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...
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| Main Authors: | , , , , , , |
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| Format: | Article |
| Language: | English |
| Published: |
UiTM Press
2024
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| Subjects: | |
| Online Access: | https://ir.uitm.edu.my/id/eprint/101340/1/101340.pdf https://ir.uitm.edu.my/id/eprint/101340/ |
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