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 …

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 …

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 …

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 …

In this paper an attempt has been made to find out the better mixing of fuel and air in the
supersonic ramjet engines (SCRAMJET). For this the modified and innovated computational …

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 …

A three-dimensional numerical investigation has been carried out on the performance and
combustion characteristics of a scramjet combustor with and without cavity for various strut …

The demand for the enhancement of scramjet performance is increasing worldwide due to
its tremendous and upcoming applications. The major challenge in scramjet engines is the …

In this research paper numerical analysis of scramjet combustor has been carried out with
different passive techniques to improve the mixing efficiency of supersonic airstream and …

Numerical analysis of the supersonic combustion and flow structure through a scramjet
engine at Mach 7 with alternating wedge fuel injection and with three angle of attack (α=− 3° …