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The influence of laminate stacking sequence on ballistic limit using a combined Experimental/FEM/Artificial Neural Networks (ANN) methodology

机译:结合实验/有限元/人工神经网络(ANN)方法对层压板堆叠顺序对弹道极限的影响

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AbstractComposite laminates subjected to high velocity impacts are usually studied by means of experimental or numerical approaches. Nevertheless, these techniques are not appropriate to analyze the wide range of possibilities in the design of laminates (a great amount of time and economic resources are required); therefore, more efficient methods would be desirable.This work presents the capability of an ANN approach to predict the change of the ballistic limit with the laminate stacking sequence, and hence to find the optimum laminate combination. In order to obtain a refined ANN tool, a combined methodology of experimental and finite element method has been used. The results of the experimentally validated FEM model, are used to provide the data to the ANN. Once trained, the ANN is able to predict accurately the ballistic limit of composite laminates studied. The ANN allows studying very efficiently the whole possibilities of laminate stacking sequence using the common orientations, in symmetric 12 plies laminates (4096 cases). In addition, a deeper comprehension of composite plates when subjected to high velocity impact has been achieved by means of the analysis of the results. Conclusions obtained can be used by composite design engineers to improve ballistic performance of composite plates.
机译: 摘要 经受高速冲击的复合层压板通常通过实验或数值方法进行研究。然而,这些技术不适用于分析层压板设计中的各种可能性(需要大量时间和经济资源);因此,更有效的方法是可取的。 这项工作提出了一种ANN方法预测弹道变化的能力。限制层压板的堆叠顺序,从而找到最佳的层压板组合。为了获得改进的人工神经网络工具,已使用了实验方法和有限元方法的组合方法。经过实验验证的FEM模型的结果用于将数据提供给ANN。一旦经过训练,人工神经网络就能够准确预测所研究的复合材料层压板的弹道极限。通过ANN,可以在对称的12层层压板(4096例)中使用通用方向非常有效地研究层压板堆叠顺序的全部可能性。另外,通过对结果的分析,已经获得了复合板在受到高速冲击时的更深刻的理解。复合设计工程师可以使用获得的结论来改善复合板的弹道性能。

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