Very high cycle fatigue behaviors of a turbine engine blade alloy at various stress ratios-Reference-Cited by-同舟云学术

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Very high cycle fatigue behaviors of a turbine engine blade alloy at various stress ratios

Published:2017-06 Issue: Volume:99 Page:35-43
ISSN:0142-1123
Container-title:International Journal of Fatigue
language:en
Short-container-title:International Journal of Fatigue

Author:

Yang Kun,He Chao,Huang Qi,Huang Zhi Yong,Wang Cong,Wang Qingyuan,Liu Yong Jie,Zhong Bin

Funder

National Natural Science Research Foundation of China

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering,Mechanics of Materials,General Materials Science,Modeling and Simulation

Reference36 articles.

1. An assessment of the role of near-threshold crack growth in high-cycle-fatigue life prediction of aerospace titanium alloys under turbine engine spectra;Larsen;Int J Fract,1996

2. Effect of shot peening on fretting fatigue of Ti811 alloy at elevated temperature;Zhang;Int J Fatigue,2009

3. Fatigue limit - material property as an opened or closed system? Practical view on the aircraft components failures in GCF area;Shanyavskiy;Int J Fatigue,2006

4. Gigacycle fatigue of ferrous alloys;Wang;Fatigue Fract Eng Mater Struct,1999

5. Effects of stress ratio on high-cycle and very-high-cycle fatigue behavior of a Ti–6Al–4V alloy;Liu;Mater Sci Eng A,2015

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