We conduct an experimental investigation on the implementation of cat-ear-shaped film
cooling holes for thermal protection in a hydrogen-air rotating detonation engine (RDE). The …

In order to increase turbine efficiency and prevent metal materials from being corroded by
high temperatures, one of the great important methods for turbine blade cooling is film …

Transpiration cooling with phase change is an effective method for protecting high heat flux
walls from ablation in combustion chambers and spaceflight vehicles. The combustion …

To address the thermal protection challenges associated with the rotating detonation engine
(RDE) in engineering applications, this study employs a three-dimensional numerical …

The rotating detonation gas turbine boasts several advantageous characteristics, including
self-pressurization, minimal entropy increase, high thermal efficiency, and a high thrust-to …

The rotating detonation engine (RDE) has attracted considerable interest as a potential new
propulsion system, owing to its ability to self-pressurize, its high thrust-to-weight ratio, and its …

Rotating detonation combustors establish a detonation wave that continuously circulates
inside a small annulus. The presence of the detonation wave and the downstream oblique …

In this paper, numerical simulations are conducted to investigate the effects of the
combustion modes and structure parameters of the combustion chamber of a rotating …

In this short letter, we report an experimental investigation on the integration of film cooling
for thermal protection in a 72-mm cylindrical rotating detonation engine (RDE). The cooling …

A new combustor has been developed for an experimental test campaign on film cooling for
hollow-type Rotating Detonation Engines (RDEs). In support of these research efforts, a …