Propellant injection and turbulent combustion in high-pressure engines is often dominated
by real-gas effects. However, previous studies suggested that the departure of the fluid …

In this study, we investigate the averaging and modeling of real fluid equations of state (EoS)
used in the context of numerical simulations of flows under conditions relevant to liquid …

The increased modeling complexity needed to simulate high-pressure combustion in rocket
engines results in significant computational costs–costs which are not always justified for …

CFD simulations of turbulent reacting flows based on finite rate chemistry often employ
reduced kinetic mechanisms to decrease the computational cost, especially if the …

In this work the effect of the injector lateral confinement on flowfields and thermal loads in
the injection region of a rocket combustion chamber is investigated. The reference test case …

随着高效率, 大推力燃烧技术的发展, 跨/超临界流体流动在先进动力装置中越发常见.
研究跨/超临界流体流动与燃烧具有重要的应用价值. 由于真实工况下实验测量成本高, 风险大 …

Several aspects make nitrocellulose based powders adequate as a solid propellant for
rockets and missiles and the prefe rable propellant to be used in firearms and artillery: it …

The article is devoted to the analysis of the flame anchoring mechanism in the test case
MASCOTTE C-60 RCM2 on supercritical hydrogen/oxygen combustion at 60 bar, with …

The primary purpose of this paper is to develop high-fidelity combustion models for
hydrothermal flames. Based on the flamelet/progress variable (FPV) model, comprehensive …

The article is devoted to the analysis of the flame anchoring mechanism in the test case
MASCOTTE C-60 RCM2 on supercritical hydrogen/oxygen combustion at 60 bar, with …