HE design of air-breathing vehicles with supersonic combustion (scramjets) has been
investigated for several decades. However, the layout of a supersonic combustion chamber …

A lobed hydrogen strut injector is investigated for use in scramjet (supersonic combustion
ramjet) engines at moderate combustor Mach numbers. The paper deals with the design of a …

In view of the very high freestream velocity of scramjets reaching Mach 10, fuel residence
time is on the order of milliseconds1 and supersonic combustion presents a challenge in …

Mixing characteristics of various strut injectors in supersonic flows were examined using
Planar Laser-Induced Fluorescence technique. CFD studies were used to further the …

SUPERSONIC combustion inherently involves some difficulties not present in other
combustion systems. The high flow velocities in the combustor, which can reach several …

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 …

As a result of the very high freestream velocity of scramjets reaching Mach 10, fuel residence
time is on the order of milliseconds, 1 and efficient supersonic combustion presents a …

An experimental investigation of cavity-based flameholders with strut injectors in a
supersonic flow is reported. In this ongoing research program, emphasis is placed on …

The concept of supersonic combustion ramjet (scramjet) engines has intrigued propulsion
engineers for over 40 years. However, a functional vehicle has yet to capitalize on the …

The strut-based injector has been found to be one of the most promising injector designs for
a supersonic combustor, offering enhanced mixing of fuel and air. The mixing and flow field …