Assessment of linearized buckling and nonlinear behavior of composite panels
A conventional approach to the computation of critical loads of structures is to linearize the prebuckling state and to solve the resulting eigenproblem in order to obtain buckling loads as well as buckling modes. However, this approach is flawed, or extremely misleading, if in reality the prebuckli...
Main Author: | Luciano Alves Martins |
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Other Authors: | Alfredo Rocha de Faria |
Format: | Others |
Language: | English |
Published: |
Instituto Tecnológico de Aeronáutica
2009
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Subjects: | |
Online Access: | http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=1289 |
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