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Article

Influence of Jute Fiber Volume Fraction on the Mechanical Properties of Epoxy Matrix Composites: Applications in Motorcycle Fairing Design

by
Paul Edgardo Medina Agurto
1,
Elmer Rolando Polo Briceño
1,
Saúl Andrés Hernández Moreno
2,
Oscar Humberto Sierra Herrera
2,
Mario Eduardo González Niño
2,
Jersson X. Leon-Medina
2 and
Rodolpho Fernando Váz
3,*
1
Facultad de Ingeniería y Arquitectura, Escuela de Ingeniería Mecánica Eléctrica, Universidad Señor de Sipán, Chiclayo 14001, Peru
2
Escuela de Ingeniería Electromecánica, Universidad Pedagógica y Tecnológica de Colombia, Facultad Seccional Duitama, Carrera 18 con Calle 22, Duitama 150461, Colombia
3
Stony Brook University, Room 130 Heavy Engineering Bldg., Stony Brook, NY 11794, USA
*
Author to whom correspondence should be addressed.
Appl. Sci. 2025, 15(10), 5515; https://doi.org/10.3390/app15105515
Submission received: 7 April 2025 / Revised: 9 May 2025 / Accepted: 12 May 2025 / Published: 14 May 2025

Abstract

:
This study explores the relationship between the volumetric fraction of jute fiber and the mechanical properties of epoxy matrix composites for motorcycle fairings, highlighting the feasibility of jute fibers due to their strength and sustainability. Through a methodology that includes meticulous fiber cleaning, precise mold fabrication, and rigorous evaluation of tensile and impact properties, the study provides an innovative perspective in composite materials engineering. The results demonstrate that composites with jute fibers are viable for manufacturing fairings with excellent thermal and mechanical performance, opening new avenues for motorcycle manufacturing that prioritize both performance and environmental responsibility.

1. Introduction

Currently, composite materials engineering stands at a crucial juncture, facing the challenge of integrating sustainability and efficiency into its applications. Jute fiber, in particular, has emerged as an eco-friendly and cost-effective alternative to synthetic fibers for critical structural applications [1], such as motorcycle fairings. In terms of mechanical strength, jute and hemp fibers [2] present the most significant values compared to other natural fibers, with ranges of 400–800 and 550–900 MPa, respectively [3]. This robustness is attributable to their high cellulose content, making them particularly suitable for structural applications in the composite materials industry, such as motorcycle fairings, where a combination of lightweight and mechanical strength is required. This study delves into how the volumetric fraction of jute fiber affects the mechanical properties of epoxy matrix composites, especially in motorcycle fairing design, an area that has not been exhaustively explored until now.
This study builds upon previous works, such as those by Veeraprabahar et al. [4], which underscore the importance of thermal insulation properties in natural fiber composites like coconut and jute fibers in polyurethane foam, which can maintain thermal conductivity at optimal levels; high-temperature tests indicate exceptional performance at over 350 °C, especially in compositions with 10% of these fibers. This thermal insulation characteristic would not only provide better protection for the rider’s lower extremities against engine heat but also contribute to the durability and performance of the fairing. Additionally, Alhijazi et al. [2] highlight the advantages of natural fiber composites (NFCs) in terms of lightweightness and sustainability. These studies provide crucial context for understanding the potential application of jute fiber in the automotive sector. Likewise, it is demonstrated how the addition of jute fiber to epoxy resin composites can significantly improve their mechanical strength [5,6,7], a crucial finding for designing more resilient and lightweight fairings. On the other hand, Arputhabalan et al. [8] offer insight into the sustainability of jute fiber in epoxy composites, an essential aspect in the quest for environmentally responsible solutions.
Gukendran et al. [6] highlight the versatility and effectiveness of jute fiber in composite material applications. Treatment with SiO2 nanoparticles improved the jute fibers´ surface energy and tensile strength by 11.7 and 17.9%, respectively. Moreover, jute composites in polypropylene and polylactic acid matrices showed significant variations in behavior under load [9]. Hybrid jute and E-Glass composites in an epoxy resin matrix showed a notable 150% increase in tensile strength [10]. Conversely, applications of these natural fibers in jute fiber-reinforced concrete showed improvement in strength and durability with an optimal fiber ratio between 1 and 2% [11]. These collective findings underscore the potential of jute fiber in reinforcing and improving the mechanical properties of various composites and materials.
The study by Ramesh et al. [5] demonstrates how hydrophobic treatment can be crucial to improving the durability of composite materials in humid environments, reducing moisture absorption to 2.71%, and improving mechanical strength. In the work by Arputhabalan et al. [8], the relevance of the volumetric fiber fraction in the mechanical performance of epoxy composites is highlighted, an essential aspect for designing structural components. Ku et al. [12] reveal that a proper balance between fiber fraction and matrix is key to optimizing tensile strength (reaching 42 MPa) and fatigue resistance, vital in applications subjected to cyclic loads. Finally, Martinez and Puente [13] emphasize the importance of ceramic fillers in improving properties such as tensile strength, crucial for applications where impact resistance and stiffness are prioritized. These findings are fundamental for motorcycle fairing design, where strength, durability, and lightweight properties are critical.
However, despite these advances, significant gaps exist in the literature, especially regarding the mechanical optimization of epoxy resin and jute fiber composites for specific applications such as motorcycle fairings. This study aims to fill these gaps, offering a detailed analysis of the effective integration of jute fiber into epoxy composites for fairing design. The challenges in fiber surface uniformity, fiber–matrix adhesion, and thermal resistance, key elements to ensure the viability of these materials in automotive environments, will be addressed. Additionally, the impact of different surface treatments on jute fibers will be explored, as well as their long-term behavior and durability in various environments.
This study proposes a comprehensive analysis that enriches the theoretical understanding of the interactions between jute fiber and epoxy matrix and also offers practical insights for their implementation in the automotive industry. By considering fiber orientation and manufacturing techniques for a motorcycle fairing piece, this work aims to develop fairings that are not only mechanically robust and lightweight but also sustainable and suitable for the modern automotive industry.
The central issue of this study lies in the urgent need to develop more sustainable and efficient motorcycle fairings. Traditionally, manufacturing these components has relied on materials that, while functional, do not meet the increasing environmental sustainability standards. Furthermore, strength and thermal insulation efficiency are often not optimized. This challenge becomes more relevant in a context where the demand for environmentally responsible vehicles is rising. Therefore, this research evaluates jute fiber-reinforced epoxy composites as a viable alternative, seeking to overcome these limitations and move towards a more environmentally friendly solution in the motorcycle industry.
The performance of tests with different volumetric fractions of jute fiber in composite plates aims to comprehensively evaluate the traction and impact properties of the composite material. By varying the volumetric fraction of fiber in each plate, the number of layers was adjusted, directly influencing the strength and other characteristics of the resulting composite. This variation in the number of layers allows for collecting a wide range of data, which is essential for understanding the influence of different reinforcement content on mechanical properties. Upon completion of the tests, comparing these results with previous studies on the same subject enables a critical analysis of the viability and performance of the developed composites following existing industry standards [9]. The growing use of natural fiber composites in automotive structures, like underfloor panels and engine covers, further confirms their potential in lightweight and sustainable vehicle design [14].
Jute fiber from Corchorus olitorius and Corchorus capsularis plants [15] is valued for its strength, flexibility, and mechanical properties, making it useful in different sectors, like textiles and automotive [16]. Figure 1 shows commonly available natural jute fibers. India produces approximately 55% of the world´s total production of jute, followed by Bangladesh and China [17]. In Peru, it is recognized as a priority resource, supporting both economic and environmental goals. Jute absorbs CO2 and releases O2, helping combat climate change. It grows well in regions like Loreto and Ucayali, where the climate and soil are ideal for its cultivation [18].
Surface modification of fibers using chemical agents enhances the mechanical properties of composites, particularly when using 15 mm fiber length [10]. To optimize the performance of NFCs, it is essential to utilize treated fibers and assess their erosion wear resistance [7]. Notably, H2O2 treatment has been shown to improve mechanical properties further [20]. Additionally, jute fiber-reinforced composites exhibit mechanical characteristics comparable to those of glass fiber-reinforced composites [21]. Jute fiber demonstrates a promising balance between mechanical performance, cost, and sustainability, making it a suitable candidate for structural applications such as motorcycle fairing design, where strength-to-weight ratio is critical [22].
On the other hand, Reddy et al. [23] developed a hybrid composite incorporating 20% jute fiber and varying pomegranate peel-powder content (2–8%). Mechanical tests revealed that strength improved up to 6% filler, but higher concentrations led to agglomeration and property deterioration. The study concluded that this combination not only enhances mechanical performance but also reduces costs, eliminates synthetic fibers, and promotes more sustainable manufacturing. Bhargav and Babu [24] investigated biodegradable polymers as eco-friendly alternatives to synthetic fibers, aiming to reduce environmental impact and resource depletion. They focus on natural fibers like jute, which are renewable and offer better mechanical properties, though they face challenges such as poor bonding with the matrix and water absorption. Their research shows that adding TiO2 to jute composites enhances their strength, flexibility, and resistance to erosion.
Fiber–matrix compatibilization systems improve the bond between fibers and matrices, enhancing adhesion, load transfer, and overall mechanical performance [25]. These systems, including coupling agents and matrix modifiers, help overcome challenges like poor fiber–matrix compatibility and defects [26]. Manual laminating, used in motorcycle fairing design, involves layering jute fibers soaked in epoxy resin, allowing precise control over fiber orientation and layer thickness, which affects the fairing’s strength and performance [27]. Epoxy resin, known for its strength, adhesion, and stability, is widely used in composites for aerospace, automotive, and construction applications, offering durability and resistance to extreme conditions [28].

2. Materials and Methods

2.1. Preparation of Specimens for Tensile and Impact Testing

The fiber volume fraction ( V f ) in a composite material represents the fiber volume ratio to total composite volume, directly influencing its mechanical properties. Figure 2 shows natural jute fiber with a mesh-type weave or 90/0°. Manufacturing proportions for jute fiber-reinforced epoxy matrix composites is shown in Table 1. From here on, only the jute fiber volume content is present, considering the complement percentage of epoxy volumetric content in the composite composition. It is determined using the densities and masses of both fiber and matrix, assuming minimal void content [21]. The calculation is as follows in (1):
V f = m f i b e r ρ f i b e r m f i b e r ρ f i b e r + m r e sin ρ r e sin
where m f i b e r and m r e s i n are the mass of fiber and resin, respectively. In addition, ρ f i b e r and ρ r e s i n are the density of fiber and resin, respectively.
Different amounts of jute fiber reinforcement layers were used based on the target volumetric fraction of the composite, as detailed in Table 1. Each layer consisted of a textile sheet measuring 15 × 20 cm². The fabrication of the composite materials was carried out using the hand lay-up process, a technique widely employed for the production of small-batch laminated structures. East Coast Resin epoxy resin was used, with an average density of 1.15 g/cm³, for jute fiber with a density of 1.35 g/cm³. The system consists of the resin (component A) and the hardener (component B), which must be mixed according to the manufacturer’s specified ratio. The recommended mixing ratio is 1:1 by volume, meaning one part resin to one part hardener.

Process Description

The manufacturing and evaluation processes for jute fiber-reinforced epoxy matrix composites is described and illustrated in Table 2. This manufacturing and evaluation method allows for a comprehensive comparison of jute fiber composites at different volumetric proportions showed in Figure 3 and Figure 4, providing a detailed understanding of how these variations affect the mechanical properties of the composite material.

2.2. Tensile Testing

The samples’ strength was measured by tensile testing using a Tecnotest 60TN universal testing machine. The dimensions of the samples and the testing parameters were performed according to the ASTM D638 standard [29]. Three tensile tests were done for each volumetric fraction of jute fiber on epoxy composite, and the average result was calculated.

2.3. Impact Testing

The effect of the volumetric fraction of jute fiber on the toughness of the epoxy matrix composite was evaluated by impact tests, following the DIN EN ISO 179-1 standard [30] impact tester. Three tests were performed for each composition of jute fiber-reinforced epoxy composites, and the average result was calculated.

2.4. Impact Testing Simulating

Vehicles such cars, motorcycles, and trains—among many others—are bodies in motion and are exposed to impacts of solid bodies, such as road debris and rocks. For simulating the impact resistance of jute fiber-reinforced epoxy composite Bajaj Dominar 400 motorcycle fairings, a 3D model of each part was made using Dassault Systèmes SolidWorks CAD software 2023 student version.
The motorcycle front cowl was chosen for this study due to its relatively simple geometry and high exposure to impacts.

2.4.1. Composite Material Properties for Simulation

Using the CES EduPack software 2023 student version, the virtual synthesis of a composite material with an epoxy resin matrix reinforced with jute fiber was successfully achieved. This modeling process relied on precise adjustments to the fiber volume fraction to align the simulated mechanical properties with those experimentally observed in tensile tests. Such calibration enables more accurate inferences of additional mechanical properties of the composite material, as demonstrated by the data generated by the software. This methodological approach, supported by the direct correlation between experimental results and modeling, ensures that the properties derived from the composite material accurately reflect its behavior under real-world conditions. Table 3 shows the physical properties of jute fiber-reinforced epoxy composite, adjusted to experimental tensile stress.

2.4.2. Properties of AISI 1020 Carbon Steel

For the impact resistance analysis of the motorcycle fairing, a simulation method was employed, incorporating spherical projectiles made of AISI 1020 carbon steel, selected for their excellent hardness properties and required density to simulate impacts from solid entities such as debris and asphalt fragments that the motorcycle fairing will be exposed to. Table 4 shows the mechanical properties of AISI 1020 carbon steel.

2.4.3. Simulation of Spherical Body Impact on the Motorcycle Front Fairing

These spheres, with a diameter of 20 mm, exceed the dimensions of objects typically found in real traffic scenarios. This ensures a conservative model intensifying the impact conditions for a more rigorous evaluation of the fairing’s behavior. Table 5 shows the conditions of spherical impacting bodies.
The spheres that impact the motorcycle front fairing, traveling at a speed of 54 km/h, strike it at different angles and surfaces of the fairing, as positioned in the manner shown in Figure 5. The boundary conditions included the effect of gravity (9.81 m/s²) and structural constraints applied at the mounting points of the fairing, replicating its actual attachment on naked-type motorcycles. The domain discretization was carried out using a mesh of tetrahedral solid elements of type SOLID185, with an average element size of 6.781 × 10−3 m. A localized refinement was applied in the areas anticipated for impact to capture the local material response more accurately.
Additionally, a mesh convergence study was performed, verifying that the variations in the results of the Von Mises equivalent stress remained below the 5% threshold, thus ensuring numerical stability and the reliability of the computational model.

2.5. Make a Motorcycle Fairing Part

Using photogrammetry to measure a real component and the 3D model made in Solidworks software to draw it, a mold for the fairing was manufactured using Fused Deposition Modeling (FDM) technology, employing polylactic acid (PLA) filament. An extruder with a 6 mm diameter nozzle was used, and a layer height of 0.16 mm was configured to achieve high surface resolution on the mold. Subsequently, meticulous post-processing of the mold was carried out, including manual sanding to minimize ridges and other surface defects resulting from the 3D printing process. This step is essential to ensure the surface quality of the final fairing and improve fiber adhesion to the mold. To enhance finish quality and facilitate demolding operation, the mold was covered with a 3M vinyl film. This layer provided a smoother and more homogeneous surface, essential for manufacturing of high-quality composites. The complete manufacturing process of motorcycle fairing made of jute fiber-reinforced epoxy composite is shown in Figure 6.

3. Results and Discussion

The structural design of motorcycle fairings demands a detailed analysis of the configuration of jute fiber layers, as the laminar arrangement determines the mechanical strength and rigidity of the component [13]. Figure 3 and Figure 4 show the specimens for the experimental tests; tensile strength is paramount, as it correlates with the fairing’s ability to withstand dynamic forces in operation, contributing to aerodynamic stability and structural integrity [31]. Regarding impact resistance, its importance is accentuated in collision scenarios, where a sturdy fairing can mean the difference between minor or major damage for both the rider and the motorcycle, acting as a crucial protective barrier [4]. Tensile strength is crucial, as it relates to the fairing’s ability to withstand dynamic forces during operation, contributing to both aerodynamic stability and structural integrity [32]. Therefore, the appropriate selection of the number of layers and the understanding of tensile and impact properties enhance performance and are also essential for safety in motorcycle engineering. The testing results are shown in Table 6, presenting the tensile and impact behavior of the composite material.
Tensile and impact tests conducted on jute fiber composites reveal that a volumetric fraction of 26.7% provides an optimal balance between strength and energy absorption, with an average maximum stress of 42.94 MPa and impact energy of 16.83 kJ/m². This balance is crucial for motorcycle fairings, which must withstand significant forces during everyday use and provide protection in impact situations. The selection of this volumetric fraction is key to developing fairings that meet aesthetic and performance standards and enhance the overall safety of the vehicle.
In the comparison of jute fiber-reinforced epoxy composite and the same 90 and 0° fiber orientation, a key distinction in mechanical behavior attributable to differences in weave architecture and laminate thickness is observed. While composites with “mesh” weave in this research show a tendency towards higher displacement at maximum load, reflecting increased ductility and deformation capacity under applied loads, results obtained by Naranjo [11], with “twill” weave, exhibit higher maximum stress values despite having a lower thickness; this can be inferred from Table 7. Woven jute fiber with an estimated weight of 106.67 g/m² was used, calculated from a 25 cm × 15 cm sample weighing 4 g. In contrast, the study conducted by Naranjo et al. reports an actual weight of 390 g/m², obtained from a mass of 2.4375 g over an effective area of 62.5 cm², corresponding to the dimensions of the tensile specimen (250 × 25 mm²). This phenomenon can be interpreted as a significant influence of twill weave on the material’s tensile strength, as shown in Figure 7, due to more effective fiber alignment, favoring load transfer.

3.1. Impact Simulation

Figure 8 shows the impact energy absorption graph for jute fiber-reinforced epoxy composites with 90/0° orientation with different reinforcement volumetric fractions. The creation of a detailed 3D model of the Bajaj motorcycle fairing marked a key step in our engineering project. Using photogrammetry, high-resolution images captured the vehicle from various angles, enabling accurate reconstruction in SolidWorks. This model became a vital tool for visualization, analysis, and manufacturing, offering insights into the fairing’s structural and aesthetic dynamics. The integration of digital technologies optimized development and ensured well-informed design decisions aligned with performance goals.
In motorcycle fairing design (see Figure 9), components like the tail section and fender improve aerodynamics, protect the rider from impacts and engine heat, and preserve critical parts of the vehicle [33]. Using epoxy composites reinforced with jute fibers enhances the fairing’s mechanical properties, offering a sustainable alternative that improves impact resistance and durability. By adjusting the volume fraction of jute fibers, manufacturers can optimize these composites for better rider protection and vehicle performance [4]. Recent Computational Fluid Dynamics-CFD based studies on high-performance motorcycle fairings, such as those conducted on the Honda™ RS, confirm that even small aerodynamic refinements can yield measurable performance gains—emphasizing the importance of material optimization and design synergy [34]. The aerodynamic behavior of motorcycle fairings is not only governed by geometry but also by the physical properties of the material used. Studies with fiberglass prototypes have shown that lighter, smoother materials can significantly reduce drag forces and improve stability at high speeds—insights that support the exploration of natural fiber composites such as jute for sustainable and functional fairing designs [35].
The computerized impact simulation modeled the motorcycle front fairing using a jute fiber-reinforced epoxy composite. The results, obtained through a finite element analysis, provided critical metrics such as directional deformation and Von Mises equivalent stress. These indicators are essential for evaluating the fairing’s structural response under impact loads. Directional deformation offers a detailed view of the fairing’s distortion in the direction of impact, while the Von Mises equivalent stress is a key parameter for determining the onset of yielding or material failure under multiaxial loading conditions.

Von Mises Equivalent Stresses

The finite element simulation conducted in ANSYS for the motorcycle front fairing, as shown in Figure 5 and Figure 10, composed of an epoxy resin matrix reinforced with 26.7% jute fiber, indicates a maximum Von Mises equivalent stress of 35.12 MPa at the established simulation time.
When comparing this maximum stress value with the material’s yield strength, experimentally determined as 41.80 MPa, it is observed that the stress induced by the simulated impact remains below the yield threshold. This suggests that, although the material is subjected to a significant load, it does not reach the point of permanent plastic deformation under the modeled impact conditions, as shown in Figure 11 and Figure 12.
Under the parameters of this specific simulation, which represents a collision with projected objects during driving, the fairing would not exhibit structural failure, maintaining its integrity.

3.2. Motorcycle Fairing Manufacturing

The 3D modeling (see Figure 13) of a Bajaj Dominar 400 motorcycle was carried out to identify the most suitable sections of the fairing for the application of composite materials. The front cowl was selected due to its relatively simple geometry and manageable dimensions, facilitating the comparative analysis of the mechanical properties of the composite material.
Following the manual lay-up procedure, woven jute fiber was laid up in 0 and 90° orientations on the prepared mold. Each fiber layer was impregnated with epoxy resin, ensuring complete and uniform saturation. Curing was carried out at room temperature, carefully controlling the times to ensure proper polymerization of the epoxy matrix and thus achieve a composite with mechanical properties optimized for its aerodynamic function in motorcycle fairings.
In this way, the natural fiber composite dome stands out for its focus on sustainability, while also offering a lower total manufacturing cost (see Figure 14 and Figure 15). Although the tensile strength of the composite dome is slightly lower than that of the commercial dome, its performance remains within an acceptable range for practical applications, showing adequate yield strength to withstand typical loads under driving conditions. Furthermore, the smooth finish and reduced susceptibility to scratches reflect a commitment to aesthetics and durability. The slightly lower weight of the natural fiber composite may reduce the motorcycle total weight, potentially improving fuel efficiency and maneuverability.
In the comparison presented in Table 8, two motorcycle front fairings are contrasted: one made of jute fiber-reinforced epoxy composite and a commercial one made of polycarbonate.

4. Conclusions

The conclusions of this research highlight the potential of jute fibers as reinforcement in epoxy matrix composites for automotive industry applications, particularly in the manufacturing of motorcycle fairings. The optimized orientation of jute fibers in the composite parts ensures the necessary mechanical strength, while their high cellulose content contributes to structural integrity and tensile strength, with ranges of 29.6–45.6 MPa and impact resistance of 16.83 kJ/m². The viability of these materials is further reinforced by their adequate thermal conductivity, which is crucial for thermal protection in the vicinity of the engine and for rider safety.
The fabrication of a motorcycle fairing cowl using a composite material with a volumetric fraction of 26.7% jute fiber has proven to be a successful decision in achieving a balance between tensile and impact strength. Experimental results indicating maximum stress of 42.94 MPa and impact energy of 16.83 kJ/m² underscore the material’s ability to withstand aerodynamic forces and impact conditions common in driving environments. The resulting cowl meets structural durability requirements and contributes to rider safety by efficiently absorbing energy in case of collisions. This advancement in fairing materials represents a significant step towards innovation in motorcycle design, where integrating sustainable and high-performance composite materials aligns with current trends in automotive engineering.
Furthermore, for the design and manufacturing of motorcycle fairings, the results of this research emphasize the importance of proper selection of fiber weave and laminate configuration. Fairings, which require a combination of structural rigidity and impact resistance without fracturing, would benefit from mesh weave for its increased ductility and energy-absorbing capacity, qualities that help mitigate damage in case of minor impacts and constant vibrations. On the other hand, twill weave, offering superior tensile strength, would be suitable for areas of the fairing subject to high aerodynamic loads, where rigidity is paramount to maintain aerodynamic stability and fairing shape at high speeds. This duality of properties suggests a hybrid design strategy, where both types of weaves could be used in different areas of the fairing, adapting each section to the type of load and expected performance, thus maximizing efficiency and safety on the motorcycle.

Author Contributions

Conceptualization, P.E.M.A., E.R.P.B. and S.A.H.M.; methodology, P.E.M.A., E.R.P.B. and S.A.H.M.; investigation, P.E.M.A., E.R.P.B., S.A.H.M., O.H.S.H. and M.E.G.N.; writing—original draft preparation, P.E.M.A., E.R.P.B., S.A.H.M., O.H.S.H., M.E.G.N., J.X.L.-M. and R.F.V.; writing—review and editing, J.X.L.-M. and R.F.V. All authors have read and agreed to the published version of the manuscript.

Funding

This research received no external funding.

Institutional Review Board Statement

Not applicable.

Informed Consent Statement

Not applicable.

Data Availability Statement

The raw data supporting the conclusions of this article will be made available by the authors on request.

Conflicts of Interest

The authors declare no conflicts of interest.

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Figure 1. (a) Untreated (raw jute) and (b) chemically treated jute fibers. Adapted from Wang et al. [19].
Figure 1. (a) Untreated (raw jute) and (b) chemically treated jute fibers. Adapted from Wang et al. [19].
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Figure 2. Natural jute fiber with a mesh-type weave or 90°/0°.
Figure 2. Natural jute fiber with a mesh-type weave or 90°/0°.
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Figure 3. CNC cutting of jute fiber and epoxy resin plates.
Figure 3. CNC cutting of jute fiber and epoxy resin plates.
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Figure 4. Specimens prepared for tensile and impact testing. Volumetric fraction of jute fiber: (a) 12.5, (b) 21.4, (c) 26.7, and (d) 28.6%.
Figure 4. Specimens prepared for tensile and impact testing. Volumetric fraction of jute fiber: (a) 12.5, (b) 21.4, (c) 26.7, and (d) 28.6%.
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Figure 5. Spheres and motorcycle fairing for simulation.
Figure 5. Spheres and motorcycle fairing for simulation.
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Figure 6. Manufacturing process of motorcycle front cowl made of jute fiber-reinforced epoxy composite.
Figure 6. Manufacturing process of motorcycle front cowl made of jute fiber-reinforced epoxy composite.
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Figure 7. Stress-strain results for jute fiber-reinforced epoxy composites.
Figure 7. Stress-strain results for jute fiber-reinforced epoxy composites.
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Figure 8. Impact energy absorption results for jute fiber-reinforced epoxy composites.
Figure 8. Impact energy absorption results for jute fiber-reinforced epoxy composites.
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Figure 9. Three-dimensional model of Bajaj motorcycle in SolidWorks software.
Figure 9. Three-dimensional model of Bajaj motorcycle in SolidWorks software.
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Figure 10. Details of mesh for front fairing components.
Figure 10. Details of mesh for front fairing components.
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Figure 11. Impact stresses of the 4 spheres on the motorcycle front fairing.
Figure 11. Impact stresses of the 4 spheres on the motorcycle front fairing.
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Figure 12. Stress-strain curve for 26.7% jute fiber-reinforced epoxy sample.
Figure 12. Stress-strain curve for 26.7% jute fiber-reinforced epoxy sample.
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Figure 13. Selected front cowl from Bajaj motorcycle 3D model.
Figure 13. Selected front cowl from Bajaj motorcycle 3D model.
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Figure 14. Jute fiber-reinforced epoxy composite motorcycle front cowl.
Figure 14. Jute fiber-reinforced epoxy composite motorcycle front cowl.
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Figure 15. Jute fiber-reinforced epoxy composite front cowl placed on Bajaj motorcycle.
Figure 15. Jute fiber-reinforced epoxy composite front cowl placed on Bajaj motorcycle.
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Table 1. Manufacturing proportions for jute fiber-reinforced epoxy composites.
Table 1. Manufacturing proportions for jute fiber-reinforced epoxy composites.
Composite Composition (Vol.%)
(Measuring Instrument Scale)Jute Fiber Layers
Jute fiberEpoxy resin
12.587.56
21.478.68
26.773.39
28.671.410
Table 2. Summary of processes for the manufacture and evaluation of jute fiber and epoxy matrix composites.
Table 2. Summary of processes for the manufacture and evaluation of jute fiber and epoxy matrix composites.
StepProcessImage
1Jute fibers were immersed in a solution of alcohol, distilled water, and ice for 24 h to remove impurities.Applsci 15 05515 i001
2A mold was constructed using ASTM A36 steel and Shielded Metal Arc Welding (SMAW).Applsci 15 05515 i002
3Jute fibers were cut to the dimensions of the mold, polyvinyl alcohol was applied to the mold, and epoxy resin was prepared and applied along with the layers of fiber. The mold was closed and taken to the compression press for 72 h. Finally, demolding was performed.Applsci 15 05515 i003
4Each composite plate with a specific volume of jute fiber was cut using CNC.Applsci 15 05515 i004
5Tensile and impact testing specimens were cut from each plate.Applsci 15 05515 i005
Table 3. Physical and mechanical properties of jute fiber-reinforced epoxy resin composite, adjusted to experimental tensile stress.
Table 3. Physical and mechanical properties of jute fiber-reinforced epoxy resin composite, adjusted to experimental tensile stress.
PropertiesValuesUnits
Physical properties
Density1.11–1.43103 kg/m³
Mechanical properties
Young’s modulus2.36–2.45GPa
Yield strength (elastic limit)36.1–71.9MPa
Tensile strength45.3–89.6MPa
Compressive strength56.4–128MPa
Flexural modulus2.25–3.79GPa
Flexural strength (modulus of rupture)36.2–71.9MPa
Shear modulus0.381–1.95GPa
Bulk modulus2.00–2.70GPa
Poisson’s ratio0.391–0.407
Thermal properties
Thermal conductivity0.181–0.196W/m·°C
Specific heat capacity1.0243–1.0293J/g·°C
Thermal expansion coefficient80.2µstrain/°C
Primary production energy, CO2 and water
Embedded energy, primary production108–152MJ/kg
CO2 footprint, primary production5.55–7.82kg/kg
Table 4. Mechanical properties of AISI 1020 carbon steel. Obtained from CES EduPack software.
Table 4. Mechanical properties of AISI 1020 carbon steel. Obtained from CES EduPack software.
PropertiesValuesUnits
Mechanical properties
Young’s modulus205–215GPa
Specific stiffness26.1–27.4MN·m/kg
Yield strength (elastic limit)265–325MPa
Yield strength with temperature272–272MPa
Tensile strength355–435MPa
Specific strength33.8–41.4kJ/kg·m
Elongation28–43% strain
Tangent modulus671MPa
Compressive strength521–563MPa
Flexural modulus205–215GPa
Flexural strength (modulus of rupture)355–435MPa
Shear modulus79–84GPa
Bulk modulus158GPa
Poisson’s ratio0.285–0.295
Shape factor61
Hardness110–130HV
Elastic stored energy (springs)169–249kJ/m³
Fatigue strength at 107 cycles207–248MPa
Fatigue strength model (stress amplitude)180–277MPa
Table 5. Conditions of spherical bodies.
Table 5. Conditions of spherical bodies.
CharacteristicValueUnit
Object speed2m/s
Object radius20mm
Object weight33g
Height from ground (Sphere 1)73cm
Height from ground (Sphere 2)58cm
Height from ground (Sphere 3)98cm
Height from ground (Sphere 4)105cm
Table 6. Results of tensile and impact tests.
Table 6. Results of tensile and impact tests.
Tensile TestImpact Test
Volumetric Fraction of Jute Fiber (%)Average Maximum Stress (MPa)Average Energy (kJ/m²)
12.544.1814.83
21.439.7615.17
26.742.9416.83
28.641.6715.83
Table 7. Comparative table of results obtained in tensile tests.
Table 7. Comparative table of results obtained in tensile tests.
Weave TypeJute Fiber (%)Thickness (mm)Stress (MPa)Displacement (mm)
Results obtainedMesh12.505.0044.25.6
21.4039.86.9
26.7042.95.5
28.6041.75.5
Results by Naranjo [11]Twill303.5129.62.9
3.5124.42.9
3.9145.63.9
Table 8. Comparison of jute fiber-reinforced epoxy manufactured fairing piece versus polycarbonate.
Table 8. Comparison of jute fiber-reinforced epoxy manufactured fairing piece versus polycarbonate.
Jute Fiber Reinforced Epoxy DomePolycarbonate Dome
ImageApplsci 15 05515 i006Applsci 15 05515 i007
Thickness (mm)33–4.5
Tensile Strength (MPa)39.6–44.155–75
Yield Stress/Yield Strength (MPa)4165
Surface/FinishSmooth–Does not scratch easilySmooth–Scratches easily
Weight (g)183216
Material OriginEpoxy matrix and natural fibers–Petroleum-derived
Non-biodegradable matrix and renewable fibers–Non-renewable
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MDPI and ACS Style

Medina Agurto, P.E.; Polo Briceño, E.R.; Hernández Moreno, S.A.; Sierra Herrera, O.H.; González Niño, M.E.; Leon-Medina, J.X.; Váz, R.F. Influence of Jute Fiber Volume Fraction on the Mechanical Properties of Epoxy Matrix Composites: Applications in Motorcycle Fairing Design. Appl. Sci. 2025, 15, 5515. https://doi.org/10.3390/app15105515

AMA Style

Medina Agurto PE, Polo Briceño ER, Hernández Moreno SA, Sierra Herrera OH, González Niño ME, Leon-Medina JX, Váz RF. Influence of Jute Fiber Volume Fraction on the Mechanical Properties of Epoxy Matrix Composites: Applications in Motorcycle Fairing Design. Applied Sciences. 2025; 15(10):5515. https://doi.org/10.3390/app15105515

Chicago/Turabian Style

Medina Agurto, Paul Edgardo, Elmer Rolando Polo Briceño, Saúl Andrés Hernández Moreno, Oscar Humberto Sierra Herrera, Mario Eduardo González Niño, Jersson X. Leon-Medina, and Rodolpho Fernando Váz. 2025. "Influence of Jute Fiber Volume Fraction on the Mechanical Properties of Epoxy Matrix Composites: Applications in Motorcycle Fairing Design" Applied Sciences 15, no. 10: 5515. https://doi.org/10.3390/app15105515

APA Style

Medina Agurto, P. E., Polo Briceño, E. R., Hernández Moreno, S. A., Sierra Herrera, O. H., González Niño, M. E., Leon-Medina, J. X., & Váz, R. F. (2025). Influence of Jute Fiber Volume Fraction on the Mechanical Properties of Epoxy Matrix Composites: Applications in Motorcycle Fairing Design. Applied Sciences, 15(10), 5515. https://doi.org/10.3390/app15105515

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