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Mechanics-Based Modeling Approach for Rapid Prediction of Low Velocity Impact Damage in Composite Laminates

机译:基于力学的复合材料层合板低速冲击损伤快速预测建模方法

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A mechanics-based modeling approach is developed to rapidly predict damage in polymer matrix composites resulting from a low velocity impact event. The approach is incorporated into a computer code that provides an efficient means to assess the damage resistance for a range of material systems, layup configurations, and impact scenarios. It is envisioned that the developed approach will aid in early design and analysis of composite structures where sizing and layup decisions must be made, and evaluating the feasibility of a large number of laminate configurations using numerical approaches such as finite element analysis (FEA) is prohibitively expensive. Therefore, the goal of the modeling approach is to predict the impact damage size given the laminate configuration and impact scenario. This information can then be used to determine the residua) strength of the material. To be useful in such a context, the tool is designed to run quickly (<2 minutes) to allow a large number of design cases to be investigated. The results presented demonstrate that the model is capable of efficiently predicting low velocity impact damage size, shape, and location within an acceptable accuracy suitable for preliminary design and analysis of composite structures.
机译:开发了一种基于力学的建模方法,以快速预测低速冲击事件对聚合物基复合材料的损害。该方法被并入计算机代码中,该计算机代码提供了一种有效的方法来评估一系列材料系统,铺层配置和撞击情况下的抗损伤性。可以预见的是,开发的方法将有助于必须进行尺寸和铺层决定的复合结构的早期设计和分析,并且使用数值方法(例如有限元分析(FEA))评估大量层压板配置的可行性是令人望而却步的。昂贵的。因此,建模方法的目标是在给定层压板配置和冲击场景的情况下预测冲击破坏的大小。然后,该信息可用于确定材料的残留强度。为了在这种情况下有用,该工具旨在快速运行(<2分钟),以调查大量设计案例。提出的结果表明,该模型能够在可接受的精度范围内有效预测低速冲击损伤的大小,形状和位置,适用于复合结构的初步设计和分析。

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