• Proceedings of the Korean Society of Propulsion Engineers Conference
• /
• 2004.03a
• /
• pp.205-210
• /
• 2004

The pulse detonation engine (PDE) has recently expected as a new aerospace propulsion system. The PDE system has high thermal efficiency because of its constant-volume combustion and its simple tube structure. We measured thrust of single-tube pulse detonation rocket (PDR) by two methods using the PDR-Engineering Model (full scale model) for ground testing. The first involved measuring the displacement of the PDR-EM by laser displacement meter, and the second involved measuring the time-averaged thrust by combining a load cell and a spring-damper system. From these two measurements, we obtained 130.1 N of time-averaged thrust, which corresponds to 321.2 sec of effective specific impulse (ISP). As well, we measured the heat flux in the wall of PDE tubes. The heat flux was approximately 400 ㎾/$m^2$. We constructed the PDR-Flight Mode] (PDR-FM). In the vertical flight test in a laboratory, the PDR-FM was flying and keeping its altitude almost constant during 0.3 sec.

• Proceedings of the Korean Society of Computer Information Conference
• /
• 2021.01a
• /
• pp.283-284
• /
• 2021

본 논문에서는 서로 다른 진화 전략의 병렬화를 구현하기 위해 섬 모델을 도입하고 자원 간의 균형을 유지하기 위해 Monod 모델을 활용하는 PDE-EM이라는 생태 모델 알고리즘을 기반으로 한 새로운 병렬 DE를 제안하도록 한다. 각 섬은 동일한 자원으로 서로 다른 전략으로 진화한다. 지정된 세대 수마다 섬의 진화 정도에 따라 등급이 매겨지고, Monod 모델을 활용하여 각 섬에 다양한 자원이 할당된다.