The structural environment as a factor affecting coating failure in aircraft joints

Author:

Tiong Ung Hing,Clark Graham

Publisher

Elsevier BV

Subject

Applied Mathematics

Reference26 articles.

1. Tailoring the structural integrity process to meet the challenges of aging aircraft;Simpson;International Journal of Fatigue,1999

2. G. Clark, Corrosion and the management of structural integrity, In: ICAF’99:Structural Integrity for the Next Millennium (Rudd, JL editor.) EMAS Ltd Warley 1999.

3. Mechanical failure of thin brittle coatings;Strawbridge;Engineering Failure Analysis,1995

4. Airlines Aloha, Flight 243, Boeing 737-200, N73711, near Maui Hawaii, April 28, 1988. Washington, D. C. 20594: NTSB/AAR-89/03, National Transportation Safety Board, 1989.

5. S. Furuta, H. Terada, H. Sashikuma, Fatigue strength of fuselage joint structures under ambient and corrosive environment. In: ICAF’97: Fatigue in New and Aging Aircraft: EMAS Ltd., 1997, pp. 231–249.

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