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Paper VI.1

Buckling and Dynamic Behaviour of Laminate Composite Plates using a Discrete Higher-Order Displacement Model

J. Simoes Moita*

C.M. Mota Soares#, C.A. Mota Soares#
*University of Algarve, Faro, Portugal
#Institute of Mechanical Engineering, I.S.T., Lisbon, Portugal

doi:10.4203/ccp.41.6.1

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J. Simoes Moita, "Buckling and Dynamic Behaviour of Laminate Composite Plates using a Discrete Higher-Order Displacement Model", in B.H.V. Topping, (Editor), "Advances in the Analysis and Design of Composites", Civil-Comp Press, Edinburgh, UK, pp 113-127, 1996. doi:10.4203/ccp.41.6.1

Abstract

This paper deals with buckling and free vibrations of multilaminated structures of arbitrary geometry and lay-up using a single layer higher order shear deformation theory discrete model. This model is based on a eight node C⁰ serendipity finite element with ten degrees of freedom per node to contemplate general applications. The present model is tested on the evaluation of buckling loads and free vibrations of multilaminated plates and shells. The effects of different number of layers, lamination angles, material anisotropy, and length or radius to thickness ratios are studied.

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Front Page Browse CCP CSETS CTR IJRT Other Authors Search Purchase Guide FAQ Contact us	Civil-Comp Proceedings ISSN 1759-3433 CCP: 41 ADVANCES IN THE ANALYSIS AND DESIGN OF COMPOSITES Edited by: B.H.V. Topping Paper VI.1 Buckling and Dynamic Behaviour of Laminate Composite Plates using a Discrete Higher-Order Displacement Model J. Simoes Moita* C.M. Mota Soares#, C.A. Mota Soares# *University of Algarve, Faro, Portugal #Institute of Mechanical Engineering, I.S.T., Lisbon, Portugal doi:10.4203/ccp.41.6.1 purchase the full-text of this paper Full Bibliographic Reference for this paper J. Simoes Moita, "Buckling and Dynamic Behaviour of Laminate Composite Plates using a Discrete Higher-Order Displacement Model", in B.H.V. Topping, (Editor), "Advances in the Analysis and Design of Composites", Civil-Comp Press, Edinburgh, UK, pp 113-127, 1996. doi:10.4203/ccp.41.6.1 Abstract This paper deals with buckling and free vibrations of multilaminated structures of arbitrary geometry and lay-up using a single layer higher order shear deformation theory discrete model. This model is based on a eight node C⁰ serendipity finite element with ten degrees of freedom per node to contemplate general applications. The present model is tested on the evaluation of buckling loads and free vibrations of multilaminated plates and shells. The effects of different number of layers, lamination angles, material anisotropy, and length or radius to thickness ratios are studied. purchase the full-text of this paper (price £20) go to the previous paper go to the next paper return to the table of contents return to the book description purchase this book (price £58 +P&P)
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