Buckling analysis of a laminated cylindrical shell under torsion subjected to mixed boundary conditions
type: Item
instance of: scholarly article
title: Buckling analysis of a laminated cylindrical shell under torsion subjected to mixed boundary conditions
zbMATH Open document ID: 0937.74030
DOI: 10.1016/S0020-7683(98)00178-4
author: V. Pereyra
published in: International Journal of Solids and Structures
publication date: 2000-05-25T00:00:00Z
review text: First-order shear deformation theory and Donnell's shallow shell approximation form the basis for the study of linear bifurcation problem for cross-ply laminated cylindrical shells under torsion. Functional degrees of freedom are axial forces, in-plane shear forces, axial bending moments, torsional moments and transverse deflections. Truncated double Fourier series arise in a general linear matrix eigenvalue problem. Experience shows that six terms in axial direction and ten terms in circumferential direction are sufficient for an accuracy of four digits.
Mathematics Subject Classification ID: 74G60
Mathematics Subject Classification ID: 74K25
Mathematics Subject Classification ID: 74E30
zbMATH DE Number: 1341445
zbMATH Keywords: first-order shear deformation theory
zbMATH Keywords: Donnell's shallow shell approximation
zbMATH Keywords: linear bifurcation problem
zbMATH Keywords: mixed boundary conditions
zbMATH Keywords: cross-ply laminated cylindrical shell
zbMATH Keywords: torsion
zbMATH Keywords: truncated double Fourier series
zbMATH Keywords: general linear matrix eigenvalue problem
reviewed by: Klaus Rohwer
MaRDI profile type: Publication
description: scientific article; zbMATH DE number 1341445