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Alexander Jaust
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Alexander Kissinger
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- Aline Schäfer Rodrigues AlineSRS
- Anna Mareike Kostelecky anna_m_kostelecky
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Bernd Flemisch
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- Caroline Heckel CarolineHeckel
- Cedric Riethmüller CRieth
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Christoph Grüninger
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Cynthia Michalkowski
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David Werner
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- Felix Weinhardt felixw
- Feb 10, 2017
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* Current one is not compatible with staggerdGrid
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* Add ref solution * Add L2 error norm function
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* Use correct viscosity * Use correct yasp grid
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* Use new SourceValues, BoundaryValues * Test not working yet
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* Use new BoundaryValues class
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* Add reference solution * clean-up problem * rename input file
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* fix error (typo) in source-term * adapt to new interface
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*Add more indices, make easier to use
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*staggerd/problem.hh no longer required
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Not working yet!
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* isWall function now also works in 3D
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* Specializations for 2d and 3d not required anymore
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* Use correct codimensions for subIndex * Use correct number of subentities (i.e. vertices (2d) and edges (3)) * add missing break statements
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* remove offset * use common function
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* Make discretization test compile again
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* No longer needed
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* Get rid of fullFace stencils, not required anymore * Use new map in assembler and localJacobian
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* Replace setRowSizes_ and addIndices_ functions with occupationPattern concept
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* Allows usage of range-based for-loop
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* Make use of [] operator of staggeredPriVars class
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* Make base staggered discretization more general
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* Set fluxVars in model-specific propertyDefaults * Remove unused code from staggered VolVars
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* Move all flux calculations form localResidual to fluxVars * Move stencil computation from stencils to fluxVars FluxVars will 4 provide different specilizations: - single component, isothermal - single component, non-isothermal - multi component, isothermal - multi component, non-isothermal LocalResidual has to be adapted accordingly. Can be extended for turbulence models.
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* Can be accessed with regular priVar indices * In the problem, a helper type has to be used in order to specifiy the velocities as vectors
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*Greatly improves performance because only the local residual of the dof of interest gets calculated (not the whole element)
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* Cell dof and and individual face dofs can now be treated separately
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* Remove unused code * Use chached values of the residua for calculation of derivatives
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*Test may fail due to tiny velocity discrepancies (no flow involved in this test)
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* Stokes (Re=1) and Navier-Stokes (Re=1000) flow regimes
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* Affects normal advective momentum flux and pressure term
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