...
首页> 外文期刊>Engineering Applications of Computational Fluid Mechanics >Numerical Study of Flow Around Iced Wind Turbine Airfoil
【24h】

Numerical Study of Flow Around Iced Wind Turbine Airfoil

机译:风力涡轮机翼型绕流的数值研究

获取原文
           

摘要

AbstractThis investigation analyzes the impact of ice accretion on the aerodynamic coefficients of a wind turbine airfoil. Three blade sections located at different radial positions were analyzed. Numerical simulations were conducted over a two-dimensional clean and ice-accreted NACA 63–415 airfoil at various angles of attack. The results for pressure, lift, and drag coefficients were inspected at an angle of 13° for which experimental data were available. The streamlines around the clean and iced airfoil were also inspected, in order to evaluate the ice impact on lift and drag. The simulations were carried out using the commercial package FLUENT, and turbulence was addressed with the SST k - ω) model.
机译:摘要这项研究分析了积冰对风力涡轮机翼型气动系数的影响。分析了位于不同径向位置的三个叶片部分。对二维洁净且积冰的NACA 63-415机翼以不同的迎角进行了数值模拟。压力,升力和阻力系数的结果以13°的角度进行检查,可获得实验数据。还检查了干净和结冰的机翼周围的流线,以评估结冰对升力和阻力的影响。使用商业软件包FLUENT进行了仿真,并使用SST k-ω)模型解决了湍流问题。

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