Comparison between composite and metallic patches for repairing aircraft structures of aluminum alloy 7075 T6-Reference-Cited by-同舟云学术

Comparison between composite and metallic patches for repairing aircraft structures of aluminum alloy 7075 T6

Published:2015-11 Issue: Volume:80 Page:128-135
ISSN:0142-1123
Container-title:International Journal of Fatigue
language:en
Short-container-title:International Journal of Fatigue

Author:

Bachir Bouiadjra Bachir,Benyahia Fayçal,Albedah Abdulmohsen,Bachir Bouiadjra Bel Abbes,Khan Sohail M.A.

Funder

Deanship of Scientific Research at King Saud University

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering,Mechanics of Materials,General Materials Science,Modelling and Simulation

Reference24 articles.

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3. The effects of disbands on the stress intensity factor of aluminium panels repaired using composite materials;Ouinas;Compos Struct,2007

4. Fatigue crack growth of bonded composite repairs in gigacycle regime;Wang;Int J Fatigue,2006

5. Damage tolerance of bonded aircraft structures;Alderliesten;Int J Fatigue,2009

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