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 …

The mixing and combustion process plays an important role in the realization of the scramjet
engine, and the transverse injection from a wall orifice is widely employed for the simplest …

The present paper aims to provide a summary report on recent research progress about
unstart mechanism, detection and control of hypersonic inlet to help the researchers working …

In an air-breathing engine the flow deceleration from supersonic to subsonic conditions
takes places inside the isolator through a gradual compression consisting of a series of …

The ramjet and scramjet modes can be realized in the same flowpath using the thermal
choking approach, and the dual-mode scramjet combustor has attracted an increasing …

Airbreathing aero-engines are regarded as excellent propulsion devices from ground takeoff
to hypersonic flight, and require control systems to ensure their efficient and safe operation …

A review of recent research outcomes in downstream flow choking-driven unstart is
presented. Unstart is a flow phenomenon at the inlet that severely reduces the air mass flow …

The multi-strut injector is one of the most favourable perspectives for the mixing
improvement in between the hydrogen and the high-speed air, and its parametric …

With the maturation of the scramjet technologies, the urgent development of the combined
cycle propulsion system has been put forward, and it can help the vehicle to launch and land …

Abstract The two-dimensional Reynolds-Averaged Navier–Stokes (RANS) equations
coupled with the two equation Shear stress transport k–ω turbulence model as well as the …