Supersonic spray combustion is one of the most significant physiochemical processes that
occurs in the scramjet propulsion system, and related research can motivate the …

A hybrid Eulerian-Lagrangian solver RYrhoCentralFoam is developed based on
OpenFOAM® to simulate detonative combustion in two-phase gas-liquid mixtures. For …

摘要斜爆轰是气相爆轰物理的一个重要研究方向, 在航空航天新型动力领域有重要的潜在应用
价值. 作为激波诱导的高速燃烧, 斜爆轰波可以简化为包含能量添加的间断面. 然而 …

Rotating detonation combustion (RDC) fuelled with partially pre-vaporized n-heptane sprays
and gaseous hydrogen is studied with an Eulerian-Lagrangian method and a simplified two …

Although the morphology of oblique detonation waves (ODWs) has been widely studied, it
remains impossible to predict the wave systems in the initiation region, which is a critical …

Kerosene/air two-phase rotating detonation is numerically investigated to find out the limits
of detonation stability as a function of total pressure and total temperature considering the …

The propagation characteristics and stability of droplet-laden two-phase rotating detonation
waves are studied by theoretical analysis and numerical simulations. The stability criterion of …

Initiation and stabilization of oblique detonation waves (ODWs) are important to the
successful application of oblique detonation engines (ODEs), which, however, have been …

The propagation of multiple detonation waves in the two-dimensional modeled rotating
detonation combustor fueled by premixed kerosene/air mixtures is numerically investigated …

This study reports the first experiments of a large-scale hydrogen-fueled oblique detonation
engine model conducted in a hypersonic wind tunnel. The stabilization characteristic of …