Composite to metal bonding in aerospace and other applications
Author:
Publisher
Elsevier
Link
http://woodhead.metapress.com/index/X167L41T46267Q24.pdf
Reference86 articles.
1. The relative merits of the Boeing wedge test and the double cantilever beam test for assessing the durability of adhesively bonded joints, with particular reference to the use of fracture mechanics;Adams;Int. J. Adhes. Adhes.,2009
2. Effect of surface treatment on fatigue behavior of metal/carbon fiber laminates;Almeida;J. Mater. Sci.,2008
3. Mode I fracture of epoxy bonded composite joints: 1. Quasi-static loading;Ashcroft;Int. J. Adhes. Adhes.,2001
4. Adhesion in hostile environments;Armstrong;Int. J. Adhes. Adhes.,1992
5. Efforts to standardize aerospace composite repairs,1988–2003;Armstrong;Proc. Inst. Mech. Eng. G- J. Aero. Eng.,2003
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