Viscoplastic constitutive model considering strain rate sensitivity under multiaxial thermomechanical fatigue loading

被引:3
|
作者
Li, Dao-Hang [1 ]
Shang, De-Guang [1 ,3 ]
Chen, Hong [2 ]
Cong, Ling-Hua [2 ]
Wang, Jin-Jie [1 ]
Mao, Zheng-Yu [1 ]
Chen, Chao-Lin [1 ]
Guo, Yi-Er [1 ]
Yin, Xiang [1 ]
机构
[1] Beijing Univ Technol, Fac Mat & Mfg, Beijing, Peoples R China
[2] Aircraft Strength Res Inst China, Xian, Peoples R China
[3] Beijing Univ Technol, Fac Mat & Mfg, Beijing 100124, Peoples R China
基金
中国国家自然科学基金;
关键词
high-temperature materials; multiaxial loading; strain rate sensitivity; thermomechanical fatigue; viscoplastic constitutive model; NICKEL-BASE SUPERALLOY; LOW-CYCLE FATIGUE; TEMPERATURE-RANGE; CREEP-BEHAVIOR; STEEL; PLASTICITY; EQUATIONS; DAMAGE; RESPONSES; DEFORMATION;
D O I
10.1111/ffe.13939
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Strain rate sensitivity will change the cyclic mechanical response of materials under multiaxial thermomechanical fatigue loading; thus, it will lead to errors in fatigue life prediction if strain rate sensitivity is not considered in constitutive simulation. In order to more accurately express the time/rate dependence of viscoplastic behavior, a strain rate sensitivity factor is proposed to modify the viscoplastic function of Chaboche model first. On this basis, a viscoplastic constitutive model considering strain rate sensitivity under multiaxial thermomechanical fatigue loading is proposed, which can describe the varying influence of strain rate sensitivity on cyclic mechanical behavior. Meanwhile, the exponential isotropic hardening rule with the linear term is adopted to characterize the initial rapid softening and subsequent stable softening of the material under fatigue loading at elevated temperature. Moreover, the material-dependent nonproportional hardening coefficient and the loading path-dependent rotation factor are used in the kinematic hardening rule to consider the effect of nonproportional additional hardening on the cyclic mechanical behavior of materials. Finally, the proposed method is verified by the stress-strain data of titanium alloy TC4 and Ni-based superalloy GH4169 under uniaxial and multiaxial thermomechanical fatigue loadings, and a good agreement is obtained.
引用
收藏
页码:1455 / 1472
页数:18
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