Large deformation dynamic finite element analysis of delaminated composite plates using contact-impact conditions


Autoria(s): Chandrashekhar, M; Ganguli, Ranjan
Data(s)

2014

Resumo

A new C-0 composite plate finite element based on Reddy's third order theory is used for large deformation dynamic analysis of delaminated composite plates. The inter-laminar contact is modeled with an augmented Lagrangian approach. Numerical results show that the widely used ``unconditionally stable'' beta-Newmark method presents instability problems in the transient simulation of delaminated composite plate structures with large deformation. To overcome this instability issue, an energy and momentum conserving composite implicit time integration scheme presented by Bathe and Baig is used. It is found that a proper selection of the penalty parameter is very crucial in the contact simulation. (C) 2014 Elsevier Ltd. All rights reserved.

Formato

application/pdf

Identificador

http://eprints.iisc.ernet.in/50358/1/com_str_144_92_2014.pdf

Chandrashekhar, M and Ganguli, Ranjan (2014) Large deformation dynamic finite element analysis of delaminated composite plates using contact-impact conditions. In: COMPUTERS & STRUCTURES, 144 . pp. 92-102.

Publicador

PERGAMON-ELSEVIER SCIENCE LTD

Relação

http://dx.doi.org/ 10.1016/j.compstruc.2014.07.025

http://eprints.iisc.ernet.in/50358/

Palavras-Chave #Aerospace Engineering (Formerly, Aeronautical Engineering)
Tipo

Journal Article

PeerReviewed