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...
Main Authors: | , , , , , |
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Format: | Conference or Workshop Item |
Language: | English English |
Published: |
IOP Publishing
2016
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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 |