首页> 外文会议>ASME/JSME Joint Fluids Engineering Conference >NUMERICAL ANALYSIS OF YAWED INFLOW EFFECTS ON A HAWT ROTOR
【24h】

NUMERICAL ANALYSIS OF YAWED INFLOW EFFECTS ON A HAWT ROTOR

机译:HAWT转子撕裂流入效应的数值分析

获取原文
获取外文期刊封面目录资料

摘要

We describe a method of calculating yawed inflow effects on horizontal axis wind turbine rotors. Yawed inflow brings about asymmetric induced velocity distributions on the rotor plane due to inclined vortex wake constructions. Along with the effect from the undisturbed wind velocity components in the rotor plane, the asymmetric induced velocity gives rise to a periodically fluctuating load on the rotor blade. For the calculation of yawed inflow phenomena, an inviscid aerodynamic model based on the asymptotic acceleration potential method is adopted, where the rotor blades are represented by spanwise and chordwise pressure distributions composed of analytical first-order asymptotic solutions for the Laplace equation. Combined with dynamic stall models, the yawed inflow effects on the HAWT rotor have been calculated and compared with the experimental results. The calculation of the interaction between the structural dynamics and the aerodynamics has been also attempted for the flapwise oscillation of the rotor blade with flexibility at the root.
机译:我们描述了一种计算横轴风力涡轮机转子的偏航流入效应的方法。随着涡旋唤醒结构,随着涡旋唤醒结构,随着涡旋唤醒结构,撕裂的流入带来了转子平面上的不对称感应速度分布。随着来自转子平面中未受干扰的风速分量的影响,不对称诱导速度导致转子叶片上的周期性波动。为了计算Rawed流入现象,采用基于渐近加速度潜在方法的反式空气动力学模型,其中转子叶片由由Laplace方程的分析一阶渐近溶液组成的翼展和赤曲线压力分布。结合动态失速型号,已经计算了HAWT转子对HAWT转子的偏航流入效果并与实验结果进行了比较。还试图计算结构动力学和空气动力学之间的相互作用,用于转子叶片的浮动振荡,在根部的柔韧性。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号