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 …

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 …

The oblique and traverse configurations of injecting gaseous fuel in a low-aspect-ratio
supersonic combustor are characterized and compared numerically using a validated code …

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 …

To avoid inlet-combustor interaction, a two-staged supersonic combustor was introduced to
increase the pressure in the divergent section under a limitation of peak pressure at its …

N supersonic combustion chambers, fast mixing of fuel and air is essential for a stable self
ignition, good combustion performance, and low NOx emissions. Different types of injectors …

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

High-fidelity simulations with a validated methodology are employed to explore the physical
processes associated with different injection strategies on supersonic combustion. The …