Random-Loading Fatigue Crack Growth Behavior of Some Aluminum and Titanium Alloys-Reference-Cited by-同舟云学术

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Random-Loading Fatigue Crack Growth Behavior of Some Aluminum and Titanium Alloys

Published: Issue: Volume: Page:74-74-27
ISSN:
Container-title:Structural Fatigue in Aircraft
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Author:

Smith S. H.

Publisher

ASTM International

Cited by 11 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. Nonlinear Ultrasonics for Early Damage Detection;Virtual and Mobile Healthcare;2020

2. Nonlinear Ultrasonics for Early Damage Detection;Emerging Design Solutions in Structural Health Monitoring Systems;2015

3. Bibliography;Fatigue Damage;2009-01

4. Fatigue life prediction under random loading using total hysteresis energy;International Journal of Pressure Vessels and Piping;1998-11

5. 1966;Bibliography on the Fatigue of Materials, Components and Structures;1990

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