The effects of manufacturing-induced and in-service related bonding quality reduction on the mode-I fracture toughness of composite bonded joints for aeronautical use

Author:

Markatos D.N.,Tserpes K.I.,Rau E.,Markus S.,Ehrhart B.,Pantelakis Sp.

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites

Reference31 articles.

1. Adhesive bonding: science, technology and applications;Adams,2005

2. Adhesively bonded joints in composite materials: an overview;Banea;Proc Inst Mech Eng, Part L: J Mater Des Appl,2009

3. Bonded joints with composite adherends. Part I. Effect of specimen configuration, adhesive thickness, spew fillet and adherend stiffness on fracture;Taib;Int J Adhes Adhes,2006

4. Butkus LM, Johnson WS. Designing for the durability of bonded structures. Presented at the FAA/NASA symposium on continued airworthiness of aircraft structures, Atlanta; 1996. p. 28–30. [August].

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