Damage tolerance related to the damage area of impacted carbon/epoxy composite laminates

This study aimed to analyze the damage tolerance of a carbon/epoxy composite laminate (AS4/8552) impacted at low velocity, relating residual strength values with the impact energy and delaminated area. AS4/8552 laminated plates [0°3/90°/±45°]S were submitted to low-velocity impact tests with three e...

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Published in:Journal of composite materials 2023-08, Vol.57 (19), p.2985-2993
Main Authors: Targino, Talita Galvão, Dantas da Cunha, Rayane, Ribeiro, Gleicy de Lima Xavier, Paiva da Costa Ferreira, Evans, Freire Júnior, Raimundo Carlos Silverio, Daniel Diniz Melo, José
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container_end_page 2993
container_issue 19
container_start_page 2985
container_title Journal of composite materials
container_volume 57
creator Targino, Talita Galvão
Dantas da Cunha, Rayane
Ribeiro, Gleicy de Lima Xavier
Paiva da Costa Ferreira, Evans
Freire Júnior, Raimundo Carlos Silverio
Daniel Diniz Melo, José
description This study aimed to analyze the damage tolerance of a carbon/epoxy composite laminate (AS4/8552) impacted at low velocity, relating residual strength values with the impact energy and delaminated area. AS4/8552 laminated plates [0°3/90°/±45°]S were submitted to low-velocity impact tests with three energy levels: 30 J, 45 J and 74 J. Next, the test specimens were analyzed by X-ray computed tomography to check for cracks and delaminations, and compression after impact (CAI) tests conducted to assess their residual strength. The results indicate that above the minimum energy level of low-velocity impact to cause damage, the residual strength of the laminate may be related to the delaminated area.
doi_str_mv 10.1177/00219983231181942
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title Damage tolerance related to the damage area of impacted carbon/epoxy composite laminates
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