Spring-back simulation of unidirectional carbon epoxy L- shaped laminate composites manufactured through autoclave processing

This paper presents an original method in predicting the spring-back for composite aircraft structures using non-linear Finite Element Analysis (FEA) and is an extension of the previous accompanying study on flat geometry samples. Firstly, unidirectional prepreg lay-up samples are fabricated on moul...

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Veröffentlicht in:	IOP conference series. Materials Science and Engineering 2016-02, Vol.114 (1), p.12025-12035
Hauptverfasser:	Nasir, M N M, Mezeix, L, Aminanda, Y, Seman, M A, Rivai, A, Ali, K M
Format:	Artikel
Sprache:	eng
Schlagworte:	Aircraft components Aircraft structures Angles (geometry) Comparative studies Corners Deformation Deformation effects Finite element method Flats Interfacial properties Mathematical models
Online-Zugang:	Volltext
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