On the theoretical modeling of fatigue crack growth

被引:61
作者
Hosseini, Zahra S. [1 ,2 ]
Dadfarnia, Mohsen [1 ,2 ]
Somerday, Brian P. [2 ,3 ]
Sofronis, Petros [1 ,2 ]
Ritchie, Robert O. [2 ,4 ,5 ]
机构
[1] Univ Illinois, Dept Mech Sci & Engn, Urbana, IL 61801 USA
[2] Kyushu Univ, WPI, I2CNER, Fukuoka, Fukuoka 8190395, Japan
[3] Southwest Res Inst, San Antonio, TX 78238 USA
[4] Lawrence Berkeley Natl Lab, Mat Sci Div, Berkeley, CA 94720 USA
[5] Univ Calif Berkeley, Dept Mat Sci & Engn, Berkeley, CA 94720 USA
关键词
FINITE-ELEMENT-ANALYSIS; ELASTIC-PLASTIC ANALYSIS; COHESIVE ZONE MODEL; LOW-CYCLE FATIGUE; GENERALIZED THEORY; PROPAGATION; CLOSURE; STEEL; TEMPERATURE; DERIVATION;
D O I
10.1016/j.jmps.2018.07.026
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Although fatigue is by far the most common mode of failure of structural materials, mechanistic understanding is still lacking. For example, the fundamental Paris law which relates the crack growth rate to stress-intensity factor range is still phenomenological and no reliable mechanistic model has been established for a given material or class of materials despite numerous investigations over a half a century. This work is an attempt to theoretically model fatigue crack propagation induced by alternating crack-tip plastic blunting and re-sharpening in the mid-range of growth rates on the basis of inputs from experiments that measure macroscopic material behavior, e.g., response to uniaxial cycling loading. In particular, we attempt to predict Paris law behavior by accounting for the material constitutive behavior in response to cyclic loading by modeling crack advance solely in terms of the underlying plastic dissipation. We obtain the steady-state condition for crack growth based on plastic dissipation, numerically using finite element analysis, which involves a methodology to address plastic closure upon unloading. For a given stress-intensity range, we calculate the crack propagation rate from the steady-state condition through each cycle of loading and unloading of a cracked compact-tension specimen, without resorting to any specific criterion for crack advance. Published by Elsevier Ltd.
引用
收藏
页码:341 / 362
页数:22
相关论文
共 74 条
[1]  
Anderson T.L., 2017, Fracture Mechanics: Fundamentals and Applications, DOI [10.1201/9781315370293, DOI 10.1201/9781315370293, 10.1201/9781315370293/fracture-mechanics-ted-anderson, DOI 10.1201/9781315370293/FRACTURE-MECHANICS-TED-ANDERSON]
[2]  
[Anonymous], 1980, ASTM Special Technical Publication, DOI DOI 10.1520/STP36972S
[3]  
Armstrong P.J., 1966, CEGB REPORT NO RDBN
[4]   Anatomy of coupled constitutive models for ratcheting simulation [J].
Bari, S ;
Hassan, T .
INTERNATIONAL JOURNAL OF PLASTICITY, 2000, 16 (3-4) :381-409
[5]   A cohesive zone model for fatigue and creep-fatigue crack growth in single crystal superalloys [J].
Bouvard, J. L. ;
Chaboche, J. L. ;
Feyel, F. ;
Gallerneau, F. .
INTERNATIONAL JOURNAL OF FATIGUE, 2009, 31 (05) :868-879
[6]  
Chaboche J., 1989, J Eng Mater Technol, V111, P409, DOI DOI 10.1115/1.3226488
[7]   TIME-INDEPENDENT CONSTITUTIVE THEORIES FOR CYCLIC PLASTICITY [J].
CHABOCHE, JL .
INTERNATIONAL JOURNAL OF PLASTICITY, 1986, 2 (02) :149-188
[8]   ON SOME MODIFICATIONS OF KINEMATIC HARDENING TO IMPROVE THE DESCRIPTION OF RATCHETTING EFFECTS [J].
CHABOCHE, JL .
INTERNATIONAL JOURNAL OF PLASTICITY, 1991, 7 (07) :661-678
[9]  
Coffin J., 1954, T AM SOC MECH ENG, V76, P931
[10]   Elastoplastic finite element analysis of three-dimensional fatigue crack growth in aluminum shafts subjected to axial loading [J].
de-Andrés, A ;
Pérez, JL ;
Ortiz, M .
INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 1999, 36 (15) :2231-2258