An analytical model of plasticity induced crack closure

被引:5
作者
Antunes, F. V. [1 ]
Rodrigues, D. M. [1 ]
Branco, R. [2 ]
机构
[1] Univ Coimbra, Dept Mech Eng, CEMUC, Rua Luis Reis Santos, P-3030788 Coimbra, Portugal
[2] Polytech Inst Coimbra, Dept Mech Eng, P-3030129 Coimbra, Portugal
来源
FATIGUE 2010 | 2010年 / 2卷 / 01期
关键词
Plasticity induced crack closure; finite element method; micromechanisms; residual plastic wake; FINITE-ELEMENT-ANALYSIS; NUMERICAL-SIMULATION; MESH SIZE; FATIGUE; GROWTH; STRESS; BEHAVIOR; IDENTIFICATION; PARAMETERS; ROUGHNESS;
D O I
10.1016/j.proeng.2010.03.109
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Accurate and non-conservative measurements of fatigue crack growth rate are essential when designing efficient structures to be subjected to cyclic loading. Crack closure is a main mechanism of fatigue crack propagation and must be included. Numerical models have been successfully developed to predict plasticity induced crack closure (PICC), however a full understanding of the links between physical parameters, residual plastic wake and PICC has not been achieved yet. The objective of the present paper is the identification of the main micromechanisms involved in PICC and the establishment of qualitative and quantitative links between plastic deformation and the level of PICC. An M(T) specimen with 200x60x0.2 mm(3) and an initial crack of 10 mm was studied. It was found that the linear superposition applies to the effect of individual plastic wedges on the PICC level. The vertical elongation of the plastic wedge,Delta y, was considered and found adequate to quantify the weight of individual plastic wedges in the residual plastic wake. The effect of an individual plastic wedge was found to have an exponential decrease with the distance to the crack tip, d. An empirical model was developed relating the PICC level of individual plastic wedges with the distance d and the plastic deformation level, Delta y, and was applied successfully to predict PICC evolution from residual plastic wakes. (C) 2010 Published by Elsevier Ltd.
引用
收藏
页码:1005 / 1014
页数:10
相关论文
共 31 条
[11]  
Elber W., 1971, Damage tolerance in aircraft structures, P230, DOI DOI 10.1520/STP486-EB
[12]   Influence of minimum element size to determine crack closure stress by the finite element method [J].
González-Herrera, A ;
Zapatero, J .
ENGINEERING FRACTURE MECHANICS, 2005, 72 (03) :337-355
[13]   A reexamination of plasticity-induced crack closure in fatigue crack propagation [J].
Jiang, YY ;
Feng, ML ;
Ding, F .
INTERNATIONAL JOURNAL OF PLASTICITY, 2005, 21 (09) :1720-1740
[14]   Elucidation of fatigue crack closure behaviour in surface crack by 3-D finite element analysis [J].
Kim, Joo-Sung ;
Kang, Jae Youn ;
Song, Ji-Ho .
INTERNATIONAL JOURNAL OF FATIGUE, 2007, 29 (01) :168-180
[15]   Finite-element analysis of fatigue crack closure under plane strain conditions: stabilization behaviour and mesh size effect [J].
Lee, HJ ;
Song, JH .
FATIGUE & FRACTURE OF ENGINEERING MATERIALS & STRUCTURES, 2005, 28 (03) :333-342
[16]   ON THE FINITE-ELEMENT ANALYSIS OF FATIGUE CRACK CLOSURE .1. BASIC MODELING ISSUES [J].
MCCLUNG, RC ;
SEHITOGLU, H .
ENGINEERING FRACTURE MECHANICS, 1989, 33 (02) :237-252
[17]   Three-dimensional numerical simulation of the deep-drawing process using solid finite elements [J].
Menezes, LF ;
Teodosiu, C .
JOURNAL OF MATERIALS PROCESSING TECHNOLOGY, 2000, 97 (1-3) :100-106
[18]   Study on the influence of work-hardening modeling in springback prediction [J].
Oliveira, M. C. ;
Alves, J. L. ;
Chaparro, B. M. ;
Menezes, L. F. .
INTERNATIONAL JOURNAL OF PLASTICITY, 2007, 23 (03) :516-543
[19]   Automatic correction of the time step in implicit simulations of the stamping process [J].
Oliveira, MC ;
Menezes, LF .
FINITE ELEMENTS IN ANALYSIS AND DESIGN, 2004, 40 (13-14) :1995-2010
[20]   Improvement of a frictional contact algorithm for strongly curved contact problems [J].
Oliveira, MC ;
Alves, JL ;
Menezes, LF .
INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN ENGINEERING, 2003, 58 (14) :2083-2101