angleUnits is a more logical name for the user-input as it specifies the units
of the angles written rather than the format of the numbers. The previous name
angleFormat is supported for backwards-compatibility
Class
Foam::functionObjects::rigidBodyState
Description
Writes the rigid body motion state.
Usage
\table
Property | Description | Required | Default value
type | type name: rigidBodyState | yes |
angleUnits | degrees or radians | no | radians
\endtable
Example of function object specification:
\verbatim
rigidBodyState
{
type rigidBodyState;
libs ("librigidBodyState.so");
angleUnits degrees;
}
\endverbatim
Class
Foam::functionObjects::sixDoFRigidBodyState
Description
Writes the 6-DoF motion state.
Example of function object specification:
\verbatim
sixDoFRigidBodyState
{
type sixDoFRigidBodyState;
libs ("libsixDoFRigidBodyState.so");
angleUnits degrees;
}
\endverbatim
Usage
\table
Property | Description | Required | Default value
type | type name: sixDoFRigidBodyState | yes |
angleUnits | degrees or radians | no | radian
\endtable
The cavitation models used by the interFoam solver and the
compressibleVoF solver module can now be applied regardless of the
ordering of the liquid and vapour phases. A "liquid" keyword is now
required in the model specification in order to control which phase is
considered to be the condensed liquid state. Previously the liquid phase
was assumed to be the first of the two phases.
No advantage was found in the specific snappyHexMesh settings previously
specified for this case. This case now uses settings from the standard
snappyHexMesh.cfg file.
The rotating region has also been modified to align better with the
original block mesh. For sliding interface problems this is important in
order to reliably get good conformance to the cylinder edges.
The thermodynamic density field is now named "rho" by default and only renamed
"thermo:rho" by solvers that create and maintain a separate continuity density
field which is named "rho". This change significantly simplifies and
standardises the specification of schemes and boundary conditions requiring
density as it is now always named "rho" or "rho.<phase>" unless under some very
unusual circumstances the thermodynamic rather than continuity density is
required for a solver maintaining both.
The advantage of this change is particularly noticeable for multiphase
simulations in which each phase has its own density now named "rho.<phase>"
rather than "thermo:rho.<phase>" as separate phase continuity density fields are
not required so for multiphaseEulerFoam the scheme specification:
"div\(alphaRhoPhi.*,\(p\|thermo:rho.*\)\)" Gauss limitedLinear 1;
is now written:
"div\(alphaRhoPhi.*,\(p\|rho.*\)\)" Gauss limitedLinear 1;
Replacing the specific twoPhaseChangeModel with a consistent and general fvModel
interface will support not just cavitation using the new VoFCavitation fvModel
but also other phase-change and interface manipulation models in the future and
is easier to use for case-specific and other user customisation.
Description
General cell set selection class for models that apply to sub-sets
of the mesh.
Currently supports cell selection from a set of points, a specified cellSet
or cellZone or all of the cells. The selection method can either be
specified explicitly using the \c selectionMode entry or inferred from the
presence of either a \c cellSet, \c cellZone or \c points entry. The \c
selectionMode entry is required to select \c all cells.
Usage
Examples:
\verbatim
// Apply everywhere
selectionMode all;
// Apply within a given cellSet
selectionMode cellSet; // Optional
cellSet rotor;
// Apply within a given cellZone
selectionMode cellZone; // Optional
cellSet rotor;
// Apply in cells containing a list of points
selectionMode points; // Optional
points
(
(2.25 0.5 0)
(2.75 0.5 0)
);
\endverbatim
All tutorials updated and simplified.
Description
User convenience class to handle the input of time-varying rotational speed
in rad/s if \c omega is specified or rpm if \c rpm is specified.
Usage
For specifying the rotational speed in rpm of an MRF zone:
\verbatim
MRF
{
cellZone rotor;
origin (0 0 0);
axis (0 0 1);
rpm 60;
}
\endverbatim
or the equivalent specified in rad/s:
\verbatim
MRF
{
cellZone rotor;
origin (0 0 0);
axis (0 0 1);
rpm 6.28319;
}
\endverbatim
or for a tabulated ramped rotational speed of a solid body:
\verbatim
mover
{
type motionSolver;
libs ("libfvMeshMovers.so" "libfvMotionSolvers.so");
motionSolver solidBody;
cellZone innerCylinder;
solidBodyMotionFunction rotatingMotion;
origin (0 0 0);
axis (0 1 0);
rpm table
(
(0 0)
(0.01 6000)
(0.022 6000)
(0.03 4000)
(100 4000)
);
}
\endverbatim
The following classes have been updated to use the new Function1s::omega class:
solidBodyMotionFunctions::rotatingMotion
MRFZone
rotatingPressureInletOutletVelocityFvPatchVectorField
rotatingTotalPressureFvPatchScalarField
rotatingWallVelocityFvPatchVectorField
and all tutorials using these models and BCs updated to use rpm where appropriate.
The cellProc field is the field of cell-processor labels.
The names "distribution" and "dist" have been removed as these are
ambiguous in relation to other forms of distribution and to distance.
This utility now always creates two patches, and only creates duplicate
faces when they connect to different cells and point in opposite
directions. Now that ACMI has been removed, there is no need to create
duplicate faces on the same cell and with similar orientations. This is
unituitive and is now considered an invalid mesh topology.
The preferred syntax for createBaffles is now as follows:
internalFacesOnly true;
baffles
{
cyclics
{
type faceZone;
zoneName cyclicFaces;
owner
{
name cyclicLeft;
type cyclic;
neighbourPatch cyclicRight;
}
neighbour
{
name cyclicRight;
type cyclic;
neighbourPatch cyclicLeft;
}
}
}
Note that the 'patches' sub-dictionary is not needed any more; the
'owner' and 'neighbour' sub-dictionaries can be in the same dictionary
as the parameters with which faces are selected. For backwards
compatibility, however, a 'patches' sub-dictionary is still permitted,
as are keywords 'master' and 'slave' (in place of 'owner' and
'neighbour', respectively).
The 'patchPairs' syntax has been removed. Whilst consise, this syntax
made a number of assumptions and decisions regarding naming conventions
that were not sufficiently intuitive for the user to understand without
extensive reference to the code. If identical boundaries are desired on
both sides of the patch, dictionary substitution provides a more
intuitive way of minimising the amount of specifiection required. For
example, to create two back-to-back walls, the following specification
could be used:
internalFacesOnly true;
fields true;
baffles
{
walls
{
type faceZone;
zoneName wallFaces;
owner
{
name baffleWallLeft;
type wall;
patchFields
{
p
{
type zeroGradient;
}
U
{
type noSlip;
}
}
}
neighbour
{
name baffleWallRight;
$owner; // <-- Use the same settings as for the owner
}
}
}
The following examples in the tutorials ($FOAM_TUTORIALS) directory have
been converted from using AMI to the new NCC system:
+ compressible/rhoPimpleFoam/RAS/annularThermalMixer
+ incompressible/pimpleFoam/RAS/propeller
+ lagrangian/particleFoam/mixerVessel2D (formerly mixerVesselAMI2D)
+ multiphase/interFoam/RAS/mixerVessel
+ multiphase/interFoam/RAS/propeller
+ multiphase/multiphaseEulerFoam/laminar/mixerVessel2D (formerly mixerVesselAMI2D)
The following tutorial has been converted from using ACMI:
+ incompressible/pimpleFoam/RAS/oscillatingInlet
The following tutorial has been converted from using Repeat AMI:
+ incompressible/pimpleFoam/RAS/impeller
The following tutorial has been added to demonstrate NCC's ability to
create a sufficiently conservative solution in a closed domain to
maintain phase fraction boundedness:
+ multiphase/interFoam/laminar/mixerVessel2D
The following tutorials have been added to demonstrate NCC's ability to
simulate partially overlapping couples on curved surfaces:
+ incompressible/pimpleFoam/RAS/ballValve
+ multiphase/compressibleInterFoam/RAS/ballValve
The following tutorial has been added to provide a simple comparison of
the conservation behaviour of AMI and NCC:
+ incompressible/pimpleFoam/laminar/nonConformalChannel
The following tutorial has been removed, as there were sufficiently many
examples involving this geometry:
+ incompressible/pimpleFoam/laminar/mixerVesselAMI2D
On unstructured collocated meshes the Reynolds stress tends to decouple from the
velocity creating pronounced staggering patterns in the solution. This effect
is reduced or eliminated by a special coupling algorithm which replaces the
gradient diffusion component of the Reynolds stress with the equivalent compact
representation on the mesh, i.e. div-grad with Laplacian in the DivDevRhoReff function:
template<class BasicMomentumTransportModel>
template<class RhoFieldType>
Foam::tmp<Foam::fvVectorMatrix>
Foam::ReynoldsStress<BasicMomentumTransportModel>::DivDevRhoReff
(
const RhoFieldType& rho,
volVectorField& U
) const
{
tmp<volTensorField> tgradU = fvc::grad(U);
const volTensorField& gradU = tgradU();
const surfaceTensorField gradUf(fvc::interpolate(gradU));
// Interpolate Reynolds stress to the faces
// with either a stress or velocity coupling correction
const surfaceVectorField Refff
(
(this->mesh().Sf() & fvc::interpolate(R_))
// Stress coupling
+ couplingFactor_
*(this->mesh().Sf() & fvc::interpolate(this->nut()*gradU))
// or velocity gradient coupling
// + couplingFactor_
// *fvc::interpolate(this->nut())*(this->mesh().Sf() & gradUf)
- fvc::interpolate(couplingFactor_*this->nut() + this->nu())
*this->mesh().magSf()*fvc::snGrad(U)
- fvc::interpolate(this->nu())*(this->mesh().Sf() & dev2(gradUf.T()))
);
return
(
fvc::div(fvc::interpolate(this->alpha_*rho)*Refff)
- correction(fvm::laplacian(this->alpha_*rho*this->nuEff(), U))
);
}
In the above two options for the coupling term are provided, one based on the
stress correction (un-commented) and an alternative based an the velocity
gradient correction (commented). Tests run so far indicate that the stress
correction provides better coupling while minimising the error introduced.
A new tutorial case ductSecondaryFlow is provided which demonstrates the updated
coupling algorithm on the simulation of the classic secondary flow generated in
rectangular ducts.
It is not clear for what cases the minVol control is useful or necessary and for
some cases it causes problems with snapping and layer addition if not set to a
sufficiently small value.
The defaultPatch type currently defaults to empty which is appropriate for 1D
and 2D cases but not when creating the initial blockMesh for snappyHexMesh as
the presence of empty patches triggers the inappropriate application of 2D point
constraint corrections following snapping and morphing. To avoid this hidden
problem a warning is now generated from blockMesh when the defaultPatch is not
explicitly set for cases which generate a default patch, i.e. for which the
boundary is not entirely defined. e.g.
.
.
.
Creating block mesh topology
--> FOAM FATAL IO ERROR:
The 'defaultPatch' type must be specified for the 'defaultFaces' patch, e.g. for snappyHexMesh
defaultPatch
{
name default; // optional
type patch;
}
or for 2D meshes
defaultPatch
{
name frontAndBack; // optional
type empty;
}
.
.
.
All the tutorials have been update to include the defaultPatch specification as
appropriate.
motionSmootherAlgoCheck::checkMesh is used by snappyHexMesh to check the mesh
after snapping and morphing. The minVol test which checks for collapsed cells
is now relative to the cube of the minimum bounding box length so that it is
less dependent on the size of the geometry and less likely to need changing for
very small geometries.
The default value is set in
etc/caseDicts/mesh/generation/meshQualityDict
etc/caseDicts/mesh/generation/meshQualityDict.cfg
//- Minimum cell pyramid volume relative to min bounding box length^3
// Set to a fraction of the smallest cell volume expected.
// Set to very negative number (e.g. -1e30) to disable.
minVol 1e-10;
The unused minArea and minTriangleTwist tests have been removed
For most multiphase flows it is more appropriate to evaluate the total pressure
from the static pressure obtained from p_rgh rather than from p_rgh directly.
The unreliable extrapolateProfile option has been replaced by the more flexible
and reliable profile option which allows the velocity profile to be specified as
a Function1 of the normalised distance to the wall. To simplify the
specification of the most common velocity profiles the new laminarBL (quadratic
profile) and turbulentBL (1/7th power law) Function1s are provided.
In addition to the new profile option the flow rate can now be specified as a
meanVelocity, volumetricFlowRate or massFlowRate, all of which are Function1s of
time.
The following tutorials have been updated to use the laminarBL profile:
multiphase/multiphaseEulerFoam/laminar/titaniaSynthesis
multiphase/multiphaseEulerFoam/laminar/titaniaSynthesisSurface
The following tutorials have been updated to use the turbulentBL profile:
combustion/reactingFoam/Lagrangian/verticalChannel
combustion/reactingFoam/Lagrangian/verticalChannelLTS
combustion/reactingFoam/Lagrangian/verticalChannelSteady
compressible/rhoPimpleFoam/RAS/angledDuct
compressible/rhoPimpleFoam/RAS/angledDuctLTS
compressible/rhoPimpleFoam/RAS/squareBendLiq
compressible/rhoPorousSimpleFoam/angledDuctImplicit
compressible/rhoSimpleFoam/angledDuctExplicitFixedCoeff
compressible/rhoSimpleFoam/squareBend
compressible/rhoSimpleFoam/squareBendLiq
heatTransfer/chtMultiRegionFoam/shellAndTubeHeatExchanger
heatTransfer/chtMultiRegionFoam/shellAndTubeHeatExchanger
incompressible/porousSimpleFoam/angledDuctImplicit
incompressible/porousSimpleFoam/straightDuctImplicit
multiphase/interFoam/RAS/angledDuct
Class
Foam::flowRateInletVelocityFvPatchVectorField
Description
Velocity inlet boundary condition creating a velocity field with
optionally specified profile normal to the patch adjusted to match the
specified mass flow rate, volumetric flow rate or mean velocity.
For a mass-based flux:
- the flow rate should be provided in kg/s
- if \c rho is "none" the flow rate is in m3/s
- otherwise \c rho should correspond to the name of the density field
- if the density field cannot be found in the database, the user must
specify the inlet density using the \c rhoInlet entry
For a volumetric-based flux:
- the flow rate is in m3/s
Usage
\table
Property | Description | Required | Default value
massFlowRate | Mass flow rate [kg/s] | no |
volumetricFlowRate | Volumetric flow rate [m^3/s]| no |
meanVelocity | Mean velocity [m/s]| no |
profile | Velocity profile | no |
rho | Density field name | no | rho
rhoInlet | Inlet density | no |
alpha | Volume fraction field name | no |
\endtable
Example of the boundary condition specification for a volumetric flow rate:
\verbatim
<patchName>
{
type flowRateInletVelocity;
volumetricFlowRate 0.2;
profile laminarBL;
}
\endverbatim
Example of the boundary condition specification for a mass flow rate:
\verbatim
<patchName>
{
type flowRateInletVelocity;
massFlowRate 0.2;
profile turbulentBL;
rho rho;
rhoInlet 1.0;
}
\endverbatim
Example of the boundary condition specification for a volumetric flow rate:
\verbatim
<patchName>
{
type flowRateInletVelocity;
meanVelocity 5;
profile turbulentBL;
}
\endverbatim
The \c volumetricFlowRate, \c massFlowRate or \c meanVelocity entries are
\c Function1 of time, see Foam::Function1s.
The \c profile entry is a \c Function1 of the normalised distance to the
wall. Any suitable Foam::Function1s can be used including
Foam::Function1s::codedFunction1 but Foam::Function1s::laminarBL and
Foam::Function1s::turbulentBL have been created specifically for this
purpose and are likely to be appropriate for most cases.
Note
- \c rhoInlet is required for the case of a mass flow rate, where the
density field is not available at start-up
- The value is positive into the domain (as an inlet)
- May not work correctly for transonic inlets
- Strange behaviour with potentialFoam since the U equation is not solved
See also
Foam::fixedValueFvPatchField
Foam::Function1s::laminarBL
Foam::Function1s::turbulentBL
Foam::Function1s
Foam::flowRateOutletVelocityFvPatchVectorField
Zoltan only work in parallel so zoltanDecomp can only be used for redistribution
but is much more flexible than ptscotch and provides a range of geometric, graph
and hypergraph methods which can operate in either "partition" or "repartition",
the latter being particularly useful for dynamic load-balancing by migrating
cells between processors rather than creating a completely different
decomposition, thus reducing communication.
Class
Foam::zoltanDecomp
Description
Zoltan redistribution in parallel
Note: Zoltan methods do not support serial operation.
Parameters
- lb_method : The load-balancing algorithm
- block : block partitioning
- random : random partitioning
- rcb : recursive coordinate bisection
- rib : ecursive inertial bisection
- hsfc : Hilbert space-filling curve partitioning
- reftree : refinement tree based partitioning
- graph : choose from collection of methods for graphs
- hypergraph : choose from a collection of methods for hypergraphs
- lb_approach The desired load balancing approach. Only lb_method =
hypergraph or graph uses the lb_approach parameter. Valid values are
- partition : Partition without reference to the current distribution,
recommended for static load balancing.
- repartition : Partition starting from the current data distribution
to keep data migration low, recommended for dynamic load balancing.
- refine : Quickly improve the current data distribution
Default values
- debug_level 0
- imbalance_tol 1.05
- lb_method graph
- lb_approach repartition
Usage
To select the Zoltan graph repartition method add the following entries to
decomposeParDict:
distributor zoltan;
libs ("libzoltanRenumber.so");
The Zoltan lb_method and lb_approach can be changed by adding the
corresponding entries to the optional zoltanCeoffs sub-dictionary, e.g.:
zoltanCoeffs
{
lb_method hypergraph;
lb_approach partition;
}
An example of using Zoltan for redistribution during snappyHexMesh is provided
commented out in
tutorials/incompressible/simpleFoam/motorBike/system/decomposeParDict
and fordynamic load-balancing in
tutorials/multiphase/interFoam/RAS/floatingObject/system/decomposeParDict.
Note that Zoltan must first be compiled in ThirdParty-dev by downloading from
the link in the README file and running Allwmake and then compiling zoltanDecomp
by running Allwmake in src/parallel/decompose.
When snappyHexMesh is run in parallel it re-balances the mesh during refinement
and layer addition by redistribution which requires a decomposition method
that operates in parallel, e.g. hierachical or ptscotch. decomposePar uses a
decomposition method which operates in serial e.g. hierachical but NOT
ptscotch. In order to run decomposePar followed by snappyHexMesh in parallel it
has been necessary to change the method specified in decomposeParDict but now
this is avoided by separately specifying the decomposition and distribution
methods, e.g. in the incompressible/simpleFoam/motorBike case:
numberOfSubdomains 6;
decomposer hierarchical;
distributor ptscotch;
hierarchicalCoeffs
{
n (3 2 1);
order xyz;
}
The distributor entry is also used for run-time mesh redistribution, e.g. in the
multiphase/interFoam/RAS/floatingObject case re-distribution for load-balancing
is enabled in constant/dynamicMeshDict:
distributor
{
type distributor;
libs ("libfvMeshDistributors.so");
redistributionInterval 10;
}
which uses the distributor specified in system/decomposeParDict:
distributor hierarchical;
This rationalisation provides the structure for development of mesh
redistribution and load-balancing.
Basic support is now provided for dynamic mesh redistribution, particularly for
load-balancing. The mesh distributor is selected in the optional 'distributor'
entry in dynamicMeshDict, for example in the
multiphase/interFoam/RAS/floatingObject tutorial case when run in parallel using
the new Allrun-parallel script
distributor
{
type decomposer;
libs ("libfvMeshDistributors.so");
redistributionInterval 10;
}
in which the 'decomposer' form of redistribution is selected to call the mesh
decomposition method specified in decomposeParDict to re-decompose the mesh for
redistribution. The redistributionInterval entry specifies how frequently mesh
redistribution takes place, in the above every 10th time-step. An optional
maxImbalance entry is also provided to control redistribution based on the cell
distribution imbalance:
Class
Foam::fvMeshDistributor::decomposer
Description
Dynamic mesh redistribution using the decomposer
Usage
Example of single field based refinement in all cells:
\verbatim
distributor
{
type decomposer;
libs ("libfvMeshDistributors.so");
// How often to redistribute
redistributionInterval 10;
// Maximum fractional cell distribution imbalance
// before rebalancing
maxImbalance 0.1;
}
\endverbatim
Currently mesh refinement/unrefinement and motion with redistribution is
supported but many aspects of OpenFOAM are not yet and will require further
development, in particular fvModels and Lagrangian.
Also only the geometry-based simple and hierarchical decomposition method are
well behaved for redistribution, scotch and ptScotch cause dramatic changes in
mesh distribution with a corresponding heavy communications overhead limiting
their usefulness or at least the frequency with which they should be called to
redistribute the mesh.
The surfaceVectorField Uf is used instead of the flux field phi for ddtPhiCorr
in moving mesh cases to handle linear and rotating motion and must mapped from
the volVectorField U to new faces created by cell splitting or merging in mesh
refinement/unrefinement.
The floatingObject tutorial has been update to demonstrate this functionality by
adding the following topoChanger entry to dynamicMeshDict:
topoChanger
{
type refiner;
libs ("libfvMeshTopoChangers.so");
// How often to refine
refineInterval 1;
// Field to be refinement on
field alpha.water;
// Refine field in between lower..upper
lowerRefineLevel 0.001;
upperRefineLevel 0.999;
// Have slower than 2:1 refinement
nBufferLayers 1;
// Refine cells only up to maxRefinement levels
maxRefinement 1;
// Stop refinement if maxCells reached
maxCells 200000;
// Flux field and corresponding velocity field. Fluxes on changed
// faces get recalculated by interpolating the velocity. Use 'none'
// on surfaceScalarFields that do not need to be reinterpolated.
correctFluxes
(
(phi none)
(nHatf none)
(rhoPhi none)
(alphaPhi.water none)
(meshPhi none)
(ghf none)
);
// Write the refinement level as a volScalarField
dumpLevel true;
}
Note that currently only single rigid body motion is supported (but multi-body
support will be added shortly) and the Crank-Nicolson scheme is not supported.
Mesh motion and topology change are now combinable run-time selectable options
within fvMesh, replacing the restrictive dynamicFvMesh which supported only
motion OR topology change.
All solvers which instantiated a dynamicFvMesh now instantiate an fvMesh which
reads the optional constant/dynamicFvMeshDict to construct an fvMeshMover and/or
an fvMeshTopoChanger. These two are specified within the optional mover and
topoChanger sub-dictionaries of dynamicFvMeshDict.
When the fvMesh is updated the fvMeshTopoChanger is first executed which can
change the mesh topology in anyway, adding or removing points as required, for
example for automatic mesh refinement/unrefinement, and all registered fields
are mapped onto the updated mesh. The fvMeshMover is then executed which moved
the points only and calculates the cell volume change and corresponding
mesh-fluxes for conservative moving mesh transport. If multiple topological
changes or movements are required these would be combined into special
fvMeshMovers and fvMeshTopoChangers which handle the processing of a list of
changes, e.g. solidBodyMotionFunctions:multiMotion.
The tutorials/multiphase/interFoam/laminar/sloshingTank3D3DoF case has been
updated to demonstrate this new functionality by combining solid-body motion
with mesh refinement/unrefinement:
/*--------------------------------*- C++ -*----------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration | Website: https://openfoam.org
\\ / A nd | Version: dev
\\/ M anipulation |
\*---------------------------------------------------------------------------*/
FoamFile
{
format ascii;
class dictionary;
location "constant";
object dynamicMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
mover
{
type motionSolver;
libs ("libfvMeshMovers.so" "libfvMotionSolvers.so");
motionSolver solidBody;
solidBodyMotionFunction SDA;
CofG (0 0 0);
lamda 50;
rollAmax 0.2;
rollAmin 0.1;
heaveA 4;
swayA 2.4;
Q 2;
Tp 14;
Tpn 12;
dTi 0.06;
dTp -0.001;
}
topoChanger
{
type refiner;
libs ("libfvMeshTopoChangers.so");
// How often to refine
refineInterval 1;
// Field to be refinement on
field alpha.water;
// Refine field in between lower..upper
lowerRefineLevel 0.001;
upperRefineLevel 0.999;
// Have slower than 2:1 refinement
nBufferLayers 1;
// Refine cells only up to maxRefinement levels
maxRefinement 1;
// Stop refinement if maxCells reached
maxCells 200000;
// Flux field and corresponding velocity field. Fluxes on changed
// faces get recalculated by interpolating the velocity. Use 'none'
// on surfaceScalarFields that do not need to be reinterpolated.
correctFluxes
(
(phi none)
(nHatf none)
(rhoPhi none)
(alphaPhi.water none)
(meshPhi none)
(meshPhi_0 none)
(ghf none)
);
// Write the refinement level as a volScalarField
dumpLevel true;
}
// ************************************************************************* //
Note that currently this is the only working combination of mesh-motion with
topology change within the new framework and further development is required to
update the set of topology changers so that topology changes with mapping are
separated from the mesh-motion so that they can be combined with any of the
other movements or topology changes in any manner.
All of the solvers and tutorials have been updated to use the new form of
dynamicMeshDict but backward-compatibility was not practical due to the complete
reorganisation of the mesh change structure.
for consistency with the regionToCell topo set source and splitMeshRegions and
provides more logical extension to the multiple and outside point variants insidePoints,
outsidePoint and outsidePoints.
The mesh in the upstream region of this case has been refined back to
its original density. This restores the wave propagation behaviour
through this region.
to provide a single consistent code and user interface to the specification of
physical properties in both single-phase and multi-phase solvers. This redesign
simplifies usage and reduces code duplication in run-time selectable solver
options such as 'functionObjects' and 'fvModels'.
* physicalProperties
Single abstract base-class for all fluid and solid physical property classes.
Physical properties for a single fluid or solid within a region are now read
from the 'constant/<region>/physicalProperties' dictionary.
Physical properties for a phase fluid or solid within a region are now read
from the 'constant/<region>/physicalProperties.<phase>' dictionary.
This replaces the previous inconsistent naming convention of
'transportProperties' for incompressible solvers and
'thermophysicalProperties' for compressible solvers.
Backward-compatibility is provided by the solvers reading
'thermophysicalProperties' or 'transportProperties' if the
'physicalProperties' dictionary does not exist.
* phaseProperties
All multi-phase solvers (VoF and Euler-Euler) now read the list of phases and
interfacial models and coefficients from the
'constant/<region>/phaseProperties' dictionary.
Backward-compatibility is provided by the solvers reading
'thermophysicalProperties' or 'transportProperties' if the 'phaseProperties'
dictionary does not exist. For incompressible VoF solvers the
'transportProperties' is automatically upgraded to 'phaseProperties' and the
two 'physicalProperties.<phase>' dictionary for the phase properties.
* viscosity
Abstract base-class (interface) for all fluids.
Having a single interface for the viscosity of all types of fluids facilitated
a substantial simplification of the 'momentumTransport' library, avoiding the
need for a layer of templating and providing total consistency between
incompressible/compressible and single-phase/multi-phase laminar, RAS and LES
momentum transport models. This allows the generalised Newtonian viscosity
models to be used in the same form within laminar as well as RAS and LES
momentum transport closures in any solver. Strain-rate dependent viscosity
modelling is particularly useful with low-Reynolds number turbulence closures
for non-Newtonian fluids where the effect of bulk shear near the walls on the
viscosity is a dominant effect. Within this framework it would also be
possible to implement generalised Newtonian models dependent on turbulent as
well as mean strain-rate if suitable model formulations are available.
* visosityModel
Run-time selectable Newtonian viscosity model for incompressible fluids
providing the 'viscosity' interface for 'momentumTransport' models.
Currently a 'constant' Newtonian viscosity model is provided but the structure
supports more complex functions of time, space and fields registered to the
region database.
Strain-rate dependent non-Newtonian viscosity models have been removed from
this level and handled in a more general way within the 'momentumTransport'
library, see section 'viscosity' above.
The 'constant' viscosity model is selected in the 'physicalProperties'
dictionary by
viscosityModel constant;
which is equivalent to the previous entry in the 'transportProperties'
dictionary
transportModel Newtonian;
but backward-compatibility is provided for both the keyword and model
type.
* thermophysicalModels
To avoid propagating the unnecessary constructors from 'dictionary' into the
new 'physicalProperties' abstract base-class this entire structure has been
removed from the 'thermophysicalModels' library. The only use for this
constructor was in 'thermalBaffle' which now reads the 'physicalProperties'
dictionary from the baffle region directory which is far simpler and more
consistent and significantly reduces the amount of constructor code in the
'thermophysicalModels' library.
* compressibleInterFoam
The creation of the 'viscosity' interface for the 'momentumTransport' models
allows the complex 'twoPhaseMixtureThermo' derived from 'rhoThermo' to be
replaced with the much simpler 'compressibleTwoPhaseMixture' derived from the
'viscosity' interface, avoiding the myriad of unused thermodynamic functions
required by 'rhoThermo' to be defined for the mixture.
Same for 'compressibleMultiphaseMixture' in 'compressibleMultiphaseInterFoam'.
This is a significant improvement in code and input consistency, simplifying
maintenance and further development as well as enhancing usability.
Henry G. Weller
CFD Direct Ltd.
and only needed if there is a name clash between entries in the source
specification and the set specification, e.g. "name":
{
name rotorCells;
type cellSet;
action new;
source zoneToCell;
sourceInfo
{
name cylinder;
}
}
With this change both
blockMesh -dict fineBlockMeshDict
blockMesh -dict system/fineBlockMeshDict
are supported, if the system/ path is not specified it is assumed
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.
When using 'simple' or 'hierarchical' decomposition it is useful to slightly rotate a
coordinate-aligned block-mesh to improve the processor boundaries by avoiding
irregular cell distribution at those boundaries. The degree of slight rotation
is controlled by the 'delta' coefficient and a value of 0.001 is generally
suitable so to avoid unnecessary clutter in 'decomposeParDict' 'delta' now
defaults to this value.
The FOAM file format has not changed from version 2.0 in many years and so there
is no longer a need for the 'version' entry in the FoamFile header to be
required and to reduce unnecessary clutter it is now optional, defaulting to the
current file format 2.0.
