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Evaluation of a progressive failure analysis methodology for laminated composite structures
Author(s) -
David W. Sleight,
Norman F. Knight,
John Wang
Publication year - 1997
Publication title -
28th structures, structural dynamics and materials conference
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.1997-1187
Subject(s) - structural engineering , finite element method , composite number , lamination , progressive collapse , failure assessment , materials science , material failure theory , nonlinear system , shell (structure) , composite material , engineering , reinforced concrete , physics , layer (electronics) , quantum mechanics
A Progressive failure analysis methodology has been developed for predicting the nonlinear response and failure of laminated composite structures. The progressive failure analysis uses C{superscript}1 plate and shell elements based on classical lamination theory to calculate the in-plane stresses. Several failure criteria, including the maximum strain criterion, Hashin''s criterion, and Christensen''s criterion, are used to predict the failure mechanisms. The progressive failure analysis model is implemented into a general purpose finite element code and can predict the damage and response of laminated composite structures from initial loading to final failure.

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