516 515 517
+f 517 518 516
+f 518 517 519
+f 519 520 518
+f 520 519 262
+f 262 261 520
+# </faces>
diff --git a/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter_snappyHexMesh/system/controlDict b/tutorials/incompressible/pimpleDyMFoam/wingFlutter/wingFlutter_snappyHexMesh/system/controlDict
new file mode 100644
index 0000000000000000000000000000000000000000..1259284a3dd89fb74d4b9604de1ad95bfc48653e
--- /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 0000000000000000000000000000000000000000..2dc0a0a25e2f99ce5eb53af57cf68543bf23eff6
--- /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 0000000000000000000000000000000000000000..ae2773bf8427d7793f43ab80d4ecaafa8668ced2
--- /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 0000000000000000000000000000000000000000..d85a6d5e98b59c810afe7590c7ed30a471c408d0
--- /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 0000000000000000000000000000000000000000..2300d79207167b29935dfe749886a76ea289e261
--- /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;
+
+
+// ************************************************************************* //