A crashworthiness optimisation procedure for the design of full-composite fuselage section

Crashworthiness of composites is a key-point in the design of new aeronautical structures. Special attention has been addressed in the last years to the energy absorption mechanisms of dedicated components in order to limit the structural damages and to preserve the occupants’ safety. Remarkable pro...

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Veröffentlicht in:	IOP conference series. Materials Science and Engineering 2021-02, Vol.1038 (1), p.12058
Hauptverfasser:	Manzo, M, Perfetto, D, Caputo, F, Di Palma, L, Chiariello, A, Waimer, M
Format:	Artikel
Sprache:	eng
Schlagworte:	Airframes Composite structures Crashworthiness Design improvements Design modifications Design of experiments Design optimization Energy absorption Finite element method Fuselages Impact strength Impact tests Mathematical models Model testing Sensitivity analysis Structural damage
Online-Zugang:	Volltext
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