考虑多晶材料疲劳行为受晶粒拓扑结构的影响,建立了多晶材料Voronoi镶嵌的有限元微观结构模型,并在Voronoi边界插入内聚力单元模拟晶界特性。在此基础上,基于Abaqus双线性内聚力本构关系,建立了内聚力单元的疲劳累积损伤模型,定义了损...考虑多晶材料疲劳行为受晶粒拓扑结构的影响,建立了多晶材料Voronoi镶嵌的有限元微观结构模型,并在Voronoi边界插入内聚力单元模拟晶界特性。在此基础上,基于Abaqus双线性内聚力本构关系,建立了内聚力单元的疲劳累积损伤模型,定义了损伤变量,损伤判据以及损伤规律;通过Abaqus UMAT(User-defined material mechanical behavior)子程序编写了内聚力单元疲劳损伤的数值计算程序,实现了对微观结构下材料滚动接触疲劳裂纹萌生与扩展的行为模拟。以滚子与滚道的接触疲劳分析为例,将数值模拟结果与实测结果相比,表明了该数值仿真方法模拟多晶材料裂纹形成和扩展的有效性。展开更多
Fatigue and tensile behaviors of homogenized WE 54 magnesium alloy before and after immersion in simulated body fluid(SBF)were investigated.According to the tensile test,the alloy without immersion in SBF solution has...Fatigue and tensile behaviors of homogenized WE 54 magnesium alloy before and after immersion in simulated body fluid(SBF)were investigated.According to the tensile test,the alloy without immersion in SBF solution has the highest tensile strength of 278 MPa,which decreased to 190 MPa after 336 h of immersion..The fatigue life of the homogenized WE 54 magnesium alloy before immersion in the SBF solution under a constant stress of 15 MPa is 3598 cycles.However,the fatigue life of the alloy decreased to 453 cycles after 336 h of immersion in the SBF solution under the same stress.Examination of the fracture surface of the samples by SEM reveals that the origin of the fatigue crack before immersion is micro-pores and defects.While corrosion pits and cracks are the main reasons for forming the initial fatigue crack after immersion.Moreover,the results obtained from practical work were evaluated and compared to theoretical calculations.The area of the hysteresis loops of the samples after the fatigue test,determined using Triangles and Monte Carlo methods,decreased from 4954.5 MPa and 4842.9 MPa before immersion to 192.0 MPa and 175.8 MPa after 336 h of immersion,respectively.展开更多
文摘考虑多晶材料疲劳行为受晶粒拓扑结构的影响,建立了多晶材料Voronoi镶嵌的有限元微观结构模型,并在Voronoi边界插入内聚力单元模拟晶界特性。在此基础上,基于Abaqus双线性内聚力本构关系,建立了内聚力单元的疲劳累积损伤模型,定义了损伤变量,损伤判据以及损伤规律;通过Abaqus UMAT(User-defined material mechanical behavior)子程序编写了内聚力单元疲劳损伤的数值计算程序,实现了对微观结构下材料滚动接触疲劳裂纹萌生与扩展的行为模拟。以滚子与滚道的接触疲劳分析为例,将数值模拟结果与实测结果相比,表明了该数值仿真方法模拟多晶材料裂纹形成和扩展的有效性。
文摘Fatigue and tensile behaviors of homogenized WE 54 magnesium alloy before and after immersion in simulated body fluid(SBF)were investigated.According to the tensile test,the alloy without immersion in SBF solution has the highest tensile strength of 278 MPa,which decreased to 190 MPa after 336 h of immersion..The fatigue life of the homogenized WE 54 magnesium alloy before immersion in the SBF solution under a constant stress of 15 MPa is 3598 cycles.However,the fatigue life of the alloy decreased to 453 cycles after 336 h of immersion in the SBF solution under the same stress.Examination of the fracture surface of the samples by SEM reveals that the origin of the fatigue crack before immersion is micro-pores and defects.While corrosion pits and cracks are the main reasons for forming the initial fatigue crack after immersion.Moreover,the results obtained from practical work were evaluated and compared to theoretical calculations.The area of the hysteresis loops of the samples after the fatigue test,determined using Triangles and Monte Carlo methods,decreased from 4954.5 MPa and 4842.9 MPa before immersion to 192.0 MPa and 175.8 MPa after 336 h of immersion,respectively.
