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

被引:107
作者
Herrema, Austin J. [1 ]
Johnson, Emily L. [1 ]
Proserpio, Davide [2 ]
Wu, Michael C. H. [1 ]
Kiendl, Josef [2 ]
Hsu, Ming-Chen [1 ]
机构
[1] Iowa State Univ, Dept Mech Engn, 2025 Black Engn, Ames, IA 50011 USA
[2] Norwegian Univ Sci & Technol, Dept Marine Technol, O Nielsens Veg 10, N-7052 Trondheim, Norway
基金
美国国家科学基金会;
关键词
Isogeometric analysis; Kirchhoff-Love shell; Patch coupling; Penalty parameter; Non-matching interface; Wind turbine blade; FLUID-STRUCTURE INTERACTION; THIN SHELLS; FORMULATIONS; NURBS;
D O I
10.1016/j.cma.2018.08.038
中图分类号
T [工业技术];
学科分类号
08 ;
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.
引用
收藏
页码:810 / 840
页数:31
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