contributor author | N. Kumar | |
contributor author | T. R. Tauchert | |
date accessioned | 2017-05-08T23:35:22Z | |
date available | 2017-05-08T23:35:22Z | |
date copyright | September, 1991 | |
date issued | 1991 | |
identifier issn | 0195-0738 | |
identifier other | JERTD2-26439#204_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/108452 | |
description abstract | Response of a cylindrical panel made of layers of composite material and subjected to in-plane loads is investigated. Prebuckling deformations are determined for antisymmetric angle-ply and cross-ply panels having simply supported boundary conditions. Buckling solutions are obtained via the Rayleigh-Ritz method. Nonlinear programming is used to optimize the designs. Design variables are taken as fiber orientations and/or thicknesses of different layers. Numerical results are presented for different materials and different geometrical parameters, including aspect ratio and curvature-to-length ratio. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Design of Composite Cylindrical Panels for Maximum Axial and Shear Buckling Capacity | |
type | Journal Paper | |
journal volume | 113 | |
journal issue | 3 | |
journal title | Journal of Energy Resources Technology | |
identifier doi | 10.1115/1.2905806 | |
journal fristpage | 204 | |
journal lastpage | 209 | |
identifier eissn | 1528-8994 | |
keywords | Composite materials | |
keywords | Shear (Mechanics) | |
keywords | Design | |
keywords | Buckling | |
keywords | Nonlinear programming | |
keywords | Rayleigh-Ritz methods | |
keywords | Deformation | |
keywords | Boundary-value problems | |
keywords | Fibers AND Stress | |
tree | Journal of Energy Resources Technology:;1991:;volume( 113 ):;issue: 003 | |
contenttype | Fulltext | |