journal article·2021-09

Effects of micro-scale corrosion damage features and local microstructure on fatigue crack initiation location

Noelle Easter C. Co, James T. Burns

Publisher page

Abstract

No abstract is available for this record. The assistant can identify its topic from the title, but cannot infer the study’s results.

Source: Not provided · Quality: missing

Research context

OpenAlex topics: Fatigue and fracture mechanics · Non-Destructive Testing Techniques · Hydrogen embrittlement and corrosion behaviors in metals

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

References (100+)

Show source-provided references
1. Lincoln JW. Risk Assessments of Aging Aircraft. Ohio, USA: 2000.
2. Lincoln JW. Managing the Aging Aircraft Problem. Ohio, USA: 2001.
3. New Generation High Strength High Damage Tolerance 7085 Thick Alloy Product with Low Quench Sensitivity
4. Aerospace applications metallurgical insights into the improved performance of Aluminum Alloy 7085 thick products
5. Aluminum aerospace alloys at ALCAN
6. Aluminum alloys for aircraft structures
7. Application of modern aluminum alloys to aircraft10.1016/0376-0421(95)00004-6 ↗
8. Recent development in aluminium alloys for aerospace applications10.1016/S0921-5093(99)00674-7 ↗
9. Effect of corrosion severity on fatigue evolution in Al-Zn-Mg-Cu10.1016/j.corsci.2009.10.006 ↗
10. On fatigue crack initiation from corrosion pits in 7075–T7351 aluminum alloy10.1016/S1359-6462(00)00434-6 ↗
11. 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 ↗
12. Investigation into crack initiation from corrosion pit in 7075–T6 under ambient laboratory and saltwater environments10.1016/j.engfracmech.2014.12.016 ↗
13. Driving forces for localized corrosion-to-fatigue crack transition in Al-Zn-Mg-Cu10.1111/j.1460-2695.2011.01568.x ↗
14. Koch G, Hagerdorn E, Berens A. Effect of preexisting corrosion on fatigue cracking of aluminum alloys 2024-T3 and 7075-T6. Ohio, USA: 1995.10.21236/ADA430616 ↗
15. Environment sensitive fatigue crack tip processes and propagation in aerospace aluminum alloys
16. Effect of chloride concentration on the corrosion–fatigue crack behavior of an age-hardenable martensitic stainless steel10.1016/j.ijfatigue.2016.05.022 ↗
17. Wanhill RJH, De Luccia JJ. An AGARD-coordinated corrosion fatigue cooperative testing programme. AGARD Report No. 695; 1982.
18. Typical fatigue-initiating discontinuities in metallic aircraft structures10.1016/j.ijfatigue.2011.10.017 ↗
19. Influence of grain structure and slip planarity on fatigue crack growth in low alloying artificially aged 2xxx aluminium alloys10.1016/j.ijfatigue.2006.08.005 ↗
20. The effect of constituent particles in aluminum alloys on fatigue damage evolution: Statistical observations10.1016/j.ijfatigue.2009.02.036 ↗
21. Relationship between fracture toughness, fracture path, and microstructure of 7050 aluminum alloy: Part I. Quantitative characterization10.1007/s11661-998-0246-3 ↗
22. A study of nucleation and fatigue behavior of an aerospace aluminum alloy 2024–T310.1016/j.ijfatigue.2004.06.010 ↗
23. Initiation of fatigue cracks in commercial aluminium alloys and the subsequent propagation of very short cracks10.1016/0013-7944(75)90004-1 ↗
24. Fatigue life prediction from inclusion initiated cracks10.1016/S0142-1123(97)00136-9 ↗
25. Observations of fatigue crack initiation in 7075–T65110.1016/j.ijfatigue.2009.06.003 ↗
26. Corrosion fatigue crack initiation in aluminum alloys 7075 and 705010.5006/1.3294379 ↗
27. Crawford BR, Loader C, Sharp PK. The effect of pitting corrosion on the position of aircraft structural failures; 2004.
29. Fatigue cracking from a corrosion pit in an aircraft bulkhead10.1016/j.engfailanal.2014.01.020 ↗
30. Effects of macro-scale corrosion damage feature on fatigue crack initiation and fatigue behavior10.1016/j.ijfatigue.2017.05.028 ↗
31. Galvanic corrosion-induced fatigue crack initiation and propagation behavior in AA7050-T745110.5006/2132 ↗
32. Fatigue crack formation and growth from localized corrosion in Al-Zn-Mg-Cu10.1016/j.engfracmech.2008.11.005 ↗
33. Equivalent crack size model for pre-corrosion fatigue life prediction of aluminum alloy 7075–T610.1016/j.ijfatigue.2016.03.035 ↗
34. Predicting fatigue crack initiation through image-based micromechanical modeling10.1016/j.actamat.2006.10.038 ↗
35. Data-Science Analysis of the Macro-scale Features Governing the Corrosion to Crack Transition in AA7050-T745110.1007/s11837-018-2864-6 ↗
36. 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 ↗
37. Diffraction characterization of microstructure scale fatigue crack growth in a modern Al-Zn-Mg-Cu alloy10.1016/j.ijfatigue.2011.08.003 ↗
38. ASTM International. ASTM E112 Standard Test Methods for Determining Average Grain Size; 2013.
39. ASTM International. ASTM E1382 Standard Test Methods for Determining Average Grain Size Using Semiautomatic and Automatic Image Analysis; 2010.
40. Determination of cathodic and anodic charge from operando X-ray tomography observation of galvanic corrosion of aluminum alloy 7050–T7451 and 304 stainless steel in a simulated fastener10.5006/1871 ↗
41. Liu C, Rafla VN, Scully JR, Kelly RG. Mathematical modeling of potential and current distributions for atmospheric corrosion of galvanic coupling in airframe components. Corros. 2015, Dallas, Texas: NACE International; 2015.10.5006/C2015-05579 ↗
42. ASTM International. ASTM G1 Standard Practice for Preparing, Cleaning, and Evaluating Corrosion Test; 1999.
43. Effect of initiation feature on microstructure-scale fatigue crack propagation in Al-Zn-Mg-Cu10.1016/j.ijfatigue.2011.08.001 ↗
44. Effect of low temperature on fatigue crack formation and microstructure-scale propagation in legacy and modern Al-Zn-Mg-Cu alloys10.1016/j.ijfatigue.2013.06.025 ↗
45. Fatigue crack initiation at a notch10.1016/j.ijfatigue.2010.09.007 ↗
46. Three-dimensional characterization of microstructurally small fatigue-crack evolution using quantitative fractography combined with post-mortem X-ray tomography and high-energy X-ray diffraction microscopy10.1016/j.actamat.2014.05.021 ↗
47. Marker loads for quantitative fractography of fatigue cracks in aerospace alloys
48. An experimental evaluation of fatigue crack growth10.1016/j.engfailanal.2004.04.002 ↗
49. Barter SA. Fatigue crack growth in 7050T7451 aluminium alloy thick section plate with a surface condition simulating some regions of the F / A-18 structure. Report No. DSTO-TR-1458. Fishermans Bend, Victoria, Australia; 2003.
50. Characterisation of pitting corrosion by white light interferometry10.1016/j.corsci.2006.04.022 ↗
51. Multiscale characterization of pitting corrosion and application to an aluminum alloy10.1016/S0997-7538(00)00162-5 ↗
52. ISO 25178-2:2012 Geometrical product specifications (GPS) — Surface texture: Areal — Part 2: Terms, definitions and surface texture parameters. International Organization for Standardization; 2012.
53. Telesman J. Review of the effects of microstructure on fatigue in aluminum alloys. NASA Technical Memorandum 83626. Ohio, USA; 1984.
54. Microstructural dependence of fracture toughness in high-strength 7000 forging alloys10.1016/j.engfracmech.2007.10.010 ↗
55. A structural integrity prognosis system10.1016/j.engfracmech.2008.09.007 ↗
56. Effects of inclusions, grain boundaries and grain orientations on the fatigue crack initiation and propagation behavior of 2524–T3 Al alloy10.1016/j.msea.2013.05.053 ↗
57. Characterizations of pore and constituent particle populations in 7050–T7451 aluminum plate alloys10.1007/s11661-998-0263-2 ↗
58. Reconstruction of grains and subgrains from electron backscatter diffraction maps10.1111/j.0022-2720.2004.01297.x ↗
59. Grain and subgrain characterisation by electron backscatter diffraction10.1023/A:1017973432592 ↗
60. Electron backscatter diffraction of grain and subgrain structures—resolution considerations10.1046/j.1365-2818.1999.00579.x ↗
61. Characterisation of fine-scale microstructures by electron backscatter diffraction (EBSD)10.1016/j.scriptamat.2004.05.016 ↗
62. Quantitative metallography by electron backscattered diffraction10.1046/j.1365-2818.1999.00578.x ↗
63. Electron backscatter diffraction study on microstructure, texture, and strain evolution in armco iron severely deformed by the differential speed rolling method10.1007/s11661-015-2760-4 ↗
64. Recrystallization and texture development in hot rolled 1050 aluminum10.4028/www.scientific.net/MSF.467-470.357 ↗
65. Understanding a microstructure using GOS (grain orientation spread) and its application to recrystallization study of hot deformed Al-Cu-Mg alloys10.4028/www.scientific.net/MSF.558-559.153 ↗
66. Three-dimensional finite element analysis using crystal plasticity for a parameter study of microstructurally small fatigue crack growth in a AA7075 aluminum alloy10.1016/j.ijfatigue.2008.03.027 ↗
67. Maitland T, Sitzman S. Electron Backscatter Diffraction (EBSD) Technique and Materials Characterization Examples. In: Zhou W, Wang ZL, editors. Scanning Microsc. Nanotechnol. Tech. Appl., Springer; 2007. p. 41–75.10.1007/978-0-387-39620-0_2 ↗
68. Fatigue life prediction of corrosion-damaged high-strength steel using an equivalent stress riser (ESR) model Part I: Test development and results10.1016/j.ijfatigue.2009.05.006 ↗
69. Rusk DT, Hoppe W, Braisted W, Powar N. Corrosion fatigue life prediction using an equivalent stress riser model. In: 11th Jt. NASA/FAA/DoD Conf. Aging Aircr., Phoenix, AZ; 2008.
70. Campbell F. Manufacturing Technology for Aerospace Structural Materials. Manuf. Technol. Aerosp. Struct. Mater., Elsevier; 2006. p. 15–92. https://doi.org/10.1016/B978-185617495-4/50002-0.10.1016/B978-185617495-4/50002-0 ↗
71. Structure–property correlations in Al 7050 and Al 7055 high-strength aluminum alloys10.1016/j.msea.2007.05.116 ↗
72. McMurtrey MD, Burns JT. Corrosion effects on the initiation life and crack growth rate of 7075-T6511 aluminum. In: Proceeding DoD Allied Nations Corros. Conf.; 2015.
73. Buchheit RG, Birbilis N, Gambina F. Characterization and modeling of localized corrosion damage accumulation for aircraft structural integrity. In: Int. Conf. Fract. 11, Turin, Italy; 2005.
74. Electrochemical characteristics of intermetallic phases in aluminum alloys10.1149/1.1869984 ↗
75. Operando observation of galvanic corrosion between aluminum alloy 7050–T7451 and 304 stainless steel in a simulated fastener arrangement using X-ray tomography10.5006/1813 ↗
76. Tiryakioğlu M, Staley J. Physical Metallurgy and Effect of Alloying Additions in Aluminum Alloys. In: Totten, George E; MacKenzie DS, editor. Handb. Alum. vol. 1 Phys. Metall. Process., New York, NY: Marcel Dekker, Inc.; 2003. p. 81–210.
77. Hatch · 2005
78. Effect of microstructure on strain localization in a 7050 aluminum alloy: Comparison of experiments and modeling for various textures10.1016/j.msea.2016.03.012 ↗
79. Predicting fatigue crack initiation from coupled microstructure and corrosion morphology effects10.1016/j.engfracmech.2019.106661 ↗
80. Effects of grain boundary- and triple junction-character on intergranular fatigue crack nucleation in polycrystalline aluminum10.1007/s10853-007-2236-z ↗
81. Roles of microstructure in fatigue crack initiation10.1016/j.ijfatigue.2009.10.005 ↗
82. Influence of grain structure and crystallographic orientation on fatigue crack propagation behavior of 7050 alloy thick plate10.1016/j.ijfatigue.2014.03.009 ↗
83. Relations between microstructure, precipitation, age-formability and damage tolerance of Al-Cu-Mg-Li (Mn, Zr, Sc) alloys for age forming10.1016/j.msea.2005.11.023 ↗
84. Estimating fatigue sensitivity to polycrystalline Ni-base superalloy microstructures using a computational approach10.1111/j.1460-2695.2007.01159.x ↗
85. Influence of grain orientations on the initiation of fatigue damage in an Al-Li alloy10.1046/j.1365-2818.1999.00573.x ↗
86. Fatigue and monotonic loading crack nucleation and propagation in bimodal grain size aluminum alloy10.1016/j.actamat.2011.02.029 ↗
87. Littlewood DJ. A nonlocal approach to modeling crack nucleation in AA 7075-T651. In: ASME 2011 Int Mech Eng Congr Expo IMECE 2011; 2011.10.1115/IMECE2011-64236 ↗
88. The effect of grain size on the fatigue of commercially pure aluminium10.1111/j.1460-2695.1995.tb00868.x ↗
89. On the difference between the misorientation dependences of the energies of tilt and twist boundaries10.1016/0036-9748(87)90390-5 ↗
90. On the micromechanics of void growth by prismatic-dislocation loop emission10.1016/j.jmps.2005.10.011 ↗
91. Microstructural-based physics of failure models to predict fatigue reliability 2006;00:520–5
92. Influence of microstructure variability on short crack behavior through postulated micromechanical short crack driving force metrics10.1016/j.engfracmech.2015.03.001 ↗
93. The physics of fatigue crack initiation10.1016/j.ijfatigue.2012.10.009 ↗
94. The effect of intermediate thermomechanical treatments on the fatigue properties of a 7050 aluminum alloy10.1007/BF02652213 ↗
95. The effect of copper content and degree of recrystallization on the fatigue resistance of 7XXX type aluminum alloys I. Low cycle corrosion fatigue10.1016/0025-5416(79)90167-8 ↗
96. The effect of copper content and degree of recrystallization on the fatigue resistance of 7XXX-type aluminum alloys II Fatigue crack propagation10.1016/0025-5416(80)90209-8 ↗
97. Polycrystal constraint and grain subdivision10.1016/S0749-6419(98)00018-7 ↗
98. Review on slip transmission criteria in experiments and crystal plasticity models10.1007/s10853-015-9553-4 ↗
99. Fatigue Crack Initiation In WASPALOY at 20 °C10.1007/s11661-007-9178-6 ↗
100. Fatigue crack growth along planar slip bands10.1016/0001-6160(84)90229-3 ↗