journal article·2017-03

Fatigue life calculation for a specimen with an impact pit considering impact damage, residual stress relaxation and elastic-plastic fatigue damage

Zhixin Zhan, Weiping Hu, Fei Shen, Qingchun Meng, Jing Pu, Zhidong Guan

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Abstract

Abstract In this study, a continuum damage mechanics based method is proposed to calculate the fatigue life of a specimen with an impact pit. The impact process is simulated by a quasi-static analysis. The residual stress and the impact damage are calculated. Then, the elastic-plastic fatigue damage of the material is considered as the specimen experiences cyclic loading. The residual stress relaxation is investigated via a coupled analysis of the residual stress and elastic-plastic damage evolution. The calculated results agree well with the experimental results. The effects of the impact depth and radius that the impact object has on the fatigue failure are also discussed.
Source: openaire · Quality: candidate unverified · Source record ↗

Research context

OpenAlex topics: Fatigue and fracture mechanics · Surface Treatment and Residual Stress · High-Velocity Impact and Material Behavior

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

References (39)

Show source-provided references
1. Defect tolerance assessment of a helicopter component subjected to multiaxial load10.1016/j.engfracmech.2010.06.012 ↗
2. Application of damage tolerance principles to the design of helicopters10.1016/j.ijfatigue.2008.05.010 ↗
3. Experimental method for and theoretical research on defect tolerance of fixed plate based on damage mechanics10.1016/j.cja.2013.04.017 ↗
4. Fatigue-life prediction using local stress-strain concepts10.1007/BF02326426 ↗
5. The strength of metals under combined alternating stresses10.1243/PIME_PROC_1935_131_008_02 ↗
6. Foreign object damage on the leading edge of gas turbine blades10.1016/j.ast.2014.01.001 ↗
7. Influence of foreign object damage (FOD) on the fatigue life of simulated Ti-6Al-4V airfoils10.1016/S0734-743X(00)00044-0 ↗
8. Influence of foreign-object damage on crack initiation and early crack growth during high-cycle fatigue of Ti–6Al–4V10.1016/S0013-7944(00)00045-X ↗
9. Continuous damage mechanics—a tool to describe phenomena before crack initiation10.1016/0029-5493(81)90007-8 ↗
10. Kachanov · 1986 · 1
11. Lemaitre · 1996 · 1
12. Continuum damage mechanics-based approach to the fatigue life prediction for 7050–T7451 aluminum alloy with impact pit10.1177/1056789515608232 ↗
13. Residual stress distributions and their influence on fatigue lifetimes10.1016/S0142-1123(01)00133-5 ↗
14. An evaluation of shot peening, residual stress and stress relaxation on the fatigue life of AISI 4340 steel10.1016/S0142-1123(01)00205-5 ↗
15. Schijve · 2001
16. The effect of residual stress relaxation by the vibratory stress relief technique on the textures of grains in AA 6061 aluminum alloy10.1016/j.msea.2014.03.037 ↗
17. Evaluation of residual stress relaxation and its effect on fatigue strength of AISI 316L stainless steel ground surfaces: experimental and numerical approaches10.1016/j.ijfatigue.2012.10.008 ↗
18. Stability of machining induced residual stresses in Inconel 718 under quasi-static loading at room temperature10.1016/j.msea.2014.09.118 ↗
19. Residual stress relaxation and low-and high-cycle fatigue behavior of shot-peened medium-carbon steel10.1016/j.ijfatigue.2013.07.001 ↗
20. Fatigue and residual stress relaxation of deep rolled differently aged aluminum alloy AA611010.1016/j.msea.2005.11.064 ↗
21. Modeling of residual stress relaxation of fatigue in 2024–T351 aluminum alloy10.1016/j.ijfatigue.2010.08.012 ↗
22. Stability of machining induced residual stresses in Inconel 718 under quasi-static loading at room temperature10.1016/j.msea.2014.09.118 ↗
23. Mechanical relaxation of localized residual stresses associated with foreign object damage10.1016/S0921-5093(02)00543-9 ↗
24. Investigation of residual stress relaxation under cyclic load10.1016/S0142-1123(01)00132-3 ↗
25. Effect of shot-peening variables and residual stresses on the fatigue life of leaf-spring specimens
26. Finite element modelling of shot peening process: prediction of the compressive residual stresses, the plastic deformations and the surface integrity10.1016/j.msea.2006.03.097 ↗
27. The residual stress state due to a spherical hard-body impact10.1016/S0167-6636(01)00064-3 ↗
28. Lemaitre · 1990
29. Lemaitre · 1994 · 346
30. Lemaitre · 2005 · 188
31. On some modifications of kinematic hardening to improve the description of ratchetting effects10.1016/0749-6419(91)90050-9 ↗
32. Uniaxial ratcheting and fatigue failure of tempered 42CrMo steel: damage evolution and damage-coupled visco-plastic constitutive model10.1016/j.ijplas.2008.06.004 ↗
33. A non-linear continuous fatigue damage model10.1111/j.1460-2695.1988.tb01216.x ↗
34. Multiaxial fatigue damage modelling at macro scale of Ti–6Al–4V alloy10.1016/j.ijfatigue.2009.03.003 ↗
35. The fatigue life prediction for structure with surface scratch considering cutting residual stress, initial plasticity damage and fatigue damage10.1016/j.ijfatigue.2015.01.011 ↗
36. A non-local approach based on the hypothesis of damage dissipation potential equivalence to the effect of stress gradient in fretting fatigue10.1016/j.ijfatigue.2016.04.028 ↗
37. Effects of fatigue damage and wear on fretting fatigue under partial slip condition10.1016/j.wear.2015.07.012 ↗
38. Military Handbook – MIL-HDBK-5H: metallic materials and elements for aerospace vehicle structures.US Department of Defense; 1998.
39. Wu · 1998 · vol. 1