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Merge branch 'master' of /home/dm4/OpenFOAM/OpenFOAM-dev

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This commit is contained in:
mattijs
2012-01-24 12:36:37 +00:00
parent 1e7d220ebc b600aefcb8
commit 036d5b9898
42 changed files with 303 additions and 67 deletions
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4
applications/solvers/lagrangian/sprayFoam/Make/options
View File

@ -1,4 +1,5 @@
EXE_INC = \
-I$(FOAM_SOLVERS)/lagrangian/reactingParcelFoam \
-I$(LIB_SRC)/finiteVolume/lnInclude \
-I${LIB_SRC}/meshTools/lnInclude \
-I$(LIB_SRC)/turbulenceModels/compressible/turbulenceModel \
@ -20,8 +21,7 @@ EXE_INC = \
-I$(LIB_SRC)/ODE/lnInclude \
-I$(LIB_SRC)/regionModels/regionModel/lnInclude \
-I$(LIB_SRC)/regionModels/surfaceFilmModels/lnInclude \
-I$(LIB_SRC)/combustionModels/lnInclude \
-I$(FOAM_SOLVERS)/lagrangian/reactingParcelFoam
-I$(LIB_SRC)/combustionModels/lnInclude
EXE_LIBS = \

0
applications/solvers/lagrangian/sprayFoam/sprayEnginFoam/Make/files → applications/solvers/lagrangian/sprayFoam/sprayEngineFoam/Make/files
View File

0
applications/solvers/lagrangian/sprayFoam/sprayEnginFoam/Make/options → applications/solvers/lagrangian/sprayFoam/sprayEngineFoam/Make/options
View File

0
applications/solvers/lagrangian/sprayFoam/sprayEnginFoam/createClouds.H → applications/solvers/lagrangian/sprayFoam/sprayEngineFoam/createClouds.H
View File

0
applications/solvers/lagrangian/sprayFoam/sprayEnginFoam/logSummary.H → applications/solvers/lagrangian/sprayFoam/sprayEngineFoam/logSummary.H
View File

73
applications/solvers/lagrangian/sprayFoam/sprayEngineFoam/pEqn.H Normal file
View File

@ -0,0 +1,73 @@
rho = thermo.rho();
volScalarField rAU(1.0/UEqn.A());
U = rAU*UEqn.H();
if (pimple.transonic())
{
surfaceScalarField phid
(
"phid",
fvc::interpolate(psi)
*(
((fvc::interpolate(U) & mesh.Sf()) - fvc::meshPhi(rho, U))
+ fvc::ddtPhiCorr(rAU, rho, U, phi)
)
);
while (pimple.correctNonOrthogonal())
{
fvScalarMatrix pEqn
(
fvm::ddt(psi, p)
+ fvm::div(phid, p)
- fvm::laplacian(rho*rAU, p)
==
parcels.Srho()
);
pEqn.solve(mesh.solver(p.select(pimple.finalInnerIter())));
if (pimple.finalNonOrthogonalIter())
{
phi == pEqn.flux();
}
}
}
else
{
phi =
fvc::interpolate(rho)
*(
((fvc::interpolate(U) & mesh.Sf()) - fvc::meshPhi(rho, U))
+ fvc::ddtPhiCorr(rAU, rho, U, phi)
);
while (pimple.correctNonOrthogonal())
{
fvScalarMatrix pEqn
(
fvm::ddt(psi, p)
+ fvc::div(phi)
- fvm::laplacian(rho*rAU, p)
==
parcels.Srho()
);
pEqn.solve(mesh.solver(p.select(pimple.finalInnerIter())));
if (pimple.finalNonOrthogonalIter())
{
phi += pEqn.flux();
}
}
}
#include "rhoEqn.H"
#include "compressibleContinuityErrs.H"
U -= rAU*fvc::grad(p);
U.correctBoundaryConditions();
K = 0.5*magSqr(U);
dpdt = fvc::ddt(p);

0
applications/solvers/lagrangian/sprayFoam/sprayEnginFoam/readEngineTimeControls.H → applications/solvers/lagrangian/sprayFoam/sprayEngineFoam/readEngineTimeControls.H
View File

2
applications/solvers/lagrangian/sprayFoam/sprayEnginFoam/sprayEngineFoam.C → applications/solvers/lagrangian/sprayFoam/sprayEngineFoam/sprayEngineFoam.C
View File

@ -74,6 +74,8 @@ int main(int argc, char *argv[])
Info<< "Crank angle = " << runTime.theta() << " CA-deg" << endl;
mesh.move();
parcels.evolve();
#include "rhoEqn.H"

0
applications/solvers/lagrangian/sprayFoam/sprayEnginFoam/startSummary.H → applications/solvers/lagrangian/sprayFoam/sprayEngineFoam/startSummary.H
View File

4
applications/solvers/multiphase/compressibleTwoPhaseEulerFoam/interfacialModels/dragModels/dragModel/dragModel.H
View File

@ -114,11 +114,11 @@ public:
//- the dragfunction K used in the momentum eq.
// ddt(alpha*rhoa*Ua) + ... = ... alpha*beta*K*(Ua-Ub)
// ddt(beta*rhob*Ub) + ... = ... alpha*beta*K*(Ub-Ua)
// **********************************<EFBFBD>NB ! *****************************
// ********************************** NB! *****************************
// for numerical reasons alpha and beta has been
// extracted from the dragFunction K,
// so you MUST divide K by alpha*beta when implemnting the drag function
// **********************************<EFBFBD>NB ! *****************************
// ********************************** NB! *****************************
virtual tmp<volScalarField> K(const volScalarField& Ur) const = 0;
};

4
applications/solvers/multiphase/compressibleTwoPhaseEulerFoam/interfacialModels/heatTransferModels/heatTransferModel/heatTransferModel.H
View File

@ -114,12 +114,12 @@ public:
//- the heat-transfer function K used in the enthalpy eq.
// ddt(alpha*rhoa*ha) + ... = ... alpha*beta*K*(Ta - Tb)
// ddt(beta*rhob*hb) + ... = ... alpha*beta*K*(Tb - Ta)
// **********************************<EFBFBD>NB ! *****************************
// ********************************** NB!*****************************
// for numerical reasons alpha and beta has been
// extracted from the heat-transfer function K,
// so you MUST divide K by alpha*beta when implementing the
// heat-transfer function
// **********************************<EFBFBD>NB ! *****************************
// ********************************** NB!*****************************
virtual tmp<volScalarField> K(const volScalarField& Ur) const = 0;
};

4
applications/solvers/multiphase/interPhaseChangeFoam/phaseChangeTwoPhaseMixtures/Kunz/Kunz.H
View File

@ -35,8 +35,8 @@ Description
\verbatim
Kunz, R.F., Boger, D.A., Stinebring, D.R., Chyczewski, Lindau. J.W.,
Gibeling, H.J., Venkateswaran, S., Govindan, T.R.,
“A Preconditioned Implicit Method for Two-Phase Flows with Application
to Cavitation Prediction,”
"A Preconditioned Implicit Method for Two-Phase Flows with Application
to Cavitation Prediction,"
Computers and Fluids,
29(8):849-875, 2000.
\endverbatim

4
applications/solvers/multiphase/multiphaseEulerFoam/interfacialModels/dragModels/dragModel/dragModel.H
View File

@ -131,11 +131,11 @@ public:
//- the dragfunction K used in the momentum eq.
// ddt(alpha*rhoa*Ua) + ... = ... alpha*beta*K*(Ua-Ub)
// ddt(beta*rhob*Ub) + ... = ... alpha*beta*K*(Ub-Ua)
// **********************************<EFBFBD>NB ! *****************************
// ********************************** NB! *****************************
// for numerical reasons alpha and beta has been
// extracted from the dragFunction K,
// so you MUST divide K by alpha*beta when implemnting the drag function
// **********************************<EFBFBD>NB ! *****************************
// ********************************** NB! *****************************
virtual tmp<volScalarField> K(const volScalarField& Ur) const = 0;
};

4
applications/solvers/multiphase/multiphaseEulerFoam/interfacialModels/heatTransferModels/heatTransferModel/heatTransferModel.H
View File

@ -114,12 +114,12 @@ public:
//- the heat-transfer function K used in the enthalpy eq.
// ddt(alpha*rhoa*ha) + ... = ... alpha*beta*K*(Ta - Tb)
// ddt(beta*rhob*hb) + ... = ... alpha*beta*K*(Tb - Ta)
// **********************************<EFBFBD>NB ! *****************************
// ********************************** NB! *****************************
// for numerical reasons alpha and beta has been
// extracted from the heat-transfer function K,
// so you MUST divide K by alpha*beta when implementing the
// heat-transfer function
// **********************************<EFBFBD>NB ! *****************************
// ********************************** NB! *****************************
virtual tmp<volScalarField> K(const volScalarField& Ur) const = 0;
};

4
applications/solvers/multiphase/twoPhaseEulerFoam/interfacialModels/dragModels/dragModel/dragModel.H
View File

@ -114,11 +114,11 @@ public:
//- the dragfunction K used in the momentum eq.
// ddt(alpha*rhoa*Ua) + ... = ... alpha*beta*K*(Ua-Ub)
// ddt(beta*rhob*Ub) + ... = ... alpha*beta*K*(Ub-Ua)
// **********************************<EFBFBD>NB ! *****************************
// ********************************** NB ! *****************************
// for numerical reasons alpha and beta has been
// extracted from the dragFunction K,
// so you MUST divide K by alpha*beta when implemnting the drag function
// **********************************<EFBFBD>NB ! *****************************
// ********************************** NB ! *****************************
virtual tmp<volScalarField> K(const volScalarField& Ur) const = 0;
};

1
applications/utilities/mesh/generation/extrude/extrudeToRegionMesh/extrudeToRegionMesh.C
View File

@ -1637,6 +1637,7 @@ int main(int argc, char *argv[])
#include "addRegionOption.H"
#include "addOverwriteOption.H"
argList::addOption("dict", "name", "specify alternative dictionary");
#include "setRootCase.H"
#include "createTime.H"

37
applications/utilities/postProcessing/dataConversion/foamToEnsightParts/foamToEnsightParts.C
View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | Copyright (C) 2011 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2011-2012 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -35,6 +35,9 @@ Usage
\param -ascii \n
Write Ensight data in ASCII format instead of "C Binary"
\parm -name \<subdir\>\n
define sub-directory name to use for Ensight data (default: "Ensight")
\param -noZero \n
Exclude the often incomplete initial conditions.
@ -46,6 +49,9 @@ Usage
Suppress writing the geometry. Can be useful for converting partial
results for a static geometry.
\param -width \<n\>\n
width of Ensight data subdir
Note
- no parallel data.
- writes to \a Ensight directory to avoid collisions with foamToEnsight.
@ -96,6 +102,19 @@ int main(int argc, char *argv[])
"suppress writing the geometry. "
"Can be useful for converting partial results for a static geometry"
);
argList::addOption
(
"name",
"subdir",
"define sub-directory name to use for Ensight data "
"(default: \"Ensight\")"
);
argList::addOption
(
"width",
"n",
"width of Ensight data subdir"
);
// the volume field types that we handle
wordHashSet volFieldTypes;
@ -133,7 +152,21 @@ int main(int argc, char *argv[])
// always write the geometry, unless the -noMesh option is specified
bool optNoMesh = args.optionFound("noMesh");
fileName ensightDir = args.rootPath()/args.globalCaseName()/"Ensight";
// adjust output width
if (args.optionFound("width"))
{
ensightFile::subDirWidth(args.optionRead<label>("width"));
}
// define sub-directory name to use for Ensight data
fileName ensightDir = "Ensight";
args.optionReadIfPresent("name", ensightDir);
if (!ensightDir.isAbsolute())
{
ensightDir = args.rootPath()/args.globalCaseName()/ensightDir;
}
fileName dataDir = ensightDir/"data";
fileName caseFileName = "Ensight.case";
fileName dataMask = fileName("data")/ensightFile::mask();

2
etc/config/settings.csh
View File

@ -372,7 +372,7 @@ unsetenv MPI_ARCH_PATH MPI_HOME FOAM_MPI_LIBBIN
switch ("$WM_MPLIB")
case OPENMPI:
setenv FOAM_MPI openmpi-1.5.3
setenv FOAM_MPI openmpi-1.5.4
# optional configuration tweaks:
_foamSource `$WM_PROJECT_DIR/bin/foamEtcFile config/openmpi.csh`

12
etc/config/settings.sh
View File

@ -114,6 +114,16 @@ Linux)
export WM_LDFLAGS='-mabi=64 -G0'
;;
armv7l)
WM_ARCH=linuxARM7
export WM_COMPILER_LIB_ARCH=32
export WM_CC='gcc'
export WM_CXX='g++'
export WM_CFLAGS='-fPIC'
export WM_CXXFLAGS='-fPIC'
export WM_LDFLAGS=
;;
ppc64)
WM_ARCH=linuxPPC64
export WM_COMPILER_LIB_ARCH=64
@ -393,7 +403,7 @@ unset MPI_ARCH_PATH MPI_HOME FOAM_MPI_LIBBIN
case "$WM_MPLIB" in
OPENMPI)
export FOAM_MPI=openmpi-1.5.3
export FOAM_MPI=openmpi-1.5.4
# optional configuration tweaks:
_foamSource `$WM_PROJECT_DIR/bin/foamEtcFile config/openmpi.sh`

2
src/OpenFOAM/Make/files
View File

@ -45,7 +45,9 @@ primitives/Tensor/lists/symmTensorList.C
primitives/Tensor/lists/tensorList.C
primitives/Vector/complexVector/complexVector.C
#if !defined(WM_SP)
primitives/Vector/floatVector/floatVector.C
#endif
primitives/Vector/labelVector/labelVector.C
primitives/Vector/vector/vector.C
primitives/Vector/lists/vectorList.C

4
src/OpenFOAM/primitives/Vector/floatVector/floatVector.H
View File

@ -47,11 +47,11 @@ namespace Foam
typedef Vector<float> floatVector;
//- Data associated with floatVector type are contiguous
#if !defined(WM_SP)
template<>
inline bool contiguous<floatVector>() {return true;}
#endif
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

68
src/conversion/ensight/file/ensightFile.C
View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | Copyright (C) 2011 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2011-2012 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -24,6 +24,7 @@ License
\*---------------------------------------------------------------------------*/
#include "ensightFile.H"
#include <sstream>
// * * * * * * * * * * * * * * Static Data Members * * * * * * * * * * * * * //
@ -31,6 +32,53 @@ bool Foam::ensightFile::allowUndef_ = false;
Foam::scalar Foam::ensightFile::undefValue_ = Foam::floatScalarVGREAT;
// default is width 8
Foam::string Foam::ensightFile::mask_ = "********";
Foam::string Foam::ensightFile::dirFmt_ = "%08d";
// * * * * * * * * * * * * * Static Member Functions * * * * * * * * * * * * //
Foam::string Foam::ensightFile::mask()
{
return mask_;
}
Foam::string Foam::ensightFile::subDir(const label n)
{
char buf[32];
sprintf(buf, dirFmt_.c_str(), n);
return buf;
}
void Foam::ensightFile::subDirWidth(const label n)
{
// enforce max limit to avoid buffer overflow in subDir()
if (n < 1 || n > 31)
{
return;
}
// appropriate printf format
std::ostringstream oss;
oss << "%0" << n << "d";
dirFmt_ = oss.str();
// set mask accordingly
mask_.resize(n, '*');
}
Foam::label Foam::ensightFile::subDirWidth()
{
return mask_.size();
}
// * * * * * * * * * * * * * * * * Constructors * * * * * * * * * * * * * * //
Foam::ensightFile::ensightFile
@ -247,22 +295,4 @@ Foam::Ostream& Foam::ensightFile::writeBinaryHeader()
}
// * * * * * * * * * * * * * Static Member Functions * * * * * * * * * * * * //
Foam::string Foam::ensightFile::mask()
{
char buf[16] = "********";
return buf;
}
Foam::string Foam::ensightFile::subDir(const label n)
{
char buf[16];
sprintf(buf, "%08d", n);
return buf;
}
// ************************************************************************* //

19
src/conversion/ensight/file/ensightFile.H
View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | Copyright (C) 2011 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2011-2012 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -57,6 +57,12 @@ class ensightFile
//- value to represent undef in results
static scalar undefValue_;
//- The '*' mask appropriate for subDir
static string mask_;
//- The printf format for zero-padded subdirectory numbers
static string dirFmt_;
// Private Member Functions
@ -88,12 +94,19 @@ public:
//- Return setting for whether 'undef' values are allowed in results
static bool allowUndef();
//- '*' mask appropriate for subDir
//- The '*' mask appropriate for subDir
static string mask();
//- consistent zero-padded numbers for subdirectories
//- Consistent zero-padded numbers for subdirectories
static string subDir(const label);
//- Set width of subDir and mask. Default width is 8 digits.
// Max width is 31 digits.
static void subDirWidth(const label);
//- Return current width of subDir and mask.
static label subDirWidth();
// Edit

2
src/lagrangian/molecularDynamics/molecule/reducedUnits/reducedUnits.H
View File

@ -104,7 +104,7 @@ public:
//- Construct with no argument, uses default values:
// length = 1nm
// mass = 1.660538782e−27kg (unified atomic mass unit)
// mass = 1.660538782e-27kg (unified atomic mass unit)
// temperature = 1K (therefore, energy = 1*kb)
reducedUnits();

2
src/lagrangian/molecularDynamics/old/reducedUnits/reducedUnits.H
View File

@ -104,7 +104,7 @@ public:
//- Construct with no argument, uses default values:
// length = 1nm
// mass = 1.660538782e−27kg (unified atomic mass unit)
// mass = 1.660538782e-27kg (unified atomic mass unit)
// temperature = 1K (therefore, energy = 1*kb)
reducedUnits();

8
src/meshTools/AMIInterpolation/patches/cyclic/cyclicAMIPolyPatch/cyclicAMIPolyPatch.C
View File

@ -366,7 +366,7 @@ Foam::cyclicAMIPolyPatch::cyclicAMIPolyPatch
AMIPtr_(NULL),
AMIReverse_(false),
surfPtr_(NULL),
surfDict_(dictionary::null)
surfDict_(fileName("surface"))
{
// Neighbour patch might not be valid yet so no transformation
// calculation possible
@ -474,7 +474,7 @@ Foam::cyclicAMIPolyPatch::cyclicAMIPolyPatch
AMIPtr_(NULL),
AMIReverse_(pp.AMIReverse_),
surfPtr_(NULL),
surfDict_(dictionary::null)
surfDict_(pp.surfDict_)
{
// Neighbour patch might not be valid yet so no transformation
// calculation possible
@ -501,7 +501,7 @@ Foam::cyclicAMIPolyPatch::cyclicAMIPolyPatch
AMIPtr_(NULL),
AMIReverse_(pp.AMIReverse_),
surfPtr_(NULL),
surfDict_(dictionary::null)
surfDict_(pp.surfDict_)
{
if (nbrPatchName_ == name())
{
@ -825,7 +825,7 @@ void Foam::cyclicAMIPolyPatch::write(Ostream& os) const
<< token::END_STATEMENT << nl;
}
if (surfDict_ != dictionary::null)
if (!surfDict_.empty())
{
os.writeKeyword(surfDict_.dictName());
os << surfDict_;

11
src/meshTools/mappedPatches/mappedPolyPatch/mappedPatchBase.C
View File

@ -798,7 +798,7 @@ Foam::mappedPatchBase::mappedPatchBase
AMIPtr_(NULL),
AMIReverse_(false),
surfPtr_(NULL),
surfDict_(dictionary::null)
surfDict_(fileName("surface"))
{}
@ -824,7 +824,7 @@ Foam::mappedPatchBase::mappedPatchBase
AMIPtr_(NULL),
AMIReverse_(false),
surfPtr_(NULL),
surfDict_(dictionary::null)
surfDict_(fileName("surface"))
{}
@ -850,7 +850,7 @@ Foam::mappedPatchBase::mappedPatchBase
AMIPtr_(NULL),
AMIReverse_(false),
surfPtr_(NULL),
surfDict_(dictionary::null)
surfDict_(fileName("surface"))
{}
@ -876,7 +876,7 @@ Foam::mappedPatchBase::mappedPatchBase
AMIPtr_(NULL),
AMIReverse_(false),
surfPtr_(NULL),
surfDict_(dictionary::null)
surfDict_(fileName("surface"))
{}
@ -1216,9 +1216,12 @@ void Foam::mappedPatchBase::write(Ostream& os) const
<< token::END_STATEMENT << nl;
}
if (!surfDict_.empty())
{
os.writeKeyword(surfDict_.dictName());
os << surfDict_;
}
}
}

2
src/sampling/meshToMeshInterpolation/tetOverlapVolume/tetOverlapVolume.H
View File

@ -81,8 +81,8 @@ class tetOverlapVolume
const point& fc
) const;
public:
public:
//- Runtime type information
ClassName("tetOverlapVolume");

10
src/turbulenceModels/compressible/LES/Smagorinsky/Smagorinsky.H
View File

@ -2,7 +2,7 @@
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | Copyright (C) 2011 OpenFOAM Foundation
\\ / A nd | Copyright (C) 2011-2012 OpenFOAM Foundation
\\/ M anipulation |
-------------------------------------------------------------------------------
License
@ -113,7 +113,13 @@ public:
// calculated from the given velocity gradient
tmp<volScalarField> k(const tmp<volTensorField>& gradU) const
{
return (2.0*ck_/ce_)*sqr(delta())*magSqr(dev(symm(gradU)));
volSymmTensorField D(symm(gradU));
volScalarField a(ce_/delta());
volScalarField b((2.0/3.0)*tr(D));
volScalarField c(2*ck_*delta()*(dev(D) && D));
return sqr((-b + sqrt(sqr(b) + 4*a*c))/(2*a));
}
//- Return SGS kinetic energy

2
src/turbulenceModels/compressible/RAS/SpalartAllmaras/SpalartAllmaras.H
View File

@ -33,7 +33,7 @@ Description
"A One-Equation Turbulence Model for Aerodynamic Flows"
P.R. Spalart,
S.R. Allmaras,
La Recherche A´rospatiale, No. 1, 1994, pp. 5–21.
La Recherche Aerospatiale, No. 1, 1994, pp. 5-21.
Extended according to:

2
src/turbulenceModels/incompressible/RAS/SpalartAllmaras/SpalartAllmaras.H
View File

@ -33,7 +33,7 @@ Description
"A One-Equation Turbulence Model for Aerodynamic Flows"
P.R. Spalart,
S.R. Allmaras,
La Recherche A´rospatiale, No. 1, 1994, pp. 5–21.
La Recherche Aerospatiale, No. 1, 1994, pp. 5-21.
Extended according to:

4
tutorials/incompressible/pisoFoam/les/motorBike/lesFiles/fvSolution
View File

@ -105,8 +105,8 @@ PIMPLE
relaxationFactors
{
U 1;
nuTilda 1;
"U.*" 1;
"nuTilda.*" 1;
}

16
wmake/rules/linuxARM7Gcc/c Normal file
View File

@ -0,0 +1,16 @@
.SUFFIXES: .c .h
cWARN = -Wall
cc = gcc
include $(RULES)/c$(WM_COMPILE_OPTION)
cFLAGS = $(GFLAGS) $(cWARN) $(cOPT) $(cDBUG) $(LIB_HEADER_DIRS) -fPIC
ctoo = $(WM_SCHEDULER) $(cc) $(cFLAGS) -c $$SOURCE -o $@
LINK_LIBS = $(cDBUG)
LINKLIBSO = $(cc) -shared
LINKEXE = $(cc) -Xlinker --add-needed -Xlinker -z -Xlinker nodefs

21
wmake/rules/linuxARM7Gcc/c++ Normal file
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@ -0,0 +1,21 @@
.SUFFIXES: .C .cxx .cc .cpp
c++WARN = -Wall -Wextra -Wno-unused-parameter -Wold-style-cast
CC = g++
include $(RULES)/c++$(WM_COMPILE_OPTION)
ptFLAGS = -DNoRepository -ftemplate-depth-100
c++FLAGS = $(GFLAGS) $(c++WARN) $(c++OPT) $(c++DBUG) $(ptFLAGS) $(LIB_HEADER_DIRS) -fPIC
Ctoo = $(WM_SCHEDULER) $(CC) $(c++FLAGS) -c $$SOURCE -o $@
cxxtoo = $(Ctoo)
cctoo = $(Ctoo)
cpptoo = $(Ctoo)
LINK_LIBS = $(c++DBUG)
LINKLIBSO = $(CC) $(c++FLAGS) -shared -Xlinker --add-needed -Xlinker --no-as-needed
LINKEXE = $(CC) $(c++FLAGS) -Xlinker --add-needed -Xlinker --no-as-needed

2
wmake/rules/linuxARM7Gcc/c++Debug Normal file
View File

@ -0,0 +1,2 @@
c++DBUG = -ggdb3 -DFULLDEBUG
c++OPT = -O0 -fdefault-inline

3
wmake/rules/linuxARM7Gcc/c++Opt Normal file
View File

@ -0,0 +1,3 @@
c++DBUG =
#c++OPT = -O3 -floop-optimize -falign-loops -falign-labels -falign-functions -falign-jumps -mcpu=cortex-a9 -mfpu=vfpv3-d16 -mfloat-abi=hard
c++OPT = -O2 -mcpu=cortex-a9 -mfpu=vfpv3-d16 -mfloat-abi=soft

2
wmake/rules/linuxARM7Gcc/c++Prof Normal file
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c++DBUG = -pg
c++OPT = -O2

2
wmake/rules/linuxARM7Gcc/cDebug Normal file
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cDBUG = -ggdb -DFULLDEBUG
cOPT = -O1 -fdefault-inline -finline-functions

3
wmake/rules/linuxARM7Gcc/cOpt Normal file
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cDBUG =
#cOPT = -O3 -floop-optimize -falign-loops -falign-labels -falign-functions -falign-jumps -mcpu=cortex-a9 -mfpu=vfpv3-d16 -mfloat-abi=hard
cOPT = -O3 -mcpu=cortex-a9 -mfpu=vfpv3-d16 -mfloat-abi=hard

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wmake/rules/linuxARM7Gcc/cProf Normal file
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cDBUG = -pg
cOPT = -O2

9
wmake/rules/linuxARM7Gcc/general Normal file
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CPP = cpp -traditional-cpp $(GFLAGS)
LD = ld
PROJECT_LIBS = -l$(WM_PROJECT) -ldl
include $(GENERAL_RULES)/standard
include $(RULES)/c
include $(RULES)/c++

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wmake/rules/linuxARM7Gcc/mplibHPMPI Normal file
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PFLAGS =
PINC = -I$(MPI_ARCH_PATH)/include -D_MPICC_H
PLIBS = -L$(MPI_ARCH_PATH)/lib/linux_ia32 -lmpi