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Consideration of Lamination Structural Analysis in a Multi-Layered Composite and Failure Analysis on Wing Design Application
A finite element (FE) model is developed to study the structural performance on a composite wing of a UAV with a tubercle design at the leading edge of the wing. The experimental study of the designation of the composite at the wing skin is carried out to prove the simulation validity through materi...
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| Опубликовано в: : | Materials (Basel) |
|---|---|
| Главные авторы: | , , , , |
| Формат: | Artigo |
| Язык: | Inglês |
| Опубликовано: |
MDPI
2021
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| Предметы: | |
| Online-ссылка: | https://ncbi.nlm.nih.gov/pmc/articles/PMC8269891/ https://ncbi.nlm.nih.gov/pubmed/34279278 https://ncbi.nlm.nih.govhttp://dx.doi.org/10.3390/ma14133705 |
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