A critical consideration for the use of Al-cladding for protecting aircraft aluminum alloy 2024 against corrosion-Reference-Cited by-同舟云学术

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A critical consideration for the use of Al-cladding for protecting aircraft aluminum alloy 2024 against corrosion

Published:2012-02 Issue:1 Volume:57 Page:36-42
ISSN:0167-8442
Container-title:Theoretical and Applied Fracture Mechanics
language:en
Short-container-title:Theoretical and Applied Fracture Mechanics

Author:

Pantelakis Sp.G.,Chamos A.N.,Kermanidis Al.Th.

Publisher

Elsevier BV

Subject

Applied Mathematics,Mechanical Engineering,Condensed Matter Physics,General Materials Science

Reference20 articles.

1. Structural Integrity of Aging Airplanes;Atluri,1991

2. AGARD Workshop. Fatigue in the presence of corrosion, in: RTO Meeting Proceedings, vol. 18, Corfu, Greece, 5–9 October 1998.

3. BRITE/EURAM No 1053. Structural Maintenance of Aging Aircraft (SMAAC), CEC Brussels, Final Report, Brussels, 1999.

4. Corrosion-induced hydrogen embrittlement in aluminum alloy 2024;Kamoutsi;Corrosion Science,2006

5. Corrosion-induced hydrogen embrittlement of 2024 and 6013 aluminum alloys;Petroyiannis;Theoretical and Applied Fracture Mechanics,2004

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