COMP: resolve conflict

ReleaseNotes-dev

@@ -184,6 +184,8 @@
     + =setSet=: allows time range (e.g. 0:100) in combination with -batch argument
     to execute the commands for multiple times.
 * Post-processing
+  + =paraFoam=, =foamToVTK=: full support for polyhedral cell type in recent
+     Paraview versions.
   + =foamToEnsight=: parallel continuous data. new =-nodeValues= option to generate and output nodal
     field data.
   + =singleCellMesh=: new utility to convert mesh and fields to a single cell

applications/solvers/multiphase/twoPhaseEulerFoam/kineticTheoryModels/kineticTheoryModel/kineticTheoryModel.C

@@ -218,7 +218,7 @@ void Foam::kineticTheoryModel::solve(const volTensorField& gradUat)
     //  The solution is higly unstable close to the packing limit.
     gs0_ = radialModel_->g0
     (
-        min(max(alpha_, 1e-6), alphaMax_ - 0.01),
+        min(max(alpha_, scalar(1e-6)), alphaMax_ - 0.01),
         alphaMax_
     );
 
@@ -255,7 +255,7 @@ void Foam::kineticTheoryModel::solve(const volTensorField& gradUat)
     volScalarField J1 = 3.0*betaPrim;
     volScalarField J2 =
         0.25*sqr(betaPrim)*da_*sqr(Ur)
-       /(max(alpha_, 1e-6)*rhoa_*sqrtPi*(ThetaSqrt + TsmallSqrt));
+       /(max(alpha_, scalar(1e-6))*rhoa_*sqrtPi*(ThetaSqrt + TsmallSqrt));
 
     // bulk viscosity  p. 45 (Lun et al. 1984).
     lambda_ = (4.0/3.0)*sqr(alpha_)*rhoa_*da_*gs0_*(1.0+e_)*ThetaSqrt/sqrtPi;
@@ -309,7 +309,11 @@ void Foam::kineticTheoryModel::solve(const volTensorField& gradUat)
         volScalarField t1 = K1*alpha_ + rhoa_;
         volScalarField l1 = -t1*trD;
         volScalarField l2 = sqr(t1)*tr2D;
-        volScalarField l3 = 4.0*K4*max(alpha_, 1e-6)*(2.0*K3*trD2 + K2*tr2D);
+        volScalarField l3 =
+            4.0
+           *K4
+           *max(alpha_, scalar(1e-6))
+           *(2.0*K3*trD2 + K2*tr2D);
 
         Theta_ = sqr((l1 + sqrt(l2 + l3))/(2.0*(alpha_ + 1.0e-4)*K4));
     }

applications/test/momentOfInertia/Make/options

 EXE_INC = \
-    -I$(LIB_SRC)/meshTools/lnInclude
+    -I$(LIB_SRC)/meshTools/lnInclude \
+    -I$(LIB_SRC)/triSurface/lnInclude
 
 EXE_LIBS = \
     -lmeshTools

applications/test/momentOfInertia/Test-momentOfInertia.C

@@ -26,180 +26,38 @@ Application
 
 Description
     Calculates the inertia tensor and principal axes and moments of a
-    test face and tetrahedron.
+    test face, tetrahedron and mesh.
 
 \*---------------------------------------------------------------------------*/
 
+#include "argList.H"
+#include "Time.H"
+#include "polyMesh.H"
 #include "ListOps.H"
 #include "face.H"
 #include "tetPointRef.H"
 #include "triFaceList.H"
 #include "OFstream.H"
 #include "meshTools.H"
+#include "momentOfInertia.H"
 
 // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
 
 using namespace Foam;
 
-void massPropertiesSolid
-(
-    const pointField& pts,
-    const triFaceList triFaces,
-    scalar density,
-    scalar& mass,
-    vector& cM,
-    tensor& J
-)
+int main(int argc, char *argv[])
 {
-    // Reimplemented from: Wm4PolyhedralMassProperties.cpp
-    // File Version: 4.10.0 (2009/11/18)
-
-    // Geometric Tools, LC
-    // Copyright (c) 1998-2010
-    // Distributed under the Boost Software License, Version 1.0.
-    // http://www.boost.org/LICENSE_1_0.txt
-    // http://www.geometrictools.com/License/Boost/LICENSE_1_0.txt
-
-    // Boost Software License - Version 1.0 - August 17th, 2003
-
-    // Permission is hereby granted, free of charge, to any person or
-    // organization obtaining a copy of the software and accompanying
-    // documentation covered by this license (the "Software") to use,
-    // reproduce, display, distribute, execute, and transmit the
-    // Software, and to prepare derivative works of the Software, and
-    // to permit third-parties to whom the Software is furnished to do
-    // so, all subject to the following:
-
-    // The copyright notices in the Software and this entire
-    // statement, including the above license grant, this restriction
-    // and the following disclaimer, must be included in all copies of
-    // the Software, in whole or in part, and all derivative works of
-    // the Software, unless such copies or derivative works are solely
-    // in the form of machine-executable object code generated by a
-    // source language processor.
-
-    // THE SOFTWARE IS PROVIDED "AS IS", WITHOUT WARRANTY OF ANY KIND,
-    // EXPRESS OR IMPLIED, INCLUDING BUT NOT LIMITED TO THE WARRANTIES
-    // OF MERCHANTABILITY, FITNESS FOR A PARTICULAR PURPOSE, TITLE AND
-    // NON-INFRINGEMENT. IN NO EVENT SHALL THE COPYRIGHT HOLDERS OR
-    // ANYONE DISTRIBUTING THE SOFTWARE BE LIABLE FOR ANY DAMAGES OR
-    // OTHER LIABILITY, WHETHER IN CONTRACT, TORT OR OTHERWISE,
-    // ARISING FROM, OUT OF OR IN CONNECTION WITH THE SOFTWARE OR THE
-    // USE OR OTHER DEALINGS IN THE SOFTWARE.
-
-    const scalar r6 = 1.0/6.0;
-    const scalar r24 = 1.0/24.0;
-    const scalar r60 = 1.0/60.0;
-    const scalar r120 = 1.0/120.0;
-
-    // order:  1, x, y, z, x^2, y^2, z^2, xy, yz, zx
-    scalarField integrals(10, 0.0);
-
-    forAll(triFaces, i)
-    {
-        const triFace& tri(triFaces[i]);
-
-        // vertices of triangle i
-        vector v0 = pts[tri[0]];
-        vector v1 = pts[tri[1]];
-        vector v2 = pts[tri[2]];
-
-        // cross product of edges
-        vector eA = v1 - v0;
-        vector eB = v2 - v0;
-        vector n = eA ^ eB;
-
-        // compute integral terms
-        scalar tmp0, tmp1, tmp2;
-
-        scalar f1x, f2x, f3x, g0x, g1x, g2x;
-
-        tmp0 = v0.x() + v1.x();
-        f1x = tmp0 + v2.x();
-        tmp1 = v0.x()*v0.x();
-        tmp2 = tmp1 + v1.x()*tmp0;
-        f2x = tmp2 + v2.x()*f1x;
-        f3x = v0.x()*tmp1 + v1.x()*tmp2 + v2.x()*f2x;
-        g0x = f2x + v0.x()*(f1x + v0.x());
-        g1x = f2x + v1.x()*(f1x + v1.x());
-        g2x = f2x + v2.x()*(f1x + v2.x());
-
-        scalar f1y, f2y, f3y, g0y, g1y, g2y;
-
-        tmp0 = v0.y() + v1.y();
-        f1y = tmp0 + v2.y();
-        tmp1 = v0.y()*v0.y();
-        tmp2 = tmp1 + v1.y()*tmp0;
-        f2y = tmp2 + v2.y()*f1y;
-        f3y = v0.y()*tmp1 + v1.y()*tmp2 + v2.y()*f2y;
-        g0y = f2y + v0.y()*(f1y + v0.y());
-        g1y = f2y + v1.y()*(f1y + v1.y());
-        g2y = f2y + v2.y()*(f1y + v2.y());
-
-        scalar f1z, f2z, f3z, g0z, g1z, g2z;
-
-        tmp0 = v0.z() + v1.z();
-        f1z = tmp0 + v2.z();
-        tmp1 = v0.z()*v0.z();
-        tmp2 = tmp1 + v1.z()*tmp0;
-        f2z = tmp2 + v2.z()*f1z;
-        f3z = v0.z()*tmp1 + v1.z()*tmp2 + v2.z()*f2z;
-        g0z = f2z + v0.z()*(f1z + v0.z());
-        g1z = f2z + v1.z()*(f1z + v1.z());
-        g2z = f2z + v2.z()*(f1z + v2.z());
-
-        // update integrals
-        integrals[0] += n.x()*f1x;
-        integrals[1] += n.x()*f2x;
-        integrals[2] += n.y()*f2y;
-        integrals[3] += n.z()*f2z;
-        integrals[4] += n.x()*f3x;
-        integrals[5] += n.y()*f3y;
-        integrals[6] += n.z()*f3z;
-        integrals[7] += n.x()*(v0.y()*g0x + v1.y()*g1x + v2.y()*g2x);
-        integrals[8] += n.y()*(v0.z()*g0y + v1.z()*g1y + v2.z()*g2y);
-        integrals[9] += n.z()*(v0.x()*g0z + v1.x()*g1z + v2.x()*g2z);
-    }
-
-    integrals[0] *= r6;
-    integrals[1] *= r24;
-    integrals[2] *= r24;
-    integrals[3] *= r24;
-    integrals[4] *= r60;
-    integrals[5] *= r60;
-    integrals[6] *= r60;
-    integrals[7] *= r120;
-    integrals[8] *= r120;
-    integrals[9] *= r120;
-
-    // mass
-    mass = integrals[0];
-
-    // center of mass
-    cM = vector(integrals[1], integrals[2], integrals[3])/mass;
-
-    // inertia relative to origin
-    J.xx() = integrals[5] + integrals[6];
-    J.xy() = -integrals[7];
-    J.xz() = -integrals[9];
-    J.yx() = J.xy();
-    J.yy() = integrals[4] + integrals[6];
-    J.yz() = -integrals[8];
-    J.zx() = J.xz();
-    J.zy() = J.yz();
-    J.zz() = integrals[4] + integrals[5];
-
-    // inertia relative to center of mass
-    J -= mass*((cM & cM)*I - cM*cM);
-
-    // Apply density
-    mass *= density;
-    J *= density;
-}
+    argList::addOption
+    (
+        "cell",
+        "label",
+        "cell to use for inertia calculation, defaults to 0"
+    );
 
+    #include "setRootCase.H"
+    #include "createTime.H"
+    #include "createPolyMesh.H"
 
-int main(int argc, char *argv[])
-{
     scalar density = 1.0;
 
     {
@@ -286,16 +144,7 @@ int main(int argc, char *argv[])
         vector cM = vector::zero;
         tensor J = tensor::zero;
 
-        massPropertiesSolid
-        (
-
-            pts,
-            tetFaces,
-            density,
-            m,
-            cM,
-            J
-        );
+        momentOfInertia::massPropertiesSolid(pts, tetFaces, density, m, cM, J);
 
         vector eVal = eigenValues(J);
 
@@ -344,7 +193,50 @@ int main(int argc, char *argv[])
         {
             str << "l " << nPts + 1 << ' ' << i + 1 << endl;
         }
+    }
+
+    {
+        const label cellI = args.optionLookupOrDefault("cell", 0);
+
+        tensorField mI = momentOfInertia::meshInertia(mesh);
+
+        tensor& J = mI[cellI];
+
+        vector eVal = eigenValues(J);
 
+        Info<< nl
+            << "Inertia tensor of cell " << cellI << " " << J << nl
+            << "eigenValues (principal moments) " << eVal << endl;
+
+        J /= cmptMax(eVal);
+
+        tensor eVec = eigenVectors(J);
+
+        Info<< "eigenVectors (principal axes, from normalised inertia) " << eVec
+            << endl;
+
+        OFstream str("cell_" + name(cellI) + "_inertia.obj");
+
+        Info<< nl << "Writing scaled principal axes of cell " << cellI << " to "
+            << str.name() << endl;
+
+        const point& cC = mesh.cellCentres()[cellI];
+
+        scalar scale = mag
+        (
+            (cC - mesh.faceCentres()[mesh.cells()[cellI][0]])
+           /eVal.component(findMin(eVal))
+        );
+
+        meshTools::writeOBJ(str, cC);
+        meshTools::writeOBJ(str, cC + scale*eVal.x()*eVec.x());
+        meshTools::writeOBJ(str, cC + scale*eVal.y()*eVec.y());
+        meshTools::writeOBJ(str, cC + scale*eVal.z()*eVec.z());
+
+        for (label i = 1; i < 4; i++)
+        {
+            str << "l " << 1 << ' ' << i + 1 << endl;
+        }
     }
 
     Info<< nl << "End" << nl << endl;

applications/utilities/mesh/generation/extrudeMesh/Allwclean → applications/utilities/mesh/generation/extrude/Allwclean

@@ -3,6 +3,7 @@ cd ${0%/*} || exit 1    # run from this directory
 set -x
 
 wclean libso extrudeModel
-wclean
+wclean extrudeMesh
+wclean extrudeToRegionMesh
 
 # ----------------------------------------------------------------- end-of-file

applications/utilities/mesh/generation/extrudeMesh/Allwmake → applications/utilities/mesh/generation/extrude/Allwmake

@@ -3,6 +3,8 @@ cd ${0%/*} || exit 1    # run from this directory
 set -x
 
 wmake libso extrudeModel
-wmake
+wmake extrudeMesh
+wmake extrudeToRegionMesh
+
 
 # ----------------------------------------------------------------- end-of-file

applications/utilities/mesh/generation/extrudeMesh/Make/options → applications/utilities/mesh/generation/extrude/extrudeMesh/Make/options

 EXE_INC = \
     -IextrudedMesh \
-    -IextrudeModel/lnInclude \
+    -I../extrudeModel/lnInclude \
     -I$(LIB_SRC)/finiteVolume/lnInclude \
     -I$(LIB_SRC)/surfMesh/lnInclude \
     -I$(LIB_SRC)/meshTools/lnInclude \

applications/utilities/mesh/generation/extrudeMesh/extrudeMesh.C → applications/utilities/mesh/generation/extrude/extrudeMesh/extrudeMesh.C

@@ -214,9 +214,8 @@ int main(int argc, char *argv[])
     (
         IOobject
         (
-            "extrudeProperties",
-            runTimeExtruded.constant(),
-            regionDir,
+            "extrudeMeshDict",
+            runTimeExtruded.system(),
             runTimeExtruded,
             IOobject::MUST_READ_IF_MODIFIED
         )

applications/utilities/mesh/generation/extrudeMesh/extrudeProperties → applications/utilities/mesh/generation/extrude/extrudeMesh/extrudeMeshDict

@@ -10,7 +10,7 @@ FoamFile
     version     2.0;
     format      ascii;
     class       dictionary;
-    object      extrudeProperties;
+    object      extrudeMeshDict;
 }
 // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //