executed with foamRun for single region simulations of foamMultiRun for
multi-region simulations. Replaces multiphaseEulerFoam and all the
corresponding tutorials have been updated and moved to
tutorials/modules/multiphaseEuler.
Class
Foam::solvers::multiphaseEuler
Description
Solver module for a system of any number of compressible fluid phases with a
common pressure, but otherwise separate properties. The type of phase model
is run time selectable and can optionally represent multiple species and
in-phase reactions. The phase system is also run time selectable and can
optionally represent different types of momentum, heat and mass transfer.
Uses the flexible PIMPLE (PISO-SIMPLE) solution for time-resolved and
pseudo-transient and steady simulations.
Optional fvModels and fvConstraints are provided to enhance the simulation
in many ways including adding various sources, Lagrangian
particles, surface film etc. and constraining or limiting the solution.
SourceFiles
multiphaseEuler.C
See also
Foam::solvers::compressibleVoF
Foam::solvers::fluidSolver
Foam::solvers::incompressibleFluid
The surfaceFilm fvModel has been renamed surfaceFilms, and can now have
a number of independent film models specified.
For example, the hotBoxes tutorial could be modified to have separate
film regions for the boxes and for the floor. In which case, the names
of the separate films would need specifying as shown below.
surfaceFilms
{
type surfaceFilms;
surfaceFilms (boxesFilm floorFilm); // <-- new entry
libs ("libsurfaceFilmModels.so");
}
The old fvModel name, surfaceFilm, has been maintained for backwards
compatibility.
The Lagrangian surface film model now also requires the coupled
surfaceFilms to be specified when there is not just a single
default-named film. For example, in constant/cloudProperties:
subModels
{
surfaceFilmModel thermoSurfaceFilm;
thermoSurfaceFilmCoeffs
{
surfaceFilms (boxesFilm floorFilm); // <-- new entry
interactionType splashBai;
deltaWet 0.0005;
Adry 2630;
Awet 1320;
Cf 0.6;
}
...
}
so that it can now be used with either the isothermalFluid or fluid solver
modules, thus supporting non-uniform fluid properties, compressibility and
thermal effect. This development makes the special potentialFreeSurfaceFoam
solver redundant as both the isothermalFluid and fluid solver modules are more
general and has been removed and replaced with a user redirection script.
The tutorials/multiphase/potentialFreeSurfaceFoam cases have been updated to run
with the isothermalFluid solver module:
tutorials/multiphase/potentialFreeSurfaceFoam/oscillatingBox
tutorials/multiphase/potentialFreeSurfaceFoam/movingOscillatingBox
which demonstrate how to upgrade potentialFreeSurfaceFoam cases to
isothermalFluid.
executed with foamRun for single region simulations of foamMultiRun for
multi-region simulations. Replaces compressibleInterFoam and all the
corresponding tutorials have been updated and moved to
tutorials/modules/compressibleVoF.
Class
Foam::solvers::compressibleVoF
Description
Solver module for for 2 compressible, non-isothermal immiscible fluids
using a VOF (volume of fluid) phase-fraction based interface capturing
approach, with optional mesh motion and mesh topology changes including
adaptive re-meshing.
The momentum and other fluid properties are of the "mixture" and a single
momentum equation is solved.
Either mixture or two-phase transport modelling may be selected. In the
mixture approach a single laminar, RAS or LES model is selected to model the
momentum stress. In the Euler-Euler two-phase approach separate laminar,
RAS or LES selected models are selected for each of the phases.
Uses the flexible PIMPLE (PISO-SIMPLE) solution for time-resolved and
pseudo-transient and steady simulations.
Optional fvModels and fvConstraints are provided to enhance the simulation
in many ways including adding various sources, Lagrangian
particles, surface film etc. and constraining or limiting the solution.
SourceFiles
compressibleVoF.C
See also
Foam::solvers::fluidSolver
MRF (multiple reference frames) can now be used to simulate SRF (single
reference frame) cases by defining the MRF zone to include all the cells is the
mesh and applying appropriate boundary conditions. The huge advantage of this
is that MRF can easily be added to any solver by the addition of forcing terms
in the momentum equation and absolute velocity to relative flux conversions in
the formulation of the pressure equation rather than having to reformulate the
momentum and pressure system based on the relative velocity as in traditional
SRF. Also most of the OpenFOAM solver applications and all the solver modules
already support MRF.
To enable this generalisation of MRF the transformations necessary on the
velocity boundary conditions in the MRF zone can no longer be handled by the
MRFZone class itself but special adapted fvPatchFields are required. Although
this adds to the case setup it provides much greater flexibility and now complex
inlet/outlet conditions can be applied within the MRF zone, necessary for some
SRF case and which was not possible in the original MRF implementation. Now for
walls rotating within the MRF zone the new 'MRFnoSlip' velocity boundary
conditions must be applied, e.g. in the
tutorials/modules/incompressibleFluid/mixerVessel2DMRF/constant/MRFProperties
case:
boundaryField
{
rotor
{
type MRFnoSlip;
}
stator
{
type noSlip;
}
front
{
type empty;
}
back
{
type empty;
}
}
similarly for SRF cases, e.g. in the
tutorials/modules/incompressibleFluid/mixerSRF case:
boundaryField
{
inlet
{
type fixedValue;
value uniform (0 0 -10);
}
outlet
{
type pressureInletOutletVelocity;
value $internalField;
}
rotor
{
type MRFnoSlip;
}
outerWall
{
type noSlip;
}
cyclic_half0
{
type cyclic;
}
cyclic_half1
{
type cyclic;
}
}
For SRF case all the cells should be selected in the MRFproperties dictionary
which is achieved by simply setting the optional 'selectionMode' entry to all,
e.g.:
SRF
{
selectionMode all;
origin (0 0 0);
axis (0 0 1);
rpm 1000;
}
In the above the rotational speed is set in RPM rather than rad/s simply by
setting the 'rpm' entry rather than 'omega'.
The tutorials/modules/incompressibleFluid/rotor2DSRF case is more complex and
demonstrates a transient SRF simulation of a rotor requiring the free-stream
velocity to rotate around the apparently stationary rotor which is achieved
using the new 'MRFFreestreamVelocity' velocity boundary condition. The
equivalent simulation can be achieved by simply rotating the entire mesh and
keeping the free-stream flow stationary and this is demonstrated in the
tutorials/modules/incompressibleFluid/rotor2DRotating case for comparison.
The special SRFSimpleFoam and SRFPimpleFoam solvers are now redundant and have
been replaced by redirection scripts providing details of the case migration
process.
executed with foamRun for single region simulations of foamMultiRun for
multi-region simulations. Replaces pimpleFoam, pisoFoam and simpleFoam and all
the corresponding tutorials have been updated and moved to
tutorials/modules/incompressibleFluid.
Class
Foam::solvers::incompressibleFluid
Description
Solver module for steady or transient turbulent flow of incompressible
isothermal fluids with optional mesh motion and change.
Uses the flexible PIMPLE (PISO-SIMPLE) solution for time-resolved and
pseudo-transient and steady simulations.
Optional fvModels and fvConstraints are provided to enhance the simulation
in many ways including adding various sources, constraining or limiting
the solution.
Reference:
\verbatim
Greenshields, C. J., & Weller, H. G. (2022).
Notes on Computational Fluid Dynamics: General Principles.
CFD Direct Ltd.: Reading, UK.
\endverbatim
SourceFiles
incompressibleFluid.C
See also
Foam::solvers::fluidSolver
Foam::solvers::isothermalFluid
Application
foamPostProcess
Description
Execute the set of functionObjects specified in the selected dictionary
(which defaults to system/controlDict) or on the command-line for the
selected set of times on the selected set of fields.
The functionObjects are either executed directly or for the solver
optionally specified as a command-line argument.
Usage
\b foamPostProcess [OPTION]
- \par -dict <file>
Read control dictionary from specified location
- \par -solver <name>
Solver name
- \par -libs '(\"lib1.so\" ... \"libN.so\")'
Specify the additional libraries loaded
-\par -region <name>
Specify the region
- \par -func <name>
Specify the name of the functionObject to execute, e.g. Q
- \par -funcs <list>
Specify the names of the functionObjects to execute, e.g. '(Q div(U))'
- \par -field <name>
Specify the name of the field to be processed, e.g. U
- \par -fields <list>
Specify a list of fields to be processed,
e.g. '(U T p)' - regular expressions not currently supported
- \par -time <ranges>
comma-separated time ranges - eg, ':10,20,40:70,1000:'
- \par -latestTime
Select the latest time
- \par -list
List the available configured functionObjects
Example usage:
- Print the list of available configured functionObjects:
\verbatim
foamPostProcess -list
\endverbatim
- Execute the functionObjects specified in the controlDict of the
fluid region for all the available times:
\verbatim
foamPostProcess -region fluid
\endverbatim
- Execute the functionObjects specified in the controlDict
for the 'fluid' solver in the 'cooling' region for the latest time only:
\verbatim
foamPostProcess -solver fluid -region cooling -latestTime
\endverbatim
A postProcess redirection script is provided for backward-compatibility.
in which different solver modules can be selected in each region to for complex
conjugate heat-transfer and other combined physics problems such as FSI
(fluid-structure interaction).
For single-region simulations the solver module is selected, instantiated and
executed in the PIMPLE loop in the new foamRun application.
For multi-region simulations the set of solver modules, one for each region, are
selected, instantiated and executed in the multi-region PIMPLE loop of new the
foamMultiRun application.
This provides a very general, flexible and extensible framework for complex
coupled problems by creating more solver modules, either by converting existing
solver applications or creating new ones.
The current set of solver modules provided are:
isothermalFluid
Solver module for steady or transient turbulent flow of compressible
isothermal fluids with optional mesh motion and mesh topology changes.
Created from the rhoSimpleFoam, rhoPimpleFoam and buoyantFoam solvers but
without the energy equation, hence isothermal. The buoyant pressure
formulation corresponding to the buoyantFoam solver is selected
automatically by the presence of the p_rgh pressure field in the start-time
directory.
fluid
Solver module for steady or transient turbulent flow of compressible fluids
with heat-transfer for HVAC and similar applications, with optional
mesh motion and mesh topology changes.
Derived from the isothermalFluid solver module with the addition of the
energy equation from the rhoSimpleFoam, rhoPimpleFoam and buoyantFoam
solvers, thus providing the equivalent functionality of these three solvers.
multicomponentFluid
Solver module for steady or transient turbulent flow of compressible
reacting fluids with optional mesh motion and mesh topology changes.
Derived from the isothermalFluid solver module with the addition of
multicomponent thermophysical properties energy and specie mass-fraction
equations from the reactingFoam solver, thus providing the equivalent
functionality in reactingFoam and buoyantReactingFoam. Chemical reactions
and/or combustion modelling may be optionally selected to simulate reacting
systems including fires, explosions etc.
solid
Solver module for turbulent flow of compressible fluids for conjugate heat
transfer, HVAC and similar applications, with optional mesh motion and mesh
topology changes.
The solid solver module may be selected in solid regions of a CHT case, with
either the fluid or multicomponentFluid solver module in the fluid regions
and executed with foamMultiRun to provide functionality equivalent
chtMultiRegionFoam but in a flexible and extensible framework for future
extension to more complex coupled problems.
All the usual fvModels, fvConstraints, functionObjects etc. are available with
these solver modules to support simulations including body-forces, local sources,
Lagrangian clouds, liquid films etc. etc.
Converting compressibleInterFoam and multiphaseEulerFoam into solver modules
would provide a significant enhancement to the CHT capability and incompressible
solvers like pimpleFoam run in conjunction with solidDisplacementFoam in
foamMultiRun would be useful for a range of FSI problems. Many other
combinations of existing solvers converted into solver modules could prove
useful for a very wide range of complex combined physics simulations.
All tutorials from the rhoSimpleFoam, rhoPimpleFoam, buoyantFoam, reactingFoam,
buoyantReactingFoam and chtMultiRegionFoam solver applications replaced by
solver modules have been updated and moved into the tutorials/modules directory:
modules
├── CHT
│ ├── coolingCylinder2D
│ ├── coolingSphere
│ ├── heatedDuct
│ ├── heatExchanger
│ ├── reverseBurner
│ └── shellAndTubeHeatExchanger
├── fluid
│ ├── aerofoilNACA0012
│ ├── aerofoilNACA0012Steady
│ ├── angledDuct
│ ├── angledDuctExplicitFixedCoeff
│ ├── angledDuctLTS
│ ├── annularThermalMixer
│ ├── BernardCells
│ ├── blockedChannel
│ ├── buoyantCavity
│ ├── cavity
│ ├── circuitBoardCooling
│ ├── decompressionTank
│ ├── externalCoupledCavity
│ ├── forwardStep
│ ├── helmholtzResonance
│ ├── hotRadiationRoom
│ ├── hotRadiationRoomFvDOM
│ ├── hotRoom
│ ├── hotRoomBoussinesq
│ ├── hotRoomBoussinesqSteady
│ ├── hotRoomComfort
│ ├── iglooWithFridges
│ ├── mixerVessel2DMRF
│ ├── nacaAirfoil
│ ├── pitzDaily
│ ├── prism
│ ├── shockTube
│ ├── squareBend
│ ├── squareBendLiq
│ └── squareBendLiqSteady
└── multicomponentFluid
├── aachenBomb
├── counterFlowFlame2D
├── counterFlowFlame2D_GRI
├── counterFlowFlame2D_GRI_TDAC
├── counterFlowFlame2DLTS
├── counterFlowFlame2DLTS_GRI_TDAC
├── cylinder
├── DLR_A_LTS
├── filter
├── hotBoxes
├── membrane
├── parcelInBox
├── rivuletPanel
├── SandiaD_LTS
├── simplifiedSiwek
├── smallPoolFire2D
├── smallPoolFire3D
├── splashPanel
├── verticalChannel
├── verticalChannelLTS
└── verticalChannelSteady
Also redirection scripts are provided for the replaced solvers which call
foamRun -solver <solver module name> or foamMultiRun in the case of
chtMultiRegionFoam for backward-compatibility.
Documentation for foamRun and foamMultiRun:
Application
foamRun
Description
Loads and executes an OpenFOAM solver module either specified by the
optional \c solver entry in the \c controlDict or as a command-line
argument.
Uses the flexible PIMPLE (PISO-SIMPLE) solution for time-resolved and
pseudo-transient and steady simulations.
Usage
\b foamRun [OPTION]
- \par -solver <name>
Solver name
- \par -libs '(\"lib1.so\" ... \"libN.so\")'
Specify the additional libraries loaded
Example usage:
- To run a \c rhoPimpleFoam case by specifying the solver on the
command line:
\verbatim
foamRun -solver fluid
\endverbatim
- To update and run a \c rhoPimpleFoam case add the following entries to
the controlDict:
\verbatim
application foamRun;
solver fluid;
\endverbatim
then execute \c foamRun
Application
foamMultiRun
Description
Loads and executes an OpenFOAM solver modules for each region of a
multiregion simulation e.g. for conjugate heat transfer.
The region solvers are specified in the \c regionSolvers dictionary entry in
\c controlDict, containing a list of pairs of region and solver names,
e.g. for a two region case with one fluid region named
liquid and one solid region named tubeWall:
\verbatim
regionSolvers
{
liquid fluid;
tubeWall solid;
}
\endverbatim
The \c regionSolvers entry is a dictionary to support name substitutions to
simplify the specification of a single solver type for a set of
regions, e.g.
\verbatim
fluidSolver fluid;
solidSolver solid;
regionSolvers
{
tube1 $fluidSolver;
tubeWall1 solid;
tube2 $fluidSolver;
tubeWall2 solid;
tube3 $fluidSolver;
tubeWall3 solid;
}
\endverbatim
Uses the flexible PIMPLE (PISO-SIMPLE) solution for time-resolved and
pseudo-transient and steady simulations.
Usage
\b foamMultiRun [OPTION]
- \par -libs '(\"lib1.so\" ... \"libN.so\")'
Specify the additional libraries loaded
Example usage:
- To update and run a \c chtMultiRegion case add the following entries to
the controlDict:
\verbatim
application foamMultiRun;
regionSolvers
{
fluid fluid;
solid solid;
}
\endverbatim
then execute \c foamMultiRun
The reconstructPar utility now reconstructs the mesh if and when it is
necessary to do so. The reconstructParMesh utility is therefore no
longer necessary and has been removed.
It was necessary/advantagous to consolidate these utilities into one
because in the case of mesh changes it becomes increasingly less clear
which of the separate utilities is responsible for reconstructing data
that is neither clearly physical field nor mesh topology; e.g., moving
points, sets, refinement data, and so on.
If files of the same name exist in different sub-directories of the main
directory, e.g. 'inletPatch/0/patch.vtk' and 'outletPatch/0/patch.vtk', a
further index is appended to the name in the generated links, e.g.
'patch0.0000.vtk' and 'patch1.0000.vtk'
When cloning a case, users can copy the field data from the
from the latest time directory in the source case, using
the -latestTime option.
The -startFrom option enables the copied time directory to be
renamed, often as the '0' (zero) directory in the new case, e.g.
foamCloneCase -latestTime -startFrom 0 sourceCase newCase
When the time directories in the source and new cases are
different, the uniform directory and flux field "phi" are
deleted from the copied time directory to avoid incorrect
initial state.
This major development provides coupling of patches which are
non-conformal, i.e. where the faces of one patch do not match the faces
of the other. The coupling is fully conservative and second order
accurate in space, unlike the Arbitrary Mesh Interface (AMI) and
associated ACMI and Repeat AMI methods which NCC replaces.
Description:
A non-conformal couple is a connection between a pair of boundary
patches formed by projecting one patch onto the other in a way that
fills the space between them. The intersection between the projected
surface and patch forms new faces that are incorporated into the finite
volume mesh. These new faces are created identically on both sides of
the couple, and therefore become equivalent to internal faces within the
mesh. The affected cells remain closed, meaning that the area vectors
sum to zero for all the faces of each cell. Consequently, the main
benefits of the finite volume method, i.e. conservation and accuracy,
are not undermined by the coupling.
A couple connects parts of mesh that are otherwise disconnected and can
be used in the following ways:
+ to simulate rotating geometries, e.g. a propeller or stirrer, in which
a part of the mesh rotates with the geometry and connects to a
surrounding mesh which is not moving;
+ to connect meshes that are generated separately, which do not conform
at their boundaries;
+ to connect patches which only partially overlap, in which the
non-overlapped section forms another boundary, e.g. a wall;
+ to simulate a case with a geometry which is periodically repeating by
creating multiple couples with different transformations between
patches.
The capability for simulating partial overlaps replaces the ACMI
functionality, currently provided by the 'cyclicACMI' patch type, and
which is unreliable unless the couple is perfectly flat. The capability
for simulating periodically repeating geometry replaces the Repeat AMI
functionality currently provided by the 'cyclicRepeatAMI' patch type.
Usage:
The process of meshing for NCC is very similar to existing processes for
meshing for AMI. Typically, a mesh is generated with an identifiable set
of internal faces which coincide with the surface through which the mesh
will be coupled. These faces are then duplicated by running the
'createBaffles' utility to create two boundary patches. The points are
then split using 'splitBaffles' in order to permit independent motion of
the patches.
In AMI, these patches are assigned the 'cyclicAMI' patch type, which
couples them using AMI interpolation methods.
With NCC, the patches remain non-coupled, e.g. a 'wall' type. Coupling
is instead achieved by running the new 'createNonConformalCouples'
utility, which creates additional coupled patches of type
'nonConformalCyclic'. These appear in the 'constant/polyMesh/boundary'
file with zero faces; they are populated with faces in the finite volume
mesh during the connection process in NCC.
For a single couple, such as that which separates the rotating and
stationary sections of a mesh, the utility can be called using the
non-coupled patch names as arguments, e.g.
createNonConformalCouples -overwrite rotatingZoneInner rotatingZoneOuter
where 'rotatingZoneInner' and 'rotatingZoneOuter' are the names of the
patches.
For multiple couples, and/or couples with transformations,
'createNonConformalCouples' should be run without arguments. Settings
will then be read from a configuration file named
'system/createNonConformalCouplesDict'. See
'$FOAM_ETC/caseDicts/annotated/createNonConformalCouplesDict' for
examples.
Boundary conditions must be specified for the non-coupled patches. For a
couple where the patches fully overlap, boundary conditions
corresponding to a slip wall are typically applied to fields, i.e
'movingWallSlipVelocity' (or 'slip' if the mesh is stationary) for
velocity U, 'zeroGradient' or 'fixedFluxPressure' for pressure p, and
'zeroGradient' for other fields. For a couple with
partially-overlapping patches, boundary conditions are applied which
physically represent the non-overlapped region, e.g. a no-slip wall.
Boundary conditions also need to be specified for the
'nonConformalCyclic' patches created by 'createNonConformalCouples'. It
is generally recommended that this is done by including the
'$FOAM_ETC/caseDicts/setConstraintTypes' file in the 'boundaryField'
section of each of the field files, e.g.
boundaryField
{
#includeEtc "caseDicts/setConstraintTypes"
inlet
{
...
}
...
}
For moving mesh cases, it may be necessary to correct the mesh fluxes
that are changed as a result of the connection procedure. If the
connected patches do not conform perfectly to the mesh motion, then
failure to correct the fluxes can result in noise in the pressure
solution.
Correction for the mesh fluxes is enabled by the 'correctMeshPhi' switch
in the 'PIMPLE' (or equivalent) section of 'system/fvSolution'. When it
is enabled, solver settings are required for 'MeshPhi'. The solution
just needs to distribute the error enough to dissipate the noise. A
smooth solver with a loose tolerance is typically sufficient, e.g. the
settings in 'system/fvSolution' shown below:
solvers
{
MeshPhi
{
solver smoothSolver;
smoother symGaussSeidel;
tolerance 1e-2;
relTol 0;
}
...
}
PIMPLE
{
correctMeshPhi yes;
...
}
The solution of 'MeshPhi' is an inexpensive computation since it is
applied only to a small subset of the mesh adjacent to the
couple. Conservation is maintained whether or not the mesh flux
correction is enabled, and regardless of the solution tolerance for
'MeshPhi'.
Advantages of NCC:
+ NCC maintains conservation which is required for many numerical
schemes and algorithms to operate effectively, in particular those
designed to maintain boundedness of a solution.
+ Closed-volume systems no longer suffer from accumulation or loss of
mass, poor convergence of the pressure equation, and/or concentration
of error in the reference cell.
+ Partially overlapped simulations are now possible on surfaces that are
not perfectly flat. The projection fills space so no overlaps or
spaces are generated inside contiguously overlapping sections, even if
those sections have sharp angles.
+ The finite volume faces created by NCC have geometrically accurate
centres. This makes the method second order accurate in space.
+ The polyhedral mesh no longer requires duplicate boundary faces to be
generated in order to run a partially overlapped simulation.
+ Lagrangian elements can now transfer across non-conformal couplings in
parallel.
+ Once the intersection has been computed and applied to the finite
volume mesh, it can use standard cyclic or processor cyclic finite
volume boundary conditions, with no need for additional patch types or
matrix interfaces.
+ Parallel communication is done using the standard
processor-patch-field system. This is more efficient than alternative
systems since it has been carefully optimised for use within the
linear solvers.
+ Coupled patches are disconnected prior to mesh motion and topology
change and reconnected afterwards. This simplifies the boundary
condition specification for mesh motion fields.
Resolved Bug Reports:
+ https://bugs.openfoam.org/view.php?id=663
+ https://bugs.openfoam.org/view.php?id=883
+ https://bugs.openfoam.org/view.php?id=887
+ https://bugs.openfoam.org/view.php?id=1337
+ https://bugs.openfoam.org/view.php?id=1388
+ https://bugs.openfoam.org/view.php?id=1422
+ https://bugs.openfoam.org/view.php?id=1829
+ https://bugs.openfoam.org/view.php?id=1841
+ https://bugs.openfoam.org/view.php?id=2274
+ https://bugs.openfoam.org/view.php?id=2561
+ https://bugs.openfoam.org/view.php?id=3817
Deprecation:
NCC replaces the functionality provided by AMI, ACMI and Repeat AMI.
ACMI and Repeat AMI are insufficiently reliable to warrant further
maintenance so are removed in an accompanying commit to OpenFOAM-dev.
AMI is more widely used so will be retained alongside NCC for the next
version release of OpenFOAM and then subsequently removed from
OpenFOAM-dev.
Solver for steady or transient buoyant, turbulent flow of compressible fluids
for ventilation and heat-transfer, with optional mesh motion and mesh topology
changes. Created by merging buoyantSimpleFoam and buoyantPimpleFoam to provide
a more general solver and simplify maintenance.
With the general run-time selectable fvMeshMovers engine compression simulations
can be performed with reactingFoam so there is no longer any need for engine
specific solvers or engineMesh.
An engineFoam script is provided to redirect users to reactingFoam with
instructions.
With the general run-time selectable fvMeshMovers engine compression simulations
can be performed with rhoPimpleFoam so there is no longer any need for engine
specific solvers.
A coldEngineFoam script is provided to redirect users to rhoPimpleFoam with
instructions.
topoSet is a more flexible and extensible replacement for setSet using standard
OpenFOAM dictionary input format rather than the limited command-line input
format developed specifically for setSet. This replacement allows for the
removal of a significant amount of code simplifying maintenance and the addition
of more topoSet sources.
For example, 'foamInfo RosinRammler' includes in the output:
Model
This appears to be the 'RosinRammler' model of the 'distributionModels' family.
The models in the 'distributionModels' family are:
+ exponential
+ fixedValue
+ general
+ massRosinRammler
+ multiNormal
+ normal
+ RosinRammler
+ uniform
to avoid further confusion from users migrating from very old OpenFOAM versions.
The surfaceFeatureExtract utility has been superseded and replaced by by the
more general surfaceFeatures utility.
surfaceFeatures reads a surfaceFeaturesDict input file with a much
simpler, more convenient format. Example surfaceFeaturesDict files
can be found in the tutorial and template cases, e.g. located as
follows:
find \$FOAM_TUTORIALS -name surfaceFeaturesDict
find \$FOAM_ETC -name surfaceFeaturesDict
The generation script has also been modified slightly to prevent empty
entries being generated for scripts with no options; e.g., the scripts
in $WM_PROJECT_DIR/bin that report a change in application name
splitBaffles identifies baffle faces; i.e., faces on the mesh boundary
which share the exact same set of points as another boundary face. It
then splits the points to convert these faces into completely separate
boundary patches. This functionality was previously provided by calling
mergeOrSplitBaffles with the "-split" option.
mergeBaffles also identifes the duplicate baffle faces, but then merges
them, converting them into a single set of internal faces. This
functionality was previously provided by calling mergeOrSplitBaffles
without the "-split" option.
The fireFoam solver has solver has been replaced by the more general
buoyantReactingFoam solver, which supports buoyant compressible reacting flow
coupled to multiple run-time-selectable lagrangian clouds and surface film
modelling and optional hydrostatic initialisation of the pressure and p_rgh.
Hydrostatic initialisation of the pressure fields is useful for large fires in
open domains where the stability of the initial flow is dominated by the initial
pressure distribution in the domain and at the boundaries. The optional
hydrostaticInitialization switch in fvSolution/PIMPLE with
nHydrostaticCorrectors enables hydrostatic initialisation, e.g.
PIMPLE
{
momentumPredictor yes;
nOuterCorrectors 1;
nCorrectors 2;
nNonOrthogonalCorrectors 0;
hydrostaticInitialization yes;
nHydrostaticCorrectors 5;
}
and the resulting ph_rgh field can be used with the prghTotalHydrostaticPressure
p_rgh boundary condition to apply this hydrostatic pressure distribution at the
boundaries throughout the simulation.
See the following cases for examples transferred from fireFoam:
$FOAM_TUTORIALS/combustion/buoyantReactingFoam/RAS
