Proceedings of the Korean Society of Propulsion Engineers Conference (한국추진공학회:학술대회논문집)
- 2003.10a
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- Pages.91-94
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- 2003
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- 1975-342X(pISSN)
Influence of Streamwise Vortices on Normal Shock-Wave/Boundary Layer Interaction
유동방향의 와류가 충격파와 경계층의 상호간섭에 미치는 영향
Abstract
An experimental study has been carried out in a supersonic blow-down wind tunnel for examining the influence of streamwise vortices on normal shock-wave/boundary layer interaction. It has been reported by the earlier investigator the streamwise vortices generated by the blowing jets can significantly suppress the shock-induced separation and reduce the wave drag. The blowing jets generate the streamwise vortices with 45
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