Adds overset discretisation to selected physics:
- diffusion : overLaplacianDyMFoam
- incompressible steady : overSimpleFoam
- incompressible transient : overPimpleDyMFoam
- compressible transient: overRhoPimpleDyMFoam
- two-phase VOF: overInterDyMFoam
The overset method chosen is a parallel, fully implicit implementation
whereby the interpolation (from donor to acceptor) is inserted as an
adapted discretisation on the donor cells, such that the resulting matrix
can be solved using the standard linear solvers.
Above solvers come with a set of tutorials, showing how to create and set-up
simple simulations from scratch.
- eliminates the PtrList requirement (more flexible)
COMP: use tmp intermediate for volPointInterpolation return value
- gcc 4.8.5 had some weird issue of otherwise not binding a const-ref.
(in foamVtkInternalWriterTemplates.C)
- Use on/off vs longer compressed/uncompressed.
For consistency, replaced yes/no with on/off.
- Avoid the combination of binary/compressed,
which is disallowed and provokes a warning anyhow
- By definition, binary STL uses float (not double) when reading.
The ascii STL should be the same. This reduces memory overhead when
loading files. The older triSurface reader had float, the surfMesh
reader had double, but now has float.
- Inconsistency in the STL merge-tolerances between triSurface reader,
surfMesh reader and WM_SP vs WM_DP. Now use consistent tolerances
conrresponding to 10,100 * doubleSMALL.
- Similar float/double code adjustments for TRI format since this is
very similar to the STL reader and had a similar inconsistency between
the triSurface and surfMesh version. The AC3D reader still uses
double when reading, but this can be revisited in the future (and can
then remove the stichTriangles method too).
- only treat text as an option if it is preceded by 0-4 spaces.
This prevents the description of an option from being accidentally
detected as an option.
Solver for low Mach no. flows with adiabatic thermodynamics and updated
pressure-velocity coupling given by the RCM interpolation procedure
described in
\verbatim
Knacke, T. (2013).
Potential effects of Rhie & Chow type interpolations in airframe
noise simulations. In: Schram, C., Dénos, R., Lecomte E. (ed):
Accurate and efficient aeroacoustic prediction approaches for
airframe noise, VKI LS 2013-03.
\endverbatim
Original code supplied by Thilo Knacke, CFD E+F GmbH
contact: info@cfd-berlin.com
Integrated into OpenFOAM by OpenCFD Ltd.
