This paper addresses the physiochemical mechanisms involved in transcritical and
supercritical vaporization, mixing, and combustion processes in contemporary liquid-fueled …

The present paper reviews recent achievements in numerical modeling of super-and
transcritical injection processes during the last 20 years. First, it provides an overview of …

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 …

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

ABSTRACT A detailed understanding of liquid propellant combustion is necessary for the
development of improved and more reliable propulsion systems. This article describes …

Injection of liquid fluid initially at subcritical temperature into an environment in which the
temperature and pressure exceed the thermodynamic critical conditions is an important …

Combustion processes involved in cryogenic propellant LOX/H2 systems are very complex.
In order to improve understanding and modeling of such processes, a test facility, called …

The thermophysical characteristics of a liquid-oxygen–hydrogen flame at supercritical
pressure are investigated, with emphasis placed on the near-field region just downstream of …

Liquid jet injection into a quiescent gaseous environment has been experimentally and
analytically studied covering subcritical to supercritical conditions. The focus was placed on …

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 …