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 …

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 …

Efficient combustion schemes are increasingly vital as scramjet expansion into higher Mach
numbers emerges as a leading trend. Thus, in the current work, an LES investigation on …

Scramjet engines can potentially revolutionize terrestrial and space transportation but face
the challenge of proper fuel-air mixing and stable combustion. Scramjet combustors with …

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 …

The mixing concept of fuel and air is the burning issue for hypersonic vehicles (scramjet)
due to the less resident time of supersonic air in the combustion chamber. So far, significant …

Mixing fuel and air in a scramjet combustor is one of the key challenges in its development
due to the short residence time available. Strut based injection is considered a viable …

This study aims at investigating the effect of a multistrut‐based hydrogen injector in a
scramjet combustor underreacting case. The numerical analysis is carried out using two …

The efficient fuel mixing in the combustion tank enhances the overall performance of
scramjet. Current attempt examines the existence of the strut on the fuel mixing of the multi …

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 …