Driving forces for localized corrosion-to-fatigue crack transition in Al-Zn-Mg-Cu

Author:

BURNS J. T.,LARSEN J. M.,GANGLOFF R. P.

Publisher

Wiley

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference114 articles.

1. Bucci , R. J. Konish , H. J. Shaw , B. J. 1995 A technical plan to address aircraft structural problems arising from corrosion/corrosion fatigue USAF Corrosion Fatigue Planning Meeting

2. Cole , G. K. Clark , G. Sharp , P. K. 1997 The implication of corrosion with respect to aircraft structural integrity, Report DSTO-RR-0201

3. Koch , G. H. Hagerdorn , E. L. Berens , A. P. 1995 Effect of preexisting corrosion on fatigue cracking of aluminum alloys 2024-T3 and 7075-T6, Contract AFRL-VA-WP-TR-2004-3057

4. Management of Corrosion of Aircraft

5. Corrosion and fatigue research - structural issues and relevance to naval aviation;Hoffman;Int. J. Fatigue,2001

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