한국추진공학회:학술대회논문집 (Proceedings of the Korean Society of Propulsion Engineers Conference)
- 한국추진공학회 2008년 영문 학술대회
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- Pages.480-485
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- 2008
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- 1975-342X(pISSN)
Preliminary Design of Movable Air-Turbo Ramjet Engine Intake
- Lee, Kyung-Jae (Korea Aerospace Research Institute, Advanced Propulsion System Department) ;
- Kang, Sang-Hun (Korea Aerospace Research Institute, Advanced Propulsion System Department) ;
- Lee, Yang-Ji (Korea Aerospace Research Institute, Advanced Propulsion System Department) ;
- Yang, Soo-Seok (Korea Aerospace Research Institute, Advanced Propulsion System Department) ;
- Lee, Dae-Sung (Korea Aerospace Research Institute, Aeronautics Program Office) ;
- Kwak, Jae-Su (Korea Aerospace University, Aerospace & Mechanical Engineering Department)
- 발행 : 2008.03.30
초록
In this study, two types of ramjet intake were designed for the flight condition of Mach number 2 and 5 and numerical analysis was performed. In order to widen the flight envelope range(Mach number