한국전산유체공학회:학술대회논문집
- 2005.04a
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- Pages.213-218
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- 2005
The Numerical Study on the Supersonic Flow field with a Bump
Bump가 있는 초음속 유동장의 수치적 연구
Abstract
The purpose of this study is the characteristics of an innovative inlet system with shock/boundary layer interactions by using various types of bumps which are substituted for the conventional bleeding system in supersonic inlet. This study performs a comprehensive numerical effort that be directed at better understanding the three-dimensional flowfield includes shock/boundary layer interaction and growth of turbulent boundary layer that occur around a three-dimensional bump in a supersonic inlet. The characteristics of boundary layer seen in the current numerical simulations indicates the potential capability of the three-dimensional bump to control shock/boundary layer interaction in supersonic inlets.
Keywords