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Hygrothermal effects on the translaminar fracture toughness of a highly toughened aerospace CFRP: Experimental characterisation and model prediction

Sengodan, Ganapathi A; Li, Shangkai; Allegri, Giuliano; Hallett, Stephen R

Authors

Ganapathi A Sengodan

Shangkai Li

Giuliano Allegri

Stephen R Hallett



Abstract

The translaminar fracture toughness of wet (fully saturated) and dry (as manufactured) IM7/8552 laminates was measured using compact tension tests. Cross-ply ([90/0]8S) and quasi-isotropic ([90/45/0/-45]4S) laminates were tested at three different temperatures, namely 23 °C, 40 °C and 90 °C. The translaminar fracture toughness decreases non-linearly with the temperature for the dry laminates. However, for the wet laminates, the translaminar fracture toughness increases. The room-temperature tested wet cross-ply laminates exhibited a lower fracture toughness than the dry laminates. However, the initiation fracture toughness of the wet quasi-isotropic laminates is higher than for the dry laminates at all the test temperatures. The fractographic analysis of the failed specimens revealed that the hot-wet conditions promote additional fibre pull-out, which increases the fracture energy. The degradation of the epoxy matrix in the wet multi-directional laminates affected the progressive failure mechanism, and either increased or decreased the overall fracture energy depending on the lay-up sequence. For example, the initiation fracture toughness of the elevated temperature (90 °C) in wet quasi-isotropic specimens is ~17% higher than the room temperature (23 °C) dry laminates.

Presentation Conference Type Conference Paper (published)
Acceptance Date Jul 26, 2021
Online Publication Date Aug 3, 2021
Publication Date Aug 18, 2021
Deposit Date Sep 8, 2023
Print ISSN 1359-835X
Publisher Elsevier
Volume 150
DOI https://doi.org/10.5075/978-X-XXX-XXXXX-X
Keywords Translaminar; composites; fracture toughness; hygro-thermal; fibre pull-out


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