Role of extruded texture on fatigue crack growth in a high strength aluminum alloy thick-walled cylinder

被引:5
作者
Malik, M. A. [1 ]
Salam, I. [1 ]
Muhammad, W. [1 ]
Ejaz, N. [1 ]
机构
[1] Natl Univ Sci & Technol, Coll Elect & Mech Engn, Dept Mech Engn, Rawalpindi 46000, Pakistan
关键词
Aluminum alloy; Fatigue crack growth; Paris constants; Post-fracture analysis; BEHAVIOR; MICROSTRUCTURE; ENVIRONMENT; CONSTANT; MODEL;
D O I
10.1007/s12206-008-1220-0
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
In present study, as a basic step for modeling the fatigue behavior of an extruded Al alloy cylinder, the fatigue crack growth data of the alloy was collected in two orientations. Microstructural analysis revealed that the material had recrystallized grains and clusters of constituent particles aligned in the direction of extrusion. Fatigue life of the samples revealed a shorter fatigue life representing a higher fatigue crack growth rate in transverse direction. The Paris constants C and m were found to be 4 x 10(-11) and 3.4 for the transverse orientation. The same constants were found to be 2 x 10(-10) and 2.6 for the longitudinal direction. Post fracture analysis revealed that the topographical appearance of the fractured surfaces in two orientations was different. The mechanism of crack growth was the formation of striations. The present study revealed that the texture of the constituent particles created during extrusion process has a pronounced effect on the crack growth rate in two orientations.
引用
收藏
页码:1261 / 1269
页数:9
相关论文
共 24 条
[1]   Fatigue crack growth analysis of pre-strained 7475-T7351 aluminum alloy [J].
Al-Rubaie, Kassim S. ;
Barroso, Emerson K. L. ;
Godefroid, Leonardo B. .
INTERNATIONAL JOURNAL OF FATIGUE, 2006, 28 (08) :934-942
[2]  
[Anonymous], 2000, J ENG MATER-T ASME, DOI DOI 10.1115/1.3225026
[3]  
[Anonymous], 1996, ANN BOOK ASTM STAND
[4]   Evaluation of overload effects on fatigue crack growth and closure [J].
Borrego, LP ;
Ferreira, JM ;
da Cruz, JMP ;
Costa, JM .
ENGINEERING FRACTURE MECHANICS, 2003, 70 (11) :1379-1397
[5]  
DeBartolo EA, 2001, INT J FATIGUE, V23, pS79, DOI 10.1016/S0142-1123(01)00122-0
[6]  
Fonte MA, 2001, INT J FATIGUE, V23, pS311, DOI 10.1016/S0142-1123(01)00179-7
[7]   Laser and shot peening effects on fatigue crack growth in friction stir welded 7075-T7351 aluminum alloy joints [J].
Hatamleh, Omar ;
Lyons, Jed ;
Forman, Royce .
INTERNATIONAL JOURNAL OF FATIGUE, 2007, 29 (03) :421-434
[8]   Recent development in aluminium alloys for aerospace applications [J].
Heinz, A ;
Haszler, A ;
Keidel, C ;
Moldenhauer, S ;
Benedictus, R ;
Miller, WS .
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 2000, 280 (01) :102-107
[9]   Influence of grain structure and slip planarity on fatigue crack growth in low alloying artificially aged 2xxx aluminium alloys [J].
Kamp, N. ;
Gao, N. ;
Starink, M. J. ;
Sinclair, I. .
INTERNATIONAL JOURNAL OF FATIGUE, 2007, 29 (05) :869-878
[10]   Four-point-bend fatigue of AA 2026 aluminum alloys [J].
Li, JX ;
Zhai, T ;
Garratt, MD ;
Bray, GH .
METALLURGICAL AND MATERIALS TRANSACTIONS A-PHYSICAL METALLURGY AND MATERIALS SCIENCE, 2005, 36A (09) :2529-2539