首页> 外文期刊>Materials Science and Engineering >Indentation creep-fatigue test on aluminum alloy 2A12
【24h】

Indentation creep-fatigue test on aluminum alloy 2A12

机译:铝合金2A12的压痕蠕变疲劳试验

获取原文
获取原文并翻译 | 示例
           

摘要

Generally, the creep-fatigue behavior of materials is obtained by tensile/compression tests. In the present study, we explore the possibility of investigating the creep-fatigue behavior of aluminum alloy 2A12 at 200 ℃ by using indentation creep-fatigue test with a flat cylindrical indenter. The experimental results show that the evolution of indentation depth with the number of cycles experiences two stages: a short transient stage and then a steady state with an approximate constant indentation depth propagation rate. The micro-observations on craters undergoing creep-fatigue and pure creep loadings indicate that the fatigue loading accelerates the evolution of damage and leads to the nucleation of cracks around the crater. These findings are useful to probe the creep-fatigue properties of materials with the indentation test.
机译:通常,材料的蠕变疲劳行为是通过拉伸/压缩测试获得的。在本研究中,我们探索了通过使用带有扁平圆柱形压头的压痕蠕变疲劳试验研究200A铝合金2A12的蠕变疲劳行为的可能性。实验结果表明,随着循环次数的增加,压痕深度的演化经历了两个阶段:短暂的过渡阶段,然后是具有近似恒定的压痕深度传播速率的稳态。经受蠕变疲劳和纯蠕变载荷的弹坑的微观观察表明,疲劳载荷加速了损伤的发展并导致弹坑周围的裂纹成核。这些发现对于通过压痕测试来探究材料的蠕变疲劳特性很有用。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号