ePrints@IIScePrints@IISc Home | About | Browse | Latest Additions | Advanced Search | Contact | Help

On Uniform Approximate Solutions in Bending of Symmetric Laminated Plates

Vijayakumar, K (2013) On Uniform Approximate Solutions in Bending of Symmetric Laminated Plates. In: CMC-COMPUTERS MATERIALS & CONTINUA, 34 (1). pp. 1-25.

Full text not available from this repository.
Official URL: http://dx.doi.org/10.3970/cmc.2013.034.001


A layer-wise theory with the analysis of face ply independent of lamination is used in the bending of symmetric laminates with anisotropic plies. More realistic and practical edge conditions as in Kirchhoff's theory are considered. An iterative procedure based on point-wise equilibrium equations is adapted. The necessity of a solution of an auxiliary problem in the interior plies is explained and used in the generation of proper sequence of two dimensional problems. Displacements are expanded in terms of polynomials in thickness coordinate such that continuity of transverse stresses across interfaces is assured. Solution of a fourth order system of a supplementary problem in the face ply is necessary to ensure the continuity of in-plane displacements across interfaces and to rectify inadequacies of these polynomial expansions in the interior distribution of approximate solutions. Vertical deflection does not play any role in obtaining all six stress components and two in-plane displacements. In overcoming lacuna in Kirchhoff's theory, widely used first order shear deformation theory and other sixth and higher order theories based on energy principles at laminate level in smeared laminate theories and at ply level in layer-wise theories are not useful in the generation of a proper sequence of 2-D problems converging to 3-D problems. Relevance of present analysis is demonstrated through solutions in a simple text book problem of simply supported square plate under doubly sinusoidal load.

Item Type: Journal Article
Related URLs:
Additional Information: copyright for this article belongs to TECH SCIENCE PRESS
Keywords: Plates; bending; laminates; elasticity
Department/Centre: Division of Mechanical Sciences > Aerospace Engineering (Formerly, Aeronautical Engineering)
Date Deposited: 07 Nov 2013 06:00
Last Modified: 07 Nov 2013 06:05
URI: http://eprints.iisc.ernet.in/id/eprint/47695

Actions (login required)

View Item View Item