Experimental and finite element analysis on the performance of vacuum-assisted resin infused single scarf repairs

Author:

Tzetzis D.,Hogg P.J.

Publisher

Elsevier BV

Subject

Applied Mathematics,General Mathematics

Reference39 articles.

1. Baker AA, Chester RJ, Hugo GR, Radtke TC. Scarf Repairs to graphite/epoxy components, composite repair of military aircraft structures. In: AGARD conference proceedings 550, 79th meeting of the structures and materials panel on composite repair of military aircraft structures, October 3–5; Spain, 1994. p. 19/1–12.

2. Repair of cracked or defective metallic aircraft components with advanced fibre composites – an overview of australian work;Baker;Compos Struct,1984

3. Bonded composite repair of fatigue-cracked primary aircraft structure;Baker;Compos Struct,1999

4. Repair of mirage III aircraft using the BFRP crack patching technique;Baker;Theor App Fract Mech,1984

5. Baker A, Chester RJ, Retchford MJ, Roberts JA. The development of a boron/epoxy doubler system for the F-111 wing pivot fitting-materials engineering aspects. In: International conference on aircraft damage assessment and repair, Melbourne; August 1991.

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