Numerical analysis of unsteady compressor performance under boundary conditions caused by pulsed detonation combustion

DOI10.1007/978-3-030-90727-3_17OpenAlexW3212085668MaRDI QIDQ2094205

Tim Rähse, Panagiotis Stathopoulos, Nicolai Neumann, Dieter Peitsch

Publication date: 28 October 2022

Full work available at URL: https://doi.org/10.1007/978-3-030-90727-3_17

zbMATH Keywords

pressure gain combustioncompressor performanceunsteady 1D-Euler simulation

Mathematics Subject Classification ID

Gas dynamics (general theory) (76N15) Combustion (80A25) Reaction effects in flows (76V05) Basic methods in fluid mechanics (76Mxx)

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