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

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 …

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

In this study, the performances of a Mach 9 oblique detonation engine fueled by hydrogen
are numerically investigated by solving the multi-species reactive Reynolds-averaged …

Oblique detonation waves (ODWs) are hypersonic combustion phenomena induced by
oblique shock waves. When applied to air-breathing engines, ODWs offer high thermal cycle …

In this paper, an improved κ-CNI scheme CE/SE Euler solver with chemical source terms is
applied to investigate the propagation characteristics and propulsive performance of …

A numerical study of the longitudinal pulsed detonation (LPD) is conducted in the present
paper. The occurrence mechanism of the LPD, called shock wave amplification by coherent …

The mechanisms of the multiplicity and bifurcation of detonation waves in 3D rotating
detonation engines (RDEs) with cavity combustor and array-holes injection are numerically …

Detonation-based propulsion has been an area of interest in the scientific community in
terms of detonative combustion providing higher efficiency. However, most detonation …