Fatigue life prediction under variable amplitude loading using a non-linear damage accumulation model
Source abstract
Abstract
Most of engineering components in service are usually subjected to variable cyclic loading. It is important to predict fatigue life and deal with the issue about fatigue damage accumulation for these components. One of the largest difficulties in fatigue failure analysis is to find a representative ‘damage criterion’ which can be easily connected with the Wöhler curve taken as the known material data. The most commonly used model is the Miner’s rule which ignores the loading history effect, under the same loading conditions the experimental results are higher than the Miner expectations for low-to-high load sequence and are lower than the Miner expectations for high-to-low load sequence. The fatigue driving stress that causes fatigue damage is presented to predict residual fatigue life under variable amplitude loading. It increases with loading cycles until equals the fatigue strength when fracture occurs. By determining the equivalent number of cycles that yields the same fatigue driving stress as the previous loads, the remaining life can be predicted. The proposed damage criterion is connected cycle by cycle to the Wöhler curve and the experimental results are in a good agreement with the model predictions.
Source: crossref · Quality: baseline
Research context
OpenAlex topics: Fatigue and fracture mechanics · Engineering Structural Analysis Methods · Material Properties and Failure Mechanisms
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
School of Mechanical, Electronic, and Industrial Engineering, University of Electronic Science and Technology of China, Chengdu, Sichuan, P.R. China
References (43)
Show source-provided references
1. Aid A · Materials and Selection · 2011 · 32 · 183
2. 10.1016/j.msea.2011.12.10510.1016/j.msea.2011.12.105 ↗
3. Bao M · Journal of Beijing Polytechnic University · 2001 · 27 · 434
4. Bui-Quoc T · Journal of Materials · 1971 · 6 · 718
5. Buxbaum AO (1987) Structure fatigue design . Machine Press, pp.224–232.
6. 10.1115/1.317366210.1115/1.3173662 ↗
7. 10.1111/j.1460-2695.1988.tb01216.x10.1111/j.1460-2695.1988.tb01216.x ↗
8. 10.1016/S0142-1123(98)00018-810.1016/S0142-1123(98)00018-8 ↗
9. 10.1007/s00773020001210.1007/s007730200012 ↗
10. 10.1016/j.ijpvp.2013.10.01310.1016/j.ijpvp.2013.10.013 ↗
11. 10.1016/j.apenergy.2013.04.04710.1016/j.apenergy.2013.04.047 ↗
12. Dowling NE · Journal of Materials · 1972 · 7 · 71
13. 10.1016/S0142-1123(97)00081-910.1016/S0142-1123(97)00081-9 ↗
14. Gatts RR · Journal of Fluids Engineering, Transactions of the ASME · 1961 · 83 · 52910.1115/1.3664588 ↗
15. Ince A and Glinka G (2014) A generalized fatigue damage parameter for multiaxial fatigue life prediction under proportional and non-proportional loadings. International Journal of Fatigue. 62: 34–41.10.1016/j.ijfatigue.2013.10.007 ↗
16. 10.1177/105678951244880310.1177/1056789512448803 ↗
17. Krouse M · ASTM STP · 1967 · 415 · 384
18. 10.1177/105678951244963810.1177/1056789512449638 ↗
19. 10.1016/j.ijfatigue.2011.03.00610.1016/j.ijfatigue.2011.03.006 ↗
20. 10.1111/j.1460-2695.2005.00877.x10.1111/j.1460-2695.2005.00877.x ↗
21. Lee YL, Pan J, Hathaway R, (2005) Fatigue Testing and Analysis Theory and Practice, Elsevier: Butterworth–Heinemann Press, pp. 44–66.
22. 10.1115/1.344368910.1115/1.3443689 ↗
23. 10.1016/j.mechmat.2013.11.00810.1016/j.mechmat.2013.11.008 ↗
24. 10.1007/s11003-006-0097-210.1007/s11003-006-0097-2 ↗
25. 10.1007/BF0005351910.1007/BF00053519 ↗
26. Marco SM · Transactions of the ASME · 1954 · 76 · 627
27. 10.1016/j.ijfatigue.2006.02.04310.1016/j.ijfatigue.2006.02.043 ↗
28. 10.1016/j.ijfatigue.2004.08.00510.1016/j.ijfatigue.2004.08.005 ↗
29. 10.1243/03093247V12426210.1243/03093247V124262 ↗
30. Miner MA · Journal of Applied Mechanics · 1945 · 68 · 339
31. 10.1098/rspa.2009.034810.1098/rspa.2009.0348 ↗
32. 10.1016/S0141-0296(02)00055-X10.1016/S0141-0296(02)00055-X ↗
33. Richart FE · Proceedings of the American Society for Testing and Materials · 1948 · 48 · 767
34. Shang DG · Acta Aeronautica ET Astronautica Sinica · 1998 · 19 · 647
35. 10.1016/S0142-1123(98)00069-310.1016/S0142-1123(98)00069-3 ↗
36. Valluri SR · Aerospace Engineering · 1961 · 20 · 18
37. 10.1080/15376490231722485110.1080/153764902317224851 ↗
38. Xie LY · Chinese Journal of Applied Mechanics · 1992 · 9 · 32
39. Ye DY · 1996
40. 10.1016/j.engfracmech.2012.04.02110.1016/j.engfracmech.2012.04.021 ↗
41. 10.1515/tjj-2012-001310.1515/tjj-2012-0013 ↗
42. 10.1177/105678951245603010.1177/1056789512456030 ↗
43. 10.1177/105678951039707710.1177/1056789510397077 ↗