Browse Topic: Composite materials

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Numerical Investigation of Low Velocity Impact Perforation in Natural–Synthetic Hybrid Composites for Automotive Applications2026-01-0246To be published on 04/07/2026
The increasing demand for sustainable and lightweight materials in the automotive industry has accelerated interest in natural fiber reinforced polymer composites. However, their limited impact resistance restricts application in structural and crash-relevant components. This work presents a numerical investigation of the low velocity impact (LVI) and perforation behavior of jute (J) and flax natural fiber reinforced epoxy composites (N) and their glass fiber (G) hybrid forms with synthetic fiber reinforced epoxy laminates (S), using LS-DYNA. A finite element model, developed with a discounted ply approach and MAT54 damage model, was first validated against published experimental data for glass/epoxy laminates, showing strong correlation in peak load and energy absorption. The validated model was then extended to simulate bidirectional natural fiber and hybrid laminates under 2–10 J impacts, replicating typical energy levels relevant to low-speed collisions and road debris impacts in
Mache, Ashok, Pingulkar, Harshad, Ambhore, Nitin, Hujare, Pravin, Salve, Aniket
High Strain-Rate Behaviors of Fiber Reinforced Composites in Principal and Off-Axis Directions2026-01-0175To be published on 04/07/2026
Materials can exhibit significantly different mechanical behaviors compared to quasi-static conditions at high strain rates (> 100 s-1). High strain rate tests using setups such as SHPB (Split-Hopkinson Pressure Bar) can provide, in a practicable manner, the stress-strain relations for a material at high strain rates. Such properties are vitally needed for activities such as simulation-driven impact safety design of composite structures deployed in the form of automotive body parts and assembly, and other sub-systems. Although the behaviors of isotropic and ductile materials such as various metallic alloys appear to have been extensively studied and reported in literature, dependence of mechanical properties of fiber-reinforced composites especially in different off-axis directions are extremely difficult to come across. To fill up this void, a detailed experimental study has been carried out on high strain rate mechanical characterization of orthotropic glass, carbon and a natural
Bawa, Prashant, Deb, Anindya, Zhu, Feng
Investigation into Dynamic Behavior of Jute-Glass-Aluminium Hybrid Polymer Composites for Automotive Applications2026-01-0245To be published on 04/07/2026
The research work in this paper investigates the development and dynamic characterization of lightweight hybrid polymer composites tailored for automotive applications. Fiber-reinforced polymer composites, owing to their high specific strength and stiffness, have emerged as promising candidates to replace conventional materials. Expanding on the current trend of hybridization that blends natural and synthetic fibers to optimize mechanical strength and vibration-damping behavior, this study incorporates aluminum perforated sheets (Al) as additional reinforcement to increase stiffness without significantly increasing weight. Jute (J) fibers, known for their inherent damping capability, were combined with glass fibers (G) and Al sheets. Six symmetric hybrid laminates G/J/Al/J/G, J/G/Al/G/J, J/J/Al/J/J, G/G/G/Al/G/G/G, and J/J/J/J/J were fabricated using hand lay-up followed by compression molding. The modal frequencies and damping properties were obtained through experimental testing
Salve, Aniket, Mache, Ashok, Nalawade, Dattatraya, Joshi, Shardul
A Study on Fatigue Life Prediction Method for Point-Based Joints Considering Multiple Fracture Modes – FDS, Blind Rivet, and Blind Nut Focus2026-01-0180To be published on 04/07/2026
The application of light weight alloys for vehicle bodies such as aluminum alloys and composite materials are rapidly advancing to support the construction of multi-material vehicle bodies. These materials play a crucial role in reducing overall vehicle weight, enhancing fuel efficiency, and complying with increasingly strict environmental regulations. As the automotive industry continues to evolve toward electrification and sustainability, the integration of lightweight and high-performance materials has become a key design strategy. However, the use of multiple materials introduces new challenges in manufacturing, particularly in joining technologies. Since different materials have varying mechanical properties, thermal behaviors, and surface characteristics, selecting appropriate joining methods is essential to ensure structural integrity and durability. Depending on the material types, thicknesses, production processes, and cost constraints, various joining techniques—such as
Takuno, Sougo, Isono, Toshiyuki, Urakawa, Kazushi, Goto, Suguru, Kawamura, Hiroaki, Niisato, Eita, Ishigami, Yuta
Multi-Objective Topology Optimization for Cost and Time Minimization in Fiber Reinforced Additive Manufacturing2026-01-0257To be published on 04/07/2026
Fiber Reinforced Additive Manufacturing (FRAM) combines the geometric freedom of additive manufacturing with the high strength-to-weight ratio of composite materials, enabling the production of lightweight, high-performance automotive components. The anisotropic nature of fiber-reinforced composites makes their mechanical performance highly dependent on fiber orientation relative to applied loads. Leveraging this directional behavior through optimization provides opportunities to enhance structural efficiency while reducing vehicle weight. Conventional FRAM research has largely focused on structural objectives such as compliance minimization, often overlooking manufacturability challenges. In particular, support structures - temporary features required for overhang fabrication - can significantly increase print time, material usage, and production cost, limiting industrial adoption. To address this gap, this research introduces a novel multi-objective topology optimization framework
Wotten, Erik, Kim, Il Yong
Anisotropic mechanical property simulation of fiber reinforced PEEK using composite theory and comparison to experimental results2026-01-0256To be published on 04/07/2026
The mechanical properties of 3D printed composites have been shown to vary due to the manufacturing infill direction due to artifacts from the printing process. PEEK (Polyether Ether Ketone) and PEEK reinforced with carbon fiber were studied for these experiments because they are widely used for their high strength properties. 3D printed composites that behave with anisotropic characteristics have been evaluated under Laminate Composite Theory (LCT), which can be used to determine the mechanical properties of these 3D printed composites. By changing the orientation of the extruded strands in a 3D printed part, the structure can be optimized in a specific orientation for specific loading conditions, and LCT can be applied for simulating mechanical responses. Three point bending tests were performed on rectangular 3D printed samples and compared to a 3D simulation using LCT for a similar bending load. This allows for the use of LCT in combination with a finite element software such as
Bradley, Coilin, Garcia, Jordan, Sibley, Brian
Development of an Advanced Tensile Testing Method for HDPE Composites in High Draw Molded Hollow Circular Regions: Effects of Sample Preparation, Asymmetry, Thermal Conditions, Pull Speed, and Fixture Parameters.2026-01-0204To be published on 04/07/2026
High-density polyethylene (HDPE) composites, particularly in high draw molded hollow circular configurations, present unique challenges in evaluating mechanical performance under tensile stress due to anisotropic deformation, geometric asymmetry, and localized thermal gradients. This study introduces an advanced tensile testing methodology designed specifically to assess such regions with greater precision and reproducibility. The method incorporates refined sample preparation protocols, tailored fixture geometry, and adjustable pull speeds to accommodate varying thermal histories and draw ratios inherent to molded sections. Systematic variation of asymmetrical, temperature conditions, and clamping techniques revealed significant impacts on tensile strength, elongation at break, and strain distribution. Findings emphasize the necessity of customized testing frameworks for molded composite geometries and demonstrate that fixture alignment and thermal conditioning are critical to
BHALERAO, SAURABH SHANKAR
Thermal Performance of Natural Fiber Hybrid Composites for Automotive Insulation Applications2026-01-0244To be published on 04/07/2026
This study investigates the thermal conductivity of natural-fiber-based hybrid polymer composites with potential automotive insulation applications. With the increasing demand for lightweight, sustainable, and thermally efficient materials in vehicle cabins, under-hood systems, and electric vehicle battery enclosures, natural fiber composites present a promising alternative to conventional glass-fiber composites. Three distinct composite configurations were fabricated: pure glass, glass-jute hybrid, and glass-jute-coir hybrid, using general-purpose polyester resin as the matrix. The composites were manufactured using the hand lay-up method. Thermal conductivity measurements were conducted using the ASTM C177 guarded hotplate method on composite plates. Results indicate that the hybrid composite with glass, jute, and coir fibres has the lowest thermal conductivity, making it the most effective for insulation applications. This study demonstrates that natural fibre-reinforced composites
Mache, Ashok, Salve, Aniket, Chinchanikar, Satish, Borse, Hardik, Deshmukh, Omkar, Mahadikpatil, Siddhi, Kulkarni, Aparna
Wear and Friction of PTFE and PEEK Coated Cast Iron for Piston Ring Application2026-01-0240To be published on 04/07/2026
In engine 30% of the total energy is lost due to the friction between piston ring and cylinder liner due to their constant rubbing motion. A piston that reciprocates at high speeds has piston rings that constantly scrape against the wall leading to high frictional losses within the engine. The engine has to work against this resistance to provide the required power, and hence it will consume more fuel. For this reason, material used for these components is more crucial. Reduction of surface friction between moving parts in order to increase overall efficiency can be achieved by suitable coating. The most commonly used piston rings are coated with chromium layers that are electroplated which is being replaced by chrome plating. Low coefficient of friction (COF) and high wear resistance can be achieved by self-lubricating coating of PTFE and PEEK polymer-based composite coatings. Experimental results showed that the PEEK and PTFE coating performed better in terms of friction and wear
Rajendran, R., Tamilarasan, T R, J, Chandradass
Vibrational Analysis of Hybrid Composite Laminated Plates of E – Glass and Areca Fibers with Brake Pad Waste Powder2026-28-00732/12/2026
This study focuses on the vibration analysis of hybrid composite laminated plates fabricated from E-glass Fiber and areca Fiber reinforced with epoxy resin. The hybrid laminates were prepared using the Vacuum Assisted Resin Transfer Moulding (VARTM) process with different stacking sequences and Fiber ratios, where brake lining powder was also incorporated as a filler in selected configurations to enhance mechanical and damping properties. The fabricated plates (280 × 280 mm) were subjected to experimental modal analysis using an impact hammer and accelerometer setup, with data acquisition carried out through DEWESoft software. Natural frequencies and damping ratios were determined under three boundary conditions (C- C-C-C, C-F-C-F, and C-F-F-F). The results revealed that Plate 1, with E-glass outer layers, areca reinforcement, and filler addition, exhibited the best vibration performance, achieving a maximum natural frequency of 332.8 Hz under C-C-C-C condition, while Plate 2 showed a
D R, Rajkumar, O, Vivin Lenin, R, Saktheevel, R G, Ajay Krishna, Ng, Bhavan
Modelling and Analysis of Complex Shaped Cracks2026-28-00482/12/2026
This study provides an extensive analysis through finite element analysis (FEA) on the effects of fatigue crack growth in three different materials: Structural steel, Titanium alloy (Ti Grade 2), and printed circuit board (PCB) laminates based on epoxy/aramid. A simulation of the materials was created using ANSYS Workbench with static and cyclic loading to examine how the materials were expected to fail. The method was based on LEFM and made use of the Maximum Circumferential Stress Criterion to predict where cracks would happen and how they would progress. Normalizing SIFs while a crack was under mixed loading conditions was achieved using the EDI method [84]. We used Paris Law to model fatigue crack growth using constants (C and m) for the materials from previous studies and/or tests. For example, in the case of titanium Grade 2, we found Paris Law constants with C values from 1.8 × 10-10 to 7.9 × 10-12 m/cycle and m values from 2.4 to 4.3, which illustrate differing effects of their
T, Lokesh, Bhaskara Rao, Lokavarapu
Genetic Algorithm Based Optimization of Chaboche Kinematic Hardening Parameters along with the Validation of FE Model through Characterized Crack Initiation2026-28-00862/12/2026
In the context of electro-mobility for commercial vehicles, the failure analysis of a connector panel in a DCDC converter is crucial, particularly regarding crack initiation at the interface of busbar and plastic component. This analysis requires a thorough understanding of thermo-mechanical behavior under thermal cyclic loads, necessitating kinematic hardening material modeling to account for the Bauschinger effect. As low cycle fatigue (LCF) test data is not available for glass fiber reinforced polyamide based thermoplastic composite (PA66GF), we have adopted a novel approach of determining non-linear Chaboche Non-Linear Kinematic Hardening (NLK) model parameters from monotonic uniaxial temperature dependent tensile test data of PA66GF. In this proposed work a detailed discussion has been presented on manual calibration and Genetic Algorithm (GA) based optimization of Chaboche parameters. Due to lack of fiber orientation dependent test data for PA66GF, here von Mises yield criteria
Basu, Parichay, Srinivasappa, Naveen
Effect of Sebastiana Rostrata Fiber Loading on the Tribological Behaviour of Polycaprolactone Biocomposite2026-28-00212/12/2026
This study investigates the tribological behaviour of Sesbania rostrata fiber (SRF) reinforced polycaprolactone (PCL) biocomposites using a pin-on-disc wear couple. The stationary SRF/PCL composite specimen interacted with a rotating EN31 steel disc (64 HRC), establishing the sliding wear interface in accordance with ASTM G99 standards. Composite laminates containing 10, 20, and 30 wt% SRF were evaluated at a sliding velocity of 1 m/s over a fixed distance of 1000 m under varying normal loads. The incorporation of SRF significantly enhanced the wear performance relative to neat PCL, with 20 wt% fiber loading achieving the lowest coefficient of friction and specific wear rate due to improved load transfer, stronger interfacial adhesion, and a more uniform laminate structure. In contrast, the 30 wt% composite exhibited fiber agglomeration, reduced homogeneity, and weakened fiber–matrix interactions, resulting in increased wear. SEM microstructural analysis confirmed the formation of a
Raja, K., Senthil Kumar, M.S.
Aerospace & Defense Technology: February 202626AERP022/5/2026
Plasma Surface Activation for Stronger, More Durable CFRP Bonds in Aerospace Smarter Pyrovalve Alternatives for Modern Missile and Munition Launcher Applications Aerospace Aluminum Laser Welding: Advancing Material Performance for the Future of Flight Model-Based Design Is Shaping the Next Phase of eVTOL Systems Development How RF-over-Fiber is Providing the Backbone of Next Generation Mil/Aero Networks NASA Demonstrates a First-of-Its-Kind Space Communications A Rainfield Simulator for Hypersonic Testing The U.S. Army Space and Missile Defense Command Technical Center's Aerophysics Research Facility, (ARF), fired a successful hypersonic shot to test its new rainfield simulator. Next Generation Carbon Fiber Composites 3D Printer for Hypersonic Research Auburn University's Applied Research Institute in Huntsville is adding some serious fiber to its diet. The Critical Impact Of SAE Aerospace Standards: Certified AS1895/7 and /23 Metal Seals How engineers can ensure safety, reliability
Aerospace Aluminum Laser Welding: Advancing Material Performance for the Future of Flight26AERP02_032/1/2026
Between the 1920s and 1930s, aluminum started replacing wood as the primary material in aircraft construction and soon became the backbone of modern aviation. Its popularity stemmed from a combination of properties, high strength-to-weight ratio, corrosion resistance, and ease of forming that made it ideal for demanding aerospace applications. Throughout much of the 20th century, high-strength aluminum alloys dominated aircraft design, accounting for 70-80 percent of commercial airframes and more than half of many military aircraft. Even after the introduction of fiber-polymer composites in the early 2000s, aluminum has remained a critical material because it continues to offer the strength, lightness, and versatility needed for modern aviation. Industry forecasts predict that commercial air travel will double in the next 25 years, which means more pollution will be released into the atmosphere. One way to help reduce these emissions is by building airplane fuselages and wings with
Plasma Surface Activation for Stronger, More Durable CFRP Bonds in Aerospace26AERP02_012/1/2026
Carbon fiber-reinforced polymers (CFRPs) have become essential in modern aerospace structures, from fuselage skins and wing components to nacelles, interior structures, and a growing range of primary load-bearing parts. Their high strength-to-weight ratio delivers major benefits in fuel efficiency, payload capacity, and fatigue performance. Yet achieving reliable adhesive bonds on CFRP surfaces remains a persistent engineering challenge. The low intrinsic surface energy of composites - particularly under thermal cycling, vibration, and moisture exposure - limits bond durability unless surfaces are properly prepared. Plasma surface treatment has emerged as a pivotal solution, offering a fast, controllable, and non-destructive way to increase surface energy, improve wettability, and enhance adhesion across complex geometries. This is especially important as the aerospace industry transitions from thermoset to thermoplastic composites (TPCs), which enable faster processing, lower
Design and Development of a Lightweight Aluminium Cascade System for Type IV COPVs for Stationary and Mobile Applications2026-26-04851/16/2026
The global push for clean energy has made hydrogen a central element in decarbonizing transport, industrial processes, and energy systems. Effective hydrogen storage and distribution are critical to supporting this transition, and type IV Composite Overwrapped Pressure Vessels (COPVs) have emerged as the preferred solution due to their lightweight, high pressure capacity, hydrogen embrittlement and corrosion resistance. However, the cascade infrastructure used to house and transport these vessels has lagged behind in innovation. Steel-based cascades, while strong, are heavy prone to corrosion, and unsuitable for mobile deployment. This paper introduces a custom designed aluminium cascade system offering a 65% weight reduction while maintaining structural integrity and safety. Designed for mobile use, the system features modularity, better damping, and enhanced corrosion protection. The paper outlines design methodology, material selection, fabrication process, and comparative
Parasumanna, Ajeet Babu, Muthusamy, Hariprasad, Ammu, Vnsu Viswanath, Kola, Immanuel Raju
Bioadhesive Sponge Stops Internal BleedingTBMG-544071/1/2026
Researchers combined mussel adhesive protein with decellularized extracellular matrix (dECM) to develop a composite hemostatic sponge that offers both strong tissue adhesion and biocompatible biodegradability.
Study on the Influence of Liquid Composite Swivel Arm Positioning Nodes on the Dynamic Performance of High-Speed Trains2025-99-025512/23/2025
Rubber components are an important part of the suspension system of high-speed trains, and the complex nonlinear characteristics of rubber parts have a significant impact on the vehicle dynamic performance. This paper establishes a nonlinear dynamics model of the liquid composite swivel arm positioning node, which can reflect the dynamic stiffness and dynamic damping characteristics of the rubber components that change nonlinearly with the frequency and amplitude, and also has a fast calculation speed. The vehicle dynamics simulation model considering the longitudinal stiffness nonlinear characteristics of the arm node is established, and the influence of the stiffness nonlinearity of the liquid composite arm positioning node on the dynamic performance of the vehicle, such as straight-line stability and curve passing ability, is studied in depth through numerical simulation.
Cheng, Junqiang, Yang, Chen, Li, Longtao, Cong, Rilong, Hu, Tingzhou
Injection Molding Parameters Optimization to Enhance Mechanical Properties of Glass-Fiber Reinforced PA9T Polymer2025-36-012412/18/2025
The use of polymeric materials and polymer -based composites as alternatives to metals in conventional applications is a widely adopted strategy. These materials provide advantages in terms of processability, cost-effectiveness, and, most notably, weight reduction. This study aimed to develop and optimize the injection molding process for producing PA9T (Polyphthalamide 9T) components reinforced with varying amounts of glass fiber to achieve optimal mechanical and physical properties. To enhance mechanical performance, different glass fiber loadings were investigated. The study employed the Taguchi method with an L9 orthogonal array design. The selected variable parameters were material composition (PA9T reinforced with 30, 35, and 50 wt% glass fiber), injection pressure (1000, 1500, and 2000 bar), injection temperature (320, 330, and 340 °C), and injection speed (100, 125, and 150 mm/s). The Taguchi method was chosen because it allows for the identification of optimal process
Mendonça, Arthur S., Michelotti, Alvaro Canto, Berto, Lucas F., Salvaro, Diego B., Binder, Cristiano
Influence of the PTFE on the Tribological and Mechanical Properties of a Fiber-Reinforced Polyphthalamide2025-36-022112/18/2025
Materials science and engineering are essential for advancing energy-efficient mechanical systems through lightweight structures and friction reduction. Among engineering polymers, polyphthalamides (PPA) are widely used for their superior thermochemical and mechanical properties. This study investigates the influence of polytetrafluoroethylene (PTFE) on the mechanical and tribological performance of a commercial polymer matrix composite (PMC) reinforced with 30wt% glass fiber. Self-lubricating composites were manufactured by injection molding with PTFE contents ranging from 0-15 wt%. Density was measured using Archimedes’ method. Mechanical properties were measured through ISO 527 tensile testing, while tribological behavior was evaluated using ball-on-flat reciprocating tests under 189N (630 MPa), 2 H frequency, and 10 mm strokes for 60 minutes, employing a 10 mm diameter AISI 52100 steel sphere as counter-body. Friction coefficient (COF) was monitored throughout testing, and wear
Hromatka, Matheus, Salvaro, Diego B., Binder, Cristiano, Michelotti, Alvaro C., Berto, Lucas F.
Biocomposite of Euterpe oleracea Mart and Cocos nucifera l. : Sustainable Materials2025-36-016312/18/2025
Brazil is recognized for its vast biodiversity and abundance of natural resources, many of which are still underutilized. In an effort to promote sustainability and innovation, there is a growing movement to replace non-recyclable materials with ecological alternatives. Within this context, acai leaves (Euterpe oleracea Mart.) and coconut leaves (Cocos nucifera L.) appear as potential natural reinforcements in polymer composites. This study aims to evaluate the mechanical properties of composites formed by these sheets, using polyester resin as the matrix phase. Tensile strength tests were conducted on specimens, following the ASTM D 638M standard, to determine the mechanical properties of the composites. The results obtained were compared with data from the existing literature in order to validate the effectiveness of the composites produced. Additionally, fractures in the specimens were visually analyzed for a better understanding of the failure mechanisms.
Dias, Roberto Yuri Costa, Santos Borges, Larissa, Brandao, Leonardo William Macedo, Mendonca Maia, Pedro Victor, Silva de Mendonça, Alian Gomes, Fujiyama, Roberto Tetsuo
Mechanical Tensile Behavior of Polyester Composites with Addition of Banana and Sugarcane Fibers2025-36-015412/18/2025
Polymer composites with the addition of natural fibers have gained prominence as a sustainable and technically viable alternative to conventional synthetic materials, especially in applications that require a balance between mechanical performance and environmental responsibility. This study evaluated the mechanical behavior of composites produced with plant fibers from banana (Musa sapientum) and sugarcane (Saccharum officinarum L.), both sourced from the northern region of Brazil. The fibers, used in their natural state without chemical treatment, were cut to a uniform length of 5 mm for standardization. The polymer matrix used was unsaturated terephthalic polyester resin, pre-accelerated and catalyzed with methyl ethyl ketone peroxide (MEKP). The molding of test samples was performed manually in silicone molds, according to ASTM D638 specifications, to ensure repeatability and comparability of results. The mechanical tests revealed that the composites made with sugarcane fibers had
Santos Borges, Larissa, Dias, Roberto Yuri Costa, Brandao, Leonardo William Macedo, Mendonca Maia, Pedro Victor, Silva de Mendonça, Alian Gomes, Fujiyama, Roberto Tetsuo
Synergistic Effects of Graphene Oxide and Nanoclay on the Structural and Electrical Properties of Automotive Nanocomposite Insulation2025-36-016112/18/2025
As vehicles become increasingly connected and electrified, the demand for high-performance cables and electrical connectors is growing quickly. Electrical insulation materials play an essential role in protecting and insulating those critical components, ensuring reliability, safety and durability. The development of a more robust composite material is essential to promote sustainability and energy efficiency, in both component application and its manufacturing processes. This research explores the development of advanced nanocomposite material for automotive electrical applications. The nanocomposite material comprises low-density polyethylene (LDPE), ethylene-vinyl acetate (EVA), nanoclay (NC) and graphene oxide (GO), processed via melt mixing in a twin-screw extruder. A design of experiments (DOE) was performed using 23, factorial design two levels and three variables (wt.% of EVA, NC and GO), to evaluate the effect of each variable on the material performance. Mechanical tests
Horiuchi, Lucas Nao, Kerche, Eduardo Fischer, Gonçalves, Everaldo Carlos, Polkowski, Rodrigo
Natural Fibers Applied in the Automotive Industry in Brazil: A Review2025-36-017012/18/2025
There is a growing demand for new materials that meet mechanical and structural performance requirements, with specific properties, especially in the automotive industry. From a context of innovation and global needs to be met, there is the appreciation of composite materials, specifically applied in the automotive sector, since these can be obtained from the combination of two or more different materials, obtaining certain properties from the individual characteristics of its phases, expanding the availability of materials to be used in this sector. In recent years the use of natural fibers in composite materials for automotive applications has gained relevance due to factors such as sustainability, low weight and good mechanical properties. The attempt to combine innovation and environmental preservation make such applications promising, aiming to obtain ecological solutions, considering that natural fibers of vegetable origin such as sisal, jute and flax are biodegradable and
Dias, Roberto Yuri Costa, Santos Borges, Larissa dos, Brandao, Leonardo William Macedo, Mendonca Maia, Pedro Victor de, Silva de Mendonça, Alian Gomes da, Fujiyama, Roberto Tetsuo
Natural Fiber Composites with Nanomaterials: A Sustainable Alternative to Metals in the Automotive Industry2025-36-004012/18/2025
This paper analyzes the potential of combining natural fibers with nanomaterials to develop advanced composites for automotive sector applications, providing a sustainable alternative to parts traditionally produced with metallic materials. The metallic alloy in the automotive industry is widely used in vehicle manufacturing, but faces significant challenges, such as high production costs, high weight, susceptibility to corrosion, and rigorous recycling processes. Natural fibers stand out for favorable mechanical properties, low cost, low weight, and eco-friendly material, making promising alternatives to metals and synthetic fibers. The combination of natural fibers and nanomaterials creates composites with improved mechanical and thermal, reducing any limitations inherent to natural fibers. Therefore, composites combined, called hybrid, have a high potential for use in various automotive components, such as in structural and non-structural applications. This study also analyzes the
Corrêa, Karytha, Cabral, Gabriel, Santiago, Marcelo, Veloso, Verônica, Chaves, Matheus
Review of Through-the-Thickness Reinforcement Technologies Applied to Aircraft CFRP Composites2025-99-035512/17/2025
Carbon fiber-reinforced polymer (CFRP) composites are widely used in aircraft structures for weight reduction due to their high specific strength and modulus. However, their weak interlaminar properties lead to high sensitivity to out-of-plane loads such as impact, making them prone to delamination damage, which threatens flight safety. To enhance interlaminar performance, through-thickness reinforcement technologies, particularly Z-pinning and stitching, have become key research focuses. This paper systematically reviews the manufacturing processes, structural mechanical characteristics, and application progress in aerospace structures of these two mainstream through-thickness reinforcement technologies. Research shows that Z-pintechnology, by implanting metal or CFRP pins, and stitching technology, by sewing multiple fabric layers with fiber threads, both effectively bridge interlaminar cracks, significantly improving the impact resistance of composites. However, the implantation
Cui, Bo, Zhang, Yongjie, Zhang, Chuzhe, Jin, Tao
Mechanical System Innovation for Next-Generation Electric Vehicles: Lightweight and Energy Recovery Co-Design2025-99-033412/17/2025
Aiming at the technical bottlenecks of electric vehicles (EVs) in terms of range, energy efficiency and thermal management, this paper proposes an innovative mechanical system design scheme that integrates lightweight materials, topology-optimised structure and mechatronic energy recovery. Through multi-physics simulation and experimental verification, the coupling mechanism between mechanical design and electrochemical performance is revealed, providing theoretical support for the development of energy-efficient electric vehicles. The research adopts a hybrid structure of carbon fiber reinforced polymer (CFRP) and aluminum alloy, and combines it with topology optimization technology to achieve lightweight (18% weight reduction) and improved impact resistance (40% improvement in energy absorption) of the battery box; the design of a bimodal energy recovery system integrating flywheel energy storage and magnetorheological damper, which can achieve an energy recovery efficiency of 82.7
Xu, Nanxin, Song, Ziyang, Han, Qiyu, Chen, Xiaoxian, Miao, Zhengchen, Song, Jinlong
Carbon Fiber and Fiberglass Epoxy Prepreg Products with 350 °F (177 °C) Cure for Aerospace ApplicationsAMS6891A (Current)12/16/2025
The intent of this specification is for the procurement of carbon fiber and fiberglass epoxy prepreg products with 350 °F (177 °C) cure for aerospace applications; therefore, no qualification or equivalency threshold values are provided. Users that intend to conduct a new material qualification or equivalency program must refer to the production quality assurance section (4.3) of this base specification, AMS6891.
AMS P17 Polymer Matrix Composites Committee
Micromachining through Ultrasonic-Assisted Electrochemical Discharge Process: A Review05-19-03-002112/3/2025
As demand for microcomponents has escalated in diverse areas of automotive, medicine, communications, electronics, optics, biotechnology, and avionics industries, there is a need for hybrid manufacturing techniques that can effectively micromachine hard and brittle materials. Electrochemical discharge machining (ECDM) is an advanced manufacturing process for machining difficult-to-cut materials. With a need for precision and accuracy, tool kinematics is a potential research area in ECDM for achieving geometrical dimensioning and tolerances (GD&T). Therefore, the present study reviews the ultrasonic vibration–assisted ECDM (UA-ECDM) hybrid process and the performance of its process parameters (voltage, electrolyte type and its concentration, electrode material, pulse duration, and amplitude) on the material removal rate (MRR), tool electrode wear (TEW), surface integrity, and difficult-to-cut materials. Also, the present work mentions current problems (debris and bubbles trapped
Prajapati, Mehul S., Lalwani, Devdas I.
Carbon Fiber and Fiberglass Epoxy Prepreg Products with 350 °F (177 °C) Cure for Aerospace Applications: Type 35, Class 1, Grade 191AMS6891/1A (Current)12/1/2025
The intent of this specification is for the procurement of the material listed on the QPL; therefore, no qualification or equivalency threshold values are provided. Users that intend to conduct a new material qualification or equivalency program must refer to the Quality Assurance section of the base specification, AMS6891.
AMS P17 Polymer Matrix Composites Committee
Automated fiber placement with Ramy Harik25AUTP12_0912/1/2025
AFP can build complex, lightweight structures, but cost concerns keep its use in the automotive industry to a minimum. For now, anyway. Ramy Harik, a Fulbright alumnus and director of the Clemson Composites Center, is pushing the boundaries of manufacturing with his latest book, Automated Fiber Placement: Status, Challenges, and Evolution coauthored with Alex Brasington. The book, published by SAE in June of 2025, serves as a comprehensive guide to automated fiber placement (AFP), a cutting-edge technology crucial for building complex, lightweight structures in the aerospace and automotive industries. The book aims to offer a thorough understanding of AFP's transformative potential for students, engineers, and industry professionals. The book synthesizes a decade of research, explaining how AFP supports the rise of advanced air mobility and sustainable structures for commercial and defense aircraft, space habitats, and beyond.
Blanco, Sebastian
3D Construction of Biologically Derived MaterialsTBMG-5430212/1/2025
NASA has developed a novel approach for macroscale biomaterial production by combining synthetic biology with 3D printing. Cells are biologically engineered to deposit desired materials, such as proteins or metals, derived from locally available resources. The bioengineered cells build different materials in a specified 3D pattern to produce novel microstructures with precise molecular composition, thickness, print pattern, and shape. Scaffolds and reagents can be used for further control over material product. This innovation provides modern design and fabrication techniques for custom-designed organic or organic-inorganic composite biomaterials produced from limited resources.
Self-Healing Biodegradable Composites for Off-Highway Vehicles in Extreme Environments2025-28-021111/6/2025
Off-highway vehicles (OHVs) frequently operate in extreme environments—ranging from arid deserts and frozen tundras to dense forests and abrasive mining zones—where structural wear, impact damage, and environmental stress compromise their material integrity. Frequent repairs and component replacements increase operational costs, downtime, and environmental waste, making durability and sustainability key concerns for next-generation vehicle systems. This paper explores a novel class of self-healing biodegradable composites, inspired by biological systems, to address these challenges. The proposed materials combine bio-based resins, microencapsulated healing agents, and shape-memory polymers (SMPs) to autonomously repair microcracks and surface-level damage when triggered by thermal, UV, or mechanical stimuli. The design draws inspiration from natural self-healing systems such as tree bark and reptile skin, replicating their regenerative behavior to enhance structural resilience in OHVs
Vashisht, Shruti
Development of Integral Forming for New “NMAX” YECVT Parts Using the Plate Forging Method2025-32-000511/3/2025
Yamaha Motor Engineering Co., Ltd. provides plastic processing technology based on fuel tank press forming technology, and is developing various plastic processing methods, including forging, and developing mold equipment to realize them. This time, the core parts of the YECVT unit mounted on Yamaha Motor Co., Ltd.'s small premium scooter "NMAX" were not made by welding individual parts to each other, but by integrally forming them from a single thick plate using the cold forming method, resulting in lightweight, compact, high-strength, high-precision parts. By incorporating a composite plastic processing method that takes advantage of the characteristics of the material while making full use of analysis technology and mold technology, we were able to develop a composite plastic processing method (plate forging method) that creates new added value and mass produce it. In addition,this development has made it possible to achieve a thickness increase of 1.7 times the standard material
Hongo, Hironari, Tamaru, Shogo, Uda, Shinnosuke
Temperature Effect on Fatigue Performance of Thermoset and Thermoplastic Composites2025-32-000611/3/2025
The growing demand for lightweight, durable, and high-performance materials in industries such as aerospace, automotive, and energy has driven the development and evaluation of thermoset and thermoplastic composites. Within this framework the static and fatigue mechanical behavior of one thermoset material and two thermoplastic composites are investigated in the (-30° +120°C) temperature range, to simulate extreme environmental conditions. The results from the tensile tests show the different mechanical behavior of the investigated materials, while the cyclic test results highlight the significant impact of temperature on structural properties, offering useful insights for their application in temperature-sensitive environments. This research is partially funded by the Italian Ministry of Enterprises and Made in Italy (MIMIT) within the project ”New Generation of Modular Intelligent Oleo-dynamic Pumps with Axial Flux Electric Motors,” submitted under the ”Accordi per l’Innovazione
Chiocca, Andrea, Sgamma, Michele, Franceschini, Alessandro, Vestri, Alessio, mancini, Simone, Bucchi, Francesco, Frendo, Francesco, Squarcini, Raffaele
Nanofibers Yield Stronger, Tougher Carbon Fiber CompositesTBMG-5412111/1/2025
Researchers at the U.S. Department of Energy (DOE)’s Oak Ridge National Laboratory (ORNL) have developed an innovative new technique using carbon nanofibers to enhance binding in carbon fiber and other fiber-reinforced polymer composites — an advance likely to improve structural materials for automobiles, airplanes and other applications that require lightweight and strong materials.
Dome Profile Optimization and Stress Analysis of Type IV Composite Cylinders Using a CLT-Based MATLAB Program and FEA Validation2025-28-037410/30/2025
Type IV composite pressure (CP) vessels composed of a plastic liner and composite layers require special design attention to the dome region. The cylindrical portion of the composite cylinder is wrapped with composite layers consisting of the 900 hoop layers and low-angle helical layers, whereas the dome surface carries helical layers only. The winding angle of the helical layers being a constant over the cylindrical portion starts to vary from the cylinder-dome junction toward the boss at the top continuously. Along with the winding angle, the composite thickness also varies continuously resulting in a maximum thickness at the top crown region. The complete analysis and layer-wise stress prediction of Type IV composite cylinders for service pressures up to 70 MPa was analyzed by the Classical Lamination theory (CLT)-based MATLAB program. The MATLAB program developed in this work for the dome initially performs the dome profile generation through the numerical integration of the dome
R. S., Nakandhrakumar, Tandi, Ronak, M, Ramakrishnan, Raja, Selvakumar, Elumalai, Sangeethkumar, Velmurugan, Ramanathan
Composite Materials Handbook Volume 3 - Revision HR-64010/16/2025
The third volume of this six-volume compendium provides methodologies and lessons learned for the design, analysis, manufacture, and field support of fiber-reinforced, polymeric-matrix composite structures. It also provides guidance on material and process specifications and procedures for using the data that is presented in Volume 2. The information provided is consistent with the guidance provided in Volume 1, and is an extensive compilation of the current knowledge and experiences of engineers and scientists from industry, government, and academia who are active in composites. The Composite Materials Handbook, referred to by industry groups as CMH-17, is a six-volume engineering reference tool that contains over 1,000 records of the latest test data for polymer matrix, metal matrix, ceramic matrix, and structural sandwich composites. CMH-17 provides information and guidance necessary to design and fabricate end items from composite materials. It includes properties of composite
CMH-17
FibreCoat’s New Radar-Absorbing ‘Stealth’ Fiber Reinforced Composites for Spacecraft, Aircraft and TanksTBMG-537539/1/2025
FibreCoat, the German materials startup, has developed a groundbreaking fiber reinforced composite that is capable of making aircraft, tanks and spacecraft invisible to radar surveillance.
FibreCoat's New Radar-Absorbing ‘Stealth’ Fiber Reinforced Composites for Spacecraft, Aircraft and Tanks25AERP09_069/1/2025
FibreCoat, the German materials startup, has developed a groundbreaking fiber reinforced composite that is capable of making aircraft, tanks and spacecraft invisible to radar surveillance. The company was officially founded in Aachen, Germany, in 2020, however its core founding team first began developing new approaches to the use of materials that make commercial and military vehicles invisible to radar as back as 2014. FibreCoat is known for inventing a novel technology to coat metals and plastics onto fibers, thus combining the properties of the fibers and the coating material, during the fiber-spinning process.
Nanofibers Yield Stronger, Tougher Carbon Fiber CompositesTBMG-535478/1/2025
Researchers at the U.S. Department of Energy (DOE)’s Oak Ridge National Laboratory (ORNL) have developed an innovative new technique using carbon nanofibers to enhance binding in carbon fiber and other fiber-reinforced polymer composites — an advance likely to improve structural materials for automobiles, airplanes and other applications that require lightweight and strong materials.
Effect of Zirconia and Quarry Dust Reinforcements on Mechanical Properties of Al7079 Composite05-19-01-00086/29/2025
In this work, the microstructure and mechanical behavior of AL7079 metal matrix composites (MMCs) mixed with zirconia and quarry dusts are analyzed. The high-strength Al7079 can be further improved by the addition of zirconia particulates and quarry dust particles, a cost-effective reinforcement. Composite samples with different weight fractions of zirconia (2%, 4%, and 6%) and quarry dust (2%) were produced via a stir-casting technique. Scanning electron microscope (SEM) was engaged to examine the microstructure of the composites, which showed that the reinforcements were well integrated and bonded perfectly to the matrix material. A simple mechanical test of hardness, tensile, and impact strength revealed enrichment in hardness and tensile strength in comparison to the Al7079 alone, whereas the impact strength decreased. Composite containing 6% zirconia and 2% quarry dust improved both the hardness (95 BHN) and tensile strength (186 MPa) by 7%, outperforming the remaining composition
Madan Kumar, K.N., Sathyanarayana, G.M., Kuldeep, B., Manu, S.S., Manjunath Yadav, S., Anand, H.R.
Modern Low Friction Coating Technology for Automotive Tribology2025-01-02476/16/2025
The aim of this work is to present the overviewing results of the low friction coating technology for modern automotive application with the themes, e.g. electric vehicle (EV), R&D trends and bioethanol fuel application. According to Forbes, China, armed with EV, could have several companies among the top 10 global brands by sales in 2030. EV’s friction is more severe than traditional powertrain friction. For the protection of EV’s wear and friction, the coatings, diamond like carbon (DLC) and CrCuN, are compared in the literature. Global coating companies developed with the keywords: hybrid process, low-temperature coating process for polymer material. Last coating conferences showed R&D trends: coating for polymer materials, tetrahedral amorphous carbon (taC) coating, low-temperature coating process and multi-elements containing coatings. In Korea, research institutions, universities and Hyundai Motor Group have a long-term project for the development of ultralow friction coatings of
Cha, Sung Chul, Moon, Kyoung Il, Kim, Jongkuk, Park, Chang Ho, Kim, Dong Sik
Automated Fiber Placement: Status, Challenges, and EvolutionR-5116/11/2025
Discover the cutting-edge technology driving the next generation of aerospace, automotive, and space exploration. Automated Fiber Placement: Status, Challenges, and Evolution offers a comprehensive dive into AFP—an innovative method that’s transforming how complex, lightweight structures are built. Over the last 50 years, fiber-reinforced composites have revolutionized industries, particularly aerospace, with carbon fiber reinforced polymers at the forefront. AFP has enabled lighter, more durable aircraft with reduced fuel consumption and improved longevity. As the aerospace industry advances with new platforms like the Boeing 787 and Airbus A350, AFP continues to evolve, integrating machine learning and automation to deliver higher efficiency and lower costs. This book serves as an essential guide, presenting a decade of research in clear, accessible language. Whether you're a student, engineer, or industry professional, you'll gain a thorough understanding of AFP and its
Harik, Ramy, Brasington, Alex
Carbon Fiber-Carbon Nanotube Yarn Hybrid ReinforcementTBMG-532336/1/2025
Innovators at the NASA Glenn Research Center have developed a toughened hybrid reinforcement material made from carbon fiber and carbon nanotube (CNT) yarn for use in polymer matrix composites (PMCs). The new material improves toughness and damping properties of PMCs, enhancing impact resistance, fatigue life, as well as structural longevity.
Influence of Strain Rate Effect on Mechanical and Crashworthiness Properties of CFRP Composite Structures05-19-01-00025/6/2025
Composite materials are increasingly utilized in industries such as automotive and aerospace due to their lightweight nature and high strength-to-weight ratio. Understanding how strain rate affects the mechanical and crashworthiness properties of CFRP composites is essential for accurate impact simulations and improved safety performance. This study examines the strain rate sensitivity of CFRP composites through mechanical testing and finite element analysis (FEA). Experimental results confirm that compressive strength increases by 100%–200% under dynamic loading, while stiffness decreases by up to 22% at a strain rate of 50 s−1, consistent with trends observed in previous studies. A sled test simulation using LS-Dyna demonstrated that the CFRP crash box sustained an average strain rate of 46.5 s−1, aligning with realistic impact conditions. Incorporating strain rate–dependent material properties into the FEA model significantly improved correlation with experimental crashworthiness
Badri, Hesam, Jayasree, Nithin Amirth, Loukodimou, Vasiliki, Omairey, Sadik, Bradbury, Aidan, Lidgett, Mark, Page, Chris, Kazilas, Mihalis
Acoustic Evaluation of Fiber-Based Materials for Engine Bay Applications2025-01-01155/5/2025
A newly formulated fiber-based material was developed to offer a sustainable alternative to foam-based vehicle acoustic products. The fiber-based material was designed to be used in multiple vehicle acoustic applications, with different blends of the material available depending on the application. It performs well as an engine bay sound absorber due to its high heat tolerance and good absorption performance. A study was conducted to evaluate the sound absorption performance of this fiber-based material, specifically the engine bay blends, in comparison to that of current foam-based products. The results from this study show that the sound absorption performance of this new fiber-based material can match that of current foam-based materials while providing a sustainable and fully recyclable product, unlike the foam.
Krugh, Jack
Material Adapted Method for the Repair of Curved Thermoplastic Composite Structures by Induction Welding of Patches2025-01-01655/2/2025
Thermoplastic fiber-reinforced polymer composites (TPC) are gaining relevance in aviation due to their high specific strength, stiffness, potential recyclability and the ability to be repaired thanks to their meltability. To maximize their potential, efficient repair methods are needed to maintain aircraft safety and structural integrity. This article introduces a novel repair technique for damaged TPC structures, involving the joining of a repair patch with induction welding using a susceptor material. The susceptor consists of a material with high electrical conductivity and magnetic permeability and therefore reacts stronger to the electromagnetic field than the composite, even if the composite is carbon fiber based. I. e. the thermal energy is specifically concentrated in the repair area. In this study, the susceptor was placed on the patch and also in the welding zone. The repair process begins by identifying and preparing the damaged area, followed by precise scarfing. Care is
Geiger, Markus, Glaap, Anton, Schiebel, Patrick, May, David
Comparison of Different Joining Techniques as a Benchmark for Integrally Joined Thermoformed Components Based on Tailored rCF Organosheets2025-01-01705/2/2025
Climate-neutral aviation requires resource-efficient composite manufacturing technologies and solutions for the reuse of carbon fibers (CF). In this context, thermoplastic composites (TPC) can make a strong contribution. Thermoforming of TPC is an efficient and established process for aerospace components. Its efficiency could be further increased by integration of joining processes, which would otherwise be separate processes requiring additional time and equipment. In this work, an integrative two-step thermoforming process for hollow box structures is presented. The starting point are two organosheets, i.e. fiber-reinforced thermoplastic sheets. First, one of the organosheets, intended for the bottom skin of the uplift structure, is thermoformed. After cooling, the press opens, the organosheet remains in the press and an infrared heater is pivoted in, to locally heat up just the joining area. Meanwhile, a second organosheet, intended for the top skin, is heated and thermoformed and
Vocke, Richard, Seeßelberg, Lorenz, Focke, Oliver, Dietrich, Jan Yorrick, Jobke, Katrin, Albe, Christopher, May, David
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