Effect of laser shock processing on fatigue crack growth and fracture toughness of 6061-T6 aluminum alloy

Yang, 2001, Mater. Sci. Eng. A, 298, 296, 10.1016/S0921-5093(00)01277-6 Hong, 1998, Mater. Sci. Eng. A, 257, 322, 10.1016/S0921-5093(98)00793-X Tsay, 2003, Corr. Sci., 45, 1985, 10.1016/S0010-938X(03)00036-2 Rankin, 2003, Mater. Sci. Eng. A, 349, 279, 10.1016/S0921-5093(02)00811-0 Chu, 1999, Mater. Sci. Eng. A, 260, 260, 10.1016/S0921-5093(98)00889-2 Peyre, 1995, Opt. Quant. Electron., 27, 1213, 10.1007/BF00326477 Smith, 2000, J. Mater. Eng. Perform., 9, 33, 10.1361/105994900770346259 Schmidt-Uhlig, 2000, Eur. Phys. J. Appl. Phys., 9, 235, 10.1051/epjap:2000109 Fatigue and Fracture Resistance of non-ferrous alloy, ASM Handbook, vol. 19, ASM International, Materials Park, OH, 1996. ASTM 2002, Annual book of ASTM Standards, v.03.01 no. E837-01, Standard Test Method for Determining Residual Stresses by the Hole–Drilling Strain Gage Method. ASTM 2002, Annual book of ASTM Standards, v.03.01 no. E647-00 Standard Test Method for Measurement of Fatigue Crack Growth Rates. Anderson, 1995 ASTM 2002, Annual book of ASTM Standards, v.03.01 no. E399-97, Standard Test Method for Plane Stress Fracture Toughness of Metallic Materials.