Analysis of Fatigue Indicator Parameters for Ti-6Al-4V microstructures using extreme value statistics in the transition fatigue regime
Source abstract
Abstract
Abstract Extreme value (EV) statistics have been previously utilized to model the tails of distributions of computed Fatigue Indicator Parameters (FIPs) to provide a method of ranking microstructures in terms of resistance to fatigue crack formation under identical loading conditions. FIPs that capture the two primary transgranular mechanisms for fatigue crack formation and early stages of growth in bimodal Ti-6Al-4V are computed for cyclic strain-controlled loading conditions corresponding to transition fatigue where there is perceptible macroscopic plastic cyclic strain, but the polycrystal cyclic elastic strain range dominates the cyclic plastic strain range. A statistical volume element (SVE) ensemble approach is employed, in which a large number of microstructure samples are constructed for simulation. The peaks-over-threshold method is used to identify extreme values within the FIP distributions which are then fit to the Generalized Pareto Distributions, enabling rank-ordering of various microstructures with regard to resistance to fatigue crack formation. Microstructure attributes including the grain size, orientation, and nearest neighbor arrangements are quantified in the neighborhood of FIP ‘hot spots’.
Source: openaire · Quality: candidate unverified · Source record ↗
Research context
OpenAlex topics: Fatigue and fracture mechanics · High Temperature Alloys and Creep · Hydrogen embrittlement and corrosion behaviors in metals
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (52)
Show source-provided references
1. Lütjering G, Williams JC. Titanium based intermetallics. Titanium; 2007. p. 337–66.
2. Microstructure-based fatigue modeling of cast A356–T6 alloy10.1016/S0013-7944(02)00021-8 ↗
3. Computational micromechanics of microstructures in the HCF-VHCF regimes10.1016/j.ijfatigue.2016.05.019 ↗
4. Microstructure-based crystal plasticity modeling of cyclic deformation of Ti–6Al–4V10.1016/j.ijplas.2006.11.009 ↗
5. Simulation of slip band evolution in duplex Ti-6Al-4V10.1016/j.actamat.2009.10.025 ↗
6. Zhang M. Crystal plasticity modeling of Ti-6Al-4V and its application in cyclic and fretting fatigue analysis. PhD Thesis. Georgia Institute of Technology; 2008.
7. Analysis of Fatigue Indicator Parameters for Ti-6Al-4V microstructures using extreme value statistics in the HCF regime10.1016/j.ijfatigue.2020.106096 ↗
8. Prediction of maximum fatigue indicator parameters for duplex Ti–6Al–4V using extreme value theory10.1016/j.actamat.2020.02.009 ↗
9. Microstructure-sensitive extreme-value probabilities of high-cycle fatigue for surface vs. subsurface crack formation in duplex Ti–6Al–4V10.1016/j.actamat.2011.09.031 ↗
10. Microstructure-sensitive modeling of high cycle fatigue10.1016/j.ijfatigue.2009.03.021 ↗
11. Simulated microstructure-sensitive extreme value probabilities for high cycle fatigue of duplex Ti–6Al–4V10.1016/j.ijplas.2011.01.006 ↗
12. Microstructure-sensitive extreme value probabilities for high cycle fatigue of Ni-base superalloy IN10010.1016/j.ijplas.2009.08.001 ↗
13. Microstructure-sensitive HCF and VHCF simulations10.1016/j.ijfatigue.2012.09.014 ↗
14. Effects of algorithmic simulation parameters on the prediction of extreme value fatigue indicator parameters in duplex Ti-6Al-4V10.1016/j.ijfatigue.2020.105865 ↗
15. Microstructure-sensitive computational estimates of driving forces for surface versus subsurface fatigue crack formation in duplex Ti-6Al-4V and Al 7075–T610.1007/s11837-019-03804-1 ↗
16. Assessment of small fatigue crack growth driving forces in single crystals with and without slip bands10.1007/s10704-012-9726-y ↗
17. Mesoscale modeling of microstructurally small fatigue cracks in metallic polycrystals10.1016/j.msea.2014.01.015 ↗
18. ABAQUS Unified FEA. 2015. Dassault Systemes: Cedex, France.
19. DREAM.3D: a digital representation environment for the analysis of microstructure in 3D10.1186/2193-9772-3-5 ↗
20. An overview on the use of titanium in the aerospace industry10.1016/0921-5093(96)10233-1 ↗
21. Influence of processing on microstructure and mechanical properties of (α+β) titanium alloys10.1016/S0921-5093(97)00778-8 ↗
22. Influence of microstructure on high-cycle fatigue of Ti-6Al-4V: bimodal vs. lamellar structures10.1007/s11661-002-0160-z ↗
23. Microstructure-sensitive computational modeling of fatigue crack formation10.1016/j.ijfatigue.2010.01.003 ↗
24. Dwell-sensitive fatigue under biaxial loads in the near-alpha titanium alloy IMI68510.1016/0142-1123(94)90194-5 ↗
25. A review of dwell sensitive fatigue in titanium alloys: the role of microstructure, texture and operating conditions10.1016/S0142-1123(03)00145-2 ↗
26. Lengthscale-dependent, elastically anisotropic, physically-based hcp crystal plasticity: application to cold-dwell fatigue in Ti alloys10.1016/j.ijplas.2006.10.013 ↗
27. Experimentally validated dwell and cyclic fatigue crack nucleation model for α–titanium alloys10.1016/j.scriptamat.2016.08.031 ↗
28. Crystallography of Fatigue Crack Initiation and Growth in Fully Lamellar Ti-6Al-4V10.1007/s11661-009-0064-2 ↗
29. Homogenized constitutive and fatigue nucleation models from crystal plasticity FE simulations of Ti alloys, Part 2: Macroscopic probabilistic crack nucleation model10.1016/j.ijplas.2013.02.008 ↗
30. On the mechanism of fatigue and dwell-fatigue crack initiation in Ti-6Al-4V10.1016/j.scriptamat.2020.03.031 ↗
31. Concurrent operation of 〈c + a〉 slip and twinning under cyclic loading of Ti-6Al-4V10.1016/j.scriptamat.2018.07.033 ↗
32. Analysis of deformation mechanisms operating under fatigue and dwell-fatigue loadings in an α/β titanium alloy10.1016/j.ijfatigue.2019.105341 ↗
33. The effects of crystallographic orientation on fatigue crack initiation behavior in Ti-6Al-4V10.1016/j.ijfatigue.2018.07.039 ↗
34. On the mechanisms of fatigue facet nucleation in titanium alloys10.1111/j.1460-2695.2008.01284.x ↗
35. Dunne F, Walker A, Rugg D. A systematic study of hcp crystal orientation and morphology effects in polycrystal deformation and fatigue. In: Proceedings of the Royal Society of London A: Mathematical, Physical and Engineering Sciences; 2007. The Royal Society.10.1098/rspa.2007.1833 ↗
36. Fatigue crack nucleation: mechanistic modelling across the length scales10.1016/j.cossms.2014.02.005 ↗
37. A critical plane approach to multiaxial fatigue damage including out-of-phase loading10.1111/j.1460-2695.1988.tb01169.x ↗
38. Simulation-based strategies for microstructure-sensitive fatigue modeling10.1016/j.msea.2006.08.129 ↗
39. Determination of the size of the representative volume element for random composites: statistical and numerical approach10.1016/S0020-7683(03)00143-4 ↗
40. A three-dimensional crystal plasticity model for duplex Ti–6Al–4V10.1016/j.ijplas.2006.11.006 ↗
41. Cyclic plasticity experiments and polycrystal plasticity modeling of three distinct Ti alloy microstructures10.1016/j.ijplas.2013.10.004 ↗
42. Fatigue hot spot simulation for two Widmanstätten titanium microstructures10.1016/j.ijfatigue.2016.05.002 ↗
43. Extreme value analysis of tail departure from log-normality in experimental and simulated grain size distributions10.1016/j.actamat.2013.06.001 ↗
44. Partnership for an Advanced Computing Environment (PACE). 2021, Georgia Institute of Technology. https://pace.gatech.edu/ [accessed 4/12/2021].
45. Simulating the effect of grain boundaries on microstructurally small fatigue crack growth from a focused ion beam notch through a three-dimensional array of grains10.1016/j.actamat.2016.04.006 ↗
46. Effect of microstructure on the elasto-viscoplastic deformation of dual phase titanium structures10.1007/s00466-017-1467-3 ↗
47. Uncertainty-quantified parametrically homogenized constitutive models (UQ-PHCMs) for dual-phase α/β titanium alloys10.1038/s41524-020-00379-3 ↗
48. Characterization of fatigue crack-initiation facets in relation to lifetime variability in Ti–6Al–4V10.1016/j.ijfatigue.2011.11.017 ↗
49. Deformation heterogeneities and their role in life-limiting fatigue failures in a two-phase titanium alloy10.1016/j.actamat.2014.08.034 ↗
50. Local texture and fatigue crack initiation in a Ti-6Al-4V titanium alloy10.1046/j.1460-2695.2002.00480.x ↗
51. Effect of crystallographic orientation and geometrical compatibility on fatigue crack initiation and propagation in rolled Ti-6Al-4V alloy10.1016/j.actamat.2019.07.025 ↗
52. Microplasticity in HCF of Ti-6Al-4V10.1016/S0142-1123(01)00119-0 ↗