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Effect of fibre orientation on mechanical properties of carbon fibre composites

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Title Effect of fibre orientation on mechanical properties of carbon fibre composites
 
Creator Subhedar, Kiran Mahadeo
Chauhan, Gaurav Singh
Singh, Bhanu Pratap
Dhakate, Sanjay Rangnath
 
Subject Carbon fibre composite
FEA
Flexural properties
Laminate composites
 
Description 1100-1103
The research aims to investigate the carbon fibre composite laminate for effect of their layer configuration including their number and relative orientation of fibre angles on their mechanical properties and its consistency with the results obtained from simulated data using finite element analysis (FEA) on mechanical properties. The laminate composite with four types of  fiber layer orientations were prepared using total eight layers including unidirectional and cross ply layers with different orientations. The flexural properties of the samples were evaluated. The results of experiments found consistent with the simulated data and it indicates that the fibre orientations and its layer sequence influence the characteristics of laminate composites. The composite with 0° orientated unidirectional fibre layers shows maximum flexural strength. The flexural strain is higher for laminate composite having layers with cross plies (45° fibre orientations). The different position of cross ply in the sequence shows variations in flexural properties because the typical nature of the three point bending flexural test of laminate composite where top side layers are under compression and bottom side layers are under tension.
 
Date 2021-02-22T08:44:53Z
2021-02-22T08:44:53Z
2020-12
 
Type Article
 
Identifier 0975-1017 (Online); 0971-4588 (Print)
http://nopr.niscair.res.in/handle/123456789/56265
 
Language en_US
 
Rights CC Attribution-Noncommercial-No Derivative Works 2.5 India
 
Publisher NISCAIR-CSIR, India
 
Source IJEMS Vol.27(6) [December 2020]