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 …

Pressure-gain combustion has gained attention for airbreathing ramjet engine applications
owing to its better thermodynamic efficiency and fuel consumption rate. In contrast with …

Oblique detonation waves (ODWs) are induced by oblique shock waves (OSWs) and hold
significant research value for air-breathing ramjet engines due to their high thermodynamic …

Oblique detonation waves (ODWs) have been studied widely as the basis of detonation-
based hypersonic engines, but there are few studies on ODWs in a confined space. This …

Two-dimensional wedge-stabilized oblique detonations in stoichiometric and fuel-lean H
2/O 2/Ar mixtures with water mists are studied using Eulerian-Lagrangian method. The …

The shock-induced combustion ramjet (Shcramjet) based on oblique detonation waves
(ODWs) is among the promising choices for hypersonic propulsion systems. An …

Reliable detonation initiation is critical in detonation engines, especially for oblique
detonation engines covering a wide range of flight regimes. The widely-studied oblique …

The structure of an oblique detonation wave (ODW) induced by a wedge is investigated via
numerical simulations and Rankine–Hugoniot analysis. The two-dimensional Euler …

Hysteresis phenomenon of the oblique detonation wave (ODW) is numerically studied. Two-
dimensional unsteady reactive Euler equations are numerically solved as governing …

The wedge-induced oblique detonation wave (ODW) at low inflow Mach number is
investigated via Rankine–Hugoniot analysis and numerical simulations. The results show …