Abstract
The paper deals with a dynamic response of thin rectangular plate subjected to in-plane pulse loading of different triangular and rectangular shape. The investigated plates are made of unidirectional fibre composites, which are modelled as orthotropic material with principal directions of orthotropy parallel to the plate edges. The structures are assumed to be simply supported at the loaded ends and five different boundary conditions at non-loaded edges. Dynamic response of thin plates are calculated using analytical-numerical method and finite element method for comparison.
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Kubiak, T. (2006). COMPOSITE PLATES DYNAMIC BUCKLING OF THIN -WALLED. In: Sadowski, T. (eds) IUTAM Symposium on Multiscale Modelling of Damage and Fracture Processes in Composite Materials. SOLID MECHANICS AND ITS APPLICATIONS, vol 135. Springer, Dordrecht. https://doi.org/10.1007/1-4020-4566-2_14
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DOI: https://doi.org/10.1007/1-4020-4566-2_14
Publisher Name: Springer, Dordrecht
Print ISBN: 978-1-4020-4565-3
Online ISBN: 978-1-4020-4566-0
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