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This study investigates fuel-oxygen mixing and detonation propagation in a linear rotating detonation engine (RDE) using hydrogen and oxygen injected into argon. Experiments revealed that decreasing the channel width from 12 mm to 8 mm resulted in a steady detonation wave with an average velocity of 2140 m/s, attributed to argon dilution. The findings suggest that the observed velocity deficits in operational RDEs may be due to preburning of the fuel-oxygen mixture, which was not present in this controlled

Author
Mek Punyawich
Language
EN