Finite element method on topology optimization applied to laminate composite of fuselage structure

This research applies a numerical study of topology optimization of laminate composite structures by using a finite element method (FEM). In this methodology, the plies orientation is excluded from the optimization. The geometry-based optimization from frames of a MALE UAV fuselage structure is pres...

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Detalhes bibliográficos

Principais autores:	Aribowo Agus, Adhynugraha Muhammad Ilham, Megawanto Fadli Cahya, Hidayat Arif, Muttaqie Teguh, Wandono Fajar Ari, Nurrohmad Abian, Chairunnisa, Saraswati Sherly Octavia, Wiranto Ilham Bagus, Al Fikri Iqbal Reza, Saputra Muhammad Dito
Formato:	Artigo
Idioma:	Inglês
Publicado em:	De Gruyter 2023-04-01
coleção:	Curved and Layered Structures
Assuntos:	topology optimization fuselage structure male uav finite element method
Acesso em linha:	https://doi.org/10.1515/cls-2022-0191
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