The continuously increasing interest in alternative aircraft propulsion systems is caused by
the requirements and demands set by international institutions and government …

The effects of the exit convergent ratio on the propagation behavior (ie, initiation processes
and propagation characteristics) of rotating detonations utilizing liquid kerosene have been …

The rotating detonation engine (RDE) is an innovative and practical pressure-gain device for
rocket and ramjet propulsion, and has been widely investigated. The present work aims to …

The carbon emissions caused by the aviation industry are an urgent problem that requires
attention. Efficient energy utilisation and control of pollutants and greenhouse gas emissions …

This paper presents work on a demonstrator rocket powered by a rotating detonation engine
(RDE) fed by liquid propellants. Key to the success of the project was the development of a …

Detonation has promising applications in advanced propulsion systems, and numerical
simulation is widely used to gain insights into the complex interaction between the …

The propagation characteristics of a hydrogen-rich gas/air rotating detonation wave (RDW)
were investigated for different blockage ratios (BRs). Two rotating detonation chamber …

We present a numerical simulation of a two-phase rotating detonation fueled by liquid
ethanol and pre-heated air in a two-dimensional rotating detonation combustor. The study …

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

Due to their high thermal cycle efficiency and compact combustor, oblique detonation
engines hold great promise for hypersonic propulsion. Previous numerical simulations of …