Fatigue Life Prediction Based on FS Criterion for Multi-Axial Loading

Article Preview

Abstract:

The Fatemi–Socie criterion is evaluated using the combined axial torsion fatigue testing results obtained from extensive experiments on thin-walled tubular specimens made from 304 stainless steel. The Fatemi–Socie criterion combines the maximum shear strain amplitude with a consideration of the normal stress on the critical plane. Rainflow cycle counting and Morrow’s plastic work interaction rule are used to calculate fatigue damage. The fatigue life prediction is conducted by using the maximum shear strain plane as the critical plane by considering the weight function and the maximum damage plane as the critical plane. It is concluded that the results gained by two approaches are both acceptable for the case examined.

You might also be interested in these eBooks

Info:

Periodical:

Key Engineering Materials (Volumes 452-453)

Pages:

605-608

Citation:

Online since:

November 2010

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2011 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] A. Fatemi, L. Yang: Cumulative fatigue damage and life prediction theories, a survey of the state of the art for homogeneous materials. Int. J. Fatigue, Vol. 20 (1998), p.9.

DOI: 10.1016/s0142-1123(97)00081-9

Google Scholar

[2] F.A. Kandil, M.W. Brown, and K.J. Miller: Biaxial low-cycle fatigue fracture of 316 stainless steel at elevated temperature, Book 280, The Metal Society, London, (1982), p.203.

Google Scholar

[3] C.H. Wang and M.W. Brown: A path-independent parameter for fatigue under proportional and non-proportional loading. Fatigue Fract. Engng. Mater. Struct., Vol. 16(1993), p.1285.

DOI: 10.1111/j.1460-2695.1993.tb00739.x

Google Scholar

[4] K.N. Smith, P. Watson and T.H. Topper: A stress-strain function for the fatigue of metals, Journal of Materials, Vol. 5(1970), p.767.

Google Scholar

[5] A. Fatemi and D.F. Socie: A critical plane approach to multiaxial fatigue damage including out-of-plane loading. Fatigue Fract. Engng. Mater. Struct, Vol. 14(1988), p.149.

DOI: 10.1111/j.1460-2695.1988.tb01169.x

Google Scholar

[6] J.A. Bannantine and D.F. Socie: A variable amplitude multiaxial fatigue life prediction method, In: Kussmaul K, McDiarmid D. Socie D, editors. ESIS10. London: Mechanical Engineering Publications, (1991), p.35.

Google Scholar

[7] C.H. Wang and M.W. Brown: Life prediction techniques for variable amplitude multiaxial fatigue-Part 1: Theories. Transactions ASME, J. Engng. Mat. Tech., Vol. 18(1996), p.367.

DOI: 10.1115/1.2806821

Google Scholar

[8] C. H Wang. and M.W. Brown: Life prediction techniques for variable amplitude multiaxial fatigue-Part 2: Comparison with experimental results. J. Engng. Mat. Tech., Vol. 18(1996), p.371.

DOI: 10.1115/1.2806822

Google Scholar

[9] J.D. Morrow: The effect of selected sub-cycle sequences in fatigue loading histories, In Random Fatigue Life Predictions, ASME Publication PVP 72, (1986), p.43.

Google Scholar

[10] K.S. Kim, B.L. Lee, and J.C. Park: Biaxial fatigue of stainless steel 304 under irregular loading. fatigue and fracture mechanics: ASTM STP 1389, Halford G.R. and Gallagher, Eds., American Society for Testing and Materials, West Conshohocken, PA (2000).

DOI: 10.1520/stp14795s

Google Scholar

[11] X. Chen, D. Jin: Kwang Soo Kim, A weight function-critical plane approach for low-cycle fatigue under variable amplitude multiaxial loading, Fatigue Fract. Engng. Mater. Struct., Vol. 29 (2006), p.331.

DOI: 10.1111/j.1460-2695.2006.01003.x

Google Scholar