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A continuity re-relaxed thin shell formulation for static and dynamic analyses of linear problems

机译:连续性再松弛的薄壳公式,用于线性问题的静态和动态分析

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This paper presents a curvature-constructed triangular element for static, free vibration and explicit dynamic analyses of shell structures by using a continuity re-relaxed technique. In the present method, the formulation is based on the classical thin shell theory, and only the translational displacements are treated as the filed variables that are assumed piecewisely linear. A set of three-node triangular background cells is adopted to discretize the problem domain. The curvature field in an element is constructed using the continuity re-relaxed technique, which can relax the continuity requirement of the trial function. The membrane strain filed is formulated same as the practice of standard FEM. Based on the principle of virtual work, the discertized system equations are finally formed. As the rotational displacements are not considered as the basic degrees of freedom, the essential boundary conditions of this part are imposed in the process of forming the curvature field. In order to validate the efficiency and accuracy of the present method, several numerical examples are studied. The results demonstrate that the present formulation can achieve very stable and accurate solutions with the less consuming of CPU time.
机译:本文提出了一种曲率构造的三角形单元,通过使用连续性再松弛技术对壳体结构进行静态,自由振动和显式动力分析。在本方法中,该公式基于经典的薄壳理论,并且仅将平移位移视为假定为分段线性的场变量。采用一组三节点三角形背景单元来离散问题域。单元中的曲率场是使用连续性再松弛技术构造的,这可以放宽试验函数的连续性要求。膜应变的配制与标准FEM的实践相同。基于虚拟工作原理,最终形成了离散化的系统方程。由于旋转位移不被视为基本自由度,因此在形成曲率场的过程中会施加该部分的基本边界条件。为了验证本方法的效率和准确性,研究了几个数值示例。结果表明,本发明的配方可以实现非常稳定和准确的解决方案,并且减少了CPU时间的消耗。

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