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Critical load of an axially compressed sandwich cylindrical panel
Authors:Zbigniew Laszczyk  Waclaw Szyc
Affiliation:Institute of Applied Mechanics, Poznan University of Technology, Poland
Abstract:The problem of critical load of an axially compressed open sandwich cylindrical shell with two straightlinear edges free is presented. Large angle of the shell sector, geometrical and physical symmetry of the facings are assumed. The simply formula for calculation critical stress in the shell is presented. (© 2006 WILEY-VCH Verlag GmbH & Co. KGaA, Weinheim)
Keywords:
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