Effect of corrosion severity on fatigue evolution in Al–Zn–Mg

Effect of corrosion severity on fatigue evolution in Al–Zn–Mg–Cu

Published:2010-02 Issue:2 Volume:52 Page:498-508
ISSN:0010-938X
Container-title:Corrosion Science
language:en
Short-container-title:Corrosion Science

Author:

Burns James T.,Kim Sangshik,Gangloff Richard P.

Publisher

Elsevier BV

Subject

General Materials Science,General Chemical Engineering,General Chemistry

Reference46 articles.

1. Predicting fatigue life of pre-corroded 2024-T3 aluminum;Gruenberg;Intl. J. Fatigue,2004

2. Fatigue crack formation and growth from localized corrosion in Al–Zn–Mg–Cu;Kim;Eng. Fract. Mech.,2009

3. K. Sharp, T. Mills, S. Russo, G. Clark, Q. Liu, Effects of exfoliation corrosion on the fatigue life of two high-strength aluminum alloys, Aging Aircraft 2000, FAA/DoD/NASA, 2001.

4. The EIFS distribution for anodized and pre-corroded 7010-T7651 under constant amplitude loading;Crawford;Fatigue Fract. Eng. Mater. Struct.,2005

5. R.P. Gangloff, J.T. Burns, S. Kim, Laboratory characterization and fracture mechanics modeling of corrosion–fatigue interaction for aluminum alloy substitution, Final Report, Contract F09650-03-D-0001, WPAFB, OH, 2005.

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