I. Introduction uture space transport vehicles or even aircrafts are supposed to use air
breathing propulsion systems for their flight in a wide range of hypersonic Mach numbers …

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

Future space transport vehicles or even high speed aircrafts are supposed to use air
breathing propulsion systems for their flight in a wide range of hypersonic Mach numbers …

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 …

Supersonic combustion experiments of a complete scramjet configuration consisting of
intake, combustor and nozzle were performed in the High Enthalpy Shock Tunnel Göttingen …

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 …

The successful operation of scramjets for access-to-space application will strongly depend
on its capability to sustain efficient supersonic combustion while accelerating to higher and …

A multivariate assumed PDF approach together with finite-rate chemistry is used for the
simulation of the HyShot supersonic combustion configuration. Because the combustor …

A numerical investigation of the effect of the hydrogen-air reaction mechanism on the
prediction of supersonic combustion was conducted. Different reaction mechanisms with …

With the overall goal to clarify the physics of compressible (supersonic) combustion, a 3D
LES of the HyShot supersonic combustor has been performed and is reported in this paper …