期刊文献+

16MnR钢过载峰作用下的疲劳裂纹扩展行为研究 被引量:10

Study on Crack Growth Behavior of 16MnR Subjected to Single Tensile Overload
下载PDF
导出
摘要 基于有限元法和Jiang-Sehitoglu循环塑性本构模型,动态模拟单个过载峰作用下裂纹扩展中的裂纹闭合行为。提取不同加载工况下的裂纹闭合和张开载荷,并考察不同工况和不同裂纹长度对裂纹闭合和张开载荷的影响。根据详细的裂纹闭合分析结果,研究单个拉伸过载下疲劳裂纹在不同阶段的扩展行为与裂纹闭合的对应关系,认为过载后裂纹闭合行为的改变是引起裂纹扩展行为改变的主要机理。根据有限元分析结果,提出一种改进的等效应力强度因子范围的计算方法,将其作为疲劳裂纹在整个扩展过程中的驱动力。拟合出单个过载峰作用下16MnR材料的裂纹扩展速率的预测公式,并将预测结果与试验结果进行对比,结果吻合。 The crack closure in the process of dynamic crack propagation is modeling by the finite element method and Jiang-Sehitoglu cyclic plastic constitutive model.The crack closure loading and opening loading are obtained by the FE results with different loading conditions.The influence of different maximum loadings and crack lengths will be analyzed.The relationship between crack propagation behavior and crack closure will be studied based on the FE results.The crack closure is considered as the main mechanism on crack propagation behavior.An improved model to calculate the effective stress intensity factor range will be proposed and the effective stress intensity factor range is considered as the driving force of crack propagation.The prediction formulation of crack growth rate is fitted about the 16MnR steel.The predicted results will be compared with the results of the crack growth experiments and the predicted results are very close to the obtained results in experiments.
出处 《机械工程学报》 EI CAS CSCD 北大核心 2013年第16期84-90,共7页 Journal of Mechanical Engineering
基金 国家自然科学基金(51175469 50975260) 浙江省自然科学基金(Z1091027)资助项目
关键词 裂纹闭合 等效应力强度因子范围 过载机理 裂纹扩展速率预测 Crack closure Effective stress intensity factor range Overload mechanism Crack growth rate prediction
  • 相关文献

参考文献16

  • 1BORREGO L P, FERREIRA J M, PINHO da CRUZ J M, et al. Evaluation of overload effects on fatigue crack growth and closure[J]. Engineering Fracture Mechanics, 2003, 70: 1379-1397.
  • 2SINGH K D, PARRY M amplitude fatigue crack R, SINCLAIR I. Variable growth behavior-a short overload[J]. Journal of Mechanical Science and Technology, 2011, 25(3): 663-673.
  • 3ELBER W. Fatigue crack closure under cyclic tension[J]. Engineering Fracture Mechanics, 1970, 2: 37-45.
  • 4ELBER W. The significance of fatigue crack closure, damage tolerance in aircraft structures[J]. ASTM STP, 1971, 486: 230-242.
  • 5ALLISON J E. Measurement of crack-tip stress distributions by x-ray difffraction[J]. ASTM STP, 1979, 677. 550-562.
  • 6TAIRA S, TANAKA K. Local residual stress near fatigue crack tip[J]. Transactions, Iron and Steel Institute of Japan, 1979, 19: 411-418.
  • 7刘建涛,杜平安.考虑过载效应的金属材料疲劳裂纹扩展试验数据拟合及疲劳裂纹扩展速度计算方法研究[J].机械工程学报,2012,48(4):85-91. 被引量:4
  • 8WANG X, GAO Z, ZHAO T, et al. An experimental study of the crack growth behavior of 16MnR pressure vessel steel[J]. ASME Journal Pressure Vessel Technol., 2009, 131(2): 021402-021401-9.
  • 9MCCLUNG R C, SEHITOGLU H. On the finite element analysis of fatigue crack closure-l: Basic modelling issues[J]. Engng. Fract: Mech., 1989, 33: 237-252.
  • 10JIANG Y, FENG M, DING E A reexamination of plasticity-induced crack closure in fatigue crack propagation [J]. International Journal of Plasticity, 2005, 21: 1720-1740.

二级参考文献18

共引文献3

同被引文献73

引证文献10

二级引证文献59

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部