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An efficient computational model for fluid-structure interaction in application to large overall motion of wind turbine with flexible blades

机译:流体-结构相互作用的有效计算模型在具有柔性叶片的风力涡轮机大运动中的应用

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This paper proposes a very efficient computational model for fluid-structure interaction problems corresponding to steady-state flow representing a large overall motion of wind turbines with flexible blades. The model of turbine blades is based upon the 3D solids finite elements with drilling rotations. The proposed 3D solids model is fully able to describe the flexibility blades large overall motion and easily capture both bending and torsional motion thanks to using an enhanced strain field. The model efficiency is further reinforced by using the 3D panel method that fits naturally with proposed 3D solid finite elements for blades. The proposed panel method is the corresponding modification of the potential fluid flow by introducing a vorticity layer at the fluid-structure interface and Bernoulli's conservation momentum equation in order to provide quantification for the blade thrust. The fluid-structure interaction is enforced through an efficient iterative procedure providing on one hand a very fast computation of aerodynamic loads, which is sufficiently accurate for computing the overall thrust on the blade, and on the other hand a sufficiently accurate representation of the stress states suitable for fatigue studies. The proposed computational model performance is illustrated with several numerical simulations, including the practical case of a full-scale NREL 5MW wind turbine. (C) 2019 Elsevier inc. All rights reserved.
机译:本文提出了一个非常有效的计算模型,用于流体-结构相互作用问题,该问题与稳态流相对应,稳态流表示具有柔性叶片的风力涡轮机的整体运动较大。涡轮叶片的模型基于具有钻井旋转的3D实体有限元。所提出的3D实体模型完全能够描述柔性叶片的大整体运动,并且由于使用了增强的应变场,因此可以轻松捕获弯曲和扭转运动。通过使用3D面板方法可以进一步提高模型效率,该方法自然适合建议的3D叶片实体有限元。所提出的面板方法是通过在流体-结构界面处引入涡旋层和伯努利的守恒动量方程式来对潜在的流体流量进行相应的修改,以便对叶片推力进行量化。流体-结构的相互作用通过有效的迭代过程来实现,一方面提供了非常快速的空气动力学载荷计算,对于计算叶片上的总推力而言,该精度足够准确;另一方面,可以充分准确地表示应力状态适合疲劳研究。通过数个数值模拟对拟议的计算模型性能进行了说明,其中包括满量程NREL 5MW风力发电机的实际案例。 (C)2019爱思唯尔公司版权所有。

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