Effect of initiation feature on microstructure-scale fatigue crack propagation in Al–Zn–Mg–Cu
Source abstract
Abstract
Abstract High fidelity measurements of constituent particle or corrosion topography nucleated fatigue crack growth rates (da/dN) are established for 7075-T651 in humid air. Values of microstructure-scale da/dN are determined by microscopy of programmed load-induced crack surface markers, rather than surface-only measurements. Both pristine and corroded specimen da/dN from various applied stress levels are successfully correlated using continuum-elastic stress intensity (ΔK or ΔK and Kmax) or dislocation-based (Bilby–Cottrell–Swindon) crack tip opening displacement (cyclic ϕ and ϕmax), with the former accounting for the gradient of elastic stress concentration due to the initiating feature. Values of da/dN vary by an order of magnitude at each fixed driving force due to microstructural influences that result in a locally irregular crack front. Grain-scale models using stress intensity closure or slip-based crystal plasticity do not capture experimental da/dN variability. Due to an inadequate mechanistic basis, mechanics-inspired models of da/dN do not predict multiple growth regimes that are typical of environment enhanced cracking. An elastic ΔK-based description of long crack da/dN data for a given alloy-environment can be transformed to a continuum elastic–plastic ϕc basis to provide a mean crack growth rate description. Coupling mean rates with a statistical description of microstructure sensitive variability, and dislocation or crystal plasticity-finite element modeling of component ϕc for non-continuum cracking, will enhance prognosis in the MSC regime.
Source: openaire · Quality: candidate unverified · Source record ↗
Research context
OpenAlex topics: Fatigue and fracture mechanics · Aluminum Alloy Microstructure Properties · Metal Forming Simulation Techniques
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (100+)
Show source-provided references
1. Larsen · 2005
2. 2009
3. Crystallography of fatigue crack propagation in precipitation-hardened Al–Cu–Mg/Li10.1007/s11661-007-9344-x ↗
4. Environment sensitive fatigue crack tip processes and propagation in aerospace aluminum alloys
5. Chemical and metallurgical aspects of environmentally assisted fatigue crack-growth in 7075-T651 aluminum-alloy10.1007/BF02645142 ↗
6. Simulation-based strategies for microstructure-sensitive fatigue modeling10.1016/j.msea.2006.08.129 ↗
7. The merging of fatigue and fracture mechanics concepts: a historical perspective10.1016/S0376-0421(98)00006-2 ↗
8. Mechanisms of environmentally assisted cracking in Al–Zn–Mg single-crystals10.1016/0010-938X(82)90062-2 ↗
9. Fatigue crack formation and growth from localized corrosion in Al–Zn–Mg–Cu10.1016/j.engfracmech.2008.11.005 ↗
10. Effect of corrosion severity on fatigue evolution in Al–Zn–Mg–Cu10.1016/j.corsci.2009.10.006 ↗
11. Multiple fatigue crack growth in pre-corroded 2024-T3 aluminum10.1016/j.ijfatigue.2005.06.026 ↗
12. Predicting fatigue life of pre-corroded 2024-T3 aluminum from breaking load tests10.1016/j.ijfatigue.2003.10.010 ↗
13. Fatigue modeling for aircraft structures containing natural exfoliation corrosion10.1016/j.ijfatigue.2006.07.003 ↗
14. Corrosion pit size distributions and fatigue lives – a study of the EIFS technique for fatigue design in the presence of corrosion10.1016/S0142-1123(03)00069-0 ↗
15. Effects of pitting corrosion on the fatigue behavior of aluminum alloy 7075-T6: modeling and experimental studies10.1016/S0921-5093(00)01216-8 ↗
16. Sharp K, Mills T, Russo S, Clark G, Liu Q. Effects of exfoliation corrosion on the fatigue life of two high-strength aluminum alloys. In: FAA/DoD/NASA aging aircraft 2000, St. Louis, MO; 2001.
17. Characterisation of equivalent initial flaw sizes in 7050 aluminium alloy10.1111/j.1460-2695.2006.01050.x ↗
18. Hertzberg · 1996
19. Suresh · 1998
20. Wei · 2010
21. Harter JA. AFGROW Program Version 4.12.15.0. AFRL/VASM, WPAFB, OH; 2008. .
22. Fatigue crack-growth modeling by successive blocking of dislocations10.1098/rspa.1992.0067 ↗
23. Interactions of fatigue cracks with elastic obstacles10.1023/A:1011041612941 ↗
24. Modelling microstructurally sensitive fatigue short crack growth10.1098/rspa.1994.0131 ↗
25. Ravichandran · 1999
26. Ritchie · 1986
27. Larsen · 1992
28. Miller · 1992
29. Propagation of short fatigue cracks10.1179/imr.1984.29.1.445 ↗
30. A simplified laboratory approach for the prediction of short crack behavior in engineering structures10.1111/j.1460-2695.1988.tb01183.x ↗
31. Fatigue-life prediction methodology using small-crack theory10.1016/S0142-1123(98)00058-9 ↗
32. The generalised Frost–Dugdale approach to modelling fatigue crack growth10.1016/j.engfailanal.2007.11.007 ↗
33. Estimation of the effects of plasticity and resulting crack closure during small fatigue crack growth10.1023/A:1007690904863 ↗
34. Crack growth of physically small cracks10.1016/j.ijfatigue.2007.01.031 ↗
35. Crack-tip stresses and their effect on stress intensity factor for crack propagation10.1016/j.engfracmech.2007.07.019 ↗
36. Crack tip driving forces and crack growth representation under fatigue10.1016/S0142-1123(03)00105-1 ↗
37. Polycrystal orientation distribution effects on microslip in high cycle fatigue10.1016/S0142-1123(02)00057-9 ↗
38. Mechanics of fatigue crack-propagation by crack-tip plastic blunting10.1016/0013-7944(84)90163-2 ↗
39. Microstructural-based physics of failure models to predict fatigue reliability
40. Crack initiation and small fatigue crack growth behaviour of squeeze-cast Al–Si aluminium alloys10.1111/j.1460-2695.1997.tb00281.x ↗
41. Three-dimensional finite element simulations of microstructurally small fatigue crack growth in 7075 aluminium alloy10.1111/j.1460-2695.2006.01035.x ↗
42. Microstructure-based fatigue modeling of cast A356-T6 alloy10.1016/S0013-7944(02)00021-8 ↗
43. Crack tip displacements of microstructurally small cracks in 316L steel and their dependence on crystallographic orientations of grains10.1111/j.1460-2695.2007.01098.x ↗
44. The influence of grains’ crystallographic orientations on advancing short crack10.1016/j.ijfatigue.2007.01.030 ↗
45. Estimating fatigue sensitivity to polycrystalline Ni-base superalloy microstructures using a computational approach10.1111/j.1460-2695.2007.01159.x ↗
46. Vector CTD analysis for crystallographic crack-growth10.1016/0956-7151(90)90079-V ↗
47. A small fatigue crack growth relationship and its application to cast aluminum10.1016/j.actamat.2004.12.004 ↗
48. Small fatigue crack growth in metallic materials: a model and its application to engineering alloys10.1016/j.actamat.2007.08.022 ↗
49. A model for the formation of fatigue striations and its relationship with small fatigue crack growth in an aluminum alloy10.1016/j.ijfatigue.2010.05.005 ↗
50. Simulating small crack growth behaviour using crystal plasticity theory and finite element analysis10.1111/j.1460-2695.2004.00720.x ↗
51. A study of small crack growth in aluminum alloy 7075-T610.1016/S0142-1123(02)00025-7 ↗
52. Effect of surface texture on the initiation and propagation of small fatigue cracks in a forged 6082 aluminum-alloy10.1016/0921-5093(93)90493-X ↗
53. The effect of grain size on the fatigue of commercially pure aluminium10.1111/j.1460-2695.1995.tb00868.x ↗
54. Driving forces for localized corrosion-to-fatigue crack transition in Al–Zn–Mg–Cu10.1111/j.1460-2695.2011.01568.x ↗
55. Burns JT. The effect of initiation feature and environment on fatigue crack formation and early propagation in Al–Zn–Mg–Cu. PhD Dissertation. Charlottesville (VA): Materials Science and Engineering, University of Virginia; 2010.
56. 1998
57. 2005
58. Observations of fatigue crack initiation in 7075-T65110.1016/j.ijfatigue.2009.06.003 ↗
59. ASTM · 2007 · vol. 03.02
60. Burns JT. Modeling fatigue behavior of pre-corroded aluminum alloys using linear elastic fracture mechanics. MS thesis. Charlottesville (VA): Materials Science and Engineering, University of Virginia; 2006.
61. Gangloff RP, Burns JT, Kim S. Laboratory characterization and fracture mechanics modeling of corrosion–fatigue interaction for aluminum alloy substitution. Final report. Contract F09650-03-D-001. WPAFB, OH; 2005.
62. ASTM · 2007 · vol. 03.01
63. ASTM · 2005 · vol. 03.01
64. Fatigue as a process of cyclic brittle microfracture10.1111/j.1460-2695.2005.00857.x ↗
65. The role of air in fatigue load interaction10.1046/j.1460-2695.2003.00582.x ↗
66. Equivalent initial flaw size testing and analysis of transport aircraft skin splices10.1046/j.1460-2695.2003.00637.x ↗
67. In situ SEM observations of the contrasting effects of an overload on small fatigue crack growth at two different load ratios in 2024-T351 aluminium alloy10.1016/S0142-1123(97)00010-8 ↗
68. Fatigue crack surface crystallography near crack initiating particle clusters in precipitation hardened legacy and modern Al–Zn–Mg–Cu alloys10.1016/j.ijfatigue.2011.01.018 ↗
69. Micromechanisms of multistage fatigue crack growth in a high-strength aluminum alloy10.1016/j.actamat.2006.11.009 ↗
70. Three dimensional microstructures: statistical analysis of second phase particles in AA 7075-T65110.4028/www.scientific.net/MSF.519-521.1 ↗
71. Reliability-based reassessment of corrosion fatigue life10.1016/S0167-4730(01)00002-9 ↗
72. Fatigue growth of small corner cracks in aluminum 6061-T65110.1016/S0142-1123(97)00033-9 ↗
73. Multiple crack interaction and its effect on stress intensity factor10.1016/0013-7944(91)90152-Q ↗
74. Crack shielding and amplification due to multiple microcracks interacting with a macrocrack10.1007/s10704-007-9094-1 ↗
75. Stress concentration factor formulas useful for all notch shapes in a flat test specimen under tension and bending10.1520/JTE12327J ↗
76. Integrity prognosis system10.1016/j.engfracmech.2008.09.007 ↗
77. Cyclic deformation of ferritic steel II. Stage-II crack-propagation10.1016/0956-7151(91)90142-N ↗
78. Environmental fatigue-crack surface crystallography for Al–Zn–Cu–Mg–Mn/Zr10.1007/s11661-008-9522-5 ↗
79. One, no one, and one hundred thousand crack propagation laws: a generalized Barenblatt and Botvina dimensional analysis approach to fatigue crack growth10.1016/j.jmps.2008.09.002 ↗
80. What is fatigue damage? A view point from the observation of low cycle fatigue process10.1016/j.ijfatigue.2004.10.009 ↗
81. The transition between small and long fatigue crack behavior and its relation to microstructure10.1016/j.ijfatigue.2007.09.008 ↗
82. Accurate stress intensity factor solutions for corner cracks at a hole10.1016/S0013-7944(03)00207-8 ↗
83. Stress-intensity equations for cracks in three-dimensional bodies
84. The EIFS distribution for anodized and pre-corroded 7010-T7651 under constant amplitude loading10.1111/j.1460-2695.2005.00912.x ↗
85. Fatigue crack growth from corrosion damage in 7075-T6511 aluminium alloy under aircraft loading10.1016/S0142-1123(02)00168-8 ↗
86. Residual life prediction methods for gas–turbine components10.1016/0025-5416(88)90551-4 ↗
87. An empirical surface crack solution for fatigue propagation analysis of notched components
88. Stress-intensity factor equations for cracks in three-dimensional finite bodies subjected to tension and bending loads
89. Harter JA. An alternative closed-form stress intensity solution for the single part-through and through-the-thickness cracks at offset holes. Contract AFRL-VA-QP-TR-1999-3001. WPAFB, OH; 1999.10.21236/ADA363701 ↗
90. Fracture-mechanics and surface-chemistry studies of fatigue crack-growth in an aluminum-alloy10.1007/BF02700451 ↗
91. Critical assessment of the model for transport-controlled fatigue crack growth
92. Small crack growth and fatigue life predictions for high-strength aluminium alloys. Part I: Experimental and fracture mechanics analysis10.1046/j.1460-2695.1998.00080.x ↗
93. Small-crack growth and fatigue life predictions for high-strength aluminium alloys. Part II: Crack closure and fatigue analyses10.1046/j.1460-2695.2000.00242.x ↗
94. A nonlinear fracture mechanics approach to growth of small cracks
95. Observations on micro-structurally sensitive fatigue crack growth in a widmanstatten Ti–6Al–4V alloy10.1007/BF02646877 ↗
96. Quantitative analysis of microstructural effects on fatigue crack growth in widmanstatten Ti–6Al–4V and Ti–8Al–1Mo–1V10.1016/0013-7944(79)90138-3 ↗
97. Environmentally assisted fatigue in the gaseous atmosphere
98. Some critical aspects of low rate fatigue crack propagation in metallic materials10.1016/j.ijfatigue.2009.10.013 ↗
99. Ageing dependent intrinsic fatigue crack propagation in AA2024
100. Scully JR, Young GA. Hydrogen embrittlement and hydrogen environment embrittlement in Al alloys. In: Gangloff RP, Somerday BP, editors. Gaseous hydrogen embrittlement of materials in energy technologies, vol. 1. Cambridge (UK): Woodhead Publishing Ltd., in press.