A review of fundamental research in combustion stabilization for hypersonic airbreathing
propulsion is presented. Combustion in high-speed airbreathing propulsion systems …

This paper describes a numerical and experimental investigation of the combustion process
in an ethylene-fueled scramjet combustor. The combustion process could be divided into six …

The dynamics of an optical axisymmetric scramjet, preferred for generic combustion and
flameholding studies without the corner boundary-layer effects that distort the freestream …

The present study deals with the implication of a strut profile on the combustion
characteristics of a cavity-based scramjet combustor. Three different strut profiles namely …

Five detailed hydrogen combustion chemical kinetics mechanisms coupled with a partially
stirred reactor (PaSR) combustion model were applied with large eddy simulation (LES) to …

The present study investigates the implication of a dual cavity on combustion and mixing
characteristics of strut based combustor numerically. A scramjet combustor with and without …

Experiments were conducted at Mach 2.52 to investigate the effect of gas addition on the
mixing and combustion characteristics of the liquid kerosene in a scramjet combustor. Two …

Experimental investigations of laser-induced plasma (LIP) ignition processes were
conducted in an ethylene-fueled scramjet combustor with a rear-wall-expansion cavity. The …

Inlet buzz driven by flow choking in circular dual-mode scramjets is experimentally
investigated in high-enthalpy Mach 4.5 flows. Circular scramjet models with two different …

This paper presents the effect of cavity-based injection in an axisymmetric supersonic
combustor using numerical investigation. An axisymmetric cavity-based angled and …