Advanced Search

Journal Navigation

Journal Home

Subscriptions

Archive

Contact Us

Table of Contents

SAGETRACK

Sign In to gain access to subscriptions and/or personal tools.
Journal of Reinforced Plastics and Composites
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
Right arrow Citation Map
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
Right arrow Citing Articles via Scopus
Google Scholar
Right arrow Articles by Arlsan, N.
Right arrow Articles by Gur, M.
Right arrow Search for Related Content
Social Bookmarking
Add to CiteULike   Add to Complore   Add to Connotea   Add to Del.icio.us   Add to Digg   Add to Reddit   Add to Technorati   Add to Twitter  
What's this?

Elasto-Plastic Stress Analysis of Thermoplastic Matrix Composite Laminated and Perforated Plates under In-Plane Loading

N. Arlsan

Department of Mechanical Engineering, Firat University, Elazig, Turkey, narslan{at}firat.edu.tr

H. Pihtili

Department of Mechanical Engineering, Firat University, Elazig, Turkey

M. Gur

Department of Mechanical Engineering, Firat University, Elazig, Turkey

The study presents an elasto-plastic stress analysis in symmetric and antisymmetric cross-ply reinforced thermoplastic matrix composite laminated plates. The thermoplastic matrix composite layer reinforced by long stainless steel fiber is manufactured by using moulds under the action of 2 MPa pressure and heating up to 200°C. A laminated and perforated plate consists of four thermoplastic matrix layers is reinforced cross-ply and bonded symmetrically or antisymmetrically. The first-order shear deformation theory and nine node Lagrangian finite element are used. The residual stresses and the expansions of plastic regions are illustrated for various cases. The in-plane load and the layer orientation angle are increased gradually.

Journal of Reinforced Plastics and Composites, Vol. 20, No. 14-15, 1222-1252 (2001)
DOI: 10.1106/JFP5-0YME-8FD8-NM1L
Add to CiteULike CiteULike   Add to Complore Complore   Add to Connotea Connotea   Add to Del.icio.us Del.icio.us   Add to Digg Digg   Add to Reddit Reddit   Add to Technorati Technorati   Add to Twitter Twitter    What's this?


This article has been cited by other articles:


Home page
 Journal of Reinforced Plastics and CompositesHome page
M. Kucuk
Elastoplastic Stress Analysis and Residual Stresses in Metal-matrix-laminated Plates under In-plane and Transverse Loading
Journal of Reinforced Plastics and Composites, January 1, 2006; 25(2): 161 - 173.
[Abstract] [PDF]

Home page
 Journal of Reinforced Plastics and CompositesHome page
M. Ozbay and D. Ozer
The Analysis of Elasto-plastic Stresses in the Composite Laminate with a Circular Hole Subjected to In-plane Loads by Means of Finite Element Method
Journal of Reinforced Plastics and Composites, April 1, 2005; 24(6): 621 - 631.
[Abstract] [PDF]