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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Bibliographic Details
Main Authors: M. Nasir, M. Nazreen, Mezeix, Laurent, Aminanda, Yulfian, Seman, Adam, Rivai, Ahmad, Ali, Karim Mansur
Format: Conference or Workshop Item
Language:English
English
Published: IOP Publishing 2016
Subjects:
Online Access:http://irep.iium.edu.my/50019/
http://irep.iium.edu.my/50019/
http://irep.iium.edu.my/50019/
http://irep.iium.edu.my/50019/3/50019.pdf
http://irep.iium.edu.my/50019/5/50019-Spring-back%20simulation%20of%20unidirectional%20carbon-SCOPUS.pdf