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低噪声风力机翼型设计方法及实验分析

汪泉 陈进 程江涛 王君 孙金风 游颖

汪泉, 陈进, 程江涛, 等 . 低噪声风力机翼型设计方法及实验分析[J]. 北京航空航天大学学报, 2015, 41(1): 23-28. doi: 10.13700/j.bh.1001-5965.2014.0072
引用本文: 汪泉, 陈进, 程江涛, 等 . 低噪声风力机翼型设计方法及实验分析[J]. 北京航空航天大学学报, 2015, 41(1): 23-28. doi: 10.13700/j.bh.1001-5965.2014.0072
WANG Quan, CHEN Jin, CHENG Jiangtao, et al. Wind turbine airfoil design method with low noise and experimental analysis[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(1): 23-28. doi: 10.13700/j.bh.1001-5965.2014.0072(in Chinese)
Citation: WANG Quan, CHEN Jin, CHENG Jiangtao, et al. Wind turbine airfoil design method with low noise and experimental analysis[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(1): 23-28. doi: 10.13700/j.bh.1001-5965.2014.0072(in Chinese)

低噪声风力机翼型设计方法及实验分析

doi: 10.13700/j.bh.1001-5965.2014.0072
基金项目: 国家自然科学基金资助项目(51405140);国家863计划资助项目(2012AA051301);湖北工业大学博士科研启动金资助项目(BSQD13016)
详细信息
    通讯作者:

    汪泉(1984-),男,湖北武汉人,讲师, quan_wang2003@163.com,主要研究方向为机械系统优化设计及可再生能源装备设计理论与方法.

  • 中图分类号: TK83;TH12

Wind turbine airfoil design method with low noise and experimental analysis

  • 摘要: 为了研究风力机翼型的噪声特性,基于翼型泛函集成理论与翼型噪声计算模型,建立了低噪声翼型优化设计数学模型,提出在设计攻角情况下升阻比与噪声比值最大为目标函数,对优化后的新翼型CQU-DTU-B18翼型与NACA-64-618翼型在相同的风洞实验及风速条件下进行了噪声对比分析.研究表明,理论噪声计算模型虽然与实验数据有一定的偏差,但是翼型的升压级随频率的变化趋势是一致的,表明了翼型噪声计算模型的准确性;相比NACA-64-618翼型,CQU-DTU-B18翼型具有更低的噪声特性,从而验证了该设计方法的可行性.对于如何设计低噪声翼型及怎样降低翼型噪声具有重要的指导作用.

     

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出版历程
  • 收稿日期:  2014-02-24
  • 网络出版日期:  2015-01-20

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