Redesigning of a Canard Control Surface of an Advanced Fighter Aircraft: Effect on Buckling and Aerodynamic Behavior
A redesign of canard control-surface of an advanced all-metallic fighter aircraft was carried out by using carbon fibre composite (CFC) for ribs and panels. In this study ply-orientations of CFC structure are optimized using a Genetic-Algorithm (GA) with an objective function to have minimum failure...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
De Gruyter
2015-01-01
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| Series: | Curved and Layered Structures |
| Subjects: | |
| Online Access: | http://www.degruyter.com/view/j/cls.2015.2.issue-1/cls-2015-0010/cls-2015-0010.xml?format=INT |