Rotating detonation engine

A prototype RDE under test at the Marshall Space Flight Center

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]

  1. ^ "More power, no moving parts: The quest to fly a rotating detonation engine".
  2. ^ 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. S2CID 73520772.
  3. ^ Wolanski, Piotr (2013). "Detonative Propulsion". Proceedings of the Combustion Institute. 34 (1): 125–158. Bibcode:2013PComI..34..125W. doi:10.1016/j.proci.2012.10.005.
  4. ^ Птичкин, Сергей (January 18, 2018). "В России испытали модель детонационного двигателя для ракет будущего". Российская газета (in Russian). Retrieved February 10, 2018.
  5. ^ Cao, Huan; Wilson, Donald (2013). "Parametric Cycle Analysis of Continuous Rotating Detonation Ejector-Augmented Rocket Engine". 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. doi:10.2514/6.2013-3971. ISBN 978-1-62410-222-6.
  6. ^ 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.

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