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DYNAMIC ANALYSIS OF LAMINATED COMPOSITE SHELLS WITH HOFFMAN YIELD CRITERION

机译:霍夫曼屈服准则的复合层合壳的动力分析。

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This paper presents a numerical study of the dynamic response of composite shells under impulsive loading. The material is modelled by anisotropic Hoffman yield surface, which permits different tensile and compressive strengths. An explicit time-integration algorithm is employed to expedite dynamic analysis. Four-node shell elements with only one Gauss point are used. Hour-glass control is used to suppress element instability. Numerical examples are presented to address various aspects of the study, including single-iteration schemes suitable for parallel processing.
机译:本文对复合材料壳在冲击载荷下的动力响应进行了数值研究。该材料以各向异性霍夫曼屈服面为模型,该屈服面允许不同的拉伸和压缩强度。采用显式时间积分算法来加速动态分析。使用只有一个高斯点的四节点壳单元。沙漏控制用于抑制元素不稳定。给出了数值示例以解决研究的各个方面,包括适用于并行处理的单迭代方案。

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