In this paper, we perform the behavior of aeronautics composite material subjected to a low energy impact. The proposed study considers the dynamic impact between a small piece of granular material and a large body of composite material. The principal aim is to simulate the impact of runway debris thrown up by the landing gear against an airplane structure. In the simulation, a CFRP composite panel impacted by granular particles at low speed is considered. The finite element analysis, initially on the macroscale and subsequently on the micro-scale, shows the delamination inside the composite according to the experimental results.
RUNWAY DEBRIS IMPACT ON AIRCRAFT COMPOSITE PARTS / Buonsanti, Michele; Leonardi, Giovanni; Ceravolo, F. - 754:(2017), pp. 283-286. (Intervento presentato al convegno FDM 2017 FRACTURE DAMAGE MECHANICS nel GIUGNO 2017) [10.4028/www.scientific.net/KEM.754.283].
RUNWAY DEBRIS IMPACT ON AIRCRAFT COMPOSITE PARTS
BUONSANTI, Michele;LEONARDI, Giovanni
;CERAVOLO F
2017-01-01
Abstract
In this paper, we perform the behavior of aeronautics composite material subjected to a low energy impact. The proposed study considers the dynamic impact between a small piece of granular material and a large body of composite material. The principal aim is to simulate the impact of runway debris thrown up by the landing gear against an airplane structure. In the simulation, a CFRP composite panel impacted by granular particles at low speed is considered. The finite element analysis, initially on the macroscale and subsequently on the micro-scale, shows the delamination inside the composite according to the experimental results.I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.