Scramjet combustors are emerging technologies in the aerospace industry, but this
technology has a great challenge like air-fuel mixing at supersonic speed. Hence, worldwide …

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 …

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 …

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 …

The supersonic airflow and injected fuel stream mixing process is complicated for a scramjet
combustor because of little supersonic air resident time and high airflow stream momentum …

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 …

A detailed numerical analysis on a scramjet combustor is carried out by introducing an
innovative shaped strut in place of the conventional strut. The design of newly added strut …

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 …

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 …