Optimization of composite wing structure with static, buckling, and flutter constraints using the finite element method / Muhammad Kusni ... [et al.]

In airplane structural design, creating a strong yet lightweight structure is crucial. During the preliminary design phase, structural sizing optimization is necessary to achieve an efficient and lightweight structure that meets safety standards. Composite materials offer a high strength-to-weight r...

Full description

Bibliographic Details

Main Authors:	Kusni, Muhammad, Syamsudin, H., Gunawan, L., Hadi, Bambang Kismono, Darmanto, Seno, Muflikhun, M. Akhsin, Widiramdhani, Martina
Format:	Article
Language:	en
Published:	UiTM Press 2024
Subjects:	Engineering mathematics. Engineering analysis
Online Access:	https://ir.uitm.edu.my/id/eprint/101340/1/101340.pdf https://ir.uitm.edu.my/id/eprint/101340/
Tags:	Add Tag No Tags, Be the first to tag this record!