Experimental study of crack growth in thin sheet 2024-T3 aluminum under tension-torsion loading

被引:55
|
作者
Sutton, MA [1 ]
Helm, JD
Boone, ML
机构
[1] Univ S Carolina, Dept Mech Engn, Columbia, SC 29208 USA
[2] Correlated Solut Inc, W Columbia, SC 29169 USA
[3] Westinghouse Nucl, Columbia, SC 29250 USA
基金
美国国家航空航天局;
关键词
fracture surface characterization; single edge-cracked 2024-T3 aluminum specimen; tension-torsion loading; 3D COD measurements by computer vision;
D O I
10.1023/A:1011014917851
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
To assess the viability of using a critical COD criterion for flaws in 2024-T3 aluminum experiencing tension stresses (S-P) and torsion stresses (S-T), the enclosed work presents (a) a complete set of measurements for critical COD during crack growth under nominal tension-torsion loading, (b) the evolution of crack path with crack growth and (c) crack surface shape as a function of loading. Data from this work will provide an important experimental database for use in assessing the predictive capability of advanced, three-dimensional, crack growth simulation tools. Results for COD during crack growth under tension-torsion loading indicates that the measured critical COD for tension-torsion loading is constant during crack growth. In addition, the value of COD measured using image correlation methods is approximately 8% larger than observed for in-plane tension-shear, with much of the increase apparently due to specimen deformations in the crack tip vicinity. In addition, crack path evolution data for the range of S-T/S-P considered in this work show that the crack experiences both tunneling and slant fracture during loading, with tunneling rapidly decreasing (a) as crack growth progresses for all S-T/S-P values or (b) as S-T/S-P increases. Furthermore, results indicate that tearing during tension-torsion loading always occurs in a manner so that the crack surfaces tend to interfere during growth. Finally, crack surface shape data indicates that, with the exception of a small secondary transition, the direction of crack growth remains stable along a straight line oriented along the initial fatigue crack direction for the range of S-T/S-P being considered.
引用
收藏
页码:285 / 301
页数:17
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