Record Details

Effect of fibre orientation on mechanical properties of carbon fibre composites

Online Publishing @ NISCAIR

View Archive Info
 
 
Field Value
 
Authentication Code dc
 
Title Statement Effect of fibre orientation on mechanical properties of carbon fibre composites
 
Added Entry - Uncontrolled Name Subhedar, Kiran Mahadeo; Advanced Carbon Products, Division of Advanced Materials and Devices, CSIR-National Physical Laboratory (NPL), New Delhi 110 112, India
Chauhan, Gaurav Singh; Advanced Carbon Products, Division of Advanced Materials and Devices, CSIR-National Physical Laboratory (NPL), New Delhi 110 112, India
Singh, Bhanu Pratap; Advanced Carbon Products, Division of Advanced Materials and Devices, CSIR-National Physical Laboratory (NPL), New Delhi 110 112, India
Dhakate, Sanjay Rangnath; Advanced Carbon Products, Division of Advanced Materials and Devices, CSIR-National Physical Laboratory (NPL), New Delhi 110 112, India
 
Uncontrolled Index Term Carbon fibre composite, FEA, Flexural properties, Laminate composites
 
Summary, etc. 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.
 
Publication, Distribution, Etc. Indian Journal of Engineering and Materials Sciences (IJEMS)
2021-03-24 10:24:59
 
Electronic Location and Access application/pdf
http://op.niscair.res.in/index.php/IJEMS/article/view/47552
 
Data Source Entry Indian Journal of Engineering and Materials Sciences (IJEMS); ##issue.vol## 27, ##issue.no## 6 (2020): IJEMS- DECEMBER 2020
 
Language Note en
 
Terms Governing Use and Reproduction Note Except where otherwise noted, the Articles on this site are licensed under Creative Commons License: CC Attribution-Noncommercial-No Derivative Works 2.5 India © 2015. The Council of Scientific & Industrial Research, New Delhi.