Interaction effects due to overloads and underloads on fatigue crack growth

被引:0
作者
Romeiro, F. [1 ]
de Freitas, M. [2 ]
da Fonte, M. [3 ]
机构
[1] Polythen Inst Leiria ESTG, P-2401951 Leiria, Portugal
[2] Inst Superior Tecnico, Lisbon 1049001, Portugal
[3] ENIDH, Naut Sch, Arcos 2770058, Portugal
来源
ADVANCES IN FRACTURE AND DAMAGE MECHANICS VI | 2007年 / 348-349卷
关键词
variable amplitude loading; plasticity-induced crack closure; overloads; underloads;
D O I
10.4028/www.scientific.net/KEM.348-349.333
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Under constant amplitude loading, a single variable (Delta K) or K-max are required in crack growth relationships. The transferability of fatigue laws, obtained under constant amplitude loading to variable amplitude fatigue, requires at least an additional variable, whose evolution with crack length accounts for the interactions effects between cycles of different types. This paper presents an analysis of fatigue crack growth tests on M(T) specimens made of a medium carbon steel. The specimens are subjected to repeated blocks of cycles made up of one or several overloads separated by a variable number of baseline cycles and two baseline stress ratios. The main objective of this study is to better understand the mechanisms at the origin of interactions effects due to the presence of overloads (or underloads) at different locations of each block loading Results have shown that the interaction effects are closely related to the cyclic plastic behaviour of the material and also the so-called Bauschinger effect.
引用
收藏
页码:333 / +
页数:2
相关论文
共 10 条
[1]  
[Anonymous], ECNR96007
[2]  
*ESA PUBL DIV, 1995, FAT CRACK GROWTH COM
[3]  
JONGE JB, 1993, 77 M AGARD STRUCT MA, P5
[4]   ON THE FINITE-ELEMENT ANALYSIS OF FATIGUE CRACK CLOSURE .2. NUMERICAL RESULTS [J].
MCCLUNG, RC ;
SEHITOGLU, H .
ENGINEERING FRACTURE MECHANICS, 1989, 33 (02) :253-272
[5]   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
[6]  
NEWMAN JC, 1981, 748 ASTM STP, P53
[7]  
OMMIER S, 2001, INT J FATIGUE, V23, pS111
[8]  
Pommier S, 2000, FATIGUE FRACT ENG M, V23, P129, DOI 10.1046/j.1460-2695.2000.00259.x
[9]   Effect of fatigue crack growth of interactions between overloads [J].
Pommier, S ;
De Freitas, M .
FATIGUE & FRACTURE OF ENGINEERING MATERIALS & STRUCTURES, 2002, 25 (07) :709-722
[10]  
ROMEIRO F, 2003, 1439 ASTM STP