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Nonlinear aeroelastic response of wind turbines using Simo-Vu-Quoc rods

机译:使用Simo-Vu-Quoc杆的风力涡轮机的非线性气动弹性响应

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A methodology is presented to obtain the nonlinear aeroelastic response of horizontal axis wind turbines using accurate and computationally efficient aerodynamic and structural descriptions. For computing the geometrically nonlinear deformations of the rotor blades, we employ Simo-Vu-Quoc’s geometrically exact finite-strain spatial rod model, which treats the displacements of the beam reference line and the rotations of the cross-section as configuration variables, without any restrictions on their magnitudes or those of the resulting 1-D strain measures. The structural description is Lagrangian, obviating the need for an explicit definition of centrifugal/coriolis forces. Towards the aerodynamic side, Blade Element Momentum Theory enhanced with several important corrections is employed, along with a dynamic stall model that accounts for the unsteady effects. A comprehensive treatment of the aeroelastic computations within the restrictions imposed by the aerodynamic theory is presented with the aid of a ‘shadow’ frame of reference rotating rigidly with the deforming blades. A novel strategy ‘primes’ the aeroelastic solver by moderating the response of rotor in its acceleration phase. An integrated MATLAB toolWindGEARincorporating the two coupled codes is developed to simulate the fully-coupled aeroelastic response of the NREL 5 MW wind turbine. The results, when compared with published data, establish WindGEAR firmly as a robust wind turbine nonlinear aeroelastic analysis tool in time-domain.
机译:提出了一种使用精确且计算效率高的空气动力学和结构描述来获得水平轴风力涡轮机的非线性空气弹性响应的方法。为了计算转子叶片的几何非线性变形,我们采用Simo-Vu-Quoc的几何精确有限应变空间杆模型,该模型将梁参考线的位移和横截面的旋转视为配置变量,而没有任何限制其大小或所产生的一维应变度量的大小。结构上的描述是拉格朗日式,不需要明确定义离心力/科里奥利力。在空气动力学方面,采用了经过多次重要修正后增强的叶片元素动量理论,以及考虑了非稳态影响的动态失速模型。在空气动力学理论施加的限制范围内,借助变形叶片刚性旋转的“影子”参照系,对空气弹性计算进行了全面处理。一种新颖的策略是通过调节转子在加速阶段的响应来“灌注”气动弹性求解器。开发了集成了两个耦合代码的集成MATLAB工具WindGEAR,以模拟NREL 5 MW风力涡轮机的完全耦合气动弹性响应。与已发布的数据相比,该结果将WindGEAR牢固地确立为时域中强大的风力涡轮机非线性气动弹性分析工具。

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