Article ID Journal Published Year Pages File Type
6702528 Composite Structures 2018 13 Pages PDF
Abstract
The subject of the paper is a cylindrical panel with symmetrically varying mechanical properties in the thickness direction. The nonlinear hypothesis of deformation of the straight line normal to the panel neutral surface is assumed. Based on the principle of stationary potential energy differential equations of equilibrium are obtained. The system of the equations is analytically solved and the critical loads of cylindrical panel are derived. Moreover, a simplified model of the cylindrical panel without shear effect is formulated. The results of critical loads for example structures are calculated and presented in Tables.
Related Topics
Physical Sciences and Engineering Engineering Civil and Structural Engineering
Authors
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