This study describes a rotating detonation combustor (RDC) equipped with a set of nozzle
guide vanes (NGVs) of variable number and inclination angle. Different instrumented guide …

In the past decade, pressure gain combustion research has promised over 10 percentage-
points of increase in power plant thermal efficiency. Alas, to realize such potential gain, one …

Rotating detonation turbine engine is receiving considerable attention due to its' high cycle
efficiency, outstanding thrust characteristics, self-pressurization, and energy-saving …

Although inherently unstable, existing research in rotating detonation combustion supports
its application in notionally steady processes resulting in greater availability compared to …

The influence of guide vanes on the combustion efficiency and pressure gain characteristic
of rotating detonation combustor was studied. In this experiment, aviation kerosene (RP-3) …

A three-stream combined Joule-Humphrey cycle that employs a heat recovery stream to
function as a recuperator is presented. Based on an in-house developed thermodynamic …

In this study, the two-dimensional numerical simulations are conducted to study the flow field
characteristics, turbine performance and loss mechanism of integrated system of rotating …

Under the prism of introducing pioneering technologies in the propulsive field, the Rotating
Detonation Engine (RDE) continuously attracts the Gas Turbine (GT) research community …

Pressure gain combustion cycles are under the spotlight due to their higher theoretical cycle
thermal efficiency compared to conventional machines. Under this prism, a constant-volume …

In rotating detonation engines the turbine inlet conditions may be transonic with
unprecedented unsteady fluctuations. To ensure an acceptable engine performance, the …