首页> 外文OA文献 >Fatigue life and crack growth prediction methodology
【2h】

Fatigue life and crack growth prediction methodology

机译:疲劳寿命和裂纹扩展预测方法

摘要

The capabilities of a plasticity-induced crack-closure model and life-prediction code to predict fatigue crack growth and fatigue lives of metallic materials are reviewed. Crack-tip constraint factors, to account for three-dimensional effects, were selected to correlate large-crack growth rate data as a function of the effective-stress-intensity factor range (delta(K(sub eff))) under constant-amplitude loading. Some modifications to the delta(K(sub eff))-rate relations were needed in the near threshold regime to fit small-crack growth rate behavior and endurance limits. The model was then used to calculate small- and large-crack growth rates, and in some cases total fatigue lives, for several aluminum and titanium alloys under constant-amplitude, variable-amplitude, and spectrum loading. Fatigue lives were calculated using the crack growth relations and microstructural features like those that initiated cracks. Results from the tests and analyses agreed well.
机译:综述了塑性诱导裂纹闭合模型和寿命预测代码预测金属材料疲劳裂纹扩展和疲劳寿命的功能。选择裂纹尖端约束因子来解决三维效应,以便在恒定振幅下将大裂纹增长率数据与有效应力强度因子范围(delta(K(sub eff)))的函数相关联加载中。在近阈值状态下需要对delta(K(sub eff))-rate关系进行一些修改,以适应小裂纹的生长速率行为和耐力极限。然后,该模型用于计算在恒定振幅,可变振幅和频谱载荷下几种铝和钛合金的小裂纹和大裂纹增长率,在某些情况下还可以计算总疲劳寿命。疲劳寿命是使用裂纹扩展关系和引发裂纹的微观结构特征来计算的。测试和分析的结果一致。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利

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