journal article·2020-07

Challenging the “ΔKeff is the driving force for fatigue crack growth” hypothesis

Julián Andrés Ortiz González, Jaime Tupiassú Pinho de Castro, Marco Antonio Meggiolaro, Giancarlo Luis Gómez Gonzáles, José Luiz de França Freire

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Abstract

Abstract Tests are used to verify the hypothesis “the fatigue crack growth (FCG) driving force is the effective stress intensity factor range ΔKeff″. The tests are performed measuring FCG rates in steel and aluminum C(T) and DC(T) specimens under fixed {ΔK, Kmax} loading conditions and during FCG delays induced by single overloads. Crack-opening loads Pop are redundantly measured along the crack path in all tests, using independent near and far field strain-gages, as well as Digital Image Correlation (DIC) techniques. Finally, elastoplastic strain loops within the reverse plastic zone ahead of crack tips are measured using a stereo microscope DIC system.
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Research context

OpenAlex topics: Fatigue and fracture mechanics · Non-Destructive Testing Techniques · Ultrasonics and Acoustic Wave Propagation

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

References (49)

Show source-provided references
1. A rational analytic theory of fatigue
2. A critical analysis of crack propagation laws10.1115/1.3656900 ↗
3. Fatigue design techniques, vol. 3: crack propagation, temperature and statistical effects
4. Fatigue crack closure under cyclic tension10.1016/0013-7944(70)90028-7 ↗
5. Elber W. The significance of fatigue crack closure. Damage Tolerance in Aircraft Structures, ASTM STP 486; 1971: 230–42. https://doi.org/10.1520/STP26680S.10.1520/STP26680S ↗
6. von Euw EFG, Hertzberg RW, Roberts R. Delay effects in fatigue crack propagation. ASTM STP 513; 1972: 230–59. https://doi.org/10.1520/STP34123S.10.1520/STP34123S ↗
7. Current aspects of fatigue10.1179/msc.1977.11.8-9.274 ↗
8. Four lectures on fatigue crack growth10.1016/0013-7944(79)90038-9 ↗
9. Newman JC. A crack-closure model for predicting fatigue crack growth under aircraft spectrum loading. Methods and Models for Predicting Fatigue Crack Growth under Random Loading, ASTM STP 748; 1981: 53–84. https://doi.org/10.1520/STP28334S.10.1520/STP28334S ↗
10. de Koning AU, Liefting G. Analysis of crack-opening behavior by application of a discretized strip yield model. Mechanics of Fatigue Crack Closure, ASTM STP 982; 1988: 437–58. https://doi.org/10.1520/STP27224S.10.1520/STP27224S ↗
11. Newman JC. An evaluation of the plasticity-induced crack-closure concept and measurement methods. NASA/TN-1998-208430, Langley Research Center; 1998.
12. A strip-yield algorithm for the analysis of closure evaluation near the crack tip10.1016/j.engfracmech.2004.10.003 ↗
13. Crack closure under high load-ratio conditions for Inconel-718 near threshold behavior10.1016/j.engfracmech.2008.09.009 ↗
14. Kemp · 1990
15. Load interaction effects during fatigue crack growth under variable amplitude loading – a literature review – part I: empirical trends10.1046/j.1460-2695.1998.00083.x ↗
16. Load interaction effects during fatigue crack Growth under variable amplitude loading – a literature review – part II: qualitative interpretation10.1046/j.1460-2695.1999.00158.x ↗
17. Fatigue crack closure: a review of the physical phenomena10.1111/ffe.12578 ↗
18. Singular and non-singular approaches for predicting fatigue crack growth behavior10.1016/j.ijfatigue.2005.07.018 ↗
19. The effective fatigue threshold: significance of the loading cycle below the crack-opening load10.1016/0142-1123(94)90199-6 ↗
20. Analysis of vacuum fatigue crack growth results and its implications10.1016/j.ijfatigue.2005.07.026 ↗
21. Unified approach to fatigue damage evaluation
22. Reconsideration of fatigue crack closure10.1016/0956-716X(92)90164-A ↗
23. A review of crack closure, fatigue crack threshold and related phenomena10.1016/0921-5093(94)90351-4 ↗
24. Crack tip driving forces and crack growth representation under fatigue10.1016/S0142-1123(03)00105-1 ↗
25. A new (ΔK+Kmax)0.5 driving force parameter for crack growth in aluminum alloys10.1016/S0142-1123(01)00023-8 ↗
26. ΔKeff parameter under re-examination10.1016/S0142-1123(03)00129-4 ↗
27. Correlation and prediction of fatigue crack growth for different R-ratios using Kmax and ΔK+ parameters10.1016/j.engfracmech.2003.06.001 ↗
28. Fatigue crack growth mechanisms in steels10.1016/S0142-1123(03)00128-2 ↗
29. Some critical remarks on the use of potential drop and compliance systems to measure crack growth in fatigue experiments
30. Assessment of the fatigue crack closure phenomenon in damage-tolerant aluminium alloy by in-situ high-resolution synchrotron X-ray microtomography10.1080/1478643031000115754 ↗
31. Fatigue and damage in structural materials studied by x-ray tomography10.1146/annurev-matsci-070511-155111 ↗
32. Schijve · 2001
33. Ruckert COFT, Tarpani JR, Milan MT, Bose WW, Spinelli D. Evaluating Berkovitz’s K-parametrization method to predict fatigue loads in failure investigations. Proceedings SAE Fatigue 2004, paper 2004-01-2211. https://doi.org/10.1361/105994906X150759.10.1361/105994906X150759 ↗
34. NASGRO Fracture Mechanics and Fatigue Crack Growth Analysis Software Reference Manual, Version 4.02, NASA 2002.
35. A crack-opening stress equation for fatigue crack growth10.1007/BF00020751 ↗
36. Newman JC, Crews JH, Bigelow CA, Dawicke DS. Variations of a global constraint factor in cracked bodies under tension and bending loads. ASTM STP 1244; 1995: 21–42. https://doi.org/10.1520/STP14629S.10.1520/STP14629S ↗
37. Using the strip-yield mechanics to model fatigue crack growth by damage accumulation ahead of the crack tip10.1016/j.ijfatigue.2017.06.039 ↗
38. Fatigue crack growth predictions based on damage accumulation ahead of the crack tip calculated by strip-yield procedures10.1016/j.ijfatigue.2018.03.001 ↗
39. Crack closure effects on fatigue damage ahead of crack tips10.1016/j.ijfatigue.2019.03.039 ↗
40. Paris PC; Hermann L. Twenty years of reflections on questions involving fatigue crack growth, part II: some observations of fatigue crack closure. Fatigue Thresholds 1:11-33, EMAS 1982.
41. Verification of the ΔKeff hypothesis along the fatigue crack path in thin and thick Al specimens10.3221/IGF-ESIS.49.03 ↗
42. On DIC measurements of ΔKeff to verify if it is the FCG driving force
43. Can ΔKeff be assumed as the driving force for fatigue crack growth?10.3221/IGF-ESIS.33.13 ↗
44. Crack shape evolution under bending-induced partial closure10.1016/j.engfracmech.2017.10.002 ↗
45. Crack retardation equations for the propagation of branched fatigue cracks10.1016/j.ijfatigue.2005.07.016 ↗
46. A J-integral approach using digital image correlation for evaluating stress intensity factors in fatigue cracks with closure effects10.1016/j.tafmec.2017.02.008 ↗
47. Sutton · 2009
48. Using DIC techniques to measure strain ranges inside the cyclic plastic zone ahead of a fatigue crack tip10.3221/IGF-ESIS.49.08 ↗
49. Influence of stress state on crack growth retardation10.1520/STP23215S ↗