Title of article
Buckling of the composite orthotropic clamped–clamped cylindrical shell loaded by transverse inertia forces
Author/Authors
A.V. Lopatin، نويسنده , , E.V. Morozov، نويسنده ,
Issue Information
روزنامه با شماره پیاپی سال 2013
Pages
8
From page
471
To page
478
Abstract
The paper is concerned with the buckling analysis of the composite orthotropic cylindrical shell with clamped edges subjected to inertia loading. The problem is characterised by a non-uniform pre-buckling stress state. To address this, the relevant governing system of differential equations with variable coefficients has been derived and solved using Galerkin method. As a result, the problem of determining the critical acceleration causing the buckling of shell is reduced to the solution of the corresponding generalised eigenvalue problem. Using the proposed approach, the critical accelerations are calculated for the glass-fibre reinforced shells with various dimensional and stiffness parameters. Results of calculations are compared with those based on finite-element modelling and analysis.
Keywords
Galerkin method , Critical acceleration , Composite cylindrical shells , Transverse inertia loading , Buckling
Journal title
COMPOSITE STRUCTURES
Serial Year
2013
Journal title
COMPOSITE STRUCTURES
Record number
1344969
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