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ZSGH4169合金细观力学行为的数值模拟

蔚夺魁 杨晓光 张克实

蔚夺魁, 杨晓光, 张克实. ZSGH4169合金细观力学行为的数值模拟[J]. 航空动力学报, 2013, 28(11): 2572-2578.
引用本文: 蔚夺魁, 杨晓光, 张克实. ZSGH4169合金细观力学行为的数值模拟[J]. 航空动力学报, 2013, 28(11): 2572-2578.
YU Duo-kui, YANG Xiao-guang, ZHANG Ke-shi. Numerical simulation of meso-mechanical response for superalloy ZSGH4169[J]. Journal of Aerospace Power, 2013, 28(11): 2572-2578.
Citation: YU Duo-kui, YANG Xiao-guang, ZHANG Ke-shi. Numerical simulation of meso-mechanical response for superalloy ZSGH4169[J]. Journal of Aerospace Power, 2013, 28(11): 2572-2578.

ZSGH4169合金细观力学行为的数值模拟

Numerical simulation of meso-mechanical response for superalloy ZSGH4169

  • 摘要: 基于晶体塑性本构理论,利用多晶代表性单元从细观尺度研究了ZSGH4169合金在650℃条件下考虑双轴应力状态的循环应力应变行为.计算结果表明:该合金在双轴拉伸应力控制下存在与低周疲劳试验常用的单轴应力状态一致的棘轮效应.对两种应力状态下的结果进行对比发现,在1150MPa应力单轴循环载荷下初始循环残余应变比双轴应力状态高出3倍,且双轴应力状态下最终循环稳定,残余应变约为1.2%,但在单轴应力状态下是不稳定的.对应力和塑性应变累积不均匀性的分析表明:单轴和双轴拉伸状态下,虽然应力和应变分布的不均匀性都随着循环数的增加而增加,但单轴拉伸状态下平均应力随循环数增加,而双轴拉伸状态下几乎为常数.

     

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出版历程
  • 收稿日期:  2012-10-16
  • 刊出日期:  2013-11-28

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