The compressible nature of the supersonic combustion flow field results in significant
temperature and pressure fluctuations. In the standard Flamelet/Progress Variable (FPV) …

The turbulence–chemistry interaction model with finite-rate chemistry is a common model for
solving supersonic turbulent combustion and takes into consideration the interaction …

An approach that combines numerical, experimental, and theoretical analyses has been
implemented to investigate the effects of the injection parameters on the flame flashback …

To investigate the relationship between the thrust performance and combustion mode in a
scramjet combustor, the acceleration process of a symmetrical tandem-cavity combustor is …

A zonal nonequilibrium model (ZNM) based on the concept of zonal representation of the
nonequilibrium relaxation times is proposed. ZNM, together with dynamic zone flamelet …

The combustion characteristics and flame stabilization mechanisms in an axisymmetric
scramjet with a high-enthalpy inflow are investigated numerically in this paper. To consider …

The scale effect of flame flashbacks inside an ethylene-fueled scramjet combustor was
investigated through an approach that combines numerical, experimental, and theoretical …

Understanding and accurately modeling combustion processes in engines across a wide
range of operating conditions is critical for advancing both subsonic and supersonic …

The mixing and combustion characteristics in a cavity flameholding combustor under inlet
Mach number 2.92 are numerically investigated with ethylene injection. Dimensionless …

An axisymmetric model scramjet assisted with cavity flameholder is numerically investigated.
Three‐dimensional Reynolds‐averaged Navier‐Stokes simulation is carried out to reveal …