A theory that explains the operating pressures where liquid injection processes transition
from exhibiting classical two-phase spray atomization phenomena to single-phase diffusion …

Injection of liquid fuel (or oxidizer in the case of liquid rockets) in systems where the working
fluid exceeds the thermodynamic critical condition of the liquid phase is not well understood …

A comprehensive framework has been established for studying laminar counterflow diffusion
flames for general fluids over the entire regime of thermodynamic states. The model …

This paper extends past analyses of liquid-oxygen-hydrogen flames at supercritical pressure
by providing quantitative results that characterize multicomponent diffusion processes in the …

Large-Eddy Simulation of transcritical combustion is considered in this article. This analysis
is motivated by rocket propulsion applications where cryogenic oxygen is injected at low …

THIS review of multiregime large-eddy simulation (LES) approaches is motivated by
propulsive applications. Such applications cover a broad range of combustion regimes, with …

The transition of classical spray atomization processes to single-phase continuous dense-
fluid mixing dynamics with diminished surface tension forces is poorly understood. Recently …

Mixing is a key point for thrust and efficiency of combustion systems. It becomes crucial in
the case Liquid Rocket Engines as large investments are involved. Besides, the pressure in …

This work presents a study of non-premixed flames at supercritical-pressure conditions.
Emphasis is placed on flame stability in liquid rocket engines fueled with liquid oxygen and …

Previously, a theory has been presented that explains how discrete vapor–liquid interfaces
become diminished at certain high-pressure conditions in a manner that leads to well known …