| Issue |
EPJ Web Conf.
Volume 355, 2026
4th International Conference on Sustainable Technologies and Advances in Automation, Aerospace and Robotics (STAAAR 2025)
|
|
|---|---|---|
| Article Number | 02011 | |
| Number of page(s) | 13 | |
| Section | Additive Manufacturing and Sustainable Materials | |
| DOI | https://doi.org/10.1051/epjconf/202635502011 | |
| Published online | 03 March 2026 | |
https://doi.org/10.1051/epjconf/202635502011
Influence of Aerosil-200 Nanofiller on the Flexural and Compressive Behaviour of Glass Fiber Reinforced Epoxy Composites
1 Assistant Professor, Department of Mechanical Engineering, Matrusri Engineering College, Saidabad, Hyderabad - 500059, India
2 Assistant Professor, Department of Mechanical Engineering, St. Joseph’s College of Engineering, Old Mahabalipuram Road, Chennai – 600119, Tamil Nadu, India
3 Assistant Professor, Department of Mechanical Engineering, Matrusri Engineering College, Saidabad, Hyderabad - 500059, India
4 Assistant professor, Department of Mechanical engineering, Ballari Institute of Technology and Management, Ballari, affiliated to Visvesvaraya Technological University, Belagavi, Karnataka 583104, India
5 UG Scholar, Department of Mechanical Engineering, St. Joseph’s College of Engineering, Old Mahabalipuram Road, Chennai – 600119, Tamil Nadu, India
6 UG Scholar, Department of Mechanical Engineering, St. Joseph’s College of Engineering, Old Mahabalipuram Road, Chennai – 600119, Tamil Nadu, India
* Corresponding author: This email address is being protected from spambots. You need JavaScript enabled to view it.
Published online: 3 March 2026
Abstract
This study examines the impact of Aerosil-200 nanofiller on the mechanical properties of glass fiber reinforced epoxy composites in laminated plates and thin cylindrical shells. Composite specimens were produced with a hand lay-up method with nanofiller contents of 0%, 1%, 2%, 3%, and 4% by weight. Flexural tests on laminated specimens (ASTM D790) and compression tests on cylindrical shells were conducted to assess the impact of nanofiller on bending resistance and axial load-bearing capacity. The experimental results demonstrate a gradual improvement in flexural strength with an increase in nanofiller content up to 3%, with a maximum strength of 590.59 N/mm2, in contrast to 399.9 N/mm² for the unfilled laminate. A comparable trend is noted in compression testing, wherein the 3% nanofiller shell demonstrates the maximum compressive strength of 157.663 N/mm² and a peak load of 58.230 kN. The 4% filled sample exhibits diminished performance, with strength decreasing to 116.34 N/mm². The results indicate that Aerosil-200 markedly improves mechanical performance up to an ideal filler concentration of 3%, after which material degradation ensues. This study offers critical insights for optimizing nanofiller loading in composite materials to enhance flexural and compressive performance.
© The Authors, published by EDP Sciences, 2026
This is an Open Access article distributed under the terms of the Creative Commons Attribution License 4.0, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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