Post-impact Fatigue Performance of 2198-T8 Aluminum-Lithium Alloy Sheet with Pre-crack-Reference-Cited by-同舟云学术

Post-impact Fatigue Performance of 2198-T8 Aluminum-Lithium Alloy Sheet with Pre-crack

Published:2023-05-16 Issue:6 Volume:51 Page:20220546
ISSN:0090-3973
Container-title:Journal of Testing and Evaluation
language:en
Short-container-title:J. Test. Eval.

Author:

Zhang X. Y.¹,Cui Z. F.²,Pan X. C.²,Chen Z.³,Dong T. J.¹,Chen Y. J.⁴

Affiliation:

1. Engineering Technology Training Center, Civil Aviation University of China, No. 2898 Jinbei Rd., Tianjin 300300, China

2. Sino-European Institute of Aviation Engineering, Civil Aviation University of China, No. 2898 Jinbei Rd., Tianjin 300300, China

3. Aeronautical Engineering Institute, Civil Aviation University of China, No. 2898 Jinbei Rd., Tianjin 300300, China

4. Sino-European Institute of Aviation Engineering, Civil Aviation University of China, No. 2898 Jinbei Rd., Tianjin 300300, China (Corresponding author), e-mail: yjchen@cauc.edu.cn, https://orcid.org/0000-0002-1832-5503

Publisher

ASTM International

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

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4. Defects as a Root Cause of Fatigue Failure of Metallic Components. III: Cavities, Dents, Corrosion Dents, Scratches;Zerbsr;Engineering Failure Analysis,2019

5. P. Shivalli, “The Effect of Dents on Fatigue Life and Fatigue Crack Growth of Aluminum 2024-T3 Bare Sheet” (PhD diss., Wichita State University, 2006).