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).File in questo prodotto:
Non ci sono file associati a questo prodotto.
I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.


