This study explores the effect of differing inlet and outlet boundary conditions on the
operation and performance of a rotating detonation combustor (RDC) over an annulus mass …

Rotating detonation as a kind of pressure gain combustion is expected to greatly improve
efficiency when applied to gas turbine engines. In this paper, the operation of rotating …

Owing to the pressure gain combustion characteristics, the gas turbine can enhance the
system thermodynamic cycle efficiency by integrating a rotating detonation combustor …

Aiming at the coupling problem between rotating detonation combustor and turbine
components, this paper uses methane recuperation gas as fuel and adopts two-dimensional …

The physics of shock-boundary layer interactions (SBLIs) in a supersonic turbine cascade at
Mach 2.0 and Reynolds number 395,000, based on the axial chord, is investigated through …

Utilizing a neural network, individual down-axis images of combustion waves in the rotating
detonation engine (RDE) can be classified according to the number of detonation waves …

To enable the coupling of the unsteady, high-enthalpy flow exiting a Rotating Detonation
Combustor (RDC) with a subsonic turbine, an ejector may be installed between the …

In this paper, in response to the current demand for new aerospace power in the aerospace
field, thermodynamic performance and thermal efficiency advantages of existing constant …

Any outlet restriction downstream of pressure gain combustion (PGC), such as turbine
blades, affects its flow field and may cause additional thermodynamic losses. The …

Rotating Detonation Combustors (RDC) are one promising implementation of the Pressure
Gain Combustion (PGC) concept that is associated with potential performance gains in gas …