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 …

In order to obtain propagation characteristics of a rotating detonation wave (RDW) of
cracked kerosene gas (CKG) and ambient temperature air, a series of experiments were …

Three-dimensional numerical simulations are performed on air-breathing rotating detonation
combustors with detailed H 2/air chemistry. Detonation-related flow structures and pressure …

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

A numerical study of the longitudinal pulsed detonation (LPD) is conducted in the present
paper. The occurrence mechanism of the LPD, called shock wave amplification by coherent …

In this short Letter, the structure of a rotating detonation wave (RDW) fueled by biofuel is
revealed and expounded. A simulation is carried out under an Eulerian–Lagrangian …

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 …

A three-dimensional upwind conservation element and solution element method (CESE) in
cylindrical coordinates is first developed to effectively solve the unsteady reactive Euler …