- Nov 18, 2017
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Now pimpleDyMFoam is exactly equivalent to pimpleFoam when running on a staticFvMesh. Also when the constant/dynamicMeshDict is not present a staticFvMesh is automatically constructed so that the pimpleDyMFoam solver can run any pimpleFoam case without change. pimpleDyMFoam: Store Uf as an autoPtr for better error handling pimpleFoam: Set initial deltaT from the Courant number for improved stability on start-up and compatibility with pimpleDyMFoam ENH: pimpleFoam: Merged dynamic mesh functionality of pimpleDyMFoam into pimpleFoam and replaced pimpleDyMFoam with a script which reports this change. The pimpleDyMFoam tutorials have been moved into the pimpleFoam directory. This change is the first of a set of developments to merge dynamic mesh functionality into the standard solvers to improve consistency, usability, flexibility and maintainability of these solvers. Henry G. Weller CFD Direct Ltd. tutorials/incompressible/pimpleFoam: Updated pimpleDyMFoam tutorials to run pimpleFoam Renamed tutorials/incompressible/pimpleFoam/RAS/wingMotion/wingMotion2D_pimpleDyMFoam -> tutorials/incompressible/pimpleFoam/RAS/wingMotion/wingMotion2D_pimpleFoam
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- Aug 18, 2017
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- Oct 10, 2017
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- May 10, 2018
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Andrew Heather authored
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- Sep 19, 2017
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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.
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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.
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- Oct 31, 2017
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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.
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- Dec 09, 2017
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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.
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- Nov 10, 2017
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Patch contributed by Mattijs Janssens Resolves bug-report https://bugs.openfoam.org/view.php?id=2744
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- Nov 07, 2017
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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.
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- Oct 27, 2017
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Patch contributed by Mattijs Janssens Resolves bug-report https://bugs.openfoam.org/view.php?id=2712
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- Oct 23, 2017
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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.
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- Oct 19, 2017
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by setting the optional switch YInfZero to true.
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- Oct 18, 2017
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in the limit of the phase fraction -> 0 Can be used with the Maxwell non-Newtonian laminar stress model when used in multiphase solvers.
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- Sep 04, 2017
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Patch contributed by Bruno Santos Resolves patch request https://bugs.openfoam.org/view.php?id=2684
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- Apr 04, 2018
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Andrew Heather authored
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- Jul 13, 2017
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for consistency with other rotating BCs.
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- Dec 14, 2017
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- Dec 15, 2017
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e.g. odeCoeffs { solver seulex; absTol 1e-12; relTol 0.0001; maxSteps 1e+06; } maxSteps defaults to 10000 for backward compatibility.
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- Dec 13, 2017
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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.
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- Dec 01, 2017
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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
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- Nov 29, 2017
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- Nov 22, 2017
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- Nov 16, 2017
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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
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- Nov 14, 2017
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Resolves bug-report https://bugs.openfoam.org/view.php?id=2758
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- Nov 09, 2017
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Patch contributed by Timo Niemi, VTT. Resolves patch request https://bugs.openfoam.org/view.php?id=2753 STYLE: TDACChemistryModel: Removed unnecessary warning messages Patch contributed by Francesco Contino
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- Nov 06, 2017
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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.
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- Nov 07, 2017
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Patch contributed by Björn Pfeiffelmann Resolves patch request https://bugs.openfoam.org/view.php?id=2713
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- Nov 02, 2017
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Resolves bug-report https://bugs.openfoam.org/view.php?id=2748
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- Oct 31, 2017
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- Oct 30, 2017
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ENH: compressibleInterPhaseTransportFoam: New variant of compressibleInterFoam supporting separate phase stress models 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.
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- Oct 27, 2017
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Resolves bug-report https://bugs.openfoam.org/view.php?id=2739
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- Oct 26, 2017
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Resolves bug-report https://bugs.openfoam.org/view.php?id=2740
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- Oct 20, 2017
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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.
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- Oct 19, 2017
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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.
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- Oct 18, 2017
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Patch contributed by Jakub Benda Resolves bug-report https://bugs.openfoam.org/view.php?id=2727
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- Oct 17, 2017
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which avoids the need for field interpolation and snGrad specification and evaluation. Resolves patch request https://bugs.openfoam.org/view.php?id=2725 wallHeatFlux: Filter out coupled patches Resolves bug-report https://bugs.openfoam.org/view.php?id=2776
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