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Penalty coupling of non-matching isogeometric Kirchhoff-Love shell patches with application to composite wind turbine blades

机译:等距Kirchhoff-Love壳体不匹配补丁的惩罚耦合及其在复合材料风力涡轮机叶片中的应用

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摘要

Isogeometric analysis (IGA) has been a particularly impactful development in the realm of Kirchhoff-Love thin-shell analysis because the high-order basis functions employed naturally satisfy the requirement of C-1 continuity. Still, engineering models of appreciable complexity, such as wind turbine blades, are typically modeled using multiple surface patches and, often, neither rotational continuity nor conforming discretization can be practically obtained at patch interfaces. A penalty approach for coupling adjacent patches is therefore presented. The proposed method imposes both displacement and rotational continuity and is applicable to either smooth or non-smooth interfaces and either matching or non-matching discretization. The penalty formulations require only a single, dimensionless penalty coefficient for both displacement and rotation coupling terms, alleviating the problem-dependent nature of the penalty parameters. Using this coupling methodology, numerous benchmark problems encapsulating a variety of analysis types, geometrical and material properties, and matching and non-matching interfaces are addressed. The coupling methodology produces consistently accurate results throughout all tests. Furthermore, the suggested penalty coefficient of alpha = 10(3) is shown to be effective for the wide range of problem configurations addressed. Finally, a realistic wind turbine blade model, consisting of 27 patches and 51 coupling interfaces and having a chordwise- and spanwise-variant composite material definition, is subjected to buckling, vibration, and nonlinear deformation analyses using the proposed approach. (C) 2018 Elsevier B.V. All rights reserved.
机译:等距几何分析(IGA)在Kirchhoff-Love薄壳分析领域中尤其具有影响力,因为采用的高阶基函数自然可以满足C-1连续性的要求。仍然,诸如风力涡轮机叶片之类的具有相当复杂性的工程模型通常使用多个表面补丁来建模,并且通常在补丁界面处实际上无法获得旋转连续性或一致的离散化。因此,提出了一种用于耦合相邻补丁的惩罚方法。所提出的方法强加了位移和旋转连续性,并且适用于光滑或不光滑的界面以及匹配或不匹配的离散化。对于位移和旋转耦合项,惩罚公式仅需要单个无量纲的惩罚系数,从而减轻了惩罚参数的问题相关性。使用这种耦合方法,可以解决封装各种分析类型,几何和材料属性以及匹配和不匹配界面的众多基准问题。在所有测试中,耦合方法都能产生一致准确的结果。此外,建议的惩罚系数α= 10(3)对于解决的各种问题配置均有效。最后,使用提出的方法对包含27个面片和51个耦合界面并具有弦向和跨度变化的复合材料定义的真实的风力涡轮机叶片模型进行屈曲,振动和非线性变形分析。 (C)2018 Elsevier B.V.保留所有权利。

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