- Feb 10, 2017
-
-
* Current one is not compatible with staggerdGrid
-
-
* Add ref solution * Add L2 error norm function
-
-
-
* Use correct viscosity * Use correct yasp grid
-
* Use new SourceValues, BoundaryValues * Test not working yet
-
* Use new BoundaryValues class
-
* Add reference solution * clean-up problem * rename input file
-
* fix error (typo) in source-term * adapt to new interface
-
-
*Add more indices, make easier to use
-
*staggerd/problem.hh no longer required
-
Not working yet!
-
* isWall function now also works in 3D
-
* Specializations for 2d and 3d not required anymore
-
* Use correct codimensions for subIndex * Use correct number of subentities (i.e. vertices (2d) and edges (3)) * add missing break statements
-
-
-
* remove offset * use common function
-
* Make discretization test compile again
-
-
* No longer needed
-
* Get rid of fullFace stencils, not required anymore * Use new map in assembler and localJacobian
-
-
* Replace setRowSizes_ and addIndices_ functions with occupationPattern concept
-
* Allows usage of range-based for-loop
-
-
* Make use of [] operator of staggeredPriVars class
-
* Make base staggered discretization more general
-
* Set fluxVars in model-specific propertyDefaults * Remove unused code from staggered VolVars
-
* 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.
-
* 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
-
-
*Greatly improves performance because only the local residual of the dof of interest gets calculated (not the whole element)
-
* Cell dof and and individual face dofs can now be treated separately
-
* Remove unused code * Use chached values of the residua for calculation of derivatives
-
*Test may fail due to tiny velocity discrepancies (no flow involved in this test)
-
* Stokes (Re=1) and Navier-Stokes (Re=1000) flow regimes
-
* Affects normal advective momentum flux and pressure term
-
