Micromechanisms of multistage fatigue crack growth in a high-strength aluminum alloy

被引:134
作者
Xue, Y.
El Kadiri, H.
Horstmeyer, M. F.
Jordon, J. B.
Weiland, H.
机构
[1] Mississippi State Univ, Ctr Adv Vehicular Syst, Starkville, MS 39759 USA
[2] Alcoa Tech Ctr, Alcoa Ctr, PA 15069 USA
关键词
fatigue fractographics; aluminum alloy; anisotropic microstructure; micromechanism-crack propagation;
D O I
10.1016/j.actamat.2006.11.009
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
This study reveals the micromechanisms of fatigue damage formation and evolution with respect to particle topology and grain size and orientation in a rolled 7075-T651 Al alloy. Systematic observations were made of the variations in the fracture surfaces and damage micromechanisms, which were characterized in three fatigue stages: fatigue crack formation, micro structurally/physically small cracks and long cracks. The fatigue crack was formed exclusively at the fractured Fe-rich intermetallic constituent particles preferably located at or near the specimen surface. Large impurities, such as metallic oxides, were also observed to influence the crack nucleation mechanisms. The presence of these impurities close to the nucleation sites was correlated with an approximate 30% reduction in fatigue life. In the microstructurally and physically small crack regimes, the crack front showed a rough localized brittle fatigue fracture along the crack propagation direction in addition to some localized ductile fatigue fracture. Changes in striation size across grain boundaries were clearly observed. In the long crack regime, the fracture surface became rougher but the overall surface tended to be perpendicular to the loading direction, indicating a Mode I fracture. The ramification of the results for a micro structure-based multistage model that comprises crack incubation, small crack growth and long crack growth is discussed in detail. (c) 2006 Acta Materialia Inc. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码:1975 / 1984
页数:10
相关论文
共 16 条
[1]  
ABELKIS PR, 1978, ASTM SPECIAL TECHNIC, P213
[2]  
*ASM, 1991, ASM HDB, V2
[3]  
Forsyth P. J. E., 1961, P CRACK PROPAGATION, P76
[4]   THE INFLUENCE OF CRACK TIP PLASTICITY IN THE GROWTH OF SMALL FATIGUE CRACKS [J].
LANKFORD, J ;
DAVIDSON, DL ;
CHAN, KS .
METALLURGICAL TRANSACTIONS A-PHYSICAL METALLURGY AND MATERIALS SCIENCE, 1984, 15 (08) :1579-1588
[5]   FATIGUE CRACK MICROMECHANISMS IN INGOT AND POWDER METALLURGY-7XXX ALUMINUM-ALLOYS IN AIR AND VACUUM [J].
LANKFORD, J ;
DAVIDSON, DL .
ACTA METALLURGICA, 1983, 31 (08) :1273-1284
[6]  
Maenning W.W., 1997, ASM Handbook Fatigue and Fracture, P303
[7]   Micro structure-based fatigue modeling of cast A356-T6 alloy [J].
McDowell, DL ;
Gall, K ;
Horstemeyer, MF ;
Fan, J .
ENGINEERING FRACTURE MECHANICS, 2003, 70 (01) :49-80
[8]   FATIGUE CRACK INITIATION AND GROWTH UNDER MIXED-MODE LOADING IN ALUMINUM-ALLOYS 2017-T3 AND 7075-T6 [J].
OTSUKA, A ;
TOHGO, K ;
MATSUYAMA, H .
ENGINEERING FRACTURE MECHANICS, 1987, 28 (5-6) :721-+
[9]  
Phillips EP, 1988, ASTM STP, P505
[10]   CRACK OPENING STRESS MEASUREMENTS OF SURFACE CRACKS IN 7075-T6 ALUMINUM-ALLOY PLATE SPECIMEN THROUGH ELECTRON FRACTOGRAPHY [J].
PUTRA, IS ;
SCHIJVE, J .
FATIGUE & FRACTURE OF ENGINEERING MATERIALS & STRUCTURES, 1992, 15 (04) :323-338