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

• Main Authors: Kusni, Muhammad, Syamsudin, H., Gunawan, L., Hadi, Bambang Kismono, Darmanto, Seno, Muflikhun, M. Akhsin, Widiramdhani, Martina
• Format: Article
• Language: English
• 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/
• Institution: Universiti Teknologi Mara

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...