摘要
引入试验中正交设计的思想,通过数值模拟研究了风力机翼型尾缘襟翼不同参数的影响。采用带有转捩模型的SST k-ω湍流模型模拟了基于S809的尾缘襟翼的尺寸、偏斜角度和形状的影响。结果表明:尾缘襟翼尺寸、偏斜角度对于翼型相关气动参数影响较大,在考查参数范围内折中采用10%弦长、偏斜10°的尾缘襟翼综合性能较好;尾缘襟翼形状函数影响相对较小,采用变化较平缓的尾缘襟翼有利于保持流动稳定性。
Introducing the orthogonal experimental design method, influences of different parameters such as the size, angle and shape, on the wind turbine airfoil S809 with a trailing edge flap are studied using SST k - w turbulence model with a transition model. The results indicate that the flap size and angle have big influences on aerodynamic properties of wind turbine airfoil. Among the studied parameters, the flap with 10% chord length and 10° flap angle obtains better performances. The shape of the flap has relatively smaller influences, but it makes for a stable flowfield using a mildly changing flap shape.
出处
《工程热物理学报》
EI
CAS
CSCD
北大核心
2012年第8期1322-1325,共4页
Journal of Engineering Thermophysics
基金
国家自然科学基金资助项目(No.50876105)
国家自然科学基金重点项目(No.50836006)
关键词
风力机翼型
尾缘襟翼
正交设计
wind turbine airfoil
trailing edge flap
orthogonal design