Rotating detonation combustor downstream transition passage design considerations

DOI10.1007/978-3-030-90727-3_11OpenAlexW3211437268MaRDI QIDQ2094189

Donald Ferguson, Guillermo Paniagua, James E. Braun

Publication date: 28 October 2022

Full work available at URL: https://doi.org/10.1007/978-3-030-90727-3_11

zbMATH Keywords

rotating detonation combustorssubsonic passagesupersonic passage

Mathematics Subject Classification ID

General theory of rotating fluids (76U05) Combustion (80A25) Reaction effects in flows (76V05) Basic methods in fluid mechanics (76M99)

Uses Software

• CFD++

Cites Work

• Unnamed Item
• On the transient response of the turbulent boundary layer inception in compressible flows

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