Simulation of fatigue crack growth in aluminium alloy 7075-T7351 under spike overload and aircraft spectrum loading
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OpenAlex topics: Fatigue and fracture mechanics · Material Properties and Failure Mechanisms · Engineering Diagnostics and Reliability
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References (36)
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1. T.J. Owen, Maj. Gen., F-15 Structures Mishap, in: ASIP Conference, San Antonio, TX, USA. 2008.
2. R.J.H. Wanhill, Molent, L., Barter, S.A., and Amsterdam, E., Milestone Case Histories in Aircraft Structural Integrity Update 2015 in, National Aerospace Laboratory NLR.10.1016/B978-0-12-803581-8.00847-X ↗
3. FAA, Damage-tolerance and fatigue evaluation of structure, in, US Department of Transportation Federal Aviation Administration, 2011.
4. Analysis of stresses and strains near the end of a crack traversing a plate10.1115/1.4011547 ↗
5. A rational analytic theory of fatigue, the trend in engineering
6. W. Elber, The significance of fatigue crack closure, ASTM STP 486 American Society for Testing and Materials, West Conshohocken, Pennsylvania, USA, (1971) 230-242.10.1520/STP26680S ↗
7. Fatigue crack closure under cyclic tension10.1016/0013-7944(70)90028-7 ↗
8. Yielding of steel sheets containing slits10.1016/0022-5096(60)90013-2 ↗
9. J.C. Newman Jr, FASTRAN: A Fatigue Crack Growth Life-Prediction Code Based on the Crack-Closure Concept Version 5.4 User Guide, in, Fatigue & Fracture Associates LLC, Eupora MS, USA. 2013.
10. J.C. Newman, Prediction of Fatigue Crack Growth under Variable-Amplitude and Spectrum Loading Using a Closure Model, in: P.R. Abelkis, C.M. Hudson (Eds.), ASTM International, West Conshohocken, PA, 1982, pp. 255-277.10.1520/STP28863S ↗
11. A. de Koning, U., Ten Hoeve., J., and Henriksen, T.K., Description of crack growth using the strip-yield model for computation of crack opening loads, crack tip stretch, and strain rates, in: ASTM STP 1343, American Society for Testing and Materials, West Conshohocken, PA, 1999, pp. 459-474.10.1520/STP15774S ↗
12. Fatigue crack propagation for a through thickness crack: a crack propagation law considering cyclic plasticity near the crack tip10.1016/j.ijfatigue.2003.12.006 ↗
13. A computational approach for fatigue crack propagation in ship structures under random sequence of clustered loading10.1007/s00773-008-0014-5 ↗
14. Mechanical examination of crack length dependency and material dependency on threshold stress intensity factor range with Dugdale model10.1016/j.engfracmech.2015.01.003 ↗
15. Fatigue thresholds of precracked specimens predicted by modified strip-yield model for plasticity-induced crack closure10.1016/j.tafmec.2022.103635 ↗
16. K.F. Walker, McCoy, M., Ogden, R., and Maxfield, K., Crack growth prediction challenge in wide 7075 T7351 panels, in: ASIP Conference, On-Line. 2020.
17. On the strain energy release rate and fatigue crack growth rate in metallic alloys10.1016/j.engfracmech.2023.109292 ↗
18. Back to basics for the fatigue crack growth rate in metallic alloys
19. J. Schijve, Significance of fatigue cracks in micro-range and macro-range, in, ASTM STP 415, Philadelphia PA. 1967.10.1520/STP47238S ↗
20. J.C. Newman Jr, Discussion on Cyclic Crack Growth Transitional Behaviour, in: Fatigue Crack Propagation ASTM, 1967, pp. 380-383.
21. C.M. Hudson, Effect of Stress Ratio on Fatigue-Crack Growth in 7075-T6 and 2024-T3 Aluminium Alloy Specimens, TN D-5390 (1969).10.1016/0013-7944(69)90003-4 ↗
22. C.M. Hudson, Stidies of Fatigue Crack Growth in Alloys Suitable for Elevated Temperature Applications, TN D-2743 (1965).
23. Fatigue Crack Growth on Several Materials under Single-Spike Overloads and Aircraft Spectra during Constraint-Loss Behavior
24. J.C. Newman Jr, and Walker, K.F., Fatigue crack growth on several materials under single spike overloads and aircraft spectra, in: International Committee on Aeronautical Fatigue, Delft, The Netherlands. 2023.10.1520/MPC20230074 ↗
25. J.C. Newman Jr, and Walker, K.F., Fatigue-Crack-Growth under Single-Spike Overloads/Underloads and Aircraft Spectra during Constraint-Loss Behavior, in: Aircraft Structural Integrity Program Conference, Phoenix AZ USA, 2022.
26. Anon, E-647 Standard Test Method for Measurement of Fatigue Crack Growth Rates, in, ASTM International. 2011.
27. J.C. Newman Jr, Chang, C, Xiao, L., Mear, M.E., and Kale, V.J., FADD2D Fracture Analysis by Distributed Dislocations Version 1.0 User Guide for Personal Computers with Demonstration Example, in, Mississippi State University, 2006.
28. A boundary element method for two dimensional linear elastic fracture analysis10.1007/BF00033829 ↗
29. MINITWIST: A shortened version of TWIST, in, LBF-Bericht FB-146
30. Validation of the Two-Parameter Fracture Criterion using 3D finite-element analyses with the critical CTOA fracture criterion10.1016/j.engfracmech.2015.11.007 ↗
31. J.C. Newman Jr, Fracture Analysis of Various Cracked Configurations in Sheet and Plate Materials, in: ASTM STP 605 Properties Related to Fracture Toughness, ASTM, 1976, pp. 104-123.10.1520/STP27802S ↗
32. Rainflow-on-the-Fly Methodology: Fatigue-Crack Growth under Aircracft Spectrum Loading
33. L. Smith, and Feiger, J., A-10 Fatigue and Failure Analysis Variable Amplitude Fatigue Crack Grwoth Rate Test Plan, in, Southwest Research Institute, 2020.
34. Effects of Constraint on Crack Growth Under Aircraft Spectrum Loading
35. J.C. Newman Jr, Crews, J.H., Bigelow, C.A., and Dawicke, D.S., Variations of a global constraint factor in cracked bodies under tension and bending loads, in: M. Kirk, A. Bakker (Eds.) Constraint effects in fracture: Theory and applications, ASTM STP 1244, ASTM, 1995, pp. 21-42.10.1520/STP14629S ↗
36. Crack-growth calculations in 7075–T7351 aluminum alloy under various load spectra using an improved crack-closure model10.1016/j.engfracmech.2004.01.004 ↗