首页> 外文会议>AIAA/CEAS aeroacoustics conference >Trailing Edge Noise Prediction of Wind Turbine Airfoils: A Benchmark Exercise
【24h】

Trailing Edge Noise Prediction of Wind Turbine Airfoils: A Benchmark Exercise

机译:风力机翼型的后缘噪声预测:基准测试

获取原文
获取外文期刊封面目录资料

摘要

This paper presents a trailing edge noise prediction study of two state-of-the-art wind turbine airfoils, benchmarked against dedicated aerodynamic and acoustic wind tunnel experiments. Blind predictions were carried out by three institutes with long experience in trailing edge noise simulation: the German Aerospace Centre (DLR), the Danish Technical University (DTU), and the Institute of Aerodynamics and Gas Dynamics (IAG) at the University of Stuttgart. Experimental data and engineering predictions were provided by Siemens Gamesa Renewable Energy (SGRE). While the aerodynamic predictions generally show good agreement, the acoustic results of the different codes exhibit substantial scatter, even in terms of relative sound pressure levels. This means that for industrial design decisions, where high accuracy is needed (<1 dB), evaluation of the trailing edge noise for different airfoils still requires the combined application of measurement and simulation tools. Both techniques feature inherent uncertainties and scatter which currently cannot meet the targeted accuracy.
机译:本文介绍了两种最先进的风力涡轮机翼型的后缘噪声预测研究,以专用的空气动力学和声学风洞实验为基准。盲预测是由在后缘噪声模拟方面具有丰富经验的三个研究所进行的:德国航空航天中心(DLR),丹麦技术大学(DTU)和斯图加特大学的空气动力学和气体动力学研究所(IAG)。实验数据和工程预测由西门子歌美a可再生能源(SGRE)提供。尽管空气动力学预测通常显示出良好的一致性,但不同代码的声学结果甚至在相对声压级方面也表现出很大的分散性。这意味着对于需要高精度(<1 dB)的工业设计决策,评估不同翼型的后缘噪声仍然需要结合使用测量和仿真工具。两种技术都具有固有的不确定性和分散性,目前无法满足目标精度。

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