Published June 22, 2020 | Version v1
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Effects of hot-wet storage aging, CNT-integration and damping layer interposition on static and fatigue interlaminar shear response of a UD Graphite/Epoxy material system

  • 1. Hellenic Aerospace Industry
  • 2. Element Materials Technology Seville

Description

The present work aims at experimental quantification of the effect of hot-wet storage aging on the static and
fatigue interlaminar shear response of three UD Graphite-Epoxy based material systems: a control laminate, a
CNT-treated laminate and a lamination including an embedded damping veil. In this context, specimens have
been fabricated and tested for determination of the interlaminar shear strength (ILSS) according to the relevant
ASTM standard, and the effects of the above mentioned constituents on the response of non-aged (RT) and aged
(HW) specimens have been investigated. The experimental data, presented in batch mode, indicated that aging
leads to severe degradation of the interlaminar shear strength and relevant fatigue endurance of all material
systems, whereas the CNT-treated laminate appeared to be the most sensitive configuration. In the case of nonaged specimens, CNT-treatment led to larger failure strains and a clear bilinear response, while all three material
systems exhibited similar values of interlaminar shear strength.

Notes

The current work has received funding from EU Horizon 2020 Clean Sky II project SHERLOC (Structural Health Monitoring, Manufacturing and Repair Technologies for Life Management of Composite Fuselage) under Grant Agreement No CS2-AIR-GAM-2014-2015-01.

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