A rotating detonation engine (RDE) uses a form of pressure gain combustion, where one or more detonations continuously travel around an annular channel.[1] Computational simulations and experimental results have shown that the RDE has potential in transport and other applications.[2][3]
In detonative combustion, the flame front expands at supersonic speed. It is theoretically up to 25% more efficient than conventional deflagrative combustion,[4] offering potentially major fuel savings.[5][6]
Disadvantages include instability and noise.[citation needed]
^Lu, Frank; Braun, Eric (July 7, 2014). "Rotating Detonation Wave Propulsion: Experimental Challenges, Modelling, and Engine Concepts". Journal of Propulsion and Power. 30 (5). The American Institute of Aeronautics and Astronautics: 1125–1142. doi:10.2514/1.B34802. S2CID73520772.
^Schwer, Douglas; Kailasanath, Kailas (September 25, 2010). "Numerical Investigation of the Physics of Rotating Detonation Engines". Proceedings of the Combustion Institute. 33 (2). Elsevier, Inc.: 2195–2202. Bibcode:2011PComI..33.2195S. doi:10.1016/j.proci.2010.07.050.