Multiaxial high-cycle fatigue life prediction model based on the critical plane approach considering mean stress effects
Source abstract
Abstract
The aim of this paper is to propose a modified multiaxial high-cycle fatigue criterion based on the critical plane approach. The proposed criterion contains three parameters, that is, shear stress amplitude, normal stress amplitude and mean normal stress. In order to take into account the mean shear stress effects, the critical plane is determined by the maximum shear stress. In the proposed multiaxial fatigue criterion, the influence of mean normal stress on fatigue damage is also considered. Based on the proposed criterion, the multiaxial fatigue life is predicted, and the results showed a good agreement with experimental data obtained from some literatures.
Source: crossref · Quality: baseline
Research context
OpenAlex topics: Fatigue and fracture mechanics · Probabilistic and Robust Engineering Design · High Temperature Alloys and Creep
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
College of Mechanical Engineering and Applied Electronics Technology, Beijing University of Technology, Beijing, P.R. China
References (31)
Show source-provided references
1. Brown MW and Miller KJ (1982) Two decades of progress in the assessments of multiaixial low-cycle fatigue life. Low-Cycle Fatigue and Life Prediction ASTM482-499.10.1520/STP32442S ↗
2. 10.1016/S0142-1123(00)00075-X10.1016/S0142-1123(00)00075-X ↗
3. 10.1016/S0142-1123(98)00046-210.1016/S0142-1123(98)00046-2 ↗
4. 10.1016/S0142-1123(98)00047-410.1016/S0142-1123(98)00047-4 ↗
5. 10.1016/j.matdes.2015.02.00810.1016/j.matdes.2015.02.008 ↗
6. 10.1016/j.ijfatigue.2011.03.00110.1016/j.ijfatigue.2011.03.001 ↗
7. Findley WN (1959) A theory for the effect of mean stress on the fatigue of metals under combined torsion and axial load or bending. Journal of Engineering Materials and Technology-Transactions of the ASME 81: 301–306.
8. Findley WN (1956) Modified theories of fatigue failure under combined stress. Proceedings of the Society of Experimental Stress Analysis 14: 35–46.
9. 10.1016/j.ijfatigue.2004.05.00610.1016/j.ijfatigue.2004.05.006 ↗
10. Gough HJ, Pollard HV (1935) The strength of metals under combined alternating stress. Process Instrument Mechanic Engineering 131: 3–8.
11. 10.1016/j.tafmec.2014.08.00410.1016/j.tafmec.2014.08.004 ↗
12. 10.1016/j.ijfatigue.2010.08.00110.1016/j.ijfatigue.2010.08.001 ↗
13. 10.1016/j.tafmec.2014.07.01510.1016/j.tafmec.2014.07.015 ↗
14. 10.1016/j.ijfatigue.2009.01.00610.1016/j.ijfatigue.2009.01.006 ↗
15. 10.1016/j.ijfatigue.2005.01.00310.1016/j.ijfatigue.2005.01.003 ↗
16. 10.1046/j.1460-2695.2000.00291.x10.1046/j.1460-2695.2000.00291.x ↗
17. 10.1299/jsme1958.20.25710.1299/jsme1958.20.257 ↗
18. 10.1111/j.1460-2695.1991.tb00673.x10.1111/j.1460-2695.1991.tb00673.x ↗
19. 10.1299/jsmemag.49.334_310.1299/jsmemag.49.334_3 ↗
20. 10.1016/S0142-1123(96)00064-310.1016/S0142-1123(96)00064-3 ↗
21. 10.1177/105678950933831710.1177/1056789509338317 ↗
22. 10.1115/1.308638710.1115/1.3086387 ↗
23. 10.1111/j.1460-2695.2009.01381.x10.1111/j.1460-2695.2009.01381.x ↗
24. 10.1016/j.ijfatigue.2007.08.01810.1016/j.ijfatigue.2007.08.018 ↗
25. 10.1111/j.1460-2695.2011.01594.x10.1111/j.1460-2695.2011.01594.x ↗
26. 10.1111/j.1460-2695.2008.01228.x10.1111/j.1460-2695.2008.01228.x ↗
27. 10.1016/j.ijfatigue.2004.11.01210.1016/j.ijfatigue.2004.11.012 ↗
28. 10.1115/1.322499510.1115/1.3224995 ↗
29. 10.1007/s11665-014-1335-710.1007/s11665-014-1335-7 ↗
30. Zhang CC, Yao WX (2010) A new model for life prediction of multiaxial high-cycle fatigue. Chinese Journal of Theoretical and Applied Mechanics 42: 1225–1330. in Chinese.
31. 10.1111/j.1460-2695.2010.01523.x10.1111/j.1460-2695.2010.01523.x ↗