Performance evaluation of a backward-facing H2-fueled supersonic combustion chamber with dual-strut injector: efficiency and shock wave analysis

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Computational fluid dynamics analysis reveals efficiency and shock wave interactions in scramjets, indicating design impacts.

High combustion efficiency reached 99.9% at Mach 3 due to optimal strut injector design.
Key performance metrics were measured, focusing on mixing efficiency and shock wave structure.
This study employed computational fluid dynamics simulations using ANSYS Fluent and a Finite-Rate Eddy-Dissipation model.
The findings suggest significant implications for scramjet design and operation, particularly under varying Mach conditions.

Roga et al. (2025) studied this question.

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