Simulation details. All simulations are run at $Pr=1$ and $\eta=0.6$. The columns from left to right indicate: case number, Rayleigh number $Ra$, Rossby number $Ro$, the number of grid points in the l
This dataset contains the results of 175 Reynolds-Averaged Navier–Stokes (RANS) simulations of ammonia–hydrogen combustion in a staged Stagnation-Point Reverse-Flow (SPRF) combustor, as presented in t
Input files and scripts sufficient to reproduce the results shown in the paper "Ocellaris: a discontinuous Galerkin finite element solver for high density ratio two phase flows". A version of Ocellar
Simulation data in CGNS format.Files can be interpreted using ParaView.For methodology please refer to the linked article.Three files are included:- Jet_FGM: adiabatic FGM model- Jet_FGM_nonadiabatic:
