Multi-strut injection is an approach to increase the overall performance of Scramjet while
reducing the risk of thermal choking in a supersonic combustor. Hence computational …

Computational simulation of Scramjet combustor at Mach 2.5 through two struts and with
three angle of attack (α=− 3°, α= 0° and α= 3°) have been presented and discussed in 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 …

In this research paper computational fluid dynamic simulations of scramjet combustor at
Mach 2 with innovative strut fuel injections have been presented and discussed. In scramjet …

A numerical analysis of the inlet-combustor interaction and flow structure through a scramjet
engine at a flight Mach number M= 6 with parallel injection (Strut with circular inlet) is …

Mixing and combustion of a fuel with supersonic airstream in a scramjet combustor is a
complex phenomenon because of very less resident time of the air in the combustion …

The multi-strut injector is one of the most favourable perspectives for the mixing
improvement in between the hydrogen and the high-speed air, and its parametric …

Detailed numerical analysis on a cavity-based scramjet combustor is carried out by
introducing an innovatively shaped strut and multi strut with backward-facing step to …

In this research paper, passive method has been considered to improve the mixing and
combustion efficiency of scramjet combustor. Modified and innovative strut injector designs …

Numerical investigation of Scramjet combustor is performed with the help of center lobed
strut to act as a parallel fuel injector. The geometry of the combustor plays a major role to get …