| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 10283727 | Composite Structures | 2012 | 9 Pages |
Abstract
Based on the classical shell theory with the geometrical nonlinearity in von Karman-Donnell sense and the smeared stiffeners technique, the governing equations of motion of eccentrically stiffened functionally graded cylindrical panels with geometrically imperfections are derived in this paper. The characteristics of free vibration and nonlinear responses are investigated. The nonlinear dynamic buckling of cylindrical panel acted on by axial loading is considered. The nonlinear dynamic critical buckling loads are found according to the criterion suggested by Budiansky-Roth. Some numerical results are given and compared with the ones of other authors.
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Authors
Dao Huy Bich, Dao Van Dung, Vu Hoai Nam,