journal article·2021-12Open access

Crack nucleation from non-metallic inclusions in aluminum alloys described by peridynamics simulations

Mohammad Rezaul Karim, Kai Kadau, Santosh Narasimhachary, Francesco Radaelli, Christian Amann, Kaushik Dayal, Stewart Silling, Timothy C. Germann

Abstract

Abstract Conventional engineering methods oftentimes have challenges in the quantification of crack nucleation processes from manufacturing defects that are relevant for engineering component lifing. We present peridynamic simulation framework for the description of the crack nucleation process from cluster of non-metallic inclusions in aluminum alloys. Our non-local simulation framework characterizes crack nucleation process as multiple micro-crack nucleation events from individual inclusions, and eventually one micro-crack dominates. We define individual stages of the crack nucleation process, i.e., nucleation, micro-crack, technical, and crack initiation, that allow a quantification and meta model development of both the individual stages and the entire crack nucleation process.
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Research context

OpenAlex topics: Numerical methods in engineering · Fatigue and fracture mechanics · Geotechnical Engineering and Underground Structures

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References (53)

Show source-provided references
1. Sankaran · 2017
2. Recent advances in the development of aerospace materials10.1016/j.paerosci.2018.01.001 ↗
3. Application of modern aluminum alloys to aircraft10.1016/0376-0421(95)00004-6 ↗
4. Vrana J, Zimmer A, Lohmann H, Heinrich W, S. AG. Evolution of the ultrasonic inspection over the past decades on the example of heavy rotor forgings, 19th WCNDT, München, Germany; 2016.
5. Defects as a root cause of fatigue failure of metallic components. II: Non-metallic inclusions10.1016/j.engfailanal.2019.01.054 ↗
6. Defects as a root cause of fatigue failure of metallic components. III: Cavities, dents, corrosion pits, scratches10.1016/j.engfailanal.2019.01.034 ↗
7. Defects as a root cause of fatigue failure of metallic components. I: Basic aspects10.1016/j.engfailanal.2019.01.055 ↗
8. Peridynamic states and constitutive modeling10.1007/s10659-007-9125-1 ↗
9. Top500.org, LANL CTS-1 Grizzly - Tundra Extreme Scale, Xeon E5-2695v4 18C 2.1GHz, Intel Omni-Path | TOP500, https://www.top500.org/system/178972, (Accessed 29 April 2021).
10. Microstructural development during hot forging of Al 7075 powder10.1016/j.jallcom.2015.03.099 ↗
11. Fatigue properties and cracking mechanisms of a 7075 aluminum alloy under axial and torsional loadings10.1016/j.prostr.2019.12.069 ↗
12. Multiaxial fatigue behavior and life prediction of 7075–T651 aluminum alloy under two-step loading
13. Study on fatigue crack initiation and propagation from forging defects10.1016/j.prostr.2017.11.100 ↗
14. Evaluation of NDT-signals for use in the fracture mechanics safety analysis10.1080/09603409.1998.11689587 ↗
15. Die Bedeutung der Ultraschall-Ersatzreflektorgrösse für die Bruchmechanik, untersucht an schweren Schmiedestücken für Turbomaschinen
16. Schwant R, Timo D. Life assessment of general electric large steam turbine rotors, Life assessment and improvement of turbo-generator rotors for fossil plants; 1984, 3.
17. A rational analytic theory of fatigue
18. A three component model for representing wide range fatigue crack growth data10.1016/0013-7944(79)90067-5 ↗
19. Service load fatigue damage—a historical perspective10.1016/S0142-1123(99)00054-7 ↗
20. Mechanisms of fatigue-crack propagation in ductile and brittle solids10.1023/A:1018655917051 ↗
21. Fatigue crack initiation and propagation from inclusions in steel forgings
22. Manual and mechanized ultrasonic inspection of large components in respect of flaw estimation by fracture mechanics10.1016/0029-5493(89)90151-9 ↗
23. Berger C, Mayer K, Oberparleiter W, Scarlin R. Initiation of fatigue cracks at non-metallic inclusions in large forgings. In: Fracture 84, Elsevier, 1984, pp. 2107-2116.10.1016/B978-1-4832-8440-8.50213-1 ↗
24. The stress analysis of cracks, Handbook
25. Advances in simulation of arbitrary 3D crack growth using FRANC3D NG ICF12
26. Belytschko · 2013
27. Extended finite element method for cohesive crack growth10.1016/S0013-7944(01)00128-X ↗
28. Reformulation of elasticity theory for discontinuities and long-range forces10.1016/S0022-5096(99)00029-0 ↗
29. Peridynamic theory for progressive damage prediction in center-cracked composite laminates10.1016/j.compstruct.2009.02.015 ↗
30. Damage progression from impact in layered glass modeled with peridynamics
31. Why do cracks branch? A peridynamic investigation of dynamic brittle fracture10.1007/s10704-015-0056-8 ↗
32. Silling · 2014
33. Probabilistic fracture mechanics for heavy-duty gas turbine rotor forgings10.1115/1.4038524 ↗
34. Radaelli F, Kadau K, Amann C, Gumbsch P. Probabilistic fracture mechanics framework including crack nucleation of rotor forging flaws. In: Turbo Expo: Power for Land, Sea, and Air, American Society of Mechanical Engineers, 2019. p. V07AT32A002.10.1115/GT2019-90418 ↗
35. Peridynamic theory of solid mechanics10.1016/S0065-2156(10)44002-8 ↗
36. Linearized theory of peridynamic states10.1007/s10659-009-9234-0 ↗
37. Aluminum A. Understanding Cold Finished Aluminum Alloys: Alloy 7075, Technical Data Sheet, 2.
38. Numerical modeling of the effect of randomly distributed inclusions on fretting fatigue-induced stress in metals10.3390/met8100836 ↗
39. A study of nucleation and fatigue behavior of an aerospace aluminum alloy 2024–T310.1016/j.ijfatigue.2004.06.010 ↗
40. A study of thermomechanical behaviour and grain size evolution of AA7050 under hot forging conditions
41. Kervick · 2006
42. Simulated extreme value fatigue sensitivity to inclusions and pores in martensitic gear steels10.1016/j.engfracmech.2011.01.027 ↗
43. Narasimhachary SB, Smith K, Shinde SR, Amann C, Kadau K, Iyer S. Life Assessment of Large Gas Turbine Blades, in: Turbo Expo: Power for Land, Sea, and Air, American Society of Mechanical Engineers, 2019, pp. V07AT31A015.10.1115/GT2019-91630 ↗
44. A. E606/E606M-12, Standard test method for strain-controlled fatigue testing, in, ASTM International West Conshohocken, PA; 2012.
45. 647: Standard test method for measurement of fatigue crack growth rates
46. Influence of orientation and temperature on the fatigue crack growth of a nickel-based directionally solidified superalloy10.1016/j.msea.2014.09.007 ↗
47. Additive manufacturing in the context of structural integrity10.1016/j.ijfatigue.2016.07.005 ↗
48. Material point method calculations with explicit cracks
49. Simulation of dynamic fracture with the material point method using a mixed J-integral and cohesive law approach10.1007/s10704-011-9602-1 ↗
50. Crack nucleation in variational phase-field models of brittle fracture10.1016/j.jmps.2017.09.006 ↗
51. A phase field method to simulate crack nucleation and propagation in strongly heterogeneous materials from direct imaging of their microstructure10.1016/j.engfracmech.2015.03.045 ↗
52. A phase-field model for cohesive fracture10.1002/nme.4553 ↗
53. Multiscale simulation from atomistic to continuum–coupling molecular dynamics (MD) with the material point method (MPM)10.1080/14786430600625578 ↗