Modeling turbulent non-premixed combustion remains a challenge in the context of Large
Eddy Simulation (LES) in complex geometries and for realistic conditions, taking into …

This investigation outlines a data-assisted approach that employs random forest classifiers
for local and dynamic submodel assignment in turbulent-combustion simulations. This …

Measurements of the heat loads in experimental lab-scale rocket combustors are essential
in order to obtain information about the mixing and energy release of the propellants, the …

Abstract This work presents Large Eddy Simulations of a single-element GOx-GCH 4
combustion chamber at elevated pressure. A robust and efficient flamelet model accounting …

The single element GCH 4/GOx rocket combustion chamber developed at the Technische
Universität München has been computed using Large Eddy Simulation. The aim of this work …

Heat load measurements in experimental lab-scale rocket combustors are essential in order
to obtain information about the mixing and energy release of the propellants, the …

This work, along with other attempts in the scope of the Transregio SFB/TR-40 program [3],
numerically reconstructs combustion behaviour in a film cooled rocket combustion chamber …

M ny papers were published in the past years addressing the merits of methane as a
propellant candidate. In fact, the propellant combination LOX/methane is a good propellant …

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 …

Given growing competition in the business space launch market, more researchers are
evaluating the merit of methane as a potential propellant. In this study, a rocket combustion …