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 …

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 …

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 …

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 …

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 …

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 …

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 …

The prevalence of complex phenomena associated with the fuel mixing of a supersonic
stream in scramjet combustor is inherently occurred due to the short residence time. An …

A parametric study of combustor inlet configuration for supersonic combustion ramjet
(Scramjet) engine has been conducted by solving two-dimensional full Navier–Stokes …