The role of annular 2-lobe nozzle in a strut injection system on the mechanism of fuel distribution at a scramjet engine

D Wei, Y Jiao, N Zhang, H Gao, H Yu - Energy, 2024 - Elsevier
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 …

Fuel mixing and diffusion behind the unswept ramp injector with lobed nozzle at combustor of scramjet engine

SA Abdollahi, SF Ranjbar, MB Ehghaghi - Energy, 2024 - Elsevier
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 …

Effect of wedge strut fuel injection nozzles arrangement for a model scramjet engine

OR Kummitha, KR Kandula - International Journal of Hydrogen Energy, 2024 - Elsevier
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 …

Investigation of strut-ramp injector in a Scramjet combustor: Effect of strut geometry, fuel and jet diameter on mixing characteristics

RK Soni, A De - Journal of Mechanical Science and Technology, 2017 - Springer
The strut-based injector has been found to be one of the most promising injector designs for
a supersonic combustor, offering enhanced mixing of fuel and air. The mixing and flow field …

Experimental and numerical studies of a strut injector for round scramjet combustors

C Rock, J Schetz, R Ungewitter - 16th AIAA/DLR/DGLR International …, 2009 - arc.aiaa.org
In view of the very high freestream velocity of scramjets reaching Mach 10, fuel residence
time is on the order of milliseconds1 and supersonic combustion presents a challenge in …

Effect of inner strut on mass diffusion and mixing efficiency of cross fuel jet inside the scramjet combustor

Z Li, J Leng, NH Abu-Hamdeh, MN Ajour… - … Communications in Heat …, 2023 - Elsevier
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 …

Computational study of the coaxial air and fuel jet through a 3-lobe strut injector for efficient fuel mixing in a supersonic combustion chamber

NB Ali, A Basem, P Ghodratallah, PK Singh, KT Falih… - Energy, 2024 - Elsevier
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 …

Numerical simulation of the internal and external flowfields of a scramjet fuel strut injector including conjugate heat transfer

B Rust, P Gerlinger, JM Lourier, M Aigner… - 17th AIAA International …, 2011 - arc.aiaa.org
N supersonic combustion chambers, fast mixing of fuel and air is essential for a stable self
ignition, good combustion performance, and low NOx emissions. Different types of injectors …

[HTML][HTML] Computational simulation of multi-strut central lobed injection of hydrogen in a scramjet combustor

G Choubey, KM Pandey, D Sharma, A Debbarma - Perspectives in Science, 2016 - Elsevier
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 …

Improvement of the fuel mixing of ramp injector system via 4-lobe nozzle at scramjet engine

W Fu, NA Razak, H Wang, X Sun, Z Song - Energy, 2024 - Elsevier
The ramp injection system has been extensively used for the fuel distribution and mixing
inside the combustor of scramjet engines. This article presents a three-dimensional …