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Experimental and Finite Element Characterization of the Crippling Failure of Composite Stiffeners
Progressive failure analysis based on the complete unloading method was conducted to investigate the crippling failure of carbon/epoxy composite stiffeners under axial compression. A modified arc-length algorithm was incorporated into a nonlinear finite element method to trace the equilibrium path a...
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Published in: | Key engineering materials 2006-12, Vol.326-328, p.1773-1776 |
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Main Authors: | , , , , , |
Format: | Article |
Language: | English |
Citations: | Items that this one cites |
Online Access: | Get full text |
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Summary: | Progressive failure analysis based on the complete unloading method was conducted to
investigate the crippling failure of carbon/epoxy composite stiffeners under axial compression. A
modified arc-length algorithm was incorporated into a nonlinear finite element method to trace the
equilibrium path after local buckling. For the validation of the finite element method, several
carbon/epoxy Z-section stiffeners were tested in compression. The finite element results on the
buckling and crippling stresses showed good agreement with the experimental results. |
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ISSN: | 1013-9826 1662-9795 1662-9795 |
DOI: | 10.4028/www.scientific.net/KEM.326-328.1773 |