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The mechanical effect of functionalization in laminated composite material.

The mechanical effect of functionalization in laminated composite material.

Authors :
Saracoglu, Goksel
Ceritbinmez, Ferhat
Özkan, Vildan
Yapici, Ahmet
Source :
Aircraft Engineering & Aerospace Technology. 2023, Vol. 95 Issue 7, p1005-1015. 11p.
Publication Year :
2023

Abstract

Purpose: This study aims to systematically compare the effect of increasing fiber–matrix interface adhesion and matrix toughness in layered composite materials. Design/methodology/approach: Silane ((3-glycidyloxypropyl) trimethoxysilane) was applied to strengthen the fiber–matrix interface connection in e-glass/epoxy laminated composite material. Using a cationic surfactant, 0.1% multi-walled carbon nanotubes (CNTs) were added to the matrix in two different ways, by with and without chemical functionalization using the vacuum infusion method. Findings: In the results obtained from the three-point bending test specimens, it was determined that the synergistic effect of silane application and non-functionalized CNT in the matrix was higher in terms of flexural modulus and strength values. Practical implications: The functionalization of multi-walled CNT did not give the expected results because of reasons such as viscosity increase and agglomeration in the matrix. Originality/value: In this study, a simple model for normalization and prediction purposes was developed, which allows the determination of the flexural modulus and un-notched flexural strength values from one test result of the notched specimen. A systematic comparison was performed by varying each parameter in the composite material. [ABSTRACT FROM AUTHOR]

Details

Language :
English
ISSN :
17488842
Volume :
95
Issue :
7
Database :
Academic Search Index
Journal :
Aircraft Engineering & Aerospace Technology
Publication Type :
Academic Journal
Accession number :
164010324
Full Text :
https://doi.org/10.1108/AEAT-08-2022-0229