The combustor employed in small and medium-sized turboshaft engines is characterized by
a small flame tube height and a large distance between adjacent burners, rendering it …

We investigate the behavior of evaporating droplets in a two-phase rotating detonation
engine (RDE) fueled by liquid ethanol, a renewable energy source and hydrogen carrier …

This study employs rainbow schlieren deflectometry (RSD) to characterize the unsteady,
supersonic/subsonic exhaust plume of a rotating detonation combustor (RDC). First, RSD …

With the rotating detonation engine's (RDE) development to engineering applications, the
selection and optimization of nozzle is garnering great concerns, with the aim to maximize …

The sensitivity of rotating detonation combustor operation and performance to the length of
the combustion chamber was characterized using continuous variation of the chamber …

Current total pressure measurement techniques in rotating detonation combustors (RDCs)
are based on different assumptions and therefore show different applicability for specific …

In this paper, the mechanism of rotating detonation is analytically discussed using a two-
dimensional sheet model. Two ratios are employed in this discussion: the ratio of the sonic …

Multiphase reactant injection in rotating detonation combustors (RDCs) gives rise to
additional complexities as compared to gas-gas systems, as liquid breakup and evaporation …

A 1.6 inch/4.1 cm diameter water-cooled rotating detonation rocket combustor was designed
and tested using gaseous oxygen and methane propellants at operating pressures from 5 …

This study presents a fatigue assessment for a Rotating Detonation Rocket Engine (RDRE)
combustor under combined thermal and pressure loading conditions, incorporating mean …