Consideration of lamination structural analysis in a multi-layered composite and failure analysis on wing design application

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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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Bibliographic Details
Main Authors:	Basri, Ernnie Illyani, Hameed Sultan, Mohamed Thariq, Basri, Adi Azriff, Mustapha, Faizal
Format:	Article
Published:	Multidisciplinary Digital Publishing Institute 2021
Online Access:	http://psasir.upm.edu.my/id/eprint/96513/

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