Optimising fatigue crack growth predictions for small cracks under variable amplitude loading
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OpenAlex topics: Fatigue and fracture mechanics · Structural Health Monitoring Techniques · Ultrasonics and Acoustic Wave Propagation
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References (48)
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1. The practical need for short fatigue crack growth rate models10.1016/j.ijfatigue.2020.105980 ↗
2. Typical fatigue-initiating discontinuities in metallic aircraft structures10.1016/j.ijfatigue.2011.10.017 ↗
3. The lead crack fatigue lifing framework10.1016/j.ijfatigue.2010.09.009 ↗
4. Department of Defense Joint Service Specification Guide, Aircraft Structures. JSSG-2006, U.S. Department of Defense; 1998.
5. Department of Defense Standard Practice - Aircraft Structural Integrity Program. MIL-STD-1530D, U.S. Department of Defense; 2016.
6. Initiation of fatigue cracks in commercial aluminium alloys and the subsequent propagation of very short cracks10.1016/0013-7944(75)90004-1 ↗
7. Short cracks in aerospace structures
8. Characterizing small fatigue cracks in metallic alloys10.1007/s11661-004-0103-y ↗
9. Fatigue-life prediction methodology using small-crack theory10.1016/S0142-1123(98)00058-9 ↗
10. Dislocation theory based short crack model and its application for aircraft aluminum alloys10.1016/j.engfracmech.2009.07.022 ↗
11. Small fatigue crack growth in metallic materials: A model and its application to engineering alloys10.1016/j.actamat.2007.08.022 ↗
12. Barter S, Burchill M, Jones M. Improving the prediction of small crack growth in 7XXX aluminium alloys. In: 28th ICAF Symposium, Helsinki, Finland; 2015.
13. Burchill M, Barter S, Amsterdam E. Improved predictions for combat aicraft fatigue life from a novel testing program. In: 15th Australian International Aerospace Congress (AIAC15), Melbourne, Australia; 2014.
14. On small fatigue crack growth rates in AA7085-T7452
15. Lessons from a fatigue prediction challenge for an aircraft wing shear post10.1016/j.ijfatigue.2019.02.007 ↗
16. Measured fatigue crack growth increments versus predictions for small cracks in 7XXX aluminium alloys10.1016/j.ijfatigue.2017.07.013 ↗
17. The effect of compressive peak stress on fatigue behaviour10.1016/0142-1123(86)90041-1 ↗
18. The importance of compressive stresses on fatigue crack propagation rate10.1016/j.ijfatigue.2005.07.003 ↗
19. Fatigue crack acceleration effects during tensile underloads in 7010 and 8090 aluminium alloys10.1016/j.ijfatigue.2006.02.048 ↗
20. Effect of underloads in small fatigue crack growth10.1016/j.ijfatigue.2021.106706 ↗
21. Observations of crack path changes caused by periodic underloads in AA7050-T745110.1016/j.ijfatigue.2007.08.021 ↗
22. Machine Learning-Based predictions of crack growth rates in an aeronautical aluminium alloy10.1016/j.tafmec.2024.104278 ↗
23. Bayesian neural network analysis of fatigue crack growth rate in nickel base superalloys10.2355/isijinternational.36.1373 ↗
24. Use of modern numerical methods for life predictions
25. Analysis of stress ratio effects on fatigue propagation in a sintered duplex steel by experimentation and artificial neural network approaches10.1016/j.ijfatigue.2004.01.004 ↗
26. A comparison study of machine learning based algorithms for fatigue crack growth calculation10.3390/ma10050543 ↗
27. Zhi · 2019
28. White · 2019
29. Dixon B, Krieg B, Hodgen C. Easigrow Enhanced Capabilities for Release 2.1.0. DSTG-TN-XX, Defence Science and Technology Group (to be published).
30. Particle swarm optimization
31. Particle Swarm Optimization
32. Barter SA, Wanhill RJH. Marker loads for quantitative fractography (QF) of fatigue in aerospace alloys. In: ICAF 2009: bridging the gap between theory and operational practice, Rotterdam, The Netherlands; 2009.10.1007/978-90-481-2746-7_2 ↗
33. Quantification of the fatigue severity of porosity in aluminium alloy 7050–T7451 thick plate10.1016/j.ijfatigue.2018.05.019 ↗
34. Equivalent initial damage sizes (EIDS) for type 1C anodised aluminium alloy 7085–T7452 under variable amplitude loading10.1016/j.engfailanal.2023.107578 ↗
35. Outcomes from the fatigue testing of seventeen centre fuselage structures10.1016/j.ijfatigue.2018.02.018 ↗
36. Simpson D, Molent L, Graham A, Landry N, Schmidt N, Roussel J. The Canadian and Australian F/A-18 international follow-on structural test project. In: ICAS 2002 congress, Torronto, Canada, International Council of the Aeronautical Sciences; 2002.
37. Callihan TN. F/A-18E/F full scale structural fatigue testing. In: ASIP conference San Antonio, Texas: 4-6 December 2007; 2007.
38. A fractographic study of fatigue crack growth from a cold expanded fastener hole at an engineering “crack initiation” scale10.1111/ffe.14245 ↗
39. Suresh · 1998
40. Simple rainflow counting algorithms10.1016/0142-1123(82)90018-4 ↗
41. Stress-Intensity factor equations for cracks in three-dimensional finite bodies subjected to tension and bending loads
42. The effect of overloads on threshold and crack closure10.1016/0142-1123(85)90027-1 ↗
43. The effect of crack growth retardation when comparing constant amplitude to variable amplitude loading in an aluminium alloy
44. Microstructurally small fatigue crack growth rates in aluminium alloys for developing improved predictive models10.1051/matecconf/201816513004 ↗
45. Dixon · 2008
46. Newman · 1981 · 53
47. An engineering model for propagation of small cracks in fatigue10.1016/S0013-7944(96)00057-4 ↗
48. Clerc