APPLIED LASER, Volume. 33, Issue 3, 259(2013)
The Effect of Laser Shock Peening on Fatigue Property of 7050 Aluminum Alloy Fastener Hole
[2] [2] XIONG JUNJIANG. Fatigue Life Design For Aircraft Structure[M]. Beijing: Beihang University Press, 2004: 24-26.
[4] [4] ZHANG SHUANGJIE, LI QIANG, WANG LIJUAN.Analysis on the Formig Limit of Cold Open-die Extrusion with Mandrel for the Thick-walled Tube[J]. Journal of Mechanical Engineering, 2010, 46(22): 53-57.
[5] [5] YANG J M, HER Y .C, HAN N, et al. Laser Shock Peening on Fatigue Behavior of 2024-T3 Al Alloy with Fastener Holes and Stopholes[J]. Materials Science and Engineering A, A298, 2001(1): 296-299.
[6] [6] ZHANG HONG, YU CHENGYE. Laser shock processing of Holes[J]. Surface Engineering, 22(2): 153-156.
[7] [7] ZOU SHIKUN, CAO ZIWEN, ZHAO YONG. Laser peening of aluminum alloy 7050 with fastener holes[J]. Chinese Optics Letters, 2008, 6(2): 116-119..
[8] [8] LI HANGYUE, HU NAISAI, HE JIAWEN. An Analytical model of Compressive Residual Stress Effect on Clousure[J]. ACTA Metallurgica Sinica,, 1998, 34(8): : 847-851.
[9] [9] OMAR HATAMLEH, JED LYONS, ROYCE FORMAN.Laser and shot peening effects on fatigue crack growth in friction stirwelded 7075-T7351 aluminum alloy joints[J].International Journal of Fatigue, 2007(29): 421-434.
[10] [10] HU NAISAI, XU KEWEI, FANG GANG. Residual Stress Relaxation and Dislocation Sub-structure Change of Shot Peening Components[J]. China Surface Engineering, 1992, (01): 24-28.
Get Citation
Copy Citation Text
Cao Ziwen, Che Zhigang, Zou Shikun, Zhao Yong. The Effect of Laser Shock Peening on Fatigue Property of 7050 Aluminum Alloy Fastener Hole[J]. APPLIED LASER, 2013, 33(3): 259
Received: Nov. 10, 2012
Accepted: --
Published Online: Aug. 28, 2013
The Author Email: Ziwen Cao (svip@163.com)