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Title
The influence of laminate stacking sequence on layered composites edge effectsAuthors
Yu.I. Dudarkov, E.A. Levchenko, M.V. LimoninOrganization
Central Aerohydrodynamic Institute named after professor N. E. ZhukovskyZhukovsky, Moscow region, Russia
Abstract
The numerical-experimental results of the investigation of influence of laminate stacking sequence on edge effects that occurs on structure free edges are presented. Three-dimensional models of composites have been used for calculations. It was shown and experimentally confirmed that laminate stacking sequence significantly effects on normal stress rate and distribution on laminate free edges.Keywords
edge effect, finite element method, layered composites, delamination stressesFor citing this article
Dudarkov Yu.I., Levchenko E.A., Limonin M.V. The influence of laminate stacking sequence on layered composites edge effects // The Research of the Science City, 2014, no. 3, pp. 25-30.
This Article is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License (CC BY-NC 4.0).