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首页> 外文期刊>International Journal of Fatigue >Fatigue tests and damage model development on Al-Si-Mg aluminum alloys with low-velocity impact pit
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Fatigue tests and damage model development on Al-Si-Mg aluminum alloys with low-velocity impact pit

机译:低速冲击坑Al-Si-Mg铝合金疲劳试验及损伤模型开发

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摘要

An experimental-analytical investigation was conducted to study the fatigue properties of ZL114A aluminum alloy with low-velocity impact pit. The analysis of the fracture surfaces indicated that the cracks initiated at the position with tension residual stress rather than at the pit. Considering that the pit depth has a direct correlation with the magnitude of residual stresses, a new damage evolution equation involving a dimensionless parameter about pit depth was proposed to reflect the detrimental effect of pit. The proposed model was applied to the fatigue life prediction of specimens and hole plates with impact pit, and the result was within a twice-error band compared with the experimental data.
机译:进行了一种实验分析研究以研究ZL114A铝合金与低速冲击坑的疲劳性能。 裂缝表面的分析表明裂缝在张力残余应力而不是在坑中发起的裂缝。 考虑到凹坑深度与残余应力的大小直接相关,提出了一种涉及关于凹坑深度的无量纲参数的新的损伤演化方程,以反映坑的不利影响。 所提出的模型应用于具有冲击坑的标本和孔板的疲劳寿命预测,结果与实验数据相比,结果是两次错误带内。

著录项

  • 来源
    《International Journal of Fatigue》 |2021年第12期|106466.1-106466.11|共11页
  • 作者单位

    School of Aeronautic Science and Engineering Beihang University Beijing 100191 China;

    School of Aeronautic Science and Engineering Beihang University Beijing 100191 China;

    Hunan Aviation Powerplant Research Institutee Aero Engine (Group) Corporation of China Zhuzhou 412002 China;

    School of Aeronautic Science and Engineering Beihang University Beijing 100191 China;

    School of Aeronautic Science and Engineering Beihang University Beijing 100191 China Shen Zhen Institute of Beihang University Shenzhen 518000 China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Aluminum alloy; Impact pit; Continuum damage mechanics; Fatigue life; Damage evolution model;

    机译:铝合金;冲击坑;连续伤害力学;疲劳生活;损伤进化模型;

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