Experimental and numerical investigation on fatigue crack growth behavior of commercial pure titanium under I-II mixed mode loading at negative load ratios

被引:34
作者
Zhang, Peng [1 ,2 ]
Xie, Lin-qi [1 ,2 ]
Zhou, Chang-yu [1 ,2 ]
He, Xiao-hua [1 ,2 ]
机构
[1] Nanjing Tech Univ, Sch Mech & Power Engn, Nanjing 211816, Peoples R China
[2] Jiangsu Key Lab Design & Manufacture Extreme Pres, Nanjing 211816, Peoples R China
基金
中国国家自然科学基金;
关键词
Fatigue crack growth; I-II mixed mode crack; Negative load ratio; Fracture criterion; Crack closure; FRACTURE-BEHAVIOR; PROPAGATION; MECHANISMS; DUCTILE; STRAIN;
D O I
10.1016/j.ijfatigue.2020.105700
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
With the increase of design and application parameters for pressurized structures, the mixed mode fatigue crack growth (FCG) behavior has become a concerned problem in the field of structural integrity. In order to understand FCG behavior of I-II mixed mode crack growth at negative load ratios, an improved compact tensile shear (CTS) specimen of commercial pure titanium is taken to study the effects of load ratio and loading angle on I-II mixed mode FCG behavior through experiments and finite element method (FEM), which mechanism is discussed in depth as well. The contribution of mode I and mode II crack growth driving forces to I-II mixed mode FCG is analyzed. The changes of crack fracture criterion and the mechanism of crack growth in I-II mixed mode FCG process are revealed, and the competition relationship between two crack closure mechanisms of I-II mixed mode crack at negative load ratios is explained. An improved fatigue crack growth rate (FCGR) model that can make I-II mixed mode FCGR normalized is proposed by considering both the crack closure and the crack fracture criterion eventually.
引用
收藏
页数:14
相关论文
共 39 条
[1]  
[Anonymous], J BASIC ENG T ASME
[2]   ELASTIC PLASTIC FRACTURE-BEHAVIOR OF AN ALUMINUM-ALLOY UNDER MIXED-MODE LOADING [J].
AOKI, S ;
KISHIMOTO, K ;
YOSHIDA, T ;
SAKATA, M ;
RICHARD, HA .
JOURNAL OF THE MECHANICS AND PHYSICS OF SOLIDS, 1990, 38 (02) :195-213
[3]   Mixed-mode fatigue crack growth behaviour in aluminium alloy [J].
Borrego, LP ;
Antunes, FV ;
Costa, JM ;
Ferreira, JM .
INTERNATIONAL JOURNAL OF FATIGUE, 2006, 28 (5-6) :618-626
[4]   TIME-INDEPENDENT CONSTITUTIVE THEORIES FOR CYCLIC PLASTICITY [J].
CHABOCHE, JL .
INTERNATIONAL JOURNAL OF PLASTICITY, 1986, 2 (02) :149-188
[5]  
Clayton J. Q., 1976, Metal Science, V10, P63, DOI 10.1179/030634576790432083
[6]  
Elber W., 1971, The significance of fatigue crack closure, Damage tolerance in aircraft structures, V486, P230, DOI DOI 10.1520/STP26680S
[7]  
Griffith A. A., 1921, PHILOS T R SOC A, V221, P163, DOI [10.1098/rsta.1921.0006, DOI 10.1098/RSTA.1921.0006]
[8]   Improved modeling of the effect of R-ratio on crack growth rate [J].
Huang, Xiaoping ;
Moan, Torgeir .
INTERNATIONAL JOURNAL OF FATIGUE, 2007, 29 (04) :591-602
[9]  
Hussain M.A., 1974, ASTM SPEC TECH PUBL, V560, P2
[10]   CRACK-PROPAGATION RATE IN 7075-T6 PLATES UNDER CYCLIC TENSILE AND TRANSVERSE SHEAR LOADINGS [J].
IIDA, S ;
KOBAYASHI, AS .
JOURNAL OF BASIC ENGINEERING, 1969, 91 (04) :764-+