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) …

A novel strut with sawtooth grooves arranged at the trailing edge of a normal strut was
developed to improve the performance of a scramjet combustor. Through numerical …

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 …

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

In this study, the following strut configurations were proposed to improve the combustion
performance of a scramjet combustor with a strut:(1) BS-1: strut with periodic rectangular …

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 …

This study delves into the investigation of multi-scale flow structures and combustion
characteristics in a cavity-enhanced circular scramjet operating under a Mach-4.5 …

This paper presents a high-efficiency and high-fidelity approach to model supersonic
combustion using the extended flamelet-generated manifold (FGM) and the Eulerian …

During the operation of hypersonic vehicles, a reciprocal coupling effect is manifested
between the inlet and the combustion chamber. This results in an unavoidable non …