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Assessment of Effective Elastic Properties of Honeycomb Cores by Modal Finite Element Analyses

机译:模态有限元分析评估蜂窝核心有效弹性特性

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The main issue in analyzing honeycomb structures is the substantial computational effort that has to be spent in modeling and analyzing them with a multi-cell construction core by maintaining the actual geometry. Therefore, the common practice in the finite element modeling is to replace them by an equivalent orthotropic material. The determinations of these equivalent properties of the homogenized core are based on analytical or numerical relationships usually obtained from pure axial and shearing loads. By using these initial estimations of the equivalent properties, a homogenized model works well for in-plane deformations but may give large errors for out-of plane deformations which generally take place in panel or sandwich homogenized structures. This paper presents a numerical method that can be used to correct some of the equivalent elastic properties of the homogenized core to work properly in bending and torsion based on some modal analyses applied first for a real honeycomb panel, to obtain a reference solution, and then on the homogenized orthotropic panel where some of the equivalent elastic constant are iteratively improved by an optimization algorithm to fit the reference solution. The analyzed types of honeycomb cores are the commercial ones in three cell configurations: square, regular hexagonal and re-entrant shapes. The calculations show that some of the equivalent elastic properties obtained in the classical approach must be corrected with factors larger than five as to obtain correct results in bending and torsion loads.
机译:在分析蜂窝结构的主要问题是,在建模和维护的实际几何结构与多小区建设的核心分析他们花费的大量的计算工作。因此,在有限元建模的通常做法是通过等效正交各向异性材料来取代它们。的均化的芯的等效这些性能的测定是基于通常由纯轴向和剪切载荷获得分析或数字的关系。通过使用相同的性能的这些初始估计,均质化的模型可以很好地用于在平面内的变形,但可能得到大的误差为平面外变形其通常发生在面板或夹层均化结构。本文提出了可用于纠正一些的均化核心工作的等效弹性性能的适当的弯曲和施加的第一一个真正的蜂窝板基于一些模态分析扭转,以获得参比溶液,然后数值方法的均质化正交各向异性面板,其中一些的等效弹性常数的迭代通过最优化算法改进,以适应所述参考溶液上。该分析类型的蜂窝芯的有三种电池配置了商业的:正方形,正六边形和重入的形状。计算结果表明,一些在经典的方法中获得的等效弹性特性的必须以大于5的因素进行校正,以在弯曲和扭转载荷获得正确的结果。

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