Consideration of Lamination Structural Analysis in a Multi-Layered Composite and Failure Analysis on Wing Design Application

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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Bibliographic Details
Main Authors: Ernnie Illyani Basri, Mohamed Thariq Hameed Sultan, Adi Azriff Basri, Faizal Mustapha, Kamarul Arifin Ahmad
Format: Article
Language:English
Published: MDPI AG 2021-07-01
Series:Materials
Subjects:
laminates composite
computational modeling
finite element analysis
failure assessment
Online Access:https://www.mdpi.com/1996-1944/14/13/3705

Internet

https://www.mdpi.com/1996-1944/14/13/3705

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