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The mechanical effect of functionalization in laminated composite material.
The mechanical effect of functionalization in laminated composite material.
- 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