Author:
Khalili S.M.R.,Ghadjar R.,Sadeghinia M.,Mittal R.K.
Subject
Civil and Structural Engineering,Ceramics and Composites
Reference17 articles.
1. Advances in the bonded composite repair of metallic aircraft structure;Baker,2002
2. Ratwani MM. Analysis of cracked adhesively bonded laminated structures. Paper No. 78483R, AIAA/ASME. In: 19th Structures, structural dynamics and materials conference, Bethesda, MD, American Institute of aeronautics and astronautics Special Publications, 1290 Avenue of Americas, New York, NY 10019, 1978. p. 988–94.
3. An FEAM based methodology for analyzing composite patch repairs of metallic structures;Nagaswamy;Structure Integrity Aging Aircraft, ASME,1995
4. Investigation of cracked thick aluminum panel repaired with bonded composite patch;Schubbe;Eng Fract Mech,1999
5. Modeling of cracked thick metallic structure with bonded composite repair using three-layer technique;Schubbe;Compos Struct,1999
Cited by
26 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