The only platform to conjointly host open-source CFD and DSMC codes designed for atmospheric re-entry analysis
- hyFoam CFD solver (supersonic combusting flows)
- hy2Foam CFD solver (hypersonic reacting flows)
- Coming soon: ARC, a low computationally demanding 3-D Ablative Response Code
- dsmcFoam+ code (direct simulation Monte Carlo)
- Coming soon: hyperFoam, a hybrid CFD-DSMC solver
Please visit the hyStrath Wiki page
git clone https://github.com/vincentcasseau/hyStrath.git --branch master --single-branch && cd hyStrath/
./install-all.sh 8 > logInstall 2>&1 &where 8 is the number of processors to be used during the installation.
- Master branch ported to OpenFOAM v1706
- Minor DSMC corrections
- CFD and DSMC rearrangements for future integration of the hybrid solver
[hy2Foam] V. Casseau et al., 12/2016: A Two-Temperature Open-Source CFD Model for Hypersonic Reacting Flows, Part Two: Multi-Dimensional Analysis
[ARC] V. Renato et al., 09/2017: Multi-dimensional Ablation and Thermal Response Program for Martian Entry Analysis
GitHub coordinator: Dr Vincent Casseau
Contributors: Dr Vincent Casseau, Daniel E.R. Espinoza, Dr Christopher J. Capon, Dr Jimmy-John O.E. Hoste, Dr Viola Renato, Dr Rodrigo C. Palharini, Dr Craig White, Dr Melrose Brown, Prof Russell R. Boyce, Dr Thomas J. Scanlon, Dr Richard E. Brown
External contributors: the Micro & Nano Flows Group, R.Tech Engineering
- blockMeshDG by Anton Kidess (https://openfoamwiki.net/index.php/Contrib_blockMeshDG)
- makeAxialMesh by Bernhard Gschaider (http://openfoamwiki.net/index.php/Contrib/MakeAxialMesh)