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 …

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 …

The optimization of non-premixed rotating detonation combustors (RDCs) requires improved
understanding of the coupled effects of reactant stratification, fluid property gradients, and …

Geometric throats are commonly applied to rocket combustors to increase pressure and
specific impulse. This paper presents the results from thrust measurements of an …

JP-10/air two-phase detonation and rotating detonation engine (RDE) are numerically
studied to find out their limits of physical values as a function of equivalence ratio …

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

Rotating detonation engines (RDEs) have received significant attention from industry and
academia alike, owing to their numerous advantages, such as pressure gain combustion …

Two-dimensional rotating detonation waves (RDWs) with separate injections of hydrogen
and air are simulated using the Navier–Stokes equations together with a detailed chemical …

In this paper, an improved κ-CNI scheme CE/SE Euler solver with chemical source terms is
applied to investigate the propagation characteristics and propulsive performance of …