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A Simplified Fatigue Design Methodology for Composite Structures

机译:复合结构的简化疲劳设计方法

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摘要

A simplified methodology is presented to predict fatigue life and residual strength of composite structures. To avoid excessive amount of tests that are required for model characterization, the model parameters(strength degradation parameter, fatigue shape parameter) are assumed as function of fatigue life. S-N curve is used to extract fatigue life that is required to characterize the stress levels comprising a randomly-ordered load spectrum. And different stress ratios are handled with Goodman correction approach(fatigue envelope). It is assumed that the residual strength is a monotonically decreasing function of the number of loading cycles and applied fatigue stress ratio. And the residual strength distribution after an arbitrary load cycles is represented by two parameter Weibull functions.
机译:提出了一种简化的方法来预测复合结构的疲劳寿命和残余强度。为了避免模型表征所需的过多测试,将模型参数(强度退化参数,疲劳形状参数)假定为疲劳寿命的函数。 S-N曲线用于提取疲劳寿命,疲劳寿命是表征包括随机排序的载荷谱的应力水平所需的。并采用Goodman校正方法(疲劳包络)处理不同的应力比。假定残余强度是加载次数和所施加疲劳应力比的单调递减函数。任意载荷循环后的残余强度分布由两个参数威布尔函数表示。

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