[mkraposhin]

Dear OpenFOAM users!

We finished development of hybrid Kurganov-Tadmore/PISO semi-implicit solver for all-mach number flows

You can download it with tutorials at github https://github.com/mkraposhin/pisoCentralFoam

git link https://github.com/mkraposhin/pisoCentralFoam.git

Solver description located in git archive and wiki https://github.com/mkraposhin/pisoCentralFoam/wiki

Model was tested in Mach numbers from 0.01 to 6 for cases:

1. Laminar flow in channel
2. Laminar flow around cylinder
3. Turbulent flow around cylinder
4. Shock Tube test (Sod's problem)
5. forward supersonic test
6. backward step supersonic case
7. Converging-Diverging nozzle
8. Oblique shock

Model was implemented for OpenFOAM of next versions:
- OpenFOAM 2.3.0
- OpenFOAM 2.4.0
- OpenFOAM-dev (thanks to Hassan Kassem)
- foam-extend 3.1

Youtube video


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