This paper presents the results of tests conducted on a curved stiffened panel to evaluate its damage tolerance capabilities. The panel was made from dry carbon preforms using Liquid Resin Infusion (LRI) followed by an Out-of-Autoclave curing. Non-linear Finite Element analysis results are also presented and compared to the measurements. The research was funded by Clean Sky 2 JU, under EU H2020 RIP, GA No 807089 (Work Area Leader: Leonardo Aircraft).

DAMAGE TOLERANCE OF A CURVED COMPOSITE STIFFENED PANEL FABRICATED BY AN OUT OF AUTOCLAVE – LIQUID RESIN INFUSION PROCESS

Fanteria D.
Membro del Collaboration Group
;
Boni L.
Membro del Collaboration Group
;
2024-01-01

Abstract

This paper presents the results of tests conducted on a curved stiffened panel to evaluate its damage tolerance capabilities. The panel was made from dry carbon preforms using Liquid Resin Infusion (LRI) followed by an Out-of-Autoclave curing. Non-linear Finite Element analysis results are also presented and compared to the measurements. The research was funded by Clean Sky 2 JU, under EU H2020 RIP, GA No 807089 (Work Area Leader: Leonardo Aircraft).
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11568/1340311
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