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On the nonlinear dynamics of shell structures: Combining a mixed finite element formulation and a robust integration scheme

机译:关于壳结构的非线性动力学:结合混合有限元公式和鲁棒积分方案

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In this work, we present an approach to analyze the nonlinear dynamics of shell structures, which combines a mixed finite element formulation and a robust integration scheme. The structure is spatially discretized with extensible-director-based solid-degenerate shells. The semi-discrete equations are temporally discretized with a momentum-preserving, energy-preserving/decaying method, which allows to mitigate the effects due to unresolved high-frequency content. Additionally, kinematic constraints are employed to render structural junctions. Finally, the method, which can be used to analyze blades of wind turbines or wings of airplanes effectively, is tested and its capabilities are illustrated by means of examples.
机译:在这项工作中,我们提出了一种分析壳结构非线性动力学的方法,该方法结合了混合有限元公式和鲁棒积分方案。该结构在空间上使用基于可扩展导演的固体简并壳离散化。半离散方程通过动量保持,能量保持/衰减方法在时间上离散,这可以减轻由于未解决的高频含量引起的影响。另外,采用运动学约束来绘制结构连接。最后,测试了可用于有效分析风力涡轮机叶片或飞机机翼的方法,并通过示例说明了其功能。

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