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 …

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 …

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 …

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 …

This paper investigates the finite-time tracking control problem of the hypersonic flight
vehicle (HFV) with state constraints. Firstly, a control-oriented model is introduced to enable …

The mixing and combustion characteristics of liquid kerosene spray in a cavity-based
supersonic combustor under a Mach 2.52 inflow are experimentally and numerically …

The periodic flame flashback phenomenon in an ethylene-fueled cavity-based scramjet
combustor was numerically investigated by a three-dimensional unsteady Reynolds …

This paper presents experimental data examining the flameholding performance of a
scramjet cavity with an inclined front wall. Mach 8 flight-equivalent flows were delivered to …

Vitiation effect is vital in the combustion-heated wind-tunnel experiments. NO 2 is an active
vitiated species which can affect the combustion properties of hydrocarbons. Ignition delay …

Hypersonic airbreathing engines rely on scramjet combustion processes, which involve high-
speed, compressible, and highly turbulent reacting flows. The combustion environment and …