Subcritical damage mechanisms of bolted joints in CFRP composite laminates

Author:

Ataş A.,Soutis C.

Publisher

Elsevier BV

Subject

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

Reference30 articles.

1. Hart-Smith LJ. Bolted joints in graphite–epoxy composites. Douglas Aircraft Company, NASA Langley Report NASA CR-144899; 1976.

2. Mechanically-fastened joints for advanced composites – phenomenological considerations and simple analyses;Hart-Smith,1980

3. Design and analysis of bolted and riveted joints in fibrous composite structures;Hart-Smith,2003

4. Strength prediction of mechanical joints in composite laminates based on subcritical damage modelling;Atas,2012

5. Fracture mechanisms and failure analysis of carbon fibre/toughened epoxy composites subjected to compressive loading;Jumahat;Compos Struct,2010

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