Mathematics and Mechanics of Solids

 

Advanced Search

Journal Navigation

Journal Home

Subscriptions

Archive

Contact Us

Table of Contents

Register here to gain access to SAGE's 500+ Journals Online

Click here to sign up for SAGE Journal Email Alerts today!

Sign In to gain access to subscriptions and/or personal tools.
This Article
Right arrow Full Text (PDF)
Right arrow References
Right arrow Alert me when this article is cited
Right arrow Alert me if a correction is posted
Services
Right arrow Email this article to a friend
Right arrow Similar articles in this journal
Right arrow Alert me to new issues of the journal
Right arrow Add to Saved Citations
Right arrow Download to citation manager
Right arrowRequest Permissions
Right arrow Request Reprints
Right arrow Add to My Marked Citations
Citing Articles
Right arrow Citing Articles via HighWire
Right arrow Citing Articles via Google Scholar
Google Scholar
Right arrow Articles by Soldatos, K. P.
Right arrow Articles by Watson, P.
Right arrow Search for Related Content
Social Bookmarking
 Add to CiteULike   Add to Connotea   Add to Del.icio.us   Add to Digg   Add to Reddit   Add to Technorati  
What's this?
Mathematics and Mechanics of Solids, Vol. 2, No. 4, 459-489 (1997)
DOI: 10.1177/108128659700200405

Accurate Stress Analysis of Laminated Plates Combining a Two-Dimensional Theory with the Exact Three-Dimensional Solution for Simply Supported Edges

Kostas P. Soldatos

Philip Watson

Department of Theoretical Mechanics, University of Nottingham, Nottingham NG7 2RD, United Kingdom

This paper proposes a method for improving the performance of two-dimensional, higher order theories of homogeneous and laminated composite plates. The method is based on the appropriate specification of through-thickness shape functions which are suitable for the accurate stress analysis of plates, on the basis of a general six-degrees-of-freedom plate theory (G6DOFPT). G6DOFPT takes both transverse shear and transverse normal deformation effects into consideration using three shape functions, each of which is associated with one of the three unknown displacement components. Specification of these three shape functions is achieved by solving the corresponding equations of three-dimensional elasticity for a simply supported plate. Thus, the shape functions correspond to the exact elasticity solution presented in previous work. Hence, no results are shown for simply supported plates because, in that case, the present method will yield the results of the exact elasticity analysis. Instead, new results are presented and discussed. These deal with the cylindrical bending of homogeneous orthotropic and two-layered laminates which have both edges rigidly clamped. The new method is considered as the appropriate match of the new shape functions with the equations of G6DOFPT. This is a very promising combination because it employs through-thickness displacement and stress distributions having an "exact" shape away from the edge boundaries. In addition, it takes advantage of the relative ease with which solutions are obtained from the governing equations of a two-dimensional theory, especially in cases which involve complicated edge boundary conditions.


Add to CiteULike CiteULike   Add to Connotea Connotea   Add to Del.icio.us Del.icio.us   Add to Digg Digg   Add to Reddit Reddit   Add to Technorati Technorati    What's this?


This article has been cited by other articles:


Home page
Mathematics and Mechanics of SolidsHome page
K. P. Soldatos
General Solutions for the Statics of Anisotropic, Transversely Inhomogeneous Elastic Plates in Terms of Complex Functions
Mathematics and Mechanics of Solids, December 1, 2006; 11(6): 596 - 628.
[Abstract] [PDF]