Proceedings of the Korean Society of Propulsion Engineers Conference (한국추진공학회:학술대회논문집)
- 2008.03a
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- Pages.756-760
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- 2008
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- 1975-342X(pISSN)
A Design Optimization Study of Diffuser Shape in a Supersonic Inlet
- Lim, S. (School of Mechanical Engineering, Yeungnam University) ;
- Koh, D.H. (School of Mechanical Engineering, Yeungnam University) ;
- Kim, S.D. (School of Automotive, Industrial and Mechanical Engineering, Daegu University) ;
- Song, D.J. (School of Mechanical Engineering, Yeungnam University)
- Published : 2008.03.30
Abstract
Optimum shape of Double-cone supersonic inlet is studied by using numerical methods. Double-cone intake shape is used for the design optimization study. And the total pressure recovery at the exit is used to assess the aerodynamic performance of the inlet.