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Development
openfoam
Commits
1cff9e54
Commit
1cff9e54
authored
Nov 24, 2008
by
mattijs
Browse files
merge
parents
5a85f3c8
dfba9d77
Changes
174
Hide whitespace changes
Inline
Side-by-side
applications/solvers/Lagrangian/kinematicParcelFoam/Make/options
View file @
1cff9e54
EXE_INC = \
-I$(LIB_SRC)/lagrangian/basic/lnInclude \
-I$(LIB_SRC)/lagrangian/intermediate/lnInclude \
-I$(LIB_SRC)/finiteVolume/lnInclude \
-I$(LIB_SRC)/thermophysicalModels/specie/lnInclude \
-I$(LIB_SRC)/thermophysicalModels/basic/lnInclude \
-I$(LIB_SRC)/thermophysicalModels/combustion/lnInclude \
-I$(LIB_SRC)/thermophysicalModels/radiation/lnInclude \
-I$(LIB_SRC)/turbulenceModels/RAS
-I$(LIB_SRC)/turbulenceModels/compressible/turbulenceModel \
-I$(LIB_SRC)/finiteVolume/lnInclude
EXE_LIBS = \
-llagrangian \
-llagrangianIntermediate \
-lfiniteVolume \
-lmeshTools \
-lthermophysicalFunctions \
-lbasicThermophysicalModels \
/* -lcombustionThermophysicalModels */ \
-lspecie \
-lradiation \
-lcompressibleRASModels
-lcompressibleRASModels \
-lcompressibleLESModels \
-lfiniteVolume \
-lmeshTools
applications/solvers/Lagrangian/kinematicParcelFoam/createFields.H
View file @
1cff9e54
...
...
@@ -32,12 +32,12 @@
mesh
);
#
include "compressibleCreatePhi.H"
#
include "compressibleCreatePhi.H"
Info
<<
"Creating turbulence model
\n
"
<<
endl
;
autoPtr
<
compressible
::
RAS
Model
>
turbulence
autoPtr
<
compressible
::
turbulence
Model
>
turbulence
(
compressible
::
RAS
Model
::
New
compressible
::
turbulence
Model
::
New
(
rho
,
U
,
...
...
applications/solvers/Lagrangian/kinematicParcelFoam/kinematicParcelFoam.C
View file @
1cff9e54
...
...
@@ -26,14 +26,14 @@ Application
kinematicParcelFoam
Description
Transient solver for a single kinematicCloud. Uses precalculated velocity
Transient solver for a single kinematicCloud. Uses pre
-
calculated velocity
field to evolve a cloud.
\*---------------------------------------------------------------------------*/
#include "fvCFD.H"
#include "basicThermo.H"
#include "
compressible/RASModel/RAS
Model.H"
#include "
turbulence
Model.H"
#include "basicKinematicCloud.H"
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
...
...
@@ -49,7 +49,7 @@ int main(int argc, char *argv[])
#include "createFields.H"
#include "compressibleCourantNo.H"
// * *
* * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
//
* * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
Info
<<
"
\n
Starting time loop
\n
"
<<
endl
;
...
...
applications/solvers/combustion/PDRFoam/Make/options
View file @
1cff9e54
...
...
@@ -9,7 +9,8 @@ EXE_INC = \
-I$(LIB_SRC)/thermophysicalModels/specie/lnInclude \
-I$(LIB_SRC)/thermophysicalModels/basic/lnInclude \
-I$(LIB_SRC)/thermophysicalModels/combustion/lnInclude \
-I$(LIB_SRC)/turbulenceModels/RAS/compressible/lnInclude \
-I$(LIB_SRC)/turbulenceModels \
-I$(LIB_SRC)/turbulenceModels/compressible/RAS/lnInclude \
-I$(LIB_SRC)/thermophysicalModels/laminarFlameSpeed/lnInclude \
-I$(LIB_SRC)/finiteVolume/lnInclude \
-I$(LIB_SRC)/dynamicFvMesh/lnInclude \
...
...
applications/solvers/combustion/PDRFoam/PDRModels/turbulence/PDRkEpsilon/PDRkEpsilon.C
View file @
1cff9e54
...
...
@@ -50,7 +50,7 @@ PDRkEpsilon::PDRkEpsilon
const
volScalarField
&
rho
,
const
volVectorField
&
U
,
const
surfaceScalarField
&
phi
,
basicThermo
&
thermophysicalModel
const
basicThermo
&
thermophysicalModel
)
:
RASModel
(
typeName
,
rho
,
U
,
phi
,
thermophysicalModel
),
...
...
applications/solvers/combustion/PDRFoam/PDRModels/turbulence/PDRkEpsilon/PDRkEpsilon.H
View file @
1cff9e54
...
...
@@ -77,20 +77,19 @@ public:
// Constructors
//- from components
//-
Construct
from components
PDRkEpsilon
(
const
volScalarField
&
rho
,
const
volVectorField
&
U
,
const
surfaceScalarField
&
phi
,
basicThermo
&
thermophysicalModel
const
basicThermo
&
thermophysicalModel
);
// Destructor
~
PDRkEpsilon
()
{}
virtual
~
PDRkEpsilon
()
{}
// Member Functions
...
...
applications/solvers/combustion/PDRFoam/kEpsilon.H
deleted
100644 → 0
View file @
5a85f3c8
if
(
turbulence
)
{
volScalarField
divU
=
fvc
::
div
(
Uf
&
mesh
.
Sf
());
tmp
<
volTensorField
>
tgradU
=
fvc
::
grad
(
Uf
);
volScalarField
G
=
2
*
mut
*
(
tgradU
()
&&
dev
(
symm
(
tgradU
())));
tgradU
.
clear
();
// Add the blockage generation term so that it is included consistently
// in both the k and epsilon equations
volScalarField
GR
=
rho
*
mag
(
U
)
*
(
U
&
CT
&
U
);
# include "wallFunctions.H"
// Dissipation equation
fvScalarMatrix
epsEqn
(
betav
*
fvm
::
ddt
(
rho
,
epsilon
)
+
fvm
::
div
(
phi
,
epsilon
)
-
fvm
::
laplacian
(
fvc
::
interpolate
(
alphaEps
*
muEff
),
epsilon
)
==
C1
*
(
betav
*
G
+
GR
)
*
epsilon
/
k
-
fvm
::
SuSp
((
2
.
0
/
3
.
0
*
C1
)
*
betav
*
rho
*
divU
,
epsilon
)
-
fvm
::
Sp
(
C2
*
betav
*
rho
*
epsilon
/
k
,
epsilon
)
);
# include "wallDissipation.H"
epsEqn
.
solve
();
bound
(
epsilon
,
dimensionedScalar
(
"0"
,
epsilon
.
dimensions
(),
1.0e-15
));
// Turbulent kinetic energy equation
solve
(
betav
*
fvm
::
ddt
(
rho
,
k
)
+
fvm
::
div
(
phi
,
k
)
-
fvm
::
laplacian
(
fvc
::
interpolate
(
alphak
*
muEff
),
k
)
==
betav
*
G
+
GR
-
fvm
::
SuSp
(
2
.
0
/
3
.
0
*
betav
*
rho
*
divU
,
k
)
-
fvm
::
Sp
(
betav
*
rho
*
epsilon
/
k
,
k
)
);
bound
(
k
,
dimensionedScalar
(
"0"
,
k
.
dimensions
(),
0
.
0
));
//- Re-calculate turbulence viscosity
mut
=
Cmu
*
rho
*
sqr
(
k
)
/
epsilon
;
# include "wallViscosity.H"
}
muEff
=
mut
+
thermo
->
mu
();
applications/solvers/combustion/XiFoam/Make/options
View file @
1cff9e54
EXE_INC = \
-I$(LIB_SRC)/engine/lnInclude \
-I$(LIB_SRC)/finiteVolume/lnInclude \
-I$(LIB_SRC)/sampling/lnInclude \
-I$(LIB_SRC)/thermophysicalModels/specie/lnInclude \
-I$(LIB_SRC)/thermophysicalModels/basic/lnInclude \
-I$(LIB_SRC)/thermophysicalModels/combustion/lnInclude \
-I$(LIB_SRC)/turbulenceModels/RAS \
-I$(LIB_SRC)/thermophysicalModels/laminarFlameSpeed/lnInclude
-I$(LIB_SRC)/turbulenceModels/compressible/turbulenceModel \
-I$(LIB_SRC)/thermophysicalModels/laminarFlameSpeed/lnInclude \
-I$(LIB_SRC)/sampling/lnInclude \
-I$(LIB_SRC)/finiteVolume/lnInclude
EXE_LIBS = \
-lengine \
-lfiniteVolume \
-lmeshTools \
-lcompressibleRASModels \
-lcompressibleLESModels \
-lbasicThermophysicalModels \
-lcombustionThermophysicalModels \
-lspecie \
-llaminarFlameSpeedModels
-llaminarFlameSpeedModels \
-lfiniteVolume \
-lmeshTools
applications/solvers/combustion/XiFoam/XiFoam.C
View file @
1cff9e54
...
...
@@ -52,7 +52,7 @@ Description
#include "fvCFD.H"
#include "hhuCombustionThermo.H"
#include "
compressible/RASModel/RAS
Model.H"
#include "
turbulence
Model.H"
#include "laminarFlameSpeed.H"
#include "ignition.H"
#include "Switch.H"
...
...
applications/solvers/combustion/XiFoam/createFields.H
View file @
1cff9e54
...
...
@@ -48,9 +48,9 @@
Info
<<
"Creating turbulence model
\n
"
<<
endl
;
autoPtr
<
compressible
::
RAS
Model
>
turbulence
autoPtr
<
compressible
::
turbulence
Model
>
turbulence
(
compressible
::
RAS
Model
::
New
compressible
::
turbulence
Model
::
New
(
rho
,
U
,
...
...
@@ -60,7 +60,7 @@
);
Info
<<
"Creating field DpDt
\n
"
<<
endl
;
volScalarField
DpDt
=
volScalarField
DpDt
=
fvc
::
DDt
(
surfaceScalarField
(
"phiU"
,
phi
/
fvc
::
interpolate
(
rho
)),
p
);
...
...
applications/solvers/combustion/Xoodles/Make/files
deleted
100644 → 0
View file @
5a85f3c8
Xoodles.C
EXE = $(FOAM_APPBIN)/Xoodles
applications/solvers/combustion/Xoodles/Make/options
deleted
100644 → 0
View file @
5a85f3c8
EXE_INC = \
-I$(LIB_SRC)/engine/lnInclude \
-I$(LIB_SRC)/finiteVolume/lnInclude \
-I$(LIB_SRC)/meshTools/lnInclude \
-I$(LIB_SRC)/sampling/lnInclude \
-I$(LIB_SRC)/turbulenceModels/LES \
-I$(LIB_SRC)/turbulenceModels/LES/LESdeltas/lnInclude \
-I$(LIB_SRC)/thermophysicalModels/specie/lnInclude \
-I$(LIB_SRC)/thermophysicalModels/basic/lnInclude \
-I$(LIB_SRC)/thermophysicalModels/combustion/lnInclude \
-I$(LIB_SRC)/thermophysicalModels/laminarFlameSpeed/lnInclude \
-I../XiFoam
EXE_LIBS = \
-lengine \
-lfiniteVolume \
-lmeshTools \
-lbasicThermophysicalModels \
-lcombustionThermophysicalModels \
-lspecie \
-lcompressibleLESModels \
-llaminarFlameSpeedModels
applications/solvers/combustion/Xoodles/Xoodles.C
deleted
100644 → 0
View file @
5a85f3c8
/*---------------------------------------------------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | Copyright (C) 1991-2008 OpenCFD Ltd.
\\/ M anipulation |
-------------------------------------------------------------------------------
License
This file is part of OpenFOAM.
OpenFOAM is free software; you can redistribute it and/or modify it
under the terms of the GNU General Public License as published by the
Free Software Foundation; either version 2 of the License, or (at your
option) any later version.
OpenFOAM is distributed in the hope that it will be useful, but WITHOUT
ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or
FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License
for more details.
You should have received a copy of the GNU General Public License
along with OpenFOAM; if not, write to the Free Software Foundation,
Inc., 51 Franklin St, Fifth Floor, Boston, MA 02110-1301 USA
Application
Xoodles
Description
Compressible premixed/partially-premixed combustion solver with large-eddy
simulation (LES) turbulence modelling.
Combusting LES code using the b-Xi two-equation model.
Xi may be obtained by either the solution of the Xi transport
equation or from an algebraic exression. Both approaches are
based on Gulder's flame speed correlation which has been shown
to be appropriate for LES by comparison with the results from the
spectral model.
Strain effects are encorporated directly into the Xi equation
but not in the algebraic approximation. Further work need to be
done on this issue, particularly regarding the enhanced removal rate
caused by flame compression. Analysis using results of the spectral
model will be required.
For cases involving very lean Propane flames or other flames which are
very strain-sensitive, a transport equation for the laminar flame
speed is present. This equation is derived using heuristic arguments
involving the strain time scale and the strain-rate at extinction.
the transport velocity is the same as that for the Xi equation.
\*---------------------------------------------------------------------------*/
#include "fvCFD.H"
#include "hhuCombustionThermo.H"
#include "compressible/LESModel/LESModel.H"
#include "laminarFlameSpeed.H"
#include "ignition.H"
#include "IFstream.H"
#include "OFstream.H"
#define divDevRhoReff divDevRhoBeff
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
int
main
(
int
argc
,
char
*
argv
[])
{
#include "setRootCase.H"
#include "createTime.H"
#include "createMeshNoClear.H"
#include "readEnvironmentalProperties.H"
#include "createFields.H"
#include "readPISOControls.H"
#include "readCombustionProperties.H"
#include "initContinuityErrs.H"
Info
<<
"
\n
Starting time loop
\n
"
<<
endl
;
for
(
runTime
++
;
!
runTime
.
end
();
runTime
++
)
{
Info
<<
"Time = "
<<
runTime
.
timeName
()
<<
nl
<<
endl
;
#include "compressibleCourantNo.H"
#include "rhoEqn.H"
turbulence
->
correct
();
#include "UEqn.H"
// --- PISO loop
for
(
int
corr
=
1
;
corr
<=
nCorr
;
corr
++
)
{
#include "ftEqn.H"
#include "bEqn.H"
#include "huEqn.H"
#include "hEqn.H"
if
(
!
ign
.
ignited
())
{
hu
==
h
;
}
#include "pEqn.H"
}
runTime
.
write
();
rho
=
thermo
->
rho
();
Info
<<
"ExecutionTime = "
<<
runTime
.
elapsedCpuTime
()
<<
" s"
<<
" ClockTime = "
<<
runTime
.
elapsedClockTime
()
<<
" s"
<<
nl
<<
endl
;
}
Info
<<
"End
\n
"
<<
endl
;
return
(
0
);
}
// ************************************************************************* //
applications/solvers/combustion/Xoodles/createFields.H
deleted
100644 → 0
View file @
5a85f3c8
Info
<<
"Reading thermophysical properties
\n
"
<<
endl
;
autoPtr
<
hhuCombustionThermo
>
thermo
(
hhuCombustionThermo
::
New
(
mesh
)
);
combustionMixture
&
composition
=
thermo
->
composition
();
volScalarField
rho
(
IOobject
(
"rho"
,
runTime
.
timeName
(),
mesh
,
IOobject
::
NO_READ
,
IOobject
::
AUTO_WRITE
),
thermo
->
rho
()
);
volScalarField
&
p
=
thermo
->
p
();
const
volScalarField
&
psi
=
thermo
->
psi
();
volScalarField
&
h
=
thermo
->
h
();
volScalarField
&
hu
=
thermo
->
hu
();
volScalarField
&
b
=
composition
.
Y
(
"b"
);
Info
<<
"min(b) = "
<<
min
(
b
).
value
()
<<
endl
;
const
volScalarField
&
T
=
thermo
->
T
();
Info
<<
"
\n
Reading field U
\n
"
<<
endl
;
volVectorField
U
(
IOobject
(
"U"
,
runTime
.
timeName
(),
mesh
,
IOobject
::
MUST_READ
,
IOobject
::
AUTO_WRITE
),
mesh
);
# include "compressibleCreatePhi.H"
Info
<<
"Creating turbulence model
\n
"
<<
endl
;
autoPtr
<
compressible
::
LESModel
>
turbulence
(
compressible
::
LESModel
::
New
(
rho
,
U
,
phi
,
thermo
())
);
Info
<<
"Creating field DpDt
\n
"
<<
endl
;
volScalarField
DpDt
=
fvc
::
DDt
(
surfaceScalarField
(
"phiU"
,
phi
/
fvc
::
interpolate
(
rho
)),
p
);
Info
<<
"Creating field Xi
\n
"
<<
endl
;
volScalarField
Xi
(
IOobject
(
"Xi"
,
runTime
.
timeName
(),
mesh
,
IOobject
::
MUST_READ
,
IOobject
::
AUTO_WRITE
),
mesh
);
Info
<<
"Creating the unstrained laminar flame speed
\n
"
<<
endl
;
autoPtr
<
laminarFlameSpeed
>
unstrainedLaminarFlameSpeed
(
laminarFlameSpeed
::
New
(
thermo
)
);
Info
<<
"Reading strained laminar flame speed field Su
\n
"
<<
endl
;
volScalarField
Su
(
IOobject
(
"Su"
,
runTime
.
timeName
(),
mesh
,
IOobject
::
MUST_READ
,
IOobject
::
AUTO_WRITE
),
mesh
);
dimensionedScalar
SuMin
=
0
.
01
*
Su
.
average
();
dimensionedScalar
SuMax
=
4
*
Su
.
average
();
Info
<<
"Calculating turbulent flame speed field St
\n
"
<<
endl
;
volScalarField
St
(
IOobject
(
"St"
,
runTime
.
timeName
(),
mesh
,
IOobject
::
NO_READ
,
IOobject
::
AUTO_WRITE
),
Xi
*
Su
);
multivariateSurfaceInterpolationScheme
<
scalar
>::
fieldTable
fields
;
if
(
composition
.
contains
(
"ft"
))
{
fields
.
add
(
composition
.
Y
(
"ft"
));
}
fields
.
add
(
b
);
fields
.
add
(
h
);
fields
.
add
(
hu
);
applications/solvers/combustion/coldEngineFoam/Make/options
View file @
1cff9e54
...
...
@@ -2,15 +2,16 @@ EXE_INC = \
-I../engineFoam \
-I../XiFoam \
-I$(LIB_SRC)/engine/lnInclude \
-I$(LIB_SRC)/finiteVolume/lnInclude \
-I$(LIB_SRC)/thermophysicalModels/specie/lnInclude \
-I$(LIB_SRC)/thermophysicalModels/basic/lnInclude \
-I$(LIB_SRC)/thermophysicalModels/combustion/lnInclude \
-I$(LIB_SRC)/turbulenceModels/RAS/compressible/lnInclude
-I$(LIB_SRC)/turbulenceModels/compressible/turbulenceModel \
-I$(LIB_SRC)/finiteVolume/lnInclude
EXE_LIBS = \
-lengine \
-lfiniteVolume \
-lcompressibleRASModels \
-lcompressibleLESModels \
-lbasicThermophysicalModels \
-lspecie
-lspecie \
-lfiniteVolume
applications/solvers/combustion/coldEngineFoam/coldEngineFoam.C
View file @
1cff9e54
...
...
@@ -34,7 +34,7 @@ Description
#include "engineTime.H"
#include "engineMesh.H"
#include "basicThermo.H"
#include "
RAS
Model.H"
#include "
turbulence
Model.H"
#include "OFstream.H"
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
...
...
applications/solvers/combustion/coldEngineFoam/createFields.H
View file @
1cff9e54
...
...
@@ -42,9 +42,9 @@
Info
<<
"Creating turbulence model
\n
"
<<
endl
;
autoPtr
<
compressible
::
RAS
Model
>
turbulence
autoPtr
<
compressible
::
turbulence
Model
>
turbulence
(
compressible
::
RAS
Model
::
New
compressible
::
turbulence
Model
::
New
(
rho
,
U
,
...
...
applications/solvers/combustion/dieselEngineFoam/Make/options
View file @
1cff9e54
EXE_INC = \
-I../engineFoam \
-I$(LIB_SRC)/finiteVolume/lnInclude \
-I$(LIB_SRC)/turbulenceModels/RAS \
-I$(LIB_SRC)/turbulenceModels/compressible/turbulenceModel \
-I$(LIB_SRC)/lagrangian/basic/lnInclude \
-I$(LIB_SRC)/lagrangian/dieselSpray/lnInclude \
-I$(LIB_SRC)/thermophysicalModels/liquids/lnInclude \
...
...
@@ -14,11 +13,13 @@ EXE_INC = \
-I$(LIB_SRC)/../applications/solvers/combustion/XiFoam \
-I$(LIB_SRC)/thermophysicalModels/chemistryModel/lnInclude \
-I$(LIB_SRC)/ODE/lnInclude \
-I$(LIB_SRC)/engine/lnInclude
-I$(LIB_SRC)/engine/lnInclude \
-I$(LIB_SRC)/finiteVolume/lnInclude \
EXE_LIBS = \
-lengine \
-lcompressibleRASModels \
-lcompressibleLESModels \
-lcombustionThermophysicalModels \
-lfiniteVolume \
-llagrangian \
...
...
applications/solvers/combustion/dieselEngineFoam/createFields.H
View file @
1cff9e54
...
...
@@ -58,9 +58,9 @@ volScalarField kappa
);
Info
<<
"Creating turbulence model.
\n
"
<<
nl
;
autoPtr
<
compressible
::
RAS
Model
>
turbulence
autoPtr
<
compressible
::
turbulence
Model
>
turbulence
(
compressible
::
RAS
Model
::
New
compressible
::
turbulence
Model
::
New
(
rho
,
U
,
...
...
@@ -70,7 +70,7 @@ autoPtr<compressible::RASModel> turbulence
);
Info
<<
"Creating field DpDt
\n
"
<<
endl
;
volScalarField
DpDt
=
volScalarField
DpDt
=
fvc
::
DDt
(
surfaceScalarField
(
"phiU"
,
phi
/
fvc
::
interpolate
(
rho
)),
p
);
Info
<<
"Constructing chemical mechanism"
<<
endl
;
...
...
applications/solvers/combustion/dieselEngineFoam/dieselEngineFoam.C
View file @
1cff9e54
...
...
@@ -34,7 +34,7 @@ Description
#include "engineTime.H"
#include "engineMesh.H"
#include "hCombustionThermo.H"
#include "
compressible/RASModel/RAS
Model.H"
#include "
turbulence
Model.H"
#include "spray.H"
#include "chemistryModel.H"
#include "chemistrySolver.H"
...
...
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