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 continuous detonation engine (CDE) is based on detonation waves and is a new jet
engine concept that is expected to bring a technical revolution to current aviation and …

A rotating detonation engine (RDE) combustion chamber fed by hydrogen–air mixtures of
different composition was modeled numerically using 3D geometry. The RDE is a new type …

Two-dimensional numerical simulations are performed to investigate the effects of spatially
discrete slot injection of reactants on the features of detonation wavelets in a rotating …

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

The propagating velocity behavior, mathematical model and influencing factors of rotating
detonation waves and counter-rotating shock waves in a hollow combustor with Laval …

The flow-field structure and pressure gain performance of a rotating detonation engine with
banded distribution of reactants have been studied using two-dimensional numerical …

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 …

Controlling the rotating detonation combustor (RDC) is crucial for enhancing propulsion
system safety, efficiency, and overall performance. Swift and precise identification of the …

A series of numerical simulations of RDE modeling real injection nozzles with different exit
widths are performed in this paper. The effects of nozzle exit width on chamber inlet state …