Non-linear finite element analysis of thin composite structures
Data(s) |
13/02/2009
13/02/2009
1997
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Formato |
application/pdf |
Identificador |
ICCM-11 PROCEEDINGS ICCM-11 Proceedings. - Australia, 1997. - VoI. 6, p. 808-818 |
Idioma(s) |
eng |
Relação |
http://www.bib.ualg.pt/artigos/DocentesEST/MOINonLiFin.pdf |
Direitos |
openAccess |
Palavras-Chave | #Elementos finitos #620 #Non-linear analysis #Finite elements #Multilaminate shells |
Tipo |
conferenceObject |
Resumo |
A non-conforming three-node triangular finite element with 18 degree of freedom, is used in conjugation with the Kirchhoff theory for the non-linear analysis of thin composite plate-shell structure. The formulation of the geometrically non-linear analysis is based on an updated Lagrangian formulation associated with the Newton-Raphson iterative technique, which incorporates an automatic arc-length control procedure. |