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 …

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 …

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 modification in the ramjet engine, known as the Supersonic Ramjet Combustion,
completes the combustion at supersonic speeds. Inside the combustion chamber, the mixing …

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 …

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 …

The present study discusses the effects of reacting and non-reacting flow conditions on the
flow physics of a scramjet combustor. A cavity based supersonic combustor with a triangular …

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 …

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 …