[1] SHEN Y Y, ZHAI W J. Cold extrusion family introduction of FTI’s reinforcement techniques of holes[J]. Civil Aircraft Design and Research, 1998(1): 1-7(in Chinese).

[2] QIAN X M, JIANG Y F, GUAN H B, et al. Research and application of strengthening technology for fastening holes of aircraft structures[J]. Journal of Mechanical Strength, 2011, 33(5): 749-753(in Chinese).

[3] CAO Z W, CHE Z G, ZOU S K, et al. The effect of laser shock peening on fatigue property of 7050 aluminum alloy fastener hole[J]. Applied Laser, 2013, 33(3): 259-262(in Chinese).

[4] WANG Q, WANG X, GAO Y K, et al. Effect of strengthened hole on the fatigue life of TC18 titanium alloy[J]. Materials Engineering, 2011, 39(2): 84-86(in Chinese).

[5] SHEPARD M J, SMITH P R, AMER M S. Introduction of compressive residual stresses in Ti-6Al-4V simulated airfoils via laser shock processing[J]. Journal of Materials Engineering and Performance, 2001, 10(6): 670-678.

[6] WANG J M, ZHOU Q L, JIANG Y F, et al. Numerical simulation of sheet deformation by hollow laser shock[J]. Laser Technology, 2012, 36(6): 727-730(in Chinese) .

[7] WANG S B, FAN Y, WU H X, et al. Research of strengthening 7050 aerial aluminum alloy structural material with laser shock processing[J]. Chinese Journal of Lasers, 2014, 31(1): 125-128(in Chinese) .

[8] JIANG Y F, CHENG Z J, DING B, et al. Residual stress and fatigue failure in hole specimen by one side laser shock processing[J]. Laser ＆ Infrared, 2014, 44(10): 1090-1094(in Chinese) .

[9] FAN Y, WANG S B, WU H X, et al. Experimental research of laser shock processing on aerial aluminum alloy[J]. Laser Technology, 2003, 27(4): 273-275(in Chinese).

[10] PEYRE P, MERRIEN P, LIEURADE H P, et al. Laser induced shockwaves as surface treatment for 7075-T7351 aluminum alloy[J]. Surface Engineering, 1995, 11(1): 47-52.

[11] MONTROSS C S, WEI T, YE L, et al. Laser shock processing and its effects on microstructures and properties of metal alloy: a review[J]. International Journal of Fatigue, 2002, 24(10): 1021-1036.

[12] JIANG Y F, ZHANG J W, JING R, et al. Analysis of the residual stress field in hole specimen by laser shock processing with different power density[J]. Laser ＆ Infrared, 2012, 42 (8): 866-869 (in Chinese) .

[13] CUELLAR S D, HILL M R, de WALD A T, et al. Residual stress and fatigue life in laser shock peened open hole samples[J]. International Journal of Fatigue, 2012, 44: 8-13.

[14] FAN Y, WANG S B, WU H X, et al. Research of residual compressive stress induced by laser shock processing on 7050 aerial aluminum alloy[J]. Applied Laser, 2003, 23(1): 5-8(in Chinese).

[15] ZHOU J Zh, YANG X D, HUANG S, et al. Residual stress field of ZK60 specimen with central hole induced by both-side laser shot peening[J].Chinese Journal of Lasers, 2010, 37(7): 1850-1855(in Chinese).