Enhanced bonded aircraft repair using nano-modified adhesives

Author:

Gkikas G.,Sioulas D.,Lekatou A.,Barkoula N.M.,Paipetis A.S.

Publisher

Elsevier BV

Subject

Applied Mathematics,General Mathematics

Reference49 articles.

1. Joining and repair of aircraft composite structures;Baker,1997

2. Yu S, Tong MN, Critchlow G. Use of carbon nanotubes reinforced epoxy as adhesives to join aluminium plates. Mater Des 2010;31 [Supplement 1(0):S126–S9].

3. Adhesive joints in composite laminates—a combined numerical/experimental estimate of critical energy release rates;Balzani;Int J Adhes Adhes,2012

4. Manufacturing processes for advanced composites;Campbell,2004

5. Baker AA, Roberts JD, Rose LRF. Experimental study of overlap joint parameters relevant to the K reduction due to crack-patching. In: National SAMPE symposium and exhibition (proceedings), SAMPE, Azusa, CA, USA, 1983. p. 627–39.

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