Low-cycle fatigue performance and life prediction of a P/M nickel-based superalloy with artificial surface defect at elevated temperature-Reference-Cited by-同舟云学术

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Low-cycle fatigue performance and life prediction of a P/M nickel-based superalloy with artificial surface defect at elevated temperature

Published:2023-12 Issue: Volume:294 Page:109725
ISSN:0013-7944
Container-title:Engineering Fracture Mechanics
language:en
Short-container-title:Engineering Fracture Mechanics

Author:

Wang Zhifang,Shi Yi^ORCID,Yang Xiaoguang,Shi Duoqi

Funder

National Natural Science Foundation of China

China Postdoctoral Science Foundation

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference32 articles.

1. U.S. Department of Defense. Engine Structural Integrity Program (ENSIP). MIL-HDBK-1783B. 2004(Sep.).

2. Fatigue Life of Nickel Powder Rotating Life-Limited Parts;U.S. Department of Transport;FAA,2023

3. Effect of a large population of seeded alumina inclusions on crack initiation and small crack fatigue crack growth in Udimet 720 nickel-base disk superalloy[J];Telesman;Int J Fatigue,2021

4. Effects of high-temperature exposures on the fatigue life of superally Unimet720[R];Gabb,2002

5. T.P. Gabb, J. Telesman, P.T. Kantzos, et al. Initial assessment of the effects of nonmetallic inclusions on fatigue life of powder-metallurgy-processed Udimet720[R]. NASA Technical Memorandum, NASA/TM-2002-211571, 2002:1-12.

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