Effect of skin and spar laminate orientations on flutter of composite uav wing
This paper presents an analytical study on the optimisation of composite laminate orientation lay-up to achieve the maximum flutter with minimum weight penalty. The study is carried out by using UTM CAMAR UAV swept back wing as a case study where the wing consists of two spars located at 35% and 55%...
| Main Authors: | , , , , , , , , |
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| Format: | Article |
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The Aeronautical and Astronautical Society of the Republic of China
2019
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