Buckling analysis of laminated composite plates using an efficient C0 FE model
Buckling analysis of laminated composite plates is carried out by using an efficient C0 FE model developed based on higher order zigzag theory. In this model the first derivatives of transverse displacement have been treated as independent variables to overcome the problem of C¹ continuity associate...
Main Authors: | S. K. Singh, A. Chakrabarti |
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Format: | Article |
Language: | English |
Published: |
Marcílio Alves
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Series: | Latin American Journal of Solids and Structures |
Subjects: | |
Online Access: | http://www.scielo.br/scielo.php?script=sci_arttext&pid=S1679-78252012000300003&lng=en&tlng=en |
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