Computational Analysis of 3D Lattice Structures for Skin in Real-Scale Camber Morphing Aircraft
Conventional or fixed wings require a certain thickness of skin material selection that guarantees structurally reliable strength under expected aerodynamic loadings. However, skin structures of morphing wings need to be flexible as well as stiff enough to deal with multi-axial structural stresses f...
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| Principais autores: | , , |
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| 格式: | Artigo |
| 語言: | Inglês |
| 出版: |
MDPI AG
2019-07-01
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| 叢編: | Aerospace |
| 主題: | |
| 在線閱讀: | https://www.mdpi.com/2226-4310/6/7/79 |
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