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A Strength-Based Wearout Model for Predicting the Life of Composite Structures

机译:基于强度的磨损模型,用于预测复合结构寿命

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摘要

A model to predict the residual strength and life of polymric composite structures subjected to spectrum fatigue loadings is described. The model is based on the fundamental assumptions that the structure undergoes proportional loading, that the residual strength is a monotonically decreasing function of the number of fatigue cycles, and that both the life distribution due to continuous constant amplitude cycling and theresidual strength distribution after an arbitrary load history may be represented by two parameter Weibull functions. The model also incorporates a "cycle mix factor" to account for the drastic reduction of fatigue life that may be caused by a large number of charges in the stress amplitude of the loading. The model's predictions are compared to experiemntally determined fatigue life dsitributions for uniaxial loadings of a number of laminates comprised of different materials and layups. Constant-amplitude, two-stress level, and spectrum fatigue loadings, including the FALSTAFF (Fighter Aircraft Loading STAndard For Fatigue) spectrum, are considered. The theoretical fatigue life distributions are shown to correlate well with the experimental results. Moreover, excllent correlation of theory and experiment is obtained for an "average fatigue life" that is based on the 63.2
机译:描述了预测经受光谱疲劳载荷的多种复合结构的剩余强度和寿命的模型。该模型基于该结构经历比例负荷的根本假设,即残余强度是疲劳循环次数的单调减少,并且在任意后引起的寿命分布和其存在的恒定强度分布负载历史可以由两个参数Weibull功能表示。该模型还包括“循环混合因子”,以解释可能是由负载应力幅度的大量电荷引起的疲劳寿命的急剧降低。将模型的预测进行了比较,以实现由不同材料和上篮的多个层压板的单轴载荷的疲劳寿命D批读。考虑恒定,双应力水平和频谱疲劳负荷,包括Falstaff(疲劳疲劳)谱的Falstaff(战斗机装载标准)。理论疲劳寿命分布显示与实验结果相比好。此外,基于63.2的“平均疲劳寿命”获得了理论和实验的易相关性

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