In the present Paper, the simulation of the flow inside an experimental GOX/GCH 4 rocket
thrust chamber is undertaken. The combustor's injector consists of seven individual coaxial …

Direct numerical simulations (DNS) are conducted to analyze the effect of recess in the
mixing and combustion performance of gaseous methane—oxygen injection systems. The …

In this work, the combustion and thermal recombination in the boundary layer of a single-
element methane/oxygen rocket combustor is investigated using large-eddy simulations …

The current work presents the extension of the flamelet model for turbulent combustion
calculations to account for deviations from adiabatic conditions. The aforementioned …

The design phase of a rocket combustion chamber relies on the prediction of the wall heat
fluxes, in order to optimize the components to prevent thermal damage. Based on the …

The spray combustion of LOX/GCH4 in the pintle injector is simulated to study the
combustion characteristics at a subcritical condition by considering the effects of pintle …

Targeting the numerical simulation of rocket thrust chamber applications with cooled wall
structures, this research work presents a concept to extend the standard flamelet combustion …

We undertake the modeling of the combustion of highly swirling fuel sprays using the
Flamelet-Generated-Manifold (FGM) combustion-chemistry-reduction technique, especially …

This work aims to compare two non-adiabatic flamelet combustion models for the simulation
of a subscale single-injector GCH4/GO2 combustion chamber in rocket-like operative …

The fluid species composition plays a vital role in the wall heat transfer prediction and can
be significantly impacted by non-adiabatic effects in the vicinity of cooled wall structures …