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Numerical, Experimental and Analytical Correlation for Predicting the Structural Behavior of Composite Structures Under Impact

机译:用于预测碰撞下复合结构结构行为的数值,实验和分析相关性

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In the present work, numerical, experimental and analytical results regarding impact events on composite structure are presented. The test case consists in a classic 24 plies CAI specimen (100×150 mm) subjected to 10 J impact. The work can be divided into two phases. The first phase is finalized to the definition of a procedure able to provide a robust numerical model, which can simulate accurately the structural response of composite plates subjected to impact events. At this phase, the numerical results are compared with analytical ones. In the second phase, both inter- and intra-lamina failure are considered. Regarding the inter-laminar failure, an experimental-numerical procedure is defined in order to set the right parameters related to cohesive behaviour. For both phases, trade-off analyses on the main numerical parameters are performed. All numerical results are compared with experimental ones in terms of both energy balance and damaged area.
机译:在本作的工作中,提出了关于复合结构的影响事件的数值,实验和分析结果。 测试壳体在经典的24层上进行CAI样本(100×150mm),经受10次撞击。 这项工作可分为两个阶段。 第一阶段最终确定能够提供一种能够提供鲁棒数值模型的程序的定义,其可以精确地模拟经受冲击事件的复合板的结构响应。 在此阶段,将数值结果与分析术进行比较。 在第二阶段,考虑了层内突发性和内部内部衰竭。 关于层间失败,定义了实验数量的过程,以便设定与凝聚力相关的正确参数。 对于两个阶段,执行主要数值参数的权衡分析。 在能量平衡和受损区域方面,将所有数值结果与实验结果进行比较。

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