Experimentation of premixed rotating detonation engine using variable slot feed plenum

摘要

A premixed supply of fuel and oxidizer was fed through five concentric feed slots and detonated in a rotating detonation engine, representing the first known successful airbreathing premixed rotating detonation engine. The premixed feed system successfully arrested flashback. An operating map was constructed and compared to a nonpremixed rotating detonation engine. Mixing effects were shown to be important by comparing measured wave speeds to theoretical Chapman-Jouguet detonation velocities, published computational fluid dynamics results, and similar nonpremixed rotating detonation engines. High-speed imagery indicated that the wave speed measurements should account for the circumferential velocity of the gases relative to the detonation and that the Chapman-Jouguet calculation should account for partial mixing with combustion products.