Proceedings of the Korean Society of Propulsion Engineers Conference (한국추진공학회:학술대회논문집)
- 2011.11a
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- Pages.1-4
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- 2011
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- 1975-342X(pISSN)
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
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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