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 |
| 卷 | 43 |
| 期 | 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
学术指纹
探究 '铝合金薄板冲击后疲劳试验与谱载寿命' 的科研主题。它们共同构成独一无二的学术指纹。引用此
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