한국추진공학회:학술대회논문집 (Proceedings of the Korean Society of Propulsion Engineers Conference)
- 한국추진공학회 2004년도 제22회 춘계학술대회논문집
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- Pages.699-702
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- 2004
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- 1975-342X(pISSN)
Study on the Affects of Mounting Axisymmetric Inlet to Airframe
- Ando, Yohei (Graduate School of Science and Technology, Keio University) ;
- Matsuo, Akiko (Department of Mechanical Engineering, Keio University) ;
- Kojima, Takayuki (Institute of Space Technology and Aeronautics (ISTA), Japan Aerospace) ;
- Maru, Yusuke (Graduate School of Engineering, The University of Tokyo) ;
- Sato, Tetsuya (Institute of Space Technology and Aeronautics (ISTA), Japan Aerospace)
- 발행 : 2004.03.01
초록
In this study, the affect of mounting axisymmetrical supersonic inlet to airfoil, which has 65 degree swept angle was numerically investigated. The parameter for this calculation are tree stream Mach number M=2.0 and 2.5, the distance between inlet spike and airfoil lower surface