Modeling of fatigue behavior in pre-corroded AZ31 magnesium alloy

IF 3.2 Q2 MATERIALS SCIENCE, MULTIDISCIPLINARY
Hamed Bahmanabadi , Madjid Shamsarjmand
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Abstract

In this paper, the mechanical and fatigue behavior of pre-corroded wrought AZ31 magnesium alloy was studied. For this purpose, the standard 3.5 wt.% NaCl corrosive solution was used. The samples were immersed for 3–24 h to characterize the effect of immersion time on the mechanical properties of AZ31 alloy. Standard specimens were also immersed for 1–3 h for the fatigue testing. Results of tensile tests showed that thorough the immersion of 0–24 h, the deviation of ultimate tensile stress and yield stress were less than 4 % and 6 %, respectively. Moreover, the deviation of elastic modulus was less than 20 %. Although, the elongation was deviated by 81 % through the immersion of 0–24 h. A drastic decrease was observed in the fatigue lifetime of pre-corroded alloy compared to the bare alloy. As the immersion time increased, the fatigue lifetime decreased. Maximum reduction in fatigue strength occurred when the immersion time was 3 h and the stress amplitude was 82.5 MPa. Fatigue results also showed that the Levenberg-Marquardt was a good method to find the materials' constants, as the maximum and average relative errors were 10.28 % and 2.78 %, respectively. The fatigue fracture surfaces of pre-corroded specimens indicated the brittle fracture. The Basquin model was used for fatigue lifetime prediction. A new model was proposed with a new parameter, initial virtual crack size, to relate the immersion time to the fatigue lifetime using the Paris equation. The fatigue lifetime of 1–3-h pre-corroded AZ31 magnesium alloy was estimated by the new model with acceptable relative errors.

Abstract Image

预腐蚀 AZ31 镁合金的疲劳行为建模
本文研究了预腐蚀锻造 AZ31 镁合金的机械和疲劳行为。为此,采用了标准的 3.5 wt.% 氯化钠腐蚀溶液。样品浸泡 3-24 小时,以确定浸泡时间对 AZ31 合金机械性能的影响。标准试样也浸泡了 1-3 小时进行疲劳测试。拉伸试验结果表明,浸泡 0-24 小时后,极限拉伸应力和屈服应力的偏差分别小于 4 % 和 6 %。此外,弹性模量的偏差也小于 20%。与裸合金相比,预腐蚀合金的疲劳寿命急剧下降。随着浸泡时间的延长,疲劳寿命也在缩短。当浸泡时间为 3 小时,应力幅值为 82.5 兆帕时,疲劳强度下降最大。疲劳结果还表明,Levenberg-Marquardt 是找到材料常数的良好方法,其最大和平均相对误差分别为 10.28 % 和 2.78 %。预腐蚀试样的疲劳断裂表面显示为脆性断裂。巴斯金模型用于疲劳寿命预测。利用新参数(初始虚拟裂纹尺寸)提出了一个新模型,使用帕里斯方程将浸泡时间与疲劳寿命联系起来。新模型估算了 1-3 小时预腐蚀 AZ31 镁合金的疲劳寿命,其相对误差可以接受。
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来源期刊
Forces in mechanics
Forces in mechanics Mechanics of Materials
CiteScore
3.50
自引率
0.00%
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0
审稿时长
52 days
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