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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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Bibliographic Details
Published in:Key engineering materials 2006-12, Vol.326-328, p.1773-1776
Main Authors: Choi, Jin Ho, Son, Hee Jin, Choi, Ji Young, Choi, Sang Min, Kweon, Jin Hwe, Che, Woo Seong
Format: Article
Language:English
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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.
ISSN:1013-9826
1662-9795
1662-9795
DOI:10.4028/www.scientific.net/KEM.326-328.1773