Author:
Arnold W S,Marshall I H,Wood J
Abstract
The problem of clamp-up in bolted composite joints has been studied using three-dimensional finite element techniques. In contrast to previous work, a contact analysis has been incorporated enabling both the pin and washer to be modelled. Friction and clamp-up distribution have been shown to significantly effect stress levels in the vicinity of a fastener hole. The results have shown reasonable correlation with experimentally observed strengths and failure modes.
Subject
Mechanical Engineering,Aerospace Engineering
Cited by
3 articles.
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