Modelling of adhesive bonding for aircraft structures applying the insertion squeeze flow method

Author:

Burka P.,Liu X.,Thompson M.C.,Sheridan J.

Publisher

Elsevier BV

Subject

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

Reference10 articles.

1. Adhesive bonding studied for joints in aircraft structures;Ritter;Adv Mater Processes,2005

2. MoJo. Modular joints for composite aircraft components. Appendix i. Description of work. Tech. rep.; sixth framework programme specific targeted research or innovation project MoJo; 2006.

3. Joining fibre-reinforced plastics;Matthews,1987

4. Wong R. Sandwich constructions in the starship. In: Materials working for you in the 21st century. SAMPE symposium and exhibition, vol. 37; 1992. p. 186–97.

5. Composites affordability initiative: transitioning advanced aerospace technologies through cost and risk reduction;Russel;The AMMTIAC Quart,2006

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