The hyStrath GitHub repository is featuring hypersonic and rarefied gas dynamics code developments released under license GPL-3.0. It is the only platform to conjointly host open-source CFD and DSMC codes designed for atmospheric entry analysis.
pdFoam
Capon et al. (2017) - Ion Orbital Motion Structures in LEO
hy2Foam
Casseau et al. (2016) - Mach 20 Flow of Nitrogen Around a Cylinder
hyFoam
Hoste et al. (2017) - Experimental Schlieren and CFD Results for Lorrain's Scramjet
hyFoam
Hoste et al. (2017) - Pressure Coefficient for Lorrain's Scramjet, Fuel-Off Conditions
dsmcFoam+
Palharini (2014) - Heat Transfer Coefficient for the Pathfinder Probe at 86 km Altitude
rhoCentralFoam
Espinoza et al. (2015) - Sod Shock Tube Simulation with Adaptive Mesh Refinement (AMR)
ARC
Renato and Scanlon (2017) - 3-D Ablation and Thermal Response for the Pathfinder Capsule
ARC
Renato and Scanlon (2017) - 3-D Ablation and Thermal Response for the Pathfinder Capsule
hyperFoam
Espinoza (2018) - Buffer Layers Methodology of the Hybrid CFD-DSMC Solver
hyperFoam
Espinoza (2018) - Hybrid CFD-DSMC Simulation of a Mach 6 Hypersonic Cylinder
pdFoam
Capon et al. (2017) - Mach 10 Flow of Argon Around a Cylinder
dsmcFoam+
Casseau and White (2018) - Random Porous Media Generation Matching a Target Porosity
dsmcFoam+
Casseau and White (2018) - Relation Between Porosity and Effective Diffusivity
rhoCentralFoam
Espinoza (2018) - Mach 9 Hollow Cylinder Simulation at 0 Degrees Angle of Attack
hyFoam
Hoste and Casseau (2021) - HB-2 Flare, Geometry
hyFoam
Hoste and Casseau (2021) - HB-2 Flare, Heat Flux Profile
dsmcFoam+
Palharini (2014) - Temperature Contours Over the Orion Command Module at 95 and 105 km Altitude