XiEngineFoam is a premixed/partially-premixed combustion engine solver which
exclusively uses the Xi flamelet combustion model.
engineFoam is a general engine solver for inhomogeneous combustion with or
without spray supporting run-time selection of the chemistry-based combustion
model.
Standard crank-connecting rod and the new free-piston kinematics motion options
are provides, others can easily be added.
Contributed by Francesco Contino and Nicolas Bourgeois, BURN Research Group.
The patch magSf calculation has been changed so that it uses the same
triangulation as the overlap algorithm. This improves consistency and
means that for exactly conforming patches (typically before any mesh
motion) the weights do not require normalisation.
Resolves bug-report https://bugs.openfoam.org/view.php?id=2785
ENH: compressibleInterFoam family: merged two-phase momentum stress modelling from compressibleInterPhaseTransportFoam
The new momentum stress model selector class
compressibleInterPhaseTransportModel is now used to select between the options:
Description
Transport model selection class for the compressibleInterFoam family of
solvers.
By default the standard mixture transport modelling approach is used in
which a single momentum stress model (laminar, non-Newtonian, LES or RAS) is
constructed for the mixture. However if the \c simulationType in
constant/turbulenceProperties is set to \c twoPhaseTransport the alternative
Euler-Euler two-phase transport modelling approach is used in which separate
stress models (laminar, non-Newtonian, LES or RAS) are instantiated for each
of the two phases allowing for different modeling for the phases.
Mixture and two-phase momentum stress modelling is now supported in
compressibleInterFoam, compressibleInterDyMFoam and compressibleInterFilmFoam.
The prototype compressibleInterPhaseTransportFoam solver is no longer needed and
has been removed.
Another exception has been added to globalIndexAndTransform to prevent
transformations being generated from coupled patch pairs marked with
coincident-full-match transformations. Foamy generates such patches, and
the faces on them at intermediate stages of meshing can be degenerate,
making the calculation of transformations unreliable. This change
enforces the definition that coincident-full-match patch pairs are not
transformed.
To unsure fvOptions are instantiated for post-processing createFvOptions.H must
be included in createFields.H rather than in the solver directly.
Resolves bug-report https://bugs.openfoam.org/view.php?id=2733
BUG: porousSimpleFoam: moved createFvOptions.H into createFields.H for -postProcess option
Resolves bug-report https://bugs.openfoam.org/view.php?id=2733
BUG: solvers: Moved fvOption construction into createFields.H for post-processing
This ensures that the fvOptions are constructed for the -postProcessing option
so that functionObjects which process fvOption data operate correctly in this
mode.
The absolute value of the the time has been added to the rigid body
model state. This value is not directly necessary for calculating the
evolution of the rigid body system, it just facilitates the
implementation of sub-models which are in some way time-dependent.
Mixture molecular weight is now evaluated in heThermo like everything
else, relying on the low level specie mixing rules. Units have also been
corrected.
SpecieMixture: Pure virtual definition for W to prevent Clang warning
to support the evaporation of the solvent from the wax film and the changes in
viscosity caused by the reduction in solvent content.
BUG: filmViscosityModel::thixotropicViscosity: Corrected sign of impingement rate
to compensate for rhoSp having the wrong sign
BUG: surfaceFilmModels::waxSolventEvaporation: Corrected handling of impingement
ENH: surfaceFilmModels::waxSolventViscosity: Changed mixing to mole-fraction based
ENH: surfaceFilmModels::thermoSingleLayer: Added call to solveContinuity before updateSubmodels
to allow sub-models to solve transport equations for conserved properties
In the event that matching centroids across a coupled patch pair fails,
we fall back to matching the face point average. The latter can be
obtained more reliably on degenerate faces as the calculation does not
involve division by the face area.
This fallback was already implemented as part of processorPolyPatch.
This change also applies it to the faceCoupleInfo class used by
reconstructParMesh.
In this version of compressibleInterFoam separate stress models (laminar,
non-Newtonian, LES or RAS) are instantiated for each of the two phases allowing
for completely different modeling for the phases.
e.g. in the climbingRod tutorial case provided a Newtonian laminar model is
instantiated for the air and a Maxwell non-Newtonian model is instantiated for
the viscoelastic liquid. To stabilize the Maxwell model in regions where the
liquid phase-fraction is 0 the new symmTensorPhaseLimitStabilization fvOption is
applied.
Other phase stress modeling combinations are also possible, e.g. the air may be
turbulent but the liquid laminar and an RAS or LES model applied to the air
only. However, to stabilize this combination a suitable fvOption would need to
be applied to the turbulence properties where the air phase-fraction is 0.
Henry G. Weller, Chris Greenshields
CFD Direct Ltd.
The restraints generate either joint-local (tau) or global (fx) forces.
At the moment they all generate the latter. This change corrects three
of the four restraints so that the forces are in the gobal coordinate
system and not the local coordinate system of the body.
The problem with this is that the forward dynamics code then transforms
most of the forces back to the body local coordinate system. A better
solution would be to associate restraints which are more sensibly
defined in a local frame with the joints instead of the bodies, and
return the forces as part of the tau variable.
Two boundary conditions for the modelling of semi-permeable baffles have
been added. These baffles are permeable to a number of species within
the flow, and are impermeable to others. The flux of a given species is
calculated as a constant multipled by the drop in mass fraction across
the baffle.
The species mass-fraction condition requires the transfer constant and
the name of the patch on the other side of the baffle:
boundaryField
{
// ...
membraneA
{
type semiPermeableBaffleMassFraction;
samplePatch membranePipe;
c 0.1;
value uniform 0;
}
membraneB
{
type semiPermeableBaffleMassFraction;
samplePatch membraneSleeve;
c 0.1;
value uniform 1;
}
}
If the value of c is omitted, or set to zero, then the patch is
considered impermeable to the species in question. The samplePatch entry
can also be omitted in this case.
The velocity condition does not require any special input:
boundaryField
{
// ...
membraneA
{
type semiPermeableBaffleVelocity;
value uniform (0 0 0);
}
membraneB
{
type semiPermeableBaffleVelocity;
value uniform (0 0 0);
}
}
These two boundary conditions must be used in conjunction, and the
mass-fraction condition must be applied to all species in the
simulation. The calculation will fail with an error message if either is
used in isolation.
A tutorial, combustion/reactingFoam/RAS/membrane, has been added which
demonstrates this transfer process.
This work was done with support from Stefan Lipp, at BASF.
To disable face correspondence checking set
checkFaceCorrespondence off;
in blockMeshDict. This is necessary in the rare cases where adjacent block
faces do not need to correspond because they are geometrically collapsed,
e.g. to form a pole/axis.
Resolves bug-report https://bugs.openfoam.org/view.php?id=2711
ENH: foamyHexMesh: Made default region volume type that of it's parent
Foamy surface conformation entries have a "meshableSide" entry which
controls which side of the surface is to be meshed. Typically this is
set "inside" for boundaries and "both" for baffles. A sub-region's
default entry is now taken from it's parent, rather than a specific
value (it was "inside"). This is consistent with how other entries are
handled.
surfaceConformation
{
locationInMesh (0 0 0);
geometryToConformTo
{
baffle
{
featureMethod extractFeatures;
includedAngle 120;
meshableSide both; // <-- per-surface setting
regions
{
disk
{
meshableSide both; // <-- per-region setting*
// *in this example, this entry is not needed, as it
// is taken from the per-surface setting above
}
}
}
// ...
}
}
ENH: foamyHexMesh: Added (reinstated) baffle patches
A patch can now be assigned to a baffle surface. This assignment will
take precedence over any face-zones.
surfaceConformation
{
locationInMesh (0 0 0);
geometryToConformTo
{
disk
{
featureMethod extractFeatures;
includedAngle 120;
meshableSide both; // <-- baffle
patchInfo
{
type wall;
inGroups (walls);
}
}
// ...
}
}
STYLE: foamyHexMesh: Switched off output of all the secondary meshes
The integration of force and heat transfer onto the particle is
facilitated by a run-time-selectable integration scheme. These schemes
were written to generate the value at the end of an intregration step
and also an average value over the step from which the total transfer
was computed.
The average value in the Euler scheme was implemented incorrectly, which
resulted in the momentum and heat transfer processes being
non-conservative. Implementing the average correctly, however, would
have inteoduced a number of trancendental functions which would have
negated the purpose of the Euler scheme as the cheap and stable option.
The schemes have been rewritten to generate changes over the step,
rather than the final value. This change is then used to calculate the
transfers. Regardless of the scheme, this formulation is guaranteed to
be conservative, and the Euler scheme remains computationally
inexpensive.
This change was made with help from Timo Niemi, VTT
This resolves bug report https://bugs.openfoam.org/view.php?id=2666
ENH: integrationSchemes: Further simplification and optimisation
Removed templating from integration schemes, improved the name
convention, and optimised the utilisation so that the virtual call is
only made once per integration in the KinematicParcel and the
ThermoParcel.
BUG: integrationSchemes: Corrections to coupled/non-coupled force splitting
The integration splitting implemented in commit a5806207 has been shown
to be incorrect in some cases. A new procedure has been implemented
which can correctly split the implicit-explicit integral into a number
of pieces, in order to calculate the contribution of each. This is
intended for integrating coupled and non-coupled particle momentum and
heat transfers.
However, currently there is only ever one implicit coefficient used in
these transfers (there is no implicit non-coupled contribution). The
evaluation has therefore been short-cutted to only do the integration
with respect to the coupled contributions. The splitting functionality
has been retained in case additional separate implicit coefficients are
required in the future.
This change was made with help from Timo Niemi, VTT
This resolves bug report https://bugs.openfoam.org/view.php?id=2666
