DT Banuti, V Hannemann, K Hannemann… - Combustion and …, 2016 - Elsevier
This paper introduces a new model for real gas thermodynamics, with improved accuracy, performance, and robustness compared to state-of-the-art models. It is motivated by the …
G Li, B Shi, N Wang, Q Li, M Zhao - Applied Thermal Engineering, 2024 - Elsevier
This study focuses on the fundamental combustion instability issues in staged combustion for liquid oxygen/kerosene rocket engines. A comprehensive and high-fidelity numerical …
H Müller, M Pfitzner, J Matheis, S Hickel - Journal of Propulsion and …, 2016 - arc.aiaa.org
Large-eddy simulations are carried out for the coaxial injection of liquid nitrogen and preheated hydrogen at supercritical pressures. The conditions are similar to that in typical …
While increased pressure and temperature contribute to an overall efficiency gain in the mixing of propellants and oxidizers, characteristic of conditions in the combustion chambers …
Although OpenFOAM is a widely-used open source computational fluid dynamics (CFD) tool, it is limited to numerical simulations of multi-dimensional reacting/nonreacting flows at …
In Liquid Rocket Engines, higher combustion efficiencies come at the cost of the propellants exceeding their critical point conditions and entering the supercritical domain. The term fluid …
A new era in spaceflight has begun. What used to be an endeavor of nations, is now achieved by private companies. When the first man-made object, the A4 rocket, reached …
Supercritical nitrogen jet behavior is modeled using an incompressible but variable density approach developed for variable density jets. Following mechanical and thermal breakup …
The injection of nitrogen under supercritical and transcritical conditions, where the injection temperature is below nitrogen's critical point, but the pressure is above it, is considered in …