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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Bibliographic Details

Published in:	Curved and Layered Structures
Main Authors:	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
Format:	Article
Language:	English
Published:	De Gruyter 2023-04-01
Subjects:	topology optimization fuselage structure male uav finite element method
Online Access:	https://doi.org/10.1515/cls-2022-0191