Supersonic spray combustion is one of the most significant physiochemical processes that
occurs in the scramjet propulsion system, and related research can motivate the …

The combustion modes in two different scramjet combustors with the mass flow rates of 1.8
kg/s and 3.6 kg/s are experimentally investigated to explore the scaling effects on …

The combustion of aluminum particles in solid rocket motor plays an important role in energy
release of propellants. However, due to the limited residence time, aluminum particles may …

Transcritical shock-droplet interactions (TSDIs) occur in a spectrum of high-speed
propulsion systems involving liquid fuel injection.“Transcritical” behavior refers to a condition …

In this paper, numerical simulations are carried out to study the propagation characteristics
of detonation waves in carbon particle-laden two-phase pyrolysis mixtures consisting of C …

The ignition process and flame propagation with ethylene fuel in cavity-stabilized scramjet
by a Multi-Channel Gliding Arc (MCGA) at Mach 2.0 were investigated. Effects of …

Scramjet has become one of the most efficient hypersonic vehicles because of its broad
application potentiality. The ground direct-connected test is a relatively easy and economical …

The study of interaction between shock wave and mixing layer commonly existed in rocket
based combined cycle engine is of profound significance for mixing enhancement in …

In this paper, the Eulerian Stochastic Field (ESF) model in the Transported Probability
Density Function (TPDF) class model is combined with the Flamelet Generated Manifolds …

In the airworthiness fireproof test of aviation components, the NexGen burner is an
internationally recognized new burner, which may accurately control the flow of fuel and air …