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Analytical Modeling of Impact Resistance and Damage Tolerance of Laminated Composite Plates

机译:层合复合板的耐冲击性和损伤容忍度的解析模型

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摘要

The present study is concerned with a fully analytical model for predicting impact resistance and damage tolerance characteristics of laminated fiber reinforced composite plates. The energy balance for damage development during the impact process is established with the help of a localized deformation field, in which various effects such as the anisotropy of the delaminated sublaminates, elastic property degradation due to matrix cracking, multiple delaminations, and membrane deformation within the damage zone are taken into account. This results in upper and lower bounds of the dclamination threshold load and a deflection-dependent critical load for stable delamination propagation. On the basis of the conservation of energy principle, simple relationships are found between the resulting damage area and the impact energy as well as the peak impact load. The global buckling load of damaged rectangular plates is derived from the energy-based stability criterion, and the residual ultimate strength is calculated using the von Karman postbuckling strength theory. The analytical solutions obtained turn out to be capable of providing highly accurate predictions compared with the standard impact and the compression-after-impact experiments of carbon-fiber-reinforced polyetherimide and aromatic polymer composites.
机译:本研究涉及用于预测层压纤维增强复合材料板的抗冲击性和损伤耐受特性的完全分析模型。在局部变形场的帮助下,建立了在冲击过程中破坏发展的能量平衡,在该场中,各种作用(例如分层的次层压体的各向异性,由于基体裂纹导致的弹性性能下降,多次分层以及膜内部的膜变形)考虑到损坏区域。这会导致分层阈值载荷的上限和下限以及与偏差相关的临界载荷,以实现稳定的分层传播。根据能量守恒原理,可以在产生的破坏面积与冲击能量以及峰值冲击载荷之间找到简单的关系。损坏的矩形板的整体屈曲载荷是从基于能量的稳定性准则中得出的,并且残余残余极限强度是根据冯·卡曼的后屈曲强度理论计算的。与标准冲击和碳纤维增强聚醚酰亚胺和芳族聚合物复合材料的撞击后压缩实验相比,所获得的分析解决方案能够提供高度准确的预测。

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