Abstract

Fiber-reinforced composites are gradually replacing the traditional materials in many engineering applications. However, for many applications these materials are still unsuitable, due to their lack of toughness. In this context, hybridization is a promising strategy in which two or more types of fiber are combined to obtain a better balance of mechanical properties compared to non-hybrid composites. Therefore, the main goal of this work is to study the hybridization effect on the static performance and interlaminar shear strength. For this purpose, carbon, glass, and Kevlar fibers were used and combined in different proportions. It was possible to conclude that there is an ideal value of fiber content to maximize both properties and, depending on the type of fiber, they should be placed specifically on the compression or tensile side. For example, for composites involving carbon and glass fibers the latter must be placed on the compression side, and for a value of 17% by weight the flexural strength decreases by only 2.8% and the bending modulus by around 19.8%. On the other hand, when Kevlar fibers are combined with glass or carbon fibers, the Kevlar ones must always be placed on the tensile side and with an ideal value of 13% by weight.

Highlights

  • Fiber-reinforced composites are one of the most remarkable families of materials for technological and structural applications

  • In terms of bending modulus, the highest value was obtained for the carbon/epoxy composite, with an average value of 48.4 GPa, while the glass/epoxy composite showed a decrease of about 54.3% and the Kevlar/epoxy composite around 56.6%

  • Carbon, glass, and Kevlar fibers were combined with different fiber contents and placed in very specific positions

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Summary

Introduction

Fiber-reinforced composites are one of the most remarkable families of materials for technological and structural applications Nowadays, they are widely used in sectors such as the automotive and military industries, the renewable energy industry, infrastructures, medicine, and sports, but their sector of predilection is the aeronautical field [1,2]. High-modulus fibers (such as carbon fibers) or low-elongation (LE) fibers have the advantage of providing stiffness and load carrying capacity but less elongation and compressive strength, while lower-modulus fibers (such as glass and Kevlar fibers) or high-elongation (HE) fibers are characterized by lower stiffness, higher elongation, and damage tolerance Their combination allows one to improve the toughness, the final strength and stiffness are inferior to those of the high modulus [7,8]. It is possible to obtain more complex configurations by combining two of the three configurations, the first is the simplest and cheapest

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