Abstract
Nowadays, the demand for fiber-based composites increases continuously compared to conventional materials because of their excellent mechanical properties. Synthetic fibers have specific advantages over natural fibers. It includes strength to weight ratio, durability, wrinkle resistance, and the ability to absorb moisture is less. However, the synthetic material having a few demerits also. To overcome the drawbacks of the synthetic fiber-based composite, an attempt is made to fabricate the hybrid composite specimen to obtain the combined benefits of the synthetic and natural fiber-based composites. The potential applications of the hybrid composites are aerospace, marine, and industrial structural applications. The composite specimen has been fabricated by using different natural and synthetic fibers, namely, Abaca (A), Hemp (H), Kevlar (K), and Glass (G). The three different hybrid composite specimens have been fabricated, each consisting of 5 layers are as follows, 1) the first and last layers of the specimen are Kevlar, and the remaining layers are Abaca fibers, 2) the first and last layers are Glass, and remaining layers are Hemp fibers, 3) first and the last layer is Glass, and remaining layers are Abaca fibers. The experimental results of the Glass/Hemp based composite have been compared with the simulation results. A good agreement has been found between the experimental and the simulation results. The Kevlar/Abaca composite displays a maximum load-carrying capacity in tensile, flexural, and impact is 5600 N, 86 kgf, and 3.625 J, respectively, followed by the Glass/Hemp and Glass/Abaca composites. It is due to the load being transferred in the following order during tests, which is as follows: matrix, natural fibers, and synthetic fibers. The displacement corresponds to load, which also increases during tests due to the percentage of elongation of the fibers. The interfacial bonding between the matrix and the fiber is also responsible for better results.