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Corrosion-fatigue life prediction for notched components based on the local strain and linear elastic fracture mechanics concepts

机译:基于局部应变和线性弹性断裂力学概念的缺口构件腐蚀疲劳寿命预测

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An initiation-propagation model based on the local strain and linear elastic fracture mechanics concepts has been investigated for application to predict the fatigue life of notched components exposed to a corrosive environment. Estimates of the corrosion-fatigue crack initiation lives were obtained using strain-life relationships. The Paris power law was used to obtain the estimates of corrosion-fatigue crack propagation lives. Estimated corrosion-fatigue lives were compared with the experimentally obtained corrosion-fatigue life data using centre-notched specimens of three types of modified Al-2.5Mg alloy exposed to an Arabian Gulf seawater environment. Good fatigue life estimates were obtained both in air and in Arabian Gulf seawater environments for all three types of alloy. It is shown that good corrosion-fatigue life predictions can be made by determining the relevant fatigue parameters via a few simple constant-amplitude fatigue tests on smooth specimens and a few crack growth rate tests in the environment at the frequency of interest.
机译:已经研究了基于局部应变和线性弹性断裂力学概念的初始传播模型,用于预测暴露在腐蚀环境下的缺口构件的疲劳寿命。利用应变-寿命关系获得了腐蚀疲劳裂纹萌生寿命的估计值。巴黎幂定律用于获得腐蚀疲劳裂纹扩展寿命的估计值。使用暴露在阿拉伯海湾海水环境中的三种类型的改性Al-2.5Mg合金的中心缺口样品,将估算的腐蚀疲劳寿命与实验获得的腐蚀疲劳寿命数据进行了比较。对于这三种合金,在空气和阿拉伯海湾海水环境中均获得了良好的疲劳寿命估算。结果表明,通过在光滑标本上进行一些简单的恒定振幅疲劳测试以及在环境中以感兴趣的频率进行一些裂纹扩展速率测试,确定相关的疲劳参数,可以得出良好的腐蚀疲劳寿命预测。

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