Effect of tip speed ratio of rear stage impeller on the performance of contra-rotating wind turbine

被引:0
|
作者
Li, Zhiqiang [1 ]
Li, Zhiming [1 ]
机构
[1] Beihang Univ, Sch Energy Power Engn, Natl Key Lab Sci & Technol Aeroengine Aerothermod, Beijing 100191, Peoples R China
来源
PROCEEDINGS OF THE 3RD INTERNATIONAL CONFERENCE ON ADVANCES IN ENERGY AND ENVIRONMENTAL SCIENCE 2015 | 2015年 / 31卷
关键词
wind power; contra-rotating wind turbine; tip speed ratio; numerical simulation;
D O I
暂无
中图分类号
TE [石油、天然气工业]; TK [能源与动力工程];
学科分类号
0807 ; 0820 ;
摘要
Based on the experimental research and numerical calculation of the Contra-Rotating Wind Turbine (CRWT) by using the technique of the aero-engine and propeller, the effect of the tip speed ratio of the rear stage on the performance of the contra-rotating wind turbine is studied by using numerical simulation method in this paper. The computational results show that there is an optimal tip speed ratio on the rear stage of the contra-rotating wind turbine under medium wind speed in order to achieve the highest output power. Below the optimal value, boundary layer separation of the rotor blade is serious, output power is lower, and output torque is larger; above the optimal value, the opposite situation occurs. Through analyzing the computational results, the optimal value of tip speed ratio of rear stage impeller is 1.667.
引用
收藏
页码:1003 / 1007
页数:5
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