Composite laminate under influence of temperature and moisture

The static response of simply supported carbon/epoxy composite plates in a hygrothermal environment is carried out using the general purpose finite element program COSMOS. The static load model and the hygrothermal incorporation are solved separately. The hygrothermal effect is introduced by using e...

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Main Authors: Kormaníková Eva, Kotrasová Kamila
Format: Article
Language:English
Published: EDP Sciences 2016-01-01
Series:MATEC Web of Conferences
Online Access:http://dx.doi.org/10.1051/matecconf/20167604002
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author Kormaníková Eva
Kotrasová Kamila
author_facet Kormaníková Eva
Kotrasová Kamila
author_sort Kormaníková Eva
collection DOAJ
description The static response of simply supported carbon/epoxy composite plates in a hygrothermal environment is carried out using the general purpose finite element program COSMOS. The static load model and the hygrothermal incorporation are solved separately. The hygrothermal effect is introduced by using empirical relations for degrading the material stiffness properties of the matrix. The corresponding ply properties are calculated using Mori-Tanaka method. A parametric study is conducted by varying the fiber volume fraction and the fiber orientation of the angle plies in the laminate.
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spelling doaj.art-f15369adc1aa41848b98d1134452df3f2022-12-21T22:24:16ZengEDP SciencesMATEC Web of Conferences2261-236X2016-01-01760400210.1051/matecconf/20167604002matecconf_cscc2016_04002Composite laminate under influence of temperature and moistureKormaníková Eva0Kotrasová Kamila1TUKE, Faculty of Civil Engineering, Department of Structural MechanicsTUKE, Faculty of Civil Engineering, Department of Structural MechanicsThe static response of simply supported carbon/epoxy composite plates in a hygrothermal environment is carried out using the general purpose finite element program COSMOS. The static load model and the hygrothermal incorporation are solved separately. The hygrothermal effect is introduced by using empirical relations for degrading the material stiffness properties of the matrix. The corresponding ply properties are calculated using Mori-Tanaka method. A parametric study is conducted by varying the fiber volume fraction and the fiber orientation of the angle plies in the laminate.http://dx.doi.org/10.1051/matecconf/20167604002
spellingShingle Kormaníková Eva
Kotrasová Kamila
Composite laminate under influence of temperature and moisture
MATEC Web of Conferences
title Composite laminate under influence of temperature and moisture
title_full Composite laminate under influence of temperature and moisture
title_fullStr Composite laminate under influence of temperature and moisture
title_full_unstemmed Composite laminate under influence of temperature and moisture
title_short Composite laminate under influence of temperature and moisture
title_sort composite laminate under influence of temperature and moisture
url http://dx.doi.org/10.1051/matecconf/20167604002
work_keys_str_mv AT kormanikovaeva compositelaminateunderinfluenceoftemperatureandmoisture
AT kotrasovakamila compositelaminateunderinfluenceoftemperatureandmoisture