In this work, the damage identification for a composite landing gear component has been performed by the study of its dynamic behaviour. Fiber optic sensors were used for acquire the vibration signature of the system in its undamaged condition and during a high energy impact. The vibration test on the damaged component underlined a modification on the system response which should be considered for the health status assessment.
Damage detection in composite landing gear component using frequency response method / Breglio, G.; Fienga, F.; Irace, A.; Mennella, F.; Petrazzuoli, L.; Laudati, A.; Giordano, M.; Martone, A.. - 3:(2016), pp. 1972-1978. (Intervento presentato al convegno 8th European Workshop on Structural Health Monitoring, EWSHM 2016 tenutosi a esp nel 2016).
Damage detection in composite landing gear component using frequency response method
Breglio G.;Fienga F.;Irace A.;
2016
Abstract
In this work, the damage identification for a composite landing gear component has been performed by the study of its dynamic behaviour. Fiber optic sensors were used for acquire the vibration signature of the system in its undamaged condition and during a high energy impact. The vibration test on the damaged component underlined a modification on the system response which should be considered for the health status assessment.I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.
