Numerical investigations of a hydrogen-fueled scramjet combustor at cruise flight conditions
of Mach 8 at an altitude of 30 km have been performed. Two combustor configurations were …

Future space transport vehilce or even aircraft are supposed to use airbreathing propulsion
systems for their flight in a wide range of hypersonic Mach numbers. The great benefit of …

The combustion characteristics of a hydrogen-fueled scramjet combustor were investigated
experimentally and numerically. One nonreacting case (case 1), and two different …

Numerical exploration of non-reacting and reacting flow field of hydrogen fueled scramjet
combustor is presented. Three-dimensional Navier–Stokes equations with K–ε turbulence …

A numerical study of combustion enhancement has been performed for a Mach 2 model
scramjet (supersonic combustion ramjet) combustor. The configuration used is similar to the …

In the arena of design of combustion chamber of scramjet engine lots of development are
still going on. A properly designed combustor shall promote sufficient mixing of the fuel and …

The combustion process in a hydrogen fueled scramjet combustor with a rearwall-expansion
cavity was investigated numerically under inflow conditions of Ma= 2.52 with stagnation …

DESPITE the promising progress made toward the use of alternative flight solutions such as,
among others, the pulsed detonation technology, high-speed airbreathing engines remain …

The development of novel air-breathing engines such as supersonic combustion ramjets
(scramjets) depends on the understanding of supersonic mixing, self-ignition and …

A modification in the ramjet engine, known as the Supersonic Ramjet Combustion,
completes the combustion at supersonic speeds. Inside the combustion chamber, the mixing …