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A Review of Some Key Developments in the Analysis of the Effects of Impact Upon Composite Structures

机译:对复合结构影响影响的一些关键发展述评

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This paper reviews work at the Aeronautical Research Institute of Sweden, and addresses major issues of importance in evaluating the effect of impact on composite structures. Some more extensive reviews of work by other researchers are referenced. The paper addresses impact response and damage formation, damage characterization, and residual strength and stability by combination of experiments and analysis. Studies showing that impact response type depends on impactor-plate mass ratio are presented. Small mass impact is generally more critical at a given configuration and energy. Analytical models for small mass impact and for damage initiation and growth during large mass impact are discussed. Rate dependency of matrix-dominated properties is briefly discussed. Geometric and constitutive characterization of impact damage zones is presented and the influence of degraded properties demonstrated. The use of an FE-based plate model to simulate delamination growth due to sub-laminate buckling and panel skin buckling in stiffened panels after impact is described. Skin buckling causes a sleep increase in delamination strain energy release rate and should be prevented.
机译:本文审查了瑞典航空研究院的工作,并解决了评估对复合结构影响影响的重要性问题。参考其他研究人员的一些更广泛的工作审查。本文通过对实验和分析的组合解决了影响响应和损伤形成,损伤表征和残余强度和稳定性。显示出现冲击响应类型的研究取决于撞击板质量比。在给定的配置和能量中,小的质量影响通常更为关键。讨论了对小型造型和大量影响损伤启动和生长的分析模型。简要讨论了矩阵主导的属性的速率依赖性。提出了影响损伤区的几何和本构体表征,并表现出降解性能的影响。使用Fe基板模型来模拟由于次压板弯曲和面板皮肤弯曲引起的分层生长。皮肤屈曲导致睡眠增加分层应变能量释放速率,并且应该防止。

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