Proceedings of the Korean Society of Propulsion Engineers Conference (한국추진공학회:학술대회논문집)

The Korean Society of Propulsion Engineers (한국추진공학회)
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Rotating Detonation Engine Study in AGU

  • Hayashi, A. Koichi (Department of Mechanical Engineering, Aoyama Gakuin University) ;
  • Uemura, Yuho (Department of Mechanical Engineering, Aoyama Gakuin University) ;
  • Yamada, Takayuki (Department of Mechanical Engineering, Aoyama Gakuin University) ;
  • Yamada, Eisuke (Department of Mechanical Engineering, Aoyama Gakuin University)
  • Published : 2011.11.24
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Abstract

Detonation is useful phenomena to get an effective thrust for aerospace vehicle. Fast pressure rise of detonation provides a cycle close to the constant volume system to use energy efficiently. From this point detonation can be used as an aerospace engine system. There are several types of detonation engine; pulse detonation engine (PDE) which provides a thrust by detonation intermittently, and oblique detonation engine (ODE), spin detonation engine (SDE), and rotating detonation engine (RDE) which, on the other hand, provide a continuous thrust.

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