A crashworthiness optimisation procedure for the design of full-composite fuselage section
Abstract 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. Remar...
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Published in | IOP conference series. Materials Science and Engineering Vol. 1038; no. 1; p. 12058 |
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Main Authors | , , , , , |
Format | Journal Article |
Language | English |
Published |
Bristol
IOP Publishing
01.02.2021
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Subjects | |
Online Access | Get full text |
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