Assessment of statistical and kinetics-based models for lox-methane green propellant combustion
In this article, we present a comprehensive review and numerical analysis of liquid oxygen
(LOx)-methane (CH 4) combustion at supercritical pressures. A detailed review of numerical …
(LOx)-methane (CH 4) combustion at supercritical pressures. A detailed review of numerical …
Multi-phase impact on the heat load characteristics of a multi-element methane-oxygen rocket thrust chamber
D Rahn, H Riedmann, O Haidn - International Journal of Heat and Mass …, 2021 - Elsevier
Aiming at the capability to numerically model relevant operating conditions in rocket thrust
chambers, this research work introduces a real gas multi-phase data extension to …
chambers, this research work introduces a real gas multi-phase data extension to …
[PDF][PDF] Definition and Evaluation of Advanced Rocket Thrust Chamber Demonstrator Concepts
D Eiringhaus, H Riedmann, O Knab - Future Space-Transport …, 2021 - library.oapen.org
Since the beginning of the German collaborative research center SFBTRR 40 in 2008
ArianeGroup has been involved as industrial partner and supported the research activities …
ArianeGroup has been involved as industrial partner and supported the research activities …
[PDF][PDF] 3D conjugate heat transfer analysis of a 100 kN class liquid rocket combustion chamber
D Eiringhaus, H Riedmann, O Knab… - … for Aeronautics and …, 2019 - researchgate.net
In order to cut the development costs of liquid rocket engines full-scale hardware tests are
supplemented with numerical analyses. For the correct prediction of the engine performance …
supplemented with numerical analyses. For the correct prediction of the engine performance …