[1] [1] Marandi S M, Rahmani K, Tajdari M. Foreign object damage on the leading edge of gas turbine blades[J]. Aerospace Science and Technology, 2014, 33(1): 65-75.

[2] [2] Orchowski N J, Mohammed R D, Clark G, et al.. The post-repair performance of Ti-6Al-4V after foreign object damage[J]. Procedia Engineering, 2011, 10: 3622-3627.

[3] [3] Zabeen S, Preuss M, Withers P J. Residual stresses caused by head-on and 45° foreign object damage for a laser shock peened Ti-6Al-4V alloy aerofoil[J]. Materials Science and Engineering A, 2013, 560: 518-527.

[4] [4] Witek L. Crack propagation analysis of mechanically damaged compressor blades subjected to high cycle fatigue[J]. Engineering Failure Analysis, 2011, 18(4): 1223-1232.

[5] [5] Mishra R K, Srivastav D K, Srinivasan K, et al.. Impact of foreign object damage on an aero gas turbine engine[J]. Journal of Failure Analysis & Prevention, 2015, 15(1): 25-32.

[6] [6] Frankel P G, Withers P J, Preuss M, et al.. Residual stress fields after FOD impact on flat and aerofoil-shaped leading edges[J]. Mechanics of Materials, 2012, 55: 130-145.

[7] [7] Zhang X, Chan B, Lama S, et al.. Influence of impact dents on the fatigue strength of aluminium alloy friction stir welds[J]. Procedia Engineering, 2010, 2(1): 1691-1700.

[8] [8] Duo P, Liu J, Dini D, et al.. Evaluation and analysis of residual stresses due to foreign object damage[J]. Mechanics of Materials, 2007, 39(3): 199-211.

[9] [9] Zhou Z, Gill A S, Telang A, et al.. Experimental and finite element simulation study of thermal relaxation of residual stresses in laser shock peened IN718 SPF superalloy[J]. Experimental Mechanics, 2014, 54(9): 1597-1611.

[10] [10] Tian Qing, Zhou Jianzhong, Huang Shu, et al.. Relaxation of residual stress on laser-peened surface during cyclic loading[J]. Laser & Optoelectronics Progress, 2014, 51(8): 081403.

[11] [11] Lin B, Lupton C, Spanrad S, et al.. Fatigue crack growth in laser-shock-peened Ti-6Al-4V aerofoil specimens due to foreign object damage[J]. International Journal of Fatigue, 2014, 59: 23-33.

[12] [12] Spanrad S, Tong J. Characterisation of foreign object damage (FOD) and early fatigue crack growth in laser shock peened Ti-6AL-4V aerofoil specimens[J]. Materials Science and Engineering A, 2011, 528(4-5): 2128-2136.

[13] [13] Zabeen S, Preuss M, Withers P J. Evolution of a laser shock peened residual stress field locally with foreign object damage and subsequent fatigue crack growth[J]. Acta Materialia, 2015, 83: 216-226.

[14] [14] Maxwell D C, Nicholas T. A rapid method for generation of a Haigh diagram for high cycle fatigue[M]// Fatigue and fracture mechanics. West Conshohocken: ASTM International, 1999, 29: 626-641.

[15] [15] Liu Lijun. Analysis on fatigue influencing factors and notch effect of high strength bolt used in grid structure with bolt-sphere joints[D]. Taiyuan: Taiyuan University of Technology, 2003.

[16] [16] Nicholas T, Thompson S R, Porter W J, et al.. Comparison of fatigue limit strength of Ti-6Al-4V in tension and torsion after real and simulated foreign object damage[J]. International Journal of Fatigue, 2005, 27(10-12): 1637-1643.

[17] [17] Ruschau J, Thompson S R, Nicholas T. High cycle fatigue limit stresses for airfoils subjected to foreign object damage[J]. International Journal of Fatigue, 2003, 25(9-11): 955-962.

[18] [18] Lanning D B, Nicholas T, Haritos G K. On the use of critical distance theories for the prediction of the high cycle fatigue limit stress in notched Ti-6Al-4V[J]. International Journal of Fatigue, 2005, 27(1): 45-47.

[19] [19] Lin B, Zabeen S, Tong J, et al.. Residual stresses due to foreign object damage in laser-shock peened aerofoils: Simulation and measurement[J]. Mechanics of Materials, 2015, 82: 78-90.

[20] [20] Feng Yayun, Ye Yunxia, Lian Zuchang, et al.. Experimental research on effect of surface quality of copper treated by laser shock peening[J]. Laser & Optoelectronics Progress, 2015, 52(10): 101401.

[21] [21] Liu Wencai, Dong Jie, Zhai Chunquan, et al.. Influence of shot peening on high cycle fatigue properties of high-strength wrought magnesium alloy ZK60-T5[J]. Journal of Zhengzhou University (Engineering Science), 2009, 30(1): 1-5.

[22] [22] Wang X M, Shi J. Validation of Johnson-Cook plasticity and damage model using impact experiment[J]. International Journal of Impact Engineering, 2013, 60: 67-75.

[23] [23] Brockman R A, Braisted W R, Olson S E, et al.. Prediction and characterization of residual stresses from laser shock peening[J]. International Journal of Fatigue, 2012, 36(1): 96-108.