Fatigue crack growth behavior of beta-annealed Ti–6Al–2Sn–4Zr–xMo (x= 2, 4 and 6) alloys: Influence of microstructure and stress ratio

Author:

Qiu Jianke,Feng Xin,Ma Yingjie,Lei Jiafeng,Liu Yuyin,Huang Aijun,Rugg David,Yang Rui

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

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

Reference64 articles.

1. An overview on the use of titanium in the aerospace industry;Boyer;Mater Sci Eng A,1996

2. Progress in structural materials for aerospace systems;Williams;Acta Mater,2003

3. USAF damage tolerant design handbook: guidelines for the analysis and design of damage tolerant aircraft;Wood;United States Air Force,1979

4. EASA CM-PIFS-007 Issue: 01. Engine critical parts-damage tolerance assessment manufacturing and surface induced anomalies. European Aviation Safety Agency; 2013.

5. 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,1989

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