The Life Assessment by Linear Cumulative Damage Rule for Cold Dwell Fatigue of Ti-6Al-4V

Author:

OTA Yutaro1,KUBUSHIRO Keiji2,YAMAZAKI Yasuhiro3

Affiliation:

1. Technology Platform Center, IHI Corporation

2. Asia Solution Center, IHI ASIA PACIFIC(Thailand) Co., Ltd.

3. Graduate school of Science and Engineering, Chiba University

Publisher

Society of Materials Science, Japan

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science

Reference26 articles.

1. 1) M. R. Bache, “A review of dwell sensitive fatigue in titanium alloys: the role of microstructure, texture and operating conditions”, International Journal of Fatigue, Vol.25, pp.1079-1087 (2003).

2. 2) M. R. Bache, M. Cope, H.M. Davies, W.J. Evans and G. Harrison, “Dwell sensitive fatigue in a near alpha titanium alloy at ambient temperature”, International Journal of Fatigue, Vol.19, No.1, pp. S83-S88 (1997).

3. 3) K. Wang, F. Wang, W.-C. Cui and A.-L. Tian, “Prediction of cold dwell-fatigue crack growth of titanium alloys”, Acta Metallurgica Sinica (English Letter), Vol. 28, Issue 5, pp. 619–627 (2015).

4. 4) F. Wang and W. Cui, “Experimental investigation on dwell-fatigue property of Ti-6Al-4V ELI used in deep-sea manned cabin”, Materials Science & Engineering A, Vol.642, pp.136-141 (2015).

5. 5) D. Ozturk, A.L. Pilchak and S. Ghosh, “Experimentally validated dwell and cyclic fatigue crack nucleation model for α–titanium alloys”, Scripta Materialia, Vol.127, pp.15-18 (2017).

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