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NPU-WA系列风力机翼型设计与风洞实验

乔志德 宋文萍 高永卫

空气动力学学报2012,Vol.30Issue(2):260-265,6.
空气动力学学报2012,Vol.30Issue(2):260-265,6.

NPU-WA系列风力机翼型设计与风洞实验

Design and experiment of the NPU-WA airfoil family for wind turbines

乔志德 1宋文萍 1高永卫1

作者信息

  • 1. 西北工业大学,翼型、叶栅空气动力学国家重点实验室,陕西西安710072
  • 折叠

摘要

Abstract

NPU-WA airfoil family is designed for MW-size wind turbines and it is featured by advanced aerodynamic performance at high lift and high Reynolds number. Wind tunnel tests show that the airfoils are of higher lift to drag ratio than present wind turbine airfoils at high lift and high Reynolds number and insen-sitivity of maximum lift to leading edge roughness, which are satisfied the main design requirements. From this study the NPU-WA airfoil data base including geometry and the wind tunnel test performance at Reynolds number from 1. 0×106-5. 0×106 are developed. The airfoils can be applied to MW-size wind turbine design for the China industry with independent intellectual property rights.

关键词

NPU-WA翼型族/翼型设计/风洞实验

Key words

NPU-WA airfoil family/ airfoil design/ wind tunnel test

分类

能源科技

引用本文复制引用

乔志德,宋文萍,高永卫..NPU-WA系列风力机翼型设计与风洞实验[J].空气动力学学报,2012,30(2):260-265,6.

基金项目

国家高技术研究发展计划(863计划)(2007AA052448) (863计划)

空气动力学学报

OA北大核心CSCDCSTPCD

0258-1825

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