Fatigue Crack Growth with Negative Stress Ratio Following Single Overloads in 2024-T3 and 7075-T6 Aluminum Alloys-Reference-Cited by-同舟云学术

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Fatigue Crack Growth with Negative Stress Ratio Following Single Overloads in 2024-T3 and 7075-T6 Aluminum Alloys

Published: Issue: Volume: Page:27-27-14
ISSN:
Container-title:Fatigue Crack Growth Under Spectrum Loads
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Author:

Stephens RI,Chen DK,Hom BW

Publisher

ASTM International

Cited by 17 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Effect of Microstructure on Fatigue Damage Accumulation in 7075 Aluminum Alloy Subjected to a Single Compressive Overload;Metals;2024-08-28

2. Fatigue Crack Growth Evaluation of IMO Type B Spherical LNG Cargo Tank Considering the Effect of Stress Ratio and Load History;Journal of Welding and Joining;2022-02-28

3. Underloading, Overloading and Cumulative Damage;Structural Integrity;2021-11-19

4. Effect of periodic underloads on fatigue crack growth in three steels used in hydraulic turbine runners;International Journal of Fatigue;2016-04

5. Fatigue crack growth and closure behavior under random loadings in 7475-T7351 aluminum alloy;International Journal of Fatigue;2013-02

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