Fatigue crack growth in a laser shock peened residual stress field
Tài liệu tham khảo
Montross, 2002, Laser shock processing and its effects on microstructure and properties of metal alloys: a review, Int J Fatigue, 24, 1021, 10.1016/S0142-1123(02)00022-1
Fitzpatrick ME, Lodini A. Analysis of Residual Stress by Diffraction using Neutron and Synchrotron Radiation. 2003.
Macherauch, 1986, 167
Withers, 2001, Residual stress. Part 1–measurement techniques, MaterSci Technol, 17, 355, 10.1179/026708301101509980
Reimers, 2008
Achintha, 2011, Eigenstrain modelling of residual stresses generated by laser shock peening, J Mater Process Technol, 211, 1091, 10.1016/j.jmatprotec.2011.01.011
LaRue, 2007, Predicting the effect of residual stress on fatigue crack growth, Int J Fatigue, 29, 508, 10.1016/j.ijfatigue.2006.05.008
Bueckner, 1958, The propagation of cracks and the energy of elastic deformation, Trans Am Soc Mech Eng, 80, 1225-1230
Underwood JH, Pook LP, Sharples JK. Fatigue-Crack Propagation Through a Measured Residual Stress Field in Alloy Steel. Flaw Growth Fract; 1977;ASTM STP 6:402–15.
Fukuda S, Yasuyuki T. An Experimental Study of Redistribution of Welding Residual Stress with Fattgue Crack Extension 1978:67–72.
Chandawanich, 1979, An experimental study of fatigue crack initiation and growth from coldworked holes, Eng Fract Mech, 11, 609, 10.1016/0013-7944(79)90122-X
Lam, 1989, The effect of residual stress and its redistribution of fatigue crack growth, Theor Appl Fract Mech, 12, 59, 10.1016/0167-8442(89)90015-3
Stress, 1982, Intensity factors, crack profiles, and fatigue crack growth rates in residual stress fields, Residual Stress Eff Fatigue, 776, 13
Wolf, 1970, Fatigue crack closure under cyclic tension, Eng Fract Mech, 2, 37, 10.1016/0013-7944(70)90028-7
Newman JC. A crack-closure model for predicting fatigue crack growth under aircraft spectrum loading. Methods Model Predict Fatigue Crack Growth under Random Load 1981;748:53–84. http://doi.org/10.1520/STP28334S.
Newman, 198424, A crack opening stress equation for fatigue crack growth, Int J Fract
Hill, 2012, Fatigue crack closure in residual stress bearing materials, J ASTM Int, 9, 65, 10.1520/JAI104071
Garcia, 2016, Fatigue crack growth in residual stress fields, Int J Fatigue, 87, 326, 10.1016/j.ijfatigue.2016.02.020
Kashaev, 2017, Effects of laser shock peening on the microstructure and fatigue crack propagation behaviour of thin AA2024 specimens, Int J Fatigue, 98, 223, 10.1016/j.ijfatigue.2017.01.042
SAE International. AMS4296B 2012.
Prime MB, Gonzales AR. the Contour Method: Simple 2-D Mapping of Residual Stresses. Sixth Int Conf Residual Stress Int Conf Residual Stress July 10-12, 2000;836:617–24.
ASTM Standard E647 − 13a. Standard Test Method for Measurement of Fatigue Crack Growth Rates. Am Soc Test Mater 2014:1–50. http://doi.org/10.1520/E0647-13A.2.
Dasssult Systemes. ABAQUS User’s Manual, version 6.14 2014.
MathWorks. MATLAB User’s Manual, version R2013b 2013.
Liljedahl, 2010, The effect of weld residual stresses and their re-distribution with crack growth during fatigue under constant amplitude loading, Int J Fatigue, 32, 735, 10.1016/j.ijfatigue.2009.10.012
Krueger, 2002
Solanki, 2004, Finite element analysis of plasticity-induced fatigue crack closure: an overview, Eng Fract Mech, 71, 149, 10.1016/S0013-7944(03)00099-7
Gozin, 2012, 2D and 3D finite element analysis of crack growth under compressive residual stress field, Int J Solids Struct, 49, 3316, 10.1016/j.ijsolstr.2012.07.014
Walker, 1970, The effect of stress ratio during crack propagation and fatigue for 2024–T3 and 7075–T6 aluminum ASTM STP, Am Soc Test Mater, 1