Crash simulation and drop test of civil airplane fuselage section

Abstract

To study the crashworthiness of a civil airplane fuselage section under vertical crash condition, a finite element model of this fuselage section was developed, and numerical simulations of the fuselage section under 7 m/s vertical impact condition is performed using LS-DYNA explicit finite element code. Then a drop test of the structure is conducted, the… (More)

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