Influence of plasma-enhanced combustion on RBCC engine using URANS
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DOI: 10.1038/s41598-024-81145-z
Abstract: The rocket-based combined-cycle (RBCC) engine is regarded as one of the most viable propulsion systems for single-stage-to-orbit launch vehicles. Because of the relatively low total temperature of the incoming flow, it is difficult to maintain… read more here.
Keywords: combustion; rbcc; mode transition; rbcc engine ... See more keywords