TY - JOUR
T1 - Influence of fabric orientation and compression factor on the mechanical properties of 3D E-glass reinforced epoxy composites
AU - Nayak, Suhas Yeshwant
AU - Satish, Shenoy B.
AU - Sultan, Mohamed Thariq Hameed
AU - Kini, Chandrakant R.
AU - Rajath Shenoy, K.
AU - Samant, Rashmi
AU - Sarvade, Praneeth P.
AU - Basri, Adi Azriff
AU - Mustapha, Faizal
N1 - Publisher Copyright:
© 2020 The Author(s). Published by Elsevier B.V. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).
PY - 2020
Y1 - 2020
N2 - 3-D E-glass fabric reinforced epoxy composites at 6 mm thickness were fabricated for various orientations of the binder yarn viz. 0◦, 30◦, 45◦, 60◦ and 90◦ respectively. Tensile, flexural, interlaminar shear stress tests were conducted to ascertain the influence of binder yarn orientation on the mechanical properties of the composites. The composites with 0◦ binder yarn orientation showed the best strength followed by 90◦ whilst the others showed highly depleted traits in comparison. Shear stress induced at the interface of each lamina was seen as the major reason for drop in the strength. A secondary study was carried out to explore the effect of compression factor during fabrication on the mechanical properties of the composites. Laminates with varying thickness namely, 4 mm, 5 mm and 7 mm but, with same number of plies of 3D E-glass fabric at 0◦ orientation were fabricated. The test results were compared with the results of 6 mm composites from the primary study. The results showed that, compression factor affected the mechanical properties of the composites and had a direct relation with increasing compression factor up to a certain value beyond which a drop in properties was seen. Composites pressed to a thickness of 5 mm showed the best properties. Drop in properties was attributed to close packing of reinforcement and crushing of fibres leading to inefficient stress transfer. Scanning electron microscopy was employed to understand the modes of failure. The major failure modes observed were delamination, matrix cracking and debonding. Based on the results obtained, these composites can be seen as a material system for applications like ballistic armours, structural renovations and automobile components.
AB - 3-D E-glass fabric reinforced epoxy composites at 6 mm thickness were fabricated for various orientations of the binder yarn viz. 0◦, 30◦, 45◦, 60◦ and 90◦ respectively. Tensile, flexural, interlaminar shear stress tests were conducted to ascertain the influence of binder yarn orientation on the mechanical properties of the composites. The composites with 0◦ binder yarn orientation showed the best strength followed by 90◦ whilst the others showed highly depleted traits in comparison. Shear stress induced at the interface of each lamina was seen as the major reason for drop in the strength. A secondary study was carried out to explore the effect of compression factor during fabrication on the mechanical properties of the composites. Laminates with varying thickness namely, 4 mm, 5 mm and 7 mm but, with same number of plies of 3D E-glass fabric at 0◦ orientation were fabricated. The test results were compared with the results of 6 mm composites from the primary study. The results showed that, compression factor affected the mechanical properties of the composites and had a direct relation with increasing compression factor up to a certain value beyond which a drop in properties was seen. Composites pressed to a thickness of 5 mm showed the best properties. Drop in properties was attributed to close packing of reinforcement and crushing of fibres leading to inefficient stress transfer. Scanning electron microscopy was employed to understand the modes of failure. The major failure modes observed were delamination, matrix cracking and debonding. Based on the results obtained, these composites can be seen as a material system for applications like ballistic armours, structural renovations and automobile components.
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U2 - 10.1016/j.jmrt.2020.05.111
DO - 10.1016/j.jmrt.2020.05.111
M3 - Article
AN - SCOPUS:85087338379
SN - 2238-7854
VL - 9
SP - 8517
EP - 8527
JO - Journal of Materials Research and Technology
JF - Journal of Materials Research and Technology
IS - 4
ER -