The influence of the struts on mass diffusion system of lateral hydrogen micro jet in combustor of scramjet engine: Numerical study

L Ma, X Liu, H Liu, A Alizadeh, M Shamsborhan - Energy, 2023 - Elsevier
The mechanism of fuel injection and system of fuel mixing have a crucial effect in the
combustion process in scramjet engines. The present study discusses the injection of fuel …

Influence of lateral single jets for thermal protection of reentry nose cone with multi-row disk spike at hypersonic flow: computational study

Y Shi, Q Cheng, A Alizadeh, H Yan, G Choubey… - Scientific Reports, 2023 - nature.com
The main challenge for the advancement of current high-speed automotives is aerodynamic
heating. In this study, the application of lateral jet for thermal protection of the high-speed …

Comparison of the different shapes of extruded annular nozzle on the fuel mixing of the hydrogen jet at supersonic combustion chamber

Y Li, G Zhu, Y Chao, L Chen, A Alizadeh - Energy, 2023 - Elsevier
The fuel mixing mechanism is a critical aspect of the propulsion system of hypersonic
vehicles. This study aimed to comprehensively investigate a novel jet configuration that …

Influence of coaxial fuel–air jets on mixing performance of extruded nozzle at supersonic combustion chamber: Numerical study

X Shi, D Song, H Tian, A Alizadeh, MA Ali… - Physics of …, 2023 - pubs.aip.org
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 …

The impact of inner air jet on fuel mixing mechanism and mass diffusion of single annular extruded nozzle at supersonic combustion chamber

S Shang, G Sun, Z Yu, A Alizadeh, MA Ali… - … Communications in Heat …, 2023 - Elsevier
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 …

Numerical investigation of compressible flow around nose cone with multi-row disk and multi coolant jets

R Iranmanesh, A Alizadeh, M Faraji, G Choubey - Scientific Reports, 2023 - nature.com
Due to sever aerodynamic heating, the protection of forebody of scramjet is crucial for
hypersonic flight. In present work, a new cooling system is proposed and investigated for the …

Computational study of the cavity flow over sharp nose cone in supersonic flow

F Pish, TD Manh, MB Gerdroodbary… - … Journal of Modern …, 2020 - World Scientific
Heat and drag reduction on the nose cone is a significant issue for increasing the speed of
the supersonic vehicles. In this paper, computational fluid dynamic method is applied to …

Usage of extruded diamond multi-injectors for improvement of fuel mixing inside the supersonic combustion chamber

H Seraj, F Hosseinnejad, Y Rostamiyan, K Fallah - Scientific Reports, 2023 - nature.com
The main attention of this work is to investigate the usage of diamond multi extruded
injectors on the fuel distribution in combustor of scramjet. This study applied the …

Improvement of fuel mixing of single ejected 2-lobe fuel injector using shock generator at supersonic flow

H Seraj, F Hosseinnejad, Y Rostamiyan… - International Journal of …, 2024 - Elsevier
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 …

Using shock generator for the fuel mixing of the extruded single 4-lobe nozzle at supersonic combustion chamber

A Alizadeh, DJ Jasim, N Sohrabi, M Ahmed… - Scientific Reports, 2024 - nature.com
The importance of the fuel injection configuration on the propulsion efficiency of high-speed
vehicles is apparent. In this article, the use of an annular extruded 4-lobe nozzle for the …