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覆冰粗糙度对翼型气动特性影响的数值研究

何志辉 张永恒 张旭耀 张沥 李泽 杨文涛

极地研究2023,Vol.35Issue(4):566-579,14.
极地研究2023,Vol.35Issue(4):566-579,14.DOI:10.13679/j.jdyj.20230021

覆冰粗糙度对翼型气动特性影响的数值研究

Numerical study of the effect of ice roughness on the aerodynamic characteristics of symmetric and asymmetric airfoils

何志辉 1张永恒 1张旭耀 1张沥 1李泽 1杨文涛2

作者信息

  • 1. 兰州交通大学,新能源与动力工程学院,甘肃 兰州 730070
  • 2. 三峡新能源太阳山发电有限公司,宁夏 吴忠 751999
  • 折叠

摘要

Abstract

When wind turbines operate in cold regions,the blade is prone to ice formation,which changes the blade's shape and affects its aerodynamic performance.To assess the influence of icing surface roughness on the aerodynamic performance of wind turbine blade airfoils,the aerodynamic characteristics of two types of airfoils,symmetric(NACA-0012)and asymmetric(NACA-23012),were compared under the same icing conditions and icing roughness parameters using a computational fluid dynamics method.The results showed that when rime ice was generated at the leading edge of both NACA0012 and NACA23012 airfoils,the ice roughness had a significant effect on the aerodynamic performance of both icing airfoils.When horn ice was generated at the leading edge of both airfoils,the effect of ice roughness on the aerodynamic per-formance of the NACA23012 icing airfoil was small,and only increased the width of the separation vortex at the trailing edge of the airfoil.There was,a greater effect of horn ice on the NACA0012 airfoil than the NACA23012 airfoil,which delayed the stall angle of attack of NACA0012 icing airfoil.In addition,when rime ice was generated at the leading edge of both NACA0012 and NACA23012 airfoils,the drag coefficient of NACA23012 with rime ice airfoil increased faster than that of NACA0012 icing airfoil.

关键词

风力机/寒冷地区/翼型结冰/覆冰粗糙度/气动性能

Key words

wind turbine/cold regions/airfoil icing/ice roughness/aerodynamic performance

引用本文复制引用

何志辉,张永恒,张旭耀,张沥,李泽,杨文涛..覆冰粗糙度对翼型气动特性影响的数值研究[J].极地研究,2023,35(4):566-579,14.

基金项目

国家自然科学基金地区基金(51566007)资助 (51566007)

极地研究

OA北大核心CSCDCSTPCD

1007-7073

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