Computational study of transverse oblique injectors for improvement of fuel mixing in scramjet engine of supersonic vehicles

Author:

Wang Haicui,Ma Zhimin,Bian Jing,Cao Liang,Tan Ji-Ke,Li Dong

Publisher

Elsevier BV

Reference36 articles.

1. The impact of inner air jet on fuel mixing mechanism and mass diffusion of single annular extruded nozzle at supersonic combustion chamber;Shang;Int Commun Heat Mass Tran,2023

2. Comparison of the different shapes of extruded annular nozzle on the fuel mixing of the hydrogen jet at supersonic combustion chamber;Li;Energy,2023

3. The influence of the struts on mass diffusion system of lateral hydrogen micro jet in combustor of scramjet engine: numerical study;Ma;Energy,2023

4. Influence of coaxial fuel–air jets on mixing performance of extruded nozzle at supersonic combustion chamber: numerical study;Shi;Phys Fluids,2023

5. Aerodynamic heating in supersonic and hypersonic flows: advanced techniques for drag and aero-heating reduction;Gerdroodbary,2022

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