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Fatigue-Life Prediction Methodology Using Small-Crack Theory

机译:基于小裂纹理论的疲劳寿命预测方法

摘要

This paper reviews the capabilities of a plasticity-induced crack-closure model to predict fatigue lives of metallic materials using 'small-crack theory' for various materials and loading conditions. Crack-tip constraint factors, to account for three-dimensional state-of-stress effects, were selected to correlate large-crack growth rate data as a function of the effective-stress-intensity factor range (delta K(eff)) under constant-amplitude loading. Some modifications to the delta k(eff)-rate relations were needed in the near-threshold regime to fit measured small-crack growth rate behavior and fatigue endurance limits. The model was then used to calculate small- and large-crack growth rates, and to predict total fatigue lives, for notched and un-notched specimens made of two aluminum alloys and a steel under constant-amplitude and spectrum loading. Fatigue lives were calculated using the crack-growth relations and microstructural features like those that initiated cracks for the aluminum alloys and steel for edge-notched specimens. An equivalent-initial-flaw-size concept was used to calculate fatigue lives in other cases. Results from the tests and analyses agreed well.
机译:本文回顾了塑性诱导裂纹闭合模型在各种材料和载荷条件下使用“小裂纹理论”预测金属材料疲劳寿命的能力。选择裂纹尖端约束因素以解决三维应力状态影响,以将大裂纹增长率数据与恒定条件下有效应力强度因子范围(δK(eff))的函数相关联-振幅加载。在接近阈值状态下,需要对delta k(eff)-速率关系进行一些修改,以适应所测得的小裂纹生长速率行为和疲劳耐受极限。然后,该模型用于计算由两种铝合金和钢制成的带缺口和无缺口试样在恒定振幅和频谱载荷下的小裂纹和大裂纹增长率,并预测总疲劳寿命。疲劳寿命的计算方法是使用裂纹扩展关系和微观结构特征,例如那些引起铝合金和边缘缺口试样的钢产生裂纹的特征。在其他情况下,使用等效的初始缺陷大小概念来计算疲劳寿命。测试和分析的结果一致。

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