Rotating detonation combustors (RDC) are at the forefront of pressure gain combustion
(PGC) research, utilizing one or more azimuthally spinning detonation waves, an intrinsically …

The counter-rotating shock wave and wave direction control of the hollow rotating detonation
combustor with Laval nozzle are studied. The in-house solver BYRFoam, developed on the …

Rotating detonation engines (RDEs), which are hoped to achieve significant performance
improvements in propulsion systems, have received much attention in recent years. The …

The counter-rotating shock wave phenomenon and instability mechanisms in the hollow
rotating detonation combustor with a Laval nozzle are investigated. The in-house solver …

A statistical particle path tracking method is applied to a hollow rotating detonation engine
(RDE) with a Laval nozzle, and the flow field characteristics are investigated. The in-house …

Rotating detonation engines (RDEs) are widely studied because of their compact
configurations and high thermal cycle efficiency. In this paper, a series of numerical …

Characteristics of continuous rotating detonation (CRD) in a cavity-based annular combustor
are studied through three-dimensional simulations, which are solved in OpenFOAM with a …

This paper focuses on rotating detonation combustor (RDC) experiments involving two
configurations, a hollow and flow-through RDC, using hydrogen–air and ethylene–air …

In order to investigate the relationship between high frequency tangential instability and
continuous rotating detonation, series of H 2/Air rotating detonations are experimentally …

Outlet nozzles for a rotating detonation combustor were designed to meet a downstream
turbine and reduce the high pressure and heat load caused by the oblique shock wave at …