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

The ignition and flame propagation in an axisymmetric supersonic combustor were
investigated. The laser-induced plasma was employed to ignite the supersonic inflow with a …

The present study numerically investigates the combustion characteristics and performance
of a direct-connect gaseous hydrogen-fueled scramjet combustor depending on the injector …

Combustion in scramjets generally proceeds in diffusion mode due to the independent
injection of fuel and air streams. However, premixed combustion is also important especially …

The ignition and stable combustion processes play a crucial role in the operation of a
scramjet engine. This study aims to investigate the effect of fuel reactivity on auto-ignition …

The cavity-assisted scramjet has been proven to be the most promising propulsion system
for air-breathing hypersonic vehicles. In this paper, numerical simulations of a Mach 8 …

This paper investigates the combustion performance of a scramjet engine in which hydrogen
fuel is injected into the flow field through transverse injectors. An unsteady numerical …

This study investigates the fluid dynamics and mixing characteristics of an oscillating sonic
jet injected into a supersonic cross flow of Mach 2.1 using experimental and computational …

In this paper, the influences of boundary layer injection on skin friction reduction are
numerically studied using Reynolds-averaged Navier-Stokes equations. The methodology is …

The combustor is the core component of the scramjet engine, and stable combustion is the
prerequisite for the efficient operation of the scramjet engine. This paper investigates …