Numerical simulation of a methane-oxygen rotating detonation rocket engine

Prakash, S; Raman, V; Lietz, CF; Hargus, WA; Schumaker, SA

Prakash, S (corresponding author), Univ Michigan, Dept Aerosp Engn, Ann Arbor, MI 48109 USA.

PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2021; 38 (3): 3777

Abstract

The rotating detonation engine (RDE) is an important realization of pressure gain combustion for rocket applications. The RDE system is characterized ......

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