Recently, with the development of detonation-based propulsion systems, scholars have
begun to study how to perform mode control on the rotating detonation combustor (RDC). It …

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 …

Solid–gas rotating detonation engines have been widely studied, but experimental
limitations have prevented the full information of the flow field from being revealed. This …

The rotating detonation combustor (RDC) has received remarkable attention in the
aerospace community. In this work, an experimental RDC model supplied by liquid …

Controlling the rotating detonation combustor (RDC) is crucial for enhancing propulsion
system safety, efficiency, and overall performance. Swift and precise identification of 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 turbine engine is receiving considerable attention due to its' high cycle
efficiency, outstanding thrust characteristics, self-pressurization, and energy-saving …

The current study aims to evaluate and investigate the development of projection-based
reduced-order models (ROMs) for efficient and accurate rotating detonation engine (RDE) …

Optimizing the structure of the rotating detonation engine (RDE) is an effective way of
improving its performance. In this paper, a variable cross section RDE with convergent …