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铝合金薄板冲击后疲劳试验与谱载寿命

  • Yibo Zhang*
  • , Di Chen
  • , Zhengqiang Cheng
  • , Peiliang Shen
  • , Junjiang Xiong
  • *此作品的通讯作者
  • Shanghai Aircraft Design and Research Institute
  • Beihang University

科研成果: 期刊稿件文章同行评审

摘要

Tests of low velocity impact are performed on the sheets of AAs 2524-T3 and 7075-T62, respectively, with four different impact forces, and static and fatigue experiments are conducted on the intact and post-impact sheets under static tensile, constant amplitude and block spectrum loading. The impact-dent size, static and fatigue properties, and spectrum-loading life are determined, with the effect of impact on fatigue characteristics and damage mechanism analyzed and discussed from fractographic and experimental observations. An S-N-Kt surface model is proposed to depict fatigue characteristics for fatigue lifetime prediction of post-impact sheets subjected to block spectrum loading. A new concept is applied for experimental data and a reasonable agreement obtained between the theoretical and experimental results, demonstrating the effective and practical use of the developed surface model. A nonlinear elastic-plastic FE model based on the Johnson-Cook constitutive equation is generated to model the residual stress patterns and stress concentration around the impact-dent, and fatigue lives of post-impact sheets of AAs 2524-T3 and 7075-T62 subjected to block spectrum loading are predicted from the S-N-Kt surface model. Good agreements have been achieved between predictions and experiments.

投稿的翻译标题Fatigue experiments and lifetime for post-impact sheets of aluminum-alloys(AAs) under block spectrum loading
源语言繁体中文
期刊论文编号224811
期刊Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
43
1
DOI
出版状态已出版 - 25 1月 2022

关键词

  • Aluminum-alloy sheet
  • Block spectrum loading
  • Fatigue
  • Lifetime
  • Low velocity impact

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