Controlling the rotating detonation combustor (RDC) is crucial for enhancing propulsion
system safety, efficiency, and overall performance. Swift and precise identification of the …

Due to their high thermal cycle efficiency and compact combustor, oblique detonation
engines hold great promise for hypersonic propulsion. Previous numerical simulations of …

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 …

When a detonation wave hits a rigid wall, a reverse shock is created. This occurrence is
common in closed pipe detonation experiments. To better comprehend the propagation …

When propagating in an annular combustion chamber, the detonation wave reflects under
the effect of wall curvature. In order to comprehend the reflection mechanism, a high-speed …

We investigate the behavior of evaporating droplets in a two-phase rotating detonation
engine (RDE) fueled by liquid ethanol, a renewable energy source and hydrogen carrier …

Two-dimensional numerical simulations were performed in this study to look at the diffraction
and subsequent evolution of an irregular structure detonation in a stoichiometric hydrogen …

Utilizing a two-phase supersonic chemically reacting flow solver with the Eulerian-
Lagrangian method implemented in OpenFOAM, this study computationally investigates the …

Shock wave caused by a sudden release of high-energy, such as explosion and blast,
usually affects a significant range of areas. The utilization of a uniform fine mesh to capture …

Detonation initiation is important not only for the development of advanced detonation
engines and but also for the control of accidental explosion. There are mainly two types of …