Author:
Hosseini-Toudeshky Hossein,Ghaffari Mir Ali,Mohammadi Bijan
Subject
Civil and Structural Engineering,Ceramics and Composites
Reference23 articles.
1. Fredell RW, Barneveld W, Vogelesang LV. Design and testing of bonded GLARE patches in the repair of fuselage fatigue cracks in large transport aircraft. In: Proceedings of the 39th international SAMPE symposium, April 11−14, Anaheim, CA, 1994.
2. Nonlinear analysis of bonded composite patch repair of cracked aluminum panels;Naboulsi;Compos Struct,1998
3. Fatigue crack growth of adhesively repaired panel using perfectly and imperfectly composite patches;Naboulsi;Theor Appl Fract Mech,1997
4. Characterization of fatigue crack growth in aluminum panels with a bonded composite patch;Naboulsi;Compos Struct,1997
5. Mixed-mode fatigue crack growth in aluminium plates with composite patches;Chung;Int J Fatigue,2003
Cited by
22 articles.
订阅此论文施引文献
订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献