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Fatigue crack growth under mixed-mode loadings.

机译:混合模式载荷下的疲劳裂纹扩展。

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摘要

The adoption of damage tolerance design concept along with increased demand for accurate residual structure and component life predictions have provided growing demand for the study of fatigue crack growth under mixed mode loadings in mechanical components. In this study, four-point bending and shear specimens made of SAE 1045 steel asymmetrically loaded under different initial KSeveral special tests were also conducted to study the effects of mode I compressive load, fatigue precracking, and prior overloads on fatigue crack growth. When the mode I load component was in compression under mixed mode I and II loadings, no fatigue crack growth was observed. Also, under mode II loading, when the specimen was not fatigue precracked, fatigue crack growth did not occur. Based on limited test data, it was found that initial mode I overloads result in accelerated fatigue crack growth rates on the subsequent mode II load cycles. Initial mode II overloads, however, retard fatigue crack growth rates during the subsequent mode II load cycles. Under large mode II loading, a crack propagated in mode II for a short distance before it changed its growth direction to mode I.
机译:损伤容限设计概念的采用以及对精确残余结构和部件寿命预测的需求不断增长,对研究机械部件在混合模式载荷下疲劳裂纹扩展的需求日益增长。在这项研究中,还对由SAE 1045钢制成的四点弯曲和剪切试样在不同的初始KS下进行了多次特殊测试,以研究I型压缩载荷,疲劳预裂纹和先前的过载对疲劳裂纹扩展的影响。当模式I载荷分量在混合模式I和II载荷下处于压缩状态时,未观察到疲劳裂纹扩展。同样,在模式II载荷下,当试样未疲劳预裂纹时,不会发生疲劳裂纹扩展。根据有限的测试数据,发现初始I型过载会在随后的II型载荷循环中导致加速的疲劳裂纹扩展速率。但是,初始模式II过载会在随后的模式II负载周期中延迟疲劳裂纹扩展速率。在较大的模式II载荷下,裂纹在模式II中传播了很短的距离,然后才将其生长方向更改为模式I。

著录项

  • 作者

    Qian, Jin.;

  • 作者单位

    The University of Toledo.;

  • 授予单位 The University of Toledo.;
  • 学科 Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 1995
  • 页码 200 p.
  • 总页数 200
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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