Research Article
Jun 1975
Nonlinear Analysis of Unsymmetrically Laminated Plates
Publication: Journal of the Engineering Mechanics Division
Volume 101, Issue 3
Abstract
The nonlinear behavior of unsymmetric filamentary composite laminated plates is investigated. The simplifying reduced stiffness model is used to demonstrate its adequacy in predicting the nonlinear deflection and stress characteristics of the laminates. The effect of coupling that exists in such laminates as well as the effect of large lateral loads producing excessive deflections are studied. Experimental results obtained from tests on various laminated plates with different boundary conditions are compared with the predicted theoretical values. The governing equations are solved by means of a finite difference scheme and an iterative process.
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Published In
Journal of the Engineering Mechanics Division
Volume 101 • Issue 3 • June 1975
Pages: 169 - 186
Copyright
© 1975 American Society of Civil Engineers.
History
Published in print: Jun 1975
Published online: Feb 3, 2021
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Authors
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Samir A. Zaghloul
Design Engr., Induecon Consultants of Canada Ltd., Ontario, Canada; formerly, Research Asst., Dept. of Civ. Engrg., Univ. of Windsor, Windsor, Canada
John B. Kennedy, M.ASCE
Prof. and Head; Dept. of Civ. Engrg., Univ. of Windsor, Windsor, Canada
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Terms of Use: ASCE Library Cards are for individual, personal use only. Reselling, republishing, or forwarding the materials to libraries or reading rooms is prohibited.
Terms of Use: ASCE Library Cards are for individual, personal use only. Reselling, republishing, or forwarding the materials to libraries or reading rooms is prohibited.