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A novel creep-fatigue stiffness degradation model for composite materials

机译:复合材料蠕变疲劳刚度退化模型

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摘要

In this paper, a novel creep-fatigue stiffness degradation model for composite materials is introduced. The model proposed a nonlinear stress-strain constitutive equation in the form of a function of time and cycles simultaneously. The presented model consists of a linear elastic component, which is degraded as a function of cycles, and a nonlinear time-dependent component, which combines both time- and cycle-dependent nature of fatigue phenomena in an integrated formulation. The model predictions are validated by the experimental data taken from the literature for short fiber E-glass/polyamide6,6 and [+/- 45](2s) HTA(12 K)/6376 epoxy. It is shown that the model has the capability to predict the stress-strain curve after cycles of loading, taking into account the time-dependent response of composites. It is shown that under high stress levels, the development of fatigue mean strain is dominated by fatigue damages; under lower stress levels, however, the mean strain is mostly controlled by time-dependent viscoelastic strains.
机译:本文介绍了一种新型的复合材料蠕变疲劳刚度退化模型。该模型以时间和周期的函数形式提出了非线性应力-应变本构方程。提出的模型由线性弹性分量和非线性时间相关分量组成,该线性弹性分量随周期而降低,非线性依赖时间的分量将疲劳现象的时间和周期依赖性质结合在一个整体公式中。通过从文献中获得的短纤维E-玻璃/聚酰胺6,6和[+/- 45](2s)HTA(12 K)/ 6376环氧树脂的实验数据验证了模型的预测。结果表明,考虑到复合材料随时间变化的响应,该模型能够预测载荷循环后的应力-应变曲线。结果表明,在高应力水平下,疲劳平均应变的发展主要由疲劳损伤引起。然而,在较低的应力水平下,平均应变主要由时间依赖性粘弹性应变控制。

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