The usage of non-aligned multi-circular winding injectors for efficient fuel mixing inside the scramjet engine

Author:

Ben Ali Naim,Basem Ali,Ghodratallah Pooya,Singh Pradeep Kumar,jasim Dheyaa J.,Sultan Abbas J.,Eladeb Aboulbaba,Kolsi Lioua,El-Shafay A.S.

Publisher

Elsevier BV

Reference48 articles.

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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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