Developing supersonic combustion models with efficiency, accuracy and practicality is
important foundation to deeply understand the complex combustion processes in scramjet …

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

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 …

High-enthalpy gas streams in a real engine or wind tunnel will contain some trace gases;
however, this is often ignored in many studies. To investigate transverse fuel-jet mixing and …

We numerically investigate the mixing and combustion process of a kerosene jet injected
into a scramjet combustor with dual-cavity at different global fuel equivalence ratios using a …

Supersonic combustion is a complex phenomenon with multi-physical coupling, and the
thermal-acoustic coupling under supersonic inflow is also a matter of concern. In this work …

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

In this study, the effect of boundary layer thickness on supersonic combustion in an ethylene-
fueled scramjet combustor under Mach 5.5 flight conditions is studied by employing …

This paper presents a practical method for optimizing reaction progress variables for FPV
models, and the potential of this method is demonstrated in the application of a scramjet …

Due to the different structure and flow mechanism, whether the scale effect law obtained at
the rectangular interface can be applied to the axisymmetric combustor remains to be urgent …