Wall thermal boundary conditions and turbulent models can affect flow and combustion
simulations but are seldom considered in the turbulent modeling of supersonic combustors …

A series of numerical simulations were performed to investigate the feasibility and
performance of the premixed ammonia/hydrogen/air rotating detonation engines. A 19 …

Due to the complexity and short timescale of detonation, it is usually difficult to capture its
transient characteristics experimentally. Advanced numerical methods are essential for …

As rotating detonation engine (RDE) is maturing toward engineering implementation, it is a
crucial step in developing real-time diagnostics capable of monitoring the combustion state …

The product of kerosene pre-combustion pyrolysis is typically used as the fuel for rotating
detonation, and pure air at an ambient temperature is used as the oxidizer. The temperature …

Partially or completely reusing launch vehicles significantly reduces expenses for
manufacturing and testing in space missions. Thus, Reusable Launch Vehicles (RLV) can …

The two-dimensional simulation of two-phase rotating detonation engines commonly adopts
the nozzle–wall configuration, which is inconsistent with the real configurations in …

Hydrogen/air rotating detonation turbine engine is expected to become a new generation of
aerospace power plant because of its compact structure, high cycle thermal efficiency, and …

This study investigates the characteristics of stable and unstable cells and wavefronts of
detonation waves propagating in annular channels with different inner radii and channel …

A noncircular cross-sectioned combustor holds the potential to facilitate the flexible design of
continuous rotating detonation (CRD) engines, meeting the demands of airframe/engine …