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Profile stall characteristics, aerodynamic damping and design implications for wind turbine blades

机译:轮廓失速特性,空气动力学阻尼以及对风机叶片的设计影响

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Aeroelastic stability of wind turbine blades is considered and design implications are discussed. ^The investigation is motivated by recent concern on destructive 'edgewise' vibrations of modern, half-megawatt scale, blades. ^The work has two parts. ^First, results from an investigation on a one-section model problem are presented. ^The model is derived combining a spring-mass-damper equivalent of the structure with 'nonstationary' aerodynamics based on a linearized version of the ONERA dynamic stall model. ^The stability characteristics are then investigated in terms of the defining non-dimensional structural and aerodynamic parameters. ^In the second part, a full blade investigation is undertaken. ^The aerodynamic modeling includes wake induced effects whereas stall is not linearized. ^This direct approach permits to check the trends and indications from the first part on a commercial blade using a state of the art aeroelastic model. ^A parametric investigation is carried out with respect to the poststall behavior of the airfoils in the outboard region as well as with respect to the basic flap and edge eigenfrequencies. ^The paper presents the results of this study and discusses the corresponding design implications. ^(Author)
机译:考虑了风力涡轮机叶片的空气弹性稳定性,并讨论了设计意义。 ^最近对现代半兆瓦级叶片的破坏性“边缘”振动的关注推动了这项研究。 ^作品分为两个部分。 ^首先,给出了对单部分模型问题的调查结果。 ^基于ONERA动态失速模型的线性化版本,该模型是将结构的弹簧-质量-阻尼器等效物与“非平稳”空气动力学相结合而得出的。然后根据定义的无量纲结构和空气动力学参数研究稳定性特征。 ^在第二部分中,进行了全面的刀片调查。 ^空气动力学模型包括尾流诱发的影响,而失速未线性化。 ^这种直接方法允许使用最新的气动弹性模型从商用叶片的第一部分检查趋势和指示。 ^针对机翼在外侧区域的失速行为以及基本襟翼和边缘本征频率进行了参数研究。 ^本文介绍了这项研究的结果,并讨论了相应的设计含义。 ^(作者)

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