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Applied Composite Materials
Erschienen in: Applied Composite Materials 6/2013

01.12.2013

A Stacked-Shell Finite Element Approach for Modelling a Dynamically Loaded Composite Bolted Joint Under in-Plane Bearing Loads

verfasst von: G. M. K. Pearce, A. F. Johnson, A. K. Hellier, R. S. Thomson

Erschienen in: Applied Composite Materials | Ausgabe 6/2013

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Abstract

This paper presents the results of a study into a novel application of the “stacked-shell” laminate modelling approach to dynamically loaded bolted composite joints using the explicit finite element code PAM-CRASH. The stacked-shell approach provides medium-high fidelity resolution of the key joint failure modes, but is computationally much more efficient than full 3D modelling. For this work, a countersunk bolt in a composite laminate under in-plane bearing loading was considered. The models were able to predict the onset of damage, failure modes and the ultimate load of the joint. It was determined that improved debris models are required in order to accurately capture the progressive bearing damage after the onset of joint failure.
Vorheriger Artikel Integrated Design for Manufacturing of Braided Preforms for Advanced Composites Part I: 2D Braiding
Nächster Artikel Numerical Simulation of Impact Responses on Through-thickness Stitched Foam Core Sandwich Composite

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Metadaten
Titel
A Stacked-Shell Finite Element Approach for Modelling a Dynamically Loaded Composite Bolted Joint Under in-Plane Bearing Loads
verfasst von
G. M. K. Pearce
A. F. Johnson
A. K. Hellier
R. S. Thomson
Publikationsdatum
01.12.2013
Verlag
Springer Netherlands
Erschienen in
Applied Composite Materials / Ausgabe 6/2013
Print ISSN: 0929-189X
Elektronische ISSN: 1573-4897
DOI
https://doi.org/10.1007/s10443-013-9316-9

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