Small fatigue crack growth behavior of titanium alloy TC4 at different stress ratios-Reference-Cited by-同舟云学术

Small fatigue crack growth behavior of titanium alloy TC4 at different stress ratios

Published:2018-08-29 Issue:1 Volume:42 Page:339-351
ISSN:8756-758X
Container-title:Fatigue & Fracture of Engineering Materials & Structures
language:en
Short-container-title:Fatigue Fract Eng Mater Struct

Author:

Hu Xu-Teng¹,Zhu Lei¹^ORCID,Jiang Rong¹,Song Ying-Dong¹²,Qu Shou-Dao³

Affiliation:

1. Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering; Nanjing University of Aeronautics and Astronautics; Nanjing Jiangsu China

2. State Key Laboratory of Mechanics and Control of Mechanical Structures; Nanjing University of Aeronautics and Astronautics; Nanjing Jiangsu China

3. Herbert Gleiter Institute of Nanoscience; Nanjing University of Science and Technology; Nanjing Jiangsu China

Funder

Nanjing University of Aeronautics and Astronautics

Fundamental Research Funds for the Central Universities

Jiangsu Innovation Program for Graduate Education

National Natural Science Foundation of China

Publisher

Wiley

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Link

http://onlinelibrary.wiley.com/wol1/doi/10.1111/ffe.12911/fullpdf

Reference40 articles.

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2. Foreign-object damage and high-cycle fatigue of Ti-6Al-4V;Peters;Mater Sci Eng A,2001

3. Ritchie RO Suresh S Hutchinson JW Milligan WW Thompson AW High-cycle fatigue and time-dependent failure in metallic alloys for propulsion systems. AFOSR-MURI High-Cycle Fatigue Program Third Progress Report F49620-97-1-0365 1999

4. On the use of the Goodman diagram for high cycle fatigue design;Nicholas;Int J Fract,1996

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