Proceedings of the Korean Society of Propulsion Engineers Conference (한국추진공학회:학술대회논문집)
- 2011.11a
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- Pages.830-834
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- 2011
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- 1975-342X(pISSN)
A Numerical Study of Blade Sweep Effect in Supersonic Turbine Rotor
초음속 터빈의 로터 블레이드 스윕 효과에 대한 수치적 연구
- Published : 2011.11.24
Abstract
In this study, we performed three-dimensional CFD analysis to investigate the effect of the rotor blade sweep of a partial admission supersonic turbine on the stage performance and the flow field. The computations are conducted for three different sweep cases, No sweep(NSW), Backward sweep(BSW), and Forward sweep(FSW), using flow analysis program,
본 연구에서는 액체로켓엔진의 터보펌프용 초음속 터빈 로터 블레이드에 스윕 각도
Keywords