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Real-time prediction of aeroelastic loads of wind turbine blades in gusty and turbulent wind using an improved load model

机译:使用改进的负荷模型实时预测大风和湍流风中风力涡轮机叶片的空气弹性负荷

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摘要

The traditional method of flutter analysis of wind turbine blades employs a mixed-domain (frequency and time- domain) formulation for self-excited aerodynamic loads, because flutter derivatives are functions of reduced frequencies. However, a time-domain formulation for self-excited and buffeting loads allows the equations of motion to be continuously solved for response time histories of wind turbine blades below flutter speed and captures the transient response in gusty and turbulent winds. The rational function coefficients and buffeting indicial function coefficients that appear in the time-domain formulation were previously extracted for the NREL 5830 airfoil section model in a wind tunnel. The objective of the current study is to evaluate how well these experimentally extracted coefficients can predict the aerodynamic loads on a blade in different wind conditions, through a separate set of tests conducted on a much larger (3.3 times) section model of the blade in a larger wind tunnel than originally used. The measured loads (lift and moment) were used to validate simulated loads using the time domain load prediction procedure. To improve the correlation between the measured and predicted loads, an improved loads model was developed using an additional lag term and its performance is presented in smooth, gusty and turbulent wind. An aeroelastic model test of a HAWT blade in a wind tunnel was used for further validation showing the efficacy of the loads model. (C) 2017 Elsevier Ltd. All rights reserved.
机译:风力涡轮机叶片颤振分析的传统方法采用混合域(频域和时域)公式表示自激空气动力载荷,因为颤振导数是降低频率的函数。但是,针对自激和抖振载荷的时域公式使运动方程能够针对风振速度以下的风力涡轮机叶片的响应时间历史连续求解,并捕获了阵风和湍流风的瞬态响应。预先提取了在时域公式中出现的有理函数系数和抖振指标函数系数,用于风洞中的NREL 5830机翼截面模型。当前研究的目的是通过对一组更大(3.3倍)叶片截面模型进行的单独测试,评估这些通过实验提取的系数在不同风况下可以预测叶片上的空气动力负荷的能力。比原来使用的风洞更大。使用时域负荷预测程序,将测得的负荷(升力和力矩)用于验证模拟负荷。为了改善实测负荷与预测负荷之间的相关性,使用附加的滞后项开发了改进的负荷模型,并在平稳,阵风和湍流风中表现了其性能。在风洞中对HAWT叶片进行了气动弹性模型测试,进一步验证了载荷模型的有效性。 (C)2017 Elsevier Ltd.保留所有权利。

著录项

  • 来源
    《Engineering Structures》 |2017年第15期|103-113|共11页
  • 作者单位

    Iowa State Univ, Dept Aerosp Engn, 1200 Howe Hall,537 Bissell Rd, Ames, IA 50011 USA;

    Iowa State Univ, Dept Aerosp Engn, 1200 Howe Hall,537 Bissell Rd, Ames, IA 50011 USA;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
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