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Prediction of the Residual Structural Integrity of a Polymer Matrix Composite Construction Element

机译:聚合物基复合结构构件的残余结构完整性预测

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摘要

Polymers are time-dependent materials. Polymer matrix composites behave as viscoelastic-viscoplastic anisotropic continua. Their thermomechanical characteristics are not only time-dependent, but are strongly influenced by the variations of the environmental conditions (temperature, moisture diffusion, radiation, etc.). This concerns not only the stiffness but also the strength characteristics, related to the damage development. Due to the composite nature, the number of potential damage sources is high and the damage development has to take into account all the interactions between simple mechanical loading modes, with or without, changing environmental conditions. Following a non-linear viscoelastic-viscoplastic analysis, based on the Schapery equations and a Zapas-Crissman functional, the stiffness degradation is obtained based on short-term creep and creep-recovery measurements at different stress levels and different temperatures.A damage component is added to the viscoelastic-viscoplastic model in order to account for damage development and associated strength degradation. Results obtained in the transverse direction of an unidirectional graphite-epoxy composite are presented. The extension to complete laminates with different stacking sequences is discussed. An assumption on the interlaminar behaviour must be introduced in order to take into account the important damage source not considered in classical laminate theories.
机译:聚合物是随时间变化的材料。聚合物基复合材料表现为粘弹性-粘塑性各向异性连续体。它们的热机械特性不仅与时间有关,而且还受到环境条件(温度,水分扩散,辐射等)变化的强烈影响。这不仅涉及刚度,还涉及与损伤发展有关的强度特性。由于具有复合性质,潜在的损坏源数量很多,并且损坏的发展必须考虑到简单的机械加载模式之间的所有相互作用,无论环境条件是否发生变化。根据Schapery方程和Zapas-Crissman泛函进行非线性粘弹-粘塑性分析后,基于在不同应力水平和不同温度下的短期蠕变和蠕变恢复测量值,获得了刚度退化。添加到粘弹-粘塑性模型中,以解决损伤发展和相关强度降低的问题。给出了在单向石墨-环氧树脂复合材料的横向方向上获得的结果。讨论了具有不同堆叠顺序的完整层压板的扩展。必须引入层间行为的假设,以考虑到经典层压理论中未考虑的重要破坏源。

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