journal article·2018-11

Fatigue crack tip strain evolution and crack growth prediction under single overload in laser melting deposited Ti-6.5Al-3.5Mo-1.5Zr-0.3Si titanium alloy

Yanzeng Wu, Rui Bao

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Abstract

Abstract This paper focuses on the fatigue crack tip strain evolution in laser melting deposited Ti-6.5Al-3.5Mo-1.5Zr-0.3Si titanium alloy under constant amplitude loading plus single overload (OL). The digital image correlation (DIC) technique was used to capture and evaluate the crack tip strain fields and crack closure variation; the results showed that the strains near the crack tip become larger and the crack opening load increases after the application of the OL. The size of the retardation distance is consistent with the analysis results of the crack tip strain fields. The crack closure model based on the DIC analysis results can provide good predictions of the crack growth life for both the low and high overload ratios.
Source: openaire · Quality: candidate unverified · Source record ↗

Research context

OpenAlex topics: Additive Manufacturing Materials and Processes · Welding Techniques and Residual Stresses · Titanium Alloys Microstructure and Properties

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

References (45)

Show source-provided references
1. Leyens · 2003
2. Perspectives on titanium science and technology10.1016/j.actamat.2012.10.043 ↗
3. Prediction of the mechanical properties of forged TC11 titanium alloy by ANN10.1016/S0924-0136(01)01006-8 ↗
4. Flow softening and microstructural evolution of TC11 titanium alloy during hot deformation10.1016/j.jmatprotec.2008.04.063 ↗
5. Hot working of Ti-6Al-3Mo-2Zr-0.3Si alloy with lamellar α+β starting structure using processing map10.1016/j.matdes.2008.07.031 ↗
6. Progress and challenges of laser direct manufacturing of large titanium structural components10.3788/CJL20093612.3204 ↗
7. Microstructure and tensile properties of laser melting deposited TiC/TA15 titanium matrix composites10.1016/j.jallcom.2009.05.112 ↗
8. Characterization of microstructure and mechanical properties of laser melting deposited Ti-6.5Al-3.5Mo-1.5Zr-0.3Si titanium alloy10.1016/j.matdes.2013.11.044 ↗
9. The microstructure and mechanical behaviors of the Ti-6.5Al-3.5Mo-1.5Zr-0.3Si alloy produced by laser melting deposition10.1016/j.matchar.2014.09.002 ↗
10. Critical assessment of the fatigue performance of additively manufactured Ti-6Al-4V and perspective for future research10.1016/j.ijfatigue.2015.12.003 ↗
11. Fatigue performance of additive manufactured TiAl6V4 using electron and laser beam melting10.1016/j.ijfatigue.2016.05.001 ↗
12. Low- and high-cycle fatigue resistance of Ti-6Al-4V ELI additively manufactured via selective laser melting: Mean stress and defect sensitivity10.1016/j.ijfatigue.2017.10.021 ↗
13. On the mechanical behaviour of titanium alloy TiAl6V4 manufactured by selective laser melting: fatigue resistance and crack growth performance10.1016/j.ijfatigue.2012.11.011 ↗
14. Crack propagation and fracture toughness of Ti6Al4V alloy produced by selective laser melting
15. Evaluation of fatigue crack propagation behaviour in Ti-6Al-4V manufactured by selective laser melting10.1016/j.ijfatigue.2017.07.014 ↗
16. Fatigue crack growth behavior and microstructural mechanisms in Ti-6Al-4V manufactured by laser engineered net shaping10.1016/j.ijfatigue.2016.08.009 ↗
17. Fatigue crack growth behaviour in laser melting deposited Ti-6.5Al-3.5Mo-1.5Zr-0.3Si alloy10.1016/j.msea.2017.03.001 ↗
18. Schijve · 2009
19. Near-threshold fatigue: a review10.1016/S0142-1123(99)00053-5 ↗
20. Effect of crack closure on non-linear crack tip parameters10.1016/j.ijfatigue.2014.10.001 ↗
21. The evolution of crack-tip stresses during a fatigue overload event10.1016/j.actamat.2010.03.013 ↗
22. Measuring overload effects during fatigue crack growth in bainitic steel by synchrotron X-ray diffraction10.1016/j.ijfatigue.2014.03.015 ↗
23. A study of overload effect on fatigue crack propagation using EBSD, FIB–DIC and FEM methods10.1016/j.engfracmech.2016.04.034 ↗
24. Fatigue crack growth retardation assessment of 2024–T3 and 6061–T6 aluminium specimens10.1016/0167-8442(94)00046-4 ↗
25. Prediction of fatigue crack growth under real stress histories10.1016/S0141-0296(99)00069-3 ↗
26. Effect of underloads or overloads in fatigue crack growth by crack-tip blunting10.1016/j.engfracmech.2005.10.009 ↗
27. Crack retardation equations for the propagation of branched fatigue cracks10.1016/j.ijfatigue.2005.07.016 ↗
28. Estimation of fatigue crack growth retardation due to crack branching10.1016/j.commatsci.2003.12.003 ↗
29. Digital imaging techniques in experimental stress analysis10.1117/12.7972925 ↗
30. Digital image correlation using iterative least squares and pointwise least squares for displacement field and strain field measurements10.1016/j.optlaseng.2008.10.014 ↗
31. Evaluation of crack-tip fields from DIC data: a parametric study10.1016/j.ijfatigue.2016.03.006 ↗
32. Full field measurements of anisotropic stress intensity factor ranges in fatigue10.1016/j.engfracmech.2012.06.002 ↗
33. Crack tip deformation fields and fatigue crack growth rates in Ti-6Al-4V10.1016/j.ijfatigue.2009.02.043 ↗
34. ASTM -13. Standard method for measurement of fatigue crack growth rates. American Society for the Testing of Materials; 2013.
35. Separating plasticity-induced closure and residual stress contributions to fatigue crack retardation following an overload10.1016/j.jmps.2016.10.001 ↗
36. Analysis of stresses and strains near the end of a crack traversing a plate10.1115/1.4011547 ↗
37. Fatigue crack closure under cyclic tension10.1016/0013-7944(70)90028-7 ↗
38. Experimental evaluation of the effect of overloads on fatigue crack growth by analysing crack tip displacement fields10.1016/j.engfracmech.2016.08.026 ↗
39. Digital image correlation measurement of near-tip fatigue crack displacement fields: constant amplitude loading and load history effects10.1111/j.1460-2695.2012.01707.x ↗
40. Effect of overload on crack closure in thick and thin specimens via digital image correlation10.1016/j.ijfatigue.2013.07.002 ↗
41. Plastic zone size estimation under cyclic loadings using in situ optical microscopy fatigue testing10.1111/j.1460-2695.2011.01567.x ↗
42. Effects of a single tensile overload on fatigue crack growth in a 316L steel10.1046/j.1460-2695.1999.00225.x ↗
43. Spectrum loading and crack growth10.1115/1.3425362 ↗
44. Willenborg J, Engle RM, Wood HA. A crack growth retardation model using an effective stress concept. Report No. AFFDL-TR71-1. Air Force Flight Dynamic Laboratory. Wright-Patterson Air Force Base, USA; 1971.10.21236/ADA956517 ↗
45. Bathias · 2010