Lightweight Design of Solar UAV Wing Structures Based on Sandwich Equivalent Theory
In this paper, an equivalent method based on sandwich plate is deduced, and the equivalent parameters of the honeycomb plate are obtained. With these equivalent parameters, the honeycomb plate equivalent FEM simulation model and actual model are established, and three-point bending simulations of th...
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| Автори: | , , , |
|---|---|
| Формат: | Artigo |
| Мова: | Inglês |
| Опубліковано: |
Wiley
2021-01-01
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| Серія: | International Journal of Aerospace Engineering |
| Онлайн доступ: | http://dx.doi.org/10.1155/2021/6752410 |
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