Deformations of Laminated Cylindrical Panels with Circular Holes

M. WYGODA, A. MUC, M. BARSKI, P.D. PASTUSZAK

Abstract


The present work is devoted mainly to investigation of the buckling and post-buckling behavior of the composite cylindrical panels under axial load. The influence of the diameter of the hole on the buckling strength is studied with the use of finite element method.

Keywords


Composite, Cylindrical, Panels, Analyses, Hole, Buckling.


DOI
10.12783/dtmse/amst2016/11331

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