The dual-mode scramjet combustor is a promising candidate for the combined cycle engine
of the hypersonic airplane, and the flame propagation and stabilization process in the dual …

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) …

The asymmetric separation has a crucial effect on the performance of the scramjet. In this
study, the asymmetric separation and combustion in both rectangular and circular scramjets …

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 …

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

Abstract The Flamelet/Progress Variables (FPV) model coupled with large eddy simulation
(LES) has been performed to appraise its applicability and performance for supersonic …

Ignition characteristics in a strut-equipped dual mode combustor fueled with liquid kerosene
were observed and discussed in this paper. A series of experiments and numerical …

Under the condition of flight Mach number 7 (inlet Mach number of isolator is 3.0), it is very
difficult for kerosene-fueled scramjet to achieve auto-ignition and flame stabilization. In order …