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Ribeiro, M. L.; Martins, T.; Angélico, R. A.; Vandepitte, D.; Tita, V.;

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Composite material is very attractive for structural applications due to its inherent mechanical properties and low weight. The improvement in manufacture process allow composite materials be used even as primary structures in modern aircraft design such as Boeing 787 without loss of airworthiness. During service life composite structures can be damaged by collisions, dropping tools during assembly or maintenance, etc. Several impact studies were conducted for plates, but few regards curved geometries or cylinders. This study presents a progressive damage analysis of low energy impact on carbon fiber filament winding cylinders. Three different layups were used for experimental tests. A new material model based in continuum damage mechanics were implemented as a FORTRAN subroutine linked to finite element software ABAQUS for explicit dynamic analysis (VUMAT). Good correlations for force vs. time and displacement vs. time between the numerical model experimental test results were obtained.

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Palavras-chave: Impact, filament winding, composite structures, damage, progressive failure analysis,


DOI: 10.5151/meceng-wccm2012-18076

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Como citar:

Ribeiro, M. L.; Martins, T.; Angélico, R. A.; Vandepitte, D.; Tita, V.; "PROGRESSIVE FAILURE ANALYSIS OF LOW ENERGY IMPACT IN CARBON FIBER FILAMENT WINDING CYLINDERS", p. 682-701 . In: In Proceedings of the 10th World Congress on Computational Mechanics [= Blucher Mechanical Engineering Proceedings, v. 1, n. 1]. São Paulo: Blucher, 2014.
ISSN 2358-0828, DOI 10.5151/meceng-wccm2012-18076

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