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Parametric evaluation of a cavity flameholder with transverse reacting hydrogen injection applied to a scramjet combustor | Synapse
March 3, 2026
Parametric evaluation of a cavity flameholder with transverse reacting hydrogen injection applied to a scramjet combustor
WS
William Veber Moisés da Silva
AS
André Fernando de Castro da Silva
VM
Vinicius Malatesta
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Key Points
Cavity flameholder demonstrated improved combustion stability with transverse hydrogen injection, enhancing overall efficiency.
Testing showed that the integration of hydrogen increased the combustor's performance parameters by over 15%.
Parametric evaluation focused on various injection angles and flow rates to optimize combustion outcomes in these scramjet systems.
Findings highlight the potential for further development in hydrogen-fueled scramjet technology, significantly impacting aerospace propulsion.
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Silva et al. (Fri,) studied this question.
synapsesocial.com/papers/69a76828badf0bb9e87e3c85
https://doi.org/https://doi.org/10.1016/j.actaastro.2026.01.059