Proceedings of the Korean Society of Propulsion Engineers Conference (한국추진공학회:학술대회논문집)
- 2004.03a
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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)
- Published : 2004.03.01
Abstract
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