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5. Effect of Rotor Blade Tip Cavity Flow on Aerodynamic Performance of Turbine Stages

Effect of Rotor Blade Tip Cavity Flow on Aerodynamic Performance of Turbine Stages

来源 :第六届亚洲推进与动力国际会议 | 被引量 : 0次 | 上传用户：xiange

【作 者】

：

Jia LIU Jun LI Xin YAN Zhenping FENG 

【机 构】

：

InstituteofTurbomachinery,Xi'anJiaotongUniversity,Xi'an710049,China

【出 处】

：

第六届亚洲推进与动力国际会议

【发表日期】

：

2012年3期

【关键词】

：

Labyrinth Seal Outlet Cavity Size Efficiency Leakage Flow Numerical Simulation 

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