A methane/oxygen mixture is considered to be an appropriate propellant for many future
rocket engines due to its practicality and low cost. To better understand the combustion …

A rocket's turbulent jet radiates intense acoustic waves, which are an acoustic load for
structural components like payload, launch structure, and rocket avionics, and impact …

This paper investigates different types of longitudinal mode coupling in subscale rocket
combustion chambers using experimental data and numerical simulations. Based on a one …

The sensitivity of hybrid RANS-LES methods like Improved Delayed Detached Eddy
Simulation (IDDES) to numerical model parameter variations related to generic space …

The current work aims to study the influence of the numerical setup on a URANS model of a
single co-axial injection element under acoustic forcing. The single injector model is …

This report contains the detailed description of the study of the canonical shock-turbulence
interaction (STI) problem performed with the DLR's TAU CFD solver. STI studies reported in …