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A new doubly-curved shell element for the free vibrations of arbitrarily shaped laminated structures based on Weak Formulation IsoGeometric Analysis

机译:基于弱公式等几何分析的任意形状叠层结构自由振动的双曲壳单元

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The main aim of the paper is to present a new numerical method to solve the weak formulation of the governing equations for the free vibrations of laminated composite shell structures with variable radii of curvature. For this purpose, the integral form of the stiffness matrix is computed numerically by means of the Generalized Integral Quadrature (GIQ) method. A two-dimensional structural model is introduced to analyze the mechanical behavior of doubly-curved shells. The displacement field is described according to the basic aspects of the general Higher-order Shear Deformation Theories (HSDTs), which allow to define several kinematic models as a function of the free parameter that stands for the order of expansion. Since an Equivalent Single Layer (ESL) approach is considered, the generalized displacements evaluated on the shell middle surface represent the unknown variables of the problem, which are approximated by using the Lagrange interpolating polynomials. The mechanical behavior of the structures is modeled through only one element that includes the double curvature in its formulation, which is transformed into a distorted domain by means of a mapping procedure based on the use of NURBS (Non-Uniform Rational B-Splines) curves, following the fundamentals of the well-known Isogeometric Analysis (IGA). For these reasons, the presented methodology is named Weak Formulation Isogeometric Analysis (WFIGA) in order to distinguish it from the corresponding approach based on the strong form of the governing equations (Strong Formulation Isogeometric Analysis or SFIGA), previously introduced by the authors. Several numerical applications are performed to test the current method. The results are validated for different boundary conditions and various lamination schemes through the comparison with the solutions available in the literature or obtained by a finite element commercial software. (C) 2017 Elsevier Ltd. All rights reserved.
机译:本文的主要目的是提出一种新的数值方法,以解决曲率半径可变的层合复合壳结构自由振动控制方程的弱公式。为此,通过广义积分正交(GIQ)方法以数值方式计算刚度矩阵的积分形式。引入二维结构模型来分析双曲壳的力学行为。根据一般的高阶剪切变形理论(HSDT)的基本方面描述了位移场,该理论允许根据代表扩展顺序的自由参数来定义几个运动学模型。由于考虑了等效单层(ESL)方法,因此在壳中间表面上评估的广义位移表示问题的未知变量,这些变量通过使用Lagrange插值多项式来近似。结构的机械行为仅通过一个包含其双曲率的元素进行建模,然后通过基于NURBS(非均匀有理B样条)曲线的映射过程将其转换为扭曲的畴遵循著名的等几何分析(IGA)的基础知识。由于这些原因,本文提出的方法被称为弱公式等几何分析(WFIGA),以便将其与基于先前由作者引入的强控制方程形式(强公式等几何分析或SFIGA)相区别的相应方法。执行了多个数值应用程序以测试当前方法。通过与文献中可用的解决方案比较或通过有限元商业软件获得的解决方案进行比较,可以针对不同的边界条件和各种层压方案验证结果。 (C)2017 Elsevier Ltd.保留所有权利。

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