In this article, comprehensive simulations of the compressible air stream inside the
combustion chamber are done to disclose the mixing and circulation performance of the 3 …

The use of 2-lobe nozzle for efficient fuel mixing behind the ramp injector nozzle is
comprehensively investigated in this article. Computational fluid dynamic is applied for the …

The present investigation examines the usage of rectangular multi-injectors for fuel injection
in a supersonic combustion chamber. To evaluate the fuel jet penetration and distribution, a …

The efficient injection system has a great role on the overall enactment of air breathing
propulsion systems at supersonic flow. In this work, the usage of extruded multi-injectors in …

Increasing the mixing efficiency of the fuel jet along the combustion chamber is a crucial step
for the advancement of the current high-velocity vehicles. In this article, comprehensive …

In this research, the usage of an extruded annular nozzle for mixing fuel through the
combustion chamber is fully studied. The chief focus is to reveal the flow of the fuel jet by …

The strut injection system is a conventional technique for the injection of the fuel in
combustor in hypersonic vehicles. The present article investigates the usage of the annular …

In present paper, computational fluid dynamic is applied to evaluate hydrogen mixing
impacts of the single extruded lobe injector at supersonic cross flow. The aim of this …

Injection and mass diffusion of fuel jet released in the combustor of scramjet are the primary
processes that improve scramjet engine performance. In this work, the presence of the strut …

In this research, all-inclusive efforts are performed to understand the impact of downstream
ramp on fuel distribution of cross jet at high-speed flow inside the combustion chamber …