Static and high-rate loading of single and multi-bolt carbon–epoxy aircraft fuselage joints
Author:
Publisher
Elsevier BV
Subject
Mechanics of Materials,Ceramics and Composites
Reference37 articles.
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5. Modelling of bird strike on an aircraft wing leading edge made from fibre metal laminates – Part 2: Modelling of impact with SPH bird model;McCarthy;Appl Compos Mater,2004
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