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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Detalles Bibliográficos
Autores principales: Basri, Ernnie Illyani, Sultan, Mohamed Thariq Hameed, Basri, Adi Azriff, Mustapha, Faizal, Ahmad, Kamarul Arifin
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2021
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC8269891/
https://www.ncbi.nlm.nih.gov/pubmed/34279278
http://dx.doi.org/10.3390/ma14133705

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC8269891/
https://www.ncbi.nlm.nih.gov/pubmed/34279278
http://dx.doi.org/10.3390/ma14133705

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