The effect of rotor blade shape on the performance of the Wells turbine

被引:0
|
作者
Webster, M [1 ]
Gato, LMC
机构
[1] Coventry Univ, Sch Engn, Coventry, W Midlands, England
[2] Inst Super Tecn, Lisbon, Portugal
关键词
Wells turbine; wave energy; turbomachinery; blade section;
D O I
暂无
中图分类号
TU [建筑科学];
学科分类号
0813 ;
摘要
This paper presents an experimental investigation into the effect of blade section on the performance of the Wells turbine. The blades tested included 2 sets of symmetrical constant chord blades: one set bad standard NACA 0015 blades, whilst the other had optimized blades. The aim of the experiments was to investigate and compare the aerodynamic performance of the NACA 0015 and the optimized blades for 2 different rotor solidities.
引用
收藏
页码:227 / 230
页数:4
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