Nonlinear Analysis of Unsymmetrically Laminated Plates

by Samir A. Zaghloul, Design Engr.; Inducon Consultants of Canada Ltd., Ontario, Canada; formerly, Research Asst., Dept. of Civ. Engrg., Univ. of Windsor, Windsor, Ontario, Canada,
John B. Kennedy, (M.ASCE), Prof. and Head; Dept. of Civ. Engrg., Univ. of Windsor, Windsor, Ontario, Canada,

Serial Information: Journal of the Engineering Mechanics Division, 1975, Vol. 101, Issue 3, Pg. 169-186

Document Type: Journal Paper


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.

Subject Headings: Nonlinear analysis | Laminated materials | Plates | Displacement (mechanics) | Lateral loads | Nonlinear response | Stiffening | Coupling

Services: Buy this book/Buy this article


Return to search