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Intelligent Finite Element Method Applied to Design of Actual Composite Structures

机译:智能有限元方法在实际组合结构设计中的应用

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摘要

A computer program of three-dimensional intelligent finite element method by using shell elements has been developed in order to obtain the optimum fiber orientation and the optimum stacking symmetric of laminate composites. The developed computer program can treat a balanced symmetric laminate composites. The design object to determine the fiber orientation and the stacking sequence is the strength of laminate. The strength is evaluated by the F-value of each lamina based on Hoffman's failure criterion. And the optimum fiber orientation and the optimum stacking sequence are determined by the minimum thickness with the F-value satisfying the allowable value. As the numerical examples for actual structures, the determination of fiber orientation in each layer for a cylindrical pipe and a T-type structural component under combined load has been carried out. In the case of cylindrical pipe under three loading conditions suck as the combined internal pressure and tensile load, the only torsion load and the combined torsional and tensile load, the optimum laminates to withstand hoop stress, axial stress and shearing stress for each loading condition were obtained. Then, the optimum laminates of T-type structural component for each loading condition were estimated by using the initial fracture load. As the result, it is recognized that the proposed method is very useful for the structural design of composites.
机译:为了获得层压复合材料的最佳纤维取向和最佳堆叠对称性,开发了一种使用壳单元的三维智能有限元方法的计算机程序。开发的计算机程序可以处理平衡的对称层压复合材料。确定纤维取向和堆叠顺序的设计目标是层压材料的强度。强度是根据霍夫曼破坏准则由每个薄层的F值评估的。最佳的纤维取向和最佳的堆叠顺序由最小厚度确定,其中F值满足允许值。作为实际结构的数值示例,已经确定了在组合载荷下圆柱管和T型结构部件的每一层中的纤维取向。对于圆柱形管,在三种载荷条件下,由于内部压力和拉伸载荷,唯一的扭转载荷以及扭转和拉伸载荷的共同作用,在每种载荷条件下承受环向应力,轴向应力和剪切应力的最佳层压板为获得。然后,通过使用初始断裂载荷估算出每种载荷条件下的最佳T型结构部件层压板。结果,认识到所提出的方法对于复合材料的结构设计非常有用。

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