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首页> 外文期刊>Journal of aerospace engineering >Multiscale Method for Geometrical Nonlinear Analysis of Fluid Actuated Cellular Structures with Arbitrary Polygonal Microstructures
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Multiscale Method for Geometrical Nonlinear Analysis of Fluid Actuated Cellular Structures with Arbitrary Polygonal Microstructures

机译:具有任意多边形微观结构的流体驱动蜂窝结构几何非线性分析的多尺度方法

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摘要

Fluid actuated cellular structures are morphing structures inspired by the nastic movement of plants. These materials have a wide array of applications from morphing aircraft wings to soft robotics. The nonlinear shape-morphing behaviors of the fluid actuated cellular structures composed of randomly distributed polygonal motor cells are investigated in this work. A new multiscale modeling framework based on multiscale finite-element methods is proposed to simulate the nonlinear behaviors of such adaptive materials with irregular polygonal microstructures. The multiscale displacement and hydraulic pressure base functions are firstly constructed to establish the relationship between the microstructures of the fluidic actuating cells and the macroscopic deformation on the polygonal coarse-scale mesh. Then, the corotational formulation for geometrically nonlinear analysis is integrated to this multiscale method to decompose the nonlinear deformations of the polygonal coarse-grid element into rigid-body motions and pure deformational displacements. In addition, a master-slave displacement relationship is employed to ensure the displacement continuity at the interface between the polygonal multiscale coarse-grid elements and the traditional fine-scale elements in a same computational model. Several representative examples including a smart wing structure are investigated to validate the accuracy and efficiency of the proposed polygonal multiscale corotational method.
机译:流体驱动的细胞结构是受植物鼻腔运动启发的变形结构。这些材料具有广泛的应用,从变形飞机机翼到软机器人。在这项工作中研究了由随机分布的多边形运动细胞组成的流体驱动细胞结构的非线性形状变形行为。提出了一种基于多尺度有限元方法的多尺度建模框架,以模拟这种具有不规则多边形微观结构的自适应材料的非线性行为。首先构造多尺度位移和液压基函数,以建立流体致动单元的微观结构与多边形粗尺度网格上的宏观变形之间的关系。然后,将几何非线性分析的确定公式集成到此多尺度方法中,以将多边形粗网格元素的非线性变形分解为刚体运动和纯变形位移。另外,在同一计算模型中,采用主从位移关系来确保多边形多尺度粗网格元素与传统细尺度元素之间的界面处的位移连续性。研究了包括智能机翼结构在内的几个代表性示例,以验证所提出的多边形多尺度校正方法的准确性和效率。

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