Pin and bolt bearing strength of fibreglass/aluminium laminates

Author:

Caprino G.,Squillace A.,Giorleo G.,Nele L.,Rossi L.

Publisher

Elsevier BV

Subject

Mechanics of Materials,Ceramics and Composites

Reference18 articles.

1. Development of fibre metal laminates for advanced aerospace structures;Vogelesang;J Mater Process Technol,2000

2. Fiber metal laminates—matching the best in composites and metals;Shankar;Mater Technol,1994

3. Vercammen RWA, Ottens HH. Full-scale glare fuselage panel tests. National Aerospace Laboratory, NLR TP 97278; 1997

4. Design and testing of bonded GLARE patches in the repair of fuselage fatigue cracks in large transport aircraft;Fredell,1994

5. Bridging stress distribution in centre-cracked fiber reinforced metal laminates: modeling and experiment;Ya-Jun;Eng Fract Mech,1999

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